EUTE 21A (EUTE W3)
Satellite information EUTE 21A (EUTE W3)
| Spacetrack Directory Name | EUTE 21A (EUTE W3) |
| Alternative name | EUTELSAT W3, EUTELSAT W6 |
| Follow EUTE 21A (EUTE W3) | EUTE 21A (EUTE W3) Tracker |
| Pass predictions EUTE 21A (EUTE W3) | Pass predictions EUTE 21A (EUTE W3) |
| Orbit launches |
1999-04-12 (27 years ago)
|
| Days in orbit | 10010 |
| Country/organisation of origin | European Telecommunications Satellite Organization (EUTELSAT) (EUTE) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36297 km |
| Apogee | 36325 km |
| Orbit slope (inclination) | 10.73° |
| Laps per day | 1 |
| Height EUTE 21A (EUTE W3) | 36311.23 km |
Additional information EUTE 21A (EUTE W3)
EUTE 21A (EUTE W3), 25673 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Mon, 12 Apr 1999 UTC via an ATLAS IIAS 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 21A (EUTE W3) Date of exalting 12.04.1999y. Average height of ISS EUTE 21A (EUTE W3) hundred 36311.23 km. Average velocity EUTE 21A (EUTE W3) is 11000.67 km/h. Inclination EUTE 21A (EUTE W3) satellite 10.7°.TLE
Average velocity EUTE 21A (EUTE W3)
Average inclination EUTE 21A (EUTE W3)
Mean right ascension of the ascending node (RAAN) EUTE 21A (EUTE W3)
Mean argument of perigee EUTE 21A (EUTE W3)
Mean semi-major axis of the orbit EUTE 21A (EUTE W3)
Mean orbital eccentricity EUTE 21A (EUTE W3)
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