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OGO 1

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OGO 1 is classified as:


NORAD ID: 879
Int'l Code: 1964-054A
Perigee: 5,496.1 km
Apogee: 143,368.0 km
Inclination: 71.4 °
Period: 3,809.8 minutes
Semi major axis: 80803 km
RCS: 1 m2 (large)
Launch date: September 5, 1964
Source: United States (US)
Launch site: AIR FORCE EASTERN TEST RANGE (AFETR)

The purpose of the OGO 1 spacecraft, the first of a series of six Orbiting Geophysical Observatories, was to conduct diversified geophysical experiments to obtain a better understanding of the earth as a planet and to develop and operate a standardized observatory-type satellite. OGO 1 consisted of a main body that was parallelepipedal in form, two solar panels, each with a solar-oriented experiment package (SOEP), two orbital plane experiment packages (OPEP) and six appendages EP-1 through EP-6 supporting the boom experiment packages.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1   879U 64054A   19265.11099659 -.00000707  00000-0  00000+0 0  9990
2   879  71.3954 321.0390 8531350 201.6505   0.7697  0.37797330 20557
Source of the keplerian elements: AFSPC