REX 2

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REX 2 is classified as:

Military

NORAD ID: 23814

Int'l Code: 1996-014A

Perigee: 799.7 km

Apogee: 833.9 km

Inclination: 90.0 °

Period: 101.1 minutes

Semi major axis: 7187 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.

1 23814U 96014A   22342.41927616  .00000136  00000-0  53585-4 0  9997
2 23814  90.0462 336.9878 0023763  43.6024 316.7042 14.24650047389944

Source of the keplerian elements: AFSPC