ATLAS CENTAUR R/B
Satellite information ATLAS CENTAUR R/B
| Spacetrack Directory Name | ATLAS CENTAUR R/B |
| Follow ATLAS CENTAUR R/B | ATLAS CENTAUR R/B Tracker |
| Pass predictions ATLAS CENTAUR R/B | Pass predictions ATLAS CENTAUR R/B |
| Orbit launches |
1978-03-31 (48 years ago)
|
| Days in orbit | 17694 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 605 km |
| Apogee | 36185 km |
| Orbit slope (inclination) | 22.13° |
| Laps per day | 2 |
| Height ATLAS CENTAUR R/B | 24813 km |
Additional information ATLAS CENTAUR R/B
ATLAS CENTAUR R/B, 10779 is space debris in HEO originally from a launch on Fri, 31 Mar 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 R/B Date of exalting 31.03.1978y. Average height of ISS ATLAS CENTAUR R/B hundred 24813 km. Average velocity ATLAS CENTAUR R/B is 12319.21 km/h. Inclination ATLAS CENTAUR R/B satellite 22.14°.TLE
Average velocity ATLAS CENTAUR R/B
Average inclination ATLAS CENTAUR R/B
Mean right ascension of the ascending node (RAAN) ATLAS CENTAUR R/B
Mean argument of perigee ATLAS CENTAUR R/B
Mean semi-major axis of the orbit ATLAS CENTAUR R/B
Mean orbital eccentricity ATLAS CENTAUR R/B
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