OCR · A-Level · Physics

    Course version: H556 · Version from Sept 2015

    Planetary motion: (a) Kepler’s three laws of planetary motion

    Kepler's three laws describe how planets move around the Sun.

    Checked against the OCR H556 specification (opens in a new tab) on .

    • Point 1 of 5
    • 4 key terms

    Study notes

    From the checked teaching notes for this specification point.

    The idea

    Kepler's three laws describe how planets move around the Sun. The first law states that each planet moves in an ellipse with the Sun at one focus. The second law states that the line joining a planet to the Sun sweeps out equal areas in equal times, so a planet moves faster when nearer the Sun. The third law states that the square of the orbital period T is proportional to the cube of the semi-major axis a: T² ∝ a³, or T²/a³ is constant for all planets orbiting the same central body. For circular orbits a is the orbital radius r, giving T² ∝ r³. These laws are empirical but follow from Newton's law of gravitation and centripetal force.

    What earns the marks

    • States Kepler's first law: planets move in ellipses with the Sun at one focus.
    • States Kepler's second law: the radius vector from Sun to planet sweeps equal areas in equal times.
    • States Kepler's third law: T² ∝ a³ for planets orbiting the same central mass.
    • Explains that the second law implies a planet's orbital speed is greatest at perihelion and least at aphelion.
    • Applies T² ∝ r³ to circular orbits, where the semi-major axis equals the orbital radius.

    Common mistakes and how to put them right

    • Describing planetary orbits as perfect circles.

      Put it right: Kepler's first law requires ellipses with the Sun at one focus.

    • Stating the third law as T ∝ a³ or T² ∝ a².

      Put it right: The correct relationship is T² ∝ a³.

    • Claiming the Sun is at the centre of the ellipse.

      Put it right: It is at one focus, not the geometric centre.

    • Applying T² ∝ a³ to planets orbiting different stars without accounting for the different central masses.

    Exam tips

    • Learn all three laws with their precise wording, since multiple-choice questions often test one law at a time.
    • Use the constant form T²/a³ when comparing two planets orbiting the same body.
    • Remember that the second law is about equal areas in equal times, not equal distances or equal speeds.
    • Link the third law to Newton's law of gravitation to show it is not an independent assumption.

    Try the lesson

    The start of the Planetary motion: (a) Kepler’s three laws of planetary motion lesson, made from checked teaching notes for this specification point.

    Listen

    Kepler's three laws describe how planets move around the Sun. The first law states that each planet moves in an ellipse with the Sun at one focus. The second law states that the line joining a planet to the Sun sweeps out equal areas in equal times, so a planet moves faster when nearer the Sun. The third law states that the square of the orbital period T is proportional to the cube of the semi-major axis a: T² ∝ a³, or T²/a³ is constant for all planets orbiting the same central body. For circular orbits a is the orbital radius r, giving T² ∝ r³. These laws are empirical but follow from Newton's law of gravitation and centripetal force. A strong answer earns marks for these points. States Kepler's first law: planets move in ellipses with the Sun at one focus. States Kepler's second law: the radius vector from Sun to planet sweeps equal areas in equal times. States Kepler's third law: T² ∝ a³ for planets orbiting the same central mass. Explains that the second law implies a planet's orbital speed is greatest at perihelion and least at aphelion. Exam tip: Learn all three laws with their precise wording, since multiple-choice questions often test one law at a time.

    See it

    A top-down flowchart. The top node reads 'Kepler's three laws of planetary motion' and branches to three nodes. The first branch reads 'First law: each planet moves in an ellipse with the Sun at one focus'. The second branch reads 'Second law: the line joining planet to Sun sweeps out equal areas in equal times' and leads to a node reading 'Planet moves faster when nearer the Sun'. The third branch reads 'Third law: T² ∝ a³' and leads to two nodes: 'T²/a³ is constant for all planets orbiting the same central body' and 'For circular orbits a is the orbital radius r, giving T² ∝ r³'.
    A classification of Kepler's three laws of planetary motion with the key statement of each law.

    Key words

    Say what each word means before you turn the card.

    Elliptical planetary orbits

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    Equal areas in equal times

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    Period–semi-major-axis relationship

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    Newtonian derivation of Kepler's laws

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    See every definition
    Elliptical planetary orbits
    Each planet moves in an ellipse with the Sun at one focus, not at the geometric centre.
    Equal areas in equal times
    The line joining a planet to the Sun sweeps out equal areas in equal times, so a planet moves faster when nearer the Sun.
    Period–semi-major-axis relationship
    The square of the orbital period T is proportional to the cube of the semi-major axis a, so T²/a³ is constant for all planets orbiting the same central body.
    Newtonian derivation of Kepler's laws
    These laws are empirical but follow from Newton's law of gravitation and centripetal force.

    Label the diagram

    Some boxes have lost their names. Pick the right name for each number.

    The diagram again, with 3 boxes numbered instead of named. A top-down flowchart. The top node reads 'Kepler's three laws of planetary motion' and branches to three nodes. The first branch reads 'First law: each planet moves in an ellipse with the Sun at one focus'. The second branch reads 'Second law: the line joining planet to Sun sweeps out equal areas in equal times' and leads to a node reading 'Planet moves faster when nearer the Sun'. The third branch reads 'Third law: T² ∝ a³' and leads to two nodes: 'T²/a³ is constant for all planets orbiting the same central body' and 'For circular orbits a is the orbital radius r, giving T² ∝ r³'.
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    • 3Box 3

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