Kepler's third law described the relation between semi-major axis (or average distance to the star) and
the orbital period (how long it takes to complete one lap) as follows: a^3 / p^2 = constant In the case of our Solar system the constant is 1 This means that, for this problem: a^3 / p^2 = 1 p^2 = a^3 p = a^(3/2) The semi major axis is given as 101 million km. We need to convert this into AU where 1 AU is approximately 150 million Km 101 million Km = (101x1) / 150 = 0.67 AU
Now, we substitute in the equation to get the orbital period as follows: p = (0.67)^(3/2) = 0.548 earth years