Computing...

Input information:

mean anomaly | 85°  (degrees)\neccentricity | 0.6


Results for orbital motion:

eccentric anomaly (E) | 115.9°  (degrees)\ntrue anomaly (f) | 145.2°  (degrees)\nflight path angle (phi_fpa) | 34°  (degrees)\nradial distance from primary focus (r) | 12623 km  (kilometers)\n(radial position computed assuming semi-major axis (a) 10,000 km)


Relation between eccentric anomaly and true anomaly:


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