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| 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.
2025-001 Falcon 9 Block 5 Cape Canaveral Space Force Station | 2025 Jan 4, 01:27 UTC | |
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, 00:37 | 33644 | 0.7977 | 429 | 54103 | 1023.57 | 26.91 | 178 | | | | 2025 Jan 12, 08:04 | 35003 | 0.7806 | 1301 | 55949 | 1086.24 | 24.51 | 181 | | | | 2025 Jan 21, 18:00 | 36130 | 0.7658 | 2082 | 57421 | 1139.08 | 20.40 | 182 | | | | 2025 Jan 29, 13:50 | 37689 | 0.7409 | 3385 | 59236 | 1213.60 | 17.14 | 184 | | | | 2025 Feb 5, 10:58 | 38998 | 0.7172 | 4652 | 60588 | 1277.40 | 14.64 | 185 | | | | 2025 Feb 11, 18:22 | 39974 | 0.6915 | 5953 | 61238 | 1325.62 | 12.65 | 187 | | | | 2025 Feb 18, 07:07 | 40883 | 0.6586 | 7577 | 61432 | 1371.10 | 10.71 | 188 | | | | 2025 Feb 25, 00:36 | 41578 | 0.6191 | 9460 | 60940 | 1406.22 | 8.93 | 189 | | | | 2025 Mar 5, 21:32 | 42156 | 0.5684 | 11815 | 59740 | 1435.63 | 7.23 | 191 | 163°.8 E | | | 2025 Mar 12, 00:00 | 42576 | 0.5276 | 13735 | 58659 | 1457.14 | 6.49 | 192 | | | | 2025 Mar 19, 03:07 | 41639 | 0.4986 | 14498 | 56023 | 1409.31 | 5.03 | 192 | | | | 2025 Mar 26, 09:29 | 40700 | 0.4676 | 15290 | 53354 | 1361.91 | 4.06 | 191 | | | | 2025 Apr 2, 07:21 | 43408 | 0.3630 | 21274 | 52785 | 1500.07 | 3.30 | 195 | | | | 2025 Apr 9, 18:37 | 43479 | 0.2996 | 24073 | 50128 | 1503.74 | 2.57 | 196 | | | | 2025 Apr 16, 02:32 | 44114 | 0.2513 | 26651 | 48819 | 1536.80 | 2.02 | 199 | | | | 2025 Apr 24, 11:59 | 45061 | 0.1863 | 30290 | 47076 | 1586.59 | 1.36 | 207 | | | | 2025 May 1, 13:09 | 43038 | 0.1073 | 32043 | 41277 | 1480.93 | 0.84 | 199 | | | | 2025 May 7, 00:54 | 43087 | 0.0537 | 34395 | 39022 | 1483.45 | 0.47 | 211 | | | | 2025 May 12, 04:11 | 42101 | 0.0084 | 35369 | 36076 | 1432.84 | 0.15 | 151 | 44°.2 E | | | 2025 May 16, 17:57 | 42164 | 0.0002 | 35780 | 35793 | 1436.08 | 0.10 | 250 | 44°.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, 13:41 | 33491 | 0.7972 | 414 | 53811 | 1016.59 | 26.84 | 178 | | | |
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, 11:32 | 24388 | 0.7310 | 182 | 35838 | 631.73 | 28.48 | 180 | | | | 2025 Jan 13, 19:03 | 42195 | 0.0064 | 35546 | 36088 | 1437.64 | 10.21 | 189 | 120°.1 E | | | 2025 Jan 14, 15:16 | 42166 | 0.0059 | 35540 | 36036 | 1436.17 | 10.21 | 185 | 120°.0 E | | | 2025 Jan 16, 08:07 | 42169 | 0.0058 | 35547 | 36034 | 1436.30 | 10.21 | 185 | 119°.9 E | | | 2025 Jan 16, 18:20 | 42162 | 0.0057 | 35545 | 36022 | 1435.94 | 10.21 | 184 | 119°.9 E | | | 2025 Jan 21, 14:14 | 42163 | 0.0056 | 35547 | 36023 | 1436.02 | 10.22 | 184 | 120°.1 E | | | 2025 Mar 27, 20:57 | 42163 | 0.0059 | 35535 | 36034 | 1435.98 | 10.35 | 183 | 119°.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, 01:00 | 24839 | 0.7372 | 151 | 36772 | 649.33 | 28.46 | 180 | | | |
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, 16:00 | 6680 | 0.0002 | 301 | 303 | 90.56 | 43.00 | 282 | | | | 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, 03:44 | 6675 | 0.0003 | 295 | 299 | 90.47 | 43.01 | 252 | | | | 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, 17:19 | 6899 | 0.0001 | 521 | 522 | 95.05 | 70.00 | 172 | | | | 2025 Mar 24, 01:50 | 6922 | 0.0002 | 542 | 545 | 95.52 | 70.00 | 278 | | | | 2025 Apr 11, 20:27 | 6955 | 0.0002 | 576 | 578 | 96.21 | 70.00 | 174 | | | | 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, 18:00 | 6692 | 0.0002 | 313 | 315 | 90.80 | 43.01 | 277 | | | | 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, 11:01 | 7021 | 0.0013 | 634 | 652 | 97.59 | 54.98 | 297 | | | | 2026 Jan 1, 04:17 | 7233 | 0.0009 | 848 | 861 | 102.03 | 54.97 | 263 | | | | 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, 10:45 | 6813 | 0.0321 | 216 | 654 | 93.28 | 54.94 | 359 | | | |
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, 20:00 | 6676 | 0.0002 | 296 | 299 | 90.47 | 43.01 | 279 | | | | 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 | |
in space
|
| Payload list to follow. |
| |
2025-010 Falcon 9 Block 5 Kennedy Space Center | 2025 Jan 15, 06:11 UTC | |
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 | | |
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, 07:37 | 187730 | 0.9651 | 176 | 362529 | 13491.54 | 35.17 | 346 | | | |
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, 08:37 | 17210 | 0.4894 | 2409 | 19254 | 374.47 | 30.00 | 267 | | | |
2025-012 CZ 2D Jiuquan Space Centre | 2025 Jan 17, 04:07 UTC | |
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, 22:52 | 6901 | 0.0008 | 517 | 528 | 95.08 | 97.48 | 273 | 10:25 | | | 2025 Jan 20, 15:38 | 6902 | 0.0009 | 518 | 529 | 95.10 | 97.48 | 262 | 10:25 | | | 2025 May 7, 04:25 | 6891 | 0.0008 | 507 | 518 | 94.88 | 97.46 | 246 | 10:24 | | | 2025 Oct 12, 14:51 | 6891 | 0.0008 | 507 | 519 | 94.88 | 97.45 | 75 | 10:24 | | | 2026 Mar 5, 22:36 | 6891 | 0.0005 | 509 | 516 | 94.88 | 97.43 | 238 | 10:22 | | | 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, 15:21 | 6901 | 0.0009 | 517 | 529 | 95.09 | 97.48 | 281 | 10:25 | | | 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, 15:23 | 6901 | 0.0009 | 517 | 530 | 95.09 | 97.49 | 270 | 10:25 | | | 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, 15:23 | 6902 | 0.0008 | 518 | 530 | 95.12 | 97.48 | 266 | | | |
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, 00:37 | 6917 | 0.0014 | 529 | 548 | 95.41 | 97.61 | 282 | 16:29 | | | 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, 00:38 | 6916 | 0.0014 | 528 | 548 | 95.41 | 97.60 | 284 | 16:29 | | | 2025 Feb 1, 12:48 | 6918 | 0.0013 | 531 | 549 | 95.45 | 97.61 | 254 | 16:30 | | | 2025 Feb 2, 14:16 | 6920 | 0.0013 | 533 | 551 | 95.48 | 97.61 | 256 | 16:30 | | | 2025 Feb 3, 12:34 | 6921 | 0.0013 | 534 | 552 | 95.51 | 97.61 | 258 | 16:30 | | | 2025 Feb 4, 12:27 | 6922 | 0.0013 | 535 | 553 | 95.52 | 97.61 | 259 | 16:30 | | | 2025 Feb 6, 17:02 | 6924 | 0.0014 | 536 | 556 | 95.57 | 97.61 | 258 | 16:30 | | | 2025 Feb 23, 18:39 | 6926 | 0.0014 | 538 | 558 | 95.60 | 97.61 | 202 | 16:30 | | | 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, 00:39 | 6916 | 0.0014 | 528 | 548 | 95.40 | 97.61 | 285 | 16:29 | | | 2025 Feb 11, 09:47 | 6917 | 0.0015 | 529 | 549 | 95.42 | 97.61 | 216 | 16:30 | | | 2025 Feb 12, 00:07 | 6920 | 0.0016 | 531 | 553 | 95.49 | 97.60 | 225 | 16:30 | | | 2025 Feb 13, 04:47 | 6921 | 0.0015 | 533 | 554 | 95.51 | 97.61 | 225 | 16:30 | | | 2025 Feb 17, 13:58 | 6926 | 0.0015 | 538 | 558 | 95.61 | 97.61 | 227 | 16:30 | | | 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, 00:38 | 6916 | 0.0014 | 528 | 548 | 95.40 | 97.60 | 289 | 16:29 | | | 2025 Feb 23, 17:37 | 6914 | 0.0015 | 526 | 546 | 95.36 | 97.61 | 166 | 16:30 | | | 2025 Feb 25, 14:09 | 6917 | 0.0013 | 530 | 548 | 95.42 | 97.61 | 165 | 16:30 | | | 2025 Feb 26, 12:26 | 6918 | 0.0012 | 532 | 549 | 95.45 | 97.61 | 166 | 16:30 | | | 2025 Mar 1, 10:30 | 6922 | 0.0010 | 537 | 551 | 95.53 | 97.61 | 176 | 16:31 | | | 2025 Mar 6, 10:03 | 6925 | 0.0009 | 541 | 554 | 95.59 | 97.61 | 186 | 16:31 | | | 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, 05:06 | 6916 | 0.0014 | 528 | 547 | 95.39 | 97.61 | 284 | 16:29 | | | 2025 Feb 18, 05:39 | 6915 | 0.0014 | 527 | 547 | 95.38 | 97.61 | 187 | 16:30 | | | 2025 Feb 21, 02:06 | 6920 | 0.0012 | 534 | 550 | 95.49 | 97.61 | 193 | 16:30 | | | 2025 Feb 24, 11:22 | 6926 | 0.0009 | 542 | 554 | 95.60 | 97.61 | 209 | 16:30 | | | 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, 17:28 | 6692 | 0.0004 | 311 | 317 | 90.80 | 43.01 | 231 | | | | 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, 17:29 | 6689 | 0.0003 | 308 | 313 | 90.73 | 43.01 | 234 | | | | 2025 Jan 29, 03:19 | 6696 | 0.0002 | 317 | 319 | 90.89 | 43.01 | 250 | | | | 2025 Feb 1, 14:29 | 6691 | 0.0003 | 311 | 315 | 90.79 | 43.01 | 251 | | | | 2025 Feb 11, 10:59 | 6723 | 0.0001 | 344 | 345 | 91.42 | 43.00 | 286 | | | | 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, 17:29 | 6688 | 0.0002 | 309 | 312 | 90.73 | 43.01 | 253 | | | | 2025 Jan 29, 03:18 | 6696 | 0.0001 | 317 | 318 | 90.88 | 43.01 | 251 | | | | 2025 Feb 2, 08:36 | 6689 | 0.0003 | 310 | 313 | 90.75 | 43.01 | 249 | | | | 2025 Feb 11, 14:00 | 6724 | 0.0002 | 344 | 347 | 91.45 | 43.00 | 213 | | | | 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, 20:00 | 6647 | 0.0002 | 268 | 270 | 89.88 | 53.16 | 316 | | | | 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, 19:17 | 7182 | 0.0016 | 792 | 815 | 100.95 | 88.99 | 167 | | | | 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, 20:11 | 7097 | 0.0103 | 646 | 792 | 99.17 | 89.03 | 66 | | | |
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, 19:46 | 24376 | 0.7306 | 189 | 35807 | 631.27 | 28.48 | 180 | | | | 2025 Feb 4, 14:52 | 42165 | 0.0002 | 35780 | 35794 | 1436.11 | 2.00 | 224 | 18°.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, 17:24 | 23672 | 0.7249 | 135 | 34452 | 604.09 | 28.56 | 179 | | | |
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, 16:00 | 6669 | 0.0001 | 290 | 291 | 90.33 | 53.15 | 77 | | | | 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, 20:00 | 6696 | 0.0002 | 317 | 319 | 90.89 | 43.00 | 266 | | | | 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, 06:56 | 25267 | 0.7412 | 162 | 37615 | 666.16 | 20.75 | 178 | | | | 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, 06:54 | 25142 | 0.7398 | 164 | 37364 | 661.25 | 20.74 | 178 | | | |
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, 09:48 | 40561 | 0.8320 | 437 | 67930 | 1354.97 | 26.85 | 178 | | | | 2025 Feb 3, 08:24 | 40768 | 0.8286 | 610 | 68170 | 1365.35 | 26.11 | 178 | | | | 2025 Feb 6, 04:55 | 41304 | 0.8234 | 917 | 68933 | 1392.32 | 24.72 | 179 | | | | 2025 Feb 13, 01:32 | 42493 | 0.8071 | 1821 | 70409 | 1452.89 | 21.70 | 180 | | | | 2025 Feb 20, 05:12 | 43510 | 0.7882 | 2836 | 71429 | 1505.39 | 18.61 | 181 | | | | 2025 Feb 27, 13:56 | 44030 | 0.7638 | 4021 | 71283 | 1532.45 | 15.89 | 182 | | | | 2025 Mar 7, 01:18 | 44242 | 0.7340 | 5389 | 70338 | 1543.50 | 13.36 | 184 | | | | 2025 Mar 14, 13:23 | 44377 | 0.7032 | 6792 | 69206 | 1550.61 | 11.41 | 185 | | | | 2025 Mar 21, 00:12 | 44474 | 0.6782 | 7936 | 68257 | 1555.69 | 9.91 | 186 | | | | 2025 Mar 28, 13:10 | 44342 | 0.6566 | 8850 | 67079 | 1548.78 | 8.98 | 187 | | | | 2025 Apr 3, 23:59 | 44301 | 0.6205 | 10434 | 65412 | 1546.62 | 7.60 | 188 | | | | 2025 Apr 11, 12:36 | 44487 | 0.5801 | 12300 | 63918 | 1556.38 | 6.36 | 189 | | | | 2025 Apr 18, 00:01 | 43478 | 0.5603 | 12738 | 61462 | 1503.72 | 5.48 | 189 | | | | 2025 Apr 24, 12:02 | 43429 | 0.5100 | 14904 | 59199 | 1501.19 | 4.51 | 190 | | | | 2025 May 2, 01:09 | 44079 | 0.4586 | 17487 | 57914 | 1534.98 | 3.78 | 192 | | | | 2025 May 8, 12:17 | 44090 | 0.4107 | 19603 | 55821 | 1535.58 | 3.14 | 194 | | | | 2025 May 15, 11:39 | 44146 | 0.3644 | 21679 | 53857 | 1538.50 | 2.53 | 195 | | | | 2025 May 22, 20:30 | 44461 | 0.3197 | 23867 | 52299 | 1554.99 | 1.97 | 197 | | | | 2025 May 27, 01:57 | 45143 | 0.2941 | 25490 | 52040 | 1590.91 | 1.67 | 198 | | | | 2025 Jun 3, 12:22 | 46333 | 0.2545 | 28165 | 51744 | 1654.21 | 1.13 | 206 | | | | 2025 Jun 7, 11:22 | 47039 | 0.2316 | 29767 | 51555 | 1692.20 | 1.15 | 205 | | | | 2025 Jun 12, 13:21 | 43043 | 0.1444 | 30450 | 42880 | 1481.20 | 0.96 | 190 | | | | 2025 Jun 15, 22:36 | 42684 | 0.1325 | 30651 | 41962 | 1462.73 | 0.91 | 191 | | | | 2025 Jun 30, 06:55 | 42388 | 0.0242 | 34984 | 37036 | 1447.53 | 0.24 | 192 | | | | 2025 Jul 3, 01:58 | 42161 | 0.0075 | 35465 | 36101 | 1435.90 | 0.15 | 196 | 33°.8 E | | | 2025 Jul 13, 20:26 | 42164 | 0.0001 | 35782 | 35791 | 1436.08 | 0.08 | 316 | 32°.9 E | | | 2025 Aug 22, 21:28 | 42164 | 0.0000 | 35786 | 35787 | 1436.08 | 0.03 | 182 | 28°.9 E | | | 2025 Sep 18, 23:39 | 42160 | 0.0001 | 35779 | 35786 | 1435.88 | 0.07 | 171 | 29°.8 E | | | 2025 Oct 14, 22:06 | 42157 | 0.0002 | 35772 | 35786 | 1435.70 | 0.14 | 183 | 31°.8 E | | | 2025 Nov 10, 21:25 | 42153 | 0.0003 | 35762 | 35788 | 1435.51 | 0.21 | 198 | 35°.2 E | | | 2025 Dec 6, 10:25 | 42168 | 0.0002 | 35782 | 35797 | 1436.25 | 0.28 | 124 | 39°.6 E | | | 2025 Dec 9, 17:56 | 42303 | 0.0003 | 35913 | 35937 | 1443.17 | 0.29 | 215 | 33°.9 E | | | 2025 Dec 12, 06:46 | 42303 | 0.0003 | 35913 | 35936 | 1443.15 | 0.29 | 218 | 29°.4 E | | | 2025 Dec 15, 06:40 | 42164 | 0.0001 | 35781 | 35790 | 1436.04 | 0.30 | 254 | 29°.1 E | | | 2026 Jan 8, 19:35 | 42165 | 0.0001 | 35782 | 35791 | 1436.09 | 0.26 | 265 | 29°.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, 23:21 | 39872 | 0.8335 | 262 | 66725 | 1320.57 | 26.93 | 177 | | | |
