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CelestLab >> Orbit properties > CL_kp_M2v

CL_kp_M2v

Mean anomaly to true anomaly

Calling Sequence

[v] = CL_kp_M2v(ecc,M)

Description

Parameters

ecc:

Eccentricity (PxN or Px1)

M:

Mean anomaly [rad] (PxN or Px1)

v:

True anomaly [rad] (PxN)

Authors

Bibliography

See also

Examples

ecc = 0.1;
M = 0.2;
v = CL_kp_M2v(ecc,M)
<< CL_kp_M2Ecir Orbit properties CL_kp_characteristics >>