Orihime - .
Payload: ETS-7 Target. Nation: Japan.
Type: Navigation technology satellite. Spacecraft Bus: ETS.
Spacecraft: ETS-7 Target.
Decay Date: 1999-01-27 . USAF Sat Cat: 25424 . COSPAR: 1997-074E. Apogee: 458 km (284 mi). Perigee: 346 km (214 mi). Inclination: 34.50 deg. Period: 92.60 min. Attached to Hikoboshi. It would later separate and serve as a passive docking target for the Hikobishi active automatic docking technology spacecraft..