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Keplerian Orbits 🪐

This repository contains a Java application for simulating Keplerian orbits.

Example 1 Example 2 Example 3

Structure

The main codebase is located in the src/com/company directory. The two main classes are:

  • Main.java: This is the entry point of the application.
  • Orbit.java: This class represents a Keplerian orbit. It includes properties such as eccentricity, semi-major axis, longitude of the ascending node, argument of periapsis, inclination, and period. It also includes methods for setting up the orbit and updating the period and mean angular motion.

Building

To build the project, you will need a Java development environment. Open the project in your IDE and build it using the built-in tools.

Running

To run the application, execute the Main class from your IDE.

Contributing

Contributions are welcome. Please open an issue to discuss your ideas before making changes.

License

This project is licensed under the terms of the MIT license.

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