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CelestLab >> Orbit properties > CL_kp_v2M

CL_kp_v2M

True anomaly to mean anomaly

Calling Sequence

[M] = CL_kp_v2M(ecc,v)

Description

Parameters

ecc:

Eccentricity (PxN or Px1)

v:

True anomaly [rad] (PxN or Px1)

M:

Mean anomaly [rad] (PxN)

Authors

Bibliography

See also

Examples

ecc = 0.1;
v = 0.2;
M = CL_kp_v2M(ecc,v)
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