[IGSREPORT-19264] Wk 1612 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Dec 16 07:03:57 PST 2010


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1612   (Nov 28, 2010 - Dec 04, 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 2.1612.
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:                   
                                                                               
 igl1612[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1612 in the SP3 format.
 igl16127.sum      Combination Report for GPS Week 1612.


    
    
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  |    341.0 ns
                1  |    327.1 ns
                2  |    314.2 ns
                3  |    321.5 ns
                4  |    325.2 ns
                5  |    319.8 ns
                6  |    320.4 ns

    
         
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 1.1612, 1a.1612).
        
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 2.1612.0-6)                                                                                
    
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 3.1612.0-6). 
        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 1612 summary.                      (Nov 28, 2010 - Dec 04, 2010)

Table 1.1612.a     GPS week : 1612   MJD: 55528.0-55534.0

         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  134|    0     0     9     7   -18  -124  -.12   31   30 |       0     590   5694   6438
        |    1     1     3    44    29    58   .04           |       0    2504
cod  233|   -1     0    -2    32    24    12  -.08   14   12 |     ---     ---    ---    ---
        |    0     0     4    15    16    26   .03           |     ---     ---
esx  148|   -1     0    -6   -33   -30    52   .34   26   23 |    6516    1210   5642  14633
        |    1     1     4    34    35    57   .08           |    9497    3839
gfz  190|   -2     0    -5   -74   -21    -6  -.32   31   28 |  150815    1302   5711  14761
        |    2     2     7    33    95    43   .08           |    8764    3140
iac  n/a|    3     0     9   -26   -11    74  -.18   33   33 |  325020    -795   5671  15074
        |    2     1    10    37    28    30   .05           |    8813    2150
mcc  n/a|    4    -1    63   -21    15   357  -.43  185  185 |     ---     ---    ---    ---
        |   13     8    13   113   175   608   .26           |     ---     ---


Table 1.1612.b     GPS week : 1612   MJD: 55528.0-55534.0   

         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   15   19   23   20   19   19 |
 R02  |   16   22   15   17   23   21   18 |
 R05  |   14   15   15   17   22   22   23 |
 R06  |   27   20   14   18   19   22   21 |
 R07  |   19   20   19   17   22   27   31 |
 R08  |   15   14   17   17   17   20   27 |
 R09  |   10   10   11   12   12   14   10 |
 R10  |   10    9   10   10   13   16   14 |
 R11  |   19   21   15   12   12   20   18 |
 R12  |    7   10   10    8   10   10   11 |
 R13  |   10   10    9   11   10    9    9 |
 R15  |   13   15   10   14   13   12   11 |
 R16  |   10   10   12   10    9   10   14 |
 R17  | 4587    0    0  ---  ---  ---  --- |
 R18  |   13   11   11    7   12    8   13 |
 R19  |    9   11    9   11   11   14   12 |
 R20  |   22   16   16    9   13   16   12 |
 R21  |   14   12    7   10   13    9    9 |
 R22  |   14   19   11    8    9   15   11 |
 R23  |   12   16   11    9   11    9   10 |
 R24  |   12   11   10    9   10   11   11 |


Table 1.1612.c     GPS week : 1612   MJD: 55528.0-55534.0   

         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 1612 0   |    7    37   101   -1268     293  -16780  85.1  1733  1733 |  340973       0
brd 1612 1   |   83   -78    18   -1624   -1028  -16680  87.4  1886  1886 |  327130       0
brd 1612 2   |    5   -37    79    -386   -1244  -16140  84.5  2090  2090 |  314177       0
brd 1612 3   |  106   103   121      35    2061  -11510  86.8  2599  2599 |  321526       0
brd 1612 4   |  -36  -182   -11    -901   -1091  -13350  84.1  3385  3385 |  325158       0
brd 1612 5   |  -26   -65   150    -251   -1634  -16840  85.0  2416  2416 |  319795       0
brd 1612 6   |   19    33   266     629      54  -19790  84.5  2360  2360 |  320376       0
-------------+------------------------------------------------------------+----------------
brd 1612 mean|   22   -26   103    -538    -369  -15870  85.3  2352  2352 |  324162       0
brd 1612 sdev|   53    94    91     779    1280    2684   1.3   547   547 |    8489       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 2.1612.0  GPS week: 1612   Day: 0   MJD: 55528                            

