ESSA 2 (OT-2)
Informationen über den Satelliten. ESSA 2 (OT-2)
| Name im Katalog Spacetrack | ESSA 2 (OT-2) |
| Folge ESSA 2 (OT-2) | ESSA 2 (OT-2) Tracker |
| Flugzeiten ESSA 2 (OT-2) | Flugzeiten ESSA 2 (OT-2) |
| In die Umlaufbahn bringen |
1966-02-28 (60 vor Jahren)
|
| Tage im Orbit | 22109 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perygeum | 1354 km |
| Apogäum | 1415 km |
| Neigung der Umlaufbahn (Inklination) | 101.22° |
| Runden pro Tag | 13 |
| Höhe ESSA 2 (OT-2) | 1395.9 km |
Informationen über ESSA 2 (OT-2)
ESSA 2 (OT-2), 2091 is a payload satellite owned by ESSA (US) in SSO that was launched on Mon, 28 Feb 1966 UTC via a THOR DELTA E 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 2 (OT-2) hinausgetragen 28.02.1966r. Durchschnittshöhe ESSA 2 (OT-2) Text Nummer 1: das. 1395.9 km. Durchschnittsgeschwindigkeit ESSA 2 (OT-2) beträgt 25788.78 km/h. Neigung ESSA 2 (OT-2) Satelliten 101.22°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ESSA 2 (OT-2)
Durchschnittsgeschwindigkeit ESSA 2 (OT-2)
Durchschnitt ESSA 2 (OT-2)
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) ESSA 2 (OT-2)
Mittleres Argument des Perigäums ESSA 2 (OT-2)
Mittlere große Halbachse der Umlaufbahn ESSA 2 (OT-2)
Mittlere Bahnexzentrizität ESSA 2 (OT-2)
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