ESSA 1 (OT-3)
Informationen über den Satelliten. ESSA 1 (OT-3)
| Name im Katalog Spacetrack | ESSA 1 (OT-3) |
| Folge ESSA 1 (OT-3) | ESSA 1 (OT-3) Tracker |
| Flugzeiten ESSA 1 (OT-3) | Flugzeiten ESSA 1 (OT-3) |
| In die Umlaufbahn bringen |
1966-02-03 (60 vor Jahren)
|
| Tage im Orbit | 22134 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perygeum | 677 km |
| Apogäum | 794 km |
| Neigung der Umlaufbahn (Inklination) | 97.81° |
| Runden pro Tag | 14 |
| Höhe ESSA 1 (OT-3) | 743.15 km |
Informationen über ESSA 1 (OT-3)
ESSA 1 (OT-3), 1982 is a payload satellite owned by ESSA (US) in SSO that was launched on Thu, 03 Feb 1966 UTC via a THOR DELTA C 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 1 (OT-3) hinausgetragen 03.02.1966r. Durchschnittshöhe ESSA 1 (OT-3) Text Nummer 1: das. 743.15 km. Durchschnittsgeschwindigkeit ESSA 1 (OT-3) beträgt 26945.01 km/h. Neigung ESSA 1 (OT-3) Satelliten 97.81°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ESSA 1 (OT-3)
Durchschnittsgeschwindigkeit ESSA 1 (OT-3)
Durchschnitt ESSA 1 (OT-3)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) ESSA 1 (OT-3)
Mittleres Argument des Perigäums ESSA 1 (OT-3)
Mittlere große Halbachse der Umlaufbahn ESSA 1 (OT-3)
Mittlere Bahnexzentrizität ESSA 1 (OT-3)
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