Satellite communications system with non-geosynchronous orbits

1. A satellite communications system, comprising:

a plurality of satellites each traveling about the Earth in an orbit such that all of the plurality of satellites has an orbital period that is an integer factor of a sidereal day and all of the plurality of satellites follows a single repeating ground track relative to the surface of the Earth;

each of the plurality of satellites including communication equipment operable to communicate with at least one ground station and a plurality of user terminals to provide communication service to the plurality of user terminals; and

the orbit being oriented relative to the Earth to provide continuous satellite visibility between at least one of the plurality of satellites and a ground station in at least one targeted geographic region of the Earth on at least one repeating sky track relative to the at least one ground station, wherein the orbit for each of the plurality of satellites is oriented relative to the Earth to provide continuous satellite visibility to a ground station in a targeted geographic region of the Earth on a first repeating sky track and a second repeating sky track relative to the ground station, wherein the first repeating sky track is different than the second repeating sky track and comprise a different visible satellite in each respective one of the first sky track and the second sky track in any given time;

wherein the orbit is an elliptical orbit having an eccentricity of about 0.26, a semimajor axis of 10,500 km, an apogee of 15,000 km above sea level, and a perigee of 6,000 km above sea level, and wherein the perigee occurs relative to the southern hemisphere of the Earth.

2. The system of claim 1 , wherein the orbit is inclined relative to the Earth at a critical inclination angle.

3. The system of claim 1 , wherein the orbit comprises an orbital period of 6 sidereal hours.

4. The system of claim 1 , wherein the plurality of satellites comprises at least 12 satellites.

5. A satellite communications system, comprising:

a plurality of satellites each traveling about the Earth in an orbit such that all of the plurality of satellites has an orbital period that is an integer factor of a sidereal day and all of the plurality of satellites follows a single repeating ground track relative to the surface of the Earth;

each of the plurality of satellites including communication equipment operable to communicate with at least one ground station and a plurality of user terminals to provide communication service to the plurality of user terminals; and

the orbit being oriented relative to the Earth to provide continuous satellite visibility between at least one of the plurality of satellites and a ground station in at least one targeted geographic region of the Earth on at least one repeating sky track relative to the at least one ground station, wherein the orbit for each of the plurality of satellites is oriented relative to the Earth to provide continuous satellite visibility to a ground station in a targeted geographic region of the Earth on a first repeating sky track and a second repeating sky track relative to the ground station, wherein the first repeating sky track is different than the second repeating sky track and comprise a different visible satellite in each respective one of the first sky track and the second sky track in any given time;

wherein the orbit is an elliptical orbit having an eccentricity of about 0.26, and wherein the orbit for each of the plurality of satellites has at least an orbital period, eccentricity, semimajor axis, inclination, and longitude of ascending node, and argument of perigee, and are offset in relation to a satellite epoch for each of the plurality of satellites, and wherein the plurality of satellites are evenly spaced along the single repeating ground track.

6. The system of claim 1 , wherein the ground station has a first antenna pair dedicated to the first repeating sky track and a second antenna pair dedicated to the second repeating sky track, each respective antenna pair alternatively tracks successively visible satellites along a corresponding sky track for communication between the ground station and respective ones of the plurality of satellites.

7. The system of claim 6 , further comprising:

a first user terminal comprising communication equipment for communication with each respective one of the plurality of satellites and operative to continuously receive communications from the ground station that are relayed from respective ones of the plurality of satellites in the first repeating sky track; and

a second user terminal comprising communication equipment for communication with each respective one of the plurality of satellites and operative to continuously receive communications from the ground station that are relayed from respective ones of the plurality of satellites in the second repeating sky track;

wherein each user terminal comprises a user terminal phased array antenna with a communication range that extends to an entirety of at least one sky track for receipt of communication from the ground station relayed by respective ones of the plurality of satellites.

8. A method for control of a satellite communications system, comprising:

operating a plurality of satellites each traveling about the Earth in an orbit such that the plurality of satellites have an orbital period that is an integer factor of a sidereal day and all of the plurality of satellites follows a single repeating ground track relative to the surface of the Earth;

equipping each satellite of the plurality of satellites with communication equipment operable to communicate with at least one ground station and a plurality of user terminals to provide data communication service to the plurality of user terminals; and

orienting the orbit of each of the plurality of satellites relative to the Earth to provide continuous satellite visibility to a ground station in a targeted geographic region of the Earth on a first repeating sky track and a second repeating sky track relative to the ground station, wherein the first repeating sky track is different than the second repeating sky track and comprise a different visible satellites in each respective one of the first sky track and the second sky track in any given time;

wherein the orbit is an elliptical orbit having an eccentricity of about 0.26, a semimajor axis of 10,500 km, an apogee of 15,000 km above sea level, and a perigee of 6,000 km above sea level, and the perigee occurs relative to the southern hemisphere of the Earth.

9. The method of claim 8 , wherein the orbit is inclined relative to the Earth at a critical inclination angle.

10. The method of claim 8 , wherein the orbit comprises an orbital period of 6 sidereal hours.

11. The method of claim 8 , wherein the plurality of satellites comprises at least 12 satellites.

12. The method of claim 8 , further comprising:

tracking satellites of the plurality of satellites at the ground station using a first antenna pair dedicated to the first repeating sky track;

tracking satellites of the plurality of satellites at the ground station using a second antenna pair dedicated to the second repeating sky track; and

wherein each respective antenna pair alternatively tracks successively visible satellites along a corresponding sky track for communication between the ground station and respective ones of the plurality of satellites.

13. The method of claim 12 , further comprising:

communicating with communication equipment of a first user terminal with each successive one of the plurality of satellites in the first repeating sky track to continuously receive communications at the first user terminal from the ground station that are relayed from respective ones of the plurality of satellites in the first repeating sky track;

communicating with communication equipment of a second user terminal with each successive one of the plurality of satellites in the second repeating sky track to continuously receive communications at the second user terminal from the ground station that are relayed from respective ones of the plurality of satellites in the second repeating sky track; and

targeting a reception and a transmission pattern of a phased array antenna at each of the first user terminal and the second user terminal along at least one of the first repeating sky track or the second repeating sky track.

14. A method for control of a satellite communications system, comprising:

operating a plurality of satellites each traveling about the Earth in an orbit such that the plurality of satellites have an orbital period that is an integer factor of a sidereal day and all of the plurality of satellites follows a single repeating ground track relative to the surface of the Earth;

equipping each satellite of the plurality of satellites with communication equipment operable to communicate with at least one ground station and a plurality of user terminals to provide data communication service to the plurality of user terminals; and

orienting the orbit of each of the plurality of satellites relative to the Earth to provide continuous satellite visibility to a ground station in a targeted geographic region of the Earth on a first repeating sky track and a second repeating sky track relative to the ground station, wherein the first repeating sky track is different than the second repeating sky track and comprise a different visible satellites in each respective one of the first sky track and the second sky track in any given time;

wherein the orbit for each of the plurality of satellites has at least an orbital period, eccentricity, semimajor axis, inclination, longitude of ascending node, and argument of perigee, and are offset in relation to a satellite epoch for each of the plurality of satellites, and wherein the plurality of satellites are evenly spaced along the single repeating ground track.