Документ взят из кэша поисковой машины. Адрес оригинального документа : http://www.sai.msu.ru/neb/nss/evolu5e.htm Дата изменения: Mon May 31 00:49:47 2010 Дата индексирования: Mon Oct 1 20:52:05 2012 Кодировка:

Outer Natural Satellites Orbits Ephemerides. Outer satellites of Jupiter Choose type of the ephemeride: Trigonometric series for the orbital elements ( a, e, i, ω, Ω) Values of the orbital elements    [ output   e⋅sin(ω),  e⋅cos(ω),  sin(i)⋅sin(Ω),  sin(i)⋅cos(Ω) ] Distances between the osculating orbits Choose Satellite J06 - Himalia J07 J08 J09 J10 J11 J12 J13 J17 J18 J19 J20 J21 J22 J23 J24 J25 J26 J27 J28 J29 J30 J31 J32 J33 J34 J35 J36 J37 J38 J39 J40 J41 J42 J43 J44 J45 J46 J47 J48 J49 J50 S/2003 J2 S/2003 J3 S/2003 J4 S/2003 J5 S/2003 J9 S/2003 J10 S/2003 J12 S/2003 J15 S/2003 J16 S/2003 J18 S/2003 J19 S/2003 J23    of Jupiter Choose Second Satellite (for the distances) J07 - Elara J08 J09 J10 J11 J12 J13 J17 J18 J19 J20 J21 J22 J23 J24 J25 J26 J27 J28 J29 J30 J31 J32 J33 J34 J35 J36 J37 J38 J39 J40 J41 J42 J43 J44 J45 J46 J47 J48 J49 J50 S/2003 J2 S/2003 J3 S/2003 J4 S/2003 J5 S/2003 J9 S/2003 J10 S/2003 J12 S/2003 J15 S/2003 J16 S/2003 J18 S/2003 J19 S/2003 J23   For the Values and Distances     Enter initial date (years)       Enter final date (years) Enter step of dates (years)   Enter lower limits for amplutudes of semi-major axis Gm        eccentricity          inclination deg.          pericenter deg.                  node deg. Enter upper limit of frequency deg/year At least do not include short-period terms (f > n)