Question: Kepler's third law of planetary motion

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SUMMARY

The discussion centers on applying Kepler's Third Law of planetary motion to calculate the distance of an artificial satellite from Earth based on its orbital period. The user attempts to use the formula (Ta/Tb)^2 = (rA/rB)^3, where Ta is the satellite's period (8.5 days) and Tb is the moon's period (27.3 days), with rB being the mean distance to the moon (3.84x10^8 m). The user encounters an error in calculating the cube root of rA, leading to confusion regarding the correct application of exponent rules. The correct distance for the satellite is determined to be approximately 1.76x10^8 m.

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Jess048
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The mean distance between the Earth and the moon is 3.84x10^8 m, and the moon has an orbital period of 27.3 days. Find the distance from Earth of an artificial satellite that has an orbital period of 8.5 days.
a. 1.76x10^8 m
b. 1.76x10^4 m
c. 1.76x10^10 m
d. 5.24x10^8 m

So far I got:
I used the formula: (Ta/Tb)^2 = (rA/rB)^3
Plugged in these values:
Ta= 8.5 days
Tb= 27.3 days
rA= ?
rB= 3.84x10^8 m

rA^3=(3.84x10^8)^3(8.5/27.3)^2
=(5.489164304x10^24)^1/3
rA^3=1.829721435x10^24
This obviously is incorrect. Please help thanx!
 
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Is (10^24)^(1/3)=10^24? Something is going seriously wrong with your cube root.
 
Last edited:

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