EXPLORER 36 (GEOS 2)
Satellite information EXPLORER 36 (GEOS 2)
| Spacetrack Directory Name | EXPLORER 36 (GEOS 2) |
| Alternative name | GEODETIC EARTH ORBITING SATELLITE 2, GEODYNAMICS EXPERIMENTAL OCEAN SATELLITE 2 |
| Follow EXPLORER 36 (GEOS 2) | EXPLORER 36 (GEOS 2) Tracker |
| Pass predictions EXPLORER 36 (GEOS 2) | Pass predictions EXPLORER 36 (GEOS 2) |
| Orbit launches |
1968-01-11 (58 years ago)
|
| Days in orbit | 21420 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1082 km |
| Apogee | 1572 km |
| Orbit slope (inclination) | 105.78° |
| Laps per day | 13 |
| Height EXPLORER 36 (GEOS 2) | 1341.59 km |
Additional information EXPLORER 36 (GEOS 2)
EXPLORER 36 (GEOS 2), 3093 is a payload satellite owned by GSFC (US) in LEO that was launched on Thu, 11 Jan 1968 UTC via a THOR DELTA E1 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 EXPLORER 36 (GEOS 2) Date of exalting 11.01.1968y. Average height of ISS EXPLORER 36 (GEOS 2) hundred 1341.59 km. Average velocity EXPLORER 36 (GEOS 2) is 25880.19 km/h. Inclination EXPLORER 36 (GEOS 2) satellite 105.78°.TLE
Average velocity EXPLORER 36 (GEOS 2)
Average inclination EXPLORER 36 (GEOS 2)
Mean right ascension of the ascending node (RAAN) EXPLORER 36 (GEOS 2)
Mean argument of perigee EXPLORER 36 (GEOS 2)
Mean semi-major axis of the orbit EXPLORER 36 (GEOS 2)
Mean orbital eccentricity EXPLORER 36 (GEOS 2)
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