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Physics Fundamentals

Orbital
Mechanic

Launch satellites into stable orbits.
Real gravity. Real Kepler's laws. 8 levels.

Click anywhere to begin
🛸 Orbital Physics Game

Orbital Mechanic — The Free Online Orbital Physics Game

Orbital Mechanic is a free physics game that teaches orbital velocity, Kepler's laws, and gravitational mechanics through 8 levels of satellite launch puzzles. Discover why satellites stay up — not by reading, but by doing.

How to play

  1. 1
    Click to set your launch point: Click anywhere near the planet surface. Your satellite launches from the point on the planet closest to your click.
  2. 2
    Drag to set velocity: Drag away from your launch point. Drag direction sets velocity direction — drag distance sets speed.
  3. 3
    Find stable orbit: When your satellite enters the target orbit band (shown as a cyan ring), a progress arc appears. Hold the orbit for 3.5 seconds to achieve it.
  4. 4
    Watch for crashes and escapes: Too little velocity and you crash into the planet. Too much and you escape into space. The sweet spot is orbital velocity.
  5. 5
    Earn stars: Fewer launches = more stars. Par is shown per level — 3 stars means you matched or beat par.

The physics behind the game

Orbital velocity

v = √(GM/r)

For a circular orbit, gravity must exactly provide the centripetal force. This gives a single unique speed at every radius — too fast and the satellite spirals out, too slow and it falls inward.

Kepler's third law

T² = (4π²/GM)·r³

The orbital period scales with r^(3/2). Double the orbital radius and the period increases by 2^(3/2) ≈ 2.83×. This is why geostationary satellites must orbit at a specific altitude.

Escape velocity

v_esc = √(2GM/r)

Escape velocity is exactly √2 times the circular orbital velocity at the same radius. Launch faster than this and your satellite never returns.

Gravitational potential energy

U = −GMm/r

Orbital energy is always negative — the satellite is bound to the planet. As radius increases, energy increases (becomes less negative) and orbital velocity decreases.

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