2022-057AD - Norad Identifikationsnummer: 52759
Name im Katalog Spacetrack | ICEYE-X20 |
Alternative Bezeichnung | 2022-057AD |
Folge ICEYE-X20 | ICEYE-X20 Tracker |
Flugzeiten ICEYE-X20 | Flugzeiten ICEYE-X20 |
In die Umlaufbahn bringen |
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Tage im Orbit | 1219 |
Herkunftsland/-organisation | Finland (FIN) |
Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
Perygeum | 520 km |
Apogäum | 536 km |
Neigung der Umlaufbahn (Inklination) | 97.59° |
Runden pro Tag | 16 |
Orbit | LEO (Nicht-polar geneigt) |
Höhe ICEYE-X20 | 413.31 km |
ICEYE-X20, 52759 is a Finnish payload satellite in SSO that was launched on Wed, 25 May 2022 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 ICEYE-X20 hinausgetragen 25.05.2022r. Durchschnittshöhe ICEYE-X20 Text Nummer 1: das. 413.31 km. Durchschnittsgeschwindigkeit ICEYE-X20 beträgt 27591.8 km/h. Neigung ICEYE-X20 Satelliten 97.59°.
W tabelce, częstotliwości. ICEYE-X20.
Downlink | Modus |
---|---|
2269.685 MHz | 150k BPSK |