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, 20:00 | 6697 | 0.0001 | 318 | 319 | 90.90 | 53.15 | 46 | | | | 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, 10:47 | 6660 | 0.0012 | 274 | 290 | 90.15 | 53.17 | 248 | | | |
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, 10:49 | 24271 | 0.7212 | 390 | 35397 | 627.20 | 21.98 | 176 | | | | 2025 Feb 3, 13:02 | 26371 | 0.5824 | 4634 | 35352 | 710.32 | 12.98 | 175 | | | | 2025 Feb 5, 09:29 | 39739 | 0.0461 | 31527 | 35193 | 1313.95 | 0.56 | 170 | | | | 2025 Feb 10, 20:47 | 42115 | 0.0012 | 35685 | 35790 | 1433.57 | 0.08 | 57 | 90°.3 E | | | 2025 Feb 11, 20:31 | 42155 | 0.0003 | 35764 | 35790 | 1435.60 | 0.08 | 55 | 90°.4 E | | | 2025 Feb 12, 14:28 | 42163 | 0.0001 | 35780 | 35791 | 1436.03 | 0.08 | 34 | 90°.4 E | | | 2025 Feb 17, 22:43 | 42164 | 0.0001 | 35780 | 35792 | 1436.05 | 0.07 | 45 | 90°.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, 10:41 | 24245 | 0.7206 | 397 | 35336 | 626.15 | 21.97 | 175 | | | | 2025 Feb 6, 01:55 | 24116 | 0.7251 | 251 | 35225 | 621.18 | 21.48 | 178 | | | |
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, 20:00 | 6691 | 0.0001 | 312 | 314 | 90.78 | 43.00 | 265 | | | | 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, 01:09 | 7082 | 0.0006 | 700 | 709 | 98.86 | 45.04 | 97 | | | | 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, 01:10 | 6828 | 0.0025 | 433 | 467 | 93.59 | 44.97 | 21 | | | | 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, 18:17 | 6965 | 0.0011 | 579 | 594 | 96.41 | 81.99 | 275 | | | | 2025 Feb 19, 13:30 | 6967 | 0.0011 | 581 | 596 | 96.45 | 82.00 | 207 | | | | 2025 Dec 31, 17:36 | 6962 | 0.0009 | 578 | 590 | 96.36 | 82.00 | 250 | | | | 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, 11:47 | 6965 | 0.0015 | 576 | 597 | 96.41 | 81.99 | 260 | | | | 2025 Feb 15, 12:57 | 6967 | 0.0014 | 580 | 599 | 96.47 | 81.99 | 219 | | | | 2025 Feb 25, 12:39 | 6967 | 0.0011 | 581 | 596 | 96.45 | 82.00 | 187 | | | | 2025 Apr 6, 22:26 | 6966 | 0.0012 | 579 | 596 | 96.43 | 82.00 | 64 | | | | 2025 Apr 7, 14:31 | 6964 | 0.0013 | 576 | 595 | 96.39 | 82.00 | 54 | | | | 2025 Apr 7, 17:44 | 6966 | 0.0013 | 579 | 597 | 96.43 | 82.00 | 55 | | | | 2025 Jun 23, 09:10 | 6964 | 0.0009 | 579 | 592 | 96.39 | 82.00 | 155 | | | | 2025 Jun 23, 17:13 | 6965 | 0.0011 | 579 | 594 | 96.41 | 82.00 | 155 | | | | 2025 Dec 31, 17:41 | 6962 | 0.0009 | 578 | 591 | 96.36 | 82.00 | 250 | | | | 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, 19:49 | 6967 | 0.0013 | 580 | 598 | 96.45 | 81.99 | 267 | | | | 2025 Mar 19, 13:46 | 6965 | 0.0015 | 576 | 597 | 96.42 | 82.00 | 126 | | | | 2025 Dec 31, 17:36 | 6962 | 0.0009 | 578 | 590 | 96.35 | 81.99 | 268 | | | | 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, 23:41 | 6966 | 0.0014 | 578 | 597 | 96.43 | 82.01 | 127 | | | | 2025 Dec 31, 18:10 | 6957 | 0.0011 | 571 | 586 | 96.25 | 81.99 | 260 | | | | 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, 11:52 | 6964 | 0.0010 | 579 | 593 | 96.39 | 81.99 | 276 | | | | 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, 09:58 | 6772 | 0.0272 | 210 | 578 | 92.44 | 82.01 | 74 | | | |
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, 14:00 | 6678 | 0.0002 | 299 | 301 | 90.52 | 43.01 | 269 | | | | 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, 18:57 | 7021 | 0.0002 | 641 | 644 | 97.57 | 97.96 | 62 | 09:06 | | | 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, 20:35 | 7020 | 0.0002 | 641 | 643 | 97.56 | 97.96 | 48 | 09:06 | | | 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, 18:57 | 7020 | 0.0001 | 641 | 642 | 97.56 | 97.96 | 95 | 09:06 | | | 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, 18:56 | 7019 | 0.0001 | 640 | 642 | 97.54 | 97.96 | 329 | 09:06 | | | 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, 14:27 | 7019 | 0.0001 | 640 | 641 | 97.53 | 97.96 | 271 | 09:06 | | | 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, 00:46 | 6989 | 0.0043 | 581 | 641 | 96.92 | 97.93 | 42 | | | | 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, 19:43 | 6772 | 0.0315 | 180 | 607 | 92.44 | 97.96 | 222 | | | |
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, 16:00 | 6682 | 0.0001 | 303 | 304 | 90.60 | 53.15 | 58 | | | | 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, 15:42 | 7246 | 0.0008 | 863 | 874 | 102.32 | 50.00 | 257 | | | | 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, 15:36 | 7161 | 0.0119 | 698 | 868 | 100.51 | 50.00 | 83 | | | |
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, 18:00 | 6695 | 0.0002 | 315 | 318 | 90.86 | 43.00 | 291 | | | | 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, 16:00 | 6678 | 0.0001 | 299 | 300 | 90.51 | 43.01 | 243 | | | | 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, 14:19 | 6851 | 0.0008 | 468 | 479 | 94.07 | 59.00 | 325 | | | | 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, 14:24 | 6852 | 0.0007 | 469 | 478 | 94.07 | 59.00 | 354 | | | | 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, 06:29 | 6706 | 0.0227 | 175 | 479 | 91.08 | 59.00 | 268 | | | |
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, 16:00 | 6670 | 0.0001 | 291 | 292 | 90.35 | 53.16 | 50 | | | | 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, 20:00 | 6663 | 0.0002 | 284 | 286 | 90.21 | 43.00 | 289 | | | | 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, 18:01 | 24372 | 0.7298 | 206 | 35782 | 631.11 | 27.63 | 179 | | | | 2025 Mar 4, 19:06 | 42166 | 0.0002 | 35779 | 35796 | 1436.14 | 0.07 | 80 | 126°.0 E | | | 2025 Jun 2, 17:24 | 42248 | 0.0024 | 35770 | 35970 | 1440.36 | 0.29 | 89 | 124°.6 E | | | 2025 Jun 15, 11:30 | 42165 | 0.0004 | 35768 | 35805 | 1436.09 | 0.04 | 228 | 110°.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, 19:04 | 24363 | 0.7303 | 193 | 35777 | 630.76 | 27.69 | 180 | | | |
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, 16:00 | 6657 | 0.0004 | 276 | 281 | 90.08 | 69.99 | 275 | | | | 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 orbit | 190235 | 0.9654 | 212 | 367501 | 13762.38 | 28.52 | 216 | | | | 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 orbit | 190235 | 0.9654 | 212 | 367501 | 13762.38 | 28.52 | 216 | | | | |
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 orbit | 190235 | 0.9654 | 212 | 367501 | 13762.38 | 28.52 | 216 | | | |
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, 20:00 | 6683 | 0.0002 | 304 | 306 | 90.62 | 43.00 | 256 | | | | |
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, 13:25 | 6876 | 0.0012 | 489 | 506 | 94.56 | 97.31 | 243 | 13:30 | | | 2025 Mar 8, 17:47 | 6879 | 0.0000 | 501 | 501 | 94.63 | 97.31 | 67 | 13:29 | | | 2026 Jan 9, 07:41 | 6879 | 0.0002 | 500 | 502 | 94.64 | 97.34 | 74 | 13:15 | | | 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, 13:25 | 6876 | 0.0012 | 489 | 506 | 94.57 | 97.31 | 241 | 13:30 | | | 2025 Mar 5, 18:46 | 6879 | 0.0000 | 501 | 501 | 94.63 | 97.31 | 73 | 13:29 | | | 2026 Jan 9, 07:42 | 6879 | 0.0001 | 500 | 502 | 94.64 | 97.34 | 60 | 13:15 | | | 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, 11:34 | 6869 | 0.0016 | 480 | 501 | 94.42 | 97.14 | 323 | | | |
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, 04:51 | 6691 | 0.0006 | 309 | 317 | 90.78 | 51.63 | 312 | | | | 2025 Mar 2, 12:58 | 6796 | 0.0006 | 414 | 422 | 92.92 | 51.63 | 334 | | | | 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, 04:47 | 6580 | 0.0029 | 183 | 221 | 88.53 | 51.66 | 104 | | | |
2025-F01 - failed to reach orbit Kuaizhou-1A-Pro Jiuquan Space Centre | 2025 Mar 1, 10:00 UTC | |
|
| 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, 17:53 | 25526 | 0.0003 | 19140 | 19155 | 676.44 | 64.81 | 295 | | | | 2025 Mar 18, 23:03 | 25508 | 0.0008 | 19110 | 19150 | 675.73 | 64.83 | 236 | | | | 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, 10:58 | 25492 | 0.0011 | 19086 | 19141 | 675.09 | 64.83 | 263 | | | | 2025 Mar 3, 16:47 | 25484 | 0.0002 | 19101 | 19110 | 674.77 | 64.84 | 235 | | | | 2025 Mar 3, 22:55 | 25457 | 0.0017 | 19036 | 19121 | 673.69 | 64.82 | 198 | | | |
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, 18:00 | 6674 | 0.0001 | 294 | 296 | 90.43 | 43.00 | 253 | | | | 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, 02:34 | 7181 | 0.0002 | 801 | 804 | 100.93 | 98.61 | 7 | 01:28 | | | 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, 03:50 | 24523 | 0.7327 | 178 | 36111 | 636.96 | 19.02 | 179 | | | | 2025 Mar 17, 17:27 | 42165 | 0.0001 | 35785 | 35789 | 1436.12 | 0.01 | 322 | 90°.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, 05:02 | 24842 | 0.7376 | 141 | 36787 | 649.44 | 19.04 | 182 | | | | 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, 16:17 | 42562 | 0.0027 | 36068 | 36299 | 1456.42 | 0.04 | 7 | | | |
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, 20:16 | 7292 | 0.0013 | 904 | 923 | 103.28 | 88.99 | 167 | | | | 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, 19:10 | 7239 | 0.0065 | 814 | 908 | 102.16 | 88.99 | 80 | | | |
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, 09:36 | 7027 | 0.0015 | 638 | 659 | 97.70 | 97.95 | 163 | 17:59 | | | 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, 09:36 | 7027 | 0.0017 | 637 | 661 | 97.71 | 97.96 | 160 | 17:59 | | | 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, 19:12 | 7028 | 0.0017 | 639 | 662 | 97.74 | 97.96 | 159 | 18:00 | | | 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, 14:52 | 7029 | 0.0010 | 644 | 657 | 97.74 | 97.95 | 202 | 18:00 | | | 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, 05:07 | 7031 | 0.0010 | 646 | 660 | 97.79 | 97.96 | 224 | 18:00 | | | 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, 20:00 | 6655 | 0.0002 | 275 | 278 | 90.04 | 43.01 | 260 | | | | 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, 09:54 | 6605 | 0.0025 | 210 | 243 | 89.03 | 51.65 | 238 | | | | 2025 Mar 16, 09:41 | 6795 | 0.0006 | 412 | 421 | 92.90 | 51.64 | 28 | | | | 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, 08:33 | 6955 | 0.0006 | 573 | 582 | 96.22 | 42.02 | 290 | | | | 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, 11:50 | 6777 | 0.0242 | 235 | 563 | 92.54 | 42.03 | 289 | | | | 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, 05:21 | 6953 | 0.0008 | 569 | 581 | 96.17 | 42.02 | 318 | | | |
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, 16:59 | 6874 | 0.0009 | 489 | 502 | 94.53 | 97.49 | 276 | 10:30 | | | |
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, 17:00 | 6873 | 0.0008 | 489 | 501 | 94.52 | 97.49 | 285 | 10:30 | | | 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 | |
