JUPITER ORBITAL ELEMENTS FOR GALILEO         May 1996

	Galileo was launched on October 18, 1989, on a five-year trajectory to Jupiter.  
On the way, Galileo's flight path took it on a flyby of Venus in February 1990, then of 
Earth in December 1990. These flyby encounters provided gravity assists to help the 
spacecraft gain enough velocity to reach Jupiter. A second Earth gravity assist in 
December 1992 followed a scientific flyby of the asteroid Gaspra in October 1991.  A 
second asteroid encounter with the main-belt asteroid Ida, came in 1993. In July 1995 
Galileo released a probe to descend into the Jovian atmosphere December 7 as the main 
Galileo spacecraft, the orbiter, flew by overhead to collect the probes scientific data. The 
interplanetary orbital elements for the flight path up to this point are given in another file 
called gllele, which precedes this one.  

	Earlier that day the orbiter spacecraft flew by the Jovian moon Io for a gravity 
assist, and later it used it rocket engine to go into the first of 11 orbits about Jupiter which 
would include flybys of the moons Ganymede, Europa and Callisto. 

	The following are classic orbital elements for the Galileo orbiter spacecraft after 
the atmospheric probe separated from it, as it went into Jovian orbit and then carried out 
the orbital tour, as updated in early 1996 by the Galileo Navigational Team at the Jet 
Propulsion Laboratory.  The coordinate system is Earth Mean Ecliptic, 1950 Equinox. 

	Dates (in year/month/day format) and times (in 24-hour format) are both in 
Universal Time (UTC), also known as Greenwich Mean Time (GMT). 
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
JUPITER CENTRAL BODY CHANGE TO IO, ORBIT 0: 
Orbital Elements valid from J.D. = 2449974.45685 ET  (95/09/13  
22:56:51 GMT) 
                       to   J.D. = 2450059.24097 ET  (95/12/07  
17:45:59 GMT) 
Epoch of Orbital Elements:  J.D. = 2449974.45685 ET  (95/09/13  
22:56:51 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -4103077.3        km 
 Eccentricity       1.070722 
 Inclination        5.149            degree 
 Node Angle         58.934           degree 
 Arg of Periapsis   90.684           degree 
 Mean Anomaly      -569.528          degree 
---------- 
IO, ORBIT 0, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450059.24097 ET  (95/12/07  
17:45:59 GMT) 
    Classical Orbital Elements 
    Io                      centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -27.0             km 
 Eccentricity       101.508187 
 Inclination        10.301           degree 
 Node Angle        -140.302          degree 
 Arg of Periapsis  -58.455           degree 
 Mean Anomaly       22.437           degree 
---------- 
IO, ORBIT 0, TO JOI BURN START: 
Orbital Elements valid from J.D. = 2450059.24097 ET  (95/12/07  
17:45:59 GMT) 
                       to   J.D. = 2450059.51975 ET  (95/12/08  
00:27:25 GMT) 
Epoch of Orbital Elements:  J.D. = 2450059.24097 ET  (95/12/07  
17:45:59 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -5871176.2        km 
 Eccentricity       1.048704 
 Inclination        5.352            degree 
 Node Angle         60.480           degree 
 Arg of Periapsis   90.739           degree 
 Mean Anomaly      -.674             degree 
---------- 
JOI BURN START TO JUPITER APOAPSIS, ORBIT 0: 
Orbital Elements valid from J.D. = 2450059.51975 ET  (95/12/08  
00:27:25 GMT) 
                       to   J.D. = 2450158.77723 ET  (96/03/16  
06:38:10 GMT) 
Epoch of Orbital Elements:  J.D. = 2450059.51975 ET  (95/12/08  
00:27:25 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    9814688.8        km 
