UCS-Satellite-Database
| Id | Name of Satellite, Alternate Names | Current Official Name of Satellite | Country/Org of UN Registry | Country of Operator/Owner | Operator/Owner | Users | Purpose | Detailed Purpose | Class of Orbit | Type of Orbit | Longitude of GEO (degrees) | Perigee (km) | Apogee (km) | Eccentricity | Inclination (degrees) | Period (minutes) | Launch Mass (kg.) | Dry Mass (kg.) | Power (watts) | Date of Launch | Expected Lifetime (yrs.) | Contractor | Country of Contractor | Launch Site | Launch Vehicle | COSPAR Number | NORAD Number | Comments | Source Used for Orbital Data | Source |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 1041 | Hibari | Hibari | NR (1/22) | Japan | Tokyo Institute of Technology | Civil | Technology Demonstration | LEO | Sun-Synchronous | 0 | 548 | 572 | 1.73E-03 | 97.6 | 96 | 55 | 2021/11/8 | Tokyo Institute of Technology | Japan | Uchinoura Space Center | H2A | 2021-102F | 49400 | Will test a method of attitude control, or pointing, using the variable shape of its solar array wings. | JMSatcat/1_22 | https://spaceflightnow.com/2021/11/15/japanese-epsilon-rocket-launches-nine-small-satellites/ |
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