2024-066F - Norad Identifikationsnummer: 59447
Name im Katalog Spacetrack | QPS-SAR-7 TSUKUYOMI-II |
Alternative Bezeichnung | 2024-066F |
Folge QPS-SAR-7 TSUKUYOMI-II | QPS-SAR-7 TSUKUYOMI-II Tracker |
Flugzeiten QPS-SAR-7 TSUKUYOMI-II | Flugzeiten QPS-SAR-7 TSUKUYOMI-II |
In die Umlaufbahn bringen |
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Tage im Orbit | 440 |
Herkunftsland/-organisation | Japonia (JPN) |
Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
Perygeum | 590 km |
Apogäum | 595 km |
Neigung der Umlaufbahn (Inklination) | 45.61° |
Runden pro Tag | 15 |
Höhe QPS-SAR-7 TSUKUYOMI-II | 579.42 km |
QPS-SAR-7 TSUKUYOMI-II, 59447 is a payload satellite owned by QPS Labs (JP) in LEO that was launched on Sun, 07 Apr 2024 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 QPS-SAR-7 TSUKUYOMI-II hinausgetragen 07.04.2024r. Durchschnittshöhe QPS-SAR-7 TSUKUYOMI-II Text Nummer 1: das. 579.42 km. Durchschnittsgeschwindigkeit QPS-SAR-7 TSUKUYOMI-II beträgt 27263.63 km/h. Neigung QPS-SAR-7 TSUKUYOMI-II Satelliten 45.61°.