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Question

A satellite is in a circular orbit around an unknown planet. The satellite has a speed of 1.70×104ms-1, and radius of the orbit is 5.25×106m. A second satellite also has a circular orbit around the same planet. The orbital radius of second satellite is 8.6×106m. Determine the orbital speed of the second satellite.


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Solution

Orbital speed equation:

Consider a satellite with mass ‘m’ orbiting around a central body of mass M.

Let R be the radius of orbit for a satellite, then the velocity of a satellite moving around a central body, v=GMR, and G is the gravitational constant.=6.67×10-11Nm2kg-2.

So, vα1R(1)

Given data and calculation:

For the first satellite, orbital speed is v1=1.70×104ms-1 and the radius of the orbit is R1=5.25×106m

For the second satellite, the orbital radius is R2=8.6×106m

Let v2 be the orbital speed of the second satellite.

Using (1) we can compare the orbital velocities of satellites as

v1v2=R2R1v2=v1×R2R1

Substituting the given values,

v2=1.7×104×5.25×1068.6×106=1.33×104ms-1

Thus, the orbital speed of the second satellite is 1.33×104ms-1


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