Express mesh intersatellite optical coherent networking
An express mesh satellite network includes a plurality of satellites arranged in a constellation, each including a plurality of coherent optical modems, wherein the plurality of satellites are configured in a topology based on traffic sources and sinks on the ground where the topology includes express links where satellites are directly connected in space by the coherent optical modems based on the traffic sources and sinks. The plurality of satellites are configured to become a node in the topology when in an associated affinity area having a ground link or requiring a relay function.
1. A satellite comprising:
a plurality of coherent optical modems; and
circuitry configured to switch traffic between the plurality of optical modems,
wherein the satellite is configured to operate with a plurality of satellites in a constellation,
wherein the plurality of coherent optical modems are configured to operate in a topology for the constellation that is based on traffic sources and sinks on the ground where the topology includes express links where any of the plurality of coherent optical modems are directly connected in space based on the traffic sources and sinks; and
wherein the satellite is further configured to rotate around the Earth and to become a node in the topology when in an associated affinity area having a ground link or requiring a relay function, and wherein the topology is fixed while the plurality of satellites orbit and take roles in the topology based on their location.
2. The satellite of claim 1 , wherein the topology includes no more than three hops to reach any satellite over a geographic area.
3. The satellite of claim 1 , wherein the plurality of satellites are in Low Earth Orbit (LEO).
4. The satellite of claim 1 , wherein the plurality of satellites are in Middle Earth Orbit (MEO).
5. The satellite of claim 1 , wherein the satellite is further configured to power down or reduce power in some or all of the plurality of coherent optical modems outside of the associated affinity area.
6. The satellite of claim 1 , wherein a coherent optical modem of the plurality of coherent optical modems is further configured with a modulation format to accommodate required direct connection distance to another satellite with required bandwidth.
7. The satellite of claim 1 , wherein transmitted optical power of a coherent optical modem of the plurality of coherent optical modems is further configured to accommodate required direct connection distance to another satellite with required bandwidth.
8. An express mesh satellite network comprising:
a plurality of satellites arranged in a constellation, each including a plurality of coherent optical modems,
wherein the plurality of satellites are configured in a topology based on traffic sources and sinks on the ground where the topology includes express links where satellites are directly connected in space by the plurality of coherent optical modems based on the traffic sources and sinks,
wherein the plurality of satellites are each further configured to become a node in the topology when in an associated affinity area having a ground link or requiring a relay function, and wherein the topology is fixed while the plurality of satellites orbit and take roles in the topology based on their location.
9. The express mesh satellite network of claim 8 , wherein the topology includes no more than three hops to reach any satellite of the plurality of satellites over a geographic area.
10. The express mesh satellite network of claim 8 , wherein the plurality of satellites are in Low Earth Orbit (LEO).
11. The express mesh satellite network of claim 8 , wherein the plurality of satellites are in Middle Earth Orbit (MEO).
12. The express mesh satellite network of claim 8 , wherein the plurality of satellites are further configured to power down or reduce power in some or all of the corresponding coherent optical modems outside of the associated affinity area.
13. A method of configuring an express mesh satellite network comprising:
determining a topology for a plurality of satellites based on traffic sources and sinks on the ground where the topology includes express links where satellites are directly connected in space by coherent optical modems based on the traffic sources and sinks; and
configuring the plurality of satellites with the topology,
wherein the plurality of satellites are each further configured to become a node in the topology when in an associated affinity area having a ground link or requiring a relay function, and wherein the topology is fixed while the plurality of satellites orbit and take roles in the topology based on their location.
14. The method of claim 13 , wherein the topology includes no more than three hops to reach any satellite of the plurality of satellites over a geographic area.
15. The method of claim 13 , wherein the plurality of satellites are in Low Earth Orbit (LEO).