meanAnomaly
Mean Anomaly
https://schema.space/metasat/meanAnomaly
Description: The fraction of an elliptical orbit's period that has elapsed since the orbiting body passed periapsis, expressed as an angle which can be used in calculating the position of that body in the classical two-body problem (source)
Example: 160°
Synonym(s): None
Concept Segments: Space Segment
Concept Families: Observation, Orbital Mechanics
Crosswalk Identifiers