1. The problem statement, all variables and given/known data An asteroid of mass m is in circular orbit of radius r around the sun with speed v.It has an impact with another asteroid of mass M and is kicked into a new circular orbit with a speed 1.5v.What is the radius of the new orbit in terms r? 2. Relevant equations (v1)^2/(v2)^2 = (r2)^2 / (r1)^2 3. The attempt at a solution is it using equations based on kepler's second law or third law.