OPS 6026 (DMSP 4A F1)
Satellite information OPS 6026 (DMSP 4A F1)
| Spacetrack Directory Name | OPS 6026 (DMSP 4A F1) |
| Follow OPS 6026 (DMSP 4A F1) | OPS 6026 (DMSP 4A F1) Tracker |
| Pass predictions OPS 6026 (DMSP 4A F1) | Pass predictions OPS 6026 (DMSP 4A F1) |
| Orbit launches |
1966-09-16 (59 years ago)
|
| Days in orbit | 21902 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 668 km |
| Apogee | 837 km |
| Orbit slope (inclination) | 98.35° |
| Laps per day | 14 |
| Height OPS 6026 (DMSP 4A F1) | 757.82 km |
Additional information OPS 6026 (DMSP 4A F1)
OPS 6026 (DMSP 4A F1), 2418 is a payload satellite owned by USAF SSD (US) in SSO that was launched on Fri, 16 Sep 1966 UTC via a THOR BURNER 2 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 6026 (DMSP 4A F1) Date of exalting 16.09.1966y. Average height of ISS OPS 6026 (DMSP 4A F1) hundred 757.82 km. Average velocity OPS 6026 (DMSP 4A F1) is 26917.59 km/h. Inclination OPS 6026 (DMSP 4A F1) satellite 98.35°.TLE
Average velocity OPS 6026 (DMSP 4A F1)
Average inclination OPS 6026 (DMSP 4A F1)
Mean right ascension of the ascending node (RAAN) OPS 6026 (DMSP 4A F1)
Mean argument of perigee OPS 6026 (DMSP 4A F1)
Mean semi-major axis of the orbit OPS 6026 (DMSP 4A F1)
Mean orbital eccentricity OPS 6026 (DMSP 4A F1)
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