[IGSREPORT-18627] Wk 1583 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu May 27 06:39:31 PDT 2010


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IGS Electronic Report   27 May 06:39:33 PDT 2010      Message Number 18627
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Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1583   (May 09, 2010 - May 15, 2010) 
                                                                               
Contact: J. Ray       (jim.ray at noaa.gov),                  
         J. Griffiths (jake.griffiths at noaa.gov)                            
                                                                               
                                                                               
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 2.1583.
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:                   
                                                                               
 igl1583[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1583 in the SP3 format.
 igl15837.sum      Combination Report for GPS Week 1583.


    
    
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  |    462.3 ns
                1  |    463.7 ns
                2  |    466.9 ns
                3  |    395.3 ns
                4  |    465.1 ns
                5  |    465.9 ns
                6  |    414.4 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
               ----+--------+---------------
                4  |  BKG   | R05

    
         
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 1.1583, 1a.1583).
        
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 2.1583.0-6)                                                                                
    
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 3.1583.0-6). 
        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 1583 summary.                      (May 09, 2010 - May 15, 2010)

Table 1.1583.a     GPS week : 1583   MJD: 55325.0-55331.0

         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  129|    1     0   -10     1    -6   -22  -.08   34   25 |       0     -30   1652   1715
        |    1     1     6    22    35    73   .05           |       0      56
cod  246|   -1    -1     3    33    -7    -2  -.15   17   14 |     ---     ---    ---    ---
        |    1     0     3    18    22    32   .03           |     ---     ---
esx  142|    0    -1    10   -14    26    59   .39   27   24 |  113102     981   4034   8142
        |    2     1     6    29    54    35   .05           |   31795    4370
gfz  197|    0    -3     7  -101   -63    52  -.15   32   32 |  283412    1569   4050   7966
        |    1     3     4    48    24    61   .09           |   28881    3825
iac  n/a|    1     1    -7   -44    -4   -25  -.02   37   37 |  447641    -188   4021   8140
        |    1     1    24    20    34   124   .07           |   29577    1739
mcc  n/a|   -3     0    28  -131   -80   628   .31  164  164 |     ---     ---    ---    ---
        |   15    14    12   203   144   758   .79           |     ---     ---


Table 1.1583.b     GPS week : 1583   MJD: 55325.0-55331.0   

         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  |   10    8    9   12   11   11   10 |
 R02  |   14   10   11   10    9   12   11 |
 R03  |   12   11   13   11   10   15    8 |
 R04  |   11   13   14   13   12   39   22 |
 R05  |   12   10    9   12   17   87   29 |
 R07  |    9   10   13   13    9    8   11 |
 R08  |   10   12   11   14   12   11   15 |
 R10  |   17   20   13   16   14   19   11 |
 R11  |   28   18   20   20   18   20   19 |
 R13  |   19   22   18   15   12   16   13 |
 R14  |   15   16   13   14   14   10   15 |
 R15  |   13   18   15   18   19   20   11 |
 R17  |   14   21   15   13   15   18   14 |
 R18  |    9   10   11   10   14   13   15 |
 R19  |   14   11    9   11   14    9   11 |
 R20  |   20   14   12   15   16   15   16 |
 R21  |   15   11   11   12   15   18   11 |
 R22  |   15   12   15   10   10   15   13 |
 R23  |   12   11   10    8   12   12   17 |
 R24  |   11   12   10    8   10   12    8 |


Table 1.1583.c     GPS week : 1583   MJD: 55325.0-55331.0   

         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 1583 0   |    0   -61   134   -3456   -4168  -12940  87.8  1998  1998 |  462268       0
brd 1583 1   |    2    96   323   -2447    1856  -17700  89.0  1812  1812 |  463694       0
brd 1583 2   |   40   -37   379     460    1299  -20460  87.9  1881  1881 |  466871       0
brd 1583 3   |  -41    39   334    1942    -729  -14170  84.5  2074  2074 |  395311       0
brd 1583 4   |  124    70   286     990     403  -13770  87.4  2321  2321 |  465095       0
brd 1583 5   |   44   -30   106   -1560    1679  -13760  85.2  2406  2406 |  465896       0
brd 1583 6   |   11   -85   186   -1090    -421  -16239  88.8  3028  3028 |  414434       0
-------------+------------------------------------------------------------+----------------
brd 1583 mean|   26     0   250    -737     -11  -15577  87.2  2217  2217 |  447652       0
brd 1583 sdev|   51    69   106    1945    2089    2716   1.7   418   418 |   29778       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 2.1583.0  GPS week: 1583   Day: 0   MJD: 55325                            

