ATLAS 5 CENTAUR R/B
Satellite information ATLAS 5 CENTAUR R/B
| Spacetrack Directory Name | ATLAS 5 CENTAUR R/B |
| Follow ATLAS 5 CENTAUR R/B | ATLAS 5 CENTAUR R/B Tracker |
| Pass predictions ATLAS 5 CENTAUR R/B | Pass predictions ATLAS 5 CENTAUR R/B |
| Orbit launches |
2015-10-31 (10 years ago)
|
| Days in orbit | 3951 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 20596 km |
| Apogee | 21641 km |
| Orbit slope (inclination) | 57.36° |
| Laps per day | 2 |
| Height ATLAS 5 CENTAUR R/B | 21126.52 km |
Additional information ATLAS 5 CENTAUR R/B
ATLAS 5 CENTAUR R/B, 41020 is space debris in MEO originally from a launch on Sat, 31 Oct 2015 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 5 CENTAUR R/B Date of exalting 31.10.2015y. Average height of ISS ATLAS 5 CENTAUR R/B hundred 21126.52 km. Average velocity ATLAS 5 CENTAUR R/B is 13707.37 km/h. Inclination ATLAS 5 CENTAUR R/B satellite 57.35°.TLE
Average velocity ATLAS 5 CENTAUR R/B
Average inclination ATLAS 5 CENTAUR R/B
Mean right ascension of the ascending node (RAAN) ATLAS 5 CENTAUR R/B
Mean argument of perigee ATLAS 5 CENTAUR R/B
Mean semi-major axis of the orbit ATLAS 5 CENTAUR R/B
Mean orbital eccentricity ATLAS 5 CENTAUR R/B
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