Step 1: Express the ratio of heat rejected to heat supplied for each engine.
For any reversible engine, \(Q_{out}/Q_{in} = T_L/T_H\), where \(T_L\) and \(T_H\) are the sink and source temperatures. For engine 1, working between \(T_2\) and 200 K:
\[
\frac{Q_{out}}{Q_{in}} = \frac{200}{T_2}
\]
For engine 2, working between 800 K and \(T_2\):
\[
\frac{Q_{out}}{Q_{in}} = \frac{T_2}{800}
\]
Step 2: Use the fact that both engines share the same heat input and output.
Since \(Q_{in}\) and \(Q_{out}\) are identical for both engines, the two ratios above must be equal:
\[
\frac{200}{T_2} = \frac{T_2}{800}
\]
Step 3: Solve for \(T_2\), which turns out to be the geometric mean of the two extreme temperatures.
\[
T_2^2 = 200 \times 800 = 160000
\]
\[
T_2 = \sqrt{160000} = 400 \text{ K}
\]
\[
\boxed{T_2 = 400 \text{ K}}
\]
This matches option 3.