King 13 2.5700 +61.1775 10.0 0.56 0.04 12.36 0.27 2960 400 8.85 0.05 NGC 136 7.8858 +61.5083 4.0 0.70 0.09 13.59 0.14 5220 350 8.40 0.05 Berkeley 19 81.0117 +29.5711 5.0 0.61 0.05 0.72 12.38 0.40 3000 600 9.25 0.05 Czernik 21 81.6708 +36.0136 6.0 0.72 0.02 0.56 11.82 0.20 2300 200 9.55 0.05 Stock 8 82.0367 +34.4314 8.0 1.21 0.04 0.57 9.84 0.20 900 110 7.50 Kronberger 1 82.0917 +34.7733 5.0 0.43 ...

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... 23 Algorithm fo r evalua tion of two burn maneuv ers using linearity Input information: ( t t E1 , rEI , v t1L , t E2 2L ( ) EI )T )T ­ ­ ­ ­ the time and the state vector of initial orbit for this time ; interval of possible thrusts for transition from initial orbit to the transfer on e; the time and the state vector of the target orbit for this time ; ... We cal culate the state vector for the initial orbit for the time t1a and the target one ­ for the time t2 a . ...

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