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Pageos

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Pageos 1 Credit: Manufacturer Image

Status: Operational 1966. First Launch: 1966-06-24. Last Launch: 1966-06-24. Number: 3 . Gross mass: 55 kg (121 lb).

• Pageos 1 - . Payload: Pageos A. Mass: 55 kg (121 lb). Nation: USA. Agency: NASA Langley. Class: Earth. Type: Geodetic satellite. Spacecraft: Pageos. Decay Date: 1975-07-12 . USAF Sat Cat: 2253 . COSPAR: 1966-056A. Apogee: 4,220 km (2,620 mi). Perigee: 3,913 km (2,431 mi). Inclination: 85.40 deg. Period: 177.10 min.

  The PAGEOS (Passive Geodetic Earth Orbiting Satellite) spacecraft was a 30.48-m inflatable sphere, and had no instrumentation on board. It was the second (following GEOS 1) NASA satellite in the National Geodetic Satellites Program. The launch, orbit, separation, inflation and initial operation were nominal, with more than 40 ground stations participating in the observation program. The orbit was generally considered too high for drag-density study, although some work was done in this area by the Smithsonian Astrophysical Observatory. Additional Details: here....

• Pageos canister half - . Payload: Pageos canister half. Mass: 55 kg (121 lb). Nation: USA. Agency: NASA Langley. Spacecraft: Pageos. USAF Sat Cat: 2511 . COSPAR: 1966-056D. Apogee: 4,255 km (2,643 mi). Perigee: 4,227 km (2,626 mi). Inclination: 87.00 deg. Period: 181.50 min.

• Pageos canister half - . Payload: Pageos canister half. Mass: 55 kg (121 lb). Nation: USA. Agency: NASA Langley. Spacecraft: Pageos. USAF Sat Cat: 2256 . COSPAR: 1966-056C. Apogee: 4,276 km (2,656 mi). Perigee: 4,196 km (2,607 mi). Inclination: 86.90 deg. Period: 181.40 min.