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, 20:00 | 6680 | 0.0002 | 301 | 303 | 90.56 | 43.00 | 271 | | | | 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, 17:26 | 7883 | 0.0015 | 1493 | 1517 | 116.09 | 82.50 | 344 | | | | 2025 Apr 23, 17:58 | 7883 | 0.0014 | 1494 | 1516 | 116.09 | 82.50 | 258 | | | | 2025 Apr 25, 12:32 | 7878 | 0.0018 | 1486 | 1513 | 115.97 | 82.50 | 234 | | | | 2025 Apr 27, 16:44 | 7876 | 0.0020 | 1483 | 1513 | 115.94 | 82.50 | 225 | | | | 2025 Apr 28, 19:48 | 7873 | 0.0023 | 1477 | 1513 | 115.87 | 82.49 | 218 | | | | 2025 May 3, 21:31 | 7873 | 0.0024 | 1476 | 1513 | 115.86 | 82.49 | 206 | | | | 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, 21:18 | 7881 | 0.0014 | 1492 | 1514 | 116.06 | 82.50 | 336 | | | | 2025 Apr 14, 16:57 | 7881 | 0.0013 | 1493 | 1514 | 116.06 | 82.50 | 271 | | | | 2025 Apr 16, 09:34 | 7877 | 0.0015 | 1487 | 1511 | 115.96 | 82.50 | 246 | | | | 2025 Apr 21, 13:16 | 7873 | 0.0019 | 1480 | 1510 | 115.87 | 82.49 | 223 | | | | 2025 May 1, 18:38 | 7872 | 0.0020 | 1478 | 1510 | 115.86 | 82.49 | 199 | | | | 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, 17:25 | 7880 | 0.0014 | 1491 | 1513 | 116.04 | 82.50 | 331 | | | | 2025 Apr 1, 23:05 | 7873 | 0.0013 | 1485 | 1505 | 115.88 | 82.50 | 257 | | | | 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, 16:05 | 6916 | 0.0012 | 529 | 546 | 95.39 | 97.59 | 294 | 14:26 | | | 2025 Jun 4, 15:49 | 6910 | 0.0014 | 522 | 541 | 95.27 | 97.61 | 28 | 14:29 | | | 2025 Jun 10, 11:47 | 6918 | 0.0018 | 528 | 552 | 95.45 | 97.61 | 347 | 14:29 | | | 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, 17:29 | 6916 | 0.0012 | 529 | 546 | 95.39 | 97.60 | 287 | 14:26 | | | 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, 17:29 | 6916 | 0.0013 | 529 | 546 | 95.40 | 97.60 | 287 | 14:26 | | | 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, 17:29 | 6916 | 0.0013 | 529 | 547 | 95.40 | 97.60 | 285 | 14:26 | | | 2025 Jun 4, 16:03 | 6910 | 0.0014 | 523 | 542 | 95.28 | 97.61 | 26 | 14:28 | | | 2025 Jun 10, 05:40 | 6919 | 0.0018 | 528 | 553 | 95.46 | 97.61 | 343 | 14:29 | | | 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, 17:29 | 6916 | 0.0012 | 529 | 547 | 95.40 | 97.60 | 287 | 14:26 | | | 2025 May 31, 04:03 | 6911 | 0.0012 | 524 | 541 | 95.29 | 97.61 | 39 | 14:28 | | | 2025 Jun 6, 00:01 | 6919 | 0.0015 | 530 | 551 | 95.45 | 97.61 | 353 | 14:28 | | | 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, 17:29 | 6916 | 0.0012 | 530 | 546 | 95.40 | 97.60 | 284 | 14:26 | | | 2025 May 21, 04:03 | 6911 | 0.0014 | 523 | 542 | 95.29 | 97.61 | 72 | 14:28 | | | 2025 May 28, 14:14 | 6919 | 0.0014 | 531 | 550 | 95.46 | 97.61 | 13 | 14:28 | | | 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, 17:30 | 6916 | 0.0012 | 530 | 546 | 95.40 | 97.60 | 284 | 14:26 | | | 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, 17:29 | 6916 | 0.0011 | 530 | 546 | 95.40 | 97.60 | 281 | 14:26 | | | 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, 15:13 | 7024 | 0.0002 | 644 | 647 | 97.64 | 97.97 | 104 | 13:53 | | | 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, 11:58 | 7024 | 0.0002 | 644 | 647 | 97.64 | 97.97 | 106 | 13:53 | | | 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, 15:13 | 7023 | 0.0001 | 645 | 646 | 97.63 | 97.97 | 154 | 13:53 | | | 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, 15:13 | 7023 | 0.0001 | 644 | 645 | 97.61 | 97.97 | 325 | 13:53 | | | 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, 15:12 | 7022 | 0.0002 | 643 | 645 | 97.60 | 97.97 | 286 | 13:53 | | | 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, 04:10 | 6792 | 0.0334 | 187 | 641 | 92.85 | 97.97 | 230 | | | | 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, 04:23 | 6992 | 0.0045 | 582 | 645 | 96.97 | 97.97 | 41 | | | |
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, 20:00 | 6666 | 0.0002 | 287 | 289 | 90.28 | 43.01 | 272 | | | | 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, 19:08 | 6918 | 0.0011 | 532 | 547 | 95.44 | 97.59 | 300 | 17:25 | | | 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, 19:00 | 6920 | 0.0009 | 536 | 548 | 95.48 | 97.60 | 322 | 17:25 | | | 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, 19:00 | 6916 | 0.0013 | 529 | 546 | 95.39 | 97.60 | 287 | 17:25 | | | 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, 19:00 | 6916 | 0.0012 | 529 | 546 | 95.40 | 97.60 | 290 | 17:25 | | | 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, 19:08 | 6917 | 0.0012 | 531 | 547 | 95.43 | 97.60 | 311 | 17:25 | | | 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, 19:08 | 6916 | 0.0012 | 530 | 547 | 95.41 | 97.60 | 294 | 17:25 | | | 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, 20:00 | 7480 | 0.0015 | 1091 | 1113 | 107.30 | 64.00 | 110 | | | | 2025 Mar 27, 19:03 | 7486 | 0.0128 | 1012 | 1204 | 107.44 | 63.45 | 180 | | | | 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, 12:23 | 6918 | 0.0020 | 526 | 554 | 95.45 | 97.52 | 354 | 03:51 | | | 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, 14:06 | 6918 | 0.0020 | 526 | 554 | 95.44 | 97.52 | 357 | 03:52 | | | 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, 17:16 | 6917 | 0.0021 | 525 | 554 | 95.43 | 97.52 | 349 | 03:52 | | | 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, 17:16 | 6917 | 0.0021 | 525 | 553 | 95.42 | 97.52 | 348 | 03:52 | | | 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, 20:26 | 6917 | 0.0018 | 526 | 552 | 95.42 | 97.52 | 353 | 03:51 | | | 2025 Mar 31, 21:54 | 6917 | 0.0018 | 526 | 551 | 95.42 | 97.52 | 349 | 03:51 | | | 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, 14:03 | 6916 | 0.0020 | 524 | 551 | 95.39 | 97.51 | 343 | 03:52 | | | 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, 12:21 | 6917 | 0.0018 | 526 | 551 | 95.41 | 97.51 | 349 | 03:51 | | | 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, 18:11 | 6889 | 0.0048 | 477 | 544 | 94.84 | 97.51 | 301 | | | | 2025 Mar 30, 16:38 | 6887 | 0.0048 | 475 | 542 | 94.80 | 97.51 | 283 | | | | 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, 18:09 | 6732 | 0.0255 | 182 | 525 | 91.61 | 97.50 | 226 | | | |
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, 19:07 | 24394 | 0.7308 | 190 | 35841 | 631.94 | 27.11 | 179 | | | | 2025 Apr 4, 14:59 | 42160 | 0.0032 | 35649 | 35916 | 1435.87 | 5.50 | 359 | 80°.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, 19:14 | 23793 | 0.7248 | 169 | 34661 | 608.76 | 27.08 | 179 | | | |
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, 16:00 | 6686 | 0.0001 | 308 | 309 | 90.68 | 53.16 | 48 | | | | 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, 23:01 | 24392 | 0.7318 | 164 | 35864 | 631.89 | 19.52 | 180 | | | | 2025 Apr 7, 17:16 | 42165 | 0.0001 | 35783 | 35790 | 1436.09 | 0.06 | 106 | 152°.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, 17:45 | 23621 | 0.7252 | 113 | 34372 | 602.14 | 19.52 | 179 | | | | 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, 20:00 | 6669 | 0.0002 | 289 | 292 | 90.32 | 43.00 | 275 | | | | 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, 03:15 | 6685 | 0.0158 | 202 | 413 | 90.67 | 90.01 | 92 | 20:35 | | | 2025 Apr 1, 12:00 | 6808 | 0.0004 | 427 | 432 | 93.16 | 90.00 | 76 | 20:33 | | | 2025 Apr 4, 09:54 | 6785 | 0.0038 | 381 | 433 | 92.70 | 90.01 | 80 | 20:22 | | | 2025 Apr 4, 14:46 | 6774 | 0.0055 | 359 | 434 | 92.49 | 89.63 | 82 | 20:20 | | | 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, 15:02 | 6831 | 0.0008 | 447 | 458 | 93.64 | 55.00 | 282 | | | | 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, 14:59 | 6828 | 0.0010 | 443 | 456 | 93.58 | 55.00 | 301 | | | | 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, 15:00 | 6829 | 0.0009 | 445 | 457 | 93.60 | 54.99 | 299 | | | | 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, 14:59 | 6830 | 0.0008 | 446 | 457 | 93.62 | 55.00 | 285 | | | | 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, 13:21 | 7001 | 0.0244 | 452 | 794 | 97.17 | 43.01 | 111 | | | | 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, 20:00 | 6667 | 0.0000 | 289 | 289 | 90.30 | 53.15 | 47 | | | | 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, 16:00 | 6672 | 0.0001 | 293 | 295 | 90.40 | 43.00 | 233 | | | | 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, 18:00 | 6669 | 0.0001 | 290 | 291 | 90.32 | 53.16 | 53 | | | | 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, 11:42 | 6797 | 0.0005 | 415 | 422 | 92.94 | 51.64 | 22 | | | | 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, 14:28 | 6594 | 0.0028 | 197 | 234 | 88.81 | 51.66 | 78 | | | |
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, 21:00 | 24528 | 0.7325 | 184 | 36116 | 637.17 | 18.99 | 180 | | | | 2025 Apr 21, 16:55 | 42165 | 0.0001 | 35783 | 35790 | 1436.09 | 0.04 | 119 | 152°.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, 19:44 | 24855 | 0.7374 | 149 | 36804 | 649.95 | 19.02 | 180 | | | | 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, 01:53 | 42565 | 0.0010 | 36142 | 36231 | 1456.58 | 0.04 | 208 | | | |
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 orbit | 6678 | 0.0010 | 293 | 306 | 90.51 | 69.90 | 155 | | | | 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, 16:00 | 6676 | 0.0002 | 297 | 299 | 90.48 | 43.01 | 248 | | | | 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, 18:00 | 6692 | 0.0002 | 312 | 315 | 90.80 | 43.00 | 264 | | | | 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, 04:34 | 7492 | 0.0018 | 1100 | 1127 | 107.56 | 63.39 | 246 | | | | 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, 04:44 | 7490 | 0.0020 | 1097 | 1127 | 107.52 | 63.39 | 292 | | | | 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, 09:12 | 7383 | 0.0006 | 1000 | 1009 | 105.21 | 99.69 | 229 | 06:00 | | | 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, 09:12 | 7383 | 0.0006 | 1000 | 1009 | 105.22 | 99.69 | 222 | 06:00 | | | 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, 09:12 | 7383 | 0.0007 | 1000 | 1011 | 105.23 | 99.69 | 229 | 06:00 | | | 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, 09:13 | 7384 | 0.0008 | 1000 | 1011 | 105.24 | 99.70 | 215 | 06:00 | | | 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, 09:13 | 7385 | 0.0009 | 1000 | 1013 | 105.26 | 99.69 | 227 | 06:00 | | | 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, 09:13 | 7385 | 0.0009 | 1000 | 1013 | 105.26 | 99.70 | 225 | 06:00 | | | 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, 09:14 | 7290 | 0.0107 | 834 | 990 | 103.25 | 99.70 | 108 | | | |
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, 11:35 | 6671 | 0.0115 | 216 | 370 | 90.38 | 51.65 | 225 | | | | 2025 Apr 22, 14:40 | 6795 | 0.0005 | 413 | 421 | 92.91 | 51.64 | 64 | | | | 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, 21:08 | 6955 | 0.0005 | 573 | 580 | 96.20 | 45.40 | 172 | | | | 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, 09:55 | 6955 | 0.0007 | 572 | 581 | 96.21 | 45.41 | 196 | | | | 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, 09:20 | 6650 | 0.0119 | 193 | 352 | 89.96 | 41.46 | 125 | | | | 2025 Apr 24, 16:32 | 6761 | 0.0002 | 381 | 384 | 92.21 | 41.46 | 223 | | | | 2026 Jan 17, 18:13 | 6764 | 0.0011 | 378 | 393 | 92.27 | 41.47 | 305 | | | | 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, 19:37 | 6646 | 0.0113 | 193 | 343 | 89.86 | 41.46 | 127 | | | | 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, 14:03 | 6761 | 0.0007 | 378 | 387 | 92.20 | 41.48 | 17 | | | |
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, 18:00 | 6690 | 0.0002 | 310 | 313 | 90.75 | 43.00 | 265 | | | | 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, 20:43 | 24385 | 0.7304 | 196 | 35818 | 631.62 | 27.15 | 180 | | | | 2025 May 12, 13:55 | 42165 | 0.0002 | 35778 | 35796 | 1436.12 | 5.47 | 151 | 20°.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, 20:08 | 23778 | 0.7244 | 175 | 34625 | 608.18 | 27.09 | 179 | | | |
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, 18:00 | 6691 | 0.0002 | 312 | 314 | 90.79 | 43.01 | 258 | | | | 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, 12:14 | 7485 | 0.0012 | 1099 | 1116 | 107.42 | 86.50 | 295 | | | | 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, 12:38 | 6663 | 0.0000 | 285 | 286 | 90.22 | 53.16 | 9 | | | | 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, 20:00 | 6841 | 0.0011 | 456 | 470 | 93.86 | 51.86 | 139 | | | | 2026 Jan 1, 18:40 | 6949 | 0.0008 | 565 | 576 | 96.08 | 51.89 | 237 | | | | 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, 20:00 | 6686 | 0.0002 | 307 | 309 | 90.68 | 43.01 | 256 | | | | 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 | |
