ESSA 4 (TOS-B)
Informationen über den Satelliten. ESSA 4 (TOS-B)
| Name im Katalog Spacetrack | ESSA 4 (TOS-B) |
| Folge ESSA 4 (TOS-B) | ESSA 4 (TOS-B) Tracker |
| Flugzeiten ESSA 4 (TOS-B) | Flugzeiten ESSA 4 (TOS-B) |
| In die Umlaufbahn bringen |
1967-01-26 (59 vor Jahren)
|
| Tage im Orbit | 21770 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | hier |
| Perygeum | 1326 km |
| Apogäum | 1439 km |
| Neigung der Umlaufbahn (Inklination) | 102.08° |
| Runden pro Tag | 13 |
| Höhe ESSA 4 (TOS-B) | 1394.02 km |
Informationen über ESSA 4 (TOS-B)
ESSA 4 (TOS-B), 2657 is a payload satellite owned by ESSA (US) in SSO that was launched on Thu, 26 Jan 1967 UTC via a THOR DELTA E 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 4 (TOS-B) hinausgetragen 26.01.1967r. Durchschnittshöhe ESSA 4 (TOS-B) Text Nummer 1: das. 1394.02 km. Durchschnittsgeschwindigkeit ESSA 4 (TOS-B) beträgt 25792.09 km/h. Neigung ESSA 4 (TOS-B) Satelliten 102.08°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ESSA 4 (TOS-B)
Durchschnittsgeschwindigkeit ESSA 4 (TOS-B)
Durchschnitt ESSA 4 (TOS-B)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) ESSA 4 (TOS-B)
Mittleres Argument des Perigäums ESSA 4 (TOS-B)
Mittlere große Halbachse der Umlaufbahn ESSA 4 (TOS-B)
Mittlere Bahnexzentrizität ESSA 4 (TOS-B)
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