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: 465.4 km
Apogee: 1,296.0 km
Inclination: 30.4 °
Period: 102.4 minutes
Semi major axis: 7251 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 00694U 63047A   23264.14967916  .00004405  00000-0  55547-3 0  9991
2 00694  30.3525 165.4058 0572649 100.0117 266.5564 14.05866936  4502

Source of the keplerian elements: AFSPC