What is the Orbital Speed of a Satellite in a Circular Orbit?

AI Thread Summary
The discussion revolves around calculating the orbital speed of satellites in circular orbits and the period of the moon's orbit around Earth. For the first satellite with a known speed and radius, the second satellite's speed can be derived using the relationship between orbital speed and radius. The provided answer for the second satellite's speed is 1.3 x 10^4 m/s. For the second question regarding the moon, the mass of the Earth and the radius are used to determine the orbital period, with Kepler's third law being suggested as a useful approach. Additional guidance is sought for solving the first question effectively.
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Homework Statement



#1
A satellite is in a circular orbit around an unknown planet/ The satellite has a speed of 1.70 x 104 m/s, and the radius of the orbit is 5.25 x 106 m. A second satellite also has a circular orbit around this same planet. The orbit of this second satellite has a radius of 8.60 x 10^6 m. What is the orbital speed of the second satellite.

#2
The moon orbits the Earth at a distance of 3.85 x 108 m. Assume that this distance is between the centers of the Earth and the moon and that the mass of the Earth is 5.98 x 1024 kg. Find the period for the moon's motion around the Earth. Express the answer in days and compare it to the length of a month.

Homework Equations



I have no clue. Maybe this?

v = sqrt(GM/r)

F = G (m1m2/r2)

a = v2 / r

a = 4pi2r / T2

The Attempt at a Solution



# 1: Well, I know there is something that the two satellites could be compared to, but I can't figure what. I tried a futile stab at the question by using v12 / r = v22 / r but that didn't give me the right answer.

The answer at the back of the book is 1.3 x 104 m/s.

# 2: I don't even know how to get started on this question...I know I have radius and mass of the Earth, and I need to find the period.

Any help towards these questions would be greatly appreciated!
 
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v = \frac{2{\pi}r}{T}

Should help you in the second part if you equate it to another equation with known variables.
 
Start with Kepler's 3rd law.
 
Thanks! I got #2 with the formula T = ( 2 pi r3/2 ) / sqrt(GMe).


But I still don't get #1. Can I get some more pointers?
 
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