Satellite-position table messaging

1. A method of operating a navigation receiver, comprising:

whenever a navigation receiver has ephemeris information unavailable to it directly from orbiting navigation satellites because of weak signal conditions, then:

accepting a partial-ephemeris in a satellite-position table message from a network host that lacks at least one of the two harmonic corrections to inclination angle, Cic and Cis, of the flight trajectory of a particular orbiting navigation satellite, wherein said network host has stripped out such data from a complete almanac collected by a reference station at another location;

computing a position solution using said reduced ephemeris information from said satellite-position table message; and

outputting said position solution with an accuracy degraded due to having omitted either of said two harmonic corrections to inclination angle, Cic and Cis, in the step of computing.

2. The method of claim 1 , wherein:

the step of receiving is such that both of said two harmonic corrections to inclination angle, Cic and Cis, are missing and set to zero.

3. The method of claim 1 , wherein:

the step of receiving is such that a fee is charged to receive such satellite-position table message.

4. The method of claim 1 , wherein:

the step of receiving is such that said satellite-position table message is provided over an Internet connection from a reference station and network host.

5. A method of operating a navigation receiver, comprising:

receiving from an information source, other than an orbiting navigation satellite, a satellite-position table message that is the equivalent of the ephemeris for a particular satellite lacking at least one of the two harmonic corrections to inclination angle, Cic and Cis;

computing a position solution using said reduced ephemeris information from said satellite-position table message; and

outputting said position solution with an accuracy degraded less than a meter by having omitted either of said two harmonic corrections to inclination angle, Cic and Cis, in the step of computing;

wherein, the step of computing is such that the one of the two harmonic corrections to inclination angle, Cic and Cis,

which is omitted from the computation, can be mathematically expressed as depending on Min(C is sin(2φ k ), C ic cos(2φ k )).

6. A navigation receiver client, comprising:

an input for receiving an information source, other than an orbiting navigation satellite, a satellite-position table message that is the equivalent of the ephemeris for a particular satellite lacking at least one of the two harmonic corrections to inclination angle, Cic and Cis;

a radio for receiving microwave transmissions and measuring pseudoranges from orbiting satellite vehicles in which their respective data related to their ephemerides is unobtainable; and

a position solution output in which a position solution is determined from said pseudoranges and said satellite-position table message with at least one of the two harmonic corrections to inclination angle, Cic and Cis, set to zero;

wherein, a navigation receiver can continue to operate when ephemeris information directly from orbiting navigation satellites is unavailable to it because of weak signal conditions.

7. The navigation receiver client of claim 6 , wherein:

the input receives information obtained over the Internet for a fee.

8. The navigation receiver client of claim 6 , wherein:

the input is such that said satellite-position table message is provided over an Internet connection from a reference station and network host.