EUTE 1-F2 (ECS 2)
Satellite information EUTE 1-F2 (ECS 2) - EUTELSAT 1-F2 (ECS-2)
| Spacetrack Directory Name | EUTE 1-F2 (ECS 2) |
| Alternative name | EUTELSAT 1-F2 (ECS-2) |
| Follow EUTE 1-F2 (ECS 2) | EUTE 1-F2 (ECS 2) Tracker |
| Pass predictions EUTE 1-F2 (ECS 2) | Pass predictions EUTE 1-F2 (ECS 2) |
| Orbit launches |
1984-08-04 (42 years ago)
|
| Days in orbit | 15387 |
| Country/organisation of origin | European Telecommunications Satellite Organization (EUTELSAT) (EUTE) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36179 km |
| Apogee | 36232 km |
| Orbit slope (inclination) | 12.39° |
| Laps per day | 1 |
| Height EUTE 1-F2 (ECS 2) | 36204.75 km |
Additional information EUTE 1-F2 (ECS 2)
EUTE 1-F2 (ECS 2), 15158 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Sat, 04 Aug 1984 UTC via an ARIANE 3 launch vehicle from the French Guiana (FRGUI). 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 1-F2 (ECS 2) Date of exalting 04.08.1984y. Average height of ISS EUTE 1-F2 (ECS 2) hundred 36204.75 km. Average velocity EUTE 1-F2 (ECS 2) is 11014.52 km/h. Inclination EUTE 1-F2 (ECS 2) satellite 12.41°.TLE
Average velocity EUTE 1-F2 (ECS 2)
Average inclination EUTE 1-F2 (ECS 2)
Mean right ascension of the ascending node (RAAN) EUTE 1-F2 (ECS 2)
Mean argument of perigee EUTE 1-F2 (ECS 2)
Mean semi-major axis of the orbit EUTE 1-F2 (ECS 2)
Mean orbital eccentricity EUTE 1-F2 (ECS 2)
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