EUTE 25C (EUTE W5)
Satellite information EUTE 25C (EUTE W5)
| Spacetrack Directory Name | EUTE 25C (EUTE W5) |
| Alternative name | EUTELSAT W5, EUTELSAT 70A |
| Follow EUTE 25C (EUTE W5) | EUTE 25C (EUTE W5) Tracker |
| Pass predictions EUTE 25C (EUTE W5) | Pass predictions EUTE 25C (EUTE W5) |
| Orbit launches |
2002-11-20 (23 years ago)
|
| Days in orbit | 8689 |
| Country/organisation of origin | European Telecommunications Satellite Organization (EUTELSAT) (EUTE) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35730 km |
| Apogee | 35844 km |
| Orbit slope (inclination) | 9.16° |
| Laps per day | 1 |
| Height EUTE 25C (EUTE W5) | 35785.3 km |
Additional information EUTE 25C (EUTE W5)
EUTE 25C (EUTE W5), 27554 is a payload satellite owned by EutelsatSA (FR) in GEO that was launched on Wed, 20 Nov 2002 UTC via a DELTA 4M+(4,2) 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 25C (EUTE W5) Date of exalting 20.11.2002y. Average height of ISS EUTE 25C (EUTE W5) hundred 35785.3 km. Average velocity EUTE 25C (EUTE W5) is 11069.11 km/h. Inclination EUTE 25C (EUTE W5) satellite 9.13°.TLE
Average velocity EUTE 25C (EUTE W5)
Average inclination EUTE 25C (EUTE W5)
Mean right ascension of the ascending node (RAAN) EUTE 25C (EUTE W5)
Mean argument of perigee EUTE 25C (EUTE W5)
Mean semi-major axis of the orbit EUTE 25C (EUTE W5)
Mean orbital eccentricity EUTE 25C (EUTE W5)
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