GGSE 3
Satellite information GGSE 3
| Spacetrack Directory Name | GGSE 3 |
| Follow GGSE 3 | GGSE 3 Tracker |
| Pass predictions GGSE 3 | Pass predictions GGSE 3 |
| 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) |
| Perigee | 879 km |
| Apogee | 904 km |
| Orbit slope (inclination) | 70.08° |
| Laps per day | 14 |
| Height GGSE 3 | 898.7 km |
Additional information GGSE 3
GGSE 3, 1292 is an American payload satellite in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D launch vehicle from the Air Force Western Test Range (AFWTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite GGSE 3 Date of exalting 09.03.1965y. Average height of ISS GGSE 3 hundred 898.7 km. Average velocity GGSE 3 is 26655.93 km/h. Inclination GGSE 3 satellite 70.08°.TLE
Average velocity GGSE 3
Average inclination GGSE 3
Mean right ascension of the ascending node (RAAN) GGSE 3
Mean argument of perigee GGSE 3
Mean semi-major axis of the orbit GGSE 3
Mean orbital eccentricity GGSE 3
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