TITAN 4 CENTAUR R/B
Satellite information TITAN 4 CENTAUR R/B
| Spacetrack Directory Name | TITAN 4 CENTAUR R/B |
| Follow TITAN 4 CENTAUR R/B | TITAN 4 CENTAUR R/B Tracker |
| Pass predictions TITAN 4 CENTAUR R/B | Pass predictions TITAN 4 CENTAUR R/B |
| Orbit launches |
1995-05-14 (31 years ago)
|
| Days in orbit | 11439 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35663 km |
| Apogee | 35758 km |
| Orbit slope (inclination) | 18.34° |
| Laps per day | 1 |
| Height TITAN 4 CENTAUR R/B | 35709.68 km |
Additional information TITAN 4 CENTAUR R/B
TITAN 4 CENTAUR R/B, 23568 is space debris in GEO originally from a launch on Sun, 14 May 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 TITAN 4 CENTAUR R/B Date of exalting 14.05.1995y. Average height of ISS TITAN 4 CENTAUR R/B hundred 35709.68 km. Average velocity TITAN 4 CENTAUR R/B is 11079.15 km/h. Inclination TITAN 4 CENTAUR R/B satellite 18.33°.TLE
Average velocity TITAN 4 CENTAUR R/B
Average inclination TITAN 4 CENTAUR R/B
Mean right ascension of the ascending node (RAAN) TITAN 4 CENTAUR R/B
Mean argument of perigee TITAN 4 CENTAUR R/B
Mean semi-major axis of the orbit TITAN 4 CENTAUR R/B
Mean orbital eccentricity TITAN 4 CENTAUR R/B
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