It seems you lopped 10 000 km off just to make it work, to get it below the 21245 km/hr speed of the Falcon.
I lopped it off because it was a convenient figure and with how much map disagreement there is, it can be argued world would be a bit smaller. Sure, it happens to be within range of basically the fastest essentially-in-atmosphere manmade vehicle, but that's not much of a concession given that both of those disintegrated, and honestly was just coincidence. I used a smaller value simply because if we stuck with the RE measurement, a lot of people would reject it there and then. Always better to go lower, if you don't give something every chance then you've not made a persuasive argument against, and equally you wouldn't end up with the parameters of possibility if it does end up working.
For a lower bound agreed upon by everyone we would need to consider Sandokhan's map/FE
Sandokhan's model has very different physics which, like I mentioned, I'm not yet appealing to. He explains the ISS (and indeed other satellites) with reference to laevorotatory subquarks and an antigravity effect which, yeah, fixes a lot of problems but also need a lot of changes to accepted physics to get to. Sandokhan's model of chronological and spatial scales only exist as far as I've seen within such models.
But that assumes it is just the one body. You may have multiple such craft completing much smaller loops at a higher or lower speed (or alternatives which don't have a physical craft).
Given that the ISS is in sight theoretically nearly all the time, except when it's oversea, the practicalities of that don't really help, especially with it only being visible from one location at a time. You might be able to use it as an explanation for the ISS crossing an ocean, I suppose, vanishing from one side and another one continuing the journey, but issues like that are why I used such a low bound. However many objects there are, with only one visible at a time this suffices as a lower estimate.
What theory is your lower bound based on? Please tell us. You can't just make up some smaller lower bound that makes it less difficult for your faking scenario.
Yes. I can. That's the
point. It's
lower. Still faces plenty of problems, but if at the end of all this the conclusion is "The ISS can be faked with no difficulty whatsoever so long as you accept a 30,000km length equator," are you really so insecure that that bothers you?
It is a value that is low enough to feasibly contain most if not all FE models and still allow room to explore. Key word: low. I am giving this model every chance to work so that either a) it will be especially convincing if it turns out not to work, b) it will give an idea of how feasible FET is and ballpark estimates of various values if it does work, thus givng more data that can be discussed elsewhere. If that seriously bugs you so much,
butt out.