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by gaius 6491 days ago
Facial recognition by satellite is probably impossible. The Rayleigh formula states :

    angular resolution = (1.22 * wavelength) / diameter of lens. 
Now I don't know what altitude a spy satellite is at, so let's say 100 miles == 160,000 metres. Let's also say that you need a resolution of 1cm in order to recognize a face (probably you actually need better than that). Wavelength of light, to make the maths easy, 5x10^-7m.

    tclsh[1]% / [* 1.22 5e-07] [atan [/ 0.01 160000]]
    9.760000000000012
So that's a 10m lens, assuming you could make an optically perfect lens that big and get it into orbit. If you wanted a 1mm resolution, you would need a 100m lens. And you would probably want the entire spectrum of visible light. And I've probably guessed the altitude way too low as well...

Oh, and your subject would need to be looking straight up at the moment your satellite passed overhead on a perfectly clear day :-)

2 comments

A 10m mirror in orbit is not a big issue if it was done as a segmented mirror (e.g. what is planned for the Webb telescope) but to get to the "really cool" stage I would say that they would have had to deploy some sats that can work together to perform long baseline optical interferometry to get the same results as that 100m lens.
Now there are super-resolution techniques that allow you to see beyond the diffraction limit.
Feel free to post the relevant maths :-)