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  134|    0     1    14   -40    -1  -121  -.11   29   29 |       0    2695   5267   6053
cod  233|   -2     0    -4    54    36    -9  -.06   14   14 |     ---     ---    ---    ---
esx  148|    0     0    -1    13   -49    87   .38   28   23 |   19383   -2108   5405  10802
gfz  190|   -4    -1    -2   -91    55     7  -.38   32   28 |  165991   -2994   5472  11128
iac  n/a|    4     0    -1   -68    -3   105  -.24   28   28 |  341895   -3672   5393  10793
mcc  n/a|   24     5    69  -125   178   -78  -.33  216  216 |     ---     ---    ---    ---

Table 2.1612.1  GPS week: 1612   Day: 1   MJD: 55529                            

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  134|    3     1    12     4   -41  -213  -.10   31   30 |       0    -825   5798   6444
cod  233|   -2     0    -5    24    15    40  -.09   13   11 |     ---     ---    ---    ---
esx  148|    1     1   -15   -53    -4    88   .42   32   27 |   -7614    4725   5148  11942
gfz  190|   -4    -2   -21   -47    85     3  -.32   35   28 |  149814    2535   5223  11976
iac  n/a|    4     1    18   -19   -11    53  -.17   32   32 |  326825     317   5146  12445
mcc  n/a|   14    12    52     7   213  -214  -.84  166  166 |     ---     ---    ---    ---

Table 2.1612.2  GPS week: 1612   Day: 2   MJD: 55530                            

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  134|    1    -1     5    74   -14   -20  -.16   24   23 |       0     188   5620   6458
cod  233|   -1     0   -10    18     7     0  -.09   15   13 |     ---     ---    ---    ---
esx  148|    0     0    -2   -70   -18   -54   .44   22   20 |   -4791    3575   7836  15208
gfz  190|    0    -3    -4   -68   -31   -60  -.32   27   29 |  138308    2268   8126  15485
iac  n/a|    4    -1    26    -2     3    82  -.26   33   33 |  314854   -1045   7938  15926
mcc  n/a|    2    -2    48   -13    -4  -253  -.17  172  172 |     ---     ---    ---    ---

Table 2.1612.3  GPS week: 1612   Day: 3   MJD: 55531                            

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  134|   -1    -1     7   -20     7  -116  -.03   28   27 |       0    3151   6520   7592
cod  233|    0     0    -2    51     0   -21  -.08   13   11 |     ---     ---    ---    ---
esx  148|   -1     1    -7    -8   -31   108   .21   21   20 |    7702    3493   6409  17770
gfz  190|   -1     1    -8  -123    18    30  -.38   36   30 |  144936    2747   6449  18050
iac  n/a|    0     0    14   -52    20    54  -.15   30   30 |  322829    -978   6574  18155
mcc  n/a|  -13   -14    74  -149  -178   378  -.32  228  228 |     ---     ---    ---    ---

Table 2.1612.4  GPS week: 1612   Day: 4   MJD: 55532                            

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  134|    0    -1     7   -41    19  -136  -.17   30   28 |       0    3093   5014   5562
cod  233|    0     0     0    38    33    -2  -.03   14   10 |     ---     ---    ---    ---
esx  148|   -1     1    -6    -7   -93    77   .30   28   26 |   11579   -5535   4329  14986
gfz  190|    1     0    -2   -95    14   -69  -.23   28   20 |  156131   -3240   4293  14984
iac  n/a|    0    -2     4   -68     4   121  -.16   33   33 |  328938   -2747   4288  15254
mcc  n/a|   -9     0    63  -114   152  1456  -.62  140  140 |     ---     ---    ---    ---

