ISIS 2 DEB
Satellite information ISIS 2 DEB
| Spacetrack Directory Name | ISIS 2 DEB |
| Follow ISIS 2 DEB | ISIS 2 DEB Tracker |
| Pass predictions ISIS 2 DEB | Pass predictions ISIS 2 DEB |
| Orbit launches |
1971-04-01 (55 years ago)
|
| Days in orbit | 20242 |
| Country/organisation of origin | Kanada (CA) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1317 km |
| Apogee | 1409 km |
| Orbit slope (inclination) | 88.16° |
| Laps per day | 13 |
| Height ISIS 2 DEB | 1363.56 km |
Additional information ISIS 2 DEB
ISIS 2 DEB, 27658 is space debris in LEO originally from a launch on Thu, 01 Apr 1971 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 ISIS 2 DEB Date of exalting 01.04.1971y. Average height of ISS ISIS 2 DEB hundred 1363.56 km. Average velocity ISIS 2 DEB is 25842.63 km/h. Inclination ISIS 2 DEB satellite 88.16°.TLE
Average velocity ISIS 2 DEB
Average inclination ISIS 2 DEB
Mean right ascension of the ascending node (RAAN) ISIS 2 DEB
Mean argument of perigee ISIS 2 DEB
Mean semi-major axis of the orbit ISIS 2 DEB
Mean orbital eccentricity ISIS 2 DEB
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