GEODETIC EARTH ORBITING SATELLITE 1, GEODYNAMICS EXPERIMENTAL OCEAN SATELLITE 1 - Norad Identifikationsnummer: 1726
| Name im Katalog Spacetrack | EXPLORER 29 (GEOS 1) |
| Alternative Bezeichnung | GEODETIC EARTH ORBITING SATELLITE 1, GEODYNAMICS EXPERIMENTAL OCEAN SATELLITE 1 |
| Folge EXPLORER 29 (GEOS 1) | EXPLORER 29 (GEOS 1) Tracker |
| Flugzeiten EXPLORER 29 (GEOS 1) | Flugzeiten EXPLORER 29 (GEOS 1) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 22223 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perygeum | 1116 km |
| Apogäum | 2272 km |
| Neigung der Umlaufbahn (Inklination) | 59.38° |
| Runden pro Tag | 12 |
| Höhe EXPLORER 29 (GEOS 1) | 1722.89 km |
EXPLORER 29 (GEOS 1), 1726 is a payload satellite owned by GSFC (US) in LEO that was launched on Sat, 06 Nov 1965 UTC via a THOR DELTA E launch vehicle from the Air Force Eastern Test Range (AFETR). 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 29 (GEOS 1) hinausgetragen 06.11.1965r. Durchschnittshöhe EXPLORER 29 (GEOS 1) Text Nummer 1: das. 1722.89 km. Durchschnittsgeschwindigkeit EXPLORER 29 (GEOS 1) beträgt 25261 km/h. Neigung EXPLORER 29 (GEOS 1) Satelliten 59.38°.