Ginrei
Organisation · Japan
Original archive entry. The text, images and links below are kept as they were written.
Credit: Manufacturer Image
Microsatellite from Shinshu University to study use of LED's for long-distance communication.
Related
- Family
- Technology
- Country
- Japan
- Launch Vehicles
- H-IIA 202
- Launch Sites
- Tanegashima Y
Chronology
1 event
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: 65.01 deg. Period: 91.73 min. Microsatellite from Shinshu University to study use of LED's for long-distance communication..