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| 2026 - 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.
2026-001 Falcon 9 Block 5
Vandenberg Space Force Base | 2026 Jan 3, 02:09 UTC | COSMO-Skymed 5 2026-001A 67304 |
in space
|
| Second generation satellite as part of the COnstellation of small Satellites for Mediterranean basin Observation, equipped with a synthetic aperture imaging radar (SAR). Separated from launch vehicle at 02:22 UTC. Orbit maintained by occasional operation of a thruster. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 3, 22:41 | 7003 | 0.0004 | 622 | 627 | 97.20 | 97.86 | 173 | 17:45 | | | 2026 Jan 15, 05:22 | 7000 | 0.0002 | 621 | 623 | 97.15 | 97.85 | 90 | 17:45 | | | 2026 Jan 17, 07:35 | 7000 | 0.0002 | 620 | 623 | 97.13 | 97.84 | 89 | 17:45 | | | 2026 Jan 31, 23:06 | 7001 | 0.0001 | 622 | 623 | 97.16 | 97.87 | 84 | 17:45 | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 2
Life <1 day
|
| Launched COSMO-Skymed 5. Caused to re-enter after releasing satellite. |
| Not Catalogued - orbit parameters unavailable | |
2026-002 Falcon 9 Block 5 (Starlink Group 06-088)
Cape Canaveral Space Force Station | 2026 Jan 4, 06:48 UTC | Starlink 36490 2026-002A 67305 |
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 06:48 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
( ° ) | | |
| 2026 Jan 7, 18:00 | 6639 | 0.0002 | 260 | 263 | 89.73 | 43.00 | 257 | | | | 2026 Jun 16, 04:05 | 6861 | 0.0001 | 482 | 484 | 94.27 | 43.01 | 279 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 4
Life <1 day
|
| Launched Starlink Group 06-088. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-003 Falcon 9 Block 5 (Starlink Group 06-096)
Cape Canaveral Space Force Station | 2026 Jan 10, 00:41 UTC | Starlink 35343 2026-003A 67334 |
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 01:46 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
( ° ) | | |
| 2026 Jan 17, 06:00 | 6670 | 0.0002 | 291 | 293 | 90.36 | 43.00 | 271 | | | | 2026 Jun 15, 21:38 | 6861 | 0.0002 | 482 | 484 | 94.27 | 43.00 | 263 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 10
Life <1 day
|
| Launched Starlink Group 06-096. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-004 Falcon 9 Block 5 (Twilight)
Vandenberg Space Force Base | 2026 Jan 11, 13:44 UTC | Lemur-2 (FikretDengiz) 2026-004A 67363 |
in space
|
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Separated from launch vehicle at 14:46 UTC.
One of nine Lemur-2 satellites carried on the Twilight mission, all were placed in similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 12:22 | 6986 | 0.0007 | 602 | 613 | 96.85 | 97.80 | 258 | 05:26 | | | SPARCS (Star-Planet Activity Research CubeSat) 2026-004B 67364 |
in space
|
| 6U Cubesat equipped with a telescope to monitor flares and sunspots on a number of red dwarf stars. Launched as part of NASA's cubesat initiative. Separated from launch vehicle at 16:05 UTC but probably failed to activate. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 12:21 | 6985 | 0.0007 | 602 | 612 | 96.84 | 97.80 | 253 | 05:26 | | | |
in space
|
| 6U Cubesat from PennState University. Carries a gamma ray telescope to monitor the sky in search od high-redshift gamma-ray bursts. Separated from launch vehicle at 16:04 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 12:18 | 6985 | 0.0006 | 603 | 611 | 96.83 | 97.79 | 264 | 05:26 | | | |
in space
|
| Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Separated from launch vehicle at 16:06 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 15:28 | 6984 | 0.0005 | 602 | 609 | 96.80 | 97.80 | 248 | 05:26 | | | |
in space
|
| Small satellite fitted with a synthetic aperture radar for Earth surface imaging. Separated from launch vehicle at 16:07 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 22:00 | 6983 | 0.0003 | 603 | 606 | 96.78 | 97.80 | 243 | 05:26 | | | |
in space
|
| Small satellite fitted with a synthetic aperture radar for Earth surface imaging. Separated from launch vehicle at 16:09 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 12:15 | 6984 | 0.0005 | 603 | 609 | 96.81 | 97.80 | 253 | 05:26 | | | |
in space
|
Small satellite from Kepler Communications of Canada equipped with laser communication equipment to form the basis of an on-orbit optically-connected communications cloud for use by other satellites. Separated from launch vehicle at 16:15 UTC.
One of ten Aether satellites carried on the Twilight mission, all were inserted into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 22:00 | 6983 | 0.0003 | 602 | 607 | 96.78 | 97.80 | 243 | 05:26 | | | Capella 19 (Acadia 9) 2026-004X 67384 |
in space
|
| Small satellite from Capella Space Corp, equipped with an Earth imaging system. Separated from launch vehicle at 16:08 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 12:10 | 6982 | 0.0003 | 602 | 606 | 96.77 | 97.80 | 234 | 05:26 | | | Capella 18 (Acadia 8) 2026-004Y 67385 |
in space
|
| Small satellite from Capella Space Corp, equipped with an Earth imaging system. Separated from launch vehicle at 16:06 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 12:09 | 6982 | 0.0003 | 602 | 605 | 96.76 | 97.80 | 226 | 05:26 | | | |
in space
|
| 3U Cubesat from German company DCubed. Demonstrator/precursor for a later mission that will manufacture al tower structure in orbit. Separated from launch vehicle at 16:05 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 10:31 | 6981 | 0.0001 | 602 | 604 | 96.76 | 97.80 | 225 | 05:26 | | | |
in space
|
| 8U Cubesat from AISTech. Earth observation satellite equipped with a thermal imager to measure surface temperature in areas under observation. Separated from launch vehicle at 14:46 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 11:58 | 6893 | 0.0005 | 512 | 519 | 94.93 | 97.46 | 113 | 05:27 | | | Connecta IoT-16 2026-004AD 67390 |
in space
|
| 6U Cubesat from Turkish company Plan S. Part of an internet communications constellation. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 11:57 | 6893 | 0.0005 | 511 | 519 | 94.93 | 97.46 | 112 | 05:27 | | | Flamingo 1 2026-004AE 67391 |
in space
|
| Small satellite from US company Enduro. Mission unclear but may be a demonstrator of a system to observe other satellites in orbit. Separated from launch vehicle at 14:51 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 11:55 | 6893 | 0.0007 | 510 | 519 | 94.91 | 97.45 | 109 | 05:27 | | | Hawk 13A (Cluster 13#1) 2026-004AF 67392 |
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. Separated from launch vehicle at 14:49 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 21, 23:14 | 6892 | 0.0007 | 509 | 519 | 94.90 | 97.45 | 113 | 05:27 | | | Hawk 13C (Cluster 13#3) 2026-004AG 67393 |
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. Separated from launch vehicle at 14:52 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 00:48 | 6892 | 0.0007 | 508 | 519 | 94.90 | 97.45 | 117 | 05:27 | | | |
in space
|
| Small satellite from NASA equipped with a spectroscope to study planets in orbit around distant stars. Separated from launch vehicle at 16:12 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 15:26 | 6983 | 0.0004 | 602 | 608 | 96.79 | 97.80 | 241 | 05:26 | | | Hawk 13B (Cluster 13#2) 2026-004AK 67396 |
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. Separated from launch vehicle at 14:46 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 10:15 | 6891 | 0.0008 | 507 | 518 | 94.88 | 97.46 | 126 | 05:27 | | | CarbSAR IOD 2026-004AL 67397 |
in space
|
| Earth observation satellite using radar imaging. Its radar aerial is a demonstrator of a stowable dish. Separated from launch vehicle at 14:53 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 22:00 | 6892 | 0.0007 | 508 | 519 | 94.90 | 97.45 | 116 | 05:27 | | | Tomorrow S10 2026-004AM 67398 |
in space
|
| 6U Cubesat from US company Tomorrow.io, designed to measure temperature and humidity profiles within the Earth's atmosphere. Separated from launch vehicle at 14:47 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 22:00 | 6891 | 0.0008 | 507 | 518 | 94.88 | 97.46 | 124 | 05:27 | | | Tomorrow S11 2026-004AN 67399 |
in space
|
| 6U Cubesat from US company Tomorrow.io, designed to measure temperature and humidity profiles within the Earth's atmosphere. Separated from launch vehicle at 14:48 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 10:13 | 6890 | 0.0009 | 506 | 518 | 94.87 | 97.45 | 126 | 05:27 | | | Connecta IoT-13 2026-004AP 67400 |
in space
|
| 6U Cubesat from Turkish company Plan S. Part of an internet communications constellation. Separated from launch vehicle at 14:46. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 11:45 | 6889 | 0.0011 | 504 | 518 | 94.85 | 97.45 | 127 | 05:27 | | | Connecta IoT-14 2026-004AQ 67401 |
in space
|
| 6U Cubesat from Turkish company Plan S. Part of an internet communications constellation. Separated from launch vehicle at 14:46 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 11:43 | 6889 | 0.0011 | 503 | 519 | 94.84 | 97.45 | 122 | 05:27 | | | Connecta IoT-15 2026-004AR 67402 |
in space
|
| 6U Cubesat from Turkish company Plan S. Part of an internet communications constellation. Separated from launch vehicle at 14:48 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 22, 12:00 | 6894 | 0.0005 | 512 | 519 | 94.94 | 97.45 | 101 | 05:27 | | | Falcon 9 second stage uncatalogued |
in space
|
| Launched satellites of the SpaceX "Twilight" rideshare mission. Caused to re-enter above the central Pacific Ocean shortly before 17:00 UTC, after releasing the satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-F01 - failed to reach orbit PSLV-DL (PSLV C-62)
Satish Dhawan Space Centre, Sriharikota | 2026 Jan 12, 04:48 UTC | |
|
| Largest satellite was Theos 2, a joint UK/Thailand Earth observation mission, accompanied by 15 smaller satellites. All were lost when the launch vehicle third stage developed a fault shortly before the end of its planned firing. |
|
2026-005 Falcon 9 Block 5 (Starlink Group 06-097)
Cape Canaveral Space Force Station | 2026 Jan 13, 00:08 UTC | Starlink 36484 2026-005A 67404 |
in space
|
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 20, 20:00 | 6674 | 0.0002 | 294 | 297 | 90.43 | 43.00 | 283 | | | | 2026 Jun 14, 22:39 | 6861 | 0.0002 | 482 | 484 | 94.27 | 43.00 | 287 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 13
Life <1 day
|
| Launched Starlink Group 06-097. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-006 CZ 6A
Taiyuan Space Centre | 2026 Jan 13, 14:16 UTC | Yaogan 50-01 2026-006A 67433 |
in space
|
| Government or military Earth observation satellite in highly retrograde orbit. Possibly using radar imaging. The first orbit listed should be treated with caution, it may have been issued in error by Space-Track. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 14, 23:38 | 7197 | 0.0165 | 700 | 938 | 101.28 | 142.00 | 116 | | | | 2026 Jan 20, 18:11 | 7331 | 0.0001 | 952 | 953 | 104.10 | 142.03 | 278 | | | | CZ 6A third stage 2026-006B 67434 |
in space
|
| Launched Yaogan 50. Initial orbit may have been similar to Yaogan 50-01. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 13, 17:12 | 7064 | 0.0202 | 543 | 828 | 98.48 | 142.04 | 82 | | | |
2026-007 CZ 8A (Y-7)
Hainan Commercial Zone, Wenchang Space Centre | 2026 Jan 13, 15:25 UTC | Hulianwang Digui 18-01 (Satellite Low Orbit Internet Group 18-01) 2026-007A 67435 |
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
( ° ) | | |
| 2026 Jan 16, 09:58 | 7299 | 0.0008 | 915 | 927 | 103.44 | 50.01 | 280 | | | | CZ 8A third stage 2025-007K 67444 |
in space
|
| Launched Hulianwang Digui group 18. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 15, 04:09 | 7225 | 0.0092 | 781 | 914 | 101.87 | 50.01 | 88 | | | |
2026-008 Falcon 9 Block 5 (Starlink Group 06-098)
Cape Canaveral Space Force Station | 2026 Jan 14, 18:08 UTC | Starlink 36542 2026-008A 67445 |
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 14:14 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
( ° ) | | |
| 2026 Jan 21, 14:00 | 6657 | 0.0002 | 278 | 280 | 90.10 | 43.00 | 290 | | | | 2026 Jun 15, 20:45 | 6861 | 0.0004 | 480 | 486 | 94.27 | 43.00 | 282 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 14
Life <1 day
|
| Launched Starlink Group 06-098. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-009 CZ 2C
Jiuquan Space Centre | 2026 Jan 15, 04:01 UTC | AlSat 3A (Algeria Satellite 3A) 2026-009A 67474 |
in space
|
| Optical Earth imaging satellite, built by China for Algeria. Will work in conjunction with AlSat 3B (67646, 2026-021A). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 16, 22:03 | 6874 | 0.0011 | 488 | 503 | 94.53 | 97.47 | 262 | 10:21 | | | CZ 2C second stage 2026-009B 67475 |
in space
|
| Launched AlSat 3A. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 16, 22:37 | 6936 | 0.0099 | 489 | 627 | 95.82 | 97.18 | 217 | | | |
2026-010 Ceres 1S (Gushenxing 1 Y-7)
Towed barge, Yellow Sea - near 36° N, 119°.5 E | 2026 Jan 15, 20:10 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
( ° ) | | |
| 2026 Jan 20, 23:25 | 7223 | 0.0011 | 837 | 853 | 101.82 | 44.98 | 331 | | | | 2026 Jan 28, 21:18 | 7225 | 0.0012 | 838 | 856 | 101.86 | 44.98 | 17 | | | | 2026 Jan 31, 03:35 | 7225 | 0.0013 | 838 | 857 | 101.87 | 44.98 | 29 | | | | |
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
( ° ) | | |
| 2026 Jan 20, 23:24 | 7222 | 0.0011 | 836 | 852 | 101.81 | 44.98 | 334 | | | | 2026 Jan 28, 22:58 | 7224 | 0.0011 | 837 | 854 | 101.83 | 44.98 | 21 | | | | |
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
( ° ) | | |
| 2026 Jan 20, 23:23 | 7222 | 0.0011 | 836 | 852 | 101.80 | 44.98 | 338 | | | | 2026 Jan 28, 22:57 | 7226 | 0.0015 | 837 | 858 | 101.87 | 44.99 | 29 | | | | |
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
( ° ) | | |
| 2026 Jan 20, 23:23 | 7222 | 0.0012 | 835 | 853 | 101.80 | 44.98 | 334 | | | | 2026 Jan 28, 21:15 | 7224 | 0.0013 | 836 | 855 | 101.84 | 44.99 | 22 | | | | 2026 Feb 5, 19:12 | 7225 | 0.0012 | 837 | 855 | 101.85 | 44.98 | 71 | | | | Ceres 1S fourth stage uncatalogued |
in space
|
| Launched cluster of four Tianqi satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-F02 - failed to reach orbit CZ 3B
Xichang Space Centre | 2026 Jan 16, 16:55 UTC | |
|
| Chinese government/military satellite intended for 63° inclination HEO. Lost when the launch vehicle third stage failed to complete its firing. |
|
2026-F03 - failed to reach orbit Ceres 2 (Gushenxing 2 Y-1)
Jiuquan Space Centre | 2026 Jan 17, 04:08 UTC | |
|
| Cluster of (six?) satellites lost when launch vehicle first stage failed on first flight of new version due to an engine problem. |
|
2026-011 Falcon 9 Block 5 (NRO L-105
)
Vandenberg Space Force Base | 2026 Jan 17, 04:39 UTC | USA 572 (Starshield 0162) 2026-011A 67484 |
in space
|
One of a simultaneously-launched group of nine US government NRO intelligence gathering 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 information based on amateur observations.
All nine satellites were injected into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 22, 16:53 | 6834 | 0.0002 | 455 | 457 | 93.71 | 69.99 | 242 | | | | 2026 Feb 10, 05:10 | 6846 | 0.0002 | 467 | 469 | 93.96 | 69.99 | 212 | | | | 2026 Mar 19, 20:47 | 6955 | 0.0002 | 576 | 578 | 96.21 | 70.00 | 155 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 17
Life <1 day
|
| Launched NRO L-105 mission. Caused to re-enter about two hours after liftoff, after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-012 Falcon 9 Block 5 (Starlink Group 06-100)
Cape Canaveral Space Force Station | 2026 Jan 18, 23:31 UTC | Starlink 36551 2026-012A 67493 |
in space
|
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude.
All satellites expected to be injected initially into similar orbits at about 300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 19, 00:25 | 6638 | 0.0008 | 255 | 265 | 89.70 | 43.01 | 320 | | | | 2026 Jun 15, 03:43 | 6861 | 0.0003 | 481 | 485 | 94.27 | 42.99 | 270 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 19
Life 1 day
|
| Launched Starlink Group 06-100. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-013 CZ 12
Hainan Commercial Zone, Wenchang Space Centre | 2026 Jan 19, 07:48 UTC | Hulianwang Digui 19-01 (Satellite Low Orbit Internet Group 19-01) 2026-013A 67522 |
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
( ° ) | | |
| 2026 Jan 20, 12:18 | 7279 | 0.0011 | 893 | 909 | 103.01 | 50.01 | 239 | | | | CZ 12 second stage 2026-013K 67531 |
in space
|
| Launched Hulianwang Digui group 19. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 20, 22:10 | 7222 | 0.0069 | 794 | 894 | 101.81 | 49.99 | 134 | | | |
2026-014 Falcon 9 Block 5 (Starlink Group 17-030)
Vandenberg Space Force Base | 2026 Jan 22, 05:47 UTC | Starlink 36587 2026-014A 67532 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:49 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
( ° ) | | |
| 2026 Jan 27, 14:00 | 6649 | 0.0001 | 270 | 272 | 89.93 | 97.28 | 77 | | | | 2026 Jun 16, 03:18 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.29 | 96 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 22
Life <1 day
|
| Launched Starlink Group 17-030. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-015 Electron (The Cosmos Will See You Now)
Rocket Lab Launch Complex, New Zealand | 2026 Jan 22, 10:52 UTC | |
in space
|
| 12 Cubesat - one of a pair of simultaneously launched satellites from UK company Open Cosmos. Probable demonstrator for an unidentified planned internet broadband communications constellation and also acting as a radio frequency 'placeholder'. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 23, 23:02 | 7441 | 0.0005 | 1059 | 1066 | 106.46 | 89.00 | 120 | | | | |
in space
|
| 12 Cubesat - one of a pair of simultaneously launched satellites from UK company Open Cosmos. Probable demonstrator for an unidentified planned internet broadband communications constellation and also acting as a radio frequency 'placeholder' |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 23, 23:02 | 7441 | 0.0005 | 1059 | 1066 | 106.46 | 89.00 | 119 | | | | Electron second stage 2026-015C 67558 |
Re-entered - 2026 Feb 21
Life 30 days
|
| Launched two satelites for Open Cosmos. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 24, 18:41 | 6999 | 0.0631 | 180 | 1062 | 97.12 | 89.00 | 262 | | | | Electron third stage (kick stage) 2026-015D 67559 |
in space
|
| Launched two satelites for Open Cosmos. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 23, 23:38 | 7055 | 0.0542 | 294 | 1059 | 98.29 | 89.05 | 331 | | | |
2026-016 Falcon 9 Block 5 (Starlink Group 17-020)
Vandenberg Space Force Base | 2026 Jan 25, 17:30 UTC | Starlink 36621 2026-016A 67561 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 18:32 UTC. Initial orbit shown is the SpaceX pre-launch estimate.
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
( ° ) | | |
| 2026 Jan 25, 18:33 | 6632 | 0.0011 | 246 | 261 | 89.58 | 97.29 | 271 | | | | 2026 Jun 16, 04:08 | 6844 | 0.0000 | 465 | 466 | 93.91 | 97.28 | 138 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 25
Life <1 day
|
| Launched Starlink Group 17-020. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-017 Falcon 9 Block 5 (Starlink Group 06-100)
Cape Canaveral Space Force Station | 2026 Jan 28, 04:49 UTC | USA 581 (GPS IIIA SV09) 2026-017A 67588 |
in space
|
| Block 3 GPS Navsat. Separated from launch vehicle at 05:18 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 28, 18:17 | 16670 | 0.5941 | 388 | 20195 | 356.98 | 54.99 | 270 | | | | 2026 Jan 28, 18:17 | 16670 | 0.5941 | 388 | 20195 | 356.99 | 55.00 | 270 | | | | 2026 Feb 5, 01:48 | 26543 | 0.0020 | 20112 | 20218 | 717.28 | 55.90 | 280 | | | | 2026 Feb 6, 13:41 | 26561 | 0.0001 | 20180 | 20185 | 717.98 | 55.00 | 81 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 28
Life <1 day
|
| Launched USA 581. Caused to re-enter after releasing satellite. |
| Not Catalogued - orbit parameters unavailable | |
2026-018 Falcon 9 Block 5 (Starlink Group 17-019)
Vandenberg Space Force Base | 2026 Jan 29, 17:53 UTC | Starlink 36641 2026-018A 67589 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 18:55 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
( ° ) | | |
| 2026 Feb 5, 18:00 | 6666 | 0.0002 | 287 | 289 | 90.28 | 97.28 | 85 | | | | 2026 Jun 16, 03:56 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.28 | 87 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 29
Life <1 day
|
| Launched Starlink Group 17-019. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-019 Electron (Bridging The Swarm)
Rocket Lab Launch Complex, New Zealand | 2026 Jan 30, 01:21 UTC | |
in space
|
| Demonstrator of sensors for a future constellation of South Korean Earth observation satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 30, 08:24 | 6922 | 0.0012 | 536 | 552 | 95.52 | 97.41 | 309 | 13:42 | | | Electron second stage 2026-019B 67615 |
Re-entered - 2026 Feb 11
Life 12 days
|
| Launched Neonsat 1. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 30, 08:10 | 6750 | 0.0274 | 187 | 557 | 91.99 | 97.45 | 225 | | | | Electron third stage (kick stage) 2026-019C 67616 |
Re-entered - 2026 Mar 18
Life 47 days
|
| Launched Neonsat 1. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 30, 08:13 | 6786 | 0.0209 | 266 | 550 | 92.72 | 97.41 | 261 | | | |
2026-020 Falcon 9 Block 5 (Starlink Group 06-101)
Cape Canaveral Space Force Station | 2026 Jan 30, 07:22 UTC | Starlink 36548 2026-020A 67617 |
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 08:27 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
( ° ) | | |
| 2026 Feb 5, 18:00 | 6672 | 0.0002 | 293 | 295 | 90.40 | 43.00 | 249 | | | | 2026 Jun 15, 15:52 | 6861 | 0.0001 | 482 | 484 | 94.27 | 43.00 | 122 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jan 30
Life <1 day
|
| Launched Starlink Group 06-101. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-021 CZ 2C
Jiuquan Space Centre | 2026 Jan 31, 04:01 UTC | AlSat 3B (Algeria Satellite 3B) 2026-021A 67646 |
in space
|
| Optical Earth imaging satellite, built by China for Algeria. Will work in conjunction with AlSat 3B (67464, 2026-009A). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jan 31, 16:06 | 6874 | 0.0012 | 488 | 504 | 94.53 | 97.47 | 264 | 10:21 | | | CZ 2C second stage 2026-021B 67647 |
in space
|
| Launched AlSat 3B. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jan 31, 14:32 | 6875 | 0.0154 | 391 | 603 | 94.55 | 97.66 | 140 | | | |
2026-022 Falcon 9 Block 5 (Starlink Group 17-032)
Vandenberg Space Force Base | 2026 Feb 2, 15:47 UTC | Starlink 36719 2026-022A 67648 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 16:49 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 6, 20:00 | 6642 | 0.0001 | 263 | 265 | 89.80 | 97.28 | 75 | | | | 2026 Jun 15, 23:55 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.28 | 91 | | | | Falcon 9 second stage 2026-022AB 67673 |
Re-entered - 2026 Feb 3
Life 1 day
|
| Launched Starlink Group 17-032. Engine firing to cause re-entry was not completed successfully so the stage remained in orbit for a short while. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 2, 19:41 | 6554 | 0.0099 | 110 | 241 | 88.00 | 97.29 | 262 | | | |
2026-I01 JEM Small Satellite Orbital Deployer (J-SSOD 34)
International Space Station | 2026 Feb 3 UTC | Knacksat 2 1998-067XZ 67683 |
in space
|
| 3U Cubesat from King Mongkut's University of Technology North Bangkok. Carries an assortment of technological payloads. Released at 08:55 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 8, 14:19 | 6796 | 0.0011 | 411 | 426 | 92.94 | 51.63 | 93 | | | | |
Re-entered - 2026 Aug 1
Life 179 days
|
| 1U Cubesat developed by the Popular Autonomous University of the State of Puebla, Mexico. Caries instruments to measure ash dispersion around volcanoes. Released at 08:45 UTC. Catalogue Number and Designation subject to confirmation. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 8, 14:18 | 6795 | 0.0013 | 408 | 426 | 92.91 | 51.63 | 88 | | | | |
in space
|
| 2U Cubesat from Sapienza of Italy, carrying a test payload for inter-satellite communications to/from internet connected equipment. Released at 08:45 UTC. Catalogue Number and Designation subject to confirmation. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 8, 14:19 | 6796 | 0.0013 | 409 | 427 | 92.93 | 51.63 | 88 | | | | |
in space
|
| 1U Cubesat from Universiti Teknologi Mara, Malaysia. Equipped with an Earth observation camera and a transmission system to return images via the Internet. Released at 10:52 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 8, 12:46 | 6796 | 0.0008 | 412 | 423 | 92.92 | 51.63 | 66 | | | | LEOPARD (Light intensity Experiment with On-orbit Position and satellite Ranging Demonstration) 1998-067YD 67687 |
in space
|
| 3U Cubesat acting as a demonstrator of positioning and pointing technologies for future lunar Cubesats. Released at 10:52 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 8, 14:19 | 6796 | 0.0008 | 413 | 424 | 92.93 | 51.63 | 67 | | | | HMU-Sat 2 (Teruteru) 1998-067YE 67688 |
in space
|
| 3U Cubesat acting as a demonstrator of positioning and pointing technologies for future lunar Cubesats. Released at 10:52 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 8, 14:19 | 6796 | 0.0008 | 413 | 423 | 92.93 | 51.63 | 67 | | | |
2026-023 Soyuz 2.1b + Fregat
Plesetsk Cosmodrome | 2026 Feb 5, 18:59 UTC | Cosmos 2600 2026-023A 67674 |
in space
|
| Small military/government satellite, possibly for optical imaging, but precise mission not known. Orbit height maintained and tightly controlled by use of a thruster system. Released from launch vehicle at (probably) around 19:10 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Feb 6, 16:04 | 6706 | 0.0003 | 326 | 329 | 91.08 | 96.65 | 76 | 10:30 | | | 2026 Feb 22, 03:57 | 6700 | 0.0002 | 320 | 323 | 90.96 | 96.65 | 60 | 10:28 | | | 2026 Feb 24, 13:35 | 6698 | 0.0001 | 319 | 321 | 90.93 | 96.65 | 50 | 10:28 | | | 2026 Feb 26, 06:32 | 6700 | 0.0003 | 319 | 324 | 90.95 | 96.65 | 52 | 10:28 | | | 2026 Apr 20, 12:06 | 6701 | 0.0010 | 316 | 329 | 90.98 | 96.64 | 234 | 10:24 | | | 2026 Jun 5, 21:51 | 6700 | 0.0008 | 317 | 328 | 90.97 | 96.68 | 176 | 10:21 | | | Cosmos 2601 2026-023B 67675 |
in space
|
| One of a group of military satellites. Mission details to follow. released from launch vehicle at (probably) around 21:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Feb 6, 01:01 | 6877 | 0.0017 | 487 | 511 | 94.60 | 96.64 | 246 | 10:29 | | | 2026 Mar 3, 13:03 | 6875 | 0.0019 | 484 | 510 | 94.56 | 96.64 | 153 | 10:19 | | | 2026 Apr 20, 03:56 | 6872 | 0.0017 | 482 | 505 | 94.49 | 96.63 | 353 | 10:00 | | | Cosmos 2602 2026-023C 67676 |
in space
|
| One of a group of military satellites. Mission details to follow. released from launch vehicle at (probably) around 21:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Feb 6, 01:01 | 6877 | 0.0018 | 487 | 512 | 94.60 | 96.64 | 234 | 10:29 | | | 2026 Mar 3, 13:01 | 6875 | 0.0020 | 483 | 511 | 94.56 | 96.64 | 143 | 10:19 | | | 2026 Apr 19, 10:32 | 6872 | 0.0018 | 482 | 506 | 94.49 | 96.63 | 344 | 10:00 | | | Cosmos 2603 2026-023D 67677 |
in space
|
| One of a group of military satellites. Mission details to follow. released from launch vehicle at (probably) around 21:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Feb 6, 01:01 | 6877 | 0.0019 | 486 | 512 | 94.60 | 96.64 | 236 | 10:29 | | | 2026 Mar 3, 13:04 | 6876 | 0.0020 | 484 | 512 | 94.57 | 96.64 | 148 | 10:19 | | | 2026 Apr 20, 10:21 | 6873 | 0.0018 | 482 | 507 | 94.50 | 96.64 | 346 | 10:00 | | | Cosmos 2604 2026-023E 67678 |
in space
|
| One of a group of military satellites. Mission details to follow. released from launch vehicle at (probably) around 21:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Feb 6, 01:01 | 6877 | 0.0018 | 487 | 512 | 94.60 | 96.64 | 240 | 10:29 | | | 2026 Mar 3, 13:01 | 6875 | 0.0020 | 483 | 511 | 94.56 | 96.63 | 148 | 10:19 | | | 2026 Apr 20, 10:06 | 6871 | 0.0017 | 481 | 505 | 94.48 | 96.62 | 345 | 10:00 | | | Cosmos 2605 2026-023F 67679 |
in space
|
| One of a group of military satellites. Mission details to follow. released from launch vehicle at (probably) around 23:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Feb 6, 15:13 | 6877 | 0.0021 | 485 | 513 | 94.59 | 96.64 | 225 | 10:39 | | | 2026 Mar 3, 12:58 | 6875 | 0.0022 | 481 | 512 | 94.55 | 96.63 | 142 | 10:29 | | | 2026 Apr 20, 03:39 | 6871 | 0.0019 | 480 | 506 | 94.47 | 96.63 | 339 | 10:10 | | | Cosmos 2606 2026-023G 67680 |
in space
|
