1. The problem statement, all variables and given/known data What would be the period of a satellite moving around the sun between the orbits of the Earth adn Mars at a mean distance of 2.00 x 10^11 m? 2. Relevant equations R^3/T^2 = 3.35 x 10^18 m^3/s^2 for all objects orbiting the sun. 3. The attempt at a solution I am so confused how to solve this problem. I set it up like this so far but im really not sure what to do next/how to start solving the problem.