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REX 2

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REX 2 is classified as:


NORAD ID: 23814
Int'l Code: 1996-014A
Perigee: 800.5 km
Apogee: 835.1 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   15147.64481231  .00000117  00000-0  45524-4 0  9998
2 23814 090.1227 308.1439 0024084 054.3015 306.0414 14.24355377998426

Source of the keplerian elements: AFSPC

N2YO: 354