Central mass Explicit Euler Symplectic Euler Velocity Verlet RK4
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Energy drift over time

Integrator Race 2D: Euler vs Verlet vs RK4

Four identical bodies are launched into the same elliptical orbit around the same central mass, each advanced by a different numerical integrator — Explicit Euler, Symplectic (semi-implicit) Euler, Velocity Verlet and RK4 — using the same shared step size. Because Newton's laws are differential equations with no closed-form solution for most real scenarios, every physics or orbital-mechanics engine has to pick one of these stepping schemes, and the choice matters: explicit Euler visibly spirals outward as it leaks energy every step, the two symplectic methods keep a stable closed ellipse even at a coarse step size, and RK4 trades symplecticity for high per-step accuracy. This 2D edition pairs a pannable/zoomable top-down orbit view with a live energy-drift strip chart underneath, so the divergence is visible both spatially and as a trend over time.