ATLAS F BURNER 2 R/B
Satellite information ATLAS F BURNER 2 R/B
| Spacetrack Directory Name | ATLAS F BURNER 2 R/B |
| Follow ATLAS F BURNER 2 R/B | ATLAS F BURNER 2 R/B Tracker |
| Pass predictions ATLAS F BURNER 2 R/B | Pass predictions ATLAS F BURNER 2 R/B |
| Orbit launches |
1972-10-02 (53 years ago)
|
| Days in orbit | 19692 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 700 km |
| Apogee | 715 km |
| Orbit slope (inclination) | 98.51° |
| Laps per day | 15 |
| Height ATLAS F BURNER 2 R/B | 715.61 km |
Additional information ATLAS F BURNER 2 R/B
ATLAS F BURNER 2 R/B, 6218 is space debris in SSO originally from a launch on Mon, 02 Oct 1972 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 F BURNER 2 R/B Date of exalting 02.10.1972y. Average height of ISS ATLAS F BURNER 2 R/B hundred 715.61 km. Average velocity ATLAS F BURNER 2 R/B is 26997.34 km/h. Inclination ATLAS F BURNER 2 R/B satellite 98.52°.TLE
Average velocity ATLAS F BURNER 2 R/B
Average inclination ATLAS F BURNER 2 R/B
Mean right ascension of the ascending node (RAAN) ATLAS F BURNER 2 R/B
Mean argument of perigee ATLAS F BURNER 2 R/B
Mean semi-major axis of the orbit ATLAS F BURNER 2 R/B
Mean orbital eccentricity ATLAS F BURNER 2 R/B
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