| One of a group of military satellites. Mission details to follow. released from launch vehicle at (probably) around 23:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Feb 6, 01:01 | 6877 | 0.0022 | 484 | 514 | 94.59 | 96.63 | 230 | 10:39 | | | 2026 Mar 3, 12:59 | 6875 | 0.0024 | 480 | 513 | 94.55 | 96.63 | 139 | 10:29 | | | 2026 Apr 20, 03:40 | 6871 | 0.0020 | 479 | 507 | 94.47 | 96.62 | 335 | 10:10 | | | Cosmos 2607 2026-023H 67681 |
in space
|
| One of a group of military satellites. Mission details to follow. released from launch vehicle at (probably) around 23:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Feb 6, 01:01 | 6877 | 0.0021 | 484 | 514 | 94.59 | 96.64 | 231 | 10:39 | | | 2026 Mar 3, 12:59 | 6875 | 0.0024 | 481 | 513 | 94.55 | 96.64 | 138 | 10:29 | | | 2026 Apr 20, 02:13 | 6872 | 0.0021 | 480 | 508 | 94.49 | 96.63 | 335 | 10:10 | | | Cosmos 2608 2026-023J 67682 |
in space
|
| One of a group of military satellites. Mission details to follow. released from launch vehicle at (probably) around 23:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Feb 6, 01:01 | 6877 | 0.0021 | 484 | 514 | 94.59 | 96.64 | 228 | 10:39 | | | 2026 Mar 3, 12:57 | 6875 | 0.0024 | 480 | 513 | 94.55 | 96.64 | 135 | 10:29 | | | 2026 Apr 20, 09:57 | 6871 | 0.0020 | 479 | 507 | 94.47 | 96.63 | 330 | 10:10 | | | Fregat rocket stage uncatalogued |
Re-entered - 2026 Feb 6
Life 1 day
|
| Launched cluster of satellites. Released 023A on reaching orbit, then raised orbit to a non sun-synchronous 500 km where it released 023B - 023E at around 21:00 UTC. Used a single firing to move the RA of the Ascending Node to the east by 2.5 degrees without changing the inclination where it released 023F - 023J at around 23:00 UTC. Following retro-fire February 6 at around 01:05 UTC, re-entered above the Indian Ocean south of Australia at about 01:45 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2026-024 CZ 2F
Jiuquan Space Centre | 2026 Feb 7, 03:57 UTC | Reusable Spacecraft Test Vehicle Type 1 Flight 4 2026-024A 67689 |
in space
|
| Small re-usable spaceplane designed for long duration missions. Payload information not available. Launch time is an estimate and is ±1 minute. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 7, 11:19 | 6846 | 0.0180 | 345 | 591 | 93.95 | 49.99 | 150 | | | | 2026 Feb 9, 05:34 | 6848 | 0.0176 | 350 | 591 | 94.00 | 49.99 | 157 | | | | 2026 Feb 12, 12:08 | 6971 | 0.0006 | 588 | 597 | 96.54 | 49.99 | 264 | | | | 2026 Apr 14, 19:13 | 6971 | 0.0006 | 588 | 597 | 96.53 | 49.99 | 143 | | | | 2026 Jun 20, 10:51 | 6971 | 0.0005 | 589 | 596 | 96.53 | 49.99 | 50 | | | | 2026 Jun 27, 22:55 | 6971 | 0.0005 | 589 | 596 | 96.53 | 49.99 | 79 | | | | 2026 Jun 28, 15:00 | 6970 | 0.0004 | 589 | 594 | 96.51 | 49.99 | 90 | | | | unidentified satellite 2026-024H 69673 |
in space
|
| Appears to have separated from the spaceplane June 21 around 14:40 UTC, shortly before the spaceplane raised its own orbit by about 100 metres. As with small satellites released on earlier spaceplane missions, commenced a series of orbital manoeuvres June 26. Around July 1, passed within a few kilometres of a similar satellite (59844/2023-195G) left in orbit by the previous mission. Returned to the vicinity of the spaceplane July 9 and (possibly) linked up with it before July 11 when the spaceplane raised its orbit slightly and took the companion satellite with it. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 22, 03:03 | 6971 | 0.0006 | 589 | 596 | 96.53 | 49.99 | 57 | | | | 2026 Jun 27, 06:50 | 6967 | 0.0005 | 586 | 592 | 96.46 | 49.99 | 17 | | | | 2026 Jun 30, 13:34 | 6962 | 0.0030 | 563 | 605 | 96.35 | 49.99 | 73 | | | | 2026 Jun 30, 21:35 | 6966 | 0.0034 | 564 | 612 | 96.44 | 49.99 | 66 | | | | 2026 Jul 1, 15:16 | 6970 | 0.0038 | 566 | 619 | 96.52 | 49.99 | 76 | | | | 2026 Jul 1, 23:19 | 6977 | 0.0028 | 580 | 619 | 96.67 | 49.99 | 81 | | | | CZ 2F third stage 2026-024B 67690 |
in space
|
| Launched experimental spaceplane. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 7, 11:19 | 6845 | 0.0178 | 345 | 589 | 93.94 | 49.99 | 150 | | | |
2026-025 Falcon 9 Block 5 (Starlink Group 17-33)
Vandenberg Space Force Base | 2026 Feb 7, 20:58 UTC | Starlink 36748 2026-025A 67693 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 22:01 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 11, 16:00 | 6627 | 0.0001 | 248 | 250 | 89.48 | 97.28 | 60 | | | | 2026 Jun 16, 05:01 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.28 | 77 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 7
Life <1 day
|
| Launched Starlink Group 17-033. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-026 Falcon 9 Block 5 (Starlink Group 17-034)
Vandenberg Space Force Base | 2026 Feb 11, 17:11 UTC | Starlink 36772 2026-026A 67721 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 18:14 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 11, 18:04 | 6631 | 0.0003 | 251 | 255 | 89.57 | 97.28 | 259 | | | | 2026 Jun 16, 02:29 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.28 | 111 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 11
Life <1 day
|
| Launched Starlink Group 17-034. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-027 Jielong 3
Mobile floating platform, South China Sea near 21°.5 N, 112°.0 E | 2026 Feb 12, 06:37 UTC | Chutian 3 (Ultra Low Orbit Test Satellite) 2026-027A 67746 |
in space
|
| Development satellite for the future Chutian constellation of Earth imaging satellites that will operate below 300 kilometres for long periods, necessitating constantly maintaining the orbit against significant air drag. 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 | |
| 2026 Feb 12, 20:14 | 6892 | 0.0010 | 508 | 521 | 94.91 | 97.49 | 301 | 14:00 | | | Chutian 4 (Ultra Low Orbit Test Satellite) 2026-027B 67747 |
in space
|
| Development satellite for the future Chutian constellation of Earth imaging satellites that will operate below 300 kilometres for long periods, necessitating constantly maintaining the orbit against significant air drag. 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 | |
| 2026 Feb 12, 17:04 | 6892 | 0.0010 | 507 | 521 | 94.90 | 97.48 | 289 | 14:01 | | | Chutian 5 (Ultra Low Orbit Test Satellite) 2026-027D 67749 |
in space
|
| Development satellite for the future Chutian constellation of Earth imaging satellites that will operate below 300 kilometres for long periods, necessitating constantly maintaining the orbit against significant air drag. 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 | |
| 2026 Feb 12, 17:04 | 6891 | 0.0010 | 506 | 520 | 94.89 | 97.49 | 304 | 14:01 | | | |
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. Working together with PRSC-EO 1 (62727, 2025-012C). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Mar 4, 13:18 | 6896 | 0.0009 | 512 | 525 | 94.99 | 97.49 | 275 | 14:01 | | | 2026 Mar 8, 10:57 | 6908 | 0.0012 | 522 | 538 | 95.23 | 97.49 | 232 | 14:01 | | | Dianli Hongwai Weixing A (Power Infrared Satellite A) 2026-027xx |
in space
|
| Earth imaging satellite equipped with an infrared imager. Used to locate and study wildfires on the Earth's surface. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6892 | 0.0010 | 506 | 520 | 94.89 | 97.48 | 296 | 14:01 | | | Gangzhong 1 (CUHK 1, Chinese University of Hong Kong 1) 2026-027xx |
in space
|
| Small satellite from the Chinese University of Hong Kong. Mission is Earth observation with a high resolution imaging system. Also equipped with an AI-based processor to prepare images for transmission to the ground. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6892 | 0.0010 | 507 | 521 | 94.90 | 97.48 | 289 | 14:01 | | | Kongjian Huanjing Jiance 2026-027xx |
in space
|
| Described as a space environment monitoring satellite - covers a multitude of possible missions from observing charged particles and electric fields to tracking other satellites in orbit. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6892 | 0.0010 | 506 | 520 | 94.89 | 97.48 | 296 | 14:01 | | | Jielong 3 fourth stage 2026-027H 67753 |
Re-entered - 2026 Mar 30
Life 46 days
|
| Launched PRSC-EO 2 and six smaller satellites. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 15, 03:26 | 6773 | 0.0276 | 208 | 582 | 92.46 | 97.51 | 329 | | | |
2026-028 Proton-M + Blok DM3
Baikonur Cosmodrome | 2026 Feb 12, 08:52 UTC | Elektro-L №5 2026-028A 67756 |
in space
|
| Second generation Russian geosynchronous metsat providing a multispectral image of the complete visible hemisphere every 30 minutes with the interval increased to 15 minutes to cope with emergencies. Also equipped with multiple space weather and other meteorological sensors. Also carries a COSPAS-SARSAT search and rescue system receiver. Separated from launch vehicle at 15:30 UTC in geosynchronous drift orbit. Expected location 76° east to take over from Elektro-L №3 (44903, 2019-095A). Arrived on station March 19, first images returned March 24. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 Feb 15, 07:21 | 41800 | 0.0002 | 35414 | 35430 | 1417.52 | 0.53 | 247 | | | | 2026 Feb 18, 06:34 | 42003 | 0.0045 | 35435 | 35816 | 1427.85 | 0.51 | 50 | 113°.0 E | | | 2026 Feb 19, 06:15 | 42374 | 0.0042 | 35818 | 36174 | 1446.81 | 0.51 | 230 | 117°.1 E | | | 2026 Mar 5, 07:50 | 42376 | 0.0042 | 35820 | 36176 | 1446.89 | 0.48 | 229 | 79°.4 E | | | 2026 Mar 9, 07:40 | 42173 | 0.0006 | 35770 | 35819 | 1436.50 | 0.47 | 46 | 77°.8 E | | | 2026 Mar 12, 07:30 | 42182 | 0.0004 | 35789 | 35819 | 1436.99 | 0.46 | 42 | 77°.5 E | | | 2026 Mar 18, 07:12 | 42063 | 0.0019 | 35606 | 35764 | 1430.91 | 0.45 | 325 | 75°.8 E | | | 2026 Mar 19, 07:08 | 42165 | 0.0001 | 35785 | 35790 | 1436.12 | 0.45 | 227 | 76°.1 E | | | Jaam-e Jam 1 2026-028B 67757 |
in space
|
| Iranian small comsat owned by Islamic Republic of Iran Broadcasting (IRIB). Intended to act as a 'placeholder' for Iran's ITU-allocated location near 34° east from where it will relay a low power signal. Separated from launch vehicle at 15:38 UTC in geosynchronous drift orbit. Initial orbit similar to that of Elektro-L №5. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 Mar 2, 11:00 | 42155 | 0.0005 | 35755 | 35799 | 1435.62 | 0.49 | 116 | 34°.7 E | | | 2026 Mar 3, 10:56 | 42166 | 0.0002 | 35778 | 35798 | 1436.17 | 0.51 | 116 | 34°.8 E | | | 2026 Mar 5, 02:04 | 42159 | 0.0009 | 35743 | 35818 | 1435.80 | 0.50 | 132 | 34°.8 E | | | 2026 Mar 6, 14:07 | 42168 | 0.0005 | 35771 | 35809 | 1436.25 | 0.50 | 130 | 34°.7 E | | | 2026 Mar 10, 03:41 | 42176 | 0.0006 | 35774 | 35822 | 1436.70 | 0.49 | 134 | 34°.3 E | | | 2026 Mar 17, 05:09 | 42165 | 0.0003 | 35774 | 35799 | 1436.09 | 0.48 | 124 | 33°.9 E | | | 2026 Mar 31, 06:16 | 42166 | 0.0002 | 35781 | 35795 | 1436.16 | 0.44 | 122 | 33°.9 E | | | 2026 Apr 14, 03:58 | 42164 | 0.0002 | 35778 | 35794 | 1436.07 | 0.41 | 134 | 33°.9 E | | | 2026 Apr 28, 04:08 | 42166 | 0.0000 | 35786 | 35790 | 1436.17 | 0.37 | 283 | 33°.9 E | | | 2026 May 12, 05:12 | 42164 | 0.0001 | 35783 | 35789 | 1436.07 | 0.34 | 243 | 33°.9 E | | | 2026 May 26, 05:34 | 42166 | 0.0001 | 35785 | 35792 | 1436.19 | 0.31 | 328 | 34°.1 E | | | 2026 Jun 7, 05:01 | 42165 | 0.0001 | 35783 | 35790 | 1436.10 | 0.28 | 300 | 33°.9 E | | | 2026 Jun 19, 14:44 | 42163 | 0.0001 | 35780 | 35790 | 1436.02 | 0.25 | 293 | 34°.0 E | | | Proton Blok-DM-03 rocket stage 2026-028C 67758 |
in space
|
| Launched Elektro-L №5 and Jam-e Jam 1. Final use of this type of upper stage. Initial orbit similar to Elektro-L №5. Manoeuvred out of geosynchronous belt after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 20, 07:51 | 41368 | 0.0101 | 34571 | 35409 | 1395.60 | 0.08 | 324 | | | |
2026-029 Vulcan VC4S (USSF-87)
Cape Canaveral Space Force Station | 2026 Feb 12, 09:22 UTC | USA 582 (GSSAP 7) 2026-029A 67759 |
in space
|
| One of a pair of simultaneously-launched Geosynchronous Space Situational Awareness Program satellites to act as a sensor in the US Space Surveillance Network (SSN). It carries an experimental sensor look at objects in geosynchronous orbit with a view to identifying satellites and differentiating between payloads, rocket bodies and debris. |
| Orbit classified as 'Secret' - data withheld | | USA 583 (GSSAP 8) 2026-029B 67760 |
in space
|
| One of a pair of simultaneously-launched Geosynchronous Space Situational Awareness Program satellites to act as a sensor in the US Space Surveillance Network (SSN). It carries an experimental sensor look at objects in geosynchronous orbit with a view to identifying satellites and differentiating between payloads, rocket bodies and debris. |
| Orbit classified as 'Secret' - data withheld | | USA 584 (EELV Secondary Payload Adapter?) 2026-029C 67761 |
in space
|
| Purpose and mission not disclosed but may be an ESPA Ring carrying both onboard sensors/experiments and small satellites for release once in GEO. |
| Orbit classified as 'Secret' - data withheld | | Vulcan second stage (Centaur V) 2026-029D 67762 |
in space
|
| Launched pair of GSSAP satellites. |
| Orbit classified as 'Secret' - data withheld | |
2026-030 Ariane 64 (VA-267, Amazon LEO 01)
Centre Spatiale Guyanaise | 2026 Feb 12, 16:45 UTC | Amazon LEO 00159 (Kuiper 00159) 2026-030A 67764 |
in space
|
One member of a simultaneously-launched cluster of thirty two broadband and mobile telephone communications satellites from US company Amazon. Released from the launch vehicle in ten groups of three and one pair over a period of ~30 minutes beginning at 18:14 UTC.
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
( ° ) | | |
| 2026 Feb 19, 16:00 | 6839 | 0.0004 | 459 | 464 | 93.82 | 51.88 | 4 | | | | Ariane 6 third stage uncatalogued |
Re-entered - 2026 Feb 12
Life <1 day
|
| Launched cluster of Kuiper satellites. Retro-fire at 20:27 UTC led to re-entry above the Indian Ocean at about 21:10 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2026-031 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2026 Feb 13, 10:15 UTC | SpaceX Dragon Crew 12 (Dragon Freedom flight #5) 2026-031A 67796 |
in space
|
| Crew flight to ISS provided by SpaceX under contract to NASA. Crew members: Commander - Jessica Meir (NASA), Pilot - Jack Hathaway (NASA), Mission Specialists - Sophie Adenot (ESA) and Andrei Fedyaev (Roscosmos). Docked with the forward-facing port of the ISS Harmony module at 2014 UTC on the day of launch. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 13, 14:39 | 6603 | 0.0026 | 208 | 242 | 89.00 | 51.63 | 226 | | | | 2026 Feb 15, 04:22 | 6799 | 0.0011 | 413 | 428 | 92.99 | 51.63 | 100 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 13
Life <1 day
|
| Launched SpaceX Dragon Crew 12. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-032 Falcon 9 Block 5 (Starlink Group 17-013)
Vandenberg Space Force Base | 2026 Feb 15, 01:59 UTC | Starlink 36800 2026-032A 67797 |
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 03:01 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 23, 16:00 | 6678 | 0.0001 | 299 | 301 | 90.51 | 97.29 | 80 | | | | 2026 Jun 16, 01:50 | 6844 | 0.0002 | 465 | 467 | 93.91 | 97.28 | 89 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 15
Life <1 day
|
| Launched Starlink Group 17-013. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-033 Falcon 9 Block 5 (Starlink Group 06-103)
Cape Canaveral Space Force Station | 2026 Feb 16, 07:59 UTC | Starlink 36644 2026-033A 67821 |
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 09:03 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 23, 16:00 | 6685 | 0.0002 | 306 | 308 | 90.66 | 43.00 | 258 | | | | 2026 Jun 16, 00:32 | 6861 | 0.0001 | 483 | 483 | 94.27 | 43.01 | 242 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 16
Life <1 day
|
| Launched Starlink Group 06-103. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-034 Falcon 9 Block 5 (Starlink Group 10-036)
Cape Canaveral Space Force Station | 2026 Feb 20, 01:41 UTC | Starlink 36840 2026-034A 67850 |
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 02:45 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 25, 16:00 | 6673 | 0.0000 | 294 | 295 | 90.41 | 53.15 | 94 | | | | 2026 Jun 16, 03:25 | 6853 | 0.0001 | 474 | 476 | 94.11 | 53.16 | 98 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 20
Life <1 day
|
| Launched Starlink Group 10-036. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-035 Falcon 9 Block 5 (Starlink Group 17-025)
Vandenberg Space Force Base | 2026 Feb 21, 09:04 UTC | Starlink 36818 2026-035A 67879 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 10:06 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 25, 16:00 | 6629 | 0.0001 | 250 | 251 | 89.51 | 97.28 | 99 | | | | 2026 Jun 16, 02:10 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.29 | 82 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 21
Life <1 day
|
| Launched Starlink Group 17-025. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-036 Falcon 9 Block 5 (Starlink Group 06-104)
Cape Canaveral Space Force Station | 2026 Feb 22, 03:47 UTC | Starlink 36814 2026-036A 67904 |
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 04:51 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Feb 25, 16:00 | 6652 | 0.0002 | 273 | 275 | 89.99 | 43.00 | 261 | | | | 2026 Jun 16, 00:08 | 6861 | 0.0002 | 482 | 484 | 94.27 | 43.00 | 197 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 22
Life <1 day
|
| Launched Starlink Group 06-104. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-037 Falcon 9 Block 5 (Starlink Group 06-110)
Vandenberg Space Force Base | 2026 Feb 25, 02:04 UTC | Starlink 36301 2026-037A 67932 |
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 03:09 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 3, 14:00 | 6660 | 0.0001 | 281 | 283 | 90.15 | 43.00 | 264 | | | | 2026 Jun 15, 19:41 | 6861 | 0.0000 | 483 | 483 | 94.26 | 43.01 | 307 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 25
Life <1 day
|
| Launched Starlink Group 06-110. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-038 Falcon 9 Block 5 (Starlink Group 17-026)
Vandenberg Space Force Base | 2026 Feb 25, 14:17 UTC | Starlink 36912 2026-038A 67961 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:19 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 3, 14:00 | 6637 | 0.0001 | 258 | 259 | 89.68 | 97.28 | 99 | | | | 2026 Jun 15, 22:51 | 6844 | 0.0002 | 464 | 467 | 93.91 | 97.28 | 99 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 25
Life <1 day
|
| Launched Starlink Group 17-026. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-039 Falcon 9 Block 5 (Starlink Group 06-108)
Cape Canaveral Space Force Station | 2026 Feb 27, 12:16 UTC | Starlink 36535 2026-039A 67986 |
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 13:20 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 3, 14:00 | 6648 | 0.0002 | 269 | 271 | 89.92 | 43.00 | 279 | | | | 2026 Jun 15, 09:46 | 6861 | 0.0002 | 481 | 485 | 94.27 | 43.01 | 286 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Feb 27
Life <1 day
|
| Launched Starlink Group 06-108. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-040 Falcon 9 Block 5 (Starlink Group 17-023)
Vandenberg Space Force Base | 2026 Mar 1, 22:10 UTC | Starlink 36335 2026-040A 68015 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 23:12 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 5, 20:59 | 6621 | 0.0001 | 242 | 243 | 89.35 | 97.29 | 37 | | | | 2026 Jun 16, 02:59 | 6844 | 0.0002 | 464 | 467 | 93.90 | 97.29 | 93 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 2
Life 1 day
|
| Launched Starlink Group 17-023. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-041 Falcon 9 Block 5 (Starlink Group 10-041)
Cape Canaveral Space Force Station | 2026 Mar 2, 02:56 UTC | Starlink 36711 2026-041A 68040 |
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 14:00 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 5, 23:32 | 6646 | 0.0000 | 268 | 269 | 89.88 | 53.16 | 3 | | | | 2026 Jun 16, 03:05 | 6841 | 0.0001 | 462 | 464 | 93.85 | 53.16 | 90 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 2
Life <1 day
|
| Launched Starlink Group 10-41. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-042 Falcon 9 Block 5 (Starlink Group 10-040)
Cape Canaveral Space Force Station | 2026 Mar 4, 10:52 UTC | Starlink 36766 2026-042A 68069 |
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 11:56 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 9, 18:00 | 6650 | 0.0001 | 272 | 273 | 89.95 | 53.16 | 56 | | | | 2026 Jun 16, 02:00 | 6841 | 0.0001 | 462 | 464 | 93.85 | 53.16 | 72 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 4
Life <1 day
|
| Launched Starlink Group 10-40. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-F04 - failed to reach orbit KAIROS (Kii-based Advanced & Instant Rocket System)
Kii Space Port, Japan | 2026 Mar 5, 02:10 UTC | |
|
| Six satellites were lost when the first stage developed a fault about two minutes after liftoff, resulting in a decision to destroy the rocket. |
|
2026-043 Electron (Insight At Speed Is A Friend Indeed)
Rocket Lab Launch Complex, New Zealand | 2026 Mar 5, 23:53 UTC | BlackSky 34 (Global 34) 2026-043A 68098 |
in space
|
| Third Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc. Separated from launch vehicle Mar 6 at about 00:56 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 6, 11:23 | 6850 | 0.0007 | 467 | 476 | 94.03 | 42.02 | 274 | | | | Electron second stage 2026-043B 68099 |
Re-entered - 2026 Mar 13
Life 8 days
|
| Launched BlackSky 34 satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 6, 12:34 | 6705 | 0.0219 | 180 | 473 | 91.06 | 42.02 | 270 | | | | Electron third stage (kick stage) 2026-043C 68100 |
Re-entered - 2026 Mar 12
Life 7 days
|
| Launched BlackSky 34 satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 7, 12:49 | 6693 | 0.0187 | 190 | 440 | 90.82 | 42.12 | 32 | | | |
2026-044 Falcon 9 Block 5 (Starlink Group 17-018)
Vandenberg Space Force Base | 2026 Mar 8, 11:00 UTC | Starlink 37022 2026-044A 68101 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 12:02 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 12, 16:00 | 6634 | 0.0001 | 256 | 257 | 89.63 | 97.28 | 105 | | | | 2026 Jun 15, 20:44 | 6844 | 0.0002 | 464 | 467 | 93.91 | 97.28 | 93 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 8
Life <1 day
|
| Launched Starlink Group 17-018. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-045 Falcon 9 Block 5 (Echostar 25)
Cape Canaveral Space Force Station | 2026 Mar 10, 04:19 UTC | Echostar 25 2026-045A 68126 |
in space
|
| High capacity, high speed comsat covering the North and South America. Separated from launch vehicle at 04:54 UTC. Expected location - 110° west to join an existing cluster of Echostar satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 Mar 10, 08:18 | 17518 | 0.6208 | 264 | 22016 | 384.58 | 26.89 | 174 | | | | 2026 Mar 15, 03:38 | 19986 | 0.6668 | 281 | 26936 | 468.66 | 26.86 | 179 | | | | 2026 Mar 19, 02:28 | 28570 | 0.4748 | 8628 | 35755 | 800.97 | 9.96 | 181 | | | | 2026 Mar 23, 17:47 | 42105 | 0.0001 | 35721 | 35733 | 1433.07 | 0.07 | 193 | 129°.6 W | | | 2026 Mar 25, 11:29 | 42137 | 0.0008 | 35723 | 35795 | 1434.67 | 0.06 | 134 | 128°.9 W | | | 2026 Mar 26, 14:38 | 42165 | 0.0002 | 35777 | 35796 | 1436.09 | 0.06 | 105 | 128°.9 W | | | 2026 May 1, 17:52 | 42071 | 0.0002 | 35686 | 35700 | 1431.32 | 0.01 | 56 | 128°.0 W | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 10
Life <1 day
|
| Launched Echostar 25. |
| Not Catalogued - orbit parameters unavailable | |
2026-046 Firefly Alpha Block 1 (FLTA007, Stairway To Seven)
Vandenberg Space Force Base | 2026 Mar 12, 00:50 UTC | Lockheed Martin LM-400 Demonstrator (ICOR SV) 2026-046B 68128 |
in space
|
| Demonstrator of Lockheed Martin's LM-400 satellite bus. Payload details kept confidential. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 12, 09:33 | 6777 | 0.0013 | 390 | 408 | 92.55 | 123.09 | 340 | | | | Firefly Alpha second stage 2026-046A 68127 |
Re-entered - 2026 Apr 21
Life 40 days
|
| Instrumented rocket stage to test and demonstrate the vehicle on its return to flight following the 2025 April launch failure. Perigee lowered after releasing satellite as a test of restart capability of the rocket engine. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 12, 09:26 | 6706 | 0.0144 | 231 | 424 | 91.08 | 123.08 | 185 | | | |
2026-047 CZ 8A (Y-8)
Hainan Commercial Zone, Wenchang Space Centre | 2026 Mar 12, 19:48 UTC | Hulianwang Digui 20-01 (Satellite Low Orbit Internet Group 20-01) 2024-047A 68129 |
in space
|
One of eight 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
( ° ) | | |
| 2026 Mar 13, 13:57 | 7251 | 0.0009 | 867 | 880 | 102.42 | 50.01 | 267 | | | | CZ 8A third stage 2026-047K 68138 |
in space
|
| Launched Hulianwang Digui group 20. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 16, 21:42 | 7230 | 0.0045 | 819 | 884 | 101.97 | 49.95 | 163 | | | |
2026-048 CZ 2D
Xichang Space Centre | 2026 Mar 12, 22:33 UTC | Shiyan 30-03 2026-048A 68139 |
in space
|
| One of a pair of simultaneously-launched Earth observation satellites. Described as 'experimental' and testing unspecified observation technologies. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 13, 14:08 | 6967 | 0.0005 | 586 | 593 | 96.46 | 35.00 | 308 | | | | 2026 Mar 17, 12:51 | 6971 | 0.0004 | 590 | 596 | 96.54 | 35.00 | 274 | | | | Shiyan 30-04 2026-048B 68140 |
in space
|
| One of a pair of simultaneously-launched Earth observation satellites. Described as 'experimental' and testing unspecified observation technologies. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 13, 14:09 | 6968 | 0.0004 | 587 | 593 | 96.47 | 34.99 | 308 | | | | 2026 Mar 17, 08:03 | 6971 | 0.0003 | 591 | 595 | 96.54 | 34.99 | 278 | | | | CZ 2D second stage 2026-048C 68141 |
in space
|
| Launched Shiyan 30-03 and 30-04. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 13, 14:07 | 6959 | 0.0016 | 570 | 592 | 96.29 | 35.13 | 358 | | | |
2026-049 Falcon 9 Block 5 (Starlink Group 17-031)
Vandenberg Space Force Base | 2026 Mar 13, 14:57 UTC | Starlink 36604 2026-049A 68142 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:58 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 19, 13:52 | 6648 | 0.0001 | 270 | 270 | 89.91 | 97.28 | 65 | | | | 2026 Jun 16, 00:33 | 6844 | 0.0002 | 464 | 467 | 93.91 | 97.28 | 103 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 13
Life <1 day
|
| Launched Starlink Group 17-031. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-050 Falcon 9 Block 5 (Starlink Group 10-048)
Cape Canaveral Space Force Station | 2026 Mar 14, 12:37 UTC | Starlink 36969 2026-050A 68167 |
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 1341 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 19, 13:41 | 6660 | 0.0000 | 281 | 282 | 90.15 | 53.16 | 318 | | | | 2026 Jun 16, 04:00 | 6838 | 0.0001 | 459 | 461 | 93.79 | 53.16 | 95 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 14
Life <1 day
|
| Launched Starlink Group 10-048. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-051 CZ 6A
Taiyuan Space Centre | 2026 Mar 15, 13:22 UTC | Yaogan 50-02 2026-051A 68196 |
in space
|
| Government or military Earth observation satellite in highly retrograde orbit. Possibly using radar imaging. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 16, 16:05 | 7217 | 0.0149 | 731 | 946 | 101.69 | 142.00 | 129 | | | | 2026 Mar 17, 15:48 | 7226 | 0.0137 | 749 | 946 | 101.88 | 142.00 | 136 | | | | 2026 Mar 17, 22:35 | 7226 | 0.0136 | 749 | 946 | 101.88 | 142.00 | 137 | | | | 2026 Mar 18, 12:10 | 7245 | 0.0107 | 789 | 945 | 102.30 | 142.02 | 142 | | | | 2026 Mar 20, 00:00 | 7264 | 0.0086 | 823 | 948 | 102.68 | 141.99 | 153 | | | | 2026 Mar 23, 03:42 | 7319 | 0.0072 | 888 | 993 | 103.85 | 142.09 | 159 | | | | 2026 Mar 25, 12:52 | 7330 | 0.0002 | 951 | 954 | 104.10 | 141.99 | 221 | | | | CZ 6A third stage 2026-051B 68197 |
in space
|
| Launched Yaogan 50-02. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 16, 20:18 | 7083 | 0.0186 | 574 | 836 | 98.88 | 142.03 | 101 | | | |
2026-052 Kuaizhou 11 (Y-7)
Jiuquan Space Centre | 2026 Mar 16, 04:12 UTC | Yuxing 3-06 (Hunan University of Science and Technology-2) 2026-052B 68199 |
in space
|
| Technology demonstrator from Hunan University, Hainan - including an Earth imaging system, elements of a potential satellite re-fuelling system and a drag device to accelerate orbit decay and the end of the mission. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Mar 17, 01:54 | 6914 | 0.0012 | 528 | 544 | 95.37 | 97.54 | 264 | 10:30 | | | |
in space
|
Earth observation satellite. Separated from launch vehicle upper stage March 18 at about 17:00 UTC, around 2.5 days after launch. This may be a debris item but could be Dongpo 16 - released when its separation mechanism eventually activated.
