[IGSREPORT-15492] Wk 1443 IGLOS Final Orbits

Gerd Gendt3 igsacc at gfz-potsdam.de
Thu Sep 20 23:59:19 PDT 2007


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IGS Electronic Report   20 Sep 23:59:39 PDT 2007      Message Number 15492
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Author:   AC Coordinator / GFZ Potsdam                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1443   (Sep 02, 2007 - Sep 08, 2007) 
                                                                               
Contact: Gerd Gendt     (gendt at gfz-potsdam.de)                   
         Thomas Nischan ( nisn at gfz-potsdam.de)                             
                                                                               
                                                                               
COMBINATION STRATEGY:                                                            
---------------------                                                            
                                                                               
Ephemeris are combined as weighted averages computed over all centres.          
Each centre and satellite is given a position weight computed from the centers  
absolute deviation to the unweighted average orbit after removing small         
differences in the reference frames. These weights were applied in a            
second iteration to estimate Helmert transformation parameters for each         
center. Finally the transformation parameters with respect to the combined      
solution and the RMS of the fit are reported in Tables 2.1443.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed to
the values of the final IGS (GPS) combination.                                                    
                                                                               
                                                                               
SOFTWARE:                                                                       
---------                                                                       
                                                                               
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:

  Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS 
  Analysis Centers, Bulletin Geodesique, 69, pp 200-222.

  Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
  and Evaluation, Appendix I of the Analysis Coordinator Report, International
  GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.

  Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report, 
  International GPS Service for Geodynamics (IGS) 1995 Annual Report, 
  pp. 45-76.

  Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report, 
  International GPS Service for Geodynamics (IGS) 1996 Annual Report, 
  pp. 55-100.
                                                                               
  Weber R., 2000, IGS Technical Report 1999                                    
                                                                               
                                                                               
PRODUCTS GENERATED:                                                             
-------------------                                                             
                                                                               
The combined IGL-ephemerides are written to daily files in the SP3-format.     
The satellite accuracy codes in the header are based on the weighted rms.       
for each satellite. Note, that the result files contain all satellites          
that were analysed by at least one center. We refer to the 'REMARKS' section    
below, in case a satellite or center was excluded from the combination.         
                                                                               
The following naming convention is used for the result files:                   
                                                                               
 igl1443[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1443 in the SP3 format.
 igl14437.sum      Combination Report for GPS Week 1443.


    
    
REMARKS concerning the IGL Orbit Combination:                                  
---------------------------------------------

 1. Broadcast (brd) orbits and clocks are included in the combination for
    statistics only.

 2. Having only a few satellites the mcc orbits are included in the combination 
    for statistics only.

 3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151] 
    BKG, ESA, and CODE will start to refer their GLONASS orbit products 
    to the following satellite antenna offset (SAO) values:
    
      X/Y/Z =  0.000/0.000/0.000 meter for GLONASS and
      X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
    

 4. The satellite clock values in the combined orbit files are taken from the
    broadcast files. The following gps/glonass time offsets derived from the
    bkg summary files were added to the broadcast clocks.
    
               Day | applied clock offset
               ----+---------------------
                0  |   1111.7 ns
                1  |   1134.5 ns
                2  |   1163.0 ns
                3  |   1139.0 ns
                4  |   1163.9 ns
                5  |   1114.1 ns
                6  |   1218.9 ns

 5. The following orbit solutions were excluded from the combination
    because they were biasing the weighted average (generally indicated
    by long arc RMS).
    
