ATLAS CENTAUR 2 R/B
Satellite information ATLAS CENTAUR 2 R/B - ATLAS CENTAUR 2
| Spacetrack Directory Name | ATLAS CENTAUR 2 R/B |
| Alternative name | ATLAS CENTAUR 2 |
| Follow ATLAS CENTAUR 2 R/B | ATLAS CENTAUR 2 R/B Tracker |
| Pass predictions ATLAS CENTAUR 2 R/B | Pass predictions ATLAS CENTAUR 2 R/B |
| Orbit launches |
1963-11-27 (62 years ago)
|
| Days in orbit | 22934 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 459 km |
| Apogee | 1309 km |
| Orbit slope (inclination) | 30.36° |
| Laps per day | 14 |
| Height ATLAS CENTAUR 2 R/B | 862.2 km |
Additional information ATLAS CENTAUR 2 R/B
ATLAS CENTAUR 2 R/B, 694 is space debris in LEO originally from a launch on Wed, 27 Nov 1963 UTC via an ATLAS CENTAUR launch vehicle 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 CENTAUR 2 R/B Date of exalting 27.11.1963y. Average height of ISS ATLAS CENTAUR 2 R/B hundred 862.2 km. Average velocity ATLAS CENTAUR 2 R/B is 26726.21 km/h. Inclination ATLAS CENTAUR 2 R/B satellite 30.35°.TLE
Average velocity ATLAS CENTAUR 2 R/B
Average inclination ATLAS CENTAUR 2 R/B
Mean right ascension of the ascending node (RAAN) ATLAS CENTAUR 2 R/B
Mean argument of perigee ATLAS CENTAUR 2 R/B
Mean semi-major axis of the orbit ATLAS CENTAUR 2 R/B
Mean orbital eccentricity ATLAS CENTAUR 2 R/B
ISS
Buy us a coffee!
