INTELSAT 805 DEB
Satellite information INTELSAT 805 DEB
| Spacetrack Directory Name | INTELSAT 805 DEB |
| Follow INTELSAT 805 DEB | INTELSAT 805 DEB Tracker |
| Pass predictions INTELSAT 805 DEB | Pass predictions INTELSAT 805 DEB |
| Orbit launches |
1998-06-18 (28 years ago)
|
| Days in orbit | 10313 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36072 km |
| Apogee | 36187 km |
| Orbit slope (inclination) | 7.94° |
| Laps per day | 1 |
| Height INTELSAT 805 DEB | 36128.11 km |
Additional information INTELSAT 805 DEB
INTELSAT 805 DEB, 100397 is space debris in GEO originally from a launch on Thu, 18 Jun 1998 UTC launched from the Air Force Eastern Test Range (AFETR). 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 805 DEB Date of exalting 18.06.1998y. Average height of ISS INTELSAT 805 DEB hundred 36128.11 km. Average velocity INTELSAT 805 DEB is 11024.37 km/h. Inclination INTELSAT 805 DEB satellite 7.92°.TLE
Average velocity INTELSAT 805 DEB
Average inclination INTELSAT 805 DEB
Mean right ascension of the ascending node (RAAN) INTELSAT 805 DEB
Mean argument of perigee INTELSAT 805 DEB
Mean semi-major axis of the orbit INTELSAT 805 DEB
Mean orbital eccentricity INTELSAT 805 DEB
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