OrbitalElements

kepler.ts:27

Members

argumentOfPeriapsisreadonly

argumentOfPeriapsis: number

Argument of periapsis, radians.

eccentricityreadonly

eccentricity: number

Eccentricity, 0 ≤ e < 1. Hyperbolic trajectories are not modeled here.

epochreadonly

epoch: number

Simulation time the mean anomaly is quoted at, seconds.

inclinationreadonly

inclination: number

Inclination from the reference plane, radians.

longitudeOfAscendingNodereadonly

longitudeOfAscendingNode: number

Longitude of the ascending node, radians.

meanAnomalyAtEpochreadonly

meanAnomalyAtEpoch: number

Mean anomaly at the epoch, radians.

semiMajorAxisreadonly

semiMajorAxis: number

Semi-major axis, meters.