OPS 7898 (P/L 2)
Satellite information OPS 7898 (P/L 2)
| Spacetrack Directory Name | OPS 7898 (P/L 2) |
| Follow OPS 7898 (P/L 2) | OPS 7898 (P/L 2) Tracker |
| Pass predictions OPS 7898 (P/L 2) | Pass predictions OPS 7898 (P/L 2) |
| Orbit launches |
1971-12-14 (54 years ago)
|
| Days in orbit | 19985 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 978 km |
| Apogee | 989 km |
| Orbit slope (inclination) | 69.99° |
| Laps per day | 14 |
| Height OPS 7898 (P/L 2) | 992.96 km |
Additional information OPS 7898 (P/L 2)
OPS 7898 (P/L 2), 5680 is an American payload satellite in LEO that was launched on Tue, 14 Dec 1971 UTC via a THORAD SLV-2G 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 7898 (P/L 2) Date of exalting 14.12.1971y. Average height of ISS OPS 7898 (P/L 2) hundred 992.96 km. Average velocity OPS 7898 (P/L 2) is 26484.91 km/h. Inclination OPS 7898 (P/L 2) satellite 69.99°.TLE
Average velocity OPS 7898 (P/L 2)
Average inclination OPS 7898 (P/L 2)
Mean right ascension of the ascending node (RAAN) OPS 7898 (P/L 2)
Mean argument of perigee OPS 7898 (P/L 2)
Mean semi-major axis of the orbit OPS 7898 (P/L 2)
Mean orbital eccentricity OPS 7898 (P/L 2)
Frequency OPS 7898 (P/L 2)
In the table below we show the frequencies OPS 7898 (P/L 2).
| Downlink | Mode |
|---|---|
| 137.079 MHz | CW |
ISS
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