---
title: "Elliptical Orbit — AP Physics 1 Definition & Exam Guide"
description: "An elliptical orbit is a path where a satellite's distance from the central body changes, keeping total energy and angular momentum constant while KE and GPE trade off. Core to Topic 6.6."
canonical: "https://fiveable.me/ap-physics-1-revised/key-terms/elliptical-orbit"
type: "key-term"
subject: "AP Physics 1"
unit: "Unit 6"
---

# Elliptical Orbit — AP Physics 1 Definition & Exam Guide

## Definition

An elliptical orbit is an orbital path where the satellite's distance from the central object varies, so total mechanical energy and angular momentum stay constant while kinetic energy and gravitational potential energy continuously trade off (AP Physics 1, Topic 6.6).

## What It Is

An elliptical orbit is what you get when a satellite's [distance](/ap-physics-1-revised/key-terms/distance "fv-autolink") from the central body keeps changing as it goes around. The satellite swings in close at one point (perigee, for Earth) and far out at the other end (apogee). Because gravity is the only [force](/ap-physics-1-revised/unit-2/2-forces-and-free-body-diagrams/study-guide/jQ2Obd0dAU4QiTPN "fv-autolink") acting and it points toward the central object, two things are locked in for the whole orbit. The system's total mechanical energy is constant, and the satellite's angular momentum is constant.

Here's the part the exam loves. Even though those two totals never change, the pieces inside them do. As the satellite climbs away from the planet, gravitational potential energy goes up, so [kinetic energy](/ap-physics-1-revised/unit-3/4-conservation-of-energy/study-guide/ryRjnKmvIfMWNvdl "fv-autolink") must drop by exactly the same amount. The satellite moves fastest at perigee and slowest at apogee. Think of it like a ball rolling around a giant gravitational bowl. The total energy never changes, but the split between speed and height shifts constantly. Compare that to a circular orbit, where the distance never changes, so KE, GPE, total energy, and angular momentum are all constant individually.

## Why It Matters

Elliptical orbits live in Topic 6.6 (Motion of Orbiting Satellites) in [Unit 6](/ap-physics-1-revised/unit-6 "fv-autolink"), Energy and Momentum of Rotating Systems. They directly support learning objective 6.6.A, which asks you to describe the motion of a two-object system interacting only through gravity. The whole point of putting orbits at the end of Unit 6 is that they're the payoff for everything you've learned about conservation laws. You're not memorizing [orbit](/ap-physics-1-revised/key-terms/orbit "fv-autolink") facts. You're applying conservation of energy and conservation of angular momentum to a system where the only force is gravity. An elliptical orbit is the cleanest test of whether you can tell which quantities are conserved and which ones just trade back and forth.

## Connections

### Circular orbits (Unit 6)

A [circular orbit](/ap-physics-1-revised/unit-2/9-circular-motion/study-guide/phypMTqBWYSyW4Xd "fv-autolink") is the special case where the distance never changes, so everything is constant, including KE and GPE individually. An elliptical orbit relaxes that one condition, and suddenly KE and GPE start trading. The exam loves asking you to spot which quantities stay constant in each case.

### Conservation of angular momentum (Unit 6)

Gravity points straight at the central object, so it exerts zero torque on the satellite. That means L = mvr is constant everywhere in the orbit. If the apogee distance is twice the perigee distance, the perigee [speed](/ap-physics-1-revised/key-terms/speed "fv-autolink") must be twice the apogee speed. This is the same physics as a spinning skater pulling in her arms.

### Conservation of energy (Unit 3)

Gravity is a conservative force, so the energy bookkeeping from [Unit 3](/ap-physics-1-revised/unit-3 "fv-autolink") applies directly. In an elliptical orbit, every joule of gravitational potential energy gained is a joule of kinetic energy lost. If a problem says GPE increased by 5.0×10⁸ J, KE dropped by exactly 5.0×10⁸ J.

### [Escape velocity (Unit 6)](/ap-physics-1-revised/key-terms/escape-velocity)

Bound orbits, circular or elliptical, have negative total mechanical energy. Escape velocity is the speed where total energy hits zero and the satellite never comes back. Total energy is the dividing line between an ellipse and a one-way trip.

## On the AP Exam

Elliptical orbits show up mostly as conservation-law reasoning, not plug-and-chug. Multiple-choice stems give you a satellite at two points in its orbit and ask you to compare speeds, energies, or angular momentum. Expect three classic moves. First, use L = mvr to find a speed ratio (apogee twice as far as perigee means perigee speed is twice apogee speed). Second, use energy conservation to convert a GPE change into a KE change of equal size and opposite sign. Third, recognize that total mechanical energy depends on the semi-major axis, so a circular orbit and an elliptical orbit with the same semi-major axis have the same total energy. No released FRQ has used the term verbatim, but orbit questions are a natural fit for the qualitative-quantitative translation FRQ, where you justify which quantities are conserved and why gravity exerts no torque on the satellite.

## elliptical orbit vs Circular orbit

In a circular orbit, the distance from the central object is fixed, so total mechanical energy, GPE, KE, and angular momentum are ALL constant. In an elliptical orbit, only total mechanical energy and angular momentum are constant, while KE and GPE vary as the distance changes. If a question asks 'which quantities are constant,' your answer depends entirely on which orbit shape you're given.

## Key Takeaways

- In an elliptical orbit, total mechanical energy and angular momentum are constant, but kinetic energy and gravitational potential energy vary as the satellite's distance changes.
- The satellite moves fastest at the closest point (perigee) and slowest at the farthest point (apogee), because GPE and KE trade off while their sum stays fixed.
- Gravity exerts no torque on the satellite because the force points directly at the central object, which is why angular momentum (L = mvr) is conserved.
- If apogee distance is twice perigee distance, angular momentum conservation means perigee speed is twice apogee speed.
- A circular orbit and an elliptical orbit with the same semi-major axis have the same total mechanical energy.
- Any increase in gravitational potential energy along the orbit equals an identical decrease in kinetic energy, since gravity is a conservative force and no other forces act.

## FAQs

### What is an elliptical orbit in AP Physics 1?

It's an orbital path where the satellite's distance from the central object changes throughout the orbit. Total mechanical energy and angular momentum stay constant, but KE and GPE continuously trade off. It's tested under Topic 6.6 and learning objective 6.6.A.

### Is kinetic energy conserved in an elliptical orbit?

No. Kinetic energy changes constantly because it trades with gravitational potential energy as the distance changes. What IS conserved is the total mechanical energy (KE + GPE) and the satellite's angular momentum.

### Where does a satellite move fastest in an elliptical orbit?

At the closest point to the central object (perigee). Angular momentum L = mvr is constant, so when r is smallest, v must be largest. At apogee, the farthest point, the satellite is at its slowest.

### How is an elliptical orbit different from a circular orbit?

In a circular orbit, distance never changes, so KE, GPE, total energy, and angular momentum are all constant. In an elliptical orbit, only total energy and angular momentum are constant, while KE and GPE vary. That distinction is exactly what MCQs test.

### Does changing a circular orbit to an elliptical one change the total energy?

Not if the semi-major axis stays the same. Total mechanical energy depends on the semi-major axis, so a circular orbit of radius r and an ellipse with semi-major axis r have identical total mechanical energy.

## Related Study Guides

- [6.6 Motion of Orbiting Satellites](/ap-physics-1-revised/unit-6/6-motion-of-orbiting-satellites/study-guide/tzB1DCcspZo8vXIC)

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