ESSA 6 (TOS-D)
Informationen über den Satelliten. ESSA 6 (TOS-D)
| Name im Katalog Spacetrack | ESSA 6 (TOS-D) |
| Folge ESSA 6 (TOS-D) | ESSA 6 (TOS-D) Tracker |
| Flugzeiten ESSA 6 (TOS-D) | Flugzeiten ESSA 6 (TOS-D) |
| In die Umlaufbahn bringen |
1967-11-10 (58 vor Jahren)
|
| Tage im Orbit | 21482 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 1409 km |
| Apogäum | 1485 km |
| Neigung der Umlaufbahn (Inklination) | 102.02° |
| Runden pro Tag | 13 |
| Höhe ESSA 6 (TOS-D) | 1458.42 km |
Informationen über ESSA 6 (TOS-D)
ESSA 6 (TOS-D), 3035 is a payload satellite owned by ESSA (US) in SSO that was launched on Fri, 10 Nov 1967 UTC via a THOR DELTA E1 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 6 (TOS-D) hinausgetragen 10.11.1967r. Durchschnittshöhe ESSA 6 (TOS-D) Text Nummer 1: das. 1458.42 km. Durchschnittsgeschwindigkeit ESSA 6 (TOS-D) beträgt 25685.73 km/h. Neigung ESSA 6 (TOS-D) Satelliten 102.02°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ESSA 6 (TOS-D)
Durchschnittsgeschwindigkeit ESSA 6 (TOS-D)
Durchschnitt ESSA 6 (TOS-D)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) ESSA 6 (TOS-D)
Mittleres Argument des Perigäums ESSA 6 (TOS-D)
Mittlere große Halbachse der Umlaufbahn ESSA 6 (TOS-D)
Mittlere Bahnexzentrizität ESSA 6 (TOS-D)
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