Based on the Two line elements(TLE) - Input from the user, the program calculates the time and the date of the satellite pass. Prints out Azimuth and Elevation & plots it too.
TLE's can be obtained from www.celestrak.com
Prabhakar Subrahmanyam (2019). GUI based Satellite Tracking System (https://www.mathworks.com/matlabcentral/fileexchange/982-gui-based-satellite-tracking-system), MATLAB Central File Exchange. Retrieved .
Error in stsnew ?!
Undefined function or variable 'pro'.
Error in elaz (line 50)
K3 = (doe+pro);
where to change the inclination?
not very professional. Also, why is the azimuth 90 or 270?
incl has to be changed to i in order to work
This program would be great for a paper I'm writing but I meet the same problem computing i (inclination): Matlab tells me ther's a callback function problem.
Error in stsnew
Undefined function or variable 'incl'
Error in ==> elaz at 75
i = incl*degtorad; %Inclination
Error while evaluating uicontrol Callback
really good program and it works..
very good keep it up
This is a very useful and excellent program.
Thanks for sharing your code.
Good and Neat GUI
Moving to the Aerospace category from Physics.