Home
Class 11
PHYSICS
Distance of geostationary satellite from...

Distance of geostationary satellite from the surface of earth radius `(R_(e)=6400 km)` in terms of `R_(e)` is

A

`13.76 R_(e)`

B

`10.76 R_(e)`

C

`6.56 R_(e)`

D

`2.56 R_(e)`

Text Solution

Verified by Experts

The correct Answer is:
C
Doubtnut Promotions Banner Mobile Dark
|

Topper's Solved these Questions

  • GRAVITATION

    ERRORLESS |Exercise Kepler’s Laws of Planetary Motion|51 Videos
  • GRAVITATION

    ERRORLESS |Exercise CT|18 Videos
  • GRAVITATION

    ERRORLESS |Exercise Gravitation Potential, Energy and Escape Velocity|70 Videos
  • FRICTION

    ERRORLESS |Exercise MCQ S|125 Videos
  • MOTION IN ONE DIMENSION

    ERRORLESS |Exercise Motion In One Dimension|24 Videos

Similar Questions

Explore conceptually related problems

Calculate the height of the Apple (India's first geostationary satellite) above the surface of the earth (Radius of the earth = 6400 km and g = 9.8 ms^(-2) )

An object weighs 10 N at north pole of Earth. In a geostationary satellite distance 7 R from centre of Earth (of radius R ), what will be its (a) true weight (b) apparent weight?

Knowledge Check

  • The distance of geostationary satellite from the centre of the earth (radius R) is nearest to

    A
    5 R
    B
    6 R
    C
    7 R
    D
    8 R
  • The distance of a geo-stationary satellite from the centre of the earth is nearest to (where R=6400 km)

    A
    5R
    B
    7 R
    C
    10 R
    D
    18 R
  • What is the approximate height of a geostationary satellite from the surface of the earth?

    A
    981 km
    B
    15000 km
    C
    35,000 km
    D
    55,000 km
  • Similar Questions

    Explore conceptually related problems

    The height of geostationary orbit above the surface of the earth is h. Radius of the earth is R. The earth shrinks to half its present radius (mass remaining unchanged). Now hat will be height of a geostationary satellite above the surface of the earth?

    A geostationary satellite is at a height h above the surface of earth. If earth radius is R -

    The escape velocity from the surface of the earth is (where R_(E) is the radius of the earth )

    What is the approximate height of any geostationary satellite from earth’s surface (in km)?

    If W is the weight of a satellite on the surface of the earth, then the energy required to lauch that satellite from the surface of earth into a circular orbit of radius 3R is (here R is the radius of the earth)