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GPS Satellite broadcast ephemeris time is now referenced to TOC instead of TOE
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@ -197,7 +197,7 @@ void Gps_Ephemeris::satellitePosition(double transmitTime)
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a = d_sqrt_A*d_sqrt_A;
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a = d_sqrt_A*d_sqrt_A;
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// Time from ephemeris reference epoch
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// Time from ephemeris reference epoch
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tk = check_t(transmitTime - d_Toe);
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tk = check_t(transmitTime - d_Toc);
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// Computed mean motion
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// Computed mean motion
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n0 = sqrt(GM / (a*a*a));
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n0 = sqrt(GM / (a*a*a));
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