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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![2. For an earth-orbiting satellite, the orbital elements are: h= 79,000km2/s, e = 0.6, N= 50°, i =
110°, o = 15°, and 0 = 40°.
a. Find the state vectors in the gencentric equatorial frame.
b. What is the radius and velocity at perigee?](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F83129e4b-a8ca-4325-a6b9-e0e90b2cb1b8%2F982d8b9f-d60c-4482-b6cb-c267a6d92b98%2Fq75rcosa_processed.jpeg&w=3840&q=75)
Transcribed Image Text:2. For an earth-orbiting satellite, the orbital elements are: h= 79,000km2/s, e = 0.6, N= 50°, i =
110°, o = 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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