[IGSREPORT-19316] Wk 1614 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Dec 30 05:16:21 PST 2010


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1614   (Dec 12, 2010 - Dec 18, 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 2.1614.
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:                   
                                                                               
 igl1614[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1614 in the SP3 format.
 igl16147.sum      Combination Report for GPS Week 1614.


    
    
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  |    357.5 ns
                1  |    354.7 ns
                2  |    353.6 ns
                3  |    360.3 ns
                4  |    368.5 ns
                5  |    358.7 ns
                6  |    379.9 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 1.1614, 1a.1614).
        
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 2.1614.0-6)                                                                                
    
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 3.1614.0-6). 
        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 1614 summary.                      (Dec 12, 2010 - Dec 18, 2010)

Table 1.1614.a     GPS week : 1614   MJD: 55542.0-55548.0

         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  138|    0     0     7    11   -14    -8  -.11   27   26 |       0     347   4819   5320
        |    1     1     2    36    63   138   .03           |       0    1012
cod  236|    0     0     1    37   -12    -6  -.10   15   12 |     ---     ---    ---    ---
        |    0     0     1    24    30    29   .02           |     ---     ---
esx  156|    0    -2    -4   -69    60    29   .34   28   26 |   25945   -5549   6027  11137
        |    1     1     4    29    64    78   .05           |   11141    4100
gfz  193|    0    -3    -4  -100    50   -17  -.31   37   36 |  226728   -4517   6028  11392
        |    2     1     3    90   187    44   .09           |   11477    3308
iac  n/a|    0     0    -3   -37   -29    -2  -.05   29   29 |  362368   -1495   6020  11416
        |    1     1     8    27    37    46   .04           |    9054    2125
mcc  n/a|    4     0    48    11   -21   903  -.41  223  223 |     ---     ---    ---    ---
        |    9     6    15   118   116   389   .47           |     ---     ---


Table 1.1614.b     GPS week : 1614   MJD: 55542.0-55548.0   

         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  |   18   21   20   17   18   18   15 |
 R02  |   12   19   21   17   16   15   18 |
 R05  |   19   23   21   19   18   15   14 |
 R06  |   19   22   23   16   16   17   19 |
 R07  |   16   16   16   13   15   13   16 |
 R08  |   21   21   20   15   19   16   13 |
 R09  |   10   12   11   10   12   10   14 |
 R10  |    9    9   10   10   12   11   11 |
 R11  |   17   14   19   18   15   17   15 |
 R12  |   10    6    8   10    8    7    9 |
 R13  |   11   10   11   13    9   10    8 |
 R15  |   13   14   16   14   13   13   10 |
 R16  |   10   11   10   11   11   11   11 |
 R17  |    0    0    0    0    0    0    0 |
 R18  |   11    9   10   13   11    9   10 |
 R19  |   13    7   12   10   11   11    8 |
 R20  |   15   18   22   16   15   14   15 |
 R21  |   10   12   13   11    9    8   14 |
 R22  |   10   13   12   12   12   12   10 |
 R23  |   12   13   12    9   13   10    8 |
 R24  |   15   13   11    9   11    7   11 |


Table 1.1614.c     GPS week : 1614   MJD: 55542.0-55548.0   

         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 1614 0   |   30   122   187    -718    2687   -7022  84.6  1805  1805 |  357452       0
brd 1614 1   |   39   -24   198    1261    2699   -6490  86.6  1880  1880 |  354727       0
brd 1614 2   |   73   -24   141     444    7237  -11840  86.0  2185  2185 |  353554       0
brd 1614 3   |  -89    29   215     243    1815  -17580  84.0  1860  1860 |  360270       0
brd 1614 4   |   29    66   142    2049    -480  -20900  86.3  2058  2058 |  368528       0
brd 1614 5   |  -86    76   260   -4637   -4904  -21930  86.6  2424  2424 |  358702       0
brd 1614 6   |  -69    46   191   -2013   -2677  -24490  83.7  2331  2331 |  379897       0
-------------+------------------------------------------------------------+----------------
brd 1614 mean|  -10    41   191    -481     910  -15750  85.4  2077  2077 |  361875       0
brd 1614 sdev|   68    53    41    2254    3996    7321   1.3   243   243 |    9323       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 2.1614.0  GPS week: 1614   Day: 0   MJD: 55542                            

