Orbital Focus - International Spaceflight Facts and Figures
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Launches and Orbital Operations


Tyneside, UK
2026 May 16
Saturday, Day 136

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Orbital elements based on amateur observations

Satellite observers' discussion group

Database of amateur observations using radio

Primary source of unclassified orbital elements
2025 - Launches to Orbit and Beyond

Listed are launches, irrespective of outcome, that were irretrievably committed to flight towards orbit or intended to accelerate the payload to escape velocity. The following notes should help with understanding the launch lists.

Launch times are in UTC and are either from the launching agency or estimated by 'walking back' along the ground track to the launch site. Most orbit data and decay information comes from SpaceTrack. The Space-Track data occasionally contains inconsistencies (eg - incorrect re-entry dates or early sets of elements allocated to the wrong object) that need to be corrected from other sources.

To fill the gaps where elements are not formally published, usually because they have a classification of "Secret", some orbits are based on amateur observations. Such data is published near-daily by Mike McCants. Occasionally, orbits are estimated by myself from public data.

Space-Track sometimes has insufficient information to allocate names to objects in its catalogue. In these cases, names are derived from public information.

Apogee and perigee are measured against a spherical Earth with a radius of 6378.145 km, assumed to be situated at the focus of the orbital ellipse. The value for the orbital period is the Anomalistic Period, or time to complete one circuit of the ellipse. It is not the same as the time taken to complete one circuit of the Earth. Care should be exercised when comparing Orbital Focus data with other published orbits because they may have been derived using a different model.

Users can go straight to specific launches by pointing to the page URL followed by the three digit launch number, eg - https://www.OrbitalFocus/Diaries/Launches/Launches.php?year=2025#001


2025-001
Falcon 9 Block 5
Cape Canaveral Space Force Station
2025 Jan 4, 01:27 UTC
Thuraya 4
2025-001A
62483
in space
Comsat from the Al Yah Satellite Communications Company of the UAE to provide broadband and other data communications links across Africa, Europe, Central Asia and the Middle East. Separated from launch vehicle at 02:02 UTC. Continuously operating low thrust used to reach operational orbit. Expected location 44° east to replace Thuraya 2 (27825, 2003-026A).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Jan 5, 00:37336440.7977    429541031023.5726.91178
2025 Jan 12, 08:04350030.7806    1301559491086.2424.51181
2025 Jan 21, 18:00361300.7658    2082574211139.0820.40182
2025 Jan 29, 13:50376890.7409    3385592361213.6017.14184
2025 Feb 5, 10:58389980.7172    4652605881277.4014.64185
2025 Feb 11, 18:22399740.6915    5953612381325.6212.65187
2025 Feb 18, 07:07408830.6586    7577614321371.1010.71188
2025 Feb 25, 00:36415780.6191    9460609401406.228.93189
2025 Mar 5, 21:32421560.5684    11815597401435.637.23191163°.8 E
2025 Mar 12, 00:00425760.5276    13735586591457.146.49192
2025 Mar 19, 03:07416390.4986    14498560231409.315.03192
2025 Mar 26, 09:29407000.4676    15290533541361.914.06191
2025 Apr 2, 07:21434080.3630    21274527851500.073.30195
2025 Apr 9, 18:37434790.2996    24073501281503.742.57196
2025 Apr 16, 02:32441140.2513    26651488191536.802.02199
2025 Apr 24, 11:59450610.1863    30290470761586.591.36207
2025 May 1, 13:09430380.1073    32043412771480.930.84199
2025 May 7, 00:54430870.0537    34395390221483.450.47211
2025 May 12, 04:11421010.0084    35369360761432.840.1515144°.2 E
2025 May 16, 17:57421640.0002    35780357931436.080.1025044°.2 E
Falcon 9 second stage
2025-001B
62484
in space
Launched Thuraya 4.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 6, 13:41334910.7972    414538111016.5926.84178


2025-002
CZ 3B
Xichang Space Centre
2025 Jan 6, 20:00 UTC
Shijian 25 (Practice 25)
2025-002A
62485
in space
Mission details awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Jan 7, 11:32243880.7310    18235838631.7328.48180
2025 Jan 13, 19:03421950.0064    35546360881437.6410.21189120°.1 E
2025 Jan 14, 15:16421660.0059    35540360361436.1710.21185120°.0 E
2025 Jan 16, 08:07421690.0058    35547360341436.3010.21185119°.9 E
2025 Jan 16, 18:20421620.0057    35545360221435.9410.21184119°.9 E
2025 Jan 21, 14:14421630.0056    35547360231436.0210.22184120°.1 E
2025 Mar 27, 20:57421630.0059    35535360341435.9810.35183119°.8 E
CZ 3B fourth stage
2025-002B
62486
in space
Launched Shijian 25.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 7, 01:00248390.7372    15136772649.3328.46180


2025-003
Falcon 9 Block 5 (Starlink Group 06-071)
Cape Canaveral Space Force Station
2025 Jan 6, 20:43 UTC
Starlink 32713
2025-003A
62487
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 21:48 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 14, 16:0066800.0002    30130390.5643.00282
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jan 6
Life <1 day
Launched twenty four Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-004
Falcon 9 Block 5 (Starlink Group 12-011)
Kennedy Space Center
2025 Jan 8, 15:27 UTC
Starlink 11452
2025-004A
62511
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 16:32 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 9, 03:4466750.0003    29529990.4743.01252
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jan 8
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-005
Falcon 9 Block 5 (NRO L-153)
Vandenberg Space Force Base
2025 Jan 10, 03:53 UTC
USA 463 (Starshield 0073)
2025-005A
62532
in space
One of a simultaneously-launched group of twenty two US government NRO imaging reconnaissance satellites. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications.

All satellites were launched to a similar altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 27, 17:1968990.0001    52152295.0570.00172
2025 Mar 24, 01:5069220.0002    54254595.5270.00278
2025 Apr 11, 20:2769550.0002    57657896.2170.00174
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jan 10
Life <1 day
Launched twenty two Starshield satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-006
Falcon 9 Block 5 (Starlink Group 12-012)
Cape Canaveral Space Force Station
2025 Jan 10, 19:11 UTC
Starlink 11538
2025-006A
62554
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 20:16 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 17, 18:0066920.0002    31331590.8043.01277
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jan 10
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-007
Jielong 3 (Y5)
Mobile floating platform, Yellow Sea - 36°.6 N, 121°.2 E
2025 Jan 13, 03:00 UTC
Wei Li Kongjiang 01-01 (Centispace 1-01)
2025-007B
62576
in space
One of ten simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Also carries a demonstrator for an inter-satellite laser communication system.

All ten satellites were launched into similar orbits

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 13, 11:0170210.0013    63465297.5954.98297
2026 Jan 1, 04:1772330.0009    848861102.0354.97263
Jielong 3 fourth stage
2025-007M
62586
Re-entered - 2025 Feb 27
Life 45 days
Launched Wei Li Kongjiang 01 cluster of ten satellites. Perigee lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 13, 10:4568130.0321    21665493.2854.94359


2025-008
Falcon 9 Block 5 (Starlink Group 12-004)
Cape Canaveral Space Force Station
2025 Jan 13, 16:47 UTC
Starlink 11547
2025-008A
62587
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 17:52 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 17, 20:0066760.0002    29629990.4743.01279
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jan 13
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-009
Falcon 9 Block 5 (Transporter 12)
Vandenberg Space Force Base
2025 Jan 14, 19:09 UTC
Satellites
in space
Payload list to follow.


2025-010
Falcon 9 Block 5
Kennedy Space Center
2025 Jan 15, 06:11 UTC
Blue Ghost
2025-010A
62716
in space
Lunar lander from US company Firefly, carrying ten experiments for NASA under its Commercial Lunar Payload Services programme. Separated from launch vehicle at 07:16 UTC. Trans-lunar injection occurred February 8, at the third apogee of its initial barycentric orbit (similar to 62719, 2025-010D). Arrival in orbit around the Moon February 14 followed a 255 seconds thruster firing commencing at 01:51 UTC. Three further thruster firings resulted in a 20 x100 kilometre orbit. A thruster firing March 2 at 08:22 UTC set up the descent trajectory resulting in touchdown at 08:34 UTC (around lunar sunrise) in the Mare Crisium. Surface operations continued until March 16 and lunar sunset after which the solar cells ceased to provide power.
Landed on the Moon
Resilience
2025-010B
62717
in space
Lunar lander from Japanese company ispace. Carries Tenacious, a micro lunar rover and together they make up the Hakuto-R mission. Separated from launch vehicle at 07:43 UTC. Arrived in the vicinity of the Moon and entered orbit around it on May 6.
Entered orbit around the Moon
Falcon 9 second stage
2025-010D
62719
in space
Launched Resilience and Blue Ghost towards the Moon.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 15, 07:371877300.9651    17636252913491.5435.17346


2025-011
New Glenn (NG-1)
Cape Canaveral Space Force Station
2025 Jan 16, 07:03 UTC
New Glenn second stage
2025-011A
62720
in space
Rocket stage with attached New Glenn Pathfinder Payload equipped with instrumentation to monitor performance of the launch vehicle whilst on the launch pad and during its six hour test mission. The stage also carries US government Department of Defense sensors to evaluate a demonstrator version of Blue Origin's planned Blue Ring orbital payload carrier.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 16, 08:37172100.4894    240919254374.4730.00267


2025-012
CZ 2D
Jiuquan Space Centre
2025 Jan 17, 04:07 UTC
PRSC-EO 1
2025-012A
62725
in space
Remote sensing satellite developed by SUPARCO, Pakistan's space agency for Earth studies to support agriculture, urban planning, environmental management, disaster management, and monitoring, deforestation, glacier recession and water resources.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jan 18, 22:5269010.0008    51752895.0897.4827310:25
2025 Jan 20, 15:3869020.0009    51852995.1097.4826210:25
2025 May 7, 04:2568910.0008    50751894.8897.4624610:24
2025 Oct 12, 14:5168910.0008    50751994.8897.457510:24
2026 Mar 5, 22:3668910.0005    50951694.8897.4323810:22
Lantan 1 (Blue Carbon 1)
2025-012B
62726
in space
Small Chinese satellite for ocean studies. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jan 17, 15:2169010.0009    51752995.0997.4828110:25
Tianlu 1 (DA 01)
2025-012C
62727
in space
Small Chinese satellite for middle and upper atmosphere studies. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jan 17, 15:2369010.0009    51753095.0997.4927010:25
CZ 2D second stage
2025-012D
62728
in space
Launched cluster of three satellites including Pakistan's EO1.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 17, 15:2369020.0008    51853095.1297.48266


2025-013
Ceres 1 (Gushenxing 1 Y-16 )
Jiuquan Space Centre
2025 Jan 20, 10:11 UTC
Jitianxing A-05
2025-013A
62729
in space
Earth imaging satellite from Jitian Xingzhou Space Technology of Suzhou, China.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jan 21, 00:3769170.0014    52954895.4197.6128216:29
Yunyao-1 37
2025-013B
62730
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jan 21, 00:3869160.0014    52854895.4197.6028416:29
2025 Feb 1, 12:4869180.0013    53154995.4597.6125416:30
2025 Feb 2, 14:1669200.0013    53355195.4897.6125616:30
2025 Feb 3, 12:3469210.0013    53455295.5197.6125816:30
2025 Feb 4, 12:2769220.0013    53555395.5297.6125916:30
2025 Feb 6, 17:0269240.0014    53655695.5797.6125816:30
2025 Feb 23, 18:3969260.0014    53855895.6097.6120216:30
Yunyao-1 38
2025-013C
62731
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jan 21, 00:3969160.0014    52854895.4097.6128516:29
2025 Feb 11, 09:4769170.0015    52954995.4297.6121616:30
2025 Feb 12, 00:0769200.0016    53155395.4997.6022516:30
2025 Feb 13, 04:4769210.0015    53355495.5197.6122516:30
2025 Feb 17, 13:5869260.0015    53855895.6197.6122716:30
Yunyao-1 40
2025-013D
62732
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jan 21, 00:3869160.0014    52854895.4097.6028916:29
2025 Feb 23, 17:3769140.0015    52654695.3697.6116616:30
2025 Feb 25, 14:0969170.0013    53054895.4297.6116516:30
2025 Feb 26, 12:2669180.0012    53254995.4597.6116616:30
2025 Mar 1, 10:3069220.0010    53755195.5397.6117616:31
2025 Mar 6, 10:0369250.0009    54155495.5997.6118616:31
Yunyao-1 39
2025-013E
62733
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jan 21, 05:0669160.0014    52854795.3997.6128416:29
2025 Feb 18, 05:3969150.0014    52754795.3897.6118716:30
2025 Feb 21, 02:0669200.0012    53455095.4997.6119316:30
2025 Feb 24, 11:2269260.0009    54255495.6097.6120916:30
Ceres 1 fourth stage
uncatalogued
Re-entered - 2025 Jan 21
Life 1 day
Launched four Yunyao-1 satellites and Jitianxing A-05. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-014
Falcon 9 Block 5 (Starlink Group 13-001)
Kennedy Space Center
2025 Jan 21, 05:24 UTC
Starlink 32806
2025-014A
62735
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle about 06:29 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 24, 17:2866920.0004    31131790.8043.01231
USA 485 (Starshield 0095)
2025-014X
62756
in space
One of a pair of government NRO imaging reconnaissance satellites, launched alongside 21 SpaceX starlink satellites. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Separated from launch vehicle at 06:29 UTC. Presence on launch vehicle undeclared by SpaceX

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 24, 17:2966890.0003    30831390.7343.01234
2025 Jan 29, 03:1966960.0002    31731990.8943.01250
2025 Feb 1, 14:2966910.0003    31131590.7943.01251
2025 Feb 11, 10:5967230.0001    34434591.4243.00286
USA 486 (Starshield 0096)
2025-014Y
62757
in space
One of a pair of government NRO imaging reconnaissance satellites, launched alongside 21 SpaceX starlink satellites. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Separated from launch vehicle at 06:29 UTC. Presence on launch vehicle undeclared by SpaceX.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 24, 17:2966880.0002    30931290.7343.01253
2025 Jan 29, 03:1866960.0001    31731890.8843.01251
2025 Feb 2, 08:3666890.0003    31031390.7543.01249
2025 Feb 11, 14:0067240.0002    34434791.4543.00213
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jan 21
Life <1 day
Launched twenty one Starlink and two Starshield satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-015
Falcon 9 Block 5 (Starlink Group 11-008)
Vandenberg Space Force Base
2025 Jan 21, 15:45 UTC
Starlink 33596
2025-015A
62758
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 16:46 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 24, 20:0066470.0002    26827089.8853.16316
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jan 21
Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-016
CZ 6A (Qianfan Ji Gui polar orbit group 6)
Taiyuan Space Centre
2025 Jan 23, 05:15 UTC
Qianfan Ji Gui 06-01
2025-016A
62785
in space
One member of a simultaneously launched cluster of eighteen broadband distribution satellites for the Thousand Sails constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 5, 19:1771820.0016    792815100.9588.99167
CZ 6A third stage
2025-016U
62803
in space
Launched eighteen Qianfan Ji Gui satellites. Perigee lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 5, 20:1170970.0103    64679299.1789.0366


2025-017
CZ 3B
Xichang Space Centre
2025 Jan 23, 15:32 UTC
Tongxin Jishu Shiyan 14 (Communication Technology Test 14, TJS 14)
2025-017A
62804
in space
Satellite described as being mainly used for used for satellite communications, radio and television, data transmission, and other services, and carrying out related technical tests and verifications. Probably moved to Geosynchronous Drift Orbit January 24 at about 07:00 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Jan 23, 19:46243760.7306    18935807631.2728.48180
2025 Feb 4, 14:52421650.0002    35780357941436.112.0022418°.3 E
CZ 3B fourth stage
2025-017B
62805
Re-entered - 2026 Apr 4
Life 436 days
Launched TJS 14.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 23, 17:24236720.7249    13534452604.0928.56179


2025-018
Falcon 9 Block 5 (Starlink Group 11-006)
Vandenberg Space Force Base
2025 Jan 24, 14:07 UTC
Starlink 32883
2025-018A
62806
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:11 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 30, 16:0066690.0001    29029190.3353.1577
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jan 24
Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-019
Falcon 9 Block 5 (Starlink Group 12-007)
Cape Canaveral Space Force Station
2025 Jan 27, 22:05 UTC
Starlink 11548
2025-019A
62829
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 23:10 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 4, 20:0066960.0002    31731990.8943.00266
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jan 27
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-020
GSLV Mk II F15
Satish Dhawan Space Centre
2025 Jan 29, 00:53 UTC
NVS 02 (IRNSS 1K)
2025-020A
62850
in space
Second generation navsat in India's Regional Navigation Satellite System to provide navigation services to the Indian subcontinent and an area extending 1500 km beyond it. Released from launch vehicle at 01:12 UTC. Intended to replace IRNSS 1E (41241, 2016-003A) at 111°.75 east but a stuck valve prevented propellant flow to its thrusters leading to it being stranded in geosynchronous transfer orbit.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 29, 06:56252670.7412    16237615666.1620.75178
GSLV third stage
2025-020B
62851
in space
Launched NVS 02.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 29, 06:54251420.7398    16437364661.2520.74178


2025-021
Falcon 9 Block 5
Kennedy Space Center
2025 Jan 30, 01:34 UTC
Spainsat New Generation I
2025-021A
62852
in space
Military communications satellite built by a consortium led by Hisdesat for the Spanish Government. Continuously operating low thrust used to reach operational orbit. Separated from launch vehicle at 02:05 UTC. Expected location - 29°east or 30° west.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Feb 2, 09:48405610.8320    437679301354.9726.85178
2025 Feb 3, 08:24407680.8286    610681701365.3526.11178
2025 Feb 6, 04:55413040.8234    917689331392.3224.72179
2025 Feb 13, 01:32424930.8071    1821704091452.8921.70180
2025 Feb 20, 05:12435100.7882    2836714291505.3918.61181
2025 Feb 27, 13:56440300.7638    4021712831532.4515.89182
2025 Mar 7, 01:18442420.7340    5389703381543.5013.36184
2025 Mar 14, 13:23443770.7032    6792692061550.6111.41185
2025 Mar 21, 00:12444740.6782    7936682571555.699.91186
2025 Mar 28, 13:10443420.6566    8850670791548.788.98187
2025 Apr 3, 23:59443010.6205    10434654121546.627.60188
2025 Apr 11, 12:36444870.5801    12300639181556.386.36189
2025 Apr 18, 00:01434780.5603    12738614621503.725.48189
2025 Apr 24, 12:02434290.5100    14904591991501.194.51190
2025 May 2, 01:09440790.4586    17487579141534.983.78192
2025 May 8, 12:17440900.4107    19603558211535.583.14194
2025 May 15, 11:39441460.3644    21679538571538.502.53195
2025 May 22, 20:30444610.3197    23867522991554.991.97197
2025 May 27, 01:57451430.2941    25490520401590.911.67198
2025 Jun 3, 12:22463330.2545    28165517441654.211.13206
2025 Jun 7, 11:22470390.2316    29767515551692.201.15205
2025 Jun 12, 13:21430430.1444    30450428801481.200.96190
2025 Jun 15, 22:36426840.1325    30651419621462.730.91191
2025 Jun 30, 06:55423880.0242    34984370361447.530.24192
2025 Jul 3, 01:58421610.0075    35465361011435.900.1519633°.8 E
2025 Jul 13, 20:26421640.0001    35782357911436.080.0831632°.9 E
2025 Aug 22, 21:28421640.0000    35786357871436.080.0318228°.9 E
2025 Sep 18, 23:39421600.0001    35779357861435.880.0717129°.8 E
2025 Oct 14, 22:06421570.0002    35772357861435.700.1418331°.8 E
2025 Nov 10, 21:25421530.0003    35762357881435.510.2119835°.2 E
2025 Dec 6, 10:25421680.0002    35782357971436.250.2812439°.6 E
2025 Dec 9, 17:56423030.0003    35913359371443.170.2921533°.9 E
2025 Dec 12, 06:46423030.0003    35913359361443.150.2921829°.4 E
2025 Dec 15, 06:40421640.0001    35781357901436.040.3025429°.1 E
2026 Jan 8, 19:35421650.0001    35782357911436.090.2626529°.0 E
Falcon 9 second stage
2025-021B
62853
Launched Spainsat NG 1.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jan 30, 23:21398720.8335    262667251320.5726.93177


2025-022
Falcon 9 Block 5 (Starlink Group 11-004)
Vandenberg Space Force Base
2025 Feb 1, 23:02 UTC
Starlink 32868
2025-022A
62854
in space
One member of a simultaneously-launched cluster of twenty two broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle February 2 at 00:03 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 10, 20:0066970.0001    31831990.9053.1546
Falcon 9 second stage
2025-022Y
62878
Re-entered - 2025 Feb 19
Life 18 days
Engine firing intended to cause re-entry after releasing satellites did not occur.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 3, 10:4766600.0012    27429090.1553.17248


2025-023
H-3 22S (F-5)
Tanegashima Space Centre
2025 Feb 2, 08:30 UTC
Michibiki 6 (QZSS 6)
2025-023A
62876
in space
Quasi Zenith Satellite System satellite providing a timing and positioning service to improve navigational accuracy for users in Japan from a combination of equatorial GEO and inclined GEO, giving coverage to areas where the topography works against GPS reception. “Michibiki" translates into English as "Showing the Way". Separated from launch vehicle at 0859 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Feb 2, 10:49242710.7212    39035397627.2021.98176
2025 Feb 3, 13:02263710.5824    463435352710.3212.98175
2025 Feb 5, 09:29397390.0461    31527351931313.950.56170
2025 Feb 10, 20:47421150.0012    35685357901433.570.085790°.3 E
2025 Feb 11, 20:31421550.0003    35764357901435.600.085590°.4 E
2025 Feb 12, 14:28421630.0001    35780357911436.030.083490°.4 E
2025 Feb 17, 22:43421640.0001    35780357921436.050.074590°.5 E
H3 upper stage
2025-023B
62877
in space
Launched QZSS 6.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 2, 10:41242450.7206    39735336626.1521.97175
2025 Feb 6, 01:55241160.7251    25135225621.1821.48178


2025-024
Falcon 9 Block 5 (Starlink Group 12-003)
Cape Canaveral Space Force Station
2025 Feb 4, 10:15 UTC
Starlink 11371
2025-024A
62879
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 11:20 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 10, 20:0066910.0001    31231490.7843.00265
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Feb 4
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-025
Falcon 9 Block 5 (Maxar 3)
Kennedy Space Center
2025 Feb 4, 23:13 UTC
Worldview Legion 6
2025-025A
62900
in space
High resolution imaging satellite from Maxar Technologies of the US. Part of a constellation of six satellites providing images in response to customer demand. Separated from launch vehicle February 5 at 00:00 UTC. Space-Track has this tagged incorrectly as Legion 5.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 5, 01:0970820.0006    70070998.8645.0497
Worldview Legion 5
2025-025B
62901
in space
High resolution imaging satellite from Maxar Technologies of the US. Part of a constellation of six satellites providing images in response to customer demand. Separated from launch vehicle February 5 at 01:03 UTC. Space-Track has this tagged incorrectly as Legion 6.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 5, 01:1068280.0025    43346793.5944.9721
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Feb 4
Life <1 day
Launched pair of Worldview Legion satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-026
Soyuz-2.1v + Volga
Plesetsk Cosmodrome
2025 Feb 5, 03:59 UTC
Cosmos 2581
2025-026A
62902
in space
Small, military, satellite - mission unknown but working together with Cosmos 2582. Released from Volga rocket stage mid-late morning on day of launch, at about 2000 km behind Cosmos 2582 and Cosmos 2583. Raised orbit slightly February 19.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 5, 18:1769650.0011    57959496.4181.99275
2025 Feb 19, 13:3069670.0011    58159696.4582.00207
2025 Dec 31, 17:3669620.0009    57859096.3682.00250
Cosmos 2582
2025-026B
62903
in space
Small, military, satellite - mission unknown but working together with Cosmos 2581. Released from Volga rocket stage, together with Cosmos 2583, at about 04:30 UTC. Made rendezvous with Cosmos 2581 and moved to similar orbit February 24 probably around 21:00 UTC to begin station keeping. No further orbital manoeuvres detected following a slight adjustment June 23.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 5, 11:4769650.0015    57659796.4181.99260
2025 Feb 15, 12:5769670.0014    58059996.4781.99219
2025 Feb 25, 12:3969670.0011    58159696.4582.00187
2025 Apr 6, 22:2669660.0012    57959696.4382.0064
2025 Apr 7, 14:3169640.0013    57659596.3982.0054
2025 Apr 7, 17:4469660.0013    57959796.4382.0055
2025 Jun 23, 09:1069640.0009    57959296.3982.00155
2025 Jun 23, 17:1369650.0011    57959496.4182.00155
2025 Dec 31, 17:4169620.0009    57859196.3682.00250
Cosmos 2583 p/l 1
2025-026C
62904
in space
Small, military, satellite - mission unknown. Released from Volga rocket stage, together with Cosmos 2582, at about 04:30 UTC. Made minor thruster firing on March 15 with no significant effect on the orbit. Separated from Cosmos 2583 p/l 2 March 18 at about 20:15 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 5, 19:4969670.0013    58059896.4581.99267
2025 Mar 19, 13:4669650.0015    57659796.4282.00126
2025 Dec 31, 17:3669620.0009    57859096.3581.99268
Cosmos 2583 p/l 2
2025-026F
63330
in space
Separated from Cosmos 2583 pl/1 March 18 at about 20:15 UTC. No orbital manoeuvring detected s may be a discarded cover or other item of redundant equipment.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 18, 23:4169660.0014    57859796.4382.01127
2025 Dec 31, 18:1069570.0011    57158696.2581.99260
Volga rocket stage
2025-026D
62905
Re-entered - 2025 Feb 5
Life <1 day
Released Cosmos 2582 and Cosmos 2583 at about 04:30 UTC and then raised orbit. Orbit lowered when about 2000 km behind Cosmos 2582 to be followed by release of Cosmos 2581. Retro-fire at about 14:00 UTC led to destructive re-entry, at about 14:50 UTC, above the southern Pacific Ocean.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 5, 11:5269640.0010    57959396.3981.99276
Soyuz second stage
2025-026E
62906
Re-entered - 2025 Mar 24
Life 47 days
Launched Cosmos 2581 - Cosmos 2583.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 5, 09:5867720.0272    21057892.4482.0174


2025-027
Falcon 9 Block 5 (Starlink Group 12-009)
Cape Canaveral Space Force Station
2025 Feb 8, 19:18 UTC
Starlink 11552
2025-027A
62907
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 20:23 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 13, 14:0066780.0002    29930190.5243.01269
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Feb 8
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-028
Electron (IOT 4 You and Me)
Rocket Lab Launch Complex, New Zealand
2025 Feb 8, 20:43 UTC
Kinéis 2C (Kinéis 13)
2025-028B
62929
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Feb 10, 18:5770210.0002    64164497.5797.966209:06
Kinéis 2D (Kinéis 14)
2025-028C
62930
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Feb 10, 20:3570200.0002    64164397.5697.964809:06
Kinéis 2E (Kinéis 15)
2025-028D
62931
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Feb 10, 18:5770200.0001    64164297.5697.969509:06
Kinéis 2A (Kinéis 11)
2025-028E
62932
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Feb 10, 18:5670190.0001    64064297.5497.9632909:06
Kinéis 2B (Kinéis 12)
2025-028G
62934
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Feb 11, 14:2770190.0001    64064197.5397.9627109:06
Electron third stage (kick stage)
2025-028A
62928
in space
Launched five Kinéis satellites. Perigee lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 9, 00:4669890.0043    58164196.9297.9342
Electron second stage
2025-028F
62933
Re-entered - 2025 Feb 21
Life 13 days
Launched five Kinéis satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 10, 19:4367720.0315    18060792.4497.96222


2025-029
Falcon 9 Block 5 (Starlink Group 11-010)
Vandenberg Space Force Base
2025 Feb 11, 02:09 UTC
Starlink 32728
2025-029A
62948
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:11 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 18, 16:0066820.0001    30330490.6053.1558
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Feb 11
Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-030
CZ 8A
Wenchang Space Centre
2025 Feb 11, 09:30 UTC
Hulianwang Digui 02-01 (Satellite Low Orbit Internet Group 02-01)
2025-030A
62971
in space
One of nine simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 11, 15:4272460.0008    863874102.3250.00257
CZ 8A third stage
2025-30K
62980
in space
Launched group of nine Hulianwang Digui low orbit internet comsats. Perigee lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 11, 15:3671610.0119    698868100.5150.0083


2025-031
Falcon 9 Block 5 (Starlink Group 12-018)
Cape Canaveral Space Force Station
2025 Feb 11, 18:53 UTC
Starlink 11543
2025-031A
62981
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 19:57 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 18, 18:0066950.0002    31531890.8643.00291
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Feb 11
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-032
Falcon 9 Block 5 (Starlink Group 12-008)
Cape Canaveral Space Force Station
2025 Feb 15, 06:14 UTC
Starlink 11448
2025-032A
63005
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 07:19 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 20, 16:0066780.0001    29930090.5143.01243
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Feb 15
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-033
Electron (Fasten Your Seat Belts)
Rocket Lab Launch Complex, New Zealand
2025 Feb 18, 23:17 UTC
BlackSky 31 (Global 31)
2025-033B
63027
in space
Third Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc. Released from kick stage February 19 at 00:12 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 19, 14:1968510.0008    46847994.0759.00325
Electron third stage (kick stage)
2025-033A
63026
Re-entered - 2026 Feb 23
Life 370 days
Launched BlackSky 31 satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 19, 14:2468520.0007    46947894.0759.00354
Electron second stage
2025-033C
63028
Re-entered - 2025 Feb 26
Life 8 days
Launched BlackSky 31 satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 19, 06:2967060.0227    17547991.0859.00268


2025-034
Falcon 9 Block 5 (Starlink Group 10-012)
Cape Canaveral Space Force Station
2025 Feb 18, 23:21 UTC
Starlink 32798
2025-034A
63029
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle February 19 at 00:27 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 25, 16:0066700.0001    29129290.3553.1650
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Feb 19
Life 1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-035
Falcon 9 Block 5 (Starlink Group 12-014)
Cape Canaveral Space Force Station
2025 Feb 21, 15:19 UTC
Starlink 11550
2025-035A
63052
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 16:24 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 27, 20:0066630.0002    28428690.2143.00289
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Feb 21
Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-036
CZ 3B
Xichang Space Centre
2025 Feb 22, 12:11 UTC
Zhongxing 10R (Chinasat 10R)
2025-036A
63075
in space
Communications satellite described as providing services to users in China's transportation, emergency, energy, forestry and grassland industries, as well as to other countries in central Asia. Probably for use by government/military services. Expected location 110°.5 east to replace Zhongxing 10 (37677, 2011-026A). Arrived on station

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Feb 22, 18:01243720.7298    20635782631.1127.63179
2025 Mar 4, 19:06421660.0002    35779357961436.140.0780126°.0 E
2025 Jun 2, 17:24422480.0024    35770359701440.360.2989124°.6 E
2025 Jun 15, 11:30421650.0004    35768358051436.090.04228110°.6 E
CZ 3B fourth stage
2025-036B
63076
in space
Launched Zhongxing 10R.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 22, 19:04243630.7303    19335777630.7627.69180


2025-037
Falcon 9 Block 5 (Starlink Group 15-001)
Vandenberg Space Force Base
2025 Feb 23, 01:38 UTC
Starlink 32839
2025-037A
63077
in space
One member of a simultaneously-launched cluster of twenty two broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:39 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 28, 16:0066570.0004    27628190.0869.99275
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Feb 23
Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-038
Falcon 9 Block 5
Kennedy Space Center
2025 Feb 27, 00:16 UTC
Athena (IM-2)
2025-038A
63099
in space
Lunar landing vehicle launched under NASA's Commercial Lunar Payload Services programme. Built by US company Intuitive Machines, carrying three experiments including two surface exploration vehicles. Released from launch vehicle at 01:00 UTC. Initial Earth orbit similar to the Falcon 9 upper stage (63103, 2025-023E).