 Eccentricity       .971233 
 Inclination        5.300            degree 
 Node Angle         60.964           degree 
 Arg of Periapsis   87.684           degree 
 Mean Anomaly       .206             degree 
---------- 
JUPITER APOAPSIS, ORBIT 0, TO GANYMEDE, ORBIT 1: 
Orbital Elements valid from J.D. = 2450158.77723 ET  (96/03/16  
06:38:10 GMT) 
                       to   J.D. = 2450261.77090 ET  (96/06/27  
06:29:04 GMT) 
Epoch of Orbital Elements:  J.D. = 2450158.77723 ET  (96/03/16  
06:38:10 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    10091803.7       km 
 Eccentricity       .917105 
 Inclination        5.357            degree 
 Node Angle         67.348           degree 
 Arg of Periapsis   81.352           degree 
 Mean Anomaly       179.818          degree 
---------- 
GANYMEDE, ORBIT 1, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450261.77090 ET  (96/06/27  
06:29:04 GMT) 
    Classical Orbital Elements 
    Ganymede                centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -179.3            km 
 Eccentricity       20.401721 
 Inclination        31.057           degree 
 Node Angle         85.615           degree 
 Arg of Periapsis   77.687           degree 
 Mean Anomaly      -.520             degree 
---------- 
GANYMEDE, ORBIT 1, TO JUPITER APOAPSIS, ORBIT 1: 
Orbital Elements valid from J.D. = 2450261.77090 ET  (96/06/27  
06:29:04 GMT) 
                       to   J.D. = 2450298.31008 ET  (96/08/02  
19:25:29 GMT) 
Epoch of Orbital Elements:  J.D. = 2450261.77090 ET  (96/06/27  
06:29:04 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    4970309.2        km 
 Eccentricity       .841256 
 Inclination        4.152            degree 
 Node Angle         59.723           degree 
 Arg of Periapsis   96.707           degree 
 Mean Anomaly      -3.783            degree 
---------- 
JUPITER APOAPSIS, ORBIT 1, TO GANYMEDE, ORBIT 2: 
Orbital Elements valid from J.D. = 2450298.31008 ET  (96/08/02  
19:25:29 GMT) 
                       to   J.D. = 2450333.29214 ET  (96/09/06  
18:59:39 GMT) 
Epoch of Orbital Elements:  J.D. = 2450298.31008 ET  (96/08/02  
19:25:29 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    4964416.1        km 
 Eccentricity       .843442 
 Inclination        4.177            degree 
 Node Angle         57.326           degree 
 Arg of Periapsis   99.096           degree 
 Mean Anomaly       179.962          degree 
---------- 
GANYMEDE, ORBIT 2, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450333.29214 ET  (96/09/06  
18:59:39 GMT) 
    Classical Orbital Elements 
    Ganymede                centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -174.9            km 
 Eccentricity       17.491549 
 Inclination        80.005           degree 
 Node Angle         77.729           degree 
 Arg of Periapsis   88.614           degree 
 Mean Anomaly       .065             degree 
---------- 
GANYMEDE, ORBIT 2, TO JUPITER APOAPSIS, ORBIT 2: 
Orbital Elements valid from J.D. = 2450333.29214 ET  (96/09/06  
18:59:39 GMT) 
                       to   J.D. = 2450364.08036 ET  (96/10/07  
13:54:41 GMT) 
Epoch of Orbital Elements:  J.D. = 2450333.29214 ET  (96/09/06  
18:59:39 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    4418597.8        km 
 Eccentricity       .827478 
 Inclination        2.269            degree 
 Node Angle        -8.482            degree 
 Arg of Periapsis   167.120          degree 
 Mean Anomaly      -4.663            degree 
---------- 
JUPITER APOAPSIS, ORBIT 2, TO CALLISTO, ORBIT 3: 
Orbital Elements valid from J.D. = 2450364.08036 ET  (96/10/07  
13:54:41 GMT) 
                       to   J.D. = 2450392.06329 ET  (96/11/04  
