| Name of Satellite, Alternate Names | Chuangxin 1-1 (Innovation 1-1, Chuang Xin 1, CZ-1-1) |
| Country of Operator/Owner | China (PR) |
| Operator/Owner | Chinese Academy of Sciences |
| Users | Government |
| Purpose | Communications |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 729 |
| Apogee (km) | 748 |
| Eccentricity | 0.00133642821973693 |
| Inclination (degrees) | 98.5 |
| Period (minutes) | 99.6 |
| Launch Mass (kg.) | 100 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 21-10-2003 |
| Expected Lifetime | |
| Contractor | China Academy of Sciences |
| Country of Contractor | China (PR) |
| Launch Site | Taiyuan Launch Center |
| Launch Vehicle | Long March 3B |
| COSPAR Number | 2003-049B |
| NORAD Number | 28058 |
| Comments | Prototype of advanced telecommunications satellite for LEO. |