A 492s thruster firing February 3 at 13:41 UTC resulted in orbit around the Moon. Multiple thruster firings on March 6 resulted in touchdown near the south pole of the Moon at 17:30 UTC about 400 metres from the aim point. Communication was established with ground stations, indicating it had toppled over. Athena was planned to operate for ten days until lunar sunset but operations ceased when battery power was exhausted March 7.
Landed on the Moon
Chimera GEO 1
2025-038B
63100
in space
GEO satellite transfer vehicle from US company Epic Aerospace. Carries a 16U Cubesat from Norwegian company Space Inventor to be released into GEO. Separated from launch vehicle at 01:04 UTC. Current status unknown - not currently being tracked by Space-Track.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
estimated orbit1902350.9654    21236750113762.3828.52216
Lunar Trailblazer
2025-038C
63101
in space
NASA SIMPLEx (Small Innovative Missions for Planetary Exploration) Moon orbiter designed to map lunar resources including water. Released from launch vehicle at 01:04 UTC. Originally expected to arrive in the vicinity of the Moon 4-7 months after launch after a series of thruster firings. Radio contact was established after launch but was then lost almost immediately.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
estimated orbit1902350.9654    21236750113762.3828.52216
Odin
2025-038D
63102
in space
Asteroid exploration mission from US company AstroForge. Released from launch vehicle at 01:02 UTC. Initial Earth orbit similar to the Falcon 9 upper stage (63103, 2025-023E). Planned to fly by asteroid 2022 OB5 in 2025 late-December but AstroForge was unable to establish ongoing communication in order to direct Odin towards its target.
Heliocentric orbit
Falcon 9 second stage
2025-038E
63103
in space
Launched Athena, Odin, Lunar Trailblazer and Chimera GEO 1.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
estimated orbit1902350.9654    21236750113762.3828.52216


2025-039
Falcon 9 Block 5 (Starlink Group 12-013)
Cape Canaveral Space Force Station
2025 Feb 27, 03:34 UTC
Starlink 11629
2025-039A
63104
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:39 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 5, 20:0066830.0002    30430690.6243.00256
Falcon 9 second stage
Re-entered - 2025 Feb 27
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Orbit parameters awaited


2025-040
CZ 2C
Jiuquan Space Centre
2025 Feb 27, 07:08 UTC
Siwei Gaojing 1-03 (Superview Neo 1-03)
2025-040A
63125
in space
One of a simultaneously launched pair of commercial remote sensing satellites from the Siwei Surveying and Mapping Technology Co aimed at producing 3D Earth images. Orbit maintained precisely by frequent use of low power thruster.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Feb 27, 13:2568760.0012    48950694.5697.3124313:30
2025 Mar 8, 17:4768790.0000    50150194.6397.316713:29
2026 Jan 9, 07:4168790.0002    50050294.6497.347413:15
Siwei Gaojing 1-04 (Superview Neo 1-04)
2025-040B
63126
in space
One of a simultaneously launched pair of commercial remote sensing satellites from the Siwei Surveying and Mapping Technology Co aimed at producing 3D Earth images. Orbit maintained precisely by frequent use of low power thruster.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Feb 27, 13:2568760.0012    48950694.5797.3124113:30
2025 Mar 5, 18:4668790.0000    50150194.6397.317313:29
2026 Jan 9, 07:4268790.0001    50050294.6497.346013:15
CZ 2C second stage
2025-040C
63127
in space
Launched pair of Siwei Gaojing radar imaging satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 27, 11:3468690.0016    48050194.4297.14323


2025-041
Soyuz-2.1a
Baikonur Cosmodrome
2025 Feb 27, 21:24 UTC
Progress MS-30 (Progress 7K-MS №460)
2025-041B
63129
Re-entered - 2025 Sep 9
Life 194 days
Supplies to ISS. Initial orbit similar to launch vehicle upper stage. Docked with the rearward-facing port of the ISS Zarya module March 1 at 23:02 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 28, 04:5166910.0006    30931790.7851.63312
2025 Mar 2, 12:5867960.0006    41442292.9251.63334
Soyuz third stage
2025-041A
63128
Re-entered - 2025 Mar 1
Life 2 days
Launched Progress MS-30.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Feb 28, 04:4765800.0029    18322188.5351.66104


2025-F01 - failed to reach orbit
Kuaizhou-1A-Pro
Jiuquan Space Centre
2025 Mar 1, 10:00 UTC
Unknown payload
Rocket repotedly exploded shortly after ignition. Unclear whether the launch was an orbital attempt.


2025-042
Soyuz-2.1b + Fregat
Plesetsk Cosmodrome
2025 Mar 2, 22:22 UTC
Cosmos 2584 (Uragan-K2 №14L)
2025-042A
63130
in space
GLONASS navigation satellite to fill a space in the constellation. Separated from the launch vehicle Fregat stage at about 04:30 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 3, 17:53255260.0003    1914019155676.4464.81295
2025 Mar 18, 23:03255080.0008    1911019150675.7364.83236
Fregat rocket stage
2025-042B
63131
in space
Launched Cosmos 2584. Minor changes in orbit may be due to venting of residual propellant.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 3, 10:58254920.0011    1908619141675.0964.83263
2025 Mar 3, 16:47254840.0002    1910119110674.7764.84235
2025 Mar 3, 22:55254570.0017    1903619121673.6964.82198


2025-043
Falcon 9 Block 5 (Starlink Group 12-020)
Cape Canaveral Space Force Station
2025 Mar 3, 02:24 UTC
Starlink 11609
2025-043A
63132
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:29 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 7, 18:0066740.0001    29429690.4343.00253
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 3
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-044
Ariane 6 (VA-263)
Centre Spatiale Guyanaise
2025 Mar 6, 16:24 UTC
Composante Spatiale Optique 3 (CSO 3)
2025-044A
63156
in space
Military/Government Earth high resolution imaging satellite for the French Air and Space Forces Space Command (CDE). Third in a constellation of three satellites to replace the Helios 2 series. Aimed at 800km sun-synchronous orbit with LTDN around 01:15 near to that of CSO 1 in order to improve the revisit time over a target. Released from launch vehicle at 17:30 UTC. First commercial launch by Ariane 6. Orbit information based on data from amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 19, 02:3471810.0002    801804100.9398.61701:28
Ariane 6 third stage
uncatalogued
Re-entered - 2025 Mar 6
Life <1 day
Launched CSO 3. Caused to re-enter above the south east Indian Ocean at about 19:00 UTC on the day of launch, following retro-fire.
Not Catalogued - orbit parameters unavailable


2025-045
CZ 3B
Xichang Space Centre
2025 Mar 9, 17:17 UTC
Tongxin Jishu Shiyan 15 (Communication Technology Test 15, TJS 15)
2025-045A
63157
in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT). Appears to have moved from transfer orbit to GEO March 14 and then separated from 2025-045C about 24 hours later (date/time to be confirmed). Mission profile resembles that of TJS 3 (2018-110).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Mar 10, 03:50245230.7327    17836111636.9619.02179
2025 Mar 17, 17:27421650.0001    35785357891436.120.0132290°.3 E
CZ 3B fourth stage
2025-045B
63158
Re-entered - 2025 Aug 8
Life 152 days
Launched TJS 15.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 12, 05:02248420.7376    14136787649.4419.04182
apogee motor (CZ 3B fifth stage)
2025-045C
63299
in space
Moved TJS 15 from transfer orbit to geosynchronous drift orbit and (possibly) to its GEO location, then manoeuvred itself to graveyard orbit after releasing the satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 17, 16:17425620.0027    36068362991456.420.047


2025-046
CZ 8A (Y6)
Wenchang Space Centre - Hainan Commercial Zone
2025 Mar 11, 16:38 UTC
Qianfan Ji Gui 05-01
2025-046A
63159
in space
One member of a simultaneously launched cluster of eighteen broadband distribution satellites for the Thousand Sails constellation.

All satellites were probably injected into similar orbits at 89° inclination.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 24, 20:1672920.0013    904923103.2888.99167
CZ 8A third stage
2025-046U
63177
in space
Launched group of eighteen Qianfan Ji Gui i satellites. Perigee lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 24, 19:1072390.0065    814908102.1688.9980


2025-047
Falcon 9 Block 5
Vandenberg Space Force Base
2025 Mar 12, 03:10 UTC
PUNCH Narrow Field Imager (Polarimeter to Unify the Corona and Heliosphere)
2025-047A
63178
in space
One of a set of four simultaneously-launched small satellites from NASA to study the solar wind by tracking groups of electrons as they travel away from the Sun. Will orbit independently of the three wide field imager satellites. Released from launch vehicle at 04:03 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 13, 09:3670270.0015    63865997.7097.9516317:59
PUNCH Wide Field Imager 1 (Polarimeter to Unify the Corona and Heliosphere)
2025-047B
63179
in space
One of a set of four simultaneously-launched small satellites from NASA to study the solar wind by tracking groups of electrons as they travel away from the Sun. The three satellites equipped with wide field imaging systems will be distributed at 120° intervals round the orbit. Released from launch vehicle at 04:03 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 13, 09:3670270.0017    63766197.7197.9616017:59
PUNCH Wide Field Imager 3 (Polarimeter to Unify the Corona and Heliosphere)
2025-047C
63180
in space
One of a set of four simultaneously-launched small satellites from NASA to study the solar wind by tracking groups of electrons as they travel away from the Sun. The three satellites equipped with wide field imaging systems will be distributed at 120° intervals round the orbit. Released from launch vehicle at 04:03 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 13, 19:1270280.0017    63966297.7497.9615918:00
PUNCH Wide Field Imager 2 (Polarimeter to Unify the Corona and Heliosphere)
2025-047D
63181
in space
One of a set of four simultaneously-launched small satellites from NASA to study the solar wind by tracking groups of electrons as they travel away from the Sun. The three satellites equipped with wide field imaging systems will be distributed at 120° intervals round the orbit. Released from launch vehicle at 04:03 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 14, 14:5270290.0010    64465797.7497.9520218:00
SPHEREx (Spectro-Photometer for the History of the Universe, Epoch of Reionization and Ices Explorer)
2025-047E
63182
in space
NASA satellite to map the celestial sphere at infrared wavelengths. Released from launch vehicle at 03:52 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 14, 05:0770310.0010    64666097.7997.9622418:00
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 12
Life <1 day
Launched SPHEREx and four PUNCH satellites. Caused to re-enter above the southern Pacific Ocean at about 05:05 UTC.
Not Catalogued - orbit parameters unavailable


2025-048
Falcon 9 Block 5 (Starlink Group 12-021)
Cape Canaveral Space Force Station
2025 Mar 13, 02:36 UTC
Starlink 11602
2025-048A
63183
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:41 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 18, 20:0066550.0002    27527890.0443.01260
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 13
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-049
Falcon 9 Block 5
Kennedy Space Center
2025 Mar 14, 23:03 UTC
SpaceX Dragon Crew 10 (Dragon Endurance Flight #4)
2025-049A
63204
Re-entered - 2025 Aug 9
Life 148 days Returned to Earth
Crew flight to ISS provided by SpaceX under contract to NASA. Crew members: Commander - Anne McClain (NASA), Pilot - Nicole Ayers, Mission Specialists - Kirill Peskov (Roscosmos), and Takuya Onishi (JAXA). Initial orbit unavailable. Docked with the forward-facing port of the ISS Harmony module on March 16 at 04:04 UTC. Undocked August 8 at 22:15 UTC. Retrofire

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 15, 09:5466050.0025    21024389.0351.65238
2025 Mar 16, 09:4167950.0006    41242192.9051.6428
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 15
Life 1 day
Launched Dragon Crew 10. Caused to re-enter after releasing the spacecraft.
Not Catalogued - orbit parameters unavailable


2025-050
Electron (The Lightning God Reigns)
Rocket Lab Launch Complex, New Zealand
2025 Mar 15, 00:00 UTC
QPS-SAR 9 (Susanoo-I)
2025-050A
63205
in space
Commercial satellite from Japanese company iQPS, equipped with an Earth imaging radar. One in a constellation that will ultimately consist of 36 satellites. Separated from launch vehicle at 00:55 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 18, 08:3369550.0006    57358296.2242.02290
Electron second stage
2025-050B
63206
Re-entered - 2025 Apr 9
Life 25 days
Launched QPS-SAR 9 satellite. Initially identified by Space-Track incorrectly as the third (kick) stage.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 18, 11:5067770.0242    23556392.5442.03289
Electron third stage (kick stage)
2025-050C
63207
in space
Launched QPS-SAR 9 satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 21, 05:2169530.0008    56958196.1742.02318


2025-051
CZ 2D
Jiuquan Space Centre
2025 Mar 15, 04:11 UTC
Siwei Gaojing 3-02 (Superview Neo 3-02)
2025-051A
63208
in space
Commercial remote sensing satellites operated by Beijing Space View Technology Co. Ltd. of China. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 15, 16:5968740.0009    48950294.5397.4927610:30
Tianyan 23
2025-051B
63209
in space
Small satellite equipped with a remote sensing payload. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 15, 17:0068730.0008    48950194.5297.4928510:30
CZ 2D second stage
uncatalogued
in space
Launched Siwei Gaojing 3-02 and Tianyan 23. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-052
Falcon 9 Block 5 (Transporter 13)
Vandenberg Space Force Base
2025 Mar 15, 06:43 UTC
Satellites
in space
Payload list to follow.


2025-053
Falcon 9 Block 5 (Starlink Group 12-016)
Cape Canaveral Space Force Station
2025 Mar 15, 11:35 UTC
Starlink 11654
2025-053A
63265
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 12:40 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 21, 20:0066800.0002    30130390.5643.00271
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 15
Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-054
Angara 1.2
Plesetsk Cosmodrome
2025 Mar 16, 10:50 UTC
Cosmos 2585 (Rodnik-S)
2025-054A
63288
in space
Government/military system store-dump communications satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 17, 17:2678830.0015    14931517116.0982.50344
2025 Apr 23, 17:5878830.0014    14941516116.0982.50258
2025 Apr 25, 12:3278780.0018    14861513115.9782.50234
2025 Apr 27, 16:4478760.0020    14831513115.9482.50225
2025 Apr 28, 19:4878730.0023    14771513115.8782.49218
2025 May 3, 21:3178730.0024    14761513115.8682.49206
Cosmos 2586 (Rodnik-S)
2025-054B
63289
in space
Government/military system store-dump communications satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 17, 21:1878810.0014    14921514116.0682.50336
2025 Apr 14, 16:5778810.0013    14931514116.0682.50271
2025 Apr 16, 09:3478770.0015    14871511115.9682.50246
2025 Apr 21, 13:1678730.0019    14801510115.8782.49223
2025 May 1, 18:3878720.0020    14781510115.8682.49199
Cosmos 2587 (Rodnik-S)
2025-054C
63290
in space
Government/military system store-dump communications satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 17, 17:2578800.0014    14911513116.0482.50331
2025 Apr 1, 23:0578730.0013    14851505115.8882.50257
Angara 1.2 second stage
uncatalogued
in space
Launched Cosmos 2585 - 2587. Caused to re-enter above the Atlantic Ocean, at about 12:20 UTC on the day of launch, after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-055
Ceres 1 (Gushenxing 1 Y-10)
Jiuquan Space Centre
2025 Mar 17, 08:07 UTC
Yunyao-1 55
2025-055A
63291
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 17, 16:0569160.0012    52954695.3997.5929414:26
2025 Jun 4, 15:4969100.0014    52254195.2797.612814:29
2025 Jun 10, 11:4769180.0018    52855295.4597.6134714:29
Yunyao-1 56
2025-055B
63292
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 17:2969160.0012    52954695.3997.6028714:26
Yunyao-1 57
2025-055C
63293
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 17:2969160.0013    52954695.4097.6028714:26
Yunyao-1 58
2025-055D
63294
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 17:2969160.0013    52954795.4097.6028514:26
2025 Jun 4, 16:0369100.0014    52354295.2897.612614:28
2025 Jun 10, 05:4069190.0018    52855395.4697.6134314:29
Yunyao-1 59
2025-055E
63295
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 17:2969160.0012    52954795.4097.6028714:26
2025 May 31, 04:0369110.0012    52454195.2997.613914:28
2025 Jun 6, 00:0169190.0015    53055195.4597.6135314:28
Yunyao-1 60
2025-055F
63296
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 17:2969160.0012    53054695.4097.6028414:26
2025 May 21, 04:0369110.0014    52354295.2997.617214:28
2025 May 28, 14:1469190.0014    53155095.4697.611314:28
Zhongke 06 (Airsat 06)
2025-055G
63297
in space
Satellite for an Earth imaging constellation from AIRSAT Technology Group, China.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 17:3069160.0012    53054695.4097.6028414:26
Zhongke 07 (Airsat 07)
2025-055H
63298
in space
Satellite for an Earth imaging constellation from AIRSAT Technology Group, China.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 17:2969160.0011    53054695.4097.6028114:26
Ceres 1 fourth stage
uncatalogued
Re-entered - 2025 Mar 17
Life <1 day
Launched six Yunyao-1 satellites and two Zhongke. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-056
Electron (High Five)
Rocket Lab Launch Complex, New Zealand
2025 Mar 18, 01:31 UTC
Kinéis 4E (Kinéis 25)
2025-056A
63300
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 15:1370240.0002    64464797.6497.9710413:53
Kinéis 4C (Kinéis 23)
2025-056B
63301
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 11:5870240.0002    64464797.6497.9710613:53
Kinéis 4D (Kinéis 24)
2025-056C
63302
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 15:1370230.0001    64564697.6397.9715413:53
Kinéis 4A (Kinéis 21)
2025-056D
63303
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 15:1370230.0001    64464597.6197.9732513:53
Kinéis 4B (Kinéis 22)
2025-056E
63304
in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 18, 15:1270220.0002    64364597.6097.9728613:53
Electron second stage
2025-056F
63305
Re-entered - 2025 Apr 1
Life 14 days
Launched five Kinéis satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 18, 04:1067920.0334    18764192.8597.97230
Electron third stage (kick stage)
2025-056G
63306
in space
Launched five Kinéis satellites. Perigee lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 18, 04:2369920.0045    58264596.9797.9741


2025-057
Falcon 9 Block 5 (Starlink Group 12-025)
Cape Canaveral Space Force Station
2025 Mar 18, 19:57 UTC
Starlink 11568
2025-057A
63307
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 21:03 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 21, 20:0066660.0002    28728990.2843.01272
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 18
Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-058
Falcon 9 Block 5 (NRO L-57)
Vandenberg Space Force Base
2025 Mar 21, 06:49 UTC
USA 487 (Starshield 0097)
2025-058A
63333
in space
One of a simultaneously-launched group of eleven US government NRO imaging reconnaissance satellites. Design is related the SpaceX Starlink satellites and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications.

All satellites were launched to a similar altitude at about 70° inclination.
Orbit classified as 'Secret' - data withheld
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 21
Life <1 day
Launched eleven Starshield satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-059
Ceres 1 (Gushenxing 1 Y-17)
Jiuquan Space Centre
2025 Mar 21, 11:07 UTC
Yunyao-1 43
2025-059A
63344
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 21, 19:0869180.0011    53254795.4497.5930017:25
Yunyao-1 44
2025-059B
63345
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 21, 19:0069200.0009    53654895.4897.6032217:25
Yunyao-1 45
2025-059C
63346
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 21, 19:0069160.0013    52954695.3997.6028717:25
Yunyao-1 46
2025-059D
63347
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 21, 19:0069160.0012    52954695.4097.6029017:25
Yunyao-1 47
2025-059E
63348
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 21, 19:0869170.0012    53154795.4397.6031117:25
Yunyao-1 48
2025-059F
63349
in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 21, 19:0869160.0012    53054795.4197.6029417:25
Ceres 1 fourth stage
uncatalogued
Re-entered - 2025 Mar 21
Life <1 day
Launched six Yunyao-1 satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-060
Falcon 9 Block 5 (NRO L-69)
Cape Canaveral Space Force Station
2025 Mar 24, 17:48 UTC
USA 498 (NOSS 3-10?)
2025-060A
63350
in space
US government satellite from the National Reconnissance Office. Probably a NOSS ocean surveillance mission. Initial orbit is an estimate created from pre-launch data and published images/descriptions of the Falcon 9 upper stage venting propellant as it passed across Europe on its first orbit. Subsequent orbits are based on precise amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 24, 20:0074800.0015    10911113107.3064.00110
2025 Mar 27, 19:0374860.0128    10121204107.4463.45180
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 24
Life <1 day
Launched USA 498. Caused to re-enter above the southern Indian Ocean at about 20:50 UTC, after releasing the payload.
Not Catalogued - orbit parameters unavailable


2025-061
Electron (Finding Hot Wildfires Near You)
Rocket Lab Launch Complex, New Zealand
2025 Mar 26, 15:30 UTC
OroraTech Constellation Phase 1 001 (Lemur-2 )
2025-061A
63351
in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight built and operated by Spire and based on it's Lemur-2 bus. Equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 31, 12:2369180.0020    52655495.4597.5235403:51
OroraTech Constellation Phase 1 002 (Lemur-2 )
2025-061B
63352
in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 30, 14:0669180.0020    52655495.4497.5235703:52
OroraTech Constellation Phase 1 003 (Lemur-2 )
2025-061C
63353
in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 30, 17:1669170.0021    52555495.4397.5234903:52
OroraTech Constellation Phase 1 004 (Lemur-2 )
2025-061D
63354
in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 30, 17:1669170.0021    52555395.4297.5234803:52
OroraTech Constellation Phase 1 005 (Lemur-2 )
2025-061E
63355
in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 30, 20:2669170.0018    52655295.4297.5235303:51
2025 Mar 31, 21:5469170.0018    52655195.4297.5234903:51
OroraTech Constellation Phase 1 006 (Lemur-2 )
2025-061F
63356
in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
OroraTech Constellation Phase 1 007 (Lemur-2 )
2025-061G
63357
in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 30, 14:0369160.0020    52455195.3997.5134303:52
OroraTech Constellation Phase 1 008 (Lemur-2 )
2025-061H
63358
in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Mar 31, 12:2169170.0018    52655195.4197.5134903:51
Electron third stage (kick stage)
2025-061J
63359
in space
Launched eight OroraTech satellites. Perigee lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 26, 18:1168890.0048    47754494.8497.51301
2025 Mar 30, 16:3868870.0048    47554294.8097.51283
Electron second stage
2025-061K
63360
Re-entered - 2025 Apr 4
Life 9 days
Launched eight OroraTech satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 26, 18:0967320.0255    18252591.6197.50226


2025-062
CZ 3B
Xichang Space Centre
2025 Mar 26, 15:55 UTC
Tianlian 2-04
2022-062A
63361
in space
Second Generation data communications satellite to provide a data relay, and measurement and control service for Chinese satellites and space stations. Probably moved to geosynchronous drift orbit March 27 at around 08:15 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Mar 26, 19:07243940.7308    19035841631.9427.11179
2025 Apr 4, 14:59421600.0032    35649359161435.875.5035980°.0 E
CZ 3B fourth stage
2025-062B
63362
in space
Launched Tianlian 2-04.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 26, 19:14237930.7248    16934661608.7627.08179


2025-063
Falcon 9 Block 5 (Starlink Group 11-007)
Vandenberg Space Force Base
2025 Mar 26, 22:11 UTC
Starlink 32840
2025-063A
63363
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 23:13 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 2, 16:0066860.0001    30830990.6853.1648
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 26
Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-064
CZ 7A (Y-11)
Wenchang Space Centre
2025 Mar 29, 16:05 UTC
Tongxin Jishu Shiyan 16 (Communication Technology Test 16, TJS 16)
2025-064A
63397
in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT). Probably entered geosynchronous drift orbit Mar 30 at around 08:30 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Mar 29, 23:01243920.7318    16435864631.8919.52180
2025 Apr 7, 17:16421650.0001    35783357901436.090.06106152°.5 E
CZ 7A fourth stage
2025-064B
63398
Re-entered - 2025 Jul 28
Life 121 days
Launched TJS 16.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Mar 30, 17:45236210.7252    11334372602.1419.52179
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 17
Life 233 days
Launched Sentinel 6B. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-F02 - failed to reach orbit
Spectrum (Going Full Spectrum)
Andøya Spaceport
2025 Mar 30, 10:30 UTC


2025-065
Falcon 9 Block 5 (Starlink Group 06-080)
Cape Canaveral Space Force Station
2025 Mar 31, 19:52 UTC
Starlink 33531
2025-065A
63399
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 20:57 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 8, 20:0066690.0002    28929290.3243.00275
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Mar 31
Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-066
Falcon 9 Block 5
Kennedy Space Center
2025 Apr 1, 01:46 UTC
SpaceX Fram2 (Dragon Resilience flight #4)
2025-066A
63427
Re-entered - 2025 Apr 4
Life 3 days Returned to Earth
Science mission to polar orbit, the highest orbital inclination flown by a piloted vehicle since Soyuz 22 (1976-093A). Crew consists of Mission Commander Chun Wang, Vehicle Commander Jannicke Mikkelsen, Vehicle Pilot Rabea Rogge, and Mission Specialist and Medical Officer Eric Philips. Separated from launch vehicle at 01:56 UTC. Sixteen minutes of retro-fire, commencing April 4 at 15:26 UTC was followed by separation of the Trunk module at 15:43 UTC. Dragon splashed down in the Pacific Ocean near the coast of southern California at 16:19 UTC. Mission duration was determined by the crew's total radiation dose on orbit. Previous re-entries - the Trunk module was discarded BEFORE retro-fire and remained in orbit.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Apr 1, 03:1566850.0158    20241390.6790.019220:35
2025 Apr 1, 12:0068080.0004    42743293.1690.007620:33
2025 Apr 4, 09:5467850.0038    38143392.7090.018020:22
2025 Apr 4, 14:4667740.0055    35943492.4989.638220:20
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 1
Life <1 day
Launched SpaceX Dragon Fram 2 mission. Caused to re-enter above the Indian Ocean at about 02:40 UTC, after releasing the spacecraft.
Not Catalogued - orbit parameters unavailable


2025-067
CZ 2D (Y-78)
Jiuquan Space Centre
2025 Apr 1, 04:00 UTC
Hulianwang Jishu Shiyan 6-01 (Internet New Technology Test Satellite 6-01)
2025-067A
63428
Re-entered - 2025 Oct 16
Life 198 days
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle. Individual satellites act as test/demonstrator platforms for specific components of the system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 1, 15:0268310.0008    44745893.6455.00282
Hulianwang Jishu Shiyan 6-02 (Internet New Technology Test Satellite 6-02)
2025-067B
63429
in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle. Individual satellites act as test/demonstrator platforms for specific components of the system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 1, 14:5968280.0010    44345693.5855.00301
Hulianwang Jishu Shiyan 6-03 (Internet New Technology Test Satellite 6-03)
2025-067C
63430
in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle. Individual satellites act as test/demonstrator platforms for specific components of the system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 1, 15:0068290.0009    44545793.6054.99299
Hulianwang Jishu Shiyan 6-04 (Internet New Technology Test Satellite 6-04)
2025-067D
63431
in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle. Individual satellites act as test/demonstrator platforms for specific components of the system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 1, 14:5968300.0008    44645793.6255.00285
CZ 2D second stage
uncatalogued
Re-entered - 2025 Apr 1
Life <1 day
Launched cluster of four Hongtu 3 internet connectivity satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-068
CZ 6 (Y-14)
Taiyuan Space Centre
2025 Apr 3, 02:12 UTC
Tianping 3A-02
2025-068A
63432
in space
Reportedly for space environment studies in LEO and acting as calibration targets for ground-based visual and radar tracking equipment. May also be equipped with an Earth imaging system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 4, 13:2170010.0244    45279497.1743.01111
CZ 6 third stage
uncatalogued
in space
Launched Tianping 3A-02. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-069
Falcon 9 Block 5 (Starlink Group 11-013)
Vandenberg Space Force Base
2025 Apr 3, 13:02 UTC
Starlink 33682
2025-069A
63433
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 14:02 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 9, 20:0066670.0000    28928990.3053.1547
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 3
Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-070
Falcon 9 Block 5 (Starlink Group 06-072)
Cape Canaveral Space Force Station
2025 Apr 6, 03:07 UTC
Starlink 33679
2025-070A
63460
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:12 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 11, 16:0066720.0001    29329590.4043.00233
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 6
Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-071
Falcon 9 Block 5 (Starlink Group 11-011)
Vandenberg Space Force Base
2025 Apr 7, 23:06 UTC
Starlink 33828
2025-071A
63493
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle April 8 at 00:05 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 11, 18:0066690.0001    29029190.3253.1653
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 8
Life 1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-072
Soyuz-2.1a
Baikonur Cosmodrome
2025 Apr 8, 05:47 UTC
Soyuz MS-27 (Soyuz 11F732A48 № 758)
2025-072A
63520
Re-entered - 2025 Dec 9
Life 245 days
Crew to ISS - Sergei Ryzhikov and Alexei Zubritsky (both Roscosmos) and Jonathan Kim (NASA) . Separated from launch vehicle at 05:56 UTC. Docked with ISS Prichal module at 08:57:43 UTC. Initial orbit similar to launch vehicle upper stage.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 8, 11:4267970.0005    41542292.9451.6422
Soyuz third stage
2025-072B
63521
Re-entered - 2025 Apr 10
Life 2 days
Launched Soyuz MS-27.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 8, 14:2865940.0028    19723488.8151.6678


2025-073
CZ 3B
Xichang Space Centre
2025 Apr 10, 16:47 UTC
Tongxin Jishu Shiyan 17 (Communication Technology Test 17, TJS 17)
2025-073A
63524
in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT). Probably entered geosynchronous drift orbit April 12 at around 15:15 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Apr 10, 21:00245280.7325    18436116637.1718.99180
2025 Apr 21, 16:55421650.0001    35783357901436.090.04119152°.8 E
CZ 3B fourth stage
2025-073B
63525
in space
Launched TJS 17.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 10, 19:44248550.7374    14936804649.9519.02180
apogee motor (CZ 3B fifth stage)
2025-073C
63629
in space
Moved TJS 17 from transfer orbit to geosynchronous drift orbit and (possibly) to its GEO location, then manoeuvred itself to graveyard orbit after releasing the satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 22, 01:53425650.0010    36142362311456.580.04208


