MODULE:KNOWLEDGE-BASE
SIMULATION: ACTIVE
RETURN::Orbital Mechanics

Lagrange Points

Five Equilibria in Every Two-Body System

Co-Rotating Reference Frame
Star (primary)Planet (secondary)L4 / L5 — stableL1 / L2 / L3 — unstableTrojan particles
System Parameters

Mass ratio

50 : 1

L-points

5 total

Stable

L4, L5

Unstable

L1, L2, L3

L4/L5 angle

±60°

Triangle type

Equilateral

How They Form

Lagrange points arise where the gravitational pull of two large bodies and the centrifugal force of the rotating system exactly cancel. An object placed at one requires no thrust to maintain its position.

L4 and L5 are stable because any small displacement creates a restoring force — the Coriolis effect nudges the object back, causing it to trace slow ellipses called libration orbits.

L1, L2, and L3 are saddle points. A displacement along the axis leads away from equilibrium. Spacecraft stationed there require periodic stationkeeping burns.

Point Reference
L1Unstable

Between the two bodies

Solar observation (SOHO, DSCOVR)

Gravity from both bodies balances. Ideal for monitoring the primary, but any perturbation causes drift.

L2Unstable

Beyond the smaller body

Deep space telescopes (JWST, Herschel)

Always in the shadow of the secondary. Cold and stable enough for infrared instruments.

L3Unstable

Beyond the larger body, hidden

Theoretically none — always out of view

The least useful point. Perpetually blocked by the primary and slowly perturbed by other bodies.

L4Stable

60° ahead of secondary

Trojan asteroids, long-term debris

Forms an equilateral triangle with both bodies. Objects here librate slowly and remain for billions of years.

L5Stable

60° behind secondary

Trojan asteroids, proposed space stations

Mirror of L4. Jupiter's Trojans share this point with thousands of asteroids. Proposed for future colonies.