Orbital Periods of a Satellite

Version 1.0.0.0 (237 KB) by David Eagle
MATLAB scripts for computing the orbital periods of a satellite.
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Updated 2 Jan 2013

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PDF document and MATLAB scripts that can be used to calculate the orbital periods of a satellite. In these scripts, the astrodynamic constants (gravitational constant, equatorial radius, and gravity coefficient) are “hardwired” for the Earth. However, these fundamental constants can be easily updated for other planets or the Moon by changing the numerical values in the om_constants.m MATLAB function.

Cite As

David Eagle (2024). Orbital Periods of a Satellite (https://www.mathworks.com/matlabcentral/fileexchange/39550-orbital-periods-of-a-satellite), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2011a
Compatible with any release
Platform Compatibility
Windows macOS Linux

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Version Published Release Notes
1.0.0.0