MCQEasyJEE 2023Satellites & Orbital Velocity

JEE Physics 2023 Question with Solution

Given below are two statements:

Statement I: If EE be the total energy of a satellite moving around the Earth, then its potential energy will be E2\frac{E}{2}.

Statement II: The kinetic energy of a satellite revolving in an orbit is equal to the half the magnitude of total energy EE.

Options:

  • A

    Both Statement I and Statement II are incorrect

  • B

    Statement I is incorrect but Statement II is correct

  • C

    Statement I is correct but Statement II is incorrect

  • D

    Both Statement I and Statement II are correct

Answer

Correct answer:A

Step-by-step solution

Standard Method

Given: Two statements about the energy of a satellite revolving around the Earth.

Find: Which statement is correct.

For a satellite in a circular orbit, the standard energy relations are:

PE=2KEPE = -2KE

and

E=KE+PE=KE2KE=KEE = KE + PE = KE - 2KE = -KE

So,

KE=E=EKE = -E = |E|

and also

PE=2EPE = 2E

because EE is negative.

Now analyze the statements:

  1. Statement I: It says potential energy is E2\frac{E}{2}. But from the orbital energy relation,
PE=2EPE = 2E

So Statement I is incorrect.

  1. Statement II: It says kinetic energy is equal to half the magnitude of total energy. But actually,
KE=EKE = |E|

not

KE=E2KE = \frac{|E|}{2}

So Statement II is also incorrect.

Therefore, both statements are incorrect. The correct option is A.

Using orbital energy relations from the solution text

Given:

  • E=KE+PEE = KE + PE
  • PE=2KEPE = -2KE

Find: Truth values of Statement I and Statement II.

Substitute PE=2KEPE = -2KE into total energy:

E=KE+(2KE)E = KE + (-2KE) E=KEE = -KE

Hence,

KE=E=EKE = -E = |E|

Now use PE=2KEPE = -2KE:

PE=2EPE = -2|E|

Since E<0E < 0 for a bound satellite orbit, this is equivalently written as

PE=2EPE = 2E

Therefore:

  • Statement I is false because it gives PE=E2PE = \frac{E}{2} instead of PE=2EPE = 2E.
  • Statement II is false because it gives KE=E2KE = \frac{|E|}{2} instead of KE=EKE = |E|.

Therefore, both statements are incorrect. The correct option is A.

Common mistakes

  • Assuming PE=E2PE = \frac{E}{2} by confusing gravitational orbital energy with some generic energy split is incorrect. For a satellite in circular orbit, the correct relation is PE=2EPE = 2E because the total energy EE is negative.

  • Taking the magnitude of total energy incorrectly and writing KE=E2KE = \frac{|E|}{2} is wrong. First use E=KEE = -KE for orbital motion, then conclude KE=EKE = |E|.

  • Ignoring the sign of total energy leads to wrong conclusions. A bound satellite has negative total energy, so sign handling must be done carefully before comparing KEKE, PEPE, and EE.

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