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,
![d = 4.3* 10^7\ km = 4.3* 10^(10)\ m](https://img.qammunity.org/2021/formulas/physics/college/nhwfn4b5gdb6rfjcfd95019yr5rof3sn0a.png)
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 :
![v=\sqrt{(GM)/(r)}](https://img.qammunity.org/2021/formulas/physics/college/n8adp9d0tyq1tsu0xdi23qi6h91b89ko1w.png)
M is the mass of the sun,
![M=2* 10^(30)\ kg](https://img.qammunity.org/2021/formulas/physics/college/n859sirmjpa6ndl3e9pz6f0gspx2fgxjpn.png)
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.