ATLAS CENTAUR 2 R/B

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ATLAS CENTAUR 2 R/B is classified as:

• Brightest

NORAD ID: 694
Int'l Code: 1963-047A
Perigee: 466.3 km
Apogee: 1,317.2 km
Inclination: 30.4 °
Period: 102.7 minutes
Semi major axis: 7262 km
RCS: 7.867 m² (large)
Launch date: November 27, 1963
Source: United States (US)
Launch site: AIR FORCE EASTERN TEST RANGE (AFETR)

This Atlas Centaur 2 launch vehicle was used for a performance and structural integrity test. It was instrumented with 2000 pounds of sensors, equipment, and telemetry
Note: This is a ROCKET BODY

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1   694U 63047A   20303.13806806  .00000323  00000-0  26082-4 0  9999
2   694  30.3594 234.7128 0585803 267.5254  85.8191 14.02652305855505

Source of the keplerian elements: AFSPC