Dongpo 16 was Included in the formal news announcement of launch success but other information sources, and initial orbit data issued by Space-Track, covered only seven rather than the eight expected satellites. Dongpo 16 seems the most likely candidate for the missing vehicle. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 19, 16:42 | 7049 | 0.0549 | 284 | 1058 | 98.17 | 97.34 | 2 | | | | |
in space
|
| Earth observation satellite - equipped with a radar imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6914 | 0.0011 | 528 | 544 | 95.36 | 97.54 | 268 | 10:30 | | | |
in space
|
| Earth observation satellite - equipped with an optical imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6914 | 0.0010 | 528 | 543 | 95.35 | 97.54 | 262 | 10:30 | | | |
in space
|
| Earth observation satellite equipped with a radar imaging system from the JuanTian Intelligent Technology Co of |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6914 | 0.0012 | 528 | 544 | 95.37 | 97.54 | 264 | 10:30 | | | |
in space
|
| Small satellite from Xingzhong Space Partners of China. Equipped with a demonstrator payload for an Earth observation system using optical and infrared imaging systems. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0009 | 528 | 541 | 95.33 | 97.54 | 263 | 10:30 | | | |
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. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6915 | 0.0012 | 528 | 545 | 95.38 | 97.54 | 262 | 10:30 | | | |
in space
|
| Small satellite from Xingzhong Space Partners of China equipped with demonstrator payload for an Earth observation mission using optical and infrared imaging systems. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0010 | 528 | 541 | 95.33 | 97.54 | 259 | 10:30 | | | Kuaizhou 11 third stage 2026-052H 68205 |
in space
|
| Launched cluster of eight satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 16, 21:35 | 7050 | 0.0550 | 285 | 1060 | 98.19 | 97.34 | 11 | | | |
2026-053 Falcon 9 Block 5 (Starlink Group 17-024)
Vandenberg Space Force Base | 2026 Mar 17, 05:19 UTC | Starlink 36986 2026-053A 68207 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:31 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 23, 18:00 | 6662 | 0.0001 | 283 | 285 | 90.20 | 97.28 | 76 | | | | 2026 Jun 16, 03:41 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.28 | 90 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 17
Life <1 day
|
| Launched Starlink Group 17-024. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-054 Falcon 9 Block 5 (Starlink Group 10-046)
Cape Canaveral Space Force Station | 2026 Mar 17, 13:27 UTC | Starlink 37027 2026-054A 68232 |
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 14:29 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 17, 14:19 | 6636 | 0.0004 | 255 | 260 | 89.66 | 53.16 | 341 | | | | 2026 Jun 15, 09:24 | 6841 | 0.0001 | 462 | 464 | 93.85 | 53.16 | 89 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 17
Life <1 day
|
| Launched Starlink Group 10-046. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-055 Falcon 9 Block 5 (Starlink Group 10-033)
Cape Canaveral Space Force Station | 2026 Mar 19, 14:20 UTC | Starlink 37162 2025-055A 68262 |
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 15:21 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 24, 16:00 | 6645 | 0.0001 | 267 | 268 | 89.86 | 53.16 | 94 | | | | 2026 Jun 15, 20:44 | 6841 | 0.0001 | 462 | 464 | 93.85 | 53.16 | 71 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 19
Life <1 day
|
| Launched Starlink Group 10-033. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-056 Electron (Eight Days A Week)
Rocket Lab Launch Complex, New Zealand | 2026 Mar 20, 18:10 UTC | |
in space
|
| Imaging satellite equipped with a synthetic aperture radar - produced by the University of Tokyo, the Tokyo Institute of Technology, Keio University, Japan Space Systems, and a private company - Synspective Inc of Tokyo. Will become part of a constellation of 25-30 satellites to monitor ground movement and ground changes in urban areas. The name derives from the scientific name for the owl and its sensitivity to low levels of light. Separated from launch vehicle at 19:06 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 25, 10:44 | 6946 | 0.0017 | 557 | 580 | 96.03 | 50.28 | 283 | | | | Electron stage 2 2025-056B 68292 |
Re-entered - 2026 Mar 31
Life 11 days
|
| Launched Strix 6. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6723 | 0.0253 | 175 | 515 | 91.44 | 50.27 | 260 | | | | 2026 Mar 25, 02:32 | 6710 | 0.0237 | 173 | 491 | 91.17 | 50.26 | 268 | | | | Electron stage 3 (kick stage) 2025-056C 68293 |
in space
|
| Launched Strix 6. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 25, 12:36 | 6827 | 0.0160 | 340 | 558 | 93.57 | 50.29 | 30 | | | |
2026-057 Falcon 9 Block 5 (Starlink Group 17-015)
Vandenberg Space Force Base | 2026 Mar 20, 21:51 UTC | Starlink 37107 2026-057A 68294 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 22:53 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 20, 22:44 | 6636 | 0.0003 | 256 | 260 | 89.67 | 97.29 | 253 | | | | 2026 Jun 16, 04:00 | 6820 | 0.0002 | 441 | 444 | 93.43 | 97.28 | 89 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 20
Life <1 day
|
| Launched Starlink Group 17-015. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-058 Soyuz-2.1a
Baikonur Cosmodrome | 2026 Mar 22, 11:59 UTC | Progress MS-33 (Progress 7K-MS №463) 2026-058A 68319 |
in space
|
| Supplies to ISS. Initial orbit similar to launch vehicle upper stage. Reported soon after launch that one of the radio aerials of the Kurs automatic rendezvous and docking system had not deployed, leading to the need for ISS crew to use the TORU remote control system to achieve a docking. Docked with the ISS Poisk module March 24 at 13:40 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 22, 19:14 | 6650 | 0.0012 | 264 | 279 | 89.94 | 51.64 | 152 | | | | 2026 Mar 24, 19:24 | 6799 | 0.0006 | 417 | 425 | 92.99 | 51.63 | 228 | | | | Soyuz third stage 2026-058B 68320 |
Re-entered - 2026 Mar 24
Life 2 days
|
| Launched Progress MS-33 |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 22, 19:10 | 6578 | 0.0024 | 184 | 215 | 88.49 | 51.65 | 71 | | | |
2026-059 Falcon 9 Block 5 (Starlink Group 10-62)
Cape Canaveral Space Force Station | 2026 Mar 22, 14:47 UTC | Starlink 36987 2026-059A 68321 |
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 15:48 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 31, 16:00 | 6706 | 0.0001 | 327 | 329 | 91.09 | 53.16 | 72 | | | | 2026 Jun 15, 22:46 | 6853 | 0.0001 | 474 | 476 | 94.11 | 53.16 | 78 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 22
Life <1 day
|
| Launched Starlink Group 10-62. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-060 Jielong 3 (Y-10)
Mobile floating platform, Yellow Sea - 36°.6 N, 121°.2 E | 2026 Mar 22, 15:49 UTC | Wei Li Kongjiang Group 4-01 (Centispace 02-01) 2026-060A 68350 |
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.
All ten satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 23, 05:55 | 7024 | 0.0013 | 636 | 654 | 97.63 | 54.98 | 293 | | | | 2026 Apr 10, 13:05 | 7026 | 0.0015 | 638 | 658 | 97.68 | 54.98 | 308 | | | | 2026 May 11, 04:59 | 7028 | 0.0013 | 641 | 659 | 97.72 | 54.98 | 31 | | | | 2026 Jun 12, 19:54 | 7055 | 0.0008 | 671 | 683 | 98.29 | 54.98 | 270 | | | | Jielong 3 fourth stage. uncatalogued |
|
| Launched ten Wei Li Kongjiang satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-061 Soyuz-2.1b
Plesetsk Cosmodrome | 2026 Mar 23, 17:34 UTC | Rassvet-3 01 2026-061A 68360 |
in space
|
One of sixteen simultaneously-launched Internet communications satellites. Part of a planned constellation of 300 satellites. Fifteen of the satellites had all commenced orbit raising by April 20.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 31, 15:46 | 6683 | 0.0027 | 287 | 323 | 90.62 | 82.30 | 45 | | | | 2026 Apr 9, 21:53 | 6692 | 0.0023 | 299 | 330 | 90.81 | 82.30 | 13 | | | | 2026 Jul 8, 03:47 | 6890 | 0.0000 | 512 | 512 | 94.87 | 82.29 | 205 | | | | Rassvet-3 04 2026-061D 68363 |
Re-entered - 2026 Jun 6
Life 75 days
|
| One of sixteen simultaneously-launched Internet communications satellites. Part of a planned constellation of 300 satellites. Suffered a systems failure, preventing it from commencing orbit raising towards operational height. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 31, 15:46 | 6684 | 0.0027 | 288 | 324 | 90.65 | 82.30 | 45 | | | | 2026 Apr 14, 04:37 | 6679 | 0.0023 | 285 | 316 | 90.53 | 82.30 | 353 | | | | 2026 Apr 28, 21:33 | 6667 | 0.0018 | 277 | 301 | 90.30 | 82.30 | 287 | | | | 2026 May 12, 05:44 | 6651 | 0.0019 | 260 | 285 | 89.96 | 82.30 | 222 | | | | 2026 May 26, 03:29 | 6625 | 0.0020 | 234 | 260 | 89.44 | 82.30 | 179 | | | | 2026 Jun 6, 00:22 | 6540 | 0.0009 | 156 | 167 | 87.72 | 82.29 | 233 | | | | |
in space
|
| 3U? Cubesat? - reportedly carrying space radiation detectors. Transmissions were detected in an amateur radio band but ceased after about two and a half days. No unexplained object was reported by Space-Track so the most likely scenario is that this payload was attached to one of the Rassvet satellites or the Soyuz upper stage. The orbit listed is an estimate based on reported amateur observations of the radio signal. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 24, 15:21 | 6686 | 0.0025 | 291 | 325 | 90.68 | 82.29 | 52 | | | | Soyuz third stage 2026-061S 68537 |
Re-entered - 2026 May 16
Life 54 days
|
| Launched cluster of Rassvet and other satellites. Space-Track lists this as a Fregat rocket stage probably using information gleaned from erroneous speculation in Russian social media. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 1, 11:16 | 6678 | 0.0026 | 282 | 318 | 90.52 | 82.31 | 38 | | | |
2026-062 CZ 2D
Taiyuan Space Centre | 2026 Mar 25, 22:51 UTC | Siwei Gaojing 2-05 (Superview Neo 2-05) 2026-062A 68377 |
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 using a radar imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Mar 27, 02:45 | 6884 | 0.0008 | 500 | 511 | 94.73 | 97.42 | 266 | 06:00 | | | 2026 Mar 31, 14:10 | 6882 | 0.0006 | 500 | 508 | 94.70 | 97.44 | 248 | 06:00 | | | Siwei Gaojing 2-06 (Superview Neo 2-06) 2026-062B 68378 |
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 using a radar imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Mar 26, 10:57 | 6885 | 0.0009 | 501 | 513 | 94.77 | 97.43 | 266 | 06:00 | | | CZ 2D second stage 2026-062C 68379 |
in space
|
| Launched Siwei Gaojing 2-05 and Siwei Gaojing 2-06. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 25, 23:54 | 6852 | 0.0060 | 433 | 515 | 94.08 | 97.50 | 52 | | | |
2026-063 Falcon 9 Block 5 (Starlink Group 17-17)
Vandenberg Space Force Base | 2026 Mar 26, 23:03 UTC | Starlink 36296 2026-063A 68380 |
in space
|
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 2, 18:00 | 6658 | 0.0002 | 279 | 281 | 90.11 | 97.28 | 68 | | | | 2026 Jun 16, 04:00 | 6797 | 0.0001 | 419 | 420 | 92.95 | 97.29 | 88 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 27
Life 1 day
|
| Launched Starlink Group 17-17. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-064 CZ 2C + YZ-1S
Jiuquan Space Centre | 2026 Mar 27, 04:11 UTC | |
in space
|
| Purpose unknown - described as "mainly used for scientific experiments on space environment exploration" - may carry an imaging system to photograph other satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Mar 27, 14:42 | 6873 | 0.0015 | 485 | 505 | 94.52 | 97.47 | 231 | 10:30 | | | 2026 Mar 30, 16:47 | 6874 | 0.0013 | 487 | 505 | 94.54 | 97.47 | 217 | 10:30 | | | YZ-1S rocket stage uncatalogued |
Re-entered - 2026 Mar 27
Life <1 day
|
| Launched Shiyan 33. Caused to re-enter above the Indian Ocean after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-065 Electron (Daughter Of The Stars)
Rocket Lab Launch Complex, New Zealand | 2026 Mar 28, 09:14 UTC | Celeste IOD 1 (In Orbit Demonstrator) 2026-065A 68408 |
in space
|
| 12U Cubesat - one of a simultaneously-launched pair of satellites. Test/demonstrator mission for LEO-PNT (Low Earth Orbit Positioning, Navigation, and Timing), a low orbit enhancement to Europe's Galileo MEO navigation system. Part of a planned 12 satellite constellation, including one on-orbit spare. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Mar 28, 22:34 | 6889 | 0.0016 | 500 | 522 | 94.85 | 97.41 | 287 | 21:35 | | | Celeste IOD 2 (In Orbit Demonstrator) 2026-065B 68409 |
in space
|
| 16U Cubesat - one of a simultaneously-launched pair of satellites. Test/demonstrator mission for LEO-PNT (Low Earth Orbit Positioning, Navigation, and Timing), a low orbit enhancement to Europe's Galileo MEO navigation system. Part of a planned 12 satellite constellation, including one on-orbit spare. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Mar 30, 22:01 | 6889 | 0.0013 | 503 | 520 | 94.85 | 97.41 | 274 | 21:35 | | | Electron stage 2 2026-065C 68410 |
Re-entered - 2026 Apr 3
Life 6 days
|
| Launched pair of Celeste IOD satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 29, 17:50 | 6700 | 0.0228 | 169 | 475 | 90.96 | 97.39 | 206 | | | | Electron stage 3 (kick stage) 2026-065D 68411 |
Re-entered - 2026 Apr 16
Life 19 days
|
| Launched pair of Celeste IOD satellites. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 30, 16:54 | 6722 | 0.0205 | 206 | 481 | 91.41 | 97.42 | 25 | | | |
2026-066 Lijian 2, Kinetica 2 (Y-1)
Dongfeng Commercial Zone, Jiuquan Space Centre | 2026 Mar 30, 11:00 UTC | Xin Zhengcheng 2? (Qingzhou) 2026-066A 68412 |
in space
|
| Prototype of a cargo carrying spacecraft to transport supplies and other material to the Chinese Space station. For this mission it carries 27 self-contained experimental and engineering payloads related to its future missions as a space station support vehicle. Launched with Xin Zhengcheng 1 and Tianshi 1 attached respectively to the fore and aft of the vehicle. Conducted rendezvous operations with Xin Zhengcheng 1 after it was released on April 2. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 31, 12:49 | 6813 | 0.0263 | 256 | 614 | 93.28 | 84.96 | 151 | | | | 2026 Mar 31, 20:39 | 6854 | 0.0206 | 335 | 618 | 94.13 | 84.96 | 144 | | | | 2026 Apr 2, 19:06 | 6981 | 0.0027 | 584 | 622 | 96.75 | 84.96 | 152 | | | | Xin Zhengcheng 1? 2026-066C 68414 |
in space
|
| Described as a technology demonstrator satellite but details not available. Released from Xin Zhengcheng 1 on April 2 around 15:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 2, 22:19 | 6981 | 0.0027 | 584 | 622 | 96.74 | 84.96 | 152 | | | | |
in space
|
| Described as an educational satellite but mission details not available. Built by the Aerospace Information Research Institute of the Chinese Academy of Sciences (AIRSAT). Separated from Xin Zhengcheng 2 on April 3. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 6, 13:27 | 6981 | 0.0027 | 584 | 622 | 96.75 | 84.96 | 140 | | | | Lijian 2 second stage 2026-066B 68413 |
Re-entered - 2026 Apr 13
Life 14 days
|
| Launched Qingzhou and two other satellites. Perigee lowered after releasing Qingzhou. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Mar 31, 18:24 | 6930 | 0.0605 | 133 | 972 | 95.69 | 84.72 | 207 | | | |
2026-067 Falcon 9 Block 5 (Transporter 16)
Vandenberg Space Force Base | 2026 Mar 30, 11:02 UTC | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:56 UTC. Identified by Nico Janssen from radio transmissions. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:07 | 6888 | 0.0004 | 508 | 513 | 94.82 | 97.45 | 117 | 02:45 | | | |
in space
|
| 8U Cubesat from Greek company Planetek Hellas to demonstrate a laser-based satellite-ground communications link. Separated from launch vehicle at 11:58 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:08 | 6889 | 0.0004 | 508 | 513 | 94.83 | 97.45 | 129 | 02:45 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:56 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:08 | 6888 | 0.0003 | 508 | 513 | 94.83 | 97.45 | 108 | 02:45 | | | Ermis 2 (Hermes 2) 2026-067E 68420 |
in space
|
| 6U Cubesat from developed by the National and Kapodistrian University of Athens (NKUA) in collaboration with OQ Hellas, carring an optical communication system for use with internet-connect items on the ground, and an optical Earth imaging system. Separated from launch vehicle at 11:57 UTC. Identified by Nico Janssen from radio transmissions. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:08 | 6888 | 0.0004 | 508 | 513 | 94.82 | 97.44 | 97 | 02:45 | | | |
in space
|
| 16U Cubesat - Earth imaging satellite to monitor land use. One of a pair of similar satellites carried on the Transporter 16 mission. Separated from launch vehicle at 11:56 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:10 | 6889 | 0.0003 | 509 | 513 | 94.84 | 97.45 | 98 | 02:45 | | | BRO 19 (Breizh Reconnaissance Orbiter 19) 2026-067G 68422 |
in space
|
| 6U Cubesat from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Separated from launch vehicle at 11:58 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:11 | 6889 | 0.0003 | 509 | 513 | 94.84 | 97.44 | 95 | 02:45 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:59 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:11 | 6889 | 0.0002 | 509 | 513 | 94.85 | 97.45 | 104 | 02:45 | | | Spacevan 002 (Wings of Light) 2026-067J 68424 |
in space
|
| Orbital transfer vehicle from US company Exotrail carrying five hosted payloads and a 6U Cubesat (AEPEX) that will be released later. Separated from launch vehicle at 12:08 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:19 | 6891 | 0.0000 | 513 | 513 | 94.88 | 97.45 | 205 | 02:45 | | | Ermis 3 (Hermes 3) 2026-067K 68425 |
in space
|
| 8U Cubesat from developed by the National and Kapodistrian University of Athens (NKUA), carring an optical communication system for use with internet-connect items on the ground, and an optical Earth imaging system. Separated from launch vehicle at 11:58 UTC. Identified by Nico Janssen from radio transmissions. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 00:03 | 6890 | 0.0002 | 510 | 513 | 94.85 | 97.45 | 136 | 02:45 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:01 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:12 | 6889 | 0.0002 | 510 | 512 | 94.84 | 97.45 | 138 | 02:45 | | | Out of the Box 2026-067N 68428 |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:01 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:14 | 6890 | 0.0002 | 511 | 513 | 94.86 | 97.45 | 149 | 02:45 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:01 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:16 | 6890 | 0.0001 | 511 | 512 | 94.86 | 97.45 | 198 | 02:45 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:56 UTC. 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 | |
| 2026 Apr 14, 03:12 | 6889 | 0.0002 | 510 | 513 | 94.85 | 97.45 | 106 | 02:45 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:59 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:14 | 6890 | 0.0002 | 510 | 513 | 94.85 | 97.45 | 159 | 02:45 | | | |
in space
|
| Small satellite from Satellogic of Argentina providing Earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Separated from launch vehicle at 12:07 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:16 | 6890 | 0.0001 | 512 | 513 | 94.87 | 97.45 | 192 | 02:45 | | | T.MicroSat 2 2026-067T 68433 |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:59 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:31 | 6894 | 0.0004 | 513 | 518 | 94.94 | 97.45 | 292 | 02:44 | | | |
in space
|
| 16U Cubesat - Earth imaging satellite to monitor land use. One of a pair of similar satellites carried on the Transporter 16 mission. Separated from launch vehicle at 11:59 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:12 | 6890 | 0.0002 | 510 | 513 | 94.85 | 97.45 | 139 | 02:45 | | | ION SCV 019 (Astounding Alexandra) 2026-067V 68435 |
in space
|
| Satellite carrier from D-Orbit carrying three hosted payloads of customer-suppled experiments/sensors and Cubesat deployers containing four 8U Luciada cubesats for later release. Separated from launch vehicle at 12:09 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:20 | 6891 | 0.0001 | 513 | 514 | 94.89 | 97.45 | 267 | 02:45 | | | 2026 May 20, 03:19 | 6891 | 0.0003 | 511 | 516 | 94.89 | 97.45 | 129 | 02:44 | | | 2026 May 27, 20:26 | 6883 | 0.0016 | 494 | 516 | 94.72 | 97.45 | 100 | 02:44 | | | Hawk 14B (Cluster 14#2) 2026-067W 68436 |
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. Separated from launch vehicle at 12:09 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:21 | 6892 | 0.0001 | 514 | 514 | 94.91 | 97.45 | 272 | 02:45 | | | AiglonSat 1 2026-067X 68437 |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:01 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:17 | 6890 | 0.0000 | 512 | 512 | 94.86 | 97.45 | 215 | 02:44 | | | Hawk 14C (Cluster 14#3) 2026-067AB 68441 |
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. Separated from launch vehicle at 12:11 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:23 | 6891 | 0.0001 | 512 | 514 | 94.88 | 97.45 | 347 | 02:44 | | | |
in space
|
| Small satellite from Satellogic of Argentina providing Earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Separated from launch vehicle at 12:01 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:27 | 6893 | 0.0003 | 513 | 516 | 94.92 | 97.45 | 307 | 02:44 | | | Dream Big 1 2026-067AD 68443 |
in space
|
0.5U Cubesat built by a consortium of Universities and industry to teach students the elements of building and launching a satellite. One of six similar satellites carries on this launch. Separated from launch vehicle at 12:05 UTC.
All satellites were released into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 01:53 | 6893 | 0.0003 | 513 | 517 | 94.92 | 97.45 | 310 | 02:44 | | | Sharjah Sat 2 2026-067AE 68444 |
in space
|
| 6U Cubesat from Sharjah Academy for Astronomy, Space Sciences and Technology (SAASST) of the University of Sharjah. Earth observation ission equipped with a high rolution imaging system. Separated from launch vehicle at 12:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:13 | 6890 | 0.0002 | 510 | 513 | 94.85 | 97.45 | 142 | 02:45 | | | HADES (SpinnyONE) 2026-067AG 68446 |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:56 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:32 | 6893 | 0.0005 | 512 | 519 | 94.93 | 97.44 | 311 | 02:44 | | | Hawk 14A (Cluster 14#1) 2026-067AJ 68448 |
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. Separated from launch vehicle at 12:07 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:24 | 6891 | 0.0002 | 512 | 514 | 94.88 | 97.45 | 331 | 02:44 | | | IRIDE-MS1 Eaglet 2-09 2026-067AK 68449 |
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 eight similar satellites carried on this launch. Separated from launch vehicle at 12:02 UTC.
All satellites were released into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:26 | 6892 | 0.0002 | 513 | 516 | 94.91 | 97.45 | 321 | 02:44 | | | |
in space
|
| Norwegian satellite carrying an AIS (Automatic Identification System) receiver to monitor maritime traffic in Norwegian and international waters. Separated from launch vehicle at 12:02 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 01:54 | 6893 | 0.0004 | 513 | 517 | 94.93 | 97.45 | 297 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:58 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:31 | 6894 | 0.0004 | 513 | 518 | 94.93 | 97.45 | 296 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:58 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:31 | 6894 | 0.0004 | 513 | 518 | 94.93 | 97.44 | 310 | 02:44 | | | COSMO (Compact Spaceborne Magnetic Observatory) 2026-067AW 68460 |
in space
|
| 6U Cubesat (6x1) from the University of Colrado conducting high resolution magnetic field studies. Separated from launch vehicle at 11:57 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:32 | 6894 | 0.0004 | 513 | 518 | 94.94 | 97.44 | 302 | 02:44 | | | Unamuno (Garai B) 2026-067AZ 68463 |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:05 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:25 | 6892 | 0.0002 | 513 | 515 | 94.91 | 97.45 | 318 | 02:44 | | | FGN 100 d3 2026-067BA 68464 |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:07 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:25 | 6892 | 0.0002 | 513 | 515 | 94.91 | 97.45 | 332 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:07 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:25 | 6892 | 0.0002 | 513 | 516 | 94.91 | 97.45 | 329 | 02:44 | | | Ermis 1 (Hermes 1) 2026-067BE 68468 |
in space
|
| 6U Cubesat from developed by the National and Kapodistrian University of Athens (NKUA) in collaboration with OQ Hellas, carring an optical communication system for use with internet-connect items on the ground, and an optical Earth imaging system. Separated from launch vehicle at 11:56 UTC. |
| Orbit parameters awaited | | W Series 6 2026-067BF 68469 |
Re-entered - 2026 May 18
Life 49 days
|
| Mission details to follow. Separated from launch vehicle at 12:08 UTC. Descent vehicle was caused to re-enter the atmosphere 2026 May 18 and landed by parachute in the Koonibba Test Range, South Australia. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:24 | 6892 | 0.0002 | 513 | 515 | 94.91 | 97.45 | 317 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:56 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 03:34 | 6894 | 0.0005 | 512 | 520 | 94.95 | 97.44 | 301 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:27 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:20 | 6973 | 0.0003 | 593 | 597 | 96.59 | 97.76 | 245 | 02:44 | | | Vigoride 7 (NOM4DRide) 2026-067BK 68473 |
in space
|
| Satellite carrier from US company Momentus Systems. Separated from launch vehicle at 12:07 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 7, 08:00 | 6893 | 0.0003 | 513 | 517 | 94.92 | 97.45 | 349 | 02:45 | | | Black Kite 2 2026-067BL 68474 |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:27 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:00 | 6969 | 0.0004 | 588 | 594 | 96.50 | 97.75 | 93 | 02:44 | | | Unicorn 2S 2026-067BM 68475 |
in space
|
| 3p PocketQube satellite. Mission details to follow. Separated from launch vehicle at 13:27 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 20:42 | 6973 | 0.0002 | 593 | 596 | 96.58 | 97.75 | 288 | 02:44 | | | Fossasat 2E-25 2026-067BQ 68478 |
in space
|
| 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Separated from launch vehicle at 13:29 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:03 | 6970 | 0.0003 | 589 | 594 | 96.51 | 97.75 | 115 | 02:44 | | | Lemur-2 (Irina) 2026-067BS 68480 |
in space
|
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. One of nine similar satellites carried on this launch. Separated from launch vehicle at 13:27 UTC.