Table 2.1612.5  GPS week: 1612   Day: 5   MJD: 55533                            

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  134|    0    -1     9    45   -44  -107  -.13   34   32 |       0   -3485   6454   7115
cod  233|    0     2     0    22    39    35  -.10   16   13 |     ---     ---    ---    ---
esx  148|   -3     0    -4   -74   -35    51   .30   25   23 |    8934     298   4880  17588
gfz  190|   -5     2     4   -19  -110    46  -.39   30   31 |  148064    2891   4890  17590
iac  n/a|    3    -2     4    20   -26    37  -.18   37   37 |  318865    2971   4846  17967
mcc  n/a|   10    -7    54   112   -17   645  -.58  166  166 |     ---     ---    ---    ---

Table 2.1612.6  GPS week: 1612   Day: 6   MJD: 55534                            

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  134|    0     2     7    27   -56  -154  -.13   43   41 |       0    -682   5190   5845
cod  233|    0     0     3    20    35    43  -.12   16   11 |     ---     ---    ---    ---
esx  148|   -2    -3    -8   -32    16    10   .31   25   22 |   10421    4027   5487  14136
gfz  190|    0    -1    -4   -76  -182    -3  -.20   29   28 |  152464    4911   5525  14118
iac  n/a|    6     0    -2     8   -65    68  -.10   36   36 |  320936    -413   5513  14983
mcc  n/a|    4    -1    84   130  -229   567  -.12  205  205 |     ---     ---    ---    ---

       
       
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 3.1612.0  GPS week: 1612   Day: 0   MJD: 55528                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 2450   35   12   25   27   44  ---   16 |    76   75   74   71   90  ---    75
 R02E | 2644   31   21   21   32   41  ---   16 |   108  131  132  129  130  ---   125
 R05E | 2810   30   12   27   35   34  403   14 |    97   97  104  110   80  129    93
XR06E | 3416   49   32   36  ---  ---  ---   26 |    42   37   51  ---  ---  ---    36
 R07E | 1814   36   18   42  ---   42  ---   19 |    20   24   55  ---   53  ---    31
 R08E |  871   37   11   26   25   31  195   14 |    22   26   38   38   46   66    27
 R09  | 1192   11    6   17   21   30  ---    9 |    25   29   36   38   35  ---    28
 R10  | 1364   14   10   13   18   27  ---    9 |    34   31   36   33   53  ---    34
 R11  | 1141   39   22   42   46   34   87   19 |    37   58   65   70   54   28    51
 R12  |  723   14    8   15   24   15  ---    7 |    25   28   29   35   28  ---    25
 R13  | 1732   11   12   26   27   20  ---   10 |    27   28   39   37   28  ---    26
 R15  | 2247   29    7   34   33   21  117   12 |    40   28   35   42   41   41    31
 R16  |  649   23    9   17   13   22  ---    9 |    32   37   41   36   34  ---    33
XR17  |>>>>>  ---  --- 2791  --- 5900  --- 4587 |   ---  ---    2  ---    1  ---  9999
 R18  | 2113   31   18   14   48   23  ---   12 |    44   55   68   67   50  ---    53
 R19  |  803   19    7   14   48   22  ---    8 |    41   54   70   72   56  ---    54
 R20  | 1724   54   16   58   21   22  ---   21 |    42   43   71   53   51  ---    43
 R21  | 1011   26   23   27   22   19  ---   13 |    43   70   69   72   44  ---    56
 R22  | 2268   31    8   32   26   24  ---   13 |    33   54   74   69   37  ---    49
 R23  | 1645   35    7   15   22   23  109   11 |    26   50   57   63   59  122    46
 R24  | 1241   13   14   27   46   25  ---   11 |    42   53   67   82   56  ---    52
------+-----------------------------------------+-------------------------------------
 RMS  | 1732   29   14   28   32   28  216      |T   42   50   57   62   51   77    48
 WRMS | 1732   29   14   23   28   28  216      |NE  35   44   50   54   41   63    41
 MEDI | 1724   30   12   26   26   24  117      |MD  37   43   57   63   50   66    43

