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This geometric relationship defines the orientation of the spacecraft’s orbital plane with respect to the mean Sun. The MLTAN/RAAN relationship is important for mission design of sun-synchronous, repeating ground track, and other types of mission orbits that must satisfy Sun-orbit plane and other lighting constraints.
Cite As
David Eagle (2026). Mean Local Time of the Ascending Node (https://www.mathworks.com/matlabcentral/fileexchange/39085-mean-local-time-of-the-ascending-node), MATLAB Central File Exchange. Retrieved .
General Information
- Version 1.1.0.0 (370 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
