INTELSAT 804
Satellite information INTELSAT 804 - INTELSAT 804 (IS-804)
| Spacetrack Directory Name | INTELSAT 804 |
| Alternative name | INTELSAT 804 (IS-804) |
| Follow INTELSAT 804 | INTELSAT 804 Tracker |
| Pass predictions INTELSAT 804 | Pass predictions INTELSAT 804 |
| Orbit launches |
1997-12-21 (28 years ago)
|
| Days in orbit | 10492 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 35766 km |
| Apogee | 35820 km |
| Orbit slope (inclination) | 13.24° |
| Laps per day | 1 |
| Height INTELSAT 804 | 35786.96 km |
Additional information INTELSAT 804
INTELSAT 804, 25110 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Sun, 21 Dec 1997 UTC via an ARIANE 42L 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 INTELSAT 804 Date of exalting 21.12.1997y. Average height of ISS INTELSAT 804 hundred 35786.96 km. Average velocity INTELSAT 804 is 11068.93 km/h. Inclination INTELSAT 804 satellite 13.22°.TLE
Average velocity INTELSAT 804
Average inclination INTELSAT 804
Mean right ascension of the ascending node (RAAN) INTELSAT 804
Mean argument of perigee INTELSAT 804
Mean semi-major axis of the orbit INTELSAT 804
Mean orbital eccentricity INTELSAT 804
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