(adsbygoogle = window.adsbygoogle || []).push({}); 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. http://img65.imageshack.us/img65/8821/keplerslawas4.png [Broken]

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# Homework Help: Kepler's Laws Problem

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