Home
Class 11
PHYSICS
A satellite of mass m moves around the E...

A satellite of mass m moves around the Earth in a circular orbit with speed v. The potential energy of the satellite is

A

`1/2 mv^(2)`

B

`-1/2mv^(2)`

C

`3/4mv^(2)`

D

`5/4mv^(2)`

Text Solution

Verified by Experts

The correct Answer is:
B
Promotional Banner

Topper's Solved these Questions

  • GRAVITATION

    NARAYNA|Exercise EXERCISE -I (C.W.)|50 Videos
  • GRAVITATION

    NARAYNA|Exercise EXERCISE -I (H.W.)|56 Videos
  • GRAVITATION

    NARAYNA|Exercise EVALUATE YOURSELF-4|8 Videos
  • FRICTION

    NARAYNA|Exercise Passage type of questions I|6 Videos
  • KINETIC THEORY OF GASES

    NARAYNA|Exercise LEVEL-III(C.W)|52 Videos

Similar Questions

Explore conceptually related problems

A satellite moves around the earth in a circular orbit with speed v . If m is the mass of the satellite, its total energy is

If a satellite of mass 400 kg revolves around the earth in an orbit with speed 200 m/s then its potential energy is

If a satellite of mass 400 kg revolves around the earth in an orbit with speed 200 m/s then its potential energy is

A satellite is moving with constant speed V in a circular orbit around earth. The kinetic energy of the satellite is

A satellite is revolving around the earth in a circular orbit of radius r with speed v. What will be the effect on speed f satellite if radius is decreased by 5% ?

A satellite is revolving around earth in a circular orbit. At some instant the speed of the satellite is increased sqrt(2) times its orbital speed keeping its direction unchanged. Then, the new path of the satellite is :

A satellite is moveing in a circular orbit around the earth. The total energy of the satellite is E=-2xx10^(5) J . The amount of energy to be imparted to the satellite to transfer it to be orbit where its potential energy is U=-2xx10^(5)J is equal to ................

A satellite of mass m_0 is revolving around the earth in circular orbit at a height of 3R from surface of the earth the areal velocity of satellite is (where R is radius of earth and M_0 is the mass of earth)