ATLAS 3B CENTAUR R/B
Satellite information ATLAS 3B CENTAUR R/B
| Spacetrack Directory Name | ATLAS 3B CENTAUR R/B |
| Follow ATLAS 3B CENTAUR R/B | ATLAS 3B CENTAUR R/B Tracker |
| Pass predictions ATLAS 3B CENTAUR R/B | Pass predictions ATLAS 3B CENTAUR R/B |
| Orbit launches |
2005-02-03 (21 years ago)
|
| Days in orbit | 7882 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 1019 km |
| Apogee | 1176 km |
| Orbit slope (inclination) | 63.82° |
| Laps per day | 13 |
| Height ATLAS 3B CENTAUR R/B | 1107.5 km |
Additional information ATLAS 3B CENTAUR R/B
ATLAS 3B CENTAUR R/B, 28538 is space debris in LEO originally from a launch on Thu, 03 Feb 2005 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 3B CENTAUR R/B Date of exalting 03.02.2005y. Average height of ISS ATLAS 3B CENTAUR R/B hundred 1107.5 km. Average velocity ATLAS 3B CENTAUR R/B is 26281.69 km/h. Inclination ATLAS 3B CENTAUR R/B satellite 63.82°.TLE
Average velocity ATLAS 3B CENTAUR R/B
Average inclination ATLAS 3B CENTAUR R/B
Mean right ascension of the ascending node (RAAN) ATLAS 3B CENTAUR R/B
Mean argument of perigee ATLAS 3B CENTAUR R/B
Mean semi-major axis of the orbit ATLAS 3B CENTAUR R/B
Mean orbital eccentricity ATLAS 3B CENTAUR R/B
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