Table 3.1612.1  GPS week: 1612   Day: 1   MJD: 55529                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 1168   29    9   34   40   39  ---   15 |    69   76   93   92   98  ---    80
 R02E | 2834   58   28   30   31   45  ---   22 |    87  118  118  113  110  ---   107
 R05E |  859   25   12   34   37   39  235   14 |    64   71   77   89   74  124    67
XR06E | 2142   28   17   45  ---  ---  ---   19 |    27   32   37  ---  ---  ---    23
 R07E | 2971   27   19   42  ---   54  ---   19 |    18   27   40  ---   54  ---    26
 R08E | 2470   28   13   23   41   39  219   14 |    28   22   34   46   43   49    22
 R09  | 2550   21    9   19   36   24  ---   10 |    24   31   40   50   26  ---    26
 R10  | 1947   19    8   15   28   23  ---    9 |    30   24   34   32   35  ---    26
 R11  |  844   39   20   59   36   35   91   20 |    29   53   85   77   52   22    48
 R12  |  557   24    8   19   21   20  ---    9 |    27   28   36   40   32  ---    26
 R13  | 1222   15    7   26   16   24  ---    9 |    23   24   39   32   29  ---    23
 R15  | 2587   39   15   31   58   30  118   15 |    33   26   37   58   32   33    24
 R16  | 1537   27    8   22   14   17  ---   10 |    24   38   44   40   23  ---    31
XR17  | ----  ---    4  ---  ---  ---  ---    0 |   --- 9999  ---  ---  ---  ---  9999
 R18  | 1942   17   13   29   15   16  ---   10 |    30   35   66   47   35  ---    38
 R19  |  863   18   11   26   36   29  ---   11 |    24   25   46   54   35  ---    27
 R20  | 1401   37   11   30   31   41  ---   16 |    14   20   48   42   43  ---    23
 R21  | 2735   28   10   29   27   22  ---   11 |    19   41   54   52   39  ---    37
 R22  | 1213   39   13   47   43   40  ---   18 |    17   37   65   70   32  ---    28
 R23  | 1213   42   12   40   45   26  111   16 |    15   39   68   77   27   53    32
 R24  | 1927   22   12   26   48   16  ---   10 |    20   29   49   59   26  ---    26
------+-----------------------------------------+-------------------------------------
 RMS  | 1885   31   13   32   35   32  166      |T   31   39   55   59   44   56    37
 WRMS | 1885   30   11   27   28   32  166      |NE  23   32   50   52   33   36    29
 MEDI | 1537   27   12   29   36   29  118      |MD  24   31   46   52   35   49    26

