Home
Class 10
PHYSICS
How much time a satellite in an orbit ...

How much time a satellite in an orbit at height 35780 km above earth's surface would take , if the mass of the earth would have been four time its original mass ?

Text Solution

Verified by Experts

Given : New Mass of Earth (M) ` = 4 xx (6 xx 10^(24))kg`
`= 24 xx 10^(24) kg`.
Altitude of the satellite (h) ` = 35780 km` .
` = 35780 xx 10^(3)m`
To find : Time required for revolution . (T) = ?
Formulae : `V = sqrt((GM)/(R+h))`
`T = (2pi (R+h))/(v)`
Solution : `V = sqrt((GM)/(R+h))`
` therefore V = sqrt((6.67 xx 10^(-11) xx 24 xx 10^(24))/(6.4 xx 10^(6) + 35780 xx 10^(3)))`
`therefore V = sqrt(37.59 xx 10^(6))`
` V = 6.160 km //s`
` T = (2 pi (R + h))/(v)`
` = ( 2 xx 3.14 xx 6400 + 35780)/(6.16)`
` = 43001. 68 sec`
` T = 11.94 hr ~ 12 ` hours .
`therefore` The satellite will take approximately 12 hours to revolve around earth.
Promotional Banner

Topper's Solved these Questions

  • SPACE MISSIONS

    CHETAN PUBLICATION|Exercise DEFINE THE FOLLOWING|7 Videos
  • SPACE MISSIONS

    CHETAN PUBLICATION|Exercise WRITE SHORT NOTES :|4 Videos
  • SPACE MISSIONS

    CHETAN PUBLICATION|Exercise CHOOSE AND RE - WRITE WITH THE CORRECT OPTIONS|10 Videos
  • SOCIAL HEALTH

    CHETAN PUBLICATION|Exercise ASSIGNMENT - 9|12 Videos
  • TOWARDS GREEN ENERGY

    CHETAN PUBLICATION|Exercise ASSIGNMENT - 5|13 Videos

Similar Questions

Explore conceptually related problems

An artificial satellite is at a height of 35780 km from the Earth's surface .What is the period of revolution of this satellite ?

A geostationary satellite is orbiting the earth at a height of 5R above the surface of the earth, R being the radius of the earth. Find the time period of another satellite at a height of 2R from the surface of the earth.

The acceleration due to gravity at a height 1 km above the earth is the same sa at depth d below the surface of earth . Then

A geo-stationary satellite is orbiting the Earth of a height of 6R above the surface of Earth R being the radius of the Earth calculate the time period of another satellite at a height of 2.5R from the surface of Earth.

A satellite of mass 1000 kg is supposed to orbit the earth at a height of 2000 km above the earth's surface. Find a. its speed in the orbit b . its kinetic energy.

A satellite is projected vertically upwards from an earth station. At what height above the earth's surface will the force on the satellite due to the earth be reduced to half its value at the earth station? (Radius of the earth is 6400 km.)

Orbit of a satellite between 180 km .to 2000km from Earth's surface .

Orbital velocity V = sqrt((GM)/(R+h)) Suppose the orbit of a satellite is exactly 35780 km above the earth's surface , how much time the satellite will take to complete one revolution around the earth ?

A simple pendulum has a time peirod T_(1) when on the earth's surface & T_(2) when taken to a height & above the earth's surface, where R is the radius of the earth. What is the value of T_(2)//T_(1) ?

A remote sensing satellite of the Earth revolves in a circular orbit at a height of 250 km above the Earth's surface. What is the (i) Orbital speed and (ii) period of revolution of the satellite. Radius of the Earth, R=6.38xx10^(6)m , and acceleration due to gravity on the surface of the Earth, g=9.8ms^(-2)