SolarSystem.NoradKeplerEqTolerance Property |
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DescriptionThis property has been Deprecated. This property no longer has any effect.
Controls the tolerance used in solving Kepler's equation in the Norad propagator. 1e-12 is the value suggested in Spacetrack Report #6, and 1e-6 is the value suggested in Spacetrack Report #3.
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.
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