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## Homework Statement

Suppose that a satellite is in a circular orbit at a height of 2.00x10^6 m above Earth's surface. What is the tangential speed of a satellite in this orbit?

## Homework Equations

v

_{t}=rw

## The Attempt at a Solution

I have been stuck for almsot 30 minutes, I think that the height is the radius but then I have no method of finding the angular speed.