The GPS satellites are at an altitude that gives them an orbit of 12* hours. 
But during that time the earth has made half a rotation. Thus it takes -two- SV 
orbits and -one- earth rotation to get back to the same geometry. It is this 
24* hour ground-track repeat time that is of interest in high-precision work.

That's why you often see GPS time-transfer data based on days*, rather than 
just a few thousand seconds or 12 hours. This is not likely to affect any of 
you working on home GPSDO projects. But it is a concern for the folks that do 
positioning at mm levels.

* Fun facts:
1) Right, it's not actually 24 hours (solar day); instead it's closer to 23h 
56m (sidereal day).
2) However, if you look closely you find it's not precisely a sidereal day 
(86164 s) either; instead the repeat time is closer to 86155 s, due to 
gravitational effects (inclined orbits, non-spherical earth).
3) If you look even closer you find each SV has its own repeat time; 86155 is 
merely the constellation average.
4) Also the per-SV repeat times are not constant; they slowly drift by about 10 
seconds a year. As the orbit decays and the repeat time gets out of spec, an 
orbital maneuver puts the SV back.

For a nice description of this effect, here's a short 2-page summary:
http://www.insidegnss.com/pdf/ig0806_gnss-solutions.pdf

For deeper technical details, start with these papers:
http://spot.colorado.edu/~kristine/gpsrep.pdf
http://www.isprs.org/proceedings/XXXVII/congress/4_pdf/162.pdf
http://web.gps.caltech.edu/classes/ge167/file/Ragheb2007.pdf

And finally, to see the effect on a GPSDO, I have some ADEV plots at:
http://leapsecond.com/pages/sidereal/
http://leapsecond.com/pages/sidereal/14years.htm

/tvb
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