Given the equation of the elliptical orbit is (x+2.5)^2/22,350.25+y^2/22,344=1.
This equation can be written as
![\begin{gathered} ((x+2.5)^2)/(22350.25)+(y^2)/(22344)=1 \\ ((x+2.5))/((149.5)^2)+(y^2)/((149.479)^2)=1 \end{gathered}](https://img.qammunity.org/2023/formulas/mathematics/college/nluni2z0xk6rbmuu5broag0294lyz8k4lt.png)
Now, if we shift this path by 2.5 units to left then we get
![(x^2)/((149.5)^2)+(y^2)/((149.479)^2)=1](https://img.qammunity.org/2023/formulas/mathematics/college/xkntb0kzuxeipmqfcma3mw9fmc81vnqmwu.png)
The farthest distance of the earth from the sun will be 149.5 - 2.5 = 147 million of kilometers
Thus, option C is correct.