Kepler's 1st and 2nd law illustrated

    Caption: Kepler's 3 laws of planetary motion are given below. The first 2 of Kepler's 3 laws of planetary motion illustrated compactly in the adjacent diagram.

    Kepler's 3 laws of planetary motion:

    1. Kepler's 1st law: A planet orbits the Sun in an ellipse with the Sun at one ellipse focus.

    2. Kepler's 2nd law: The planet orbital radius sweeps out equal areas in equal times.

      This means the planets move faster the nearer they are to the Sun, fastest at perihelion, and slowest at perihelion.

    3. Kepler's 3rd law: The square of the orbital period is proportional to the cube of the semi-major axis of the elliptical orbit. The semi-major axis is mean mean orbital radius a conventional definition.



      The formula version for the limit that Kepler's 3rd law is exact (see discussion below) is

        P_y = [1/sqrt(M/M_☉)]*r_AU**(3/2)  ,

      where P_y is orbital period in Julian years to 6-digit accuracy/precision, M_☉ is solar mass unit = 1.98855*10**30 kg, and r_AU is mean orbital radius in astronomical units. Note Julian year = 3652.25 exactly by definition.

    The actual planetary orbits obey the 3 laws to high accuracy.

    The 3 laws also are exact for ideal gravitationally-bound gavitational two-body system in the limit of one body being infinitely massive. The infinitely massive body remains at one ellipse focus while the other body orbits it obeying the 3 laws.

    Credit/Permission: © Han-Kwang Nienhuys (AKA User:Hankwang), 2007 / Creative Commons CC BY-SA 3.0.
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