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pan Hole
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At page http://www.qsl.net/vk3jed/doppler.html" is discussed Doppler shift at various ham radio frequencies. I calculated for this Doppler shift relative velocity of their satellite as 6720 m/s. Their satellite in height of 800 km above ground and at circular orbit should have velocity of 7453 m/s (orbital speed). I thought that difference between these two values should be max 465 m/s (rotation of Earth at equator), but it is almost twice as much... Any ideas?
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