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: 464.9 km
Apogee: 1,286.5 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   24116.11407219  .00003205  00000-0  39272-3 0  9994
2   694  30.3580  43.3597 0566856 195.6054 162.6387 14.07309149 34690

Source of the keplerian elements: AFSPC