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REX 2

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REX 2 is classified as:


NORAD ID: 23814
Int'l Code: 1996-014A
Perigee: 800.7 km
Apogee: 829.0 km
Inclination: 90.0 °
Period: 101.0 minutes
Semi major axis: 7185 km
RCS: 0.6208 m2 (medium)
Launch date: March 9, 1996
Source: United States (US)
Launch site: AIR FORCE WESTERN TEST RANGE (AFWTR)

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   25165.52039117  .00000134  00000-0  52009-4 0  9993
2 23814  90.0172 340.5857 0019650 267.0629  92.8315 14.25229014520829
Source of the keplerian elements: AFSPC