ESSA 7 (TOS-E)
Informationen über den Satelliten. ESSA 7 (TOS-E)
| Name im Katalog Spacetrack | ESSA 7 (TOS-E) |
| Folge ESSA 7 (TOS-E) | ESSA 7 (TOS-E) Tracker |
| Flugzeiten ESSA 7 (TOS-E) | Flugzeiten ESSA 7 (TOS-E) |
| In die Umlaufbahn bringen |
1968-08-16 (58 vor Jahren)
|
| Tage im Orbit | 21202 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 1431 km |
| Apogäum | 1473 km |
| Neigung der Umlaufbahn (Inklination) | 101.57° |
| Runden pro Tag | 13 |
| Höhe ESSA 7 (TOS-E) | 1463.43 km |
Informationen über ESSA 7 (TOS-E)
ESSA 7 (TOS-E), 3345 is a payload satellite owned by ESSA (US) in SSO that was launched on Fri, 16 Aug 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 7 (TOS-E) hinausgetragen 16.08.1968r. Durchschnittshöhe ESSA 7 (TOS-E) Text Nummer 1: das. 1463.43 km. Durchschnittsgeschwindigkeit ESSA 7 (TOS-E) beträgt 25677.51 km/h. Neigung ESSA 7 (TOS-E) Satelliten 101.57°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ESSA 7 (TOS-E)
Durchschnittsgeschwindigkeit ESSA 7 (TOS-E)
Durchschnitt ESSA 7 (TOS-E)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) ESSA 7 (TOS-E)
Mittleres Argument des Perigäums ESSA 7 (TOS-E)
Mittlere große Halbachse der Umlaufbahn ESSA 7 (TOS-E)
Mittlere Bahnexzentrizität ESSA 7 (TOS-E)
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