DODECAPOLE 2
Satellite information DODECAPOLE 2
| Spacetrack Directory Name | DODECAPOLE 2 |
| Follow DODECAPOLE 2 | DODECAPOLE 2 Tracker |
| Pass predictions DODECAPOLE 2 | Pass predictions DODECAPOLE 2 |
| Orbit launches |
1965-08-13 (61 years ago)
|
| Days in orbit | 22301 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 883 km |
| Apogee | 939 km |
| Orbit slope (inclination) | 90.07° |
| Laps per day | 14 |
| Height DODECAPOLE 2 | 866.34 km |
Additional information DODECAPOLE 2
DODECAPOLE 2, 1510 is a payload satellite owned by NRL (US) in LEO that was launched on Fri, 13 Aug 1965 UTC via a THOR ABLESTAR 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 DODECAPOLE 2 Date of exalting 13.08.1965y. Average height of ISS DODECAPOLE 2 hundred 866.34 km. Average velocity DODECAPOLE 2 is 26714.84 km/h. Inclination DODECAPOLE 2 satellite 90.07°.TLE
Average velocity DODECAPOLE 2
Average inclination DODECAPOLE 2
Mean right ascension of the ascending node (RAAN) DODECAPOLE 2
Mean argument of perigee DODECAPOLE 2
Mean semi-major axis of the orbit DODECAPOLE 2
Mean orbital eccentricity DODECAPOLE 2
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