ATLAS 14E R/B
Satellite information ATLAS 14E R/B
| Spacetrack Directory Name | ATLAS 14E R/B |
| Follow ATLAS 14E R/B | ATLAS 14E R/B Tracker |
| Pass predictions ATLAS 14E R/B | Pass predictions ATLAS 14E R/B |
| Orbit launches |
1984-09-08 (41 years ago)
|
| Days in orbit | 15329 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1323 km |
| Apogee | 20017 km |
| Orbit slope (inclination) | 64.96° |
| Laps per day | 4 |
| Height ATLAS 14E R/B | 12995.32 km |
Additional information ATLAS 14E R/B
ATLAS 14E R/B, 15272 is space debris in HEO originally from a launch on Sat, 08 Sep 1984 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 14E R/B Date of exalting 08.09.1984y. Average height of ISS ATLAS 14E R/B hundred 12995.32 km. Average velocity ATLAS 14E R/B is 16144.66 km/h. Inclination ATLAS 14E R/B satellite 64.96°.TLE
Average velocity ATLAS 14E R/B
Average inclination ATLAS 14E R/B
Mean right ascension of the ascending node (RAAN) ATLAS 14E R/B
Mean argument of perigee ATLAS 14E R/B
Mean semi-major axis of the orbit ATLAS 14E R/B
Mean orbital eccentricity ATLAS 14E R/B
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