How can this be wrong? (Simple circular motion)

AI Thread Summary
The discussion revolves around calculating the centripetal acceleration of a satellite in a circular orbit 730 km above Earth's surface with a period of 99.2 minutes. The initial calculation for velocity was performed using the formula v = distance/time, where the distance was calculated as 2πR. However, the mistake identified was not accounting for the Earth's radius when determining the total radius of the orbit. The correct approach requires adding Earth's radius to the altitude of the satellite to find the true radius of the orbit. This clarification emphasizes the importance of using the correct radius in centripetal acceleration calculations.
lando45
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"An Earth satellite moves in a circular orbit 730 km above the Earth's surface. The period of the motion is 99.2 min. What is the magnitude of the centripetal acceleration of the satellite?"

OK so to solve this I used the formula centripetal acceleration = v^2/r

To calculate velocity (v) I did the following:

v = distance traveled (d) / time taken (t)
d = 2piR = 2 x pi x 730,000 = 4586725.274m
t = 99.2 x 60 = 5952s
v = d/t = 4586725.274/5952 = 770.619ms^-1

Then we already have r which is 730,000m so v^2/r is:

770.619^2/730,000 = 0.813ms^-2

But this is answer is wrong...HOW?!
 
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From is where is the radius of the orbit measured?
 
Ah! So I need to add the radius of planet Earth to the overall radius?
 
lando45 said:
Ah! So I need to add the radius of planet Earth to the overall radius?

You aren't given an overall radius, you are given the height above the Earth's surface. You need to find the radius of the circle that is the orbit.

It looks like you're basically on the right track.
 
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