All satellites were released into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 21:57 | 6968 | 0.0005 | 586 | 594 | 96.48 | 97.76 | 113 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:28 UTC. Identified by Nico Janssen from radio transmissions. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:05 | 6970 | 0.0003 | 589 | 594 | 96.52 | 97.76 | 141 | 02:44 | | | Vindlér 2.0.3 2026-067BW 68484 |
in space
|
| Small SIGINT satellite from US company SNC. Carries muti-band receivers to detect and analyse radio signal from the ground. Separated from launch vehicle at 13:32 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:07 | 6970 | 0.0002 | 591 | 594 | 96.53 | 97.76 | 133 | 02:44 | | | Capella 20 (Acadia 10) 2026-067BX 68485 |
in space
|
| Small satellite from Capella Space Corp, equipped with an Earth imaging system. Separated from launch vehicle at 13:31 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:06 | 6970 | 0.0002 | 590 | 593 | 96.52 | 97.75 | 121 | 02:44 | | | Vindlér 2.0.2 2026-067BY 68486 |
in space
|
| Small SIGINT satellite from US company SNC. Carries muti-band receivers to detect and analyse radio signal from the ground. Separated from launch vehicle at 13:30 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:07 | 6971 | 0.0002 | 591 | 594 | 96.53 | 97.75 | 119 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:28 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:02 | 6969 | 0.0003 | 589 | 593 | 96.50 | 97.75 | 94 | 02:44 | | | Vindlér 2.0.1 2026-067CA 68488 |
in space
|
| Small SIGINT satellite from US company SNC. Carries muti-band receivers to detect and analyse radio signal from the ground. Separated from launch vehicle at 13:33 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:11 | 6971 | 0.0001 | 593 | 594 | 96.55 | 97.75 | 119 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:29 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:13 | 6972 | 0.0001 | 593 | 595 | 96.56 | 97.76 | 197 | 02:44 | | | ICEYE X 71 2026-067CG 68494 |
in space
|
Small satellite fitted with a synthetic aperture radar for Earth surface imaging. One of six similar satellites carried on this launch. Separated from launch vehicle at 13:29 UTC.
All satellites were released into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:13 | 6972 | 0.0001 | 593 | 594 | 96.56 | 97.76 | 192 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:17 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:23 | 6979 | 0.0002 | 600 | 602 | 96.71 | 97.76 | 194 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:28 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:15 | 6972 | 0.0001 | 594 | 595 | 96.57 | 97.75 | 296 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:31 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:12 | 6972 | 0.0000 | 593 | 594 | 96.56 | 97.75 | 139 | 02:44 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:27 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 14, 14:28 | 6974 | 0.0003 | 594 | 598 | 96.60 | 97.75 | 265 | 02:44 | | | GEMS 2 (Amethyst) 2026-067CT 68505 |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:27 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 13, 22:23 | 6974 | 0.0004 | 593 | 599 | 96.60 | 97.76 | 256 | 02:44 | | | AEPEX (Atmospheric Effects of Precipitation through Energetic X-rays) 2026-067CU 68506 |
in space
|
| 6U Cubesat - from the University of Colorado studying charged particles falling from the Earth's radiation belts to lower altitudes. Released from Spacevan 002 (68424/2026-067J) around May 14. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 20, 22:04 | 6888 | 0.0004 | 508 | 513 | 94.83 | 97.45 | 146 | 02:44 | | | Lusiada 1 (Camões) 2026-067CV 68507 |
in space
|
| 8U Cubesat (4 x 2) - owned by LusoSpace of Portugal, carring a VDES system for relaying messages between aircraft and ground stations. Released from ION SCV (68435/2026-067CV) around, probably, May 24. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 27, 03:01 | 6890 | 0.0005 | 509 | 516 | 94.87 | 97.46 | 124 | 02:44 | | | |
in space
|
| 6U - Cubesat - from US company Lunar Outpost to demonstrate autonomous 'swarm' operations by a fleet of robotic satellites in LEO for the USAF and USSF. Released from Spacevan 002 (68424/2026-067J) probably around May 25. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 28, 19:53 | 6888 | 0.0004 | 507 | 512 | 94.81 | 97.45 | 141 | 02:44 | | | Lusiada 2 (Bessa) 2026-067CX 68836 |
in space
|
| 8U Cubesat (4 x 2) - owned by LusoSpace of Portugal, carring a VDES system for relaying messages between aircraft and ground stations. Released from ION SCV (68435/2026-067CV) mid-June. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 18, 10:47 | 6889 | 0.0011 | 503 | 519 | 94.85 | 97.45 | 19 | 02:44 | | | Lusiada 3 (Saramago) 2026-067CY 100000 |
in space
|
| 8U Cubesat (4 x 2) - owned by LusoSpace of Portugal, carring a VDES system for relaying messages between aircraft and ground stations. Released from ION SCV (68435/2026-067CV) around Jul 1. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 14, 21:45 | 6883 | 0.0006 | 501 | 508 | 94.71 | 97.46 | 271 | 02:45 | | | Lusiada 4 (Pessoa) 2026-067CZ 100139 |
in space
|
| 8U Cubesat (4 x 2) - owned by LusoSpace of Portugal, carring a VDES system for relaying messages between aircraft and ground stations. Released from ION SCV (68435/2026-067CV) 2026 mid-July. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 21, 23:03 | 6887 | 0.0006 | 505 | 513 | 94.80 | 97.46 | 310 | 02:45 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:56 UTC. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:03 UTC. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:01 UTC. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:02 UTC. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 13:28 UTC. |
| Orbit parameters awaited | | |
in space
|
| 3U Cubesat from the Aristotle University of Thessaloniki, Greece to demonstrate laser communication links between satellites and ground stations. Separated from launch vehicle at 11:57 UTC. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:00 UTC. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 12:00 UTC. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at 11:57 UTC. |
| Orbit parameters awaited | | |
in space
|
| 3p PocketQube satellite. Mission details to follow. Separated from launch vehicle at 13:27 UTC. |
| Orbit parameters awaited | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 30
Life <1 day
|
| Launched Transporter 16 Rideshare mission. Caused to re-enter at about 14:15 UTC above the Pacific Ocean after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-068 Falcon 9 Block 5 (Starlink Group 10-44)
Cape Canaveral Space Force Station | 2026 Mar 30, 21:15 UTC | Starlink 37262 2026-068A 68508 |
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 March 31 at 00:16 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 7, 04:29 | 6679 | 0.0000 | 301 | 301 | 90.53 | 53.16 | 95 | | | | 2026 Jun 15, 21:27 | 6841 | 0.0001 | 462 | 463 | 93.85 | 53.16 | 94 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Mar 30
Life <1 day
|
| Launched Starlink Group 10-44. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-069 SLS
Kennedy Space Center | 2026 Apr 1, 22:35 UTC | Artemis 2 (Orion 2, Integrity) 2026-069A 68538 |
Re-entered - 2026 Apr 11
Life 10 days
Returned to Earth |
| Lunar fly-by mission carring crew consisting of NASA astronauts Reid Wiseman (commander), Victor Glover (pilot), Christina Koch (mission specialist), and Jeremy Hansen (mission specialist) of the Canadian Space Agency. Separated from launch vehicle April 2 at 01:57 UTC. A six minute firing of the Service Propulsion System April 2 at 23:49 UTC placed Artemis in barycentric orbit and on a trajectory to meet the Moon. A further mid course engine firing was made April 5 and Artemis passed behind the Moon, as viewed from Earth, on April 6. Splashed down in the Pacific Ocean off California April 11 at 00:07 UTC. The first orbit listed is an estimate based on NASA information. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 2, 04:30 | 41488 | 0.8434 | 120 | 70100 | 1401.67 | 28.53 | 70 | | | | 2026 Apr 2, 23:32 | 231743 | 0.9815 | -2089 | 452818 | 18504.15 | 28.15 | 83 | | | | 2026 Apr 5, 07:30 | 175750 | 0.9964 | -5751 | 344494 | 12220.86 | 56.36 | 34 | | | | 2026 Apr 8, 21:20 | 220232 | 0.9846 | -2977 | 430686 | 17142.77 | 39.72 | 44 | | | | 2026 Apr 9, 12:57 | 187779 | 0.9762 | -1908 | 364710 | 13496.79 | 37.54 | 47 | | | | 2026 Apr 9, 23:56 | 199413 | 0.9731 | -1013 | 387082 | 14770.26 | 37.70 | 46 | | | | |
Re-entered - 2026 Apr 2
Life 1 day
|
| 12U Cubesat built by Neurospace for the German government to test electronic components for a future lunar rover in space conditions. Separated from the launch vehicle April 2 at around 03:58 UTC. Re-entered Earth's atmosphere at the end of its first circuit as the result of a very low perigee. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 2, 13:12 | 41576 | 0.8430 | 149 | 70247 | 1406.14 | 28.34 | 78 | | | | Space Weather CubeSat-1 2026-069C 68540 |
Re-entered - 2026 Apr 4
Life 3 days
|
| 12U Cubesat from Saudi Arabia carrying an instrument to detect and measure solar particles in Earth-Moon space. Separated from the launch vehicle April 2 at around 03:58 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 2, 12:20 | 41798 | 0.8375 | 414 | 70426 | 1417.38 | 28.35 | 77 | | | | |
Re-entered - 2026 Apr 2
Life 1 day
|
| 12U Cubesat from the (South) Korea Aerospace Administration. Carries a a dosimeter made of material designed to mimic human tissue to measure space radiation levels as it passes through the van Allen radiation belts. Separated from the launch vehicle April 2 at around 03:58 UTC. Re-entered Earth's atmosphere at the end of its first circuit as the result of a very low perigee. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 2, 16:16 | 41547 | 0.8450 | 61 | 70276 | 1404.63 | 28.33 | 78 | | | | Atenea (Athena) uncatalogued |
Re-entered - 2026 Apr 2
Life 1 day
|
| 12U Cubesat from Argentina's space agency equipped with radiation detectors and samples of radiation shielding materials. Separated from the launch vehicle April 2 at around 03:58 UTC. Re-entered Earth's atmosphere at the end of its first circuit as the result of a very low perigee. |
| Not Catalogued - orbit parameters unavailable | | SLS third stage (Interim Cryogenic Propulsion Stage) 2026-069E 68655 |
Re-entered - 2026 Apr 2
Life 1 day
|
| Launched Artemis 2 and Cubesats. Caused to re-enter after releasing Artemis 2 and the four Cubesats. Unusually for an object that would not normally be classified as secret, this object was Catalogued but no orbit information was published. |
| Orbit parameters awaited | |
2026-070 Falcon 9 Block 5 (Starlink Group 10-58)
Cape Canaveral Space Force Station | 2026 Apr 2, 11:55 UTC | Starlink 37326 2026-070A 68542 |
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 at 12:58 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 7, 20:20 | 6645 | 0.0000 | 266 | 267 | 89.84 | 53.16 | 92 | | | | 2026 Jun 15, 13:54 | 6841 | 0.0001 | 462 | 463 | 93.85 | 53.16 | 75 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 2
Life <1 day
|
| Launched Starlink Group 10-58. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-F05 - failed to reach orbit Tianlong 3 (Y1)
Dongfeng Commercial Zone, Jiuquan Space Centre | 2026 Apr 3, 04:17 UTC | |
|
| Lost when launch vehicle failed during ascent. |
|
2026-071 Soyuz-2.1a + Fregat
Plesetsk Cosmodrome | 2026 Apr 3, 06:28 UTC | Meridian 11 (Meridian-M № 21L) 2026-071A 68571 |
in space
|
| HEO military/government comsat to support Russian forces, commercial shipping and communication ground stations at northern latitudes across Russia. Meridian also supports the clandestine short messaging system formerly provided by the Parus satellites. Fourth mission using the Meridian-M version. Probably moved to operational orbit around April 15. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 7, 08:22 | 26734 | 0.7239 | 1003 | 39710 | 725.05 | 62.78 | 285 | | | | 2026 Apr 17, 09:37 | 26555 | 0.7214 | 1019 | 39335 | 717.77 | 62.78 | 285 | | | | Fregat rocket stage 2026-071B 68572 |
in space
|
| Mission details to follow. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 3, 07:42 | 26518 | 0.7314 | 745 | 39535 | 716.27 | 63.06 | 285 | | | |
2026-072 Atlas V 551 (KA-04, Amazon LEO 05)
Cape Canaveral Space Force Station | 2026 Apr 4, 05:36 UTC | Amazon LEO 00131 (Kuiper 00131) 2026-072A 68573 |
in space
|
One member of a simultaneously-launched cluster of twenty nine 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
( ° ) | | |
| 2026 Apr 9, 12:06 | 6833 | 0.0007 | 450 | 460 | 93.69 | 51.87 | 122 | | | | Atlas V third stage (Centaur) uncatalogued |
Re-entered - 2026 Apr 4
Life <1 day
|
| Launched twenty nine Kuiper satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | | Atlas V third stage (Centaur) uncatalogued |
Re-entered - 2026 Apr 4
Life <1 day
|
| Launched twenty nine Kuiper satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-073 Falcon 9 Block 5 (Starlink Group 17-35)
Vandenberg Space Force Base | 2026 Apr 7, 02:50 UTC | Starlink 37135 2026-073A 68602 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:51 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 16, 16:21 | 6706 | 0.0000 | 328 | 328 | 91.10 | 97.29 | 122 | | | | 2026 Jun 16, 01:55 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.28 | 97 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 7
Life <1 day
|
| Launched Starlink Group 17-35. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-074 Minotaur IV (STP-29A)
Vandenberg Space Force Base | 2026 Apr 7, 11:33 UTC | ASTRA HyRAX (Auburn Satellite Testbed for Retrodirective Array – Hybrid Retrodirective Array in X-band) 2026-074A 68627 |
in space
|
| 3U Cubesat from Auburn University carrying SIGINT radio receivers to study and classify other satellites in orbit. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 8, 04:18 | 6875 | 0.0016 | 486 | 507 | 94.54 | 60.02 | 302 | | | | |
in space
|
| 16U Cubesat carrying a collection of sensors/instruments related to tactical space warfare. One of a simultaneously-launched pair. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 7, 22:00 | 6874 | 0.0015 | 486 | 507 | 94.54 | 60.02 | 308 | | | | |
in space
|
| ?U Cubesat - one of a simultaneously-launched pair from the United States Army Space and Missile Defense Command carrying a collection of sensors/instruments related to tactical space warfare. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 8, 04:18 | 6873 | 0.0017 | 483 | 507 | 94.51 | 60.02 | 312 | | | | |
in space
|
| Small satellite for the US military Space Test Program carrying a number of sensors related to tracking other satellites among others. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 8, 07:27 | 6872 | 0.0015 | 483 | 504 | 94.49 | 60.02 | 317 | | | | |
in space
|
| ?U Cubesat - one of a simultaneously-launched pair from the United States Army Space and Missile Defense Command carrying a collection of sensors/instruments related to tactical space warfare. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 8, 04:17 | 6871 | 0.0016 | 481 | 504 | 94.46 | 60.03 | 323 | | | | |
in space
|
| 16U Cubesat carrying a collection of sensors/instruments related to tactical space warfare. One of a simultaneously-launched pair. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 8, 04:17 | 6869 | 0.0017 | 480 | 503 | 94.43 | 60.02 | 330 | | | | AGS 6 (Aggiesat 6) 2026-074H 68634 |
in space
|
| 6U Cubesat used as a demonstrator mission from the Texas A&M University to demonstrate detection and orbit determination of other satellites by using their radio transmissions, in this case - any of the Iridium satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 8, 04:17 | 6868 | 0.0018 | 478 | 502 | 94.41 | 60.02 | 334 | | | | |
in space
|
| 4U Cubesat from the University of Colorado carrying receivers to detect VLF radio transmissions coming from the ground such as the effect of lightning or VLF radio transmitters. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 8, 04:18 | 6872 | 0.0018 | 482 | 506 | 94.50 | 60.02 | 316 | | | | Minotaur fourth stage 2026-074E 68631 |
in space
|
| Launched STP-29A cluster of satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 7, 22:00 | 6872 | 0.0014 | 484 | 504 | 94.49 | 60.02 | 315 | | | |
2026-075 CZ 8 (Y-7)
Hainan Commercial Zone, Wenchang Space Centre | 2026 Apr 7, 13:32 UTC | Qianfan Ji Gui 04-01 (Qianfan 109) 2026-075A 68636 |
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
( ° ) | | |
| 2026 Apr 15, 16:20 | 7199 | 0.0014 | 811 | 831 | 101.32 | 88.99 | 187 | | | | 2026 Apr 16, 05:51 | 7199 | 0.0014 | 811 | 832 | 101.32 | 88.99 | 185 | | | | 2026 Jun 17, 14:06 | 7447 | 0.0002 | 1067 | 1070 | 106.59 | 88.99 | 103 | | | | CZ 8 third stage 2026-075U 68654 |
in space
|
| Launched Qianfan Ji Gui group 4. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 15, 14:21 | 7137 | 0.0074 | 706 | 811 | 100.00 | 88.99 | 94 | | | | 2026 Apr 16, 05:21 | 7137 | 0.0074 | 706 | 811 | 100.00 | 88.99 | 91 | | | |
2026-076 CZ 6A
Taiyuan Space Centre | 2026 Apr 8, 19:38 UTC | Hulianwang Digui 21-01 (Satellite Low Orbit Internet Group 21-01) 2026-076A 68656 |
in space
|
One of five 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
( ° ) | | |
| 2026 Apr 9, 00:15 | 7332 | 0.0008 | 948 | 959 | 104.13 | 86.50 | 206 | | | | Hulianwang Digui 21-02 (Satellite Low Orbit Internet Group 21-02) 2026-076B 68657 |
in space
|
| Internet communication satellite. Part of a large constellation. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 9, 00:15 | 7331 | 0.0007 | 948 | 958 | 104.11 | 86.50 | 219 | | | | Hulianwang Digui 21-03 (Satellite Low Orbit Internet Group 21-03) 2026-076C 68658 |
in space
|
| Internet communication satellite. Part of a large constellation. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 9, 01:59 | 7330 | 0.0006 | 948 | 957 | 104.10 | 86.49 | 209 | | | | Hulianwang Digui 21-04 (Satellite Low Orbit Internet Group 21-04) 2026-076D 68659 |
in space
|
| Internet communication satellite. Part of a large constellation. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 9, 01:59 | 7330 | 0.0005 | 948 | 956 | 104.09 | 86.49 | 204 | | | | Hulianwang Digui 21-05 (Satellite Low Orbit Internet Group 21-05) 2026-076E 68660 |
in space
|
| Internet communication satellite. Part of a large constellation. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 9, 01:59 | 7330 | 0.0005 | 947 | 955 | 104.08 | 86.49 | 201 | | | | CZ 6A third stage 2026-076F 68661 |
in space
|
| Launched Hulianwang Digui group 21. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 9, 01:54 | 7240 | 0.0107 | 784 | 939 | 102.17 | 86.50 | 110 | | | |
2026-077 Falcon 9 Block 5 (Starlink Group 17-21)
Vandenberg Space Force Base | 2026 Apr 11, 05:04 UTC | Starlink 67195 2026-077A 68662 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:06 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 24, 12:28 | 6722 | 0.0001 | 343 | 345 | 91.41 | 97.28 | 72 | | | | 2026 Jun 16, 03:39 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.28 | 91 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 11
Life <1 day
|
| Launched Starlink Group 17-021. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-078 Jielong 3
Mobile floating platform, South China Sea near 21°.5 N, 112°.0 E | 2026 Apr 11, 11:32 UTC | Hulianwang Jishu Shiyan 8 (Internet Connectivity Test 8) 2026-078A 68687 |
in space
|
| Second generation test satellite for Chinese government communications system for use by Internet-connected devices. Acts as test/demonstrator platform for a specific component of the system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 12, 04:22 | 7381 | 0.0009 | 996 | 1009 | 105.17 | 86.50 | 287 | | | | Lijian 1 third stage 2026-078C 68690 |
in space
|
| Launched Hulianwang Jishu Shiyan 8. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 11, 22:25 | 7066 | 0.0445 | 373 | 1002 | 98.52 | 86.64 | 25 | | | | unidentified object 2026-078B 68688 |
in space
|
| Probable item of debris, possibly connected with disposal of the Jielong 3 upper stage. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 11, 22:42 | 7198 | 0.0253 | 638 | 1002 | 101.30 | 86.59 | 24 | | | |
2026-079 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2026 Apr 11, 11:41 UTC | Cygnus NG-24 (SS Steven R Nagel) 2026-079A 68689 |
in space
|
| Northrop Grumman Cygnus-XL vehicle carrying supplies and equipment to ISS under CRS-2 contract with NASA. Separated from launch vehicle at 11:56 UTC. Captured by ISS Remote Manipulator Apr 13 at 17:20 UTC. Docked to downward facing port of the ISS unity module later the same day. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 11, 13:07 | 6625 | 0.0006 | 243 | 251 | 89.44 | 51.66 | 290 | | | | 2026 Apr 13, 19:29 | 6798 | 0.0006 | 416 | 424 | 92.97 | 51.63 | 309 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 11
Life <1 day
|
| Launched Cygnus NG 24. Caused to re-enter after releasing spacecraft. |
| Not Catalogued - orbit parameters unavailable | |
2026-080 Lijian 1 (Y-12)
Dongfeng Commercial Zone, Jiuquan Space Centre | 2026 Apr 14, 04:03 UTC | Jilin-1 High Resolution 07A 02 (Jilin-1 GF07B 02) 2026-080xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 549 | 95.40 | 97.66 | 282 | 10:29 | | | Jilin-1 High Resolution 07A 03 (Jilin-1 GF07B 03) 2026-080xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 549 | 95.40 | 97.66 | 282 | 10:29 | | | Jilin-1 High Resolution 07A 04 (Jilin-1 GF07B 04) 2026-080xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 549 | 95.40 | 97.66 | 282 | 10:29 | | | Jilin-1 High Resolution 07B 02 (Jilin-1 GF07B 02) 2026-080xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 549 | 95.40 | 97.66 | 282 | 10:29 | | | Jilin-1 High Resolution 07B 03 (Jilin-1 GF07B 03) 2026-080xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 549 | 95.40 | 97.66 | 282 | 10:29 | | | Jilin-1 High Resolution 07B 04 (Jilin-1 GF07B 04) 2026-080xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 549 | 95.40 | 97.66 | 282 | 10:29 | | | Jilin-1 High Resolution 07C 02 (Jilin-1 GF07C 02) 2026-080xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 549 | 95.40 | 97.66 | 282 | 10:29 | | | Jilin-1 High Resolution 07C 03 (Jilin-1 GF07C 03) 2026-080xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 549 | 95.40 | 97.66 | 282 | 10:29 | | | Jielong 3 fourth stage uncatalogued |
in space
|
| Launched cluster of eight Jilin-1 satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-081 Falcon 9 Block 5 (Starlink Group 10-24)
Cape Canaveral Space Force Station | 2026 Apr 14, 09:33 UTC | |
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 10:34 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 23, 17:13 | 6703 | 0.0002 | 323 | 326 | 91.02 | 53.16 | 41 | | | | 2026 Jun 15, 15:25 | 6841 | 0.0001 | 462 | 463 | 93.85 | 53.16 | 84 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 14
Life <1 day
|
| Launched Starlink Group 10-24. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-082 Falcon 9 Block 5 (Starlink Group 17-27)
Vandenberg Space Force Base | 2026 Apr 15, 04:29 UTC | |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:30 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 25, 22:00 | 6706 | 0.0001 | 327 | 329 | 91.10 | 97.28 | 90 | | | | 2026 Jun 16, 04:11 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.28 | 84 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 15
Life <1 day
|
| Launched Starlink Group 17-27. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-083 Soyuz-2.1b + Volga
Plesetsk Cosmodrome | 2026 Apr 16, 23:19 UTC | Cosmos 2609 2026-083B 68754 |
in space
|
| Military satellite maybe working alongside the other satellites from this launch. Separated from Volga stage April 17 at about 01:05 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 17, 22:59 | 6925 | 0.0009 | 541 | 553 | 95.59 | 98.25 | 259 | 15:08 | | | 2026 Apr 28, 23:36 | 6923 | 0.0010 | 538 | 552 | 95.54 | 98.25 | 232 | 15:12 | | | 2026 May 5, 21:19 | 6923 | 0.0011 | 537 | 552 | 95.54 | 98.12 | 208 | 15:14 | | | 2026 Jul 27, 08:07 | 6928 | 0.0010 | 543 | 556 | 95.64 | 98.13 | 250 | 15:37 | | | Cosmos 2610 2026-083F 68758 |
in space
|
| Suggested by theorists to be part of a co-ordinated interception mission along with the other satellites from this launch. Target suggested as ICEYE X-36 (59103/2024-043F), a radar-imaging satellite rumoured to be used by Ukraine as an aid to identifying battlefield targets. Separated from Volga stage April 17 at about 00:15 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 18, 05:22 | 6925 | 0.0010 | 540 | 554 | 95.58 | 96.95 | 254 | 14:48 | | | 2026 Apr 29, 21:55 | 6926 | 0.0010 | 541 | 554 | 95.60 | 96.96 | 212 | 14:44 | | | 2026 May 15, 15:46 | 6926 | 0.0011 | 540 | 555 | 95.60 | 97.73 | 156 | 14:39 | | | 2026 May 16, 07:43 | 6925 | 0.0011 | 540 | 555 | 95.59 | 97.80 | 156 | 14:39 | | | 2026 Jul 27, 07:41 | 6925 | 0.0009 | 540 | 553 | 95.57 | 97.81 | 279 | 14:47 | | | Cosmos 2611 2026-083G 68759 |
in space
|
| Suggested by theorists to be part of a co-ordinated interception mission along with the other satellites from this launch. Target suggested as ICEYE X-36 (59103/2024-043F), a radar-imaging satellite rumoured to be used by Ukraine as an aid to identifying battlefield targets. Separated from Volga stage April 17 probably about 2 hours after lift-off. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 18, 05:22 | 6925 | 0.0010 | 539 | 554 | 95.58 | 96.95 | 254 | 14:48 | | | 2026 Apr 29, 21:55 | 6926 | 0.0011 | 541 | 556 | 95.62 | 96.95 | 223 | 14:44 | | | 2026 May 20, 09:02 | 6926 | 0.0013 | 540 | 557 | 95.61 | 97.29 | 150 | 14:37 | | | 2026 May 20, 23:23 | 6926 | 0.0012 | 540 | 557 | 95.61 | 97.81 | 147 | 14:37 | | | 2026 Jul 27, 08:07 | 6926 | 0.0010 | 540 | 554 | 95.60 | 97.82 | 286 | 14:45 | | | Cosmos 2612 2026-083H 68762 |
in space
|
| Suggested by theorists to be part of a co-ordinated interception mission along with the other satellites from this launch. Target suggested as ICEYE X-36 (59103/2024-043F), a radar-imaging satellite rumoured to be used by Ukraine as an aid to identifying battlefield targets. Separated from Volga stage April 17 probably about 2 hours after lift-off. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 18, 05:22 | 6924 | 0.0011 | 538 | 554 | 95.57 | 96.95 | 254 | 14:48 | | | 2026 Apr 29, 21:53 | 6924 | 0.0012 | 538 | 554 | 95.57 | 96.96 | 208 | 14:44 | | | 2026 May 16, 04:20 | 6924 | 0.0013 | 536 | 555 | 95.56 | 97.25 | 153 | 14:39 | | | 2026 May 16, 21:52 | 6924 | 0.0014 | 536 | 555 | 95.56 | 97.85 | 151 | 14:39 | | | 2026 Jul 27, 06:56 | 6923 | 0.0011 | 537 | 553 | 95.54 | 97.86 | 274 | 14:48 | | | Cosmos 2613 2026-083J 68763 |
in space
|
| Suggested by theorists to be part of a co-ordinated interception mission along with the other satellites from this launch. Target suggested as ICEYE X-36 (59103/2024-043F), a radar-imaging satellite rumoured to be used by Ukraine as an aid to identifying battlefield targets. Separated from Volga stage April 17 probably about 2 hours after lift-off. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 18, 05:22 | 6924 | 0.0011 | 538 | 554 | 95.57 | 96.95 | 254 | 14:48 | | | 2026 Apr 29, 21:52 | 6922 | 0.0010 | 537 | 551 | 95.53 | 96.96 | 214 | 14:44 | | | 2026 May 14, 07:35 | 6923 | 0.0011 | 537 | 552 | 95.53 | 97.30 | 163 | 14:39 | | | 2026 May 14, 15:33 | 6923 | 0.0010 | 538 | 552 | 95.55 | 97.71 | 156 | 14:39 | | | 2026 May 15, 07:29 | 6922 | 0.0010 | 537 | 552 | 95.53 | 97.78 | 158 | 14:39 | | | 2026 Jul 5, 14:56 | 6922 | 0.0010 | 537 | 550 | 95.52 | 97.78 | 0 | 14:45 | | | 2026 Jul 6, 06:52 | 6928 | 0.0007 | 545 | 555 | 95.64 | 97.79 | 304 | 14:45 | | | 2026 Jul 27, 06:54 | 6928 | 0.0007 | 545 | 554 | 95.64 | 97.78 | 208 | 14:47 | | | Cosmos 2614 2026-083K 68764 |
in space
|
| Suggested by theorists to be part of a co-ordinated interception mission along with the other satellites from this launch. Target suggested as ICEYE X-36 (59103/2024-043F), a radar-imaging satellite rumoured to be used by Ukraine as an aid to identifying battlefield targets. Separated from Volga stage April 17 probably about 2 hours after lift-off. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 18, 05:22 | 6924 | 0.0011 | 538 | 553 | 95.56 | 96.95 | 250 | 14:48 | | | 2026 Apr 29, 21:51 | 6922 | 0.0011 | 536 | 551 | 95.52 | 96.95 | 218 | 14:44 | | | 2026 May 20, 22:49 | 6922 | 0.0013 | 535 | 552 | 95.52 | 96.96 | 146 | 14:37 | | | 2026 May 21, 06:48 | 6925 | 0.0010 | 540 | 553 | 95.58 | 97.29 | 130 | 14:37 | | | 2026 May 21, 22:44 | 6928 | 0.0008 | 544 | 555 | 95.64 | 97.77 | 105 | 14:37 | | | 2026 Jul 27, 07:58 | 6927 | 0.0005 | 545 | 552 | 95.62 | 97.78 | 234 | 14:43 | | | Soyuz third stage 2026-083A 68753 |
in space
|
| Launched cluster of Cosmos satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 17, 22:46 | 6878 | 0.0065 | 455 | 545 | 94.61 | 98.26 | 76 | | | | Volga rocket stage 2026-083D 68756 |
in space
|
| Launched cluster of Cosmos satellites. Separated from Soyuz third stage at about 23:29 UTC. The first orbit listed is an estimate. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 17, 00:01 | 6878 | 0.0065 | 455 | 545 | 94.61 | 98.26 | 76 | 15:08 | | | 2026 Apr 17, 02:16 | 6925 | 0.0011 | 539 | 554 | 95.58 | 96.95 | 265 | 15:08 | | | 2026 Apr 18, 12:51 | 6850 | 0.0013 | 463 | 481 | 94.03 | 96.90 | 267 | 14:51 | | | |
Re-entered - 2026 Apr 18
Life 2 days
|
| Possibly separated from Volga stage during operation of the Soyuz upper stage. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 17, 18:54 | 6691 | 0.0243 | 150 | 476 | 90.79 | 98.25 | 70 | | | | |
Re-entered - 2026 Jul 15
Life 90 days
|
| Possibly separated from Volga stage April 17 at about 00:15 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 17, 00:40 | 6875 | 0.0062 | 454 | 539 | 94.55 | 98.25 | 80 | | | |
2026-084 CZ 4C
Jiuquan Space Centre | 2026 Apr 17, 04:10 UTC | Daqi 2 (Atmosphere Environment Monitoring Satellite) 2026-084A 68760 |
in space
|
| Environment Monitoring satellite equipped with a cluster of active instrumentation, including a LIDAR, to monitor the build-up of aerosols, dust and polluting gases relating to climate change, such as carbon dioxide, in the Earth's atmosphere. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 17, 23:19 | 7064 | 0.0005 | 682 | 689 | 98.47 | 98.29 | 243 | 10:25 | | | 2026 Apr 18, 07:32 | 7065 | 0.0004 | 684 | 690 | 98.50 | 98.29 | 240 | 10:25 | | | 2026 Apr 21, 22:46 | 7079 | 0.0001 | 701 | 701 | 98.79 | 98.29 | 291 | 10:25 | | | CZ 4C third stage 2026-084B 68761 |
in space
|
| Launched Daqi 2. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 18, 07:04 | 6981 | 0.0124 | 516 | 689 | 96.74 | 98.29 | 41 | | | |
2026-085 New Glenn (NG-3)
Cape Canaveral Space Force Station | 2026 Apr 19, 11:25 UTC | BlueBird 7 (SpaceMobile 007) 2026-085A 68765 |
Re-entered - 2026 Apr 20
Life 1 day
|
