Allie B.

asked • 06/26/20

I need the answer to this plz

The velocity of the satellite orbiting Earth is related to the distance the satellite is from the center of the Earth by the function, v=(sqrt)1.24•10^12/r, where the v is velocity in miles per hour and r is the distance from the center of the Earth in miles.


1)GPS satellites travel in mid Earth orbits. If mid Earth orbit is from 4077 to 26197 miles from the center of the Earth, What is the domain and range of the function?


2)What is the inverse of the function?


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