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Turns out variable (on/off based on an MEM file) inter-satellite links isn't really doable, but this is the way to do it : two sensors on the satellite (2 IRIDIUM antennas or 2 GNSS antennas, depending on the simulation) with their own specs (angle, frame). Also have mission events in VTS linked to the respective IRIDIUM and GNSS satellites that say AOS_1 and LOS_1 (1 or 2 depending on the sensor) when there is a visibility window with TOLOSAT as computed by the Python code.
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