A satellite is orbits the earth in an elliptical orbit of eccentricity of 0.6. For the flight path angle ß = 10°, the value of eccentric anomaly is a) 0.6987 rad b) 0.4895 rad c) 0.5987 rad d) 0.2373 rad

Elements Of Electromagnetics
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This question is based on satellites, so I kept it under mechanical engineering. The question is attached as an image. Thank you.

A satellite is orbits the earth in an elliptical orbit of eccentricity of 0.6. For the
flight path angle 3 = 10°, the value of eccentric anomaly is
a) 0.6987 rad
b) 0.4895 rad
c) 0.5987 rad
d) 0.2373 rad
Transcribed Image Text:A satellite is orbits the earth in an elliptical orbit of eccentricity of 0.6. For the flight path angle 3 = 10°, the value of eccentric anomaly is a) 0.6987 rad b) 0.4895 rad c) 0.5987 rad d) 0.2373 rad
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