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ATLAS CENTAUR 2 R/B

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ATLAS CENTAUR 2 R/B is classified as:


NORAD ID: 694
Int'l Code: 1963-047A
Perigee: 466.7 km
Apogee: 1,319.0 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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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 00694U 63047A   18226.47576032  .00000290  00000-0  26597-4 0  9996
2 00694  30.3564 355.5659 0586724 104.6109 262.0256 14.02339065742170
Source of the keplerian elements: AFSPC