NORAD ID: 694 Int'l Code: 1963-047A
Perigee: 467.7 km
Apogee: 1,357.9 km
Inclination: 30.4 °
Period: 103.1 minutes
Semi major axis: 7,283.8 km
Launch date: November 27, 1963
Source: United States (US)
Comments: 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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