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  129|    1     2   -10   -18     2   -60  -.07   25   27 |       0     -85   1673   1726
cod  246|   -3     0     5    58   -17    11  -.17   15   15 |     ---     ---    ---    ---
esx  142|    0    -1     7   -22     5    73   .37   27   24 |  124500     653   4187   6298
gfz  197|    0    -4     7   -91   -63    36  -.11   29   29 |  294878     522   4227   6553
iac  n/a|    2     3   -17   -81    24   -11   .09   38   38 |  462604     177   4173   6739
mcc  n/a|  -25     2     9   -74   -97   417   .81  154  154 |     ---     ---    ---    ---

Table 2.1583.1  GPS week: 1583   Day: 1   MJD: 55326                            

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  129|    0     0   -12    39     0   -16  -.07   21   23 |       0     -32   1615   1679
cod  246|   -2    -1     6    16   -37     9  -.13   17   15 |     ---     ---    ---    ---
esx  142|   -1    -1    15   -39    65    78   .29   30   28 |  140607   -6366   4383   8058
gfz  197|    0     2     9  -104   -65   115  -.02   30   30 |  300760   -4711   4398   7812
iac  n/a|    1     1    -4   -29     6     0   .05   31   31 |  463868   -1361   4359   8215
mcc  n/a|    7    -6    24   -98   151   724  1.42  128  128 |     ---     ---    ---    ---

Table 2.1583.2  GPS week: 1583   Day: 2   MJD: 55327                            

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  129|    1    -1   -15    15   -55   -37  -.01   25   26 |       0      68   1820   1891
cod  246|   -2     0     1    45   -21     0  -.15   14   14 |     ---     ---    ---    ---
esx  142|    2    -3     2   -49    98    79   .44   24   22 |  127524    8695   4423   7376
gfz  197|    0    -5     0   -87   -62    69  -.22   33   33 |  297770    6862   4425   7369
iac  n/a|    2     1    12   -24   -35   -40  -.04   29   29 |  465171    3357   4417   7620
mcc  n/a|   21     1    20  -244  -196    81  1.01  135  135 |     ---     ---    ---    ---

Table 2.1583.3  GPS week: 1583   Day: 3   MJD: 55328                            

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  129|    0     0   -15    11    -4  -117  -.12   22   23 |       0       3   1615   1674
cod  246|    0    -1    -3    41    34    50  -.12   17   13 |     ---     ---    ---    ---
esx  142|   -1     0    11   -33    -9    90   .38   23   21 |   58238     576   3488   9291
gfz  197|    2    -7     8  -178   -92   135  -.22   32   32 |  232995     505   3486   7921
iac  n/a|    2     4    13   -28    -5  -142  -.05   30   30 |  396492    -639   3472   7903
mcc  n/a|  -17    24    43    -4  -194   204  -.52  273  273 |     ---     ---    ---    ---

Table 2.1583.4  GPS week: 1583   Day: 4   MJD: 55329                            

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  129|    0     0     3    -7   -19   -64  -.16   57   23 |       0      -6   1752   1819
cod  246|    0    -2     7    10    -3   -52  -.16   14   11 |     ---     ---    ---    ---
esx  142|    0     0    22    -5    41   -16   .45   25   23 |  135587    1084   4128   7649
gfz  197|   -1    -1    15   -93   -15    15  -.06   32   32 |  302907    -534   4159   8058
iac  n/a|    0     3   -58   -40   -19   229   .00   35   35 |  465702   -2085   4105   8100
mcc  n/a|   -9     6    45  -109   -12  -176  -.06  137  137 |     ---     ---    ---    ---

Table 2.1583.5  GPS week: 1583   Day: 5   MJD: 55330                            

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  129|    3     0    -7   -19    60   107  -.05   53   25 |       0     -84   1513   1582
cod  246|    1    -2     2    15   -11   -27  -.20   31   14 |     ---     ---    ---    ---
esx  142|   -4    -1     6    21   -66    56   .42   37   24 |  127494     487   3930   8908
gfz  197|    2    -4     4   -21   -85    36  -.16   44   44 |  303456    4454   3971   8689
iac  n/a|   -1     1     2   -46    48  -120  -.08   58   58 |  466188    -703   3929   8663
mcc  n/a|    3   -20    28   129    34  1084   .14  131  131 |     ---     ---    ---    ---

