HINODE (SOLAR B)
Informationen über den Satelliten. HINODE (SOLAR B)
| Name im Katalog Spacetrack | HINODE (SOLAR B) |
| Folge HINODE (SOLAR B) | HINODE (SOLAR B) Tracker |
| Flugzeiten HINODE (SOLAR B) | Flugzeiten HINODE (SOLAR B) |
| In die Umlaufbahn bringen |
2006-09-22 g.02:00 (19 vor Jahren)
|
| Tage im Orbit | 7017 |
| Herkunftsland/-organisation | Japonia (JPN) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | KSCUT (Uchinoura Space Center, Japan) |
| WWW | hier |
| Kategorie | |
| Perygeum | 665 km |
| Apogäum | 691 km |
| Neigung der Umlaufbahn (Inklination) | 98.07° |
| Runden pro Tag | 15 |
| Orbit | LEO (Sonnenbahn-synchron) |
| Höhe HINODE (SOLAR B) | 680.85 km |
Informationen über HINODE (SOLAR B)
HINODE (SOLAR B), 29479 is a payload satellite owned by ISAS/JAXA (JP) in SSO that was launched on Fri, 22 Sep 2006 UTC via an M-V 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 HINODE (SOLAR B) hinausgetragen 22.09.2006r. Durchschnittshöhe HINODE (SOLAR B) Text Nummer 1: das. 680.85 km. Durchschnittsgeschwindigkeit HINODE (SOLAR B) beträgt 27063.69 km/h. Neigung HINODE (SOLAR B) Satelliten 98.08°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. HINODE (SOLAR B)
Durchschnittsgeschwindigkeit HINODE (SOLAR B)
Durchschnitt HINODE (SOLAR B)
Frequenzen HINODE (SOLAR B)
W tabelce, częstotliwości. HINODE (SOLAR B).
| Downlink | Modus |
|---|---|
| 2256.219 MHz | FM |