13:30:06 GMT) 
Epoch of Orbital Elements:  J.D. = 2450364.08036 ET  (96/10/07  
13:54:41 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    4413984.2        km 
 Eccentricity       .829388 
 Inclination        2.292            degree 
 Node Angle        -8.611            degree 
 Arg of Periapsis   167.252          degree 
 Mean Anomaly      -179.985          degree 
---------- 
CALLISTO, ORBIT 3, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450392.06329 ET  (96/11/04  
13:30:06 GMT) 
    Classical Orbital Elements 
    Callisto                centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -121.2            km 
 Eccentricity       29.924953 
 Inclination        13.779           degree 
 Node Angle         52.705           degree 
 Arg of Periapsis   98.275           degree 
 Mean Anomaly      -1.307            degree 
---------- 
CALLISTO, ORBIT 3, TO JUPITER APOAPSIS, ORBIT 3: 
Orbital Elements valid from J.D. = 2450392.06329 ET  (96/11/04  
13:30:06 GMT) 
                       to   J.D. = 2450415.36666 ET  (96/11/27  
20:46:57 GMT) 
Epoch of Orbital Elements:  J.D. = 2450392.06329 ET  (96/11/04  
13:30:06 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3512146.2        km 
 Eccentricity       .814721 
 Inclination        1.966            degree 
 Node Angle        -34.297           degree 
 Arg of Periapsis  -158.705          degree 
 Mean Anomaly      -16.814           degree 
---------- 
JUPITER APOAPSIS, ORBIT 3, TO EUROPA, ORBIT 4: 
Orbital Elements valid from J.D. = 2450415.36666 ET  (96/11/27  
20:46:57 GMT) 
                       to   J.D. = 2450436.78853 ET  (96/12/19  
06:54:27 GMT) 
Epoch of Orbital Elements:  J.D. = 2450415.36666 ET  (96/11/27  
20:46:57 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3514197.3        km 
 Eccentricity       .813654 
 Inclination        1.968            degree 
 Node Angle        -34.273           degree 
 Arg of Periapsis  -158.660          degree 
 Mean Anomaly      -179.935          degree 
---------- 
EUROPA, ORBIT 4, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450436.78853 ET  (96/12/19  
06:54:27 GMT) 
 
    Classical Orbital Elements 
    Europa                  centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -107.3            km 
 Eccentricity       22.030617 
 Inclination        178.208          degree 
 Node Angle         151.986          degree 
 Arg of Periapsis  -179.625          degree 
 Mean Anomaly      -1.008            degree 
---------- 
EUROPA, ORBIT 4, TO JUPITER APOAPSIS, ORBIT 4: 
Orbital Elements valid from J.D. = 2450436.78853 ET  (96/12/19  
06:54:27 GMT) 
                       to   J.D. = 2450452.57414 ET  (97/01/04  
01:45:44 GMT) 
Epoch of Orbital Elements:  J.D. = 2450436.78853 ET  (96/12/19  
06:54:27 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    2900585.7        km 
 Eccentricity       .776628 
 Inclination        1.964            degree 
 Node Angle        -34.364           degree 
 Arg of Periapsis  -162.364          degree 
 Mean Anomaly       1.977            degree 
---------- 
JUPITER APOAPSIS, ORBIT 4, TO EUROPA NON-TARGETED, ORBIT 5: 
Orbital Elements valid from J.D. = 2450452.57414 ET  (97/01/04  
01:45:44 GMT) 
                       to   J.D. = 2450468.55103 ET  (97/01/20  
01:12:27 GMT) 
Epoch of Orbital Elements:  J.D. = 2450452.57414 ET  (97/01/04  
01:45:44 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    2899664.7        km 
 Eccentricity       .777193 
 Inclination        1.960            degree 
 Node Angle        -34.405           degree 
 Arg of Periapsis  -162.329          degree 
 Mean Anomaly      -179.948          degree 