| Commercial 5G broadband satellite from US company AST Spacemobile to provide direct mobile phone services from orbit. The launch vehicle failed to fire properly for a second time in order to circularise the orbit at 500 km. The satellite separated from the launch vehicle about 1.5 hrs after launch but was left in an unusable orbit with very low perigee. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 19, 11:38 | 6702 | 0.0253 | 154 | 494 | 91.01 | 36.11 | 160 | | | | New Glenn second stage uncatalogued |
Re-entered - 2026 Apr 19
Life <1 day
|
| Launched BlueBird 7. Reached orbit but apparently re-entered (either deliberately or through natural orbit decay) and probably on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2026-086 Falcon 9 Block 5 (Starlink Group 17-22)
Vandenberg Space Force Base | 2026 Apr 19, 16:03 UTC | |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 17:04 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 27, 13:35 | 6669 | 0.0002 | 289 | 292 | 90.33 | 97.28 | 345 | | | | 2026 Jun 16, 04:00 | 6844 | 0.0001 | 464 | 466 | 93.91 | 97.28 | 106 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 19
Life <1 day
|
| Launched Starlink Group 17-22. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-087 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2026 Apr 21, 06:53 UTC | USA 585 (GPS IIIA SV10) 2026-087A 68791 |
in space
|
| Block 3 GPS Navsat - final launch in series. Separated from launch vehicle at 08:22 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 22, 08:11 | 16672 | 0.5942 | 387 | 20201 | 357.07 | 55.00 | 270 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 21
Life <1 day
|
| Launched USA 585. Caused to re-enter above the Indian Ocean near South Africa about five and a half hours after lift off, after releasing satellite. |
| Not Catalogued - orbit parameters unavailable | |
2026-088 Electron (Kakushin Rising)
Rocket Lab Launch Complex, New Zealand | 2026 Apr 23, 03:09 UTC | |
in space
|
| 1U Cubesat from the Future Science institute, Japan to demonstrate a multi-spectral imager and associated data processing system before transmitting data to Earth. Replacement for predecessor lost in launch failure 2022-F05. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 23, 08:37 | 6925 | 0.0013 | 538 | 556 | 95.59 | 97.50 | 296 | 15:30 | | | 2026 Jul 9, 06:21 | 6923 | 0.0015 | 535 | 556 | 95.55 | 97.51 | 38 | 15:27 | | | |
in space
|
| 2U Cubesat from Japan's National Institute of Technology (KOSEN) for marine studies including sub-sea crustal deformation. Also carries demonstrator of a multi-point communications system. Replacement for predecessor lost in launch failure 2022-F05. 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 | |
| 2026 Apr 23, 08:37 | 6925 | 0.0014 | 536 | 556 | 95.58 | 97.50 | 294 | 15:30 | | | 2026 Jul 8, 22:06 | 6923 | 0.0016 | 534 | 556 | 95.54 | 97.51 | 34 | 15:27 | | | PRELUDE (Precursory electric field observation CubeSat Demonstrator) 2026-088C 68794 |
in space
|
| 6U Cubesat equipped with a VLF radio receiver to study electromagnetic emissions from earthquakes. 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 | |
| 2026 Apr 23, 08:37 | 6924 | 0.0012 | 538 | 554 | 95.56 | 97.50 | 286 | 15:30 | | | 2026 Jul 8, 15:28 | 6922 | 0.0013 | 535 | 553 | 95.53 | 97.51 | 29 | 15:27 | | | OrigamiSat 2 2026-088D 68795 |
in space
|
| 3U Cubesat built as a demonstrator for a “multifunctional” membrane panel about 1.5m square and deployed from a 1m mast . Thin-film devices attached throughout the membrane will demonstrate designs for low-mass array aerials and solar arrays. The structure acts as an air brake resulting in more rapid orbit decay and a shorter orbit life compared with other satellites from the launch. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 23, 08:37 | 6921 | 0.0014 | 533 | 553 | 95.50 | 97.50 | 267 | 15:30 | | | 2026 Jul 8, 21:53 | 6917 | 0.0015 | 528 | 549 | 95.41 | 97.51 | 9 | 15:27 | | | ARICA 2 (AGU Remote Innovative Cubesat Alert system) 2026-088E 68796 |
in space
|
| 2U Cubesat from Aoyama Gakuin University, Japan. Equipped with a radio system capable of relaying data via other satellites, such as Globalstar and Iridium, of alerts from its onboard gamma-ray burst detector. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 23, 08:36 | 6921 | 0.0015 | 532 | 553 | 95.49 | 97.50 | 267 | 15:30 | | | 2026 Jul 8, 22:02 | 6919 | 0.0016 | 530 | 551 | 95.45 | 97.51 | 10 | 15:27 | | | WasedaSat Zero 2 2026-088F 68797 |
in space
|
| 1U Cubesat from Waseda University, Japan to demonstrate a satellite chassis created in one piece by 3D printing. It was intended to unfold and deploy a membrane panel. Replacement for predecessor lost in launch failure 2022-F05. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 23, 08:36 | 6921 | 0.0015 | 532 | 553 | 95.49 | 97.49 | 266 | 15:30 | | | 2026 Jul 8, 15:29 | 6918 | 0.0015 | 529 | 550 | 95.43 | 97.51 | 10 | 15:27 | | | MAGNARO 2 (MAGnetically separating NAno-satellite with Rotation for Orbit control) 2026-088G 68798 |
in space
|
| 3U Cubesat from Nagoyo University, Japan. Consists of two satellites, Magnaro-Tigris (2U) and Magnaro-Piscis (1U), joined magnetically. They are expected to separate 6-12 months after launch and conduct formation manoeuvres using air resistance to control the distance between them. Replacement for predecessor lost in launch failure 2022-F05. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 23, 08:36 | 6919 | 0.0018 | 529 | 554 | 95.47 | 97.50 | 276 | 15:30 | | | 2026 Jul 7, 23:18 | 6918 | 0.0019 | 526 | 553 | 95.43 | 97.51 | 14 | 15:28 | | | |
in space
|
| 3U Cubesat to demonstrate an intelligent monitoring system for satellite and spacecraft batteries. 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 | |
| 2026 Apr 23, 08:36 | 6919 | 0.0018 | 529 | 554 | 95.47 | 97.50 | 271 | 15:30 | | | 2026 Jul 9, 05:31 | 6917 | 0.0019 | 526 | 553 | 95.43 | 97.51 | 10 | 15:27 | | | Electron second stage 2026-089J 68800 |
Re-entered - 2026 May 4
Life 11 days
|
| Launched group of eight Japanese satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 23, 08:25 | 6743 | 0.0279 | 177 | 552 | 91.84 | 97.50 | 212 | | | | Electron third stage (kick stage) 2026-089K 68801 |
Re-entered - 2026 May 12
Life 19 days
|
| Launched group of eight Japanese satellites. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 23, 08:26 | 6751 | 0.0267 | 193 | 553 | 92.01 | 97.50 | 265 | | | |
2026-089 Falcon 9 Block 5 (Starlink Group 17-14)
Vandenberg Space Force Base | 2026 Apr 23, 03:23 UTC | Starlink 37471 2026-089A 68802 |
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 04:24 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 27, 14:28 | 6649 | 0.0001 | 270 | 271 | 89.92 | 97.29 | 96 | | | | 2026 Jun 16, 04:00 | 6820 | 0.0002 | 441 | 443 | 93.42 | 97.29 | 93 | | | |
2026-090 Angara 1.2
Plesetsk Cosmodrome | 2026 Apr 23, 08:29 UTC | Cosmos 2615 2026-090A 68826 |
in space
|
| Small military/government satellite, possibly for optical imaging, but precise mission not known. One of four similar satellites similar carried on the same launch. Orbit lowered gradually and expected to reach about 285 km where orbit height will be maintained and tightly controlled by use of a thruster system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 24, 17:42 | 6708 | 0.0012 | 322 | 338 | 91.13 | 96.65 | 244 | 00:06 | | | 2026 May 31, 07:41 | 6700 | 0.0018 | 309 | 333 | 90.96 | 96.65 | 102 | 00:03 | | | Cosmos 2616 2026-090B 68827 |
in space
|
| Small military/government satellite, possibly for optical imaging, but precise mission not known. One of four similar satellites similar carried on the same launch. Orbit lowered gradually and expected to reach about 285 km where orbit height will be maintained and tightly controlled by use of a thruster system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 24, 16:11 | 6708 | 0.0012 | 322 | 338 | 91.13 | 96.65 | 244 | 00:06 | | | 2026 May 31, 12:11 | 6703 | 0.0018 | 313 | 337 | 91.02 | 96.65 | 102 | 00:03 | | | Cosmos 2617 2026-090C 68828 |
in space
|
| Small military/government satellite, possibly for optical imaging, but precise mission not known. One of four similar satellites similar carried on the same launch. Orbit lowered gradually and expected to reach about 285 km where orbit height will be maintained and tightly controlled by use of a thruster system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 24, 17:42 | 6708 | 0.0012 | 322 | 338 | 91.12 | 96.65 | 243 | 00:06 | | | 2026 May 31, 18:14 | 6703 | 0.0019 | 312 | 338 | 91.03 | 96.65 | 102 | 00:03 | | | Cosmos 2618 2026-090D 68829 |
in space
|
| Small military/government satellite, possibly for optical imaging, but precise mission not known. One of four similar satellites similar carried on the same launch. Orbit lowered gradually and expected to reach about 285 km where orbit height will be maintained and tightly controlled by use of a thruster system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Apr 24, 17:42 | 6708 | 0.0013 | 321 | 338 | 91.12 | 96.65 | 241 | 00:06 | | | 2026 May 31, 18:05 | 6701 | 0.0018 | 311 | 335 | 90.99 | 96.65 | 104 | 00:03 | | | Angara 1.2 second stage uncatalogued |
Re-entered - 2026 Apr 23
Life <1 day
|
| Launched Cosmos 2615 - 2618. Caused to re-enter after releasing them. |
| Not Catalogued - orbit parameters unavailable | |
2026-091 CZ 2D
Xichang Space Centre | 2026 Apr 24, 06:35 UTC | Hulianwang Jishu Shiyan 9-01 (Internet Connectivity Test 9-01) 2026-091A 68831 |
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. Individual satellites are built by a variety of manufacturers and act as test/demonstrator platforms for specific components of the system. Orbit maintained by period use of thruster. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 24, 15:30 | 6885 | 0.0009 | 501 | 513 | 94.77 | 55.00 | 278 | | | | Hulianwang Jishu Shiyan 9-02 (Internet Connectivity Test 9-02) 2026-091B 68832 |
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. Individual satellites are built by a variety of manufacturers and act as test/demonstrator platforms for specific components of the system. Orbit maintained by period use of thruster. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 24, 15:30 | 6886 | 0.0009 | 502 | 514 | 94.78 | 55.00 | 270 | | | | Hulianwang Jishu Shiyan 9-03 (Internet Connectivity Test 9-03) 2026-091C 68833 |
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. Individual satellites are built by a variety of manufacturers and act as test/demonstrator platforms for specific components of the system. Orbit maintained by period use of thruster. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 24, 15:30 | 6885 | 0.0009 | 501 | 512 | 94.75 | 55.00 | 285 | | | | Hulianwang Jishu Shiyan 9-04 (Internet Connectivity Test 9-04) 2026-091D 68834 |
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. Individual satellites are built by a variety of manufacturers and act as test/demonstrator platforms for specific components of the system. Orbit maintained by period use of thruster. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 24, 15:30 | 6884 | 0.0009 | 500 | 512 | 94.73 | 55.00 | 294 | | | | CZ 2D second stage uncatalogued |
Re-entered - 2026 Apr 24
Life <1 day
|
| Launched Hulianwang Jishu Shiyan 9 satellite group. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-092 CZ 6
Taiyuan Space Centre | 2026 Apr 25, 12:15 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. Working together with PRSC-EO 1 (62727, 2025-012C) and PRCS-EO 2 (67752, 2025-027G). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 25, 21:25 | 6926 | 0.0005 | 544 | 551 | 95.60 | 38.00 | 322 | | | |
2026-093 Soyuz-2.1a
Baikonur Cosmodrome | 2026 Apr 25, 22:21 UTC | Progress MS-34 (Progress 7K-MS №464) 2026-093A 68837 |
in space
|
| Supplies to ISS. Initial orbit similar to launch vehicle upper stage. Docked with rearward-facing port of ISS Zarya module April 28 at 00:00:45 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 26, 05:38 | 6706 | 0.0010 | 321 | 334 | 91.08 | 51.63 | 15 | | | | 2026 Apr 28, 04:47 | 6798 | 0.0007 | 415 | 424 | 92.96 | 51.63 | 359 | | | | Soyuz third stage 2026-093B 68838 |
Re-entered - 2026 Apr 27
Life 2 days
|
| Launched Progress MS-34. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 26, 05:32 | 6579 | 0.0025 | 184 | 217 | 88.50 | 51.65 | 87 | | | |
2026-094 Falcon 9 Block 5 (Starlink Group 17-16)
Vandenberg Space Force Base | 2026 Apr 26, 14:37 UTC | Starlink 37475 2026-094A 68839 |
in space
|
One member of a simultaneously-launched cluster of twenty five broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:38 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Apr 30, 16:00 | 6639 | 0.0001 | 260 | 262 | 89.73 | 97.28 | 84 | | | | 2026 Jun 15, 23:45 | 6844 | 0.0001 | 465 | 467 | 93.91 | 97.28 | 93 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 26
Life <1 day
|
| Launched Starlink Group 17-16. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-095 Atlas V 551 (KA-04, Amazon LEO 06)
Cape Canaveral Space Force Station | 2026 Apr 28, 00:52 UTC | Amazon LEO 00299 (Kuiper 00299) 2026-095A 68864 |
in space
|
One member of a simultaneously-launched cluster of twenty nine 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
( ° ) | | |
| 2026 Apr 30, 16:00 | 6835 | 0.0009 | 451 | 463 | 93.73 | 51.87 | 126 | | | | Atlas V third stage (Centaur) uncatalogued |
Re-entered - 2026 Apr 28
Life <1 day
|
| Launched twenty nine Kuiper satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-096 Falcon 9 Heavy
Kennedy Space Center | 2026 Apr 28, 14:16 UTC | Viasat 3 F3 (Viasat 3 APAC) 2026-096A 68893 |
in space
|
| Commercial comsat for the aviation industry, government and private consumers. Planned to provide broadband services to the Asia Pacific region. Orbit raising via near-continuous electric thrust that commenced operation May 10. Expected location near 157° east. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 May 4, 07:54 | 34461 | 0.1470 | 23016 | 33150 | 1061.10 | 2.71 | 180 | | | | 2026 May 9, 19:38 | 34461 | 0.1470 | 23016 | 33151 | 1061.10 | 2.70 | 180 | | | | 2026 May 15, 12:24 | 34852 | 0.1435 | 23472 | 33476 | 1079.21 | 2.61 | 180 | | | | 2026 May 22, 12:09 | 36194 | 0.1282 | 25177 | 34456 | 1142.15 | 2.34 | 181 | | | | 2026 May 30, 02:43 | 37283 | 0.0975 | 27268 | 34541 | 1194.04 | 1.70 | 181 | | | | 2026 Jun 8, 13:29 | 38877 | 0.0752 | 29577 | 35421 | 1271.46 | 1.47 | 190 | | | | 2026 Jun 10, 12:02 | 39625 | 0.0853 | 29866 | 36627 | 1308.31 | 1.45 | 181 | | | | 2026 Jun 13, 00:13 | 39625 | 0.0853 | 29867 | 36628 | 1308.33 | 1.45 | 181 | | | | 2026 Jun 22, 04:24 | 40940 | 0.0373 | 33037 | 36088 | 1374.00 | 0.87 | 182 | | | | 2026 Jun 30, 13:54 | 41903 | 0.0023 | 35431 | 35620 | 1422.76 | 0.38 | 146 | | | | 2026 Jul 3, 13:19 | 41982 | 0.0023 | 35506 | 35702 | 1426.78 | 0.29 | 134 | | | | 2026 Jul 5, 19:43 | 42163 | 0.0006 | 35762 | 35809 | 1436.03 | 0.17 | 170 | 158°.5 E | | | Falcon 9 third stage 2026-096B 68894 |
in space
|
| Launched Viasat 3 F3. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 5, 00:00 | 34426 | 0.1483 | 22941 | 33154 | 1059.45 | 2.71 | 180 | | | |
2026-097 Falcon 9 Block 5 (Starlink Group 17-36)
Vandenberg Space Force Base | 2026 Apr 30, 02:32 UTC | Starlink 37527 2026-097A 68895 |
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 03:33 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 4, 18:00 | 6661 | 0.0002 | 282 | 284 | 90.17 | 97.29 | 94 | | | | 2026 Jun 16, 02:17 | 6844 | 0.0001 | 465 | 466 | 93.91 | 97.28 | 98 | | | |
2026-098 Ariane 64 (VA-268, Amazon LEO 02)
Centre Spatiale Guyanaise | 2026 Apr 30, 08:57 UTC | Amazon LEO 00370 (Kuiper 00370) 2026-098A 68919 |
in space
|
One member of a simultaneously-launched cluster of thirty two broadband and mobile telephone communications satellites from US company Amazon. Released from the launch vehicle in ten groups of three and one pair over a period of ~25 minutes beginning at 10:26 UTC.
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
( ° ) | | |
| 2026 May 5, 06:00 | 6845 | 0.0015 | 456 | 477 | 93.93 | 51.88 | 0 | | | | Ariane 6 third stage uncatalogued |
Re-entered - 2026 Feb 12
Life <1 day
|
| Launched cluster of Kuiper satellites. Retro-fire at 11:39 UTC, after releasing satellites, led to re-entry above the Indian Ocean at about 12:20 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2026-099 Falcon 9 Block 5 (Starlink Group 10-38)
Cape Canaveral Space Force Station | 2026 May 1, 18:06 UTC | Starlink 37258 2026-099A 68951 |
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 19:06 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 12, 20:00 | 6706 | 0.0001 | 327 | 329 | 91.09 | 53.16 | 87 | | | | 2026 Jun 16, 04:23 | 6841 | 0.0001 | 462 | 463 | 93.85 | 53.16 | 64 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Apr 23
Life <1 day
|
| Launched Starlink Group 10-38. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-100 Falcon 9 Block 5 (CAS500-2 Rideshare)
Vandenberg Space Force Base | 2026 May 4, 06:59 UTC | PEARL-1B (Propagation Experiment using kurz-Above-band Radio in LEO) 2026-100A 68980 |
in space
|
| 8U Cubesat carrying space technology experiments. Will fly in tandem with PEARL 1A, also carried on this launch. Separated from launch vehicle at L+143 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 12:02 | 6975 | 0.0006 | 593 | 601 | 96.62 | 97.74 | 282 | 22:41 | | | IRIDE-MS2 Hawk for Earth Observation 7 2026-100B 68981 |
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. Separated from launch vehicle at L+145 minutes.. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:59 | 6973 | 0.0003 | 593 | 597 | 96.58 | 97.74 | 286 | 22:41 | | | IRIDE-MS2 Hawk for Earth Observation 10 2026-100C 68982 |
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. Separated from launch vehicle at L+145 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:59 | 6972 | 0.0002 | 593 | 596 | 96.57 | 97.74 | 304 | 22:41 | | | IRIDE-MS2 Hawk for Earth Observation 11 2026-100D 68983 |
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. Separated from launch vehicle at L+150 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:58 | 6972 | 0.0002 | 593 | 595 | 96.56 | 97.74 | 281 | 22:41 | | | IRIDE-MS2 Hawk for Earth Observation 12 2026-100E 68984 |
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. Separated from launch vehicle at L+145 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:59 | 6973 | 0.0003 | 593 | 597 | 96.58 | 97.74 | 298 | 22:41 | | | IRIDE-MS2 Hawk for Earth Observation 13 2026-100F 68985 |
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. Separated from launch vehicle at L+145 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:56 | 6971 | 0.0001 | 592 | 593 | 96.54 | 97.74 | 227 | 22:41 | | | IRIDE-MS2 Hawk for Earth Observation 14 2026-100G 68986 |
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. Separated from launch vehicle at L+145 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:56 | 6971 | 0.0000 | 592 | 593 | 96.53 | 97.74 | 171 | 22:41 | | | IRIDE-MS2 Hawk for Earth Observation 15 2026-100H 68987 |
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. Separated from launch vehicle at L+149 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| Forest 17 (Telperion) 2026-100J 68988 |
in space
|
| 8U Cubesat from German company Oratech. Equipped with thermal imaging sensors to detect and observe wildfires across Greece. One of four similar satellites carried on this launch. Separated from launch vehicle at L+142 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| PEARL-1A (Propagation Experiment using kurz-Above-band Radio in LEO) 2026-100L 68990 |
in space
|
| 8U Cubesat carrying space technology experiments. Will fly in tandem with PEARL 1B, also carried on this launch. Separated from launch vehicle at L+144 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 12:00 | 6973 | 0.0004 | 593 | 598 | 96.59 | 97.73 | 308 | 22:41 | | | Earth Daily 2 2026-100M 68991 |
in space
|
| Small satellite built by Loft for Earth Daily Analytics. Equipped with an Earth imaging system controlled by onboard artificial intelligence to detect and study natural events. Separated from launch vehicle at L+149 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:58 | 6972 | 0.0002 | 593 | 596 | 96.57 | 97.74 | 290 | 22:41 | | | Earth Daily 7 2026-100N 68992 |
in space
|
| Small satellite built by Loft for Earth Daily Analytics. Equipped with an Earth imaging system controlled by onboard artificial intelligence to detect and study natural events. Separated from launch vehicle at L+151 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:58 | 6972 | 0.0002 | 593 | 595 | 96.56 | 97.74 | 285 | 22:41 | | | Earth Daily 4 2026-100P 68993 |
in space
|
| Small satellite built by Loft for Earth Daily Analytics. Equipped with an Earth imaging system controlled by onboard artificial intelligence to detect and study natural events. Separated from launch vehicle at L+150 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:57 | 6972 | 0.0001 | 593 | 594 | 96.55 | 97.74 | 272 | 22:41 | | | |
in space
|
| Small satellite from NuSpace of Singapore. Carrying test equipment for an internet-connected messaging relay system. One of two similar satellites carried on this launch. Separated from launch vehicle at L+143 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:53 | 6969 | 0.0003 | 589 | 593 | 96.49 | 97.74 | 85 | 22:41 | | | |
in space
|
| Small satellite fitted with a synthetic aperture radar for Earth surface imaging. Separated from launch vehicle at L+146 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:57 | 6971 | 0.0001 | 592 | 594 | 96.54 | 97.74 | 251 | 22:41 | | | |
in space
|
| Small satellite fitted with a synthetic aperture radar for Earth surface imaging. Separated from launch vehicle at L+146 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:59 | 6973 | 0.0003 | 593 | 596 | 96.57 | 97.74 | 288 | 22:41 | | | Earth Daily 6 2026-100T 68997 |
in space
|
| Small satellite built by Loft for Earth Daily Analytics. Equipped with an Earth imaging system controlled by onboard artificial intelligence to detect and study natural events. Separated from launch vehicle at L+146 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:57 | 6971 | 0.0001 | 593 | 594 | 96.55 | 97.74 | 266 | 22:41 | | | Forest 16 (Sowitasghot) 2026-100U 68998 |
in space
|
| 8U Cubesat from German company Oratech. Equipped with thermal imaging sensors to detect and observe wildfires across Greece. One of four similar satellites carried on this launch. Separated from launch vehicle at L+145 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:55 | 6970 | 0.0001 | 591 | 593 | 96.52 | 97.74 | 159 | 22:41 | | | Forest 18 (Mangoshrikhand) 2026-100V 68999 |
in space
|
| 8U Cubesat from German company Oratech. Equipped with thermal imaging sensors to detect and observe wildfires across Greece. One of four similar satellites carried on this launch. Separated from launch vehicle at L+144 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 05:28 | 6970 | 0.0002 | 591 | 593 | 96.52 | 97.74 | 74 | 22:41 | | | Gemini-Pollux 2026-100W 69000 |
in space
|
| Mission details to follow. Separated from launch vehicle at L+142 minutes. Catalogue Number and designation identified by Nico Janssen via radio tracking. |
| Orbit parameters awaited | | Forest 19 (Patadastra) 2026-100X 69001 |
in space
|
| 8U Cubesat from German company Oratech. Equipped with thermal imaging sensors to detect and observe wildfires across Greece. One of four similar satellites carried on this launch. Separated from launch vehicle at L+144 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:54 | 6969 | 0.0002 | 590 | 593 | 96.51 | 97.74 | 124 | 22:41 | | | |
in space
|
| Small satellite from NuSpace of Singapore. Carrying test equipment for an internet-connected messaging relay system. One of two similar satellites carried on this launch. Separated from launch vehicle at L+143 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 10:16 | 6968 | 0.0003 | 588 | 593 | 96.48 | 97.74 | 102 | 22:41 | | | Earth Daily 3 2026-100Z 69003 |
in space
|
| Small satellite built by Loft for Earth Daily Analytics. Equipped with an Earth imaging system controlled by onboard artificial intelligence to detect and study natural events. Separated from launch vehicle at L+149 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 10:20 | 6971 | 0.0001 | 593 | 594 | 96.55 | 97.74 | 297 | 22:41 | | | Lynk Tower 7 (GEN 1A) 2026-100AA 69004 |
in space
|
| Small satellite from Lynk Global providing two-way connectivity for broadband, voice, and text messaging globally. Separated from launch vehicle at L+79 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:14 | 6884 | 0.0005 | 503 | 510 | 94.75 | 97.41 | 131 | 22:42 | | | Lynk Tower 8 (GEN 1B) 2026-100AB 69005 |
in space
|
| Small satellite from Lynk Global providing two-way connectivity for broadband, voice, and text messaging globally. Separated from launch vehicle at L+80 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:14 | 6884 | 0.0005 | 502 | 510 | 94.74 | 97.41 | 135 | 22:42 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+79 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:13 | 6884 | 0.0006 | 501 | 510 | 94.73 | 97.41 | 142 | 22:42 | | | BRO 21 (Breizh Reconnaissance Orbiter 21) 2026-100AD 69007 |
in space
|
| 8U Cubesat from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Separated from launch vehicle at L+77 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:13 | 6884 | 0.0006 | 502 | 509 | 94.73 | 97.41 | 143 | 22:42 | | | Earth Daily 5 2026-100AE 69008 |
in space
|
| Small satellite built by Loft for Earth Daily Analytics. Equipped with an Earth imaging system controlled by onboard artificial intelligence to detect and study natural events. Separated from launch vehicle at L+146 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:58 | 6972 | 0.0002 | 593 | 596 | 96.57 | 97.74 | 296 | 22:41 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+82 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:12 | 6883 | 0.0006 | 501 | 509 | 94.72 | 97.41 | 150 | 22:42 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+81 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:12 | 6883 | 0.0005 | 501 | 508 | 94.72 | 97.41 | 153 | 22:42 | | | Jackal 0004 (Mission X-3) 2026-100AJ 69014 |
in space
|
| Satellite from US company True Anomaly, intended to conduct joint manoeuvring and rendezvous operations, reportedly together with Victus Haze Puma (69646/2026-142A) launched 2026 June 19. Separated from launch vehicle at L+81 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:09 | 6881 | 0.0006 | 499 | 507 | 94.68 | 97.41 | 178 | 22:42 | | | CAS500 2 (Compact Advanced Satellite 500-2) 2026-100AK 69013 |
in space
|
| Satellite from the Korea Aerospace Reseach Institute equipped with an optical imaging system for Earth observation to support investigation of natural resources and monitoring of the environment within South Korea. Separated from launch vehicle at L+60 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:12 | 6883 | 0.0008 | 499 | 511 | 94.72 | 97.41 | 147 | 22:42 | | | FrontierSat 2026-100AM 69015 |
in space
|
| 3U Cubesat from the University of Calgary, Canada to study charged particles and plasma in LEO. Separated from launch vehicle at L+77 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:09 | 6881 | 0.0009 | 497 | 509 | 94.67 | 97.40 | 169 | 22:42 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+77 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 9, 02:55 | 6881 | 0.0008 | 497 | 508 | 94.67 | 97.41 | 174 | 22:42 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+81 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 9, 04:00 | 6884 | 0.0006 | 502 | 509 | 94.73 | 97.41 | 144 | 22:42 | | | Pelican-8 (Edda 1 300F) 2026-100AQ 69018 |
in space
|
| Mission details to follow. Separated from launch vehicle at L+80 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 9, 04:00 | 6884 | 0.0006 | 502 | 509 | 94.73 | 97.41 | 142 | 22:42 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+81 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 9, 04:00 | 6883 | 0.0006 | 501 | 509 | 94.72 | 97.41 | 148 | 22:42 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+77 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 9, 04:40 | 6886 | 0.0006 | 503 | 512 | 94.77 | 97.41 | 109 | 22:42 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+77 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 8, 11:16 | 6886 | 0.0006 | 503 | 512 | 94.77 | 97.41 | 117 | 22:42 | | | |
in space
|
| 6U Cubesat from AISTech of Spain equipped with an infrared Earth imaging system to detect and study heat sources on the surface. Separated from launch vehicle at L+78 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 9, 03:04 | 6885 | 0.0007 | 503 | 512 | 94.76 | 97.41 | 119 | 22:42 | | | |
in space
|
| 8U CubeSat from Lithuanian company NanoAvionics. Designed to demonstrate quantum key exchange between a small satellite and a ground station using a laser communication terminal. Separated from launch vehicle at L+77 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 9, 04:38 | 6885 | 0.0005 | 504 | 510 | 94.76 | 97.41 | 116 | 22:42 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+78 minutes |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 9, 04:00 | 6885 | 0.0005 | 504 | 510 | 94.76 | 97.41 | 118 | 22:42 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+79 minutes |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+143 minutes |
| Orbit parameters awaited | | SNAPPY (Solar Neutrino Astro Particle Physics) 2026-100xx |
in space
|
| Mission details to follow. Separated from launch vehicle at L+78 minutes |
| Orbit parameters awaited | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 4
Life <1 day
|
| Launched multiple payloads to SSO. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-101 Falcon 9 Block 5 (Starlink Group 17-29)
Vandenberg Space Force Base | 2026 May 6, 03:59 UTC | Starlink 37592 2026-101A 69025 |
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 05:02 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 12, 20:00 | 6692 | 0.0001 | 313 | 315 | 90.80 | 97.29 | 104 | | | | 2026 Jun 16, 04:10 | 6844 | 0.0002 | 465 | 467 | 93.91 | 97.28 | 76 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 6
Life <1 day
|
| Launched Starlink Group 17-29. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-102 CZ 7 (Y-11)
Wenchang Space Centre | 2026 May 11, 00:14 UTC | Tianzhou 10 2026-102A 69049 |
in space
|
| Supplies to Chinese Space Station. Docked with the aft port of CSS Tianhe module at 05:11 UTC on the day of launch. Initial orbit similar to launch vehicle upper stage. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 11, 11:54 | 6760 | 0.0004 | 379 | 384 | 92.18 | 41.47 | 288 | | | | CZ 7 third stage 2026-102B 69050 |
Re-entered - 2026 May 22
Life 11 days
|
| Launched Tianzhou 10. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 11, 08:40 | 6640 | 0.0094 | 200 | 325 | 89.75 | 41.47 | 175 | | | |
2026-103 Falcon 9 Block 5 (NRO L-172)
Vandenberg Space Force Base | 2026 May 12, 02:13 UTC | USA 586 (Starshield 0171) 2026-103A 69051 |
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.
