SEASAT 1
Informationen über den Satelliten. SEASAT 1
| Name im Katalog Spacetrack | SEASAT 1 |
| Folge SEASAT 1 | SEASAT 1 Tracker |
| Flugzeiten SEASAT 1 | Flugzeiten SEASAT 1 |
| In die Umlaufbahn bringen |
1978-06-27 (48 vor Jahren)
|
| Tage im Orbit | 17636 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Kategorie | |
| Perygeum | 745 km |
| Apogäum | 747 km |
| Neigung der Umlaufbahn (Inklination) | 108.01° |
| Runden pro Tag | 14 |
| Höhe SEASAT 1 | 748.6 km |
Informationen über SEASAT 1
Seasat was the first Earth-orbiting satellite designed for remote sensing of the Earth's oceans and had on board the first spaceborne synthetic-aperture radar (SAR). The mission was designed to demonstrate the feasibility of global satellite monitoring of oceanographic phenomena and to help determine the requirements for an operational ocean remote sensing satellite system. Specific objectives were to collect data on sea-surface winds, sea-surface temperatures, wave heights, internal waves, atmospheric water, sea ice features and ocean topography. Seasat was managed by NASA's Jet Propulsion Laboratory and was launched on 27 June 1978 into a nearly circular 800 km (500 mi) orbit with an inclination of 108°. Seasat operated until 10 October 1978 (UTC), when a massive short circuit in the Agena-D bus electrical system ended the mission.
der Satellit SEASAT 1 hinausgetragen 27.06.1978r. Durchschnittshöhe SEASAT 1 Text Nummer 1: das. 748.6 km. Durchschnittsgeschwindigkeit SEASAT 1 beträgt 26935.2 km/h. Neigung SEASAT 1 Satelliten 108.01°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. SEASAT 1
Durchschnittsgeschwindigkeit SEASAT 1
Durchschnitt SEASAT 1
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) SEASAT 1
Mittleres Argument des Perigäums SEASAT 1
Mittlere große Halbachse der Umlaufbahn SEASAT 1
Mittlere Bahnexzentrizität SEASAT 1
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