INTELSAT 802
Satellite information INTELSAT 802 - INTELSAT 802 (IS-802)
| Spacetrack Directory Name | INTELSAT 802 |
| Alternative name | INTELSAT 802 (IS-802) |
| Follow INTELSAT 802 | INTELSAT 802 Tracker |
| Pass predictions INTELSAT 802 | Pass predictions INTELSAT 802 |
| Orbit launches |
1997-06-25 (29 years ago)
|
| Days in orbit | 10672 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36289 km |
| Apogee | 36520 km |
| Orbit slope (inclination) | 11.57° |
| Laps per day | 1 |
| Height INTELSAT 802 | 36404.45 km |
Additional information INTELSAT 802
INTELSAT 802, 24846 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Wed, 25 Jun 1997 UTC via an ARIANE 44P 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 802 Date of exalting 25.06.1997y. Average height of ISS INTELSAT 802 hundred 36404.45 km. Average velocity INTELSAT 802 is 10988.67 km/h. Inclination INTELSAT 802 satellite 11.54°.TLE
Average velocity INTELSAT 802
Average inclination INTELSAT 802
Mean right ascension of the ascending node (RAAN) INTELSAT 802
Mean argument of perigee INTELSAT 802
Mean semi-major axis of the orbit INTELSAT 802
Mean orbital eccentricity INTELSAT 802
ISS
Buy us a coffee!
