Description:

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 Нcr”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"