USA 141 (ATEX)
Satellite information USA 141 (ATEX)
| Spacetrack Directory Name | USA 141 (ATEX) |
| Alternative name | ADVANCED TETHER EXPERIMENT |
| Follow USA 141 (ATEX) | USA 141 (ATEX) Tracker |
| Pass predictions USA 141 (ATEX) | Pass predictions USA 141 (ATEX) |
| Orbit launches |
1998-10-03 (27 years ago)
|
| Days in orbit | 10188 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 737 km |
| Apogee | 746 km |
| Orbit slope (inclination) | 84.99° |
| Laps per day | 14 |
| Height USA 141 (ATEX) | 746.71 km |
Additional information USA 141 (ATEX)
USA 141, 25615 is an American payload satellite in LEO that was launched on Sat, 03 Oct 1998 UTC via an ARPA TAURUS 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 USA 141 (ATEX) Date of exalting 03.10.1998y. Average height of ISS USA 141 (ATEX) hundred 746.71 km. Average velocity USA 141 (ATEX) is 26938.22 km/h. Inclination USA 141 (ATEX) satellite 84.99°.TLE
Average velocity USA 141 (ATEX)
Average inclination USA 141 (ATEX)
Mean right ascension of the ascending node (RAAN) USA 141 (ATEX)
Mean argument of perigee USA 141 (ATEX)
Mean semi-major axis of the orbit USA 141 (ATEX)
Mean orbital eccentricity USA 141 (ATEX)
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