... Orbit trace . Predicted "landing point" coordinates . Orbit in the topocentrical c/s . The prediction based on the state vector of epoch 10/10/2000 give the results as follows: . ... 13.8 deg. ... W - geographical coordinates of the "landing point" . The estimated accuracy of this prediction looks as follows: the RMS error of the time is 40 sec, the RMS errors of the latitude and longitude are .05 deg. and .1 deg. Modified 16 October, 2000 . ... IKI RAN | ... INTERBALL mission  ...