TANSEI-3 (MS-T3)
Informationen über den Satelliten. TANSEI-3 (MS-T3)
| Name im Katalog Spacetrack | TANSEI-3 (MS-T3) |
| In die Umlaufbahn bringen |
1977-02-19 |
| Deorbitation |
|
| Herkunftsland/-organisation | Japonia (JPN) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | KSCUT (Uchinoura Space Center, Japan) |
| Perygeum | 806 km |
| Apogäum | 3795 km |
| Höhe TANSEI-3 (MS-T3) | 2442.29 km |
Informationen über TANSEI-3 (MS-T3)
TANSEI 3 (MS-T3), 9841 is a payload satellite owned by ISAS (JP) in LEO that was launched on Sat, 19 Feb 1977 UTC via a MU-3H 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-3 (MS-T3) hinausgetragen 19.02.1977r. Durchschnittshöhe TANSEI-3 (MS-T3) Text Nummer 1: das. 2442.29 km. Durchschnittsgeschwindigkeit TANSEI-3 (MS-T3) beträgt 24195.11 km/h. Neigung TANSEI-3 (MS-T3) Satelliten 65.76°.Durchschnittshöhe der Orbitalbahn. TANSEI-3 (MS-T3)
Durchschnittsgeschwindigkeit TANSEI-3 (MS-T3)
Durchschnitt TANSEI-3 (MS-T3)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) TANSEI-3 (MS-T3)
Mittleres Argument des Perigäums TANSEI-3 (MS-T3)
Mittlere große Halbachse der Umlaufbahn TANSEI-3 (MS-T3)
Mittlere Bahnexzentrizität TANSEI-3 (MS-T3)
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