GGSE 1 (GGRS)
Satellite information GGSE 1 (GGRS) - GGRS
| Spacetrack Directory Name | GGSE 1 (GGRS) |
| Alternative name | GGRS |
| Follow GGSE 1 (GGRS) | GGSE 1 (GGRS) Tracker |
| Pass predictions GGSE 1 (GGRS) | Pass predictions GGSE 1 (GGRS) |
| Orbit launches |
1964-01-11 (62 years ago)
|
| Days in orbit | 22932 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| Perigee | 895 km |
| Apogee | 912 km |
| Orbit slope (inclination) | 69.91° |
| Laps per day | 14 |
| Height GGSE 1 (GGRS) | 911.88 km |
Additional information GGSE 1 (GGRS)
GGSE 1 (GGRS), 728 is an American payload satellite in LEO that was launched on Sat, 11 Jan 1964 UTC via a THOR SLV-2A 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 1 (GGRS) Date of exalting 11.01.1964y. Average height of ISS GGSE 1 (GGRS) hundred 911.88 km. Average velocity GGSE 1 (GGRS) is 26631.86 km/h. Inclination GGSE 1 (GGRS) satellite 69.91°.TLE
Average velocity GGSE 1 (GGRS)
Average inclination GGSE 1 (GGRS)
Mean right ascension of the ascending node (RAAN) GGSE 1 (GGRS)
Mean argument of perigee GGSE 1 (GGRS)
Mean semi-major axis of the orbit GGSE 1 (GGRS)
Mean orbital eccentricity GGSE 1 (GGRS)
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