R1iBdZddlmZddlmZmZmZddlmZm Z ddl m Z ddl m Z mZdZdZdZeeefZd ZGd d eZGd d eZGddeZy)zThe Satellite class.) from_alpha5)wgs72oldwgs72wgs84)invjdayjday) twoline2rv)sgp4sgp4initg@cdeZdZdZdZdZedZedZe e fdZ dZ dZ d Zd Zy) Satrecz1Slow Python-only version of the satellite object.)~Omaaltaaltpamargpdotargpoatimeaycofbstarcc1cc4cc5classificationcon41d2d2201d2211d3d3210d3222d4d4410d4422d5220d5232d5421d5433dedtdel1del2del3delmodidtdmdtdnodtdomdte3eccoee2elnumemephtypeepoch epochdaysepochyrerror error_messageetagstoimincloinitintldesgirezisimpj2j3j3oj2j4 jdsatepochmdotmethodmmmomunddotndotnmno_kozai no_unkozainodecfnodedotnodeoomomgcof operationmodepeopghophopincoplo radiusearthkmrevnum satnum_strse2se3sgh2sgh3sgh4sh2sh3si2si3sinmaosl2sl3sl4tt2coft3coft4coft5coftuminx1mth2x7thm1xfactxgh2xgh3xgh4xh2xh3xi2xi3xkexl2xl3xl4xlamoxlcofxlixmcofxnizmolzmos jdsatepochFNc|jSN)rUselfs N/home/cursorai/projects/iching/venv/lib/python3.12/site-packages/sgp4/model.pynoz Satrec.no-s }}c,t|jSr)rrdrs rsatnumz Satrec.satnum1s4??++rct|}|}t|||d|t|jj xsd|_t|j |_|j }t|jd\}}|dz|dz dzz|zdz|_ t|d|_ |` |xj d zc_|S) Ni0?imr gB:Ad) gravity_constantsr intr:striprcr=divmodr<rLroundrr;)clsline1line2 whichconstryeardaysfractions rr zSatrec.twoline2rv5s&z2 u5%S$74<<--/637 $++& ||4h*qQ6= I 1- J   rc@t|}t|d\}}|dz}t|d|k(r t|d}||_||_t |\}}}}}}t |ddddd}|dz|_||z |z|_d|_ t||||||||| | | | | |y) NrgBArr rrU) rrrrLrrrr=r<rr )rropsmoderr;rrSrRr6rrCrPrUrYwholerwhole_jdymdHMSjan0s rr zSatrec.sgp4initNs&z2  ,x9$ ?e #Xq)H"#"8,1aAqAq!Q3'3w !D83!WfeUD%ueR5$ @rc||jz tz||jz tzz}t||\}}|j||fSr)rLminutes_per_dayrr r>)rjdfrtsincervs rr z Satrec.sgp4gsN'?:(((O;<D&!1zz1arc>t||\}}|j||fSr)r r>)rrrrs r sgp4_tsincezSatrec.sgp4_tsincems#D&!1zz1arcH|j}|ddlm}|t_g}tt ||}|D]&\}}|j |j ||(t |\}} } ||} || } || } t|dfx| _| _| | | fS)aCompute positions and velocities for the times in a NumPy array. Given NumPy arrays ``jd`` and ``fr`` of the same length that supply the whole part and the fractional part of one or more Julian dates, return a tuple ``(e, r, v)`` of three vectors: * ``e``: nonzero for any dates that produced errors, 0 otherwise. * ``r``: position vectors in kilometers. * ``v``: velocity vectors in kilometers per second. rarray) rnumpyrlistzipappendr lenshape)rrrrresultszjd_ifr_ielistrlistvlisterrs r sgp4_arrayzSatrec.sgp4_arrayqs  = # FL R JD$ NN499T40 1!7mue %L %L %LGQJ&!'!Qwr)__name__ __module__ __qualname____doc__ __slots__rpropertyrr classmethodWGS72r r r rrrrrrse;I( E ,,160@2  rrc$eZdZdZdZdZdZdZy) SatrecArrayz0Slow Python-only version of the satellite array.)_satrecsNcN||_|jddlm}|t_yy)Nrr)rrrr)rsatrecsrs r__init__zSatrecArray.__init__s# ::  # %K  rcg}tt||}|jD]-}|D]&\}}|j|j ||(/t|\}} } |j |} |j | } |j | } t |}t |j}||f| _||dfx| _| _| | | fS)aCompute positions and velocities for the satellites in this array. Given NumPy scalars or arrays ``jd`` and ``fr`` supplying the whole part and the fractional part of one or more Julian dates, return a tuple ``(e, r, v)`` of three vectors that are each as long as ``jd`` and ``fr``: * ``e``: nonzero for any dates that produced errors, 0 otherwise. * ``r``: (x,y,z) position vector in kilometers. * ``v``: (dx,dy,dz) velocity vector in kilometers per second. r)rrrrr rrr)rrrrrsatrecrrrrrrrrjdlenmylens rr zSatrecArray.sgp4s R mmF dv{{467 $"7mue JJu  JJu  JJu BDMM"%."E1--!'!Qwr)rrrrrrrr rrrrrs:I E&rrcLeZdZdZdZddZejZejZy) Satellitez:The old Satellite object, for compatibility with sgp4 1.x.rctt||||||}||jz tz}t||\} } | | fS)z@Return a position and velocity vector for a given date and time.)rrLrr ) rrmonthdayhourminutesecondjrrrs r propagatezSatellite.propagatesC uc4 8  O 3D!}1!t rN)r r rrr) rrrrrrrrrrrrrrs#DK B ]]FrrN)r sgp4.alpha5rsgp4.earth_gravityrrrsgp4.extrrsgp4.ior sgp4.propagationr r WGS72OLDrWGS84rrobjectrrrrrrrsc#55"+   eU*VB+&+Z  r