It's actually a lot worse than that, for two reasons:
1) 325kg mass is not accurate for iROSA, as that was for a prototype unit that was permanently jettisoned after the test and presumably didn't provide the same power as the final design. For the final design, SpaceX CRS-22 launched the first two permanent iROSA arrays with a combined mass of 1380kg, or 690 kg per array (https://www.nasa.gov/wp-content/uploads/2021/05/spacex_crs-22_mision_overview_high_res.pdf). This also ignores the mass of the parts of the existing solar system that are being re-used, which includes everything from the mounting hardware to the station, the motors to re-orient the panels, and all the electrical systems. 690kg is for basically just the bare panels and nothing else.
2) You did the math of 325kg against the entire iROSA system instead of just a single array. The new arrays (at 690 kg) provide 28 kW of power each, expected to drop to 20 kW within 10 years.
Even if we ignore the mass of all the electrical equipment and mounting equipment a standalone install would require, we still get 690kg for 20 kw, which gives us 185 watts = 6.4 kg, more than an order of magnitude more than 0.5.