Solar System Physics & Orbital Dynamics Simulator

An interactive computational model analyzing Keplerian orbits, atmospheric escape limits, and gravitational dynamics across the Solar System.

Interactive Orbital Simulator

Click on any planet in orbit or use the buttons on the right to inspect its orbital velocity and atmospheric retention characteristics.

Mathematical & Physical Foundations

Kepler's 3rd Law: T² = (4π² / G·M) · a³
Orbital Speed: v_orb ≈ √(G·M / a)
Escape Velocity: v_esc = √(2·G·M_p / R_p)
Thermal Speed: v_th = √(8·k_B·T_eq / π·m)
Jeans Atmospheric Escape Rule: A planetary body retains atmospheric gas over geological time (10⁹ yrs) if v_esc > 6 × v_th. If thermal velocity exceeds this threshold, atmospheric particles systematically escape into space.

Earth

Semi-Major Axis (a) 1.000 AU
Orbital Period (T) 1.00 yrs
Mean Orbital Speed 29.78 km/s
Surface Gravity (g) 1.00 g
Escape Velocity (v_esc) 11.19 km/s
Equilibrium Temp (T_eq) 288 K

Astrophysical Overview

Atmospheric Retention Mechanics: