ATLAS 2AS CENTAUR R/B
Satellite information ATLAS 2AS CENTAUR R/B
| Spacetrack Directory Name | ATLAS 2AS CENTAUR R/B |
| Follow ATLAS 2AS CENTAUR R/B | ATLAS 2AS CENTAUR R/B Tracker |
| Pass predictions ATLAS 2AS CENTAUR R/B | Pass predictions ATLAS 2AS CENTAUR R/B |
| Orbit launches |
2000-02-03 (26 years ago)
|
| Days in orbit | 9710 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 254 km |
| Apogee | 9087 km |
| Orbit slope (inclination) | 18.09° |
| Laps per day | 9 |
| Height ATLAS 2AS CENTAUR R/B | 3587.88 km |
Additional information ATLAS 2AS CENTAUR R/B
ATLAS 2AS CENTAUR R/B, 26072 is space debris originally from a launch on Thu, 03 Feb 2000 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 2AS CENTAUR R/B Date of exalting 03.02.2000y. Average height of ISS ATLAS 2AS CENTAUR R/B hundred 3587.88 km. Average velocity ATLAS 2AS CENTAUR R/B is 22747.9 km/h. Inclination ATLAS 2AS CENTAUR R/B satellite 18.1°.TLE
Average velocity ATLAS 2AS CENTAUR R/B
Average inclination ATLAS 2AS CENTAUR R/B
Mean right ascension of the ascending node (RAAN) ATLAS 2AS CENTAUR R/B
Mean argument of perigee ATLAS 2AS CENTAUR R/B
Mean semi-major axis of the orbit ATLAS 2AS CENTAUR R/B
Mean orbital eccentricity ATLAS 2AS CENTAUR R/B
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