PEGASUS R/B(2)
Satellite information PEGASUS R/B(2)
| Spacetrack Directory Name | PEGASUS R/B(2) |
| Follow PEGASUS R/B(2) | PEGASUS R/B(2) Tracker |
| Pass predictions PEGASUS R/B(2) | Pass predictions PEGASUS R/B(2) |
| Orbit launches |
1998-09-23 (27 years ago)
|
| Days in orbit | 10216 |
| Country/organisation of origin | USA (US) |
| Starting point | ERAS (Wallops Flight Facility, USA) |
| Perigee | 706 km |
| Apogee | 799 km |
| Orbit slope (inclination) | 44.53° |
| Laps per day | 14 |
| Height PEGASUS R/B(2) | 751.41 km |
Additional information PEGASUS R/B(2)
PEGASUS R/B(2), 25484 is space debris in LEO originally from a launch on Wed, 23 Sep 1998 UTC launched from the Pegasus Launch, Eastern Range Air Space (ERAS). 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(2) Date of exalting 23.09.1998y. Average height of ISS PEGASUS R/B(2) hundred 751.41 km. Average velocity PEGASUS R/B(2) is 26932.4 km/h. Inclination PEGASUS R/B(2) satellite 44.53°.TLE
Average velocity PEGASUS R/B(2)
Average inclination PEGASUS R/B(2)
Mean right ascension of the ascending node (RAAN) PEGASUS R/B(2)
Mean argument of perigee PEGASUS R/B(2)
Mean semi-major axis of the orbit PEGASUS R/B(2)
Mean orbital eccentricity PEGASUS R/B(2)
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