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REX 2

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    REX 2 can be found in the following categories:
    Military

    NORAD ID: 23814
    Int'l Code: 1996-014A
    Perigee: 795.6 km
    Apogee: 825.9 km
    Inclination: 90.1 °
    Period: 101.1 minutes
    Semi major axis: 7188 km
    Launch date: March 9, 1996
    Source: United States (US)
    Comments: 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.

    Two Line Element Set (TLE):

    1 23814U 96014A   15064.18445001  .00000222  00000-0  91206-4 0  9995
    2 23814 090.1285 306.9735 0021051 329.1154 030.8799 14.24326567986540
    
    
    Source: AFSPC

    NASA's NSSDC Master Catalog entry for REX 2

     
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