Orbital Mechanics Simulation Guide
This laboratory sandbox is designed to help you visually examine different **orbital profiles** (circular, eccentric ellipses, or unbound escape trajectories) and track the continuous **conservation and exchange of energy** (Kinetic vs. Gravitational Potential Energy) in real-time.
Use the controls on the left panel to pilot the satellite around Earth:
Work out how to increase or descrease the orbital radius such that the orbit remains circular.
Investigate the energy dynamic chart. What happens to the satellite's path and flight status the exact moment Total Energy (E) reaches or goes above 0 J? Observe how the exit geometry shapes itself!
Orbital Movements Explained
A **Hohmann Transfer** is a two-step, fuel-efficient maneuver used to move a spacecraft between two coplanar circular orbits of different radii using impulsive thrusts.
Hint: Try applying this two-burn technique to solve the challenge of cleanly expanding and circularizing your radius!
Physics High Laboratory
Fire thrusters along the velocity vector to change orbits in real-time.
The satellite's total energy has crossed into non-negative values.