A satellite orbiting Earth at an orbital radius r has a velocity v. Which represents the velocity if the satellite is moved to an orbital radius of 5r?

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The equation which represent the velocity, if the satellite is moved to an orbital radius of 5r is [tex]V = \frac{V}{\sqrt{5}}[/tex]

Given the following data:

  • Radius = 5r

To find the equation which represent the velocity, if the satellite is moved to an orbital radius of 5r:

Orbital velocity can be defined as the minimum velocity at which a satellite must move to remain in orbit.

Mathematically, orbital velocity is given by the formula:

[tex]V = \sqrt{\frac{GM}{r}}[/tex]

Where:

  • V is the orbital velocity.
  • G is the gravitational constant.
  • M is the mass of a satellite.
  • r is the radius.

Substituting the value of r, we have:

[tex]V = \sqrt{\frac{GM}{5r}}[/tex]

[tex]V = \frac{1}{\sqrt{5}}[/tex] × [tex]\sqrt{\frac{GM}{r}}[/tex]

Recall, [tex]V = \sqrt{\frac{GM}{r}}[/tex]

[tex]V = \frac{1}{\sqrt{5}}[/tex] × [tex]V[/tex]

[tex]V = \frac{V}{\sqrt{5}}[/tex]

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