TITAN 4B CENTAUR R/B
Satellite information TITAN 4B CENTAUR R/B
| Spacetrack Directory Name | TITAN 4B CENTAUR R/B |
| Follow TITAN 4B CENTAUR R/B | TITAN 4B CENTAUR R/B Tracker |
| Pass predictions TITAN 4B CENTAUR R/B | Pass predictions TITAN 4B CENTAUR R/B |
| Orbit launches |
2003-09-09 (22 years ago)
|
| Days in orbit | 8395 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35480 km |
| Apogee | 35772 km |
| Orbit slope (inclination) | 15.78° |
| Laps per day | 1 |
| Height TITAN 4B CENTAUR R/B | 35626.44 km |
Additional information TITAN 4B CENTAUR R/B
TITAN 4B CENTAUR R/B, 27938 is space debris in GEO originally from a launch on Tue, 09 Sep 2003 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 4B CENTAUR R/B Date of exalting 09.09.2003y. Average height of ISS TITAN 4B CENTAUR R/B hundred 35626.44 km. Average velocity TITAN 4B CENTAUR R/B is 11089.96 km/h. Inclination TITAN 4B CENTAUR R/B satellite 15.76°.TLE
Average velocity TITAN 4B CENTAUR R/B
Average inclination TITAN 4B CENTAUR R/B
Mean right ascension of the ascending node (RAAN) TITAN 4B CENTAUR R/B
Mean argument of perigee TITAN 4B CENTAUR R/B
Mean semi-major axis of the orbit TITAN 4B CENTAUR R/B
Mean orbital eccentricity TITAN 4B CENTAUR R/B
ISS
Buy us a coffee!
