Robert,

I amended the computer program and ran it through again, using 171.5 days for thrust directed towards the World and 171.5 days for thrust directed away from the World.

Assuming Eqs. 9 and 11 in "Geosynchronous satellites in a geostationary universe" hold, then we obtain

v = 0 m/s
s = 1.062 x 10^9 m

This would result in a satellite over 30.5x higher than the altitude of the 'parking orbit'.

I will now try to obtain further details.

Neville.

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