Name of Satellite, Alternate Names |
Chuangxin-3 |
Country of Operator/Owner |
China (PR) |
Operator/Owner |
Chinese Academy of Sciences |
Users |
Government |
Purpose |
Technology Development |
Class of Orbit |
LEO |
Type of Orbit |
Sun-Synchronous |
Longitude of GEO (degrees) |
0 |
Perigee (km) |
564 |
Apogee (km) |
611 |
Eccentricity |
0.00337765001796622 |
Inclination (degrees) |
97.7 |
Period (minutes) |
96.43 |
Launch Mass (kg.) |
200 |
Dry Mass (kg.) |
|
Power (watts) |
|
Date of Launch |
19-07-2013 |
Expected Lifetime |
|
Contractor |
China Academy of Sciences |
Country of Contractor |
China (PR) |
Launch Site |
Taiyuan Launch Center |
Launch Vehicle |
Long March 2C |
COSPAR Number |
2013-037C |
NORAD Number |
39210 |
Comments |
Equipped with a system for testing a manipulator arm, maybe a proof of concept for use on China´s upcoming space station. |