classical_orbit_elements_line_chart

ansys.stk.extensions.data_analysis.graphs.satellite_graphs.classical_orbit_elements_line_chart(stk_object: Satellite, start_time: Any = None, stop_time: Any = None, step: float = 60, colormap: Colormap = None, time_unit_abbreviation: str = 'UTCG', formatter: collections.abc.Callable[[float, float], str] = None) → Figure, Axes

Create a plot of the angles and the semimajor axis of the classical osculating orbital elements, sometimes referred to as Keplerian elements, computed using ephemeris with respect to the object’s J2000 coordinate system, as a function of time.

Eccentricity is not plotted.

This graph wrapper was generated from AGI\STK12\STKData\Styles\Satellite\Classical Orbit Elements.rsg.

Parameters:

stk_object : Satellite The STK Satellite object.

start_time : Any The start time of the calculation (the default is None, which implies using the scenario start time).

stop_time : Any The stop time of the calculation (the default is None, which implies using the scenario stop time).

step_time : float The step time for the calculation (the default is 60 seconds).

colormap : Colormap The colormap with which to color the data (the default is None).

time_unit_abbreviation : str The time unit for formatting (the default is “UTCG”).

formatter : Callable [[float, float], str] The formatter for time axes (the default is None).

Returns:

Figure The newly created figure.

Axes The newly created axes.

Import detail

from ansys.stk.extensions.data_analysis.graphs.satellite_graphs import classical_orbit_elements_line_chart