---------- 
EUROPA NON-TARGETED, ORBIT 5, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450468.55103 ET  (97/01/20  
01:12:27 GMT) 
    Classical Orbital Elements 
    Europa                  centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -126.2            km 
 Eccentricity       229.951822 
 Inclination        178.240          degree 
 Node Angle         166.979          degree 
 Arg of Periapsis  -173.154          degree 
 Mean Anomaly       .445             degree 
---------- 
EUROPA NON-TARGETED, ORBIT 5, TO JUPITER APOAPSIS, ORBIT 5: 
Orbital Elements valid from J.D. = 2450468.55103 ET  (97/01/20  
01:12:27 GMT) 
                       to   J.D. = 2450484.46469 ET  (97/02/04  
23:08:07 GMT) 
Epoch of Orbital Elements:  J.D. = 2450468.55103 ET  (97/01/20  
01:12:27 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    2898670.3        km 
 Eccentricity       .777155 
 Inclination        1.966            degree 
 Node Angle        -34.336           degree 
 Arg of Periapsis  -162.692          degree 
 Mean Anomaly       .366             degree 
---------- 
JUPITER APOAPSIS, ORBIT 5, TO EUROPA, ORBIT 6: 
Orbital Elements valid from J.D. = 2450484.46469 ET  (97/02/04  
23:08:07 GMT) 
                       to   J.D. = 2450500.21110 ET  (97/02/20  
17:02:57 GMT) 
Epoch of Orbital Elements:  J.D. = 2450484.46469 ET  (97/02/04  
23:08:07 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    2897813.4        km 
 Eccentricity       .777681 
 Inclination        1.970            degree 
 Node Angle        -34.301           degree 
 Arg of Periapsis  -162.723          degree 
 Mean Anomaly      -179.982          degree 
---------- 
EUROPA, ORBIT 6, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450500.21110 ET  (97/02/20  
17:02:57 GMT) 
    Classical Orbital Elements 
    Europa                  centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -106.5            km 
 Eccentricity       21.201785 
 Inclination        163.660          degree 
 Node Angle        -99.024           degree 
 Arg of Periapsis  -93.069           degree 
 Mean Anomaly      -.016             degree 
---------- 
EUROPA, ORBIT 6, TO JUPITER APOAPSIS, ORBIT 6: 
Orbital Elements valid from J.D. = 2450500.21110 ET  (97/02/20  
17:02:57 GMT) 
                       to   J.D. = 2450521.66582 ET  (97/03/14  
03:57:45 GMT) 
Epoch of Orbital Elements:  J.D. = 2450500.21110 ET  (97/02/20  
17:02:57 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3515030.3        km 
 Eccentricity       .814544 
 Inclination        1.478            degree 
 Node Angle        -31.306           degree 
 Arg of Periapsis  -169.607          degree 
 Mean Anomaly      -1.352            degree 
---------- 
JUPITER APOAPSIS, ORBIT 6, TO GANYMEDE, ORBIT 7: 
Orbital Elements valid from J.D. = 2450521.66582 ET  (97/03/14  
03:57:45 GMT) 
                       to   J.D. = 2450543.79976 ET  (97/04/05  
07:10:37 GMT) 
Epoch of Orbital Elements:  J.D. = 2450521.66582 ET  (97/03/14  
03:57:45 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3513041.0        km 
 Eccentricity       .815574 
 Inclination        1.894            degree 
 Node Angle        -29.007           degree 
 Arg of Periapsis  -171.858          degree 
 Mean Anomaly       179.778          degree 
---------- 
GANYMEDE, ORBIT 7, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450543.79976 ET  (97/04/05  
07:10:37 GMT) 
    Classical Orbital Elements 
    Ganymede                centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -143.2            km 
 Eccentricity       40.743747 
 Inclination        124.109          degree 
