Searched refs:xmnpda (Results 1 – 13 of 13) sorted by relevance
106 (10.0 * fabs (sat->tle.xndt2o/(twopi/xmnpda/xmnpda)))); in decayed()117 (10.0 * fabs (sat->tle.xndt2o/(twopi/xmnpda/xmnpda)))) < sat->jul_utc) in decayed()
467 sat->tle.xndt2o / (twopi / xmnpda / xmnpda)); in show_sat_info()482 sat->tle.xndd6o * xmnpda / (twopi / xmnpda / xmnpda)); in show_sat_info()
69 sat->tsince = (sat->jul_utc - sat->jul_epoch) * xmnpda; in predict_calc()106 sat->orbit = (long)floor((sat->tle.xno * xmnpda / twopi + in predict_calc()
255 sat->orbit = (long)floor((sat->tle.xno * xmnpda / twopi + in gtk_sat_data_init_sat()
222 temp = twopi/xmnpda/xmnpda; in select_ephemeris()223 tle->xno = tle->xno*temp*xmnpda; in select_ephemeris()225 tle->xndd6o = tle->xndd6o*temp/xmnpda; in select_ephemeris()242 if (twopi/xnodp/xmnpda >= .15625) in select_ephemeris()
129 tsince = (jul_utc - jul_epoch) * xmnpda; in main()
282 Scale_Vector( xkmper*xmnpda/secday, vel ); in Convert_Sat_State()
87 #define xmnpda 1.44E3 /* Minutes per day */ macro
364 temp = twopi/xmnpda/xmnpda; in select_ephemeris()368 sat->tle.xno = sat->tle.xno * temp * xmnpda; in select_ephemeris()370 sat->tle.xndd6o = sat->tle.xndd6o * temp / xmnpda; in select_ephemeris()387 if (twopi/xnodp/xmnpda >= .15625) in select_ephemeris()
216 #define xmnpda 1.44E3 /* Minutes per day */ macro
84 double tsince = (jul_utc - jul_epoch) * xmnpda; in getSpherical()
55 #define xmnpda 1.44E3 /* Minutes per day */ macro485 Scale_Vector(xkmper*xmnpda/secday, vel); in Convert_Sat_State()731 temp=twopi/xmnpda/xmnpda; in select_ephemeris()732 tle->xno=tle->xno*temp*xmnpda; in select_ephemeris()734 tle->xndd6o=tle->xndd6o*temp/xmnpda; in select_ephemeris()751 if (twopi/xnodp/xmnpda>=0.15625) in select_ephemeris()3793 tsince=(jul_utc-jul_epoch)*xmnpda; in Calc()3861 rv=(long)floor((tle.xno*xmnpda/twopi+age*tle.bstar*ae)*age+tle.xmo/twopi)+tle.revnum; in Calc()