GGSE 4
Satellite information GGSE 4
| Spacetrack Directory Name | GGSE 4 |
| Follow GGSE 4 | GGSE 4 Tracker |
| Pass predictions GGSE 4 | Pass predictions GGSE 4 |
| Orbit launches |
1967-05-31 (59 years ago)
|
| Days in orbit | 21645 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 895 km |
| Apogee | 911 km |
| Orbit slope (inclination) | 69.97° |
| Laps per day | 14 |
| Height GGSE 4 | 910.81 km |
Additional information GGSE 4
GGSE 4, 2828 is an American payload satellite in LEO that was launched on Wed, 31 May 1967 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 4 Date of exalting 31.05.1967y. Average height of ISS GGSE 4 hundred 910.81 km. Average velocity GGSE 4 is 26633.83 km/h. Inclination GGSE 4 satellite 69.97°.TLE
Average velocity GGSE 4
Average inclination GGSE 4
Mean right ascension of the ascending node (RAAN) GGSE 4
Mean argument of perigee GGSE 4
Mean semi-major axis of the orbit GGSE 4
Mean orbital eccentricity GGSE 4
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