TANSEI-1 (MS-T1)
Informationen über den Satelliten. TANSEI-1 (MS-T1)
| Name im Katalog Spacetrack | TANSEI-1 (MS-T1) |
| In die Umlaufbahn bringen |
1971-02-16 |
| Deorbitation |
|
| Herkunftsland/-organisation | Japonia (JPN) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | KSCUT (Uchinoura Space Center, Japan) |
| Perygeum | 982 km |
| Apogäum | 1100 km |
| Höhe TANSEI-1 (MS-T1) | 1041.53 km |
Informationen über TANSEI-1 (MS-T1)
TANSEI 1 (MS-T1), 4952 is a payload satellite owned by ISAS (JP) in LEO that was launched on Tue, 16 Feb 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 TANSEI-1 (MS-T1) hinausgetragen 16.02.1971r. Durchschnittshöhe TANSEI-1 (MS-T1) Text Nummer 1: das. 1041.53 km. Durchschnittsgeschwindigkeit TANSEI-1 (MS-T1) beträgt 26401.1 km/h. Neigung TANSEI-1 (MS-T1) Satelliten 29.67°.Durchschnittshöhe der Orbitalbahn. TANSEI-1 (MS-T1)
Durchschnittsgeschwindigkeit TANSEI-1 (MS-T1)
Durchschnitt TANSEI-1 (MS-T1)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) TANSEI-1 (MS-T1)
Mittleres Argument des Perigäums TANSEI-1 (MS-T1)
Mittlere große Halbachse der Umlaufbahn TANSEI-1 (MS-T1)
Mittlere Bahnexzentrizität TANSEI-1 (MS-T1)
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