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http://dx.doi.org/10.5140/JASS.2002.19.4.395

NORAD TLE CONVERSION FROM OSCULATING ORBITAL ELEMENT  

Lee, Byoung-Sun (Communications Satellite Development Center, ETRI)
Publication Information
Journal of Astronomy and Space Sciences / v.19, no.4, 2002 , pp. 395-402 More about this Journal
Abstract
The NORAD type Two Line Element (TLE) was obtained from the osculating orbital elements by an iterative approximation procedure. The mathematical model was presented and computer program was developed for the conversion. The osculating orbital elements of the KOMPSAT-1 were converted into the NORAD TLE. Then the effect of the SGP4 atmospheric drag coefficient ($B^*$) was analyzed by comparison of the orbit propagation results with different $B^*$ values.
Keywords
NORAD; TLE; SGP4; Orbital Element; KOMPSAT;
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  • Reference
1 Won, C.-H., Lee, J.-S., Lee, B.-S., & Eun, J.-W. 1999, ETRI Journal, 21, 29   DOI
2 Serafin, R. A. 1982, Celestial Mechanics, 26, 383   DOI
3 Cho, C.-H., Lee, B.-S., Lee, J.-S., Kim, J.-H., & Choi, K.-H. 2002, JA&SS, 19, 197
4 Walter, H. G. 1967, AJ, 72, 994   DOI
5 Boelitz, C. A. 1995, Orbit Analysis Software Survey, Proceedings of the AAS/AIAA Astrodynamics Specialists Conference 1995, AAS 95-344
6 Hoots, F. R., & Roehrich, R. L. 1980, Models for Propagation of NORAD Element Sets- Project Space Track Report No. 3 (Peterson AFB: Aerospace Defense Command)
7 URL: http://www.orbitessera.com/html/body state vectors.html (cited March 1, 2002)
8 Escobal, P. R. 1965, Methods of Orbit Determination (New York: John Wiley & Sons)
9 Beck, E. V., & Boelitz, C. A. 1997, Orbit Analysis Software Survey 1996 Update, Proceedings of the AAS/AIAA Space Flight Mechanics Conference 1997, AAS 97-100
10 Jochim, E. F., Gill, E., Montenbruck, O., & Kirschner,M. 1996, Acta Astronautica, 39, 912   DOI   ScienceOn
11 Kelso, T. S. 1997, Satellite Times, 4, 68
12 Ernandes, K. 1994, AMSAT Journal, 17, 26