If we have the satellite state vector and the station coordinates and the modified julian date, how can we find topocentric right ascension and declination, azimuth and elevation.

International Edition---engineering Mechanics: Statics, 4th Edition
4th Edition
ISBN:9781305501607
Author:Andrew Pytel And Jaan Kiusalaas
Publisher:Andrew Pytel And Jaan Kiusalaas
Chapter9: Moments And Products Of Inertia Of Areas
Section: Chapter Questions
Problem 9.22P
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If we have the satellite state vector and the station coordinates and the modified julian date, how can we find topocentric right ascension and declination, azimuth and elevation.

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