Coverage areas

BELINTERSAT-1 is a Belarusian geostationary communications satellite. It was developed and manufactured by the Chinese Academy of Space Technology (CAST) and launched on 15 January 2016 from Xichang, People’s Republic of China, by a «Long March 3B» launch vehicle.
The spacecraft is based on the DFH-4 satellite platform (China) with a service life of 15 years. It is placed at 51.5°E in geostationary orbit and provides satellite communications and broadcasting services for an area in eastern Europe, central and eastern Asia and Africa.
C-диапазон Африканский
C-диапазон Африканский
  • С-диапазон: до 16 ×36 MHz*
  • Линия вниз: 3600 - 4200 MHz;
  • Линия вверх: 5850 - 6450 MHz
  • Поляризация: левая/правая

* Опция переключения транспондеров между лучами.

Ku-диапазон Африканский
Ku-диапазон Африканский
  • Ku-диапазон: 12×36 MHz
  • Линия вниз: 10950 - 11200 MHz;
  • Линия вверх: 14000 - 14500 MHz
  • Поляризация: вертикальная/горизонтальная
4×36 MHz cross-strapped (подъем в Европейском луче, спуск в Африканском луче, Ku-диапазон).
Восточный луч
Восточный луч
  • C-диапазон: до 12 ×36 MHz*
  • Линия вниз: 3600 - 4200 MHz;
  • Линия вверх: 5850 - 6450 MHz
  • Поляризация: левая/правая

* Опция переключения транспондеров между лучами.

Европейский луч
Европейский луч
  • Ku-диапазон: 4×54 MHz, 2×36 MHz
  • Линия вниз: 10825 – 10950; 11200 – 11450 MHz;
  • Линия вверх: 12750 – 13125 MHz
  • Поляризация: вертикальная/горизонтальная
African
C-band beam
  • Number of transponders: up to 16x36 mhz *
  • Uplink frequencies: 5850 - 6450 mhz
  • Downlink frequencies: 3600 - 4200 mhz
  • Uplink polarization: lhcp & rhcp
  • Downlink polarization: lhcp & rhcp

* switch option for transponders between beams.

African
Ku-band beam
African Ku-band beam
  • Number of transponders: 12x36 mhz
  • Uplink frequencies: 14000 - 14500 mhz
  • Downlink frequencies: 10950 - 11200 mhz
  • Uplink polarization: vertical & horizontal
  • Downlink polarization: vertical & horizontal
* 4×36 mhz cross-strapped (uplink in european beam, downlink in african ku-band beam).
East
C-band beam
East C-band beam
  • Number of transponders: up to 12x36 mhz *
  • Uplink frequencies: 5850 - 6450 mhz
  • Downlink frequencies: 3600 - 4200 mhz
  • Uplink polarization: lhcp & rhcp
  • Downlink polarization: lhcp & rhcp

* switch option for transponders between beams.

European
Ku-band beam
European Ku-band beam
  • Number of transponders: 4×54 mhz, 2×36 mhz
  • Uplink frequencies: 12750 – 13125 mhz
  • Downlink frequencies: 10825 – 10950; 11200 – 11450 mhz
  • Uplink polarization: vertical & horizontal
  • Downlink polarization: vertical & horizontal
BEACONS:
Countries

Service areas:

European
Ku-band Beam:

Austria, Lithuania, Latvia, Estonia, Poland, Ukraine, Moldova, Hungary, Romania, Czech Republic, Slovakia, Germany, Norway, Finland, Sweden, Serbia, Bulgaria, Croatia, Italy, France, Great Britain, Ireland.

East
C-band Beam:

Bangladesh, Brunei, Vietnam, China, Cambodia, India, Indonesia, Laos, Mongolia, Myanmar, Nepal, Pakistan, Malaysia, Philippines, Sri Lanka, Singapore, Thailand.

African
C-band Beam:

All African countries; Asia - the countries of the Arabian Peninsula, Vietnam, Hong Kong, Laos, Myanmar, Taiwan, Thailand; Europe - Andorra, Greece, Spain, Italy, Portugal, Wales, France.

African Ku-band Beam:

Mauritania, Mali, Burkina Faso, Niger, Nigeria, Benin, Ghana, Guinea, Senegal, Togo, Gambia, Guinea-Bissau, Liberia, Cameroon, Gabon, Republic of the Congo, Democratic Republic of the Congo, Angola, Zimbabwe, Algeria, Burundi, Central African Republic, Cameroon, Canary Islands, Cape Verde, Côte d'Ivoire, Equatorial Guinea, Morocco, Chad, Uganda, Malawi, Rwanda, Sierra Leone, Sao Tome and Principe.

specification

Payload data

Band Beams TPs quantity TPs bandwidth, MHz Polarization
C African 6 to 16 36 circular
Global 2 to 4
Eastern 2 to 12
Ku African 12* 36 linear
European 2
4 54
* “Cross-strapped” option (uplink in Europe – downlink in Africa only) – 4 transponders.
The satellite’s mission control specialists constantly monitor continuous communication and periodically correct its orbital position in order to keep it in the specified position.

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