All satellites were released into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 12, 03:30 | 6671 | 0.0008 | 287 | 298 | 90.37 | 69.99 | 345 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 12
Life <1 day
|
| Launched NRO L-172 mission. |
| Not Catalogued - orbit parameters unavailable | |
2026-104 CZ 6A (Y-23)
Taiyuan Space Centre | 2026 May 12, 11:59 UTC | Qianfan Ji Gui 09-01 (Qianfan 127) 2026-104A 69073 |
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
( ° ) | | |
| 2026 May 18, 13:52 | 7202 | 0.0011 | 816 | 832 | 101.38 | 88.99 | 164 | | | | 2026 Jun 17, 06:34 | 7264 | 0.0006 | 881 | 890 | 102.68 | 88.99 | 75 | | | | CZ 6A third stage 2026-104U 69091 |
in space
|
| Launched Qianfan Ji Gui Group 9. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 18, 14:04 | 7096 | 0.0100 | 647 | 789 | 99.15 | 89.01 | 87 | | | |
2026-105 Zhuque 2E (Y-5)
Dongfeng Commercial Zone, Jiuquan Space Centre | 2026 May 14, 03:00 UTC | Zhuque 2 second stage 2026-105A 69095 |
in space
|
| Combined second stage and satellite mass simulator carried on first flight on new launch vehicle version. Mission was reported as complete success and was completed after about 29 minutes when the launch vehicle sent a separation command to simulate release of the dummy satellite. The stage then initiated an engine firing to lower perigee. The first orbit listed is an estimate. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 14, 03:31 | 7278 | 0.0001 | 899 | 901 | 102.99 | 88.98 | 150 | | | | 2026 May 14, 23:14 | 6929 | 0.0500 | 205 | 897 | 95.67 | 88.98 | 64 | | | | |
Re-entered - 2026 May 17
Life 3 days
|
| Low density item of debris in a quickly decaying orbit that separated from the rocket stage after its perigee-lowering engine firing. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 14, 10:28 | 6919 | 0.0479 | 209 | 872 | 95.46 | 88.98 | 66 | | | | 2026 May 16, 14:13 | 6756 | 0.0274 | 193 | 563 | 92.10 | 88.96 | 59 | | | |
2026-106 Lijian 1 (Y-13)
Dongfeng Commercial Zone, Jiuquan Space Centre | 2026 May 15, 04:33 UTC | Tianyan 27 (Youxi) 2026-106B 69098 |
in space
|
| Demonstrator satellite carrying a selfie camera and equipped with an intelligent data processing system. Also reportedly fitted with an electric thruster than was used to raise the orbit between launch and early-June. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 May 15, 19:54 | 6912 | 0.0013 | 525 | 543 | 95.31 | 97.50 | 280 | 10:59 | | | 2026 May 28, 16:16 | 6912 | 0.0014 | 525 | 543 | 95.32 | 97.51 | 226 | 10:59 | | | 2026 May 30, 12:47 | 6914 | 0.0013 | 527 | 545 | 95.37 | 97.49 | 217 | 10:59 | | | |
in space
|
| Earth observation satellite equipped with a radar imaging system to monitor deformation in the land surface around large-scale engineering structures such as dams, railway embankments and wind farms. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6912 | 0.0013 | 525 | 543 | 95.31 | 97.51 | 274 | 10:59 | | | Jilin-1 High Resolution 03D 55 (Jilin-1 GF03D 55) 2026-106xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6912 | 0.0013 | 525 | 543 | 95.31 | 97.51 | 274 | 10:59 | | | |
in space
|
| Commercial satellite for high-resolution remote sensing using an optical imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6912 | 0.0013 | 525 | 543 | 95.31 | 97.51 | 274 | 10:59 | | | |
in space
|
| Commercial satellite for high-resolution remote sensing using an optical imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6912 | 0.0013 | 525 | 543 | 95.31 | 97.51 | 274 | 10:59 | | | Lijian 1 third stage 2026-106F 69102 |
in space
|
Launched cluster of satellites. Perigee lowered after releasing satellites.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 15, 21:04 | 6793 | 0.0181 | 292 | 538 | 92.87 | 97.51 | 13 | | | |
2026-107 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2026 May 15, 22:05 UTC | SpaceX Dragon 2 CRS-34 2026-107A 69103 |
Re-entered - 2026 Jun 17
Life 33 days
|
| 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 May 17 at 10:37 UTC. Undocked June 16 at 17:25 UTC. Retrofire June 17 at about 11:30 UTC led to splashdown in the Pacific Ocean off California at 12:11 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 16, 02:29 | 6635 | 0.0073 | 208 | 305 | 89.64 | 51.65 | 230 | | | | 2026 May 17, 08:37 | 6797 | 0.0008 | 414 | 424 | 92.95 | 51.63 | 68 | | | | 2026 May 17, 21:00 | 6797 | 0.0008 | 414 | 424 | 92.95 | 51.63 | 70 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 16
Life 1 day
|
| Launched Dragon CRS-34. |
| Not Catalogued - orbit parameters unavailable | |
2026-108 CZ 8 (Y-8)
Hainan Commercial Zone, Wenchang Space Centre | 2026 May 17, 14:42 UTC | Qianfan Ji Gui 10-01 (Qianfan 145) 2026-108A 69104 |
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
( ° ) | | |
| 2026 May 28, 20:05 | 7229 | 0.0017 | 839 | 864 | 101.96 | 89.01 | 166 | | | | 2026 Jun 17, 12:39 | 7263 | 0.0016 | 873 | 897 | 102.68 | 89.01 | 106 | | | | CZ 8 third stage 2026-108U 69122 |
in space
|
| Launched Qianfan Ji Gui Group 10. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 28, 20:21 | 7156 | 0.0067 | 730 | 826 | 100.41 | 89.01 | 81 | | | |
2026-109 Vega-C (VV-29)
Centre Spatiale Guyanaise | 2026 May 19, 03:52 UTC | SMILE (Solar wind Magnetosphere Ionosphere Link
Explorer) 2026-109A 69123 |
in space
|
| Joint mission between the European Space Agency and the Chinese Academy of Sciences. Equipped with an x-ray camera to study the interaction between the solar wind and the Earth’s magnetic field, and an ultraviolet camera to monitor the Aurora Borealis at the same time. Separated from launch vehicle at 04:48 UTC. Reached final science orbit June 20 after eleven firings of its onboard thruster - detailed orbit is based on data provided by the European Space Agency. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 19, 15:24 | 7080 | 0.0010 | 696 | 709 | 98.82 | 70.00 | 267 | | | | 2026 Jun 7, 09:11 | 10985 | 0.3310 | 971 | 8243 | 190.97 | 69.98 | 289 | | | | estimated orbit | 69352 | 0.8355 | 5027 | 120920 | 3029.32 | 70.00 | 287 | | | | Vega fourth stage (AVUM+) uncatalogued |
Re-entered - 2026 May 19
Life <1 day
|
| Launched SMILE. |
| Not Catalogued - orbit parameters unavailable | |
2026-110 Falcon 9 Block 5 (Starlink Group 17-42)
Vandenberg Space Force Base | 2026 May 20, 02:46 UTC | Starlink 37726 2026-110A 69124 |
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 03:47 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 27, 18:00 | 6706 | 0.0001 | 327 | 329 | 91.09 | 97.28 | 107 | | | | 2026 Jun 16, 04:47 | 6797 | 0.0002 | 418 | 420 | 92.95 | 97.28 | 88 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 20
Life <1 day
|
| Launched Starlink Group 17-42. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-111 Falcon 9 Block 5 (Starlink Group 10-31)
Cape Canaveral Space Force Station | 2026 May 21, 10:04 UTC | Starlink 37395 2026-111A 69148 |
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 19:06 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 27, 16:00 | 6652 | 0.0001 | 273 | 275 | 90.00 | 53.16 | 57 | | | | 2026 Jun 16, 04:00 | 6757 | 0.0001 | 378 | 380 | 92.13 | 53.16 | 80 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 21
Life <1 day
|
| Launched Starlink Group 10-31. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-112 Electron (Viva La Strix)
Rocket Lab Launch Complex, New Zealand | 2026 May 22, 09:33 UTC | |
in space
|
| Imaging satellite equipped with a synthetic aperture radar - produced by the University of Tokyo, the Tokyo Institute of Technology, Keio University, Japan Space Systems, and a private company - Synspective Inc of Tokyo. Will become part of a constellation of 25-30 satellites to monitor ground movement and ground changes in urban areas. The name derives from the scientific name for the owl and its sensitivity to low levels of light. Separated from launch vehicle at about 10:32 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 22, 19:42 | 6940 | 0.0027 | 543 | 580 | 95.89 | 44.91 | 268 | | | | 2026 May 26, 03:33 | 6941 | 0.0025 | 546 | 580 | 95.92 | 44.91 | 286 | | | | Electron third stage (kick stage) 2026-112B 69178 |
in space
|
| Launched StriX 7. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 22, 19:42 | 6938 | 0.0028 | 540 | 579 | 95.85 | 44.91 | 269 | | | | Electron second stage 2026-112C 69179 |
Re-entered - 2026 Jun 7
Life 16 days
|
| Launched StriX 7. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 22, 20:52 | 6760 | 0.0286 | 189 | 576 | 92.20 | 44.91 | 260 | | | |
2026-113 CZ 2F
Jiuquan Space Centre | 2026 May 24, 15:08 UTC | Shenzhou 23 2026-113A 69180 |
in space
|
| Crew to CSS - Zhu Yangzhu (commander), Zhang Zhiyan (pilot) and and Li Jiaying (flight engineer). Separated from launch vehicle at 15:17 UTC. Docked with the downward-facing port of the Tianhe module at 18:45 UTC on the day of launch. Initial orbit listed is based on Chinese data. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 24, 15:18 | 6653 | 0.0124 | 193 | 358 | 90.02 | 41.47 | 100 | | | | 2026 May 25, 12:15 | 6766 | 0.0011 | 381 | 396 | 92.32 | 41.47 | 279 | | | | CZ 2F third stage 2026-113B 69181 |
Re-entered - 2026 Jun 7
Life 14 days
|
| Launched Shenzhou 23. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 25, 04:16 | 6649 | 0.0110 | 198 | 344 | 89.93 | 41.47 | 129 | | | |
2026-114 Falcon 9 Block 5 (Starlink Group 10-47)
Cape Canaveral Space Force Station | 2026 May 25, 11:48 UTC | Starlink 37380 2026-114A 69182 |
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 12:49 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 1, 14:00 | 6673 | 0.0001 | 294 | 295 | 90.41 | 53.16 | 63 | | | | 2026 Jun 16, 03:25 | 6714 | 0.0001 | 335 | 336 | 91.25 | 53.16 | 64 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 25
Life <1 day
|
| Launched Starlink Group 10-47. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-115 Falcon 9 Block 5 (Starlink Group 17-37)
Vandenberg Space Force Base | 2026 May 26, 14:50 UTC | Starlink 37613 2026-115A 69211 |
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 15:50 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 1, 14:00 | 6684 | 0.0001 | 305 | 306 | 90.63 | 97.28 | 101 | | | | 2026 Jun 16, 03:56 | 6797 | 0.0001 | 418 | 420 | 92.95 | 97.28 | 92 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 26
Life <1 day
|
| Launched Starlink Group 17-37. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-116 CZ 7A
Wenchang Space Centre | 2026 May 26, 16:16 UTC | Tongxin Jishu Shiyan 24 (Communication Technology Test 24, TJS 24) 2026-116A 69235 |
in space
|
| Chinese government owned satellite described as being primarily used to verify multi-band, high-speed satellite communication technologies. Probably entered GEO drift orbit on the day of launch at around 22:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 May 26, 22:03 | 24396 | 0.7313 | 177 | 35859 | 632.03 | 19.55 | 179 | | | | 2026 Jun 5, 22:30 | 42165 | 0.0001 | 35783 | 35790 | 1436.09 | 0.04 | 174 | 90°.3 E | | | CZ 7A fourth stage 2026-116B 69236 |
in space
|
| Launched Tongxin Jishu Shiyan 24. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 May 26, 21:56 | 23649 | 0.7252 | 120 | 34422 | 603.22 | 19.55 | 178 | | | |
2026-117 Falcon 9 Block 5 (Starlink Group 10-53)
Cape Canaveral Space Force Station | 2026 May 29, 12:57 UTC | Starlink 37665 2026-117A 69238 |
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 12:49 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 1, 14:00 | 6629 | 0.0000 | 250 | 251 | 89.51 | 53.16 | 74 | | | | 2026 Jun 16, 04:06 | 6703 | 0.0001 | 324 | 325 | 91.02 | 53.16 | 44 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 29
Life <1 day
|
| Launched Starlink Group 10-53. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-118 Atlas V 551 (KA-04, Amazon LEO 07)
Cape Canaveral Space Force Station | 2026 May 29, 23:53 UTC | Amazon LEO 00282 (Kuiper 00282) 2026-118A 69267 |
in space
|
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from US company Amazon. Satellites separated from the launch vehicle over a 27 minute period beginning May 30 at 00:20 UTC.
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
( ° ) | | |
| 2026 Jun 3, 14:00 | 6838 | 0.0012 | 452 | 468 | 93.79 | 51.86 | 135 | | | | Atlas V third stage (Centaur) uncatalogued |
Re-entered - 2026 Apr 30
Life <1 day
|
| Launched twenty nine Kuiper satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-119 Falcon 9 Block 5 (Starlink Group 17-41)
Vandenberg Space Force Base | 2026 May 30, 15:25 UTC | Starlink 37501 2026-119A 69296 |
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 16:26 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 3, 14:00 | 6661 | 0.0001 | 282 | 284 | 90.17 | 97.28 | 100 | | | | 2026 Jun 16, 04:00 | 6737 | 0.0002 | 357 | 360 | 91.71 | 97.28 | 73 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 May 30
Life <1 day
|
| Launched Starlink Group 17-41. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-120 CZ 2D (Y-119)
Xichang Space Centre | 2026 May 30, 18:07 UTC | Hulianwang Jishu Shiyan 10-01 (Internet Connectivity Test 10-01) 2026-120A 69320 |
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. Individual satellites are built by a variety of manufacturers and 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
( ° ) | | |
| 2026 Jun 1, 05:26 | 6828 | 0.0009 | 443 | 456 | 93.58 | 55.00 | 274 | | | | Hulianwang Jishu Shiyan 10-02 (Internet Connectivity Test 10-02) 2026-120B 69321 |
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. Individual satellites are built by a variety of manufacturers and 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
( ° ) | | |
| 2026 Jun 1, 05:26 | 6827 | 0.0009 | 443 | 455 | 93.56 | 55.00 | 282 | | | | Hulianwang Jishu Shiyan 10-03 (Internet Connectivity Test 10-03) 2026-120C 69322 |
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. Individual satellites are built by a variety of manufacturers and 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
( ° ) | | |
| 2026 Jun 1, 05:25 | 6826 | 0.0009 | 441 | 454 | 93.54 | 55.00 | 290 | | | | Hulianwang Jishu Shiyan 10-04 (Internet Connectivity Test 10-04) 2026-120D 69323 |
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. Individual satellites are built by a variety of manufacturers and 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
( ° ) | | |
| 2026 Jun 1, 05:25 | 6825 | 0.0010 | 440 | 453 | 93.52 | 55.00 | 299 | | | | CZ 2D second stage uncatalogued |
Re-entered - 2026 May 30
Life <1 day
|
| Launched Hulianwang Jishu Shiyan 10 group. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-121 CZ 12B (Y-1)
Dongfeng Commercial Zone, Jiuquan Space Centre | 2026 Jun 1, 08:40 UTC | Qianfan Ji Gui 08-01 (Qianfan 163) 2026-121A 69325 |
in space
|
| Broadband distribution satellite for the Thousand Sails constellation. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 1, 22:11 | 7413 | 0.0019 | 1021 | 1048 | 105.85 | 89.02 | 234 | | | | 2026 Jun 17, 08:57 | 7415 | 0.0020 | 1022 | 1051 | 105.90 | 89.01 | 188 | | | | Qianfan Ji Gui 08-02 (Qianfan 164) 2026-121B 69326 |
in space
|
| Broadband distribution satellite for the Thousand Sails constellation. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 1, 13:22 | 7412 | 0.0018 | 1020 | 1047 | 105.84 | 89.01 | 238 | | | | CZ 12B second stage 2026-121C 69327 |
in space
|
| Launched pair of Qianfan Ji Gui satellites. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 2, 23:27 | 7258 | 0.0197 | 737 | 1022 | 102.56 | 89.03 | 52 | | | |
2026-122 Falcon 9 Block 5 (Starlink Group 17-47)
Vandenberg Space Force Base | 2026 Jun 3, 15:40 UTC | Starlink 3773 2026-122A 69329 |
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 16:41 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 9, 14:00 | 6676 | 0.0001 | 297 | 298 | 90.47 | 97.29 | 89 | | | | 2026 Jun 16, 03:36 | 6706 | 0.0000 | 328 | 328 | 91.09 | 97.28 | 76 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 3
Life <1 day
|
| Launched Starlink Group 17-47. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-123 Falcon 9 Block 5 (Starlink Group 10-43)
Cape Canaveral Space Force Station | 2026 Jun 4, 10:26 UTC | Starlink 37851 2026-123A 69353 |
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 12:49 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 9, 14:00 | 6666 | 0.0001 | 287 | 289 | 90.28 | 53.16 | 51 | | | | 2026 Jun 16, 04:00 | 6706 | 0.0001 | 327 | 329 | 91.09 | 53.16 | 101 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 4
Life <1 day
|
| Launched Starlink Group 10-23. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-124 CZ 6A
Taiyuan Space Centre | 2026 Jun 4, 11:30 UTC | Qianfan Ji Gui 11-01 (Qianfan 165) 2026-124A 69382 |
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
( ° ) | | |
| 2026 Jun 10, 21:57 | 7199 | 0.0002 | 819 | 822 | 101.30 | 89.00 | 195 | | | | 2026 Jun 17, 14:38 | 7217 | 0.0003 | 837 | 841 | 101.69 | 89.00 | 117 | | | | CZ 6A third stage 2024-125U 69400 |
in space
|
| Launched Qianfan Ji Gui group 11. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 10, 23:39 | 7097 | 0.0105 | 644 | 794 | 99.17 | 89.03 | 84 | | | |
2026-125 CZ 8 (Y-9)
Hainan Commercial Zone, Wenchang Space Centre | 2026 Jun 5, 06:34 UTC | Qianfan Ji Gui 12-01 (Qianfan 183) 2026-125A 69401 |
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
( ° ) | | |
| 2026 Jun 17, 16:35 | 7232 | 0.0020 | 840 | 869 | 102.02 | 88.99 | 172 | | | | CZ 8 third stage 2026-125U 69419 |
in space
|
| Launched Qianfan Ji Gui Group 12. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 16:26 | 7155 | 0.0072 | 726 | 829 | 100.39 | 89.00 | 76 | | | |
2026-126 Falcon 9 Block 5 (Starlink Group 17-43)
Vandenberg Space Force Base | 2026 Jun 7, 04:24 UTC | Starlink 37537 2026-126A 69420 |
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 05:26 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 18, 20:00 | 6722 | 0.0001 | 343 | 345 | 91.42 | 97.28 | 89 | | | | USA 608 (Starshield 0193) 2026-126X 69441 |
in space
|
One of two US government NRO intelligence gathering satellites carried alongside the SpaceX Starlink satellites on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Separated from launch vehicle at (probably) 05:26 UTC. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 7, 06:00 | 6700 | 0.0007 | 317 | 326 | 90.96 | 97.28 | 270 | 20:11 | | | estimated orbit | 6699 | 0.0007 | 316 | 325 | 90.94 | 97.28 | 270 | 20:11 | | | USA 609 (Starshield 0194) 2026-126Y 69442 |
in space
|
One of two US government NRO intelligence gathering satellites carried alongside the SpaceX Starlink satellites on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Separated from launch vehicle at (probably) 05:26 UTC. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 7, 06:00 | 6699 | 0.0007 | 316 | 325 | 90.94 | 97.28 | 270 | 20:11 | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 7
Life <1 day
|
| Launched Starlink Group 17-43 and two Starshield satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-127 Falcon 9 Block 5 (Starlink Group 10-35)
Cape Canaveral Space Force Station | 2026 Jun 8, 10:13 UTC | Starlink 37629 2026-127A 69443 |
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 11:14 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 16, 14:00 | 6704 | 0.0001 | 325 | 326 | 91.05 | 53.16 | 36 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 8
Life <1 day
|
| Launched Starlink Group 10-35. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-128 Zhuque 2E (Y-6)
Dongfeng Commercial Zone, Jiuquan Space Centre | 2026 Jun 9, 08:23 UTC | Qianfan DTC 2026-128A 69472 |
in space
|
| Demonstrator satellite for 5G and 6G mobile phone services and their associated space-ground network. DTC stands for "Direct to Cell". Separated from launch vehicle at 08:38 UTC. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 10, 14:45 | 6778 | 0.0008 | 394 | 405 | 92.56 | 54.99 | 260 | | | | Zhongguo Yídong 02 (China Mobile 02) 2026-128B 69473 |
in space
|
| Demonstrator satellite for mobile communications networks, owned by the China Mobile Communications Group. Separated from launch vehicle at 08:38 UTC. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 9, 14:05 | 6778 | 0.0008 | 394 | 405 | 92.55 | 55.00 | 260 | | | | Zhuque 2E second stage 2026-126C 69537 |
in space
|
| Launched pair of mobile telephony comsats. Space-Track reported that the stage disintegrated at about 08:47 UTC. It shed a small number of detectable debris items but probably a lot more very small fragments. The event was about 24 minutes after lift-off and nine minutes after satellite release. Itcoincided with the stage's retro-firing that reduced orbital perigee to 336 km. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 12, 20:20 | 6758 | 0.0066 | 336 | 425 | 92.16 | 54.53 | 332 | | | |
2026-129 CZ 5 (Y-11)
Wenchang Space Centre | 2026 Jun 11, 07:30 UTC | Tongxin Jishu Shiyan 25 (Communication Technology Test 25, TJS 25) 2026-129A 69474 |
in space
|
| Chinese government owned satellite described as being mainly used to carry out multi-band and high-speed satellite communication technology verification. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 Jun 11, 11:34 | 29368 | 0.7752 | 224 | 45755 | 834.77 | 16.53 | 200 | | | | 2026 Jun 23, 20:06 | 42164 | 0.0002 | 35775 | 35796 | 1436.05 | 5.98 | 309 | 120°.2 E | | | |
in space
|
| Launched Tongxin Jishu Shiyan 25 (TJS 25). |
| Orbit parameters awaited | |
2026-130 Electron (HASTE - Curveball)
Mid Atlantic Regional Space Port, Wallops Island | 2026 Jun 11, 08:00 UTC | Electron stage 2 2026-130A 69476 |
Re-entered - 2026 Jun 12
Life 1 day
|
| Launched Curveball mission for unknown client. Orbit and decay date are estimates based on limited Space-Track data. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 11, 08:10 | 6575 | 0.0011 | 189 | 204 | 88.42 | 39.99 | 117 | | | | Electron stage 3 (modified kick stage) 2026-130B 69477 |
Re-entered - 2026 Jun 11
Life <1 day
|
| Launched Curveball mission for unknown client. Orbit is an estimate based on limited Space-Track data. It probably represents the trajectory shortly before an engine firing to precipitate re-entry of the payload in order for it to conduct an atmospheric hypersonic flight test. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 11, 08:10 | 6577 | 0.0001 | 198 | 199 | 88.46 | 40.00 | 117 | | | |
2026-131 Falcon 9 Block 5 (Starlink Group 17-44)
Vandenberg Space Force Base | 2026 Jun 11, 15:05 UTC | Starlink 37816 2026-131A 69478 |
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 16:06 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 18:00 | 6663 | 0.0001 | 284 | 285 | 90.21 | 97.28 | 80 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 11
Life <1 day
|
| Launched Starlink Group 17-44. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-132 H-3 30S (F-6)
Tanegashima Space Centre | 2026 Jun 12, 00:53 UTC | STARS-X (Space Tethered Autonomous Robotic Satellite) 2026-132A 69502 |
in space
|
| Small, two-part satellite from Shizuoka University, Japan to demonstrate unreeling and retrieval of a one kilometre long tether and using the tether moving a motorised payload along it. Separated from launch vehicle at 01:05 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 13, 10:00 | 6948 | 0.0012 | 561 | 578 | 96.06 | 97.69 | 285 | 09:45 | | | Umitsubame (Petrel) 2026-132B 69503 |
in space
|
| Small satellite from the Tokyo University of Science to verify/demonstrate a set of telescopes and cameras for Earth observation and observing objects in space. Separated from launch vehicle at 01:05 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 13, 10:00 | 6948 | 0.0012 | 561 | 578 | 96.06 | 97.70 | 288 | 09:45 | | | BRO 22 (Breizh Reconnaissance Orbiter 22) 2026-132C 69504 |
in space
|
| 8U Cubesat from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Separated from launch vehicle at 01:16 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 13, 09:59 | 6946 | 0.0014 | 558 | 577 | 96.02 | 97.69 | 299 | 09:45 | | | |
in space
|
| 6U Cubesat - from the BULL Corporation of Japan. One of a pair carried on this launch to demonstrate an aero-braking device to be used for de-orbiting future satellites. Separated from launch vehicle at 01:23 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 13, 09:58 | 6942 | 0.0011 | 556 | 572 | 95.94 | 97.69 | 315 | 09:45 | | | VERTECS (Visible Extragalactic background RadiaTion Exploration by CubeSat) 2026-132E 69506 |
in space
|
| 6U Cubesat from Kyushu Institute of Technology in cooperation other organisation within Japan and in other countries. Equipped with an imaging system to investigate cosmic background radiation in the visible spectrum. Separated from launch vehicle at 01:22 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 16, 19:34 | 6942 | 0.0012 | 556 | 573 | 95.94 | 97.69 | 309 | 09:45 | | | |
in space
|
| 6U Cubesat - from the BULL Corporation of Japan. One of a pair carried on this launch to demonstrate an aero-braking device to be used for de-orbiting future satellites. Separated from launch vehicle at 01:23 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 13, 09:58 | 6942 | 0.0011 | 556 | 571 | 95.93 | 97.69 | 320 | 09:45 | | | H-3 upper stage uncatalogued |
Re-entered - 2026 Jun 12
Life <1 day
|
| Carried simulated satellite (VEP 5) that was not separated, and launched six small satellites. Retrofire at 02:40 UTC led to destructive re-entry above the Indian Ocean south east of Australia at around 03:20 UTC |
| Not Catalogued - orbit parameters unavailable | |
2026-133 Falcon 9 Block 5 (Starlink Group 10-54)
Cape Canaveral Space Force Station | 2026 Jun 12, 12:27 UTC | Starlink 37536 2026-133A 69508 |
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 13:30 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 16, 20:00 | 6626 | 0.0001 | 247 | 248 | 89.45 | 53.16 | 60 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 12
Life <1 day
|
| Launched Starlink Group 10-54. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-134 Lijian 1 (Y-14)
Dongfeng Commercial Zone, Jiuquan Space Centre | 2026 Jun 15, 03:44 UTC | Jilin-1 High Resolution 04D 01 (Jilin-1 GF04D 01) 2026-134xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 548 | 95.40 | 97.70 | 281 | 10:11 | | | Jilin-1 High Resolution 04D 02 (Jilin-1 GF04D 02) 2026-134xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 548 | 95.40 | 97.70 | 281 | 10:11 | | | Jilin-1 High Resolution 05D 01 (Jilin-1 GF05D 01) 2026-134xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 548 | 95.40 | 97.70 | 281 | 10:11 | | | Jilin-1 High Resolution 05D 02 (Jilin-1 GF05D 02) 2026-134xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 548 | 95.40 | 97.70 | 281 | 10:11 | | | Jilin-1 High Resolution 07C 04 (Jilin-1 GF07C 04) 2026-134xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 548 | 95.40 | 97.70 | 281 | 10:11 | | | Jilin-1 High Resolution 07D 02 (Jilin-1 GF07D 02) 2026-134xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 548 | 95.40 | 97.70 | 281 | 10:11 | | | Jilin-1 High Resolution 07D 03 (Jilin-1 GF07D 03) 2026-134xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 548 | 95.40 | 97.70 | 281 | 10:11 | | | Jilin-1 High Resolution 07D 04 (Jilin-1 GF07D 04) 2026-134xx |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0015 | 528 | 548 | 95.40 | 97.70 | 281 | 10:11 | | | Lijian 1 third stage uncatalogued |
Re-entered - 2026 Jun 15
Life <1 day
|
| Launched cluster of Jilin-1 satellites. Caused to reenter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-135 Falcon 9 Block 5 (Starlink Group 17-54)
Vandenberg Space Force Base | 2026 Jun 15, 15:34 UTC | Starlink 37880 2026-135A 69546 |
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 16:36 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 25, 16:00 | 6706 | 0.0002 | 327 | 329 | 91.09 | 97.28 | 92 | | | | Falcon 9 second stage uncatalogued |
