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 |
1999-04-30 (27 years ago)
|
| Days in orbit | 9992 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 708 km |
| Apogee | 5146 km |
| Orbit slope (inclination) | 28.31° |
| Laps per day | 10 |
| Height TITAN 4B CENTAUR R/B | 3188.38 km |
Additional information TITAN 4B CENTAUR R/B
TITAN 4B CENTAUR R/B, 25725 is space debris in LEO originally from a launch on Fri, 30 Apr 1999 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 30.04.1999y. Average height of ISS TITAN 4B CENTAUR R/B hundred 3188.38 km. Average velocity TITAN 4B CENTAUR R/B is 23238.77 km/h. Inclination TITAN 4B CENTAUR R/B satellite 28.32°.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!
