In: Physics
Answer the following questions for an orbit with the following Position and Velocity vectors:
(R = 7626I + 4972J + 806K km, V = 0.626I - 0.690J - 6.160K km/s)
1. Determine the size of the size (semimajor axis) of this orbit.
2. Determine the shape (eccentricity) of this orbit.
3. Determine the inclination of this orbit.
4. Determine the right ascension of the ascending node for this orbit.
5. Determine the argument of the perigee for this orbit.
6. Determine the true anomaly for this orbit.