Name
|
Description
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AEINTG
|
The 2-element AEINTG array returned by C_LIB_PROP_SAT when the ephemeris type is 4 and analytic G2 is used.
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COSIGM
|
The 6-element COSIGM array returned by C_LIB_PROP_SPCOV.
|
Covariance
|
The covariance calculated by the propagator.
|
COVMTX
|
A property which will be set to 1 if the covariance is being propagated and 0 otherwise.
|
DeclaredName
|
The name of the object as declared.
|
DisplayName
|
The name displayed for this object in output windows such as views, plots, and reports.
|
ErrorAction
|
The action to take when an error occurs.
|
ErrorCode
|
The error code returned by the propagator or read routines on a Step Spacecraft or Get NoradSP command.
|
FKCon
|
The FK constant value.
|
GravCon
|
The gravity model to use.
|
IERC
|
The error code from the propagate routines. It is set by the Step and Get commands when the ErrorAction is 2.
|
JobSpecIndex
|
The index in the Norad SP job specification file of the job which is loaded. Indexes start at 1.
|
NoradFilename
|
Read-only property giving the name of the file from which the current job specification was read.
|
NumSpacecraft
|
Integer giving the number of spacecraft in the job specification which is currently loaded.
|
ObjectId
|
The unique identifier for the object.
|
ObjectType
|
The type of the object.
|
PARTGP4
|
The 6-element PARTGP4 array returned by C_LIB_PROP_SAT when the ephemeris type is 2.
|
PARTXYZ
|
The 6-by-9 PARTXYZ matrix returned by C_LIB_PROP_SAT when the ephemeris type is 4 and numeric G2 is used. It is flattened into a 54 element singly-indexed array.
|
RPINTG
|
The 6-element RPINTG array returned by C_LIB_PROP_SAT when the ephemeris type is 4 and analytic G2 is used.
|
SpacecraftIndex
|
The index of the spacecraft in the Norad SP job specification which is loaded. (A single job specification may contain data for more than one spacecraft. This is the index of the spacecraft in the job spec).
|
SSNAM_FLAG
|
Integer which mimics the behavior of the SSNAM_FLAG variable in the Norad SP sample application.
|
StepSize
|
The number of seconds the propagated object is advanced when the Step command is executed.
|