INMARSAT 3-F2

24307
Nummer im Katalog Spacetrack
1996-09-06
In die Umlaufbahn bringen
35865.49 km
Höhe Durchschnitt
11058.6 km/h
Durchschnittsgeschwindigkeit

Informationen über den Satelliten. INMARSAT 3-F2

Name im Katalog Spacetrack INMARSAT 3-F2
Folge INMARSAT 3-F2 INMARSAT 3-F2 Tracker
Flugzeiten INMARSAT 3-F2 Flugzeiten INMARSAT 3-F2
In die Umlaufbahn bringen 1996-09-06 (29 vor Jahren)
Tage im Orbit 10822
Herkunftsland/-organisation International Mobile Satellite Organization (INMARSAT) (IM)
Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. TYMSC (Baikonur Cosmodrome, Kazakhstan)
Kategorie
Perygeum 35846 km
Apogäum 35879 km
Neigung der Umlaufbahn (Inklination) 9.74°
Runden pro Tag 1
Orbit GEO
Höhe INMARSAT 3-F2 35865.49 km

Informationen über INMARSAT 3-F2

Marisat satellites were the first maritime telecommunications satellites and were designed to provide dependable telecommunications for commercial shipping and the U.S. Navy from stable geosynchronous orbital locations over the three major ocean regions. The three Marisat satellites, F1, F2, and F3, were built by Hughes Aircraft Corporation (HAC) for COMSAT Corporation starting in 1973. The satellites were designed to provide maritime telecommunications services in three large ocean areas, the Atlantic Ocean, the Pacific Ocean, and the Indian Ocean, and were located at 72.5° East longitude, 176.5° E, and 345° E in the geosynchronous orbital arc. The three-satellite Marisat system served as the initial INMARSAT constellation.
Ownership of the three Marisat satellites was transferred to Lockheed Martin when it bought COMSAT Corp in 2000. The Marisat-F2 satellite was acquired by INTELSAT as part of the COMSAT General Corp. acquisition in October 2004.
The three satellites were all launched in 1976. MARISAT F1 was launched on 19 February 1976, MARISAT F2 was launched on 10 June 1976, and Marisat F3 was launched at 22:44 GMT, 14 October 1976. Launch vehicle for the satellites was the McDonnell Douglas 2914 Delta rocket. The satellites were launched from Cape Canaveral by the National Aeronautics and Space Administration under contract with COMSAT. In 1981 the INMARSAT took over from the Marisat system.

der Satellit INMARSAT 3-F2 hinausgetragen 06.09.1996r. Durchschnittshöhe INMARSAT 3-F2 Text Nummer 1: das. 35865.49 km. Durchschnittsgeschwindigkeit INMARSAT 3-F2 beträgt 11058.6 km/h. Neigung INMARSAT 3-F2 Satelliten 9.32°.

Orbital Elemente

Zeige formatiertes JSON.

Durchschnittshöhe der Orbitalbahn. INMARSAT 3-F2

Durchschnittsgeschwindigkeit INMARSAT 3-F2

Durchschnitt INMARSAT 3-F2

Aktualisierungsdatum.: 2026-04-24 00:00:19
Durchschnittshöhe INMARSAT 3-F2 beträgt: 35865.49km
Durchschnittsgeschwindigkeit INMARSAT 3-F2 beträgt: 11058.6km/h
Durchschnittliche Neigung der Bahn INMARSAT 3-F2 beträgt: 9.32°
INMARSAT 3-F2 wurde am Tag in eine Umlaufbahn gebracht 1996-09-06
INMARSAT 3-F2 ist von 10822 Tage in der Umlaufbahn.