GGSE 2
Satellite information GGSE 2
| Spacetrack Directory Name | GGSE 2 |
| Follow GGSE 2 | GGSE 2 Tracker |
| Pass predictions GGSE 2 | Pass predictions GGSE 2 |
| 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 | 893 km |
| Apogee | 925 km |
| Orbit slope (inclination) | 70.08° |
| Laps per day | 14 |
| Height GGSE 2 | 917.56 km |
Additional information GGSE 2
GGSE 2, 1244 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 2 Date of exalting 09.03.1965y. Average height of ISS GGSE 2 hundred 917.56 km. Average velocity GGSE 2 is 26621.47 km/h. Inclination GGSE 2 satellite 70.08°.TLE
Average velocity GGSE 2
Average inclination GGSE 2
Mean right ascension of the ascending node (RAAN) GGSE 2
Mean argument of perigee GGSE 2
Mean semi-major axis of the orbit GGSE 2
Mean orbital eccentricity GGSE 2
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