Antenna pattern (apparent FOV) is ideally a uniform toroid around the dipole, but recent analysis shows high pattern dependency on solar panel rotation. Worst case is when solar panels are parallel to the antenna, the pattern gets deformed (up to ~50% directivity on +Z boresight for some frequencies, ~1.2dB). This is currently under analysis/discussion with Project/Airbus to find solutions. SOC/PS to be aware and maybe track this for operational implications.
any rule that is used to schedule the observation: repetition rules, continuous (plasma instruments), one-off, every orbit, every day, etc