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Shin'en
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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z Shin'en Communications payload designed to demonstrate deep space communications with a small spacecraft from a 0.915 AU x 1.089 AU x 6.8 deg solar orbit.
Status: Operational 2014. First Launch: 2014-12-03. Last Launch: 2014-12-03. Number: 1 . Gross mass: 15 kg (33 lb).
Subtopics Family: Technology. Country: Japan. Launch Vehicles: H-IIA 202. Launch Sites: Tanegashima Y. 2014 December 3 - . 04:22 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. Launch Pad: Tanegashima Y1. LV Family: H-2. Launch Vehicle: H-IIA 202.
- Shin'en-2 - . Mass: 15 kg (33 lb). Nation: Japan. Class: Technology. Type: Communications technology satellite. Spacecraft: Shin'en. USAF Sat Cat: 40320 . COSPAR: 2014-076B. Apogee: -50,912 km (-50,912 mi). Perigee: 245 km (152 mi). Inclination: 29.90 deg. Communications payload designed to demonstrate deep space communications with a small spacecraft from a 0.915 AU x 1.089 AU x 6.8 deg solar orbit..
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