Question Details

The distance of a geo-stationary satellite from the center of the earth (Radius R = 6400 km) is nearest to

Options

A

5 R

B

7 R

C

10 R

D

18 R

Correct Answer :

7 R

Solution :

The correct option is "7 R".

To understand why this is the correct option, let us go through the step-by-step derivation of the orbital radius of a geostationary satellite.

A geostationary satellite is one that remains stationary relative to a point on the Earth's surface. This means its orbital period, T, must be exactly equal to the rotational period of the Earth about its own axis:
T=24 hours=24×3600 seconds=86,400 s

For a satellite of mass m orbiting the Earth of mass M at a distance r from the center of the Earth, the gravitational force provides the necessary centripetal force for its circular motion:
GMm r2 = mω2r

Since the angular velocity ω is related to the time period T by ω=2πT, we can rewrite the equation as:
GM r2 = 2πT 2 r
Rearranging this formula to solve for the orbital radius r gives:
r3 = GMT2 4π2

We also know that the acceleration due to gravity at the Earth's surface is given by:
g = GM R2
This allows us to substitute GM=gR2 into our equation:
r3 = gR2T2 4π2

Now, substituting the standard values:
• Radius of the Earth, R6.4×106 m
• Acceleration due to gravity, g9.8 m/s2
• Period of rotation, T86,400 s
π3.14

Plugging these numbers in:
r3 9.8 × (6.4×106)2 × 86,4002 4×3.142
Evaluating this expression yields:
r4.2×107 m=42,000 km

To express this distance in terms of the Earth's radius (R=6400 km), we divide the orbital radius by R:
rR 42,0006400 6.56

The value 6.56 is closest to the integer value of 7. Therefore, the distance of a geo-stationary satellite from the center of the Earth is nearest to 7 R.

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