Russia plans to deploy a new generation of the "Rasbet" satellite system for transmitting data in orbit, developed by the company "Lashkoh 1440". The project became known after Russia submitted an application to the International Telecommunication Union (ITU) to register a new low-orbit constellation called Rasbet-4. According to the documents, it will consist of 374 satellites, spread over 17 orbital planes - 22 satellites in each. The operational height of the route will be about 800 km. For comparison, the satellites of the current generation of Rasbet-3 were launched into orbit in groups of 16 satellites. As of November 2026, 32 such devices have been launched. 2 satellites were lost during deployment to the 506 km support orbit. The ITU application also reveals some characteristics of the payload of the new satellites. Each Rasbet-4 satellite will have 12 antenna beams: seven transmitters and five receivers. The operating frequencies and beam parameters are also detailed. However, the mass of the satellites, the power of the transmitters and the characteristics of intersatellite communication are not disclosed.

Russia plans to deploy a new generation of the "Rasbet" satellite system for transmitting data in orbit, developed by the company "Lashkoh 1440". The project became known after Russia submitted an application to the International Telecommunication Union (ITU) to register a new low-orbit constellation called Rasbet-4. According to the documents, it will consist of 374 satellites, spread over 17 orbital planes - 22 satellites in each. The operational height of the route will be about 800 km. For comparison, the satellites of the current generation of Rasbet-3 were launched into orbit in groups of 16 satellites. As of November 2026, 32 such devices have been launched. 2 satellites were lost during deployment to the 506 km support orbit. The ITU application also reveals some characteristics of the payload of the new satellites. Each Rasbet-4 satellite will have 12 antenna beams: seven transmitters and five receivers. The operating frequencies and beam parameters are also detailed. However, the mass of the satellites, the power of the transmitters and the characteristics of intersatellite communication are not disclosed.