2025-074
Falcon 9 Block 5 (NRO L-192)
Vandenberg Space Force Base
2025 Apr 12, 12:25 UTC
USA 499 (Starshield 0108)
2025-074A
63526
in space
One of a simultaneously-launched group of twenty two US government NRO intelligence gathering (probably imaging) satellites. Design is related the SpaceX Starlink satellites and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
estimated orbit66780.0010    29330690.5169.90155
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 12
Life <1 day
Launched twenty two Starshield satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-075
Falcon 9 Block 5 (Starlink Group 12-017)
Kennedy Space Center
2025 Apr 13, 00:53 UTC
Starlink 11669
2025-075A
63548
in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 01:58 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 18, 16:0066760.0002    29729990.4843.01248
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 13
Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-076
Falcon 9 Block 5 (Starlink Group 06-073)
Cape Canaveral Space Force Station
2025 Apr 14, 04:00 UTC
Starlink 32959
2025-076A
63569
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:05 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 22, 18:0066920.0002    31231590.8043.00264
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 14
Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-077
Minotaur IV (NRO L-174)
Vandenberg Space Force Base
2025 Apr 16, 19:33 UTC
USA 521 (NOSS?)
2025-077A
63596
in space
US government satellite, either for intelligence gathering or testing of sensors/equipment for future missions. Orbit information from amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 21, 04:3474920.0018    11001127107.5663.39246
USA 522 (NOSS?)
2025-077B
63597
in space
US government satellite, either for intelligence gathering or testing of sensors/equipment for future missions. Orbit information from amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 13, 04:4474900.0020    10971127107.5263.39292
Minotaur fourth stage
2025-077C
63598
in space
Launched two US government satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )


2025-078
CZ 6A (Y-11)
Taiyuan Space Centre
2025 Apr 18, 22:51 UTC
Shiyan 27-01 (Test 27-01)
2025-078A
63599
in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Apr 19, 09:1273830.0006    10001009105.2199.6922906:00
Shiyan 27-02 (Test 27-02)
2025-078B
63600
in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Apr 19, 09:1273830.0006    10001009105.2299.6922206:00
Shiyan 27-03 (Test 27-03)
2025-078C
63601
in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Apr 19, 09:1273830.0007    10001011105.2399.6922906:00
Shiyan 27-04 (Test 27-04)
2025-078D
63602
in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Apr 19, 09:1373840.0008    10001011105.2499.7021506:00
Shiyan 27-05 (Test 27-05)
2025-078E
63603
in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Apr 19, 09:1373850.0009    10001013105.2699.6922706:00
Shiyan 27-06 (Test 27-06)
2025-078F
63604
in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Apr 19, 09:1373850.0009    10001013105.2699.7022506:00
CZ 6A third stage
2025-078G
63605
in space
Launched Shiyan 27 group. Orbit lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 19, 09:1472900.0107    834990103.2599.70108


2025-079
Falcon 9 Block 5 (NRO L-145)
Vandenberg Space Force Base
2025 Apr 20, 12:29 UTC
USA 523 (Starshield 0130)
2025-079A
63606
in space
One of a simultaneously-launched group of twenty two US government NRO intelligence gathering (probably imaging) satellites. Design is related the SpaceX Starlink satellites and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications.
Orbit classified as 'Secret' - data withheld
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 20
Life <1 day
Launched twenty two Starshield satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-080
Falcon 9 Block 5
Kennedy Space Center
2025 Apr 21, 08:15 UTC
SpaceX Dragon 2 CRS-32
2024-080A
63628
Re-entered - 2025 May 25
Life 34 days Returned to Earth
Carrying cargo to/from the ISS under NASA's Commercial Resupply Services (CRS) contract. Docked with the forward-facing port of the ISS Harmony Module April 22 at 12:40 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 21, 11:3566710.0115    21637090.3851.65225
2025 Apr 22, 14:4067950.0005    41342192.9151.6464
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 21
Life <1 day
Launched SpaceX Dragon 2 CRS-32. Caused to re-enter after releasing the spacecraft.
Not Catalogued - orbit parameters unavailable


2025-081
Falcon 9 Block 5 (Bandwagon 3)
Cape Canaveral Space Force Station
2025 Apr 22, 00:48 UTC
Korea 425-04
2025-081A
63630
in space
Radar imaging satellite owned by the South Korean government specifically targetting activity across the Korean peninsula.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 22, 21:0869550.0005    57358096.2045.40172
Tomorrow S7 (Tomorrow Microwave Sounder 7)
2025-081B
63631
in space
6U Cubesat from US company Tomorrow.io, designed to measure temperature and humidity profiles within the Earth's atmosphere. Catalogue Number, Designation and orbit to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 22, 09:5569550.0007    57258196.2145.41196
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 22
Life <1 day
Launched Korea 425-04 & Tomorrow S7. Caused to re-enter after releasing the satellites. Following retro-fire, Atmos Space's Phoenix 1 prototype re-entry vehicle equipped with an inflatable heat shield, separated and conducted a successful mission including splashdown about 2.5 hrs after lift-off.
Not Catalogued - orbit parameters unavailable


2025-082
CZ 2F
Jiuquan Space Centre
2025 Apr 24, 09:17 UTC
Shenzhou 20
2025-082A
63632
Re-entered - 2026 Jan 19
Life 270 days
Crew to CSS - Chen Dong (commander), Chen Zhongrui (pilot) and and Wang Jie (flight engineer). Separated from launch vehicle at 09:27 UTC. Docked with the downward-facing port of the Tianhe module at 15:49 UTC on the day of launch. Preparations for return to Earth 2025 November uncovered damage to a porthole caused by orbiting debris, making it unsafe for crew use. The crew then used the newly-arrived Shenzhou 21 for return to Earth. Undocked without crew 2026 January 18 at 16:23 UTC. Retro-fire January 19 at around 00:45 UTC led to the descent module landing at 01:34 UTC in the Dongfangheng landing zone near Jiuquan. Initial orbit listed is based on Chinese data.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 24, 09:2066500.0119    19335289.9641.46125
2025 Apr 24, 16:3267610.0002    38138492.2141.46223
2026 Jan 17, 18:1367640.0011    37839392.2741.47305
CZ 2F third stage
2025-082B
63633
Re-entered - 2025 May 3
Life 9 days
Launched Shenzhou 20.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 24, 19:3766460.0113    19334389.8641.46127
Shenzhou 20 Orbital Module
2025-082C
67481
in space
Released from Shenzhou 20 on 2026 January 19 at around 00:45 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2026 Jan 26, 14:0367610.0007    37838792.2041.4817


2025-083
Falcon 9 Block 5 (Starlink Group 06-074)
Cape Canaveral Space Force Station
2025 Apr 25, 01:52 UTC
Starlink 33879
2025-083A
63634
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:57 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 5, 18:0066900.0002    31031390.7543.00265
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 25
Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-084
CZ 3B
Xichang Space Centre
2025 Apr 27, 15:54 UTC
Tianlian 2-05
2022-084A
63662
in space
Second Generation data communications satellite to provide a data relay, and measurement and control service for Chinese satellites and space stations. Probably moved to geosynchronous drift orbit April 28 at around 08:15 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Apr 27, 20:43243850.7304    19635818631.6227.15180
2025 May 12, 13:55421650.0002    35778357961436.125.4715120°.4 E
CZ 3B fourth stage
2025-084B
63663
in space
Launched Tianlian 2-05.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Apr 27, 20:08237780.7244    17534625608.1827.09179


2025-085
Falcon 9 Block 5 (Starlink Group 12-023)
Cape Canaveral Space Force Station
2025 Apr 28, 02:09 UTC
Starlink 11651
2025-085A
63664
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:14 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 5, 18:0066910.0002    31231490.7943.01258
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 28
Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-086
CZ 5B + YZ-2
Wenchang Space Centre - Hainan Commercial Zone
2025 Apr 28, 20:10 UTC
Hulianwang Digui 03-01 (Satellite Low Orbit Internet Group 03-01)
2025-086A
63687
in space
One of ten simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 3, 12:1474850.0012    10991116107.4286.50295
YZ-2 rocket stage
uncatalogued
Re-entered - 2025 Apr 28
Life <1 day
Launched ten internet comsats. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-087
Falcon 9 Block 5 (Starlink Group 11-009)
Vandenberg Space Force Base
2025 Apr 28, 20:42 UTC
Starlink 33894
2025-087A
63697
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 21:41 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 5, 12:3866630.0000    28528690.2253.169
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 28
Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-088
Atlas V 551 (KA-01, Kuiper Atlas 1)
Cape Canaveral Space Force Station
2025 Apr 28, 23:01 UTC
Kuiper 00008
2025-088A
63724
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from US company Amazon.

All satellites expected to be injected initially into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 5, 20:0068410.0011    45647093.8651.86139
2026 Jan 1, 18:4069490.0008    56557696.0851.89237
Atlas V third stage (Centaur)
uncatalogued
Re-entered - 2025 Apr 28
Life <1 day
Launched twenty seven Kuiper satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-089
Falcon 9 Block 5 (Starlink Group 12-010)
Kennedy Space Center
2025 Apr 29, 02:34 UTC
Starlink 11677
2025-089A
63751
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:39 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 5, 20:0066860.0002    30730990.6843.01256
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Apr 29
Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-090
Vega-C (VV-26)
Centre Spatiale Guyanaise
2025 Apr 29, 08:15 UTC
Biomass
2025-090A
63772
in space
Earth Explorer mission from the European Space Agency. Carries a radar imaging system capable of penetrating forest canopy to measure the height and mass of its undergrowth in order to to estimate its carbon content. The radar can also be used for mapping the geology of many kinds of ground type. Separated from launch vehicle at 09:13 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 1, 20:1070450.0001    66666898.0998.076418:00
2025 May 10, 03:4370420.0001    66366598.0298.078818:00
Vega upper stage (Avum+)
uncatalogued
Re-entered - 2025 Apr 29
Life <1 day
Launched Biomass. Caused to re-enter after releasing the satellite.
Not Catalogued - orbit parameters unavailable


2025-F03 - failed to reach orbit
Firefly Alpha Block 1 (FLTA006, Message In A Booster)
Vandenberg Space Force Base
2025 Apr 29, 13:37 UTC
Firefly Alpha second stage
Failed orbital launch carring a Lockheed Martin LM400 satellite on a demonstrator mission. Reportedly reached 320 km altitude but failed to attain orbital velocity. Rocket and satellite re-entered and and surviving debris hit the ocean surface near Antarctica.


2025-091
Falcon 9 Block 5 (Starlink Group 06-075)
Cape Canaveral Space Force Station
2025 May 2, 01:51 UTC
Starlink 33932
2025-091A
63775
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:56 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 5, 20:0066640.0002    28528790.2443.00208
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 2
Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-092
Falcon 9 Block 5 (Starlink Group 06-084)
Kennedy Space Center
2025 May 4, 08:54 UTC
Starlink 33909
2025-092A
63804
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 09:59 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 7, 18:0066610.0002    28228490.1743.00253
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 4
Life <1 day
Launched twenty nine Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-093
Falcon 9 Block 5 (Starlink Group 06-093)
Cape Canaveral Space Force Station
2025 May 7, 01:17 UTC
Starlink 34018
2025-093A
63836
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:22 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 12, 18:0066840.0002    30430790.6343.00270
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 7
Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-094
Falcon 9 Block 5 (Starlink Group 15-003)
Vandenberg Space Force Base
2025 May 10, 00:19 UTC
Starlink 33863
2024-094A
63864
in space
One member of a simultaneously-launched cluster of twenty six broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 01:21 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 15, 16:0066710.0004    29029690.3870.00274
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 10
Life <1 day
Launched twenty six Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-095
Falcon 9 Block 5 (Starlink Group 06-091)
Cape Canaveral Space Force Station
2025 May 10, 06:28 UTC
Starlink 34116
2025-095A
63890
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 07:33 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 15, 16:0066670.0001    28828990.2943.00253
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 10
Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-096
CZ 6A (Y-9)
Taiyuan Space Centre
2025 May 11, 13:27 UTC
Yaogan 40-02 Leader
2025-096A
63918
in space
Described as a remote sensing satellite monitoring the electromagnetic environment - a description that indicates it has an electronic intelligence gathering rôle. One of three related satellites carried on the same launch to operate in a triangular formation separated from each other by about 120 km - a similar formation to the lower inclination Yaogan 31 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 12, 14:3371810.0011    795811100.9486.00262
2025 May 19, 21:1771910.0004    810816101.1586.00153
2025 May 21, 08:4872150.0007    832842101.6586.00325
2025 May 23, 20:1472300.0002    850853101.9686.0094
Yaogan 40-02 Follower
2025-096B
63919
in space
Described as a remote sensing satellite monitoring the electromagnetic environment - a description that indicates it has an electronic intelligence gathering rôle. One of three related satellites carried on the same launch to operate in a triangular formation separated from each other by about 120 km - a similar formation to the lower inclination Yaogan 31 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 12, 14:3271810.0011    795811100.9386.00264
2025 May 19, 23:0271960.0008    812824101.2685.99185
2025 May 23, 21:5772240.0007    841851101.8486.00358
2025 May 28, 20:5872300.0002    850853101.9685.9982
Yaogan 40-02 Outlier
2025-096C
63920
in space
Described as a remote sensing satellite monitoring the electromagnetic environment - a description that indicates it has an electronic intelligence gathering rôle. One of three related satellites carried on the same launch to operate in a triangular formation separated from each other by about 120 km - a similar formation to the lower inclination Yaogan 31 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 12, 15:5071800.0011    794810100.9286.00269
2025 May 18, 13:2471650.0014    777797100.6186.00269
2025 Jul 8, 20:3271670.0019    776802100.6485.9994
2025 Jul 9, 20:3771840.0020    791820101.0086.0074
2025 Jul 14, 13:3072270.0003    847851101.9186.00171
2025 Jul 15, 04:4872290.0002    850853101.9586.0095
2025 Jul 15, 20:0672290.0002    850853101.9686.0090
CZ 6A third stage
2025-096E
63922
in space
Launched Yaogan 40 Group 2. Orbit lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 12, 15:1170590.0072    63173298.3886.0266


2025-097
CZ 3C
Xichang Space Centre
2025 May 12, 18:09 UTC
Tongxin Jishu Shiyan 19 (Communication Technology Test 19, TJS 19)
2025-097A
63924
in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT). Probably entered geosynchronous drift orbit May 13 at around 10:25 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 May 12, 21:24243820.7311    17835830631.4928.58180
2026 Jan 9, 00:11421640.0003    35771358001436.063.56316141°.2 E
CZ 3C third stage
2025-097B
63925
Re-entered - 2025 Sep 7
Life 118 days
Launched TJS 19.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 12, 21:31243040.7328    11735734628.4428.60179
TJS-19 AKM
2025-097C
64094
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )


2025-098
Falcon 9 Block 5 (Starlink Group 15-004)
Vandenberg Space Force Base
2025 May 13, 01:15 UTC
Starlink 34012
2025-098A
63926
in space
One member of a simultaneously-launched cluster of twenty six broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:16 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 16, 18:0066640.0004    28328890.2370.00267
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 13
Life <1 day
Launched twenty six Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-099
Falcon 9 Block 5 (Starlink Group 06-083)
Kennedy Space Center
2025 May 13, 05:02 UTC
Starlink 34159
2025-099A
63952
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:07 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 16, 18:0066590.0001    28028290.1343.00243
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 13
Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-100
CZ 2D
Jiuquan Space Centre
2025 May 14, 04:12 UTC
Taikong Jisu
2025-100A
63982
in space
One of a cluster of twelve satellites from ADA Space of China. The group consists of several differing satellite designs and it is unclear whether they all have the same purpose, described as offering a computing service to other satellites in order to avoid bottlenecks caused by having to transmit data via ground stations before analysis.

All satellites were injected initially into similar orbits

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 14, 21:1468760.0010    49150594.5797.4126110:30
CZ 2D second stage
uncatalogued
Re-entered - 2025 May 14
Life <1 day
Launched Taikong Jisu cluster of twelve satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-101
Falcon 9 Block 5 (Starlink Group 06-067)
Cape Canaveral Space Force Station
2025 May 14, 16:38 UTC
Starlink 33871
2025-101A
63994
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 17:43 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 15, 21:4067200.0009    33634991.3843.00296
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 14
Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-102
Falcon 9 Block 5 (Starlink Group 15-005)
Vandenberg Space Force Base
2025 May 16, 13:43 UTC
Starlink 34051
2025-102A
64022
in space
One member of a simultaneously-launched cluster of twenty six broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 14:45 UTC.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 22, 22:0066760.0004    29530090.4769.99272
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 16
Life <1 day
Launched twenty six Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-103
Zhuque-2E (Y2)
Jiuquan Space Centre - Dongfeng Commercial Zone
2025 May 17, 04:12 UTC
Tianyi 29
2025-103A
64048
in space
Earth observation satellite equipped with optical imaging system for geological studies. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 17, 14:4669010.0006    51952795.0897.4113010:30
Tianyi 34
2025-103B
64049
in space
Small satellite from China's Southern University of Science and Technology equipped with an Earth studies and astronomy payloads. Carries instruments to study electric fields on orbit, aurorae, gamma ray bursts and polarisation of x-ray emissions from celestial objects. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 17, 14:4668990.0004    51952495.0697.4111410:30
Tianyi 35
2025-103C
64050
in space
Earth observation satellite equipped with a multi-spectral optical imaging system. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 17, 14:4668990.0004    51852495.0697.4210010:30
Tianyi 42
2025-103D
64051
in space
Earth observation satellite equipped with an imaging radar. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 17, 14:4668990.0005    51852495.0597.429910:30
Tianyi 45
2025-103E
64052
in space
Small satellite as an on-orbit demonstrator for a computer system to support other satellites. Also equipped with an inter-satellite laser communication system. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 17, 14:4668990.0005    51852595.0697.4211010:30
Tianyi 46
2025-103F
64053
in space
Small satellite as an on-orbit demonstrator for a computer system to support other satellites. Also equipped with an inter-satellite laser communication system. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 17, 14:4668990.0005    51852495.0597.4210510:30
Zhuque 2 second stage
2025-103G
64054
Re-entered - 2025 Jun 5
Life 19 days
Launched group of Tianqui satellites. Orbit lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 17, 14:4667670.0317    17560392.3396.1289


2025-104
Electron (The Sea God Sees)
Rocket Lab Launch Complex, New Zealand
2025 May 17, 08:17 UTC
QPS-SAR 10 (Wadatsumi-I)
2025-104A
64055
in space
Commercial satellite from Japanese company iQPS, equipped with an Earth imaging radar. One in a constellation that will ultimately consist of 36 satellites. Separated from launch vehicle at 09:07 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 18, 16:5169540.0010    56958396.1942.01282
Electron second stage
2025-104B
64056
Re-entered - 2025 Jun 26
Life 40 days
Launched QPS-SAR 10 satellite. Catalogue Number, Designation and orbit to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 18, 17:5667970.0279    22960892.9541.95255
Electron third stage (kick stage)
2025-104C
64057
Re-entered - 2025 Sep 20
Life 126 days
Launched QPS-SAR 10 satellite. Perigee lowered after releasing satellite. Catalogue Number, Designation and orbit to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 18, 18:0668180.0209    29758293.3742.01279


2025-F04 - failed to reach orbit
PSLV-XL (PSLV C-61)
Satish Dhawan Space Centre
2025 May 18, 00:29 UTC
EOS-9 (Earth Observation Satellite 9)
Indian remote sensing satellite equipped with an imaging radar. Repeat of the ES-04 mission (51656, 2022-013A). Lost when the launch vehicle third stage failed to operate.


2025-105
Ceres 1S (Gushenxing 1S Y-5)
Jiuquan Space Centre
2025 May 19, 07:38 UTC
Tianqi 16
2025-105A
64058
in space
Small satellite providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 19, 20:4072230.0012    836853101.8244.99308
2025 May 27, 16:5272240.0011    837854101.8344.98347
2025 May 30, 16:0672260.0012    839856101.8844.9815
2025 Jun 1, 12:1272260.0012    839856101.8844.9824
2025 Jun 11, 13:2672280.0012    842859101.9344.9870
2025 Jun 12, 15:0372340.0012    847864102.0544.9882
Tianqi 17
2025-105B
64059
in space
Small satellite providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 19, 20:4072230.0012    836853101.8144.98310
2025 May 29, 14:3872240.0012    838855101.8544.988
2025 Jun 11, 06:1172260.0011    840856101.8944.9870
2025 Jun 12, 15:1272290.0013    841860101.9445.0196
2025 Jun 17, 18:2672420.0022    848880102.2344.97114
2025 Jun 18, 01:1572440.0010    859873102.2644.9893
2025 Jun 18, 11:2872440.0011    858874102.2644.98105
2025 Jun 24, 00:3972680.0009    884897102.7844.98139
2025 Jun 26, 19:2972750.0009    891904102.9344.98154
Tianqi 18
2025-105C
64060
in space
Small satellite providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 20, 10:1472220.0012    835853101.8044.99315
2025 May 28, 21:3972240.0011    838854101.8544.9910
2025 May 29, 18:0172250.0012    839856101.8744.9921
2025 Jun 11, 13:4072280.0012    841858101.9244.9885
2025 Jun 12, 13:3272320.0012    846863102.0244.9890
2025 Jun 17, 10:1472420.0011    856872102.2344.98115
2025 Jun 18, 11:5672560.0011    870887102.5344.98119
2025 Jun 19, 20:2572670.0010    882896102.7544.98128
2025 Jun 22, 16:5672750.0009    891903102.9344.98145
Tianqi 20
2025-105D
64061
in space
Small satellite providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 20, 11:5672220.0013    835853101.8044.99312
2025 May 28, 04:4272240.0015    835856101.8344.981
2025 May 29, 04:2672240.0013    837856101.8544.9813
2025 May 29, 14:3772250.0012    838855101.8644.9915
2025 Jun 12, 15:1372320.0011    845861102.0044.9885
2025 Jun 19, 13:1472540.0009    869883102.4844.98120
2025 Jun 22, 13:0572750.0008    892903102.9344.98138
Ceres 1S fourth stage
uncatalogued
in space
Launched four Tianqi satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-106
CZ 7A
Wenchang Space Centre
2025 May 20, 11:50 UTC
Zhongxing 3B (Chinasat 3B)
2025-106A
64062
in space
Communication and broadcasting satellite providing voice, data, radio and television transmission services to the Chinese mainland and nearby territories.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 May 20, 17:12243780.7299    20735792631.3215.49180
2025 May 30, 17:13421650.0002    35780357941436.120.01360167°.3 E
CZ 7A fourth stage
2025-106B
64063
in space
Launched Zhongxing 3B.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 20, 17:27236060.7237    14534311601.5915.49179
2025 May 20, 17:27236060.7237    14534311601.5915.49179


2025-107
Falcon 9 Block 5 (Starlink Group 12-015)
Cape Canaveral Space Force Station
2025 May 21, 03:19 UTC
Starlink 11741
2025-107A
64064
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 28, 18:0066870.0002    30831090.7043.01262
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 21
Life <1 day
Launched Starlink Group 12-015. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-108
Lijian 1, Kinetica 1 (Y-7)
Jiuquan Space Centre - Dongfeng Commercial Zone
2025 May 21, 04:05 UTC
Tada Huyang 1
2025-108xx
in space
12U Cubesat - equipped for atmospheric and meteorological studies through observation of occultations of navigation satellites. Developed jointly by Xidian University, Tarim University and Beijing Future Aerospace Science and Technology Research Institute Co. First of an intended 108 satellite constellation.
Orbit parameters awaited
Taijing 3-04
2025-108xx
in space
Commercial satellite for high-resolution remote sensing using an optical imaging system. Catalogue Number and Designation to be confirmed.
Orbit parameters awaited
Taijing 4-02
2025-108xx
in space
Commercial remote sensing satellite using radar imaging. Catalogue Number and Designation to be confirmed.
Orbit parameters awaited
Xiguang 1-02
2025-108xx
in space
Multispectral Earth imaging satellite from private company XIOPM Space (Xi'an Institute of Optics and Precision Mechanics), with an emphasis on monitoring methane emissions. Equipped with an onboard data processing system. Precise orbit to be confirmed.
Orbit parameters awaited
Xingjiyuan 1
2025-108xx
in space
Earth observation satellite equipped with a multispectral camera to provide medium to high-resolution images.
Orbit parameters awaited
Zhuhai 01 (Xingrui 11)
2025-108xx
in space
High-resolution multi-spectral, satellite jointly developed by the Micro-Nano Spacecraft Innovation Centre of the Beijing Institute of Technology and Setret Space Technology Co., Ltd.
Orbit parameters awaited
ZK-1A rocket stage
2025-108G
64093
in space
Launched group of six satellites.
Orbit parameters awaited


2025-109
Soyuz-2.1b + Fregat
Plesetsk Cosmodrome
2025 May 23, 08:36 UTC
Cosmos 2588
2025-109A
64095
in space
Orbit height maintained by occasional use of thruster.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 23, 14:3668510.0012    46448194.0572.97238
2025 May 31, 13:5568520.0012    46648294.0872.97235
2025 Jul 9, 21:5968520.0008    46847994.0772.97174
2025 Jul 10, 16:4868530.0006    47147994.1072.97182
2025 Sep 6, 17:3668520.0002    47247594.0872.975
2025 Sep 7, 17:0868540.0003    47447894.1372.97272
2025 Nov 7, 17:1468510.0001    47247394.0572.97184
2025 Nov 8, 16:4568540.0005    47247994.1272.97238
Fregat rocket stage
uncatalogued
in space
Launched Cosmos 2588. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-110
Falcon 9 Block 5 (Starlink Group 11-016)
Vandenberg Space Force Base
2025 May 23, 22:32 UTC
Starlink 34178
2025-110A
64096
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 30, 19:1466830.0001    30530690.6353.1633
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 23
Life <1 day
Launched Starlink Group 11-016. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-111
Falcon 9 Block 5 (Starlink Group 12-022)
Cape Canaveral Space Force Station
2025 May 24, 17:19 UTC
Starlink 11727
2025-111A
64123
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 2, 20:0066990.0002    32032290.9443.00285
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 24
Life <1 day
Launched Starlink Group 12-022. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-112
Falcon 9 Block 5 (Starlink Group 17-001)
Vandenberg Space Force Base
2025 May 27, 16:57 UTC
Starlink 34314
2025-112A
64146
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 28, 17:1166500.0010    26527989.9597.60248
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 27
Life <1 day
Launched Starlink Group 17-001. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-113
Falcon 9 Block 5 (Starlink Group 10-032)
Kennedy Space Center
2025 May 28, 13:30 UTC
Starlink 34177
2025-113A
64170
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 3, 14:0066670.0000    28828990.2953.1627
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 28
Life <1 day
Launched Starlink Group 10-032. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-114
CZ 3B/G2
Xichang Space Centre
2025 May 28, 17:31 UTC
Tianwen 2
2025-114A
64197
in space
Comet sample collection and return to Earth mission aimed at near-Earth asteroid 2016HO3. It will then approach comet 311P.
Heliocentric orbit
CZ 3B fourth stage
2025-114B
64198
Re-entered - 2025 May 28
Life <1 day
Launched Tianwen 2.
Heliocentric orbit


2025-115
CZ 4B
Jiuquan Space Centre
2025 May 29, 04:12 UTC
Shijian 26 (Practice 26)
2025-115A
64199
in space
Mission not revealed but probably a military/government optical Earth observation mission.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 29, 15:2168750.0009    49050394.5597.4927110:30
2025 Jun 11, 18:0468780.0008    49450594.6097.4919010:31
2025 Dec 31, 15:4168700.0009    48549894.4497.4721310:39
CZ 4B third stage
2025-115C
64201
Re-entered - 2025 Oct 6
Life 130 days
Launched Shijian 26. Perigee lowered after releasing satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 30, 16:3667600.0158    27548992.1997.4312
debris item
2025-115B
64200
in space
Appeared in orbit at launch - may be an payload cover from the satellite. Its radar cross section suggests it may be 0.5m or more in size. Taken together with its low rate of orbital decay, it appears to be a relatively dense item.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 May 29, 13:4569130.0061    49357895.3597.5219410:30
2025 Dec 30, 10:3768600.0042    45351194.2497.5017010:35


2025-116
Falcon 9 Block 5
Cape Canaveral Space Force Station
2025 May 30, 17:37 UTC
USA 545 (GPS IIIA SV08)
2025-116A
64202
in space
Block 3 GPS Navsat. Separated from launch vehicle at 19:06 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 May 31, 01:05166830.5944    38820222357.4255.01270
2025 Jun 9, 23:50265600.0002    2017720186717.9554.96292


2025-117
Falcon 9 Block 5 (Starlink Group 11-018)
Vandenberg Space Force Base
2025 May 31, 20:10 UTC
Starlink 33966
2025-117A
64203
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 5, 16:0066600.0001    28128290.1553.1653
Falcon 9 second stage
uncatalogued
Re-entered - 2025 May 31
Life <1 day
Launched Starlink Group 11-018. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-118
Electron (Full Stream Ahead)
Rocket Lab Launch Complex, New Zealand
2025 Jun 2, 23:57 UTC
Global 32
2025-118B
64231
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 4, 12:3768500.0010    46547894.0359.00308
Electron third stage (kick stage)
2025-118A
64230
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 4, 12:3868520.0008    46847994.0758.99318
Electron second stage
2025-118C
64232
Re-entered - 2025 Jun 12
Life 10 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 4, 03:5667080.0232    17448591.1358.99267


2025-119
Falcon 9 Block 5 (Starlink Group 12-019)
Cape Canaveral Space Force Station
2025 Jun 3, 04:43 UTC
Starlink 11686
2025-119A
64233
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 9, 18:0066830.0002    30330690.6143.01255
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 3
Life <1 day
Launched Starlink Group 12-019. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-120
Falcon 9 Block 5 (Starlink Group 11-022)
Vandenberg Space Force Base
2025 Jun 4, 23:40 UTC
Starlink 34329
2025-120A
64256
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 9, 18:0066640.0001    28528690.2353.1688
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 4
Life <1 day
Launched Starlink Group 11-022. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-121
CZ 6A
Taiyuan Space Centre
2025 Jun 5, 20:45 UTC
Hulianwang Digui 04-01 (Satellite Low Orbit Internet Group 04-01)
2025-121A
64283
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 6, 16:1573810.0009    9971009105.1886.50217
Hulianwang Digui 04-02 (Satellite Low Orbit Internet Group 04-02)
2025-121B
64284
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 6, 16:1773810.0008    9971009105.1886.50218
Hulianwang Digui 04-03 (Satellite Low Orbit Internet Group 04-03)
2025-121C
64285
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 6, 16:2073800.0008    9961008105.1786.49212
Hulianwang Digui 04-04 (Satellite Low Orbit Internet Group 04-04)
2025-121D
64286
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 6, 16:1873800.0007    9961007105.1586.50204
Hulianwang Digui 04-05 (Satellite Low Orbit Internet Group 04-05)
2025-121E
64287
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 6, 17:2573800.0007    9961007105.1586.50203
CZ 6A third stage
2025-121F
64288
in space
Launched Hulianwang Digui group 04.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 6, 17:2772930.0104    839991103.3086.51112


