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 |
2015-10-08 (10 years ago)
|
| Days in orbit | 3972 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 504 km |
| Apogee | 747 km |
| Orbit slope (inclination) | 64.77° |
| Laps per day | 15 |
| Height ATLAS 5 CENTAUR R/B | 558.67 km |
Additional information ATLAS 5 CENTAUR R/B
ATLAS 5 CENTAUR R/B, 40978 is space debris in LEO originally from an American launch on Thu, 08 Oct 2015 UTC via an ATLAS V 401 launch vehicle from the Air Force Western Test Range (AFWTR). 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 08.10.2015y. Average height of ISS ATLAS 5 CENTAUR R/B hundred 558.67 km. Average velocity ATLAS 5 CENTAUR R/B is 27302.33 km/h. Inclination ATLAS 5 CENTAUR R/B satellite 64.77°.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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