ATLAS 2 CENTAUR R/B
Satellite information ATLAS 2 CENTAUR R/B
| Spacetrack Directory Name | ATLAS 2 CENTAUR R/B |
| Follow ATLAS 2 CENTAUR R/B | ATLAS 2 CENTAUR R/B Tracker |
| Pass predictions ATLAS 2 CENTAUR R/B | Pass predictions ATLAS 2 CENTAUR R/B |
| Orbit launches |
1995-01-29 (31 years ago)
|
| Days in orbit | 11544 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 291 km |
| Apogee | 20421 km |
| Orbit slope (inclination) | 26.6° |
| Laps per day | 5 |
| Height ATLAS 2 CENTAUR R/B | 11584.45 km |
Additional information ATLAS 2 CENTAUR R/B
ATLAS 2 CENTAUR R/B, 23468 is space debris in HEO originally from a launch on Sun, 29 Jan 1995 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 2 CENTAUR R/B Date of exalting 29.01.1995y. Average height of ISS ATLAS 2 CENTAUR R/B hundred 11584.45 km. Average velocity ATLAS 2 CENTAUR R/B is 16685.33 km/h. Inclination ATLAS 2 CENTAUR R/B satellite 26.61°.TLE
Average velocity ATLAS 2 CENTAUR R/B
Average inclination ATLAS 2 CENTAUR R/B
Mean right ascension of the ascending node (RAAN) ATLAS 2 CENTAUR R/B
Mean argument of perigee ATLAS 2 CENTAUR R/B
Mean semi-major axis of the orbit ATLAS 2 CENTAUR R/B
Mean orbital eccentricity ATLAS 2 CENTAUR R/B
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