INTERBALL TAIL PROBE
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The modified (by backward integration) orbital elements are usedduring the aposteriory situation analysis. See collection of the orbital elements and the accuracy problems of the SC motion calculations. The satellite position in the various coordinate systems and different parameters along the orbit as a function of time are shown on the plots and represented in the numerical files. The footprints magnetic mapping and magnetic conjugations with ground based magnetic observatories and with the other related Interagency missions are shown as well. The simulative magnetic conjugations are calculated for the following groundbased magnetic observatories: EISCAT (Northern Scandinavia) and SUPER-DARN net, and for the following Interagency missions: POLAR (NASA) and GEOTAIL (NASA, ISAS). |
Space Research Institute (IKI) Moscow, Russia |
Victoria Prokhorenko Nadezhda Belyaeva |