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NCERT Exemplar · Q30

Q.Show the nature of the following graph for a satellite orbiting the earth.

(a) KE vs orbital radius RR
(b) PE vs orbital radius RR
(c) TE vs orbital radius RR.
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For a satellite in a circular orbit around Earth, Kinetic Energy (KE) is positive and inversely proportional to the orbital radius RR, while Potential Energy (PE) and Total Energy (TE) are negative and also inversely proportional to RR. The graphs for KE, PE, and TE versus RR are all hyperbolic in nature.

When a satellite orbits the Earth, its energy is a combination of its kinetic energy due to motion and its gravitational potential energy due to its position in Earth's gravitational field. Understanding how these energies change with the orbital radius RR is fundamental to orbital mechanics.

The key idea here is that for a stable circular orbit, the gravitational force provides the exact centripetal force required. This balance allows us to express the satellite's speed, and consequently its kinetic energy, in terms of the orbital radius. The potential energy is defined relative to infinity, where it is considered zero.

Let's consider a satellite of mass mm orbiting the Earth of mass MM in a circular orbit of radius RR. GG is the universal gravitational constant.

  1. Kinetic Energy (KE) of the Satellite For a satellite in a stable circular orbit, the gravitational force provides the necessary centripetal force. The gravitational force is Fg=GMmR2F_g = \frac{GMm}{R^2}. The centripetal force required for circular motion is Fc=mv2RF_c = \frac{mv^2}{R}, where vv is the orbital speed. Equating these forces:

GMmR2=mv2R\frac{GMm}{R^2} = \frac{mv^2}{R}

From this, we can find the square of the orbital speed:

v2=GMRv^2 = \frac{GM}{R}

The kinetic energy (KE) of the satellite is given by $KE = \frac{1}{2}mv^2$. Substituting the expression for $v^2$:

KE=12m(GMR)KE = \frac{1}{2}m \left(\frac{GM}{R}\right)

KE=GMm2RKE = \frac{GMm}{2R}

*   **Nature of the graph for KE vs $R$:**
    *   KE is always positive.
    *   KE is inversely proportional to $R$ ($KE \propto \frac{1}{R}$).
    *   As $R$ increases, KE decreases.
    *   The graph will be a hyperbola in the first quadrant, approaching zero as $R$ tends to infinity.

2. Gravitational Potential Energy (PE) of the Satellite

The gravitational potential energy of a mass mm at a distance RR from a mass MM is defined as the work done to bring the mass mm from infinity to that distance RR. By convention, potential energy at infinity is taken as zero.

> [!FORMULA]

> The gravitational potential energy is given by:

> PE=−GMmRPE = -\frac{GMm}{R}

* Nature of the graph for PE vs RR:

* PE is always negative. This indicates that the satellite is bound to the Earth's gravitational field.

* PE is inversely proportional to RR (PE∝−1RPE \propto -\frac{1}{R}).

* As RR increases, the value of PE becomes less negative (i.e., it increases towards zero).

* The graph will be a hyperbola in the fourth quadrant, approaching zero from below as RR tends to infinity.

  1. Total Mechanical Energy (TE) of the Satellite The total mechanical energy (TE) of the satellite is the sum of its kinetic energy and potential energy:

TE=KE+PETE = KE + PE

Substituting the expressions for KE and PE:

TE=GMm2R+(−GMmR)TE = \frac{GMm}{2R} + \left(-\frac{GMm}{R}\right)

TE=GMm2R−2GMm2RTE = \frac{GMm}{2R} - \frac{2GMm}{2R}

$$ TE = -\frac{GMm}{2R} $$ …

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