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| 2022 - 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, and the source observations can often be found in the web-based Seesat-L discussion group. Occasionally, orbits are estimated by myself from public data.
Space-Track occasionally fails to allocate names to objects in its catalogue. In these cases, the names are derived from public information.
Apogee and perigee are measured against a spherical Earth with a radius of 6378.145 km assumedto 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.
2022-001 Falcon 9 Block 5 (Starlink Group 4-5)
Kennedy Space Center | 2022 Jan 6, 21:49 | Starlink 3321 2022-001A 50803 |
in space
|
One member of a simultaneously-launched cluster of forty nine LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 22:04 UTC.
All satellites were injected initially into similar orbits at 200-300 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 11, 20:00 | 6668 | 0.0054 | 254 | 326 | 90.31 | 53.22 | 180 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jan 6
Life <1 day
|
| Launched forty nine Starlink satellites. Caused to re-enter above the south Atlantic/south western Indian Ocean about 00:59 UTC, 1.3 circuits after lift-off. |
| Not Catalogued - orbit parameters unavailable | |
2022-002 Falcon 9 Block 5 (Transporter 3)
Cape Canaveral Space Force Station | 2022 Jan 13, 15:25 | FossaSat-2E1 (WISeSAT 1) 2022-002B 50985 |
Re-entered - 2023 Jun 23
Life 526 days
|
2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from EXOport 6 at 16:31 UTC.
One of six similar satellites carried on the Transporter 3 launch.
All are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 17:00 | 6903 | 0.0014 | 515 | 535 | 95.14 | 97.51 | 211 | | | | |
Re-entered - 2024 Nov 8
Life 1030 days
|
| Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Released from launch vehicle at 16:47 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 21:51 | 6907 | 0.0010 | 522 | 536 | 95.21 | 97.51 | 213 | | | | ION SCV-004 (Elysian Eleonora) 2022-002K 50993 |
in space
|
Satellite Carrier Vehicle built by D-Orbit - released from launch vehicle at 16:49 UTC carrying a small group of satellites for release 2022 Jan-Feb after departure from Falcon 9:
Dodona - Jan 24?
Labsat - Jan 28
Stork 1 - Jan 31
Stork 2 - Feb 3
SW1FT - Feb 4
VZLUSat 2 - Jan 26
Also hosts a payload not designed to be released as a separate satellite:
Unibap - on-orbit cloud computing demonstrator. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 23:26 | 6907 | 0.0010 | 522 | 536 | 95.21 | 97.51 | 215 | | | | MDASat-1a (Maritime Domain Awareness Satellite) 2022-002M 50995 |
in space
|
2U Cubesat from the French South African Institute of Technology. Equipped with an AIS receiver to relay short messages and navigational information from ships at sea. Released from launch vehicle at 16:36 UTC.
One of three similar satellites carried on the Transporter 3 launch.
All are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 23:27 | 6907 | 0.0009 | 523 | 535 | 95.22 | 97.50 | 210 | | | | |
Re-entered - 2024 Aug 4
Life 934 days
|
1U Cubesat from the Herzliya Science Center in Israel, carring an amateur radio payload for education purposes. Released from launch vehicle at 16:33 UTC. Identification based on amateur radio observations.
One of eight similar satellites carried on the Transporter 3 launch.
Contacts reported with all of the amateur radio payloads. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 23:27 | 6907 | 0.0009 | 523 | 535 | 95.21 | 97.50 | 211 | | | | |
Re-entered - 2023 Nov 1
Life 657 days
|
2p PocketQube from Ariel University, Israel. Equipped with an imaging system and an amateur radio payload. Released from EXOport 6 at 16:27 UTC.
One of two similar satellites carried on the Transporter 3 launch.
SATLLA-2A is reported by its owners as having failed to activate after release from the launch vehicle. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 23:23 | 6905 | 0.0013 | 518 | 536 | 95.17 | 97.52 | 215 | | | | Flock 4X-1 2022-002AK 51017 |
Re-entered - 2024 Nov 6
Life 1028 days
|
3U Cubesat - part of Planet's Flock 4X cluster of second generation imaging satellites. Released from the launch vehicle in a fifteen minute sequence commencing at 16:31 UTC.
One of forty four similar satellites carried on the Transporter 3 launch.
All are in similar orbits and are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 23:23 | 6905 | 0.0012 | 519 | 536 | 95.18 | 97.51 | 215 | | | | Lemur-2 (Ramonamae) 2022-002AP 51021 |
Re-entered - 2024 May 29
Life 867 days
|
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. Lemur-2 satellites are named after development and support team members. Released from launch vehicle at 16:32 UTC.
One of four similar satellites carried on the Tranporter 3 launch.
All are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 17:07 | 6908 | 0.0009 | 524 | 536 | 95.23 | 97.51 | 224 | | | | Grizu-263A 2022-002AT 51025 |
Re-entered - 2023 Oct 3
Life 628 days
|
| 1p PocketQube, Mission details to follow. Released from EXOport 6 at 16:25 UTC. Initial identification by Nico Janssen - based on radio tracking. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 17:02 | 6905 | 0.0013 | 518 | 536 | 95.17 | 97.52 | 216 | | | | Sich 2-1 (Sich 2-30) 2022-002AY 51030 |
in space
|
| Small satellite from Ukraine's Pivdenne (Yuzhnoye) State Design Office, to monitor the use of land, vegetation, forest, water resources and to reduce the consequences of natural disasters. Released from launch vehicle at 16:48 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 23:26 | 6907 | 0.0010 | 522 | 536 | 95.21 | 97.51 | 216 | | | | |
Re-entered - 2024 Feb 7
Life 755 days
|
| 1p PocketQube built by Nepalese university students and engineers, carries a gamma radiation sensor to be used as an aid in teaching. Also carries an amateur radio payload. Released from EXOport 6 at 16:30 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 17:02 | 6905 | 0.0013 | 518 | 536 | 95.17 | 97.51 | 216 | | | | Unicorn-2D 2022-002BA 51032 |
Re-entered - 2023 Apr 13
Life 455 days
|
3p PocketQube satellite as a demonstrator of a future constellation of night-time imaging satellites to study global light pollution.. Released from EXOport 6 at 16:25 UTC.
One of three similar satellites carried on the Transporter 3 launch.
Only one is accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 17:01 | 6904 | 0.0011 | 518 | 534 | 95.16 | 97.50 | 201 | | | | Lemur-2 + OroraTech 1 (Rohovithsa) 2022-002BE 51036 |
Re-entered - 2024 Aug 3
Life 933 days
|
6U Cubesat from Spire Global carrying the standard Lemur-2 payload but in a 6U chassis. The other half of the satellite carries a payload from German company Ororatech consisting of a thermal infrared imager to detect, record and analyse the incidence of wildfires on the Earth's surface. Released from launch vehicle at 16:32 UTC.
One of three similar satellites carried on the Transporter 3 launch.
All are accounted for but the supplementary payloads of the other two are unknown. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 17:07 | 6908 | 0.0009 | 524 | 536 | 95.23 | 97.51 | 225 | | | | IRIS-A (Intelligent Remote Sensing and Internet Satellite) 2022-002BN 51044 |
in space
|
| 2U Cubesat from the Nationa Cheng Kung University of Taiwan. Equipped with an imaging system and a comms package for relaying data from the ground via the Internet. Released from launch vehicle at 16:36 UTC. Initial identification by Nico Janssen - based on radio tracking. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 17:06 | 6908 | 0.0009 | 524 | 535 | 95.23 | 97.50 | 213 | | | | HYPSO-1 (Hyperspectral Satellite for Ocean Observation) 2022-002BX 51053 |
in space
|
| 6U Cubesat from the Norwegian University of Science and Technology to study biological activity near the ocean surface. Released from EXOport 6 at 16:28 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 15:32 | 6908 | 0.0008 | 525 | 536 | 95.24 | 97.50 | 223 | | | | Kepler 16 (Astraeus) 2022-002CB 51057 |
in space
|
6U Cubesat - Kepler Gen 1 satellite, part of a planned 140 satellite constellation from Kepler Aerospace carrying a high capacity communications system to provide links between other satellites and the ground, and a prototype of the company's Internet communications system. Released from launch vehicle at 16:36 UTC.
One of four similar satellites carried on the Transporter 3 launch.
All are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 15:32 | 6908 | 0.0008 | 525 | 536 | 95.24 | 97.51 | 217 | | | | |
in space
|
| 16U Cubesat (4x4) from UK company Sen. First in a constellation of video distribution satellites. Released from EXOport 6 at 16:27 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 15:32 | 6909 | 0.0009 | 524 | 536 | 95.24 | 97.51 | 232 | | | | BRO 5 (Breizh Reconnaissance Orbiter 5) 2022-002CF 51061 |
in space
|
| 6U Cubesat (3x2) from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Released from EXOport 6 at 16:29 UTC. Initial identification by Nico Janssen - based on radio tracking. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jan 18, 15:32 | 6909 | 0.0009 | 524 | 536 | 95.25 | 97.51 | 233 | 10:01 | | | DEWA-Sat 1 2022-002CM 51067 |
Re-entered - 2024 Oct 30
Life 1021 days
|
| 3U Cubesat from the Dubai Electricity and Water Authority, UAE to demonstrate internet connection of remote station in the area's electricity and water networks. Released from EXOport 6 at 16:28 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 15:33 | 6909 | 0.0007 | 526 | 536 | 95.26 | 97.50 | 232 | | | | |
in space
|
Small satellite fitted with a sythetic aperture radar for Earth surface imaging. Ultimately intended to be part of an eighteen satellite constellation. Released from EXOport 7 at 16:47 UTC.
One of two similar satellites carried on the Transporter 3 launch.
Both are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jan 18, 23:25 | 6906 | 0.0011 | 520 | 536 | 95.19 | 97.51 | 216 | 10:01 | | | Capella 7 (Whitney 5) 2022-002CS 51072 |
Re-entered - 2023 Aug 26
Life 590 days
|
Second generation satellite from Capella Space carrying Synthetic Aperture Radar for Earth imaging. Member of a planned thirty satellite constellation. Released from launch vehicle at 16:48 UTC.
One of two similar satellites carried on the Transporter 3 launch.
Both are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jan 18, 23:25 | 6906 | 0.0010 | 521 | 535 | 95.20 | 97.51 | 219 | 10:01 | | | |
Re-entered - 2023 Apr 4
Life 446 days
|
| 3U Cubesat from Singapore companies NuSpace and Aliena. Equipped with an electronic thruster and a comms package for relaying data from the ground via the Internet. Released from EXOport 6 at 16:28 UTC. Tentative identification from amateur observations using radio - Catalogue Number and Designation subject to confirmation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 15:20 | 6901 | 0.0013 | 513 | 532 | 95.08 | 97.52 | 253 | | | | |
Re-entered - 2024 Jan 9
Life 726 days
|
| 3p PocketQube satellite from the Technical University of Delft, Netherlands launched to demonstrate/verify the satellite design. Released from EXOport 6 at 16:24 UTC. Initial identification by Nico Janssen - based on radio tracking. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 18, 15:21 | 6901 | 0.0013 | 514 | 532 | 95.09 | 97.53 | 251 | | | | USA 320 (Starshield Demonstrator?) 2022-002CV 51075 |
Re-entered - 2024 Nov 28
Life 1050 days
|
| US government/military satellite, probably operated by, or for, the National Reconnaissance Office - SpaceX Starshield satellite that provides a hosting platform for a variety missions and uses the Starlink infrastructure for communications. Purpose unknown. Not originally declared in the manifest for this launch. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jan 18, 15:21 | 6901 | 0.0014 | 514 | 533 | 95.10 | 97.51 | 249 | 10:01 | | | 2022 Jan 22, 17:45 | 6906 | 0.0011 | 521 | 536 | 95.20 | 97.51 | 260 | 10:01 | | | 2023 Jan 31, 14:50 | 6906 | 0.0003 | 526 | 530 | 95.19 | 97.47 | 143 | 09:54 | | | 2024 Mar 23, 14:43 | 6890 | 0.0003 | 509 | 514 | 94.86 | 97.42 | 255 | 09:36 | | | USA 321 (Starshield Demonstrator?) 2022-002CX 51077 |
Re-entered - 2023 Apr 1
Life 443 days
|
| US government/military satellite, probably operated by, or for, the National Reconnaissance Office - SpaceX Starshield satellite that provides a hosting platform for a variety missions and uses the Starlink infrastructure for communications. Purpose unknown. Not originally declared in the manifest for this launch. Caused to re-enter through retro-fire. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jan 18, 15:22 | 6902 | 0.0014 | 514 | 533 | 95.11 | 97.51 | 247 | 10:01 | | | 2022 Jan 24, 18:56 | 6906 | 0.0011 | 521 | 535 | 95.19 | 97.51 | 255 | 10:01 | | | 2023 Jan 31, 14:48 | 6906 | 0.0004 | 526 | 530 | 95.19 | 97.47 | 195 | 09:55 | | | 2023 Feb 06, 11:56 | 6889 | 0.0002 | 509 | 512 | 94.83 | 97.48 | 54 | 09:55 | | | 2023 Feb 16, 04:47 | 6841 | 0.0003 | 461 | 465 | 93.86 | 97.47 | 102 | 09:55 | | | 2023 Feb 20, 10:18 | 6821 | 0.0001 | 442 | 444 | 93.44 | 97.47 | 82 | 09:56 | | | 2023 Feb 27, 11:41 | 6792 | 0.0002 | 413 | 415 | 92.84 | 97.47 | 90 | 09:57 | | | 2023 Mar 06, 11:50 | 6759 | 0.0001 | 380 | 381 | 92.16 | 97.46 | 83 | 09:59 | | | USA 322 (Starshield Demonstrator?) 2022-002CY 51078 |
Re-entered - 2023 Apr 2
Life 444 days
|
| US government/military satellite, probably operated by, or for, the National Reconnaissance Office - SpaceX Starshield satellite that provides a hosting platform for a variety missions and uses the Starlink infrastructure for communications. Purpose unknown. Not originally declared in the manifest for this launch. Caused to re-enter through retro-fire. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jan 18, 15:22 | 6902 | 0.0014 | 514 | 533 | 95.11 | 97.51 | 246 | 10:01 | | | 2022 Jan 21, 11:36 | 6906 | 0.0012 | 520 | 536 | 95.19 | 97.51 | 262 | 10:01 | | | 2023 Jan 31, 03:44 | 6906 | 0.0004 | 525 | 531 | 95.19 | 97.47 | 185 | 09:55 | | | 2023 Feb 07, 03:47 | 6885 | 0.0002 | 505 | 509 | 94.76 | 97.47 | 98 | 09:55 | | | 2023 Feb 16, 03:15 | 6841 | 0.0002 | 462 | 465 | 93.86 | 97.47 | 40 | 09:55 | | | 2023 Feb 20, 17:05 | 6821 | 0.0002 | 442 | 444 | 93.45 | 97.47 | 87 | 09:56 | | | 2023 Feb 27, 13:10 | 6789 | 0.0002 | 410 | 412 | 92.78 | 97.47 | 64 | 09:57 | | | 2023 Mar 06, 11:41 | 6757 | 0.0003 | 376 | 381 | 92.12 | 97.46 | 116 | 09:59 | | | USA 323 (Starshield Demonstrator?) 2022-002CZ 51079 |
Re-entered - 2023 Apr 2
Life 444 days
|
| US government/military satellite, probably operated by, or for, the National Reconnaissance Office - SpaceX Starshield satellite that provides a hosting platform for a variety missions and uses the Starlink infrastructure for communications. Purpose unknown. Not originally declared in the manifest for this launch. Caused to re-enter through retro-fire. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jan 18, 15:22 | 6902 | 0.0014 | 514 | 533 | 95.11 | 97.51 | 246 | 10:01 | | | 2022 Jan 25, 10:47 | 6906 | 0.0011 | 520 | 536 | 95.19 | 97.51 | 245 | 10:01 | | | 2023 Jan 31, 03:40 | 6906 | 0.0004 | 525 | 531 | 95.19 | 97.47 | 174 | 09:54 | | | 2023 Feb 06, 18:13 | 6887 | 0.0002 | 508 | 511 | 94.80 | 97.47 | 111 | 09:53 | | | 2023 Feb 13, 15:37 | 6853 | 0.0002 | 474 | 476 | 94.10 | 97.46 | 82 | 09:54 | | | 2023 Feb 20, 10:15 | 6821 | 0.0002 | 442 | 444 | 93.44 | 97.46 | 82 | 09:55 | | | 2023 Feb 27, 11:30 | 6788 | 0.0002 | 409 | 411 | 92.76 | 97.46 | 94 | 09:56 | | | 2023 Mar 06, 11:30 | 6755 | 0.0001 | 376 | 378 | 92.09 | 97.46 | 68 | 09:58 | | | |
Re-entered - 2024 May 27
Life 865 days
|
| 1.5p PocketQube satellite built by AMSAT Spain equipped with a SSTV camera module for Earth observation and an amateur radio package. Weak transmissions detected, indicating the radio aerials did not deploy properly. Released from EXOport 6 at 16:24 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 08, 21:57 | 6900 | 0.0014 | 512 | 532 | 95.08 | 97.52 | 173 | | | | |
Re-entered - 2024 May 23
Life 861 days
|
| 1.5p PocketQube satellite built jointly by AMSAT Spain and a group of European University students. Carries a sample of rock from Lanzarote and an amateur radio payload. Weak transmissions detected, indicating the radio aerials did not deploy properly. Released from EXOport 6 at 16:24 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 08, 21:58 | 6900 | 0.0015 | 512 | 533 | 95.08 | 97.52 | 173 | | | | |
Re-entered - 2024 May 23
Life 861 days
|
| 3U Cubesat from the Space Engineering Research Centre of the University of Southern California. Demonstrator mission for a range of satellite systems. Relesed from ION SCV probably Jan 24 around 06:00 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 04, 17:01 | 6904 | 0.0008 | 520 | 532 | 95.16 | 97.50 | 148 | | | | VZLUSat 2 (Výzkumný a Zkušební Letecký Ústav Satellite) 2022-002DF 51085 |
in space
|
| 3U Cubesat from the Czech Aerospace Research Centre carrying an Earth imaging system and a range of sensors to study x-rays and gamma radiation. Released from ION SCV-04 2022 Jan 26 at 15:02:31 UTC. Initial identification by Nico Janssen - based on radio tracking. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 04, 17:19 | 6910 | 0.0015 | 521 | 542 | 95.27 | 97.50 | 167 | | | | |
Re-entered - 2024 Sep 10
Life 971 days
|
| 3U Cubesat from SatRevolution of Poland testing the performance of space systems in microgravity. Released from ION SCV-04 2022 Jan 28 at about 07:30 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 04, 17:04 | 6904 | 0.0008 | 520 | 532 | 95.15 | 97.50 | 145 | | | | |
Re-entered - 2024 Apr 29
Life 837 days
|
| 3U Cubesat from SatRevolution of Poland. Part of a planned fourteen satellite constellation of Earth imaging satellites. Released from ION SCV-04 2022 Jan 31. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 04, 17:13 | 6909 | 0.0014 | 521 | 541 | 95.26 | 97.51 | 164 | | | | |
Re-entered - 2024 May 4
Life 842 days
|
| 3U Cubesat from SatRevolution of Poland. Part of a planned fourteen satellite constellation of Earth imaging satellites. Released from ION SCV-04 2022 Feb 3. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 04, 17:09 | 6905 | 0.0011 | 520 | 535 | 95.18 | 97.50 | 145 | | | | |
Re-entered - 2024 May 2
Life 840 days
|
| 3U Cubesat from SatRevolution of Poland. Carries an imaging system and an experimental computer system to process and analyse images onboard the satellite. Released from ION SCV-04 2022 Feb 4. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 10, 19:16 | 6907 | 0.0011 | 521 | 537 | 95.22 | 97.50 | 139 | | | | |
in space
|
3p PocketQube satellite from US company Mini-Cubes. Carries an internet comms package. Released from EXOport 6 at 16:30 UTC.
Status unknown. Probably either failed to release from the Falcon 9 or failed to activate. |
| Orbit parameters awaited | | Gossamer Piccolomini 2022-002xx |
in space
|
| 1U Cubesat from US company Lunasonde for geological studies from orbit. Demonstrator for an eventual constellation. Released from EXOport 6 at 16:28 UTC. |
| Orbit parameters awaited | | |
in space
|
2p PocketQube from Innova Space of Argentina as a demonstrator of the a satellite to provide internet connection. Released from EXOport 6 at 16:27 UTC.
Status unknown. Probably either failed to release from the Falcon 9 or failed to activate. |
| Orbit parameters awaited | | |
in space
|
| 1p PocketQube from PION Labs of Brazil, to demonstrate the satellite design. Carries a receiver transmitter to provide internet connectiona and an amateur radio payload. Released from EXOport 6 at 16:27 UTC. |
| Orbit parameters awaited | | |
in space
|
| 2p PocketQube satellite. Mission details to follow. Released from EXOport 6 at 16:24 UTC. |
| Orbit parameters awaited | | Unicorn 2TA-1 (Tartan Artibeus 1) 2022-002xx |
in space
|
| 1p PocketQube satellite from the Department of Electrical and Computer Engineering at Carnegie Mellon University. Demonstrator for a PocketQube powered by solar cells and testing onboard processing of sensor data. Released from EXOport 6 at 16:24 UTC. |
| Orbit parameters awaited | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jan 13
Life <1 day
|
| Launched Transporter 3 cluster of 105 satellites. Caused to re-enter above the western part of the Indian Ocean at about 18:00 UTC on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-003 LauncherOne (ST-27VPB)
Boeing 747, Pacific Ocean off California | 2022 Jan 13, 22:52 | PAN A (Pathfinder for Autonomous Navigation) 2022-003A 51094 |
Re-entered - 2024 Jan 30
Life 747 days
|
| 3U Cubesat from Cornell University to undertake rendezvous and docking with a companion satellite carried on the same launch vehicle. Part of NASA ELaNa-29 Cubesat cluster. Released from launch vehicle at 23:46 UTC. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 14, 22:32 | 6879 | 0.0006 | 497 | 505 | 94.63 | 44.98 | 295 | | | | TechEdSat 13 2022-003B 51095 |
Re-entered - 2024 Jul 13
Life 912 days
|
| 3U Cubesat from NASA Ames carrying an artificial intelligence/machine learning (AI/ML) module featuring a neuromorphic processor. Also carries a deployable aerobrake to hasten orbit decay at the end of its operational life. Released from launch vehicle at 23:46 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 14, 22:32 | 6878 | 0.0005 | 496 | 503 | 94.61 | 44.98 | 285 | | | | PAN B (Pathfinder for Autonomous Navigation) 2022-003C 51096 |
Re-entered - 2024 Aug 16
Life 946 days
|
| 3U Cubesat from Cornell University to undertake rendezvous and docking with a companion satellite carried on the same launch vehicle. Part of NASA ELaNa-29 Cubesat cluster. Released from launch vehicle at 23:46 UTC. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 14, 22:32 | 6877 | 0.0004 | 496 | 502 | 94.59 | 44.98 | 253 | | | | GEARRS 3 (Globalstar Risk Reduction Satellite) 2022-003D 51097 |
Re-entered - 2024 Aug 7
Life 937 days
|
| 3U Cubesat from Taylor University, investigating the feasibility of using the Globalstar satellite comms network for command and control of cubesats and other small satellite systems. Released from launch vehicle at 23:46 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 14, 18:47 | 6877 | 0.0004 | 496 | 501 | 94.59 | 44.98 | 274 | | | | |
Re-entered - 2023 Aug 29
Life 593 days
|
| 3U Cubesat from SatRevolution of Poland. Part of a planned fourteen satellite constellation of Earth imaging satellites. Released from launch vehicle at 23:46 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 15, 16:49 | 6875 | 0.0004 | 494 | 499 | 94.55 | 44.98 | 233 | | | | Lemur-2 + Adler 1 (Krywe) 2022-003F 51099 |
Re-entered - 2023 Sep 26
Life 621 days
|
| 6U Cubesat carrying the Austrian Particle Impact Detector (APID) to detect very small items of debris in LEO and a radar system with a 100m range. Design is based on the 3U Lemur-2 satellite from Spire but with specialised instrumentation alongside the standard Lemur-2 equipment. The satellite is named after Tom Krywe, current Chief Financial Officer of Spire. Released from launch vehicle at 23:46 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 14, 12:58 | 6875 | 0.0005 | 493 | 500 | 94.54 | 44.98 | 217 | | | | |
Re-entered - 2023 Jun 10
Life 513 days
|
| 3U Cubesat - equipped with a water powered thruster from SteamJet Systems. Released from launch vehicle at 23:46 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 14, 22:34 | 6874 | 0.0004 | 493 | 499 | 94.54 | 44.99 | 222 | | | | LauncherOne upper stage 2022-003H 51101 |
Re-entered - 2023 Oct 4
Life 629 days
|
| Launched seven smalll satellites. Perigee lowered after releasing satellites in order to accelerate orbit decay. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 14, 14:06 | 6838 | 0.0054 | 423 | 497 | 93.80 | 45.03 | 210 | | | |
2022-004 CZ 2D
Taiyuan Space Centre | 2022 Jan 17, 02:35 | Shiyan 13 (Test 13) 2022-004A 51102 |
in space
|
| Purpose unknown - described as "mainly used for space environment exploration and related technical tests". Orbit decayed naturally until mid January 2023 then perigee raised by 135 km followed by a further manoeuvre 2023 March. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jan 17, 17:14 | 7206 | 0.0653 | 357 | 1298 | 101.45 | 98.68 | 144 | 09:40 | | | 2023 Jan 12, 14:19 | 7190 | 0.0658 | 339 | 1285 | 101.12 | 98.62 | 174 | 09:44 | | | 2023 Jan 12, 19:50 | 7241 | 0.0587 | 437 | 1287 | 102.19 | 98.62 | 173 | 09:44 | | | 2023 Jan 13, 11:23 | 7256 | 0.0564 | 469 | 1287 | 102.52 | 98.62 | 170 | 09:44 | | | 2023 Jan 14, 14:53 | 7264 | 0.0566 | 474 | 1297 | 102.68 | 98.62 | 166 | 09:44 | | | 2023 Feb 21, 21:37 | 7263 | 0.0566 | 474 | 1296 | 102.67 | 98.60 | 58 | 09:39 | | | 2023 Feb 22, 13:07 | 7310 | 0.0514 | 556 | 1308 | 103.67 | 98.60 | 52 | 09:39 | | | 2023 Feb 23, 12:14 | 7323 | 0.0501 | 578 | 1312 | 103.95 | 98.61 | 48 | 09:38 | | | 2023 Feb 23, 16:49 | 7328 | 0.0502 | 582 | 1318 | 104.05 | 98.60 | 47 | 09:38 | | | CZ 2D second stage 2022-004B 51103 |
in space
|
| Launched Shiyan 13. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 17, 12:09 | 7204 | 0.0652 | 356 | 1295 | 101.42 | 98.68 | 145 | | | |
2022-005 Falcon 9 Block 5 (Starlink Group 4-6)
Kennedy Space Center | 2022 Jan 19, 02:02 | Starlink 3366 2022-005A 51104 |
in space
|
One member of a simultaneously-launched cluster of forty nine LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 02:17 UTC.
All satellites were injected initially into similar orbits at 200-300 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 24, 16:00 | 6669 | 0.0054 | 254 | 327 | 90.33 | 53.22 | 184 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jan 19
Life <1 day
|
| Launched forty nine Starlink satellites. Caused to re-enter above the south Atlantic/south western Indian Ocean about 04:10 UTC, 1.3 circuits after lift-off. |
| Not Catalogued - orbit parameters unavailable | |
2022-006 Atlas V 511
Cape Canaveral Space Force Station | 2022 Jan 21, 19:00 | USA 324 (GSSAP 5) 2022-006A 51280 |
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. Separated from launch vehicle Jan 22 at 01:35 UTC. Initial orbit based on ULA pre-launch data, others on amateur observations. 'USA' number is out of sequence. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Jan 22, 01:36 | 42514 | 0.0007 | 36106 | 36165 | 1453.97 | 0.00 | 351 | 95° west | | | USA 325 (GSSAP 6) 2022-006B 51281 |
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. Separated from launch vehicle Jan 22 at 01:45 UTC. Initial orbit based on ULA pre-launch data, others on amateur observations. 'USA' number is out of sequence. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Jan 22, 01:45 | 42499 | 0.0011 | 36075 | 36168 | 1453.22 | 0.00 | 341 | 95° west | | | Atlas V upper stage (Centaur) 2022-006C 51282 |
in space
|
| Launched GSSAP 5 & GSSAP 6. Orbit based on ULA data for the Geosynchronous Transfer Orbit. Currently in an orbit similar to the satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 21, 20:14 | 24658 | 0.7320 | 231 | 36329 | 642.25 | 25.97 | 0 | | | |
2022-007 CZ 4C
Jiuquan Space Centre | 2022 Jan 25, 23:44 | Ludi Tance 01-01 (L-SAR 01-01, Land Exploration 01-02) 2022-007A 51284 |
in space
|
| Earth surface studies satellite equipped with a large, high resolution, Synthetic Aperture Radar operating at L-band frequencies. Will work in conjunction with the L-SAR 01-02 satellite, launched 2022 Feb 26. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jan 26, 09:33 | 6976 | 0.0006 | 594 | 602 | 96.65 | 97.81 | 242 | 06:00 | | | 2022 Feb 08, 03:07 | 6982 | 0.0003 | 602 | 606 | 96.76 | 97.81 | 95 | 06:00 | | | 2022 Feb 12, 03:56 | 6981 | 0.0002 | 601 | 604 | 96.75 | 97.81 | 85 | 06:00 | | | CZ-4C upper stage 2022-007B 51285 |
in space
|
| Launched L-SAR 01A. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 26, 07:08 | 6897 | 0.0126 | 432 | 606 | 95.01 | 97.84 | 31 | | | |
2022-I01 Nanoracks Cubesat Deployer
International Space Station | 2022 Jan 26, 12:00 | GASPACS (Get Away Special Passive Attitude Control Satellite) 1998-067TB 51439 |
Re-entered - 2022 May 22
Life 116 days
|
| 1U Cubesat from Utah State University - one of four satellites in NASA's ELaNa 38 cluster, it will extend a 1m long inflatable boom to evaluate its use for supporting equipment and in satellite stabilisation. Allocation of Catalogue Number and Designation based on radio observations by amateur observers. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 28, 18:28 | 6794 | 0.0009 | 410 | 422 | 92.88 | 51.64 | 79 | | | | FEES 2 (Flexible Experimental Embedded Satellite) 1998-067TD 51441 |
Re-entered - 2022 Nov 16
Life 294 days
|
| 0.3U Cubesat - from Italian company GP Advanced Projects, carrying an imaging system, a message relay system and an amateur radio payload. Will test use of Iridium satellite system for data relay. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 28, 18:28 | 6794 | 0.0009 | 409 | 422 | 92.88 | 51.64 | 81 | | | | PATCOOL (Passive Thermal Coating Observatory Operating in Low-Earth Orbit) 1998-067TE 51442 |
Re-entered - 2022 Nov 18
Life 296 days
|
| 3U Cubesat - one of four satellites in NASA's ELaNa 38 cluster and sponsored by NASA, from the University of Florida to assess feasibility of using cryogenic surface coatings as a method of passive cooling. Actual release was 12:10 UTC, ten minutes behind FEES 2 and GASPACS. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 28, 18:28 | 6793 | 0.0009 | 409 | 421 | 92.87 | 51.64 | 91 | | | |
2022-I02 Nanoracks Cubesat Deployer
International Space Station | 2022 Jan 26, 13:30 | TARGIT (Tethering and Ranging mission of the Georgia Institute of Technology) 1998-067TC 51440 |
Re-entered - 2022 May 3
Life 97 days
|
| 3U Cubesat - one of four satellites in NASA's ELaNa 38 cluster, sponsored by NASA’s Undergraduate Student Instrument Program. It deployed a small inflatable target on a tether and used a miniaturised LiDAR imaging camera to create a 3D image of it. The target will later be released into independent orbit to allow imaging at longer distances. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 28, 18:28 | 6794 | 0.0009 | 409 | 422 | 92.88 | 51.64 | 78 | | | | 2022 Mar 29, 03:53 | 6754 | 0.0005 | 373 | 380 | 92.07 | 51.64 | 206 | | | | DAILI (Daily Atmospheric Ionospheric Limb Imager) 1998-067TF 51443 |
Re-entered - 2022 Jun 26
Life 151 days
|
| 6U Cubesat (6x1) - one of four satellites in NASA's ELaNa 38 cluster, to determine the daytime density of oxygen of the upper atmosphere, between 140 and 300 km, by analysing the spectrum of its dayglow. Actual release was 13:40 UTC, ten minutes behind TARGIT. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jan 28, 18:28 | 6793 | 0.0011 | 408 | 422 | 92.86 | 51.64 | 75 | | | |
2022-008 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2022 Jan 31, 23:11 | CSG-2 (COSMO-SkyMed Second Generation) 2022-008A 51444 |
in space
|
| Italian Space Agency second generation, follow-on, Earth imaging satellite equipped with synthetic aperture radar. Precise launch time 23:11:50 UTC, separated from launch vehicle upper stage Feb 1 at 00:11 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Feb 01, 07:22 | 7001 | 0.0004 | 620 | 626 | 97.16 | 97.90 | 128 | 17:45 | | | 2022 Feb 12, 05:07 | 6998 | 0.0002 | 619 | 621 | 97.10 | 97.89 | 89 | 17:46 | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Feb 1
Life 1 day
|
| Launched CSG 2. Caused to re-enter above the south eastern Pacific Ocean Feb 1 about 01:05 UTC, 1.3 circuits after lift-off. |
| Not Catalogued - orbit parameters unavailable | |
2022-009 Falcon 9 Block 5
Vandenberg Space Force Base | 2022 Feb 2, 20:27 | |
in space
|
| Government/military imaging reconnaissance satellite. Orbit details are based on amateur observation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6900 | 0.0010 | 515 | 529 | 95.07 | 97.40 | 160 | 12:10 | | | 2022 Apr 08, 23:12 | 6885 | 0.0023 | 491 | 522 | 94.75 | 97.40 | 33 | 12:08 | | | 2022 Jul 31, 22:49 | 6881 | 0.0021 | 489 | 518 | 94.68 | 97.40 | 12 | 12:06 | | | 2022 Sep 01, 20:37 | 6881 | 0.0020 | 489 | 516 | 94.67 | 97.41 | 268 | 12:06 | | | 2023 Mar 12, 23:03 | 6875 | 0.0012 | 489 | 505 | 94.55 | 97.41 | 90 | 12:05 | | | 2023 Aug 14, 23:21 | 6875 | 0.0003 | 495 | 499 | 94.56 | 97.41 | 68 | 12:05 | | | 2024 May 14, 22:18 | 6882 | 0.0010 | 497 | 510 | 94.69 | 97.42 | 166 | 12:02 | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Feb 2
Life <1 day
|
| Launched USA 326. Caused to re-enter with any surviving fragments hitting the Pacific Ocean near 42° north, 142° west at about 22:05 UTC on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-I03 JEM Small Satellite Orbital Deployer
International Space Station | 2022 Feb 3, 08:55 | |
Re-entered - 2023 Jan 16
Life 347 days
|
| 3U Cubesat - a collaboration between the UAE Space Agency and Bahrain’s National Space Science Agency to monitor and study terrestrial gamma ray flashes from thunderstorms and cumulus clouds. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 04, 20:43 | 6792 | 0.0011 | 407 | 421 | 92.85 | 51.65 | 108 | | | |
2022-I04 JEM Small Satellite Orbital Deployer
International Space Station | 2022 Feb 3, 10:30 | |
Re-entered - 2022 Jun 19
Life 136 days
|
| 1U Cubesat - from the Georgia Institute of Technology (USA). Demonstrator of the life-cycle of a university-built satellite from initial design to re-entry. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 04, 17:37 | 6794 | 0.0009 | 410 | 421 | 92.88 | 51.64 | 102 | | | |
2022-010 Falcon 9 Block 5 (Starlink Group 4-7)
Kennedy Space Center | 2022 Feb 3, 18:13 | Starlink 3181 2022-010F 51461 |
in space
|
One member of a simultaneously-launched cluster of forty nine LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 02:17 UTC.
