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: 465.0 km
Apogee: 1,286.6 km
Inclination: 30.4 °
Period: 102.3 minutes
Semi major axis: 7246 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   24114.19920267  .00003534  00000-0  43550-3 0  9992
2   694  30.3565  53.9813 0566839 178.8418 181.3612 14.07295975 34420

Source of the keplerian elements: AFSPC