SEDSAT (original) (raw)
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SEDSAT
American technology satellite. The SEDSAT micro-satellite was built by the Huntsville, Alabama chapter of SEDS (the Students for the Exploration and Development of Space). Technology satellite for SEDS, USA. Launched 1998.
Status: Operational 1998. First Launch: 1998-10-24. Last Launch: 1998-10-24. Number: 1 . Gross mass: 34 kg (74 lb).
SEDSAT had two amateur radio transponders and an earth imaging camera.
More at: SEDSAT.
Family: Technology, Technology satellite. Country: USA. Spacecraft: SEDS. Launch Vehicles: Thor, Delta, Delta 2 7000, Delta 7326-9.5. Projects: STS. Launch Sites: Cape Canaveral, Cape Canaveral LC17A. Agency: NASA. Bibliography: 2.
Photo Gallery
SEDSAT 1Credit: Manufacturer Image |
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- SEDSAT 1 - . Nation: USA. Agency: Boeing. Manufacturer: SEDS. Program: STS. Class: Technology. Type: Navigation technology satellite. Spacecraft: SEDSAT. USAF Sat Cat: 25509 . COSPAR: 1998-061B. Apogee: 1,050 km (650 mi). Perigee: 544 km (338 mi). Inclination: 31.40 deg. Period: 100.80 min.
Following separation of the third stage and the primary Deep Space 1 payload, the Delta second stage manoeuvred from its 185 km parking orbit to a 174 km x 2744 km x 28.5 degree orbit. It then released the SEDSAT micro-satellite, built by the Huntsville, Alabama chapter of SEDS (the Students for the Exploration and Development of Space). SEDSAT has two amateur radio transponders and an earth imaging camera.
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