MINOTAUR DEB
Satellite information MINOTAUR DEB
| Spacetrack Directory Name | MINOTAUR DEB |
| Follow MINOTAUR DEB | MINOTAUR DEB Tracker |
| Pass predictions MINOTAUR DEB | Pass predictions MINOTAUR DEB |
| Orbit launches |
2000-01-27 (26 years ago)
|
| Days in orbit | 9756 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 721 km |
| Apogee | 770 km |
| Orbit slope (inclination) | 100.2° |
| Laps per day | 15 |
| Height MINOTAUR DEB | 738.46 km |
Additional information MINOTAUR DEB
MINOTAUR DEB, 26079 is space debris in SSO originally from a launch on Thu, 27 Jan 2000 UTC launched from the Air Force Western Test Range (AFWTR). 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 MINOTAUR DEB Date of exalting 27.01.2000y. Average height of ISS MINOTAUR DEB hundred 738.46 km. Average velocity MINOTAUR DEB is 26954 km/h. Inclination MINOTAUR DEB satellite 100.2°.TLE
Average velocity MINOTAUR DEB
Average inclination MINOTAUR DEB
Mean right ascension of the ascending node (RAAN) MINOTAUR DEB
Mean argument of perigee MINOTAUR DEB
Mean semi-major axis of the orbit MINOTAUR DEB
Mean orbital eccentricity MINOTAUR DEB
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