Table 2.1583.6  GPS week: 1583   Day: 6   MJD: 55331                            

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  129|    0     0   -13   -12   -25    36  -.06   36   26 |       0     -75   1578   1635
cod  246|    0     0     1    44     4    -5  -.15   14   14 |     ---     ---    ---    ---
esx  142|   -1    -1     8    25    47    55   .39   22   23 |   77768    1742   3703   9420
gfz  197|    0    -2     9  -134   -55   -44  -.26   27   26 |  251123    3891   3688   9364
iac  n/a|    4     0    -4   -61   -51   -95  -.13   37   37 |  413465     -66   3695   9743
mcc  n/a|   -5   -14    27  -514  -247  2066  -.64  193  193 |     ---     ---    ---    ---

       
       
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 3.1583.0  GPS week: 1583   Day: 0   MJD: 55325                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  698   10   12   21   20   27  ---    9 |    30   31   37   38   35  ---    29
 R02  |  929   14   22   27   24   33  ---   13 |    65   67   73   79   67  ---    67
 R03  | 2563   18   12   26   19   27  ---   11 |    64   77   85   81   58  ---    71
 R04  | 2198   20   13   24   16   19  ---   10 |   389  382  378  384  365  ---   379
 R05  | 1363   21   15   27   29   21  ---   12 |   484  479  467  466  466  ---   474
 R07  |  782    8   11   12   35   30  ---    8 |    23   30   32   35   36  ---    28
 R08  | 1162   11   11   19   19   27  147    9 |    47   50   55   50   54  117    50
 R10E | 2380   37   14   32   29   40  ---   17 |    69   72   82   65   66  ---    69
 R11E | 1126   62   20   60   42   48  ---   27 |    43   30   51   57   54  ---    35
 R13E | 5219   36   16   26   40   56  ---   18 |    37   35   54   39   56  ---    36
 R14E | 2375   25   18   23   22   40  ---   14 |    43   36   43   38   45  ---    37
 R15E | 1115   18   13   18   35   45   79   13 |    24   20   25   34   48   42    18
 R17  | 1617   21   19   22   50   40  ---   14 |    70   69   69   71   63  ---    65
 R18  | 1878   19   12   11   24   22  ---    9 |    35   55   53   61   64  ---    49
 R19  | 1629   25    9   35   20   29  ---   14 |    44   57   76   69   63  ---    56
 R20  | 2301   21   14   29   25   73  ---   19 |    42   48   50   55   97  ---    50
 R21  | 1197   17   13   17   29   55  ---   14 |    41   45   58   54   82  ---    50
 R22  | 1520   28   18   30   20   28  ---   14 |    40   53   65   54   66  ---    52
 R23  | 1528   19   14   21   16   31  209   11 |    25   31   33   39   34   57    26
 R24  | 1415   19   17   17   29   23  ---   10 |    34   43   37   42   35  ---    35
------+-----------------------------------------+-------------------------------------
 RMS  | 1997   25   15   27   29   38  154      |T   82   85   91   90   92   72    83
 WRMS | 1997   27   15   24   29   38  154      |NE 129  133  136  136  131   87   130
 MEDI | 1520   19   14   23   24   30  147      |MD  42   48   54   54   58   57    50

Table 3.1583.1  GPS week: 1583   Day: 1   MJD: 55326                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  815   11    9   17   19   20  ---    8 |    27   28   32   40   39  ---    29
 R02  |  979   11   14   20   16   22  ---    9 |    48   51   59   48   52  ---    51
 R03  | 1428   12   14   27   17   26  ---   11 |    72   75   63   81   72  ---    70
 R04  | 1049   13   22   33   20   24  ---   13 |   424  423  426  428  415  ---   422
 R05  | 1302   18   12   17   23   21  ---    9 |   516  514  512  511  486  ---   508
 R07  | 2290   13    9   26   24   23  ---   10 |    20   27   34   32   48  ---    28
 R08  | 1579   13   19   23   21   25   79   11 |    50   67   56   57   68   60    60
 R10E | 2597   44   26   36   43   28  ---   20 |    41   67   77   67   60  ---    51
 R11E | 1161   39   22   32   53   34  ---   18 |    52   49   69   71   70  ---    53
 R13E | 2465   43   19   39   55   52  ---   22 |    18   25   40   51   63  ---    25
 R14E | 2040   20   20   36   26   38  ---   16 |    25   30   45   36   45  ---    27
 R15E | 1421   21   21   23   37   52  104   17 |    31   19   33   41   51   58    21
 R17  | 1936   14   15   51   22   60  ---   21 |    73   63   90   59   69  ---    65
 R18  | 2492   17   11   24   44   18  ---   10 |    30   41   61   68   34  ---    37
 R19  |  896   11   17   30   21   19  ---   11 |    43   49   50   51   43  ---    41
 R20  | 2260   18   19   37   27   18  ---   13 |    44   51   70   52   34  ---    43
 R21  | 1681   15   15   25   15   25  ---   11 |    20   32   31   33   42  ---    26
 R22  | 2710   21   15   20   13   23  ---   11 |    24   35   35   28   37  ---    28
 R23  | 1324   10   18   23   20   21  179   10 |    20   22   30   27   25   27    17
 R24  | 1823   11   15   35   38   18  ---   11 |    17   26   18   25   20  ---    15
------+-----------------------------------------+-------------------------------------
 RMS  | 1812   21   17   30   30   31  128      |T   79   84   91   90   88   48    80
 WRMS | 1812   23   15   28   30   31  128      |NE 133  138  138  139  138   43   134
 MEDI | 1579   14   15   26   22   23  104      |MD  31   41   50   51   48   58    37