2025-122
Falcon 9 Block 5
Cape Canaveral Space Force Station
2025 Jun 7, 04:54 UTC
SXM-10
2025-122A
64290
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Jun 7, 10:32174300.6236    18221921381.6826.98175
2025 Jun 14, 18:53317710.3269    1500635780939.295.57179
2025 Jun 17, 15:14421230.0001    35739357501433.940.1043121°.6 W
2025 Jun 20, 13:27421470.0005    35749357881435.190.10225120°.5 W
2025 Jun 21, 11:28421650.0002    35779357951436.130.09155120°.5 W
2025 Jul 17, 13:07421420.0002    35757357711434.930.0498120°.2 W
2025 Jul 30, 13:38421660.0003    35774358011436.150.03331116°.1 W
Falcon 9 Block 5
uncatalogued
Re-entered - 2025 Jun 7
Life <1 day
Launched SXM 10. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-123
Falcon 9 Block 5 (Starlink Group 15-008)
Vandenberg Space Force Base
2025 Jun 8, 14:20 UTC
Starlink 34448
2025-123A
64291
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 17, 20:0066950.0003    31431990.8669.99273
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 8
Life <1 day
Launched Starlink Group 15-008. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-124
Falcon 9 Block 5 (Starlink Group 12-024)
Cape Canaveral Space Force Station
2025 Jun 10, 13:05 UTC
Starlink 11736
2025-124A
64317
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 17, 20:0066950.0001    31631890.8643.00270
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 10
Life <1 day
Launched Starlink Group 12-024. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-125
Electron (The Mountain God Guards)
Rocket Lab Launch Complex, New Zealand
2025 Jun 11, 15:31 UTC
QPS-SAR-11 (Yamatsumi-I)
2025-125A
64340
in space
Commercial satellite from Japanese company iQPS, equipped with an Earth imaging radar. One in a constellation that will ultimately consist of 36 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 12, 14:4969540.0009    57058296.1942.01280
Electron third stage (kick stage)
2025-125B
64341
Re-entered - 2025 Sep 17
Life 98 days
Launched QPS-SAR-11.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 11, 20:4368100.0220    28258293.2142.01271
Electron second stage
2025-125C
64342
Re-entered - 2025 Jul 24
Life 43 days
Launched QPS-SAR-11

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 11, 20:4167800.0256    22857692.6042.02238


2025-126
Falcon 9 Block 5 (Starlink Group 15-006)
Vandenberg Space Force Base
2025 Jun 13, 01:54 UTC
Starlink 33977
2025-126A
64344
in space
One member of a simultaneously-launched cluster of twenty six broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 24, 20:0067020.0004    32132691.0070.00274
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 13
Life <1 day
Launched Starlink Group 15-006. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-127
Falcon 9 Block 5 (Starlink Group 12-026)
Cape Canaveral Space Force Station
2025 Jun 13, 15:29 UTC
Starlink 11732
2025-127A
64370
in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 26, 16:0067140.0001    33533791.2643.00266
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 13
Life <1 day
Launched Starlink Group 12-026. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-128
CZ 2D
Jiuquan Space Centre
2025 Jun 14, 07:56 UTC
Zhangzheng 1-02 (China Seismo-Electromagnetic Satellite)
2025-128A
64393
in space
Satellite developed by the Chinese Academy of Space Technology (CAST) and a group of Italian companies and research bodies. Carries instruments to observe and analyse ionospheric and magnetospheric phenomena linked to extreme geophysical events such as earthquakes, as well as monitoring atmospheric and Space Weather phenomena. Will work in conjuction with its predecessor Zhangzheng 1-01 (64393, 2018-015C).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jun 14, 14:2068750.0010    49050494.5697.3227314:15
2025 Jun 27, 13:5968800.0010    49550994.6697.3224414:14
2025 Jul 1, 14:1768820.0010    49751194.7097.3224514:14
CZ 2D second stage
uncatalogued
in space
Launched Hang Zheng 1-02. Caused to re-enter after releasing the satellite.
Not Catalogued - orbit parameters unavailable


2025-129
Falcon 9 Block 5 (Starlink Group 15-009)
Vandenberg Space Force Base
2025 Jun 17, 03:36 UTC
Starlink 34419
2025-129A
64412
in space
One member of a simultaneously-launched cluster of twenty six broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 26, 16:0067120.0004    33133691.2070.00270
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 17
Life <1 day
Launched Starlink Group 15-009. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-130
Falcon 9 Block 5 (Starlink Group 10-018)
Cape Canaveral Space Force Station
2025 Jun 18, 05:55 UTC
Starlink 34465
2025-130A
64438
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 29, 14:1267000.0000    32232290.9653.1561
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 18
Life <1 day
Launched Starlink Group 10-018. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-131
Angara A5 + Briz-M
Vostochny Cosmodrome
2025 Jun 19, 03:01 UTC
Cosmos 2589
2025-131A
64467
in space
Launched Cosmos 2589.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Jun 20, 18:58420670.3666    20268511101431.121.1017494°.8 E
2025 Jun 21, 17:22420670.3666    20268511101431.101.0917496°.0 E
2025 Jun 29, 19:53421840.3657    20380512311437.081.06174103°.6 E
2025 Jul 7, 17:48421650.3656    20370512041436.121.03174101°.7 E
2025 Sep 6, 16:58421710.3652    20393511921436.410.7817399°.5 E
2025 Nov 19, 17:54421770.3649    20410511871436.720.4717090°.9 E
2025 Nov 20, 19:41421920.3644    20439511891437.500.4717090°.6 E
2025 Nov 21, 19:04422240.3634    20504511881439.130.4617090°.2 E
2025 Nov 23, 18:29422090.3580    20721509411438.350.4516989°.6 E
2025 Nov 24, 13:28422070.3559    20807508501438.230.4516989°.5 E
2025 Nov 26, 13:45421880.3527    20928506911437.270.4416987°.7 E
2025 Nov 27, 17:37422670.3502    21087506911441.350.4416985°.2 E
2025 Nov 29, 09:06421990.3499    21057505841437.830.4316965°.7 E
2025 Dec 1, 13:59421820.3359    21633499741436.960.42169173°.7 E
2025 Dec 4, 17:26421610.3291    21909496571435.930.4116988°.3 E
2025 Dec 5, 17:24420980.3289    21876495651432.710.4116981°.4 E
2025 Dec 11, 13:45422600.3113    22726490371440.950.3916785°.4 E
2025 Dec 14, 22:34421660.2889    23608479681436.160.3816570°.4 E
2025 Dec 17, 17:05421440.3015    23061484701435.020.3616789°.8 E
2025 Dec 18, 20:03421150.2997    23115483591433.550.3616791°.5 E
2025 Dec 19, 13:32421010.2990    23137483091432.830.3616692°.4 E
2025 Dec 20, 13:30420470.2973    23167481711430.090.3516694°.8 E
2025 Dec 21, 16:34421530.2942    23372481771435.490.3516691°.9 E
2025 Dec 22, 06:00421250.2928    23412480811434.060.3516693°.3 E
2025 Dec 22, 22:20421520.2897    23563479851435.470.3516693°.1 E
2025 Dec 24, 15:08422370.2809    23997477221439.810.34165102°.1 E
2025 Dec 26, 08:00427550.2723    24733480211466.360.33167
2026 Feb 4, 15:34421860.1755    28406432091437.160.2115697°.8 E
2026 Feb 15, 08:13421540.1527    29341422111435.550.1915198°.7 E
2026 Feb 21, 23:57421640.1343    30124414471436.040.1714898°.2 E
2026 Feb 27, 14:22421830.1203    30730408801437.040.1614497°.1 E
2026 Mar 24, 17:47421650.0695    32855387191436.120.1312494°.3 E
2026 Apr 16, 16:37421640.0186    35000365711436.040.1310598°.4 E
2026 Apr 22, 18:10421320.0019    35673358351434.430.149797°.8 E
Cosmos 2590
2025-131D
64527
in space
One of a pair of simultaneously launched satellites. Orbit height maintained by occasional use of thruster.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Jun 23, 20:08420540.3665    20264510881430.461.0917499°.3 E
2025 Jun 26, 15:21420540.3665    20265510881430.471.08174103°.3 E
2025 Jun 27, 18:29421130.3672    20271511991433.461.07174104°.5 E
2025 Jun 28, 15:52421630.3678    20279512911436.011.07174104°.8 E
2025 Jul 11, 15:33421660.3677    20285512911436.161.01174104°.8 E
2025 Jul 12, 14:00422200.3659    20392512911438.901.01174104°.2 E
2025 Jul 16, 17:27421670.3652    20388511891436.200.99174101°.6 E
2025 Jul 22, 01:39421650.3655    20376511981436.100.97174101°.7 E
2025 Jul 23, 15:21421660.3655    20377511991436.170.96174101°.5 E
2025 Aug 14, 19:11421680.3653    20385511951436.270.86174101°.0 E
2025 Sep 6, 16:58421710.3652    20393511921436.400.7917499°.5 E
2025 Nov 14, 16:14421760.3647    20418511781436.670.5117091°.6 E
2025 Nov 19, 16:24420870.3678    20230511871432.100.4516997°.1 E
2025 Dec 2, 18:22421060.3670    20274511821433.090.39168110°.1 E
2025 Dec 4, 15:48421320.3668    20299512081434.400.38167111°.1 E
2025 Dec 4, 19:31421710.3666    20335512511436.410.38167111°.1 E
2025 Dec 5, 21:16421700.3665    20335512501436.390.38167111°.0 E
2026 Feb 21, 16:53421650.3660    20356512181436.130.12115107°.7 E
2026 Apr 15, 18:12421700.3657    20369512151436.380.2239105°.9 E
Briz-M auxiliary propellant tank
2035-131C
64469
Re-entered - 2026 Mar 1
Life 255 days
Launched Cosmos 2589 and Cosmos 2590.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 30, 11:07214240.6897    27029822520.1361.14178
Briz-M rocket stage
2025-131B
64468
in space
Launched Cosmos 2589 and Cosmos 2590.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 20, 18:46410340.3870    18775505361378.691.43171


2025-132
CZ 3B/G2
Xichang Space Centre
2025 Jun 20, 12:37 UTC
Zhongxing 9C (Chinasat 9C)
2025-132A
64470
in space
Communication and broadcasting satellite providing voice, data, radio and television transmission services to the Chinese mainland and nearby territories.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Jun 30, 19:15421650.0002    35780357941436.110.093892°.2 E
CZ 3B fourth stage
2025-132B
64471
in space
Launched Zhongxing 9C.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 22, 00:08247440.7345    19136541645.6027.66181


2025-133
Falcon 9 Block 5 (Starlink Group 10-023)
Cape Canaveral Space Force Station
2025 Jun 23, 05:58 UTC
Starlink 34493
2025-133A
64472
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 27, 18:0066680.0001    28929090.3153.1658
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 23
Life <1 day
Launched Starlink Group 10-023. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-134
Atlas V 551 (KA-02, Kuiper Atlas 2)
Cape Canaveral Space Force Station
2025 Jun 23, 09:54 UTC
Kuiper 00039
2025-134A
64500
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from US company Amazon.

All satellites expected to be injected initially into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 26, 20:0068410.0009    45646893.8451.87123
Atlas V third stage (Centaur)
uncatalogued
Re-entered - 2025 Jun 23
Life <1 day
Launched KA-02 group of Kuiper satellites.
Not Catalogued - orbit parameters unavailable


2025-135
Falcon 9 Block 5 (Transporter 14)
Vandenberg Space Force Base
2025 Jun 23, 21:25 UTC
IRIDE-MS2 Hawk for Earth Observation 2
2025-135AT
64569
in space
One satellite in an ESA Earth observation mission, led by the Italian government, that will consist of about sixty satellites in six constellations. Equipped with optical sensors.

One of seven similar satellites carried on this launch, all were placed into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 25
Life 2 days
Launched Transporter 14 satellite cluster. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-136
Falcon 9 Block 5 (Axiom 4)
Kennedy Space Center
2025 Jun 25, 06:31 UTC
AXIOM-4 (AX-4)
2025-136A
64593
Re-entered - 2025 Jul 15
Life 20 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 25, 06:4165770.0015    18920988.4751.6047
2025 Jun 25, 12:2466350.0075    20830789.6551.65212
2025 Jun 25, 12:5366370.0074    21030989.6951.65213
2025 Jun 26, 05:2267940.0002    41541792.8951.64293
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 25
Life <1 day
Launched . Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-137
Falcon 9 Block 5 (Starlink Group 10-016)
Cape Canaveral Space Force Station
2025 Jun 25, 19:54 UTC
Starlink 34280
2025-137A
64594
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 1, 18:0066690.0001    29029190.3353.16123
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 25
Life <1 day
Launched Starlink Group 10-016. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-138
Electron (Get The Hawk Outta Here)
Rocket Lab Launch Complex, New Zealand
2025 Jun 26, 17:28 UTC
Hawk 12C (Cluster 12#3)
2025-138A
64621
in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 3, 13:2969010.0013    51453295.0997.4427905:48
Hawk 12B (Cluster 12#2)
2025-138B
64622
in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 3, 13:2869000.0013    51453195.0897.4327305:48
Hawk 12A (Cluster 12#1)
2025-138C
64623
in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 3, 13:2669000.0014    51253195.0697.4327005:48
KESTREL-0A
2025-138D
64624
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 3, 13:2368980.0014    51053095.0397.4426205:48
Electron third stage (kick stage)
2025-138E
64625
Re-entered - 2025 Jul 1
Life 5 days
Launched cluster of Hawk and Kestrel satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 26, 21:2567980.0272    23560592.9897.449
Electron second stage
2025-138F
64626
Re-entered - 2025 Jul 3
Life 7 days
Launched cluster of Hawk and Kestrel satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 26, 21:3468080.0262    25160893.1797.34213


2025-139
Falcon 9 Block 5 (Starlink Group 10-034)
Cape Canaveral Space Force Station
2025 Jun 28, 04:26 UTC
Starlink 34464
2025-139A
64664
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 1, 18:0066590.0001    28028190.1253.1661
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 28
Life <1 day
Launched Starlink Group 10-034. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-140
Electron (The Harvest Goddess Thrives)
Rocket Lab Launch Complex, New Zealand
2025 Jun 28, 07:08 UTC
LYRA-4
2025-140A
64691
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 29, 13:1170340.0012    64866497.8595.98308
Electron third stage (kick stage)
2025-140B
64692
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 29, 13:1170330.0013    64666497.8295.98301
Electron second stage
2025-140C
64693
Re-entered - 2025 Jul 13
Life 15 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 29, 13:1367860.0338    17963892.7395.99220


2025-141
H-2A-202
Tanegashima Space Centre
2025 Jun 28, 16:33 UTC
GOSAT-GW (IBUKI GW)
2025-141A
64694
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jun 30, 02:2270450.0001    66766898.0998.061201:25
2025 Jul 5, 13:1470490.0004    66867398.1698.0612801:25
2025 Jul 14, 08:2570500.0006    66867698.1998.0310001:25
2025 Jul 18, 20:2770470.0001    66867098.1298.038101:25
H-2A rocket stage
2025-141B
64695
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jun 30, 01:5569800.0094    53766896.7398.05261


2025-142
Falcon 9 Block 5 (Starlink Group 15-007)
Vandenberg Space Force Base
2025 Jun 28, 17:13 UTC
Starlink 34497
2025-142A
64696
in space
One member of a simultaneously-launched cluster of twenty six broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 3, 14:0066730.0004    29229890.4270.00277
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jun 28
Life <1 day
Launched Starlink Group 15-007. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-143
Falcon 9 Block 5
Kennedy Space Center
2025 Jul 1, 21:04 UTC
MTG-S1 (Meteosat Third Generation - Sounder 1)
2025-143A
64723
in space
Meteorological satellite covering Europe and Africa, collecting vertical temperature and humidity profiles of the Earth's atmosphere. Data collected will be used for enhanced forecasting of atmospheric instability, water vapour movement, and extreme weather events like heavy rainfall, tropical cyclones, and winter storms.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Jul 2, 08:28390370.8287    308650081279.2821.22179
2025 Jul 15, 08:15422120.0012    35782358861438.521.011813°.3 W
2025 Jul 17, 13:21421650.0000    35785357891436.121.00653°.5 W
Falcon 9 upper stage
uncatalogued
Re-entered - 2025 Jul 1
Life <1 day
Launched MTG-S1. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-144
Falcon 9 Block 5 (Starlink Group 25-001)
Cape Canaveral Space Force Station
2025 Jul 2, 06:28 UTC
Starlink 34393
2025-144A
64724
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 8, 14:0066740.0001    29629790.4453.1663
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jul 2
Life <1 day
Launched Starlink Group 25-001. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-145
CZ 4C
Xichang Space Centre
2025 Jul 3, 00:00 UTC
Shiyan 28B 01
2025-145A
64753
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 8, 23:3371730.0002    793796100.7611.00114
CZ 4C third stage
2025-145B
64754
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 9, 06:4170830.0122    61979198.8810.9974


2025-146
Soyuz-2.1a
Baikonur Cosmodrome
2025 Jul 3, 19:32 UTC
Progress MS-31 (Progress 7K-MS №461)
2025-146A
64751
Re-entered - 2026 Mar 16
Life 256 days
Supplies to ISS. Initial orbit similar to launch vehicle upper stage. Docked with the downward facing port of the ISS Poisk module July 5 at 21:25 UTC. Undocked 2026 March 16 at 10:24 UTC. Retro-fire led to destructive re-entry above the southern Pacific Ocean at about 17:21 UTC the same day.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 4, 00:0767150.0001    33633891.2751.64196
2025 Jul 5, 19:5267940.0003    41441792.8851.63338
Soyuz third stage
2025-146B
64752
Re-entered - 2025 Jul 5
Life 2 days
Launched Progress MS-31.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 3, 20:0465830.0022    19021988.5951.6573


2025-147
Falcon 9 Block 5 (Starlink Group 28-001)
Cape Canaveral Space Force Station
2025 Jul 8, 08:21 UTC
Starlink 33965
2025-147A
64755
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 11, 20:0066600.0001    28228290.1553.1643
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jul 8
Life <1 day
Launched Starlink Group 28-001. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-148
Falcon 9 Block 5
Cape Canaveral Space Force Station
2025 Jul 13, 05:04 UTC
Dror 1
2025-148A
64784
in space
Israeli government multi-purpose comsat. Expected location 4° west.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Jul 13, 08:42374350.8244    197619181201.3824.22180
2025 Jul 16, 03:21374900.8224    282619411204.0023.85181
2025 Jul 20, 02:21439470.5572    13084620551528.137.27181
2025 Jul 20, 22:46524870.3043    30139620791994.521.98183
2025 Jul 23, 16:43553230.2372    35820620702158.350.83182
2025 Jul 25, 18:48458790.0786    35896431061629.980.27183
2025 Jul 28, 20:03422410.0013    35810359161439.990.03821°.2 E
2025 Jul 31, 08:00422290.0009    35811358911439.380.042921°.1 W
2025 Aug 4, 09:38421740.0004    35780358111436.550.041164°.0 W
2025 Aug 5, 09:37421630.0002    35779357911436.020.041354°.0 W
Falcon 9 second stage
2025-148B
64785
Re-entered - 2025 Jul 14
Life 1 day
Launched Dror 1.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 13, 16:55373450.8239    197617361197.0224.22180


2025-149
CZ 7
Wenchang Space Centre
2025 Jul 14, 21:34 UTC
Tianzhou 9
2025-149A
64786
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 15, 12:2267750.0009    39140392.5041.46284
CZ 7 third stage
2025-149B
64787
Re-entered - 2025 Jul 29
Life 15 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 15, 01:4466490.0104    20234089.9341.47174


2025-150
Falcon 9 Block 5 (Starlink Group 15-002)
Vandenberg Space Force Base
2025 Jul 16, 02:05 UTC
Starlink 34629
2025-150A
64790
in space
One member of a simultaneously-launched cluster of twenty six broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 22, 21:1866730.0003    29329890.4270.00282
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jul 16
Life <1 day
Launched Starlink Group 15-002. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-151
Falcon 9 Block 5 (KF-01, Kuiper Falcon 1)
Cape Canaveral Space Force Station
2025 Jul 16, 06:30 UTC
Kuiper 00069
2025-151A
64816
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from US company Amazon.

All satellites expected to be injected initially into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 23, 14:5368370.0006    45546393.7751.88159
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jul 16
Life <1 day
Launched cluster of Kuiper satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-152
Falcon 9 Block 5 (Starlink Group 17-003)
Vandenberg Space Force Base
2025 Jul 19, 03:52 UTC
Starlink 34723
2025-152A
64842
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 23, 17:0466690.0000    29029190.3397.60353
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jul 19
Life <1 day
Launched Starlink Group 17-003. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-153
Falcon 9 Block 5
Cape Canaveral Space Force Station
2025 Jul 22, 21:12 UTC
O3B mPower FM09
2025-153A
64866
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 23, 04:00112440.1964    26577075197.769.61181
2025 Aug 3, 15:11113310.1877    28257080200.058.77213
2025 Aug 4, 01:11113400.1867    28457079200.308.70214
2025 Aug 7, 22:49113880.1857    28957124201.568.48226
2025 Sep 19, 06:56124990.1008    48607381231.775.09324
2025 Sep 24, 15:58126570.0994    50217537236.194.65331
2025 Oct 8, 11:25129500.0761    55867557244.433.24355
O3B mPower FM10
2025-153B
64867
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 23, 04:00112150.1945    26557019196.999.69181
2025 Jul 31, 07:04112540.1917    27187033198.029.34204
2025 Jul 31, 07:04112540.1917    27187033198.029.34204
2025 Aug 5, 22:52113300.1862    28427061200.038.75220
Falcon 9 second stage
2025-153C
64868
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 24, 02:57112010.1941    26496997196.649.72184


2025-154
Falcon 9 Block 5 (Tracers)
Vandenberg Space Force Base
2025 Jul 23, 18:13 UTC
LIDE
2025-154A
64869
in space
12U Cubesat

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 24, 19:2169710.0005    59059696.5597.7222809:56
Tracers 1
2025-154B
64870
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 25, 17:5269700.0004    58859496.5197.7126209:56
Athena Epic
2025-154C
64871
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 24, 22:3369690.0004    58859496.5097.7126809:56
Skykraft 4A
2025-154D
64872
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 24, 15:1669690.0004    58859496.5097.7127609:56
Tracers 2
2025-154E
64873
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 24, 19:2069690.0005    58759496.4997.7227609:56
PExT
2025-154F
64874
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 24, 18:5768920.0003    51251694.9097.442409:55
REAL
2025-154G
64875
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 24, 18:5668900.0002    51051394.8597.4512209:55
Falcon 9 scond stage
uncatalogued
Re-entered - 2025 Jul 23
Life <1 day
Launched . Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-155
Soyuz-2.1b + Fregat
Vostochny Cosmodrome
2025 Jul 25, 15:55 UTC
Ionosfera-M №3
2025-155A
64876
in space
One of a pair of simultaneously-launched satellites for ionospheric studies. Joins two satellites from the 2024-199 launch to form a four satellite constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 25, 16:1871990.0002    819823101.3198.558203:16
Ionosfera-M №4
2025-155B
64877
in space
One of a pair of simultaneously-launched satellites for ionospheric studies. Joins two satellites from the 2024-199 launch to form a four satellite constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 25, 16:3871990.0002    820823101.3298.559803:16
InnoSat 16 (RS92S7)
2025-155C
64878
in space
6U Cubesat - built by Russian company Geoscan, carrying a remote sensing Earth imaging system and a navsat receiver. Identified from the SatNOGS database of items tracked by the amateur radio community.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:1268800.0010    49550994.6697.4122103:13
Geoscan 6 (RS92S6)
2025-155D
64879
in space
3U Cubesat - built by Russian company Geoscan, and equipped with two Earth observation cameras. Images and video will be transmitted using amateur radio frequencies. Identified from the SatNOGS database of items tracked by the amateur radio community.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0868780.0008    49550694.6297.4121303:13
Geoscan 1 (RS92S1)
2025-155E
64880
in space
3U Cubesat - built by Russian company Geoscan, and equipped with two Earth observation cameras. Images and video will be transmitted using amateur radio frequencies. Identified from the SatNOGS database of items tracked by the amateur radio community.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0868780.0008    49550694.6297.4121403:13
239Alferov (RS61S)
2025-155F
64881
in space
3U Cubesat - equipped with a scintillator detector to study high-energy astrophysical events, such as gamma-ray bursts. Identified from the SatNOGS database of items tracked by the amateur radio community.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0768780.0008    49550594.6197.4121403:13
Nahid 2
2025-155J
64884
in space
Small satellite from Iran. Purpose unknown but probably testing technology for an Earth imaging system. Equiooed with a propulsion system to allow minor orbit changes.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 14:3268780.0007    49550594.6197.4121403:13
Geoscan 2 (RS92S2)
2025-155Q
64890
in space
3U Cubesat - built by Russian company Geoscan, designed to test Automatic Dependent Surveillance–Broadcast (ADS-B) technology, to assess the feasibility of using ADS-B on small spacecraft to monitor unmanned aerial vehicles (UAVs). Identified from the SatNOGS database of items tracked by the amateur radio community.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0568770.0008    49450494.6097.4119903:13
Geoscan 5 (RS92S5)
2025-155R
64891
in space
3U Cubesat - built by Russian company Geoscan, carrying transceivers developed to test packet data transmissionfor remote monitoring, personal communications, and Internet of Things (IoT) applications. Identified from the SatNOGS database of items tracked by the amateur radio community.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0468770.0006    49450394.5997.4121903:13
Geoscan 4 (RS92S4)
2025-155S
64892
in space
3U Cubesat - built by Russian company Geoscan, carrying transceivers developed to test packet data transmissionfor remote monitoring, personal communications, and Internet of Things (IoT) applications. Identified from the SatNOGS database of items tracked by the amateur radio community.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0468770.0006    49450394.5997.4122003:13
Geoscan 3 (RS92S3)
2025-155T
64893
in space
3U Cubesat - built by Russian company Geoscan an a testbed for VHF communications. Identified from the SatNOGS database of items tracked by the amateur radio community.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0468770.0006    49450394.5897.4122203:13
Innosat 3 (RS92S0)
2025-155U
64894
in space
3U Cubesat - built by Russian company Geoscan, designed to test an Automatic Identification System (AIS) receiver. Identified from the SatNOGS database of items tracked by the amateur radio community.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 11:2068760.0006    49450294.5897.4122503:13
Astroline 1
2025-155x
in space
3U Cubesat - mission unknown.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0668770.0008    49450594.6097.4120203:13
Astroline 2
2025-155x
in space
3U Cubesat - mission unknown.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0668770.0009    49350594.6097.4120103:13
Astroline 3
2025-155x
in space
3U Cubesat - mission unknown.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0668780.0007    49550494.6097.4120903:13
Astroline 4
2025-155x
in space
3U Cubesat - mission unknown.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
estimated orbit68780.0007    49550594.6197.4121303:13
CSTP 4.1
2025-155x
in space
3U Cubesat from Russian STC Company. Test vehicle for satellite systems, also equipped with an amateur radio package.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0768780.0007    49550594.6197.4121303:13
CSTP 4.2
2025-155x
in space
3U Cubesat from Russian STC Company. Test vehicle for satellite systems, also equipped with an amateur radio package.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
estimated orbit68780.0007    49550594.6197.4121303:13
CSTP 4.3
2025-155x
in space
3U Cubesat from Russian STC Company. Test vehicle for satellite systems, also equipped with an amateur radio package.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 16:0668770.0009    49350594.6097.4120103:13
CSTP 4.4
2025-155x
in space
3U Cubesat from Russian STC Company. Test vehicle for satellite systems, also equipped with an amateur radio package.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 1, 14:3168770.0009    49350594.6097.4120103:13
Fregat rocket stage
uncatalogued
Re-entered - 2025 Jul 25
Life <1 day
Launched two Ionosphera satellites and eighteen accompanying smaller satellites.
Not Catalogued - orbit parameters unavailable


2025-156
Vega-C
Centre Spatiale Guyanaise
2025 Jul 26, 02:03 UTC
MICROCARB
2025-156A
64899
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 26, 19:0570340.0015    64566697.8498.0123010:42
CO3D 3
2025-156B
64900
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 27, 00:4268770.0003    49650094.5897.4517610:45
2025 Aug 25, 12:2168770.0005    49650294.5997.4410410:45
2025 Aug 26, 12:0168790.0005    49750494.6397.448710:45
2025 Aug 28, 12:5768810.0004    50050594.6797.446310:45
2025 Aug 29, 06:1968820.0004    50150794.6997.448210:45
2025 Sep 1, 02:1568840.0003    50450894.7497.448410:45
2025 Sep 2, 22:2968830.0001    50450694.7297.449210:45
CO3D 4
2025-156C
64901
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 27, 00:4268770.0003    49750194.5997.4617510:45
2025 Aug 4, 22:4268760.0004    49550194.5897.4615310:45
2025 Sep 5, 07:0068770.0005    49550394.6097.436410:46
2025 Sep 16, 22:3868900.0007    50751694.8697.4113510:45
2025 Oct 8, 09:5868830.0001    50450694.7297.449610:45
CO3D 2
2025-156D
64902
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 26, 23:2168770.0004    49650294.6097.4518210:45
2025 Aug 4, 10:0768790.0005    49750494.6397.4415810:45
2025 Aug 15, 11:5968830.0000    50550694.7297.446210:45
CO3D 1
2025-156E
64903
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 27, 00:4368780.0005    49650394.6197.4518510:45
2025 Aug 4, 11:4268790.0005    49750494.6397.4515710:45
2025 Aug 14, 05:2168830.0002    50350694.7197.4312210:45
2025 Aug 17, 04:2668830.0002    50450694.7297.4310310:45
Vega (AVUM+)
uncatalogued
Re-entered - 2025 Jul 26
Life <1 day
Launched . Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-157
Falcon 9 Block 5 (Starlink Group 10-026)
Cape Canaveral Space Force Station
2025 Jul 26, 09:01 UTC
Starlink 34647
2025-157A
64904
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 31, 18:0066680.0001    28929090.3053.1644
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jul 26
Life <1 day
Launched Starlink Group 10-026. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-158
Falcon 9 Block 5 (Starlink Group 17-002)
Vandenberg Space Force Base
2025 Jul 27, 04:31 UTC
Starlink 34705
2025-158A
64932
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 30, 20:0066690.0001    28929190.3297.6096
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jul 27
Life <1 day
Launched Starlink Group 17-002. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-159
CZ 6A
Taiyuan Space Centre
2025 Jul 27, 10:03 UTC
Hulianwang Digui 05-01 (Satellite Low Orbit Internet Group 05-01)
2025-159A
64956
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 28, 08:5173810.0008    9971009105.1886.49217
Hulianwang Digui 05-02 (Satellite Low Orbit Internet Group 05-02)
2025-159B
64957
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 28, 08:5173810.0008    9971009105.1786.50215
Hulianwang Digui 05-03 (Satellite Low Orbit Internet Group 05-03)
2025-159C
64958
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 28, 08:5173800.0008    9961008105.1686.49212
Hulianwang Digui 05-04 (Satellite Low Orbit Internet Group 05-04)
2025-159D
64959
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 28, 10:2073800.0007    9961007105.1586.50205
Hulianwang Digui 05-05 (Satellite Low Orbit Internet Group 05-05)
2025-159E
64960
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 29, 18:1573810.0007    9971008105.1786.49199
CZ 6A third stage
2025-159F
64961
in space
Launched Hulianwang Digui group 05.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 28, 21:4072930.0104    838991103.3086.50111