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, 20:10 | 7045 | 0.0001 | 666 | 668 | 98.09 | 98.07 | 64 | 18:00 | | | 2025 May 10, 03:43 | 7042 | 0.0001 | 663 | 665 | 98.02 | 98.07 | 88 | 18:00 | | | 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, 20:00 | 6664 | 0.0002 | 285 | 287 | 90.24 | 43.00 | 208 | | | | 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, 18:00 | 6661 | 0.0002 | 282 | 284 | 90.17 | 43.00 | 253 | | | | 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, 18:00 | 6684 | 0.0002 | 304 | 307 | 90.63 | 43.00 | 270 | | | | 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, 16:00 | 6671 | 0.0004 | 290 | 296 | 90.38 | 70.00 | 274 | | | | 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, 16:00 | 6667 | 0.0001 | 288 | 289 | 90.29 | 43.00 | 253 | | | | 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, 14:33 | 7181 | 0.0011 | 795 | 811 | 100.94 | 86.00 | 262 | | | | 2025 May 19, 21:17 | 7191 | 0.0004 | 810 | 816 | 101.15 | 86.00 | 153 | | | | 2025 May 21, 08:48 | 7215 | 0.0007 | 832 | 842 | 101.65 | 86.00 | 325 | | | | 2025 May 23, 20:14 | 7230 | 0.0002 | 850 | 853 | 101.96 | 86.00 | 94 | | | | 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, 14:32 | 7181 | 0.0011 | 795 | 811 | 100.93 | 86.00 | 264 | | | | 2025 May 19, 23:02 | 7196 | 0.0008 | 812 | 824 | 101.26 | 85.99 | 185 | | | | 2025 May 23, 21:57 | 7224 | 0.0007 | 841 | 851 | 101.84 | 86.00 | 358 | | | | 2025 May 28, 20:58 | 7230 | 0.0002 | 850 | 853 | 101.96 | 85.99 | 82 | | | | 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, 15:50 | 7180 | 0.0011 | 794 | 810 | 100.92 | 86.00 | 269 | | | | 2025 May 18, 13:24 | 7165 | 0.0014 | 777 | 797 | 100.61 | 86.00 | 269 | | | | 2025 Jul 8, 20:32 | 7167 | 0.0019 | 776 | 802 | 100.64 | 85.99 | 94 | | | | 2025 Jul 9, 20:37 | 7184 | 0.0020 | 791 | 820 | 101.00 | 86.00 | 74 | | | | 2025 Jul 14, 13:30 | 7227 | 0.0003 | 847 | 851 | 101.91 | 86.00 | 171 | | | | 2025 Jul 15, 04:48 | 7229 | 0.0002 | 850 | 853 | 101.95 | 86.00 | 95 | | | | 2025 Jul 15, 20:06 | 7229 | 0.0002 | 850 | 853 | 101.96 | 86.00 | 90 | | | | 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, 15:11 | 7059 | 0.0072 | 631 | 732 | 98.38 | 86.02 | 66 | | | |
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, 21:24 | 24382 | 0.7311 | 178 | 35830 | 631.49 | 28.58 | 180 | | | | 2026 Jan 9, 00:11 | 42164 | 0.0003 | 35771 | 35800 | 1436.06 | 3.56 | 316 | 141°.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, 21:31 | 24304 | 0.7328 | 117 | 35734 | 628.44 | 28.60 | 179 | | | | |
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, 18:00 | 6664 | 0.0004 | 283 | 288 | 90.23 | 70.00 | 267 | | | | 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, 18:00 | 6659 | 0.0001 | 280 | 282 | 90.13 | 43.00 | 243 | | | | 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, 21:14 | 6876 | 0.0010 | 491 | 505 | 94.57 | 97.41 | 261 | 10:30 | | | 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, 21:40 | 6720 | 0.0009 | 336 | 349 | 91.38 | 43.00 | 296 | | | | 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, 22:00 | 6676 | 0.0004 | 295 | 300 | 90.47 | 69.99 | 272 | | | | 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 | |
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, 14:46 | 6901 | 0.0006 | 519 | 527 | 95.08 | 97.41 | 130 | 10:30 | | | |
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, 14:46 | 6899 | 0.0004 | 519 | 524 | 95.06 | 97.41 | 114 | 10:30 | | | |
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, 14:46 | 6899 | 0.0004 | 518 | 524 | 95.06 | 97.42 | 100 | 10:30 | | | |
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, 14:46 | 6899 | 0.0005 | 518 | 524 | 95.05 | 97.42 | 99 | 10:30 | | | |
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, 14:46 | 6899 | 0.0005 | 518 | 525 | 95.06 | 97.42 | 110 | 10:30 | | | |
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, 14:46 | 6899 | 0.0005 | 518 | 524 | 95.05 | 97.42 | 105 | 10:30 | | | 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, 14:46 | 6767 | 0.0317 | 175 | 603 | 92.33 | 96.12 | 89 | | | |
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, 16:51 | 6954 | 0.0010 | 569 | 583 | 96.19 | 42.01 | 282 | | | | 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, 17:56 | 6797 | 0.0279 | 229 | 608 | 92.95 | 41.95 | 255 | | | | 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, 18:06 | 6818 | 0.0209 | 297 | 582 | 93.37 | 42.01 | 279 | | | |
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 | |
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, 20:40 | 7223 | 0.0012 | 836 | 853 | 101.82 | 44.99 | 308 | | | | 2025 May 27, 16:52 | 7224 | 0.0011 | 837 | 854 | 101.83 | 44.98 | 347 | | | | 2025 May 30, 16:06 | 7226 | 0.0012 | 839 | 856 | 101.88 | 44.98 | 15 | | | | 2025 Jun 1, 12:12 | 7226 | 0.0012 | 839 | 856 | 101.88 | 44.98 | 24 | | | | 2025 Jun 11, 13:26 | 7228 | 0.0012 | 842 | 859 | 101.93 | 44.98 | 70 | | | | 2025 Jun 12, 15:03 | 7234 | 0.0012 | 847 | 864 | 102.05 | 44.98 | 82 | | | | |
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, 20:40 | 7223 | 0.0012 | 836 | 853 | 101.81 | 44.98 | 310 | | | | 2025 May 29, 14:38 | 7224 | 0.0012 | 838 | 855 | 101.85 | 44.98 | 8 | | | | 2025 Jun 11, 06:11 | 7226 | 0.0011 | 840 | 856 | 101.89 | 44.98 | 70 | | | | 2025 Jun 12, 15:12 | 7229 | 0.0013 | 841 | 860 | 101.94 | 45.01 | 96 | | | | 2025 Jun 17, 18:26 | 7242 | 0.0022 | 848 | 880 | 102.23 | 44.97 | 114 | | | | 2025 Jun 18, 01:15 | 7244 | 0.0010 | 859 | 873 | 102.26 | 44.98 | 93 | | | | 2025 Jun 18, 11:28 | 7244 | 0.0011 | 858 | 874 | 102.26 | 44.98 | 105 | | | | 2025 Jun 24, 00:39 | 7268 | 0.0009 | 884 | 897 | 102.78 | 44.98 | 139 | | | | 2025 Jun 26, 19:29 | 7275 | 0.0009 | 891 | 904 | 102.93 | 44.98 | 154 | | | | |
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, 10:14 | 7222 | 0.0012 | 835 | 853 | 101.80 | 44.99 | 315 | | | | 2025 May 28, 21:39 | 7224 | 0.0011 | 838 | 854 | 101.85 | 44.99 | 10 | | | | 2025 May 29, 18:01 | 7225 | 0.0012 | 839 | 856 | 101.87 | 44.99 | 21 | | | | 2025 Jun 11, 13:40 | 7228 | 0.0012 | 841 | 858 | 101.92 | 44.98 | 85 | | | | 2025 Jun 12, 13:32 | 7232 | 0.0012 | 846 | 863 | 102.02 | 44.98 | 90 | | | | 2025 Jun 17, 10:14 | 7242 | 0.0011 | 856 | 872 | 102.23 | 44.98 | 115 | | | | 2025 Jun 18, 11:56 | 7256 | 0.0011 | 870 | 887 | 102.53 | 44.98 | 119 | | | | 2025 Jun 19, 20:25 | 7267 | 0.0010 | 882 | 896 | 102.75 | 44.98 | 128 | | | | 2025 Jun 22, 16:56 | 7275 | 0.0009 | 891 | 903 | 102.93 | 44.98 | 145 | | | | |
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, 11:56 | 7222 | 0.0013 | 835 | 853 | 101.80 | 44.99 | 312 | | | | 2025 May 28, 04:42 | 7224 | 0.0015 | 835 | 856 | 101.83 | 44.98 | 1 | | | | 2025 May 29, 04:26 | 7224 | 0.0013 | 837 | 856 | 101.85 | 44.98 | 13 | | | | 2025 May 29, 14:37 | 7225 | 0.0012 | 838 | 855 | 101.86 | 44.99 | 15 | | | | 2025 Jun 12, 15:13 | 7232 | 0.0011 | 845 | 861 | 102.00 | 44.98 | 85 | | | | 2025 Jun 19, 13:14 | 7254 | 0.0009 | 869 | 883 | 102.48 | 44.98 | 120 | | | | 2025 Jun 22, 13:05 | 7275 | 0.0008 | 892 | 903 | 102.93 | 44.98 | 138 | | | | 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, 17:12 | 24378 | 0.7299 | 207 | 35792 | 631.32 | 15.49 | 180 | | | | 2025 May 30, 17:13 | 42165 | 0.0002 | 35780 | 35794 | 1436.12 | 0.01 | 360 | 167°.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, 17:27 | 23606 | 0.7237 | 145 | 34311 | 601.59 | 15.49 | 179 | | | | 2025 May 20, 17:27 | 23606 | 0.7237 | 145 | 34311 | 601.59 | 15.49 | 179 | | | |
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, 18:00 | 6687 | 0.0002 | 308 | 310 | 90.70 | 43.01 | 262 | | | | 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 | |
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 | | |
in space
|
| Commercial satellite for high-resolution remote sensing using an optical imaging system. Catalogue Number and Designation to be confirmed. |
| Orbit parameters awaited | | |
in space
|
| Commercial remote sensing satellite using radar imaging. Catalogue Number and Designation to be confirmed. |
| Orbit parameters awaited | | |
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 | | |
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, 14:36 | 6851 | 0.0012 | 464 | 481 | 94.05 | 72.97 | 238 | | | | 2025 May 31, 13:55 | 6852 | 0.0012 | 466 | 482 | 94.08 | 72.97 | 235 | | | | 2025 Jul 9, 21:59 | 6852 | 0.0008 | 468 | 479 | 94.07 | 72.97 | 174 | | | | 2025 Jul 10, 16:48 | 6853 | 0.0006 | 471 | 479 | 94.10 | 72.97 | 182 | | | | 2025 Sep 6, 17:36 | 6852 | 0.0002 | 472 | 475 | 94.08 | 72.97 | 5 | | | | 2025 Sep 7, 17:08 | 6854 | 0.0003 | 474 | 478 | 94.13 | 72.97 | 272 | | | | 2025 Nov 7, 17:14 | 6851 | 0.0001 | 472 | 473 | 94.05 | 72.97 | 184 | | | | 2025 Nov 8, 16:45 | 6854 | 0.0005 | 472 | 479 | 94.12 | 72.97 | 238 | | | | 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, 19:14 | 6683 | 0.0001 | 305 | 306 | 90.63 | 53.16 | 33 | | | | 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, 20:00 | 6699 | 0.0002 | 320 | 322 | 90.94 | 43.00 | 285 | | | | 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, 17:11 | 6650 | 0.0010 | 265 | 279 | 89.95 | 97.60 | 248 | | | | 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, 14:00 | 6667 | 0.0000 | 288 | 289 | 90.29 | 53.16 | 27 | | | | 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 | |
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, 15:21 | 6875 | 0.0009 | 490 | 503 | 94.55 | 97.49 | 271 | 10:30 | | | 2025 Jun 11, 18:04 | 6878 | 0.0008 | 494 | 505 | 94.60 | 97.49 | 190 | 10:31 | | | 2025 Dec 31, 15:41 | 6870 | 0.0009 | 485 | 498 | 94.44 | 97.47 | 213 | 10:39 | | | 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, 16:36 | 6760 | 0.0158 | 275 | 489 | 92.19 | 97.43 | 12 | | | | 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, 13:45 | 6913 | 0.0061 | 493 | 578 | 95.35 | 97.52 | 194 | 10:30 | | | 2025 Dec 30, 10:37 | 6860 | 0.0042 | 453 | 511 | 94.24 | 97.50 | 170 | 10:35 | | |
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, 01:05 | 16683 | 0.5944 | 388 | 20222 | 357.42 | 55.01 | 270 | | | | 2025 Jun 9, 23:50 | 26560 | 0.0002 | 20177 | 20186 | 717.95 | 54.96 | 292 | | | |
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, 16:00 | 6660 | 0.0001 | 281 | 282 | 90.15 | 53.16 | 53 | | | | 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 | |
in space
|
| Mission description awaited |
epoch (UTC) | s-m axis ( km ) | eccentricity | perigee ( km ) | apogee ( km ) | period ( min ) | incl ( ° ) | ω ( ° ) | | |
| 2025 Jun 4, 12:37 | 6850 | 0.0010 | 465 | 478 | 94.03 | 59.00 | 308 | | | | 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, 12:38 | 6852 | 0.0008 | 468 | 479 | 94.07 | 58.99 | 318 | | | | 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, 03:56 | 6708 | 0.0232 | 174 | 485 | 91.13 | 58.99 | 267 | | | |
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, 18:00 | 6683 | 0.0002 | 303 | 306 | 90.61 | 43.01 | 255 | | | | 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, 18:00 | 6664 | 0.0001 | 285 | 286 | 90.23 | 53.16 | 88 | | | | 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, 16:15 | 7381 | 0.0009 | 997 | 1009 | 105.18 | 86.50 | 217 | | | | 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, 16:17 | 7381 | 0.0008 | 997 | 1009 | 105.18 | 86.50 | 218 | | | | 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, 16:20 | 7380 | 0.0008 | 996 | 1008 | 105.17 | 86.49 | 212 | | | | 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, 16:18 | 7380 | 0.0007 | 996 | 1007 | 105.15 | 86.50 | 204 | | | | 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, 17:25 | 7380 | 0.0007 | 996 | 1007 | 105.15 | 86.50 | 203 | | | | 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, 17:27 | 7293 | 0.0104 | 839 | 991 | 103.30 | 86.51 | 112 | | | |
2025-122 Falcon 9 Block 5 Cape Canaveral Space Force Station | 2025 Jun 7, 04:54 UTC | |
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, 10:32 | 17430 | 0.6236 | 182 | 21921 | 381.68 | 26.98 | 175 | | | | 2025 Jun 14, 18:53 | 31771 | 0.3269 | 15006 | 35780 | 939.29 | 5.57 | 179 | | | | 2025 Jun 17, 15:14 | 42123 | 0.0001 | 35739 | 35750 | 1433.94 | 0.10 | 43 | 121°.6 W | | | 2025 Jun 20, 13:27 | 42147 | 0.0005 | 35749 | 35788 | 1435.19 | 0.10 | 225 | 120°.5 W | | | 2025 Jun 21, 11:28 | 42165 | 0.0002 | 35779 | 35795 | 1436.13 | 0.09 | 155 | 120°.5 W | | | 2025 Jul 17, 13:07 | 42142 | 0.0002 | 35757 | 35771 | 1434.93 | 0.04 | 98 | 120°.2 W | | | 2025 Jul 30, 13:38 | 42166 | 0.0003 | 35774 | 35801 | 1436.15 | 0.03 | 331 | 116°.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, 20:00 | 6695 | 0.0003 | 314 | 319 | 90.86 | 69.99 | 273 | | | | 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, 20:00 | 6695 | 0.0001 | 316 | 318 | 90.86 | 43.00 | 270 | | | | 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, 14:49 | 6954 | 0.0009 | 570 | 582 | 96.19 | 42.01 | 280 | | | | 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, 20:43 | 6810 | 0.0220 | 282 | 582 | 93.21 | 42.01 | 271 | | | | 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, 20:41 | 6780 | 0.0256 | 228 | 576 | 92.60 | 42.02 | 238 | | | |
