EUTE 25A (HB 5)
Satellite information EUTE 25A (HB 5) - HOT BIRD 5, EUROBIRD 2
| Spacetrack Directory Name | EUTE 25A (HB 5) |
| Alternative name | HOT BIRD 5, EUROBIRD 2 |
| Follow EUTE 25A (HB 5) | EUTE 25A (HB 5) Tracker |
| Pass predictions EUTE 25A (HB 5) | Pass predictions EUTE 25A (HB 5) |
| Orbit launches |
1998-10-09 (27 years ago)
|
| Days in orbit | 10195 |
| Country/organisation of origin | European Telecommunications Satellite Organization (EUTELSAT) (EUTE) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36255 km |
| Apogee | 36352 km |
| Orbit slope (inclination) | 10.7° |
| Laps per day | 1 |
| Height EUTE 25A (HB 5) | 36303.57 km |
Additional information EUTE 25A (HB 5)
EUTE 25A (HB 5), 25495 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Fri, 09 Oct 1998 UTC via an ATLAS IIA 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 25A (HB 5) Date of exalting 09.10.1998y. Average height of ISS EUTE 25A (HB 5) hundred 36303.57 km. Average velocity EUTE 25A (HB 5) is 11001.7 km/h. Inclination EUTE 25A (HB 5) satellite 10.67°.TLE
Average velocity EUTE 25A (HB 5)
Average inclination EUTE 25A (HB 5)
Mean right ascension of the ascending node (RAAN) EUTE 25A (HB 5)
Mean argument of perigee EUTE 25A (HB 5)
Mean semi-major axis of the orbit EUTE 25A (HB 5)
Mean orbital eccentricity EUTE 25A (HB 5)
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