In astronomy, Kepler’s laws of planetary motion are three scientific laws describing the motion of planets around the sun.
- Kepler first law: The law of orbits
- Kepler’s second law: The law of equal areas
- Kepler’s third law: The law of periods
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Introduction to Kepler’s Laws
Motion is always relative. Based on the energy of the particle under motion, the motions are classified into two types:
- Bounded Motion
- Unbounded Motion
In bounded motion, the particle has negative total energy (E<0) and has two or more extreme points where the total energy is always equal to the potential energy of the particle i.e the kinetic energy of the particle becomes zero.
For eccentricity 0≤ e <1, E<0 implies the body has bounded motion. A circular orbit has eccentricity e = 0 and elliptical orbit has eccentricity e < 1.
In unbounded motion, the particle has positive total energy (E>0) and has a single extreme point where the total energy is always equal to the potential energy of the particle i.e the kinetic energy of the particle becomes zero.
For eccentricity e ≥ 1, E > 0 implies the body has unbounded motion. Parabolic orbit has eccentricity e = 1 and Hyperbolic path has eccentricity e>1.
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Kepler’s laws of planetary motion can be stated as follows:
Kepler First law – The Law of Orbits
According to Kepler’s first law, all the planets revolve around the sun in elliptical orbits having the sun at one of the foci. The point at which the planet is close to the sun is known as perihelion and the point at which the planet is farther from the sun is known as aphelion.
It is the characteristics of an ellipse that the sum of the distances of any planet from two foci is constant. The elliptical orbit of a planet is responsible for the occurrence of seasons.
Kepler’s Second Law – The Law of Equal Areas
As the orbit is not circular, the planet’s kinetic energy is not constant in its path. It has more kinetic energy near perihelion and less kinetic energy near aphelion implies more speed at perihelion and less speed (vmin) at aphelion. If r is the distance of planet from sun, at perihelion (rmin) and at aphelion (rmax), then,
rmin + rmax = 2a × (length of major axis of an ellipse) . . . . . . . (1)
For an infinitesimal movement of the planet in a time interval in an elliptical orbit, the area swept by the planet in time is given by;
dA/dt = d/dt [ 1/2 × r × (v dt)]= 1/2 × rv . . . . . (2)
At perihelion r = rmin, v = vmax then from Equation 2;
dA/dt = 1/2 × rmin × vmax) = [m × vmax × rmin]/2m = L/2m;
At aphelion r = rmax, v = vmin then from Equation 2;
dA/dt = 1/2 × vmin × rmax = [m × vmin × rmax]/2m = L/2m
Kepler’s second law states the areal velocity of a planet revolving around the sun in elliptical orbit remains constant which implies the angular momentum of a planet remains constant. As the angular momentum is constant all planetary motions are planar motions, which is a direct consequence of central force.
⇒ Check: Acceleration due to Gravity
Kepler’s Third Law – The Law of Periods
Shorter the orbit of the planet around the sun, shorter the time taken to complete one revolution. According to Kepler’s law of periods, the square of the time period of revolution (of a planet around the sun in an elliptical orbit is directly proportional to the cube of its semi-major axis).
T2 ∝ a3
Using the equations of Newton’s law of gravitation and laws of motion, Kepler’s third law takes a more general form:
P2 = 4π2 /[G(M1+ M2)] × a3
where M1 and M2 are the masses of the two orbiting objects in solar masses.