Question #162674

A satellite orbits the earth in a circle of radius 6570km find the speed of the satellite and time taken to complete one revolution


1
Expert's answer
2021-02-10T21:37:41-0500

a)

v=GMER,v=\sqrt{\dfrac{GM_E}{R}},v=6.671011 Nm2kg25.971024 kg6.57106 m=7785 ms.v=\sqrt{\dfrac{6.67\cdot10^{-11}\ \dfrac{Nm^2}{kg^2}\cdot5.97\cdot10^{24}\ kg}{6.57\cdot10^6\ m}}=7785\ \dfrac{m}{s}.

b)

T2R3=4π2GME,\dfrac{T^2}{R^3}=\dfrac{4\pi^2}{GM_E},T=4π2R3GME,T=\sqrt{\dfrac{4\pi^2R^3}{GM_E}},T=4π2(6.57106 m)36.671011 Nm2kg25.971024 kg=5302 s1 h3600 s=1.47 h.T=\sqrt{\dfrac{4\pi^2\cdot(6.57\cdot10^6\ m)^3}{6.67\cdot10^{-11}\ \dfrac{Nm^2}{kg^2}\cdot5.97\cdot10^{24}\ kg}}=5302\ s\cdot\dfrac{1\ h}{3600\ s}=1.47\ h.

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