Assume circular orbits for all calculations and use the following values for R , M , and G .
Radius of the Earth: R=6371km
Mass of the Earth: M=5.972×1024kg
Universal gravitational constant: G=6.674×10−11m3/kg/s2
1) Assume that you launch due east from Cape Canaveral and reach the orbital altitude of the ISS (400 km).
What is the velocity of your spacecraft in this orbit? Give your answer in km/s with at least 2 decimal places.
2)How large a burn is required to change your initial inclination to that of the ISS? Give your answer in km/s with at least 2 decimal places.