When a rocket accelerates in space, its trajectory, initially an ellipse, changes in both shape and size, while the Earth remains one of the foci. The new path intersects the old trajectory at the point of acceleration, maintaining the height at that location. As the rocket surpasses escape velocity, the trajectory transitions from an elliptical orbit to a hyperbolic path, indicating it is no longer in orbit. The second focus of the ellipse can shift, particularly during changes in inclination. The discussion highlights the complexities of orbital mechanics, especially with varying thrust conditions.