OPS 9444 (DSCS 2-14)
Satellite information OPS 9444 (DSCS 2-14) - DSCS-2 D14
| Spacetrack Directory Name | OPS 9444 (DSCS 2-14) |
| Alternative name | DSCS-2 D14 |
| Follow OPS 9444 (DSCS 2-14) | OPS 9444 (DSCS 2-14) Tracker |
| Pass predictions OPS 9444 (DSCS 2-14) | Pass predictions OPS 9444 (DSCS 2-14) |
| Orbit launches |
1979-11-21 (46 years ago)
|
| Days in orbit | 17094 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36308 km |
| Apogee | 36359 km |
| Orbit slope (inclination) | 8.32° |
| Laps per day | 1 |
| Height OPS 9444 (DSCS 2-14) | 36333.53 km |
Additional information OPS 9444 (DSCS 2-14)
OPS 9444 (DSCS 2-14), 11622 is an American payload satellite in GEO that was launched on Wed, 21 Nov 1979 UTC via a TITAN IIIC 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 OPS 9444 (DSCS 2-14) Date of exalting 21.11.1979y. Average height of ISS OPS 9444 (DSCS 2-14) hundred 36333.53 km. Average velocity OPS 9444 (DSCS 2-14) is 10997.84 km/h. Inclination OPS 9444 (DSCS 2-14) satellite 8.35°.TLE
Average velocity OPS 9444 (DSCS 2-14)
Average inclination OPS 9444 (DSCS 2-14)
Mean right ascension of the ascending node (RAAN) OPS 9444 (DSCS 2-14)
Mean argument of perigee OPS 9444 (DSCS 2-14)
Mean semi-major axis of the orbit OPS 9444 (DSCS 2-14)
Mean orbital eccentricity OPS 9444 (DSCS 2-14)
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