Table 3.1583.2  GPS week: 1583   Day: 2   MJD: 55327                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1472   15    9   10   19   25  ---    8 |    26   33   31   42   40  ---    29
 R02  | 1087   20   10   21   11   24  ---   10 |    29   36   41   35   38  ---    32
 R03  | 1226   15   17   28   33   26  ---   12 |    31   42   42   46   47  ---    37
 R04  | 1387   13   19   37   17   24  ---   14 |   229  224  217  214  224  ---   222
 R05  | 1197   15   13   21   33   14  ---    9 |   284  277  292  297  269  ---   278
 R07  | 3707   28   13   19   35   35  ---   13 |    22   36   46   51   49  ---    34
 R08  |  829   22    7   16   16   34  151   11 |    38   44   55   47   51   83    44
 R10E | 1744   27   14   18   54   29  ---   12 |    43   33   48   65   60  ---    37
 R11E |  959   51   17   32   63   44  ---   20 |    37   29   44   55   57  ---    31
 R13E | 2043   38   18   37   37   34  ---   17 |    44   36   49   40   51  ---    38
 R14E | 1186   27   15   21   35   28  ---   12 |    39   41   47   54   50  ---    38
 R15E | 1569   26   14   25   39   40   64   14 |    36   36   34   44   49   46    31
 R17  | 1163   31   14   28   32   33  ---   14 |    45   48   21   34   42  ---    35
 R18  | 2544   17   10   17   19   30  ---   10 |    40   57   42   52   67  ---    50
 R19  | 1027    7    9   19   39   26  ---    9 |    49   53   51   76   75  ---    54
 R20  | 3348   11   16   27   21   28  ---   12 |    46   54   66   61   43  ---    50
 R21  | 1462   29   12   20   23   14  ---   11 |    31   52   57   47   52  ---    46
 R22  | 3085   25   18   32   40   30  ---   14 |    32   41   41   35   63  ---    37
 R23  | 1189   17   10   18   26   24  166    9 |    29   26   35   31   37   38    26
 R24  | 1722   18   10   18   25   23  ---    9 |    37   42   53   42   43  ---    41
------+-----------------------------------------+-------------------------------------
 RMS  | 1881   25   14   24   33   29  135      |T   58   62   65   68   70   55    59
 WRMS | 1881   26   14   22   33   29  135      |NE  80   84   88   88   90   60    82
 MEDI | 1387   20   13   21   32   28  151      |MD  37   41   46   47   50   46    37

