Preliminary considerations
Given the differential quality of the orbital bones compared to those in the cranial vault, we first assessed the feasibility of placing laser fiber anchoring screws in the orbit in this bony region. To this end, a dry skull was employed to simulate the plan previously established in the BrainLab Workstation (Figs. 1A and 1B and Figs. 3A and 3B).
Entry point and trajectory planning
From the planning—both cadaveric and radiological simulations—it became clear (further explained in the next paragraph) that the ideal entry point in the orbit should be in the inferolateral quadrant of the orbit, specifically on the lateral wall, on the greater wing of the sphenoid, between 15 to 20 mm lateral to the upper portion (posteromedial segment) of the inferior orbital fissure and between 5 to 10 mm superior to the lower portion (anterolateral segment) of the inferior orbital fissure (Fig. 1F and 2F). 21 A strategy that was proven useful in locating this point was to first define the laterality of the entry in the axial tomography following the inferior rectus muscle to its insertion near the upper portion of the inferior orbital fissure (Fig. 1G) and mark the entry here, lateral to the inferior orbital fissure, in its upper portion, between 15–20 mm. The verticality in the sagittal plane was then defined, positioning it superior to the inferior orbital fissure (lower portion) between 5 and 10 mm (Fig. 1H).
We consider this entry area to be the most appropriate because it allows sufficient medial access to encompass the entire amygdala-hippocampus-parahippocampus complex, lateral enough to minimize compression of the orbital contents, and inferior enough to avoid injury to the vascular structures within the superior orbital fissure, Sylvian fissure, and temporal pole (Fig. 1A, 1C, 1D, and 1E and Fig. 4A and 4B).
The localization of the entry point is a dynamic step that also depends on our goal, which is targeting the amygdala-hippocampus-parahippocampus complex. Both are planned in a coordinated and simultaneous manner (Fig. 1D and 1E), requiring slight adjustments to the orbital entry point and our cerebral target to encompass the largest possible volume of mesial temporal brain structures and ensuring a safe trajectory avoiding eloquent vascular and nervous structures (midbrain, optic tract, and optic radiations—the latter situated above the temporal cerebral ventricle) (Fig. 1-I).
Transorbital approach and placement of laser fiber
The transpalpebral route previously described for the transorbital approach was used. 18–24 Fig. 2 shows a previously used approach in a patient who underwent open surgery via the transorbital route for temporal pole epilepsy. We have included these images to better demonstrate the anatomical relationships of the approach. The superior and inferior orbital fissures are anatomical landmarks that help orient the entry point in the lateral wall of the orbit, specifically in the greater wing of the sphenoid, aided by the use of stereotaxy (with or without a frame) to find the previously defined entry point during planning (Fig. 2).
We used the BrainLab neuronavigation system to help us to locate a precise entry point previously planned at the workstation. A low-profile drill was then used to perform a minimal craniotomy until the dura mater was reached. The dura mater was opened using a stylet and monopolar coagulation device. The laser probe screw was secured under neuronavigation guidance. Finally, we placed the laser cooling catheter through the screw already fixed to the bone and inserted the laser fiber into the catheter assisted by neuronavigation too, and upon reaching the final target, we tightened the screw to the laser probe (Fig. 3).
The post-procedure average vectorial error was 1.3 ± 0.2 mm, confirmed by CT and MRI.
Once the actual trajectory was fused with real-case imaging techniques, we proved that the planned structures were reached in all four cases with adequate coverage of the amygdala-hippocampus-parahippocampal complex. These trajectories were safe for the vessels in live patient simulations.
When measuring the angles of the screws in relation to the sagittal midline plane in axial cuts of tomographies in the specimen and the radiological simulations (12 in total), all had a medial direction on average measuring 6.6 ± 3.6 degrees. Similarly, all the angles of the screws and radiological simulations (in relation to the Frankfurt plane) in sagittal cuts of tomography had a superior average direction of 4.8 ± 3.5.
Overall, we did not observe any significant difficulties in performing the transorbital approach guided by neuronavigation or in placing each screw in the lateral wall of the orbit. The only issue observed in all cases was severe compression of the orbital contents by the plastic head of the screw due to the short length of the laser probe screws for the orbit, which could be resolved with longer screws (Fig. 5). We further analyze this important difficulty in the discussion section.
Comparison between transorbital approach vs occipital approach
Figure 4 shows a comparison between the transorbital and occipital approaches (both approaches simulated in the same cases) for the laser fiber trajectories used to access the temporomesial structures (amygdala-hippocampus-parahippocampus). This comparison was made as a retrospective simulation of four pre-surgical radiological studies (eight orbits) of patients who underwent temporal lobe epilepsy surgery.
For the occipital approach with the laser fiber to the temporomesial structures, the boundaries are medial: the midbrain with its surrounding vasculature; laterally, the ventricle and optic radiations; and superiorly, the optic tract and optic radiations. This determined a possible entry angle in the axial and sagittal plane on average of 9.12 ± 1.5 o and 6.5 ± 1.1 o, respectively (Fig. 4C – 4E).
In the transorbital approach, the same boundaries for protection are shared with the occipital approach. In addition, the Sylvian fissure is a superior boundary. Particular attention should be paid to the lateromedial location of the entry point because a medial entry could exert excessive compression of the orbital content. According to previously published data 25, a distance greater than or equal to 15 mm laterally from the upper portion of the inferior orbital fissure or a distance less than 15 mm from the lateral orbital edge to the orbital content is acceptable (Fig. 5A). Taking this into account, the possible entry angles in the axial and sagittal plane averaged 4.8 ± 0.9 o and 5.7 ± 0.8 o, respectively (Fig. 4A – 4C).
Thus, with the occipital approach, slightly wider possible entry angles are obtained than with the transorbital approach. Therefore, there are more options for possible trajectories to approach the mesial temporal lobe.