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, 20:00 | 6702 | 0.0004 | 321 | 326 | 91.00 | 70.00 | 274 | | | | 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, 16:00 | 6714 | 0.0001 | 335 | 337 | 91.26 | 43.00 | 266 | | | | 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, 14:20 | 6875 | 0.0010 | 490 | 504 | 94.56 | 97.32 | 273 | 14:15 | | | 2025 Jun 27, 13:59 | 6880 | 0.0010 | 495 | 509 | 94.66 | 97.32 | 244 | 14:14 | | | 2025 Jul 1, 14:17 | 6882 | 0.0010 | 497 | 511 | 94.70 | 97.32 | 245 | 14:14 | | | 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, 16:00 | 6712 | 0.0004 | 331 | 336 | 91.20 | 70.00 | 270 | | | | 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, 14:12 | 6700 | 0.0000 | 322 | 322 | 90.96 | 53.15 | 61 | | | | 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, 18:58 | 42067 | 0.3666 | 20268 | 51110 | 1431.12 | 1.10 | 174 | 94°.8 E | | | 2025 Jun 21, 17:22 | 42067 | 0.3666 | 20268 | 51110 | 1431.10 | 1.09 | 174 | 96°.0 E | | | 2025 Jun 29, 19:53 | 42184 | 0.3657 | 20380 | 51231 | 1437.08 | 1.06 | 174 | 103°.6 E | | | 2025 Jul 7, 17:48 | 42165 | 0.3656 | 20370 | 51204 | 1436.12 | 1.03 | 174 | 101°.7 E | | | 2025 Sep 6, 16:58 | 42171 | 0.3652 | 20393 | 51192 | 1436.41 | 0.78 | 173 | 99°.5 E | | | 2025 Nov 19, 17:54 | 42177 | 0.3649 | 20410 | 51187 | 1436.72 | 0.47 | 170 | 90°.9 E | | | 2025 Nov 20, 19:41 | 42192 | 0.3644 | 20439 | 51189 | 1437.50 | 0.47 | 170 | 90°.6 E | | | 2025 Nov 21, 19:04 | 42224 | 0.3634 | 20504 | 51188 | 1439.13 | 0.46 | 170 | 90°.2 E | | | 2025 Nov 23, 18:29 | 42209 | 0.3580 | 20721 | 50941 | 1438.35 | 0.45 | 169 | 89°.6 E | | | 2025 Nov 24, 13:28 | 42207 | 0.3559 | 20807 | 50850 | 1438.23 | 0.45 | 169 | 89°.5 E | | | 2025 Nov 26, 13:45 | 42188 | 0.3527 | 20928 | 50691 | 1437.27 | 0.44 | 169 | 87°.7 E | | | 2025 Nov 27, 17:37 | 42267 | 0.3502 | 21087 | 50691 | 1441.35 | 0.44 | 169 | 85°.2 E | | | 2025 Nov 29, 09:06 | 42199 | 0.3499 | 21057 | 50584 | 1437.83 | 0.43 | 169 | 65°.7 E | | | 2025 Dec 1, 13:59 | 42182 | 0.3359 | 21633 | 49974 | 1436.96 | 0.42 | 169 | 173°.7 E | | | 2025 Dec 4, 17:26 | 42161 | 0.3291 | 21909 | 49657 | 1435.93 | 0.41 | 169 | 88°.3 E | | | 2025 Dec 5, 17:24 | 42098 | 0.3289 | 21876 | 49565 | 1432.71 | 0.41 | 169 | 81°.4 E | | | 2025 Dec 11, 13:45 | 42260 | 0.3113 | 22726 | 49037 | 1440.95 | 0.39 | 167 | 85°.4 E | | | 2025 Dec 14, 22:34 | 42166 | 0.2889 | 23608 | 47968 | 1436.16 | 0.38 | 165 | 70°.4 E | | | 2025 Dec 17, 17:05 | 42144 | 0.3015 | 23061 | 48470 | 1435.02 | 0.36 | 167 | 89°.8 E | | | 2025 Dec 18, 20:03 | 42115 | 0.2997 | 23115 | 48359 | 1433.55 | 0.36 | 167 | 91°.5 E | | | 2025 Dec 19, 13:32 | 42101 | 0.2990 | 23137 | 48309 | 1432.83 | 0.36 | 166 | 92°.4 E | | | 2025 Dec 20, 13:30 | 42047 | 0.2973 | 23167 | 48171 | 1430.09 | 0.35 | 166 | 94°.8 E | | | 2025 Dec 21, 16:34 | 42153 | 0.2942 | 23372 | 48177 | 1435.49 | 0.35 | 166 | 91°.9 E | | | 2025 Dec 22, 06:00 | 42125 | 0.2928 | 23412 | 48081 | 1434.06 | 0.35 | 166 | 93°.3 E | | | 2025 Dec 22, 22:20 | 42152 | 0.2897 | 23563 | 47985 | 1435.47 | 0.35 | 166 | 93°.1 E | | | 2025 Dec 24, 15:08 | 42237 | 0.2809 | 23997 | 47722 | 1439.81 | 0.34 | 165 | 102°.1 E | | | 2025 Dec 26, 08:00 | 42755 | 0.2723 | 24733 | 48021 | 1466.36 | 0.33 | 167 | | | | 2026 Feb 4, 15:34 | 42186 | 0.1755 | 28406 | 43209 | 1437.16 | 0.21 | 156 | 97°.8 E | | | 2026 Feb 15, 08:13 | 42154 | 0.1527 | 29341 | 42211 | 1435.55 | 0.19 | 151 | 98°.7 E | | | 2026 Feb 21, 23:57 | 42164 | 0.1343 | 30124 | 41447 | 1436.04 | 0.17 | 148 | 98°.2 E | | | 2026 Feb 27, 14:22 | 42183 | 0.1203 | 30730 | 40880 | 1437.04 | 0.16 | 144 | 97°.1 E | | | 2026 Mar 24, 17:47 | 42165 | 0.0695 | 32855 | 38719 | 1436.12 | 0.13 | 124 | 94°.3 E | | | 2026 Apr 16, 16:37 | 42164 | 0.0186 | 35000 | 36571 | 1436.04 | 0.13 | 105 | 98°.4 E | | | 2026 Apr 22, 18:10 | 42132 | 0.0019 | 35673 | 35835 | 1434.43 | 0.14 | 97 | 97°.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, 20:08 | 42054 | 0.3665 | 20264 | 51088 | 1430.46 | 1.09 | 174 | 99°.3 E | | | 2025 Jun 26, 15:21 | 42054 | 0.3665 | 20265 | 51088 | 1430.47 | 1.08 | 174 | 103°.3 E | | | 2025 Jun 27, 18:29 | 42113 | 0.3672 | 20271 | 51199 | 1433.46 | 1.07 | 174 | 104°.5 E | | | 2025 Jun 28, 15:52 | 42163 | 0.3678 | 20279 | 51291 | 1436.01 | 1.07 | 174 | 104°.8 E | | | 2025 Jul 11, 15:33 | 42166 | 0.3677 | 20285 | 51291 | 1436.16 | 1.01 | 174 | 104°.8 E | | | 2025 Jul 12, 14:00 | 42220 | 0.3659 | 20392 | 51291 | 1438.90 | 1.01 | 174 | 104°.2 E | | | 2025 Jul 16, 17:27 | 42167 | 0.3652 | 20388 | 51189 | 1436.20 | 0.99 | 174 | 101°.6 E | | | 2025 Jul 22, 01:39 | 42165 | 0.3655 | 20376 | 51198 | 1436.10 | 0.97 | 174 | 101°.7 E | | | 2025 Jul 23, 15:21 | 42166 | 0.3655 | 20377 | 51199 | 1436.17 | 0.96 | 174 | 101°.5 E | | | 2025 Aug 14, 19:11 | 42168 | 0.3653 | 20385 | 51195 | 1436.27 | 0.86 | 174 | 101°.0 E | | | 2025 Sep 6, 16:58 | 42171 | 0.3652 | 20393 | 51192 | 1436.40 | 0.79 | 174 | 99°.5 E | | | 2025 Nov 14, 16:14 | 42176 | 0.3647 | 20418 | 51178 | 1436.67 | 0.51 | 170 | 91°.6 E | | | 2025 Nov 19, 16:24 | 42087 | 0.3678 | 20230 | 51187 | 1432.10 | 0.45 | 169 | 97°.1 E | | | 2025 Dec 2, 18:22 | 42106 | 0.3670 | 20274 | 51182 | 1433.09 | 0.39 | 168 | 110°.1 E | | | 2025 Dec 4, 15:48 | 42132 | 0.3668 | 20299 | 51208 | 1434.40 | 0.38 | 167 | 111°.1 E | | | 2025 Dec 4, 19:31 | 42171 | 0.3666 | 20335 | 51251 | 1436.41 | 0.38 | 167 | 111°.1 E | | | 2025 Dec 5, 21:16 | 42170 | 0.3665 | 20335 | 51250 | 1436.39 | 0.38 | 167 | 111°.0 E | | | 2026 Feb 21, 16:53 | 42165 | 0.3660 | 20356 | 51218 | 1436.13 | 0.12 | 115 | 107°.7 E | | | 2026 Apr 15, 18:12 | 42170 | 0.3657 | 20369 | 51215 | 1436.38 | 0.22 | 39 | 105°.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, 11:07 | 21424 | 0.6897 | 270 | 29822 | 520.13 | 61.14 | 178 | | | | 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, 18:46 | 41034 | 0.3870 | 18775 | 50536 | 1378.69 | 1.43 | 171 | | | |
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, 19:15 | 42165 | 0.0002 | 35780 | 35794 | 1436.11 | 0.09 | 38 | 92°.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, 00:08 | 24744 | 0.7345 | 191 | 36541 | 645.60 | 27.66 | 181 | | | |
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, 18:00 | 6668 | 0.0001 | 289 | 290 | 90.31 | 53.16 | 58 | | | | 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, 20:00 | 6841 | 0.0009 | 456 | 468 | 93.84 | 51.87 | 123 | | | | 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, 06:41 | 6577 | 0.0015 | 189 | 209 | 88.47 | 51.60 | 47 | | | | 2025 Jun 25, 12:24 | 6635 | 0.0075 | 208 | 307 | 89.65 | 51.65 | 212 | | | | 2025 Jun 25, 12:53 | 6637 | 0.0074 | 210 | 309 | 89.69 | 51.65 | 213 | | | | 2025 Jun 26, 05:22 | 6794 | 0.0002 | 415 | 417 | 92.89 | 51.64 | 293 | | | | 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, 18:00 | 6669 | 0.0001 | 290 | 291 | 90.33 | 53.16 | 123 | | | | 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, 13:29 | 6901 | 0.0013 | 514 | 532 | 95.09 | 97.44 | 279 | 05:48 | | | 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, 13:28 | 6900 | 0.0013 | 514 | 531 | 95.08 | 97.43 | 273 | 05:48 | | | 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, 13:26 | 6900 | 0.0014 | 512 | 531 | 95.06 | 97.43 | 270 | 05:48 | | | |
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, 13:23 | 6898 | 0.0014 | 510 | 530 | 95.03 | 97.44 | 262 | 05:48 | | | 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, 21:25 | 6798 | 0.0272 | 235 | 605 | 92.98 | 97.44 | 9 | | | | 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, 21:34 | 6808 | 0.0262 | 251 | 608 | 93.17 | 97.34 | 213 | | | |
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, 18:00 | 6659 | 0.0001 | 280 | 281 | 90.12 | 53.16 | 61 | | | | 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 | |
in space
|
| Mission description awaited |
epoch (UTC) | s-m axis ( km ) | eccentricity | perigee ( km ) | apogee ( km ) | period ( min ) | incl ( ° ) | ω ( ° ) | | |
| 2025 Jun 29, 13:11 | 7034 | 0.0012 | 648 | 664 | 97.85 | 95.98 | 308 | | | | 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, 13:11 | 7033 | 0.0013 | 646 | 664 | 97.82 | 95.98 | 301 | | | | 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, 13:13 | 6786 | 0.0338 | 179 | 638 | 92.73 | 95.99 | 220 | | | |
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, 02:22 | 7045 | 0.0001 | 667 | 668 | 98.09 | 98.06 | 12 | 01:25 | | | 2025 Jul 5, 13:14 | 7049 | 0.0004 | 668 | 673 | 98.16 | 98.06 | 128 | 01:25 | | | 2025 Jul 14, 08:25 | 7050 | 0.0006 | 668 | 676 | 98.19 | 98.03 | 100 | 01:25 | | | 2025 Jul 18, 20:27 | 7047 | 0.0001 | 668 | 670 | 98.12 | 98.03 | 81 | 01:25 | | | 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, 01:55 | 6980 | 0.0094 | 537 | 668 | 96.73 | 98.05 | 261 | | | |
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, 14:00 | 6673 | 0.0004 | 292 | 298 | 90.42 | 70.00 | 277 | | | | 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, 08:28 | 39037 | 0.8287 | 308 | 65008 | 1279.28 | 21.22 | 179 | | | | 2025 Jul 15, 08:15 | 42212 | 0.0012 | 35782 | 35886 | 1438.52 | 1.01 | 181 | 3°.3 W | | | 2025 Jul 17, 13:21 | 42165 | 0.0000 | 35785 | 35789 | 1436.12 | 1.00 | 65 | 3°.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, 14:00 | 6674 | 0.0001 | 296 | 297 | 90.44 | 53.16 | 63 | | | | 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, 23:33 | 7173 | 0.0002 | 793 | 796 | 100.76 | 11.00 | 114 | | | | 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, 06:41 | 7083 | 0.0122 | 619 | 791 | 98.88 | 10.99 | 74 | | | |
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, 00:07 | 6715 | 0.0001 | 336 | 338 | 91.27 | 51.64 | 196 | | | | 2025 Jul 5, 19:52 | 6794 | 0.0003 | 414 | 417 | 92.88 | 51.63 | 338 | | | | 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, 20:04 | 6583 | 0.0022 | 190 | 219 | 88.59 | 51.65 | 73 | | | |
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, 20:00 | 6660 | 0.0001 | 282 | 282 | 90.15 | 53.16 | 43 | | | | 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 | |
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, 08:42 | 37435 | 0.8244 | 197 | 61918 | 1201.38 | 24.22 | 180 | | | | 2025 Jul 16, 03:21 | 37490 | 0.8224 | 282 | 61941 | 1204.00 | 23.85 | 181 | | | | 2025 Jul 20, 02:21 | 43947 | 0.5572 | 13084 | 62055 | 1528.13 | 7.27 | 181 | | | | 2025 Jul 20, 22:46 | 52487 | 0.3043 | 30139 | 62079 | 1994.52 | 1.98 | 183 | | | | 2025 Jul 23, 16:43 | 55323 | 0.2372 | 35820 | 62070 | 2158.35 | 0.83 | 182 | | | | 2025 Jul 25, 18:48 | 45879 | 0.0786 | 35896 | 43106 | 1629.98 | 0.27 | 183 | | | | 2025 Jul 28, 20:03 | 42241 | 0.0013 | 35810 | 35916 | 1439.99 | 0.03 | 82 | 1°.2 E | | | 2025 Jul 31, 08:00 | 42229 | 0.0009 | 35811 | 35891 | 1439.38 | 0.04 | 292 | 1°.1 W | | | 2025 Aug 4, 09:38 | 42174 | 0.0004 | 35780 | 35811 | 1436.55 | 0.04 | 116 | 4°.0 W | | | 2025 Aug 5, 09:37 | 42163 | 0.0002 | 35779 | 35791 | 1436.02 | 0.04 | 135 | 4°.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, 16:55 | 37345 | 0.8239 | 197 | 61736 | 1197.02 | 24.22 | 180 | | | |
2025-149 CZ 7 Wenchang Space Centre | 2025 Jul 14, 21:34 UTC | |
in space
|
| Mission description awaited |
epoch (UTC) | s-m axis ( km ) | eccentricity | perigee ( km ) | apogee ( km ) | period ( min ) | incl ( ° ) | ω ( ° ) | | |
| 2025 Jul 15, 12:22 | 6775 | 0.0009 | 391 | 403 | 92.50 | 41.46 | 284 | | | | 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, 01:44 | 6649 | 0.0104 | 202 | 340 | 89.93 | 41.47 | 174 | | | |
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, 21:18 | 6673 | 0.0003 | 293 | 298 | 90.42 | 70.00 | 282 | | | | 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, 14:53 | 6837 | 0.0006 | 455 | 463 | 93.77 | 51.88 | 159 | | | | 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, 17:04 | 6669 | 0.0000 | 290 | 291 | 90.33 | 97.60 | 353 | | | | 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, 04:00 | 11244 | 0.1964 | 2657 | 7075 | 197.76 | 9.61 | 181 | | | | 2025 Aug 3, 15:11 | 11331 | 0.1877 | 2825 | 7080 | 200.05 | 8.77 | 213 | | | | 2025 Aug 4, 01:11 | 11340 | 0.1867 | 2845 | 7079 | 200.30 | 8.70 | 214 | | | | 2025 Aug 7, 22:49 | 11388 | 0.1857 | 2895 | 7124 | 201.56 | 8.48 | 226 | | | | 2025 Sep 19, 06:56 | 12499 | 0.1008 | 4860 | 7381 | 231.77 | 5.09 | 324 | | | | 2025 Sep 24, 15:58 | 12657 | 0.0994 | 5021 | 7537 | 236.19 | 4.65 | 331 | | | | 2025 Oct 8, 11:25 | 12950 | 0.0761 | 5586 | 7557 | 244.43 | 3.24 | 355 | | | | 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, 04:00 | 11215 | 0.1945 | 2655 | 7019 | 196.99 | 9.69 | 181 | | | | 2025 Jul 31, 07:04 | 11254 | 0.1917 | 2718 | 7033 | 198.02 | 9.34 | 204 | | | | 2025 Jul 31, 07:04 | 11254 | 0.1917 | 2718 | 7033 | 198.02 | 9.34 | 204 | | | | 2025 Aug 5, 22:52 | 11330 | 0.1862 | 2842 | 7061 | 200.03 | 8.75 | 220 | | | | 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, 02:57 | 11201 | 0.1941 | 2649 | 6997 | 196.64 | 9.72 | 184 | | | |
