GEODETIC EARTH ORBITING SATELLITE 2, GEODYNAMICS EXPERIMENTAL OCEAN SATELLITE 2 - Norad Identifikationsnummer: 3093
| Name im Katalog Spacetrack | EXPLORER 36 (GEOS 2) |
| Alternative Bezeichnung | GEODETIC EARTH ORBITING SATELLITE 2, GEODYNAMICS EXPERIMENTAL OCEAN SATELLITE 2 |
| Folge EXPLORER 36 (GEOS 2) | EXPLORER 36 (GEOS 2) Tracker |
| Flugzeiten EXPLORER 36 (GEOS 2) | Flugzeiten EXPLORER 36 (GEOS 2) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 21420 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 1082 km |
| Apogäum | 1572 km |
| Neigung der Umlaufbahn (Inklination) | 105.78° |
| Runden pro Tag | 13 |
| Höhe EXPLORER 36 (GEOS 2) | 1341.59 km |
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.
der Satellit EXPLORER 36 (GEOS 2) hinausgetragen 11.01.1968r. Durchschnittshöhe EXPLORER 36 (GEOS 2) Text Nummer 1: das. 1341.59 km. Durchschnittsgeschwindigkeit EXPLORER 36 (GEOS 2) beträgt 25880.19 km/h. Neigung EXPLORER 36 (GEOS 2) Satelliten 105.78°.