TAURUS R/B
Satellite information TAURUS R/B
| Spacetrack Directory Name | TAURUS R/B |
| Follow TAURUS R/B | TAURUS R/B Tracker |
| Pass predictions TAURUS R/B | Pass predictions TAURUS R/B |
| Orbit launches |
2000-03-12 (26 years ago)
|
| Days in orbit | 9662 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 510 km |
| Apogee | 551 km |
| Orbit slope (inclination) | 97.42° |
| Laps per day | 15 |
| Height TAURUS R/B | 450.25 km |
Additional information TAURUS R/B
TAURUS R/B, 26103 is space debris in SSO originally from a launch on Sun, 12 Mar 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 TAURUS R/B Date of exalting 12.03.2000y. Average height of ISS TAURUS R/B hundred 450.25 km. Average velocity TAURUS R/B is 27516.91 km/h. Inclination TAURUS R/B satellite 97.42°.TLE
Average velocity TAURUS R/B
Average inclination TAURUS R/B
Mean right ascension of the ascending node (RAAN) TAURUS R/B
Mean argument of perigee TAURUS R/B
Mean semi-major axis of the orbit TAURUS R/B
Mean orbital eccentricity TAURUS R/B
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