2025-154 Falcon 9 Block 5 (Tracers) Vandenberg Space Force Base | 2025 Jul 23, 18:13 UTC | |
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, 19:21 | 6971 | 0.0005 | 590 | 596 | 96.55 | 97.72 | 228 | 09:56 | | | |
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, 17:52 | 6970 | 0.0004 | 588 | 594 | 96.51 | 97.71 | 262 | 09:56 | | | 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, 22:33 | 6969 | 0.0004 | 588 | 594 | 96.50 | 97.71 | 268 | 09:56 | | | 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, 15:16 | 6969 | 0.0004 | 588 | 594 | 96.50 | 97.71 | 276 | 09:56 | | | |
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, 19:20 | 6969 | 0.0005 | 587 | 594 | 96.49 | 97.72 | 276 | 09:56 | | | |
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, 18:57 | 6892 | 0.0003 | 512 | 516 | 94.90 | 97.44 | 24 | 09:55 | | | |
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, 18:56 | 6890 | 0.0002 | 510 | 513 | 94.85 | 97.45 | 122 | 09:55 | | | 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, 16:18 | 7199 | 0.0002 | 819 | 823 | 101.31 | 98.55 | 82 | 03:16 | | | 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, 16:38 | 7199 | 0.0002 | 820 | 823 | 101.32 | 98.55 | 98 | 03:16 | | | 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, 16:12 | 6880 | 0.0010 | 495 | 509 | 94.66 | 97.41 | 221 | 03:13 | | | 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, 16:08 | 6878 | 0.0008 | 495 | 506 | 94.62 | 97.41 | 213 | 03:13 | | | 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, 16:08 | 6878 | 0.0008 | 495 | 506 | 94.62 | 97.41 | 214 | 03:13 | | | 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, 16:07 | 6878 | 0.0008 | 495 | 505 | 94.61 | 97.41 | 214 | 03:13 | | | |
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, 14:32 | 6878 | 0.0007 | 495 | 505 | 94.61 | 97.41 | 214 | 03:13 | | | 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, 16:05 | 6877 | 0.0008 | 494 | 504 | 94.60 | 97.41 | 199 | 03:13 | | | 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, 16:04 | 6877 | 0.0006 | 494 | 503 | 94.59 | 97.41 | 219 | 03:13 | | | 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, 16:04 | 6877 | 0.0006 | 494 | 503 | 94.59 | 97.41 | 220 | 03:13 | | | 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, 16:04 | 6877 | 0.0006 | 494 | 503 | 94.58 | 97.41 | 222 | 03:13 | | | 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, 11:20 | 6876 | 0.0006 | 494 | 502 | 94.58 | 97.41 | 225 | 03:13 | | | |
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, 16:06 | 6877 | 0.0008 | 494 | 505 | 94.60 | 97.41 | 202 | 03:13 | | | |
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, 16:06 | 6877 | 0.0009 | 493 | 505 | 94.60 | 97.41 | 201 | 03:13 | | | |
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, 16:06 | 6878 | 0.0007 | 495 | 504 | 94.60 | 97.41 | 209 | 03:13 | | | |
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 orbit | 6878 | 0.0007 | 495 | 505 | 94.61 | 97.41 | 213 | 03:13 | | | |
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, 16:07 | 6878 | 0.0007 | 495 | 505 | 94.61 | 97.41 | 213 | 03:13 | | | |
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 orbit | 6878 | 0.0007 | 495 | 505 | 94.61 | 97.41 | 213 | 03:13 | | | |
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, 16:06 | 6877 | 0.0009 | 493 | 505 | 94.60 | 97.41 | 201 | 03:13 | | | |
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, 14:31 | 6877 | 0.0009 | 493 | 505 | 94.60 | 97.41 | 201 | 03:13 | | | 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 | |
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, 19:05 | 7034 | 0.0015 | 645 | 666 | 97.84 | 98.01 | 230 | 10:42 | | | |
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, 00:42 | 6877 | 0.0003 | 496 | 500 | 94.58 | 97.45 | 176 | 10:45 | | | 2025 Aug 25, 12:21 | 6877 | 0.0005 | 496 | 502 | 94.59 | 97.44 | 104 | 10:45 | | | 2025 Aug 26, 12:01 | 6879 | 0.0005 | 497 | 504 | 94.63 | 97.44 | 87 | 10:45 | | | 2025 Aug 28, 12:57 | 6881 | 0.0004 | 500 | 505 | 94.67 | 97.44 | 63 | 10:45 | | | 2025 Aug 29, 06:19 | 6882 | 0.0004 | 501 | 507 | 94.69 | 97.44 | 82 | 10:45 | | | 2025 Sep 1, 02:15 | 6884 | 0.0003 | 504 | 508 | 94.74 | 97.44 | 84 | 10:45 | | | 2025 Sep 2, 22:29 | 6883 | 0.0001 | 504 | 506 | 94.72 | 97.44 | 92 | 10:45 | | | |
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, 00:42 | 6877 | 0.0003 | 497 | 501 | 94.59 | 97.46 | 175 | 10:45 | | | 2025 Aug 4, 22:42 | 6876 | 0.0004 | 495 | 501 | 94.58 | 97.46 | 153 | 10:45 | | | 2025 Sep 5, 07:00 | 6877 | 0.0005 | 495 | 503 | 94.60 | 97.43 | 64 | 10:46 | | | 2025 Sep 16, 22:38 | 6890 | 0.0007 | 507 | 516 | 94.86 | 97.41 | 135 | 10:45 | | | 2025 Oct 8, 09:58 | 6883 | 0.0001 | 504 | 506 | 94.72 | 97.44 | 96 | 10:45 | | | |
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, 23:21 | 6877 | 0.0004 | 496 | 502 | 94.60 | 97.45 | 182 | 10:45 | | | 2025 Aug 4, 10:07 | 6879 | 0.0005 | 497 | 504 | 94.63 | 97.44 | 158 | 10:45 | | | 2025 Aug 15, 11:59 | 6883 | 0.0000 | 505 | 506 | 94.72 | 97.44 | 62 | 10:45 | | | |
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, 00:43 | 6878 | 0.0005 | 496 | 503 | 94.61 | 97.45 | 185 | 10:45 | | | 2025 Aug 4, 11:42 | 6879 | 0.0005 | 497 | 504 | 94.63 | 97.45 | 157 | 10:45 | | | 2025 Aug 14, 05:21 | 6883 | 0.0002 | 503 | 506 | 94.71 | 97.43 | 122 | 10:45 | | | 2025 Aug 17, 04:26 | 6883 | 0.0002 | 504 | 506 | 94.72 | 97.43 | 103 | 10:45 | | | |
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, 18:00 | 6668 | 0.0001 | 289 | 290 | 90.30 | 53.16 | 44 | | | | 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, 20:00 | 6669 | 0.0001 | 289 | 291 | 90.32 | 97.60 | 96 | | | | 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, 08:51 | 7381 | 0.0008 | 997 | 1009 | 105.18 | 86.49 | 217 | | | | 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, 08:51 | 7381 | 0.0008 | 997 | 1009 | 105.17 | 86.50 | 215 | | | | 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, 08:51 | 7380 | 0.0008 | 996 | 1008 | 105.16 | 86.49 | 212 | | | | 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, 10:20 | 7380 | 0.0007 | 996 | 1007 | 105.15 | 86.50 | 205 | | | | 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, 18:15 | 7381 | 0.0007 | 997 | 1008 | 105.17 | 86.49 | 199 | | | | 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, 21:40 | 7293 | 0.0104 | 838 | 991 | 103.30 | 86.50 | 111 | | | |
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, 23:22 | 6881 | 0.0010 | 496 | 510 | 94.68 | 97.40 | 263 | 10:31 | | | 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, 16:31 | 6766 | 0.0170 | 272 | 503 | 92.31 | 97.43 | 353 | | | |
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, 10:29 | 7251 | 0.0008 | 867 | 879 | 102.41 | 50.00 | 272 | | | | 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, 10:29 | 7168 | 0.0119 | 705 | 875 | 100.66 | 50.00 | 87 | | | |
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, 21:55 | 6717 | 0.0001 | 338 | 340 | 91.32 | 53.15 | 105 | | | | 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 | |
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, 14:07 | 7117 | 0.0012 | 730 | 748 | 99.59 | 98.44 | 268 | 18:00 | | | 2025 Sep 4, 06:14 | 7118 | 0.0015 | 729 | 750 | 99.60 | 98.43 | 157 | 18:01 | | | 2025 Sep 4, 21:11 | 7121 | 0.0010 | 735 | 750 | 99.67 | 98.43 | 154 | 18:01 | | | 2025 Sep 12, 15:21 | 7127 | 0.0003 | 746 | 751 | 99.79 | 98.41 | 117 | 18:01 | | | 2025 Sep 15, 14:55 | 7128 | 0.0001 | 749 | 751 | 99.82 | 98.41 | 82 | 18:01 | | | 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, 05:02 | 7112 | 0.0011 | 726 | 742 | 99.48 | 98.44 | 304 | | | |
2025-164 Kuaizhou-1A-Pro Xichang Space Centre | 2025 Jul 31, 02:00 UTC | |
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, 08:04 | 6929 | 0.0006 | 546 | 555 | 95.67 | 41.13 | 246 | | | | 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, 18:00 | 6722 | 0.0002 | 343 | 346 | 91.42 | 97.61 | 92 | | | | 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, 16:04 | 6581 | 0.0017 | 192 | 214 | 88.55 | 51.65 | 7 | | | | 2025 Aug 2, 11:35 | 6794 | 0.0002 | 415 | 417 | 92.89 | 51.63 | 144 | | | | 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, 13:33 | 6719 | 0.0000 | 340 | 341 | 91.35 | 53.15 | 119 | | | | 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, 13:19 | 7276 | 0.0007 | 893 | 903 | 102.95 | 50.00 | 232 | | | | 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, 11:11 | 6955 | 0.0007 | 572 | 582 | 96.21 | 42.01 | 295 | | | | 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, 14:22 | 6954 | 0.0008 | 570 | 581 | 96.18 | 42.01 | 295 | | | | 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, 05:07 | 6775 | 0.0258 | 222 | 571 | 92.49 | 42.04 | 275 | | | |
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, 13:11 | 6973 | 0.0014 | 585 | 604 | 96.58 | 49.99 | 303 | | | | 2026 Jan 1, 03:27 | 6997 | 0.0011 | 611 | 626 | 97.07 | 49.99 | 129 | | | | 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, 21:00 | 6746 | 0.0320 | 153 | 584 | 91.91 | 50.16 | 347 | | | |
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, 20:00 | 6837 | 0.0006 | 455 | 463 | 93.77 | 51.88 | 146 | | | | 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 | |
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, 01:55 | 7183 | 0.0001 | 804 | 806 | 100.98 | 98.72 | 113 | 09:30 | | | 2025 Aug 14, 17:05 | 7190 | 0.0009 | 806 | 818 | 101.13 | 98.71 | 359 | 09:30 | | | 2025 Aug 15, 03:12 | 7191 | 0.0007 | 807 | 818 | 101.14 | 98.71 | 359 | 09:30 | | | 2025 Sep 4, 20:48 | 7193 | 0.0007 | 810 | 820 | 101.19 | 98.71 | 317 | 09:31 | | | 2025 Sep 17, 19:16 | 7193 | 0.0006 | 811 | 819 | 101.19 | 98.71 | 284 | 09:31 | | | 2025 Oct 16, 03:18 | 7193 | 0.0007 | 810 | 820 | 101.20 | 98.70 | 185 | 09:31 | | | 2025 Oct 30, 21:44 | 7198 | 0.0001 | 819 | 821 | 101.30 | 98.70 | 110 | 09:31 | | | 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 | | |
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, 20:13 | 42532 | 0.0009 | 36116 | 36192 | 1454.91 | 2.85 | 181 | | | | |
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, 02:03 | 7481 | 0.0009 | 1096 | 1109 | 107.32 | 86.50 | 297 | | | | 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, 14:00 | 6661 | 0.0001 | 282 | 284 | 90.18 | 97.60 | 72 | | | | 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, 16:00 | 6665 | 0.0001 | 287 | 288 | 90.26 | 53.16 | 59 | | | | 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, 22:32 | 7172 | 0.0004 | 791 | 797 | 100.75 | 11.00 | 41 | | | | 2025 Aug 24, 16:31 | 7173 | 0.0003 | 792 | 797 | 100.76 | 11.00 | 160 | | | | 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, 14:13 | 7381 | 0.0009 | 996 | 1009 | 105.18 | 86.50 | 218 | | | | 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, 14:12 | 7381 | 0.0009 | 996 | 1009 | 105.17 | 86.50 | 217 | | | | 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, 14:12 | 7380 | 0.0008 | 996 | 1008 | 105.16 | 86.49 | 212 | | | | 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, 14:12 | 7380 | 0.0008 | 996 | 1007 | 105.15 | 86.50 | 205 | | | | 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, 14:12 | 7379 | 0.0007 | 996 | 1007 | 105.15 | 86.50 | 204 | | | | 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, 13:48 | 7291 | 0.0105 | 836 | 989 | 103.26 | 86.51 | 112 | | | |
