USA 169
Satellite information USA 169 - USA 169 (MILSTAR-2 4)
| Spacetrack Directory Name | USA 169 |
| Alternative name | USA 169 (MILSTAR-2 4) |
| Follow USA 169 | USA 169 Tracker |
| Pass predictions USA 169 | Pass predictions USA 169 |
| Orbit launches |
2003-04-08 (23 years ago)
|
| Days in orbit | 8549 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Categories | |
| Perigee | 35775 km |
| Apogee | 35799 km |
| Orbit slope (inclination) | 12.47° |
| Laps per day | 1 |
| Orbit | GEO |
| Height USA 169 | 35788.56 km |
Additional information USA 169
USA 169, 27711 is a payload satellite owned by USAF SMC (US) in GEO that was launched on Tue, 08 Apr 2003 UTC via a TITAN 401B/CENTAUR launch vehicle from the Air Force Eastern Test Range (AFETR). 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 USA 169 Date of exalting 08.04.2003y. Average height of ISS USA 169 hundred 35788.56 km. Average velocity USA 169 is 11068.72 km/h. Inclination USA 169 satellite 12.19°.TLE
Average velocity USA 169
Average inclination USA 169
Mean right ascension of the ascending node (RAAN) USA 169
Mean argument of perigee USA 169
Mean semi-major axis of the orbit USA 169
Mean orbital eccentricity USA 169
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