Xtt__text__TEXTPB__data__DATA__cstring__TEXT __literal8__TEXT__picsymbolstub2__TEXT}` __la_sym_ptr2__DATA=P __nl_symbol_ptr__DATAT0 __textcoal_nt__TEXTlH @ l P x USTE}~<\M䍃ʍXM䍃ʍE$TD$=$iPD$T$It$;$-$$LE}~ *M䍃YE荃PXEEH8uE$E$d\@D$\@D$\D$ M荃YD$4$7X@D$X@D$ XD$t$ET[] State vectors for NORAD precision test with the '%s' model: Start time: %15.8f dT X, Xdot Y, Ydot Z, Zdot [min] [km, km/s] [km, km/s] [km, km/s] %4.0f %19.9f %19.9f %19.9f %19.9f %19.9f %19.9f ?@;x⍀xP'"c⍀cP N⍀NP9⍀9P$⍀$P1$Ë$ d d d @  h qh ^h XG1T \  X     ` \ }I q` kc  ]XB 7d ( h  y sM)kM)e ` ZIRIL G AE9E3 . (A A  ==      &lpqf{W>_doNoradTest___i686.get_pc_thunk.bx___i686.get_pc_thunk.axdyld_stub_binding_helper_propModelType_initNorad_epochDay_propModel_satVelGl_satPosGl_getStateVector_getNoradStateVector_printf_checkPropModelType_printElements