... 18.0069 ET Cet = Name |Tmz V798 EG Cha = CPD |- ... 25 06520 CO Pyx = GSC |6575.02880 CO Pyx = HV |08155 CO Pyx = IRAS |08430-2548 CO Pyx = NSV |04234 CO Pyx = Prager|3224 CP Pyx = AN |856.1936 CP Pyx = CSV |001376 CP Pyx = GSC |6576.01333 CP Pyx = HV |08163 CP Pyx = IRAS |08505-2503 CP Pyx = NSV |04286 CQ Pyx = AFGL |5254 CQ Pyx = IRAS |09116-2439 CQ Pyx = NSV |18155 VX Ret = EC |04030-5801 VX Ret = GSC |8507.00160 V356 Sge = Name |Mis V0981 V357 Sge = Name |Mis V0982 V358 Sge = ...

... 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 . ...