Propagator11Parameters#

class ansys.stk.core.stkobjects.Propagator11Parameters#

Bases: IPropagator

The 11-Parameter propagator models geostationary satellites using 11-Parameter files. The propagator uses an algorithm documented in Intelsat Earth Station Standards (IESS) IESS-412 (Rev. 2), available at www.celestrak.com.

Overview#

propagate

Propagates the satellite’s path using the specified time interval.

step

Step size. Uses Time Dimension.

ephemeris_interval

Get the propagator’s ephemeris interval.

parameter_files

Return a collection of 11-Parameter satellite definitions.

Import detail#

from ansys.stk.core.stkobjects import Propagator11Parameters

Property detail#

property Propagator11Parameters.step: float#

Step size. Uses Time Dimension.

property Propagator11Parameters.ephemeris_interval: ITimeToolTimeIntervalSmartInterval#

Get the propagator’s ephemeris interval.

property Propagator11Parameters.parameter_files: Propagator11ParametersDescriptorCollection#

Return a collection of 11-Parameter satellite definitions.

Method detail#

Propagator11Parameters.propagate(self) None#

Propagates the satellite’s path using the specified time interval.

Returns:

None