Description
Returns the X, Y, Z, VX, VY and VZ components of the current state of the Spacecraft, referenced from the CentralBody.
Timing Precision Mode
This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.
Click here to see the documentation for this object in nanosecond timing precision mode.
Overload List
Signatures
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Return Value
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Description
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Spacecraft.GetCartesianState()
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Array
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Returns the X, Y, Z, VX, VY and VZ components of the current state of the Spacecraft in the ICRF, referenced from the CentralBody. The reference frame will be evaluated at the Spacecraft's epoch.
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Spacecraft.GetCartesianState(Variable referenceFrame)
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Array
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Returns the X, Y, Z, VX, VY and VZ components of the current state of the Spacecraft in the specified frame, referenced from the CentralBody. The reference frame will be evaluated at the Spacecraft's epoch.
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Spacecraft.GetCartesianState(Variable referenceFrame, Variable frameEpoch)
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Array
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Returns the X, Y, Z, VX, VY and VZ components of the current state of the Spacecraft in the specified frame, referenced from the CentralBody. The reference frame will be evaluated at the specified frameEpoch.
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See also
Spacecraft Object
Spacecraft Propagation Guide
Coverage and Contact Analysis Guide
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