MINOTAUR R/B
Satellite information MINOTAUR R/B
| Spacetrack Directory Name | MINOTAUR R/B |
| Follow MINOTAUR R/B | MINOTAUR R/B Tracker |
| Pass predictions MINOTAUR R/B | Pass predictions MINOTAUR R/B |
| Orbit launches |
2000-01-27 (26 years ago)
|
| Days in orbit | 9707 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 743 km |
| Apogee | 789 km |
| Orbit slope (inclination) | 100.21° |
| Laps per day | 14 |
| Height MINOTAUR R/B | 773.52 km |
Additional information MINOTAUR R/B
MINOTAUR R/B, 26066 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 R/B Date of exalting 27.01.2000y. Average height of ISS MINOTAUR R/B hundred 773.52 km. Average velocity MINOTAUR R/B is 26887.79 km/h. Inclination MINOTAUR R/B satellite 100.21°.TLE
Average velocity MINOTAUR R/B
Average inclination MINOTAUR R/B
Mean right ascension of the ascending node (RAAN) MINOTAUR R/B
Mean argument of perigee MINOTAUR R/B
Mean semi-major axis of the orbit MINOTAUR R/B
Mean orbital eccentricity MINOTAUR R/B
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