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, 14:00 | 6667 | 0.0002 | 288 | 290 | 90.30 | 97.60 | 88 | | | | 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, 18:49 | 6909 | 0.0014 | 521 | 540 | 95.25 | 97.49 | 284 | 13:59 | | | 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, 02:45 | 6903 | 0.0015 | 514 | 536 | 95.13 | 97.51 | 148 | 13:58 | | | 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, 18:45 | 6909 | 0.0014 | 521 | 541 | 95.25 | 97.49 | 284 | 13:59 | | | 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, 18:44 | 6909 | 0.0014 | 521 | 541 | 95.25 | 97.49 | 283 | 13:59 | | | 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, 18:49 | 6909 | 0.0014 | 522 | 541 | 95.26 | 97.49 | 281 | 13:59 | | | 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, 22:30 | 6785 | 0.0215 | 261 | 552 | 92.69 | 97.58 | 29 | | | |
2025-181 Soyuz-2.1b Baikonur Cosmodrome | 2025 Aug 20, 17:13 UTC | |
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, 14:46 | 6676 | 0.0092 | 236 | 360 | 90.48 | 96.94 | 75 | 10:05 | | | 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, 20:06 | 6645 | 0.0115 | 191 | 344 | 89.86 | 96.95 | 58 | | | |
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, 12:07 | 6707 | 0.0013 | 321 | 338 | 91.11 | 96.59 | 229 | 01:09 | | | 2026 Apr 23, 06:11 | 6663 | 0.0007 | 280 | 289 | 90.20 | 96.59 | 51 | 00:57 | | | 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, 18:27 | 6708 | 0.0012 | 322 | 338 | 91.13 | 96.59 | 248 | 01:10 | | | 2026 Apr 23, 06:33 | 6663 | 0.0007 | 280 | 289 | 90.20 | 96.59 | 51 | 00:56 | | | 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, 05:05 | 6708 | 0.0012 | 321 | 338 | 91.12 | 96.59 | 245 | 01:09 | | | 2026 Apr 23, 02:25 | 6663 | 0.0007 | 280 | 289 | 90.20 | 96.59 | 48 | 00:56 | | | 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, 05:05 | 6708 | 0.0012 | 321 | 338 | 91.12 | 96.59 | 244 | 01:10 | | | 2026 Apr 23, 05:48 | 6663 | 0.0006 | 281 | 289 | 90.21 | 96.59 | 46 | 00:56 | | | 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, 08:42 | 6713 | 0.0002 | 333 | 336 | 91.22 | 48.80 | 85 | | | | 2026 Mar 5, 18:12 | 6770 | 0.0004 | 390 | 394 | 92.40 | 49.52 | 283 | | | | 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, 19:27 | 6707 | 0.0006 | 325 | 333 | 91.11 | 49.52 | 21 | | | | 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, 14:00 | 6678 | 0.0001 | 299 | 301 | 90.52 | 97.60 | 84 | | | | 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 | |
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, 22:15 | 7039 | 0.0012 | 653 | 669 | 97.96 | 97.97 | 317 | 11:05 | | | |
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, 16:13 | 7039 | 0.0012 | 652 | 669 | 97.95 | 97.97 | 307 | 11:05 | | | |
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, 22:15 | 7039 | 0.0012 | 653 | 669 | 97.95 | 97.97 | 312 | 11:05 | | | |
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, 16:13 | 7039 | 0.0012 | 653 | 669 | 97.96 | 97.97 | 313 | 11:05 | | | |
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, 14:35 | 7039 | 0.0010 | 654 | 668 | 97.96 | 97.97 | 300 | 11:05 | | | 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, 14:35 | 7039 | 0.0012 | 652 | 669 | 97.95 | 97.97 | 311 | 11:05 | | | 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, 16:11 | 6782 | 0.0342 | 173 | 636 | 92.65 | 97.97 | 223 | 11:05 | | |
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, 07:45 | 6753 | 0.0003 | 373 | 377 | 92.05 | 51.55 | 218 | | | | 2025 Aug 27, 11:53 | 6794 | 0.0003 | 414 | 418 | 92.89 | 51.63 | 279 | | | | 2026 Feb 26, 13:00 | 6800 | 0.0008 | 416 | 427 | 93.00 | 51.63 | 136 | | | | 2026 Feb 26, 22:17 | 6800 | 0.0008 | 416 | 427 | 93.00 | 51.63 | 137 | | | | 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, 14:52 | 7250 | 0.0007 | 867 | 877 | 102.40 | 50.01 | 274 | | | | 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, 14:09 | 7168 | 0.0116 | 707 | 873 | 100.67 | 50.01 | 89 | | | |
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, 22:31 | 6839 | 0.0004 | 458 | 463 | 93.80 | 97.25 | 142 | 10:32 | | | 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, 22:31 | 6839 | 0.0005 | 458 | 464 | 93.82 | 97.26 | 149 | 10:32 | | | |
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, 22:31 | 6839 | 0.0005 | 458 | 465 | 93.82 | 97.25 | 149 | 10:32 | | | 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, 13:50 | 6976 | 0.0005 | 595 | 602 | 96.65 | 97.77 | 124 | 10:33 | | | |
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, 13:50 | 6977 | 0.0006 | 595 | 603 | 96.66 | 97.76 | 117 | 10:33 | | | |
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, 13:51 | 6978 | 0.0004 | 596 | 603 | 96.68 | 97.77 | 104 | 10:33 | | | |
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, 13:51 | 6978 | 0.0005 | 597 | 603 | 96.68 | 97.77 | 97 | 10:33 | | | 2026 Jan 8, 22:47 | 6974 | 0.0004 | 594 | 599 | 96.61 | 97.75 | 37 | 10:31 | | | |
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, 13:51 | 6978 | 0.0005 | 597 | 603 | 96.69 | 97.77 | 94 | 10:33 | | | 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, 22:00 | 6683 | 0.0001 | 304 | 305 | 90.61 | 53.16 | 83 | | | | 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, 22:00 | 6781 | 0.0001 | 402 | 404 | 92.63 | 53.16 | 110 | | | | 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, 22:00 | 6694 | 0.0001 | 315 | 317 | 90.84 | 97.60 | 81 | | | | 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, 06:00 | 6756 | 0.0001 | 377 | 379 | 92.12 | 53.16 | 80 | | | | 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, 08:51 | 6911 | 0.0165 | 419 | 647 | 95.30 | 139.35 | 272 | | | | 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, 09:14 | 6838 | 0.0233 | 300 | 619 | 93.78 | 139.41 | 265 | | | |
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, 06:00 | 6756 | 0.0002 | 376 | 379 | 92.10 | 97.60 | 72 | | | | 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, 06:00 | 6700 | 0.0001 | 321 | 322 | 90.97 | 53.16 | 85 | | | | 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 | |
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, 21:41 | 42563 | 0.0091 | 35799 | 36571 | 1456.50 | 28.51 | 131 | | | | 2025 Sep 29, 17:13 | 42508 | 0.0079 | 35794 | 36466 | 1453.68 | 28.54 | 127 | | | | 2025 Oct 1, 07:39 | 42218 | 0.0024 | 35740 | 35940 | 1438.81 | 28.54 | 182 | 98°.6 E | | | 2025 Oct 6, 14:39 | 42164 | 0.0011 | 35739 | 35833 | 1436.06 | 28.54 | 175 | 95°.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, 10:02 | 21848 | 0.6977 | 227 | 30712 | 535.63 | 28.49 | 130 | | | |
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, 03:51 | 6882 | 0.0014 | 494 | 514 | 94.70 | 97.41 | 276 | 17:57 | | | 2025 Sep 28, 19:45 | 6880 | 0.0014 | 492 | 512 | 94.66 | 97.41 | 198 | 17:57 | | | 2025 Sep 29, 21:01 | 6879 | 0.0013 | 492 | 510 | 94.64 | 97.41 | 194 | 17:57 | | | 2025 Oct 6, 23:29 | 6881 | 0.0016 | 492 | 514 | 94.68 | 97.41 | 170 | 17:57 | | | 2025 Oct 9, 03:35 | 6882 | 0.0016 | 493 | 515 | 94.70 | 97.41 | 167 | 17:57 | | | 2025 Oct 10, 19:05 | 6885 | 0.0016 | 496 | 518 | 94.76 | 97.41 | 154 | 17:57 | | | 2025 Oct 17, 15:38 | 6895 | 0.0015 | 507 | 527 | 94.97 | 97.41 | 131 | 17:57 | | | 2025 Oct 23, 23:53 | 6907 | 0.0013 | 520 | 538 | 95.22 | 97.41 | 115 | 17:57 | | | 2025 Nov 16, 11:51 | 6909 | 0.0015 | 520 | 541 | 95.25 | 97.41 | 37 | 17:55 | | | 2025 Nov 22, 04:28 | 6910 | 0.0015 | 521 | 542 | 95.27 | 97.41 | 19 | 17:55 | | | 2025 Nov 29, 03:23 | 6915 | 0.0015 | 527 | 547 | 95.39 | 97.40 | 354 | 17:54 | | | 2025 Dec 6, 05:41 | 6919 | 0.0013 | 532 | 550 | 95.47 | 97.41 | 330 | 17:54 | | | 2025 Dec 13, 16:05 | 6922 | 0.0013 | 535 | 553 | 95.52 | 97.41 | 301 | 17:53 | | | 2025 Dec 20, 04:10 | 6919 | 0.0013 | 532 | 550 | 95.46 | 97.41 | 284 | 17:53 | | | 2025 Dec 25, 06:43 | 6918 | 0.0013 | 531 | 548 | 95.44 | 97.41 | 266 | 17:52 | | | 2026 Feb 10, 21:17 | 6916 | 0.0015 | 527 | 548 | 95.40 | 97.41 | 101 | 17:48 | | | 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, 03:51 | 6882 | 0.0013 | 495 | 513 | 94.69 | 97.41 | 278 | 17:57 | | | 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, 03:50 | 6881 | 0.0014 | 493 | 513 | 94.68 | 97.41 | 282 | 17:57 | | | 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, 03:50 | 6881 | 0.0014 | 493 | 512 | 94.67 | 97.41 | 283 | 17:57 | | | 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, 13:26 | 6703 | 0.0001 | 325 | 326 | 91.03 | 53.15 | 329 | | | | 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, 16:50 | 7181 | 0.0011 | 795 | 811 | 100.94 | 86.00 | 258 | | | | 2025 Sep 12, 20:14 | 7193 | 0.0011 | 807 | 824 | 101.20 | 86.00 | 340 | | | | 2025 Sep 15, 19:16 | 7218 | 0.0004 | 836 | 843 | 101.71 | 86.00 | 313 | | | | 2025 Sep 19, 04:50 | 7229 | 0.0002 | 850 | 853 | 101.96 | 86.00 | 113 | | | | 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, 16:50 | 7181 | 0.0011 | 795 | 811 | 100.93 | 86.00 | 260 | | | | 2025 Sep 11, 08:48 | 7184 | 0.0009 | 800 | 812 | 101.00 | 86.00 | 273 | | | | 2025 Sep 14, 14:23 | 7191 | 0.0013 | 803 | 822 | 101.14 | 86.00 | 264 | | | | 2025 Sep 15, 19:19 | 7216 | 0.0018 | 825 | 850 | 101.67 | 86.00 | 295 | | | | 2025 Sep 18, 03:20 | 7222 | 0.0008 | 839 | 850 | 101.81 | 86.00 | 288 | | | | 2025 Sep 23, 22:45 | 7229 | 0.0002 | 850 | 853 | 101.96 | 86.00 | 84 | | | | 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, 21:48 | 7177 | 0.0015 | 789 | 810 | 100.86 | 86.00 | 244 | | | | 2025 Sep 15, 03:34 | 7169 | 0.0006 | 786 | 795 | 100.68 | 86.00 | 280 | | | | 2025 Sep 16, 04:44 | 7163 | 0.0014 | 775 | 795 | 100.56 | 86.00 | 271 | | | | 2025 Oct 30, 23:42 | 7164 | 0.0019 | 772 | 800 | 100.59 | 85.99 | 124 | | | | 2025 Oct 31, 16:28 | 7170 | 0.0026 | 773 | 810 | 100.69 | 85.99 | 131 | | | | 2025 Nov 2, 07:08 | 7177 | 0.0025 | 781 | 817 | 100.86 | 85.99 | 102 | | | | 2025 Nov 3, 20:12 | 7195 | 0.0026 | 798 | 835 | 101.22 | 85.99 | 106 | | | | 2025 Nov 4, 13:05 | 7203 | 0.0015 | 814 | 836 | 101.41 | 85.99 | 89 | | | | 2025 Nov 5, 22:56 | 7213 | 0.0004 | 831 | 837 | 101.60 | 85.99 | 120 | | | | 2025 Nov 7, 19:03 | 7229 | 0.0002 | 849 | 852 | 101.95 | 85.99 | 77 | | | | 2025 Nov 10, 23:34 | 7229 | 0.0002 | 849 | 853 | 101.95 | 85.99 | 88 | | | | 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, 22:48 | 7058 | 0.0070 | 630 | 730 | 98.36 | 86.02 | 60 | | | |
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, 16:00 | 6687 | 0.0001 | 308 | 310 | 90.71 | 97.60 | 76 | | | | 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, 03:28 | 6973 | 0.0013 | 586 | 604 | 96.58 | 49.98 | 297 | | | | 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, 01:28 | 6760 | 0.0337 | 154 | 610 | 92.19 | 50.16 | 347 | | | |
2025-202 CZ 7A Wenchang Space Centre | 2025 Sep 9, 02:00 UTC | |
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, 12:25 | 13877 | 0.0001 | 7497 | 7500 | 271.14 | 20.01 | 265 | | | | 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, 09:27 | 8104 | 0.1982 | 120 | 3333 | 121.01 | 20.05 | 6 | | | |
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, 16:00 | 7326 | 0.0006 | 943 | 952 | 104.00 | 81.30 | 183 | | | | 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, 23:01 | 6636 | 0.0011 | 251 | 265 | 89.66 | 51.64 | 156 | | | | 2025 Sep 13, 20:04 | 6794 | 0.0004 | 413 | 419 | 92.89 | 51.63 | 336 | | | | 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, 21:37 | 6582 | 0.0024 | 187 | 219 | 88.56 | 51.66 | 76 | | | |
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, 02:27 | 14368 | 0.5387 | 249 | 15729 | 285.65 | 26.48 | 174 | | | | 2025 Sep 18, 16:15 | 18931 | 0.6495 | 257 | 24850 | 432.05 | 26.30 | 179 | | | | 2025 Sep 20, 19:46 | 35512 | 0.7036 | 4148 | 54120 | 1110.01 | 13.10 | 180 | | | | 2025 Sep 24, 17:54 | 42169 | 0.4489 | 16863 | 54720 | 1436.33 | 0.32 | 107 | 112°.8 E | | | 2025 Sep 30, 14:36 | 42243 | 0.4447 | 17081 | 54648 | 1440.08 | 0.31 | 107 | 112°.0 E | | | 2025 Oct 14, 19:16 | 42144 | 0.4043 | 18728 | 52804 | 1435.04 | 0.27 | 111 | 110°.4 E | | | 2025 Oct 28, 18:54 | 43065 | 0.3670 | 20884 | 52489 | 1482.31 | 0.22 | 84 | | | | 2025 Nov 12, 16:43 | 44117 | 0.3233 | 23477 | 52002 | 1537.00 | 0.18 | 84 | | | | 2025 Nov 26, 16:18 | 45318 | 0.2811 | 26200 | 51680 | 1600.17 | 0.15 | 81 | | | | 2025 Dec 8, 17:39 | 46955 | 0.2281 | 29868 | 51285 | 1687.65 | 0.13 | 86 | | | | 2025 Dec 22, 03:53 | 42163 | 0.1288 | 30353 | 41217 | 1436.02 | 0.11 | 55 | 112°.9 E | | | 2026 Jan 8, 01:06 | 42183 | 0.0804 | 32412 | 39198 | 1437.05 | 0.10 | 30 | 106°.7 E | | | 2026 Jan 18, 04:06 | 42132 | 0.0457 | 33828 | 37680 | 1434.43 | 0.10 | 15 | 108°.9 E | | | 2026 Jan 31, 02:04 | 42164 | 0.0001 | 35783 | 35790 | 1436.07 | 0.11 | 16 | 112°.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, 16:12 | 25504 | 0.0011 | 19097 | 19154 | 675.55 | 64.80 | 290 | | | | 2025 Sep 25, 08:02 | 25429 | 0.0231 | 18463 | 19639 | 672.60 | 68.24 | 120 | | | | 2025 Sep 30, 01:54 | 25481 | 0.0016 | 19062 | 19145 | 674.67 | 64.79 | 263 | | | | 2025 Oct 12, 05:41 | 25508 | 0.0013 | 19096 | 19164 | 675.74 | 64.78 | 302 | | | | 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, 05:00 | 25373 | 0.0194 | 18502 | 19487 | 670.37 | 64.79 | 276 | | | | 2025 Oct 15, 07:19 | 25385 | 0.0011 | 18980 | 19034 | 670.86 | 64.78 | 181 | | | |
