Kinetic Energy of a Planet in an Elliptical Orbit

Physics · Gravitation · NEET

A planet moves fastest when it is closest to the Sun (perihelion) and slowest when it is farthest (aphelion). So its kinetic energy KE = (1/2)mv² is maximum at perihelion and minimum at aphelion. Memory hook: "Near the Sun, run; far from the Sun, slow" — closer means faster means more KE.
Sun (S)C (aphelion)farthest, slowestKE minimumA (perihelion)nearest, fastestKE maximumBLonger arrow = higher speed = higher KE. L = m·v·r stays constant.
Elliptical orbit with the Sun at a focus. At perihelion (A) the planet is nearest and fastest, so KE is maximum; at aphelion (C) it is farthest and slowest, so KE is minimum. Angular momentum L = m·v·r is the same everywhere.

Your doubts, answered

Is the kinetic energy of a planet the same everywhere in an elliptical orbit?

No. In a circular orbit the speed is constant, so KE is constant. But an elliptical orbit has different Sun-planet distances, so the speed changes. KE is highest at perihelion (closest point) and lowest at aphelion (farthest point). Only in a perfect circle would KE stay constant.

Where exactly is kinetic energy maximum and minimum?

KE is maximum at perihelion, the point nearest the Sun. KE is minimum at aphelion, the point farthest from the Sun. This is because the planet is fastest when it is closest to the Sun and slowest when it is farthest.

Why does a planet move faster when it is closer to the Sun?

Because angular momentum L = m·v·r is conserved (gravity is a central force, so it applies no torque about the Sun). L stays constant, so when r decreases the speed v must increase. Smaller r means bigger v, which means bigger KE = (1/2)mv².

If kinetic energy keeps changing, what stays constant?

Two things stay constant: total mechanical energy E = KE + PE, and angular momentum L. As the planet nears the Sun its PE becomes more negative (it drops into a deeper well), so KE rises to keep E fixed. As it moves away, KE falls and PE rises. The trade-off keeps E constant.

How do I compare KE at three points A, B, C on the orbit?

Rank the points only by their distance from the Sun. The closest point has the largest KE, the farthest has the smallest. Do not rank by distance along the path or by which point 'looks' higher — only Sun-to-planet distance matters.

⚠️ The NEET trap
Kinetic energy is constant because the planet's orbit is fixed and total energy is conserved.
Total energy is conserved, but KE and PE trade off. KE is maximum at perihelion and minimum at aphelion; it is not constant in an ellipse.
🧠 NTA hides the trap in the words 'conserved energy'. Total energy is conserved, not kinetic energy. Only in a circle is KE constant.

Real NEET questions

NEET 2018

The kinetic energies of a planet in an elliptical orbit about the Sun at positions A, B and C are K_A, K_B and K_C. AC is the major axis and SB is perpendicular to AC at the Sun S. A is the nearest point (perihelion) and C is the farthest (aphelion). Then:

A · K_B < K_A < K_C
B · K_A > K_B > K_C
C · K_A < K_B < K_C
D · K_B > K_A > K_C
Solution: Step 1: Rank the points by distance from the Sun S. A is nearest (perihelion), C is farthest (aphelion), B is in between (foot of the perpendicular from S). Step 2: Conserve angular momentum L = m·v·r = constant, so v is largest where r is smallest. Speed order: v_A > v_B > v_C. Step 3: KE = (1/2)mv², so KE follows the speed order: K_A > K_B > K_C. Answer: B.

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Frequently asked

What is the formula for kinetic energy of a planet?

KE = (1/2)mv², where m is the planet's mass and v is its orbital speed at that point. Since v changes along an ellipse, KE also changes.

At which point is a planet's speed the highest?

At perihelion, the point closest to the Sun. This follows from angular momentum conservation: m·v·r is constant, so smaller r gives larger v.

Does angular momentum change in an elliptical orbit?

No. Gravity always points from the planet toward the Sun (a central force), so it exerts zero torque about the Sun. Angular momentum L stays constant throughout the orbit.

Is the total energy of a planet in orbit positive or negative?

Negative. Any bound orbit (closed ellipse or circle) has total energy E = KE + PE that is negative. The negative sign means the planet is trapped by the Sun's gravity and cannot escape.

How is this different from Kepler's second law?

They are the same idea seen two ways. Kepler's second law (equal areas in equal times) is a direct result of angular momentum conservation. That same conservation makes the planet fast near the Sun (high KE) and slow far away (low KE).