OPS 4988 (GREB 6)
Satellite information OPS 4988 (GREB 6)
| Spacetrack Directory Name | OPS 4988 (GREB 6) |
| Follow OPS 4988 (GREB 6) | OPS 4988 (GREB 6) Tracker |
| Pass predictions OPS 4988 (GREB 6) | Pass predictions OPS 4988 (GREB 6) |
| Orbit launches |
1965-03-09 (61 years ago)
|
| Days in orbit | 22459 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 892 km |
| Apogee | 923 km |
| Orbit slope (inclination) | 70.08° |
| Laps per day | 14 |
| Height OPS 4988 (GREB 6) | 915.82 km |
Additional information OPS 4988 (GREB 6)
OPS 4988 (GREB 6), 1271 is an American payload satellite in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D 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 4988 (GREB 6) Date of exalting 09.03.1965y. Average height of ISS OPS 4988 (GREB 6) hundred 915.82 km. Average velocity OPS 4988 (GREB 6) is 26624.68 km/h. Inclination OPS 4988 (GREB 6) satellite 70.08°.TLE
Average velocity OPS 4988 (GREB 6)
Average inclination OPS 4988 (GREB 6)
Mean right ascension of the ascending node (RAAN) OPS 4988 (GREB 6)
Mean argument of perigee OPS 4988 (GREB 6)
Mean semi-major axis of the orbit OPS 4988 (GREB 6)
Mean orbital eccentricity OPS 4988 (GREB 6)
ISS
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