Description
The STK Binary Ephemeris type for the Export Ephemeris/Attitude Tool.
Public Methods
 Export | Exports the ephemeris file. |
Public Properties
 CentralBodyName | The central body of the satellite. |
| CoordinateSystem | Whether the resulting data file should be in the Fixed, J2000, or Inertial coordinate system. If Earth or the Sun is the central body, the Inertial coordinate system is not an available option. |
| CovarianceType | Choose to export position covariance (3x3), position/velocity covariance (6x6), or no covariance information. CovarianceType is valid only if the vehicle has ephemeris with covariance. |
| IncludeInterp | Include or ignore interpolation boundaries. |
| StepSize | If the Use Ephemeris Steps option is not selected, enter a Step Size to be used for the vehicle. |
| TimePeriod | Sets the time period. Options are Use Entire Ephemeris - STK creates a data file using the Start and Stop Time specified in the vehicle's Orbit tab or Specify Time Period - STK creates a data file using the Start and Stop Time specified here. |
| UseVehicleCentralBody | Uses vehicle's central body. |
| VersionFormat | Provides the option to generate files compatible with prior versions of STK. |