Table 3.1583.3  GPS week: 1583   Day: 3   MJD: 55328                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1269   15   16   15   27   37  ---   12 |    31   23   31   21   55  ---    28
 R02  | 1841   18    9   16   21   25  ---    9 |    40   52   57   59   54  ---    49
 R03  | 1413   16   10   24   22   27  ---   11 |    75   72   79   73   79  ---    74
 R04  | 1309   20   18   28   18   20  ---   12 |   517  513  510  508  494  ---   509
 R05  | 2734   13   22   18   24   25  ---   11 |   660  621  605  607  584  ---   608
 R07  | 3545   21   11   17   45   40  ---   12 |    21   28   31   41   44  ---    26
 R08  | 2077    7   15   33   21   34  440   13 |    76   84   52   73   74  229    71
 R10E | 2254   31   28   14   44   34  ---   15 |    44   57   50   64   53  ---    47
 R11E | 1251   41   33   36   45   27  ---   20 |    59   62   78   74   76  ---    62
 R13E | 1602   28   14   30   43   28  ---   14 |    32   28   43   45   54  ---    28
 R14E | 1616   24   15   27   35   32  ---   14 |    29   23   41   37   45  ---    24
 R15E | 1727   32   20   30   42   43  100   17 |    33   46   45   66   65  103    37
 R17  | 1172   18   15   18   35   39  ---   13 |    57   76   73   59   73  ---    69
 R18  | 2136   21   12   17   29   20  ---   10 |    34   58   49   37   65  ---    50
 R19  | 1529   19   11   27   22   19  ---   11 |    58   63   81   77   61  ---    63
 R20  | 4374   32   14   21   38   39  ---   15 |    60   56   73   83   84  ---    62
 R21  |  902   22   18   19   35   26  ---   12 |    67   60   66   41   81  ---    63
 R22  | 2427   19   11   20   20   20  ---   10 |    36   45   47   46   62  ---    44
 R23  | 1280   15   10   14   29   18  142    8 |    28   29   38   52   38   79    30
 R24  | 1544   11    9   12   12   22  ---    7 |    36   31   35   37   54  ---    35
------+-----------------------------------------+-------------------------------------
 RMS  | 2074   22   17   23   32   30  273      |T   99  101  104  105  109  137    98
 WRMS | 2074   23   13   21   32   30  273      |NE 164  163  161  164  164  154   159
 MEDI | 1602   19   14   19   29   27  142      |MD  40   56   50   59   62  103    49

Table 3.1583.4  GPS week: 1583   Day: 4   MJD: 55329                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 2480   24   12   15   19   32  ---   11 |    26   29   28   42   79  ---    32
 R02  | 3780   13   10   17   18   27  ---    9 |    56   59   62   61   86  ---    60
 R03  | 1335   15   12   24   23   24  ---   10 |    38   53   54   60   75  ---    48
 R04  | 1774   13   16   22   21   31  ---   11 |   436  432  434  420  437  ---   433
 R05  | 2552  234   17   26   41   34  ---   16 |   393  543  534  523  532  ---   538
 R07  | 2360   13   10   20   27   24  ---    9 |    23   29   28   39   60  ---    28
 R08  | 3115   26    8   24   17   30  147   12 |    48   62   84   61   91  128    65
 R10E | 2940   14   11   26   46   50  ---   14 |    27   32   40   45   60  ---    28
 R11E | 2200   31   24   30   43   43  ---   17 |    57   47   53   45   62  ---    44
 R13E | 2296   15   14   28   39   29  ---   12 |    30   39   51   42   41  ---    34
 R14E | 2524   23   21   22   38   37  ---   14 |    37   58   58   74   64  ---    49
 R15E | 1517   36   18   33   54   52   90   19 |    36   47   48   60   66   58    37
 R17  | 1338   39    8   25   42   35  ---   15 |    41   46   54   66   47  ---    40
 R18  | 1402   34    8   31   34   26  ---   14 |    42   40   52   36   35  ---    35
 R19  | 1085   30   12   24   25   34  ---   13 |    54   41   38   40   38  ---    34
 R20  | 4797   20   13   31   24   52  ---   16 |    38   41   38   34   41  ---    35
 R21  |  988   24   13   32   24   36  ---   14 |    37   42   74   64   46  ---    44
 R22  | 1185   13   10   23   24   28  ---   10 |    61   46   55   44   59  ---    50
 R23  | 1066   14   16   26   19   29  163   11 |    42   45   64   35   49   77    43
 R24M | 1271   14    7   21   13   33  ---   10 |    32   36   27   35   54  ---    31
------+-----------------------------------------+-------------------------------------
 RMS  | 2320   57   14   25   32   35  137      |T   77   88   93   91  101   87    85
 WRMS | 2320   23   11   23   32   35  137      |NE 124  144  149  142  163  102   144
 MEDI | 1774   20   12   24   24   32  147      |MD  38   45   53   45   60   77    40

