Shin'en

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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

Shin'en 2 (FO 82, Fuji-OSCAR 82) Null

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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