All satellites were injected initially into similar orbits at 200-300 km altitude.
A solar storm shortly after launch caused higher than expected drag on the satellites, preventing them making orbit-raising manoeures. Many of them re-entered within a couple of weeks. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 08, 22:00 | 6663 | 0.0047 | 254 | 316 | 90.22 | 53.22 | 182 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Feb 3
Life <1 day
|
| Launched forty nine Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 20:30 UTC, 1.3 circuits after lift-off. |
| Not Catalogued - orbit parameters unavailable | |
2022-011 Soyuz-2 1A + Fregat
Plesetsk Cosmodrome | 2022 Feb 5, 07:00 | Cosmos 2553 2022-011A 51511 |
in space
|
| Military satellite described as a "technological spacecraft… equipped with newly developed on-board devices and systems for their development under radiation and heavy charged particles". |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 05, 14:51 | 8369 | 0.0005 | 1987 | 1995 | 126.98 | 67.09 | 272 | | | | 2022 Feb 06, 09:55 | 8374 | 0.0004 | 1993 | 1999 | 127.11 | 67.09 | 268 | | | | Fregat rocket stage uncatalogued |
Re-entered - 2022 Feb 5
Life <1 day
|
| Launched Cosmos 2553. Caused to re-enter - probably near 60° south, 170° east at about 09:50 UTC, about 1.4 circuits after launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-012 Soyuz ST-B + Fregat-M (VS-27)
Centre Spatiale Guyanaise | 2022 Feb 10, 18:09 | OneWeb 0410 2022-012A 51622 |
in space
|
Broadband distribution satellite for the UK company OneWeb.
One of 34 similar satellites carried on this launch, released from the Fregat stage of the launch vehicle in nine batches of four over a period of three hours. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 14, 16:00 | 6851 | 0.0015 | 463 | 484 | 94.07 | 87.40 | 235 | | | | Fregat rocket stage uncatalogued |
Re-entered - 2022 Feb 10
Life <1 day
|
| Launched cluster of 34 OneWeb satellites. Directed to destructive re-entry above the Indian Ocean at about 23:50 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2022-F01 - failed to reach orbit Rocket 3.3 (Astra LV0008)
Cape Canaveral Space Force Station | 2022 Feb 10, 20:00 | |
|
| 3U Cubesat from the University of Alabama to demonstrate a drag sail to accelerate orbit decay. Part of NASA's ELaNa 41 cluster, lost when the launch vehicle shroud failed to detach and second stage thrust vectoring failed to perform properly. |
| INCA (Ionosphere Neutron Content Analyzer) |
|
| 3U Cubesat from New Mexico State University to study the spectrum of Neutron flux in LEO. Part of NASA's ELaNa 41 cluster, lost when the launch vehicle shroud failed to detach and second stage thrust vectoring failed to perform properly. |
| |
|
| 2U Cubesat from University of California Berkeley to test and characterise the effects of orbital conditions on quantum gyroscopes built around nitrogen vacancy centres in the mineral diamond. Part of NASA's ELaNa 41 cluster, lost when the launch vehicle shroud failed to detach and second stage thrust vectoring failed to perform properly. |
| |
|
| 3U Cubesat from NASA Johnson Space Centre to demonstrate a fast, cost effective method to build a Cubesat - precise payload unknown. Part of NASA's ELaNa 41 cluster, lost when the launch vehicle shroud failed to detach and second stage thrust vectoring failed to perform properly. |
|
2022-013 PSLV-XL (PSLV C-52)
Satish Dhawan Space Centre | 2022 Feb 14, 00:29 | EOS 04 (Earth Observation Satellite 4) 2022-013A 51656 |
in space
|
| Indian remote sensing satellite equipped with Earth imaging radar. Separated from launch vehicle at 00:47 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Feb 14, 07:47 | 6906 | 0.0010 | 521 | 535 | 95.20 | 97.55 | 249 | 06:00 | | | Ispiresat 1 2022-013B 51657 |
in space
|
| Student satellite from the Indian Institute of Space Technolgy and the University of Colorado. Carries an Earth imaging thermal camera. Separated from launch vehicle at 00:47 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 14, 07:51 | 6905 | 0.0010 | 520 | 533 | 95.17 | 97.56 | 253 | | | | |
Re-entered - 2024 Nov 13
Life 1003 days
|
| Satellite from ISRO acting as a demonstrator for equipment designed for the planned India-Bhutan Joint Satellite (INS-2B). Separated from launch vehicle at 00:47 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 14, 06:28 | 6905 | 0.0009 | 520 | 533 | 95.16 | 97.56 | 259 | | | | PSLV upper stage 2022-013D 51659 |
in space
|
| Launched EOS 04 and two small satellites. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 14, 07:59 | 6897 | 0.0033 | 496 | 542 | 95.01 | 97.57 | 339 | | | |
2022-014 Soyuz-2 1A
Baikonur Cosmodrome | 2022 Feb 15, 04:25 | Progress MS-19 (Progress 7K-MS №449) 2022-014A 51660 |
Re-entered - 2022 Oct 24
Life 251 days
|
| Supplies and equipment to ISS. Docked with the Poisk module Feb 17 at 07:03 UTC, about three minutes earlier than scheduled. Undocked Oct 23 at 22:45:34 UTC. Retro-fire for four minutes Oct 24 at 01:51 UTC led to destructive re-entry above the southern Pacific Ocean at 02:24 UTC with any surviving fragments hitting the surface a few minutes later. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 15, 04:56 | 6589 | 0.0023 | 195 | 226 | 88.71 | 51.64 | 98 | | | | 2022 Feb 15, 11:57 | 6674 | 0.0028 | 278 | 315 | 90.44 | 51.64 | 329 | | | | 2022 Feb 16, 16:46 | 6677 | 0.0027 | 281 | 317 | 90.49 | 51.64 | 325 | | | | 2022 Feb 17, 12:32 | 6795 | 0.0006 | 413 | 421 | 92.91 | 51.64 | 139 | | | | 2022 Oct 23, 14:44 | 6796 | 0.0005 | 414 | 421 | 92.92 | 51.64 | 8 | | | | Soyuz upper stage 2022-014B 51661 |
Re-entered - 2022 Feb 17
Life 2 days
|
| Launched Progress MS-19. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 15, 08:59 | 6583 | 0.0028 | 186 | 223 | 88.58 | 51.66 | 66 | | | |
2022-015 Antares 230+
Wallops Flight Facility | 2022 Feb 19, 17:40 | Cygnus NG-17 (SS Piers Sellers) 2022-015A 51712 |
Re-entered - 2022 Jun 29
Life 130 days
|
| Northrop Grumman vehicle carrying supplies to ISS under CRS-2 contract with NASA. First Cygnus Enhanced version capable of boosting the ISS orbit. Capured by ISS Remote Manipulator Feb 21 at 09:44 UTC, about 9 min behind schedule. Docked with downward-facing port of the Unity module at 12:02 UTC. Undocked using Canadarm under ground control 2022 Jun 28, then released into independent orbit at 12:07 UTC. A thruster firing Jun 29 led to re-entry at about 06:55 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 19, 19:20 | 6662 | 0.0045 | 254 | 313 | 90.19 | 51.64 | 148 | | | | 2022 Feb 20, 05:07 | 6669 | 0.0054 | 254 | 327 | 90.32 | 51.64 | 148 | | | | 2022 Feb 20, 11:18 | 6716 | 0.0114 | 261 | 414 | 91.28 | 51.64 | 122 | | | | 2022 Feb 20, 16:27 | 6790 | 0.0006 | 408 | 416 | 92.80 | 51.64 | 168 | | | | 2022 Feb 21, 14:01 | 6795 | 0.0005 | 414 | 420 | 92.91 | 51.64 | 151 | | | | 2022 Jun 28, 11:40 | 6795 | 0.0005 | 413 | 420 | 92.90 | 51.64 | 282 | | | | 2022 Jun 28, 14:54 | 6798 | 0.0007 | 415 | 424 | 92.96 | 51.65 | 338 | | | | 2022 Jun 29, 06:05 | 6659 | 0.0174 | 165 | 397 | 90.13 | 51.64 | 306 | | | | NACHOS 1 (Nano-satellite Atmospheric Chemistry Hyperspectral Observation System) 2022-015D 52917 |
Re-entered - 2023 Feb 3
Life 349 days
|
| 3U Cubesat from the US Los Alamos National Laboratory using a new design of heat detector by measuring, mapping and quantifying trace gasses in support of volcanology and climate change research. Released from Cygnus NG-17 2022 Jun 28 at 20:20 UTC after leaving ISS. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 29, 19:39 | 6783 | 0.0008 | 399 | 410 | 92.65 | 51.64 | 318 | | | | Antares second stage 2022-015B 51713 |
Re-entered - 2022 Feb 25
Life 6 days
|
| Launched SS Piers Sellers. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 20, 06:36 | 6621 | 0.0090 | 183 | 303 | 89.36 | 51.62 | 143 | | | |
2022-016 Falcon 9 Block 5 (Starlink Group 4-8)
Cape Canaveral Space Force Station | 2022 Feb 21, 14:44 | Starlink 3528 2022-016A 51714 |
in space
|
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 15:47 UTC.
All satellites were injected initially into similar orbits at about 350 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 25, 16:00 | 6718 | 0.0001 | 339 | 340 | 91.32 | 53.22 | 58 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Feb 21
Life <1 day
|
| Launched forty six Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 17:00 UTC, 1.3 circuits after lift-off. |
| Not Catalogued - orbit parameters unavailable | |
2022-017 Falcon 9 Block 5 (Starlink Group 4-11)
Vandenberg Space Force Base | 2022 Feb 25, 16:12 | Starlink 3622 2022-017A 51768 |
in space
|
One member of a simultaneously-launched cluster of fifty LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 17:14 UTC.
All satellites were injected initially into similar orbits at about 350 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 02, 16:00 | 6706 | 0.0001 | 327 | 329 | 91.09 | 53.22 | 48 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Feb 25
Life <1 day
|
| Launched fifty Starlinks. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2022-018 CZ 4C
Jiuquan Space Centre | 2022 Feb 26, 23:44 | Ludi Tance 01-02 (L-SAR 01-02, Land Exploration 01-02) 2022-018A 51822 |
in space
|
| Earth surface studies satellite equipped with a large, high resolution, Synthetic Aperture Radar operating at L-band frequencies. Will work in conjunction with the L-SAR 01-01, launched 2022 Jan 25. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Feb 27, 04:38 | 6976 | 0.0004 | 595 | 601 | 96.65 | 97.81 | 267 | 06:00 | | | 2022 Mar 03, 12:48 | 6981 | 0.0001 | 602 | 604 | 96.75 | 97.80 | 128 | 06:00 | | | 2022 May 25, 02:07 | 6981 | 0.0002 | 602 | 604 | 96.75 | 97.81 | 90 | 06:00 | | | 2022 May 25, 11:48 | 6978 | 0.0003 | 598 | 602 | 96.69 | 97.81 | 62 | 06:00 | | | 2022 Jun 07, 02:56 | 6979 | 0.0002 | 599 | 602 | 96.70 | 97.81 | 104 | 06:00 | | | 2022 Jun 10, 22:54 | 6981 | 0.0002 | 602 | 604 | 96.75 | 97.81 | 103 | 06:00 | | | 2022 Jun 11, 20:25 | 6981 | 0.0002 | 601 | 604 | 96.75 | 97.81 | 103 | 06:00 | | | 2022 Dec 07, 10:47 | 6981 | 0.0002 | 601 | 604 | 96.75 | 97.81 | 63 | 06:00 | | | 2022 Dec 12, 05:49 | 6986 | 0.0013 | 599 | 616 | 96.85 | 97.76 | 146 | 06:00 | | | 2022 Dec 14, 07:55 | 6990 | 0.0002 | 610 | 613 | 96.93 | 97.81 | 92 | 06:00 | | | 2022 Dec 30, 11:55 | 6981 | 0.0001 | 602 | 604 | 96.75 | 97.81 | 116 | 06:00 | | | CZ-4C upper stage 2022-018B 51823 |
in space
|
| Launched L-SAR 01B. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 27, 05:36 | 6885 | 0.0134 | 414 | 599 | 94.75 | 97.87 | 39 | | | |
2022-019 CZ 8
Wenchang Space Centre | 2022 Feb 27, 03:06 | |
in space
|
| Small radar imaging satellite produced by the Spacety company. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | Chuangxin (Shiyan?) 2022-019xx |
in space
|
| Probably a small store-dump communications satellite developed by the Chinese Academy of Sciences, to be used to collect and relay water conservancy, hydrological and meteorological data from remote monitoring stations. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | |
in space
|
| Maritime surveillance satellite produced by the Shenzhen Aerospace Dongfanghong Satellite company. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | |
in space
|
| Maritime surveillance satellite produced by the Shenzhen Aerospace Dongfanghong Satellite company. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | Jilin-1 High Resolution 02A 01 (Jilin-1 GF02A 01) 2022-019xx |
in space
|
| Chinese high resolution, multi-spectral imaging satellite. Demonstrator for new onboard systems. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | Jilin-1 High Resolution 03D 10 (Jilin-1 GF3D 10) 2022-019xx |
in space
|
High resolution, multi-spectral imaging satellite.
One of nine similar satellites carried on this launch. All are in similar orbits. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | |
in space
|
| Mission details to follow. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | |
in space
|
| Commercial satellite for high-resolution remote sensing using an optical imaging system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | |
in space
|
| Commercial remote sensing satellite equipped with a radar imaging system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | |
in space
|
| Comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | |
in space
|
| Small satellite equipped with an Earth imaging system, and produced by the Minospace company. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | |
in space
|
| Small satellite equipped with an Earth imaging system, and produced by the Minospace company. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | |
in space
|
| Small satellite equipped with an Earth imaging system, and produced by the Minospace company. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | Xingshidai 17 (Daiyun, Star Times 17) 2022-019xx |
in space
|
| Remote sensing - equipped with a multispectral Earth imaging system, from ADA Space (Chengdu Guoxing Aerospace Technology company) of China. Also carries a laser communication system and uses an artificial intelligence system to control the creation and processing of images. Part of a planned 100 satellite constellation. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6913 | 0.0023 | 519 | 551 | 95.34 | 97.51 | 267 | 10:32 | | | CZ 8 upper stage 2022-019U 51842 |
Re-entered - 2024 Jul 28
Life 882 days
|
| Launched cluster of 22 small satellites. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Feb 27, 09:09 | 6878 | 0.0070 | 451 | 548 | 94.61 | 97.56 | 212 | | | |
2022-020 Electron (The Owl's Night Continues)
Rocket Lab Launch Complex, New Zealand | 2022 Feb 28, 20:37 | |
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. Demonstrator for a future 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. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Mar 01, 05:18 | 6942 | 0.0013 | 555 | 573 | 95.94 | 97.78 | 291 | 09:00 | | | Electron third stage (kick stage) 2022-020B 51848 |
Re-entered - 2024 May 21
Life 813 days
|
| Launched StriX-β. Perigee lowered after releasing satelite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 01, 05:14 | 6894 | 0.0061 | 474 | 558 | 94.94 | 97.09 | 30 | | | | Electron second stage 2022-020C 51849 |
Re-entered - 2022 Mar 15
Life 15 days
|
| Launched StriX-β. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 01, 06:33 | 6772 | 0.0313 | 182 | 606 | 92.44 | 97.73 | 222 | | | |
2022-021 Atlas V 541
Cape Canaveral Space Force Station | 2022 Mar 1, 21:38 | GOES 18 (Geostationary Operational Environmental Satellite) 2022-021A 51850 |
in space
|
| Imaging meteorological satellite from the North American Atmospheric Administration (NOAA). Also carries a search and rescue radio transponder. Separated from launch vehicle Mar 2 at 01:11 UTC. Reached GEO Drift Orbit Mar 15. Expected location - 136°.8 west. Test location 89°.5 west. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Mar 02, 02:48 | 28462 | 0.4635 | 8893 | 35275 | 796.45 | 9.45 | 180 | | | | 2022 Mar 08, 04:55 | 32400 | 0.2856 | 16769 | 35275 | 967.33 | 4.69 | 181 | | | | 2022 Mar 10, 15:01 | 34969 | 0.1911 | 21909 | 35272 | 1084.62 | 2.66 | 180 | | | | 2022 Mar 13, 09:48 | 38051 | 0.0949 | 28063 | 35283 | 1231.16 | 1.34 | 181 | | | | 2022 Mar 18, 12:15 | 42024 | 0.0016 | 35579 | 35713 | 1428.91 | 0.06 | 54 | 91° west | | | 2022 Mar 21, 10:34 | 42164 | 0.0001 | 35783 | 35789 | 1436.08 | 0.06 | 286 | 89° west | | | 2022 May 19, 20:45 | 42344 | 0.0002 | 35960 | 35973 | 1445.27 | 0.04 | 77 | 96° west | | | 2022 Jun 07, 06:24 | 42178 | 0.0005 | 35781 | 35819 | 1436.78 | 0.05 | 70 | 137° west | | | Atlas V upper stage 2022-021B 51851 |
in space
|
| Launched GOES-T. Perigee lowered after releasing satellite at orbital apogee. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 08, 06:06 | 27973 | 0.4767 | 8260 | 34931 | 776.03 | 9.66 | 179 | | | |
2022-022 Falcon 9 Block 5 (Starlink Group 4-9)
Kennedy Space Center | 2022 Mar 3, 14:25 | Starlink 3542 2022-022A 51852 |
in space
|
One member of a simultaneously-launched cluster of forty seven LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 09, 22:00 | 6715 | 0.0001 | 336 | 338 | 91.28 | 53.22 | 53 | | | | Falcon 9 upper stage uncatalogued |
in space
|
| Launched forty seven Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 16:40 UTC, 1.3 circuits after lift-off |
| Not Catalogued - orbit parameters unavailable | |
2022-023 CZ 2C
Xichang Space Centre | 2022 Mar 5, 06:01 | |
Re-entered - 2024 Jun 8
Life 826 days
|
| (6?)U Cubesat - commercial remote sensing satellite from Xinguan Aerospace. Technology verification vehicle for a future constellation. Catalogue Number and Designation subject to confirmation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 06, 05:22 | 6869 | 0.0016 | 480 | 502 | 94.43 | 63.44 | 298 | | | | Yinhe 2-01 (Galaxy 2-01) 2022-023xx |
in space
|
| One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6869 | 0.0015 | 480 | 501 | 94.42 | 63.44 | 302 | | | | Yinhe 2-02 (Galaxy 2-02) 2022-023xx |
in space
|
| One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6869 | 0.0015 | 480 | 501 | 94.42 | 63.44 | 302 | | | | Yinhe 2-03 (Galaxy 2-03) 2022-023xx |
in space
|
| One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6869 | 0.0015 | 480 | 501 | 94.42 | 63.44 | 302 | | | | Yinhe 2-04 (Galaxy 2-04) 2022-023xx |
in space
|
| One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6869 | 0.0015 | 480 | 501 | 94.42 | 63.44 | 302 | | | | Yinhe 2-05 (Galaxy 2-05) 2022-023xx |
in space
|
| One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6869 | 0.0015 | 480 | 501 | 94.42 | 63.44 | 302 | | | | Yinhe 2-06 (Galaxy 2-06) 2022-023xx |
in space
|
| One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6869 | 0.0015 | 480 | 501 | 94.42 | 63.44 | 302 | | | | CZ 2C second stage 2022-023H 51953 |
in space
|
| Launched cluster of seven small satellites. Seems to have raised apogee after releasing satellites, reason unknown but possibly to support instrumentation remaining attached after satellites' deployment. Orbit, Catalogue Number, Designation and orbit subject to confirmation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 06, 05:25 | 6942 | 0.0117 | 483 | 645 | 95.95 | 63.64 | 247 | | | |
2022-024 Qased (Messenger)
Shahroud Test Centre, Dasht-e Kavir, Iran | 2022 Mar 8, 05:05 | Nour 2 (Light 2) 2022-024A 51954 |
Re-entered - 2024 May 17
Life 801 days
|
| 6U Cubesat - military satellite launched by the Iranian Revolutionary Guard Corps, probably for low resolution Earth imaging - purpose was announced as "reconnaissance". |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 08, 15:36 | 6882 | 0.0013 | 495 | 513 | 94.70 | 58.30 | 238 | | | | 2023 Sep 27, 09:16 | 6822 | 0.0018 | 431 | 456 | 93.45 | 58.28 | 31 | | | | Qased upper stage 2022-024B 51955 |
in space
|
| Launched Nour 2. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 08, 15:36 | 6881 | 0.0010 | 496 | 509 | 94.67 | 58.30 | 248 | | | |
2022-025 Falcon 9 Block 5 (Starlink Group 4-10)
Cape Canaveral Space Force Station | 2022 Mar 9, 13:45 | Starlink 3700 2022-025A 51956 |
in space
|
One member of a simultaneously-launched cluster of forty eight LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 16, 14:00 | 6702 | 0.0001 | 323 | 325 | 91.01 | 53.22 | 88 | | | | Falcon 9 upper stage uncatalogued |
in space
|
| Launched forty eight Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 16:00 UTC, 1.3 circuits after lift-off |
| Not Catalogued - orbit parameters unavailable | |
2022-026 Rocket 3.3 (Astra LV0009)
Kodiak Launch Centre, Alaska | 2022 Mar 15, 16:22 | OreSat0 (Oregon Satellite 0) 2022-026K 52017 |
Re-entered - 2024 Sep 29
Life 929 days
|
| 1U Cubesat from Portland State University. Carries a colour imaging system and an amateur radio payload. Released from launch vehicle at 16:30 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Mar 17, 17:05 | 6903 | 0.0026 | 507 | 543 | 95.14 | 97.50 | 229 | 05:30 | | | SpaceBEE 112 2022-026T 52025 |
Re-entered - 2024 Jan 12
Life 668 days
|
0.25U Cubesat from Swarm Technologies to provide a two-way communications system from LEO as part of a 150 satellite constellation. To aid tracking,the satellite carries a radar retro-reflector. It also carries a GPS receiver to help determine its location.
One of twenty SpaceBEE satellites carried on the launch.
All were aimed at similar orbits and all have been confirmed as active. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Mar 18, 15:17 | 6903 | 0.0026 | 507 | 543 | 95.13 | 97.50 | 225 | 05:30 | | | Astra upper stage 2022-026A 52008 |
Re-entered - 2024 Jan 2
Life 658 days
|
| Launched multiple satellites. A further payload, S4 Crossover, remains intentionally attached to it. S4 Crossover is a Cubesat (6U) from Near Space Launch inc as a demonstrator for a possible future satellite design. It carries an Iridium satellite telephone, a Globalstar transmitter and sensors to monitor radiation and space plasma density. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 15, 18:02 | 6882 | 0.0048 | 470 | 537 | 94.69 | 97.49 | 274 | | | |
2022-027 CZ 4C
Jiuquan Space Centre | 2022 Mar 17, 07:09 | Yaogan 34-02 2022-027A 52084 |
in space
|
| Imaging satellite - orbit is similar to the Yaogan 31 electronic surveillance satellites,and the Initial orbit plane has RAAN about three degrees to the east of that of the third Yaogan 31 triplet (launch no 2021-014). Settled into formation with Yaogan 31 Group 3, sitting 34° of orbit arc behind it and following a near-identical ground track. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 17, 12:23 | 7472 | 0.0003 | 1092 | 1096 | 107.14 | 63.40 | 262 | | | | 2022 Mar 18, 11:28 | 7462 | 0.0014 | 1074 | 1094 | 106.92 | 63.39 | 263 | | | | 2023 Feb 13, 08:16 | 7468 | 0.0026 | 1070 | 1109 | 107.04 | 63.40 | 345 | | | | CZ 4C third stage 2022-027B 52085 |
in space
|
| Launched Yaogan 34-02. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 17, 08:43 | 7396 | 0.0105 | 940 | 1095 | 105.50 | 63.40 | 44 | | | |
2022-028 Soyuz-2 1A
Baikonur Cosmodrome | 2022 Mar 18, 15:55 | Soyuz MS-21 (Soyuz 11F732A48 № 750) 2022-028A 52086 |
Re-entered - 2022 Sep 29
Life 195 days
Returned to Earth |
| Carrying crew to ISS - Oleg Artemyev (commander), Denis Matveev and Sergey Korsakov (all Roscosmos). Docked, under manual control by its crew, with the Prichal module of ISS at 19:12 UTC on day of launch - due to an unspecified problem with the 'Kurs' automatic system at 180m from the ISS. Undocked, carrying its original crew 2022 Sep 29, 07:34 UTC. Following retrofire, the descent module landed near Dzhezkazgan, Russia at 10:57 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 18, 16:26 | 6590 | 0.0019 | 200 | 224 | 88.73 | 51.68 | 84 | | | | 2022 Mar 18, 17:55 | 6796 | 0.0004 | 416 | 421 | 92.94 | 51.64 | 283 | | | | 2022 Sep 28, 07:10 | 6794 | 0.0002 | 414 | 417 | 92.88 | 51.64 | 303 | | | | Soyuz upper stage 2022-028B 52087 |
Re-entered - 2022 Mar 21
Life 3 days
|
| Launched Soyuz MS-21. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 18, 16:24 | 6588 | 0.0023 | 195 | 226 | 88.70 | 51.66 | 76 | | | |
2022-029 Falcon 9 Block 5 (Starlink Group 4-12)
Cape Canaveral Space Force Station | 2022 Mar 19, 04:42 | Starlink 3537 2022-029A 52088 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 05:41 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 22, 16:00 | 6686 | 0.0010 | 301 | 315 | 90.69 | 53.22 | 295 | | | | Falcon 9 upper stage uncatalogued |
in space
|
| Launched fifty three Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 06:55 UTC, 1.3 circuits after lift-off |
| Not Catalogued - orbit parameters unavailable | |
2022-030 Soyuz-2 1A + Fregat
Plesetsk Cosmodrome | 2022 Mar 22, 12:48 | Meridian 10 (Meridian-M № 20L) 2022-030A 52145 |
in space
|
| HEO military/government comsat to support Russian forces, commercial shipping and communication ground stations at northern latitudes across Russia. Third mission for the Meridian-M version. Meridian also supports the clandestine short messaging system formerly provided by the Parus satellites. Moved to stable, operational orbit on or after Apr 18 but orbit data not published until May 18. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 23, 02:12 | 26748 | 0.7252 | 974 | 39767 | 725.61 | 62.83 | 270 | | | | 2022 Apr 02, 02:18 | 26757 | 0.7236 | 1018 | 39740 | 725.96 | 62.79 | 270 | | | | 2022 May 18, 15:21 | 26555 | 0.7209 | 1035 | 39320 | 717.77 | 62.75 | 270 | | | | Fregat rocket stage 2022-030B 52146 |
in space
|
| Launched Meridian 10. Separated from Soyuz launch vehicle together with attached Meridian-M at 12:57 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 23, 14:04 | 26589 | 0.7297 | 810 | 39612 | 719.14 | 62.80 | 270 | | | |
2022-I05 JEM Small Satellite Orbital Deployer
International Space Station | 2022 Mar 24, 09:00 | |
Re-entered - 2022 Nov 18
Life 239 days
|
| 3U Cubesat from IHI Corporation and the Space Robotics Laboratory of Tohoku University, Japan. Demonstrator of a tracking system for AIS, the identification and short messaging system for use by ships at sea. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 28, 20:08 | 6793 | 0.0004 | 412 | 418 | 92.87 | 51.64 | 14 | | | |
2022-I06 JEM Small Satellite Orbital Deployer
International Space Station | 2022 Mar 24, 12:10 | KITSUNE (Kyutech standardized bus Imaging Technology System Utilizing Networking and Electron content measurements) 1998-067TK 52148 |
Re-entered - 2023 Mar 14
Life 355 days
|
| 6U Cubesat from Kyushu Institute of Technology, Japan. Carries a high resolution Earth imaging system and a radio system to collect data from remote ground stations and sensors. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 28, 20:10 | 6794 | 0.0003 | 414 | 418 | 92.89 | 51.64 | 353 | | | |
2022-031 CZ 6A (Y-1)
Taiyuan Space Centre | 2022 Mar 29, 09:50 | |
in space
|
| Technology demonstration satellite for satellite bus including an attitude control system, thermal cladding and an onboard processing system for optical imaging. Released from launch vehicle at 10:04 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Mar 29, 15:45 | 6975 | 0.0012 | 588 | 605 | 96.61 | 97.80 | 262 | 17:00 | | | |
in space
|
| Small technology demonstration satellite, includes an Earth imaging system. Released from launch vehicle at 10:06 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Mar 29, 17:22 | 6974 | 0.0011 | 588 | 604 | 96.60 | 97.78 | 267 | 17:00 | | | CZ 6A third stage 2022-031C 52152 |
in space
|
| Launched Puijang 2 and Taikun 2. Orbit lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 29, 16:05 | 6952 | 0.0028 | 554 | 592 | 96.13 | 97.78 | 2 | | | |
2022-032 CZ 11
Jiuquan Space Centre | 2022 Mar 30, 02:29 | Tianping 2A 2022-032A 52153 |
in space
|
| Small satellite, one of a simultaneously-launched group of three. Precise purpose unknown but reportedly for space environment studies in LEO and acting as calibration targets for ground-based visual and radar tracking equipment. Probably equipped with an Earth imaging system. Catalogue Number, Designation and orbit to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Mar 30, 08:21 | 6972 | 0.0013 | 585 | 603 | 96.56 | 97.80 | 283 | 08:47 | | | Tianping 2B 2022-032C 52155 |
in space
|
| Small satellite, one of a simultaneously-launched group of three. Precise purpose unknown but reportedly for space environment studies in LEO and acting as calibration targets for ground-based visual and radar tracking equipment. Probably equipped with an Earth imaging system. Catalogue Number, Designation and orbit to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Mar 30, 12:14 | 6971 | 0.0015 | 582 | 603 | 96.53 | 97.80 | 292 | 08:47 | | | Tianping 2C 2022-032D 52156 |
in space
|
| Small satellite, one of a simultaneously-launched group of three. Precise purpose unknown but reportedly for space environment studies in LEO and acting as calibration targets for ground-based visual and radar tracking equipment. Probably equipped with an Earth imaging system. Catalogue Number, Designation and orbit to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Mar 30, 12:04 | 6971 | 0.0015 | 582 | 603 | 96.53 | 97.79 | 292 | 08:47 | | | CZ 11 fourth stage 2022-032B 52154 |
Re-entered - 2022 Apr 7
Life 8 days
|
| Launched Tianping 2A, 2B & 2C. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Mar 30, 06:33 | 6777 | 0.0387 | 137 | 662 | 92.54 | 97.63 | 322 | | | |
2022-033 Falcon 9 Block 5 (Transporter 4)
Cape Canaveral Space Force Station | 2022 Apr 1, 16:24 | Spark 1 (LEO 1) 2022-033A 52157 |
in space
|
| Small satellite from Omnispace, demonstrator for a future LEO comsat constellation to include internet connectivity. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 13:06 | 7026 | 0.0012 | 639 | 656 | 97.68 | 97.95 | 238 | | | | GNOMES 3 (GNSS Navigation and Occultation Measurement Satellite) 2022-033B 52158 |
in space
|
| Small satellite from PlanetiQ, equipped with radio receivers to observe occultations of MEO navsat signals in order to study the Earth's upper atmosphere and contribute to weather forecasting. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 17:57 | 7024 | 0.0012 | 638 | 654 | 97.64 | 97.95 | 249 | | | | EnMAP (Environmental Mapping and Analysis Program) 2022-033C 52159 |
in space
|
| German hyperspectral imaging satellite mission to monitor and characterise the Earth’s environment. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Apr 06, 13:01 | 7023 | 0.0009 | 638 | 651 | 97.62 | 97.95 | 265 | 11:00 | | | |
Re-entered - 2024 Apr 5
Life 735 days
|
| 3U Cubesat from a consortium of Brazilian and UK universities to demonstrate point-to-point and store/forward messaging communications from remote areas. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 12:46 | 6883 | 0.0009 | 499 | 511 | 94.72 | 97.39 | 282 | | | | ARCSAT (Arctic Regional Communications small SATellite) 2022-033E 52161 |
in space
|
| 6U Cubesat from Norway's Defence Research Establishment to to demonstrate the use and relevance of a satellite relay for UHF communication at high latitudes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 15:55 | 6883 | 0.0009 | 499 | 511 | 94.72 | 97.39 | 278 | | | | Lynk Tower 1 2022-033F 52162 |
in space
|
| Small satellite from Lynk Global providing two-way connectivity for broadband, voice, and text messaging globally. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 12:43 | 6882 | 0.0009 | 497 | 510 | 94.69 | 97.39 | 260 | | | | ION SCV-005 (Almighty Alexius) 2022-033G 52163 |
Re-entered - 2024 Aug 6
Life 858 days
|
Satellite Carrier Vehicle built by D-Orbit - released from launch vehicle at 17:50 UTC carrying a small group of satellites for later deployment:
Plantsat - released Apr 9,
KLEOS, KSM 2c - Released Apr 11,
KLEOS, KSM 2d - Released Apr 11,
SUCHAI 2 - released Apr 13,
SUCHAI 3 - released Apr 14,
KLEOS, KSM 2a - released May 9,
KLEOS, KSM 2b - released May 9.
Also carries a hosted payload from Upmosphere consisting of a wooden box containing personal items for clients wishing to deposit something on-orbit. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 12:44 | 6882 | 0.0009 | 497 | 510 | 94.69 | 97.39 | 261 | | | | 2022 Apr 14, 11:48 | 6881 | 0.0010 | 496 | 510 | 94.68 | 97.39 | 226 | | | | 2022 Apr 18, 12:07 | 6882 | 0.0011 | 496 | 511 | 94.69 | 97.44 | 208 | | | | 2022 Apr 19, 11:48 | 6882 | 0.0011 | 496 | 512 | 94.70 | 97.47 | 201 | | | | 2022 Apr 24, 11:51 | 6883 | 0.0013 | 496 | 514 | 94.72 | 97.59 | 181 | | | | 2022 Apr 25, 11:32 | 6883 | 0.0014 | 496 | 515 | 94.73 | 97.62 | 177 | | | | Hawk 4B (Cluster 4 #2) 2022-033J 52165 |
in space
|
| SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| Hawk 4A (Cluster 4 #1) 2022-033L 52167 |
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.
One of three similar satellites carried on this launch. All were aimed at similar orbits and are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 17:28 | 6882 | 0.0009 | 498 | 510 | 94.69 | 97.39 | 263 | | | | ÑuSat 23 (Annie Maunder) 2022-033M 52168 |
Re-entered - 2024 Nov 1
Life 945 days
|
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video.
