How to Calculate Classical Orbital Elements Using Matlab?

AI Thread Summary
Calculating classical orbital elements for a satellite or space shuttle around Earth can be accomplished using MATLAB. Users can program algorithms to extract these elements, which typically include parameters such as semi-major axis, eccentricity, inclination, and others. Resources and examples are available online to assist in developing these algorithms, making it accessible for those new to the topic. Engaging with MATLAB's built-in functions and toolboxes can also enhance the process of orbital element calculation.
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Hi!

Is there a way to calculate the classical orbital elements for a satellite or space shuttle around Earth using Matlab? I would like to get started with it since it is something that I've not tried before. so plese help

Best regards
 
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You can program an algorithm to extract orbital elements in MATLAB.
 
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