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Predicted Impact Parameters for Fragments of P/Shoemaker-Levy 9

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[Forwarded from Paul Chodas, JPL]

Here's the last edition of our Predicted Impact Parameters table before the impacts begin.

The impact times are within a few minutes of those in our previous table, dated July 11. In particular, the time for A is 2.1 minutes later, and C and F are 2.7 minutes later. The time for U moved 4 minutes earlier.

We have removed the satellite data from this table, as it was changing little from one solution to the next. In its place, we give the date of the last data point used in our orbit solutions. As you can see, despite heroic efforts, observers were unable to image fragments A and B later than July 13.

The impact time uncertainties for most of the fragments are now down in the 3-5 minute range (1-sigma). Please use at least +/- 2 sigmas for your observing windows. Also note that these predictions refer to the central condensation of each fragment.

Paul Chodas 1994 July 16 16:20 UT


Predicted Impact Parameters for Fragments of P/Shoemaker-Levy 9

P.W. Chodas, D.K. Yeomans (JPL/Caltech)
Predictions as of 1994 July 16
Date of last astrometric data in these solutions: 1994 July 14

The predictions for all fragments except Q2 are based on independent orbit solutions; our orbit reference identifier is given. The orbit solution for fragment Q2 was obtained by applying a disruption model to the orbit for Q1, and using astrometric measurements of Q2 relative to Q1.

Immediately to the right of the predicted impact times, we give the 1-sigma uncertainties in those times for all fragments except Q2. We have made an effort to make these uncertainties realistic: they are not formal uncertainty values. NOTE: To obtain a 95% confidence level, one should use a +/- 2 sigma window around the predicted impact time. The uncertainties for fragment Q2 have not been quantified, but are probably comparable to those for T.

The dynamical model used for these predictions includes perturbations due to the Sun, planets, Galilean satellites and the oblateness of Jupiter. The planetary ephemeris used was DE245.

-------------------------------------------------------------------------------
Fragment   Impact      1-sig   Jovicentric  Meridian   Angle   Orbit   Date of
          Date/Time     Unc.   Lat.   Long.   Angle    E-J-F    Ref.  Last Data
         July  (UTC)   (min)   (deg)  (deg)   (deg)    (deg)          (July UT)
--------------h--m--s----------------------------------------------------------
 A = 21   16 19:59:40   5.5   -43.13   178    64.48    98.72    A25     13.0
 B = 20   17 02:54:13   4.1   -43.16    70    63.82    99.18    B20     13.2
 C = 19   17 07:02:14   3.7   -43.37   218    65.24    98.12    C18     14.0
 D = 18   17 11:47:00   4.7   -43.45    30    65.58    97.85    D19     14.0
 E = 17   17 15:05:31   3.1   -43.47   150    65.76    97.72    E35     14.2
 F = 16   18 00:29:21   4.0   -43.56   132    64.52    98.57    F26     13.2
 G = 15   18 07:28:32   3.1   -43.59    23    66.63    97.07    G32     14.2
 H = 14   18 19:25:53   3.1   -43.73    96    66.83    96.89    H31     14.2
 K = 12   19 10:18:32   3.1   -43.80   275    67.76    96.21    K33     15.0
 L = 11   19 22:08:53   3.4   -43.91   344    68.18    95.88    L34     15.0
 N = 9    20 10:20:02   4.9   -44.29    66    67.77    96.10    N22     15.0
 P2= 8b   20 15:11:55   4.6   -44.61   244    66.68    96.80    P20     15.0
 Q2= 7b   20 19:31:43         -44.35    39    68.78    95.37
 Q1= 7a   20 19:59:10   4.5   -44.06    55    69.20    95.12    Q37     15.0
 R = 6    21 05:25:56   4.6   -44.07    37    69.44    94.94    R32     15.0
 S = 5    21 15:10:22   4.4   -44.16    30    69.80    94.67    S42     15.0
 T = 4    21 18:03:45  11.5   -44.99   137    67.34    96.26    T16      4.1
 U = 3    21 21:48:30  12.8   -44.43   272    68.81    95.33    U17      8.0
 V = 2    22 04:16:53   8.1   -44.43   146    69.50    94.83    V18     15.0
 W = 1    22 07:57:36   5.2   -44.15   278    70.44    94.21    W33     15.0
-------------------------------------------------------------------------------

Notes:
1. Fragments J=13, M=10, and P1=8a are omitted because they have faded from
   view.  The March'94 HST images show that P2=8b and G=15 have split; we do
   not have sufficient data to obtain independent predictions for the
   sub-components.

2. The impact date/time is the time the impact would be seen at the Earth, if
   the limb of Jupiter were not in the way (i.e., the time listed is the time
   of impact plus the light travel time to the Earth); the date is the day in
   July 1994; The impact time uncertainty is a 1-sigma value in minutes.

3. The impact latitude is Jovicentric (latitude measured at the center of
   Jupiter); the Jovigraphic latitudes are about 3.84 deg more negative.

4. The impact longitude is System III, measured westwards on the planet.

5. The meridian angle is the Jovicentric longitude of impact measured from
   the midnight meridian towards the morning terminator.  This relative
   longitude is known much more accurately than the absolute longitude.
   At the latitude of the impacts, the Earth limb is at meridian angle 76 deg
   and the terminator is at meridian angle 87 deg.

6. Angle E-J-F is the Earth-Jupiter-Fragment angle at impact; values greater
   than 90 deg indicate a farside impact.  All impacts will be just on the
   farside as viewed from Earth; later impacts will be closer to the limb.


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