NORAD TLE CONVERSION FROM OSCULATING ORBITAL ELEMENT | Zendy

Byoung-Sun Lee | Zendy

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NORAD TLE CONVERSION FROM OSCULATING ORBITAL ELEMENT

Author(s) -

Byoung-Sun Lee

Publication year - 2002

Publication title -

journal of astronomy and space sciences

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.273

H-Index - 11

eISSN - 2093-5587

pISSN - 2093-1409

DOI - 10.5140/jass.2002.19.4.395

Subject(s) - osculating circle , orbital elements , orbit (dynamics) , orbital decay , orbital maneuver , line (geometry) , physics , mathematical analysis , mathematics , geometry , astrophysics , astronomy , aerospace engineering , engineering , spacecraft , satellite

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

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