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Path: Orbit/OrbitCoord
-------------------------------------------------------------------------- Compute two-line elements from osculating elements -------------------------------------------------------------------------- Form: sTLE = ComputeTLE( elOsc, jD, Bstar ) -------------------------------------------------------------------------- ------ Inputs ------ elOsc (1,6) Osculating elements [a,i,W,w,e,M] jD (1,1) Julian date Bstar (1,1) Bstar drag parameter ------- Outputs ------- sTLE (3,:) Two-line elements string -------------------------------------------------------------------------- Reference: NORAD TLE CONVERSION FROM OSCULATING ORBITAL ELEMENT, Byoung-Sun Lee, J. Astron. Space Sci. 19(4), 395-402 (2002) --------------------------------------------------------------------------
Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2Date Orbit: OrbitMechanics/MeanMotn Orbit: OrbitMechanics/NORADToEl SC: BasicOrbit/RV2El
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