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Calculate the velocity of a 1650 kg satellite that is in a circular orbit of 4.2 x 106m above the surface of a planet, which has a radius 3.95 x 105 m and the period of the orbit is 2.0 hours.
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Do you have any formulas that you can use for circular motion?
Not that I know of :l
The problem needs to be solved by applying a formula. Without knowing what the formulas are that can be used to solve this kind of problem, you can't proceed. Find the formulas used for circular motion.
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