LEMUR 2 OBA-NI-JESU
Satellite information LEMUR 2 OBA-NI-JESU - 2024-022D
| Spacetrack Directory Name | LEMUR 2 OBA-NI-JESU |
| Alternative name | 2024-022D |
| Follow LEMUR 2 OBA-NI-JESU | LEMUR 2 OBA-NI-JESU Tracker |
| Pass predictions LEMUR 2 OBA-NI-JESU | Pass predictions LEMUR 2 OBA-NI-JESU |
| Orbit launches |
2024-01-31 (2 years ago)
|
| Days in orbit | 827 |
| Country/organisation of origin | USA (US) |
| Starting point | RLLB (Rocket Lab Launch Base) |
| Perigee | 521 km |
| Apogee | 538 km |
| Orbit slope (inclination) | 97.39° |
| Laps per day | 16 |
| Height LEMUR 2 OBA-NI-JESU | 427.52 km |
Additional information LEMUR 2 OBA-NI-JESU
LEMUR 2 OBA-NI-JESU, 58902 is an American payload satellite in SSO that was launched on Wed, 31 Jan 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite LEMUR 2 OBA-NI-JESU Date of exalting 31.01.2024y. Average height of ISS LEMUR 2 OBA-NI-JESU hundred 427.52 km. Average velocity LEMUR 2 OBA-NI-JESU is 27563.19 km/h. Inclination LEMUR 2 OBA-NI-JESU satellite 97.42°.TLE
Average orbit height LEMUR 2 OBA-NI-JESU
Average velocity LEMUR 2 OBA-NI-JESU
Average inclination LEMUR 2 OBA-NI-JESU
