ATLAS 41E R/B
Satellite information ATLAS 41E R/B
| Spacetrack Directory Name | ATLAS 41E R/B |
| Follow ATLAS 41E R/B | ATLAS 41E R/B Tracker |
| Pass predictions ATLAS 41E R/B | Pass predictions ATLAS 41E R/B |
| Orbit launches |
1985-03-13 (41 years ago)
|
| Days in orbit | 15143 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 729 km |
| Apogee | 775 km |
| Orbit slope (inclination) | 108.04° |
| Laps per day | 14 |
| Height ATLAS 41E R/B | 754.58 km |
Additional information ATLAS 41E R/B
ATLAS 41E R/B, 15596 is space debris in LEO originally from a launch on Wed, 13 Mar 1985 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 ATLAS 41E R/B Date of exalting 13.03.1985y. Average height of ISS ATLAS 41E R/B hundred 754.58 km. Average velocity ATLAS 41E R/B is 26923.95 km/h. Inclination ATLAS 41E R/B satellite 108.04°.TLE
Average velocity ATLAS 41E R/B
Average inclination ATLAS 41E R/B
Mean right ascension of the ascending node (RAAN) ATLAS 41E R/B
Mean argument of perigee ATLAS 41E R/B
Mean semi-major axis of the orbit ATLAS 41E R/B
Mean orbital eccentricity ATLAS 41E R/B
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