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: 466.6 km
Apogee: 1,318.0 km
Inclination: 30.4 °
Period: 102.7 minutes
Semi major axis: 7263 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   19235.89556196 +.00000302 +00000-0 +27698-4 0  9999
2   694 030.3555 094.5591 0586089 114.7038 251.5709 14.02497148795151

Source of the keplerian elements: AFSPC