ATLAS 35F R/B
Satellite information ATLAS 35F R/B
| Spacetrack Directory Name | ATLAS 35F R/B |
| Follow ATLAS 35F R/B | ATLAS 35F R/B Tracker |
| Pass predictions ATLAS 35F R/B | Pass predictions ATLAS 35F R/B |
| Orbit launches |
1980-02-09 (46 years ago)
|
| Days in orbit | 17004 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 968 km |
| Apogee | 15259 km |
| Orbit slope (inclination) | 64.39° |
| Laps per day | 5 |
| Height ATLAS 35F R/B | 9769.12 km |
Additional information ATLAS 35F R/B
ATLAS 35F R/B, 11705 is space debris in HEO originally from a launch on Sat, 09 Feb 1980 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 35F R/B Date of exalting 09.02.1980y. Average height of ISS ATLAS 35F R/B hundred 9769.12 km. Average velocity ATLAS 35F R/B is 17766.22 km/h. Inclination ATLAS 35F R/B satellite 64.39°.TLE
Average velocity ATLAS 35F R/B
Average inclination ATLAS 35F R/B
Mean right ascension of the ascending node (RAAN) ATLAS 35F R/B
Mean argument of perigee ATLAS 35F R/B
Mean semi-major axis of the orbit ATLAS 35F R/B
Mean orbital eccentricity ATLAS 35F R/B
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