You have to consider how low that orbit is. ISS is closer to earth than SF is to LA for example.
At 21,000 meters, the U-2 didn't fly that high. That's only a half marathon, and many people can run that distance easily.
In other words, I fail to understand your point, even omitting the 7.9km/second sideways velocity for LEO.
Most of the difficulty to orbit isn't distance, it's the amount of energy it takes to get something moving that fast.
Actually it's much, much worse than that, because it's actually the change in momentum involved.
I think it's logarithmic, but my math is bad.
The problem is the rocket equation. Yes, there's a natural log in there, but working against our favor.