One of five similar satellites carried on this launch. All were aimed at similar orbits and are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Apr 06, 12:44 | 6882 | 0.0008 | 498 | 510 | 94.70 | 97.39 | 267 | 10:58 | | | |
Re-entered - 2024 Oct 20
Life 933 days
|
| Small satellite to built by Nanoavionics of Lithuania to prove the MP42 platform and carring a number of technology tests and technical customer payloads including a 'cell tower in space' for mobile telephony. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 17:26 | 6880 | 0.0011 | 495 | 510 | 94.66 | 97.39 | 263 | | | | Hawk 4C (Cluster 4 #3) 2022-033P 52170 |
in space
|
| SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| |
Re-entered - 2024 Jan 13
Life 652 days
|
| Demonstrator satellite from Indian company Pixxel for a hyperspectral Earth imaging system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Apr 06, 11:05 | 6879 | 0.0012 | 492 | 510 | 94.64 | 97.39 | 256 | 10:58 | | | BRO 7 (Breizh Reconnaissance Orbiter 7) 2022-033T 52174 |
in space
|
| 6U Cubesat (3x2) from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 12:39 | 6879 | 0.0012 | 492 | 509 | 94.63 | 97.39 | 250 | | | | |
Re-entered - 2024 Apr 18
Life 748 days
|
| 1U Cubesat from the Czech Republic testing space environment sensors and carrying an amateur radio system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 11:04 | 6879 | 0.0013 | 492 | 509 | 94.63 | 97.39 | 252 | | | | SpaceBEE 128 2022-033AB 52182 |
Re-entered - 2023 Oct 11
Life 558 days
|
0.25U Cubesat from Swarm Technologies to provide a two-way communications system from LEO as part of a 150 satellite constellation. To aid tracking,the satellite carries a radar retro-reflector. It also carries a GPS receiver to help determine its location.
One of twelve SpaceBEE satellites carried on the launch. All were aimed at similar orbits and are accounted for. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 06, 17:29 | 6882 | 0.0008 | 498 | 509 | 94.70 | 97.38 | 266 | | | | |
Re-entered - 2024 Mar 4
Life 703 days
|
| 3U Cubesat from the University of Chile and the University of Santiago de Chile to study the development of a plant in a simulated Martian environment. Released from ION SCV-005 2022 Apr 9 at 14:22 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 14, 14:52 | 6878 | 0.0005 | 496 | 503 | 94.61 | 97.39 | 248 | | | | Kleos Scouting Mission 2c (KSM-2c) 2022-033AJ 52189 |
Re-entered - 2024 Aug 16
Life 868 days
|
| 6U Cubesat - one of two satellites orbiting together, designed to observe maritime activity, particularly of shipping in strategic areas not using AIS. Carries radio receivers to monitor nautical radio bands. Satellite built by GomSpace in Denmark for Luxemburg company Kleos Space. Released from ION SCV-005 on Apr 11 at 07:13 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 15, 16:13 | 6881 | 0.0010 | 496 | 510 | 94.68 | 97.38 | 221 | | | | Kleos Scouting Mission 2d (KSM-2d) 2022-033AK 52190 |
Re-entered - 2023 Dec 7
Life 615 days
|
| 6U Cubesat - one of two satellites orbiting together, designed to observe maritime activity, particularly of shipping in strategic areas not using AIS. Carries radio receivers to monitor nautical radio bands. Satellite built by GomSpace in Denmark for Luxemburg company Kleos Space. Released from ION SCV-005 on Apr 11 at 18:16 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 15, 16:13 | 6881 | 0.0010 | 496 | 510 | 94.68 | 97.38 | 221 | | | | |
Re-entered - 2024 May 25
Life 785 days
|
| 1U Cubesat from the University of Chile and the University of Santiago de Chile studying the ionosphere, Released from ION SCV-005 on Apr 13 at 08:03:04 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 15, 17:50 | 6884 | 0.0011 | 498 | 513 | 94.73 | 97.40 | 203 | | | | |
Re-entered - 2024 Oct 6
Life 919 days
|
| 1U Cubesat from the University of Chile and the University of Santiago de Chile studying the ionosphere, Released from ION SCV-005 on Apr 14 at 07:45:00 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 26, 09:28 | 6879 | 0.0010 | 494 | 508 | 94.63 | 97.38 | 196 | | | | Kleos Scouting Mission 2a (KSM-2a) 2022-033AN 52193 |
Re-entered - 2024 Feb 14
Life 684 days
|
| 6U Cubesat - one of two satellites orbiting together, designed to observe maritime activity, particularly of shipping in strategic areas not using AIS. Carries radio receivers to monitor nautical radio bands. Satellite built by GomSpace in Denmark for Luxemburg company Kleos Space. Released from ION SCV-005 on May 9 at 15:49:19 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 16, 12:47 | 6880 | 0.0014 | 493 | 511 | 94.66 | 97.40 | 131 | | | | Kleos Scouting Mission 2b (KSM-2b) 2022-033AP 52194 |
Re-entered - 2024 Aug 13
Life 865 days
|
| 6U Cubesat - one of two satellites orbiting together, designed to observe maritime activity, particularly of shipping in strategic areas not using AIS. Carries radio receivers to monitor nautical radio bands. Satellite built by GomSpace in Denmark for Luxemburg company Kleos Space. Released from ION SCV-005 on May 9 at 18:58:48 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 16, 20:41 | 6880 | 0.0014 | 493 | 512 | 94.66 | 97.40 | 131 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Apr 1
Life <1 day
|
| Launched Transporter 4 satellite cluster. Caused to re-enter above the Indian Ocean at about 18:45 UTC on day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-034 Electron (Without Mission a Beat)
Rocket Lab Launch Complex, New Zealand | 2022 Apr 2, 12:41 | BlackSky 18 (Global 18) 2022-034B 52196 |
in space
|
| Second Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc. Released from kick stage at about 13:41 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 03, 01:44 | 6813 | 0.0009 | 429 | 440 | 93.27 | 53.01 | 293 | | | | BlackSky 20 (Global 20) 2022-034C 52197 |
in space
|
| Second Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc. Released from kick stage at about 13:41 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 03, 18:49 | 6811 | 0.0010 | 426 | 440 | 93.23 | 53.00 | 285 | | | | Electron third stage (kick stage) 2022-034D 52198 |
Re-entered - 2022 Apr 6
Life 4 days
|
| Launched pair of BlackSky Global Gen 2 satellites. Perigee lowered after releasing satelites. Space-Track has this object labelled incorrectly as the Electron second stage. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 02, 20:53 | 6677 | 0.0182 | 177 | 421 | 90.50 | 52.98 | 54 | | | | Electron second stage 2022-034E 52199 |
Re-entered - 2022 Apr 11
Life 9 days
|
| Launched pair of BlackSky Global Gen 2 satellites. Space-Track has this object labelled incorrectly as the Electron kick stage. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 02, 18:24 | 6698 | 0.0208 | 181 | 459 | 90.92 | 53.03 | 243 | | | |
2022-035 CZ 4C
Jiuquan Space Centre | 2022 Apr 6, 23:47 | Gaofen 3-03 2022-035A 52200 |
in space
|
| Earth imaging satellite equipped with a Synthetic Aperture Radar with resolution of 1m. Sun-synchronous orbit plane matched to its predecessors. The satellites will work together observing targets mainly on the Earth's sea/ocean surface. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Apr 07, 04:13 | 7120 | 0.0005 | 738 | 745 | 99.64 | 98.40 | 271 | 06:02 | | | 2022 Apr 19, 12:51 | 7127 | 0.0005 | 746 | 753 | 99.80 | 98.42 | 76 | 06:02 | | | 2022 Apr 21, 19:01 | 7129 | 0.0002 | 750 | 752 | 99.85 | 98.42 | 100 | 06:02 | | | 2023 Feb 13, 10:11 | 7129 | 0.0001 | 751 | 752 | 99.85 | 98.42 | 91 | 06:03 | | | CZ 4C third stage 2022-035C 52201 |
in space
|
| Launched Gaofen 3-03. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 07, 04:09 | 7038 | 0.0113 | 580 | 739 | 97.92 | 98.40 | 51 | | | |
2022-036 Soyuz-2 1B
Plesetsk Cosmodrome | 2022 Apr 7, 11:20 | Cosmos 2554 (Lotos-S1 № 5) 2022-036A 52202 |
in space
|
| Electronic intelligence gathering - signals intelligence (SIGINT) satellite. Vehicle is based on the design of the Yantar satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 07, 17:58 | 6948 | 0.0476 | 239 | 900 | 96.06 | 67.14 | 92 | | | | 2022 Apr 08, 16:12 | 6950 | 0.0472 | 244 | 900 | 96.11 | 67.13 | 91 | | | | 2022 Apr 12, 00:15 | 7281 | 0.0008 | 897 | 909 | 103.05 | 67.15 | 318 | | | | 2022 Apr 12, 13:37 | 7285 | 0.0005 | 904 | 911 | 103.14 | 67.14 | 280 | | | | 2022 Apr 13, 06:28 | 7283 | 0.0006 | 901 | 910 | 103.10 | 67.14 | 280 | | | | Soyuz upper stage 2022-036B 52203 |
Re-entered - 2022 Nov 30
Life 237 days
|
| Launched Cosmos 2554. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 07, 16:04 | 6933 | 0.0457 | 238 | 871 | 95.75 | 67.14 | 93 | | | |
2022-037 Falcon 9 Block 5
Kennedy Space Center | 2022 Apr 8, 15:17 | SpaceX Axiom 1 (Dragon Endeavour flight #3) 2022-037A 52204 |
Re-entered - 2022 Apr 25
Life 17 days
Returned to Earth |
| Privately funded (Axiom Space) science mission to ISS using SpaceX Crew Dragon. Crew consisting of Michael Lopez Allegria (Commander), Larry Conor (Pilot), Eytan Stibbe (Mission Specialist - Israel) and Mark Pathy (Mission Specialist). Separated from launch vehicle at 15:29 UTC. Docked with forward facing port of ISS Harmony module April 9 at 12:29 UTC, about 16 min earlier than planned. Undocked, carrying original crew, 2022 April 25, 01:10 UTC. Retro-fire at 16:18 UTC was followed by splashdown at 17:06 UTC in the Atlantic Ocean off Florida. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 08, 18:35 | 6608 | 0.0034 | 207 | 252 | 89.09 | 51.64 | 228 | | | | 2022 Apr 09, 08:24 | 6795 | 0.0005 | 414 | 420 | 92.91 | 51.64 | 3 | | | | 2022 Apr 24, 13:16 | 6796 | 0.0006 | 414 | 422 | 92.92 | 51.64 | 30 | | | | 2022 Apr 25, 01:58 | 6800 | 0.0005 | 419 | 425 | 93.01 | 51.64 | 57 | | | | 2022 Apr 25, 04:37 | 6694 | 0.0134 | 226 | 405 | 90.84 | 51.65 | 163 | | | | 2022 Apr 25, 06:12 | 6692 | 0.0133 | 225 | 403 | 90.80 | 51.64 | 164 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Apr 8
Life <1 day
|
| Launched Crew Dragon Axiom 1. Caused to re- enter above the Indian Ocean about 45 mins after lift-off. |
| Not Catalogued - orbit parameters unavailable | | Crew Dragon trunk module 2022-037B 52319 |
Re-entered - 2022 May 14
Life 36 days
|
| Separated from Dragon Endeavour 2022 April 25 at 16:16 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 27, 16:45 | 6684 | 0.0123 | 223 | 388 | 90.64 | 51.89 | 173 | | | |
2022-038 CZ 3B
Xichang Space Centre | 2022 Apr 15, 12:00 | Zhongxing 6D (Chinasat 6D) 2022-038A 52255 |
in space
|
| Comsat providing radio, TV and general communications to mainland China and its territorial waters, and to other users in the Asia-Pacific region. Probably moved to Geosynchronous Drift Orbit Apr 16. Expected location - 125° east. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Apr 16, 04:12 | 24378 | 0.7289 | 232 | 35769 | 631.34 | 28.46 | 180 | | | | 2022 Apr 27, 15:02 | 42165 | 0.0002 | 35777 | 35797 | 1436.12 | 0.06 | 334 | 130° east | | | 2022 May 03, 19:18 | 42222 | 0.0003 | 35831 | 35857 | 1439.01 | 0.05 | 324 | 126° east | | | 2022 May 07, 16:49 | 42165 | 0.0002 | 35780 | 35793 | 1436.08 | 0.02 | 357 | 125° east | | | CZ 3B fourth stage 2022-038B 52256 |
in space
|
| Launched Zhongxing 6D. Orbit lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 15, 15:51 | 23652 | 0.7225 | 186 | 34362 | 603.34 | 28.47 | 179 | | | |
2022-039 CZ 4C
Taiyuan Space Centre | 2022 Apr 15, 18:16 | Daqi 1 (Atmosphere Environment Monitoring Satellite) 2022-039A 52257 |
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. An observation from Mauna Kea, Hawaii 2023 Jan 28 showed it is equipped with a downward-pointing green laser to measure pollution. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Apr 15, 21:24 | 7064 | 0.0007 | 681 | 690 | 98.47 | 98.13 | 233 | 01:35 | | | 2022 Apr 18, 13:30 | 7071 | 0.0005 | 690 | 697 | 98.63 | 98.14 | 28 | 01:35 | | | 2022 Apr 20, 12:48 | 7079 | 0.0000 | 700 | 701 | 98.79 | 98.13 | 282 | 01:35 | | | 2023 Jan 28, 07:58 | 7078 | 0.0003 | 698 | 702 | 98.78 | 98.16 | 93 | 01:27 | | | 2023 Aug 14, 10:09 | 7079 | 0.0003 | 699 | 703 | 98.79 | 98.18 | 184 | 01:24 | | | CZ 4C third stage 2022-039B 52258 |
Re-entered - 2022 May 12
Life 27 days
|
| Launched AEMS. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 15, 21:20 | 6974 | 0.0137 | 500 | 691 | 96.59 | 98.16 | 63 | | | |
2022-040 Falcon 9 Block 5
Vandenberg Space Force Base | 2022 Apr 17, 13:13 | USA 327 (NOSS 3-9 p/l 1?, Intruder?) 2022-040A 52259 |
in space
|
| Navy Ocean Surveillance Satellite (NOSS)? An expected companion satellite to create a twin satellite formation did not materialise - unclear whether this was by design or error. Orbits based on amateur observation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 22, 23:14 | 7486 | 0.0134 | 1008 | 1208 | 107.43 | 63.45 | 179 | | | | 2022 Aug 16, 19:57 | 7486 | 0.0128 | 1012 | 1204 | 107.43 | 63.44 | 178 | | | | 2022 Aug 21, 19:54 | 7484 | 0.0123 | 1015 | 1198 | 107.40 | 63.44 | 178 | | | | Falcon 9 upper stage uncatalogued |
in space
|
| Launched USA 327. Directed to a destructive re-entry above the eastern Pacific Ocean about 140 minutes after lift-off. |
| Not Catalogued - orbit parameters unavailable | |
2022-041 Falcon 9 Block 5 (Starlink Group 4-14)
Cape Canaveral Space Force Station | 2022 Apr 21, 17:51 | Starlink 3810 2022-041A 52262 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 18:50 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 25, 18:00 | 6705 | 0.0001 | 326 | 328 | 91.06 | 53.22 | 67 | | | |
2022-042 Falcon 9 Block 5
Kennedy Space Center | 2022 Apr 27, 07:52 | SpaceX Dragon Crew 4 (Dragon Freedom flight #1) 2022-042A 52318 |
Re-entered - 2022 Oct 14
Life 170 days
Returned to Earth |
| Crew flight to ISS provided by SpaceX under contract to NASA. Crew members - Kjell Lindgren (NASA), Bob Hines (NASA), Samantha Cristoforetti (ESA) and Jessica Watkins (NASA). Docked with the downward-facing port of the Harmony module at 23:37 UTC on the day of launch. Undocked 2022 Oct 14 at 14:05 UTC carrying original crew. After detaching the trunk module and retro-fire, splashed down off Florida at 20:55 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 27, 08:17 | 6579 | 0.0015 | 191 | 211 | 88.51 | 51.65 | 3 | | | | 2022 Apr 27, 12:30 | 6615 | 0.0040 | 210 | 263 | 89.23 | 51.64 | 229 | | | | 2022 Apr 28, 13:13 | 6795 | 0.0006 | 413 | 422 | 92.92 | 51.64 | 43 | | | | 2022 Oct 14, 11:21 | 6795 | 0.0003 | 414 | 419 | 92.90 | 51.64 | 303 | | | | 2022 Oct 14, 17:39 | 6785 | 0.0003 | 405 | 409 | 92.71 | 51.64 | 304 | | | | Crew Dragon trunk module 2022-042B 54047 |
Re-entered - 2023 Apr 5
Life 343 days
|
| Separated from Dragon Crew 4 shortly before retrofire. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 14, 23:56 | 6784 | 0.0006 | 402 | 410 | 92.68 | 51.33 | 311 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Apr 27
Life <1 day
|
| Launched Dragon Crew 4. Caused to re-enter above the Indian Ocean about 45 mins after lift-off. |
| Not Catalogued - orbit parameters unavailable | |
2022-043 CZ 2C
Jiuquan Space Centre | 2022 Apr 29, 04:11 | Siwei Gaojing 1-01 (Superview Neo 1-01) 2022-043A 52320 |
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. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Apr 29, 16:16 | 6873 | 0.0012 | 487 | 503 | 94.52 | 97.47 | 276 | 10:31 | | | 2022 May 07, 05:55 | 6875 | 0.0012 | 489 | 506 | 94.56 | 97.46 | 221 | 10:31 | | | 2022 Oct 16, 21:33 | 6869 | 0.0013 | 482 | 499 | 94.42 | 97.46 | 28 | 10:38 | | | 2022 Oct 17, 06:51 | 6874 | 0.0012 | 488 | 504 | 94.53 | 97.46 | 68 | 10:38 | | | Siwei Gaojing 1-02 (Superview Neo 1-02) 2022-043C 52322 |
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. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Apr 29, 16:15 | 6871 | 0.0013 | 484 | 502 | 94.47 | 97.47 | 290 | 10:31 | | | 2022 Jun 01, 18:40 | 6873 | 0.0020 | 481 | 508 | 94.51 | 97.47 | 160 | 10:32 | | | 2022 Oct 09, 21:42 | 6869 | 0.0020 | 477 | 505 | 94.42 | 97.46 | 68 | 10:38 | | | 2022 Oct 10, 05:21 | 6874 | 0.0012 | 488 | 505 | 94.54 | 97.46 | 65 | 10:38 | | | CZ 2C second stage 2022-043D 52323 |
Re-entered - 2023 Jun 20
Life 417 days
|
| Launched pair of Superview Neo 1 satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Apr 29, 07:06 | 6811 | 0.0091 | 371 | 495 | 93.24 | 97.56 | 25 | | | |
2022-044 Angara 1.2
Plesetsk Cosmodrome | 2022 Apr 29, 19:56 | Cosmos 2555 2022-044A 52330 |
Re-entered - 2022 May 17
Life 18 days
|
| Possible imaging reconnaissance satellite. Re-entry occurred within four weeks and there were no orbit adjustments. Separated from launch vehicle at 20:18 UTC. LTDN matches Cosmos 2551 (49127/2021-081A) that also re-entered naturally with no significant orbit changes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Apr 30, 05:08 | 6664 | 0.0011 | 278 | 293 | 90.22 | 96.45 | 240 | 11:30 | | | 2022 May 17, 22:17 | 6504 | 0.0014 | 117 | 135 | 87.00 | 96.42 | 229 | 11:29 | | | Orbit insertion stage uncatalogued |
Re-entered - 2022 Apr 29
Life <1 day
|
| Launched Cosmos 2555. Re-entered above the central Pacific Ocean at around 23:30 UTC after 2.3 revolutions. Orbit listed was attained after releasing the satellite and is based on analysis of amateur observations over Europe of a gas cloud resulting from the engine firing that caused reentry. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6945 | 0.0415 | 279 | 855 | 96.00 | 96.45 | 240 | | | |
2022-045 Falcon 9 Block 5 (Starlink Group 4-16)
Cape Canaveral Space Force Station | 2022 Apr 29, 21:27 | Starlink 3889 2022-045A 52331 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 22:26 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 04, 18:00 | 6699 | 0.0001 | 320 | 322 | 90.94 | 53.22 | 55 | | | | Falcon 9 upper stage uncatalogued |
in space
|
| Launched fifty three Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 23:30 UTC, 1.3 circuits after lift-off |
| Not Catalogued - orbit parameters unavailable | |
2022-046 CZ 11H
Towed barge 'Tai Rui', East China Sea - 32°.2 N, 123°.8 E | 2022 Apr 30, 03:30 | Jilin-1 High Resolution 04A 01 (Jilin-1 GF4A 01) 2022-046A 52388 |
in space
|
| Chinese high resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 01, 09:25 | 6917 | 0.0012 | 530 | 547 | 95.41 | 97.53 | 284 | 11:20 | | | Jilin-1 High Resolution 03D 07 (Jilin-1 GF3D 07) 2022-046B 52389 |
in space
|
| Chinese high resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 01, 09:25 | 6916 | 0.0010 | 531 | 545 | 95.40 | 97.54 | 284 | 11:20 | | | Jilin-1 High Resolution 03D 06 (Jilin-1 GF3D 06) 2022-046C 52390 |
in space
|
| Chinese high resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 01, 09:25 | 6916 | 0.0012 | 529 | 546 | 95.39 | 97.53 | 284 | 11:20 | | | Jilin-1 High Resolution 03D 05 (Jilin-1 GF3D 05) 2022-046D 52391 |
in space
|
| Chinese high resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 01, 22:15 | 6915 | 0.0013 | 528 | 546 | 95.38 | 97.55 | 288 | 11:20 | | | Jilin-1 High Resolution 03D 04 (Jilin-1 GF3D 04) 2022-046E 52392 |
in space
|
| Chinese high resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 01, 20:52 | 6915 | 0.0014 | 527 | 546 | 95.38 | 97.54 | 287 | 11:20 | | | CZ 11 fourth stage 2022-046F 52393 |
Re-entered - 2022 May 29
Life 29 days
|
| Launched cluster of Jilin 1 satellites. Perigee lowered after after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 02, 14:58 | 6763 | 0.0305 | 178 | 591 | 92.25 | 97.27 | 314 | | | |
2022-047 Electron (There And Back Again)
Rocket Lab Launch Complex, New Zealand | 2022 May 2, 22:49 | SpaceBEE 140 2022-047F 52399 |
Re-entered - 2024 Mar 7
Life 675 days
|
0.25U Cubesat from Swarm Technologies to provide a two-way communications system from LEO as part of a 150 satellite constellation. To aid tracking,the satellite carries a radar retro-reflector. It also carries a GPS receiver to help determine its location.
One of twenty four SpaceBEE satellites carried on this launch.
All were aimed at similar orbits, confirmation of activation awaited. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 10, 15:40 | 6906 | 0.0008 | 522 | 533 | 95.18 | 97.45 | 307 | 11:12 | | | |
Re-entered - 2024 Jun 7
Life 767 days
|
| 1p PocketQube satellite conducting tests on decoding weak signals and testing a very small satellite transmit/receive aerial. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 10, 14:06 | 6906 | 0.0008 | 523 | 534 | 95.20 | 97.45 | 315 | 11:12 | | | |
Re-entered - 2024 Aug 20
Life 841 days
|
| 1p PocketQube satellite demonstrating a weather reporting system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 10, 14:06 | 6906 | 0.0008 | 523 | 534 | 95.20 | 97.45 | 315 | 11:12 | | | |
Re-entered - 2024 May 31
Life 760 days
|
| 1p PocketQube satellite conducting tests on decoding weak signals and testing a very small satellite transmit/receive aerial. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 10, 14:06 | 6906 | 0.0008 | 523 | 534 | 95.20 | 97.45 | 316 | 11:12 | | | Unicorn 2x 2022-047AD 52421 |
Re-entered - 2023 Jun 6
Life 400 days
|
| 3p PocketQube satellite from Alba Orbital carring a night time imaging sensor to monitor light pollution across the globe. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 10, 14:06 | 6906 | 0.0008 | 522 | 534 | 95.19 | 97.45 | 316 | | | | BRO 6 (Breizh Reconnaissance Orbiter 6) 2022-047AE 52422 |
in space
|
| 6U Cubesat (3x2) from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 10, 14:09 | 6908 | 0.0007 | 525 | 534 | 95.23 | 97.45 | 328 | | | | |
in space
|
| 1.5U Cubesat from Aurora Technologies to demonstrate a water powered thruster and a de-orbit system using 'plasma drag' greated by an electrically charged ribbon. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6906 | 0.0008 | 523 | 534 | 95.20 | 97.45 | 316 | 11:12 | | | |
in space
|
| Small satellite to demonstrate satellite systems and payload for a future constellation for Internet communications. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6906 | 0.0008 | 523 | 534 | 95.20 | 97.45 | 316 | 11:12 | | | |
in space
|
| Small satellite to demonstrate satellite systems and payload for a future constellation for Internet communications. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6906 | 0.0008 | 523 | 534 | 95.20 | 97.45 | 316 | 11:12 | | | |
in space
|
| Small satellite to demonstrate satellite systems and payload for a future constellation for Internet communications. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6906 | 0.0008 | 523 | 534 | 95.20 | 97.45 | 316 | 11:12 | | | Electron second stage 2022-047AL 52428 |
Re-entered - 2022 May 18
Life 16 days
|
| Launched cluster of 34 satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 10, 06:16 | 6720 | 0.0247 | 176 | 508 | 91.37 | 97.44 | 226 | | | | Electron third stage (kick stage) 2022-047xx |
in space
|
Launched cluster of 34 satellites.
Copia - from Astrix Astonautics of New Zealand intentionally remains attached and aimed to demonstrate a large, inflatable solar panel for 1U Cubesats. Test inflation proved successful. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6909 | 0.0008 | 525 | 536 | 95.25 | 97.45 | 339 | | | |
2022-048 CZ 2D
Taiyuan Space Centre | 2022 May 5, 02:38 | Jilin-1 Wide Field 01C (Jilin-1 KF01C) 2022-048A 52443 |
in space
|
| Imaging satellite for Earth resources and land studies, particularly in relation to mining and urban construction industries. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 06, 05:31 | 6916 | 0.0012 | 530 | 546 | 95.40 | 97.68 | 264 | 09:47 | | | Jilin-1 High Resolution 03D 27 (Jilin-1 GF3D 27) 2022-048B 52450 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 06, 00:47 | 6915 | 0.0013 | 528 | 546 | 95.38 | 97.68 | 280 | 09:47 | | | Jilin-1 High Resolution 03D 28 (Jilin-1 GF3D 28) 2022-048C 52449 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 06, 00:47 | 6915 | 0.0013 | 528 | 546 | 95.38 | 97.68 | 273 | 09:47 | | | Jilin-1 High Resolution 03D 29 (Jilin-1 GF3D 29) 2022-048D 52448 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 06, 11:59 | 6915 | 0.0012 | 529 | 545 | 95.38 | 97.68 | 269 | 09:47 | | | Jilin-1 High Resolution 03D 30 (Jilin-1 GF3D 30) 2022-048E 52447 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 06, 07:07 | 6915 | 0.0013 | 528 | 546 | 95.39 | 97.68 | 270 | 09:47 | | | Jilin-1 High Resolution 03D 31 (Jilin-1 GF3D 31) 2022-048F 52446 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 06, 11:59 | 6916 | 0.0013 | 528 | 547 | 95.39 | 97.68 | 268 | 09:47 | | | Jilin-1 High Resolution 03D 32 (Jilin-1 GF3D 32) 2022-048G 52445 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 06, 05:31 | 6916 | 0.0013 | 529 | 546 | 95.39 | 97.68 | 268 | 09:47 | | | Jilin-1 High Resolution 03D 33 (Jilin-1 GF3D 33) 2022-048H 52444 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 06, 00:47 | 6916 | 0.0012 | 529 | 546 | 95.40 | 97.68 | 267 | 09:47 | | | CZ 2D second stage uncatalogued |
in space
|
| Launched cluster of Jilin-1 satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2022-049 Falcon 9 Block 5 (Starlink Group 4-17)
Kennedy Space Center | 2022 May 6, 09:42 | Starlink 3870 2022-049A 52451 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 10:36 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 13, 14:00 | 6710 | 0.0001 | 331 | 332 | 91.16 | 53.22 | 42 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 May 6
Life <1 day
|
| Launched fifty three Starlink satellites. Caused to re-enter after releasing satellites with surviving fragments hitting the south Atlantic/south western Indian Ocean about 11:55 UTC, 1.3 circuits after lift-off |
| Not Catalogued - orbit parameters unavailable | |
2022-050 CZ 7 (Y-5)
Wenchang Space Centre | 2022 May 9, 17:56 | |
Re-entered - 2022 Nov 14
Life 189 days
|
| Supplies and equipment to Chinese Space Station (CSS) in advance of the Shenzhou 14 crew mission. Made rendezvous with CSS and the final docking command was issued May 10 at 00:54 UTC. Docked with the rear port of Tianhe a few minutes later. Also includes a set of hosted payloads consisting of a set of space science and engineering sensors operated independently of the space station mission. Undocked 2022 Nov 9, 06:55 UTC. Retro-fire led to re-entry above the southern Pacific Ocean Nov 14, 23:21 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 09, 22:12 | 6748 | 0.0010 | 363 | 376 | 91.93 | 41.46 | 288 | | | | 2022 May 10, 13:55 | 6763 | 0.0012 | 376 | 393 | 92.24 | 41.47 | 306 | | | | 2022 Nov 08, 13:27 | 6766 | 0.0009 | 382 | 394 | 92.32 | 41.48 | 256 | | | | 2022 Nov 09, 15:31 | 6766 | 0.0010 | 381 | 394 | 92.31 | 41.48 | 261 | | | | 2022 Nov 09, 23:28 | 6763 | 0.0016 | 374 | 395 | 92.24 | 41.48 | 271 | | | | |
Re-entered - 2023 Feb 12
Life 279 days
|
| 6U Cubesat carrying an Earth imaging system. Released from Tianzhou 4 on Nov 13 at 22:02 UTC, after Tianzhou departed from CSS. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Nov 16, 14:26 | 6763 | 0.0015 | 375 | 395 | 92.25 | 41.48 | 331 | | | | CZ 7 third stage 2022-050C 52511 |
Re-entered - 2022 May 16
Life 7 days
|
| Launched Tianzhou 4. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 09, 23:44 | 6641 | 0.0094 | 201 | 325 | 89.77 | 41.47 | 174 | | | |
2022-F02 - failed to reach orbit Hyperbola 1 (Y4)
Jiuquan Space Centre | 2022 May 13, 07:09 | |
|
| Details awaited - lost when the launch vehicle failed to achieve orbit. |
|
2022-051 Falcon 9 Block 5 (Starlink Group 4-13)
Vandenberg Space Force Base | 2022 May 13, 22:07 | Starlink 3951 2022-051A 52533 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at about 23:11 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 18, 18:00 | 6703 | 0.0001 | 324 | 326 | 91.03 | 53.22 | 54 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 May 13
Life <1 day
|
| Launched fifty three Starlink satellites. Directed to re-enter above the Pacific Ocean within a few hours of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-052 Falcon 9 Block 5 (Starlink Group 4-15)
Cape Canaveral Space Force Station | 2022 May 14, 20:40 | Starlink 4019 2022-052A 52598 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at about 21:44 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 20, 16:00 | 6709 | 0.0001 | 330 | 331 | 91.14 | 53.22 | 91 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 May 14
Life <1 day
|
| Launched fifty three Starlink satellites. Directed to re-enter late on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-053 Falcon 9 Block 5 (Starlink Group 4-18)
Cape Canaveral Space Force Station | 2022 May 18, 10:59 | Starlink 4004 2022-053A 52656 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 11:58 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 24, 15:13 | 6709 | 0.0002 | 329 | 332 | 91.14 | 53.21 | 54 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 May 18
Life <1 day
|
| Launched fifty three Starlink satellites. Directed to re-enter late on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-054 Soyuz-2 1A
Plesetsk Cosmodrome | 2022 May 19, 08:03 | Cosmos 2556 (Bars-M №3) 2022-054A 52713 |
in space
|
| Russian government optical imaging satellite for use in cartography. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 May 19, 11:28 | 6825 | 0.0160 | 338 | 556 | 93.52 | 97.69 | 72 | 23:47 | | | 2022 May 20, 20:06 | 6828 | 0.0157 | 343 | 556 | 93.58 | 97.69 | 69 | 23:47 | | | 2022 May 21, 13:28 | 6839 | 0.0140 | 365 | 557 | 93.81 | 97.70 | 63 | 23:47 | | | 2022 May 21, 17:59 | 6860 | 0.0109 | 407 | 557 | 94.25 | 97.69 | 62 | 23:47 | | | 2022 May 22, 06:47 | 6904 | 0.0050 | 491 | 560 | 95.14 | 97.70 | 45 | 23:47 | | | 2022 May 23, 01:54 | 6947 | 0.0015 | 559 | 579 | 96.04 | 97.68 | 282 | 23:47 | | | 2022 May 23, 05:06 | 6950 | 0.0010 | 565 | 579 | 96.10 | 97.70 | 271 | 23:47 | | | 2022 Jun 20, 07:47 | 6935 | 0.0019 | 544 | 570 | 95.79 | 97.69 | 246 | 23:47 | | | 2022 Jul 10, 12:45 | 6887 | 0.0005 | 505 | 512 | 94.80 | 97.69 | 234 | 23:48 | | | 2022 Sep 30, 15:43 | 6886 | 0.0006 | 504 | 512 | 94.78 | 97.69 | 331 | 23:59 | | | 2022 Oct 01, 12:33 | 6885 | 0.0006 | 503 | 511 | 94.77 | 97.55 | 330 | 23:59 | | | 2023 Mar 31, 20:15 | 6880 | 0.0009 | 495 | 507 | 94.65 | 97.55 | 52 | 00:10 | | | 2023 Nov 22, 03:14 | 6871 | 0.0005 | 489 | 496 | 94.47 | 97.55 | 317 | 00:29 | | | 2023 Dec 21, 03:29 | 6870 | 0.0006 | 487 | 496 | 94.44 | 97.56 | 186 | 00:31 | | | 2024 Oct 31, 04:18 | 6866 | 0.0014 | 479 | 498 | 94.37 | 97.57 | 95 | 00:59 | | | Soyuz upper stage 2022-054B 52714 |
Re-entered - 2023 Jun 6
Life 383 days
|
| Launched Cosmos 2556. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 19, 09:53 | 6824 | 0.0160 | 337 | 555 | 93.51 | 97.70 | 73 | | | |
2022-055 Atlas V N22
Cape Canaveral Air Force Station | 2022 May 19, 22:54 | Starliner OrbitalFlight Test 2 (Starliner CST-100 #2, Flight 1) 2022-055A 52715 |
Re-entered - 2022 May 25
Life 6 days
Returned to Earth |
| Second test mission of Boeing-built spacecraft to be used for ferrying crew and cargo to/from ISS. No crew carried on this mission but it included a cargo, and an instrumented anthropomorphic dummy in one of the seats. Repeat of mission profile for OFT 1 in 2019, necessitated by failure to meet the goals of the earlier mission. Docked with forward-facing port of the Unity module May 21, 00:38 UTC. Undocked May 25, 18:36 UTC. Retro-fire at 23:05 UTC led to a parachute-assisted landing on the White Sands Missile Range at 22:49 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 20, 05:01 | 6745 | 0.0009 | 361 | 373 | 91.88 | 51.64 | 274 | | | | 2022 May 20, 23:38 | 6796 | 0.0005 | 415 | 421 | 92.93 | 51.64 | 140 | | | | 2022 May 25, 21:13 | 6796 | 0.0006 | 414 | 422 | 92.93 | 51.64 | 107 | | | | Atlas V upper stage (Centaur) sub-orbital |
Re-entered - 2022 May 19
Life <1 day
|
| Launched Boeing Starliner OFT 2. Re-entered the atmosphere above Indian Ocean around one hour after lift off. |
| See individual satellites for orbit info | |
2022-056 CZ 2C + YZ-1S
Jiuquan Space Centre | 2022 May 20, 10:30 | LEO Comms Test Satellite A 2022-056A 52716 |
in space
|
| Demonstrator for an LEO communications system - maybe store-dump or maybe broadband internet. Launch time chosen to match the orbit plane of a similar triplet of satellites launched 2021 Aug 24 (2021-076). |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 21, 18:24 | 7261 | 0.0018 | 870 | 896 | 102.63 | 86.00 | 303 | | | | 2023 Jun 05, 04:21 | 7259 | 0.0019 | 868 | 895 | 102.59 | 86.00 | 203 | | | | LEO Comms Test Satellite B 2022-056B 52717 |
in space
|
| Demonstrator for an LEO communications system - maybe store-dump or maybe broadband internet. Launch time chosen to match the orbit plane of a similar triplet of satellites launched 2021 Aug 24 (2021-076). Started to raise orbit at a rate of 5 km per day on May 30. Thruster firing ceased Jun 15 then resumed Jun 22. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 21, 11:32 | 7258 | 0.0013 | 871 | 890 | 102.57 | 86.00 | 303 | | | | 2022 May 28, 19:45 | 7261 | 0.0013 | 873 | 892 | 102.62 | 86.00 | 272 | | | | 2022 Jun 03, 12:47 | 7272 | 0.0013 | 885 | 904 | 102.86 | 86.00 | 271 | | | | 2022 Jun 09, 11:28 | 7295 | 0.0027 | 897 | 937 | 103.34 | 86.00 | 273 | | | | 2022 Jun 15, 11:06 | 7313 | 0.0032 | 911 | 958 | 103.73 | 86.00 | 267 | | | | 2022 Jun 22, 00:49 | 7314 | 0.0033 | 912 | 960 | 103.76 | 86.01 | 248 | | | | 2022 Jul 16, 06:15 | 7361 | 0.0026 | 964 | 1002 | 104.75 | 86.00 | 258 | | | | 2023 Jun 04, 20:22 | 7527 | 0.0045 | 1115 | 1182 | 108.31 | 86.01 | 174 | | | | LEO Comms Test Satellite C 2022-056C 52718 |
in space
|
| Demonstrator for an LEO communications system - maybe store-dump or maybe broadband internet. Launch time chosen to match the orbit plane of a similar triplet of satellites launched 2021 Aug 24 (2021-076). |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 21, 18:22 | 7258 | 0.0013 | 870 | 889 | 102.56 | 86.00 | 298 | | | | 2022 Jul 28, 18:50 | 7260 | 0.0017 | 870 | 895 | 102.61 | 86.00 | 85 | | | | 2023 Jun 05, 04:28 | 7259 | 0.0015 | 871 | 892 | 102.59 | 86.00 | 193 | | | | YZ-1S rocket stage 2022-056D 52719 |
Re-entered - 2022 May 21
Life 1 day
|
| Launched triplet of LEO communication test satellites. Perigee lowered with a thruster firing at about 12:10 UTC. Re-entered May 21 at 14:53 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 May 20, 17:54 | 6816 | 0.0507 | 92 | 784 | 93.34 | 85.95 | 299 | | | | 2022 May 20, 20:59 | 6787 | 0.0467 | 92 | 726 | 92.74 | 85.95 | 298 | | | | 2022 May 20, 22:32 | 6772 | 0.0448 | 91 | 697 | 92.44 | 85.95 | 298 | | | | 2022 May 21, 05:11 | 6700 | 0.0348 | 89 | 555 | 90.97 | 85.95 | 297 | | | | 2022 May 21, 06:10 | 6687 | 0.0329 | 89 | 529 | 90.71 | 85.95 | 296 | | | | 2022 May 21, 10:55 | 6614 | 0.0219 | 91 | 380 | 89.21 | 85.95 | 294 | | | | 2022 May 21, 12:10 | 6591 | 0.0183 | 92 | 333 | 88.75 | 85.96 | 293 | | | |
2022-057 Falcon 9 Block 5 (Transporter 5)
Cape Canaveral Space Force Station | 2022 May 25, 18:35 | Lemur-2 (TennysonLily) 2022-057A 52732 |
Re-entered - 2024 Mar 14
Life 659 days
|
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. Lemur-2 satellites are named after development and support team members.
