2. The apocenter distance of an earth satellite in an elliptical orbit is 27,500 km. with a velocity of 13,600 km./hr. Determine the eccentricity, e of the satellite's orbit path.

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2. The apocenter distance of an earth satellite in an elliptical orbit is 27,500
km. with a velocity of 13,600 km./hr. Determine the eccentricity, e of the
satellite's orbit path.
Transcribed Image Text:2. The apocenter distance of an earth satellite in an elliptical orbit is 27,500 km. with a velocity of 13,600 km./hr. Determine the eccentricity, e of the satellite's orbit path.
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