The TLI burn is timed so that as the spacecraft nears apogee it enters the Moon's sphere of influence, making a hyperbolic lunar swingby.
The spacecraft enters the Moon's sphere of influence, making a hyperbolic lunar swingby. The TLI burn is timed so that as the spacecraft nears that apogee the Moon is nearby.
The TLI burn is timed so that as the spacecraft nears that apogee the Moon is nearby. The spacecraft enters the Moon's sphere of influence, making a hyperbolic lunar swingby.
The TLI burn is timed so that as the spacecraft nears that apogee the Moon is nearby. The spacecraft enters the Moon's sphere of influence, making a hyperbolic lunar swingby.