Satellite-Groundtrack

Ground track and 3D orbit simulation of LEO satellite.

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Use:

1. Run setup.m.
2. Open initSimulationParams.m.
   1. Input initial Keplerian elements.
   2. Input simulation time in days and step time in seconds.
3. Run mainKeplerGroundTrack.m or mainNewtonGroundTrack.m.

Note: mainKeplerGroundTrack.m uses Kepler's and mainNewtonGroundTrack.m uses Newton's equation.

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References:

1. Howard D. Curtis - Orbital Mechanics For Engineering Students (4th ed.)
2. Hanspeter Schaub - Analytical Mechanics of Space Systems (2nd ed.)

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Team:

Rishav, Rohit, Sagar and Shishir