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Intended to render regional and foreign television and radio distribution network service, collection of news, direct television broadcasting, multimedia and Internet, data transmission, telephony, videoconferences, and VSAT-based Intranet.
FUNCTIONAL SPECIFICS
The satellite is delivered to a supporting orbit (Hcr=500 km), then flies over to a geostationary orbit by means of its own electric propulsion engine.
Orbit | geostationary |
Weight of the satellite at the supporting orbit Ícr”500 km, i=51°, kg | 2,600—2,850 |
Weight of the relay with the antenna feeder device, kg | 150—400 |
Number of relays | 10—50 |
Power allocated for the payload, W | up to 7,000 |
Duration of flight from the supporting orbit to the geostationary one, days | 200—300 |
Active operation life, years | 15 |
| Launch vehicle | "Dnepr" |
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