EUTE 2-F3
Satellite information EUTE 2-F3 - EUTELSAT 2-F3
| Spacetrack Directory Name | EUTE 2-F3 |
| Alternative name | EUTELSAT 2-F3 |
| Follow EUTE 2-F3 | EUTE 2-F3 Tracker |
| Pass predictions EUTE 2-F3 | Pass predictions EUTE 2-F3 |
| Orbit launches |
1991-12-07 (34 years ago)
|
| Days in orbit | 12694 |
| Country/organisation of origin | European Telecommunications Satellite Organization (EUTELSAT) (EUTE) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36046 km |
| Apogee | 36078 km |
| Orbit slope (inclination) | 14.81° |
| Laps per day | 1 |
| Height EUTE 2-F3 | 36061.47 km |
Additional information EUTE 2-F3
EUTE 2-F3, 21803 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Sat, 07 Dec 1991 UTC via an ATLAS II 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.
satellite EUTE 2-F3 Date of exalting 07.12.1991y. Average height of ISS EUTE 2-F3 hundred 36061.47 km. Average velocity EUTE 2-F3 is 11033.07 km/h. Inclination EUTE 2-F3 satellite 14.81°.TLE
Average velocity EUTE 2-F3
Average inclination EUTE 2-F3
Mean right ascension of the ascending node (RAAN) EUTE 2-F3
Mean argument of perigee EUTE 2-F3
Mean semi-major axis of the orbit EUTE 2-F3
Mean orbital eccentricity EUTE 2-F3
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