Hodoyoshi-3 from Satellite Dataset
Source dataset: Satellite Dataset, curated by  SkyLover

  About Hodoyoshi-3

Designed for technology development, Hodoyoshi-3 is a government satellite operated by University of Tokyo and NESTRA (Japan).

Delivered via Dnepr (launch vehicle) from Dombarovsky Air Base, it was launched into space on 19 June 2014 and orbits the Earth as a sun-synchronous LEO satellite. Hodoyoshi-3 was constructed by University of Tokyo (Japan).

Hodoyoshi-3 has a launch mass of 60 kg and navigates with the COSPAR ID 2014-033F and NORAD ID 40015.

With an orbital eccentricity of 3.78E-03, the satellite's perigee, which is the point of the orbit closest to the Earth's center of mass, is 613km while its apogee, which is the point of the orbit farthest from the Earth's center of mass, is 666km. It takes 98 minutes to orbit the Earth.

With generated usable power of 50 watts, Hodoyoshi-3 orbits at an inclination of 98 degrees to the equatorial plane of the Earth.


 Compare Hodoyoshi-3 with Starlink-1708 from USA.

 Compare Hodoyoshi-3 with SpaceBEE-45 from USA.

  Data: Hodoyoshi-3 

Satellite Dataset

  Lists relating to Hodoyoshi-3

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