ATLAS CENTAUR 2 DEB
Satellite information ATLAS CENTAUR 2 DEB
| Spacetrack Directory Name | ATLAS CENTAUR 2 DEB |
| Follow ATLAS CENTAUR 2 DEB | ATLAS CENTAUR 2 DEB Tracker |
| Pass predictions ATLAS CENTAUR 2 DEB | Pass predictions ATLAS CENTAUR 2 DEB |
| Orbit launches |
1963-11-27 (62 years ago)
|
| Days in orbit | 22934 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 597 km |
| Apogee | 1407 km |
| Orbit slope (inclination) | 29.92° |
| Laps per day | 14 |
| Height ATLAS CENTAUR 2 DEB | 994.5 km |
Additional information ATLAS CENTAUR 2 DEB
ATLAS CENTAUR 2 DEB, 698 is space debris in LEO originally from a launch on Wed, 27 Nov 1963 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 2 DEB Date of exalting 27.11.1963y. Average height of ISS ATLAS CENTAUR 2 DEB hundred 994.5 km. Average velocity ATLAS CENTAUR 2 DEB is 26485.88 km/h. Inclination ATLAS CENTAUR 2 DEB satellite 29.92°.TLE
Average velocity ATLAS CENTAUR 2 DEB
Average inclination ATLAS CENTAUR 2 DEB
Mean right ascension of the ascending node (RAAN) ATLAS CENTAUR 2 DEB
Mean argument of perigee ATLAS CENTAUR 2 DEB
Mean semi-major axis of the orbit ATLAS CENTAUR 2 DEB
Mean orbital eccentricity ATLAS CENTAUR 2 DEB
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