Searched refs:tle_line_1 (Results 1 – 4 of 4) sorted by relevance
| /dports/misc/libpredict/libpredict-2.0.0/src/ |
| H A D | orbit.c | 16 predict_orbital_elements_t* predict_parse_tle(const char *tle_line_1, const char *tle_line_2) in predict_parse_tle() argument
23 m->satellite_number = atol(SubString(tle_line_1,SUBSTRING_BUFFER_LENGTH,substring_buffer,2,6)); in predict_parse_tle()
24 m->element_number = atol(SubString(tle_line_1,SUBSTRING_BUFFER_LENGTH,substring_buffer,64,67)); in predict_parse_tle()
25 m->epoch_year = atoi(SubString(tle_line_1,SUBSTRING_BUFFER_LENGTH,substring_buffer,18,19)); in predict_parse_tle()
26 strncpy(m->designator, SubString(tle_line_1,SUBSTRING_BUFFER_LENGTH,substring_buffer,9,16),8); in predict_parse_tle()
27 m->epoch_day = atof(SubString(tle_line_1,SUBSTRING_BUFFER_LENGTH,substring_buffer,20,31)); in predict_parse_tle()
34 …m->derivative_mean_motion = atof(SubString(tle_line_1,SUBSTRING_BUFFER_LENGTH,substring_buffer,33… in predict_parse_tle()
35 tempnum=1.0e-5*atof(SubString(tle_line_1,SUBSTRING_BUFFER_LENGTH,substring_buffer,44,49)); in predict_parse_tle()
36 m->second_derivative_mean_motion = tempnum/pow(10.0,(tle_line_1[51]-'0')); in predict_parse_tle()
37 tempnum=1.0e-5*atof(SubString(tle_line_1,SUBSTRING_BUFFER_LENGTH,substring_buffer,53,58)); in predict_parse_tle()
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| /dports/misc/libpredict/libpredict-2.0.0/examples/basic/ |
| H A D | main.c | 11 const char *tle_line_1 = "1 25544U 98067A 15129.86961041 .00015753 00000-0 23097-3 0 9998"; in main() local
15 predict_orbital_elements_t *iss = predict_parse_tle(tle_line_1, tle_line_2); in main()
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| /dports/misc/libpredict/libpredict-2.0.0/ |
| H A D | README.md | 47 predict_orbital_elements_t *orbital_elements = orbital_elements = predict_parse_tle(tle_line_1, tle…
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| /dports/misc/libpredict/libpredict-2.0.0/include/predict/ |
| H A D | predict.h.in | 127 * \param tle_line_1 First 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);
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