| Name of Satellite, Alternate Names | Turksat 4A |
| Country of Operator/Owner | Turkey |
| Operator/Owner | Turksat |
| Users | Commercial |
| Purpose | Communications |
| Class of Orbit | GEO |
| Type of Orbit | |
| Longitude of GEO (degrees) | 50 |
| Perigee (km) | 35776 |
| Apogee (km) | 35797 |
| Eccentricity | 0.000249071910618766 |
| Inclination (degrees) | 0.01 |
| Period (minutes) | 1436.08 |
| Launch Mass (kg.) | 4869 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 14-02-2014 |
| Expected Lifetime | 15 yrs. |
| Contractor | Mitsubishi Electric Corporation |
| Country of Contractor | Japan |
| Launch Site | Baikonur Cosmodrome |
| Launch Vehicle | Proton |
| COSPAR Number | 2014-007A |
| NORAD Number | 39522 |
| Comments | Will move to 42 East when joined by Turksat 4B. |