OPS 0100 DEB *
Satellite information OPS 0100 DEB * - OPS 0100 DEB
| Spacetrack Directory Name | OPS 0100 DEB * |
| Alternative name | OPS 0100 DEB |
| Follow OPS 0100 DEB * | OPS 0100 DEB * Tracker |
| Pass predictions OPS 0100 DEB * | Pass predictions OPS 0100 DEB * |
| Orbit launches |
1967-04-14 (59 years ago)
|
| Days in orbit | 21692 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1044 km |
| Apogee | 1086 km |
| Orbit slope (inclination) | 90.35° |
| Laps per day | 14 |
| Height OPS 0100 DEB * | 1074.61 km |
Additional information OPS 0100 DEB *
OPS 0100 DEB *, 4843 is space debris in LEO originally from a launch on Fri, 14 Apr 1967 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 0100 DEB * Date of exalting 14.04.1967y. Average height of ISS OPS 0100 DEB * hundred 1074.61 km. Average velocity OPS 0100 DEB * is 26338.79 km/h. Inclination OPS 0100 DEB * satellite 90.35°.TLE
Average velocity OPS 0100 DEB *
Average inclination OPS 0100 DEB *
Mean right ascension of the ascending node (RAAN) OPS 0100 DEB *
Mean argument of perigee OPS 0100 DEB *
Mean semi-major axis of the orbit OPS 0100 DEB *
Mean orbital eccentricity OPS 0100 DEB *
ISS
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