| Name of Satellite, Alternate Names | Göktürk 2 |
| Country of Operator/Owner | Turkey |
| Operator/Owner | Turkish Ministry of National Defense |
| Users | Military |
| Purpose | Earth Observation |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 669 |
| Apogee (km) | 690 |
| Eccentricity | 0.00148946733810909 |
| Inclination (degrees) | 98.16 |
| Period (minutes) | 98.35 |
| Launch Mass (kg.) | 409 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 18-12-2012 |
| Expected Lifetime | 5 yrs. |
| Contractor | TÜBİTAK Space Technologies Research Institute/Turkish Aerospace Industries |
| Country of Contractor | Turkey |
| Launch Site | Jiuquan Satellite Launch Center |
| Launch Vehicle | Long March 2D |
| COSPAR Number | 2012-073A |
| NORAD Number | 39030 |
| Comments | High resolution earth observation. Second and third in production. |