INTELSAT 33E DEB
Satellite information INTELSAT 33E DEB - 0 INTELSAT 33E DEB
| Spacetrack Directory Name | INTELSAT 33E DEB |
| Alternative name | 0 INTELSAT 33E DEB |
| Follow INTELSAT 33E DEB | INTELSAT 33E DEB Tracker |
| Pass predictions INTELSAT 33E DEB | Pass predictions INTELSAT 33E DEB |
| Orbit launches |
2016-08-24 (10 years ago)
|
| Days in orbit | 3652 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 34818 km |
| Apogee | 36134 km |
| Orbit slope (inclination) | 1.61° |
| Laps per day | 1 |
| Height INTELSAT 33E DEB | 35476.99 km |
Additional information INTELSAT 33E DEB
INTELSAT 33E DEB, 61990 is space debris in GEO originally from a launch on Wed, 24 Aug 2016 UTC launched from the French Guiana (FRGUI). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite INTELSAT 33E DEB Date of exalting 24.08.2016y. Average height of ISS INTELSAT 33E DEB hundred 35476.99 km. Average velocity INTELSAT 33E DEB is 11110.07 km/h. Inclination INTELSAT 33E DEB satellite 1.6°.TLE
Average velocity INTELSAT 33E DEB
Average inclination INTELSAT 33E DEB
Mean right ascension of the ascending node (RAAN) INTELSAT 33E DEB
Mean argument of perigee INTELSAT 33E DEB
Mean semi-major axis of the orbit INTELSAT 33E DEB
Mean orbital eccentricity INTELSAT 33E DEB
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