LEMUR 2 ROCINANTE
Satellite information LEMUR 2 ROCINANTE - 2024-043BB
| Spacetrack Directory Name | LEMUR 2 ROCINANTE |
| Alternative name | 2024-043BB |
| Orbit launches |
2024-03-04 g.01:00 |
| Deorbitation |
|
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 506 km |
| Apogee | 519 km |
| Height LEMUR 2 ROCINANTE | 393.99 km |
Additional information LEMUR 2 ROCINANTE
LEMUR 2 ROCINANTE, 59147 is an American payload satellite in SSO that was launched on Mon, 04 Mar 2024 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 ROCINANTE Date of exalting 04.03.2024y. Average height of ISS LEMUR 2 ROCINANTE hundred 393.99 km. Average velocity LEMUR 2 ROCINANTE is 27632.55 km/h. Inclination LEMUR 2 ROCINANTE satellite 97.51°.Average orbit height LEMUR 2 ROCINANTE
Average velocity LEMUR 2 ROCINANTE
Average inclination LEMUR 2 ROCINANTE
ISS
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