Untitled

% Loop through each TLE file    
for i = 1:7758
    tleFile = tleFiles{i};
    tleFilePath = tleFile;
    [epochYearArray, month, day] = extractTLEData(tleFilePath);
    
    try
        % Create the satellite object using the TLE file
        sat = satellite(sc, tleFile);
        
        % Calculate the year for the specified date
        year = 2000 + epochYearArray;
        
        % Specify the time for which you want to get position and velocity
        time = datetime(year, month, day, 12, 0, 0);

        % Compute position and velocity in ECEF coordinate frame
        [position, velocity] = states(sat, time, "CoordinateFrame", "ecef");

        % Display the results
        disp("TLE File: " + tleFile);
        position_realn(i) = (norm(position') / 1000) - 6371;
        velocity_realn(i) = norm(velocity') / 1000;
        disp(time);
        disp("Position (ECEF) [km]: " + position_realn(i));
        disp("Velocity (ECEF) [km/s]: " + velocity_realn(i));
        disp("-------------------------------");

    catch exception
        fprintf('Inconsistent data in iteration %d, skipped.\n', i);
        disp("Error Message: " + exception.message);
    end
end