If a space based solar power station was built in aereostationary orbit, would it be designed the same as one in geostationary orbit?Would mars's thinner atmosphere allow laser power beaming? (what about dust storms?; if yes could such a system be implemented on an early martian-base-sized small scale?)Is there much advantage from the fact that this orbit is half as wide as the equivalent geostationary orbit. So there is less beam divergence, and a more concentrated beam?