Ballistic life-time
Orbit trace
Predicted "landing point" coordinates
Orbit in the topocentrical c/s
The prediction based on the state vector of epoch 06/09/2000 give the results as follows:
The estimated accuracy of this prediction looks as follows: the RMS error of the time is 2 min, the RMS errors of the latitude and longitude are .5 deg. and 1. deg.
To be continued. The more precise prediction will be done later.
Modified 19 September, 2000 Victoria Prokhorenko
