Hodoyoshi-3 and 4 Mission

Objectives and Applications

The primary mission of H3 and H4 is Earth observation by using various optical sensors. H3 has two different cameras which are low- and mid-resolution with a GSD (Ground Sampling Distance) of 250 m and 40 m; on the other hand, H4 has one relatively high-resolution camera with a GSD of 6-10 m. Furthermore, the satellites have various secondary mission instruments, for example, wide-angle mini cameras, hosted payload boxes, technology demonstration module and materials, UHF data receiving system for a Store and Forward mission, in order to provide opportunities for rapid new technology demonstration on orbit and low-cost commercial usage like advertisement in space.

Mission Summary

Full Name
Hodoyoshi-3 and 4
Mission Status
Operational (nominal)
Mission Agencies
ISSL UT
Launch Date
19 Jun 2014
Mission Links
EOL Date
Jun 2025
EO Portal Info

Orbit Details

Orbit Type
Inclined, non-sun-synchronous
Orbit Period
97.4 minutes
Orbit Sense
Ascending
Orbit Inclination
97.6 deg
Orbit Altitude
600 km
Orbit Longitude
Orbit LST
Repeat Cycle
NORAD Catalog #
International Designator

Mission Instruments

Mission Measurements

OpenSearch Datasets

No IDN OpenSearch datasets found.