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CEPE
American satellite. Cylindrical Electrostatic Probe Experiment (orbital experiment attached to Delta second stage)

Status: Operational 1970. First Launch: 1970-12-11. Last Launch: 1970-12-11. Number: 1 .



Country: USA. Spacecraft: TIROS. Launch Vehicles: Thor, Delta, Thor Delta N6. Launch Sites: Vandenberg, Vandenberg SLC2W. Agency: NASA Greenbelt. Bibliography: 2, 279.

1970 December 11 - . 11:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Thor. Launch Vehicle: Thor Delta N6.
  • CEPE - . Nation: USA. Agency: NASA Greenbelt. Program: Tiros. Spacecraft: CEPE. USAF Sat Cat: 4794 . COSPAR: 1970-106B. Apogee: 1,484 km (922 mi). Perigee: 1,426 km (886 mi). Inclination: 101.7042 deg. Period: 114.92 min.


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