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Interactive Flight Manual

Orbital Mechanics Simulation Guide

Core Purpose

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:

  • Orbit Viewport: Left-click and drag on the right viewport to rotate camera; right-click to pan; scroll to zoom.
  • Prograde Burn: Fires engines forward to increase kinetic energy and raise the opposite side of the orbit.
  • Retrograde Burn: Fires engines backward to decrease speed and drop orbital heights.
🎯 Flight Directives & Challenges
01.

Work out how to increase or descrease the orbital radius such that the orbit remains circular.

02.

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!

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Orbital Mechanics Sandbox

Physics High Laboratory

Fire thrusters along the velocity vector to change orbits in real-time.

Rocket Engine Controls

sec
Real-Time Energy Levels Sorted: U → K → E
LIVE FLIGHT TELEMETRY In Orbit
Kinetic Energy (K):0.00 J
Potential Energy (U):0.00 J
Total Energy (E):0.00 J
Apsides Diagnostics
Perigee: ⓘ Perigee Altitude:
The point in an orbit where the satellite is closest to the planet, measured as altitude from the surface. Velocity peaks to its absolute maximum here.
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Apogee: ⓘ Apogee Altitude:
The point in an orbit where the satellite is farthest from the planet, measured as altitude from the surface. Velocity falls to its absolute minimum here.
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satellite not to scale 😉