Dual LEO satellite system and method for global coverage
The present invention relates to satellite systems and more particularly, to the provision of a satellite system and method for communications applications, with global coverage. An optimal method of providing global broadband connectivity has been discovered which uses two different LEO constellations with inter-satellite links among the satellites in each constellation, and inter-satellite links between the constellations. The first constellation is deployed in a polar LEO orbit with a preferred inclination of 99.5 degrees and a preferred altitude of 1000 km. The second constellation is deployed in an inclined LEO orbit with a preferred inclination of 37.4 degrees and a preferred altitude of 1250 km.
1. A satellite system for global communications comprising:
a first set of satellites in a polar LEO (low Earth orbit) constellation; a second set of satellites in an inclined LEO constellation;
a first user terminal for transmitting to, and receiving signals from, said first and second set of satellites; and
a Gateway, a base station or a second user terminal for transmitting to, and receiving signals from, said first and second set of satellites;
each of said first and second set of satellites having an ISL (inter-satellite link) functionality with respect to satellites in the polar LEO constellation and with satellites in the inclined LEO constellation;
wherein the Gateway, the base station, or the second user terminal are operable to avoid interference with a GEO satellite user terminal by switching the Gateway, the base station or the second user terminal to an alternate LEO satellite that has an angular separation with a GEO satellite greater than a calculated discrimination angle, as measured at the GEO user terminal.
2. The satellite system of claim 1 , wherein said polar LEO constellation comprises six planes, equally spaced.
3. The satellite system of claim 2 , wherein said planes of said polar LEO constellation are inclined between 80 degrees and 100 degrees.
4. The satellite system of claim 3 , wherein said planes of said polar LEO constellation are inclined about 99.5 degrees.
5. The satellite system of claim 1 , wherein said inclined LEO constellation comprises five planes, equally spaced.
6. The satellite system of claim 5 , wherein said planes of said inclined LEO constellation are inclined between 5 degrees and 75 degrees.
7. The satellite system of claim 6 , wherein said planes of said inclined LEO constellation are inclined about 37.4 degrees.
8. The satellite system of claim 1 , wherein said polar LEO constellation comprises about 72 satellites and said inclined LEO constellation comprises about 45 satellites, the system thereby providing global coverage with a minimum elevation angle of about 20 degrees.
9. The satellite system of claim 1 , wherein said satellites of said polar LEO constellation orbit at an altitude of between 800 km and 1400 km.
10. The satellite system of claim 9 , wherein said satellites of said polar LEO constellation orbit at an altitude of about 1000 km.
11. The satellite system of claim 1 , wherein said satellites of said inclined LEO constellation orbit at an altitude of between 800 km and 1400 km.
12. The satellite system of claim 11 , wherein said satellites of said inclined LEO constellation orbit at an altitude of about 1250 km.
13. The satellite system of claim 1 , wherein excess capacity in the polar LEO constellation in the higher latitudes is used to transfer data traffic, via the ISL, from both LEO constellations to a Gateway located in the North for a connection to a terrestrial network.
14. The satellite system of claim 1 , each of said first and second set of satellites having an IP router functionality.
15. The satellite system of claim 14 , each of said first and second set of satellites having an IP router load management functionality.
16. The satellite system of claim 1 , wherein said communications comprises broadband communications.
17. The satellite system of claim 1 , wherein said first user terminal includes an electronically scanned array antenna for communicating with said first and second set of satellites.
18. A method of operation for a global communications satellite system for comprising:
launching a first set of satellites in a polar LEO (low Earth orbit) constellation; launching a second set of satellites in an inclined LEO constellation; using a user terminal, transmitting communications data to a first satellite in said first or second set of satellites;
communicating said communications data from said first satellite, to a second satellite in said first or second set of satellites using an ISL (inter-satellite link);
transmitting said communications data from said second satellite, to a polar Gateway; and
avoiding interference with a GEO satellite user terminal by switching the polar Gateway to an alternate LEO satellite that has an angular separation with a GEO satellite greater than a calculated discrimination angle, as measured at the GEO satellite user terminal.