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REX 2

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REX 2 is classified as:


NORAD ID: 23814
Int'l Code: 1996-014A
Perigee: 801.8 km
Apogee: 833.7 km
Inclination: 90.1 °
Period: 101.1 minutes
Semi major axis: 7188 km
RCS: 0.6208 m2 (medium)
Launch date: March 9, 1996
Source: United States (US)

REX 2 (Radiation EXperiment 2) was an American military minispacecraft launched from Vandenberg AFB by a Pegasus XL rocket. The rocket was carried aloft in the belly of a L-1011 aircraft to 12 km altitude before release and ignition. It is an Air Force Rome Laboratory ionospheric research satellite which will test the effects of the atmosphere on radio transmissions, and will employ GPS for on-board navigation and attitude control.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 23814U 96014A   15216.35096223  .00000096  00000-0  36481-4 0  9994
2 23814 090.1283 309.1303 0022232 179.5641 180.5575 14.24367786  8205

Source of the keplerian elements: AFSPC

N2YO: 548