2025-160
Hyperbola-1(2) (Shuang QuXIan-1(2))
Jiuquan Space Centre
2025 Jul 29, 04:11 UTC
ENSHI XIDA SHANQUAN
2025-160A
64962
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 29, 23:2268810.0010    49651094.6897.4026310:31
SQX-1 rocket stage
2025-160B
64963
Re-entered - 2025 Dec 25
Life 149 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 29, 16:3167660.0170    27250392.3197.43353


2025-F05 - failed to reach orbit
Eris
Bowen Orbital Spaceport
2025 Jul 29, 22:35 UTC


2025-162
CZ 8A
Wenchang Space Centre - Hainan Commercial Zone
2025 Jul 30, 00:00 UTC
Hulianwang Digui 06-01 (Satellite Low Orbit Internet Group 06-01)
2025-162A
65043
in space
One of nine simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 31, 10:2972510.0008    867879102.4150.00272
CZ 8A third stage
2025-162K
65052
in space
Launched Hulianwang Digui group 06.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Jul 31, 10:2971680.0119    705875100.6650.0087


2025-161
Falcon 9 Block 5 (Starlink Group 10-029)
Cape Canaveral Space Force Station
2025 Jul 30, 03:37 UTC
Starlink 34617
2025-161A
65015
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 13, 21:5567170.0001    33834091.3253.15105
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jul 30
Life <1 day
Launched Starlink Group 10-029. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-163
GSLV Mk II F16
Satish Dhawan Space Centre
2025 Jul 30, 12:10 UTC
NISAR
2025-163A
65053
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Jul 31, 14:0771170.0012    73074899.5998.4426818:00
2025 Sep 4, 06:1471180.0015    72975099.6098.4315718:01
2025 Sep 4, 21:1171210.0010    73575099.6798.4315418:01
2025 Sep 12, 15:2171270.0003    74675199.7998.4111718:01
2025 Sep 15, 14:5571280.0001    74975199.8298.418218:01
GSLV third stage
2025-163B
65054
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 1, 05:0271120.0011    72674299.4898.44304


2025-164
Kuaizhou-1A-Pro
Xichang Space Centre
2025 Jul 31, 02:00 UTC
PRSC-S 1
2025-164A
65055
in space
Remote sensing satellite developed by SUPARCO, Pakistan's space agency. Equipped a radar imaging system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 1, 08:0469290.0006    54655595.6741.13246
Kuaizhou 1A upper stage
uncatalogued
Re-entered - 2025 Jul 31
Life <1 day
Launched PRSC-S1.
Not Catalogued - orbit parameters unavailable


2025-165
Falcon 9 Block 5 (Starlink Group 13-004)
Vandenberg Space Force Base
2025 Jul 31, 18:35 UTC
Starlink 34788
2025-165A
65056
in space
One member of a simultaneously-launched cluster of nineteen broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 8, 18:0067220.0002    34334691.4297.6192
USA 549 (Starshield 0152)
2025-165V
65075
in space
Mission description awaited. Initial obit similar to Starlink 34788.
Orbit classified as 'Secret' - data withheld
USA 550 (Starshield 0153)
2025-165W
65076
in space
Mission description awaited. Initial obit similar to Starlink 34788.
Orbit classified as 'Secret' - data withheld
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Jul 31
Life <1 day
Launched Starlink Group 13-004. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-166
Falcon 9 Block 5 (SpaceX crew 11)
Kennedy Space Center
2025 Aug 1, 15:43 UTC
SpaceX Dragon Crew 11
2025-166A
65077
Re-entered - 2026 Jan 15
Life 167 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 1, 16:0465810.0017    19221488.5551.657
2025 Aug 2, 11:3567940.0002    41541792.8951.63144
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 1
Life <1 day
Launched. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-167
Falcon 9 Block 5 (Starlink Group 10-030)
Cape Canaveral Space Force Station
2025 Aug 4, 07:57 UTC
Starlink 34771
2025-167A
65078
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 15, 13:3367190.0000    34034191.3553.15119
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 4
Life <1 day
Launched Starlink Group 10-030. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-168
CZ 12
Wenchang Space Centre - Hainan Commercial Zone
2025 Aug 4, 10:21 UTC
Hulianwang Digui 07-01 (Satellite Low Orbit Internet Group 07-01)
2025-168A
65106
in space
One of nine simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 5, 13:1972760.0007    893903102.9550.00232
CZ 12 second stage
2025-168K
65115
in space
Launched Hulianwang Digui group 07.
Orbit parameters awaited


2025-169
Electron (Live, Laugh, Launch)
Rocket Lab Launch Complex, New Zealand
2025 Aug 5, 04:10 UTC
QPS-SAR-12 (Kushinada-I)
2025-169A
65116
in space
Commercial satellite from Japanese company iQPS, equipped with an Earth imaging radar. One in a constellation that will ultimately consist of 36 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 8, 11:1169550.0007    57258296.2142.01295
Electron third stage (kick stage)
2025-169B
65117
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 8, 14:2269540.0008    57058196.1842.01295
Electron second stage
2025-169C
65118
Re-entered - 2025 Sep 5
Life 31 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 8, 05:0767750.0258    22257192.4942.04275


2025-170
Jielong 3
Jiuquan Space Centre
2025 Aug 8, 16:31 UTC
Geesat 4-01
2025-170A
65119
in space
Small satellite owned by China's Geely automotive group. Part of a system to provide supplementary navigation information to self-driving motor vehicles.

One of eleven similar satellites carried on this launch, all were placed in similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 11, 13:1169730.0014    58560496.5849.99303
2026 Jan 1, 03:2769970.0011    61162697.0749.99129
Jielong 3 fourth stage
2025-170N
65131
Re-entered - 2025 Aug 12
Life 4 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 8, 21:0067460.0320    15358491.9150.16347


2025-171
Falcon 9 Block 5 (KF-02, Kuiper Falcon 2)
Cape Canaveral Space Force Station
2025 Aug 11, 12:35 UTC
Kuiper 00081
2025-171A
65132
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from US company Amazon.

All satellites expected to be injected initially into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 18, 20:0068370.0006    45546393.7751.88146
Falcon 9 upper stage
uncatalogued
Re-entered - 2025 Aug 11
Life <1 day
Launched cluster of Kuiper satellites.
Not Catalogued - orbit parameters unavailable


2025-172
Ariane 62 (VA-264)
Centre Spatiale Guyanaise
2025 Aug 13, 00:37 UTC
METOP-SGA1
2025-172A
65159
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 14, 01:5571830.0001    804806100.9898.7211309:30
2025 Aug 14, 17:0571900.0009    806818101.1398.7135909:30
2025 Aug 15, 03:1271910.0007    807818101.1498.7135909:30
2025 Sep 4, 20:4871930.0007    810820101.1998.7131709:31
2025 Sep 17, 19:1671930.0006    811819101.1998.7128409:31
2025 Oct 16, 03:1871930.0007    810820101.2098.7018509:31
2025 Oct 30, 21:4471980.0001    819821101.3098.7011009:31
Ariane 6 third stage
uncatalogued
Re-entered - 2025 Aug 13
Life <1 day
Launched Metop-SGA1. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-173
Vulcan VC4S
Cape Canaveral Space Force Station
2025 Aug 13, 00:56 UTC
Navigation Technology Satellite 3 (NTS-3)
2025-173A
65160
in space
Military navigation satellite built by Harris systems to test/demonstrate a Department of Defense military navigation system for use by troops in the field.
Orbit classified as 'Secret' - data withheld
USA 554
2025-173B
65161
in space
May be a demonstrator/test satellite hosting a range of technological payloads. Orbit information based on amateur observation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Dec 25, 20:13425320.0009    36116361921454.912.85181
USA 571
2025-173E
67480
in space
Precise mission unknown. Catalogued by Space-Track 2026 Jan 16 so may have separated from USA 554 around the turn of 2025/2026.
Orbit classified as 'Secret' - data withheld
Vulcan second stage (Centaur V)
2025-173C
65162
in space
Launched USA 554 and NTS 3.
Orbit classified as 'Secret' - data withheld


2025-174
CZ 5B/YZ2
Wenchang Space Centre
2025 Aug 13, 06:43 UTC
Hulianwang Digui 08-01 (Satellite Low Orbit Internet Group 08-01)
2025-174A
65164
in space
One of ten simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 14, 02:0374810.0009    10961109107.3286.50297
CZ 5B second stage
uncatalogued
in space
Launched Hulianwang Digui group 08. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-175
Falcon 9 Block 5 (Starlink Group 17-004)
Vandenberg Space Force Base
2025 Aug 14, 05:05 UTC
Starlink 34956
2025-175A
65174
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 20, 14:0066610.0001    28228490.1897.6072
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 14
Life <1 day
Launched Starlink Group 17-004. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-176
Falcon 9 Block 5 (Starlink Group 10-020)
Cape Canaveral Space Force Station
2025 Aug 14, 12:29 UTC
Starlink 34981
2025-176A
65198
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 20, 16:0066650.0001    28728890.2653.1659
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 14
Life <1 day
Launched Starlink Group 10-020. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-F06 - failed to reach orbit
Zhuque 2E
Jiuquan Space Centre
2025 Aug 15, 01:17 UTC


2025-177
CZ 4C
Xichang Space Centre
2025 Aug 17, 08:55 UTC
Shiyan 28B-02
2025-177A
65226
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 17, 22:3271720.0004    791797100.7511.0041
2025 Aug 24, 16:3171730.0003    792797100.7611.00160
CZ 4C third stage
2025-177B
65234
in space
Launched Shiyan 28B-02
Orbit parameters awaited


2025-178
CZ 6A
Taiyuan Space Centre
2025 Aug 17, 14:15 UTC
Hulianwang Digui 09-01 (Satellite Low Orbit Internet Group 09-01)
2025-178A
65228
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 18, 14:1373810.0009    9961009105.1886.50218
Hulianwang Digui 09-02 (Satellite Low Orbit Internet Group 09-02)
2025-178B
65229
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 18, 14:1273810.0009    9961009105.1786.50217
Hulianwang Digui 09-03 (Satellite Low Orbit Internet Group 09-03)
2025-178C
65230
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 18, 14:1273800.0008    9961008105.1686.49212
Hulianwang Digui 09-04 (Satellite Low Orbit Internet Group 09-04)
2025-178D
65231
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 18, 14:1273800.0008    9961007105.1586.50205
Hulianwang Digui 09-05 (Satellite Low Orbit Internet Group 09-05)
2025-178E
65232
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 18, 14:1273790.0007    9961007105.1586.50204
CZ 6A third stage
2025-178F
65233
in space
Launched Hulianwang Digui group 09.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 18, 13:4872910.0105    836989103.2686.51112


2025-179
Falcon 9 Block 5 (Starlink Group 17-005)
Vandenberg Space Force Base
2025 Aug 18, 16:26 UTC
Starlink 34842
2025-179A
65235
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 22, 14:0066670.0002    28829090.3097.6088
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 18
Life <1 day
Launched Starlink Group 17-005. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-180
Lijian 1, Kinetica 1 (Y-8)
Jiuquan Space Centre - Dongfeng Commercial Zone
2025 Aug 19, 07:33 UTC
name not known
2025-180A
65259
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 19, 18:4969090.0014    52154095.2597.4928413:59
name not known
2025-180B
65260
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Jan 9, 02:4569030.0015    51453695.1397.5114813:58
name not known
2025-180C
65261
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 19, 18:4569090.0014    52154195.2597.4928413:59
name not known
2025-180D
65262
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 19, 18:4469090.0014    52154195.2597.4928313:59
name not known
2025-180E
65263
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 19, 18:4969090.0014    52254195.2697.4928113:59
ZK-1A rocket stage
2025-180F
65264
Re-entered - 2025 Nov 16
Life 89 days
Launched cluster of five satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 19, 22:3067850.0215    26155292.6997.5829


2025-181
Soyuz-2.1b
Baikonur Cosmodrome
2025 Aug 20, 17:13 UTC
Bion M-2
2025-181A
65265
Re-entered - 2025 Sep 23
Life 34 days Returned to Earth
Recoverable micro-gravity experiments satellite based on hybrid of the Zenit re-entry cabin and the Yantar instrument unit, carrying several biological payloads including a group of 75 mice and 1500 fruit flies. The chosen orbit inclination was matched to plans for a future Russian space station in order to assess the likely radiation dose that would be experienced by crew members. Following retro-fire at about 06:15 UTC on September 23, the re-entry vehicle landed near Orenburg, Russia at around 07:00 UTC from a southbound ground track. Initial orbit similar to the launch vehicle.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 22, 14:4666760.0092    23636090.4896.947510:05
Soyuz third stage
2025-181B
65266
Re-entered - 2025 Aug 31
Life 11 days
Launched Bion-M 02.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 20, 20:0666450.0115    19134489.8696.9558


2025-182
Angara 1.2
Plesetsk Cosmodrome
2025 Aug 21, 09:32 UTC
Cosmos 2591
2025-182A
65267
in space
Small military/government satellite, possibly for optical imaging, but precise mission not known. Orbit height maintained and controlled by occasional use of thrusters.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 25, 12:0767070.0013    32133891.1196.5922901:09
2026 Apr 23, 06:1166630.0007    28028990.2096.595100:57
Cosmos 2592
2025-182B
65268
in space
Small military/government satellite, possibly for optical imaging, but precise mission not known. Orbit height maintained and controlled by occasional use of thrusters.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 21, 18:2767080.0012    32233891.1396.5924801:10
2026 Apr 23, 06:3366630.0007    28028990.2096.595100:56
Cosmos 2593
2025-182C
65269
in space
Small military/government satellite, possibly for optical imaging, but precise mission not known. Orbit height maintained and controlled by occasional use of thrusters.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 22, 05:0567080.0012    32133891.1296.5924501:09
2026 Apr 23, 02:2566630.0007    28028990.2096.594800:56
Cosmos 2594
2025-182D
65270
in space
Small military/government satellite, possibly for optical imaging, but precise mission not known. Orbit height maintained and controlled by occasional use of thrusters.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 22, 05:0567080.0012    32133891.1296.5924401:10
2026 Apr 23, 05:4866630.0006    28128990.2196.594600:56
Angara 1.2 second stage
uncatalogued
in space
Launched Cosmos 2591 - 2594. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable


2025-183
Falcon 9 Block 5
Kennedy Space Center
2025 Aug 22, 03:50 UTC
USA 555 (OTV-8, X-37B(#2 Flight 4?))
2025-183A
65271
in space
Flight of USAF/Boeing X-37B space plane. Full mission not disclosed but it carries laser communications equipment for use with ground stations and relay satellites, and an inertial guidance device based on quantum physics. Orbit information is based on amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 9, 08:4267130.0002    33333691.2248.8085
2026 Mar 5, 18:1267700.0004    39039492.4049.52283
LIMASat (LIMASAT, Limasat)
2025-183B
65272
in space
Small satellite with unknown mission carried into orbit with the X-37B spaceplane OTV 8 launch. Probably released from the spaceplane soon after reaching space.. Orbit information is based on amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 8, 19:2767070.0006    32533391.1149.5221
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 22
Life <1 day
Launched USA 555 and LIMASat.
Not Catalogued - orbit parameters unavailable


2025-184
Falcon 9 Block 5 (Starlink Group 17-006)
Vandenberg Space Force Base
2025 Aug 22, 17:04 UTC
Starlink 34922
2025-184A
65273
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 27, 14:0066780.0001    29930190.5297.6084
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 22
Life <1 day
Launched Starlink Group 17-006. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-185
Electron (Live, Laugh, Launch)
Rocket Lab Launch Complex, New Zealand
2025 Aug 23, 22:42 UTC
Dresden
2025-185A
65297
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 24, 22:1570390.0012    65366997.9697.9731711:05
Fourier
2025-185B
65298
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 25, 16:1370390.0012    65266997.9597.9730711:05
Stark
2025-185C
65299
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 24, 22:1570390.0012    65366997.9597.9731211:05
Basil
2025-185E
65301
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 25, 16:1370390.0012    65366997.9697.9731311:05
Dojo
2025-185F
65302
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 25, 14:3570390.0010    65466897.9697.9730011:05
Electron third stage (kick stage)
2025-185D
65300
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 25, 14:3570390.0012    65266997.9597.9731111:05
Electron second stage
2025-185G
65303
Re-entered - 2025 Sep 4
Life 12 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 25, 16:1167820.0342    17363692.6597.9722311:05


2025-186
Falcon 9 Block 5
Cape Canaveral Air Force Station
2025 Aug 24, 06:45 UTC
SpaceX Dragon 2 CRS-33
2025-186A
65304
Re-entered - 2026 Feb 27
Life 187 days
Undocked 2026 January 26 at 17:05 UTC. Retrofire February 27 at around 07:05 UTC led to splashdown in the Pacific Ocean off California at about 07:44 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 24, 07:4567530.0003    37337792.0551.55218
2025 Aug 27, 11:5367940.0003    41441892.8951.63279
2026 Feb 26, 13:0068000.0008    41642793.0051.63136
2026 Feb 26, 22:1768000.0008    41642793.0051.63137
Falcon 9 second stage
uncatalogued
in space
Launched
Not Catalogued - orbit parameters unavailable


2025-187
CZ 8A
Wenchang Space Centre - Hainan Commercial Zone
2025 Aug 25, 19:08 UTC
Hulianwang Digui 10-01 (Satellite Low Orbit Internet Group 10-01)
2025-187A
65305
in space
One of nine simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 27, 14:5272500.0007    867877102.4050.01274
CZ 8A third stage
2025-187K
65314
in space
Launched Hulianwang Digui group 10.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Aug 27, 14:0971680.0116    707873100.6750.0189


2025-188
Falcon 9 Block 5
Vandenberg Space Force Base
2025 Aug 26, 18:53 UTC
Pelican-300A
2025-188A
65315
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 27, 22:3168390.0004    45846393.8097.2514210:32
PELICAN-300B
2025-188B
65316
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 27, 22:3168390.0005    45846493.8297.2614910:32
NAOS
2025-188C
65317
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 27, 22:3168390.0005    45846593.8297.2514910:32
Capella 16 (Acadia 6)
2025-188D
65318
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 28, 13:5069760.0005    59560296.6597.7712410:33
FFLY03
2025-188E
65319
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 28, 13:5069770.0006    59560396.6697.7611710:33
FFLY01
2025-188F
65320
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 28, 13:5169780.0004    59660396.6897.7710410:33
LEAP-1
2025-188G
65321
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 28, 13:5169780.0005    59760396.6897.779710:33
2026 Jan 8, 22:4769740.0004    59459996.6197.753710:31
FFLY02
2025-188H
65322
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Aug 28, 13:5169780.0005    59760396.6997.779410:33
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 26
Life <1 day
Launched
Not Catalogued - orbit parameters unavailable


2025-189
Falcon 9 Block 5 (Starlink Group 10-056)
Cape Canaveral Space Force Station
2025 Aug 27, 11:10 UTC
Starlink 34899
2025-189A
65323
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 5, 22:0066830.0001    30430590.6153.1683
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 27
Life <1 day
Launched Starlink Group 10-056. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-190
Falcon 9 Block 5 (Starlink Group 10-011)
Kennedy Space Center
2025 Aug 28, 08:12 UTC
Starlink 34244
2025-190A
65351
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 12, 22:0067810.0001    40240492.6353.16110
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 28
Life <1 day
Launched Starlink Group 10-011. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-191
Falcon 9 Block 5 (Starlink Group 17-007)
Vandenberg Space Force Base
2025 Aug 30, 04:59 UTC
Starlink 34985
2025-191A
65379
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 5, 22:0066940.0001    31531790.8497.6081
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 30
Life <1 day
Launched Starlink Group 17-007. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-192
Falcon 9 Block 5 (Starlink Group 10-014)
Cape Canaveral Space Force Station
2025 Aug 31, 11:49 UTC
Starlink 35031
2025-192A
65404
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 14, 06:0067560.0001    37737992.1253.1680
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Aug 31
Life <1 day
Launched Starlink Group 10-014. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-193
Shavit-2
Palmachim AFB, Israel
2025 Sep 2, 19:30 UTC
Ofeq 19 (Horizon 19)
2025-193A
65432
in space
Israeli electro-optical (probably) reconnaissance satellite to monitor the Middle East from highly retrograde orbit. Orbit information based on amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 1, 08:5169110.0165    41964795.30139.35272
Shavit 2 second stage
2025-193B
65433
Re-entered - 2026 Jan 6
Life 126 days
Launched Offeq 19. Orbit information based on amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 1, 09:1468380.0233    30061993.78139.41265


2025-194
Falcon 9 Block 5 (Starlink Group 17-008)
Vandenberg Space Force Base
2025 Sep 3, 03:51 UTC
Starlink 35142
2025-194A
65434
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 13, 06:0067560.0002    37637992.1097.6072
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 3
Life <1 day
Launched Starlink Group 17-008. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-195
Falcon 9 Block 5 (Starlink Group 10-022)
Cape Canaveral Space Force Station
2025 Sep 3, 11:56 UTC
Starlink 34784
2025-195A
65458
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 13, 06:0067000.0001    32132290.9753.1685
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 3
Life <1 day
Launched Starlink Group 10-022. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-196
CZ 3C/G3Z
Xichang Space Centre
2025 Sep 5, 02:34 UTC
Shiyan 29
2025-196A
65486
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Sep 5, 21:41425630.0091    35799365711456.5028.51131
2025 Sep 29, 17:13425080.0079    35794364661453.6828.54127
2025 Oct 1, 07:39422180.0024    35740359401438.8128.5418298°.6 E
2025 Oct 6, 14:39421640.0011    35739358331436.0628.5417595°.1 E
CZ 3C rocket stage
2025-196B
65487
in space
Launched Shiyan 29.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 8, 10:02218480.6977    22730712535.6328.49130


2025-197
Ceres 1 (Gushenxing 1 y-15)
Jiuquan Space Centre
2025 Sep 5, 11:39 UTC
name not known
2025-197A
65488
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Sep 8, 03:5168820.0014    49451494.7097.4127617:57
2025 Sep 28, 19:4568800.0014    49251294.6697.4119817:57
2025 Sep 29, 21:0168790.0013    49251094.6497.4119417:57
2025 Oct 6, 23:2968810.0016    49251494.6897.4117017:57
2025 Oct 9, 03:3568820.0016    49351594.7097.4116717:57
2025 Oct 10, 19:0568850.0016    49651894.7697.4115417:57
2025 Oct 17, 15:3868950.0015    50752794.9797.4113117:57
2025 Oct 23, 23:5369070.0013    52053895.2297.4111517:57
2025 Nov 16, 11:5169090.0015    52054195.2597.413717:55
2025 Nov 22, 04:2869100.0015    52154295.2797.411917:55
2025 Nov 29, 03:2369150.0015    52754795.3997.4035417:54
2025 Dec 6, 05:4169190.0013    53255095.4797.4133017:54
2025 Dec 13, 16:0569220.0013    53555395.5297.4130117:53
2025 Dec 20, 04:1069190.0013    53255095.4697.4128417:53
2025 Dec 25, 06:4369180.0013    53154895.4497.4126617:52
2026 Feb 10, 21:1769160.0015    52754895.4097.4110117:48
name not known
2025-197B
65489
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Sep 8, 03:5168820.0013    49551394.6997.4127817:57
name not known
2025-197C
65490
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Sep 8, 03:5068810.0014    49351394.6897.4128217:57
name not known
2025-197D
65491
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Sep 8, 03:5068810.0014    49351294.6797.4128317:57
Ceres 1 fourth stage
uncatalogued
in space
Launched cluster of four small satellites.
Not Catalogued - orbit parameters unavailable


2025-198
Falcon 9 Block 5 (Starlink Group 10-057)
Kennedy Space Center
2025 Sep 5, 12:32 UTC
Starlink 35226
2025-198A
65492
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 18, 13:2667030.0001    32532691.0353.15329
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 5
Life <1 day
Launched Starlink Group 10-057. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-199
CZ 6A
Taiyuan Space Centre
2025 Sep 6, 16:34 UTC
Yaogan 40-03 Leader
2025-199B
65545
in space
Described as a remote sensing satellite monitoring the electromagnetic environment - a description that indicates it has an electronic intelligence gathering rôle. One of three related satellites carried on the same launch to operate in a triangular formation separated from each other by about 120 km - a similar formation to the lower inclination Yaogan 31 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 8, 16:5071810.0011    795811100.9486.00258
2025 Sep 12, 20:1471930.0011    807824101.2086.00340
2025 Sep 15, 19:1672180.0004    836843101.7186.00313
2025 Sep 19, 04:5072290.0002    850853101.9686.00113
Yaogan 40-03 Follower
2025-199C
65546
in space
Described as a remote sensing satellite monitoring the electromagnetic environment - a description that indicates it has an electronic intelligence gathering rôle. One of three related satellites carried on the same launch to operate in a triangular formation separated from each other by about 120 km - a similar formation to the lower inclination Yaogan 31 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 8, 16:5071810.0011    795811100.9386.00260
2025 Sep 11, 08:4871840.0009    800812101.0086.00273
2025 Sep 14, 14:2371910.0013    803822101.1486.00264
2025 Sep 15, 19:1972160.0018    825850101.6786.00295
2025 Sep 18, 03:2072220.0008    839850101.8186.00288
2025 Sep 23, 22:4572290.0002    850853101.9686.0084
Yaogan 40-03 Outlier
2025-199D
65547
in space
Described as a remote sensing satellite monitoring the electromagnetic environment - a description that indicates it has an electronic intelligence gathering rôle. One of three related satellites carried on the same launch to operate in a triangular formation separated from each other by about 120 km - a similar formation to the lower inclination Yaogan 31 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 12, 21:4871770.0015    789810100.8686.00244
2025 Sep 15, 03:3471690.0006    786795100.6886.00280
2025 Sep 16, 04:4471630.0014    775795100.5686.00271
2025 Oct 30, 23:4271640.0019    772800100.5985.99124
2025 Oct 31, 16:2871700.0026    773810100.6985.99131
2025 Nov 2, 07:0871770.0025    781817100.8685.99102
2025 Nov 3, 20:1271950.0026    798835101.2285.99106
2025 Nov 4, 13:0572030.0015    814836101.4185.9989
2025 Nov 5, 22:5672130.0004    831837101.6085.99120
2025 Nov 7, 19:0372290.0002    849852101.9585.9977
2025 Nov 10, 23:3472290.0002    849853101.9585.9988
CZ 6A third stage
2025-199F
65549
in space
Launched the Yaogan 40-03 group.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 9, 22:4870580.0070    63073098.3686.0260


2025-200
Falcon 9 Block 5 (Starlink Group 17-009)
Vandenberg Space Force Base
2025 Sep 6, 18:06 UTC
Starlink 35112
2025-200A
65520
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 19, 16:0066870.0001    30831090.7197.6076
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 6
Life <1 day
Launched Starlink Group 17-009. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-201
Jielong 3
Jiuquan Space Centre
2025 Sep 8, 19:48 UTC
Geesat 5-01
2025-201A
65550
in space
Small satellite owned by China's Geely automotive group. Part of a system to provide supplementary navigation information to self-driving motor vehicles.