               Day | Centre | PRN list
               ----+--------+---------------
                0  |  COD   | R15
                0  |  ESX   | R10 R14 R23 R24
                1  |  COD   | R15
                1  |  ESX   | R10 R14 R23 R24
                2  |  COD   | R15
                2  |  ESX   | R10 R14 R23 R24
                2  |  IAC   | R24
                3  |  COD   | R15
                3  |  ESX   | R02 R03 R10 R14 R18 R19 R21 R23 R24
                4  |  COD   | R15
                4  |  ESX   | R10 R14 R23 R24
                5  |  COD   | R15
                5  |  ESX   | R02 R03 R04 R10 R14 R18 R19 R21 R23 R24
                6  |  COD   | R15 R21
                6  |  ESX   | R02 R03 R10 R14 R18 R19 R21 R23 R24

    
         
ORBIT COMBINATION AND EVALUATION STATISTICS:                                    
--------------------------------------------                                    
      
Table 1 summarizes all statistics for the week. It contains means and standard 
        deviations over the week of satellite ephemeris  and  clock correction
        transformation parameters for each centre (Tables 1.1443, 1a.1443).
        
Table 2 contains the complete  ephemeris  and  clock correction transformation
        parameters (includes both the apriori and a posteriori values) for each
        centre and each day (Tables 2.1443.0-6)                                                                                
    
Table 3 contains two types of daily  RMS  for each satellite and centre, along
        with the computed  satellite position sigmas  for the  combined orbits 
        (tables 3.1443.0-6). 
        The first type of satellite RMS is based on orbit combination and  the
        second RMS type is a result of the 7-day arc evaluation of each centre
        ephemerides.
                                                                               
   
      
      
Table 1: Week 1443 summary.                      (Sep 02, 2007 - Sep 08, 2007)

Table 1.1443.a     GPS week : 1443   MJD: 54345.0-54351.0

         Mean and standard deviations of transformation parameters to the 
         combined IGL orbit.
         WRMS - orbit RMS weighted by the SP3 header accuracy codes.
         STA  - Mean number of stations in the daily solutions.
   
CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg   56|    1     0    -7   -17    31  -206  -.04   44   39 |       0    2386   5538   6251
        |    2     3     7    85    34   170   .14           |       0    3381
cod  168|   -2    -4     0    58   -41   163   .01   44   38 |     ---     ---    ---    ---
        |    3     4     6    69    30   166   .13           |     ---     ---
esx   40|    4    -1   -24    26   143    60  -.24  351   82 | -107292  -16989  14920  27878
        |   14     9    13    77   124   482   .23           |  765734   22397
iac  n/a|    3     0    20   -10   -14   -47   .17   51   51 | 1148481   -4614  14700  27896
        |    4     2    14    58    52   147   .17           |   36767   14371
mcc  n/a|   -8     3    88   133   149  1047   .87  117  117 |     ---     ---    ---    ---
        |   27    15    12   146   312   382   .63           |     ---     ---


Table 1.1443.b     GPS week : 1443   MJD: 54345.0-54351.0   

         Satellite position sigmas for the combined orbits
         (coded in the IGS SP3 orbit files).
         "E" flags eclipsing satellites.
         Units: mm.

              Day of GPS week
 PRN  |    0    1    2    3    4    5    6 |  Remarks
------+------------------------------------+------------------------------------------
 R01  |   16   14   26   27   35   23   25 |
 R04  |   24   22   31   23   28   28   36 |
 R06  |   24   20   24   23   30   32   33 |
 R07  |   25   20   25   22   31   24   20 |
 R08  |   22   26   25   30   19   39   39 |
 R10  |   38   32   21   26   27   25   30 |
 R14  |   23   25   18   23   33   29   32 |
 R21  |   34   18   26   21  ---  ---  --- |
 R23  |   44   43   42   34   34   36   51 |
 R24  |   27   45  163   93   57   61  105 |


Table 1.1443.c     GPS week : 1443   MJD: 54345.0-54351.0   

         Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
         Mean and standard deviations of the transformation parameters for the
         whole gpsweek.

