GEO LEO SSO
Geosynchronous orbit has a circumference of 265000km and Earth has a diameter of 12600km so the shadow of a GEO satellite races across half the equator in a little over an hour once each day. The area of the Earth that catches sun light is 125 million square km. From the point of view of someone on the equator, in theory it would be possible to detect a tiny dot flicking across the sun once per day but it is not something you would be able to see. Loss of sunlight: 4 parts per billion, but you get back some of that energy from the microwaves.
For a low Earth orbit, the satellite spends about half its time in shadow over the night side and the other half casting a shadow over the day side. That area of Earth that catches sunlight still applies. If you happen to be on the very narrow path of the shadow you might notice the sun dim for a tenth of a second. Again, some of the tiny fraction of sunlight blocked by the satellite would be made up for by the microwave energy beamed from the satellite. Less this time because a LEO satellite spend half its time in shadow while the GEO is in the dark for far less time.
What I have seen of SOLARIS is extremely vague. I think they are talking about sun synchronous orbit. This is a weird type of LEO. The satellite crosses over the dawn area of Earth, goes over one of the poles then back across the dusk to the other pole. The Earth is a slightly flattened sphere. The gravitational pull from the bulge twists the orbit around so that the satellite remains in SSO despite the Earth going around the sun each year. The satellite would remain in sunlight all the time and its shadow would never fall on Earth. The satellite could only beam power down to stations almost directly below. These would only ever get coverage for a short time during dusk and dawn. Using several satellites each ground station could have a satellite over head each dusk and dawn. It would take many ground stations to take advantage of the continuous sunlight available to each satellite.
What gets me is the vagueness. I have to guess the orbit from clues in the slides. The conversion efficiency from sunlight to microwaves sounds impossible. Sunlight is a mixture of wave lengths. Layers of solar panels have a preferred wave length. Anything longer does not generate electricity. Anything shorter, some of the energy is wasted. If you are prepared to pay astronomical prices you can make a panel with a few layers, each with a different preferred wave length. The hinted conversion efficiency seems to magic this problem away. Finally, the really big one: what if you zero the cost of launching the satellites. How in space could these satellites and ground stations be cheaper than solar panels on Earth?