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There was a mistake in the satellite orbit radius expression:
rk = a0 * (1 + e0 * cos(ek)) + crc * cos(2 * u0k) + crs * sin(2 * u0k)it was replaced by:
rk = a0 * (1 - e0 * cos(ek)) + crc * cos(2 * u0k) + crs * sin(2 * u0k)check r_k expression in here