| Name of Satellite, Alternate Names | Shiyan 7 (SY7, Experimental Satellite 7) |
| Country of Operator/Owner | China (PR) |
| Operator/Owner | Chinese Academy of Space Technology (CAST) |
| Users | Military |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 668 |
| Apogee (km) | 672 |
| Eccentricity | 0.000284090909090909 |
| Inclination (degrees) | 98.06 |
| Period (minutes) | 98.15 |
| Launch Mass (kg.) | |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 19-07-2013 |
| Expected Lifetime | |
| Contractor | Chinese Academy of Space Technology (CAST) |
| Country of Contractor | China (PR) |
| Launch Site | Taiyuan Launch Center |
| Launch Vehicle | Long March 4C |
| COSPAR Number | 2013-037B |
| NORAD Number | 39209 |
| Comments | Possibly testing systems for detection of orbiting space debris or tracking missile launches. |