One of FOUR similar satellites carried on the Tranporter 5 launch. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:38 | 6910 | 0.0008 | 526 | 538 | 95.28 | 97.52 | 235 | | | | Pathfinder Technology Demonstrator 3 (PTD-3) 2022-057C 52734 |
Re-entered - 2024 Sep 14
Life 843 days
|
| 6U Cubesat from NASA as the first in a series of missions using a new commercial spacecraft bus. Carried the TeraByte InfraRed Delivery , or TBIRD, payload developed by the Massachusetts Institute of Technology’s Lincoln Laboratory in collaboration with NASA’s Goddard Space Flight Center. It aims to demonstrate a 200 GB/s laser-based comms downlink. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:37 | 6909 | 0.0009 | 525 | 537 | 95.26 | 97.52 | 229 | | | | Cicero-2 2 (Community Initiative for Cellular Earth Remote Observation) 2022-057D 52735 |
Re-entered - 2024 Sep 9
Life 838 days
|
| 6U Cubesat equipped to perform GPS and Galileo radio occultation observations by the Earth's atmosphere and undertake surface remote sensing by reflected navigation satellite signals. One of a simultaneously pair in an upgrade to the existing CICERO constellation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:37 | 6909 | 0.0008 | 526 | 537 | 95.26 | 97.51 | 225 | | | | GHGSat C3 (Luca) 2022-057F 52737 |
in space
|
| Small satellite in a constellation being built for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:36 | 6909 | 0.0008 | 525 | 537 | 95.26 | 97.51 | 221 | | | | |
in space
|
| 1U Cubesat from Czech company Spacemaniac. Built for Planetum for astronomical studies by cluster of Prague observatories and planetariums, also carrying an amateur radio payload. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:36 | 6909 | 0.0008 | 525 | 536 | 95.25 | 97.51 | 218 | | | | Connecta T1.1 2022-057H 52739 |
in space
|
| 3U Cubesat from Turkish company Plan-S as a demonstrator for a constellation of broadband communications satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:36 | 6909 | 0.0009 | 525 | 537 | 95.25 | 97.52 | 223 | | | | Lemur-2 + Hancom payload (Sejong 1) 2022-057J 52740 |
Re-entered - 2024 Jul 26
Life 793 days
|
| 6U Cubesat carrying a payload from the Hancom company of South Korea, equipped with a multispectral Earth imaging system. Design is based on the 3U Lemur-2 satellite from Spire but with specialised instrumentation alongside the standard Lemur-2 equipment. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jun 01, 13:35 | 6909 | 0.0010 | 524 | 538 | 95.25 | 97.53 | 227 | 13:10 | | | Cicero-2 1 (Community Initiative for Cellular Earth Remote Observation) 2022-057K 52741 |
Re-entered - 2024 Sep 18
Life 847 days
|
| 6U Cubesat equipped to perform GPS and Galileo radio occultation observations by the Earth's atmosphere and undertake surface remote sensing by reflected navigation satellite signals. One of a simultaneously pair in an upgrade to the existing CICERO constellation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:35 | 6909 | 0.0010 | 524 | 537 | 95.25 | 97.52 | 224 | | | | |
Re-entered - 2024 Oct 1
Life 860 days
|
| 6U Cubesat from Fleet Space - one of a planned constellation of 140 satellites to provide internet connectivity for ground based sensors. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:35 | 6909 | 0.0008 | 525 | 536 | 95.25 | 97.51 | 216 | | | | Agile Microsatellite (AMS) 2022-057N 52745 |
Re-entered - 2023 Oct 17
Life 510 days
|
| 6U Cubesat from MIT Lincoln Laboratory carrying a remote sensing payload. It will also be used to demonstrate satellite operations in an extremely low orbit. Released from Sherpa AC-1 before it too was released from the Falcon 9 rocket. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:34 | 6908 | 0.0009 | 524 | 536 | 95.23 | 97.51 | 207 | | | | GHGSat C5 (Diako) 2022-057N 52744 |
in space
|
| Small satellite in a constellation being built for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:34 | 6908 | 0.0009 | 524 | 537 | 95.24 | 97.52 | 219 | | | | GHGSat C4 (Penny) 2022-057Q 52746 |
in space
|
| Small satellite in a constellation being built for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:34 | 6908 | 0.0009 | 524 | 536 | 95.23 | 97.51 | 209 | | | | ÑuSat 28 (Alice Lee) 2022-057R 52747 |
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.
One of four similar satellites carried on the Transporter 5 launch. All are in similar orbits. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:33 | 6908 | 0.0010 | 523 | 536 | 95.23 | 97.52 | 213 | | | | |
Re-entered - 2024 Apr 8
Life 684 days
|
| Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Released from launch vehicle at 16:47 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:32 | 6907 | 0.0010 | 522 | 536 | 95.22 | 97.51 | 205 | | | | Hawk 5A (Alex Witko, Cluster 5 #1) 2022-057AB 52757 |
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.
One of THREE similar satellites carried on the Transporter 5 launch. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:31 | 6907 | 0.0010 | 522 | 536 | 95.21 | 97.52 | 208 | | | | Vigoride 3 2022-057AE 52760 |
in space
|
Satellite carrier from US company Momentus Systems, carrying a number of hosted payloads, Cubesats and PocketQubes to be released in the weeks after launch. Planned lifetime for the hosted payloads is six months. Experienced several problems after departing the launch vehicle the major of which was the solar array failing to function at full capacity, restricting the ability to release the satellites and provide power to the hosted payloads.
Satellites:
Fossasat 2E 9 - 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity - not released.
Fossasat 2E 10 - 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity - not released.
Fossasat-2E 11 - released May 28,
Fossasat-2E 12 - released May 28,
Fossasat-2E 13 - released Jul 18,
Veery Hatchling (Orion/FS-1) - released Jul 18,
Fossasat 2E 7 - released Jul 30,
Fossasat 2E 8- released Jul 30,
SelfieSat - released late-August. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:30 | 6906 | 0.0011 | 521 | 536 | 95.20 | 97.52 | 205 | | | | 2022 Jul 18, 03:10 | 6906 | 0.0013 | 519 | 537 | 95.19 | 97.52 | 55 | | | | 2022 Jul 30, 13:37 | 6906 | 0.0012 | 519 | 536 | 95.19 | 97.52 | 16 | | | | ION SCV-006 (Thrilling Thomas) 2022-057AF 52761 |
in space
|
Satellite Carrier Vehicle built by D-Orbit carrying a pair of satellites for later deployment:
Guardian - released Jul 5 at 12:54 UTC,
SBUDNIC - released 2022 Jun 9 at 09:31:27 UTC.
Also carries two hosted payloads:
Crypto 1 - protype 1U Cubesat for undertaking cryptographic transactions from an orbiting space vehicle.
Gen 01 - from secretive, possibly Italian, company/organisation called Genergo, testing a novel space propulsion system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:30 | 6906 | 0.0011 | 520 | 536 | 95.20 | 97.52 | 206 | | | | |
in space
|
Small satellite fitted with a sythetic aperture radar for Earth surface imaging.
One of FIVE similar satellites carried on the Transporter 5 launch. All are in similar orbits. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jun 01, 13:30 | 6906 | 0.0011 | 520 | 536 | 95.19 | 97.52 | 208 | 13:10 | | | Sherpa AC-1 2022-057AH 52763 |
in space
|
Satellite carrier vehicle carrying two hosted paylods:
Huginn - demonstrator for a navigation system in LEO,
TROOP 3 (Train Rapid on Orbit Payload) - carrying a number of payloads for paying customers and designed to operate for eight years.
Also released three satellites while still attached to the Falcon 9:
Agile Microsatellite - see separate entry,
CNCE 4 - see separate entry,
CNCE 5 - see separate entry. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:29 | 6906 | 0.0012 | 519 | 536 | 95.19 | 97.52 | 203 | | | | Urdaneta (ArmSat 1) 2022-057AK 52765 |
in space
|
| 16U-CubeSat from Spanish company Satlantis, equipped with a camera and a binocular telescope for Earth imaging. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:27 | 6905 | 0.0013 | 518 | 536 | 95.17 | 97.52 | 200 | | | | Varisat 1C (Celestis 21) 2022-057AL 52766 |
in space
|
| 6U Cubesat from US company OmniTeq to test use of satellites to carry communications from ships at sea using HF frequencies. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 02, 00:34 | 6905 | 0.0013 | 517 | 536 | 95.17 | 97.52 | 201 | | | | CNCE 4 (Cubesat Networked Communications Experiment) 2022-057AM 52767 |
Re-entered - 2024 Apr 23
Life 699 days
|
| 3U Cubesat from the US Missile Defense Agency to demonstrate networked radio communication between satellites on orbit. One of a simulaneously-launched pair released from Sherpa AC-1 before it too was released from the Falcon 9 rocket. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:27 | 6905 | 0.0013 | 518 | 535 | 95.16 | 97.51 | 199 | | | | CNCE 5 (Cubesat Networked Communications Experiment) 2022-057AN 52768 |
Re-entered - 2024 Apr 18
Life 694 days
|
| 3U Cubesat from the US Missile Defense Agency to demonstrate networked radio communication between satellites on orbit. One of a simulaneously-launched pair released from Sherpa AC-1 before it too was released from the Falcon 9 rocket. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:27 | 6905 | 0.0013 | 517 | 535 | 95.16 | 97.51 | 199 | | | | Platform 1 (Sharedsat 2141) 2022-057AQ 52770 |
in space
|
| 6U Cubesat from Endurosat carrying a number of unspecified payloads. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:26 | 6904 | 0.0013 | 517 | 535 | 95.16 | 97.51 | 193 | | | | Spark 2 (Omni LEO 2) 2022-057AR 52771 |
in space
|
| Small satellite from Omnispace, demonstrator for a future LEO comsat constellation to include internet connectivity. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:25 | 6904 | 0.0014 | 516 | 535 | 95.15 | 97.52 | 196 | | | | C-POD 1 (Cubesat Proximity Operations Demonstration) 2022-057AS 52772 |
Re-entered - 2024 Jun 9
Life 746 days
|
| 3U Cubesat - one of two satellites launched as a joined pair, making 6U, from NASA Ames to demonstrate rendezvous, station keeping and docking of Cubesats. Separated from C-POD 2 (52780/2022-057BB) on 2022 Oct 20 around 06:30-07:00 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:25 | 6904 | 0.0014 | 516 | 535 | 95.14 | 97.52 | 194 | | | | FossaSat-2E 11 2022-057AS 52750 |
Re-entered - 2023 Sep 8
Life 471 days
|
| 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride May 28. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:29 | 6905 | 0.0012 | 519 | 535 | 95.18 | 97.52 | 210 | | | | FossaSat-2E 12 2022-057AT 52773 |
Re-entered - 2023 Oct 31
Life 524 days
|
| 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride May 28. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:29 | 6905 | 0.0012 | 519 | 536 | 95.18 | 97.52 | 210 | | | | SBUDNIC (Satellite by Brown University, D-Orbit, and the National Italian Council for Research) 2022-057AU 52774 |
Re-entered - 2023 Aug 10
Life 442 days
|
| 3U CubeSat developed by Brown University in collaboration with the Institute on Atmospheric Pollution of the National Research Council of Italy to collect and panoramic views of space. Released from ION SCV-006 Jun 9 at 09:31:27 UTC. After its mission is complete, SBUDNIC will deploy a drag sail to deorbit itself. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 21, 14:19 | 6902 | 0.0009 | 518 | 530 | 95.11 | 97.52 | 149 | | | | Guardian 1 2022-057AV 52775 |
in space
|
| 6U CubeSat from by Aistech carrying a multispectral telescope for imaging to support commercial services linked to environmental sustainability. Released from ION SCV-006 Jul 5 at 12:54 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 13, 13:41 | 6908 | 0.0012 | 522 | 538 | 95.24 | 97.52 | 86 | | | | Fossasat-2E 13 2022-057AW 52776 |
Re-entered - 2024 Feb 3
Life 619 days
|
| 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride 2022 Jul 18 ~08:00-09:00 UTC together with Veery Hatchling (52777/2022-057AX). |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 29, 13:39 | 6903 | 0.0015 | 514 | 535 | 95.13 | 97.52 | 10 | | | | Veery Hatchling (Veery FS-1) 2022-057AX 52777 |
Re-entered - 2024 Apr 11
Life 687 days
|
| 1p PocketQube from Fossasat built for Careweather carrying a wind scatterometer as a demonstrator for a future constellation of weather monitoring satellites. The satellite carries a four-panel drag device to shorten orbital lifetime. Separated from Vigoride 3 2022 Jul 18, ~08:00-09:00 UTC together with Fossasat 2E-13 (52776/2022-057AW) |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 29, 13:38 | 6903 | 0.0015 | 514 | 535 | 95.13 | 97.52 | 10 | | | | FossaSat-2E 7 2022-057AY 52778 |
Re-entered - 2023 Aug 22
Life 454 days
|
| 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride Jul 30. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 13:11 | 6906 | 0.0013 | 519 | 537 | 95.19 | 97.52 | 344 | | | | FossaSat-2E 8 2022-057AZ 52779 |
Re-entered - 2023 Oct 31
Life 524 days
|
| 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride Jul 30. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 11, 11:24 | 6906 | 0.0013 | 519 | 537 | 95.20 | 97.52 | 341 | | | | |
Re-entered - 2024 Sep 6
Life 835 days
|
2U Cubesat - from NTNU of Norway. Equipped with external LCD-display to show pictures sent in by the public. A camera mounted on an arm will photograph the screen with the Earth in the background. Released from Vigoride 3 late-August and initially identified by amateur observers using radio techniques. Space-Track eventually published orbit data at the end of September.
|
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 27, 13:38 | 6905 | 0.0011 | 519 | 535 | 95.17 | 97.53 | 166 | | | | C-POD 2 (Cubesat Proximity Operations Demonstration) 2022-057BB 52780 |
Re-entered - 2024 Jun 14
Life 751 days
|
| 3U Cubesat - one of two satellites launched as a joined pair, making 6U, from NASA Ames to demonstrate rendezvous, station keeping and docking of Cubesats. Separated from C-POD 1 (52772/2022-057AS) on 2022 Oct 20 around 06:30-07:00 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 27, 06:16 | 6899 | 0.0015 | 511 | 531 | 95.04 | 97.53 | 53 | | | | |
in space
|
| 1.5U Cubesat from Bronco Space to demonstrate Artificial Intelligence and Machine Learning for analysing Earth Images produced by an onboard imaging system before transmission to Earth. Indication is that the satellite failed to activate properly after release from Falcon 9 upper stage. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:33 | 6908 | 0.0009 | 523 | 536 | 95.23 | 97.51 | 205 | | | | |
in space
|
| 3U Cubesat from the University of Turku, Finland equipped with a charged-particle telescope to study the near-Earth radiation environment. Also carries a plasma brake to take the satellite out of orbit at the end of its life. Indication is that the satellite failed to activate properly after release from Falcon 9 upper stage. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 01, 13:35 | 6909 | 0.0008 | 525 | 536 | 95.24 | 97.51 | 215 | | | | |
Re-entered - 2022 May 25
Life <1 day
|
Launched Transporter 5 cluster of satellites. Caused to re-enter above the south eastern Pacific Ocean around 20:30 UTC.
Carried Nanoracks hosted payload:
Mars Demo 1 - to demonstrate debris-free metal cutting in microgravity and a vacuum. The experiment was contained within a closed container and was partially successful in that one of three samples were cut by the saw. |
| Not Catalogued - orbit parameters unavailable | |
2022-058 CZ 2C
Xichang Space Centre | 2022 Jun 2, 04:00 | GeeSat 1-01 2022-058A 52785 |
in space
|
Small satellite owned by China's Geely automotive group. Part of a system to provide supplementary navigation information to self-driving motor vehicles.
One of nine similar satellites carried on this launch. All are in similar orbits. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 02, 10:05 | 6988 | 0.0014 | 600 | 619 | 96.88 | 49.99 | 288 | | | | CZ 2C second stage 2022-058K 52794 |
in space
|
| Launched cluster of nine Geesats. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 02, 09:59 | 6912 | 0.0104 | 462 | 606 | 95.32 | 50.16 | 41 | | | |
2022-059 Soyuz-2 1A
Baikonur Cosmodrome | 2022 Jun 3, 09:32 | Progress MS-20 (Progress 7K-MS №450) 2022-059A 52795 |
Re-entered - 2023 Feb 7
Life 249 days
|
| Supplies and equipment to ISS. Docked with the Zvezda module at 16:02 UTC (time to be confirmed). Undocked 2023 Feb 7, 04:56 UTC. Retro-fire at 08:04 UTC led to destructive re-entry above the southern Pacific Ocean with any surviving fragments hitting the ocean surface at about 08:44 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 03, 10:01 | 6583 | 0.0024 | 189 | 221 | 88.59 | 51.66 | 71 | | | | 2022 Jun 03, 11:31 | 6795 | 0.0005 | 414 | 420 | 92.91 | 51.65 | 190 | | | | Soyuz upper stage 2022-059B 52796 |
Re-entered - 2022 Jun 5
Life 2 days
|
| Launched Progress MS-20. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 03, 10:04 | 6582 | 0.0027 | 186 | 221 | 88.56 | 51.65 | 70 | | | |
2022-060 CZ 2F
Jiuquan Space Centre | 2022 Jun 5, 02:44 | Shenzhou 14 2022-060A 52797 |
Re-entered - 2022 Dec 4
Life 182 days
Returned to Earth |
| Crew to CSS - Chen Dong (commander), Liu Yang and Cai Xuzhe. Docked with the downward-facing port of the Tianhe module at 09:42 UTC. Initial orbit similar to rocket upper stage. Undocked, carrying original crew, 2022 Dec 4 at 03:01 UTC. Retro-fire at 11:21 UTC led to landing near Jiuquan at about 12:10:29 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 05, 16:28 | 6766 | 0.0004 | 385 | 391 | 92.31 | 41.47 | 221 | | | | 2022 Dec 02, 14:10 | 6768 | 0.0006 | 386 | 394 | 92.35 | 41.48 | 0 | | | | CZ 2F third stage 2022-060B 52798 |
Re-entered - 2022 Jun 21
Life 16 days
|
| Launched Shenzhou 14. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 05, 13:05 | 6648 | 0.0108 | 198 | 341 | 89.91 | 41.47 | 126 | | | | Shenzhou 14 Orbital Module 2022-060G 54704 |
Re-entered - 2023 Oct 12
Life 494 days
|
| Released from Shenzhou 14 2022 Dec 4, at 11:20 UTC. Space-Track was tardy in issuing orbit info, initial orbit was probably about 385 x 394 km. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Dec 12, 13:06 | 6765 | 0.0007 | 382 | 392 | 92.29 | 41.48 | 116 | | | |
2022-061 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2022 Jun 8, 21:04 | Nilesat 301 2022-061B 52817 |
in space
|
| Egyptian comsat providing communication services to the Middle East including TV broadcasting, broadband and internet connectivity. Released from launch vehicle at 21:37 UTC. Expected location - 7° west. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Jun 09, 13:44 | 29019 | 0.7694 | 312 | 44969 | 819.92 | 18.64 | 179 | | | | 2022 Jun 10, 10:00 | 33671 | 0.5246 | 9627 | 44958 | 1024.80 | 7.28 | 179 | | | | 2022 Jun 13, 20:52 | 41929 | 0.2247 | 26132 | 44971 | 1424.09 | 1.93 | 179 | | | | 2022 Jun 14, 16:39 | 46815 | 0.0971 | 35889 | 44983 | 1680.08 | 0.60 | 178 | | | | 2022 Jun 14, 21:36 | 47103 | 0.1005 | 35990 | 45460 | 1695.65 | 0.49 | 186 | | | | 2022 Jun 22, 10:53 | 42165 | 0.0000 | 35785 | 35788 | 1436.09 | 0.03 | 272 | 10° west | | | 2022 Jul 04, 21:00 | 42133 | 0.0002 | 35748 | 35761 | 1434.47 | 0.02 | 157 | 7° west | | | Falcon 9 upper stage 2022-061B 52818 |
in space
|
| Launched Nilesat 301. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 10, 08:02 | 29000 | 0.7694 | 309 | 44934 | 819.13 | 18.65 | 180 | | | |
2022-F03 - failed to reach orbit Rocket 3.3 (Astra LV0010)
Cape Canaveral Space Force Station | 2022 Jun 12, 17:43 | TROPICS 02 (Time-Resolved Observations of Precipitation structure and storm Intensity with a Constellation of Smallsats) |
|
| 3U Cubesat - one of a simultaneously-launched pair from NASA in co-operation with MIT Lincoln Laboratory. Carried on first launch of three to set up a constellation of six satellites to study thermodynamics of the troposphere and precipitation in storm centres within the tropical region of the Earth's atmosphere. Lost when the launch vehicle second stage shut down early and failed to reach orbital velocity. |
| TROPICS 04 (Time-Resolved Observations of Precipitation structure and storm Intensity with a Constellation of Smallsats) |
|
| 3U Cubesat - one of a simultaneously-launched pair from NASA in co-operation with MIT Lincoln Laboratory. Carried on first launch of three to set up a constellation of six satellites to study thermodynamics of the troposphere and precipitation in storm centres within the tropical region of the Earth's atmosphere. Lost when the launch vehicle second stage shut down early and failed to reach orbital velocity. |
|
2022-062 Falcon 9 Block 5 (Starlink Group 4-19)
Kennedy Space Center | 2022 Jun 17, 16:09 | Starlink 4091 2022-062A 52830 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 16:25 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 22, 14:00 | 6679 | 0.0041 | 273 | 328 | 90.53 | 53.22 | 56 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jun 17
Life <1 day
|
| Launched fifty three Starlink satellites. Directed to destructive re-entry above the eastern Pacific Ocean at around 17:30 UTC on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-063 Falcon 9 Block 5
Vandenberg Space Force Base | 2022 Jun 18, 14:19 | |
in space
|
| German military satellite carrying an imaging radar system. Successor to the SAR-Lupe satellites launched 2006-2008. Orbital data ceased to be published as of 2022 Jun 23. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jun 19, 08:32 | 7125 | 0.0006 | 743 | 751 | 99.76 | 98.40 | 129 | 05:59 | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jun 18
Life <1 day
|
| Launched SARah 1. Directed to destructive re-entry above the mid Pacific Ocean at around 15:30 UTC on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-064 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2022 Jun 19, 04:27 | Globalstar-2 M087 (Globalstar-2 FM-15) 2022-064A 52888 |
in space
|
| Part of constellation of satellites providing on-demand telephone and low-speed data communications. Held as a ground spare for more than ten years after launch of the earlier constellation of Globalstar satellites. Released from the launch vehicle at 06:20 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 20, 16:03 | 7497 | 0.0009 | 1111 | 1125 | 107.66 | 51.98 | 319 | | | | 2022 Jul 17, 06:30 | 7497 | 0.0010 | 1111 | 1126 | 107.66 | 51.97 | 27 | | | | USA 328 (Starshield Demonstrator?) 2022-064B 52889 |
in space
|
| US government/military satellite, probably operated by, or for, the National Reconnaissance Office - SpaceX Starshield satellite that provides a hosting platform for a variety missions and uses the Starlink infrastructure for communications. Purpose unknown. Not originally declared in the manifest for this launch. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 22, 22:43 | 6903 | 0.0011 | 518 | 533 | 95.14 | 53.01 | 214 | | | | USA 329 (Starshield Demonstrator?) 2022-064C 52890 |
in space
|
| US government/military satellite, probably operated by, or for, the National Reconnaissance Office - SpaceX Starshield satellite that provides a hosting platform for a variety missions and uses the Starlink infrastructure for communications. Purpose unknown. Not originally declared in the manifest for this launch. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 22, 22:43 | 6903 | 0.0010 | 519 | 532 | 95.14 | 53.02 | 227 | | | | USA 330 (Starshield Demonstrator?) 2022-064D 52891 |
in space
|
| US government/military satellite, probably operated by, or for, the National Reconnaissance Office - SpaceX Starshield satellite that provides a hosting platform for a variety missions and uses the Starlink infrastructure for communications. Purpose unknown. Not originally declared in the manifest for this launch. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 22, 22:44 | 6903 | 0.0009 | 519 | 531 | 95.14 | 53.00 | 296 | | | | 2022 Jul 02, 09:21 | 6904 | 0.0008 | 521 | 531 | 95.15 | 53.00 | 333 | | | | USA 331 (Starshield Demonstrator?) 2022-064E 52892 |
in space
|
| US government/military satellite, probably operated by, or for, the National Reconnaissance Office - SpaceX Starshield satellite that provides a hosting platform for a variety missions and uses the Starlink infrastructure for communications. Purpose unknown. Not originally declared in the manifest for this launch. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 25, 09:24 | 6904 | 0.0003 | 524 | 528 | 95.15 | 53.01 | 354 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jun 19
Life <1 day
|
| Launched Globalstar FM-15 and four US government Starshield satellites. Directed to destructive re-entry above the eastern Pacific Ocean at around 07:45 UTC on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-065 KSLV-II (Nuri)
Naro Space Centre, South Korea | 2022 Jun 21, 07:00 | Performance Verification Satellite 2022-065A 52894 |
in space
|
Instrumented payload to monitor performance of the rocket during launch and at satellite separation. Released from the launch vehicle at 07:14 UTC.