in space
|
| Launched Starlink Group 17-54. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-136 CZ 3B
Xichang Space Centre | 2026 Jun 16, 09:45 UTC | Shijian 31 (Practice 31) 2026-136A 69570 |
in space
|
| Chinese government/military satellite described as "mainly used for space environment detection", maybe indicating that its rôle is to observe and measure orbits of other orbiting objects. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 16, 20:21 | 24378 | 0.7310 | 178 | 35820 | 631.31 | 63.46 | 172 | | | | 2026 Jun 23, 17:41 | 27323 | 0.6941 | 1979 | 39911 | 749.13 | 63.48 | 172 | | | | CZ 3B fourth stage 2026-136B 69571 |
in space
|
| Launched Shijian 31. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 16, 09:45 | 26521 | 0.7530 | 171 | 40114 | 716.37 | 51.06 | 225 | | | | 2026 Jun 17, 03:09 | 24687 | 0.7369 | 117 | 36501 | 643.38 | 63.43 | 171 | | | |
2026-137 CZ 12
Hainan Commercial Zone, Wenchang Space Centre | 2026 Jun 17, 02:44 UTC | Hulianwang Digui 22-01 (Satellite Low Orbit Internet Group 22-01) 2026-137A 69572 |
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
( ° ) | | |
| 2026 Jun 18, 07:22 | 7299 | 0.0012 | 912 | 930 | 103.43 | 50.00 | 231 | | | | CZ 12 second stage 2026-137K 69581 |
in space
|
| Launched Hulianwang Digui group 22. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 17:24 | 7232 | 0.0077 | 798 | 910 | 102.01 | 49.99 | 116 | | | |
2026-138 Kuaizhou 11 (Y-13)
Jiuquan Space Centre | 2026 Jun 17, 03:58 UTC | Wei Li Kongjiang Group 5-01 (Centispace 02-11) 2026-138A 69582 |
in space
|
One of eight simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 20:20 | 7218 | 0.0010 | 833 | 848 | 101.73 | 55.14 | 276 | | | | Wei Li Kongjiang Group 5-02 (Centispace 02-12) 2026-138B 69583 |
in space
|
One of eight simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 20:20 | 7218 | 0.0009 | 833 | 846 | 101.71 | 55.15 | 280 | | | | Wei Li Kongjiang Group 5-03 (Centispace 02-13) 2026-138C 69584 |
in space
|
One of eight simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 20:20 | 7218 | 0.0009 | 833 | 846 | 101.71 | 55.15 | 277 | | | | Wei Li Kongjiang Group 5-04 (Centispace 02-14) 2026-138D 69585 |
in space
|
One of eight simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 20:20 | 7217 | 0.0008 | 833 | 845 | 101.70 | 55.15 | 276 | | | | Wei Li Kongjiang Group 5-05 (Centispace 02-15) 2026-138E 69586 |
in space
|
One of eight simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 16:56 | 7217 | 0.0008 | 833 | 844 | 101.70 | 55.14 | 274 | | | | Wei Li Kongjiang Group 5-06 (Centispace 02-16) 2026-138F 69587 |
in space
|
One of eight simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 18:38 | 7217 | 0.0008 | 833 | 845 | 101.70 | 55.15 | 285 | | | | Wei Li Kongjiang Group 5-07 (Centispace 02-17) 2026-138G 69588 |
in space
|
One of eight simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 20:20 | 7216 | 0.0007 | 833 | 844 | 101.68 | 55.15 | 278 | | | | Wei Li Kongjiang Group 5-08 (Centispace 02-18) 2026-138J 69636 |
in space
|
One of eight simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 18, 23:26 | 7217 | 0.0008 | 833 | 845 | 101.70 | 55.14 | 279 | | | | Kuaizhou upper stage 2026-138H 69628 |
in space
|
| Launched Wei Li Kongjiang Group 5. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 17:47 | 6915 | 0.0509 | 185 | 889 | 95.38 | 55.15 | 83 | | | |
2026-139 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2026 Jun 17, 06:39 UTC | BlueBird 8 (SpaceMobile 008) 2026-139A 69589 |
in space
|
| Commercial 5G broadband satellite from US company AST Spacemobile to provide direct mobile phone services from orbit. One of three similar satellites carried on this launch. Released from launch vehicle at 07:33 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 20:49 | 6907 | 0.0004 | 526 | 531 | 95.21 | 53.00 | 322 | | | | BlueBird 9 (SpaceMobile 009) 2026-139B 69590 |
in space
|
| Commercial 5G broadband satellite from US company AST Spacemobile to provide direct mobile phone services from orbit. One of three similar satellites carried on this launch. Released from launch vehicle at 07:33 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 22:24 | 6906 | 0.0004 | 526 | 531 | 95.20 | 53.00 | 335 | | | | BlueBird 10 (SpaceMobile 010) 2026-139C 69591 |
in space
|
| Commercial 5G broadband satellite from US company AST Spacemobile to provide direct mobile phone services from orbit. One of three similar satellites carried on this launch. Released from launch vehicle at 07:33 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 16:03 | 6906 | 0.0004 | 525 | 530 | 95.19 | 53.00 | 342 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 17
Life <1 day
|
| Launched three Bluebird comsats. The third orbit listed is after retro-fire to cause re-entry above the southern Pacific Ocean at around 09:35 UTC. Space-Track issued orbital data for this object against the catalogue numbers of 39A, 39B & 39C, leaving this object uncatalogued as is the norm for Falcon 9 upper stages. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 17, 06:48 | 6729 | 0.0298 | 150 | 551 | 91.55 | 53.00 | 48 | | | | 2026 Jun 17, 07:25 | 6909 | 0.0005 | 527 | 534 | 95.25 | 53.01 | 275 | | | | 2026 Jun 17, 08:26 | 6671 | 0.0431 | 5 | 580 | 90.37 | 52.97 | 284 | | | |
2026-140 Ariane 64 P160C (VA-269, Amazon LEO 03)
Centre Spatiale Guyanaise | 2026 Jun 17, 12:21 UTC | Amazon LEO 00423 (Kuiper 00423) 2026-140A 69592 |
in space
|
One member of a simultaneously-launched cluster of thirty six broadband and mobile telephone communications satellites from US company Amazon. Released from the launch vehicle in groups over a period of ~25 minutes beginning at 12:47 UTC.
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
( ° ) | | |
| 2026 Jun 25, 14:00 | 6825 | 0.0014 | 437 | 457 | 93.52 | 51.88 | 196 | | | | Ariane 6 third stage uncatalogued |
Re-entered - 2026 Jun 17
Life <1 day
|
| Launched cluster of Kuiper satellites. Retro-fire at 15:01 UTC, after releasing satellites, led to re-entry above the Indian Ocean at about 15:40 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2026-141 Falcon 9 Block 5 (NRO L-79)
Vandenberg Space Force Base | 2026 Jun 19, 08:53 UTC | USA 610 (Starshield 0195) 2026-141A 69637 |
in space
|
One of two US government NRO intelligence gathering satellites carried on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6822 | 0.0003 | 442 | 446 | 93.46 | 70.00 | 150 | | | | USA 611 (Starshield 0196) 2026-141B 69638 |
in space
|
One of two US government NRO intelligence gathering satellites carried on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6824 | 0.0004 | 443 | 448 | 93.49 | 70.00 | 270 | | | | USA 612 (Starshield 0197) 2026-141C 69639 |
in space
|
One of two US government NRO intelligence gathering satellites carried on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6824 | 0.0006 | 442 | 450 | 93.50 | 70.00 | 150 | | | | USA 613 (Starshield 0198) 2026-141D 69640 |
in space
|
One of two US government NRO intelligence gathering satellites carried on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6823 | 0.0004 | 442 | 447 | 93.47 | 70.00 | 150 | | | | USA 614 (Starshield 0199) 2026-141E 69641 |
in space
|
One of two US government NRO intelligence gathering satellites carried on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6822 | 0.0004 | 441 | 446 | 93.45 | 70.00 | 150 | | | | USA 615 (Starshield 0200) 2026-141F 69642 |
in space
|
One of two US government NRO intelligence gathering satellites carried on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6808 | 0.0003 | 428 | 432 | 93.18 | 70.02 | 150 | | | | USA 616 (Starshield 0201) 2026-141G 69643 |
in space
|
One of two US government NRO intelligence gathering satellites carried on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6808 | 0.0003 | 428 | 432 | 93.18 | 70.01 | 150 | | | | USA 617 (Starshield 0202) 2026-141H 69644 |
in space
|
One of two US government NRO intelligence gathering satellites carried on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6808 | 0.0003 | 428 | 432 | 93.18 | 70.02 | 150 | | | | USA 618 (Starshield 0203) 2026-141J 69645 |
in space
|
One of two US government NRO intelligence gathering satellites carried on this launch. Design is related the Starlink satellites and provides a hosting platform for a variety of missions such as imaging, SIGINT, ELINT etc, possibly using the Starlink infrastructure for communications. Orbit information based on limited Space-Track data.
|
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6808 | 0.0003 | 428 | 432 | 93.18 | 70.01 | 150 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 19
Life <1 day
|
| Launched group of Starshield satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-142 Electron (Victus Haze)
Rocket Lab Launch Complex, New Zealand | 2026 Jun 19, 10:19 UTC | Victus Haze Puma 2026-142A 69646 |
in space
|
| Built by Rocket Lab for the USSF using its Photon design that uses the Electron third stage (kick stage) as the satellite bus. Described as being to "demonstrate rendezvous and proximity operations". A few hours after launch it approached to within a few tens of kilometres of Jackal 0004 (69014/2026-100AJ) and photographed it. Launch not announced for several days after the event. Used as demonstration to show Rocket Lab ability to prepare and launch Electron with 24 hours notice. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jun 19, 23:21 | 6782 | 0.0084 | 347 | 461 | 92.64 | 97.45 | 250 | 22:41 | | | 2026 Jun 22, 21:00 | 6843 | 0.0008 | 460 | 471 | 93.90 | 97.40 | 30 | 22:41 | | | 2026 Jun 23, 23:49 | 6882 | 0.0021 | 489 | 518 | 94.69 | 97.45 | 304 | 22:41 | | | Electron second stage 2026-142B 69647 |
Re-entered - 2026 Jun 28
Life 9 days
|
| Launched Victus Haze mission. The first orbit listed is derived from limited data released by Space-Track within a few hours of lift-off. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 19, 23:00 | 6681 | 0.0194 | 173 | 432 | 90.57 | 97.44 | 237 | | | | 2026 Jun 22, 18:56 | 6661 | 0.0170 | 170 | 395 | 90.16 | 97.44 | 236 | | | |
2026-I02 JEM Small Satellite Orbital Deployer (J-SSOD 37)
International Space Station | 2026 Jun 19, 11:10 UTC | Hokushin 1 1998-067YH 69648 |
in space
|
| 3U Cubesat from a consortium of Tohoku University, Hokkaido University, and the Muroran Institute of Technology, Japan. Equipped as a demonstrator of future Moon exploration technology, including a micro thruster to control the orbit. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 21, 18:26 | 6795 | 0.0006 | 412 | 421 | 92.90 | 51.63 | 235 | | | |
2026-143 Falcon 9 Block 5 (Starlink Group 17-28)
Vandenberg Space Force Base | 2026 Jun 21, 16:39 UTC | Starlink 37656 2026-143A 69649 |
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 17:43 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 26, 18:00 | 6671 | 0.0002 | 291 | 293 | 90.36 | 97.29 | 64 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 21
Life <1 day
|
| Launched Starlink Group 17-28. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-144 CZ 7A
Wenchang Space Centre | 2026 Jun 23, 02:10 UTC | Tongxin Jishu Shiyan 26A (Communication Technology Test 26A, TJS 26A) 2026-144A 69674 |
in space
|
| Chinese government owned satellite described as being mainly used for satellite communication, radio and television, data transmission and other services, and carries out related technical tests and verification. Probably entered GEO drift orbit around 08:00 UTC on day of launch. Initial GEO location put it alongside TJS 5 (44978.2020-002A) suggesting it is either a replacement for it or is supplementing its service. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 Jun 23, 07:54 | 24387 | 0.7315 | 171 | 35848 | 631.69 | 19.52 | 180 | | | | 2026 Jul 7, 19:23 | 42166 | 0.0003 | 35774 | 35802 | 1436.16 | 6.96 | 347 | 107°.6 E | | | CZ 7A fourth stage 2026-144B 69675 |
in space
|
| Launched Tongxin Jishu Shiyan 26A. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 23, 07:47 | 23645 | 0.7251 | 121 | 34413 | 603.07 | 19.51 | 179 | | | |
2026-U01 Falcon 9 Block 5 (Uncatalogued orbital launch)
Cape Canaveral Space Force Station | 2026 Jun 23, 10:53 UTC | Starfall Demo uncatalogued |
Re-entered - 2026 Jun 23
Life <1 day
Returned to Earth |
| Demonstrator for SpaceX cargo transportation system to be used either between space and ground or for rapid global delivery of cargo across the globe. Re-entered above the Pacific Ocean, possibly at a similar time to the launch vehicle upper stage and near the end of the second Earth circuit (to be confirmed). Splashdown off California would have been at around 14:20 UTC. The vehicle was picked up by a ship-borne recovery team. |
| Not Catalogued - orbit parameters unavailable | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 23
Life <1 day
|
| Launched Starfall Demo Mission, may have carried additional payloads. Initial orbital inclination ~40°. Caused to re-enter at the end of its second circuit of the Earth at around 14:10 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2026-145 Falcon 9 Block 5 (Starlink Group 17-45)
Vandenberg Space Force Base | 2026 Jun 25, 03:30 UTC | Starlink 38005 2026-145A 69677 |
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 04:32 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 29, 18:00 | 6681 | 0.0001 | 302 | 304 | 90.59 | 97.29 | 87 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 25
Life <1 day
|
| Launched Starlink Group 17-45. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-146 Electron (Ten Owl Of Ten)
Rocket Lab Launch Complex, New Zealand | 2026 Jun 26, 17:43 UTC | |
in space
|
| Imaging satellite equipped with a synthetic aperture radar - produced by the University of Tokyo, the Tokyo Institute of Technology, Keio University, Japan Space Systems, and a private company - Synspective Inc of Tokyo. Will become part of a constellation of 25-30 satellites to monitor ground movement and ground changes in urban areas. The name derives from the scientific name for the owl and its sensitivity to low levels of light. Separated from launch vehicle 55-60 minutes after lift-off. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 27, 07:01 | 6932 | 0.0009 | 547 | 560 | 95.73 | 41.99 | 276 | | | | Electron stage 2 2026-146B 69702 |
in space
|
| Launched StriX 8. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 27, 20:21 | 6758 | 0.0211 | 237 | 522 | 92.14 | 42.08 | 259 | | | | Electron stage 3 (kick stage) 2026-146C 69703 |
in space
|
| Launched StriX 8. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 27, 22:57 | 6930 | 0.0011 | 544 | 560 | 95.69 | 41.99 | 278 | | | |
2026-147 Falcon 9 Block 5 (Starlink Group 17-40)
Vandenberg Space Force Base | 2026 Jun 28, 13:09 UTC | Starlink 38055 2026-147A 69704 |
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 14:10 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 30, 18:00 | 6644 | 0.0001 | 266 | 267 | 89.83 | 97.28 | 101 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 28
Life <1 day
|
| Launched Starlink Group 17-40. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-148 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2026 Jun 29, 02:29 UTC | Sirius XM-11 2026-148A 69728 |
in space
|
| Commercial comsat providing services to the continental USA including digital audio radio broadcast directly to cars, homes and portable radios. Separated from launch vehicle at 02:59 UTC. Expected location 116° west. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 Jul 1, 19:27 | 18820 | 0.6481 | 245 | 24639 | 428.25 | 26.88 | 177 | | | | 2026 Jul 2, 18:38 | 20869 | 0.6818 | 263 | 28719 | 500.06 | 26.82 | 178 | | | | 2026 Jul 6, 15:32 | 32370 | 0.3010 | 16248 | 35735 | 965.97 | 5.00 | 180 | | | | 2026 Jul 8, 13:21 | 40935 | 0.0288 | 33378 | 35735 | 1373.71 | 0.31 | 162 | | | | 2026 Jul 10, 17:47 | 42109 | 0.0001 | 35726 | 35736 | 1433.25 | 0.13 | 41 | 121°.2 W | | | 2026 Jul 11, 11:07 | 42136 | 0.0006 | 35732 | 35783 | 1434.61 | 0.12 | 280 | 120°.9 W | | | 2026 Jul 13, 16:35 | 42166 | 0.0002 | 35779 | 35795 | 1436.14 | 0.12 | 175 | 120°.5 W | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jun 29
Life <1 day
|
| Launched Sirius XM 11. Cause to reenter at about 08:30 UTC, above the Pacific Ocean off Mexico after releasing satellite. The orbit listed was issued by Space-Track against the catalogue number for the satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jun 30, 04:56 | 16296 | 0.5952 | 219 | 19618 | 345.06 | 26.99 | 175 | | | |
2026-149 CZ 4B
Jiuquan Space Centre | 2026 Jul 1, 23:46 UTC | Haiyang 2-05 (Ocean 2-05) 2026-149A 69737 |
in space
|
| Oceanographic satellite to observe ocean surface heights, wave heights and wind patterns. Replacement for Haiyang 2-02 (43655, 2018-081A). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 2, 09:35 | 7315 | 0.0012 | 928 | 946 | 103.77 | 99.34 | 262 | 06:00 | | | 2026 Jul 2, 23:26 | 7324 | 0.0011 | 938 | 954 | 103.97 | 99.35 | 245 | 06:00 | | | 2026 Jul 4, 06:42 | 7339 | 0.0008 | 955 | 966 | 104.27 | 99.35 | 219 | 06:00 | | | 2026 Jul 7, 16:28 | 7343 | 0.0005 | 961 | 969 | 104.37 | 99.35 | 202 | 06:00 | | | 2026 Jul 9, 17:14 | 7344 | 0.0001 | 965 | 967 | 104.40 | 99.34 | 109 | 06:00 | | | CZ 4B third stage 2026-149B 69738 |
in space
|
| Launched Haiyang 2-05. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 2, 14:20 | 7170 | 0.0199 | 649 | 934 | 100.69 | 99.32 | 6 | | | |
2026-150 Falcon 9 Block 5 (Starlink Group 17-46)
Vandenberg Space Force Base | 2026 Jul 2, 02:58 UTC | Starlink 38033 2026-150A 69739 |
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 03:59 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 7, 12:00 | 6694 | 0.0002 | 315 | 317 | 90.84 | 97.29 | 69 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 2
Life <1 day
|
| Launched Starlink Group 17-46. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-151 Atlas V 551 (KA-04, Amazon LEO 08)
Cape Canaveral Space Force Station | 2026 Jul 2, 04:24 UTC | Amazon LEO 00258 (Kuiper 00258) 2026-151A 69763 |
in space
|
One member of a simultaneously-launched cluster of twenty nine 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
( ° ) | | |
| 2026 Jul 8, 14:00 | 6838 | 0.0012 | 451 | 468 | 93.78 | 51.87 | 147 | | | | Atlas V third stage (Centaur) uncatalogued |
Re-entered - 2026 Apr 30
Life <1 day
|
| Launched twenty nine Kuiper satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-I03 Nanoracks Cubesat Deployer (NRCSD 30)
International Space Station | 2026 Jul 2 UTC | |
in space
|
| 1U Cubesat from the Arizona State University. Carries an amateur radio package. Released from ISS at 10:30 UTC (to be confirmed). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6794 | 0.0010 | 409 | 423 | 92.89 | 51.63 | 287 | | | | HUCSat (Harvard Undergraduate CubeSat) 1998-067xx |
in space
|
| 2U Cubesat to test shape memory materials in satellite construction and a low-power communications system. Released from ISA at 09:00 UTC (to be confirmed). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6794 | 0.0010 | 409 | 423 | 92.89 | 51.63 | 287 | | | | LEOPARDSat 1 (Low Earth Orbit Platform for Aerospace Research and Development Satellite 1) 1998-067xx |
in space
|
| 1U Cubesat from the University of Cincinnati to measure radiation levels in LEO. Released from ISS at 10:30 UTC (to be confirmed). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6794 | 0.0010 | 409 | 423 | 92.89 | 51.63 | 287 | | | | PROVES Alcyone (Pleiades Rapid Orbital Verification Experiment System) 1998-067xx |
in space
|
| 1U Cubesat - demonstrator of an off-the-shelf Cubesat design. Built under the Pleiades inter-university program involving six universities in the US. Carries an amateur radio package. Released from ISS at 10:30 UTC (to be confirmed). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6794 | 0.0010 | 409 | 423 | 92.89 | 51.63 | 287 | | | | PROVES Atlas (Pleiades Rapid Orbital Verification Experiment System) 1998-067xx |
in space
|
| 1U Cubesat - demonstrator of an off-the-shelf Cubesat design. Built under the Pleiades inter-university program involving six universities in the US. Carries an amateur radio package. Released from ISS at 10:30 UTC (to be confirmed). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6794 | 0.0010 | 409 | 423 | 92.89 | 51.63 | 287 | | | | PROVES Electra (Pleiades Rapid Orbital Verification Experiment System) 1998-067YP 69799 |
in space
|
| 1U Cubesat - demonstrator of an off-the-shelf Cubesat design. Built under the Pleiades inter-university program involving six universities in the US. Carries an amateur radio package. Released from ISS at 11:40 UTC (to be confirmed). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 10, 09:44 | 6794 | 0.0010 | 409 | 423 | 92.89 | 51.63 | 287 | | | |
2026-152 Pegasus XL
Lockheed L-1011 aircraft, Ronald Reagan Space and Missile Test Range | 2026 Jul 3, 08:36 UTC | |
in space
|
| Satellite servicing vehicle from Katalyst Space Technologies to visit NASA's Neil Gehrels Swift Observatory (28485, 2004-047A). After a fly-around inspection, it is planned to dock, boost the orbit and then depart, leaving Swift to continue its gamma ray studies mission. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 3, 23:17 | 6755 | 0.0023 | 362 | 392 | 92.09 | 20.60 | 195 | | | | Pegasus third stage 2026-152A 69793 |
in space
|
| Launched Link 1. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 3, 23:17 | 6755 | 0.0022 | 362 | 392 | 92.09 | 20.60 | 196 | | | |
2026-153 CZ 6A
Taiyuan Space Centre | 2026 Jul 4, 09:30 UTC | Qianfan Ji Gui 13-01 (Qianfan 201) 2026-153A 69800 |
in space
|
One member of a simultaneously launched cluster of eighteen broadband distribution satellites for the Thousand Sails constellation. Catalogue Number and Designation to be confirmed.
All satellites were injected into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 15, 21:00 | 7181 | 0.0008 | 797 | 809 | 100.94 | 88.99 | 180 | | | | CZ 6A third stage 2024-153U 69818 |
in space
|
| Launched Qianfan Ji Gui group 13. Perigee lowered after releasing satellites. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 13, 16:02 | 7093 | 0.0087 | 653 | 776 | 99.07 | 89.02 | 92 | | | |
2026-154 Falcon 9 Block 5 (Starlink Group 10-50)
Cape Canaveral Space Force Station | 2026 Jul 5, 10:50 UTC | Starlink 37520 2026-154A 69819 |
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 11:53 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 8, 14:00 | 6638 | 0.0001 | 259 | 260 | 89.71 | 53.16 | 56 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 5
Life <1 day
|
| Launched Starlink Group 10-50. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-155 CZ 8A (Y-9)
Hainan Commercial Zone, Wenchang Space Centre | 2026 Jul 5, 13:43 UTC | Qianfan Ji Gui 15-01 (Qianfan 219) 2026-155A 69848 |
in space
|
| One member of a simultaneously launched cluster of twenty 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
( ° ) | | |
| 2026 Jul 13, 12:56 | 7199 | 0.0030 | 799 | 842 | 101.30 | 89.01 | 233 | | | | CZ 8A third stage 2026-155W 69868 |
in space
|
| Launched Qianfan Ji Gui Group 15. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 13, 13:26 | 7109 | 0.0105 | 656 | 806 | 99.43 | 88.97 | 108 | | | |
2026-156 Falcon 9 Block 5 (Transporter 17)
Vandenberg Space Force Base | 2026 Jul 7, 08:12 UTC | CAS500 4 (Compact Advanced Satellite 500-4) 2026-156A 69869 |
in space
|
| Satellite from the Korea Aerospace Reseach Institute equipped with an optical imaging system for Earth observation to support investigation of natural resources and monitoring of the environment within South Korea. Separated from launch vehicle at L+150 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:22 | 7272 | 0.0012 | 886 | 903 | 102.87 | 98.99 | 185 | 22:52 | | | |
in space
|
| Small satellite fitted with a synthetic aperture radar for Earth surface imaging. Separated from launch vehicle at L+63 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:58 | 6971 | 0.0008 | 587 | 599 | 96.54 | 97.75 | 101 | 22:53 | | | Pelican 11 (Tech Demonstration 2) 2026-156C 69871 |
in space
|
| Demonstrator satellite from Planet Labs carrying a high resolution Earth imager and other systems to be used in a new generation of Earth imaging satellites. Separated from launch vehicle at L+69 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 16:34 | 6971 | 0.0008 | 587 | 598 | 96.54 | 97.76 | 104 | 22:53 | | | TOM 1 (Telematics earth Observation Mission 1) 2026-156D 69872 |
in space
|
| 3U Cubesat from a consortium led by Zentrum für Telematik (ZFT) of Würzburg, Germany. One of a group of three satellites carried on the same launch, to fly in formation and use an imaging system conduct in 3D studies of plumes from volcanoes on the Earth's surface. Separated from launch vehicle at L+60 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:33 | 6974 | 0.0005 | 592 | 599 | 96.60 | 97.75 | 73 | 22:53 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+68 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:59 | 6971 | 0.0007 | 588 | 598 | 96.54 | 97.76 | 101 | 22:53 | | | |
in space
|
| 8U Cubesat from the local givernment of Bavaria, Germany. Equipped with a high resolution Earth imaging system to study natural resources. Separated from launch vehicle at L+56 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:32 | 6973 | 0.0005 | 592 | 599 | 96.59 | 97.75 | 87 | 22:53 | | | |
in space
|
| 8U Cubesat from the local givernment of Bavaria, Germany. Equipped with a high resolution Earth imaging system to study natural resources. Separated from launch vehicle at L+57 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:31 | 6973 | 0.0005 | 592 | 599 | 96.59 | 97.75 | 84 | 22:53 | | | ION SCV 023 (Joyful Julia) 2026-156H 69876 |
in space
|
| Satellite carrier from D-Orbit carrying four hosted payloads of customer-suppled experiments/sensors and Cubesat deployers containing three cubesats for later release. Separated from launch vehicle at L+62 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 16:31 | 6970 | 0.0009 | 586 | 598 | 96.52 | 97.73 | 108 | 22:53 | | | |
in space
|
| 8U Cubesat from the local givernment of Bavaria, Germany. Equipped with a high resolution Earth imaging system to study natural resources. Separated from launch vehicle at L+57 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:30 | 6973 | 0.0006 | 591 | 599 | 96.58 | 97.75 | 84 | 22:53 | | | LA3 (Anduril 216) 2026-156L 69879 |
in space
|
| Mission details to follow. Separated from launch vehicle at L+64 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:24 | 6971 | 0.0007 | 588 | 598 | 96.55 | 97.76 | 100 | 22:53 | | | Hyperion GR 1 2026-156Q 69883 |
in space
|
| Small satellite from Open Cosmos Aegean. First of ten satellites carrying an Earth imaging system, equipped with AI for image processing and fitted with a laser communication system for space to ground use. Separated from launch vehicle at L+60 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:26 | 6972 | 0.0007 | 589 | 598 | 96.56 | 97.75 | 96 | 22:53 | | | Earth Daily 8 (YAM 17) 2026-156R 69884 |
in space
|
| Small satellite built by Loft for Earth Daily Analytics. Equipped with an Earth imaging system controlled by onboard artificial intelligence to detect and study natural events. Separated from launch vehicle at L+64 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:19 | 6970 | 0.0009 | 586 | 598 | 96.53 | 97.75 | 105 | 22:53 | | | |
in space
|
Earth imaging satellite from Axelspace of Japan. One of seven similar satellites carried on this launch. Separated from launch vehicle at L+63 minutes.
