OrbitStateObservationGenerator Object

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Description

The OrbitStateObservationGenerator object creates observations to use in the fit of a trajectory. The typical use case is for when generating a Norad state as part of the NoradStateEstimator object.

 

Inheritance Hierarchy: ObjectàOrbitStateObservationGenerator

 

Available In Editions:

Mission

 

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

 

Properties
Methods

 

See also

Norad Two-Line Element Set File

Using Two-Line Element Sets

NoradStateEstimator

TLECatalog

TwoLineElement