Artful Dodger
"Neko no me"
This is way off topic so 1 question: How long does it take to deorbit from 90 km just due to atmospheric drag?
"Due to atmospheric drag, the lowest altitude above the Earth at which an object in a circular orbit can complete at least one full revolution without propulsion is approximately 150 km (93 mi) while the lowest perigee of an elliptical revolution is approximately 90 km (56 mi)"
Orbital decay
Okay, I'll agree, for the sake of the forum, that it IS way off topic.
Since we inda 'zone now, I'll answer the question: anything in a cirular orbit below 150 km, or an elipitical orbit with a perigee of less than 90 km, will deorbit in less than 1 orbit due to atmospheric drag. And that's from ORBITAL speed, not a paltry Mach 2ish.
Sir Richard never left Earth's atmosphere, by it's functional definition (ie: it's effect on sattelites).
Cheers!