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REX 2

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REX 2 is classified as:


NORAD ID: 23814
Int'l Code: 1996-014A
Perigee: 800.0 km
Apogee: 835.5 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   15245.71608434 +.00000067 +00000-0 +24125-4 0  9999
2 23814 090.1256 309.5570 0024644 089.7522 270.6494 14.24371939012160

Source of the keplerian elements: AFSPC

N2YO: 287