ssapy.compute
Tools for orbital dynamics, satellite tracking, and celestial mechanics.
Functions
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Calculate observed altitude and azimuth of orbiting objects as viewed at specified times and locations. |
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Calculate observed direction-cosines of orbiting objects as viewed at specified times and positions. |
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Determine components of position r parallel and perpendicular to sun unit vector. |
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Find satellite overhead passes for a collection of observers. |
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Calculate satellite ground track on the outer product of all supplied times and state vectors or orbits. |
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Quickly estimate observed altitude and azimuth of orbiting objects as viewed at specified times and locations. |
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Calculate observed right ascension, declination, and slant range of orbiting objects as viewed at specified times and positions. |
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Calculate ra/dec rate and slant range rate of orbit at specified times and observer positions and velocities. |
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Convert object angles and observer position to 3D observer position |
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Refine a satellite overhead pass. |
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Calculate positions and velocities on the outer product of all supplied orbits and times. |
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Convert object and observer position and velocity to angles. |
Classes
A container for NumPy arrays that makes them hashable and immutable. |
Class Inheritance Diagram
