OTS 2
Satellite information OTS 2
| Spacetrack Directory Name | OTS 2 |
| Follow OTS 2 | OTS 2 Tracker |
| Pass predictions OTS 2 | Pass predictions OTS 2 |
| Orbit launches |
1978-05-11 (48 years ago)
|
| Days in orbit | 17653 |
| Country/organisation of origin | European Space Agency (ESA) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36066 km |
| Apogee | 36147 km |
| Orbit slope (inclination) | 7.83° |
| Laps per day | 1 |
| Height OTS 2 | 36106.48 km |
Additional information OTS 2
OTS 2, 10855 is a payload satellite owned by ESA (ESA) in GEO that was launched on Thu, 11 May 1978 UTC via a DELTA 3914 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 OTS 2 Date of exalting 11.05.1978y. Average height of ISS OTS 2 hundred 36106.48 km. Average velocity OTS 2 is 11027.22 km/h. Inclination OTS 2 satellite 7.86°.TLE
Average velocity OTS 2
Average inclination OTS 2
Mean right ascension of the ascending node (RAAN) OTS 2
Mean argument of perigee OTS 2
Mean semi-major axis of the orbit OTS 2
Mean orbital eccentricity OTS 2
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