All satellites were injected into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:24 | 6972 | 0.0007 | 588 | 599 | 96.55 | 97.75 | 96 | 22:53 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+63 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:56 | 6970 | 0.0008 | 586 | 598 | 96.53 | 97.76 | 108 | 22:53 | | | |
in space
|
| Small satellite fitted with a synthetic aperture radar for Earth surface imaging. Separated from launch vehicle at L+63 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 15:01 | 6972 | 0.0007 | 589 | 598 | 96.55 | 97.75 | 98 | 22:53 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+63 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 16:32 | 6970 | 0.0008 | 586 | 598 | 96.52 | 97.75 | 108 | 22:53 | | | |
in space
|
| Small satellite fitted with a synthetic aperture radar for Earth surface imaging. Separated from launch vehicle at L+63 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 16:31 | 6970 | 0.0009 | 586 | 598 | 96.52 | 97.75 | 107 | 22:53 | | | ICEYE X-80 2026-156AA 69893 |
in space
|
| Small satellite fitted with a synthetic aperture radar for Earth surface imaging. Separated from launch vehicle at L+72 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 15:01 | 6972 | 0.0007 | 589 | 598 | 96.55 | 97.75 | 96 | 22:53 | | | Pirx 1 (Mikroglob 1) 2026-156AC 69895 |
in space
|
| Mission details to follow. Separated from launch vehicle at L+66 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:59 | 6971 | 0.0008 | 588 | 599 | 96.54 | 97.75 | 98 | 22:53 | | | BRO-31 (Breizh Reconnaissance Orbiter 31) 2026-156AD 69896 |
in space
|
| 8U Cubesat from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Separated from launch vehicle at L+62 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 16:30 | 6970 | 0.0009 | 585 | 598 | 96.51 | 97.75 | 108 | 22:53 | | | Fossasat 2E 26 2026-156AG 69899 |
in space
|
| 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Separated from launch vehicle at L+62 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:27 | 6972 | 0.0007 | 590 | 599 | 96.57 | 97.75 | 88 | 22:53 | | | |
in space
|
| 8U Cubesat from the local givernment of Bavaria, Germany. Equipped with a high resolution Earth imaging system to study natural resources. Separated from launch vehicle at L+58 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:30 | 6973 | 0.0006 | 591 | 599 | 96.58 | 97.75 | 84 | 22:53 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+59 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:30 | 6973 | 0.0005 | 591 | 598 | 96.58 | 97.76 | 93 | 22:53 | | | TOM 3 (Telematics earth Observation Mission 3) 2026-156AP 69906 |
in space
|
| 3U Cubesat from a consortium led by Zentrum für Telematik (ZFT) of Würzburg, Germany. One of a group of three satellites carried on the same launch, to fly in formation and use an imaging system conduct in 3D studies of plumes from volcanoes on the Earth's surface. Separated from launch vehicle at L+57 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:30 | 6973 | 0.0006 | 591 | 599 | 96.58 | 97.75 | 81 | 22:53 | | | |
in space
|
| 8U Cubesat from the local givernment of Bavaria, Germany. Equipped with a high resolution Earth imaging system to study natural resources. Separated from launch vehicle at L+56 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:31 | 6973 | 0.0005 | 591 | 599 | 96.58 | 97.75 | 85 | 22:53 | | | TOM 2 (Telematics earth Observation Mission 2) 2026-156AX 69914 |
in space
|
| 3U Cubesat from a consortium led by Zentrum für Telematik (ZFT) of Würzburg, Germany. One of a group of three satellites carried on the same launch, to fly in formation and use an imaging system conduct in 3D studies of plumes from volcanoes on the Earth's surface. Separated from launch vehicle at L+60 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:33 | 6974 | 0.0004 | 593 | 599 | 96.60 | 97.76 | 80 | 22:53 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+60 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:18 | 6970 | 0.0009 | 586 | 598 | 96.52 | 97.75 | 107 | 22:53 | | | |
in space
|
| Small satellite from Open Cosmos funded by the regional government of the Balearic Islands, Spain. Carries an Earth imaging system, equipped with AI for image processing and fitted with a laser communication system for space to ground use. Separated from launch vehicle at L+62 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:54 | 6970 | 0.0009 | 585 | 598 | 96.52 | 97.75 | 107 | 22:53 | | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+61 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 16:30 | 6970 | 0.0009 | 585 | 598 | 96.52 | 97.75 | 106 | 22:53 | | | Centauri-9 2026-156BH 69924 |
in space
|
| Mission details to follow. Separated from launch vehicle at L+57 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:52 | 6969 | 0.0010 | 585 | 598 | 96.51 | 97.75 | 106 | 22:53 | | | Replicator-2 2026-156BL 69927 |
in space
|
| Mission details to follow. Separated from launch vehicle at L+61 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 06:48 | 6969 | 0.0010 | 584 | 598 | 96.50 | 97.75 | 113 | 22:53 | | | GRITSS (Geodetic Reference Instrument Transponder for Small Satellites) 2026-156BQ 69931 |
in space
|
| Mission details to follow. Separated from launch vehicle at L+56 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:49 | 6969 | 0.0011 | 583 | 598 | 96.49 | 97.75 | 106 | 22:53 | | | |
in space
|
| 16U Cubesat - demonstrator for the United Arab Emirates' planned constellation to improve the precision of existing space-based navigation systems. Separated from launch vehicle at L+55 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:45 | 6968 | 0.0012 | 581 | 598 | 96.47 | 97.75 | 107 | 22:53 | | | |
in space
|
| 3U Cubesat from a group of ESA states aimed at testing/verifying security systems for satellites on orbit.. Separated from launch vehicle at L+55 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:47 | 6968 | 0.0012 | 582 | 598 | 96.48 | 97.75 | 104 | 22:53 | | | CloudCT precursor 2026-156BY 69939 |
in space
|
| 3U Cubesat -demonstrator for systems to be used in a future constellation of imaging satellites studying small clouds in the Earth's atmosphere. Separated from launch vehicle at L+58 minutes. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 13:11 | 6968 | 0.0011 | 582 | 598 | 96.48 | 97.76 | 115 | 22:53 | | | Lemur 2 (Eleonore) 2026-156BZ 69940 |
in space
|
3U? Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. One of ten similar satellites carried on this launch. Separated from launch vehicle at L+55 minutes.
All satellites were injected into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2026 Jul 20, 14:46 | 6968 | 0.0012 | 582 | 598 | 96.48 | 97.76 | 109 | 22:53 | | | BOHR (Betavoltaic Orbital High-Reliability) 2026-156xx |
in space
|
| Mission details to follow. Separated from launch vehicle at L+58 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+56 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+64 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+67 minutes. |
| Orbit parameters awaited | | IPoS (Interoperability Protocol over Satellite) 2026-156xx |
in space
|
| Mission details to follow. Separated from launch vehicle at L+56 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+63 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+59 minutes. |
| Orbit parameters awaited | | KOYO (Kinetic Optical Yaw Observer) 2026-156xx |
in space
|
| Mission details to follow. Separated from launch vehicle at L+55 minutes. |
| Orbit parameters awaited | | MARMOTSat (Mission for Atmospheric Radio Measurements with Open-source Technology Satellite) 2026-156xx |
in space
|
| Mission details to follow. Separated from launch vehicle at L+56 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+60 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+57 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+64 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+64 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+59 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+55 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+62 minutes. |
| Orbit parameters awaited | | SCION-X (Scintillation and IONosphere eXtended) 2026-156xx |
in space
|
| Mission details to follow. Separated from launch vehicle at L+58 minutes. |
| Orbit parameters awaited | | SPEAR 1A (Space Power and Energy Advanced Recon 1A) 2026-156xx |
in space
|
| Mission details to follow. Separated from launch vehicle at L+61 minutes. |
| Orbit parameters awaited | | SPEAR 1B (Space Power and Energy Advanced Recon 1B) 2026-156xx |
in space
|
| Mission details to follow. Separated from launch vehicle at L+61 minutes. |
| Orbit parameters awaited | | SPEAR 1C (Space Power and Energy Advanced Recon 1C) 2026-156xx |
in space
|
| Mission details to follow. Separated from launch vehicle at L+61 minutes. |
| Orbit parameters awaited | | |
in space
|
| Mission details to follow. Separated from launch vehicle at L+55 minutes. |
| Orbit parameters awaited | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 7
Life <1 day
|
| Launched Transporter 16 Rideshare mission. Caused to re-enter above the eastern Pacific Ocean at about 10:30 UTC, after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-157 Falcon 9 Block 5 (Starlink Group 10-42)
Cape Canaveral Space Force Station | 2026 Jul 9, 09:25 UTC | Starlink 37886 2026-157A 69943 |
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 09:28 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 15, 04:00 | 6673 | 0.0001 | 294 | 295 | 90.41 | 53.16 | 67 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 9
Life <1 day
|
| Launched Starlink Group 10-42. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-158 CZ 10B (Y-1)
Hainan Commercial Zone, Wenchang Space Centre | 2026 Jul 10 UTC | Hulianwang Jishu Shiyan 11 (Internet Connectivity Test 11) 2026-158A 69972 |
in space
|
| Second generation test satellite for Chinese government communications system for use by Internet-connected devices. Individual satellites are built by a variety of manufacturers and 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
( ° ) | | |
| 2026 Jul 10, 20:23 | 7186 | 0.0005 | 804 | 812 | 101.04 | 49.99 | 287 | | | | CZ 10B second stage 2026-158C 69974 |
in space
|
| Launched Hulianwang Jishu Shiyan 11. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 10, 19:59 | 7057 | 0.0198 | 540 | 819 | 98.34 | 49.97 | 185 | | | |
2026-159 Falcon 9 Block 5 (Starlink Group 17-48)
Vandenberg Space Force Base | 2026 Jul 11, 03:01 UTC | Starlink 38024 2026-159A 69975 |
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 04:03 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 14, 00:53 | 6647 | 0.0000 | 269 | 269 | 89.89 | 97.28 | 234 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 11
Life <1 day
|
| Launched Starlink Group 10-48. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-160 Falcon 9 Block 5 (Starlink Group 15-14)
Vandenberg Space Force Base | 2026 Jul 14, 01:28 UTC | Starlink 38128 2026-160A 100001 |
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 02:29 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 22, 01:27 | 6711 | 0.0006 | 329 | 337 | 91.18 | 70.00 | 271 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 14
Life <1 day
|
| Launched Starlink Group 15-17. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-161 Falcon 9 Block 5 (Starlink Group 10-45)
Cape Canaveral Space Force Station | 2026 Jul 14, 09:10 UTC | Starlink 37844 2026-161A 100028 |
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 10:13 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 21, 20:00 | 6678 | 0.0001 | 299 | 301 | 90.52 | 53.16 | 63 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 14
Life <1 day
|
| Launched Starlink Group 10-45. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-162 Soyuz 2.1a
Baikonur Cosmodrome | 2026 Jul 14, 14:47 UTC | Soyuz MS-29 (Soyuz 11F732A48 № 759) 2026-162A 100057 |
in space
|
| Crew to ISS - Pyotr Dubrov and Anna Kikina, (both Roscosmos) and Anil Menon (NASA) . Separated from launch vehicle at 14:56 UTC. Docked with ISS Prichal module at 17:52 UTC. Initial orbit similar to launch vehicle upper stage. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 14, 20:43 | 6798 | 0.0007 | 415 | 424 | 92.96 | 51.63 | 297 | | | | Soyuz third stage 2026-162B 100058 |
Re-entered - 2026 Jul 17
Life 3 days
|
| Launched Soyuz MS-29. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 15, 23:03 | 6574 | 0.0016 | 185 | 207 | 88.41 | 51.65 | 78 | | | |
2026-163 Falcon 9 Block 5
Vandenberg Space Force Base | 2026 Jul 16, 20:32 UTC | SDA Transport Layer 510 (Praetorian SDA 510) 2026-163A 100059 |
in space
|
Operational Tranche 1 satellite built by York Space Systems for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". One of twenty one similar satellites carried on this launch. Equipped with an optical communications system be used to collect data from active target tracking satellites in the constellation for onward relay to ground stations.
All satellites were injected into similar orbits. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 23, 23:26 | 7323 | 0.0013 | 935 | 954 | 103.93 | 81.48 | 189 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 16
Life <1 day
|
| Launched SDA T1TL-E group. Caused to re-enter above the southern Atlantic Ocean at about 22:40 UTC after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-164 Vikram 1 (Aagaman)
Satish Dhawan Space Centre, Sriharikota | 2026 Jul 18, 06:35 UTC | Solaras S3 2026-164B 100082 |
in space
|
| 3U Cubesat from Akshath Aerospace of India - carries a solar radiation sensor and an amateur radio slow scan TV system. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 18, 10:37 | 6825 | 0.0007 | 441 | 452 | 93.51 | 59.93 | 311 | | | | |
in space
|
| 3U Cubesat from Skyroot Aerospace carrying sensors to monitor performance of the launch vehicle including an imaging system. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 18, 10:37 | 6825 | 0.0007 | 442 | 452 | 93.52 | 59.93 | 269 | | | | Vikram 1 fourth stage 2026-164A 100080 |
in space
|
| Carried two Cubesats on first launch of commercially developed rocket from Skyrootoot Aerospace of India. Also hosted, but not intended for release, space technology demonstrations from Cosmoserve (India) and DCubed (Germany). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 18, 12:11 | 6825 | 0.0009 | 441 | 454 | 93.53 | 59.93 | 292 | | | |
2026-165 Soyuz-2.1b
Plesetsk Cosmodrome | 2026 Jul 19, 17:51 UTC | Rassvet-3 17 2026-165A 100083 |
in space
|
One of sixteen simultaneously-launched Internet communications satellites. Part of a planned constellation of 300 satellites.
All satellites were launched into similar orbits |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 23, 10:52 | 6686 | 0.0028 | 289 | 327 | 90.69 | 82.30 | 63 | | | | Soyuz third stage 2026-165S 100142 |
in space
|
| Launched cluster of Rassvet satellites. Launch time is estimate based on an observation from the Subaru telescope, Hawaii on July 20. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 23, 12:24 | 6687 | 0.0027 | 291 | 327 | 90.70 | 82.29 | 62 | | | |
2026-166 Falcon 9 Block 5 (Starlink Group 17-39)
Vandenberg Space Force Base | 2026 Jul 21, 14:49 UTC | |
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 15:50 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 28, 14:00 | 6701 | 0.0002 | 322 | 324 | 90.99 | 97.28 | 97 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 21
Life <1 day
|
| Launched Starlink Group 17-39. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-167 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2026 Jul 21, 21:15 UTC | MRV 1 (Mission Robotic Vehicle 1) 2026-167A 100125 |
in space
|
| Northrop Grumman satellite support vehicle for GEO. Reportedly will install an additional set of observational instruments onto an existing US classified ESPA Ring satellite. Separated from launch vehicle at 21:50 UTC. Catalogue Number, Designation and orbit to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 23, 07:35 | 28915 | 0.7687 | 309 | 44765 | 815.53 | 25.63 | 181 | | | | MEP 1 (Mission Extension Pod 1) 2026-167B 100126 |
in space
|
| Northrop Grumman satellite support vehicle. Will link up to an existing on-orbit satellite to supply station-keeping service and thereby extend mission life. Separated from launch vehicle at 22:00 UTC. Catalogue Number, Designation and orbit to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 23, 07:38 | 28945 | 0.7690 | 309 | 44826 | 816.82 | 25.63 | 181 | | | | MEP 2 (Mission Extension Pod 2) 2026-167C 100127 |
in space
|
| Northrop Grumman satellite support vehicle. Will link up to an existing on-orbit satellite to supply station-keeping service and thereby extend mission life. Separated from launch vehicle at 22:10 UTC. Catalogue Number, Designation and orbit to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 22, 18:04 | 28914 | 0.7688 | 307 | 44765 | 815.49 | 25.63 | 180 | | | | MEP 3 (Mission Extension Pod 3) 2026-167D 100128 |
in space
|
| Northrop Grumman satellite support vehicle. Will link up to an existing on-orbit satellite to supply station-keeping service and thereby extend mission life. Separated from launch vehicle at 22:20 UTC. Catalogue Number, Designation and orbit to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 23, 07:37 | 28938 | 0.7689 | 309 | 44811 | 816.53 | 25.64 | 181 | | | | Falcon 9 second stage uncalalogued |
Re-entered - 2026 Jul 22
Life 1 day
|
| Launched MRV 1 and three MEP vehicles. Caused to re-enter above the central Pacific Ocean July 22 at about 11:20 UTC, after releasing satellites. |
| Orbit parameters awaited | |
2026-168 Gravity 1 (Y-4)
Mobile floating platform, East China Sea - 31°.2 N, 123°.7 E | 2026 Jul 22, 02:54 UTC | |
in space
|
| Earth observation satellite - equipped with an optical imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0019 | 524 | 551 | 95.40 | 97.54 | 335 | 10:59 | | | |
in space
|
| Earth observation satellite - equipped with an optical imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0019 | 524 | 551 | 95.40 | 97.54 | 335 | 10:59 | | | |
in space
|
| Earth observation satellite - equipped with a radar imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0019 | 524 | 551 | 95.40 | 97.54 | 335 | 10:59 | | | |
in space
|
| Earth observation satellite - equipped with a radar imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0019 | 524 | 551 | 95.40 | 97.54 | 335 | 10:59 | | | |
in space
|
| Earth observation satellite - equipped with a radar imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0019 | 524 | 551 | 95.40 | 97.54 | 335 | 10:59 | | | |
in space
|
| Earth observation satellite - equipped with a radar imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0019 | 524 | 551 | 95.40 | 97.54 | 335 | 10:59 | | | |
in space
|
| Demonstrator/test satellite carrying a range of potential future satellite sub-systems including an Earth imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0019 | 524 | 551 | 95.40 | 97.54 | 335 | 10:59 | | | |
in space
|
| Multispectral Earth imaging satellite equipped with multiple Earth imaging systems. Also carries an onboard data processing system for image processing prior to transmission to the ground. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0019 | 524 | 551 | 95.40 | 97.54 | 335 | 10:59 | | | Zi Dingxiang 3 (Lilac 3) 2026-168xx |
in space
|
| Small satellite as a demonstrator of a disc-shaped design. Equipped with a VLF radio transmitter/receiver to study the characteristics of ionospheric plasma waves and space-to-ground propagation of VLF transmissions |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6916 | 0.0019 | 524 | 551 | 95.40 | 97.54 | 335 | 10:59 | | | Gravity 1 fourth stage 2026-168K 100138 |
in space
|
| Launched cluster of small satellites. perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 22, 05:27 | 6804 | 0.0154 | 321 | 531 | 93.09 | 97.54 | 77 | | | |
2026-169 CZ 3B
Xichang Space Centre | 2026 Jul 23, 12:00 UTC | Tianlian 2-06 2026-169A 100140 |
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 July 23 at around 18:00 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 Jul 23, 17:43 | 24392 | 0.7297 | 215 | 35813 | 631.89 | 27.01 | 179 | | | | CZ 3B fourth stage 2026-169B 100141 |
in space
|
| Launched Tianlian 2-06. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 23, 17:45 | 24497 | 0.7326 | 172 | 36065 | 635.94 | 27.02 | 179 | | | |
2026-170 Lijian 1 (Y-15)
Dongfeng Commercial Zone, Jiuquan Space Centre | 2026 Jul 23, 23:33 UTC | |
in space
|
| Satellite developed by Liangxi Aerospace Technology Group and Aotian Technology of China. First Chinese commercial satellite for space debris monitoring and first in the LX-30 constellation. Equipped with wide-field survey and high-resolution imaging systems, |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6922 | 0.0015 | 533 | 554 | 95.52 | 97.55 | 282 | 06:00 | | | Jitianxing A-04 2026-170xx |
in space
|
| Possible demonstrator of a space-based computing and AI system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6922 | 0.0015 | 533 | 554 | 95.52 | 97.55 | 282 | 06:00 | | | Tianyi 48 (Chenguang- 1) 2026-170xx |
in space
|
| Technology demonstration satellite carrying an on-orbit data centre. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6922 | 0.0015 | 533 | 554 | 95.52 | 97.55 | 282 | 06:00 | | | |
in space
|
| Multispectral Earth imaging satellite equipped with multiple Earth imaging systems. Also carries an onboard data processing system for image processing prior to transmission to the ground. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6922 | 0.0015 | 533 | 554 | 95.52 | 97.55 | 282 | 06:00 | | | Yinglong Fengguang-1 2026-170xx |
in space
|
| Commercial meteorological satellite developed by Shanghai Xuntian Qianhe Space Technology for Jiangsu Yinglong Satellite Technology. Equipped with microwave temperature and humidity sounders, and an infrared imaging system. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6922 | 0.0015 | 533 | 554 | 95.52 | 97.55 | 282 | 06:00 | | | Lijian 1 third stage uncatalogued |
Re-entered - 2026 Jul 24
Life 1 day
|
| Launched cluster of five satellites. Caused to reenter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-171 Falcon 9 Block 5 (Starlink Group 17-51)
Vandenberg Space Force Base | 2026 Jul 25, 15:51 UTC | Starlink 38182 2026-171A 100148 |
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 16:53 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 29, 22:46 | 6660 | 0.0009 | 276 | 288 | 90.15 | 97.28 | 318 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Jul 25
Life <1 day
|
| Launched Starlink Group 17-51. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-172 CZ 7A
Wenchang Space Centre | 2026 Jul 29, 11:50 UTC | Tianlian 3-01 2026-172A 100172 |
in space
|
| Third 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 July 29 at around 17:40 UTC. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2026 Jul 29, 17:34 | 24384 | 0.7295 | 217 | 35795 | 631.56 | 15.44 | 180 | | | | CZ 7A fourth stage 2026-172B 100173 |
in space
|
| Launched Tianlian 3-01. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 29, 17:28 | 23660 | 0.7239 | 154 | 34410 | 603.65 | 15.41 | 179 | | | |
2026-173 CZ 6A (Y-18)
Taiyuan Space Centre | 2026 Jul 30, 01:00 UTC | Tongxin Jishu Shiyan 27A (Communication Technology Test 27A, TJS 27A) 2026-173A 100174 |
in space
|
| One of a pair of simultaneously-launched satellites described as "mainly used for satellite communication, radio and television, data transmission and other services, and carries out relevant technical tests and verification". |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Aug 1, 15:39 | 7532 | 0.0007 | 1149 | 1159 | 108.42 | 64.79 | 231 | | | | Tongxin Jishu Shiyan 27B (Communication Technology Test 27B, TJS 27B) 2026-173C 100176 |
in space
|
| One of a pair of simultaneously-launched satellites described as "mainly used for satellite communication, radio and television, data transmission and other services, and carries out relevant technical tests and verification". |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Jul 31, 14:21 | 7531 | 0.0006 | 1148 | 1158 | 108.41 | 64.79 | 239 | | | | |
in space
|
| Launched Tongxin Jishu Shiyan 27A & B. Perigee lowered after releasing satellites. Initial orbit listed is an estimate based on limited orbit information from Space-Track. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Aug 1, 07:18 | 7428 | 0.0098 | 977 | 1123 | 106.18 | 64.80 | 111 | | | |
2026-174 Falcon 9 Block 5 (NRO L-95)
Cape Canaveral Space Force Station | 2026 Jul 30, 07:10 UTC | USA 619 (NOSS 4-06?, Intruder?) 2026-174A 100178 |
in space
|
| US government satellite from the National Reconnaissance Office. Latest successor to the NOSS (Navy Ocean Surveillance System) for electronic intelligence gathering (ELINT). |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 7484 | 0.0127 | 1011 | 1201 | 107.39 | 63.44 | 182 | | | | Falcon 9 second stage uncatalogued |
in space
|
| Launched USA 619. Caused to re-enter above the eastern Pacific Ocean at around 08:40 UTC, after releasing the satellite. Completed less than one circuit of the Earth but reached orbital velocity. |
| Not Catalogued - orbit parameters unavailable | |
2026-175 Falcon 9 Block 5 (Starlink Group 17-52)
Vandenberg Space Force Base | 2026 Aug 1, 03:08 UTC | |
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 04:06 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Aug 4, 18:00 | 6667 | 0.0002 | 288 | 290 | 90.29 | 97.29 | 72 | | | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Aug 1
Life <1 day
|
| Launched Starlink Group 17-52. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-176 CZ 8A (Y-10)
Hainan Commercial Zone, Wenchang Space Centre | 2026 Aug 4, 08:52 UTC | Hulianwang Digui 23-01 (Satellite Low Orbit Internet Group 23-01) 2026-176A 100203 |
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. |
| Orbit parameters awaited | | CZ 8A third stage 2026-176K 100212 |
in space
|
| Launched Hulianwang Digui group 23. Perigee lowered after releasing satellites. |
| Orbit parameters awaited | |
2026-177 Falcon 9 Block 5 (Starlink Group 17-53)
Vandenberg Space Force Base | 2026 Aug 4, 17:05 UTC | |
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 18:06 UTC.
All satellites expected to be injected initially into similar orbits at 250-300 km altitude. |
| Orbit parameters awaited | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Aug 4
Life <1 day
|
| Launched Starlink Group 17-53. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2026-178 Jielong 3 (Y-12)
Ship-borne launch platform, Yellow Sea - 36° N, 121.5° E | 2026 Aug 5, 02:38 UTC | Dongfang Huiyan Gao Guangpu 01 (Dongfang Xinglian 05) 2026-178A 100237 |
in space
|
| Remote sensing satellite equipped with AI software capable of selecting areas of interest by comparing images with previous passes over the same area. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Aug 5, 10:26 | 7167 | 0.0013 | 779 | 798 | 100.63 | 98.56 | 289 | | | | Dongfang Huiyan Gao Guangpu 02 (Dongfang Xinglian 06) 2026-178B 100238 |
in space
|
| Remote sensing satellite equipped with AI software capable of selecting areas of interest by comparing images with previous passes over the same area. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Aug 5, 12:07 | 7168 | 0.0010 | 783 | 796 | 100.65 | 98.55 | 334 | | | | Jielong 3 fourth stage 2026-178C 100239 |
in space
|
| Launched pair of Dongfang Huiyan High Spectrum satellites. Perigee lowered after releasing satellites. |
| Orbit parameters awaited | |
2026-179 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2026 Aug 5, 07:49 UTC | BlueBird 13 (SpaceMobile 013) 2026-179A 100240 |
in space
|
| Commercial 5G broadband satellite from US company AST Spacemobile to provide direct mobile phone services from orbit. One of three similar satellites carried on this launch. Released from launch vehicle at 08:36 UTC. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Aug 5, 09:18 | 6905 | 0.0005 | 524 | 531 | 95.18 | 52.99 | 14 | | | | BlueBird 12 (SpaceMobile 012) 2026-179B 100241 |
in space
|
| Commercial 5G broadband satellite from US company AST Spacemobile to provide direct mobile phone services from orbit. One of three similar satellites carried on this launch. Released from launch vehicle at 08:41 UTC. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Aug 5, 09:18 | 6904 | 0.0004 | 523 | 528 | 95.15 | 53.00 | 306 | | | | BlueBird 11 (SpaceMobile 011) 2026-179C 100242 |
in space
|
| Commercial 5G broadband satellite from US company AST Spacemobile to provide direct mobile phone services from orbit. One of three similar satellites carried on this launch. Released from launch vehicle at 08:46 UTC. Catalogue Number and Designation to be confirmed. |
| Orbit parameters awaited | | Falcon 9 second stage uncatalogued |
Re-entered - 2026 Aug 5
Life <1 day
|
| Launched triplet of Bluebird satellites. Caused to re-enter above the Indian Ocean at about 10:15 UTC, after releasing satellites. Orbit shown is probably the pre-disposal one. Space-Track issued the info against 100242/2026-179C. |
epoch (UTC) | s-m axis
( km ) |
eccentricity | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2026 Aug 5, 09:17 | 6881 | 0.0125 | 417 | 589 | 94.68 | 53.52 | 239 | | | |
|
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