Hodoyoshi

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Hodoyoshi
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Hodoyoshi 4
Credit: Manufacturer Image

Satellite of the University of Tokyo and AXELSPACE, carried an imager with 6.8m resolution and 28 km swath. Sun synchronous orbit; 1100 GMT local time of the descending node. Technology, Earth observation satellite for University of Tokyo, NESTRA, Japan. Launched 2014.

Status: Operational 2014. First Launch: 2014-06-19. Last Launch: 2014-11-06. Number: 3 . Gross mass: 58 kg (127 lb).

More at: Hodoyoshi.

Subtopics

Hodoyoshi 4 Technology, Earth observation satellite for University of Tokyo, NESTRA, Japan. Launched 2014.

Hodoyoshi 1 Technology, Earth observation satellite built by University of Tokyo, NESTRA, Axelspace for University of Tokyo, NESTRA, Japan. Launched 2014.

Hodoyoshi 2 (RISESat) Null

Family: Surveillance. Country: Japan. Launch Vehicles: Dnepr. Launch Sites: Dombarovskiy.

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Hodoyoshi 3
Credit: Manufacturer Image

Hodoyoshi-1
Credit: Manufacturer Image

2014 June 19 - . 19:11 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: Dnepr.

Hodoyoshi 4 - . Mass: 64 kg (141 lb). Nation: Japan. Spacecraft: Hodoyoshi. USAF Sat Cat: 40011 . COSPAR: 2014-033B. Apogee: 651 km (404 mi). Perigee: 612 km (380 mi). Inclination: 97.98 deg. Period: 97.34 min. Experimental earth-observation satellite by the University of Toky with a 5 m ground resolution..

Hodoyoshi 3 - . Mass: 58 kg (127 lb). Nation: Japan. Spacecraft: Hodoyoshi. USAF Sat Cat: 40015 . COSPAR: 2014-033F. Apogee: 666 km (413 mi). Perigee: 612 km (380 mi). Inclination: 97.97 deg. Period: 97.50 min. Experimental earth-observation satellite by the University of Toky with a 40 m ground resolution..

2014 November 6 - . 07:35 GMT - . Launch Site: Dombarovskiy. Launch Complex: Dombarovskiy. Launch Pad: Yasniy. LV Family: R-36M. Launch Vehicle: Dnepr.

Hodoyoshi-1 - . Mass: 50 kg (110 lb). Nation: Japan. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Hodoyoshi. USAF Sat Cat: 40299 . COSPAR: 2014-070B. Apogee: 513 km (318 mi). Perigee: 496 km (308 mi). Inclination: 97.45 deg. Period: 94.70 min. Satellite of the University of Tokyo and AXELSPACE, carried an imager with 6.8m resolution and 28 km swath. Sun synchronous orbit; 1100 GMT local time of the descending node..

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