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  138|    0     0     4    12   -69   -34  -.15   28   28 |       0    -136   3917   4345
cod  236|    0     0     0    63    28    10  -.08   12   11 |     ---     ---    ---    ---
esx  156|   -1    -4    -6  -110   119     3   .31   31   30 |   40115   -1119   4484   9755
gfz  193|   -1    -1     0   -67  -144   -39  -.30   32   39 |  216439    -445   4477  10119
iac  n/a|    0     0     3   -40   -82     3   .01   33   33 |  355838     846   4482   9272
mcc  n/a|   -9    -3    33   186  -235  1078  -.12  221  221 |     ---     ---    ---    ---

Table 2.1614.1  GPS week: 1614   Day: 1   MJD: 55543                            

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  138|    1     2     8   -27  -102   145  -.11   32   29 |       0     301   2582   2798
cod  236|    0    -1     1    47    20   -59  -.06   16   12 |     ---     ---    ---    ---
esx  156|   -2     0    -1   -54    75    23   .28   26   26 |   19499   -7675   5210   9896
gfz  193|    0    -2     0  -204  -167   -19  -.38   42   41 |  216994   -2340   5245   9533
iac  n/a|    0     1    -4   -21   -57   -75  -.08   33   33 |  355683    -302   5192   9440
mcc  n/a|   -2     3    19   160   -48  1125  -.10  214  214 |     ---     ---    ---    ---

Table 2.1614.2  GPS week: 1614   Day: 2   MJD: 55544                            

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  138|    2     0    12    16    28  -119  -.07   33   30 |       0    1697   4176   4795
cod  236|   -1     0     1     2   -10    10  -.13   17   13 |     ---     ---    ---    ---
esx  156|    0    -2    -5   -24     3    34   .37   31   29 |   21642   -4267   5205  10165
gfz  193|    4    -5    -9  -171   131    -5  -.43   45   45 |  217067   -4414   5205  10306
iac  n/a|    2     2    -6   -16   -36    30  -.07   29   29 |  354564    -485   5202  10021
mcc  n/a|    0    10    57   -38    74  1382  -.20  177  177 |     ---     ---    ---    ---

Table 2.1614.3  GPS week: 1614   Day: 3   MJD: 55545                            

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  138|    0     0     6    71    76  -198  -.09   25   24 |       0     500   3662   4029
cod  236|    0     0     0     5   -50    10  -.08   16   14 |     ---     ---    ---    ---
esx  156|    1     0    -2   -90   -49   123   .29   26   25 |   23425  -12456   5642  10053
gfz  193|    0    -3    -5    -8   339    11  -.30   36   34 |  229796  -10395   5690  10361
iac  n/a|    0     0     1   -18    37    66  -.10   27   27 |  362749   -3766   5634  11230
mcc  n/a|    3    -2    58   -59   116  1059  -.06  200  200 |     ---     ---    ---    ---

Table 2.1614.4  GPS week: 1614   Day: 4   MJD: 55546                            

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  138|    1     2     5    42    32   175  -.11   25   25 |       0    -688   3641   3891
cod  236|   -1     1     0    37   -47   -37  -.11   15   13 |     ---     ---    ---    ---
esx  156|    0    -4    -9   -90    47   -93   .34   26   25 |   30147    -518   6219  11490
gfz  193|    1    -5    -6    31   187   -80  -.24   33   32 |  233428   -2385   6223  11722
iac  n/a|    1     0     4   -16   -17    -5  -.06   28   28 |  367002     587   6236  11841
mcc  n/a|   13   -10    55  -136   -83   870  -.55  232  232 |     ---     ---    ---    ---