 Node Angle         66.757           degree 
 Arg of Periapsis   92.933           degree 
 Mean Anomaly      -.242             degree 
---------- 
GANYMEDE, ORBIT 7, TO JUPITER APOAPSIS, ORBIT 7: 
Orbital Elements valid from J.D. = 2450543.79976 ET  (97/04/05  
07:10:37 GMT) 
                       to   J.D. = 2450559.98356 ET  (97/04/21  
11:35:17 GMT) 
Epoch of Orbital Elements:  J.D. = 2450543.79976 ET  (97/04/05  
07:10:37 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3030500.0        km 
 Eccentricity       .790709 
 Inclination        2.532            degree 
 Node Angle         13.730           degree 
 Arg of Periapsis   142.894          degree 
 Mean Anomaly       9.043            degree 
---------- 
JUPITER APOAPSIS, ORBIT 7, TO GANYMEDE, ORBIT 8: 
Orbital Elements valid from J.D. = 2450559.98356 ET  (97/04/21  
11:35:17 GMT) 
                       to   J.D. = 2450576.16506 ET  (97/05/07  
15:56:39 GMT) 
Epoch of Orbital Elements:  J.D. = 2450559.98356 ET  (97/04/21  
11:35:17 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3028177.3        km 
 Eccentricity       .792084 
 Inclination        2.676            degree 
 Node Angle         11.437           degree 
 Arg of Periapsis   145.214          degree 
 Mean Anomaly       179.822          degree 
---------- 
GANYMEDE, ORBIT 8, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450576.16506 ET  (97/05/07  
15:56:39 GMT) 
    Classical Orbital Elements 
    Ganymede                centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -141.0            km 
 Eccentricity       30.923994 
 Inclination        151.567          degree 
 Node Angle         69.320           degree 
 Arg of Periapsis   92.369           degree 
 Mean Anomaly      -1.126            degree 
---------- 
GANYMEDE, ORBIT 8, TO JUPITER APOAPSIS, ORBIT 8: 
Orbital Elements valid from J.D. = 2450576.16506 ET  (97/05/07  
15:56:39 GMT) 
                       to   J.D. = 2450602.01844 ET  (97/06/02  
12:25:31 GMT) 
Epoch of Orbital Elements:  J.D. = 2450576.16506 ET  (97/05/07  
15:56:39 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3914168.3        km 
 Eccentricity       .830560 
 Inclination        2.316            degree 
 Node Angle        -11.817           degree 
 Arg of Periapsis   163.064          degree 
 Mean Anomaly      -5.930            degree 
---------- 
JUPITER APOAPSIS, ORBIT 8, TO CALLISTO, ORBIT 9: 
Orbital Elements valid from J.D. = 2450602.01844 ET  (97/06/02  
12:25:31 GMT) 
                       to   J.D. = 2450625.07512 ET  (97/06/25  
13:47:08 GMT) 
Epoch of Orbital Elements:  J.D. = 2450602.01844 ET  (97/06/02  
12:25:31 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3912465.8        km 
 Eccentricity       .831357 
 Inclination        2.326            degree 
 Node Angle        -11.887           degree 
 Arg of Periapsis   163.162          degree 
 Mean Anomaly       179.925          degree 
---------- 
CALLISTO, ORBIT 9, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450625.07512 ET  (97/06/25  
13:47:08 GMT) 
    Classical Orbital Elements 
    Callisto                centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -115.0            km 
 Eccentricity       25.517103 
 Inclination        178.002          degree 
 Node Angle         97.001           degree 
 Arg of Periapsis   141.265          degree 
 Mean Anomaly       .899             degree 
---------- 
CALLISTO, ORBIT 9, TO JUPITER APOAPSIS, ORBIT 9: 
Orbital Elements valid from J.D. = 2450625.07512 ET  (97/06/25  
13:47:08 GMT) 
                       to   J.D. = 2450668.72932 ET  (97/08/08  
05:29:11 GMT) 
Epoch of Orbital Elements:  J.D. = 2450625.07512 ET  (97/06/25  
