PEGASUS R/B
Satellite information PEGASUS R/B
| Spacetrack Directory Name | PEGASUS R/B |
| Follow PEGASUS R/B | PEGASUS R/B Tracker |
| Pass predictions PEGASUS R/B | Pass predictions PEGASUS R/B |
| Orbit launches |
1993-04-25 (33 years ago)
|
| Days in orbit | 12177 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 741 km |
| Apogee | 831 km |
| Orbit slope (inclination) | 69.92° |
| Laps per day | 14 |
| Height PEGASUS R/B | 792.34 km |
Additional information PEGASUS R/B
PEGASUS R/B, 22639 is space debris in LEO originally from a launch on Sun, 25 Apr 1993 UTC via a PEGASUS launch vehicle 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 PEGASUS R/B Date of exalting 25.04.1993y. Average height of ISS PEGASUS R/B hundred 792.34 km. Average velocity PEGASUS R/B is 26853 km/h. Inclination PEGASUS R/B satellite 69.92°.TLE
Average velocity PEGASUS R/B
Average inclination PEGASUS R/B
Mean right ascension of the ascending node (RAAN) PEGASUS R/B
Mean argument of perigee PEGASUS R/B
Mean semi-major axis of the orbit PEGASUS R/B
Mean orbital eccentricity PEGASUS R/B
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