Table 2.1614.5  GPS week: 1614   Day: 5   MJD: 55547                            

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  138|    0     0     6   -26   -13   -77  -.10   21   21 |       0    1605   8964   9892
cod  236|    0     0     2    62    -9     4  -.11   13   11 |     ---     ---    ---    ---
esx  156|   -1    -3    -8   -65   127   129   .39   28   26 |    8447   -5857   6690  12413
gfz  193|   -1    -4    -8  -178    84    56  -.35   34   33 |  225646   -4863   6657  13108
iac  n/a|    0     2    -8   -79   -38     4   .00   29   29 |  360525   -3975   6684  12779
mcc  n/a|   16     0    62   -26    31   603 -1.38  247  247 |     ---     ---    ---    ---

Table 2.1614.6  GPS week: 1614   Day: 6   MJD: 55548                            

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  138|   -2     0     9    -6   -50    53  -.14   25   23 |       0    -844   6797   7490
cod  236|    0     0     5    46   -18    13  -.11   14   12 |     ---     ---    ---    ---
esx  156|    2    -1     1   -51    99   -16   .41   27   24 |   38344   -6954   8741  14188
gfz  193|   -1    -5    -2  -102   -75   -47  -.17   34   27 |  247729   -6779   8702  14600
iac  n/a|    0     0   -18   -71   -10   -44  -.06   26   26 |  380219   -3374   8714  15332
mcc  n/a|    8     1    49   -10    -9   207  -.44  270  270 |     ---     ---    ---    ---

       
       
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 3.1614.0  GPS week: 1614   Day: 0   MJD: 55542                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1135   30   16   25   23   57  ---   18 |    21  ---   33   21   51  ---     0
 R02  |  976   24   13   18   20   33  ---   12 |    48  ---   49   45   57  ---     0
 R05  | 1398   29   18   43   34   50   81   19 |    99  ---   96  103  110   70     0
 R06  | 1485   40   12   48   44   40  ---   18 |    23  ---   28   36   46  ---     0
 R07  | 2927   28   13   35   54   44  ---   16 |    20  ---   47   49   49  ---     0
 R08  | 2143   54   20   33   27   49  204   21 |    37  ---   40   34   54   70     0
 R09  |  611   20   10   19   27   25  ---   10 |    20  ---   37   40   25  ---     0
 R10  |  856   17    9   21   12   16  ---    8 |    19  ---   37   20   21  ---     0
 R11  | 1546   24   15   51   28   27  100   16 |    33  ---   77   49   51   23     0
 R12  | 2082   20    6   22   18   26  ---   10 |    30  ---   42   31   25  ---     0
 R13  | 3680   24   11   25   23   21  ---   11 |    40  ---   46   40   27  ---     0
 R15  | 1199   15   11   23   18   41   76   12 |    22  ---   30   34   29   33     0
 R16  |  563   23    4   29   26   15  ---   10 |    23  ---   46   37   27  ---     0
XR17  | ----  ---    4  ---  ---  ---  ---    0 |   ---  ---  ---  ---  ---  ---     0
 R18  | 2904   26   12   28   29   12  433   11 |    35  ---   49   57   49  127     0
 R19  |  868   23   10   40   36   15  ---   12 |    36  ---   85   78   56  ---     0
 R20  | 2695   25   17   26   32   42  ---   15 |    26  ---   55   61   50  ---     0
 R21  |  853   26   13   15   28    9  ---    9 |    40  ---   65   72   58  ---     0
 R22  | 1555   18    6   28   66   17  ---    9 |    47  ---   78   79   56  ---     0
 R23  | 1401   20   11   27   35   30  203   11 |    35  ---   65   49   68   71     0
 R24  |  942   37    8   38   21   27  ---   15 |    23  ---   74   61   55  ---     0
------+-----------------------------------------+-------------------------------------
 RMS  | 1805   28   12   31   32   33  221      |T   33  ---   53   49   48   65   ---
 WRMS | 1805   28   11   30   39   33  221      |NE  33  ---   53   49   48   65   ---
 MEDI | 1398   24   11   27   27   27  100      |MD  30  ---   47   45   50   70   ---

