OPS 0856 DEB
Satellite information OPS 0856 DEB
| Spacetrack Directory Name | OPS 0856 DEB |
| Follow OPS 0856 DEB | OPS 0856 DEB Tracker |
| Pass predictions OPS 0856 DEB | Pass predictions OPS 0856 DEB |
| Orbit launches |
1966-08-19 (60 years ago)
|
| Days in orbit | 21930 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1319 km |
| Apogee | 5377 km |
| Orbit slope (inclination) | 87.41° |
| Laps per day | 9 |
| Height OPS 0856 DEB | 3315.71 km |
Additional information OPS 0856 DEB
OPS 0856 DEB, 24647 is space debris in LEO originally from a launch on Fri, 19 Aug 1966 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 0856 DEB Date of exalting 19.08.1966y. Average height of ISS OPS 0856 DEB hundred 3315.71 km. Average velocity OPS 0856 DEB is 23081.67 km/h. Inclination OPS 0856 DEB satellite 87.41°.TLE
Average velocity OPS 0856 DEB
Average inclination OPS 0856 DEB
Mean right ascension of the ascending node (RAAN) OPS 0856 DEB
Mean argument of perigee OPS 0856 DEB
Mean semi-major axis of the orbit OPS 0856 DEB
Mean orbital eccentricity OPS 0856 DEB
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