2021-059AE - Norad Identifikationsnummer: 48907
| Name im Katalog Spacetrack | MANDRAKE 2 ABLE |
| Alternative Bezeichnung | 2021-059AE |
| Folge MANDRAKE 2 ABLE | MANDRAKE 2 ABLE Tracker |
| Flugzeiten MANDRAKE 2 ABLE | Flugzeiten MANDRAKE 2 ABLE |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 1765 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | hier |
| Perygeum | 520 km |
| Apogäum | 535 km |
| Neigung der Umlaufbahn (Inklination) | 97.7° |
| Runden pro Tag | 16 |
| Höhe MANDRAKE 2 ABLE | 443.73 km |
MANDRAKE 2 ABLE, 48907 is an American payload satellite in SSO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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 MANDRAKE 2 ABLE hinausgetragen 30.06.2021r. Durchschnittshöhe MANDRAKE 2 ABLE Text Nummer 1: das. 443.73 km. Durchschnittsgeschwindigkeit MANDRAKE 2 ABLE beträgt 27530.17 km/h. Neigung MANDRAKE 2 ABLE Satelliten 97.7°.
W tabelce, częstotliwości. MANDRAKE 2 ABLE.
| Downlink | Modus |
|---|---|
| 400.498 MHz | FSK |