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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 304 | CE-SAT-1 (Canon Electric Satellite 1) | CE-SAT-1 | Japan | Japan | Canon Electronics | Commercial | Technology Development | Optical Imaging | LEO | Sun-Synchronous | 0 | 497 | 517 | 1.45E-03 | 97.45 | 94.76 | 3 | 2017/6/22 | Canon Electronics Space Technology Laboratory | Japan | Satish Dhawan Space Centre | PSLV | 2017-036E | 42769 | Create a high-resolution Earth-imaging system by combining a Cassegrain telescope with a conventional Canon image sensor found in the firm’s EOS product line. | JMSatcat/10_17 | https://www.canonwatch.com/canons-satellite-ce-sat-1-is-in-orbit-building-a-high-resolution-earth-imaging-system-using-eos-5d-mark-iii/ | |||
| 305 | CE-SAT-2B (Canon Electric Satellite 2B) | CE-SAT-2B | Japan | Japan | Canon Electronics | Commercial | Technology Demonstration | Optical Imaging | LEO | Sun-Synchronous | 0 | 507 | 523 | 1.16E-03 | 97.5 | 94.2 | 36 | 2020/10/28 | 2 | Canon Electronics Space Technology Laboratory | Japan | Rocket Lab Launch Complex 1 | Electron | 2020-077F | 46818 | 2 year demonstration mission on three types of cameras. | JMSatcat/12_20 | https://spaceflightnow.com/2020/10/28/rocket-lab-successfully-launches-satellites-for-planet-and-canon/ |
Total: 2