Home
Class 11
PHYSICS
Is it possible to put an artificial sate...

Is it possible to put an artificial satellite in an orbit in such a way that it always remain visible directly over New Delhi ?

Text Solution

Verified by Experts

The correct Answer is:
NA
Since New Delhi is not on the equatorial plane and geostationary satellite is launched on the equatorial plane, the given satellite is false.
Promotional Banner

Topper's Solved these Questions

  • GRAVITATION

    CENGAGE PHYSICS ENGLISH|Exercise SCQ_TYPE|12 Videos

  • GRAVITATION

    CENGAGE PHYSICS ENGLISH|Exercise MCQ_TYPE|4 Videos

  • GRAVITATION

    CENGAGE PHYSICS ENGLISH|Exercise Fill In The Blanks|5 Videos

  • FLUID MECHANICS

    CENGAGE PHYSICS ENGLISH|Exercise INTEGER_TYPE|1 Videos

  • KINEMATICS-1

    CENGAGE PHYSICS ENGLISH|Exercise Integer|9 Videos

Similar Questions

Explore conceptually related problems

Is it possible to put an artifical satellite into orbit in such a way that it will always remain directly over New Delhi.

Is it possible to place an artificial satellite in an orbit such that it is always visible over kota ? Write down the reason.

Orbital velocity of an artificial satellite does not depend upon

What would happen to an artificial satellite, if its orbital velocity is slightly decreased due to some defects in it?

No part of India is situated on the equator. Is it possible to have a geostationary satellilte which always remains over New Delhi?

No part of India is situated on the equator. Is it possible to have a geostationary satellilte which always remains over New Delhi?

The time period of an artificial satellite in a circular orbit of radius R is 2 days and its orbital velocity is v_(0) . If time period of another satellite in a circular orbit is 16 days then

An artificial satellite of Earth nears the end of its life due to air resistance. While still in orbit:

An artificial satellite moving in a circular orbit around the earth has a total energy E_(0) . Its potential energy is

An artificial satellite moving in a circular orbit around the earth has a total energy E_(0) . Its potential energy is