•Fixed a crash in the Spacecraft Orbit Determination general page
•Corrected an issue where TDRS / BRTS Doppler processing wouldn't give good residuals in some cases
•Variational equations is now properly set as the default CovariancePropagationMethod for new Spacecraft objects
•Addressed an error when using some Orbit Determination properties with a Spacecraft initialized in the GUI
•Internal calculations using the TEME frame now use the most up-to-date state instead of a cached state
•The fixed lag smoother can no longer run out of memory and error when called too frequently |