LEMUR 2 EMBRIONOVIS
Satellite information LEMUR 2 EMBRIONOVIS - 2023-084AQ
| Spacetrack Directory Name | LEMUR 2 EMBRIONOVIS |
| Alternative name | 2023-084AQ |
| Follow LEMUR 2 EMBRIONOVIS | LEMUR 2 EMBRIONOVIS Tracker |
| Pass predictions LEMUR 2 EMBRIONOVIS | Pass predictions LEMUR 2 EMBRIONOVIS |
| Orbit launches |
2023-06-12 (3 years ago)
|
| Days in orbit | 1107 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 513 km |
| Apogee | 536 km |
| Orbit slope (inclination) | 97.63° |
| Laps per day | 15 |
| Height LEMUR 2 EMBRIONOVIS | 478.09 km |
Additional information LEMUR 2 EMBRIONOVIS
LEMUR 2 EMBRIONOVIS, 56970 is an American payload satellite in SSO that was launched on Mon, 12 Jun 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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 EMBRIONOVIS Date of exalting 12.06.2023y. Average height of ISS LEMUR 2 EMBRIONOVIS hundred 478.09 km. Average velocity LEMUR 2 EMBRIONOVIS is 27461.05 km/h. Inclination LEMUR 2 EMBRIONOVIS satellite 97.61°.TLE
Average orbit height LEMUR 2 EMBRIONOVIS
Average velocity LEMUR 2 EMBRIONOVIS
Average inclination LEMUR 2 EMBRIONOVIS
ISS
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