2. For an earth-orbiting satellite, the orbital elements are: h = 79,000km2/s, e=0.6, Q= 50°, i = 110°, = 15°, and 0 = 40°. a. Find the state vectors in the gencentric equatorial frame. b. What is the radius and velocity at perigee?
2. For an earth-orbiting satellite, the orbital elements are: h = 79,000km2/s, e=0.6, Q= 50°, i = 110°, = 15°, and 0 = 40°. a. Find the state vectors in the gencentric equatorial frame. b. What is the radius and velocity at perigee?
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