Technical details of Satellite TurkmenAlem 52.0°E

- Transponders: 38 active Ku-band (shared over 3 beams)

- Design Lifetime: 15 years

- Orbltal Position: GEO, 52.0°East

- Payload: Consumption 8 kW, mass 352kg

- Number of beams: 3 (East, West, Mena)

- Manufacturer: Thales Alenia Space (France)

- Platform: SpaceBus 4000С2

- Consumption: 10 kW

- Dry mass: 1839 kg

- Solar array: Power 11,3 kW

- Battery energy 18,2 kWh

- Launch mass: 4731 kg