Description

Object Model

Public Methods

Export

Exports the ephemeris file.

Public Properties

CentralBodyName	The central body of the satellite.
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.
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.
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 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	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.

CoClasses that Implement IAgVeEphemerisCCSDSv2ExportTool