| 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. |