Searched refs:SUN_E (Results 1 – 2 of 2) sorted by relevance
506 static final double SUN_E = 0.016713; // Eccentricity of orbit field in CalendarAstronomer602 norm2PI(trueAnomaly(meanAnomaly, SUN_E) + SUN_OMEGA_G), in getSunLongitude()
532 #define SUN_E 0.016713 // Eccentricity of orbit macro655 longitude = norm2PI(trueAnomaly(meanAnomaly, SUN_E) + SUN_OMEGA_G); in getSunLongitude()