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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: 466.1 km
Apogee: 1,311.6 km
Inclination: 30.4 °
Period: 102.6 minutes
Semi major axis: 7259 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   22146.73624449  .00002020  00000-0  24792-3 0  9994
2 00694  30.3599 309.3935 0582304 219.0666 136.6466 14.03507180936632
Source of the keplerian elements: AFSPC