REX 2
Satellite information REX 2
| Spacetrack Directory Name | REX 2 |
| Follow REX 2 | REX 2 Tracker |
| Pass predictions REX 2 | Pass predictions REX 2 |
| Orbit launches |
1996-03-09 (30 years ago)
|
| Days in orbit | 11126 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 795 km |
| Apogee | 825 km |
| Orbit slope (inclination) | 90.01° |
| Laps per day | 14 |
| Height REX 2 | 819.48 km |
Additional information REX 2
REX 2, 23814 is a payload satellite owned by USAF STP (US) in LEO that was launched on Sat, 09 Mar 1996 UTC via a PEGASUS XL 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 REX 2 Date of exalting 09.03.1996y. Average height of ISS REX 2 hundred 819.48 km. Average velocity REX 2 is 26801.64 km/h. Inclination REX 2 satellite 90.01°.TLE
Average velocity REX 2
Average inclination REX 2
Mean right ascension of the ascending node (RAAN) REX 2
Mean argument of perigee REX 2
Mean semi-major axis of the orbit REX 2
Mean orbital eccentricity REX 2
ISS
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