Carries four Cubesats scheduled for release at intervals. All were released on time:
STEP Cube Lab-II - released Jun 29,
RANDEV - released Jun 30,
SNUGLITE 2 - released Jul 3,
MIMAN - released Jul 5. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jun 22, 05:30 | 7079 | 0.0008 | 695 | 707 | 98.80 | 98.02 | 232 | 15:36 | | | Dummy satellite 2022-065B 52895 |
in space
|
| 1.6 tonne mass to simulate a satellite payload. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 21, 21:15 | 7077 | 0.0007 | 694 | 704 | 98.76 | 98.02 | 254 | | | | STEP Cube Lab-II (Space Technology Experimental Project CubeSat Laboratory) 2022-065D 52897 |
in space
|
| 6U Cubesat from Chosun University, equipped for Earth imaging in visible and infrared bands of the spectrum. Released from Performance Verification Satellite Jun 29, 07:50 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jun 29, 12:21 | 7077 | 0.0007 | 694 | 704 | 98.76 | 98.02 | 227 | 15:35 | | | RANDEV (Repeater Arrangement & Disaster Early View) 2022-065E 52898 |
in space
|
| 3U Cubesat developed by the Korea Advanced Institute of Science and Technology. carrying an imaging system to study hazardous areas around volcanoes, clouds and coasts. Released from Performance Verification Satellite Jun 30 at about 22:50 UTC |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jul 01, 10:40 | 7076 | 0.0009 | 692 | 704 | 98.73 | 98.01 | 244 | 15:35 | | | SNUGLITE 2 (Seoul National University Global navigation satellite system Laboratory satellITE) 2022-065F 52899 |
in space
|
| 3U Cubesat from Seoul National University to demonstrate use of radio occultation of navsat signals as a means of measuring aspects of the Earth's upper atmosphere. Released from Performance Verification Satellite Jul 3 at about 08:00 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jul 04, 14:02 | 7077 | 0.0007 | 693 | 704 | 98.74 | 98.02 | 215 | 15:35 | | | MIMAN (Multi-spectral Imaging for Monitoring Aerosol by Nanosatellite) 2022-065G 52900 |
in space
|
| 3U Cubesat from Yonsei University to monitor dust in the upper atmosphere. Released from Performance Verification Satellite Jul 5 at at about 09:30 UTC. Precise orbit to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jul 07, 09:35 | 7077 | 0.0007 | 694 | 704 | 98.75 | 98.02 | 198 | 15:35 | | | Unidentified payload 2022-065H 52983 |
in space
|
| Released from Performance Verification Satellite Jul 7 around 08:00 UTC. Catalogued by Space-Track as a "Dummy Cubesat". Maybe 6U in size. Not listed in published payload schedule. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 07, 12:54 | 7078 | 0.0007 | 695 | 704 | 98.77 | 98.01 | 199 | | | | KSLV-II upper stage 2022-065C 52896 |
in space
|
| Launched Performance Verification Satellite and a dummy payload. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 21, 10:08 | 7064 | 0.0016 | 674 | 697 | 98.47 | 98.07 | 10 | | | |
2022-066 Kuaizhou 1A
Jiuquan Space Centre | 2022 Jun 22, 02:08 | Tianxing-1 01 2022-066A 52901 |
Re-entered - 2023 Mar 29
Life 280 days
|
| Described as a test satellite used for experiments such as space environment detection. Low orbit meant that a thruster firing every few days was needed to maintain height and, thereby, LTDN. Orbit adjustment frequency reduced late 2022 and manoeuvres ceased 2023 February 1. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jun 22, 04:45 | 6661 | 0.0012 | 275 | 292 | 90.18 | 96.76 | 278 | 08:29 | | | 2022 Jun 24, 14:13 | 6663 | 0.0009 | 279 | 291 | 90.22 | 96.74 | 233 | 08:29 | | | 2022 Jun 28, 17:30 | 6659 | 0.0010 | 274 | 288 | 90.14 | 96.74 | 213 | 08:30 | | | 2022 Jun 29, 03:53 | 6666 | 0.0011 | 281 | 296 | 90.28 | 96.74 | 267 | 08:30 | | | 2023 Feb 01, 21:33 | 6680 | 0.0015 | 292 | 312 | 90.56 | 96.76 | 50 | 08:44 | | | 2023 Mar 28, 17:55 | 6509 | 0.0009 | 126 | 137 | 87.11 | 96.69 | 255 | 08:49 | | | Kaizhou 1A upper stage 2022-066B 52902 |
Re-entered - 2022 Jun 23
Life 1 day
|
| Launched Tianxing 1. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 22, 06:24 | 6688 | 0.0298 | 111 | 509 | 90.72 | 96.80 | 319 | | | |
2022-067 Ariane 5ECA (VA-257)
Centre Spatiale Guyanaise | 2022 Jun 22, 21:50 | GSat 24 (GSat N1) 2022-067A 52903 |
in space
|
| High capacity comsat built by the Indian Space Research Organisation for NewSpace India Limited (NSIL) to provide high-quality television, telecommunications and broadcasting services. Initially, the entire capacity will be used by Tata Play for direct to home TV. Separated from launch vehicle at 22:29 UTC. Expected location 83° east. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Jun 23, 14:05 | 24383 | 0.7278 | 259 | 35751 | 631.52 | 6.01 | 179 | | | | 2022 Jun 24, 11:02 | 24374 | 0.7278 | 257 | 35734 | 631.17 | 6.01 | 179 | | | | 2022 Jun 24, 16:27 | 26817 | 0.5719 | 5103 | 35775 | 728.42 | 3.32 | 179 | | | | 2022 Jun 25, 11:09 | 31365 | 0.3444 | 14186 | 35789 | 921.38 | 1.34 | 181 | | | | 2022 Jun 28, 12:00 | 42056 | 0.0033 | 35540 | 35816 | 1430.55 | 0.09 | 332 | 85° east | | | 2022 Jun 30, 12:49 | 42032 | 0.0027 | 35539 | 35769 | 1429.33 | 0.10 | 334 | 88° east | | | 2022 Jul 04, 07:31 | 42078 | 0.0013 | 35644 | 35755 | 1431.66 | 0.09 | 328 | 93° east | | | 2022 Jul 05, 09:21 | 42135 | 0.0004 | 35742 | 35772 | 1434.59 | 0.09 | 239 | 93° east | | | 2022 Jul 11, 10:00 | 42166 | 0.0009 | 35750 | 35825 | 1436.14 | 0.08 | 194 | 94° east | | | 2022 Nov 15, 21:45 | 42165 | 0.0002 | 35777 | 35796 | 1436.10 | 0.01 | 96 | 94° east | | | 2022 Nov 17, 12:53 | 42244 | 0.0001 | 35860 | 35872 | 1440.15 | 0.02 | 81 | 80° east | | | 2022 Nov 17, 19:13 | 42165 | 0.0004 | 35769 | 35804 | 1436.09 | 0.07 | 191 | 83° east | | | |
in space
|
| Comsat covering Malaysia, Indonesia, South Asia and Australia, replacing the retired MEASAT 3 (29648/2006-056A). Launched 47 minutes into a 100 minute launch window. Separated from launch vehicle at 22:18 UTC. Expected location alongside Measat 3a and Measat 3b at 91°.5 east. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Jun 23, 04:41 | 24378 | 0.7279 | 255 | 35745 | 631.34 | 5.98 | 178 | | | | 2022 Jun 28, 10:44 | 42090 | 0.0012 | 35660 | 35763 | 1432.26 | 0.08 | 280 | 89° east | | | 2022 Jul 01, 10:38 | 42160 | 0.0005 | 35761 | 35802 | 1435.84 | 0.10 | 143 | 91° east | | | 2022 Jul 02, 22:06 | 42164 | 0.0001 | 35780 | 35792 | 1436.06 | 0.09 | 112 | 92° east | | | Ariane 5 upper stage 2022-067D 52906 |
in space
|
| Launched Measat 3d and GSat 24. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 24, 07:45 | 24340 | 0.7280 | 243 | 35681 | 629.86 | 6.17 | 181 | | | |
2022-068 CZ 2D
Xichang Space Centre | 2022 Jun 23, 02:22 | Yaogan 35-02 Follower 1 2022-068A 52909 |
Re-entered - 2024 Apr 19
Life 666 days
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 23, 18:14 | 6872 | 0.0008 | 488 | 499 | 94.48 | 35.00 | 270 | | | | 2022 Jul 03, 10:54 | 6872 | 0.0008 | 489 | 499 | 94.49 | 34.99 | 350 | | | | 2022 Jul 10, 02:57 | 6875 | 0.0007 | 492 | 502 | 94.56 | 34.99 | 59 | | | | 2022 Nov 24, 14:19 | 6875 | 0.0010 | 490 | 503 | 94.55 | 35.00 | 212 | | | | 2023 Jan 19, 11:43 | 6869 | 0.0007 | 486 | 496 | 94.43 | 35.00 | 349 | | | | 2023 Feb 15, 06:10 | 6865 | 0.0008 | 481 | 493 | 94.35 | 35.00 | 256 | | | | 2023 Aug 26, 23:38 | 6837 | 0.0006 | 454 | 463 | 93.76 | 34.99 | 227 | | | | Yaogan 35-02 Leader 2022-068B 52908 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 23, 18:13 | 6869 | 0.0010 | 485 | 498 | 94.44 | 34.99 | 291 | | | | 2022 Jul 03, 02:26 | 6872 | 0.0011 | 487 | 502 | 94.50 | 35.00 | 24 | | | | 2022 Jul 05, 13:08 | 6875 | 0.0008 | 491 | 502 | 94.55 | 35.00 | 58 | | | | 2023 Feb 15, 06:11 | 6873 | 0.0015 | 484 | 505 | 94.51 | 35.00 | 301 | | | | 2023 Aug 27, 00:18 | 6871 | 0.0012 | 484 | 501 | 94.46 | 35.00 | 175 | | | | Yaogan 35-02 Follower 2 2022-068C 52907 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Ceased manoeuvring 2022 Nov 24, orbit then began to decay naturally and it fell out of the group. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 23, 15:05 | 6870 | 0.0009 | 486 | 499 | 94.46 | 35.00 | 281 | | | | 2022 Jul 02, 12:55 | 6874 | 0.0006 | 492 | 499 | 94.52 | 34.99 | 323 | | | | 2022 Jul 07, 18:02 | 6875 | 0.0006 | 493 | 501 | 94.55 | 35.00 | 28 | | | | 2023 Feb 15, 13:36 | 6872 | 0.0005 | 491 | 498 | 94.50 | 35.00 | 263 | | | | 2023 Aug 27, 00:23 | 6871 | 0.0013 | 484 | 502 | 94.48 | 35.00 | 247 | | | | CZ 2D second stage 2022-068D 52910 |
Re-entered - 2023 Mar 8
Life 258 days
|
| Launched Yaogan group 35 group 2. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 23, 15:05 | 6871 | 0.0009 | 487 | 499 | 94.47 | 35.00 | 272 | | | |
2022-069 CZ 4C
Jiuquan Space Centre | 2022 Jun 27, 15:46 | Gaofen 12-03 2022-069A 52912 |
in space
|
| Earth observation using radar and high resolution optical sensors for Earth imaging to "support land surveys, crop management, urban and road network planning". |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jun 27, 20:03 | 6975 | 0.0003 | 595 | 599 | 96.62 | 97.98 | 232 | 22:02 | | | 2022 Jun 28, 12:10 | 6975 | 0.0006 | 593 | 601 | 96.62 | 97.99 | 260 | 22:02 | | | 2022 Jun 29, 08:09 | 6992 | 0.0002 | 612 | 615 | 96.97 | 97.99 | 181 | 22:02 | | | 2022 Jun 29, 15:52 | 7000 | 0.0009 | 615 | 628 | 97.14 | 97.98 | 137 | 22:02 | | | 2022 Jun 30, 06:11 | 7006 | 0.0003 | 626 | 630 | 97.26 | 97.98 | 31 | 22:02 | | | 2022 Jul 01, 18:18 | 7007 | 0.0001 | 628 | 629 | 97.28 | 97.98 | 116 | 22:02 | | | 2023 Feb 13, 05:02 | 7005 | 0.0003 | 625 | 629 | 97.24 | 97.97 | 100 | 22:09 | | | CZ 4 C upper stage 2022-069B 52913 |
in space
|
| Launched Gaofen 12-03. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 27, 18:47 | 6923 | 0.0074 | 493 | 596 | 95.54 | 97.97 | 46 | | | |
2022-070 Electron (CAPSTONE)
Rocket Lab Launch Complex, New Zealand | 2022 Jun 28, 09:55 | CAPSTONE (Cislunar Autonomous Positioning System Technology Operations and Navigation Experiment) 2022-070A 52914 |
in space
|
| Lunar spacecraft owned and operated by Advanced Space. Purpose of CAPSTONE is to test and verify orbit operational procedures for NASA's planned Lunar Gateway. Released from Rocket Lab's Photon rocket stage Jul 4 at 07:18 UTC. Enter a Near Rectilinear Halo Orbit (NRHO) in Lunar space 2022 Nov 14 for a test/evaluation programme expected to last six months to test evaluate use of the halo orbit. |
| Earth-Moon Barycentric Orbit | | Electron second stage 2022-070B 52915 |
Re-entered - 2022 Jun 28
Life <1 day
|
| Launched CAPSTONE. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 28, 12:02 | 6541 | 0.0013 | 154 | 171 | 87.74 | 39.11 | 267 | | | | Photon rocket stage (Photon 3) 2022-070C 52916 |
in space
|
Instrumented rocket stage that launched CAPSTONE. Intended to make a fly-by of the Moon and return images but none were published.
Engine firing Jul 4 at 06:56 UTC placed it in Barycentric orbit after which it released CAPSTONE.
|
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 28, 10:54 | 6985 | 0.0627 | 169 | 1045 | 96.83 | 39.12 | 330 | | | | 2022 Jun 30, 17:09 | 13242 | 0.4989 | 257 | 13470 | 252.75 | 39.09 | 343 | | | | 2022 Jul 01, 05:46 | 26657 | 0.7505 | 274 | 40285 | 721.91 | 39.05 | 344 | | | | 2022 Jul 03, 03:24 | 41615 | 0.8405 | 258 | 70215 | 1408.08 | 39.08 | 344 | | | |
2022-071 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2022 Jun 29, 21:04 | |
in space
|
| Comsat providing data services, and TV and radio services to North America, South America and the Caribbean. Released from launch vehicle at 21:37 UTC. Expected location 135° west. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Jun 30, 13:20 | 24332 | 0.7253 | 305 | 35603 | 629.54 | 16.53 | 179 | | | | 2022 Jul 01, 09:00 | 28901 | 0.4538 | 9407 | 35639 | 814.96 | 6.28 | 180 | | | | 2022 Jul 04, 10:34 | 42032 | 0.0003 | 35640 | 35668 | 1429.31 | 0.06 | 153 | 146° west | | | 2022 Jul 04, 18:17 | 42025 | 0.0003 | 35634 | 35659 | 1428.95 | 0.06 | 169 | 146° west | | | 2022 Jul 06, 14:06 | 42079 | 0.0009 | 35663 | 35740 | 1431.74 | 0.06 | 4 | 143° west | | | 2022 Jul 07, 06:44 | 42127 | 0.0006 | 35724 | 35774 | 1434.15 | 0.06 | 267 | 142° west | | | 2022 Jul 12, 17:36 | 42165 | 0.0000 | 35786 | 35788 | 1436.11 | 0.05 | 286 | 142° west | | | 2022 Jul 21, 23:44 | 42165 | 0.0001 | 35783 | 35789 | 1436.08 | 0.06 | 310 | 142° west | | | 2022 Jul 25, 12:40 | 42108 | 0.0000 | 35729 | 35731 | 1433.22 | 0.06 | 59 | 139° west | | | 2022 Jul 31, 09:57 | 42108 | 0.0000 | 35729 | 35730 | 1433.19 | 0.03 | 62 | 135° west | | | 2022 Aug 02, 16:27 | 42165 | 0.0002 | 35777 | 35796 | 1436.09 | 0.03 | 202 | 135° west | | | Falcon 9 upper stage 2022-071B 52934 |
in space
|
| Launched SES 22. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jun 30, 20:50 | 24331 | 0.7253 | 306 | 35601 | 629.52 | 16.54 | 180 | | | |
2022-072 PSLV-CA (PSLV C-53)
Satish Dhawan Space Centre | 2022 Jun 30, 12:30 | DS-EO (Earth Observation Satellite 6) 2022-072A 52935 |
in space
|
| Multispectral Earth imaging payload for land studies, from Singapore's Defence Science and Technology Agency. Separated from launch vehicle at 12:47 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jul 01, 11:51 | 6946 | 0.0007 | 563 | 573 | 96.02 | 9.99 | 328 | 21:59 | | | |
in space
|
| Small satellite from Singapore carrying an Earth imaging radar system. Separated from launch vehicle at 12:48 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 01, 12:02 | 6944 | 0.0009 | 560 | 573 | 95.99 | 9.99 | 336 | | | | |
in space
|
| 3U Cubesat - student built satellite from the Research Centre at Singapore's NTU School of Electrical and Electronic Engineering. Equipped with a Solar spectrometer and an Earth imaging system. Separated from launch vehicle at 12:48 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 01, 02:25 | 6925 | 0.0024 | 531 | 564 | 95.59 | 9.90 | 194 | | | | PSLV upper stage + POEM 1 2022-072B 52936 |
Re-entered - 2024 May 23
Life 693 days
|
| Launched DC-EO and two other satellites. Carries POEM PSLV Orbital Experimental Module 2 carrying six hosted payloads, two of which are from India. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 01, 23:12 | 6945 | 0.0008 | 562 | 573 | 96.01 | 9.99 | 337 | | | |
2022-073 Atlas V 541
Cape Canaveral Space Force Station | 2022 Jul 1, 23:15 | USA 332 (Wide Field of View Testbed) 2022-073A 52940 |
in space
|
| Testbed for sensors to be employed in the next generation of missile detection satellite that will replace the Space Based Infrared System (SBIRS). Released from the launch vehicle Jul 2, 05:04 UTC. The first orbit listed is an estimate based on information from ULA then, Jul 17, Space-Track started issuing orbit data with initial hint that orbit was raised around Jul 7. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Jul 02, 05:24 | 42513 | 0.0007 | 36106 | 36164 | 1453.95 | 0.00 | 201 | 99° east | | | 2022 Jul 17, 17:11 | 42668 | 0.0012 | 36240 | 36340 | 1461.89 | 0.05 | 126 | 18° east | | | 2022 Jul 24, 03:43 | 42668 | 0.0012 | 36238 | 36341 | 1461.87 | 0.05 | 150 | 23° west | | | 2022 Aug 01, 14:50 | 42668 | 0.0013 | 36237 | 36344 | 1461.90 | 0.07 | 154 | 77° west | | | 2022 Aug 05, 00:07 | 42669 | 0.0012 | 36238 | 36343 | 1461.91 | 0.08 | 153 | 98° west | | | 2022 Aug 13, 08:40 | 42668 | 0.0012 | 36238 | 36342 | 1461.90 | 0.09 | 167 | 152° west | | | 2022 Aug 18, 17:56 | 42670 | 0.0012 | 36239 | 36344 | 1461.97 | 0.11 | 168 | 174° east | | | 2022 Aug 26, 11:42 | 42518 | 0.0001 | 36138 | 36143 | 1454.20 | 0.12 | 209 | 134° east | | | 2022 Aug 29, 22:34 | 42375 | 0.0001 | 35992 | 36001 | 1446.84 | 0.14 | 169 | 123° east | | | 2022 Aug 31, 12:10 | 42267 | 0.0026 | 35781 | 35997 | 1441.32 | 0.14 | 255 | 120° east | | | 2022 Sep 01, 15:33 | 42164 | 0.0001 | 35783 | 35788 | 1436.04 | 0.13 | 170 | 119° east | | | 2023 Jul 25, 14:05 | 42164 | 0.0004 | 35771 | 35802 | 1436.07 | 0.98 | 54 | 119° east | | | USA 333 (USSF-12 Ring) 2022-073B 52941 |
in space
|
| EELV Secondary Payload Adapter (ESPA) hosting a quantity of secret test/demonstration payloads. Released from the launch vehicle Jul 2, 05:20 UTC. The first orbit listed is an estimate based on information from ULA. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Jul 02, 05:24 | 42624 | 0.0018 | 36167 | 36323 | 1459.60 | 0.01 | 172 | 99° east | | | |
in space
|
| Small satellite, possibly a Cubesat (3U or 6U?) with classified payload. Probably released from USA 333 mid-August. |
| Orbit classified as 'Secret' - data withheld | | Atlas V upper stage (Centaur) 2022-073C 52942 |
in space
|
| Launched WFOV Testbed and USSF-12 Ring. Orbit raised after releasing satellites. Estimated orbits based on ULA information, all others are from amateur observation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6870 | 0.0287 | 295 | 689 | 94.46 | 28.20 | 180 | | | | estimated orbit | 42624 | 0.0018 | 36167 | 36323 | 1459.60 | 0.01 | 172 | | | | 2022 Aug 23, 02:52 | 44499 | 0.0436 | 36181 | 40061 | 1556.99 | 0.09 | 9 | | | |
2022-074 LauncherOne (STP-27A)
Boeing 747, Pacific Ocean off California | 2022 Jul 2, 06:52 | |
Re-entered - 2024 Aug 2
Life 762 days
|
| 6U Cubesat from the US Air Force Research Laboratory (AFRL) intended to test and evaluate radio communications and mesh networking for use in military operations. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 03, 05:05 | 6874 | 0.0004 | 493 | 499 | 94.54 | 44.99 | 268 | | | | NACHOS 2 (NanoSat Atmospheric Chemistry Hyperspectral Observation System) 2022-074B 52945 |
Re-entered - 2024 Jun 27
Life 726 days
|
| 3U Cubesat from the US Los Alamos National Laboratory to detect, map, and quantify Earth’s trace gasses in support of volcanology and climate change research. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 03, 05:56 | 6874 | 0.0004 | 493 | 499 | 94.53 | 44.99 | 255 | | | | Slingshot 1 2022-074D 52947 |
Re-entered - 2024 Sep 11
Life 802 days
|
| 12U Cubesat (4x3) testing SatCat5, a data interface that uses Ethernet-type communication between payloads using low power serial communications. Carries an experiment to test precise control of attitude for aiming at targets on Earth, and a GPS receiver. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 03, 05:55 | 6873 | 0.0004 | 492 | 497 | 94.50 | 44.98 | 228 | | | | |
Re-entered - 2023 Oct 5
Life 460 days
|
| 3U or 6U Cubesat from the US Department of Defense to demonstrate communications systems with ground-based sensors and experiments, possibly using Internet links. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 03, 05:56 | 6874 | 0.0005 | 492 | 499 | 94.52 | 44.99 | 246 | | | | CTIM-FD (Compact Total Irradiance Monitor - Flight Demonstration) 2022-074G 52950 |
Re-entered - 2023 Dec 7
Life 523 days
|
| 6U Cubesat from the University of Colorado at Boulder, to test an instrument the Earth's Total Solar Irradiation. One of two satellites flown on the same launch under NASA's ELaNa-39 mission. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 03, 05:56 | 6874 | 0.0004 | 493 | 498 | 94.53 | 45.00 | 251 | | | | Gunsmoke-L 2 & L 3 2022-074H 52951 |
Re-entered - 2023 Dec 28
Life 544 days
|
| 3U Cubesat - pair of conjoined satellites from the US Army's Space and Missile Defense Command to support military operations by providing battlefield imagery from orbit. Design of each is based on Los Alamos National Laboratory's Prometheus 1.5U Cubesat with the Gunsmoke payload occupying a further 1.5U. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 03, 01:13 | 6874 | 0.0004 | 493 | 499 | 94.53 | 44.98 | 237 | | | | |
Re-entered - 2024 May 11
Life 679 days
|
| 3U Cubesat from NASA Langley Research Center to demonstrate differential GPS to determine satellite position for use in future formation flying in orbit. Equipped with gravity gradient stabilisation boom. One of two satellites flown on the same launch under NASA's ELaNa-39 mission. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 03, 05:56 | 6871 | 0.0005 | 489 | 497 | 94.47 | 44.98 | 207 | | | | LauncherOne upper stage 2022-074C 52946 |
Re-entered - 2023 Dec 7
Life 523 days
|
| Launched cluster of small satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 03, 05:47 | 6841 | 0.0047 | 430 | 495 | 93.85 | 44.99 | 214 | | | |
2022-075 Soyuz-2 1B + Fregat
Plesetsk Cosmodrome | 2022 Jul 7, 09:18 | Cosmos 2557 (Uragan-K1 № 16L) 2022-075A 52984 |
in space
|
| GLONASS-K navigation satellite. It also carries radio receiving equipment for the COSPAS-SARSAT international search and rescue system. Released from launch vehicle around 15:00 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 08, 10:13 | 25517 | 0.0003 | 19130 | 19148 | 676.09 | 64.82 | 270 | | | | 2022 Jul 11, 18:07 | 25537 | 0.0007 | 19141 | 19178 | 676.89 | 64.83 | 359 | | | | 2022 Jul 21, 15:36 | 25508 | 0.0008 | 19110 | 19150 | 675.74 | 64.81 | 285 | | | | Fregat rocket stage 2022-075B 52985 |
in space
|
| Launched Cosmos 2557 (GLONASS K) navsat. Orbit raised after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 08, 13:54 | 25864 | 0.0107 | 19208 | 19764 | 689.94 | 64.79 | 95 | | | |
2022-076 Falcon 9 Block 5 (Starlink Group 4-21)
Cape Canaveral Space Force Station | 2022 Jul 7, 13:11 | Starlink 4260 2022-076A 52986 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 12, 16:00 | 6687 | 0.0031 | 288 | 329 | 90.69 | 53.22 | 55 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jul 7
Life <1 day
|
| Launched fifty three Starlink satellites. Directed to re-enter later on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-077 Falcon 9 Block 5 (Starlink Group 3-1)
Vandenberg Space Force Base | 2022 Jul 11, 01:39 | Starlink 4362 2022-077A 53043 |
in space
|
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 02:41 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 15, 14:00 | 6721 | 0.0002 | 342 | 344 | 91.40 | 97.66 | 100 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jul 11
Life <1 day
|
| Launched forty six Starlink satellites. Directed to re-enter on the day of launch, above the mid-Pacific Ocean at about 03:30 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2022-078 CZ 3B
Xichang Space Centre | 2022 Jul 12, 16:30 | Tianlian 2-03 2022-078A 53100 |
in space
|
| Second Generation data communications satellite to provide a data relay, and measurement and control service for Chinese satellites and space stations. Launch completes planned constellation of three second-generation vehicles once satellite is on-station in GEO. Probably moved to Geosynchronous Drift Orbit 2022 Jul 13. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Jul 13, 00:00 | 24390 | 0.7305 | 194 | 35829 | 631.78 | 27.17 | 175 | | | | 2022 Jul 24, 22:15 | 42165 | 0.0002 | 35777 | 35798 | 1436.12 | 3.00 | 190 | 11° east | | | CZ 3B fourth stage 2022-078B 53101 |
Re-entered - 2023 Oct 20
Life 465 days
|
| Launched Tianlian 2-03. Orbit lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 12, 23:57 | 23780 | 0.7251 | 159 | 34644 | 608.23 | 27.12 | 174 | | | |
2022-079 Electron (Wise One Looks Ahead, NRO L-162)
Rocket Lab Launch Complex, New Zealand | 2022 Jul 13, 06:30 | |
in space
|
| Satellite built for US National Reconnaissance Office launched as NRO L-162 mission. Precise purpose not known but probably Earth observation. Released from launch vehicle around 07:30 UTC. Launched 90 mins into two hour window with delay due to weather. |
| Orbit classified as 'Secret' - data withheld | | Electron second stage 2022-079B 53103 |
Re-entered - 2022 Oct 2
Life 81 days
|
| Launched USA 334. Orbit classified as 'Secret' until 2022 September 19. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 19, 09:53 | 6683 | 0.0108 | 233 | 377 | 90.62 | 40.05 | 88 | | | | Electron third stage (kick stage) 2022-079C 53104 |
in space
|
| Launched USA 334. |
| Orbit classified as 'Secret' - data withheld | |
2022-080 Vega-C (VV-21)
Centre Spatiale Guyanaise | 2022 Jul 13, 13:13 | LaReS 2 (Laser Relativity Satellite 2) 2022-080A 53105 |
in space
|
| Italian Space Agency (ASI) passive satellite with a high density, made of 390 kg of tungsten and being 0.364m in diameter. It has 92 corner cube laser reflectors to be used for extremely accurate measurement of range. Its purpose is to help study aspects of the theory of relativity. Separated from launch vehicle at 14:37 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 15, 02:33 | 12268 | 0.0006 | 5882 | 5897 | 225.37 | 70.14 | 291 | | | | |
in space
|
| 3U Cubesat from the Italian Space Agency and Sapienza University of Rome, carrying an experiment to grow plants in the radiation environment experienced in the Earth's van Allen radiation belts. Released from launch vehicle together with the other Cubesats at ~15:23 UTC. Based on amateur observation, Space-Track has this item incorrectly tagged as 53109/2022-080E. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 16, 04:12 | 12221 | 0.0009 | 5833 | 5854 | 224.10 | 70.15 | 239 | | | | |
in space
|
3U Cubesat from the Italian Space Agency working with a group of science institutions, carrying a micro laboratory to provide a platform for an automatic bioanalytical experiments in space. Uses chemiluminescence to identify individual substances. Released from launch vehicle together with the other Cubesats at ~15:23 UTC.
|
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 19, 21:57 | 12227 | 0.0012 | 5835 | 5863 | 224.26 | 70.16 | 252 | | | | |
in space
|
| 3U Cubesat from the University of Maribor Faculty of Electrical Engineering, Slovenia to measure ionizing radiation with the aim of modeling the magnetosphere environment and better understanding space weather. Released from launch vehicle together with the other Cubesats at ~15:23 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 19, 06:59 | 12227 | 0.0015 | 5830 | 5867 | 224.25 | 70.00 | 251 | | | | MTCube 2 (Robusta 1F) 2022-080E 53109 |
in space
|
| 1U Cubesat carrying a payload from the University of Montpellier, France to measure errors induced by radiation into several different types of flash memory. Released from launch vehicle together with the other Cubesats at ~15:23 UTC. Based on amateur observation, Space-Track has this item incorrectly tagged as 53106/2022-080B. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 17, 13:49 | 12221 | 0.0009 | 5832 | 5854 | 224.10 | 70.14 | 244 | | | | |
in space
|
| 1U Cubesat from ARCA Dynamics of Italy to study the Earth's magnetosphere. Released from launch vehicle together with the other Cubesats at ~15:23 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 18, 04:46 | 12222 | 0.0026 | 5812 | 5875 | 224.11 | 70.15 | 149 | | | | |
in space
|
| 1U Cubesat carrying a payload from the University of Montpellier, France to study short circuits induced by space radiation in electronic circuits. Released from launch vehicle together with the other Cubesats at ~15:23 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 19, 21:51 | 12222 | 0.0009 | 5833 | 5855 | 224.11 | 70.15 | 223 | | | | Vega C upper stage (AVUM+) 2022-080H 53112 |
in space
|
| Launched LARES 2 and six Cubesats. Navigation warnings issued from CSG indicate planned destructive re-entry above the south western Pacific Ocean around 16:00 UTC on day of launch, but later information from ESA suggested that de-orbit may not have been part of the mission as flown. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 17, 02:36 | 12221 | 0.0009 | 5832 | 5854 | 224.09 | 70.11 | 258 | | | |
2022-081 Falcon 9 Block 5
Kennedy Space Center | 2022 Jul 15, 00:44 | SpaceX Dragon 2 CRS-25 2022-081A 53113 |
Re-entered - 2022 Aug 20
Life 36 days
Returned to Earth |
| Carrying a cargo to/from the ISS under NASA's Commercial Resupply Services (CRS) contract. Docked with the forward-facing port of the Harmony module of ISS Jul 16 at 16:21 UTC. Undocked Aug 19 at 15:05 UTC. Retro-fire Aug 20 at 18:05 UTC followed separation of the Trunk section, and splashdown in the Atlantic Ocean off Cape Canaveral occurred ~18:53 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 15, 01:07 | 6579 | 0.0011 | 193 | 208 | 88.50 | 51.65 | 8 | | | | 2022 Jul 15, 05:05 | 6616 | 0.0048 | 206 | 269 | 89.25 | 51.65 | 232 | | | | 2022 Jul 15, 23:22 | 6618 | 0.0053 | 205 | 275 | 89.30 | 51.65 | 234 | | | | 2022 Jul 16, 11:34 | 6792 | 0.0006 | 410 | 418 | 92.85 | 51.64 | 15 | | | | 2022 Jul 16, 12:56 | 6795 | 0.0005 | 413 | 420 | 92.90 | 51.64 | 17 | | | | 2022 Aug 18, 13:01 | 6794 | 0.0005 | 412 | 420 | 92.89 | 51.64 | 134 | | | | 2022 Aug 19, 18:41 | 6784 | 0.0005 | 402 | 409 | 92.67 | 51.65 | 153 | | | | 2022 Aug 19, 21:40 | 6665 | 0.0147 | 189 | 385 | 90.25 | 51.65 | 171 | | | | 2022 Aug 20, 09:33 | 6666 | 0.0148 | 190 | 386 | 90.28 | 51.62 | 172 | | | | 2022 Aug 20, 16:44 | 6666 | 0.0142 | 193 | 382 | 90.26 | 51.64 | 171 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jul 15
Life <1 day
|
| Launched SpaceX Dragon 2 CRS-25. Directed to re-enter later on the day of launch. |
| Not Catalogued - orbit parameters unavailable | | Dragon 2 trunk module 2022-081B 53584 |
Re-entered - 2022 Aug 31
Life 47 days
|
| Separated from Dragon 2 CRS-25 2022 August 20 prior to retrofire. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 21, 15:37 | 6659 | 0.0135 | 192 | 371 | 90.14 | 51.64 | 175 | | | |
2022-082 CZ 2C
Taiyuan Space Centre | 2022 Jul 15, 22:57 | Siwei Gaojing 2-01 (Superview Neo 2-01) 2022-082A 53128 |
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 ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jul 16, 17:42 | 6870 | 0.0012 | 484 | 500 | 94.46 | 97.38 | 264 | 06:04 | | | 2022 Oct 20, 13:05 | 6867 | 0.0012 | 481 | 497 | 94.40 | 97.39 | 292 | 06:05 | | | 2022 Oct 23, 16:50 | 6873 | 0.0007 | 490 | 499 | 94.50 | 97.39 | 314 | 06:05 | | | 2024 Nov 24, 19:56 | 6870 | 0.0002 | 491 | 493 | 94.46 | 97.39 | 90 | 06:08 | | | Siwei Gaojing 2-02 (Superview Neo 2-02) 2022-082C 53130 |
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 ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jul 16, 17:42 | 6868 | 0.0012 | 482 | 498 | 94.41 | 97.39 | 281 | 06:04 | | | 2022 Oct 10, 19:49 | 6868 | 0.0011 | 483 | 497 | 94.41 | 97.39 | 338 | 06:05 | | | 2022 Oct 11, 02:02 | 6871 | 0.0007 | 489 | 498 | 94.47 | 97.39 | 350 | 06:05 | | | 2022 Oct 12, 19:06 | 6873 | 0.0008 | 489 | 500 | 94.51 | 97.39 | 355 | 06:05 | | | 2024 Nov 24, 22:04 | 6870 | 0.0002 | 491 | 493 | 94.46 | 97.39 | 90 | 06:08 | | | CZ 2C second stage 2022-082D 53131 |
Re-entered - 2024 Apr 30
Life 655 days
|
| Launched pair of Siwei Gaojing satellites. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 16, 12:30 | 6837 | 0.0049 | 425 | 493 | 93.77 | 97.36 | 12 | | | |
2022-083 Falcon 9 Block 5 (Starlink Group 4-22)
Cape Canaveral Space Force Station | 2022 Jul 17, 14:20 | Starlink 4063 2022-083A 53132 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 14:35 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 21, 18:00 | 6684 | 0.0036 | 282 | 329 | 90.63 | 53.22 | 52 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Jul 17
Life <1 day
|
| Launched fifty three Starlink satellites. Directed to re-enter later on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-I07 Manual release during EVA
International Space Station | 2022 Jul 21, 16:02 | YuZGU-55 № 8 (Tanyusha 8) 1998-067TR 53306 |
Re-entered - 2023 Jan 27
Life 190 days
|
| 3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 25, 19:19 | 6794 | 0.0005 | 412 | 419 | 92.88 | 51.64 | 52 | | | | Tsiolkovsky-Ryazan № 2 1998-067TS 53307 |
Re-entered - 2023 Jan 31
Life 194 days
|
| 3U Cubesat from Ryazan State Radiotechnical University, carrying radio transmitting equipment to calibrate the sensitivity of radio telescopes of the Pushchino Observatory. Released within a forty minute period during Russian EVA from ISS. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 27, 08:52 | 6793 | 0.0004 | 412 | 418 | 92.87 | 51.64 | 55 | | | | YuZGU-55 № 12 (Tanyusha 12) 1998-067TT 53308 |
Re-entered - 2023 Jan 31
Life 194 days
|
| 3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 25, 20:52 | 6793 | 0.0004 | 412 | 418 | 92.87 | 51.64 | 43 | | | | YuZGU-55 № 5 (Tanyusha 5) 1998-067TU 53309 |
Re-entered - 2023 Jan 31
Life 194 days
|
| 3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 25, 19:19 | 6793 | 0.0005 | 412 | 418 | 92.87 | 51.64 | 61 | | | | YuZGU-55 № 9 (Tanyusha 9) 1998-067TV 53310 |
Re-entered - 2023 Jan 31
Life 194 days
|
| 3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 27, 07:30 | 6793 | 0.0005 | 412 | 418 | 92.87 | 51.64 | 67 | | | | Tsiolkovsky-Ryazan № 1 1998-067TW 53311 |
Re-entered - 2023 Jan 27
Life 190 days
|
| 3U Cubesat from Ryazan State Radiotechnical University, carrying radio transmitting equipment to calibrate the sensitivity of radio telescopes of the Pushchino Observatory. Released within forty minutes of the launch time shown, during Russian EVA from ISS. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 27, 06:02 | 6793 | 0.0004 | 412 | 418 | 92.87 | 51.64 | 48 | | | | YuZGU-55 № 6 (Tanyusha 6) 1998-067TX 53312 |
Re-entered - 2023 Jan 31
Life 194 days
|
| 3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 25, 19:19 | 6793 | 0.0005 | 411 | 419 | 92.87 | 51.64 | 58 | | | | YuZGU-55 № 7 (Tanyusha 7) 1998-067TY 53313 |
Re-entered - 2023 Jan 31
Life 194 days
|
| 3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 25, 19:18 | 6793 | 0.0005 | 412 | 418 | 92.87 | 51.64 | 58 | | | | YuZGU-55 № 10 (Tanyusha 10) 1998-067TZ 53321 |
Re-entered - 2023 Jan 31
Life 194 days
|
| 3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 27, 08:52 | 6793 | 0.0004 | 412 | 418 | 92.87 | 51.64 | 65 | | | | YuZGU-55 № 11 (Tanyusha 11) 1998-067UA 53322 |
Re-entered - 2023 Jan 31
Life 194 days
|
| 3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 25, 20:52 | 6794 | 0.0004 | 413 | 418 | 92.88 | 51.64 | 49 | | | |
2022-084 Falcon 9 Block 5 (Starlink Group 3-2)
Vandenberg Space Force Base | 2022 Jul 22, 17:39 | Starlink 4391 2022-084A 53189 |
in space
|
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 18:42:03 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 27, 14:00 | 6710 | 0.0002 | 331 | 333 | 91.17 | 97.66 | 97 | | | | Falcon 9 upper stage uncatalogued |
in space
|
| Launched forty six Starlink satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2022-085 CZ 5B
Wenchang Space Centre | 2022 Jul 24, 06:22 | |
in space
|
| Module for Chinese Space Station, precise launch time 06:22:32 UTC, released from launch vehicle at 06:30:47 UTC about 5700 km behind CSS. Docked with forward-facing port of Tianhe module of CSS at 19:13 UTC on day of launch. Transferred to side port of docking module 2022 Sep 30 in ~60 min operation completed at 04:44 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6619 | 0.0089 | 182 | 300 | 89.32 | 41.45 | 168 | | | | 2022 Jul 24, 17:08 | 6756 | 0.0008 | 372 | 384 | 92.11 | 41.46 | 227 | | | | 2022 Jul 24, 17:52 | 6761 | 0.0007 | 378 | 388 | 92.21 | 41.47 | 272 | | | | 2022 Jul 24, 18:15 | 6762 | 0.0007 | 379 | 388 | 92.22 | 41.47 | 278 | | | | CZ 5 second stage 2022-085B 53240 |
Re-entered - 2022 Jul 30
Life 6 days
|
| Launched Wentian. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 24, 14:45 | 6619 | 0.0089 | 182 | 300 | 89.32 | 41.45 | 168 | | | | 2022 Jul 27, 15:54 | 6592 | 0.0064 | 172 | 256 | 88.78 | 41.48 | 195 | | | | 2022 Jul 30, 15:57 | 6507 | 0.0016 | 119 | 140 | 87.07 | 41.47 | 234 | | | |
2022-086 Falcon 9 Block 5 (Starlink Group 4-26)
Kennedy Space Center | 2022 Jul 24, 13:38 | Starlink 4056 2022-086A 53242 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 28, 20:00 | 6682 | 0.0040 | 278 | 331 | 90.61 | 53.22 | 53 | | | | Falcon 9 upper stage uncatalogued |
in space
|
| Launched fifty three Starlink satellites. Directed to re-enter later on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-087 Lijian 1, Kinetica 1 (Y-1)
Jiuquan Space Centre | 2022 Jul 27, 04:12 | SATech 01 (Space Technology Test Satellite) 2022-087A 53299 |
in space
|
| Satellite from the Institute of Microsatellite Innovation of the Chinese Academy of Sciences, Shanghai. Payload includes SUTRI (Solar Upper Transition Region Imager), a solar imaging camera capable of taking full-disk pictures of solar regions between the solar chromosphere and corona, an x-ray telescope and a gamma-ray astronomy instrument. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Jul 27, 13:40 | 6881 | 0.0014 | 493 | 512 | 94.67 | 97.41 | 285 | 10:31 | | | Atmospheric Density Detection Test Satellite 2022-087xx |
in space
|
| Spherical satellite for upper atmosphere studies by measuring variations in air drag at orbital altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6879 | 0.0013 | 492 | 510 | 94.64 | 97.40 | 286 | 10:31 | | | Electromagnetic Assembly Test Satellite 1 2022-087xx |
