ATLAS CENTAUR DEB
Satellite information ATLAS CENTAUR DEB
| Spacetrack Directory Name | ATLAS CENTAUR DEB |
| Follow ATLAS CENTAUR DEB | ATLAS CENTAUR DEB Tracker |
| Pass predictions ATLAS CENTAUR DEB | Pass predictions ATLAS CENTAUR DEB |
| Orbit launches |
1978-06-29 (48 years ago)
|
| Days in orbit | 17634 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 855 km |
| Apogee | 35591 km |
| Orbit slope (inclination) | 22.1° |
| Laps per day | 2 |
| Height ATLAS CENTAUR DEB | 24338.92 km |
Additional information ATLAS CENTAUR DEB
ATLAS CENTAUR DEB, 25253 is space debris in HEO originally from a launch on Thu, 29 Jun 1978 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 ATLAS CENTAUR DEB Date of exalting 29.06.1978y. Average height of ISS ATLAS CENTAUR DEB hundred 24338.92 km. Average velocity ATLAS CENTAUR DEB is 12478.78 km/h. Inclination ATLAS CENTAUR DEB satellite 22.07°.TLE
Average velocity ATLAS CENTAUR DEB
Average inclination ATLAS CENTAUR DEB
Mean right ascension of the ascending node (RAAN) ATLAS CENTAUR DEB
Mean argument of perigee ATLAS CENTAUR DEB
Mean semi-major axis of the orbit ATLAS CENTAUR DEB
Mean orbital eccentricity ATLAS CENTAUR DEB
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