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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: 466.5 km
Apogee: 1,318.3 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   694U 63047A   19143.36132646  .00000158  00000-0  93490-5 0  9992
2   694  30.3557 243.9610 0586383  31.4012 332.0267 14.02474368781775
Source of the keplerian elements: AFSPC