OPS 5798 DEB
Satellite information OPS 5798 DEB
| Spacetrack Directory Name | OPS 5798 DEB |
| Follow OPS 5798 DEB | OPS 5798 DEB Tracker |
| Pass predictions OPS 5798 DEB | Pass predictions OPS 5798 DEB |
| Orbit launches |
1964-10-06 (61 years ago)
|
| Days in orbit | 22613 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 957 km |
| Apogee | 993 km |
| Orbit slope (inclination) | 90.22° |
| Laps per day | 14 |
| Height OPS 5798 DEB | 973.17 km |
Additional information OPS 5798 DEB
OPS 5798 DEB, 903 is space debris in LEO originally from a launch on Tue, 06 Oct 1964 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 OPS 5798 DEB Date of exalting 06.10.1964y. Average height of ISS OPS 5798 DEB hundred 973.17 km. Average velocity OPS 5798 DEB is 26519.95 km/h. Inclination OPS 5798 DEB satellite 90.22°.TLE
Average velocity OPS 5798 DEB
Average inclination OPS 5798 DEB
Mean right ascension of the ascending node (RAAN) OPS 5798 DEB
Mean argument of perigee OPS 5798 DEB
Mean semi-major axis of the orbit OPS 5798 DEB
Mean orbital eccentricity OPS 5798 DEB
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