Table 3.1612.2  GPS week: 1612   Day: 2   MJD: 55530                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 1108   38   15   34   41   50  ---   19 |    79   86  111   89  114  ---    93
 R02E | 2142   22   20   25   29   41  ---   15 |    50   52   80   64   61  ---    55
 R05E |  943   30   17   21   43   43  164   15 |    44   70   66   90   68  105    58
XR06E | 2808   28   11   22  ---  ---  ---   14 |    59   39   37  ---  ---  ---    42
 R07E | 2398   36   18   40  ---   43  ---   19 |    21   27   37  ---   45  ---    19
 R08E | 2752   26   24   22   25   47  247   16 |    28   24   27   31   45   43    19
 R09  | 4256   27   12   13   23   23  ---   10 |    32   32   37   31   28  ---    29
 R10  | 2601   22    9   16   21   23  ---    9 |    31   28   35   36   38  ---    26
 R11  | 1074   26   20   33   27   24   97   15 |    52   55   69   63   44   30    51
 R12  | 1016   17   11   24   33   15  ---   10 |    22   24   45   43   29  ---    27
 R13  |  875   16   10   21   18   19  ---    9 |    27   32   46   37   35  ---    31
 R15  | 2597   21   14   14   25   21  124   10 |    33   26   38   32   40   44    26
 R16  | 1641   15   13   25   34   30  ---   11 |    22   34   52   40   25  ---    31
XR17  | ----  ---    6  ---  ---  ---  ---    0 |   --- 9999  ---  ---  ---  ---  9999
 R18  | 1086   26    5   13   33   33  ---   11 |    32   48   50   44   57  ---    44
 R19  |  645   14   10   15   29   27  ---    9 |    30   41   42   58   42  ---    37
 R20  | 1372   32   14   18    8   51  ---   16 |    36   36   45   38   45  ---    36
 R21  | 3142    9   11   10   17   21  ---    7 |    40   53   47   50   35  ---    44
 R22  |  649   18    9   18   26   30  ---   10 |    30   36   41   32   39  ---    32
 R23  | 1189   13   21   17   20   25  189   11 |    28   42   38   36   31  103    29
 R24  | 3231   26   11   13   17   22  ---   10 |    38   42   52   51   49  ---    42
------+-----------------------------------------+-------------------------------------
 RMS  | 2089   24   15   22   27   33  172      |T   36   41   49   48   45   65    38
 WRMS | 2089   23   13   20   29   33  172      |NE  32   37   45   42   38   59    34
 MEDI | 1372   22   12   18   25   27  164      |MD  32   36   45   40   42   44    32

Table 3.1612.3  GPS week: 1612   Day: 3   MJD: 55531                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 3038   42   29   18   28   68  ---   22 |    55   74   60   52   83  ---    61
 R02E | 2580   36   11   32   30   43  ---   17 |   102  108   95  111  126  ---   104
 R05E | 1528   37   18   25   35   44  312   17 |    66   90   91   93   78  334    82
XR06E | 2765   38   14   25   32  ---  ---   17 |    40   54   61   33  ---  ---    48
 R07E | 4200   37   12   30   75   44  ---   17 |    17   34   49   67   52  ---    31
 R08E | 3936   47   17   22   28   35  241   17 |    34   30   40   37   41  115    26
 R09  | 4274   27   10   19   18   26  ---   11 |    46   40   50   36   36  ---    40
 R10  | 2609   28    9   12   11   18  ---    9 |    26   31   32   34   32  ---    28
 R11  | 2281   24   17   24   26   22   89   12 |    48   62   51   50   49   35    52
 R12  | 1299   16    8   11   11   24  ---    8 |    34   34   26   24   33  ---    29
 R13  |  888   15   10   23   29   25  ---   10 |    28   34   48   49   32  ---    33
 R15  | 2968   37   12   24   29   21  154   13 |    38   39   40   30   41   82    34
 R16  | 1363   28    9   14   30   21  ---   10 |    37   35   42   46   37  ---    35
 R18  | 1094    8    8   10   13   21  ---    7 |    62   54   62   60   66  ---    59
 R19  | 1181   21   14   25   71   12  ---   10 |    43   52   71   92   58  ---    55
 R20  | 1702   14   11   13   19   26  ---    9 |    53   46   49   48   42  ---    45
 R21  | 4634   12   10   23   38   21  ---    9 |    52   59   74   89   47  ---    58
 R22  |  959   11   12   16   30   16  ---    8 |    45   50   60   48   52  ---    50
 R23  | 1222   18   10   16   19   15  271    8 |    27   36   36   36   30  201    31
 R24  | 2036   21   13   15   54   14  ---    9 |    31   50   54   91   42  ---    44
------+-----------------------------------------+-------------------------------------
 RMS  | 2598   28   13   21   36   30  228      |T   44   50   54   56   51  153    47
 WRMS | 2598   27   11   20   30   30  228      |NE  40   44   49   52   42  106    42
 MEDI | 2036   24   11   19   29   22  241      |MD  40   46   50   48   42  115    44

