| Name of Satellite, Alternate Names | Satellite Zhangguo Ziyuan 2C (ZY-2C, JB-3C) |
| Country of Operator/Owner | China (PR) |
| Operator/Owner | Chinese Academy of Space Technology |
| Users | Military |
| Purpose | Reconnaissance |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 555 |
| Apogee (km) | 606 |
| Eccentricity | 0.00366880080569743 |
| Inclination (degrees) | 97.2 |
| Period (minutes) | 96.3 |
| Launch Mass (kg.) | |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 04-11-2004 |
| Expected Lifetime | 3-5 yrs. |
| Contractor | Chinese Academy of Space Technology (CAST) |
| Country of Contractor | China (PR) |
| Launch Site | Taiyuan Launch Center |
| Launch Vehicle | Chang Zheng 4B |
| COSPAR Number | 2004-044A |
| NORAD Number | 28470 |
| Comments | Third digital imaging spacecraft launched by Chinese government for reconnaissance purposes. |