Table 3.1583.5  GPS week: 1583   Day: 5   MJD: 55330                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 2123   16   14   24   28   24  ---   11 |    17   16   27   27   32  ---    18
 R02  | 4298   28   15   19   21   23  ---   12 |    83   87   84   88   94  ---    84
 R03  | 2425   31   16   34   17   21  ---   15 |    90   99   90   95   96  ---    92
 R04  | 1506   38   36   41   41  137  ---   38 |   815  817  818  813  754  ---   803
 R05  | 1698  210  110  109  114  175  ---   86 |   910 9999 9999 9999  915  ---   975
 R07  | 1078   12   11   15   25   19  ---    8 |    18   22   29   30   33  ---    20
 R08  | 1673   23    9   25   37   18   56   11 |    88   99   95  104  100   43    93
 R10E | 2564   36   25   35   31   35  ---   18 |    31   40   61   46   49  ---    37
 R11E | 3477   40   21   40   49   40  ---   20 |    56   69   69   65   81  ---    65
 R13E | 1319   20   25   37   46   27  ---   16 |    32   39   50   48   32  ---    30
 R14E | 1972   19   14   14   53   25  ---   10 |    30   41   29   63   34  ---    30
 R15E | 3615   31   28   33   79   48  115   19 |    35   56   59   88   72   50    46
 R17M | 1506   34   15   15   25   57  ---   18 |    88   90   82   86  113  ---    90
 R18M | 1975   30    8   21   21   30  ---   13 |   111  118  128  119  128  ---   119
 R19M |  608   16    7   16   25   24  ---    9 |    56   55   55   66   54  ---    53
 R20M | 5490   23   14   30   27   36  ---   14 |    34   36   43   36   28  ---    29
 R21M |  942   11   19   45   38   42  ---   18 |    32   41   28   39   52  ---    28
 R22  |  995   28   24   31   35   19  ---   15 |    39   35   69   68   45  ---    42
 R23  |  899   23   13   17   24   34  187   12 |    41   30   20   29   22   39    22
 R24  | 1016   20   14   22   15   23  ---   11 |    42   30   53   40   39  ---    37
------+-----------------------------------------+-------------------------------------
 RMS  | 2405   53   31   37   44   58  131      |T  132   95   99  102  138   44   135
 WRMS | 2405   25   14   24   44   58  131      |NE 233  150  154  156  232   41   238
 MEDI | 1673   23   15   25   28   27  115      |MD  41   41   59   65   52   43    42

Table 3.1583.6  GPS week: 1583   Day: 6   MJD: 55331                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1005   16   11   21   14   24  ---   10 |    25   33   29   30   48  ---    30
 R02  | 3584   33   13   19   13   14  ---   11 |    69   95  105   88   97  ---    92
 R03  | 2888   25    7   10   23   20  ---    8 |    63   82   89   89   85  ---    80
 R04  | 6618   60   18   20   20   65  ---   22 |   589  584  584  578  540  ---   577
 R05  | 5594   82   22   21   19   84  ---   28 |   709  706  703  695  635  ---   698
 R07  | 1093   12   13   25   20   24  ---   11 |    31   35   44   41   37  ---    35
 R08  | 1827   30   16   35   15   21  106   14 |    76  102  128  104   98  111   102
 R10E | 4046   28   10   14   29   29  ---   11 |    47   66   77   68   61  ---    62
 R11E | 2572   52   21   23   45   43  ---   18 |    73   78   89   98   85  ---    78
 R13E | 1600   28   11   23   33   33  ---   12 |    32   28   45   41   33  ---    31
 R14E | 1226   26   15   33   41   32  ---   14 |    29   36   36   41   30  ---    27
 R15E | 1597   21    8   20   47   30  190   10 |    24   25   35   42   38   50    25
 R17  | 1314   40   12   20   24   30  ---   13 |   261  261  258  255  255  ---   259
 R18  | 4450   26    8   21   25   51  ---   15 |   227  227  219  230  235  ---   225
 R19  | 1133   23   10   11   19   33  ---   10 |   293  291  289  292  295  ---   291
 R20  | 4615   54   10   15   28   38  ---   16 |   186  191  188  189  195  ---   189
 R21  |  954   30   15   17   27   20  ---   11 |    46   68   65   74   65  ---    61
 R22  | 1860   22   14   28   28   28  ---   13 |    48   49   68   66   59  ---    53
 R23  | 1246   21   23   37   27   33  254   16 |    32   31   65   41   40   38    36
 R24  | 1351   15   10   13   13   17  ---    7 |    42   44   42   45   41  ---    41
------+-----------------------------------------+-------------------------------------
 RMS  | 3027   36   14   22   27   37  193      |T  145  151  157  155  148   66   149
 WRMS | 3027   26   14   23   26   37  193      |NE 182  190  201  192  182   74   189
 MEDI | 1600   26   12   20   24   30  190      |MD  48   68   77   74   65   50    62



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