One of eleven similar satellites carried on this launch, all were placed in similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 10, 03:2869730.0013    58660496.5849.98297
Jielong 3 fourth stage
2025-201N
65562
Re-entered - 2025 Sep 24
Life 16 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 9, 01:2867600.0337    15461092.1950.16347


2025-202
CZ 7A
Wenchang Space Centre
2025 Sep 9, 02:00 UTC
Yaogan 45
2025-202A
65563
in space
Described as being used for remote sensing for scientific experiments, land and resources surveys, agricultural product estimation, and disaster prevention and mitigation. Mission is probably military or government optical imaging.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 19, 12:25138770.0001    74977500271.1420.01265
CZ 7A fourth stage
2025-202B
65564
Re-entered - 2025 Oct 31
Life 52 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 20, 09:2781040.1982    1203333121.0120.056


2025-203
Falcon 9 Block 5
Vandenberg Space Force Base
2025 Sep 10, 14:12 UTC
PRAETORIAN SDA 602
2025-203A
65565
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 24, 16:0073260.0006    943952104.0081.30183
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 10
Life <1 day
Launched
Not Catalogued - orbit parameters unavailable


2025-204
Soyuz-2.1a
Baikonur Cosmodrome
2025 Sep 11, 15:54 UTC
Progress MS-32 (Progress 7K-MS №462)
2025-204A
65586
Re-entered - 2026 Apr 21
Life 222 days
Supplies to ISS. Initial orbit similar to launch vehicle upper stage. Docked with the aft port of the ISS Zvezda module September 13 at 20:23 UTC. Undocked 2026 April 20 at 22:09 UTC. Retro-fire April 21 at about 01:11 UTC led to destructive re-entry above the southern Pacific Ocean at about 01:50 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 12, 23:0166360.0011    25126589.6651.64156
2025 Sep 13, 20:0467940.0004    41341992.8951.63336
Soyuz third stage
2025-204B
65587
Re-entered - 2025 Sep 15
Life 4 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 11, 21:3765820.0024    18721988.5651.6676


2025-205
Falcon 9 Block 5
Cape Canaveral Space Force Station
2025 Sep 12, 01:56 UTC
Nusantara Lima (Nusantara 5)
2025-205A
65588
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Sep 12, 02:27143680.5387    24915729285.6526.48174
2025 Sep 18, 16:15189310.6495    25724850432.0526.30179
2025 Sep 20, 19:46355120.7036    4148541201110.0113.10180
2025 Sep 24, 17:54421690.4489    16863547201436.330.32107112°.8 E
2025 Sep 30, 14:36422430.4447    17081546481440.080.31107112°.0 E
2025 Oct 14, 19:16421440.4043    18728528041435.040.27111110°.4 E
2025 Oct 28, 18:54430650.3670    20884524891482.310.2284
2025 Nov 12, 16:43441170.3233    23477520021537.000.1884
2025 Nov 26, 16:18453180.2811    26200516801600.170.1581
2025 Dec 8, 17:39469550.2281    29868512851687.650.1386
2025 Dec 22, 03:53421630.1288    30353412171436.020.1155112°.9 E
2026 Jan 8, 01:06421830.0804    32412391981437.050.1030106°.7 E
2026 Jan 18, 04:06421320.0457    33828376801434.430.1015108°.9 E
2026 Jan 31, 02:04421640.0001    35783357901436.070.1116112°.8 E
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 12
Life <1 day
Launched
Not Catalogued - orbit parameters unavailable


2025-206
Soyuz-2.1b Fregat
Plesetsk Cosmodrome
2025 Sep 13, 02:10 UTC
Cosmos 2595 (Mozhaets 6)
2025-206A
65589
in space
Satellite name resurrected after 20 years of disuse. Designed by a student at the A.F. Mozhaisky Military Space Academy as a demonstrator of future space systems related to celestial navigation by satellites. Reportedly a 'stealth' satellite with low radar and optical visibility from the ground although it has been tracked by US sensors. Orbit information has never been released by Space-Track possibly to avoid revealing the level of ability of the US tracking network or, equally likely, in error. Orbit similar to Cosmos 2596.
Orbit classified as 'Secret' - data withheld
Cosmos 2596 (Uragan-K2 №18L)
2025-206B
65590
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 15, 16:12255040.0011    1909719154675.5564.80290
2025 Sep 25, 08:02254290.0231    1846319639672.6068.24120
2025 Sep 30, 01:54254810.0016    1906219145674.6764.79263
2025 Oct 12, 05:41255080.0013    1909619164675.7464.78302
Fregat rocket stage
2025-206C
65591
in space
Launched Cosmos 2595 and Cosmos 2596.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 19, 05:00253730.0194    1850219487670.3764.79276
2025 Oct 15, 07:19253850.0011    1898019034670.8664.78181


2025-207
Falcon 9 Block 5 (Starlink Group 17-010)
Vandenberg Space Force Base
2025 Sep 13, 17:55 UTC
Starlink 35267
2025-207A
65592
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 23, 16:0066950.0001    31531790.8597.6077
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 13
Life <1 day
Launched Starlink Group 17-010. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-208
Falcon 9 Block 5
Cape Canaveral Air Force Station
2025 Sep 14, 22:11 UTC
Cygnus NG-23 (SS William "Willie" C McCool)
2025-208A
65616
Re-entered - 2026 Mar 14
Life 181 days
First Cygnus-XL. Mission description awaited. Initial orbit shown is probably a pre-launch estimate.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 14, 22:2066210.0002    24224589.3751.65154
2025 Sep 16, 06:5366950.0103    24838690.8751.6634
2025 Sep 18, 22:1667940.0004    41341892.8851.63355
2026 Mar 12, 03:4967990.0008    41542692.9951.63183
2026 Mar 13, 13:5267950.0008    41242292.9151.63190
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 14
Life <1 day
Launched Cygnus NG-23. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-209
CZ 2C + YZ-1S
Jiuquan Space Centre
2025 Sep 16, 01:06 UTC
Hulianwang Jishu Shiyan 7-01 (Internet Connectivity Test Satellite 7-01)
2025-209A
65617
in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle. Individual satellites act as test/demonstrator platforms for specific components of the system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 17, 05:1171880.0002    808811101.0750.00156
2025 Oct 21, 06:0872160.0022    823854101.6849.9818
2025 Oct 22, 16:0172240.0001    846846101.8450.00347
2025 Oct 23, 05:3672270.0004    846851101.9049.9922
2025 Nov 1, 12:5972570.0003    877881102.5550.0026
Hulianwang Jishu Shiyan 7-02 (Internet Connectivity Test Satellite 7-02)
2025-209B
65618
in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle. Individual satellites act as test/demonstrator platforms for specific components of the system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 17, 05:1171870.0002    808811101.0750.00159
2025 Sep 20, 22:2571880.0002    809812101.0950.00173
2025 Oct 21, 02:4672200.0014    832852101.7650.0113
2025 Oct 22, 10:5872230.0001    844845101.8150.00307
2025 Oct 24, 17:1972390.0002    859862102.1550.00350
2025 Nov 1, 13:0372570.0003    877881102.5550.0030
Hulianwang Jishu Shiyan 7-03 (Internet Connectivity Test Satellite 7-03)
2025-209C
65619
in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle. Individual satellites act as test/demonstrator platforms for specific components of the system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 17, 05:1171870.0002    808810101.0650.00163
2025 Sep 20, 22:2571880.0002    809811101.0850.00179
2025 Oct 21, 21:1972190.0002    840843101.7550.00309
2025 Oct 22, 04:0672210.0001    842843101.7750.00358
2025 Oct 23, 19:0872310.0002    852854102.0050.0016
2025 Nov 1, 12:5472570.0002    878881102.5550.0045
Hulianwang Jishu Shiyan 7-04 (Internet Connectivity Test Satellite 7-04)
2025-209D
65620
in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle. Individual satellites act as test/demonstrator platforms for specific components of the system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 17, 05:1171870.0002    808810101.0650.00173
2025 Oct 15, 20:0071890.0001    810812101.1050.00308
2025 Oct 18, 00:1571990.0003    819824101.3250.00352
2025 Oct 21, 19:2772070.0002    828831101.4950.00357
2025 Oct 22, 19:0772090.0002    830832101.5350.007
2025 Nov 14, 18:4872570.0003    877882102.5550.0063
YZ-1S rocket stage
2025-209E
65621
Re-entered - 2025 Sep 19
Life 3 days
Launched Hulianwang Jishu Shiyan group 7. Perigee lowered after releasing satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 16, 14:5368710.0528    13085594.4749.98313


2025-210
Falcon 9 Block 5 (Starlink Group 10-061)
Cape Canaveral Space Force Station
2025 Sep 18, 09:30 UTC
Starlink 35247
2025-210A
65622
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 26, 14:0066950.0001    31631890.8653.1616
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 18
Life <1 day
Launched Starlink Group 10-061. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-F07 - failed to reach orbit
Zoljanah
Ayatollah Khomeini Space Centre, Iran
2025 Sep 18, 15:00 UTC


2025-I01
JEM Small Satellite Orbital Deployer
International Space Station
2025 Sep 19, 08:50 UTC
DragonFLY
1998-067xx
in space
2U Cubesat from the Kyushu Institute of Technology equipped with an amateur radio package.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 24, 11:1367890.0001    41141292.7951.63109
GHS-01 (Gifu High School Sat)
1998-067xx
in space
2U Cubesat from Gifu High School and Gifu University equipped with an Earth imaging system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 24, 11:1367890.0001    41141292.7951.63109


2025-I02
JEM Small Satellite Orbital Deployer
International Space Station
2025 Sep 19, 10:40 UTC
ASC (Atsushi Space Challenge)
1998-067xx
in space
1U Cubesat created through crowdfunding led by Japanese entertainer Atsushi Tamura - carries metal sheets and SD cards holding names of funding providers. Inteded to ispire people to look up at the sky.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 24, 11:1367890.0001    41141292.7951.63109
Hamorun (RSP-03)
1998-067xx
in space
1U Cubesat from Rymansat Spaces of Japan carrying a sytem to create sound from the patterns of stars in sky images and return them to Earth as music.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 24, 11:1367890.0001    41141292.7951.63109
STARS-Me2
1998-067xx
in space
1U Cubesat from Shizuoka University equipped with an Earth imafing syste. Part of its mission is to measure the effectiveness of its radio downlinks.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 24, 11:1367890.0001    41141292.7951.63109


2025-211
Falcon 9 Block 5 (Starlink Group 17-012)
Vandenberg Space Force Base
2025 Sep 19, 16:31 UTC
Starlink 35328
2025-211A
65652
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 26, 02:3266700.0003    29029490.3597.6036
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 19
Life <1 day
Launched Starlink Group 17-012. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-212
Falcon 9 Block 5 (Starlink Group 10-027)
Cape Canaveral Space Force Station
2025 Sep 21, 10:53 UTC
Starlink 35189
2025-212A
65676
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 7, 12:4267330.0002    35435791.6553.16196
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 21
Life <1 day
Launched Starlink Group 10-027. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-213
Falcon 9 Block 5 (NRO L-48)
Vandenberg Space Force Base
2025 Sep 22, 17:38 UTC
USA 558 (Starshield 0154)
2025-213A
65704
in space
Mission description awaited. Orbit information based on amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 21, 17:2369550.0001    57657896.2169.99271
USA 559 (Starshield 0155)
2025-213B
65705
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 21, 17:4269550.0001    57657896.2169.99271
USA 560 (Starshield 0156)
2025-213C
65706
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 24, 16:4569550.0002    57657896.2169.99179
USA 561 (Starshield 0157)
2025-213D
65707
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 24, 16:5569550.0002    57657896.2169.99179
USA 562 (Starshield 0158)
2025-213E
65708
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 25, 16:3969550.0002    57657896.2169.99177
USA 563 (Starshield 0159)
2025-213F
65709
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 28, 16:0269550.0001    57657896.2169.99260
USA 564 (Starshield 0160)
2025-213G
65710
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2026 Jan 11, 05:4069550.0001    57657896.2169.99194
USA 565 (Starshield 0151)
2025-213H
65711
in space
Mission description awaited
Orbit parameters awaited


2025-214
Jielong 3
Jiuquan Space Centre
2025 Sep 24, 07:56 UTC
Shikongxing 01 (Space Time Satellite 01)
2025-214A
65712
in space
Satellite from Beijing University carrying an experimental payload but details are not available.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 25, 17:1369730.0013    58660496.5849.98298
Geesat 6-01
2025-214B
65713
in space
Small satellite owned by China's Geely automotive group. Part of a system to provide supplementary navigation information to self-driving motor vehicles.

One of eleven similar satellites carried on this launch, all were placed in similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 25, 17:1369730.0013    58560496.5849.99297
Jielong 3 fourth stage
uncatalogued
Re-entered - 2025 Sep 24
Life <1 day
Launch cluster of Geesat satellites and Shikongxing 01.
Not Catalogued - orbit parameters unavailable


2025-215
Falcon 9 Block 5
Kennedy Space Center
2025 Sep 24, 11:30 UTC
IMAP (Interstellar Mapping and Acceleration Probe)
2025-215A
65725
Re-entered - 2025 Sep 26
Life 2 days
NASA spacecraft equipped with 10 instruments study the heliosphere by observing high-energy particles from the Sun, magnetic fields in interplanetary space, and remnants of exploded stars in interstellar space.
Stationed near the L1 Lagrange Point in the Earth-Sun system
SOLAR 1 (formerly SWFO-L1, Space Weather Follow On - Lagrange 1)
2025-215B
65726
Re-entered - 2025 Sep 26
Life 2 days
Spacecraft operated by the US National Oceanic and Atmospheric Administration to monitor the solar wind and radiation streams in the vicinity of the Earth.
Stationed near the L1 Lagrange Point in the Earth-Sun system
Carruthers Geocorona Observatory
2025-215C
65727
Re-entered - 2025 Sep 26
Life 2 days
NASA spacecraft to study the geocorona and its interaction with radiation and charged particles from Sun.
Stationed near the L1 Lagrange Point in the Earth-Sun system
Falcon 9 second stage
2025-215D
65728
Re-entered - 2025 Sep 26
Life 2 days
Launched IMAP, SWFO-1 and Carruthers to Earth-Sun Lagrange Point 1. Likely to drift away from L1 into heliocentric orbit.
Heliocentric orbit


2025-216
Falcon 9 Block 5 (Starlink Group 10-015)
Cape Canaveral Space Force Station
2025 Sep 25, 08:39 UTC
Starlink 34086
2025-216A
65734
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 7, 14:0867090.0001    33033291.1553.1593
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 25
Life <1 day
Launched Starlink Group 10-015. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-217
Atlas V 551 (KA-03, Kuiper Atlas 3)
Cape Canaveral Space Force Station
2025 Sep 25, 12:09 UTC
Kuiper 00120
2025-217A
65762
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from US company Amazon.

All satellites expected to be injected initially into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 25, 16:4668430.0011    45747293.8951.87119
Atlas V second stage (Centaur)
uncatalogued
Re-entered - 2025 Sep 25
Life <1 day
Launched cluster of Kuiper satellites.
Not Catalogued - orbit parameters unavailable


2025-218
Falcon 9 Block 5 (Starlink Group 17-011)
Vandenberg Space Force Base
2025 Sep 26, 04:26 UTC
Starlink 35330
2025-218A
65791
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 6, 14:5567030.0000    32432591.0297.6050
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 26
Life <1 day
Launched Starlink Group 17-011. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-219
CZ 4C
Jiuquan Space Centre
2025 Sep 26, 19:28 UTC
Fengyun 3H (Fengyun 3-08)
2025-219A
65815
in space
Second generation meteorological imaging satellite capable of producing three-dimensional analyses of weather Replacement for Fengyun 3D (43010, 2017-072A).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Sep 27, 23:3371850.0009    800813101.0198.6424601:41
2025 Sep 29, 09:1671910.0013    803822101.1498.6420801:41
2025 Oct 10, 14:0972040.0002    825827101.4298.658201:40
CZ 4C third stage
2025-219B
65816
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 27, 16:2570950.0122    63080399.1298.6340


2025-220
CZ 6A
Taiyuan Space Centre
2025 Sep 27, 12:40 UTC
Hulianwang Digui 11-01 (Satellite Low Orbit Internet Group 11-01)
2025-220A
65817
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 28, 07:2273810.0008    9971009105.1886.50219
Hulianwang Digui 11-02 (Satellite Low Orbit Internet Group 11-02)
2025-220B
65818
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 28, 07:2273810.0008    9971009105.1886.50218
Hulianwang Digui 11-03 (Satellite Low Orbit Internet Group 11-03)
2025-220C
65819
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 28, 07:2273800.0007    9971008105.1786.49213
Hulianwang Digui 11-04 (Satellite Low Orbit Internet Group 11-04)
2025-220D
65820
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 28, 07:2273800.0007    9971007105.1686.50205
Hulianwang Digui 11-05 (Satellite Low Orbit Internet Group 11-05)
2025-220E
65821
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 28, 07:2273800.0007    9971006105.1586.50204
CZ 6A third stage
2025-220F
65822
in space
Launched Hulianwang Digui group 11.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 28, 07:0372920.0106    837991103.2986.51112


2025-221
Falcon 9 Block 5 (Starlink Group 11-020)
Vandenberg Space Force Base
2025 Sep 29, 02:04 UTC
Starlink 35392
2025-221A
65823
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 8, 15:0466850.0001    30730890.6653.16120
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Sep 29
Life <1 day
Launched Starlink Group 11-020. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-222
CZ 2D
Xichang Space Centre
2025 Sep 29, 03:00 UTC
Shiyan 30-01
2025-222A
65851
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 30, 00:5969660.0004    58559096.4334.99308
2025 Oct 5, 04:3369670.0005    58659396.4634.9910
2025 Dec 18, 09:5469650.0006    58359296.4234.99291
2025 Dec 18, 22:4569680.0006    58559496.4734.99266
Shiyan 30-02
2025-222B
65852
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 29, 23:2369650.0005    58459196.4235.00308
2025 Oct 5, 04:3269670.0006    58559496.4635.0016
2025 Dec 18, 09:5369650.0007    58259296.4235.00295
2025 Dec 18, 22:4469680.0006    58559496.4735.00275
CZ 2D second stage
2025-222C
65853
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Sep 29, 13:4369480.0057    53060996.0634.90335


2025-223
Falcon 9 Block 5 (Starlink Group 11-039)
Vandenberg Space Force Base
2025 Oct 3, 14:06 UTC
Starlink 35208
2025-223A
65854
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 16, 02:4767190.0002    34034291.3553.15352
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 3
Life <1 day
Launched Starlink Group 11-039. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-224
Falcon 9 Block 5 (Starlink Group 10-059)
Cape Canaveral Space Force Station
2025 Oct 7, 06:46 UTC
Starlink 35270
2025-224A
65882
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 15, 14:0066730.0001    29429590.4153.1562
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 7
Life <1 day
Launched Starlink Group 10-059. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-225
Falcon 9 Block 5 (Starlink Group 11-017)
Vandenberg Space Force Base
2025 Oct 8, 03:54 UTC
Starlink 35523
2025-225A
65910
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 20, 20:0067250.0001    34634891.4853.1580
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 8
Life <1 day
Launched Starlink Group 11-017. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-I03
JEM Small Satellite Orbital Deployer
International Space Station
2025 Oct 10, 09:40 UTC
Yotsuba-KUlover
1998-067XN
65941
Re-entered - 2026 Apr 17
Life 189 days
2U Cubesat developed by students from Kyushu University and Kyushu Institute of Technology. Carries sensors to measure magnetic fields in orbit.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 11, 08:4667930.0003    41341792.8751.63190


2025-I04
JEM Small Satellite Orbital Deployer
International Space Station
2025 Oct 10, 09:50 UTC
IWATO (E-Kagaku 1)
1998-067XP
65942
Re-entered - 2026 Mar 4
Life 145 days
1U Cubesat from Japanese company e-kagaku. Used to measure the trip time of short pulses of light sent from the ground. Also carries an amateur radio package.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 12, 07:5867930.0003    41241792.8651.63233
Botan
1998-067XQ
65943
Re-entered - 2026 Apr 19
Life 191 days
1U Cubesat from Chiba Institute of Technology, Japan. Carries a camera capable of obting Earth and sky images. Also carries an amateur radio package.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 12, 07:5867930.0004    41241792.8651.63236


2025-226
Gravity 1
Jiuquan Space Centre
2025 Oct 11, 02:20 UTC
name not known
2025-226A
65938
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Oct 12, 00:0369100.0014    52254295.2897.6728210:33
name not known
2025-226B
65939
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Oct 12, 08:0069110.0014    52354295.2997.6627610:33
2025 Oct 14, 21:5869110.0014    52354395.3097.6626310:33
2025 Oct 15, 09:0669140.0018    52354895.3697.6626910:33
2025 Oct 23, 22:1969160.0020    52355195.3997.6624110:33
2025 Dec 5, 22:3869170.0021    52455395.4197.668510:36
2025 Dec 9, 07:4869180.0021    52655595.4597.666710:36
name not known
2025-226C
65940
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Oct 12, 00:0369110.0014    52354295.2997.6627910:33
Gravity 1 fourth stage
2025-226E
66205
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 27, 18:3167860.0164    29751992.7297.79339


2025-227
CZ 2D
Jiuquan Space Centre
2025 Oct 13, 10:00 UTC
Shiyan 31
2025-227A
65945
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 14, 07:3568840.0011    49851394.7380.00266
CZ 2D second stage
2025-227B
65946
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 14, 21:3968630.0022    47050094.3080.1531


2025-228
Falcon 9 Block 5 (KF-03, Kuiper Falcon 3)
Cape Canaveral Space Force Station
2025 Oct 14, 01:58 UTC
Kuiper 00101
2025-228A
65947
in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from US company Amazon.

All satellites expected to be injected initially into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 22, 14:0068410.0006    45946793.8551.88167


2025-229
Electron (Owl New World)
Rocket Lab Launch Complex, New Zealand
2025 Oct 14, 16:33 UTC
StriX 5
2025-229A
65971
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 15, 17:0369410.0041    53459195.9141.93254
Electron second stage
2025-229B
65972
Re-entered - 2025 Oct 20
Life 6 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 15, 17:3167300.0267    17253291.5741.88243
Electron third stage
2025-229C
65973
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 15, 20:1369380.0042    53158995.8541.98255


2025-230
Falcon 9 Block 5
Vandenberg Space Force Base
2025 Oct 15, 23:06 UTC
SDA 1664
2025-230A
65974
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 30, 07:3073250.0004    945950103.9981.3073
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 16
Life 1 day
Launched cluster of SDA satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-231
CZ 8A
Wenchang Space Centre - Hainan Commercial Zone
2025 Oct 16, 01:33 UTC
Hulianwang Digui 12-01 (Satellite Low Orbit Internet Group 12-01)
2025-231A
65995
in space
One of nine simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 18, 09:1472530.0007    870880102.4650.00260
CZ 8A third stage
2025-231K
66004
in space
Launched Hulianwang Digui group 12.
Orbit parameters awaited


2025-232
Falcon 9 Block 5 (Starlink Group 10-052)
Cape Canaveral Space Force Station
2025 Oct 16, 09:27 UTC
Starlink 34849
2025-232A
66005
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 24, 22:0066830.0001    30430590.6153.1662
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 16
Life <1 day
Launched Starlink Group 10-052. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-233
CZ 6A
Taiyuan Space Centre
2025 Oct 17, 07:08 UTC
Qianfan Ji Gui 07-01
2025-233A
66033
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 29, 23:2071840.0016    794817100.9988.99169
CZ 6A third stage
2025-233U
66051
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 29, 23:3370810.0086    64276498.8389.0376


2025-234
Lijian 1, Kinetica 1 (Y-9)
Jiuquan Space Centre - Dongfeng Commercial Zone
2025 Oct 19, 03:33 UTC
Pakistan HS 1 (Hyperspectral Satellite)
2025-234B
66054
in space
Earth observation satellite from Pakistan’s Space & Upper Atmosphere Research Commission (SUPARCO) - carries an optical imaging system. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Oct 20, 02:4168800.0015    49251294.6697.5128209:59
2025 Oct 27, 14:4068810.0014    49351294.6797.5025010:00
2026 Jan 9, 04:3768770.0014    48950994.5997.50110:03
2026 Jan 27, 19:1868860.0011    50051594.7897.4921910:04
Zhongke 03 (Airsat 03)
2025-234C
66055
in space
Satellite for an Earth imaging constellation from AIRSAT Technology Group, China. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Oct 20, 02:4168810.0014    49351294.6797.4628109:59
Zhongke 04 (Airsat 04)
2025-234D
66056
in space
Satellite for an Earth imaging constellation from AIRSAT Technology Group, China. Catalogue Number and Designation to be confirmed.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Oct 20, 02:4168810.0014    49351394.6797.4627909:59
Lijian 1 third stage
2025-234A
66053
in space
Launched cluster of three satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 20, 02:4168800.0014    49251294.6597.46285


2025-235
Falcon 9 Block 5 (Starlink Group 10-017)
Cape Canaveral Space Force Station
2025 Oct 19, 17:39 UTC
Starlink 35552
2025-235A
66058
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 30, 17:5366940.0001    31631790.8553.15345
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 19
Life <1 day
Launched Starlink Group 10-017. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-236
Falcon 9 Block 5 (Starlink Group 11-019)
Vandenberg Space Force Base
2025 Oct 19, 19:24 UTC
Starlink 35596
2025-236A
66086
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 31, 20:0067110.0001    33233491.1953.1666
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 19
Life <1 day
Launched Starlink Group 11-019. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-237
Falcon 9 Block 5 (Starlink Group 11-005)
Vandenberg Space Force Base
2025 Oct 22, 14:16 UTC
Starlink 35496
2025-237A
66114
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 31, 20:0066900.0001    31231390.7753.1596
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 22
Life <1 day
Launched Starlink Group 11-005. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-238
CZ 5 (Y9)
Wenchang Space Centre
2025 Oct 23, 14:30 UTC
Tongxin Jishu Shiyan 20 (Communication Technology Test 20, TJS 20)
2025-238A
66142
in space
Probably a military or government communications satellite. Described as being mainly used for multi-band and high-speed communication technology validation tests

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Oct 24, 00:30293570.7763    18945768834.2916.42165
2025 Oct 26, 22:37331310.5748    7709457961000.2510.06157
2025 Nov 3, 15:04421650.0002    35778357961436.125.9815362°.5 E
2026 Jan 8, 17:36421640.0005    35763358091436.075.826862°.4 E
CZ 5 second stage
2025-238B
66143
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 25, 12:46272710.7597    17641610746.9816.42165


2025-239
Falcon 9 Block 5
Cape Canaveral Space Force Station
2025 Oct 24, 01:30 UTC
Spainsat New Generation II
2025-239A
66144
in space
Military communications satellite built by a consortium led by Hisdesat for the Spanish Government. Separated from launch vehicle at 02:05 UTC. Continuously operating low thrust used to reach operational orbit but, around November 27 when at about 50000 kilometres altitude, the satellite was disabled either by collision with a micrometeoroid or by an onboard failure. Orbit adjustment then ceased. Expected location - 29° east or 30° west.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 24, 12:40380750.8217    409629841232.3026.78179
2025 Nov 3, 23:03391510.8116    1000645471284.9324.13181
2025 Nov 17, 20:11410990.7870    2377670641381.9819.90184
2025 Nov 20, 17:44415620.7826    2656677111405.4119.19184
2025 Nov 23, 16:31421300.7752    3094684091434.3118.15185
2025 Nov 26, 16:42427190.7682    3525691561464.4917.15186
2025 Nov 28, 17:40431470.7607    3948695891486.5516.06186
Falcon 9 stage 2
uncatalogued
Re-entered - 2025 Oct 24
Life <1 day
Launched Spainsat NG II. Caused to re-enter at about 22:00 UTC on the day of launch, after releasing satellite and above the central Indian Ocean.
Not Catalogued - orbit parameters unavailable


2025-240
Falcon 9 Block 5 (Starlink Group 11-012)
Vandenberg Space Force Base
2025 Oct 25, 14:20 UTC
Starlink 35318
2025-240A
66146
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 4, 16:0067020.0001    32432591.0153.15103
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 25
Life <1 day
Launched Starlink Group 11-022. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-241
H-3-24S
Tanegashima Space Centre
2025 Oct 26, 00:00 UTC
HTV-X1
2025-241A
66174
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 26, 22:0766960.0024    30233490.8851.62147
2025 Oct 27, 07:1467460.0031    34738991.9151.63308
2025 Oct 31, 03:5967960.0005    41442192.9251.63360
2026 Mar 5, 18:2967990.0008    41642793.0051.63161
2026 Mar 6, 13:0467990.0008    41642792.9951.63163
2026 Mar 11, 04:3567990.0008    41542692.9951.63180
2026 Mar 11, 12:3268750.0006    49350194.5651.63176
Ten Kho 2
2025-241B
68261
in space
6U Cubesat from the Okuyama Laboratory at Nikon University of Japan. Built to demonstrate a range of new communications systems. Also carries an amateur radio package. Released from HTV X-1's Small Satellite Orbital Deployer (H-SSOD) 2026 March 11 at around 09:34 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2026 Mar 18, 20:5868760.0004    49550194.5851.63187
H-3 third stage
uncatalogued
Re-entered - 2025 Oct 26
Life <1 day
Launched HTV X-1. Caused to re-enter after releasing the satellite.
Not Catalogued - orbit parameters unavailable


2025-242
CZ 3B
Xichang Space Centre
2025 Oct 26, 03:55 UTC
Gaofen 14 02
2025-242A
66175
in space
High definition imaging satellite equipped with cameras for stereo views and mapping.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Oct 26, 09:3968620.0011    47749194.2897.4427010:26
2025 Nov 30, 10:4768680.0001    48949194.4197.449110:27
2026 Apr 11, 03:3168680.0001    48949094.4097.4130310:31
CZ 3B fourth stage
2025-242B
66176
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Oct 27, 04:1968220.0105    37251693.4697.4539


2025-243
Falcon 9 Block 5 (Starlink Group 10-021)
Cape Canaveral Space Force Station
2025 Oct 26, 15:00 UTC
Starlink 35352
2025-243A
66177
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 5, 20:0067030.0001    32432591.0253.1535
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 26
Life <1 day
Launched Starlink Group 10-021. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-244
Falcon 9 Block 5 (Starlink Group 11-021)
Vandenberg Space Force Base
2025 Oct 28, 00:43 UTC
Starlink 35748
2025-244A
66206
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 5, 20:0066890.0001    31131290.7553.1557
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 28
Life <1 day
Launched Starlink Group 11-021. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-245
Falcon 9 Block 5 (Starlink Group 10-037)
Cape Canaveral Space Force Station
2025 Oct 29, 16:35 UTC
Starlink 35537
2025-245A
66234
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 6, 14:0066750.0001    29729790.4653.1579
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 29
Life <1 day
Launched Starlink Group 10-037. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-246
CZ 2F
Jiuquan Space Centre
2025 Oct 31, 15:44 UTC
Shenzhou 21
2025-246A
66263
Re-entered - 2025 Nov 14
Life 14 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 1, 15:5567650.0007    38339292.3041.47306
2025 Nov 29, 06:1467700.0011    38540092.4041.47292
CZ 2F third stage
2025-246B
66264
Re-entered - 2025 Nov 12
Life 12 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 3, 06:1266380.0100    19432789.7141.46145
Shenzhou 21 Orbital Module
2025-246C
66515
in space
awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2026 Jan 7, 20:3967540.0001    37537792.0741.4784


2025-247
Falcon 9 Block 5 (Starlink Group 11-023)
Vandenberg Space Force Base
2025 Oct 31, 20:41 UTC
Starlink 35801
2025-247A
66265
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 13, 16:0067270.0001    34834991.5153.1673
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Oct 31
Life <1 day
Launched Starlink Group 11-023. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-248
Falcon 9 Block 5
Cape Canaveral Space Force Station
2025 Nov 2, 05:09 UTC
Korsat 4
2025-248A
66293
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 16:1969510.0005    57057796.1345.411
BANDWAGON-4B
2025-248B
66294
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 14:4168910.0002    51151394.8745.40298
BANDWAGON-4C
2025-248C
66295
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 15:4568860.0002    50651094.7845.4140
BANDWAGON-4D
2025-248D
66296
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 17:3268890.0002    50951294.8345.4126
BANDWAGON-4E
2025-248E
66297
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 15:1568850.0008    50251294.7645.4132
BANDWAGON-4F
2025-248F
66298
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 15:2068850.0007    50251294.7745.4137
FGN-100-D2
2025-248G
66299
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 15:5168890.0003    50851394.8345.4010
ICEYE X-65
2025-248H
66300
in space
Small satellite fitted with a synthetic aperture radar for Earth surface imaging.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 8, 20:0068880.0003    50851294.8345.4134
ICEYE X-66
2025-248J
66301
in space
Small satellite fitted with a synthetic aperture radar for Earth surface imaging.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 8, 20:0068890.0003    50951394.8345.4021
ICEYE X-67
2025-248K
66302
in space
Small satellite fitted with a synthetic aperture radar for Earth surface imaging.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 8, 20:0068880.0004    50751294.8145.4140
STARCLOUD-1
2025-248L
66303
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 17:2168880.0004    50751294.8245.4014
BANDWAGON-4M
2025-248M
66304
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 6, 23:1568830.0009    49851094.7145.4027
BANDWAGON-4N
2025-248N
66305
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 15:0068820.0009    49851094.7045.4031
BANDWAGON-4P
2025-248P
66306
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 5, 23:3968830.0008    49951194.7245.4121
BANDWAGON-4Q
2025-248Q
66307
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 07:1468830.0008    50051094.7245.4029
TOMORROW-S8
2025-248R
66308
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 3, 12:0068890.0004    50851394.8445.40346
TOMORROW-S9
2025-248S
66309
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 3, 12:0068900.0002    51051394.8545.41359
HAVEN-DEMO
2025-248T
66312
Re-entered - 2026 Feb 5
Life 95 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 21, 00:0068900.0004    50951494.8645.40307


2025-249
LVM3 (M5)
Satish Dhawan Space Centre
2025 Nov 2, 11:56 UTC
CMS-03 (GSAT-7R)
2025-249B
66311
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Nov 2, 23:49197440.6687    16426569460.1821.40178
2025 Nov 12, 18:13421650.0004    35768358061436.110.2220493°.5 E
LVM3 third stage
2025-249A
66310
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 3, 15:11197910.6687    17926647461.8221.32179


2025-250
CZ 7A
Wenchang Space Centre
2025 Nov 3, 03:47 UTC
Yaogan 46
2025-250A
66313
in space
Described as being used for remote sensing for disaster prevention and mitigation, land resource surveys, and water conservancy and meteorological research. Mission is probably military or government optical imaging.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 3, 15:12114330.2193    25487562202.7720.01126
2025 Nov 7, 22:39138070.0049    73617497269.1020.03118
CZ 7A fourth stage
2025-250B
66314
Re-entered - 2025 Dec 11
Life 38 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 3, 20:19101680.3559    1717409170.0719.98126


