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SGPPrep
MATLAB
SGPinp = SGPPrep(tle);
Description

Prepares extracted TLE data, such as output by TLEExtract, for use by the NORAD SGP propagators (old FORTRAN convention). It also determines which SGP model to use based on the period. In general SGP requires these units: time in minutes, distance in units of earth radii, angular quantities in radians.

Parameters
Parameters 
Description 
tle [struct] 
Contains the TLE ephemeris data (See TLEExtract
Return Values
Return Values 
Description 
SGPinp [struct] 
Processed TLE data, the output of SGPPrep 
SGPinp.SSC [string] 
Space Surveillance Catalog Number 
SGPinp.node0 [scalar] 
Right ascension (rad) 
SGPinp.omega0 [scalar] 
Argument of perigee (rad) 
SGPinp.M0 [scalar] 
Mean anomaly (rad) 
SGPinp.i0 [scalar] 
Inclination (rad) 
SGPinp.n0 [scalar] 
Mean motion (rad/day) 
SGPinp.e0 [scalar] 
Eccentricity 
SGPinp.n0dotOvr2 [scalar] 
First time derivative of Mean Motion /2 
SGPinp.n0ddotOvr6 [scalar] 
Second time derivative of Mean Motion /6 
SGPinp.BSTAR [scalar] 
BSTAR drag term 
SGPinp.EpoJD [scalar] 
Epoch Julian Date 
SGPinp.Period [scalar] 
Period (min) 
SGPinp.DEEP [bool] 
Deep space propagator flag 
References

  • Hoots F., Roehrich R., Spacetrack Report No.3, 1980, pg. 70-72

See Also
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