in space
|
| Small satellite - one of a pair carried on the same launch vehicle. Mission details awaited. May still be attached to its companion satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6879 | 0.0013 | 492 | 510 | 94.64 | 97.40 | 286 | 10:31 | | | Electromagnetic Assembly Test Satellite 2 2022-087xx |
in space
|
| Small satellite - one of a pair carried on the same launch vehicle. Mission details awaited. May still be attached to its companion satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6879 | 0.0013 | 492 | 510 | 94.64 | 97.40 | 286 | 10:31 | | | |
in space
|
| Demonstrator satellite using Quantum Physics to generate security keys for secure communications links between ground and space. Developed jointly by the University of Science and Technology of China, the Jinan Institute of Quantum Technology, the Institute of Microsatellite Innovation of the Chinese Academy of Sciences, and the Shanghai Institute of Technical Physics. Follow-on from QUESS (Micius) - 41731/2016-051A. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6879 | 0.0013 | 492 | 510 | 94.64 | 97.40 | 286 | 10:31 | | | Nanyue (Guangdong Science Satellite) 2022-087xx |
in space
|
| Small satellite from the South Space Technology Co, carrying remote sensing equipment for Earth studies, in particular soil moisture content and ocean surface winds. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| estimated orbit | 6879 | 0.0013 | 492 | 510 | 94.64 | 97.40 | 286 | 10:31 | | | Lijian 1 third stage 2022-087F 53304 |
Re-entered - 2023 Apr 18
Life 265 days
|
| Launched cluster of six satellites. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 28, 07:36 | 6802 | 0.0175 | 305 | 543 | 93.05 | 97.28 | 309 | | | |
2022-088 CZ 2D
Xichang Space Centre | 2022 Jul 29, 13:28 | Yaogan 35-03 Follower 1 2022-088A 53316 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 30, 02:01 | 6872 | 0.0008 | 488 | 499 | 94.48 | 35.00 | 266 | | | | 2022 Aug 10, 22:43 | 6873 | 0.0007 | 490 | 500 | 94.51 | 35.00 | 5 | | | | 2022 Aug 13, 13:19 | 6875 | 0.0008 | 491 | 502 | 94.55 | 35.01 | 34 | | | | 2023 Feb 15, 04:54 | 6871 | 0.0009 | 487 | 500 | 94.48 | 35.00 | 282 | | | | Yaogan 35-03 Follower 2 2022-088C 53318 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 30, 02:14 | 6870 | 0.0007 | 488 | 497 | 94.46 | 35.01 | 266 | | | | 2022 Aug 08, 17:01 | 6875 | 0.0005 | 494 | 501 | 94.56 | 35.00 | 323 | | | | 2023 Feb 15, 04:54 | 6871 | 0.0003 | 491 | 495 | 94.48 | 35.00 | 272 | | | | Yaogan 35-03 Leader 2022-088E 53320 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 30, 02:14 | 6870 | 0.0010 | 485 | 498 | 94.44 | 35.00 | 287 | | | | 2022 Aug 10, 04:46 | 6875 | 0.0004 | 494 | 500 | 94.55 | 35.00 | 326 | | | | 2023 Feb 15, 04:50 | 6871 | 0.0003 | 491 | 495 | 94.48 | 35.00 | 262 | | | | CZ 2D second stage 2022-088B 53317 |
Re-entered - 2023 Mar 11
Life 225 days
|
| Launched Yaogan 35 group 3. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Jul 30, 02:14 | 6871 | 0.0009 | 487 | 500 | 94.48 | 35.00 | 269 | | | |
2022-089 Soyuz-2 1V + Volga
Plesetsk Cosmodrome | 2022 Aug 1, 20:25 | Cosmos 2558 2022-089A 53323 |
in space
|
| Military satellite possibly equipped with sensors that allow it to observe other satellites in orbit. It also may carry an Earth imaging system. Released from Volga rocket stage at 21:49 UTC. Until early 2023, orbit was co-planar with that of the US imaging reconsat USA 326 (51445/2022-009A). Orbit frequently raised to overcome decay through air drag and to maintain the LTDN. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 02, 00:53 | 6822 | 0.0013 | 435 | 452 | 93.46 | 97.26 | 261 | 12:06 | | | 2022 Aug 02, 13:21 | 6821 | 0.0010 | 436 | 450 | 93.45 | 97.25 | 266 | 12:06 | | | 2022 Sep 08, 10:23 | 6819 | 0.0012 | 432 | 449 | 93.40 | 97.20 | 133 | 12:07 | | | 2022 Sep 08, 15:03 | 6822 | 0.0016 | 433 | 455 | 93.47 | 97.20 | 145 | 12:07 | | | 2023 Mar 10, 20:50 | 6818 | 0.0007 | 435 | 444 | 93.38 | 97.19 | 162 | 12:06 | | | 2023 Mar 13, 14:14 | 6820 | 0.0004 | 439 | 444 | 93.42 | 97.21 | 136 | 12:06 | | | 2023 Mar 14, 14:10 | 6826 | 0.0003 | 445 | 450 | 93.54 | 97.25 | 104 | 12:06 | | | 2023 Mar 14, 18:18 | 6829 | 0.0007 | 446 | 455 | 93.60 | 97.26 | 168 | 12:06 | | | 2023 Mar 15, 16:50 | 6838 | 0.0011 | 452 | 467 | 93.78 | 97.26 | 243 | 12:06 | | | 2023 Mar 16, 14:38 | 6842 | 0.0011 | 456 | 471 | 93.86 | 97.25 | 332 | 12:06 | | | 2023 Mar 16, 17:11 | 6845 | 0.0011 | 459 | 474 | 93.93 | 97.29 | 292 | 12:06 | | | 2023 Apr 24, 17:16 | 6840 | 0.0010 | 455 | 469 | 93.84 | 97.29 | 164 | 12:06 | | | 2023 Aug 15, 16:23 | 6840 | 0.0007 | 457 | 467 | 93.84 | 97.28 | 116 | 12:07 | | | 2024 May 20, 17:13 | 6841 | 0.0008 | 457 | 468 | 93.84 | 97.24 | 162 | 12:03 | | | Soyuz upper stage 2022-089B 53324 |
Re-entered - 2022 Nov 19
Life 110 days
|
| Launched Cosmos 2558. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 02, 00:50 | 6735 | 0.0108 | 284 | 429 | 91.67 | 97.25 | 70 | | | | Volga rocket stage uncatalogued |
Re-entered - 2022 Aug 2
Life 1 day
|
| Launched Cosmos 2558. Caused to re-enter above the southern Pacific Ocean on a south-north trajectory Aug 2 at about 08:30 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2022-090 CZ 4B
Taiyuan Space Centre | 2022 Aug 4, 03:08 | Jumang (Terrestrial Ecosystem Carbon Monitoring Satellite) 2022-090A 53346 |
in space
|
| Terrestrial carbon monitoring satellite with a range of instruments to detect and measure such as vegetation biomass, and atmospheric aerosol and chlorophyll fluorescence. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 04, 07:20 | 6875 | 0.0009 | 491 | 504 | 94.56 | 97.47 | 250 | 10:25 | | | Head 2G (Jiaotong 4) 2022-090B 53347 |
Re-entered - 2024 May 30
Life 665 days
|
| Application satellite from Head Aerospace in the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications between internet-connected devices. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 04, 22:03 | 6874 | 0.0012 | 488 | 504 | 94.52 | 97.47 | 278 | | | | Minhang Junior 2022-090C 53348 |
Re-entered - 2023 Nov 2
Life 455 days
|
| Small satellite to allow primary and secondary school students to participate in space science research and engineering practice. Carries instruments to monitor carbon sources, and the space environment. Catalogue Number and Designation to be confirmed. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 04, 07:42 | 6874 | 0.0010 | 489 | 502 | 94.52 | 97.47 | 271 | | | | CZ 4B third stage 2022-090D 53349 |
Re-entered - 2023 Jan 17
Life 166 days
|
| Launched Terrestrial Ecosystem Carbon Monitoring Satellite. Orbit lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 04, 08:55 | 6770 | 0.0159 | 284 | 499 | 92.39 | 97.51 | 30 | | | |
2022-091 Electron (Antipodean Adventure, NRO L-199)
Rocket Lab Launch Complex, New Zealand | 2022 Aug 4, 05:00 | |
in space
|
| Satellite built for US National Reconnaissance Office launched as NRO L-199 mission. Precise purpose not known but probably Earth observation. Released from launch vehicle around 06:00 UTC and aimed at orbit around 70° inclination. Launched at the opening of a two hour window. Orbit data based on amateur observation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 20, 19:38 | 7014 | 0.0011 | 628 | 644 | 97.43 | 70.02 | 329 | | | | Electron second stage 2022-091B 53353 |
Re-entered - 2022 Oct 20
Life 77 days
|
| Launched USA 335. Orbit data based on amateur observation. On launch date, apogee was about 640 km. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 11, 03:11 | 6796 | 0.0279 | 228 | 607 | 92.92 | 70.02 | 203 | | | | Electron third stage (kick stage) 2022-091C 53354 |
in space
|
| Launched USA 335. Orbit data based on amateur observation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 11, 19:42 | 7015 | 0.0005 | 633 | 640 | 97.45 | 70.00 | 22 | | | |
2022-092 Atlas V 421
Cape Canaveral Space Force Station | 2022 Aug 4, 10:29 | USA 336 (SBIRS GEO 6) 2022-092A 53355 |
in space
|
| Missile launch detection satellite for the Space-Based Infra Red System with a combination of scanning and staring sensors. A scanning sensor is designed to provide a wide area view in search of missile launches, satellite re-entries and natural terrestrial events, while a staring sensor is designed to observe areas of particular interest with enhanced sensitivity. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Aug 05, 18:00 | 26652 | 0.5651 | 5214 | 35334 | 721.71 | 17.53 | 178 | | | | 2022 Aug 11, 15:34 | 34705 | 0.2018 | 21323 | 35331 | 1072.36 | 9.08 | 178 | | | | 2022 Aug 15, 15:24 | 41914 | 0.0047 | 35340 | 35731 | 1423.29 | 6.58 | 358 | 153° west | | | 2022 Aug 16, 08:15 | 41894 | 0.0043 | 35334 | 35697 | 1422.28 | 6.59 | 354 | 150° west | | | 2022 Aug 17, 15:32 | 42106 | 0.0007 | 35700 | 35756 | 1433.10 | 6.58 | 166 | 148° west | | | 2022 Aug 22, 12:38 | 42128 | 0.0007 | 35720 | 35781 | 1434.24 | 6.57 | 137 | 145° west | | | 2022 Aug 25, 12:01 | 42168 | 0.0002 | 35781 | 35798 | 1436.24 | 6.57 | 334 | 145° west | | | 2023 Jul 26, 14:48 | 42164 | 0.0013 | 35729 | 35842 | 1436.04 | 5.86 | 176 | 145° west | | | Atlas V upper stage (Centaur) 2022-092B 53356 |
in space
|
| Launched SBIRS GEO 6. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 05, 04:38 | 26648 | 0.5655 | 5202 | 35338 | 721.53 | 16.48 | 176 | | | |
2022-093 CZ 2F/G
Jiuquan Space Centre | 2022 Aug 4, 16:00 | Reusable Spacecraft Test Vehicle Type 1 Flight 2 2022-093A 53357 |
Re-entered - 2023 May 8
Life 277 days
Returned to Earth |
| Small re-usable spaceplane, possibly associated with China's space station programme and maybe intended for long duration missions. Vehicle used to test launch and landing technology and spacecraft materials. May be the same craft that flew an earlier mission in 2020. Released a companion satellite to conduct rendezvous and capture experiments during 2022 and 2023. Re-entered 2023 May 8 for landing on the runway at Lop Nor at about 00:20 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 04, 20:44 | 6848 | 0.0180 | 346 | 593 | 93.99 | 49.99 | 149 | | | | 2022 Aug 24, 01:59 | 6847 | 0.0181 | 346 | 593 | 93.98 | 49.99 | 229 | | | | 2022 Aug 24, 11:48 | 6851 | 0.0178 | 351 | 595 | 94.07 | 49.99 | 229 | | | | 2022 Sep 11, 13:18 | 6851 | 0.0178 | 351 | 595 | 94.06 | 49.99 | 303 | | | | 2022 Oct 23, 06:05 | 6849 | 0.0175 | 351 | 591 | 94.02 | 49.99 | 116 | | | | 2022 Oct 24, 11:02 | 6980 | 0.0008 | 597 | 608 | 96.73 | 49.99 | 261 | | | | 2023 Jan 12, 19:33 | 6980 | 0.0008 | 597 | 608 | 96.73 | 49.99 | 215 | | | | 2023 Apr 13, 07:01 | 6979 | 0.0008 | 596 | 607 | 96.71 | 49.99 | 202 | | | | 2023 Apr 14, 06:57 | 6929 | 0.0009 | 545 | 557 | 95.67 | 49.99 | 273 | | | | 2023 Apr 14, 19:37 | 6720 | 0.0010 | 335 | 349 | 91.37 | 49.99 | 273 | | | | 2023 May 06, 08:53 | 6721 | 0.0007 | 338 | 347 | 91.38 | 49.97 | 292 | | | | (Banxing 4)? 2022-093J 54218 |
Re-entered - 2023 May 8
Life 277 days
Returned to Earth |
| Speculative name and purpose but possibly used to inspect the main vehicle while on orbit and may also carry a science/technology payload. Satellites with a similar task were deployed from Shenzhou 7 (33386/2008-047A) and Tiangong 2 (41765/2016-057A). Separated from spaceplane October 29 or October 30 and first reported by Space-Track October 31. Initially kept station with it but started to move away November 2 or 3 before conducting co-ordinated manoeuvres with the spaceplane. May have been captured/re-docked with spaceplane December 12 or 13 then separated again Feb 19 or 20. Continued to conduct close manoeuvres with the spaceplane until it 'disappeared' around 2023 March 30, presumably re-captured and stowed aboard the spaceplane prior to its orbit being lowered April 13/14. Re-entered as cargo aboard the main vehicle. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 31, 18:39 | 6981 | 0.0008 | 597 | 608 | 96.74 | 49.99 | 292 | | | | 2023 Jan 12, 13:06 | 6980 | 0.0007 | 597 | 607 | 96.73 | 49.99 | 209 | | | | 2023 Jan 13, 14:52 | 6979 | 0.0025 | 584 | 619 | 96.71 | 50.06 | 147 | | | | 2023 Mar 29, 10:03 | 6979 | 0.0008 | 596 | 607 | 96.71 | 49.99 | 144 | | | | unidentified object 2022-093G 53363 |
Re-entered - 2022 Sep 5
Life 32 days
|
| Noted on day 1 of mission and assumed to be debris. On Aug 8, a minor orbit change indicated it might be an active satellite but the event could have been due to outgassing or shedding of fragments. Rapid orbit decay tends to support it being debris. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 04, 22:10 | 6847 | 0.0222 | 317 | 621 | 93.98 | 50.02 | 161 | | | | 2022 Aug 08, 11:50 | 6841 | 0.0215 | 315 | 610 | 93.84 | 50.02 | 175 | | | | 2022 Aug 09, 06:35 | 6837 | 0.0212 | 314 | 604 | 93.77 | 50.03 | 179 | | | | 2022 Sep 05, 17:24 | 6692 | 0.0064 | 271 | 357 | 90.80 | 50.03 | 284 | | | | unidentified object 2022-093H 53364 |
in space
|
| Noted on day 1 of mission and assumed to be debris. Low rate of orbit decay indicates it is a dense object so it may be a payload. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 04, 22:29 | 6945 | 0.0110 | 491 | 643 | 96.00 | 50.03 | 202 | | | | 2023 Jan 25, 19:06 | 6941 | 0.0108 | 488 | 638 | 95.92 | 50.03 | 166 | | | | 2023 May 07, 15:59 | 6938 | 0.0106 | 486 | 633 | 95.85 | 50.03 | 207 | | | | 2024 Jun 09, 02:49 | 6922 | 0.0097 | 476 | 611 | 95.51 | 50.02 | 345 | | | | CZ 2F third stage 2022-093B 53358 |
Re-entered - 2024 Feb 12
Life 557 days
|
| Launched experimental spaceplane. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 04, 20:44 | 6847 | 0.0180 | 346 | 593 | 93.98 | 49.99 | 149 | | | |
2022-094 Falcon 9 Block 5 (Starlink Group 4-26)
Cape Canaveral Space Force Station | 2022 Aug 4, 23:08 | Danuri (Korea Pathfinder Lunar Orbiter.) 2022-094A 53365 |
in space
|
| South Korean lunar mission from the Korea Aerospace Research Institute (KARI), scheduled to operate in orbit around the Moon for one year. Equipped with an array of South Korean experiments and one US built instrument. The objectives are to develop indigenous lunar exploration technologies, demonstrate a "space internet", and conduct scientific investigations of the lunar environment, topography, and resources, as well as identify potential landing sites for future missions. Initially injected into Barycentric orbit then entered orbit around the Moon 2002 Dec 16. |
| In orbit around the Moon or landed on its surface | | Falcon 9 upper stage 2022-094B 53366 |
in space
|
| Launched KPOL. |
| Earth-Moon Barycentric Orbit | |
2022-F04 - failed to reach orbit SSLV (SSLV D-1)
Satish Dhawan Space Centre | 2022 Aug 7, 03:48 | EOS 02 (Earth Observation Satellite 2) |
|
| Experimental optical remote sensing satellie from India developed in a short space of time to demonstrate rapid launch on demand ability. Aimed at ~350 km orbit with inclination 37°. Lost when VTM satellite orbit stage carried by SSLV failed to ignite, re-entered after about 0.6 orbits. |
| |
|
| 8U Cubesat - carrying 75 individual experiments provided by female students at schools across India under the 'Space Kidz India' initiative. Includes an amateur radio payload. Aimed at ~350 km orbit with inclination 37°. Lost when VTM satellite orbit stage carried by SSLV failed to ignite, re-entered after about 0.6 orbits. |
|
2022-095 Ceres 1
(Gushenxing 1 Y-3)
Jiuquan Space Centre | 2022 Aug 9, 04:11 | |
in space
|
| Small satellite to demonstrate a micro-miniature remote sensing imaging system. Also carries audio files carrying poetry, or other writing, called "Story of Love" to be played on orbit as an art project. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 10, 13:13 | 6870 | 0.0079 | 437 | 547 | 94.45 | 97.41 | 72 | 10:30 | | | |
in space
|
| Commercial remote sensing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 10, 04:55 | 6871 | 0.0080 | 438 | 549 | 94.48 | 97.41 | 75 | 10:30 | | | Taijing-1 02 (Xingshidai 12) 2022-095xx |
in space
|
| Commercial remote sensing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 10, 13:13 | 6871 | 0.0081 | 437 | 548 | 94.46 | 97.41 | 73 | 10:30 | | | Ceres 1 fourth stage 2022-095D 53387 |
in space
|
| Launched two Taijing 1 satellites, and Donghai 1. Tentative identification. May have been caused to re-enter after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 11:53 | 6867 | 0.0086 | 430 | 548 | 94.39 | 97.41 | 69 | | | |
2022-096 Soyuz-2 1B + Fregat
Baikonur Cosmodrome | 2022 Aug 9, 05:52 | |
in space
|
| Iranian Government owned imaging satellite built and managed by Russia The design is based on Russia's Canopus V. The imaging payload is operated by Iran. Thruster firings to maintain the orbit ceased 2023 December 9 and it entered a period of natural orbit decay until 2024 April 4 when thruster firings began to maintain the orbit at its new height. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 10, 09:07 | 6871 | 0.0002 | 492 | 495 | 94.48 | 97.44 | 87 | 23:00 | | | 2022 Oct 30, 21:20 | 6869 | 0.0002 | 490 | 493 | 94.43 | 97.43 | 76 | 23:02 | | | 2023 Dec 09, 01:21 | 6870 | 0.0002 | 490 | 493 | 94.45 | 97.40 | 69 | 23:09 | | | 2024 Apr 05, 12:15 | 6864 | 0.0001 | 484 | 487 | 94.32 | 97.40 | 82 | 23:11 | | | Polytech Universe 1 2022-096B 53371 |
Re-entered - 2024 Oct 9
Life 792 days
|
| 3U Cubesat from Peter the Great Polytechnic University, St Petersburg. Carries a payload to monitor radiation in LEO. One of a pair carried on the same launch vehicle. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 15:13 | 6871 | 0.0003 | 491 | 495 | 94.47 | 97.44 | 138 | | | | Polytech Universe 2 2022-096C 53372 |
Re-entered - 2024 Oct 18
Life 801 days
|
| 3U Cubesat from Peter the Great Ploytechnic University, St Petersburg. Carries a payload to monitor radiation in LEO. One of a pair carried on the same launch vehicle. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 19:44 | 6871 | 0.0002 | 491 | 494 | 94.47 | 97.44 | 127 | | | | SXC3 2110 Voenmeh (CYCLOPS) 2022-096D 53373 |
Re-entered - 2024 Mar 6
Life 575 days
|
| 3U Cubesat from the Batlic States University, Russia studying the degradation of materials samples and electronics in orbit. Also carries an amateur radio package, |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 08:59 | 6871 | 0.0002 | 491 | 494 | 94.46 | 97.44 | 128 | | | | |
Re-entered - 2024 Mar 28
Life 597 days
|
| 3U Cubesat from M V Lomonosov Moscow State University, carrying radiation detectors to register dose rates of cosmic radiation, fluxes of high-energy nuclei, and neutron fluxes. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 15:12 | 6870 | 0.0003 | 490 | 494 | 94.46 | 97.44 | 122 | | | | SXC3 218 KuzSTU (Kuzbass 300) 2022-096F 53375 |
Re-entered - 2024 May 18
Life 648 days
|
| 3U Cubesat from Kuzbass State Technical University, Russia equipped with an imaging system to monitor fires on the Earth's surface. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 13:38 | 6870 | 0.0003 | 490 | 494 | 94.45 | 97.44 | 121 | | | | |
Re-entered - 2024 May 9
Life 639 days
|
| 3U Cubesat from the Tyumen State University, Russia designed and built as a student project. Equipped with an imaging system to study oil spills in the Arctic region. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 14:59 | 6870 | 0.0003 | 490 | 494 | 94.46 | 97.44 | 127 | | | | SXC3 214 MIET-AIS 2022-096H 53377 |
Re-entered - 2024 Jun 9
Life 670 days
|
| 3U Cubesat equipped with an AIS receiver to monitor positions of ships on the ocean surface. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 11:59 | 6870 | 0.0003 | 490 | 494 | 94.45 | 97.44 | 115 | | | | |
Re-entered - 2024 Aug 18
Life 740 days
|
| 3U Cubesat from the Kazan National Research Technical University, Russia equipped with five Earth imaging cameras for remote sensing. Also carries an amateur radio package. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 11, 16:24 | 6870 | 0.0003 | 490 | 494 | 94.45 | 97.44 | 118 | | | | Skoltech B1 2022-096K 53379 |
Re-entered - 2024 Nov 27
Life 841 days
|
| 3U Cubesat from Skolkovo Institute of Science and Technology, Russia. Aimed at developing space comunications systems and studying cosmic radiation and gamma ray bursts.. Also carries an Earth inmaging system. One of a pair of similar satellites carried on the same launch. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 15:00 | 6869 | 0.0006 | 487 | 495 | 94.43 | 97.44 | 87 | | | | Skoltech B2 2022-096L 53380 |
Re-entered - 2024 Sep 29
Life 782 days
|
| 3U Cubesat from Skolkovo Institute of Science and Technology, Russia. Aimed at developing space comunications systems and studying cosmic radiation and gamma ray bursts.. Also carries an Earth inmaging system. One of a pair of similar satellites carried on the same launch. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 11, 05:24 | 6869 | 0.0006 | 487 | 495 | 94.43 | 97.44 | 92 | | | | SXC3 219 ISOI 2022-096M 53381 |
Re-entered - 2024 Jun 5
Life 666 days
|
| 3U Cubesat from the Department of Engineering Cybernetics at Samara University, Russia. Equipped with an Earth imaging system for earth resources studies. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 08:58 | 6869 | 0.0006 | 486 | 495 | 94.42 | 97.44 | 89 | | | | SXC3 2111 SibSU (ReshUCube) 2022-096N 53382 |
Re-entered - 2024 Jul 21
Life 712 days
|
| 3U Cubesat from the M S Reshetnev Siberian State University of Science and Technologies equipped to study the Earth's magnetic field and radiation on orbit. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 15:01 | 6869 | 0.0006 | 486 | 495 | 94.42 | 97.44 | 91 | | | | SXC3 218 KuzSTU (CubeSX HSE-2) 2022-096P 53383 |
Re-entered - 2024 May 9
Life 639 days
|
| 3U Cubesat from Kuzbass State Technical University, Russia. Equipped with an Earth imaging system for remote sensing and an amateur radio payload. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 08:58 | 6869 | 0.0006 | 486 | 495 | 94.42 | 97.44 | 88 | | | | SXC3 217 Siren 2022-096Q 53384 |
Re-entered - 2024 Jul 6
Life 697 days
|
| 3U Cubesat from Belgorod State University, Russia. Carries a payload to study development of plant (lilac) sprouts in microgravity and the space environment. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 13:37 | 6869 | 0.0006 | 486 | 495 | 94.42 | 97.44 | 90 | | | | Geoscan Eidelweiss 2022-096R 53385 |
Re-entered - 2024 Feb 21
Life 561 days
|
| 3U Cubesat equipped with a cold gas thruster for orbital manoeuvres. Also carries an amateur radio payload. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 10:50 | 6868 | 0.0007 | 485 | 495 | 94.41 | 97.44 | 89 | | | | SXC3 215 Vizard 2022-096T 53386 |
Re-entered - 2024 Jan 12
Life 521 days
|
| 3U Cubesat developed by school students in the Moscow Area. Equipped with an AIS receiver to monitor positions of ships on the ocean surface. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 10, 10:49 | 6868 | 0.0008 | 484 | 495 | 94.40 | 97.44 | 86 | | | | Fregat rocket stage uncatalogued |
Re-entered - 2022 Aug 9
Life <1 day
|
| Launched Khayyam and sixteen cubesats. Expected to re-enter the Earth's atmosphere at about 08:00 UTC after retro-fire. |
| Not Catalogued - orbit parameters unavailable | |
2022-097 Falcon 9 Block 5
Kennedy Space Center | 2022 Aug 10, 02:14 | Starlink 4522 2022-097A 53388 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 15, 18:00 | 6694 | 0.0019 | 303 | 329 | 90.84 | 53.22 | 52 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Aug 10
Life <1 day
|
| Launched fifty three Starlink satellites. Directed to re-enter later on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-098 CZ 6 (Y-10)
Taiyuan Space Centre | 2022 Aug 10, 04:50 | Jilin-1 High Resolution 03D 09 (Jilin-1 GF3D 09) 2022-098A 53444 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 04:35 | 6918 | 0.0010 | 533 | 547 | 95.45 | 97.53 | 250 | 11:59 | | | 2024 Oct 18, 10:25 | 6871 | 0.0007 | 488 | 498 | 94.48 | 97.53 | 360 | 12:18 | | | Jilin-1 High Resolution 03D 35 (Jilin-1 GF3D 35) 2022-098B 53445 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 01:18 | 6911 | 0.0016 | 521 | 544 | 95.29 | 97.53 | 270 | 11:59 | | | 2024 Oct 18, 10:22 | 6875 | 0.0005 | 493 | 500 | 94.55 | 97.53 | 26 | 12:19 | | | Jilin-1 High Resolution 03D 36 (Jilin-1 GF3D 36) 2022-098C 53446 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 04:35 | 6918 | 0.0011 | 532 | 548 | 95.44 | 97.54 | 252 | 11:59 | | | 2024 Oct 18, 05:36 | 6875 | 0.0006 | 493 | 501 | 94.55 | 97.53 | 46 | 12:19 | | | Jilin-1 High Resolution 03D 37 (Jilin-1 GF3D 37) 2022-098D 53447 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 01:33 | 6918 | 0.0011 | 532 | 547 | 95.43 | 97.53 | 254 | 11:59 | | | 2024 Oct 18, 11:03 | 6866 | 0.0008 | 483 | 493 | 94.37 | 97.53 | 357 | 12:17 | | | Jilin-1 High Resolution 03D 38 (Jilin-1 GF3D 38) 2022-098E 53448 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 01:21 | 6917 | 0.0011 | 531 | 546 | 95.42 | 97.53 | 264 | 11:59 | | | 2024 Oct 18, 10:11 | 6875 | 0.0008 | 492 | 502 | 94.56 | 97.53 | 51 | 12:19 | | | Jilin-1 High Resolution 03D 39 (Jilin-1 GF3D 39) 2022-098F 53449 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 04:35 | 6917 | 0.0010 | 532 | 546 | 95.41 | 97.53 | 262 | 11:59 | | | 2024 Oct 18, 11:07 | 6874 | 0.0006 | 492 | 500 | 94.53 | 97.53 | 29 | 12:17 | | | Jilin-1 High Resolution 03D 40 (Jilin-1 GF3D 40) 2022-098G 53450 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 04:34 | 6916 | 0.0007 | 533 | 543 | 95.40 | 97.53 | 264 | 11:59 | | | 2024 Oct 18, 11:32 | 6872 | 0.0005 | 490 | 497 | 94.48 | 97.53 | 57 | 12:19 | | | Jilin-1 High Resolution 03D 41 (Jilin-1 GF3D 41) 2022-098H 53451 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 04:34 | 6916 | 0.0008 | 532 | 543 | 95.39 | 97.54 | 267 | 11:59 | | | 2024 Oct 18, 11:12 | 6865 | 0.0004 | 484 | 490 | 94.34 | 97.54 | 37 | 12:23 | | | Jilin-1 High Resolution 03D 42 (Jilin-1 GF3D 42) 2022-098J 53452 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 04:35 | 6916 | 0.0009 | 532 | 543 | 95.39 | 97.53 | 273 | 11:59 | | | 2024 Oct 18, 11:28 | 6873 | 0.0005 | 491 | 498 | 94.51 | 97.53 | 50 | 12:17 | | | Jilin-1 High Resolution 03D 43 (Jilin-1 GF3D 43) 2022-098K 53453 |
in space
|
| High resolution, multi-spectral imaging satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 10, 22:05 | 6915 | 0.0009 | 531 | 543 | 95.38 | 97.53 | 282 | 11:59 | | | 2024 Oct 18, 10:09 | 6874 | 0.0005 | 492 | 499 | 94.52 | 97.53 | 53 | 12:19 | | | Yunyao-1 04 2022-098L 53454 |
Re-entered - 2024 Aug 10
Life 731 days
|
| Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 04:34 | 6915 | 0.0011 | 529 | 544 | 95.37 | 97.53 | 287 | 11:59 | | | 2024 Aug 10, 01:42 | 6520 | 0.0016 | 132 | 153 | 87.33 | 97.50 | 261 | 13:16 | | | Yunyao-1 05 2022-098M 53455 |
Re-entered - 2024 Sep 2
Life 754 days
|
| Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 06:09 | 6915 | 0.0008 | 531 | 542 | 95.37 | 97.53 | 228 | 11:59 | | | 2024 Sep 02, 18:47 | 6524 | 0.0015 | 136 | 156 | 87.40 | 97.50 | 255 | 13:19 | | | Yunyao-1 06 2022-098N 53456 |
Re-entered - 2024 Aug 23
Life 744 days
|
| Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 05:53 | 6915 | 0.0010 | 530 | 543 | 95.37 | 97.53 | 276 | 11:59 | | | 2024 Aug 23, 05:02 | 6528 | 0.0015 | 140 | 160 | 87.48 | 97.50 | 270 | 13:15 | | | Yunyao-1 07 2022-098P 53457 |
Re-entered - 2024 Sep 5
Life 757 days
|
| Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 06:08 | 6914 | 0.0014 | 526 | 545 | 95.36 | 97.53 | 295 | 11:59 | | | 2024 Sep 05, 02:28 | 6564 | 0.0015 | 176 | 195 | 88.20 | 97.48 | 277 | 13:19 | | | Yunyao-1 08 2022-098Q 53458 |
Re-entered - 2024 Aug 31
Life 752 days
|
| Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 05:45 | 6914 | 0.0009 | 530 | 543 | 95.36 | 97.53 | 275 | 11:59 | | | 2024 Aug 28, 02:04 | 6637 | 0.0012 | 251 | 267 | 89.69 | 97.51 | 267 | 13:17 | | | Yunyao-1 09? (Tianjin Binhai-1) 2022-098R 53459 |
Re-entered - 2024 Sep 3
Life 755 days
|
| Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 11, 05:45 | 6914 | 0.0011 | 528 | 544 | 95.36 | 97.53 | 294 | 11:59 | | | 2024 Sep 01, 22:56 | 6582 | 0.0014 | 194 | 213 | 88.57 | 97.50 | 277 | 13:18 | | | CZ 6 third stage uncatalogued |
in space
|
| Launched cluster of sixteen Jilin-1 and Yunyao-1 satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2022-I08 JEM Small Satellite Orbital Deployer
International Space Station | 2022 Aug 12, 09:45 | |
Re-entered - 2023 Feb 16
Life 188 days
|
| 1U Cubesat from the Kyushu Institute of Technology, Japan to study the effect of 'whiskers' in lead-free solder on the performance of satellite electronics. Also carries an amateur radio payload. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 12, 19:30 | 6792 | 0.0009 | 408 | 420 | 92.85 | 51.65 | 139 | | | | |
Re-entered - 2023 Mar 11
Life 211 days
|
| 1U Cubesat from the Happy Science University, Japan testing satellite components and technologies including infrared-based communication for an uplink. Also carries an amateur radio payload. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 13, 12:27 | 6792 | 0.0007 | 409 | 419 | 92.85 | 51.64 | 133 | | | | TUMnanoSAT 1998-067UD 53464 |
Re-entered - 2023 Jan 31
Life 172 days
|
| 1U Cubesat from the Technical University of Moldova designed to test structural elements and electronic systems for use in satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 13, 12:27 | 6792 | 0.0007 | 409 | 419 | 92.84 | 51.64 | 137 | | | |
2022-099 Falcon 9 Block 5 (Starlink Group 3-3)
Vandenberg Space Force Base | 2022 Aug 12, 21:40 | Starlink 4415 2022-099A 53465 |
in space
|
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 22:43 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 19, 14:00 | 6726 | 0.0002 | 346 | 349 | 91.49 | 97.66 | 119 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Aug 12
Life <1 day
|
| Launched forty six Starlink satellites. Re-entered over the southern Pacific Ocean at about 23:45 UTC following retro-fire. |
| Not Catalogued - orbit parameters unavailable | |
2022-100 CZ 2D
Xichang Space Centre | 2022 Aug 19, 17:37 | Yaogan 35-04 Follower 1 2022-100A 53522 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 20, 07:28 | 6875 | 0.0008 | 491 | 502 | 94.54 | 35.00 | 267 | | | | 2023 Feb 15, 09:16 | 6872 | 0.0005 | 490 | 498 | 94.49 | 35.00 | 93 | | | | Yaogan 35-04 Leader 2022-100C 53524 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 20, 07:49 | 6872 | 0.0009 | 488 | 500 | 94.49 | 35.00 | 290 | | | | 2023 Feb 15, 13:54 | 6872 | 0.0006 | 490 | 498 | 94.49 | 35.00 | 69 | | | | Yaogan 35-04 Follower 2 2022-100E 53526 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 20, 02:35 | 6873 | 0.0009 | 489 | 501 | 94.52 | 35.00 | 272 | | | | 2023 Feb 14, 17:31 | 6872 | 0.0008 | 489 | 500 | 94.49 | 35.00 | 145 | | | | CZ 2D second stage 2022-100B 53523 |
Re-entered - 2023 Mar 29
Life 222 days
|
| Launched Yaogan 35 group 4. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 20, 07:30 | 6874 | 0.0009 | 490 | 502 | 94.53 | 35.00 | 274 | | | |
2022-101 Falcon 9 Block 5 (Starlink Group 4-27)
Cape Canaveral Space Force Station | 2022 Aug 19, 19:21 | Starlink 4511 2022-101A 53527 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 19:36 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 24, 14:00 | 6682 | 0.0040 | 277 | 330 | 90.59 | 53.22 | 56 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Aug 19
Life <1 day
|
| Launched fifty three Starlink satellites. Caused to re-enter later on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-102 Kuaizhou 1A
Xichang Space Centre | 2022 Aug 23, 02:36 | Chuangxin 16A (Innovation 16A, Shiyan?) 2022-102A 53586 |
in space
|
| One of a pair of small satellites described as "mainly used in scientific experiments, new technology verification and other fields" and initially as a "double satellite assembly". Chuanxin 16B separated from it Sep 19. Orbit plane matches that of the GECAM gravity wave detection satellites launched 2021 June. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Aug 23, 10:32 | 6971 | 0.0005 | 590 | 596 | 96.54 | 29.01 | 261 | | | | 2022 Sep 19, 12:36 | 6971 | 0.0005 | 589 | 596 | 96.53 | 29.00 | 171 | | | | Chuangxin 16B (Innovation 16B, Shiyan?) 2022-102B 53876 |
in space
|
| One of a pair of small satellites described as "mainly used in scientific experiments, new technology verification and other fields". Separated from Chuangxin 16A Sep 19. Orbit plane matches that of the GECAM gravity wave detection satellites launched 2021 June. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 20, 12:41 | 6971 | 0.0005 | 589 | 596 | 96.53 | 29.00 | 183 | | | | Kuaizhou 1A fourth stage uncatalogued |
in space
|
| Launched Chuangxin 16. Caused to re-enter after releasing payload. First launch of Kuaizhou 1A from Xichang. |
| Not Catalogued - orbit parameters unavailable | |
2022-103 CZ 2D
Taiyuan Space Centre | 2022 Aug 24, 03:01 | Beijing 3B (Nanning 1) 2021-103A 53587 |
in space
|
| Commercial Earth imaging satellite from China's 21st Century Space Technology Application Company. Larger and an updated design compared with Beijing 3A, and capable of providing 3D images. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Aug 24, 06:06 | 6984 | 0.0013 | 597 | 615 | 96.81 | 97.94 | 264 | 10:09 | | | 2022 Sep 07, 02:17 | 6984 | 0.0014 | 596 | 616 | 96.81 | 97.94 | 214 | 10:10 | | | 2022 Sep 07, 12:32 | 6985 | 0.0013 | 597 | 616 | 96.82 | 97.94 | 211 | 10:10 | | | CZ 2D second stage uncatalogued |
in space
|
| Launched Beijing 3B. Caused to re-enter after releasing satellite. |
| Not Catalogued - orbit parameters unavailable | |
2022-104 Falcon 9 Block 5 (Starlink Group 4-23)
Cape Canaveral Space Force Station | 2022 Aug 28, 03:41 | Starlink 4691 2022-104A 53588 |
in space
|
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from the launch vehicle at 03:56 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 02, 14:00 | 6685 | 0.0034 | 284 | 330 | 90.66 | 53.22 | 58 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Aug 28
Life <1 day
|
| Launched fifty three Starlink satellites. Directed to re-enter at about 05:00 UTC on the day of launch. |
| Not Catalogued - orbit parameters unavailable | |
2022-105 Falcon 9 Block 5 (Starlink Group 3-4)
Vandenberg Space Force Base | 2022 Aug 31, 05:40 | Starlink 4622 2022-105A 53648 |
in space
|
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:43 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
| Orbit parameters awaited | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Aug 31
Life <1 day
|
| Launched forty six Starlink satellites. Re-entered over the Indian Ocean at about 06:00 UTC following retro-fire. |
| Not Catalogued - orbit parameters unavailable | |
2022-106 CZ 4C
Jiuquan Space Centre | 2022 Sep 2, 23:44 | Yaogan 33-02 2022-106A 53698 |
in space
|
| Described as being used for remote sensing for natural resources surveys. Specific tasks include land survey, crop yield assessment, and input to disaster monitoring and prevention plans. Equipped with synthetic aperture radar for Earth imaging provided by the Institute of Space and Space Information Innovation of the Chinese Academy of Sciences. Mission is probably military or government. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Sep 03, 06:04 | 7062 | 0.0006 | 680 | 688 | 98.44 | 98.18 | 245 | 06:00 | | | 2022 Sep 16, 04:39 | 7066 | 0.0010 | 681 | 695 | 98.52 | 98.19 | 177 | 06:00 | | | 2022 Sep 16, 17:10 | 7066 | 0.0010 | 681 | 695 | 98.52 | 98.19 | 175 | 06:00 | | | 2022 Sep 17, 05:03 | 7073 | 0.0002 | 694 | 697 | 98.67 | 98.19 | 171 | 06:00 | | | 2022 Sep 19, 02:45 | 7074 | 0.0001 | 696 | 696 | 98.69 | 98.19 | 104 | 06:00 | | | 2023 Feb 13, 06:31 | 7074 | 0.0002 | 695 | 697 | 98.68 | 98.19 | 111 | 06:00 | | | CZ 2C second stage 2022-106B 53699 |
in space
|
| Launched Yaogan 33-02. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 03, 07:20 | 6972 | 0.0144 | 493 | 694 | 96.55 | 98.20 | 51 | | | |
2022-107 Falcon 9 Block 5 (Starlink Group 4-20)
Cape Canaveral Space Force Station | 2022 Sep 5, 02:09 | |
in space
|
One member of a simultaneously-launched cluster of fifty one LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:22 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 12, 14:00 | 6711 | 0.0001 | 332 | 333 | 91.18 | 53.22 | 96 | | | | Sherpa LTC-2 2022-107BG 53754 |
in space
|
Space tug with Hosted Payload Varuna-TDM (Technology Demonstration Mission) - from Boeing, designed to test radio communications at V-band (40 - 75 GHz). A problem with Sherpa's systems prevented its orbit being raised immediately to the target 1000 km but control was restored early-October and orbit raising began.
