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Orbits and the Wider Universe

Newton's law of gravitation applied to planets and satellites

  • 3 things to know
  • Component 2

Overview

Recall questions on setting the gravitational force equal to the centripetal force, deriving the orbital speed, why the orbiting mass cancels, how speed varies with radius, and worked speed and period calculations for planets and satellites.

What you need to know

Answer each one before you reveal it.

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Key term

Why must a geostationary satellite orbit above the equator?

Key term

What provides the centripetal force that keeps a planet in orbit around a star?

Key term

Write the condition for a body of mass m in a circular orbit of radius r about a mass M.

Questions from this subtopic

Each one with the model answer underneath.

  1. 1

    Write Newton's law of gravitation in the form used for a planet of mass m orbiting a star of mass M, and state carefully what r represents.

    Model answer

    The law is F = GMm/r², with F in newtons, the masses in kilograms and G equal to 6.67 × 10⁻¹¹ N m² kg⁻². The distance r is measured between the centres of the two bodies, not from the surface of either.

  2. 2

    What provides the centripetal force that keeps a planet in orbit around a star?

    Model answer

    The gravitational attraction between the star and the planet provides the centripetal force, directed towards the star at all times.

  3. 3

    Write the condition for a body of mass m in a circular orbit of radius r about a mass M.

    Model answer

    The gravitational force equals the required centripetal force, so GMm/r² = mv²/r, where v is the orbital speed.

  4. 4

    Derive an expression for the orbital speed of a satellite in a circular orbit of radius r about a mass M.

    Model answer

    Setting GMm/r² = mv²/r and cancelling m and one factor of r gives v² = GM/r, so v = √(GM/r).

  5. 5

    Why is the mass of an orbiting satellite irrelevant to its orbital speed?

    Model answer

    The satellite's own mass appears on both sides of GMm/r² = mv²/r and cancels, so only the central mass and the orbital radius are left.

  6. 6

    How does the orbital speed of a satellite change as the orbital radius increases?

    Model answer

    The speed decreases, because v = √(GM/r) makes it inversely proportional to the square root of the radius.

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