LEMUR 2 ROCINANTE
Informationen über den Satelliten. LEMUR 2 ROCINANTE - 2024-043BB
| Name im Katalog Spacetrack | LEMUR 2 ROCINANTE |
| Alternative Bezeichnung | 2024-043BB |
| In die Umlaufbahn bringen |
2024-03-04 g.01:00 |
| Deorbitation |
|
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 506 km |
| Apogäum | 519 km |
| Höhe LEMUR 2 ROCINANTE | 414.66 km |
Informationen über 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.
der Satellit LEMUR 2 ROCINANTE hinausgetragen 04.03.2024r. Durchschnittshöhe LEMUR 2 ROCINANTE Text Nummer 1: das. 414.66 km. Durchschnittsgeschwindigkeit LEMUR 2 ROCINANTE beträgt 27590.28 km/h. Neigung LEMUR 2 ROCINANTE Satelliten 97.51°.Durchschnittshöhe der Orbitalbahn. LEMUR 2 ROCINANTE
Durchschnittsgeschwindigkeit LEMUR 2 ROCINANTE
Durchschnitt LEMUR 2 ROCINANTE
