the excentric from the mean anomaly of a planet. 
The angle SMN is therefore calculated from the series in 
*33 
the following manner : 
First term. 
R° 
/ - 
1 -f e 
Numb. 
Log. 1.7581226 
Log- 7- 1 9 6 9495 
8 -955°72i 
Log. 9-93<5*>534 
For 2d term .0000231 
Sum - o°. 1043553 
= SMH. CSM 
ACE = - 
1043322 Log. 9.0184187 
6'..i 5T67 
1 22°.. 52 ..49. 84 
Second term. 
Log. 1.7581226 
Log. 9.3221183 
Log- 4-393S990 
i5-474’399 
- O.3OIO3OO 
R° - 
d 
f- - ' 
2, Log. 
. , T ^5 ^ 73^99 
l 1 ~r e ) • Log. 9.8099602 
Numb. .0000231 Log. 5.363 1497 
: “ - 122 ..59. .5.51 
This differs from M. Delambre's conclusion only in the 
second place of the decimals. 
Example II. 
Supposing, with M. Delambre, that the mean anomaly in 
the same orbit is 96°, required the excentric anomaly. 
•75 
1.25 
We have as before 
Log. tan. 48 0 .. 
Log. tan. 33 .■4o / ..4i // .5i - - - , 
CSM = 81 ..40 ..41C51 
CMS = 14 .,19 ..18. 49 = 51558.49 
206264.8 
L °g- 9 7781513 
10.0455626 
- - 9.8237139 
Log. 4.7123003 
Lo g- 5-3 i44 2 5i 
CMS = .2499627 Log. 9.3978752 
