<commit_before>orbital_link_budget
===================

Simulates Earth orbits up to an eccentricity of 0.95.

Calculates link budget, azimuth and elevation, uptime/downtime, doppler shift.

Written for the University of British Columbia's Orbit Satellite Design Team.

Based on Satellite-Orbit-Simulation by deedydas.

The code is a bit messy (especially the function names); feel free to improve it.<commit_msg>better written<commit_after>orbital_link_budget
===================

Written for the University of British Columbia's Orbit Satellite Design Team.
Calculates link budget, azimuth and elevation, uptime/downtime, doppler shift.
Simulates Earth orbits up to an eccentricity of 0.95.

Earth Centered Inertial (ECI) coordinates draw an unchanging orbit around a rotating Earth.
Earth Centered Earth Fixed (ECEF) coordinates draw a changing orbit around a stationary Earth.

The MIT License allows you to do anything with this code as long as you attribute it properly (and there's no warranty).

Written by <NAME>

Based on Satellite-Orbit-Simulation by <NAME> (no license).
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