140 



DETERMINATION OF ELLIPTIC ORBITS. 



^ = ^-3874081 

 r* = ^2 +'8645336 

 #! = [9-6692113]r 1 



[-47712]^ 

 ' 



GI = - [8-6700167K?! - 9-5901555)(l + R 

 & = [9-6833924] (?!+ 0900552)(l + jB I 

 Vl = -[7-9242047](g 1 + 3874081)(1 + 

 ' = - -046775- [8-67002]^ -P' ai \ 

 P = -482383 + [9-68339]^ - P'& I III' 

 y = - -008399 - [7-92420]^ - F 7l J 



= P 2 + '9314223 

 = ? 2 2 + 1006681 



= [0-3183722]r 



- 3 



a 2 = + [9'2282738] (g 2 + 17286820)(1 - 

 &= - [9-9900800] (g 2 - -Q36I3Q9)(I - 

 y 2 = -[91026549](g 2 - 9314223)(1- J R 2 ) 



a"= 169151 -[9-22827] ^ 



y"= -126664 + [9-10265]E 2 +P // y 



P///== 



5599304 a 3 =- 



/3 3 = [9-6537308](g 3 - < 

 " 3 y 3 = [8'8361256](2 3 + -J 



a'" = - -240477 - [9-38107] 3 -P"'a 3 

 $"= + -450537 + [9-65373] R 5 - 



in, 



