GGSE 5
Satellite information GGSE 5
| Spacetrack Directory Name | GGSE 5 |
| Follow GGSE 5 | GGSE 5 Tracker |
| Pass predictions GGSE 5 | Pass predictions GGSE 5 |
| 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 | 901 km |
| Apogee | 916 km |
| Orbit slope (inclination) | 69.97° |
| Laps per day | 14 |
| Height GGSE 5 | 917.45 km |
Additional information GGSE 5
GGSE 5, 2834 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 5 Date of exalting 31.05.1967y. Average height of ISS GGSE 5 hundred 917.45 km. Average velocity GGSE 5 is 26621.67 km/h. Inclination GGSE 5 satellite 69.97°.TLE
Average velocity GGSE 5
Average inclination GGSE 5
Mean right ascension of the ascending node (RAAN) GGSE 5
Mean argument of perigee GGSE 5
Mean semi-major axis of the orbit GGSE 5
Mean orbital eccentricity GGSE 5
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