Module 01

Orbital
Mechanics

Adjust orbital parameters and watch the physics respond in real time. Hover the icons to learn the physics behind each control.

Interactive 2D Simulation Beginner–Intermediate
// Parameters
Altitude
400 km
200 km (LEO)36,000 km (GEO)
Velocity
7.67 km/s
Slower (ellipse)Faster (ellipse)
Orbit Shape
Hohmann Transfer
Target altitude 2,000 km
// Live Telemetry
Orbital Period
Orbital Radius
Circ. Velocity
Orbit Type Circular
Periapsis Alt. 400 km
Apoapsis Alt. 400 km
Δv (Hohmann)
// Orbit Visualizer — Real-time 2D (not to scale — log-scaled distances)
HOHMANN TRANSFER IN PROGRESS
SIMULATION RUNNING
FRAME: 0
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Newton's Gravitation
F = GMm / r²
Gravity pulls the satellite toward Earth with a force that decreases with the square of the distance. This centripetal force is what keeps the satellite in orbit instead of flying off into space.
Conservation of Energy
E = ½mv² − GMm/r
Total orbital energy is the sum of kinetic and potential energy. It stays constant in a closed orbit. This is why speeding up raises your orbit — you're adding energy to the system.
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Kepler's Third Law
T² ∝ a³
The orbital period squared is proportional to the semi-major axis cubed. Higher orbits = longer periods. The ISS completes an orbit every 92 minutes; the Moon takes 27 days.