Select one of the following values for the EstimateOrbit property:
|Orbit Estimation Options|
|true||The six element orbit state is added to the overall estimation state for filter and simulator processes using this satellite. State elements for the estimation of atmospheric density and solar pressure coefficient corrections for this satellite will be added if required by the force modeling.|
|false||An EphemerisSource attribute appears, providing the following
Note: When using the Meas File Embedded Trajectory option, ODTK cannot model light time delay for SBRange measurements. Any measurements that include the tracker trajectory need to be corrected for light time delay beforehand, or the measurement noise increased to account for LTD values.