VELA 2
Satellite information VELA 2
| Spacetrack Directory Name | VELA 2 |
| Follow VELA 2 | VELA 2 Tracker |
| Pass predictions VELA 2 | Pass predictions VELA 2 |
| Orbit launches |
1963-10-17 (62 years ago)
|
| Days in orbit | 22975 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 78585 km |
| Apogee | 138997 km |
| Orbit slope (inclination) | 47.86° |
| Laps per day | 0 |
| Height VELA 2 | 133570.23 km |
Additional information VELA 2
VELA 2, 674 is a payload satellite owned by USAF SSD (US) in HEO that was launched on Thu, 17 Oct 1963 UTC via an ATLAS AGENA D 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.
satellite VELA 2 Date of exalting 17.10.1963y. Average height of ISS VELA 2 hundred 133570.23 km. Average velocity VELA 2 is 5938.58 km/h. Inclination VELA 2 satellite 47.86°.TLE
Average velocity VELA 2
Average inclination VELA 2
Mean right ascension of the ascending node (RAAN) VELA 2
Mean argument of perigee VELA 2
Mean semi-major axis of the orbit VELA 2
Mean orbital eccentricity VELA 2
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