Home
Class 10
PHYSICS
A satellite is revolving in an orbit a h...

A satellite is revolving in an orbit a height 20200 km from the suface of the earth . Determine the speed with which the satellite is revolving around the earth. Also calcutate the time taken by the satellite to compete on revolution around the earth.

Text Solution

Verified by Experts

Analyse
Step 1: Analyse the given data in the problem and find out what needs to be calculated.
Given : Height from the surface of the earth =20200 km = `2.02xx10^(7)m`
Also we know values of the basic physical constants like G,M and R :

To find . (i) Tangential velocity `(v_(c))`
(ii) Time period of satellite (T)
Solve
Step 2: Write the formula foe tangential velocity,
`v_(c)=sqrt((GM)/(r))" " (i)`
Before getting started with tedious calcutions , first calculate the radius of the orbit from the centre of the earth.
R is the radius of the earth . As shown in figure ,the radius of the orbit 'r' is (R+H).
`therefore" " r=R+H=6400+20200=26600"km"=2.66xx10^(7)m`
Step 3 : Using equation (i) and substituing know values,
`v_(c)=sqrt((6.67xx10^(-11)xx6xx10^(24))/(2.66xx10^(7)))`
Step 4 : Separate the powers of 10 for simplification .
`thereforev_(c)=sqrt((6.67xx6)/(2.66)xx10^(6))`
For further simplification of calculation , take approximate values and contiue calcution.
`v_(c)~~sqrt((7xx6)/(3)xx10^(6))=sqrt(7xx2)xx10^(3)=sqrt(4)xx10^(3)`
Step 5 : As, 14 is not a perfect square we again use approximation for arriving at the final answer. ltbrlt Find out the upper and lower perfect squares near the required number.
Here, these values would be 9 and 16 . Hence our answer lies somewhere between 3 and 4 Also , 14 is much closer to 16 as compared to 9 which leads us to conclude the approximate value of `sqrt(14)~~3.8.`
`therefore" " v_(c)=3.8xx10^(3)"m/s"or3.8"km/s"`
Step 6 : To complete one revolution around the earth , the satellite travels distance equal to circumference of the orbit.
`therefore" Here,velocity"(v_(c))=("distance")/("time")=(2pir)/(T)rArrT=(2pir)/(v_(c))`
`therefore" " T=(2xx3.14xx2.66xx10^(7))/(3.8xx10^(3))`
Using approximations, .
`T~~=(2xx3xx3)/(4)xx10^(4)=4.5xx10^(4)s`
To convert the time in hours , divide the answer with 3600,
`T=(45000)/(3600)=(25)/(2)=12.5"hours"`
Answer check
without approximation , the answers to velocity of satellite and its time period will be as follows,
`v_(c)=sqrt((6.67xx10^(-11)xx610^(24))/(2.66xx10^(7)))=3878.8"m/s "or3.88" km/s"`
`T=(2xx3.14xx2.66xx10^(7))/(3.88xx10^(3))=43053s=11.96 "hours"`
Promotional Banner

Topper's Solved these Questions

  • SPACE MISSIONS

    TARGET PUBLICATION|Exercise Choose the correct alternative|5 Videos
  • SPACE MISSIONS

    TARGET PUBLICATION|Exercise Complete the paragraph|1 Videos
  • SOCIAL HEALTH

    TARGET PUBLICATION|Exercise CHAPTER ASSESSMENT|3 Videos
  • TOWARDS GREEN ENERGY

    TARGET PUBLICATION|Exercise Chapter Assessment|2 Videos

Similar Questions

Explore conceptually related problems

For a satellite revolving around the earth

A satellite revolving around the earth is

A satellite is revolving round the earth in an elliptical orbit :

A satellite is revolving round the earth in circular orbit

A goestationary satellite revolves around the earth from

What provides the centripetal force to a satellite revolving around the earth ?

Peridic-time of satellite revolving around the earth is (rho density of earth) .

What is the tota, energy of a satellite revolving around Earth ?

A satellite revolving around Earth loses height. How will its time period be changed?