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 |
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Tage im Orbit | 1445 |
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) | 97.69° |
Runden pro Tag | 15 |
Höhe MANDRAKE 2 ABLE | 484.14 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. 484.14 km. Durchschnittsgeschwindigkeit MANDRAKE 2 ABLE beträgt 27448.96 km/h. Neigung MANDRAKE 2 ABLE Satelliten 97.67°.
W tabelce, częstotliwości. MANDRAKE 2 ABLE.
Downlink | Modus |
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400.498 MHz | FSK |