SHINSEI (MS-F2)
Informationen über den Satelliten. SHINSEI (MS-F2)
| Name im Katalog Spacetrack | SHINSEI (MS-F2) |
| In die Umlaufbahn bringen |
1971-09-28 |
| Deorbitation |
|
| Herkunftsland/-organisation | Japonia (JPN) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | KSCUT (Uchinoura Space Center, Japan) |
| WWW | hier |
| Perygeum | 870 km |
| Apogäum | 1861 km |
| Höhe SHINSEI (MS-F2) | 1378.6 km |
Informationen über SHINSEI (MS-F2)
SHINSEI (MS-F2), 5485 is a payload satellite owned by ISAS (JP) in LEO that was launched on Tue, 28 Sep 1971 UTC via a MU-4S launch vehicle from the Kagoshima Space Center University Of Tokyo (KSCUT). 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 SHINSEI (MS-F2) hinausgetragen 28.09.1971r. Durchschnittshöhe SHINSEI (MS-F2) Text Nummer 1: das. 1378.6 km. Durchschnittsgeschwindigkeit SHINSEI (MS-F2) beträgt 25824.95 km/h. Neigung SHINSEI (MS-F2) Satelliten 32.05°.Durchschnittshöhe der Orbitalbahn. SHINSEI (MS-F2)
Durchschnittsgeschwindigkeit SHINSEI (MS-F2)
Durchschnitt SHINSEI (MS-F2)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) SHINSEI (MS-F2)
Mittleres Argument des Perigäums SHINSEI (MS-F2)
Mittlere große Halbachse der Umlaufbahn SHINSEI (MS-F2)
Mittlere Bahnexzentrizität SHINSEI (MS-F2)
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