ESSA 9 (TOS-G)
Informationen über den Satelliten. ESSA 9 (TOS-G)
| Name im Katalog Spacetrack | ESSA 9 (TOS-G) |
| Folge ESSA 9 (TOS-G) | ESSA 9 (TOS-G) Tracker |
| Flugzeiten ESSA 9 (TOS-G) | Flugzeiten ESSA 9 (TOS-G) |
| In die Umlaufbahn bringen |
1969-02-26 (57 vor Jahren)
|
| Tage im Orbit | 21015 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perygeum | 1425 km |
| Apogäum | 1505 km |
| Neigung der Umlaufbahn (Inklination) | 101.41° |
| Runden pro Tag | 13 |
| Höhe ESSA 9 (TOS-G) | 1476.66 km |
Informationen über ESSA 9 (TOS-G)
ESSA 9 (TOS-G), 3764 is a payload satellite owned by ESSA (US) in SSO that was launched on Wed, 26 Feb 1969 UTC via a THOR DELTA E1 launch vehicle from the Air Force Eastern Test Range (AFETR). 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 ESSA 9 (TOS-G) hinausgetragen 26.02.1969r. Durchschnittshöhe ESSA 9 (TOS-G) Text Nummer 1: das. 1476.66 km. Durchschnittsgeschwindigkeit ESSA 9 (TOS-G) beträgt 25655.74 km/h. Neigung ESSA 9 (TOS-G) Satelliten 101.41°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ESSA 9 (TOS-G)
Durchschnittsgeschwindigkeit ESSA 9 (TOS-G)
Durchschnitt ESSA 9 (TOS-G)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) ESSA 9 (TOS-G)
Mittleres Argument des Perigäums ESSA 9 (TOS-G)
Mittlere große Halbachse der Umlaufbahn ESSA 9 (TOS-G)
Mittlere Bahnexzentrizität ESSA 9 (TOS-G)
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