
A satellite is orbiting around the earth. In a particular orbit its time period is $ T $ and orbital speed is $ V $ . In another orbit the orbital speed is $ 2V $ , then time period will be
(A) $ 8T $
(B) $ 2T $
(C) $ T/2 $
(D) $ T/8 $
Answer
219k+ views
Hint: The orbital speed and the time period of a satellite in a particular orbit are given as, $ T \propto {V^{ - 3}} $ . So for the 2 cases we take the ratio of the time period and hence get the time period in the second case.
Formula Used In this solution we will be using the following formula,
$ T \propto {V^{ - 3}} $
where $ T $ is the time period and $ V $ is the orbital velocity.
Complete Step by Step Solution
In the problem we are given the time period and the orbital speed of a satellite in an orbit around the earth. The relation is given by,
$ T \propto {V^{ - 3}} $
So in the first case let us consider the time period as $ T $ and the orbital speed as $ V $
Hence the equation remains as,
$ T \propto {V^{ - 3}} $
In the second case let us consider the time period as $ T' $ and the orbital speed as $ V' $
So the relation in the second case will be,
$ T' \propto {V'^{ - 3}} $
Now according to the question we can write,
$ V' = 2V $
So substituting this value we get,
$ T' \propto {\left( {2V} \right)^{ - 3}} $
Now we can take the ratio of the time period in the second case to the first case as,
$ \dfrac{{T'}}{T} = \dfrac{{{{\left( {2V} \right)}^{ - 3}}}}{{{V^{ - 3}}}} $
Therefore, the $ V $ gets cancelled in this equation. So we get,
$ \dfrac{{T'}}{T} = \dfrac{{{{\left( 2 \right)}^{ - 3}}}}{1} $
Therefore, the time period in the second case will be,
$ T' = \dfrac{1}{{{2^3}}}T $
Hence the time period is, $ T' = \dfrac{T}{8} $
So the correct option is D.
Note:
The time period of a satellite in an orbit is given by,
$ T = 2\pi \sqrt {\dfrac{{{r^3}}}{{GM}}} $
and the orbital speed is given by,
$ V = \sqrt {\dfrac{{GM}}{r}} $
Hence we can write this as,
$ V = {\left( {\dfrac{{GM}}{r}} \right)^{1/2}} $
Therefore, in the formula for the time period, we can multiply $ GM $ in the numerator and the denominator as,
$ T = 2\pi \sqrt {\dfrac{{{r^3}}}{{GM}} \times \dfrac{{{{\left( {GM} \right)}^2}}}{{{{\left( {GM} \right)}^2}}}} $
Therefore, we can simplify this as,
$ T = 2\pi GM\sqrt {\dfrac{{{r^3}}}{{{{\left( {GM} \right)}^3}}}} $
We can write the terms in the root as,
$ T = 2\pi GM{\left[ {{{\left( {\dfrac{{GM}}{r}} \right)}^{1/2}}} \right]^{ - 3}} $
Therefore we can write this in terms of velocity as,
$ T = 2\pi GM{V^{ - 3}} $
Since $ 2\pi GM $ are constant, hence
$ T \propto {V^{ - 3}} $ .
Formula Used In this solution we will be using the following formula,
$ T \propto {V^{ - 3}} $
where $ T $ is the time period and $ V $ is the orbital velocity.
Complete Step by Step Solution
In the problem we are given the time period and the orbital speed of a satellite in an orbit around the earth. The relation is given by,
$ T \propto {V^{ - 3}} $
So in the first case let us consider the time period as $ T $ and the orbital speed as $ V $
Hence the equation remains as,
$ T \propto {V^{ - 3}} $
In the second case let us consider the time period as $ T' $ and the orbital speed as $ V' $
So the relation in the second case will be,
$ T' \propto {V'^{ - 3}} $
Now according to the question we can write,
$ V' = 2V $
So substituting this value we get,
$ T' \propto {\left( {2V} \right)^{ - 3}} $
Now we can take the ratio of the time period in the second case to the first case as,
$ \dfrac{{T'}}{T} = \dfrac{{{{\left( {2V} \right)}^{ - 3}}}}{{{V^{ - 3}}}} $
Therefore, the $ V $ gets cancelled in this equation. So we get,
$ \dfrac{{T'}}{T} = \dfrac{{{{\left( 2 \right)}^{ - 3}}}}{1} $
Therefore, the time period in the second case will be,
$ T' = \dfrac{1}{{{2^3}}}T $
Hence the time period is, $ T' = \dfrac{T}{8} $
So the correct option is D.
Note:
The time period of a satellite in an orbit is given by,
$ T = 2\pi \sqrt {\dfrac{{{r^3}}}{{GM}}} $
and the orbital speed is given by,
$ V = \sqrt {\dfrac{{GM}}{r}} $
Hence we can write this as,
$ V = {\left( {\dfrac{{GM}}{r}} \right)^{1/2}} $
Therefore, in the formula for the time period, we can multiply $ GM $ in the numerator and the denominator as,
$ T = 2\pi \sqrt {\dfrac{{{r^3}}}{{GM}} \times \dfrac{{{{\left( {GM} \right)}^2}}}{{{{\left( {GM} \right)}^2}}}} $
Therefore, we can simplify this as,
$ T = 2\pi GM\sqrt {\dfrac{{{r^3}}}{{{{\left( {GM} \right)}^3}}}} $
We can write the terms in the root as,
$ T = 2\pi GM{\left[ {{{\left( {\dfrac{{GM}}{r}} \right)}^{1/2}}} \right]^{ - 3}} $
Therefore we can write this in terms of velocity as,
$ T = 2\pi GM{V^{ - 3}} $
Since $ 2\pi GM $ are constant, hence
$ T \propto {V^{ - 3}} $ .
Recently Updated Pages
Two discs which are rotating about their respective class 11 physics JEE_Main

A ladder rests against a frictionless vertical wall class 11 physics JEE_Main

Two simple pendulums of lengths 1 m and 16 m respectively class 11 physics JEE_Main

The slopes of isothermal and adiabatic curves are related class 11 physics JEE_Main

A trolly falling freely on an inclined plane as shown class 11 physics JEE_Main

The masses M1 and M2M2 M1 are released from rest Using class 11 physics JEE_Main

Trending doubts
JEE Main 2026: Application Form Open, Exam Dates, Syllabus, Eligibility & Question Papers

Derivation of Equation of Trajectory Explained for Students

Hybridisation in Chemistry – Concept, Types & Applications

Understanding the Angle of Deviation in a Prism

Understanding Collisions: Types and Examples for Students

Understanding Atomic Structure for Beginners

Other Pages
JEE Advanced Marks vs Ranks 2025: Understanding Category-wise Qualifying Marks and Previous Year Cut-offs

Units And Measurements Class 11 Physics Chapter 1 CBSE Notes - 2025-26

NCERT Solutions For Class 11 Physics Chapter 8 Mechanical Properties Of Solids

Motion in a Straight Line Class 11 Physics Chapter 2 CBSE Notes - 2025-26

NCERT Solutions for Class 11 Physics Chapter 7 Gravitation 2025-26

How to Convert a Galvanometer into an Ammeter or Voltmeter