2025-251
Ariane 62 (VA-265)
Centre Spatiale Guyanaise
2025 Nov 4, 21:02 UTC
Sentinel 1D
2025-251A
66315
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 6, 17:3570730.0002    69469698.6798.19606:00


2025-252
Electron (The Nation God Navigates)
Rocket Lab Launch Complex, New Zealand
2025 Nov 5, 19:51 UTC
QPS-SAR-14 (Yachihoko-I)
2025-252A
66316
in space
Commercial satellite from Japanese company iQPS, equipped with an Earth imaging radar. One in a constellation that will ultimately consist of 36 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 6, 06:0069540.0010    56958396.1942.00272
Electron second stage
2025-252B
66317
Re-entered - 2025 Dec 5
Life 30 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 6, 05:3967800.0249    23357192.6042.00239
Electron third stage
2025-252C
66318
Re-entered - 2025 Nov 30
Life 25 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 5, 21:5667710.0209    25253592.4241.98235


2025-253
Falcon 9 Block 5 (Starlink Group 06-081)
Cape Canaveral Space Force Station
2025 Nov 6, 01:31 UTC
Starlink 35442
2025-253A
66319
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 13, 18:0066660.0002    28728990.2743.00265
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 6
Life <1 day
Launched Starlink Group 06-081. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-254
Falcon 9 Block 5 (Starlink Group 11-014)
Vandenberg Space Force Base
2025 Nov 6, 21:13 UTC
Starlink 35849
2025-254A
66348
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 17, 20:0066940.0001    31531790.8553.1659
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 6
Life <1 day
Launched Starlink Group 11-014. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-255
CZ 11H
Jiuquan Space Centre
2025 Nov 8, 21:01 UTC
Shiyan 32 01
2025-255A
66376
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 12, 22:3368200.0013    43345193.4353.00306
Shiyan 32 02
2025-255C
66378
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 12, 22:3168190.0015    43145093.3953.00310
2025 Dec 18, 19:1868280.0009    44345693.5852.99283
Shiyan 32 03
2025-255D
66379
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 12, 20:5868190.0015    43145293.4153.00307
2025 Dec 23, 04:0868140.0016    42544793.3053.0072
2025 Dec 23, 16:3568170.0013    43044793.3553.0071
2025 Dec 29, 15:3868210.0006    43944793.4453.0085
debris
2025-255B
66377
in space

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 12, 22:3268190.0015    43145193.4053.00305
debris?
2025-255E
67225
Re-entered - 2025 Dec 23
Life 45 days
Separated from Shiyan 32-02 on December 10. Low mass/cross section ratio resulted in re-entry after six days.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )


2025-256
Lijian 1, Kinetica 1 (Y-10)
Jiuquan Space Centre - Dongfeng Commercial Zone
2025 Nov 9, 03:32 UTC
Chutian 2A (Ultra Low Orbit Test Satellite)
2025-256A
66409
in space
Development satellite for the future Chutian constellation of Earth imaging satellites that will operate below 300 kilometres for long periods, necessitating constantly maintaining the orbit against significant air drag.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 12, 23:4071010.0013    71473299.2598.2827509:59
2025 Nov 20, 07:0871040.0013    71773599.3198.2824909:59
Chutian 2B (Ultra Low Orbit Test Satellite)
2025-256B
66410
in space
Development satellite for the future Chutian constellation of Earth imaging satellites that will operate below 300 kilometres for long periods, necessitating constantly maintaining the orbit against significant air drag.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 12, 23:3971010.0013    71373299.2498.2827809:59
ZK-1A rocket stage
2025-256C
66411
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 12, 22:1269420.0234    40172795.9498.32344


2025-F08 - failed to reach orbit
Ceres 1
Jiuquan Space Centre
2025 Nov 9, 04:02 UTC


2025-257
Falcon 9 Block 5 (Starlink Group 10-051)
Kennedy Space Center
2025 Nov 9, 08:10 UTC
Starlink 35139
2025-257A
66380
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 18, 16:0066900.0001    31131290.7553.1548
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 9
Life <1 day
Launched Starlink Group 10-051. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-258
CZ 12
Wenchang Space Centre - Hainan Commercial Zone
2025 Nov 10, 02:41 UTC
Hulianwang Digui 13-01 (Satellite Low Orbit Internet Group 13-01)
2025-258A
66412
in space
One of nine simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 12, 16:1871840.0014    796816100.9950.00254
CZ 12 second stage
2025-258K
66421
in space
Launched Hulianwang Digui group 13.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 12, 17:1671290.0065    70579799.8450.00141


2025-259
Falcon 9 Block 5 (Starlink Group 06-087)
Cape Canaveral Space Force Station
2025 Nov 11, 03:21 UTC
Starlink 35617
2025-259A
66422
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 19, 12:0066810.0002    30230490.5843.00269
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 11
Life <1 day
Launched Starlink Group 06-087. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-260
New Glenn (NG-1)
Cape Canaveral Space Force Station
2025 Nov 13, 20:55 UTC
Escape and Plasma Acceleration and Dynamics Explorer Blue (ESCAPADE Blue)
2025-260A
66451
in space
One of a pair of identical, simultaneously-launched, spacecraft to study Mars and to demonstrate a low cost space vehicle. Launched initially to orbit around the L2 Earth-Sun Lagrange Point befor departing towards Mars during 2026.
Stationed near the L2 Lagrange Point in the Earth-Sun system
Escape and Plasma Acceleration and Dynamics Explorer Gold (ESCAPADE Gold)
2025-260B
66452
in space
One of a pair of identical, simultaneously-launched, spacecraft to study Mars and to demonstrate a low cost space vehicle. Launched initially to orbit around the L2 Earth-Sun Lagrange Point befor departing towards Mars during 2026.
Stationed near the L2 Lagrange Point in the Earth-Sun system
New Glenn second stage
2025-260C
66453
in space
Mission description awaited
Heliocentric orbit


2025-261
Atlas V 551
Cape Canaveral Space Force Station
2025 Nov 14, 03:04 UTC
Viasat 3 F2
2025-261A
66454
in space
Commercial comsat for the aviation industry, government and private consumers. Planned to provide broadband services to Europe, the Middle East and Africa technical problems with Viasat 3 F1 ( 56370, 2023-067A) may result in it being used to support North American serices instead. Continuous thrust used to raise orbit to operating height.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Nov 18, 00:50243370.2346    1224923668629.725.61181
2025 Dec 4, 01:07243770.2342    1228923708631.295.57184
2025 Dec 19, 05:50267430.2200    1448226248725.415.09187
2026 Jan 5, 09:40302860.2073    1762930187874.234.15191
2026 Jan 15, 17:20321930.2031    1927632353958.063.75191
2026 Jan 28, 01:59360370.1629    23789355291134.713.05192
2026 Feb 12, 07:47367600.1327    25504352611169.040.71173
2026 Feb 26, 05:57415640.0571    32811375601405.510.36200
2026 Mar 4, 23:48420530.0147    35057362921430.380.1821387°.9 W
2026 Mar 9, 13:27421170.0008    35705357731433.650.1120979°.0 W
2026 Mar 12, 13:20421650.0001    35783357901436.090.1011979°.0 W
Atlas V third stage (Centaur)
2025-261B
66455
in space
Launched Viasat F2.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 14, 07:13243690.2329    1231623667630.996.57182


2025-262
Falcon 9 Block 5 (Starlink Group 06-089)
Kennedy Space Center
2025 Nov 15, 03:08 UTC
Starlink 35643
2025-262A
66456
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 24, 20:0066830.0002    30330690.6143.00273
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 15
Life <1 day
Launched Starlink Group 06-089. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-263
Falcon 9 Block 5 (Starlink Group 06-085)
Cape Canaveral Space Force Station
2025 Nov 15, 06:44 UTC
Starlink 34774
2025-263A
66485
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 21, 16:0066510.0002    27127489.9743.00263
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 15
Life <1 day
Launched Starlink Group 06-085. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-264
Falcon 9 Block 5
Vandenberg Space Force Base
2025 Nov 17, 05:21 UTC
Sentinel 6B
2025-264A
66514
in space
Ocean studies satellites launched to join Sentinel 6A. Joint NASA/ESA mission equipped with a radar altimeter to measure heights of sea level around the world. A microwave radiometer measures water vapour in the atmosphere in order to ensure the radar altimeter readings are properly calibrated. Also carries a GPS receiver and a laser reflector for precise orbit measurement.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 17, 08:2076960.0013    13081327111.9866.05271
2025 Nov 18, 23:3276960.0012    13091327111.9966.05270
2025 Dec 7, 23:0477030.0021    13091342112.1566.04269
2025 Dec 11, 20:3977140.0008    13291342112.3766.04269
2025 Dec 22, 18:5877160.0008    13321344112.4266.04270
Falcon 9 second stage.
uncatalogued
Re-entered - 2025 Nov 17
Life <1 day
Launched Sentinel 6B. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-265
Falcon 9 Block 5 (Starlink Group 06-094)
Cape Canaveral Space Force Station
2025 Nov 19, 00:12 UTC
Starlink 35924
2025-265A
66516
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 25, 16:0066730.0002    29429690.4243.00274
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 19
Life <1 day
Launched Starlink Group 06-094. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-266
CZ 2C
Jiuquan Space Centre
2025 Nov 19, 04:01 UTC
Shijian 30A (Practice 30A)
2025-266A
66545
in space
One of a simultaneously-launched group of three satellites described as being used for space environment exploration and related technology verification, suggesting that they may be used for detecting and tracking other satellites in space. Orbit raised slowly by continuous use of thruster.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 19, 19:2368970.0013    51052895.0151.80274
2025 Nov 26, 04:5368980.0013    51152995.0351.80297
2025 Dec 10, 04:2668970.0013    51052895.0151.80347
2025 Dec 24, 19:4668970.0013    51052895.0051.8038
2026 Jan 7, 11:2268980.0013    51152995.0251.8085
Shijian 30B (Practice 30B)
2025-266B
66546
in space
One of a simultaneously-launched group of three satellites described as being used for space environment exploration and related technology verification, suggesting that they may be used for detecting and tracking other satellites in space. Orbit raised slowly by continuous use of thruster.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 19, 19:2368980.0010    51352795.0351.80274
2025 Nov 26, 12:5068990.0010    51352895.0451.80299
2025 Dec 10, 04:2768980.0010    51352795.0351.80350
2025 Dec 23, 02:3968970.0011    51252695.0151.8036
2026 Jan 7, 08:1368970.0011    51252795.0251.7987
Shijian 30C (Practice 30C)
2025-266C
66547
in space
One of a simultaneously-launched group of three satellites described as being used for space environment exploration and related technology verification, suggesting that they may be used for detecting and tracking other satellites in space. Orbit raised slowly by continuous use of thruster.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 19, 09:5368990.0011    51352895.0451.80266
2025 Nov 26, 11:1668980.0011    51252895.0351.80291
2025 Dec 10, 02:5368970.0011    51152795.0151.80342
2025 Dec 24, 02:2568970.0012    51152795.0151.8031
2026 Jan 7, 03:2968970.0012    51152795.0151.8078
CZ 2C second stage
2025-266D
66548
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 20, 18:4768550.0085    41953694.1552.0698


2025-267
Electron (Follow My Speed)
Rocket Lab Launch Complex, New Zealand
2025 Nov 20, 12:43 UTC
BlackSky 33 (Global 33)
2025-267A
66554
in space
Third Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 21, 14:1868510.0007    46847894.0642.02274
Electron third stage
2025-267B
66555
in space
Launched Blacksky 33.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 21, 14:1768500.0009    46547794.0342.02284
Electron second stage
2025-267C
66556
Re-entered - 2025 Nov 28
Life 8 days
Launched Blacksky 33.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 21, 16:3266990.0219    17446790.9442.06276


2025-268
Falcon 9 Block 5 (Starlink Group 06-078)
Kennedy Space Center
2025 Nov 21, 03:39 UTC
Starlink 35699
2025-268A
66557
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 26, 16:0066670.0002    28729090.2943.00259
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 21
Life <1 day
Launched Starlink Group 06-078. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-269
CZ 3B
Xichang Space Centre
2025 Nov 21, 10:55 UTC
Tongxin Jishu Shiyan 21 (Communication Technology Test 21, TJS 21)
2025-269A
66586
in space
Probably a military or government communications satellite in HEO. Described as being mainly used for satellite communication, radio and television, data transmission and other services.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 22, 00:38265230.7518    20540084716.4551.04225
2025 Dec 5, 05:53265610.6805    210838258717.9963.27270
CZ 3B fourth stage
2025-269B
66587
Re-entered - 2026 Feb 10
Life 81 days
Launched TJS 21.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 21, 12:42264810.7521    18640020714.7651.36225


2025-270
Falcon 9 Block 5 (Starlink Group 06-079)
Cape Canaveral Space Force Station
2025 Nov 22, 07:53 UTC
Starlink 36076
2025-270A
66588
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 1, 16:0066990.0002    32032290.9543.00256
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 22
Life <1 day
Launched Starlink Group 06-079. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-271
Falcon 9 Block 5 (Starlink Group 11-030)
Vandenberg Space Force Base
2025 Nov 23, 08:48 UTC
Starlink 35940
2025-271A
66617
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 2, 14:0066900.0001    31131290.7553.16100
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Nov 23
Life <1 day
Launched Starlink Group 11-030. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-272
CZ 2F
Jiuquan Space Centre
2025 Nov 25, 04:11 UTC
Shenzhou 22
2025-272A
66645
in space
Mission to the CSS without crew at launch - space was utilised for cargo. Docked with the forward-facing port of the Tianhe module at 07:50 UTC. Replacement vehicle for use by the Shenzhou 21 crew because porthole glass on Shenzhou 20 was damaged by an impact from an item of space debris with the crack being discovered 2025 Nov as part of the departure preparations for the Shenzhou 20 crew. That crew then used Shenzhou 21 for return to Earth. Initial orbit similar to launch vehicle upper stage.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 27, 20:2367710.0011    38540092.4141.47283
CZ 2F third stage
2025-272B
66646
Re-entered - 2025 Dec 7
Life 12 days
Launched Shenzhou 22.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 5, 15:3065830.0054    16924188.6041.46210


2025-273
Angara 1.2
Plesetsk Cosmodrome
2025 Nov 25, 13:42 UTC
Cosmos 2597 (Rodnik-S)
2025-273A
66647
in space
Government/military system store-dump communications satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 25, 21:0578760.0008    14921505115.9582.50328
2025 Dec 28, 04:2178730.0011    14861503115.8782.50229
Cosmos 2598 (Rodnik-S)
2025-273B
66648
in space
Government/military system store-dump communications satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 25, 21:0578750.0008    14901504115.9282.50317
2025 Dec 6, 21:5378730.0007    14891500115.8682.50265
2025 Dec 11, 04:1678710.0008    14871499115.8382.50241
2026 Jan 3, 02:4378720.0010    14861502115.8682.50184
Cosmos 2599 (Rodnik-S)
2025-273C
66649
in space
Government/military system store-dump communications satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 25, 21:0578780.0009    14931506115.9782.50338
2025 Dec 12, 05:3978800.0006    14971507116.0282.50280
2026 Jan 18, 22:4278730.0016    14821507115.8682.50168
Angara 1.2 second stage
uncatalogued
in space
Launched three Cosmos/Rodnik satellites.
Not Catalogued - orbit parameters unavailable


2025-274
Nuri (KSLV-2)
Naro Space Centre, South Korea
2025 Nov 26, 16:13 UTC
BEE-1000
2025-274A
66650
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 28, 15:5769710.0011    58660096.5497.7430500:49
INHA-RoSAT
2025-274D
66653
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 28, 06:1769700.0010    58559896.5197.7332500:49
Jack 3
2025-274E
66654
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 27, 12:3569700.0012    58360096.5297.7431200:49
CAS500-3
2025-274F
66655
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 27, 17:2469700.0012    58360196.5297.7431200:49
Spyron
2025-274H
66657
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 29, 04:4869690.0012    58359996.4997.7432600:49
PerSat 1
2025-274J
66658
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 29, 04:4869680.0012    58259996.4897.7432900:49
Jack 4
2025-274K
66659
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 29, 04:4769680.0013    58159996.4797.7433000:49
K-Hero
2025-274L
66660
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 29, 04:4769670.0014    58059996.4697.7433000:49
Snuglite 3
2025-274M
66661
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 29, 04:4769670.0014    57959996.4597.7433100:49
E3 Tester Kari 1
2025-274N
66662
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Nov 29, 04:4669670.0015    57859996.4597.7433100:49
Cosmic
2025-274xx
in space
Mission description awaited
Orbit parameters awaited
EtriSat
2025-274xx
in space
Mission description awaited
Orbit parameters awaited
Sejong 4
2025-274xx
in space
Mission description awaited
Orbit parameters awaited
KSLV-II rocket stage
2025-274P
66663
in space
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 28, 06:0869540.0045    54460796.1897.746


2025-275
Soyuz-2.1a
Baikonur Cosmodrome
2025 Nov 27, 09:27 UTC
Soyuz MS-28 (Soyuz 11F732A48 № 753)
2025-275A
66664
in space
Crew to ISS - Sergey Kud-Sverchkov and Sergei Mikaev, (both Roscosmos) and Chris (NASA) . Separated from launch vehicle at 09:36 UTC. Docked with ISS Rassvet module at 12:34 UTC. Initial orbit similar to launch vehicle upper stage.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 27, 21:3467970.0004    41742292.9551.63178
Soyuz third stage
2025-275B
66665
Re-entered - 2025 Nov 29
Life 2 days
Mission description awaited

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 28, 17:4065610.0016    17319388.1651.6639


2025-276
Falcon 9 Block 5 (Transporter 15)
Vandenberg Space Force Base
2025 Nov 28, 18:44 UTC
Formosat 8A
2025-276A
66666
in space
Mission information to follow. Separated from launch vehicle at 21:03 UTC. First images were returned 2026 early February.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:5669440.0004    56356895.9897.6620910:28
2026 Jan 29, 11:4269370.0012    55056795.8397.666410:28
2026 Feb 3, 05:1169410.0007    55856795.9197.655110:28
Pelican 5
2025-276B
66667
in space
Mission information to follow. Separated from launch vehicle at 20:04 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 16, 22:5668910.0002    51251494.8997.4424810:27
HUNITY 1 (NMHH-1)
2025-276E
66670
in space
3p PocketQube satellite developed by students of the Budapest University of Technology and Economics, carries a number f technology demonstration payloads. Separated from launch vehicle at 19:39 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:4268930.0008    51052094.9297.4329110:27
BRO 17 (Breizh Reconnaissance Orbiter 17)
2025-276G
66672
in space
6U Cubesat from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:4468940.0005    51252094.9597.4427110:27
BRO 20 (Breizh Reconnaissance Orbiter 20)
2025-276J
66674
in space
6U Cubesat from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:5768940.0005    51251994.9497.4427310:27
Lemur-2 (DeanaandMaeve)
2025-276N
66678
in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Separated from launch vehicle at 19:39 UTC.

One of four similar satellites carried on the Transporter 15 launch. All were placed in similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:4168940.0005    51251994.9497.4427110:27
Lilium 2
2025-276P
66679
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:4268940.0005    51351994.9597.4428010:27
Otter
2025-276Q
66680
in space
Mission information to follow. Separated from launch vehicle at 19:40 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 16:2168940.0005    51251994.9497.4426610:27
ION SCV 021 (Galactic Georgius)
2025-276S
66682
in space
Satellite carrier from D-Orbit equipped with customer-suppled experiments/sensors and Cubesat deployers for later release of satellites. Separated from launch vehicle at 20:05 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:5368930.0005    51151894.9297.4525810:27
2025 Dec 25, 00:1668990.0014    51153095.0597.4516010:27
2025 Dec 25, 16:0869040.0012    51753495.1497.4512410:27
2025 Dec 25, 17:4369010.0016    51253495.1097.4516510:27
2025 Dec 26, 12:4468990.0011    51352995.0597.4414010:27
2025 Dec 26, 17:3069040.0016    51553695.1597.4412310:27
2025 Dec 26, 23:5169050.0017    51653895.1797.4311910:27
2025 Dec 28, 01:1969190.0027    52255995.4697.447310:26
2025 Dec 28, 17:1469180.0037    51456595.4397.447610:26
2025 Dec 30, 04:1669210.0043    51357395.5197.447410:26
2026 Jan 6, 03:3169240.0061    50358895.5697.556010:26
2026 Jan 6, 13:0569260.0037    52257395.6097.554710:26
2026 Jan 7, 13:0169300.0031    53057395.6897.554210:26
2026 Jan 8, 03:2369330.0026    53757395.7497.553910:26
2026 Jan 9, 12:5669370.0020    54557395.8497.552910:26
2026 Jan 10, 22:3169400.0016    55157395.9097.541910:26
2026 Jan 15, 03:1769430.0013    55657395.9597.5536010:26
2026 Jan 16, 19:1769460.0008    56257396.0197.5432710:26
2026 Jan 19, 03:2269520.0010    56758096.1497.5427410:25
2026 Jan 24, 21:0769390.0016    55057295.8997.5416410:25
2026 Jan 30, 14:4069480.0007    56457596.0697.5418310:25
2026 Feb 5, 16:2669470.0008    56357496.0497.5415610:24
2026 Feb 14, 15:0369480.0009    56357596.0597.5413110:24
2026 Feb 18, 21:3569530.0003    57357796.1797.5421510:23
6GStarLab
2025-276T
66683
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:3968930.0005    51251894.9397.4526310:27
MICE 1 (Maritime Identification and Communication systEm)
2025-276U
66684
in space
3U Cubesat from Greek company Prisma Electronics equipped with an AIS reiver to relay short messages between aircraft and the ground. Also carries a receiver to relay data from ground-based sensors to the internet. Separated from launch vehicle at 19:40 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:3568920.0004    51151794.9197.4526110:27
IMPULSE-3 MirA
2025-276X
66687
in space

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:5968940.0008    51052294.9597.446810:27
WISDOM A & B (Wideband Satellite Demonstrator Of Multimedia Services)
2025-276Y
66688
in space
Conjoined pair of 3U Cubesats. Separated from launch vehicle at 19:42 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:5168930.0004    51251794.9297.4426810:27
AC1-003
2025-276Z
66689
in space
Mission information to follow. Separated from launch vehicle at 20:03 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 19:2268930.0001    51351594.9197.4429510:27
ÑuSat 52 (Yvonne Brill)
2025-276AC
66692
in space
Small satellite from Satellogic of Argentina providing Earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Separated from launch vehicle at 20:03 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:3168920.0002    51351594.9097.4429810:27
YAM 9 (Yet Another Mission 9)
2025-276AE
66694
in space
Mission information to follow. Separated from launch vehicle at 20:04 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:2968920.0001    51251494.8997.4429210:27
IRIDE-MS1 Eaglet-2 1
2025-276AF
66695
in space
One satellite in an ESA Earth observation mission, led by the Italian government, that will consist of about sixty satellites in six constellations. Equipped with optical sensors.

One of eght similar satellites carried on this launch, all were placed into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:1768890.0001    51151294.8597.4415210:27
Pelican 6
2025-276AP
66703
in space
Mission information to follow. Separated from launch vehicle at 20:04 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 16:1068920.0001    51351594.9197.4428010:27
Flock 4H-1
2025-276AQ
66704
in space
3U Cubesat - part of Planet's Flock 4X cluster of second generation imaging satellites. Separated from launch vehicle at 19:56 UTC.

One of thirty similar satellites carried on the Transporter 15 launch. All are in similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:1968900.0001    51151394.8697.4418710:27
ÑuSat 51 (Beatrice Tinsley)
2025-276CC
66740
in space
Small satellite from Satellogic of Argentina providing Earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Separated from launch vehicle at 20:06 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 18, 17:4068910.0002    51251494.8897.44261
Black Kite 1
2025-276CD
66741
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:2668920.0001    51251494.8997.4422510:27
Mercury 1
2025-276CE
66742
in space
Mission information to follow. Separated from launch vehicle at 20:05 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:3968910.0001    51251494.8897.4421010:27
ÑuSat 47 (Melina Furman)
2025-276CF
66743
in space
Small satellite from Satellogic of Argentina providing Earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Separated from launch vehicle at 20:04 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 19, 03:1368920.0000    51351494.9097.4427810:27
AC1 001
2025-276CG
66744
in space
Mission information to follow. Separated from launch vehicle at 20:04 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 19, 03:1468920.0001    51351594.9197.4427210:27
AC2 002
2025-276CH
66745
in space
Mission information to follow. Separated from launch vehicle at 20:06 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:2868920.0001    51351494.9097.4424310:27
Varda W-5
2025-276CK
66747
Re-entered - 2026 Jan 29
Life 62 days
Mission information to follow. Separated from launch vehicle at 20:08 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 16:0668920.0001    51351494.8997.4423310:27
Umbra 11
2025-276CL
66748
in space
Mission information to follow. Separated from launch vehicle at 20:04 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 19:0768890.0002    51051294.8497.4424010:27
PIAST S1
2025-276CM
66749
in space
Mission information to follow. Separated from launch vehicle at 20:03 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:2268910.0001    51151394.8797.4421210:27
ICEYE X-58
2025-276CP
66751
in space
Mission information to follow. Separated from launch vehicle at 20:03 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 11:1768910.0002    51151494.8897.4422910:27
ICEYE X-59
2025-276CQ
66752
in space
Mission information to follow. Separated from launch vehicle at 20:09 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 16:0568910.0002    51251494.8997.4426410:27
ICEYE X-60
2025-276CR
66753
in space
Mission information to follow. Separated from launch vehicle at 20:02 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 16:1068920.0001    51351594.9097.4430710:27
ICEYE X-61
2025-276CS
66754
in space
Mission information to follow. Separated from launch vehicle at 20:02 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:2168910.0002    51151494.8797.4421510:27
ICEYE X-62
2025-276CT
66755
in space
Mission information to follow. Separated from launch vehicle at 20:05 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 03:2668910.0001    51351494.8997.4427410:27
Mauve
2025-276CU
66756
in space
Mission information to follow. Separated from launch vehicle at 19:44 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:3468900.0001    51151394.8797.4416910:27
PIAST S2 (Polish ImAging SaTellite S2)
2025-276CV
66757
in space
Mission information to follow. Separated from launch vehicle at 19:44 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:3368900.0001    51151394.8697.4416510:27
PIAST M (Polish ImAging SaTellite M)
2025-276CW
66758
in space
Mission information to follow. Separated from launch vehicle at 19:43 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:3368900.0001    51151294.8697.4414510:27
HydroGNSS Scout 1
2025-276DA
66762
in space
Mission information to follow. Separated from launch vehicle at 20:03 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:4668920.0001    51351594.9197.4429710:27
HydroGNSS Scout 2
2025-276DB
66763
in space
Mission information to follow. Separated from launch vehicle at 20:06 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 19:1868920.0001    51351594.9097.4426910:27
Nahla
2025-276DC
66764
in space
Mission information to follow. Separated from launch vehicle at 20:04 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 17:3868910.0002    51251494.8897.4421610:27
T.Microsat 1
2025-276DE
66766
in space
Mission information to follow. Separated from launch vehicle at 19:40 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 14:1768890.0002    50951294.8497.449410:27
Accenture 1
2025-276DF
66767
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 19, 04:3268890.0002    51051294.8597.449310:27
SpeQtre
2025-276DH
66769
in space
Mission information to follow. Separated from launch vehicle at 19:40 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 19, 04:3068890.0003    50951394.8497.4411210:27
Lilium 3
2025-276DJ
66770
in space
Mission information to follow. Separated from launch vehicle at 19:41 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 19, 04:3068890.0003    50951394.8497.4513110:27
GyeonggiSat 1
2025-276DK
66771
in space
6U Cubesat owned by the Gyeonggi local government region of South Korea. Equipped with an imaging system to be used to study changes in urban areas brought about by climate change. Separated from launch vehicle at 19:40 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 14:1568890.0003    50951394.8497.4512310:27
IHI-Sat 2
2025-276DL
66772
in space
Mission information to follow. Separated from launch vehicle at 19:38 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 18:5768880.0003    50851294.8297.4511010:27
GENA- OT 1
2025-276DN
66774
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 18:5868880.0003    50851294.8397.4410710:27
LUNA 1
2025-276DR
66777
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 19, 04:2368870.0003    50751294.8197.4512010:27
Foresail 1 prime
2025-276DS
66778
in space
Mission information to follow.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 18, 19:2668940.0003    51451994.9597.444110:27
ION SCV 022 (Stellar Stephanus)
2025-276DT
67483
in space
Satellite carrier from D-Orbit equipped with customer-suppled experiments/sensors and Cubesat deployers for later release of satellites. Separated from launch vehicle at 20:07 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Jan 20, 16:3269520.0010    56758196.1597.5426610:25
2026 Jan 30, 18:4069530.0011    56758396.1797.5422410:24
2026 Feb 3, 04:2869540.0011    56858496.1997.5320810:24
2026 Feb 19, 18:2769530.0012    56758496.1797.5414910:23
FossaSat-2E 22
2025-276DU
66779
in space
Mission information to follow.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Jan 29, 10:2168920.0004    51151794.9097.4325810:26
FossaSat-2E 24
2025-276DV
66780
in space
Mission information to follow.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Jan 28, 16:4368910.0003    51051594.8897.4325210:26
Lacuna 4 (Lemur-2 Celijo-SB-PK)
2025-276DW
66781
in space
4U Cubesat from Spire, providing broadband communications for internet connected devices. Released from ION SCV Stellar Stephanius (67483, 2025-276DT).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Feb 19, 18:2169510.0011    56558096.1297.5416510:23
Lemur-2 (Finnian)
2025-276DX
66782
in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Released from one of the D-Orbit satellite carriers during 2026 February.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Mar 19, 14:4469470.0007    56457496.0597.538110:21
Lemur-2 (Starlight)
2025-276DY
66783
in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Released from ION SCV Stellar Stephanus (67483, 2025-276DT) probably 2026 January.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Mar 19, 15:0469510.0017    56258596.1397.537710:20
Lemur-2 (Tartiflette)
2025-276DZ
66784
in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Released from ION SCV Stellar Stephanius (67483, 2025-276DT).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Mar 19, 14:5569520.0016    56258496.1397.538410:20
Lemur-2 (Vukasin)
2025-276EA
66785
in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Released from one of the D-Orbit satellite carriers during 2026 February.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Mar 19, 15:0369480.0011    56257796.0597.538310:21
Lemur-2 (Hotspur-Tom)
2025-276EB
66786
in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Released from ION SCV Galactic Georgius (66682, 2025-276S) 2026 January.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Mar 19, 14:4069520.0016    56258596.1497.538010:20
Lemur-2 (Myra)
2025-276EC
66787
in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Released from one of the D-Orbit satellite carriers during 2026 February.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2026 Mar 24, 22:1469480.0013    56157896.0597.536710:20
FossaSat-2E 23
2025-276ED
66788
in space
Mission information to follow.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
3UCubed A
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:47 UTC.
Orbit parameters awaited
AE5Ra
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:45 UTC.
Orbit parameters awaited
AE5Rb
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:46 UTC.
Orbit parameters awaited
AE5Rc
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:42 UTC.
Orbit parameters awaited
AI Express 1 plus (AIX-1+)
2025-276xx
in space
3U Cubesat developed co-operatively by D-Orbit and AI Express. Carries an Earth observation payload supported by an AI system and blockchain computing. Released from ION SCV Stellar Stephanius (67483, 2025-276DT).
Orbit parameters awaited
ANISC (Azerbaijan National Satellite Innovation Competition)
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.
Orbit parameters awaited
CTC-1 A
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:41 UTC.
Orbit parameters awaited
CTC-1 B
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:43 UTC.
Orbit parameters awaited
CTC-1 C
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:43 UTC.
Orbit parameters awaited
FGN Tug S01
2025-276xx
in space
Satellite carrier vehicle from Turkish company Fergani Space. Separated from launch vehicle at 20:05 UTC. Orbit reportedly raised to 700 km December 6 in a two-part manoeuvre beginning at 04:46 UTC. Spacetrack has not released any data showing an object at that height.
Orbit parameters awaited
HCT Sat 2
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:40 UTC.
Orbit parameters awaited
Lacuna 3
2025-276xx
in space
4U Cubesat from Spire, providing broadband communications for internet connected devices. Released from ION SCV Stellar Stephanius (67483, 2025-276DT).
Orbit parameters awaited
Lacuna 5
2025-276xx
in space
4U Cubesat from Spire, providing broadband communications for internet connected devices. Released from ION SCV Galactic Georgius (66682, 2025-276S).
Orbit parameters awaited
Lacuna 6
2025-276xx
in space
4U Cubesat from Spire, providing broadband communications for internet connected devices. Released from ION SCV Galactic Georgius (66682, 2025-276S).
Orbit parameters awaited
LEO Express 3
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 20:03 UTC.
Orbit parameters awaited
PHASMA Dirac
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:41 UTC.
Orbit parameters awaited
PHASMA Lamarr
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:41 UTC.
Orbit parameters awaited
PHI 1
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:38 UTC.
Orbit parameters awaited
PW6U
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:40 UTC.
Orbit parameters awaited
SARI 1
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.
Orbit parameters awaited
SARI 2
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.
Orbit parameters awaited
SPiN (Space Products and Innovation)
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:40 UTC.
Orbit parameters awaited
Toro 2
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:38 UTC.
Orbit parameters awaited
TRYAD 1 (Terrestrial Rays Analysis and Detection)
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:40 UTC.
Orbit parameters awaited
TRYAD 2 (Terrestrial Rays Analysis and Detection)
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:39 UTC.
Orbit parameters awaited
Veery Fledgling V0.5 (Veery 0G)
2025-276xx
in space
Mission information to follow. Separated from launch vehicle at 19:40 UTC.
Orbit parameters awaited
FRG-10D1
2025-276xx?
in space
6U Cubesat - demonstrator of technology to be used by a Turkish GPS system. Reportedly separated from FGN Tug S01 into 700 km orbit Dec 6 at 08:45 UTC. Spacetrack has not released any data showing an object at that height. Separation from FGN Tug S01 is not confirmed.
Orbit parameters awaited


