Description
The SPICE Ephemeris type for the Export Ephemeris/Attitude Tool.
Public Methods
 Export | Exports the ephemeris file. |
Public Properties
 CentralBodyName | The central body of the satellite. |
| Interpolation | The interpolation order value between 1 and 15. If the interpolation type is Type 13 (Hermitian), and then you are required to enter an odd interpolation order value. |
| InterpolationType | The interpolation type. |
| SatID | The identifying number for the satellite ephemeris being created. Dimensionless. |
| 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. |