OBJECT B
Satellite information OBJECT B
| Spacetrack Directory Name | OBJECT B |
| Orbit launches |
2022-03-01 |
| Deorbitation |
|
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 8902 km |
| Apogee | 35274 km |
| Height OBJECT B | 24097.65 km |
Additional information OBJECT B
ATLAS 5 CENTAUR R/B, 51851 is space debris in HEO originally from a launch on Tue, 01 Mar 2022 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 OBJECT B Date of exalting 01.03.2022y. Average height of ISS OBJECT B hundred 24097.65 km. Average velocity OBJECT B is 13105.79 km/h. Inclination OBJECT B satellite 7.34°.Average velocity OBJECT B
Average inclination OBJECT B
Mean right ascension of the ascending node (RAAN) OBJECT B
Mean argument of perigee OBJECT B
Mean semi-major axis of the orbit OBJECT B
Mean orbital eccentricity OBJECT B
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