OPS 4682 DEB
Satellite information OPS 4682 DEB - Satelita
| Spacetrack Directory Name | OPS 4682 DEB |
| Alternative name | Satelita |
| Follow OPS 4682 DEB | OPS 4682 DEB Tracker |
| Pass predictions OPS 4682 DEB | Pass predictions OPS 4682 DEB |
| Country/organisation of origin | USA (US) |
| Starting point | |
| Perigee | 1252 km |
| Apogee | 1289 km |
| Orbit slope (inclination) | 90.25° |
| Laps per day | 13 |
| Height OPS 4682 DEB | 1282.74 km |
Additional information OPS 4682 DEB
OPS 4682 DEB, 51498 is space debris in LEO originally from an American launch on Sat, 03 Apr 1965 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.
Average height of ISS OPS 4682 DEB hundred 1282.74 km. Average velocity OPS 4682 DEB is 25978.43 km/h. Inclination OPS 4682 DEB satellite 90.25°.TLE
Average velocity OPS 4682 DEB
Average inclination OPS 4682 DEB
Mean right ascension of the ascending node (RAAN) OPS 4682 DEB
Mean argument of perigee OPS 4682 DEB
Mean semi-major axis of the orbit OPS 4682 DEB
Mean orbital eccentricity OPS 4682 DEB
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