Table 3.1612.4  GPS week: 1612   Day: 4   MJD: 55532                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 2483   22   16   34   40   65  ---   20 |    59   53   58   73   77  ---    56
 R02E | 3184   54   21   42   51   50  ---   22 |    57   54   47   71   72  ---    51
 R05E | 1322   41   27   36   31   56  224   22 |    35   71   66   73   60  172    55
 R06E | 8778   47   22   23   23   40  ---   18 |    56   43   52   42   35  ---    47
XR07E | 8023   34   21  ---   71   43  ---   21 |    23   28  ---   62   50  ---    28
 R08E | 4045   44   20   22   28   35  117   17 |    42   26   42   48   48  143    31
 R09  | 4035   33    9   26   20   21  ---   12 |    27   37   47   46   35  ---    34
 R10  | 4022   36   11   27   22   23  ---   13 |    28   33   42   39   28  ---    30
 R11  | 4005   24   11   23   26   27  132   11 |    59   52   58   48   60   45    54
 R12  | 2003   18    9   23   18   18  ---    9 |    29   25   29   24   30  ---    24
 R13  | 2778   15    8   24   16   22  ---    9 |    31   32   40   37   38  ---    32
 R15  | 5014   23   10   22   24   38  118   13 |    26   31   28   38   42   69    28
 R16  | 1225   22    8   15   21   24  ---    9 |    26   29   34   28   35  ---    28
 R18  |  895   27    6   36   33   17  ---   12 |    38   48   82   76   51  ---    51
 R19  | 1311   25    7   31   31   14  ---   11 |    39   48   65   66   45  ---    46
 R20  | 1834   27   12   29   34   24  ---   12 |    49   49   44   65   36  ---    42
 R21  | 3193   13    9   41   21   25  ---   13 |    42   45   85   52   40  ---    50
 R22  |  881   21    9   14   24   23  ---    9 |    49   36   40   37   27  ---    35
 R23  |  795   13    9   28   29   25   49   10 |    23   27   38   38   46   63    28
 R24  | 1369   18   13   18   23   20  ---    9 |    41   49   47   50   46  ---    45
------+-----------------------------------------+-------------------------------------
 RMS  | 3385   30   14   28   28   33  140      |T   38   40   49   50   45   98    39
 WRMS | 3385   28   10   26   20   33  140      |NE  36   38   48   46   39   59    37
 MEDI | 2483   24   10   26   24   24  118      |MD  38   37   47   48   42   69    35

