Step-by-step explanation:
It is given that,
Speed of the spacecraft, v = 71 km/s = 71000 m/s
Distance between the spacecraft and the Sun,
It is required to proof that its orbit about the sun was closed and therefore elliptical. Let v is the speed with which the spacecraft if it is moving in circular path. It is given by :
M is the mass of the sun,
v = 55698 m/s
or
v = 55.6 km/s
The given velocity is 71 km/s while the calculated value of velocity is 55.6 km/s. It is clear that the path is not circular. It is elliptical. Hence, this is the required solution.