Step 1:
We start by using the relativistic velocity addition formula, which is given by:
\[v_{rs} = \frac{v_{re} - v_{se}}{1 - \frac{v_{re}v_{se}}{c^2}}\]
where \(v_{rs}\) is the velocity of the rocket with respect to the spaceship, \(v_{re}\) is the velocity of
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