I don't have a clue what you did, you have never posted that.
You have to add the change in PEnergy and KE of the satellite.
PE= INT Forcegravity*dh from Re to Rg
KEchange=final KE - Intial KE
now on the initial KE, remember that the launching point has a velocity as the Earth rotates.
I will be happy to critique your thinking on this.
Determine the energy neded to put 5kg, initially at rest on Earth's surface, into geosynchronous orbit.
I get 2.9*10^8 where did I gow wrong?
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