Galileo 1950B Orbital Elements

The Galileo Interplanetary Orbital elements are available in a separate file.

This set of conic elements represents the updated Galileo satellite tour T-960110. The new conic elements differ from those released previously primarily in the lower Io flyby altitude on orbit 0 and one week earlier Ganymede 1 flyby date. Please note that 'True Anomaly' (in previously released elements) has been replaced with 'Mean Anomaly.'

These elements begin when the spacecraft trajectory central body changes from Sun-centered to Jupiter-centered (September 13, 1995) and end at Jupiter apoapsis, orbit 11 (November 28, 1997). Three element sets model the initial Jupiter approach trajectory. They are:

          Jupiter Central Body Change To Io, Orbit 0
          Io, Orbit 0, To JOI Burn Start
          JOI Burn Start To Jupiter Apoapsis, Orbit 0
Thereafter, each orbit consists of two sets of elements: the first is valid from Jupiter apoapsis to the targeted satellite closest approach and the second set is for the period from satellite closest approach to the next Jupiter apoapsis. For completeness, satellite- centered elements are provided for each satellite closest approach.

Elements are provided in both Earth ecliptic and equinox of B1950 (this document) and J2000 reference frames. Times are given in Julian date (J.D.) in ephemeris time (ET) and calendar date in Greenwich Mean Time (GMT). GMT is understood to be the same as universal time (UTC). ET minus UTC is 61.184 seconds before January 1, 1996 and 62.184 seconds after this date.

The 1991 IAU values for radii and GM's were used for Jupiter and the Galilean satellites.

