speed of planet moving in elliptical orbit is doubled when move at apagee. The eccentricity of the orbit is 0.5 Due to inctease in speed its onew orbit will be:-
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Explanation:
Apogee is the farthest position from focus the planet goes to.
Perigee is the nearest position from focus the planet reaches.
From Kepler's law,
T
2
∝R
3
Hence as in this movement from apogee to perigee, R decreases, so T decreases, and hence the speed must increase.
Clearly the distance from focus(Sun) decreases.
Potential energy of system is −
r
GMm
as 'r' decreases, so does the potential energy(since it is negative).
Angular momentum is conserved since there is no external torque acting on the system of Sun and planet.
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