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What is the period of a satellite orbiting around the earth in a radius which is one half that of the distance from the earth to the moon?

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Answer:

The satellite has a period of 204.90 days

Step-by-step explanation:

The period can be determine by means of Kepler's third law:


T^(2) = r^(3) (1)

Where T is the period of revolution and r is the radius.


\sqrt{T^(2)} = \sqrt{r^(3)}


T = \sqrt{r^(3)} (2)

The distance between the moon and the Earth has a value of 384400 km, therefore:


r = (384400km)*(0.50)


r = 192200 km

Finally, equation 2 can be used:


T = \sqrt{(192200)^(3)}


T = 84261672 km

However, the period can be expressed in days, to do that it is necessary to make the conversion from kilometers to astronomical units:

An astronomical unit (AU) is the distance between the Earth and the Sun (
1.50x10^(8) km)


T = 84261672 km \cdot (1AU)/(1.50x10^(8) km)
0.561 AU

But 1 year is equivalent to 1 AU according to Kepler's third law, since 1 year is the orbital period of the Earth.


T = 0.561 AU \cdot (1year)/(1AU)
0.561 year


T = 0.561 year \cdot (365.25 days)/(1year)
204.90 days


T = 204.90 days

Hence, the satellite has a period of 204.90 days.

User Amr Bahaa
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