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 B1950
 Semi-major Axis   -4103077.3        km
 Eccentricity       1.070722
 Inclination        5.146            degree
 Node Angle         58.300           degree
 Arg of Periapsis   90.618           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 B1950
 Semi-major Axis   -27.0             km
 Eccentricity       101.508187
 Inclination        10.306           degree
 Node Angle        -141.025          degree
 Arg of Periapsis  -58.429           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 B1950
 Semi-major Axis   -5871176.2        km
 Eccentricity       1.048704
 Inclination        5.349            degree
 Node Angle         59.844           degree
 Arg of Periapsis   90.675           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 B1950
 Semi-major Axis    9814688.8        km
 Eccentricity       .971233
 Inclination        5.297            degree
 Node Angle         60.329           degree
 Arg of Periapsis   87.620           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 B1950
 Semi-major Axis    10091803.7       km
 Eccentricity       .917105
 Inclination        5.355            degree
 Node Angle         66.716           degree
 Arg of Periapsis   81.285           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 B1950
 Semi-major Axis   -179.3            km
 Eccentricity       20.401721
 Inclination        31.057           degree
 Node Angle         84.927           degree
 Arg of Periapsis   77.674           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 B1950
 Semi-major Axis    4970309.2        km
 Eccentricity       .841256
 Inclination        4.150            degree
 Node Angle         59.105           degree
 Arg of Periapsis   96.626           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 B1950
 Semi-major Axis    4964416.1        km
 Eccentricity       .843442
 Inclination        4.173            degree
 Node Angle         56.706           degree
 Arg of Periapsis   99.017           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 B1950
 Semi-major Axis   -174.9            km
 Eccentricity       17.491549
 Inclination        80.004           degree
 Node Angle         77.032           degree
 Arg of Periapsis   88.607           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 B1950
 Semi-major Axis    4418597.8        km
 Eccentricity       .827478
 Inclination        2.263            degree
 Node Angle        -9.192            degree
 Arg of Periapsis   167.132          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 B1950
 Semi-major Axis    4413984.2        km
 Eccentricity       .829388
 Inclination        2.285            degree
 Node Angle        -9.321            degree
 Arg of Periapsis   167.264          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 B1950
 Semi-major Axis   -121.2            km
 Eccentricity       29.924953
 Inclination        13.776           degree
 Node Angle         52.029           degree
 Arg of Periapsis   98.252           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 B1950
 Semi-major Axis    3512146.2        km
 Eccentricity       .814721
 Inclination        1.960            degree
 Node Angle        -35.090           degree
 Arg of Periapsis  -158.610          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 B1950
 Semi-major Axis    3514197.3        km
 Eccentricity       .813654
 Inclination        1.962            degree
 Node Angle        -35.066           degree
 Arg of Periapsis  -158.565          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 B1950
 Semi-major Axis   -107.3            km
 Eccentricity       22.030617
 Inclination        178.214          degree
 Node Angle         151.204          degree
 Arg of Periapsis  -179.708          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 B1950
 Semi-major Axis    2900585.7        km
 Eccentricity       .776628
 Inclination        1.959            degree
 Node Angle        -35.158           degree
 Arg of Periapsis  -162.269          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 B1950
 Semi-major Axis    2899664.7        km
 Eccentricity       .777193
 Inclination        1.954            degree
 Node Angle        -35.199           degree
 Arg of Periapsis  -162.234          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 B1950
 Semi-major Axis   -126.2            km
 Eccentricity       229.951822
 Inclination        178.246          degree
 Node Angle         166.249          degree
 Arg of Periapsis  -173.185          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 B1950
 Semi-major Axis    2898670.3        km
 Eccentricity       .777155
 Inclination        1.960            degree
 Node Angle        -35.129           degree
 Arg of Periapsis  -162.597          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 B1950
 Semi-major Axis    2897813.4        km
 Eccentricity       .777681
 Inclination        1.964            degree
 Node Angle        -35.094           degree
 Arg of Periapsis  -162.629          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 B1950
 Semi-major Axis   -106.5            km
 Eccentricity       21.201785
 Inclination        163.660          degree
 Node Angle        -99.700           degree
 Arg of Periapsis  -93.046           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 B1950
 Semi-major Axis    3515030.3        km
 Eccentricity       .814544
 Inclination        1.472            degree
 Node Angle        -32.119           degree
 Arg of Periapsis  -169.492          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 B1950
 Semi-major Axis    3513041.0        km
 Eccentricity       .815574
 Inclination        1.888            degree
 Node Angle        -29.787           degree
 Arg of Periapsis  -171.776          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 B1950
 Semi-major Axis   -143.2            km
 Eccentricity       40.743747
 Inclination        124.107          degree
 Node Angle         66.054           degree
 Arg of Periapsis   92.925           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 B1950
 Semi-major Axis    3030500.0        km
 Eccentricity       .790709
 Inclination        2.526            degree
 Node Angle         13.078           degree
 Arg of Periapsis   142.848          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 B1950
 Semi-major Axis    3028177.3        km
 Eccentricity       .792084
 Inclination        2.669            degree
 Node Angle         10.776           degree
 Arg of Periapsis   145.175          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 B1950
 Semi-major Axis   -141.0            km
 Eccentricity       30.923994
 Inclination        151.565          degree
 Node Angle         68.610           degree
 Arg of Periapsis   92.355           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 B1950
 Semi-major Axis    3914168.3        km
 Eccentricity       .830560
 Inclination        2.310            degree
 Node Angle        -12.536           degree
 Arg of Periapsis   163.085          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 B1950
 Semi-major Axis    3912465.8        km
 Eccentricity       .831357
 Inclination        2.319            degree
 Node Angle        -12.607           degree
 Arg of Periapsis   163.183          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 B1950
 Semi-major Axis   -115.0            km
 Eccentricity       25.517103
 Inclination        178.003          degree
 Node Angle         96.119           degree
 Arg of Periapsis   141.082          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 B1950
 Semi-major Axis    5497230.2        km
 Eccentricity       .860165
 Inclination        2.181            degree
 Node Angle        -16.788           degree
 Arg of Periapsis   158.059          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 B1950
 Semi-major Axis    5496492.6        km
 Eccentricity       .860413
 Inclination        2.185            degree
 Node Angle        -16.826           degree
 Arg of Periapsis   158.205          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 B1950
 Semi-major Axis   -114.4            km
 Eccentricity       26.584928
 Inclination        5.820            degree
 Node Angle         27.098           degree
 Arg of Periapsis   108.255          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 B1950
 Semi-major Axis    3861621.3        km
 Eccentricity       .830403
 Inclination        1.962            degree
 Node Angle        -26.241           degree
 Arg of Periapsis   177.252          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 B1950
 Semi-major Axis    3861021.8        km
 Eccentricity       .830688
 Inclination        1.928            degree
 Node Angle        -26.192           degree
 Arg of Periapsis   177.252          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 B1950
 Semi-major Axis   -113.1            km
 Eccentricity       24.786204
 Inclination        65.243           degree
 Node Angle         72.878           degree
 Arg of Periapsis   94.322           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 B1950
 Semi-major Axis    3514918.9        km
 Eccentricity       .814580
 Inclination        3.111            degree
 Node Angle        -34.019           degree
 Arg of Periapsis  -173.615          degree
 Mean Anomaly      -1.127            degree


Return to Project Galileo Homepage