[ 2 24 ] 
This Angle, being thus determined, will give by 
the common Methods 137 0 . 48'. 33" -i-, for the true 
Anomaly or Angle at the Sun: The Sine of the true 
Anomaly being in Proportion to the Sine of the 
Anomalia Eccentri, as the Semi-conjugate Axis to 
the Planet’s Diftance from the Sun. So that the 
Equation of the Centre in this Example is ij 9 .. 
48'. 33 "i* 
Example II. 
For the. Orbit of Venus. 
Suppofing, as before, the mean Diftance t to be 
Unity, and the Eccentricity /to be 0,004985-7 ; the 
conftant Numbers for this Orbit willbe, 7= 0,9930117; 
50 = 6,4116* 2'= 1,762134 j: T = 0,1751217 ; 
~t= 0,0 1 27771; and the limiting Angle 
will appear to be about 303 Degrees. 
Example. Let M be 120°. 00'. 00", as in the 
former Example. Then, fince the mean Anomaly is, 
in this Cafe, not many times lefs than the limiting 
Angle, the general Rule muft be ufed as before ; ac- 
cording to which the Number M will appear to be 
3,172787.; the Sine of A will be 0,3217917 * the 
Angle A, 18 0 , 77132 * and the Multiple n't A, or 
Angle B ; for the firft Afiumption of the Anomalta 
Eccentri will be I20°,374i6. 
This Angle B will give, by the Method before ex- 
plained, the Angle .g = 120°, 34777, or 120°. 21'. 
44! fere, for the Anomalia Eccentri correct; the Er- 
ror of which will appear, upon Examination, to be 
but a fmali Part. of a Second. 
In 
