ESSA 8 (TOS-F)
Informationen über den Satelliten. ESSA 8 (TOS-F)
| Name im Katalog Spacetrack | ESSA 8 (TOS-F) |
| Folge ESSA 8 (TOS-F) | ESSA 8 (TOS-F) Tracker |
| Flugzeiten ESSA 8 (TOS-F) | Flugzeiten ESSA 8 (TOS-F) |
| In die Umlaufbahn bringen |
1968-12-15 (57 vor Jahren)
|
| Tage im Orbit | 21081 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 1414 km |
| Apogäum | 1463 km |
| Neigung der Umlaufbahn (Inklination) | 101.71° |
| Runden pro Tag | 13 |
| Höhe ESSA 8 (TOS-F) | 1449.88 km |
Informationen über ESSA 8 (TOS-F)
ESSA 8 (TOS-F), 3615 is a payload satellite owned by ESSA (US) in SSO that was launched on Sun, 15 Dec 1968 UTC via a THOR DELTA N launch vehicle from the Air Force Western Test Range (AFWTR). 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 8 (TOS-F) hinausgetragen 15.12.1968r. Durchschnittshöhe ESSA 8 (TOS-F) Text Nummer 1: das. 1449.88 km. Durchschnittsgeschwindigkeit ESSA 8 (TOS-F) beträgt 25699.6 km/h. Neigung ESSA 8 (TOS-F) Satelliten 101.7°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ESSA 8 (TOS-F)
Durchschnittsgeschwindigkeit ESSA 8 (TOS-F)
Durchschnitt ESSA 8 (TOS-F)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) ESSA 8 (TOS-F)
Mittleres Argument des Perigäums ESSA 8 (TOS-F)
Mittlere große Halbachse der Umlaufbahn ESSA 8 (TOS-F)
Mittlere Bahnexzentrizität ESSA 8 (TOS-F)
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