Satellite system with handover for multiple gateways

1. A method of operating a satellite communication system, the method comprising:

a plurality of terminals in a region communicating with a first gateway via a first non-geostationary satellite traveling in an orbital direction along an orbital path as beams of the first non-geostationary satellite traverse the region;

a second gateway in communication with the first non-geostationary satellite handing over to a second non-geostationary satellite traveling in the orbital direction along the orbital path, the first gateway is at a first location, the second gateway is at a second location, the second location is separated from the first location in the orbital direction;

terminals of the plurality of terminals handing over to the second non-geostationary satellite as beams of the second non-geostationary satellite begin to traverse the region;

as the terminals handover to the second non-geostationary satellite, the terminals start connecting to and communicating with the second gateway via the second non-geostationary satellite;

after all of the terminals of the plurality of terminals handover to the second satellite, the first gateway handing over to the second non-geostationary satellite; and

after the first gateway hands over to the second non-geostationary satellite, the plurality of terminals in the region communicating with the first gateway via the second non-geostationary satellite.

2. The method of claim 1 , wherein:

the beams of the first non-geostationary satellite and the beams of the second non-geostationary satellite are time domain beam hopping spot beams.

3. The method of claim 1 , wherein:

beams of the first non-geostationary satellite and beams of the second non-geostationary satellite overlap.

4. The method of claim 1 , wherein:

the orbital direction is west to east; and

the first location is east of the second location.

5. The method of claim 1 , wherein:

the orbital path is along the Equator.

6. The method of claim 1 , further comprising:

the first gateway and the second gateway communicating with a common processor that is connected to a network.

7. The method of claim 1 , wherein:

at least a subset of the plurality of terminals and the first gateway are in a same spot beam of the beams of the first non-geostationary satellite.

8. The method of claim 1 , wherein:

the beams of the first non-geostationary satellite and the beams of the second non-geostationary satellite are spot beams that perform time domain beam hopping according to one or more beam hopping plans; and

the method further comprising the first non-geostationary satellite changing beam hopping plans for the beams of the first non-geostationary satellite while the first non-geostationary satellite travels along the orbital path as beams of the first non-geostationary satellite traverse the region.

9. A satellite communication system, comprising:

a first non-geostationary satellite configured to travel in an orbital direction along an orbital path and to be in wireless communication with a plurality of terminals while in a first portion of the orbital path overlying the terminals;

a first gateway configured to be at a first location that allows for wireless communication with the plurality of terminals via the first non-geostationary satellite;

a second gateway configured to be at a second location that allows for wireless communication with the plurality of terminals via the first non-geostationary satellite, the second location is separated from the first location in the orbital direction;

a shared processor connected to the first gateway and to the second gateway, the shared processor being configured to be in communication with a communication network;

the plurality of terminals being configurable to wirelessly communicate with the shared processor via the first non-geostationary satellite, the wireless communicating with the shared processor passing through an assigned one of the first gateway and the second gateway, the shared processor is configured to assign each respective terminal in the plurality of terminals to respectively communicate with the shared processor via one or the other of the first gateway and the second gateway based on a current location of the first non-geostationary satellite in the orbital path.

10. The satellite communication system of claim 9 , wherein:

the first non-geostationary satellite is configured to provide a plurality of spot beams using time domain beam hopping among the spot beams in order to provide communication between the terminals and the processor; and

the first non-geostationary satellite is configured to change hopping plans of the spot beams while the terminals communicate with the processor via the spot beams.

11. The satellite communication system of claim 9 , further comprising:

a second non-geostationary satellite, the plurality of terminals configurable to communicate with the processor via the second non-geostationary satellite and either of the first gateway and the second gateway, the processor is configured to assign each terminal to communicate with the processor via the first gateway or via the second gateway based on location of the second geostationary satellite.

12. The satellite communication system of claim 11 , wherein:

the second non-geostationary satellite is configured to travel in the orbital direction along the orbital path concurrently with the first non-geostationary satellite traveling in the orbital direction along the orbital path.

13. The satellite communication system of claim 12 , wherein:

the processor is configured to instruct the terminals to communicate with the first gateway via the first non-geostationary satellite as beams of the first non-geostationary satellite traverse the region;

the second gateway is configured to handover to the second non-geostationary satellite while the terminals to communicate with the first gateway via the first non-geostationary satellite;

the processor is configured to instruct the terminals of the plurality of terminals to start handing over to the second non-geostationary satellite as beams of the second non-geostationary satellite begin to traverse the region;

the processor is configured to instruct the terminals to start connecting to and communicating with the second gateway via the second non-geostationary satellite as the terminals handover to the second non-geostationary satellite;

the first gateway is configured to handover to the second non-geostationary satellite after all of the terminals of the plurality of terminals handover to the second satellite; and

the processor is configured to instruct the plurality of terminals in the region to communicate with the first gateway via the second non-geostationary satellite after the first gateway hands over to the second non-geostationary satellite.

14. The satellite communication system of claim 13 , wherein:

the first non-geostationary satellite configured to provide a plurality of spot beams using time domain beam hopping among the spot beams in order to provide communication between the terminals and the processor; and

the first non-geostationary satellite configured to change hopping plans and routing of the spot beams while the terminals communicate with the processor via the spot beams.

15. The satellite communication system of claim 13 , wherein:

beams of the first non-geostationary satellite and beams of the second non-geostationary satellite are configured to overlap.

16. The satellite communication system of claim 13 , wherein:

the orbital direction is west to east; and

the first location is east of the second location.

17. The satellite communication system of claim 13 , wherein:

the orbital path is along the Equator.

18. The satellite communication system of claim 13 , wherein:

at least a subset of the plurality of terminals and the first gateway are configured to be in a same spot beam of the beams of the first non-geostationary satellite.