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 |
2004-05-20 (22 years ago)
|
| Days in orbit | 8130 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 714 km |
| Apogee | 735 km |
| Orbit slope (inclination) | 99.08° |
| Laps per day | 15 |
| Height TAURUS R/B | 730.6 km |
Additional information TAURUS R/B
TAURUS R/B, 28255 is space debris in SSO originally from a launch on Thu, 20 May 2004 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 20.05.2004y. Average height of ISS TAURUS R/B hundred 730.6 km. Average velocity TAURUS R/B is 26968.82 km/h. Inclination TAURUS R/B satellite 99.08°.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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