Description
The CCSDSv3 Ephemeris type for the Export Ephemeris/Attitude Tool.
Public Methods
 Export | Exports the ephemeris file. |
Public Properties
 CentralBodyName | Gets or sets the central body of the satellite. |
| Classification | A string that specifies the classification/caveats of the data file. |
| DateFormat | Gets or sets the desired date format. |
| EphemerisFormat | Gets or sets 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. |
| FileFormat | Gets or sets the file format that will be generated by the export tool. |
| HasCovarianceData | Returns true if the object has covariance data. |
| IncludeAcceleration | Include acceleration data in the exported file. |
| IncludeCovariance | Include covariance data in the exported file. If covariance data is not available, this property becomes read-only. |
| MessageID | A string defining the message ID which should uniquely identify the message. |
| 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 | Gets or sets the reference frame of the ephemeris. |
| 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 | Gets or sets 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. |