Table 3.1612.5  GPS week: 1612   Day: 5   MJD: 55533                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 1137   23   16   16   20   66  ---   18 |    41   40   57   47   76  ---    49
 R02E | 3760   59   17   27   29   44  ---   20 |    92   98   80   82  108  ---    92
 R05E | 1136   46   26   26   36   58  269   21 |    46   64   61   67   56  130    52
 R06E | 3402   53   26   30   25   47  ---   21 |    47   51   66   36   38  ---    51
 R07E | 1644   55   26   34   41   76  ---   26 |    23   34   34   50   65  ---    25
 R08E | 4648   47   21   30   36   44  119   19 |    46   27   48   36   56   41    32
 R09  | 3655   40   20   14   21   18  ---   13 |    40   33   43   42   31  ---    32
 R10  | 2669   31    9   34   35   36  ---   15 |    26   27   48   43   36  ---    28
XR11  |13067   34   20  ---   42   35  144   19 |    40   65  ---   48   48   40    51
 R12  | 2195   27   12   18   23   16  ---   10 |    27   34   40   30   31  ---    31
 R13  | 1883   18   12   19   14   17  ---    9 |    34   29   40   31   31  ---    29
 R15  | 2052   18    8   22   19   32  129   11 |    20   29   36   32   31   58    26
 R16  | 1266   20   10   16   29   23  ---    9 |    26   33   36   39   25  ---    28
 R18  | 1372   11    9   17   19   19  ---    8 |    43   45   43   49   48  ---    44
 R19  | 2394   32    8   38   41    9  ---   13 |    32   46   80   82   40  ---    50
 R20  | 3598   31   20   28   45   30  ---   15 |    30   51   38   77   42  ---    40
 R21  |  772   19    7   19   27   15  ---    8 |    43   49   60   56   56  ---    50
 R22  |  774   21   10   40   33   28  ---   14 |    29   37   67   43   21  ---    38
 R23  |  942   18   14   10   21   18   81    8 |    30   21   29   24   32   70    23
 R24  | 1002   28   16   12   29   17  ---   10 |    32   44   42   40   45  ---    41
------+-----------------------------------------+-------------------------------------
 RMS  | 2416   34   16   25   30   37  166      |T   37   42   49   47   45   67    40
 WRMS | 2416   32   13   23   31   37  166      |NE  32   38   46   45   36   56    36
 MEDI | 1883   28   14   22   29   28  129      |MD  32   37   43   43   40   58    38

Table 3.1612.6  GPS week: 1612   Day: 6   MJD: 55534                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 1194   28   17   24   34   60  ---   18 |    47   46   62   47   84  ---    53
 R02E | 3764   49   14   28   26   42  ---   17 |    93  102   91   79   88  ---    93
 R05E | 1803   72   18   27   35   47  263   22 |    59   44   46   60   50  113    39
 R06E | 1303   64   14   25   32   48  ---   20 |    49   41   48   43   40  ---    41
 R07E | 1200   61   36   58   66   70  ---   30 |    24   38   70   45   61  ---    34
 R08E | 4749   89   32   24   27   50  224   27 |    33   39   34   36   51   51    30
 R09  | 1798   20    9   20   28   26  ---   10 |    29   41   44   51   37  ---    36
 R10  | 3856   36   12   16   23   39  ---   14 |    31   36   38   41   49  ---    33
 R11  | 2973   48   16   37   23   28  216   17 |    47   54   70   48   47   39    50
 R12  | 2052   29   12   20   26   18  ---   10 |    29   27   33   36   33  ---    27
 R13  | 1518   26    7   18   18   16  ---    9 |    29   34   45   34   30  ---    33
 R15  | 1413   17    9   19   15   31  150   10 |    31   32   40   41   38   60    32
 R16  |  593   23    7   33   22   31  ---   13 |    27   32   50   48   31  ---    31
 R18  | 1378   40    7   22   21   27  ---   13 |    42   56   79   68   70  ---    60
 R19  | 3779   38    7   22   25   11  ---   11 |    44   62   80   81   55  ---    61
 R20  | 3237   26   10   20   28   30  ---   11 |    38   53   66   71   55  ---    53
 R21  | 1162   14   11   11   20   26  ---    9 |    53   68   66   77   53  ---    62
 R22  |  959   23   14   15   37   25  ---   10 |    46   66   70   56   43  ---    58
 R23  | 1018   15   10   20   18   21  150    9 |    38   40   48   44   36   78    39
 R24  | 1049   39   14   10   25   14  ---   11 |    24   52   54   59   52  ---    47
------+-----------------------------------------+-------------------------------------
 RMS  | 2360   43   16   25   29   36  205      |T   40   48   56   53   50   68    45
 WRMS | 2360   41   11   22   28   36  205      |NE  36   46   55   53   44   59    44
 MEDI | 1413   29   12   20   25   28  216      |MD  38   41   50   48   49   60    39




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