CEN WEEK DAY |   DX    DY    DZ     RX      RY      RZ   SCL   RMS   WRMS |    TOFT   TDRFT
             |  [mm]  [mm]  [mm]  [uas]   [uas]   [uas] [ppb]  [mm]  [mm] |    [ps]  [ps/d]
-------------+------------------------------------------------------------+----------------
brd 1443 0   |  292  -286  -723    3867   -4305 -337400  94.6  5212  5212 | 1111729       0
brd 1443 1   |  -37  -356    40     338   -4576 -313400  97.9  8167  8167 | 1134528       0
brd 1443 2   |  213  -339  -346   -6301   -7810 -305400 103.8  7384  7384 | 1163037       0
brd 1443 3   |   13   301  -367   -2773   -2493 -295800  89.0  6933  6933 | 1139004       0
brd 1443 4   |  132  -246 -1203   -9819    8671 -321200 107.5  9388  9388 | 1163938       0
brd 1443 5   |    0   326 -1585    3721    1120 -319900  92.5 11250 11250 | 1114085       0
brd 1443 6   |   89   -81 -2146     118   -1014 -333900  93.7  4205  4205 | 1218863       0
-------------+------------------------------------------------------------+----------------
brd 1443 mean|  100   -97  -904   -1549   -1486 -318142  97.0  7505  7505 | 1149312       0
brd 1443 sdev|  120   294   776    5097    5302   14807   6.6  2397  2397 |   37008       0



Table 2: Daily transformation of each centre to the combined IGL orbit and
         clocks for each day of the week. The transformation displayed is the
         sum of a priori and estimated transformations.
         WRMS - RMS weighted by the centres SP3 header accuracy codes.
         STA  - Number of stations in the daily solutions.
   
Table 2.1443.0  GPS week: 1443   Day: 0   MJD: 54345                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg   56|    0     4    -6   -62    64  -273  -.09   27   28 |       0    2013   4166   4691
cod  168|   -4   -12    -2   171     0   390   .11   50   45 |     ---     ---    ---    ---
esx   40|  -10    -4   -26   -26    66   366  -.09  252   67 |   85993  -12661  16190  34856
iac  n/a|    2     1    15     0     5    -5   .22   44   44 | 1110125   -5100  16040  34665
mcc  n/a|    0     9   107   -34   -56   904   .25   59   59 |     ---     ---    ---    ---

Table 2.1443.1  GPS week: 1443   Day: 1   MJD: 54346                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg   56|    0     2   -11   -55   -17   -51  -.03   35   36 |       0     -43   2911   3168
cod  168|    2    -8     6    49    -8   -23  -.01   32   30 |     ---     ---    ---    ---
esx   40|   -5     4   -27   111   -50   280  -.17  258   76 |  -10406   -8062  14191  20982
iac  n/a|    0     4    16    22   -19   -77   .09   41   41 | 1135842   -6675  13797  21053
mcc  n/a|    5    14    83    61    97   561   .56   62   62 |     ---     ---    ---    ---

Table 2.1443.2  GPS week: 1443   Day: 2   MJD: 54347                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg   56|    4    -4     2     2    51  -138  -.16   49   45 |       0     709   6386   6790
cod  168|    0    -3     2    55   -85   122   .16   40   42 |     ---     ---    ---    ---
esx   40|    3    -1   -17   -72   151   243  -.64  250   62 |  -47887  -14563  24410  58232
iac  n/a|    5     0    -1    58  -100  -301   .41   41   41 | 1152471  -16387  23604  57366
mcc  n/a|    9     9    90   156  -201  1175   .95   57   57 |     ---     ---    ---    ---

Table 2.1443.3  GPS week: 1443   Day: 3   MJD: 54348                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg   56|    5     3    -1  -171    39  -460  -.17   53   43 |       0    1221   4434   4623
cod  168|    0    -1     0   109   -34   374   .08   64   43 |     ---     ---    ---    ---
esx   40|   -2     7   -14     7   110   149  -.30  287   63 |  -38669   11062  14207  19573
iac  n/a|   -2    -3    14     3   -65    23   .21   59   59 | 1137202   19017  12484  20071
mcc  n/a|   14    -1    76   126    53  1711   .10   45   45 |     ---     ---    ---    ---

