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Ginrei
Ginrei
Ginrei
Credit: Manufacturer Image
Microsatellite from Shinshu University to study use of LED's for long-distance communication.

AKA: SHINDAISAT. Status: Operational 2014. First Launch: 2014-02-27. Last Launch: 2014-02-27. Number: 1 . Gross mass: 33 kg (72 lb). Apogee: 371 km (230 mi).



Family: Technology. Country: Japan. Launch Vehicles: H-IIA 202. Launch Sites: Tanegashima Y.

2014 February 27 - . 18:37 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.
  • Ginrei - . Payload: SHINDAISAT. Mass: 33 kg (72 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: Ginrei. Decay Date: 2014-11-24 . USAF Sat Cat: 39572 . COSPAR: 2014-009A. Apogee: 371 km (230 mi). Perigee: 348 km (216 mi). Inclination: 65.0100 deg. Period: 91.73 min. Microsatellite from Shinshu University to study use of LED's for long-distance communication..


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