GGSE 3 DEB
Satellite information GGSE 3 DEB
| Spacetrack Directory Name | GGSE 3 DEB |
| Follow GGSE 3 DEB | GGSE 3 DEB Tracker |
| Pass predictions GGSE 3 DEB | Pass predictions GGSE 3 DEB |
| Orbit launches |
1965-03-09 (61 years ago)
|
| Days in orbit | 22459 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 865 km |
| Apogee | 893 km |
| Orbit slope (inclination) | 70.08° |
| Laps per day | 14 |
| Height GGSE 3 DEB | 889.35 km |
Additional information GGSE 3 DEB
GGSE 3 DEB, 44043 is space debris in LEO originally from a launch on Tue, 09 Mar 1965 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 GGSE 3 DEB Date of exalting 09.03.1965y. Average height of ISS GGSE 3 DEB hundred 889.35 km. Average velocity GGSE 3 DEB is 26673.1 km/h. Inclination GGSE 3 DEB satellite 70.08°.TLE
Average velocity GGSE 3 DEB
Average inclination GGSE 3 DEB
Mean right ascension of the ascending node (RAAN) GGSE 3 DEB
Mean argument of perigee GGSE 3 DEB
Mean semi-major axis of the orbit GGSE 3 DEB
Mean orbital eccentricity GGSE 3 DEB
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