HIBARI (satellite)

HIBARI
OperatorTokyo Institute of Technology
COSPAR ID2021-102F Edit this at Wikidata
SATCAT no.49400Edit this on Wikidata
Spacecraft properties
ManufacturerTokyo Institute of Technology
Launch mass55 kg (121 lb)
Dimensions50 × 50 × 50 cm (20 × 20 × 20 in)
Start of mission
Launch date9 November 2021, 00:55 UTC
RocketEpsilon (No. 5)
Launch siteUchinoura Space Center
ContractorJAXA
Orbital parameters
Reference systemGeocentric orbit (planned)
RegimeSun-synchronous orbit
Perigee altitude560 km (350 mi)
Apogee altitude560 km (350 mi)
Inclination97.6°
Instruments
Ultraviolet telescope

HIBARI is a space mission by Japan for a microsatellite that would test a new attitude control (orientation) method to achieve high accuracy pointing for its small telescope, and was launched on 9 November 2021 by an Epsilon launch vehicle as part of the Innovative Satellite Technology Demonstration Program-2 mission.[1] The key technology to be tested on HIBARI is called "Variable Shape Attitude Control" (VSAC), and it is based on reaction torque by rotating its four solar array paddles.

  1. ^ イプシロンロケット5号機による革新的衛星技術実証2号機の打上げ結果について [Innovative satellite technology demonstration by Epsilon rocket No. 5 About the launch result of No. 2] (in Japanese). JAXA. 9 November 2021. Retrieved 9 November 2021.