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 |
2003-04-28 (23 years ago)
|
| Days in orbit | 8529 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 683 km |
| Apogee | 690 km |
| Orbit slope (inclination) | 29° |
| Laps per day | 15 |
| Height PEGASUS R/B | 677.39 km |
Additional information PEGASUS R/B
PEGASUS R/B, 27784 is space debris in LEO originally from a launch on Mon, 28 Apr 2003 UTC launched from the Air Force Eastern Test Range (AFETR). 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 28.04.2003y. Average height of ISS PEGASUS R/B hundred 677.39 km. Average velocity PEGASUS R/B is 27075.13 km/h. Inclination PEGASUS R/B satellite 29°.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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