# Kepler’s Third Law – statement, equation & derivation [class 11]

Last updated on June 4th, 2023 at 02:25 pm

We will **derive the equation for** **Kepler’s Third Law** using the concept of the Period of Revolution and the equation of orbital velocity. In this process, the equation of the Time Period Of Revolution of the Earth satellite would be derived as well. We’ll also solve sample numerical problems here using this law. This post is useful for class 11 students studying physics. So let’s start!

**Kepler’s Third Law** **[statement]**

Kepler’s Third Lawor 3^{rd}Law of Kepler is an important Law of Physics, which talks about theperiod of its revolutionandhowthe.period of revolution of a satellite depends on the radius of its orbitThis law states that the square of the Orbital Period of Revolution is directly proportional to the cube of the radius of the orbit.

**Time Period of Revolution of Earth’s satellite & derivation of its Equation**

Say, the Period of revolution is T and the radius of the orbit is r.

And **r = R + h** = Radius of the earth + height of the satellite from the surface of the earth.

So the **period of revolution = T = (2 π r) /V, **where V is the Orbital Velocity of the satellite. …………. (1)

Now from the previous post on the Orbital Velocity of a Satellite, we know that orbital velocity can be expressed as **V = R √(g/r) = R (g/r) ^{1/2}**

Here g is the acceleration due to gravity and R is the radius of the earth** **…………….(2)****[ ready Reference: Orbital Velocity ]**

From equations 1 and 2, we get,

T = (2 **π** r)/V = [(2 **π** r)] /[R (g/r)^{(1/2)}]

=[ 2**π** / R]. √[r^{3}/g]

Here we get an important equation for the

Period of Revolution of Earth satellite:

T = [ 2π / R]. √[rwhere R is the radius of the earth and r = R + h^{3}/g] …………………(3)

In the next section, we will use the above equation to **derive Kepler’s Third Law**

**Derivation of Kepler’s Third Law**

The period** of Revolution of Earth’s satellite** can be expressed as **T = [ 2π / R]. √[r ^{3}/g]** [derived above, see equation 3]

Now if we square both sides of the above equation we get the following:

**T^2** =[ (4 . **π**^{2})/(R^{2})]. **r ^{3}**/g ……………………………(4)

Here, **(4. π ^{2})/(R^{2})** and

**g**are constant as the values of

**π (**Pi), g, and R are not changing with time.

So we can say,

T. …………….. (5) .[^{2}∝ r^{3}Kepler’s Third Law equation]

Here, Kepler’s Third Law equation says that the

square of the Orbital Periodof Revolution is directly proportional to thecube of the radius of the orbit.

If the orbit is not circular in the truest sense and rather elliptical, then this law states like this,

the square of the Orbital Period of Revolution varies with the cube of the semi-major axis of the orbit. This is known asKepler’s Third Law.

From this equation of **Kepler’s Third Law,** it comes out clear that the mass of the object in the revolution has no effect on the Period of Revolution.

And this law is applicable to the revolution of any planet and satellite.

Now let’s solve a numerical problem using this formula, in the next paragraph.

**Numerical Problem based on Kepler’s 3rd law**

Two satellites Y and Z are rotating around a planet in a circular orbit. The radii of the orbits for Y and Z are 4R and R respectively. Now if the speed of Y satellite is 3v then what is the speed of satellite Z?

**Solution:**

**We would use Kepler’s third law here.**

**Say, the radius of the orbit of Y and Z are Ry and Rz respectively.As given data, Ry = 4R and Rz = R**

From the 3rd Law of Kepler,

Ty^2/Tz^2 =Ry^3/Rz^3 = (4R)^3/R^3 = 64. So, Ty/Tz = 8 ……………. (1)

Continuing with this equation (equation 1) and bringing in the orbital velocity in it we get:

(2 **π **Ry/Vy) / (2 **π** Rz/Vz) = 8

=> (Ry Vz) /(Rz Vy) = 8

=> (Ry/Rz).(Vz/Vy) = 8

=> (4R/R) .(Vz/Vy) = 8

=> (Vz/Vy) = 8/4 = 2

=> **Vz = 2. Vy = 2. 3v = 6v**

**So the speed of satellite Z is 6v (answer)**

**Numerical Problem based on the Period of Revolution of the satellite**

Q1) What is the value of thePeriod of Revolution of the Earth satellite? ignore the height of the satellite above the surface of theearth.

Given: gravitational acceleration (g) = 10 m/s^2. Radius of earth = R = 6400 km. Take π as 3.14

**Solution:**

Period of revolution = T = [ 2π / R]. √[r ^3/g]

Here r = R + h. As h is to be ignored according to the question, so r =R here.So T = 2

π √(R/g) ……………. (1)

Given: R= 6400 km = 6400 X 10^3 meter. g = 10 m/s^2Putting the values given, we get,T = 2 X 3.14 X

√ [(6400X10^3)/10] = 2 X 3.14 X 800 = 5024 seconds = 83.73 minutes.

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