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HIROGARI (OPUSAT-II)

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HIROGARI (OPUSAT-II) is classified as:


NORAD ID: 47930
Int'l Code: 1998-067SG
Perigee: 391.7 km
Apogee: 394.0 km
Inclination: 51.6 °
Period: 92.3 minutes
Semi major axis: 6763 km
RCS: Unknown
Launch date: November 20, 1998
Source: Japan (JPN)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

Uplink (MHz): 436.500
Downlink (MHz): 145.900
Beacon (MHz): 145.900
Mode: 1k2AFSK/9k6/13k6GMSK CW
Call sign: JL3ZKS
Status: Active


HIROGARI is a 2U size CubeSat developed by Osaka Prefecture University and Muroran Institute of Technology. The satellite demostrates: (1) High-speed data transmission, using Reed-Solomon encoding and convolutional processing with error correction capability, in the amateur radio band which enable amateur radio satellites to communicate more efficiently, and (2) A deployment structure based on the “Miura-ori” folding method, and an optical surface measurement system that uses two-dimensional grid for the first time in space. This experiment could benefit the future deployment systems in space.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 47930U 98067SG  21342.85913568  .00021902  00000-0  26437-3 0  9999
2 47930  51.6382 189.0450 0001748 192.4370 167.6581 15.60674704 41923
Source of the keplerian elements: AFSPC