Q 1824134051.     A satellite is in an elliptic orbit around the earth with aphelion of 6R and
perihelion of 2R where R = 6400 km is the radius of the earth. Find
eccentricity of the orbit. Find the velocity of the satellite at apogee and
perigee. What should be done if this satellite has to be transferred to a
circular orbit of radius 6R?


[`G = 6.67 xx 10^(- 11)` SI unit and `M = 6 xx 10^( 24) kg`]

NCERT Exemplar 07/38/LAT
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