ATLAS 2A CENTAUR R/B
Satellite information ATLAS 2A CENTAUR R/B
| Spacetrack Directory Name | ATLAS 2A CENTAUR R/B |
| Follow ATLAS 2A CENTAUR R/B | ATLAS 2A CENTAUR R/B Tracker |
| Pass predictions ATLAS 2A CENTAUR R/B | Pass predictions ATLAS 2A CENTAUR R/B |
| Orbit launches |
2000-01-21 (26 years ago)
|
| Days in orbit | 9724 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 241 km |
| Apogee | 21017 km |
| Orbit slope (inclination) | 26.02° |
| Laps per day | 4 |
| Height ATLAS 2A CENTAUR R/B | 11753.54 km |
Additional information ATLAS 2A CENTAUR R/B
ATLAS 2A CENTAUR R/B, 26053 is space debris in HEO originally from a launch on Fri, 21 Jan 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 2A CENTAUR R/B Date of exalting 21.01.2000y. Average height of ISS ATLAS 2A CENTAUR R/B hundred 11753.54 km. Average velocity ATLAS 2A CENTAUR R/B is 16609.72 km/h. Inclination ATLAS 2A CENTAUR R/B satellite 26°.TLE
Average velocity ATLAS 2A CENTAUR R/B
Average inclination ATLAS 2A CENTAUR R/B
Mean right ascension of the ascending node (RAAN) ATLAS 2A CENTAUR R/B
Mean argument of perigee ATLAS 2A CENTAUR R/B
Mean semi-major axis of the orbit ATLAS 2A CENTAUR R/B
Mean orbital eccentricity ATLAS 2A CENTAUR R/B
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