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Searched refs:tle_line_2 (Results 1 – 4 of 4) sorted by relevance

/dports/misc/libpredict/libpredict-2.0.0/src/
H A Dorbit.c16 predict_orbital_elements_t* predict_parse_tle(const char *tle_line_1, const char *tle_line_2) in predict_parse_tle() argument
28 m->inclination = atof(SubString(tle_line_2,SUBSTRING_BUFFER_LENGTH,substring_buffer,8,15)); in predict_parse_tle()
29 m->right_ascension = atof(SubString(tle_line_2,SUBSTRING_BUFFER_LENGTH,substring_buffer,17,24)); in predict_parse_tle()
30 …m->eccentricity = 1.0e-07*atof(SubString(tle_line_2,SUBSTRING_BUFFER_LENGTH,substring_buffer,26,32… in predict_parse_tle()
31 …m->argument_of_perigee = atof(SubString(tle_line_2,SUBSTRING_BUFFER_LENGTH,substring_buffer,34,41)… in predict_parse_tle()
32 m->mean_anomaly = atof(SubString(tle_line_2,SUBSTRING_BUFFER_LENGTH,substring_buffer,43,50)); in predict_parse_tle()
33 m->mean_motion = atof(SubString(tle_line_2,SUBSTRING_BUFFER_LENGTH,substring_buffer,52,62)); in predict_parse_tle()
39 …m->revolutions_at_epoch = atof(SubString(tle_line_2,SUBSTRING_BUFFER_LENGTH,substring_buffer,63,67… in predict_parse_tle()
/dports/misc/libpredict/libpredict-2.0.0/examples/basic/
H A Dmain.c12 const char *tle_line_2 = "2 25544 51.6464 275.3867 0006524 289.1638 208.5861 15.55704207942078"; in main() local
15 predict_orbital_elements_t *iss = predict_parse_tle(tle_line_1, tle_line_2); in main()
/dports/misc/libpredict/libpredict-2.0.0/
H A DREADME.md47 …rbital_elements_t *orbital_elements = orbital_elements = predict_parse_tle(tle_line_1, tle_line_2);
/dports/misc/libpredict/libpredict-2.0.0/include/predict/
H A Dpredict.h.in128 * \param tle_line_2 Second line of NORAD two-line element set string
132 predict_orbital_elements_t* predict_parse_tle(const char *tle_line_1, const char *tle_line_2);