public static void UpdateElements(Astrobody body, double day)
{
var el = body.orbitalElements;
el.N = StarMath.WrapDeg(body.constants.N_offset + body.constants.N_scalar * day);
el.i = StarMath.WrapDeg(body.constants.i_offset + body.constants.i_scalar * day);
el.w = StarMath.WrapDeg(body.constants.w_offset + body.constants.w_scalar * day);
el.a = StarMath.WrapDeg(body.constants.a_offset + body.constants.a_scalar * day);
el.e = StarMath.WrapDeg(body.constants.e_offset + body.constants.e_scalar * day);
el.M = StarMath.WrapDeg(body.constants.M_offset + body.constants.M_scalar * day);
//CALCULATE SECONDARY ELEMENTS
el.L = StarMath.WrapDeg(el.N + el.w + el.M);
double E0 = el.M + StarMath.rad2deg * el.e * StarMath.Sin_d(el.M) * (1 + el.e * StarMath.Cos_d(el.M));
double E1 = 0;
do
{
double temp = E0;
E0 = E1;
E1 = temp - (temp - StarMath.rad2deg * el.e * StarMath.Sin_d(temp) - el.M) / (1 - el.e * StarMath.Cos_d(temp));
// console.log(`${planetType} ecc diff: ${Math.abs(E1 - E0)}`);
}while (Math.Abs(E1 - E0) > 0.005);
el.E = E1;
el.x = el.a * (StarMath.Cos_d(el.E) - el.e);
el.y = el.a * Math.Sqrt(1 - el.e * el.e) * StarMath.Sin_d(el.E);
el.r = Math.Sqrt(el.x * el.x + el.y * el.y);
el.v = StarMath.WrapDeg(StarMath.Atan2_d(el.y, el.x)); //is StarMath.WrapDeg nessecary? ie is negative bad?
el.unpertubatedEclitpticCart.x =
el.r * (StarMath.Cos_d(el.N) * StarMath.Cos_d(el.v + el.w) - StarMath.Sin_d(el.N) * StarMath.Sin_d(el.v + el.w) * StarMath.Cos_d(el.i));
el.unpertubatedEclitpticCart.y =
el.r * (StarMath.Sin_d(el.N) * StarMath.Cos_d(el.v + el.w) + StarMath.Cos_d(el.N) * StarMath.Sin_d(el.v + el.w) * StarMath.Cos_d(el.i));
el.unpertubatedEclitpticCart.z =
el.r * StarMath.Sin_d(el.v + el.w) * StarMath.Sin_d(el.i);
// el.eclipticSphere = el.eclitpticCart.ToEcliptic();
// el.eclipticSphere.longitude = StarMath.WrapDeg(el.eclipticSphere.longitude)//nesecary?
}