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, 16:00 | 6695 | 0.0001 | 315 | 317 | 90.85 | 97.60 | 77 | | | | 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, 22:20 | 6621 | 0.0002 | 242 | 245 | 89.37 | 51.65 | 154 | | | | 2025 Sep 16, 06:53 | 6695 | 0.0103 | 248 | 386 | 90.87 | 51.66 | 34 | | | | 2025 Sep 18, 22:16 | 6794 | 0.0004 | 413 | 418 | 92.88 | 51.63 | 355 | | | | 2026 Mar 12, 03:49 | 6799 | 0.0008 | 415 | 426 | 92.99 | 51.63 | 183 | | | | 2026 Mar 13, 13:52 | 6795 | 0.0008 | 412 | 422 | 92.91 | 51.63 | 190 | | | | 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, 05:11 | 7188 | 0.0002 | 808 | 811 | 101.07 | 50.00 | 156 | | | | 2025 Oct 21, 06:08 | 7216 | 0.0022 | 823 | 854 | 101.68 | 49.98 | 18 | | | | 2025 Oct 22, 16:01 | 7224 | 0.0001 | 846 | 846 | 101.84 | 50.00 | 347 | | | | 2025 Oct 23, 05:36 | 7227 | 0.0004 | 846 | 851 | 101.90 | 49.99 | 22 | | | | 2025 Nov 1, 12:59 | 7257 | 0.0003 | 877 | 881 | 102.55 | 50.00 | 26 | | | | 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, 05:11 | 7187 | 0.0002 | 808 | 811 | 101.07 | 50.00 | 159 | | | | 2025 Sep 20, 22:25 | 7188 | 0.0002 | 809 | 812 | 101.09 | 50.00 | 173 | | | | 2025 Oct 21, 02:46 | 7220 | 0.0014 | 832 | 852 | 101.76 | 50.01 | 13 | | | | 2025 Oct 22, 10:58 | 7223 | 0.0001 | 844 | 845 | 101.81 | 50.00 | 307 | | | | 2025 Oct 24, 17:19 | 7239 | 0.0002 | 859 | 862 | 102.15 | 50.00 | 350 | | | | 2025 Nov 1, 13:03 | 7257 | 0.0003 | 877 | 881 | 102.55 | 50.00 | 30 | | | | 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, 05:11 | 7187 | 0.0002 | 808 | 810 | 101.06 | 50.00 | 163 | | | | 2025 Sep 20, 22:25 | 7188 | 0.0002 | 809 | 811 | 101.08 | 50.00 | 179 | | | | 2025 Oct 21, 21:19 | 7219 | 0.0002 | 840 | 843 | 101.75 | 50.00 | 309 | | | | 2025 Oct 22, 04:06 | 7221 | 0.0001 | 842 | 843 | 101.77 | 50.00 | 358 | | | | 2025 Oct 23, 19:08 | 7231 | 0.0002 | 852 | 854 | 102.00 | 50.00 | 16 | | | | 2025 Nov 1, 12:54 | 7257 | 0.0002 | 878 | 881 | 102.55 | 50.00 | 45 | | | | 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, 05:11 | 7187 | 0.0002 | 808 | 810 | 101.06 | 50.00 | 173 | | | | 2025 Oct 15, 20:00 | 7189 | 0.0001 | 810 | 812 | 101.10 | 50.00 | 308 | | | | 2025 Oct 18, 00:15 | 7199 | 0.0003 | 819 | 824 | 101.32 | 50.00 | 352 | | | | 2025 Oct 21, 19:27 | 7207 | 0.0002 | 828 | 831 | 101.49 | 50.00 | 357 | | | | 2025 Oct 22, 19:07 | 7209 | 0.0002 | 830 | 832 | 101.53 | 50.00 | 7 | | | | 2025 Nov 14, 18:48 | 7257 | 0.0003 | 877 | 882 | 102.55 | 50.00 | 63 | | | | 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, 14:53 | 6871 | 0.0528 | 130 | 855 | 94.47 | 49.98 | 313 | | | |
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, 14:00 | 6695 | 0.0001 | 316 | 318 | 90.86 | 53.16 | 16 | | | | 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 | |
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, 11:13 | 6789 | 0.0001 | 411 | 412 | 92.79 | 51.63 | 109 | | | | 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, 11:13 | 6789 | 0.0001 | 411 | 412 | 92.79 | 51.63 | 109 | | | |
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, 11:13 | 6789 | 0.0001 | 411 | 412 | 92.79 | 51.63 | 109 | | | | 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, 11:13 | 6789 | 0.0001 | 411 | 412 | 92.79 | 51.63 | 109 | | | | |
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, 11:13 | 6789 | 0.0001 | 411 | 412 | 92.79 | 51.63 | 109 | | | |
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, 02:32 | 6670 | 0.0003 | 290 | 294 | 90.35 | 97.60 | 36 | | | | 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, 12:42 | 6733 | 0.0002 | 354 | 357 | 91.65 | 53.16 | 196 | | | | 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, 17:23 | 6955 | 0.0001 | 576 | 578 | 96.21 | 69.99 | 271 | | | | 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, 17:42 | 6955 | 0.0001 | 576 | 578 | 96.21 | 69.99 | 271 | | | | 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, 16:45 | 6955 | 0.0002 | 576 | 578 | 96.21 | 69.99 | 179 | | | | 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, 16:55 | 6955 | 0.0002 | 576 | 578 | 96.21 | 69.99 | 179 | | | | 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, 16:39 | 6955 | 0.0002 | 576 | 578 | 96.21 | 69.99 | 177 | | | | 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, 16:02 | 6955 | 0.0001 | 576 | 578 | 96.21 | 69.99 | 260 | | | | 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, 05:40 | 6955 | 0.0001 | 576 | 578 | 96.21 | 69.99 | 194 | | | | 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, 17:13 | 6973 | 0.0013 | 586 | 604 | 96.58 | 49.98 | 298 | | | | 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, 17:13 | 6973 | 0.0013 | 585 | 604 | 96.58 | 49.99 | 297 | | | | 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, 14:08 | 6709 | 0.0001 | 330 | 332 | 91.15 | 53.15 | 93 | | | | 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, 16:46 | 6843 | 0.0011 | 457 | 472 | 93.89 | 51.87 | 119 | | | | 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, 14:55 | 6703 | 0.0000 | 324 | 325 | 91.02 | 97.60 | 50 | | | | 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, 23:33 | 7185 | 0.0009 | 800 | 813 | 101.01 | 98.64 | 246 | 01:41 | | | 2025 Sep 29, 09:16 | 7191 | 0.0013 | 803 | 822 | 101.14 | 98.64 | 208 | 01:41 | | | 2025 Oct 10, 14:09 | 7204 | 0.0002 | 825 | 827 | 101.42 | 98.65 | 82 | 01:40 | | | 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, 16:25 | 7095 | 0.0122 | 630 | 803 | 99.12 | 98.63 | 40 | | | |
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, 07:22 | 7381 | 0.0008 | 997 | 1009 | 105.18 | 86.50 | 219 | | | | 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, 07:22 | 7381 | 0.0008 | 997 | 1009 | 105.18 | 86.50 | 218 | | | | 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, 07:22 | 7380 | 0.0007 | 997 | 1008 | 105.17 | 86.49 | 213 | | | | 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, 07:22 | 7380 | 0.0007 | 997 | 1007 | 105.16 | 86.50 | 205 | | | | 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, 07:22 | 7380 | 0.0007 | 997 | 1006 | 105.15 | 86.50 | 204 | | | | 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, 07:03 | 7292 | 0.0106 | 837 | 991 | 103.29 | 86.51 | 112 | | | |
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, 15:04 | 6685 | 0.0001 | 307 | 308 | 90.66 | 53.16 | 120 | | | | 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, 00:59 | 6966 | 0.0004 | 585 | 590 | 96.43 | 34.99 | 308 | | | | 2025 Oct 5, 04:33 | 6967 | 0.0005 | 586 | 593 | 96.46 | 34.99 | 10 | | | | 2025 Dec 18, 09:54 | 6965 | 0.0006 | 583 | 592 | 96.42 | 34.99 | 291 | | | | 2025 Dec 18, 22:45 | 6968 | 0.0006 | 585 | 594 | 96.47 | 34.99 | 266 | | | | 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, 23:23 | 6965 | 0.0005 | 584 | 591 | 96.42 | 35.00 | 308 | | | | 2025 Oct 5, 04:32 | 6967 | 0.0006 | 585 | 594 | 96.46 | 35.00 | 16 | | | | 2025 Dec 18, 09:53 | 6965 | 0.0007 | 582 | 592 | 96.42 | 35.00 | 295 | | | | 2025 Dec 18, 22:44 | 6968 | 0.0006 | 585 | 594 | 96.47 | 35.00 | 275 | | | | 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, 13:43 | 6948 | 0.0057 | 530 | 609 | 96.06 | 34.90 | 335 | | | |
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, 02:47 | 6719 | 0.0002 | 340 | 342 | 91.35 | 53.15 | 352 | | | | 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, 14:00 | 6673 | 0.0001 | 294 | 295 | 90.41 | 53.15 | 62 | | | | 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, 20:00 | 6725 | 0.0001 | 346 | 348 | 91.48 | 53.15 | 80 | | | | 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, 08:46 | 6793 | 0.0003 | 413 | 417 | 92.87 | 51.63 | 190 | | | |
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, 07:58 | 6793 | 0.0003 | 412 | 417 | 92.86 | 51.63 | 233 | | | | |
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, 07:58 | 6793 | 0.0004 | 412 | 417 | 92.86 | 51.63 | 236 | | | |
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, 00:03 | 6910 | 0.0014 | 522 | 542 | 95.28 | 97.67 | 282 | 10:33 | | | 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, 08:00 | 6911 | 0.0014 | 523 | 542 | 95.29 | 97.66 | 276 | 10:33 | | | 2025 Oct 14, 21:58 | 6911 | 0.0014 | 523 | 543 | 95.30 | 97.66 | 263 | 10:33 | | | 2025 Oct 15, 09:06 | 6914 | 0.0018 | 523 | 548 | 95.36 | 97.66 | 269 | 10:33 | | | 2025 Oct 23, 22:19 | 6916 | 0.0020 | 523 | 551 | 95.39 | 97.66 | 241 | 10:33 | | | 2025 Dec 5, 22:38 | 6917 | 0.0021 | 524 | 553 | 95.41 | 97.66 | 85 | 10:36 | | | 2025 Dec 9, 07:48 | 6918 | 0.0021 | 526 | 555 | 95.45 | 97.66 | 67 | 10:36 | | | 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, 00:03 | 6911 | 0.0014 | 523 | 542 | 95.29 | 97.66 | 279 | 10:33 | | | 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, 18:31 | 6786 | 0.0164 | 297 | 519 | 92.72 | 97.79 | 339 | | | |
2025-227 CZ 2D Jiuquan Space Centre | 2025 Oct 13, 10:00 UTC | |
in space
|
| Mission description awaited |
epoch (UTC) | s-m axis ( km ) | eccentricity | perigee ( km ) | apogee ( km ) | period ( min ) | incl ( ° ) | ω ( ° ) | | |
| 2025 Oct 14, 07:35 | 6884 | 0.0011 | 498 | 513 | 94.73 | 80.00 | 266 | | | | 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, 21:39 | 6863 | 0.0022 | 470 | 500 | 94.30 | 80.15 | 31 | | | |
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, 14:00 | 6841 | 0.0006 | 459 | 467 | 93.85 | 51.88 | 167 | | | |
2025-229 Electron (Owl New World) Rocket Lab Launch Complex, New Zealand | 2025 Oct 14, 16:33 UTC | |
in space
|
| Mission description awaited |
epoch (UTC) | s-m axis ( km ) | eccentricity | perigee ( km ) | apogee ( km ) | period ( min ) | incl ( ° ) | ω ( ° ) | | |
| 2025 Oct 15, 17:03 | 6941 | 0.0041 | 534 | 591 | 95.91 | 41.93 | 254 | | | | 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, 17:31 | 6730 | 0.0267 | 172 | 532 | 91.57 | 41.88 | 243 | | | | 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, 20:13 | 6938 | 0.0042 | 531 | 589 | 95.85 | 41.98 | 255 | | | |
2025-230 Falcon 9 Block 5 Vandenberg Space Force Base | 2025 Oct 15, 23:06 UTC | |
in space
|
| Mission description awaited |
epoch (UTC) | s-m axis ( km ) | eccentricity | perigee ( km ) | apogee ( km ) | period ( min ) | incl ( ° ) | ω ( ° ) | | |
| 2025 Oct 30, 07:30 | 7325 | 0.0004 | 945 | 950 | 103.99 | 81.30 | 73 | | | | 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, 09:14 | 7253 | 0.0007 | 870 | 880 | 102.46 | 50.00 | 260 | | | | 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, 22:00 | 6683 | 0.0001 | 304 | 305 | 90.61 | 53.16 | 62 | | | | 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, 23:20 | 7184 | 0.0016 | 794 | 817 | 100.99 | 88.99 | 169 | | | | 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, 23:33 | 7081 | 0.0086 | 642 | 764 | 98.83 | 89.03 | 76 | | | |
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, 02:41 | 6880 | 0.0015 | 492 | 512 | 94.66 | 97.51 | 282 | 09:59 | | | 2025 Oct 27, 14:40 | 6881 | 0.0014 | 493 | 512 | 94.67 | 97.50 | 250 | 10:00 | | | 2026 Jan 9, 04:37 | 6877 | 0.0014 | 489 | 509 | 94.59 | 97.50 | 1 | 10:03 | | | 2026 Jan 27, 19:18 | 6886 | 0.0011 | 500 | 515 | 94.78 | 97.49 | 219 | 10:04 | | | 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, 02:41 | 6881 | 0.0014 | 493 | 512 | 94.67 | 97.46 | 281 | 09:59 | | | 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, 02:41 | 6881 | 0.0014 | 493 | 513 | 94.67 | 97.46 | 279 | 09:59 | | | 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, 02:41 | 6880 | 0.0014 | 492 | 512 | 94.65 | 97.46 | 285 | | | |
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, 17:53 | 6694 | 0.0001 | 316 | 317 | 90.85 | 53.15 | 345 | | | | 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) | |