13:47:08 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    5497230.2        km 
 Eccentricity       .860165 
 Inclination        2.188            degree 
 Node Angle        -16.056           degree 
 Arg of Periapsis   158.024          degree 
 Mean Anomaly      -8.312            degree 
---------- 
JUPITER APOAPSIS, ORBIT 9, TO CALLISTO, ORBIT 10: 
Orbital Elements valid from J.D. = 2450668.72932 ET  (97/08/08  
05:29:11 GMT) 
                       to   J.D. = 2450708.51513 ET  (97/09/17  
00:20:45 GMT) 
Epoch of Orbital Elements:  J.D. = 2450668.72932 ET  (97/08/08  
05:29:11 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    5496492.6        km 
 Eccentricity       .860413 
 Inclination        2.191            degree 
 Node Angle        -16.094           degree 
 Arg of Periapsis   158.171          degree 
 Mean Anomaly       179.668          degree 
---------- 
CALLISTO, ORBIT 10, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450708.51513 ET  (97/09/17  
00:20:45 GMT) 
    Classical Orbital Elements 
    Callisto                centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -114.4            km 
 Eccentricity       26.584928 
 Inclination        5.826            degree 
 Node Angle         27.762           degree 
 Arg of Periapsis   108.289          degree 
 Mean Anomaly      -1.777            degree 
---------- 
CALLISTO, ORBIT 10, TO JUPITER APOAPSIS, ORBIT 10: 
Orbital Elements valid from J.D. = 2450708.51513 ET  (97/09/17  
00:20:45 GMT) 
                       to   J.D. = 2450735.00208 ET  (97/10/13  
12:01:58 GMT) 
Epoch of Orbital Elements:  J.D. = 2450708.51513 ET  (97/09/17  
00:20:45 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3861621.3        km 
 Eccentricity       .830403 
 Inclination        1.968            degree 
 Node Angle        -25.474           degree 
 Arg of Periapsis   177.184          degree 
 Mean Anomaly      -14.340           degree 
---------- 
JUPITER APOAPSIS, ORBIT 10, TO EUROPA, ORBIT 11: 
Orbital Elements valid from J.D. = 2450735.00208 ET  (97/10/13  
12:01:58 GMT) 
                       to   J.D. = 2450759.40780 ET  (97/11/06  
21:46:12 GMT) 
Epoch of Orbital Elements:  J.D. = 2450735.00208 ET  (97/10/13  
12:01:58 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3861021.8        km 
 Eccentricity       .830688 
 Inclination        1.934            degree 
 Node Angle        -25.424           degree 
 Arg of Periapsis   177.183          degree 
 Mean Anomaly       179.850          degree 
---------- 
EUROPA, ORBIT 11, CLOSEST APPROACH: 
Epoch of Orbital Elements:  J.D. = 2450759.40780 ET  (97/11/06  
21:46:12 GMT) 
    Classical Orbital Elements 
    Europa                  centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis   -113.1            km 
 Eccentricity       24.786204 
 Inclination        65.245           degree 
 Node Angle         73.574           degree 
 Arg of Periapsis   94.329           degree 
 Mean Anomaly      -.158             degree 
---------- 
EUROPA, ORBIT 11, TO JUPITER APOAPSIS, ORBIT 11: 
Orbital Elements valid from J.D. = 2450759.40780 ET  (97/11/06  
21:46:12 GMT) 
                       to   J.D. = 2450780.83877 ET  (97/11/28  
08:06:48 GMT) 
Epoch of Orbital Elements:  J.D. = 2450759.40780 ET  (97/11/06  
21:46:12 GMT) 
    Classical Orbital Elements 
    Jupiter                 centered, Earth ecliptic and equinox 
of J2000 
 Semi-major Axis    3514918.9        km 
 Eccentricity       .814580 
 Inclination        3.117            degree 
 Node Angle        -33.263           degree 
 Arg of Periapsis  -173.672          degree 
 Mean Anomaly      -1.127            degree