OPS 8480 (TRANSIT 5B-6)
Satellite information OPS 8480 (TRANSIT 5B-6)
| Spacetrack Directory Name | OPS 8480 (TRANSIT 5B-6) |
| Follow OPS 8480 (TRANSIT 5B-6) | OPS 8480 (TRANSIT 5B-6) Tracker |
| Pass predictions OPS 8480 (TRANSIT 5B-6) | Pass predictions OPS 8480 (TRANSIT 5B-6) |
| Orbit launches |
1965-06-24 (61 years ago)
|
| Days in orbit | 22351 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1011 km |
| Apogee | 1124 km |
| Orbit slope (inclination) | 89.87° |
| Laps per day | 14 |
| Height OPS 8480 (TRANSIT 5B-6) | 1077.47 km |
Additional information OPS 8480 (TRANSIT 5B-6)
OPS 8480 (TRANSIT 5B-6), 1420 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Thu, 24 Jun 1965 UTC via a THOR ABLESTAR 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 8480 (TRANSIT 5B-6) Date of exalting 24.06.1965y. Average height of ISS OPS 8480 (TRANSIT 5B-6) hundred 1077.47 km. Average velocity OPS 8480 (TRANSIT 5B-6) is 26333.9 km/h. Inclination OPS 8480 (TRANSIT 5B-6) satellite 89.87°.TLE
Average orbit height OPS 8480 (TRANSIT 5B-6)
Average velocity OPS 8480 (TRANSIT 5B-6)
Average inclination OPS 8480 (TRANSIT 5B-6)
Mean right ascension of the ascending node (RAAN) OPS 8480 (TRANSIT 5B-6)
Mean argument of perigee OPS 8480 (TRANSIT 5B-6)
Mean semi-major axis of the orbit OPS 8480 (TRANSIT 5B-6)
Mean orbital eccentricity OPS 8480 (TRANSIT 5B-6)
ISS
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