2025-277
CZ 7A
Wenchang Space Centre
2025 Nov 30, 12:20 UTC
Shijian 28 (Practice 28)
2025-277A
66549
in space
Mission not revealed but they may be used for detecting and tracking other satellites in space.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Nov 30, 18:06243830.7301    20435806631.5214.43180
2025 Dec 11, 05:12421640.0001    35783357891436.085.02129116°.9 E
CZ 7A fourth stage
2025-277B
66550
Re-entered - 2026 Jan 25
Life 56 days
Launched Shijian 28

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Nov 30, 08:01235910.7237    13934286600.9914.43178


2025-278
Falcon 9 Block 5 (Starlink Group 06-086)
Kennedy Space Center
2025 Dec 1, 07:44 UTC
Starlink 35867
2025-278A
66791
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 10, 12:0066740.0002    29429790.4343.00268
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 1
Life <1 day
Launched Starlink Group 06-086. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-279
Vega-C
Centre Spatiale Guyanaise
2025 Dec 1, 17:21 UTC
Kompsat 7 (Arirang 7)
2025-279A
66820
in space
KOrea Multi-Purpose SATellite to be used to support Geographical Information Systems, environmental, agricultural and oceanographic monitoring. There may also be a miltary/strategic imaging role. Replacement for KOMPSAT 3A (40536, 2015-014A). Separated from launch vehicle at 18:05 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 1, 20:3569500.0010    56557996.1197.6425502:04
Vega upper stage (Avum+)
uncatalogued
Re-entered - 2025 Dec 1
Life <1 day
Launched KOMPSAT 7. An engine firing at 19:12 UTC on the day of launch led to re-entry about 45 minutes later.
Not Catalogued - orbit parameters unavailable


2025-280
Falcon 9 Block 5 (Starlink Group 15-010)
Vandenberg Space Force Base
2025 Dec 2, 05:28 UTC
Starlink 35966
2025-280A
66821
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 10, 16:0066880.0004    30831390.7369.99271
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 2
Life <1 day
Launched Starlink Group 15-010. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-I05
Nanoracks Cubesat Deployer (NRCSD 29)
International Space Station
2025 Dec 2, 08:10 UTC
Duplex (Dual Propulsion Experiment)
1998-067XS
66906
in space
6U Cubesat from CU Aerospce to demonstrate new types of microthruster using materials than can be safely handled.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 4, 20:4567950.0004    41442092.9051.63169


2025-I06
Nanoracks Cubesat Deployer (NRCSD 29)
International Space Station
2025 Dec 2, 08:20 UTC
Silversat
1998-067XV
66909
Re-entered - 2026 Apr 23
Life 142 days
1U Cubesat from a school in Maryland. Designed to take photographs of the earth and send them out a social media messages on 'X'.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 4, 23:5067940.0005    41242092.8951.63186
ContentCube
1998-067xx
in space
1U Cubesat from a student team at Virginia Tech, designed to demonstrate operation of an OLED display screen in space.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 4, 20:4567950.0004    41442092.9051.63169
CU Alpha
1998-067xx
in space
1U Cubesat to study the properties of a highly reflective sail capable of being used for a laser-reflective satellite attitude control system.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 4, 20:4567950.0004    41442092.9051.63169
RHOK-Sat
1998-067xx
in space
1U Cubesat built as a co-operative project between Rhodes College and the University of Oklahoma's Photovoltaic Materials and Devices group. Carries experimental solar cells and equipment to measure their performance.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 4, 20:4567950.0004    41442092.9051.63169


2025-I07
Nanoracks Cubesat Deployer (NRCSD 29)
International Space Station
2025 Dec 2, 09:50 UTC
EagleSat 2
1998-067xx
in space
3U CubeSat built by the Embry-Riddle Aeronautical University - carries a scientific payload measuring energy and incident direction of high-energy cosmic rays, beta particles, gamma rays, and x-rays.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 4, 20:4567950.0004    41442092.9051.63169
Foras Promineo
1998-067xx
in space
3U Cubesat from Perkins High School in the US. carries a remote controlled robotics payload to be controlled from the ground as a game.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 4, 20:4567950.0004    41442092.9051.63169


2025-281
Falcon 9 Block 5 (Starlink Group 06-095)
Cape Canaveral Space Force Station
2025 Dec 2, 22:18 UTC
Starlink 36091
2025-281A
66848
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 10, 16:0066660.0002    28728990.2743.00281
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 3
Life 1 day
Launched Starlink Group 06-095. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-282
Zhuque-3 (Y-1)
Jiuquan Space Centre - Dongfeng Commercial Zone
2025 Dec 3, 04:00 UTC
Zhuque 3 second stage
2025-282A
66877
Re-entered - 2026 Jan 30
Life 58 days
Instrumented rocket stage from first test flight of new design of launch vehicle. Launch vehicle was intended to demonstrate landing of its first stage to allow re-use but the test was unsuccessful.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 3, 10:0871510.0881    1431403100.3056.96204


2025-283
Falcon 9 Block 5 (Starlink Group 11-025)
Vandenberg Space Force Base
2025 Dec 4, 20:42 UTC
Starlink 35866
2025-283A
66878
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 12, 20:0066690.0001    29029290.3453.1558
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 4
Life <1 day
Launched Starlink Group 11-025. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-284
Kuaizhou-1A-Pro
Jiuquan Space Centre
2025 Dec 5, 09:00 UTC
Jiaotong VDES A (VHF Data Exchange System A, VDES-A)
2025-284A
66913
in space
Relay satellites for VDES messages to/from ships at sea. VDES is an enhanced version of AIS.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 5, 19:3068840.0013    49751594.7380.40252
2025 Dec 8, 20:1168880.0008    50451594.8180.41259
2025 Dec 16, 08:2968950.0020    50353194.9680.41163
2025 Dec 20, 20:2869180.0014    53054995.4480.40268
2025 Dec 30, 04:2269500.0016    56058396.1080.40224
2026 Jan 3, 14:2869670.0020    57660396.4680.40299
2026 Jan 7, 20:1870130.0068    58768297.4180.40311
2026 Jan 8, 22:2170240.0052    61068397.6580.40310
2026 Jan 9, 14:4170470.0020    65468398.1180.40303
2026 Jan 10, 21:5370720.0016    68370598.6580.40104
2026 Jan 11, 22:4070960.0048    68375299.1580.40112
2026 Jan 12, 23:3671210.0083    68480299.6880.40108
2026 Jan 16, 15:0072220.0036    817869101.7980.41299
2026 Jan 17, 21:4172520.0007    869879102.4480.4168
2026 Jan 22, 23:1572810.0010    896911103.0680.40269
Jiaotong VDES B (VHF Data Exchange System-B, VDES-B)
2025-284B
66914
in space
One of a pair of simultaneously-launched relay satellites for VDES messages to/from ships at sea. They act as demonstrators for planned future constellation. VDES is an enhanced version of AIS.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 7, 23:3868840.0013    49751494.7380.40245
2025 Dec 9, 15:1068880.0008    50451594.8180.41257
2026 Jan 7, 20:1470130.0066    58868197.4180.39320
2026 Jan 8, 22:1770250.0048    61368197.6680.39317
2026 Jan 9, 14:3870470.0018    65668298.1280.39299
2026 Jan 10, 21:5070710.0015    68270498.6280.40116
2026 Jan 11, 22:3770960.0050    68375399.1580.40121
2026 Jan 12, 23:3271210.0084    68380399.6780.41114
2026 Jan 14, 22:2271660.0031    765810100.6180.40100
2026 Jan 16, 14:5672210.0037    816869101.7780.39296
2026 Jan 17, 21:3672520.0005    870878102.4480.40107
2026 Jan 21, 11:1872810.0011    895911103.0580.40268
2026 Jan 23, 14:5172810.0010    896911103.0680.40264
Kuaizhou 1A third stage
uncatalogued
Re-entered - 2025 Dec 5
Life <1 day
Launched pair of VDES satellites.
Not Catalogued - orbit parameters unavailable


2025-285
CZ 8A
Wenchang Space Centre - Hainan Commercial Zone
2025 Dec 6, 07:53 UTC
Hulianwang Digui 14-01 (Satellite Low Orbit Internet Group 14-01)
2025-285A
66915
in space
One of nine simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 8, 20:4172530.0008    869881102.4650.00270
CZ 8A third stage
2025-285K
66924
in space
Launched Hulianwang Digui group 14.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 8, 19:3971680.0119    705876100.6650.0193


2025-286
Falcon 9 Block 5 (Starlink Group 11-015)
Vandenberg Space Force Base
2025 Dec 7, 17:58 UTC
Starlink 35945
2025-286A
66925
in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 12, 20:0066610.0001    28228390.1653.1662
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 7
Life <1 day
Launched Starlink Group 11-015. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-287
CZ 6A
Taiyuan Space Centre
2025 Dec 8, 22:11 UTC
Hulianwang Digui 15-01 (Satellite Low Orbit Internet Group 15-01)
2025-287A
66953
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 10, 06:5573810.0008    9971009105.1886.50213
Hulianwang Digui 15-02 (Satellite Low Orbit Internet Group 15-02)
2025-287B
66954
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 10, 06:5573810.0008    9971009105.1786.50212
Hulianwang Digui 15-04 (Satellite Low Orbit Internet Group 15-04)
2025-287D
66956
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 10, 06:5473800.0007    9971007105.1686.50200
Hulianwang Digui 15-05 (Satellite Low Orbit Internet Group 15-05)
2025-287E
66957
in space
One of five simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 10, 06:5473790.0007    9961006105.1586.49198
CZ 6A third stage
2025-287F
66958
in space
Launched Hulianwang Digui group 15.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 10, 06:2072900.0107    833990103.2386.51110


2025-288
Falcon 9 Block 5 (Starlink Group 06-092)
Kennedy Space Center
2025 Dec 8, 22:26 UTC
Starlink 35887
2025-288A
66959
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 16, 14:0066770.0002    29830090.5143.00269
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 9
Life 1 day
Launched Starlink Group 06-092. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-289
CZ 4B
Jiuquan Space Centre
2025 Dec 9, 03:41 UTC
Yaogan 47
2025-289A
66988
in space
Described as being used for remote sensing for natural resources surveys. Specific tasks include land survey, crop yield assessment, and input to disaster monitoring and prevention plans. Mission is probably military or government optical imaging.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 9, 15:4468530.0009    46948294.1097.5327010:00
2025 Dec 10, 10:3568730.0003    49249794.5097.5218810:00
2025 Dec 11, 14:5868750.0001    49649794.5497.537410:00
CZ 4B third stage
2025-289B
66989
Re-entered - 2026 Mar 6
Life 87 days
Launched Yaogan 47.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 9, 21:3667480.0153    26747391.9597.5314


2025-290
CZ 3B
Xichang Space Centre
2025 Dec 9, 15:08 UTC
Tongxin Jishu Shiyan 22 (Communication Technology Test 22, TJS 22)
2025-290A
66990
in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Dec 9, 10:19243800.7302    19935805631.4128.43180
2025 Dec 18, 08:47421630.0004    35769358001436.001.9733566°.5 E
CZ 3B fourth stage
2025-290B
66991
in space
Launched TJS-22.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 10, 06:44237200.7241    16534518605.9328.45179


2025-291
Falcon 9 Block 5 (NRO L-77)
Cape Canaveral Space Force Station
2025 Dec 9, 19:16 UTC
USA 570 (NOSS 3-11?)
2025-291A
66992
in space
US government satellite from the National Reconnissance Office. Probably a NOSS ocean surveillance mission. Orbit information based on amateur observations.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 26, 19:1174840.0127    10111201107.3963.44182
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 9
Life <1 day
Launched USA 570. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable


2025-292
Lijian 1, Kinetica 1 (Y-11)
Jiuquan Space Centre - Dongfeng Commercial Zone
2025 Dec 10, 04:03 UTC
Alianqiu 813
2025-292B
66994
in space
Optical imaging satellite for Earth studies - built by China for the UAE.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 11, 21:0169310.0014    54356395.7197.65277
Dongpo Zhian 15 (Dongpo 15)
2025-292xx
in space
Radar imaging satellite for Earth studies.
Orbit parameters awaited
Jilin-1 High Resolution 07B 01 (Jilin-1 GF07B 01)
2025-292xx
in space
High resolution, multi-spectral imaging satellite.

One of eight similar satellites carried on this launch, all are in similar orbits
Orbit parameters awaited
Jilin-1 High Resolution 07C 01 (Jilin-1 GF07C 01)
2025-292xx
in space
High resolution, multi-spectral imaging satellite.

One of eight similar satellites carried on this launch, all are in similar orbits
Orbit parameters awaited
Jilin-1 High Resolution 07D 01 (Jilin-1 GF07D 01)
2025-292xx
in space
High resolution, multi-spectral imaging satellite.

One of eight similar satellites carried on this launch, all are in similar orbits
Orbit parameters awaited
Slippers 2
2025-292xx
in space
1U Cubesat from Nepal equipped with an Earth imaging system and an amateur radio package.
Orbit parameters awaited
SPNEX
2025-292xx
in space
Earth imaging and plasma studies satellite developed by China for Egypt.
Orbit parameters awaited
Yuxing 2-09
2025-292xx
in space
High resolution Earth imaging satellite.
Orbit parameters awaited
Lijian 1 third stage
2025-292K
67002
Re-entered - 2026 Mar 5
Life 85 days
Launched cluster of small satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 11, 22:4967830.0222    25455592.6597.729


2025-293
Falcon 9 Block 5 (Starlink Group 15-011)
Vandenberg Space Force Base
2025 Dec 10, 11:40 UTC
Starlink 35660
2025-293A
67003
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 17, 20:0066610.0004    28028690.1769.99267
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 10
Life <1 day
Launched Starlink Group 15-011. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-294
Falcon 9 Block 5 (Starlink Group 06-090)
Cape Canaveral Space Force Station
2025 Dec 11, 22:01 UTC
Starlink 36138
2025-294A
67030
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 17, 20:0066670.0002    28829090.3043.00276
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 11
Life <1 day
Launched Starlink Group 06-090. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-295
CZ 12
Wenchang Space Centre - Hainan Commercial Zone
2025 Dec 11, 23:00 UTC
Hulianwang Digui 16-01 (Satellite Low Orbit Internet Group 16-01)
2025-295A
67059
in space
One of nine simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation.

All satellites were injected into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 12, 05:0671840.0014    796815100.9950.00248
CZ 12 second stage
2025-295K
67068
in space
Launched Hulianwang Digui group 16.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 19, 11:4771330.0057    71479599.9249.99160


2025-296
Kuaizhou 11
Jiuquan Space Centre
2025 Dec 13, 01:08 UTC
Xi Wang 5-02 (XW-5)
2025-296A
67069
in space
Mission unclear but the name suggests it carries an amateur radio payload.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 15, 23:5168930.0014    50552594.9341.3545
2025 Dec 17, 13:4768940.0015    50652694.9441.3559
2025 Dec 23, 12:0068930.0015    50552594.9341.35103
2025 Dec 30, 04:0169060.0003    52553095.1841.35302
Dier 5-02 (B300-L02, Hope 5-02)
2025-296B
67070
in space
Two part satellite including a re-entry vehicle, developed by Beijing Ziwei Yutong Technology Co. Carries 34 payloads including one or more experimental Earth imaging systems.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 14, 08:2168920.0016    50352594.9141.3534
2025 Dec 16, 17:1368930.0016    50452794.9341.3653
Kuaizhou 11 third stage
2025-296C
67071
Re-entered - 2025 Dec 25
Life 12 days
Launched DIER 5-02 and one smaller satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 13, 03:5771310.0860    140136799.8941.34320


2025-297
Electron (RAISE And Shine)
Rocket Lab Launch Complex, New Zealand
2025 Dec 14, 03:09 UTC
RAISE 4 (RApid Innovative payload demonstration SatellitE 3)
2025-297B
67073
in space
Small satellite to carrying eight technology demonstration payloads developed by private companies, universities, and research institutions throughout Japan. One item isAxelspace's D-Sail to be deployed near mission end and use air drag to accelerate orbit decay.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 14, 22:5769230.0012    53755395.5497.4831315:30
Electron second stage
2025-297A
67072
Re-entered - 2025 Dec 24
Life 10 days
Launched RAISE 4.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 14, 22:1167330.0260    18052991.6397.48224
Electron third stage
2025-297C
67074
Re-entered - 2026 Feb 1
Life 49 days
Launched RAISE 4.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 14, 22:2267830.0209    26454792.6697.48262


2025-298
Falcon 9 Block 5 (Starlink Group 15-012)
Vandenberg Space Force Base
2025 Dec 14, 05:49 UTC
Starlink 36230
2025-298A
67075
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 20, 20:0066770.0004    29730290.5070.00269
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 14
Life <1 day
Launched Starlink Group 15-012. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-299
Falcon 9 Block 5 (Starlink Group 06-082)
Cape Canaveral Space Force Station
2025 Dec 15, 05:25 UTC
Starlink 36255
2025-299A
67102
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 20, 20:0066630.0002    28428790.2243.00270
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 15
Life <1 day
Launched Starlink Group 06-082. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-300
CZ 4B
Taiyuan Space Centre
2025 Dec 16, 03:17 UTC
Ziyuan 3-04
2025-300A
67131
in space
Remote sensing satellite equipped with a stereo mapping camera, a multispectral camera, and a laser altimeter to be used for imaging and cartography in support of geographic information resource construction, natural resource surveys and monitoring, land spatial planning and land use control, and natural resource supervision and enforcement. It will work together within Ziyuan 3-02 (41566, 2016-033A) and Ziyuan 3-03 (45939, 2020-051A).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 16, 05:5468700.0011    48450094.4597.5026910:36
2025 Dec 19, 14:1668800.0002    50150494.6697.4919010:37
CZ 4B third stage
2025-300B
67132
Re-entered - 2026 Mar 17
Life 91 days
Launched Ziyuan 3-04

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 16, 16:3667560.0174    26049592.1097.5616


2025-301
Atlas V 551 (LA-04, Kuiper Atlas 4)
Cape Canaveral Space Force Station
2025 Dec 16, 08:28 UTC
Kuiper 00144
2025-301A
67133
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from US company Amazon.

All satellites expected to be injected initially into similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 23, 18:0068380.0006    45646493.7951.87114
Atlas V third stage (Centaur)
uncatalogued
Re-entered - 2025 Dec 16
Life <1 day
Launched twenty seven Kuiper satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-302
Ariane 62 (VA-266)
Centre Spatiale Guyanaise
2025 Dec 17, 05:01 UTC
Galileo 33 (Galileo FOC FM-33)
2025-302A
67160
in space
One of a pair of simultaneously-launched Galileo FOC (Full Operation Capacity) satellites for the European Space Agency navigation system. Also carries a COSPAS-SARSAT search and rescue radio receiver to detect distress signals from the Earth's surface. Separated from launch vehicle at 03:57 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 18, 03:30293220.0008    2291922969832.8254.24238
Galileo 34 (Galileo FOC FM-34)
2025-302B
67161
in space
One of a pair of simultaneously-launched Galileo FOC (Full Operation Capacity) satellites for the European Space Agency navigation system. Also carries a COSPAS-SARSAT search and rescue radio receiver to detect distress signals from the Earth's surface. Separated from launch vehicle at 03:57 UTC.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 17, 13:37293150.0005    2292322951832.5454.23248
Ariane 6 third stage
2025-302C
67162
in space
Launched pair of Galileo satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 17, 13:37292970.0001    2291722920831.7554.24121


2025-303
Falcon 9 Block 5 (Starlink Group 06-099)
Kennedy Space Center
2025 Dec 17, 13:42 UTC
Starlink 35755
2025-303A
67163
in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 17, 14:3666490.0012    26327989.9343.01324
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 17
Life <1 day
Launched Starlink Group 06-099. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-304
Falcon 9 Block 5 (Starlink Group 15-013)
Vandenberg Space Force Base
2025 Dec 17, 15:27 UTC
Starlink 36182
2025-304A
67192
in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.

All satellites expected to be injected initially into similar orbits at about 300 km altitude.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 31, 20:1367340.0005    35335991.6770.00289
Falcon 9 second stage
uncatalogued
Re-entered - 2025 Dec 17
Life <1 day
Launched Starlink Group 15-013. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable


2025-305
Electron (Don't Be Such A Square, STP-S3)
Mid Atlantic Regional Space Port, Wallops Island
2025 Dec 18, 05:03 UTC
DiskSat 1
2025-305A
67219
in space
One of a cluster of four simultaneously-launched DiskSats. US government/military R&D mission but precise details not disclosed, although part of the mission was to demonstrate the DiskSat platform.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 20, 05:5769270.0004    54655295.6345.01275
DiskSat 2
2025-305B
67220
in space
One of a cluster of four simultaneously-launched DiskSats. US government/military R&D mission but precise details not disclosed, although part of the mission was to demonstrate the DiskSat platform.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 20, 05:5769270.0005    54655395.6445.01270
DiskSat 3
2025-305C
67221
in space
One of a cluster of four simultaneously-launched DiskSats. US government/military R&D mission but precise details not disclosed, although part of the mission was to demonstrate the DiskSat platform.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 20, 05:5769280.0005    54655395.6445.01283
DiskSat 4
2025-305D
67222
in space
One of a cluster of four simultaneously-launched DiskSats. US government/military R&D mission but precise details not disclosed, although part of the mission was to demonstrate the DiskSat platform.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 20, 04:2269280.0005    54755395.6545.01284
Electron third stage
2025-305E
67223
Re-entered - 2026 Apr 2
Life 105 days
Launched cluster of four DiskSats.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 20, 06:1268010.0179    30154593.0245.00149
Electron second stage
2025-305F
67224
Re-entered - 2026 Jan 7
Life 20 days
Launched cluster of four DiskSats.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 18, 18:2767520.0263    19755292.0345.02280


2025-306
CZ 5
Wenchang Space Centre
2025 Dec 19, 12:30 UTC
Tongxin Jishu Shiyan 23 (Communication Technology Test 23, TJS 23)
2025-306A
67226
in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Dec 21, 08:24293450.7754    21345721833.7916.40180
2025 Dec 31, 01:33421640.0002    35779357921436.065.97294175°.5 E
CZ 5 second stage
2025-306B
67227
in space
Launched Tongxin Jishu Shiyan 23 (TJS 23).

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 20, 19:22273290.7579    23941663749.3616.42179


2025-307
Electron (The Wisdom God Guides)
Rocket Lab Launch Complex, New Zealand
2025 Dec 21, 06:36 UTC
QPS-SAR-15 (Sukunami 1)
2025-307A
67228
in space
Commercial satellite from Japanese company iQPS, equipped with an Earth imaging radar. One in a constellation that will ultimately consist of 36 satellites.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 21, 08:4569540.0010    56958396.2042.01273
Electron third stage
2025-307B
67229
Re-entered - 2026 Jan 24
Life 34 days
Launched QPS-SAR-15.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 21, 08:4167860.0256    23558292.7342.00237
Electron second stage
2025-307C
67230
Re-entered - 2026 Jan 16
Life 26 days
Launched QPS-SAR-15.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 21, 08:4167800.0261    22557992.6041.98268


2025-F09 - failed to reach orbit
H3
Tanegashima Space Centre
2025 Dec 21, 19:34 UTC


2025-F10 - failed to reach orbit
Hanbit Nano
Alcantara Space Centre, Brazil
2025 Dec 23, 01:13 UTC


2025-308
CZ 12A
Jiuquan Space Centre - Dongfeng Commercial Zone
2025 Dec 23, 02:00 UTC
CZ 12A second stage
2025-308A
67231
Re-entered - 2025 Dec 28
Life 5 days
Instrumented rocket stage from first test flight of new design of launch vehicle. Launch vehicle was intended to demonstrate landing of its first stage to allow re-use but the test was unsuccessful.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 23, 11:5566000.0029    20324188.9469.71153


2025-309
LVM3 (M6)
Satish Dhawan Space Centre
2025 Dec 24, 03:25 UTC
BlueBird 6 (SpaceMobile 006)
2025-309A
67232
in space
Commercial 5G broadband satellite from US company AST Spacemobile, to provide direct mobile phone services from orbit.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 26, 18:0368910.0010    50652094.8853.00329
LVM3 third stage
2025-309B
67233
in space
Launched Bluebird 6.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 26, 17:5868860.0010    50151594.7852.94356


2025-310
Soyuz-2.1a
Plesetsk Cosmodrome
2025 Dec 25, 14:11 UTC
Obzor-R 1 (Obzor-R № 1)
2025-310A
67234
in space
Russian government Earth observation satellite equipped with an imaging radar.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 25, 23:1968030.0306    21763393.0797.977805:59
2025 Dec 27, 23:4769110.0152    42863895.2997.977305:59
2026 Jan 5, 05:3170270.0002    64765097.7097.974605:59
2026 Jan 7, 16:0670210.0001    64264497.5897.9720506:00
Soyuz third stage
2025-310B
67235
Re-entered - 2026 Mar 18
Life 83 days
Launched Obzor-R 1.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 25, 23:1868010.0303    21662993.0297.9777


2025-311
CZ 8A
Wenchang Space Centre
2025 Dec 25, 23:26 UTC
Hulianwang Digui 17-01 (Satellite Low Orbit Internet Group 17-01)
2025-311A
67236
in space
Internet communication satellite. Designed to fly in relatively-low orbit as part of a large constellation.

One of nine similar satellites carried on this launch. All were placed in similar orbits.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2026 Jan 4, 20:2872990.0006    916925103.4250.01303
CZ 8A third stage
2025-311K
67245
in space
Launched Hulianwang Digui group 17.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2026 Jan 6, 23:2772290.0089    786915101.9450.00124


2025-312
CZ 3B
Xichang Space Centre
2025 Dec 26, 16:07 UTC
Fengyun 4C (Fengyun 4-03)
2025-312A
67246
in space
Second generation meteorological imaging satellite capable of producing three-dimensional analyses of weather systems. Date of entry into Geosynchronous Drift Orbit not known.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Dec 26, 21:47243970.7308    19035847632.0628.47180
2026 Jan 7, 16:41421640.0003    35773357991436.070.0954133°.0 E
CZ 3B fourth stage
2025-312B
67247
in space
Launched Fengyun 4C.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 27, 17:43236600.7246    13834425603.6328.45180


2025-313
Soyuz-2.1b
Vostochny Cosmodrome
2025 Dec 28, 13:18 UTC
Multi-sats
2025-313A
67248
in space
Mission Description awaited
Orbit parameters awaited


2025-314
CZ 4B
Jiuquan Space Centre
2025 Dec 30, 04:12 UTC
Tianhui 7
2025-314A
67300
in space
Cartographic and imaging satellite.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
Desc Node
Local Time
2025 Dec 31, 12:4368680.0003    48849294.4197.414910:30
CZ 4B third stage
2025-314B
67301
Re-entered - 2026 Apr 4
Life 95 days
Launched Tianhui 7.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 30, 12:5567490.0150    27047291.9797.3817


2025-315
CZ 7A (Y-7)
Wenchang Space Centre
2025 Dec 30, 22:40 UTC
Shijian 29-01 (Practice 29-01)
2025-315A
67302
in space
One of a pair of related satellites in a dual launch, to be used for detecting and tracking other objects in orbit.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2025 Dec 30, 17:55243950.7296    21835817632.0119.51179
2026 Jan 9, 20:22421650.0001    35781357921436.103.0030173°.1 E
Shijian 29-02 (Practice 29-02)
2025-315C
67403
in space
One of a pair of related satellites in a dual launch, to be used for detecting and tracking other objects in orbit. Released from Shijian 29-01 around 2026 Jan 9.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
GEO    
Longitude
2026 Jan 13, 00:48421650.0001    35784357901436.103.0133373°.1 E
CZ 7A fourth stage
2025-315B
67303
in space
Launched Shijian 29-01 and 29-02.

epoch (UTC)         
s-m axis
( km )

eccentricity
perigee
( km )
apogee
( km )
period
( min )
incl 
( ° )
ω  
( ° )
2025 Dec 31, 04:18236720.7234    16934419604.1219.77179


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