Separated from launch vehicle at 02:57 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 11, 13:41 | 6685 | 0.0010 | 300 | 314 | 90.66 | 53.21 | 296 | | | | 2022 Oct 07, 09:03 | 6664 | 0.0009 | 280 | 292 | 90.24 | 53.21 | 3 | | | | 2022 Oct 07, 21:04 | 6684 | 0.0034 | 283 | 328 | 90.64 | 53.21 | 65 | | | | 2022 Oct 12, 20:28 | 6712 | 0.0015 | 324 | 343 | 91.20 | 53.22 | 260 | | | | 2022 Nov 04, 16:12 | 6700 | 0.0014 | 312 | 331 | 90.96 | 53.21 | 353 | | | | 2022 Nov 11, 08:45 | 6696 | 0.0013 | 309 | 326 | 90.88 | 53.21 | 18 | | | | 2022 Nov 16, 19:57 | 6793 | 0.0131 | 326 | 504 | 92.87 | 53.22 | 229 | | | | 2022 Nov 22, 23:08 | 7076 | 0.0522 | 328 | 1067 | 98.73 | 53.23 | 244 | | | | 2022 Nov 23, 14:19 | 7108 | 0.0477 | 391 | 1069 | 99.40 | 53.25 | 246 | | | | Falcon 9 upper stage uncatalogued |
in space
|
| Launched fifty one Starlink satellites and Sherpa LTC. Caused to re-enter above the Indian Ocean at about 04:15 UTC after releasing the satellites. |
| Not Catalogued - orbit parameters unavailable | |
2022-108 Kuaizhou 1A
Jiuquan Space Centre | 2022 Sep 6, 02:24 | Centispace-1 S3 2022-108A 53757 |
in space
|
| Demonstrator for an LEO navigation enhancement system being developed by Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Will also be used to test the Beidou system and to test an inter-satellite laser communication system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 06, 07:11 | 7077 | 0.0008 | 693 | 705 | 98.75 | 53.53 | 279 | | | | Centispace-1 S4 2022-108B 53758 |
in space
|
| Demonstrator for an LEO navigation enhancement system being developed by Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Will also be used to test the Beidou system and to test an inter-satellite laser communication system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 06, 07:11 | 7079 | 0.0008 | 695 | 707 | 98.79 | 53.53 | 261 | | | | Kuazhou 1A upper stage 2022-108C 53759 |
Re-entered - 2022 Nov 5
Life 60 days
|
| Launched Centispace S3 & S4. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 06, 07:09 | 6860 | 0.0413 | 199 | 766 | 94.25 | 53.56 | 80 | | | |
2022-109 CZ 2D
Xichang Space Centre | 2022 Sep 6, 04:19 | Yaogan 35-05 Follower 2 2022-109A 53760 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 06, 17:02 | 6875 | 0.0008 | 491 | 502 | 94.55 | 35.00 | 265 | | | | 2023 Feb 15, 13:03 | 6872 | 0.0007 | 489 | 498 | 94.48 | 35.00 | 272 | | | | Yaogan 35-05 Leader 2022-109B 53761 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 06, 12:08 | 6873 | 0.0008 | 489 | 500 | 94.51 | 34.99 | 281 | | | | 2022 Sep 07, 00:58 | 6873 | 0.0009 | 489 | 501 | 94.51 | 35.00 | 287 | | | | 2022 Sep 15, 06:39 | 6874 | 0.0006 | 492 | 501 | 94.54 | 35.00 | 355 | | | | 2023 Feb 15, 09:50 | 6872 | 0.0004 | 491 | 496 | 94.49 | 34.99 | 303 | | | | Yaogan 35-05 Follower 1 2022-109D 53763 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 06, 12:00 | 6874 | 0.0007 | 491 | 501 | 94.53 | 35.00 | 264 | | | | 2022 Sep 10, 08:51 | 6875 | 0.0006 | 493 | 501 | 94.55 | 34.99 | 309 | | | | 2023 Feb 15, 09:54 | 6872 | 0.0006 | 490 | 498 | 94.49 | 35.00 | 291 | | | | CZ 2D second stage 2022-109E 53764 |
Re-entered - 2023 Mar 28
Life 203 days
|
| Launched Yaogan 35 group 5. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 06, 12:08 | 6874 | 0.0009 | 490 | 502 | 94.54 | 34.99 | 263 | | | |
2022-I09 Nanoracks Cubesat Deployer
International Space Station | 2022 Sep 6, 09:10 | CapSat 1 (Capacitor Satellite) 1998-067UH 53770 |
Re-entered - 2023 Jan 31
Life 147 days
|
| 1U Cubesat - demonstrator from the Weiss School, Florida to evaluate use of a capacitor-based power system. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 09, 23:06 | 6792 | 0.0003 | 411 | 416 | 92.83 | 51.64 | 286 | | | | |
Re-entered - 2023 Jan 22
Life 138 days
|
| 2U Cubesat - from the University of South Alabama, equipped to measure plasma electron density in LEO. Results will allow studies of the topside F region of the Earth's ionosphere. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 09, 23:06 | 6791 | 0.0003 | 411 | 416 | 92.83 | 51.64 | 288 | | | | |
Re-entered - 2023 Feb 28
Life 175 days
|
| 2U Cubesat - from the University of Florida, equipped with an atmospheric drag device that can be re-configured to control the rate of orbital decay. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative. Note - Space-Track has this catalogued as a debris item. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 11, 06:04 | 6793 | 0.0002 | 413 | 417 | 92.87 | 51.64 | 221 | | | |
2022-I10 Nanoracks Cubesat Deployer
International Space Station | 2022 Sep 6, 09:20 | BeaverCube 1998-067UF 53768 |
Re-entered - 2023 Apr 12
Life 218 days
|
| 3U Cubesat - from the Massachussetts Institute of Technology, to take temperature measurements of the Earth's sea surface and cloud tops. It also carries a low-power electric thruster that will be used to change the orbit height by about 500 metres. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 09, 23:06 | 6792 | 0.0001 | 413 | 415 | 92.85 | 51.64 | 311 | | | | CLICK A (CubeSat Laser Infrared Crosslink) 1998-067UG 53769 |
Re-entered - 2023 Apr 1
Life 207 days
|
| 3U Cubesat - demonstrator mission from the Massachusetts Institute of Technology, University of Florida and NASA Ames Research Center. It will test laser communications equipment for a later pair of CLICK satellites. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 09, 23:06 | 6792 | 0.0001 | 413 | 415 | 92.84 | 51.64 | 309 | | | |
2022-110 Ariane 5ECA (VA-258)
Centre Spatiale Guyanaise | 2022 Sep 7, 21:45 | Eutelsat Konnect VHTS (Very High Throughput Satellite) 2022-110A 53765 |
in space
|
| Comsat to provide high-speed Internet access across Europe, especially to isolated regions with poor terrestrial coverage. Separated from launch vehicle at 22:13 UTC. Orbit raising from transfer orbit used continuously operating thruster. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Sep 08, 20:12 | 36742 | 0.8180 | 308 | 60418 | 1168.14 | 3.37 | 175 | | | | 2022 Sep 15, 14:30 | 37704 | 0.8077 | 871 | 61781 | 1214.35 | 3.41 | 178 | | | | 2022 Sep 22, 02:50 | 38585 | 0.7917 | 1661 | 62753 | 1257.15 | 3.19 | 179 | | | | 2022 Sep 29, 09:53 | 40215 | 0.7741 | 2707 | 64966 | 1337.63 | 2.79 | 182 | | | | 2022 Oct 06, 16:48 | 41810 | 0.7502 | 4068 | 66796 | 1418.03 | 2.48 | 183 | | | | 2022 Oct 17, 00:00 | 42837 | 0.7019 | 6393 | 66526 | 1470.59 | 2.14 | 187 | | | | 2022 Oct 20, 14:34 | 43052 | 0.6854 | 7168 | 66181 | 1481.69 | 1.95 | 185 | | | | 2022 Oct 26, 16:59 | 43432 | 0.6541 | 8645 | 65462 | 1501.30 | 1.83 | 188 | | | | 2022 Nov 04, 14:31 | 42914 | 0.6243 | 9744 | 63329 | 1474.57 | 1.50 | 186 | | | | 2022 Nov 11, 21:35 | 43777 | 0.5681 | 12528 | 62271 | 1519.27 | 1.31 | 186 | | | | 2022 Nov 17, 18:24 | 44277 | 0.5343 | 14243 | 61554 | 1545.34 | 1.16 | 187 | | | | 2022 Nov 23, 16:16 | 43894 | 0.4947 | 15803 | 59229 | 1525.33 | 1.03 | 187 | | | | 2022 Dec 01, 16:00 | 43831 | 0.4391 | 18207 | 56698 | 1522.04 | 0.92 | 193 | | | | 2022 Dec 08, 12:51 | 43833 | 0.3954 | 20124 | 54787 | 1522.18 | 0.75 | 186 | | | | 2022 Dec 15, 14:59 | 43734 | 0.3516 | 21978 | 52734 | 1517.03 | 0.66 | 186 | | | | 2022 Dec 21, 16:43 | 43678 | 0.3324 | 22779 | 51821 | 1514.10 | 0.57 | 182 | | | | 2022 Dec 28, 22:00 | 43400 | 0.2507 | 26142 | 47901 | 1499.64 | 0.46 | 186 | | | | 2023 Jan 04, 12:00 | 43060 | 0.2035 | 27918 | 45446 | 1482.09 | 0.40 | 182 | | | | 2023 Jan 13, 17:18 | 42774 | 0.1361 | 30573 | 42218 | 1467.31 | 0.30 | 179 | | | | 2023 Jan 18, 12:34 | 42502 | 0.1347 | 30397 | 41850 | 1453.34 | 0.25 | 176 | | | | 2023 Jan 25, 13:03 | 42476 | 0.0599 | 33554 | 38641 | 1452.03 | 0.18 | 151 | 17° east | | | 2023 Jan 29, 22:33 | 42369 | 0.0292 | 34752 | 37229 | 1446.52 | 0.17 | 133 | 4° east | | | 2023 Feb 02, 06:52 | 42261 | 0.0047 | 35686 | 36080 | 1441.03 | 0.17 | 123 | 3° east | | | 2023 Feb 07, 09:05 | 42166 | 0.0003 | 35775 | 35800 | 1436.16 | 0.15 | 44 | 3° east | | | 2023 Jul 25, 06:40 | 42165 | 0.0003 | 35774 | 35799 | 1436.11 | 0.05 | 28 | 3° east | | | Ariane 5 upper stage 2022-110B 53766 |
in space
|
| Launched Eutelsat Konnect VHTS. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 10, 07:27 | 36143 | 0.8160 | 274 | 59256 | 1139.71 | 3.14 | 170 | | | |
2022-111 Falcon 9 Block 5 (Starlink Group 4-2)
Kennedy Space Center | 2022 Sep 11, 01:20 | |
in space
|
One member of a simultaneously-launched cluster of thirty four LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:09 UTC.
All satellites were injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 19, 22:00 | 6728 | 0.0001 | 349 | 351 | 91.53 | 53.21 | 108 | | | | BlueWalker 3 2022-111AL 53807 |
in space
|
| Demonstrator satellite for a potential constellation of comsats to provide direct connection to hand held mobile phones. Its Launch Vehicle Adapter separated from Falcon 9 at 03:23 UTC after the rocket raised its orbit above the Starlink release height. Until about Nov 11 the satellite was contained within the Adapter at which time it was released into independent orbit. On Nov 14, satellite owner AST SpaceMobile announced it had unfolded its 64 square metre arial array. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Nov 14, 18:05 | 6888 | 0.0014 | 500 | 520 | 94.83 | 53.20 | 117 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Sep 11
Life <1 day
|
| Launched Bluewalker 3 and thirty four Starlink satellites. Caused to re-enter with surviving fragments hitting the south western Pacific Ocean north of New Zealand at about 04:15 UTC, 1.3 circuits after lift-off. |
| Not Catalogued - orbit parameters unavailable | |
2022-112 CZ 7A (Y-4)
Wenchang Space Centre | 2022 Sep 13, 13:18 | Zhongxing 1E (Chinasat 1E) 2022-112A 53813 |
in space
|
| Communications satellite described as carrying high-quality voice, data and radio and TV transmissions. Probably for government/military services. Moved to geosynchronous drift orbit late on September 14. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Sep 13, 22:47 | 24369 | 0.7302 | 197 | 35785 | 630.99 | 13.93 | 174 | | | | 2022 Sep 20, 23:33 | 42158 | 0.0001 | 35775 | 35785 | 1435.77 | 1.51 | 231 | 81° east | | | 2022 Sep 23, 13:29 | 42165 | 0.0003 | 35776 | 35797 | 1436.09 | 1.50 | 252 | 81° east | | | CZ 7 third stage 2022-112B 53814 |
Re-entered - 2022 Oct 13
Life 30 days
|
| Launched Zhongxing 1E. Perigee lowered after releasing satellite causing it not to be acknowledged by Space-Track for ten days. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 23, 06:00 | 21953 | 0.7044 | 111 | 31038 | 539.51 | 13.93 | 181 | | | |
2022-113 Electron (The Owl Spreads Its Wings)
Rocket Lab Launch Complex, New Zealand | 2022 Sep 15, 20:38 | |
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. Released from launch vehicle at 21:32 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Sep 16, 21:19 | 6944 | 0.0013 | 557 | 575 | 95.99 | 97.66 | 294 | 09:00 | | | Electron second stage 2022-113B 53816 |
Re-entered - 2022 Sep 28
Life 13 days
|
| Launched Strix 1. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 16, 05:00 | 6761 | 0.0300 | 180 | 586 | 92.21 | 97.66 | 224 | | | | Electron third stage (kick stage) 2022-113C 53817 |
in space
|
| Launched Strix 1. Did not perform usual perigee-lowering manoeuvre after satellite release. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 16, 18:07 | 6944 | 0.0013 | 557 | 575 | 95.99 | 97.66 | 296 | | | |
2022-114 Falcon 9 Block 5 (Starlink Group 4-34)
Cape Canaveral Space Force Station | 2022 Sep 19, 00:18 | Starlink 4749 2022-114A 53818 |
in space
|
One member of a simultaneously-launched cluster of fifty four LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude.
All satellites expected to be injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 23, 16:00 | 6687 | 0.0031 | 288 | 330 | 90.70 | 53.22 | 55 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Sep 19
Life <1 day
|
| Launched fifty four Starlink satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2022-115 CZ 2D
Jiuquan Space Centre | 2022 Sep 20, 23:15 | Yunhai-1 03 2022-115A 53877 |
in space
|
| Meteorological satellite developed by the Shanghai Academy of Spaceflight Technology (SAST) to be used for observation of atmospheric, marine and space environments, disaster prevention and scientific experiments. Replaces Yunhai 1-01. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Sep 22, 08:44 | 7143 | 0.0014 | 756 | 775 | 100.14 | 98.50 | 256 | 05:31 | | | 2022 Sep 25, 11:46 | 7148 | 0.0010 | 763 | 777 | 100.24 | 98.50 | 272 | 05:31 | | | 2022 Sep 26, 05:42 | 7156 | 0.0004 | 775 | 780 | 100.41 | 98.49 | 2 | 05:31 | | | 2022 Sep 26, 07:19 | 7160 | 0.0002 | 781 | 784 | 100.50 | 98.48 | 60 | 05:31 | | | CZ 2D second stage 2022-115B 53878 |
in space
|
| Launched Yunhai 1-03. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 21, 02:23 | 7046 | 0.0125 | 580 | 756 | 98.10 | 98.55 | 43 | | | |
2022-116 Soyuz-2 1A
Baikonur Cosmodrome | 2022 Sep 21, 13:54 | Soyuz MS-22 (Soyuz 11F732A48 № 751, Konstantin Tsiolkovsky) 2022-116A 53879 |
Re-entered - 2023 Mar 28
Life 188 days
Returned to Earth |
| Carried crew to ISS - Sergey Prokovyev (commander) and Dmitri Petelin (both Roscosmos) and Frank Rubio (NASA). Separated from launch vehicle at 14:03 UTC. Docked with the Rassvet module at 17:06 UTC. Suffered loss of pressure in its cooling system 2022 December leading to a decision to return it to Earth without a crew. It was replaced at ISS by Soyuz MS-23, launched without crew. Soyuz MS-22 undocked 2023 March 28 at 09:57:27 UTC. Retrofire at 10:51 UTC led to landing 147 km south east of Dzhezkazgan at 11:45:58 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 21, 14:26 | 6590 | 0.0012 | 204 | 220 | 88.74 | 51.63 | 97 | | | | 2022 Sep 21, 17:00 | 6794 | 0.0002 | 415 | 418 | 92.89 | 51.64 | 282 | | | | 2023 Mar 27, 13:27 | 6796 | 0.0006 | 414 | 422 | 92.93 | 51.64 | 137 | | | | Soyuz third stage 2022-116B 53880 |
Re-entered - 2022 Sep 24
Life 3 days
|
| Launched Soyuz MS-22. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 21, 14:22 | 6577 | 0.0021 | 185 | 213 | 88.47 | 51.65 | 29 | | | |
2022-117 Delta 4 Heavy
Vandenberg Space Force Base | 2022 Sep 24, 22:25 | USA 338 (KH-11 Block-5 F-3/Crystal?) 2022-117A 53883 |
in space
|
| KH-11 reconnaissance satellite. Orbital elements not released by Spacetrack so parameters are based on work by amateur observers. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 26, 08:54 | 6766 | 0.0008 | 382 | 393 | 92.30 | 73.57 | 25 | | | | 2022 Sep 28, 12:48 | 6784 | 0.0012 | 398 | 414 | 92.69 | 73.58 | 5 | | | | Delta 4 upper stage uncatalogued |
Re-entered - 2022 Sep 24
Life <1 day
|
| Launched USA 338. Caused to re-enter above the eastern Pacific Ocean Sep 25 around 00:00 UTC |
| Not Catalogued - orbit parameters unavailable | |
2022-118 Kuaizhou 1A
Taiyuan Space Centre | 2022 Sep 24, 22:55 | Shiyan 14 (Test 14) 2022-118A 53884 |
in space
|
| Purpose unknown - described as "mainly used to conduct scientific experiments and verify new technologies". Catalogue Number and Designation subject to confirmation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Sep 25, 03:23 | 6876 | 0.0013 | 488 | 506 | 94.56 | 97.52 | 260 | 06:02 | | | Shiyan 15 (Test 15) 2022-118B 53885 |
in space
|
| Purpose unknown but probably an imaging satellite - described as being to "provide data in the fields of land survey, urban planning, and disaster prevention and mitigation". Catalogue Number and Designation subject to confirmation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Sep 25, 03:23 | 6874 | 0.0010 | 488 | 503 | 94.52 | 97.52 | 269 | 06:02 | | | Kuaizhou 1A fourth stage 2022-118C 53942 |
Re-entered - 2023 Nov 6
Life 408 days
|
| Launched Shiyan 14 and Shiyan 15. Perigee lowered after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 25, 03:21 | 6866 | 0.0277 | 298 | 678 | 94.37 | 97.52 | 5 | | | |
2022-119 Falcon 9 Block 5 (Starlink Group 4-35)
Cape Canaveral Space Force Station | 2022 Sep 24, 23:32 | Starlink 5028 2022-119A 53886 |
in space
|
One member of a simultaneously-launched cluster of fifty two LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude.
All satellites expected to be injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 30, 12:00 | 6682 | 0.0034 | 281 | 327 | 90.60 | 53.22 | 63 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Sep 25
Life 1 day
|
| Launched fifty three Starlink satellites. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2022-120 CZ 2D
Xichang Space Centre | 2022 Sep 26, 13:38 | Yaogan 36-01 Follower 2 2022-120A 53943 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-01 (launch 2021-101) satellites so may represent an enhancement of the constellation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 26, 21:27 | 6871 | 0.0009 | 486 | 498 | 94.46 | 34.99 | 268 | | | | 2022 Oct 06, 18:50 | 6871 | 0.0009 | 486 | 499 | 94.47 | 35.00 | 11 | | | | 2022 Nov 12, 06:53 | 6875 | 0.0004 | 495 | 500 | 94.56 | 35.00 | 332 | | | | 2023 Feb 15, 09:31 | 6871 | 0.0004 | 490 | 496 | 94.48 | 35.00 | 167 | | | | 2023 Aug 31, 05:27 | 6871 | 0.0002 | 492 | 494 | 94.48 | 34.99 | 145 | | | | Yaogan 36-01 Follower 1 2022-120D 53946 |
Re-entered - 2024 Jun 28
Life 641 days
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-01 (launch 2021-101) satellites so may represent an enhancement of the constellation. 2023 March, this satellite ceased to manoeuvre and fell out of the operating formation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 27, 05:32 | 6871 | 0.0008 | 488 | 499 | 94.48 | 35.00 | 270 | | | | 2022 Oct 06, 18:51 | 6871 | 0.0008 | 487 | 498 | 94.46 | 35.00 | 349 | | | | 2022 Nov 12, 04:38 | 6875 | 0.0008 | 491 | 503 | 94.55 | 35.00 | 319 | | | | 2023 Feb 15, 09:32 | 6871 | 0.0004 | 490 | 496 | 94.48 | 35.00 | 142 | | | | 2023 Aug 31, 01:39 | 6843 | 0.0004 | 462 | 467 | 93.89 | 34.99 | 129 | | | | Yaogan 36-01 Leader 2022-120E 53947 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-01 (launch 2021-101) satellites so may represent an enhancement of the constellation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 26, 21:26 | 6870 | 0.0010 | 485 | 498 | 94.44 | 35.00 | 288 | | | | 2022 Oct 07, 06:01 | 6871 | 0.0007 | 488 | 497 | 94.46 | 35.00 | 22 | | | | 2022 Nov 12, 06:49 | 6875 | 0.0006 | 493 | 501 | 94.55 | 35.00 | 45 | | | | 2023 Feb 15, 09:27 | 6872 | 0.0008 | 488 | 499 | 94.48 | 35.00 | 190 | | | | 2023 Aug 31, 05:23 | 6871 | 0.0004 | 491 | 496 | 94.47 | 34.99 | 233 | | | | CZ 2D second stage 2022-120C 53945 |
Re-entered - 2023 May 13
Life 229 days
|
| Launched Yaogan 36 Group 1. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Sep 27, 05:31 | 6871 | 0.0010 | 486 | 500 | 94.47 | 35.00 | 273 | | | |
2022-121 CZ 6 (Y-9)
Taiyuan Space Centre | 2022 Sep 26, 23:50 | Shiyan 16A (Test 16A) 2022-121A 53948 |
in space
|
| Purpose unknown but probably an imaging satellite - described as to be "used in the fields of land survey, urban planning, and disaster prevention and mitigation". Catalogue Number and Designation subject to confirmation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Sep 27, 02:52 | 6891 | 0.0011 | 505 | 521 | 94.88 | 97.45 | 270 | 06:59 | | | Shiyan 16B (Test 16B) 2022-121B 53949 |
Re-entered - 2024 Oct 22
Life 757 days
|
| Purpose unknown but probably an imaging satellite - described as to be "used in the fields of land survey, urban planning, and disaster prevention and mitigation". Catalogue Number and Designation subject to confirmation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Sep 27, 02:52 | 6890 | 0.0010 | 505 | 519 | 94.87 | 97.45 | 272 | 06:59 | | | Shiyan 17 (Test 17) 2022-121C 53950 |
in space
|
| Purpose unknown but probably an imaging satellite - described as to be "used in the fields of land survey, urban planning, and disaster prevention and mitigation". Catalogue Number and Designation subject to confirmation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Sep 27, 02:51 | 6890 | 0.0012 | 503 | 520 | 94.85 | 97.46 | 284 | 06:59 | | | CZ 6 third stage uncatalogued |
in space
|
| Launched Shiyan 16A & B and Shiyan 17. Caused to re-enter after releasing satellites. |
| Not Catalogued - orbit parameters unavailable | |
2022-122 Firefly Alpha (FLTA002)
Vandenberg Space Force Base | 2022 Oct 1, 07:01 | |
Re-entered - 2022 Oct 6
Life 5 days
|
| 3U Cubesat from Teachers In Space to collect atmospheric pressure, temperature, and radiation data and make it available for to schools and colleges for educational use. Amateur Radio users reported possible signal reception until at least Oct 4. Re-entry date is an estimate. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 01, 12:39 | 6627 | 0.0045 | 219 | 279 | 89.49 | 136.89 | 164 | | | | |
Re-entered - 2022 Oct 3
Life 2 days
|
PockeQube deployer carrying five PocketQube satellites that were expected to be released into orbit soon after Picobus separated from the Firefly upper stage:
Qubik-3
Qubik-4
FOSSASat-1B
Genesis G (Astroland 1)
Genesis J (Astroland 2)
Re-entry date is an estimate. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6626 | 0.0044 | 219 | 278 | 89.47 | 136.90 | 168 | | | | |
Re-entered - 2022 Oct 3
Life 2 days
|
| 1p PocketQube developed by Spain's Fossa Systems - demonstrator of communications satellite that uses low power radio transmission to provide internet connectivity. Amateur Radio users reported reception of signals up to re-entry Oct 3. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6626 | 0.0044 | 219 | 278 | 89.47 | 136.90 | 168 | | | | Genesis G (Astroland 1) 2022-122xx |
Re-entered - 2022 Oct 3
Life 2 days
|
| 2p PocketQube from AMSAT-EA carrying an amateur radio payload. Amateur Radio users reported possible signal reception up to re-entry on Oct 3. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6626 | 0.0044 | 219 | 278 | 89.47 | 136.90 | 168 | | | | Genesis J (Astroland 2) 2022-122xx |
Re-entered - 2022 Oct 3
Life 2 days
|
| 2p PocketQube from AMSAT-EA carrying an amateur radio payload. Amateur Radio users reported possible signal reception up to re-entry on Oct 3. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6626 | 0.0044 | 219 | 278 | 89.47 | 136.90 | 168 | | | | |
Re-entered - 2022 Oct 3
Life 2 days
|
| 1p PocketQube from Libre Space Foundation, part of an experiment designed to support identification of individual satellites early in their life and to generate accurate orbital elements from radio tracking. Amateur Radio users reported signal reception up to re-entry in the early hours of Oct 3. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6626 | 0.0044 | 219 | 278 | 89.47 | 136.90 | 168 | | | | |
Re-entered - 2022 Oct 3
Life 2 days
|
| 1p PocketQube from Libre Space Foundation, part of an experiment designed to support identification of individual satellites early in their life and to generate accurate orbital elements from radio tracking. Amateur Radio users reported signal reception up to re-entry in the early hours of Oct 3. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6626 | 0.0044 | 219 | 278 | 89.47 | 136.90 | 168 | | | | |
Re-entered - 2022 Oct 2
Life 1 day
|
| 3U Cubesat from NASA Ames equipped with a moveable drag sail to test control of orbit decay through varying its orientation. Unexpectedly low orbit prevented testing of the sail. Also carried a small quantity of space experiments. Re-entry date is an estimate. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6626 | 0.0044 | 219 | 278 | 89.47 | 136.90 | 168 | | | | Firefly Alpha upper stage 2022-122E 53959 |
Re-entered - 2022 Oct 7
Life 6 days
|
| Launched 3 satellites. Carried Firefly Capsule containing postcards, a book and artwork provided by Teachers In Space and Girl Scouts of Austin. Mission was a test of the launch vehicle, intended to reach 296 x 301 km orbit but fell 20+ km short of planned apogee. Subsequent second firing of upper stage failed to raise perigee sufficiently and resulted in earlier than planned re-entry. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6616 | 0.0046 | 208 | 268 | 89.26 | 136.89 | 167 | | | | 2022 Oct 02, 04:02 | 6625 | 0.0039 | 222 | 273 | 89.45 | 136.88 | 171 | | | |
2022-123 Atlas V 531
Cape Canaveral Space Force Station | 2022 Oct 4, 21:36 | |
in space
|
| One of a pair of simultaneously launched comsats from SES to provide services to the US. Separated from launch vehicle Oct 5 at 03:14 UTC. Expected location 103° west. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Oct 06, 15:22 | 41351 | 0.0003 | 34959 | 34987 | 1394.73 | 1.87 | 159 | | | | 2022 Oct 13, 15:00 | 41506 | 0.0010 | 35087 | 35169 | 1402.58 | 1.81 | 177 | 166° west | | | 2022 Oct 16, 07:09 | 41730 | 0.0062 | 35091 | 35612 | 1413.92 | 1.39 | 105 | 149° west | | | 2022 Oct 19, 15:37 | 42151 | 0.0008 | 35740 | 35805 | 1435.38 | 0.67 | 247 | 141° west | | | 2022 Oct 24, 08:01 | 42165 | 0.0003 | 35773 | 35801 | 1436.12 | 0.08 | 83 | 141° west | | | 2022 Nov 18, 12:50 | 42165 | 0.0003 | 35773 | 35801 | 1436.11 | 0.02 | 119 | 141° west | | | 2022 Nov 21, 11:45 | 42046 | 0.0001 | 35662 | 35673 | 1430.02 | 0.02 | 300 | 137° west | | | 2022 Dec 14, 15:09 | 42157 | 0.0001 | 35777 | 35782 | 1435.72 | 0.07 | 327 | 103° west | | | 2022 Dec 20, 20:56 | 42166 | 0.0001 | 35785 | 35791 | 1436.16 | 0.08 | 93 | 103° west | | | |
in space
|
| One of a pair of simultaneously launched comsats from SES to provide services to the US. Separated from launch vehicle at 03:54 UTC. Expected location 131° west. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Oct 06, 08:00 | 41263 | 0.0034 | 34744 | 35026 | 1390.28 | 1.88 | 184 | | | | 2022 Oct 13, 16:33 | 41477 | 0.0067 | 34822 | 35375 | 1401.08 | 1.66 | 168 | | | | 2022 Oct 24, 16:48 | 42162 | 0.0003 | 35770 | 35798 | 1435.96 | 0.06 | 126 | 143° west | | | 2022 Oct 27, 07:09 | 42166 | 0.0003 | 35773 | 35803 | 1436.16 | 0.06 | 139 | 143° west | | | 2022 Nov 10, 18:23 | 42165 | 0.0001 | 35784 | 35789 | 1436.10 | 0.04 | 340 | 143° west | | | 2022 Nov 14, 17:06 | 42087 | 0.0001 | 35705 | 35713 | 1432.14 | 0.04 | 98 | 139° west | | | 2022 Nov 22, 17:57 | 42122 | 0.0009 | 35707 | 35780 | 1433.89 | 0.05 | 355 | 131° west | | | 2022 Nov 25, 14:19 | 42166 | 0.0002 | 35779 | 35797 | 1436.17 | 0.04 | 102 | 131° west | | | Atlas V upper stage (Centaur) 2022-123C 53962 |
in space
|
| Launched SES 20 and SES 21. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 06, 08:12 | 40232 | 0.0289 | 32690 | 35018 | 1338.50 | 1.86 | 198 | | | |
2022-124 Falcon 9 Block 5
Kennedy Space Center | 2022 Oct 5, 16:00 | SpaceX Dragon Crew 5 (Dragon Endurance Flight #2) 2022-124A 53963 |
Re-entered - 2023 Mar 12
Life 158 days
Returned to Earth |
| Crew flight to ISS provided by SpaceX under contract to NASA. Crew members - Nicole Mann (commander) & Josh Cassada (both NASA), Koichi Wakata (JAXA), and Anna Kikina (Roscosmos). Precise launch time 16:00:56. Separated from launch vehicle at 15:13:03 UTC. Docked with forward port of Harmony module Oct 6 at 21:14 UTC, about 30 mins after the originally published time. Undocked, carrying its original crew, 2023 Mar 11 at 07:19 UTC. Retro-fire Mar 12 at 01:11 UTC led to splashdown at about 02:02 UTC in the Gulf of Mexico off Florida. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 05, 16:24 | 6578 | 0.0014 | 191 | 210 | 88.50 | 51.65 | 358 | | | | 2022 Oct 05, 19:17 | 6597 | 0.0015 | 209 | 228 | 88.87 | 51.65 | 250 | | | | 2022 Oct 06, 11:28 | 6598 | 0.0021 | 206 | 233 | 88.89 | 51.68 | 223 | | | | 2022 Oct 06, 17:43 | 6795 | 0.0003 | 415 | 418 | 92.90 | 51.64 | 278 | | | | 2022 Oct 06, 19:12 | 6793 | 0.0004 | 412 | 417 | 92.86 | 51.64 | 263 | | | | 2022 Oct 07, 15:20 | 6795 | 0.0003 | 415 | 419 | 92.92 | 51.64 | 266 | | | | 2023 Mar 10, 13:15 | 6797 | 0.0006 | 415 | 423 | 92.96 | 51.64 | 69 | | | | 2023 Mar 11, 09:34 | 6786 | 0.0004 | 405 | 411 | 92.72 | 51.63 | 76 | | | | 2023 Mar 11, 14:10 | 6734 | 0.0079 | 303 | 410 | 91.66 | 51.65 | 56 | | | | 2023 Mar 11, 23:00 | 6734 | 0.0081 | 301 | 410 | 91.65 | 51.64 | 57 | | | | Crew Dragon trunk module 2022-124B 55840 |
Re-entered - 2023 Apr 27
Life 204 days
|
| Separated from Dragon Crew 5 shortly before retrofire. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2023 Mar 12, 10:56 | 6733 | 0.0082 | 299 | 410 | 91.64 | 51.32 | 58 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Oct 5
Life <1 day
|
| Launched Crew Dragon 5. Caused to re-enter above Indian Ocean at around 17:00 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2022-125 Falcon 9 Block 5 (Starlink Group 4-29)
Vandenberg Space Force Base | 2022 Oct 5, 23:10 | Starlink 4633 2022-125A 53964 |
in space
|
One member of a simultaneously-launched cluster of fifty two LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle Oct 6 at 00:13:02 UTC.
