Norad Identifikationsnummer: 5485
| Name im Katalog Spacetrack | SHINSEI (MS-F2) |
| Folge SHINSEI (MS-F2) | SHINSEI (MS-F2) Tracker |
| Flugzeiten SHINSEI (MS-F2) | Flugzeiten SHINSEI (MS-F2) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 20097 |
| 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 |
| Neigung der Umlaufbahn (Inklination) | 32.06° |
| Runden pro Tag | 13 |
| Höhe SHINSEI (MS-F2) | 1381.99 km |
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. 1381.99 km. Durchschnittsgeschwindigkeit SHINSEI (MS-F2) beträgt 25814.04 km/h. Neigung SHINSEI (MS-F2) Satelliten 32.05°.
W tabelce, częstotliwości. SHINSEI (MS-F2).
| Downlink | Modus |
|---|---|
| 136.694 MHz | CW |