Table 2.1443.4  GPS week: 1443   Day: 4   MJD: 54349                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg   56|    3     0   -20    45     4  -370   .16   66   49 |       0     400   5445   5722
cod  168|   -7     0    -2     0   -59    46  -.16   30   30 |     ---     ---    ---    ---
esx   40|   14     4   -14     0   316   146  -.23  271   77 | 1259918  -36360  13502  22539
iac  n/a|    6     0    45    10     8    14   .31   66   66 | 1171594  -19855  14048  22936
mcc  n/a|    1    -2    72   350   -12   693  1.14  216  216 |     ---     ---    ---    ---

Table 2.1443.5  GPS week: 1443   Day: 5   MJD: 54350                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg   56|   -1     0    -4    50     5  -161  -.14   40   34 |       0    2641   4828   5169
cod  168|   -5     0   -12    63   -59   203   .10   42   33 |     ---     ---    ---    ---
esx   40|   31   -21   -16    19   135 -1020  -.31  858  111 | -999999   -2277  11857  18440
iac  n/a|    5     0    20  -123    56   164   .08   57   57 | 1115153   10345  11916  17972
mcc  n/a|  -32   -25    94   292   625  1242  1.93  194  194 |     ---     ---    ---    ---

Table 2.1443.6  GPS week: 1443   Day: 6   MJD: 54351                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg   56|   -1     0   -12    67    71    13   .12   41   37 |       0    9761  10601  13594
cod  168|   -6    -7     8   -40   -43    29  -.18   48   44 |     ---     ---    ---    ---
esx   40|    0     0   -51   147   276   255   .09  282  120 | -999999  -56065  10086  20530
iac  n/a|    9     1    30   -42    10  -147  -.11   49   49 | 1216981  -13647  11011  21214
mcc  n/a|  -60    22    97   -16   544  1045  1.18  183  183 |     ---     ---    ---    ---

       
       
Table 3: Daily fit for each satellite and each centre resulting from weighted
         average combination and from long arc orbit dynamics (7-day). The
         first IGL column gives resulting satellite accuracy measures found in
         SP3 header. The last IGL column gives the RMS fit of the IGL orbit
         when processed through the 7-day arc evaluation.

         "E"    stands for eclipsing satellites (earth).
         "M"    stands for eclipsing satellites (moon).
         "X"    stands for excluded from the statistics but included in IGL orbit.
         "T"    stands for Total long arc orbit RMS for all satellites.
         "NE"   stands for long arc orbit RMS for Non-Eclipsing satellites only.
         "MEDI" stands for median of the centre's satellite RMS.
         "MD"
         Units: mm.

Table 3.1443.0  GPS week: 1443   Day: 0   MJD: 54345                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 2314   20   32   50   21  ---   16 |    32   53   45   41  ---    35
 R04  | 3334   22   52   85   32  ---   24 |    38   40  237   34  ---    29
 R06  | 4214   20   39   94   35  ---   23 |    39   41   54   45  ---    34
 R07  | 3374   44   35   46   47   59   25 |    29   45   78   53   49    35
 R08  | 4975   17   40   78   36  ---   21 |    37   43   63   48  ---    35
 R10  | 3322   41   47  426   70  ---   37 |    23   51  223   65  ---    26
 R14  | 5993   16   52  376   30  ---   23 |    62   63  231   64  ---    60
 R21  |10909   22   48  169   18  ---   34 |    19  692 9999   18  ---    69
 R23  | 2854   28   86  442   71  ---   43 |    47   61  196   78  ---    46
XR24  | 5012   37   51  ---   22  ---   26 |  9999 9999  --- 9999  ---  9999
------+------------------------------------+--------------------------------
 RMS  | 5212   27   50  252   44   59      |T   36  121  140   49   49    41
 WRMS | 5212   28   45   67   44   59      |NE  36  121  140   49   49    41
 MEDI | 3374   22   47   94   32   59      |MD  37   51   78   48   49    35

