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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: 466.8 km
Apogee: 1,321.2 km
Inclination: 30.4 °
Period: 102.7 minutes
Semi major axis: 7265 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   17112.48416339 +.00000914 +00000-0 +10458-3 0  9994
2   694 030.3594 111.3022 0588029 268.2607 085.0588 14.02042842674893
Source of the keplerian elements: AFSPC