You find out that your competitor has also designed a new satellite! You'd like to figure out what orbital elements they have chosen. After taking measurements of the position and velocity of their spacecraft, you calculate the following: h= 110 E. IJK km²/s, ē = [-02 -0.2 IJK What eccentricity have they chosen for their orbit? Hint: For the following, you won't need the exact values from h, only the direction it is pointing. In degrees, what is the inclination of their orbit? In degrees, what is the right ascension of the ascending node (RAAN) of their orbit? In degrees, what is the argument of perigee w of their orbit?

You find out that your competitor has also designed a new satellite! You'd like to figure out what orbital elements they have chosen. After taking measurements of the position and velocity of their spacecraft, you calculate the following: h= 110 E. IJK km²/s, ē = [-02 -0.2 IJK What eccentricity have they chosen for their orbit? Hint: For the following, you won't need the exact values from h, only the direction it is pointing. In degrees, what is the inclination of their orbit? In degrees, what is the right ascension of the ascending node (RAAN) of their orbit? In degrees, what is the argument of perigee w of their orbit?