Table 3.1443.1  GPS week: 1443   Day: 1   MJD: 54346                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 3752   20   16   46   19  ---   13 |    53   43   47   49  ---    45
 R04  | 6254   23   23   89   29  ---   22 |    22   27  283   27  ---    19
 R06  |11555   20   23   83   20  ---   19 |    41   38   60   34  ---    33
 R07  | 3772   27   32   41   38   62   19 |    36   38   49   45   36    23
 R08  | 5944   50   42   57   37  ---   26 |    29   37   33   80  ---    31
 R10  | 3236   40   34  429   58  ---   32 |    13   46  198   50  ---    24
 R14  | 3955   43   19  402   38  ---   25 |    34   40  188   64  ---    34
 R21  |17600   17   26   64   27  ---   17 |    15  753 9999   18  ---    88
 R23  | 5296   51   54  476   73  ---   42 |    31   58  125   74  ---    40
XR24  | 6990   76   62  ---   47  ---   44 |  9999 9999  --- 9999  ---  9999
------+------------------------------------+--------------------------------
 RMS  | 8166   35   32  258   41   62      |T   30  120  122   49   36    37
 WRMS | 8166   36   30   76   41   62      |NE  30  120  122   49   36    37
 MEDI | 5296   27   26   83   37   62      |MD  31   40   60   49   36    33

Table 3.1443.2  GPS week: 1443   Day: 2   MJD: 54347                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 4587   69   50   24   30  ---   26 |    45   81   63   38  ---    48
 R04  | 8098   83   36   59   32  ---   31 |    49   62  192   70  ---    48
 R06  |12684   44   33   45   42  ---   23 |    42   39   53   48  ---    42
 R07  | 3192   48   45   42   34   57   24 |    27   32   47   37   52    22
 R08  | 4437   32   45   33   53  ---   24 |    43   37   55   51  ---    32
 R10  | 3324   32   24  409   31  ---   20 |    41   38   90   29  ---    24
 R14  | 4053   27   25  405   24  ---   18 |    42   38  169   49  ---    37
 R21  |12037   26   33   71   39  ---   26 |    21  603 9999   18  ---    99
 R23  | 6394   54   55  465   65  ---   41 |    43   51  168   67  ---    41
XR24  |10653  187  141  ---  382  ---  162 |  9999 9999  --- 9999  ---  9999
------+------------------------------------+--------------------------------
 RMS  | 7383   49   40  250   41   57      |T   39  109  104   45   52    43
 WRMS | 7383   45   42   62   41   57      |NE  39  109  104   45   52    43
 MEDI | 4587   44   36   59   34   57      |MD  42   39   63   48   52    41

Table 3.1443.3  GPS week: 1443   Day: 3   MJD: 54348                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 5156   52   52   48   30  ---   26 |    30   61   50   31  ---    35
 R04  | 7029   51   44   40   20  ---   23 |    55   70  287   45  ---    39
 R06  | 6685   41   40   35   39  ---   22 |    68   39   54   81  ---    53
 R07  | 3416   52   39   28   31   45   22 |    37   47   29   40   99    30
 R08  | 5047   29   37   58   71  ---   30 |    48   49   48   81  ---    43
 R10  | 4773   39   31  448   40  ---   26 |    51   33  198   52  ---    28
 R14  | 5029   35   23  371   38  ---   23 |    39   47  180   74  ---    48
XR21  |11284  ---   25 1818   15  ---   21 |   --- 9999 9999   25  ---   133
 R23  | 6941   57   44  460   39  ---   33 |    65   46  195   72  ---    52
 R24  |13361   94  156  428  134  ---   93 |  9999 9999  127 9999  ---  9999
------+------------------------------------+--------------------------------
 RMS  | 6933   53   64  287   59   45      |T   49   49  129   55   99    51
 WRMS | 6933   43   43   63   59   45      |NE  49   49  129   55   99    51
 MEDI | 5156   51   39   58   38   45      |MD  48   47  127   52   99    43

