Description
Child object of the Spacecraft holding the NoradSGP4 orbital state.
Users cannot create instances of this type of object. However, users can access instances of this object type that have been created indirectly, for example as children of other objects. Users can also access any static properties and methods on this object type.
Inheritance Hierarchy: ObjectàNoradSGP4State
Available In Editions:
Engineer
Mission
Timing Precision Mode
This page describes functionality in nanosecond timing precision mode.
Name
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Description
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DeclaredName
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The name of the object as declared.
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DisplayName
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The name displayed for this object in output windows such as views, plots, and reports.
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E
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The NoradSGP4 element set Eccentricity.
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I
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The NoradSGP4 element set Inclination, referenced to the True Equator Mean Equinox coordinate frame.
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MA
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The NoradSGP4 element set Mean Anomaly.
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MeanMotion
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The NoradSGP4 element set Mean Motion.
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ObjectId
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The unique identifier for the object.
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ObjectType
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The type of the object.
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RAAN
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The NoradSGP4 element set Right Ascension of the Ascending Node, referenced to the True Equator Mean Equinox coordinate frame.
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W
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The NoradSGP4 element set Argument of Perigee, referenced to the True Equator Mean Equinox coordinate frame.
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Name
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Description
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ClearSavedStates
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Clears previous saved states for this object.
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GetFromFile
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Load the object state from the specified FreeFlyer object file.
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GetFromString
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Load the object state from the specified string.
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PutToFile
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Convert the object state to FreeFlyer object xml and write to a file.
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PutToString
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Convert the object state to FreeFlyer object xml and return as a string.
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ReferenceEquals
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Returns 1 if the argument refers to the calling object and 0 otherwise.
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Restore
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Restore an object's state from a previously saved state.
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Save
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Save the object's state so that it can be restored later.
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