b) Real satellites are complicated objects (see photo above). To simplify the problem, suppose the satellite is a spherical black body with a 0.3 m radius. Suppose the satellite's electronics generated 3900 Watts. What would be the equilibrium temperature, Teq, of the satellite? Okeedoke, so I started with the equation T=oT^4. So... 3900 J=(5.67x10^-8 W/m^2K^4)T^4 T=(3900 J/(5.67x10^-8 W/m^2 K^4))^(1/4) Which gives me an incorrect answer... any hints in the right direction?