OPS 6226
Satellite information OPS 6226 - OPS 6226 (DMSP 5C F7)
| Spacetrack Directory Name | OPS 6226 |
| Alternative name | OPS 6226 (DMSP 5C F7) |
| Follow OPS 6226 | OPS 6226 Tracker |
| Pass predictions OPS 6226 | Pass predictions OPS 6226 |
| Orbit launches |
1975-05-24 (51 years ago)
|
| Days in orbit | 18771 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 775 km |
| Apogee | 850 km |
| Orbit slope (inclination) | 98.6° |
| Laps per day | 14 |
| Height OPS 6226 | 819.5 km |
Additional information OPS 6226
OPS 6226, 7816 is a payload satellite owned by SAMSO (US) in SSO that was launched on Sat, 24 May 1975 UTC via a THOR BURNER 2A 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 OPS 6226 Date of exalting 24.05.1975y. Average height of ISS OPS 6226 hundred 819.5 km. Average velocity OPS 6226 is 26801.73 km/h. Inclination OPS 6226 satellite 98.6°.TLE
Average velocity OPS 6226
Average inclination OPS 6226
Mean right ascension of the ascending node (RAAN) OPS 6226
Mean argument of perigee OPS 6226
Mean semi-major axis of the orbit OPS 6226
Mean orbital eccentricity OPS 6226
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