Description
The CCSDS Ephemeris type for the Export Ephemeris/Attitude Tool.
Public Methods
 Export | Exports the ephemeris file. |
Public Properties
 CentralBodyName | The central body of the coordinate system in which to express the ephemeris. |
| DateFormat | The desired date format. |
| EphemerisFormat | The desired format to be used for representing the position and velocity information as either scientific notation or floating point notation. Scientific notation is recommended when possible. |
| ObjectID | A string defining the Object ID - to be specified as the international spacecraft designator, also known as an NSSDC identifier. |
| ObjectName | A name for the Object. By recommendation of the CCSDS standard, the name from the SPACEWARN Bulletin should be used. |
| Originator | A string that specifies an identifier of the organization producing the data file. |
| ReferenceFrame | The reference frame in which to express the ephemeris. Some frames are allowed for use only when the CentralBodyName is Earth or Moon. |
| ReferenceFramesSupported | Returns an array of valid choices. |
| 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. |
| TimePrecision | If selected, STK uses the Step Size specified in the vehicle's Basic properties. If not selected, specify a Step Size. Dimensionless. |
| TimeSystem | The time system of the ephemeris. |
| UseSatelliteCenterAndFrame | Use the satellite center and frame. Setting the property to 'True' will cause CentralBody and ReferenceFrame properties become read-only. |