Table 3.1443.4  GPS week: 1443   Day: 4   MJD: 54349                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 6570   89   37   61   66  ---   35 |    60   26   43   60  ---    21
 R04  | 4916   56   24   83   33  ---   28 |    72   41  611   31  ---    44
 R06  |10795   30   32   81   67  ---   30 |    29   43  106   64  ---    38
 R07  | 2397   69   24   49   78  216   30 |    31   32  102   97   85    38
 R08  | 5750   21   26   39   48  ---   19 |    27   30   62   45  ---    24
 R10  | 4394   23   22  406   67  ---   27 |    20   36  171   36  ---    26
 R14  | 3701   57   27  412   63  ---   32 |    21   61  151   69  ---    47
 R23  | 6319   63   33  419   55  ---   33 |    75   84  139   76  ---    71
 R24  |22307  119   43  364   95  ---   57 |  9999 9999  170 9999  ---  9999
------+------------------------------------+--------------------------------
 RMS  | 9388   66   30  271   66  216      |T   41   44  172   59   85    38
 WRMS | 9388   49   30   77   66  216      |NE  41   44  172   59   85    38
 MEDI | 5750   57   27   83   66  216      |MD  29   36  139   60   85    38

Table 3.1443.5  GPS week: 1443   Day: 5   MJD: 54350                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 4636   39   28   63   44  ---   23 |    24   30   81   66  ---    32
 R04  | 2340   33   39 2400   44  ---   27 |    38   42 9999   41  ---    35
 R06  |16487   25   42  159   47  ---   31 |    30   60  117   47  ---    35
 R07  | 2032   33   27  121   22  194   23 |    23   47  121   47   49    31
 R08  | 4935   22   36  234   46  ---   39 |    18   41  218   46  ---    19
 R10  | 2398   35   26  412   43  ---   24 |    27   23  156   37  ---    20
 R14  | 2706   42   30  422   50  ---   29 |    22   44  182   55  ---    35
 R23  | 5926   52   47  482   50  ---   35 |    44   47  175   48  ---    40
 R24  |27647   62   78  432  116  ---   61 |  9999 9999  231 9999  ---  9999
------+------------------------------------+--------------------------------
 RMS  |11254   40   42  858   57  194      |T   28   41  160   48   49    30
 WRMS |11254   34   33  111   57  194      |NE  28   41  160   48   49    30
 MEDI | 4636   35   36  412   46  194      |MD  24   42  156   47   49    32

Table 3.1443.6  GPS week: 1443   Day: 6   MJD: 54351                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 3541   29   44  104   32  ---   25 |    19   32   45   46  ---    24
 R04  | 1887   22   33  212   47  ---   36 |    29   41  719   40  ---    34
 R06  | 5501   36   55  153   39  ---   33 |    71   46  124   45  ---    52
 R07  | 2778   25   34   56   41  183   20 |    50   46   55   32   38    35
 R08  | 5187   47   46  199   50  ---   39 |    33   44  154   41  ---    30
 R10  | 2361   39   34  384   54  ---   30 |    29   46  211   60  ---    35
 R14  | 2803   42   41  400   52  ---   31 |    43   67  177   58  ---    44
 R23  | 6857   68   79  457   66  ---   50 |    81   72  222   81  ---    62
XR24  |38315  ---   60 1147  139  ---  104 |   --- 9999  243 9999  ---  9999
------+------------------------------------+--------------------------------
 RMS  | 4205   41   48  282   49  183      |T   44   49  216   50   38    39
 WRMS | 4205   37   44  120   49  183      |NE  44   49  216   50   38    39
 MEDI | 3541   36   44  212   50  183      |MD  33   46  177   45   38    35



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