All satellites expected to be injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 11, 18:00 | 6707 | 0.0002 | 327 | 330 | 91.10 | 53.22 | 31 | | | | Falcon 9 upper stage uncatalogued |
Re-entered - 2022 Oct 6
Life 1 day
|
| Launched fifty four Starlink satellites. Caused to re-enter above the Pacific Ocean Oct 6 at around 01:00 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2022-126 CZ 11H
Mobile floating platform, Yellow Sea - 36°.6 N, 121°.2 E | 2022 Oct 7, 13:10 | Centispace-1 S5 2022-126A 54020 |
in space
|
| Satellite for a LEO navigation enhancement system being developed by Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Will also be used to test the Beidou system and to test an inter-satellite laser communication system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 07, 19:11 | 7078 | 0.0013 | 691 | 709 | 98.78 | 55.00 | 295 | | | | Centispace-1 S6 2022-126B 54021 |
in space
|
| Satellite for a LEO navigation enhancement system being developed by Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Will also be used to test the Beidou system and to test an inter-satellite laser communication system. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 07, 16:07 | 7078 | 0.0015 | 689 | 710 | 98.76 | 55.00 | 293 | | | | CZ 11H fourth stage 2022-126C 54022 |
Re-entered - 2024 Apr 21
Life 562 days
|
| Launched Centispace 1 S5 and S6 duo. Perigee lowered after releasing satellites. Launch location was 3 km offshore mainland China near Qingdao. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 07, 16:08 | 6928 | 0.0346 | 310 | 790 | 95.65 | 56.15 | 312 | | | |
2022-127 Electron (It Argos Up From Here)
Rocket Lab Launch Complex, New Zealand | 2022 Oct 7, 17:09 | |
in space
|
| Satellite from General Atomics of the US hosting Argos 4 payload from the US National Oceanographic and Atmospheric Administration. Argos will collect weather and climate data via radio beacons at remote locations around the Earth. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Oct 07, 19:31 | 7131 | 0.0012 | 744 | 762 | 99.89 | 98.32 | 300 | 05:35 | | | Electron third stage (kick stage) 2022-127B 54024 |
in space
|
| Launched GAzelle. Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 07, 21:08 | 7031 | 0.0144 | 552 | 754 | 97.79 | 98.30 | 21 | | | | Electron second stage 2022-127C 54025 |
Re-entered - 2023 Feb 27
Life 143 days
|
| Launched GAzelle. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 07, 19:51 | 6902 | 0.0353 | 280 | 767 | 95.11 | 98.34 | 219 | | | |
2022-128 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2022 Oct 8, 23:05 | |
in space
|
| Intelsat-owned communications satellite serving North America. Launched together with Galaxy 34. Released from launch vehicle at 23:37 UTC. Expected location 133° west to replace Galaxy 15 (28884/2005-041A). |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Oct 09, 01:26 | 16442 | 0.5935 | 305 | 19823 | 349.71 | 26.84 | 175 | | | | 2022 Oct 11, 09:44 | 16538 | 0.5958 | 307 | 20013 | 352.78 | 26.88 | 178 | | | | 2022 Oct 14, 19:12 | 24393 | 0.7254 | 320 | 35709 | 631.90 | 26.53 | 180 | | | | 2022 Oct 16, 02:24 | 26405 | 0.5932 | 4363 | 35692 | 711.70 | 15.58 | 180 | | | | 2022 Oct 17, 10:00 | 30663 | 0.3725 | 12863 | 35706 | 890.59 | 6.86 | 179 | | | | 2022 Oct 18, 02:51 | 39022 | 0.0825 | 29424 | 35865 | 1278.58 | 1.06 | 178 | | | | 2022 Oct 20, 17:58 | 40647 | 0.0353 | 32835 | 35703 | 1359.27 | 0.40 | 174 | | | | 2022 Oct 25, 22:10 | 42137 | 0.0000 | 35758 | 35760 | 1434.70 | 0.04 | 237 | 133° west | | | 2022 Oct 26, 18:35 | 42164 | 0.0003 | 35773 | 35799 | 1436.07 | 0.03 | 285 | 133° west | | | |
in space
|
| Intelsat-owned communications satellite serving North America. Launched together with Galaxy 33. Released from launch vehicle at 23:43 UTC. Expected location 129° west to replace Galaxy 12 (27715/2003-013). |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Oct 09, 02:40 | 16449 | 0.5937 | 305 | 19837 | 349.93 | 26.84 | 175 | | | | 2022 Oct 13, 15:00 | 22768 | 0.7066 | 302 | 32478 | 569.84 | 26.63 | 180 | | | | 2022 Oct 17, 10:30 | 24433 | 0.7235 | 377 | 35734 | 633.48 | 26.28 | 182 | | | | 2022 Oct 18, 00:27 | 26718 | 0.5741 | 5001 | 35679 | 724.38 | 14.36 | 183 | | | | 2022 Oct 20, 01:00 | 30772 | 0.3651 | 13161 | 35628 | 895.37 | 6.61 | 183 | | | | 2022 Oct 26, 09:55 | 42101 | 0.0016 | 35657 | 35790 | 1432.86 | 0.06 | 211 | 149° west | | | 2022 Oct 29, 03:20 | 42168 | 0.0002 | 35782 | 35797 | 1436.24 | 0.06 | 175 | 148° west | | | 2022 Nov 24, 05:31 | 42080 | 0.0001 | 35697 | 35707 | 1431.78 | 0.00 | 243 | 146° west | | | 2022 Dec 13, 03:08 | 42165 | 0.0002 | 35779 | 35794 | 1436.09 | 0.02 | 93 | 129° west | | | Falcon 9 upper stage 2022-128C 54028 |
in space
|
| Launched Galaxy 33 and Galaxy 34. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 10, 22:51 | 16439 | 0.5936 | 302 | 19820 | 349.60 | 26.84 | 178 | | | |
2022-129 CZ 2D
Jiuquan Space Centre | 2022 Oct 8, 23:43 | Kuafu 1 (Advanced Space-based Solar Observatory, ASO-S) 2022-129A 54029 |
in space
|
| Science satellite studying solar flares and coronal mass ejection, and the solar magnetic field. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Oct 09, 20:41 | 7101 | 0.0013 | 713 | 732 | 99.25 | 98.27 | 264 | 05:59 | | | CZ 2D second stage 2022-129B 54030 |
in space
|
| Launched Kuafu 1 (ASOS-S). Perigee lowered after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 09, 04:32 | 7088 | 0.0020 | 696 | 725 | 98.98 | 98.19 | 117 | | | |
2022-130 Soyuz-2 1B + Fregat
Plesetsk Cosmodrome | 2022 Oct 10, 02:52 | Cosmos 2559 (Uragan-K1 № 17L) 2022-130A 54031 |
in space
|
| GLONASS-K navigation satellite. It also carries radio receiving equipment for the COSPAS-SARSAT international search and rescue system. Released from Fregat at about 06:15 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 11, 13:10 | 25529 | 0.0002 | 19147 | 19155 | 676.56 | 64.78 | 323 | | | | 2022 Oct 31, 12:34 | 25508 | 0.0008 | 19110 | 19149 | 675.73 | 64.78 | 225 | | | | Fregat rocket stage 2022-130B 54032 |
in space
|
| Launched Cosmos 2559 (GLONASS K). Apogee raised after releasing satellite. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 11, 03:35 | 25659 | 0.0035 | 19190 | 19372 | 681.74 | 64.89 | 229 | | | |
2022-F05 - failed to reach orbit Epsilon
Uchinoura Space Center, Japan | 2022 Oct 12, 00:50 | |
|
| 1U Cubesat from the Future Science institute, Japan to demonstrate a multi-spectral imager and associated data processing system before transmitting data to Earth. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly. |
| |
|
| 2U Cubesat from Japan's National Institute of Technology (KOSEN) for marine studies including sub-sea crustal deformation. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Also carries demonstrator of a multi-point communications system. Lost when launcher third stage failed to separate properly. |
| |
|
| Science satellite from Kanazawa University, Japan fitted with sensors to study x-ray and gamma ray emissions associated with gravity waves. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly. |
| MAGNARO (MAGnetically separating NAno-satellite with Rotation for Orbit control) |
|
| 3U Cubesat from Nagoyo University, Japan. Consists of two satellites, Magnaro-Tigris (2U) and Magnaro-Piscis (1U), joined magnetically. They were to separated 6-12 months after launch and conduct formation manoeuvres using air resistance to control the distance between them. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly. |
| |
|
| 2U Cubesat to be used to monitor and measure degradation of off-the-shelf electronic components. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly. |
| PETREL (Platform for Extra and Terrestrial Remote Examination with LCTF) |
|
| Small satellite from the Tokyo Institute of Technology carrying a multi-spectral camera for ocean studies. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly. |
| RAISE 3 (RApid Innovative payload demonstration SatellitE 3) |
|
| Small satellite to demonstrate a range of technology including radio systems, an onboard comuter, a water-based thruster, a plasma thruster and a folded, deployable mebrane panel. Also carries a drag sail to accelerate orbit decay. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly. |
| STARS-X (Space Tethered Autonomous Robotic Satellite) |
|
| Two-part satellite from Shizuoka University. The two halves are connected by a 1 km tether to carry a 'climber' moving along the tether with a net to capture space debris. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly. |
| |
|
| 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. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly. |
|
2022-131 Proton-M + Blok DM3
Baikonur Cosmodrome | 2022 Oct 12, 15:00 | |
in space
|
| Russian built comsat to be operated by Angosat of Angola with coverage of Africa and southern Europe. Replaces Angosat 1 (43087/2017-086A) that failed while in GEO drift orbit. Released from launch vehicle around 21:00 UTC. Anticipated to enter service 2022 Nov. Expected location - 23° east. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Oct 13, 14:04 | 42567 | 0.0001 | 36183 | 36195 | 1456.68 | 0.03 | 119 | 85° east | | | 2022 Oct 21, 19:12 | 42475 | 0.0002 | 36088 | 36105 | 1451.96 | 0.02 | 124 | 45° east | | | 2022 Oct 27, 14:18 | 42300 | 0.0001 | 35916 | 35927 | 1443.00 | 0.05 | 69 | 28° east | | | 2022 Oct 31, 00:00 | 42207 | 0.0002 | 35820 | 35838 | 1438.24 | 0.03 | 207 | 24° east | | | 2022 Nov 03, 11:34 | 42167 | 0.0001 | 35784 | 35794 | 1436.23 | 0.03 | 208 | 23° east | | | Blok DM-03 rocket stage 2022-131B 54034 |
in space
|
| Launched Angosat. Initial orbit shown is while Angosat was still attached. Apogee raised after releasing satellites. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 12, 20:37 | 24595 | 0.7312 | 233 | 36201 | 639.78 | 48.87 | 359 | | | | 2022 Oct 17, 19:23 | 42887 | 0.0081 | 36162 | 36856 | 1473.16 | 0.16 | 173 | | | |
2022-132 CZ 2C
Taiyuan Space Centre | 2022 Oct 12, 22:53 | Huanjing 2E (S-SAR 01) 2022-132A 54035 |
in space
|
| Chinese Earth surface imaging satellite equipped with a synthetic aperture radar operating at S-band frequencies. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Oct 13, 07:50 | 6873 | 0.0012 | 487 | 503 | 94.51 | 97.40 | 271 | 06:00 | | | 2023 May 10, 07:15 | 6865 | 0.0002 | 485 | 488 | 94.34 | 97.39 | 87 | 06:01 | | | 2023 May 12, 14:25 | 6878 | 0.0003 | 498 | 502 | 94.61 | 97.39 | 43 | 06:01 | | | 2023 May 17, 13:49 | 6882 | 0.0007 | 499 | 509 | 94.70 | 97.39 | 351 | 06:01 | | | CZ 2C second stage 2022-132E 54039 |
in space
|
| Launched Huanjing 2E. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 13, 08:21 | 6897 | 0.0047 | 487 | 552 | 95.01 | 97.25 | 209 | | | |
2022-133 CZ 2D
Xichang Space Centre | 2022 Oct 14, 19:12 | Yaogan 36-02 Follower 1 2022-133A 54042 |
in space
|
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-02 (launch 2022-068) satellites so may represent an enhancement of the constellation. 2022 December, this satellite ceased to maintain its orbit and fell out of the operating formation. However, it continued to make periodic thruster firings.
NOTE: Until Oct 26, Space-Track identified this object as 54046/2022-133E. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 15, 04:26 | 6871 | 0.0008 | 488 | 499 | 94.47 | 34.99 | 266 | | | | 2022 Oct 24, 07:16 | 6871 | 0.0007 | 488 | 497 | 94.46 | 35.00 | 342 | | | | 2022 Nov 16, 03:23 | 6874 | 0.0008 | 490 | 502 | 94.53 | 35.00 | 200 | | | | 2023 Feb 15, 12:27 | 6872 | 0.0008 | 488 | 499 | 94.48 | 35.00 | 326 | | | | Yaogan 36-02 Follower 2 2022-133B 54043 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-02 (launch 2022-068) satellites so may represent an enhancement of the constellation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 15, 03:01 | 6870 | 0.0009 | 486 | 498 | 94.45 | 34.99 | 282 | | | | 2022 Oct 20, 22:39 | 6872 | 0.0008 | 488 | 499 | 94.48 | 34.99 | 340 | | | | 2022 Nov 16, 09:56 | 6875 | 0.0009 | 490 | 503 | 94.55 | 35.00 | 255 | | | | 2023 Feb 15, 13:59 | 6871 | 0.0012 | 485 | 501 | 94.48 | 35.00 | 328 | | | | Yaogan 36-02 Leader 2022-133D 54045 |
in space
|
| Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-02 (launch 2022-068) satellites so may represent an enhancement of the constellation. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 15, 03:01 | 6869 | 0.0009 | 485 | 497 | 94.43 | 34.99 | 288 | | | | 2022 Oct 24, 00:31 | 6872 | 0.0014 | 484 | 503 | 94.48 | 35.00 | 2 | | | | 2022 Nov 16, 03:15 | 6875 | 0.0007 | 492 | 501 | 94.54 | 35.00 | 244 | | | | 2023 Feb 15, 13:58 | 6872 | 0.0011 | 486 | 501 | 94.48 | 35.00 | 342 | | | | CZ 2D second stage 2022-133E 54046 |
Re-entered - 2023 Aug 26
Life 316 days
|
Launched Yaogan 36 Group 2. Space-Track tags this item as debris but the scatter pattern of objects after launch points to it being the CZ upper stage.
NOTE: Until Oct 26, Space-Track identified this object as 54042/2022-133A. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 15, 03:00 | 6871 | 0.0009 | 487 | 499 | 94.46 | 35.00 | 272 | | | |
2022-134 Falcon 9 Block 5
Cape Canaveral Space Force Station | 2022 Oct 15, 05:22 | Eutelsat Hot Bird 13F 2022-134A 54048 |
in space
|
| Comsat providing direct TV service to homes in Europe. Released from launch vehicle at 05:58 UTC. Expected location - 13° east as part of the replacement program for Hotbirds 9A, 13B and 13C. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | GEO
Longitude | |
| 2022 Oct 16, 17:20 | 34452 | 0.8041 | 372 | 55775 | 1060.65 | 26.83 | 181 | | | | 2022 Oct 22, 09:35 | 35443 | 0.7960 | 854 | 57277 | 1106.79 | 25.11 | 182 | | | | 2022 Nov 01, 18:55 | 37475 | 0.7709 | 2207 | 59987 | 1203.30 | 21.37 | 185 | | | | 2022 Nov 11, 07:12 | 39494 | 0.7553 | 3285 | 62947 | 1301.85 | 18.39 | 187 | | | | 2022 Nov 21, 17:38 | 41992 | 0.7300 | 4962 | 66266 | 1427.27 | 15.19 | 188 | | | | 2022 Nov 21, 18:05 | 41400 | 0.7258 | 4974 | 65069 | 1397.19 | 15.12 | 187 | | | | 2022 Nov 22, 20:00 | 41194 | 0.7358 | 4506 | 65125 | 1386.79 | 14.97 | 189 | | | | 2022 Nov 29, 04:39 | 42609 | 0.7064 | 6133 | 66328 | 1458.84 | 13.45 | 190 | | | | 2022 Dec 07, 22:56 | 43212 | 0.6812 | 7397 | 66271 | 1489.93 | 11.87 | 191 | | | | 2022 Dec 14, 04:38 | 43826 | 0.6372 | 9520 | 65375 | 1521.79 | 10.07 | 191 | | | | 2022 Dec 22, 09:42 | 43802 | 0.5944 | 11386 | 63461 | 1520.53 | 8.21 | 193 | | | | 2022 Dec 27, 21:49 | 43955 | 0.5623 | 12862 | 62293 | 1528.54 | 7.49 | 195 | | | | 2023 Jan 04, 22:00 | 44160 | 0.5140 | 15083 | 60481 | 1539.25 | 5.89 | 196 | | | | 2023 Jan 11, 20:00 | 44088 | 0.4682 | 17068 | 58352 | 1535.46 | 5.13 | 196 | | | | 2023 Jan 18, 20:00 | 44069 | 0.4208 | 19149 | 56233 | 1534.49 | 4.14 | 198 | | | | 2023 Jan 25, 12:41 | 43657 | 0.3715 | 21060 | 53497 | 1513.00 | 3.56 | 200 | | | | 2023 Feb 03, 00:00 | 43669 | 0.3019 | 24107 | 50475 | 1513.63 | 2.55 | 201 | | | | 2023 Feb 08, 06:01 | 43763 | 0.2723 | 25466 | 49303 | 1518.50 | 2.47 | 205 | | | | 2023 Feb 15, 16:01 | 41050 | 0.2246 | 25451 | 43892 | 1379.51 | 1.78 | 203 | | | | 2023 Feb 23, 14:24 | 43197 | 0.1476 | 30443 | 43195 | 1489.15 | 1.28 | 204 | | | | 2023 Mar 01, 10:40 | 42869 | 0.0967 | 32347 | 40634 | 1472.21 | 0.87 | 204 | 50° east | | | 2023 Mar 10, 21:35 | 42263 | 0.0219 | 34958 | 36811 | 1441.10 | 0.31 | 196 | 3° east | | | 2023 Mar 16, 01:10 | 42166 | 0.0000 | 35787 | 35789 | 1436.17 | 0.12 | 325 | 2° east | | | 2023 Apr 02, 06:24 | 42164 | 0.0001 | 35783 | 35789 | 1436.06 | 0.08 | 158 | 2° east | | | 2023 Apr 03, 09:03 | 42207 | 0.0001 | 35825 | 35833 | 1438.25 | 0.08 | 159 | 1° east | | | 2023 Apr 05, 09:14 | 42169 | 0.0002 | 35783 | 35800 | 1436.33 | 0.07 | 105 | 0° east | | | 2023 Apr 06, 20:37 | 42164 | 0.0001 | 35781 | 35791 | 1436.07 | 0.07 | 74 | 0° east | | | 2023 Jul 25, 23:54 | 42165 | 0.0002 | 35780 | 35793 | 1436.09 | 0.08 | 335 | 1° east | | | Falcon 9 upper stage 2022-134B 54049 |
in space
|
| Launched Hotbird 13F. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 18, 22:20 | 34702 | 0.8048 | 397 | 56251 | 1072.25 | 26.84 | 181 | | | |
2022-135 Angara 1.2
Plesetsk Cosmodrome | 2022 Oct 15, 19:55 | Cosmos 2560 2022-135A 54050 |
Re-entered - 2022 Dec 10
Life 56 days
|
| Possible imaging reconnaissance satellite carried on a test launch of the Angara 1.2 rocket. LTDN matches Cosmos 2555 (52330/2022-044A) and Cosmos 2551 (49127/2021-081A), First launch attempt cancelled late in countdown on Oct 14. Re-entered naturally. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Oct 15, 23:16 | 6714 | 0.0011 | 329 | 344 | 91.26 | 96.35 | 250 | 11:30 | | | 2022 Dec 09, 19:24 | 6540 | 0.0005 | 159 | 166 | 87.74 | 96.31 | 286 | 11:19 | | | orbit insertion stage uncatalogued |
Re-entered - 2022 Oct 15
Life <1 day
|
| Launched Cosmos 2560. Apogee raised after releasing satellite. Caused to re-enter above central Pacific Ocean at about 23:30 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6908 | 0.0291 | 329 | 731 | 95.24 | 96.35 | 250 | | | |
2022-136 Falcon 9 Block 5 (Starlink Group 4-36)
Cape Canaveral Space Force Station | 2022 Oct 20, 14:50 | Starlink 5195 2022-136A 54051 |
in space
|
One member of a simultaneously-launched cluster of fifty four LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:05 UTC.
All satellites expected to be injected initially into similar orbits at about 330 km altitude. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 25, 16:00 | 6681 | 0.0032 | 282 | 324 | 90.58 | 53.22 | 56 | | | | Falcon 9 upper stage uncatalogued |
in space
|
| Launched fifty four Starlink satellites. Caused to re-enter above the Indian Ocean at around (probably) 16:00 UTC. |
| Not Catalogued - orbit parameters unavailable | |
2022-137 Soyuz-2 1V + Volga
Plesetsk Cosmodrome | 2022 Oct 21, 19:20 | Cosmos 2561 2022-137A 54109 |
in space
|
| Military satellite, one of a simultaneously-launched, but not necessarily related, pair - purpose unknown but may have an Earth observation mission. Released from Volga stage shortly after 20:17 UTC. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Oct 22, 10:36 | 6793 | 0.0008 | 409 | 421 | 92.86 | 97.08 | 263 | 10:58 | | | 2023 Jan 30, 22:22 | 6782 | 0.0007 | 399 | 409 | 92.64 | 97.07 | 257 | 10:58 | | | 2023 Jan 31, 12:16 | 6784 | 0.0009 | 399 | 412 | 92.67 | 97.07 | 245 | 10:58 | | | 2023 Apr 05, 21:22 | 6771 | 0.0009 | 387 | 399 | 92.42 | 97.06 | 16 | 10:59 | | | 2023 Apr 06, 14:20 | 6784 | 0.0011 | 398 | 414 | 92.69 | 97.06 | 219 | 10:59 | | | 2023 Sep 19, 12:39 | 6767 | 0.0008 | 383 | 395 | 92.34 | 97.05 | 242 | 11:02 | | | 2023 Sep 19, 20:22 | 6775 | 0.0012 | 389 | 405 | 92.50 | 97.05 | 243 | 11:02 | | | 2023 Sep 21, 10:56 | 6775 | 0.0012 | 389 | 405 | 92.49 | 97.04 | 237 | 11:02 | | | 2023 Sep 21, 16:16 | 6782 | 0.0013 | 395 | 413 | 92.64 | 97.03 | 258 | 11:02 | | | 2023 Sep 22, 10:07 | 6785 | 0.0012 | 398 | 415 | 92.69 | 97.04 | 240 | 11:02 | | | 2023 Sep 26, 14:35 | 6784 | 0.0012 | 397 | 414 | 92.68 | 97.05 | 224 | 11:02 | | | 2023 Sep 26, 19:14 | 6794 | 0.0013 | 407 | 424 | 92.88 | 97.05 | 241 | 11:02 | | | 2023 Oct 29, 13:41 | 6788 | 0.0014 | 401 | 419 | 92.77 | 97.04 | 125 | 11:01 | | | 2023 Oct 29, 18:20 | 6796 | 0.0008 | 413 | 423 | 92.93 | 97.04 | 183 | 11:01 | | | 2023 Oct 30, 19:08 | 6804 | 0.0012 | 417 | 434 | 93.08 | 97.04 | 245 | 11:01 | | | 2023 Oct 31, 19:59 | 6811 | 0.0012 | 425 | 441 | 93.23 | 97.04 | 241 | 11:01 | | | 2023 Nov 01, 14:39 | 6818 | 0.0013 | 431 | 449 | 93.38 | 97.04 | 236 | 11:01 | | | 2023 Nov 03, 21:13 | 6828 | 0.0012 | 441 | 458 | 93.58 | 97.04 | 240 | 11:00 | | | Cosmos 2562 2022-137B 54110 |
Re-entered - 2023 Nov 8
Life 383 days
|
| Military satellite, one of a simultaneously-launched, but not necessarily related, pair. Released from Volga stage shortly after 20:17 UTC. 2022 November - Resurs-P 3 (41386, 2016-016A) manoeuvred alongside it and was then used as a rendezvous target, possibly to test a satellite servicing mission profile. Manoeuvres ceased 2023 July 26 and the orbit then decayed naturally up to re-entry. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | Desc Node
Local Time | |
| 2022 Oct 22, 13:42 | 6791 | 0.0008 | 408 | 419 | 92.83 | 97.08 | 255 | 10:58 | | | 2022 Oct 28, 10:35 | 6791 | 0.0009 | 407 | 419 | 92.82 | 97.08 | 231 | 10:58 | | | 2022 Oct 28, 16:46 | 6789 | 0.0010 | 404 | 417 | 92.78 | 97.08 | 247 | 10:58 | | | 2022 Oct 31, 12:51 | 6786 | 0.0012 | 400 | 416 | 92.73 | 97.08 | 247 | 10:58 | | | 2022 Nov 14, 21:39 | 6785 | 0.0013 | 398 | 415 | 92.69 | 97.08 | 190 | 10:58 | | | 2022 Nov 16, 09:08 | 6770 | 0.0005 | 389 | 395 | 92.40 | 97.10 | 223 | 10:58 | | | 2023 Jan 15, 21:27 | 6763 | 0.0013 | 376 | 393 | 92.24 | 97.19 | 30 | 11:04 | | | 2023 Jan 16, 13:19 | 6769 | 0.0016 | 380 | 402 | 92.38 | 97.19 | 348 | 11:04 | | | 2023 Jan 23, 15:49 | 6768 | 0.0015 | 379 | 400 | 92.35 | 97.19 | 320 | 11:05 | | | 2023 Jan 24, 17:59 | 6764 | 0.0012 | 377 | 394 | 92.26 | 97.19 | 359 | 11:05 | | | 2023 Jan 25, 12:27 | 6763 | 0.0012 | 377 | 393 | 92.26 | 97.18 | 357 | 11:05 | | | 2023 Jan 25, 18:36 | 6763 | 0.0012 | 377 | 394 | 92.26 | 97.18 | 356 | 11:05 | | | 2023 Feb 13, 13:17 | 6760 | 0.0011 | 374 | 389 | 92.18 | 97.18 | 280 | 11:07 | | | 2023 Feb 13, 18:26 | 6763 | 0.0014 | 375 | 394 | 92.25 | 97.18 | 270 | 11:07 | | | 2023 Feb 15, 20:40 | 6763 | 0.0014 | 375 | 395 | 92.25 | 97.18 | 265 | 11:08 | | | 2023 Feb 16, 21:16 | 6760 | 0.0010 | 375 | 389 | 92.19 | 97.18 | 266 | 11:08 | | | 2023 Mar 27, 22:26 | 6753 | 0.0011 | 367 | 382 | 92.04 | 97.17 | 113 | 11:12 | | | Soyuz upper stage 2022-137C 54111 |
Re-entered - 2022 Nov 3
Life 13 days
|
| Launched Cosmos 2661 and 2662 pair. Originally planned for launch Oct 18. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| 2022 Oct 22, 04:27 | 6672 | 0.0156 | 189 | 398 | 90.39 | 97.08 | 71 | | | | Volga rocket stage 2022-137D 54112 |
Re-entered - 2022 Oct 22
Life 1 day
|
| Launched Cosmos 2561 and 2562 pair. Orbit circularised at about 20:17 UTC. First orbit listed covers the period when Volga and the satellites were still attached to each other. Caused to re-enter after releasing the satellites, possibly as late as Oct 22, around 07:15 UTC. Originally planned for launch Oct 18. |
epoch (UTC) | s-m axis
( km ) | ecc | perigee
( km ) | apogee
( km ) | period
( min ) | incl
( ° ) | ω
( ° ) | | |
| estimated orbit | 6673 | 0.0161 | 188 | 403 | 90.42 | 97.08 | 72 | | | | 2022 Oct 21, 22:47 | 6793 | 0.0007 | 410 | 419 | 92.86 | 97.08 | 263 | | | |
2022-138 LVM3 (M2)
Satish Dhawan Space Centre | 2022 Oct 22, 18:37 | OneWeb 0490 2022-138A 54113 |
in space
|
Broadband distribution satellite for the UK company OneWeb.
One of 36 similar satellites carried on this launch, released from the upper stage of the launch vehicle in nine batches of four over a period of three hours. |
epoch (UTC) | s-m axis
( km ) | ecc | pe | |
