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A satellite is to be launched into a sun-synchronous, circular orbit with a period of 103.8 minutes. Hint: Omega_dot for a sun-synchronous orbit is 1.991e-7
A satellite is to be launched into a sun-synchronous, circular orbit with a period of 103.8 minutes. Hint: Omega_dot for a sun-synchronous orbit is 1.991e-7 rad/s. (a) Determine the required altitude of the orbit. (b) Calculate the inclination of the orbit. (c) Find the apsidal rotation rate of the orbit. 2
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Auditing Cases An Active Learning Approach
Authors: Mark S. Beasley, Frank A. Buckless, Steven M. Glover, Douglas F. Prawitt
2nd Edition
0130674842, 978-0130674845
