Using the equation P2 = (4 * pi2 * a3)/(G(M+m)) to find the orbital period of Earth where:
P = orbital period
a = semi-major axis = 1.50e11 m
G = 6.67e-11 m3 kg-1 s-2
M = mass of sun (in this case) = 1.989e30 kg
m = mass of Earth = 5.972e24 kg
I have been trying to find the orbital...