
SES 10 [Airbus Defence and Space]
SES ordered in February 2014 the SES 10 comsat to expand SESs capabilities in Latin America and the Caribbean through high power beams tailored to provide direct-to-home broadcasting, enterprise and broadband connectivity services in the entire region.
SES-10s comprehensive coverage includes Mexico, Central America and South America, as well as the Caribbean. The satellite will be positioned at the 67 West orbital position, pursuant to an agreement between the Andean Community (Bolivia, Colombia, Ecuador and Peru) and SES, which provides for use of the Andean Communitys Simon Bolivar 2 satellite network. The specifically designed beam of SES-10 over the Andean Community Member States, combined with its optimum elevation angle, represents a unique proposition for telecommunications operators, broadcasters and service providers for the Andean countries.
With 50 high-power Ku-band transponders, the satellite will provide replacement capacity for the current satellites, AMC-3 and AMC-4, as well as incremental capacity at the 67 West slot. SES has been providing key services to customers in the region from this orbital slot since 2010. SES-10 will be built by Airbus Defence and Space based on the Eurostar-3000 platform. The satellite is designed to operate for 15 years in geosynchronous orbit, utilizing an electric plasma propulsion system for on-orbit manoeuvres and a chemical system for initial orbit raising and some on-orbit manoeuvres. SES-10 will have an electrical power of 13 kW and its launch mass on Falcon-9 is expected to be about 5300 kilograms. The satellite will also fly Flexible Command Receivers, whose frequency agility provides for more robust satellite command link operations.
SES-10 is slated for launch on board a SpaceX Falcon-9 v1.2 launch vehicle, using the first reused Falcon-9 core.
| Nation: | Luxembourg |
|---|---|
| Type / Application: | Communication |
| Operator: | SES |
| Contractors: | Airbus Defence and Space |
| Equipment: | 50 high-power Ku-Band transponders |
| Configuration: | Eurostar-3000 |
| Propulsion: | ? × SPT-100 Stationary Plasma Thrusters |
| Power: | 2 deployable solar arrays, batteries |
| Lifetime: | 15 years |
| Mass: | 5300 kg |
| Orbit: | GEO |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| SES 10 | 2017-017A | 30.03.2017 | CCK LC-39A | Falcon-9 v1.2 |