Table 3.1614.1  GPS week: 1614   Day: 1   MJD: 55543                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1355   32   21   28   46   63  ---   20 |    28  ---   51   43   51  ---     0
 R02  | 2090   39   25   21   33   47  ---   18 |    64  ---   65   40   67  ---     0
 R05  |  974   63   20   39   45   42   89   23 |   102  ---  105   95  105   78     0
 R06  | 1445   49   22   41   55   46  ---   21 |    30  ---   26   44   44  ---     0
 R07  | 1699   28   14   36   83   33  ---   15 |    20  ---   30   85   35  ---     0
 R08  | 1900   48   23   31   54   47  258   20 |    39  ---   43   74   48  102     0
 R09  |  497   28   13   17   22   27  ---   11 |    28  ---   39   50   24  ---     0
 R10  | 1982   16    9   16   18   23  ---    9 |    16  ---   26   26   21  ---     0
 R11  | 1083   25   17   30   50   25   97   13 |    27  ---   49   47   39   26     0
 R12  | 2544   12    7   14   22   12  ---    6 |    18  ---   29   21   19  ---     0
 R13  | 2705   27   11   16   54   13  ---    9 |    24  ---   34   50   31  ---     0
 R15  |  964   22   10   21   31   42   60   14 |    24  ---   33   35   24   38     0
 R16  | 1013   23    9   18   32   26  ---   10 |    26  ---   31   35   20  ---     0
XR17  | ----  ---    4  ---  ---  ---  ---    0 |   ---  ---  ---  ---  ---  ---     0
 R18  | 4109   19    8   16   33   20  385    9 |    37  ---   43   54   20   73     0
 R19  | 1666   10   12    8   31   18  ---    7 |    37  ---   31   54   22  ---     0
 R20  | 2126   35   23   32   43   38  ---   17 |    31  ---   35   49   37  ---     0
 R21  | 1515   16   17   27   32   21  ---   11 |    30  ---   47   58   27  ---     0
 R22  | 2075   32   15   27   37   12  ---   12 |    37  ---   59   87   46  ---     0
 R23  |  846   26   10   29   39   25  199   12 |    26  ---   51   49   39   78     0
 R24  | 1516   37    7   27   30   17  ---   12 |    30  ---   64   61   48  ---     0
------+-----------------------------------------+-------------------------------------
 RMS  | 1879   32   16   26   42   33  214      |T   33  ---   44   52   38   65   ---
 WRMS | 1879   29   12   26   41   33  214      |NE  33  ---   44   52   38   65   ---
 MEDI | 1516   27   13   27   33   25   97      |MD  28  ---   39   49   35   73   ---

Table 3.1614.2  GPS week: 1614   Day: 2   MJD: 55544                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  863   38   23   30   30   46  ---   19 |    24  ---   35   51   54  ---     0
 R02  | 1817   56   26   22   49   39  ---   20 |    51  ---   65   74   76  ---     0
 R05  | 1704   57   21   34   42   34  125   20 |    60  ---   78   63   80  128     0
 R06  | 2559   48   24   45   54   46  ---   22 |    41  ---   33   48   46  ---     0
 R07  | 2375   21   17   35  104   35  ---   15 |    28  ---   35   91   37  ---     0
 R08  | 2573   51   21   37   66   31  233   19 |    52  ---   36   46   45  101     0
 R09  |  592   28   11   18   35   21  ---   11 |    22  ---   33   45   29  ---     0
 R10  | 1489   18    8   19   34   24  ---   10 |    21  ---   25   37   20  ---     0
 R11  | 1119   31   21   49   58   33   87   19 |    23  ---   68   75   48   38     0
 R12  | 2539   14    8   16   31   16  ---    7 |    17  ---   26   36   22  ---     0
 R13  | 2507   19   14   30   31   11  ---   11 |    21  ---   39   37   23  ---     0
 R15  | 3730   32   13   36   25   34   97   16 |    27  ---   46   27   22   40     0
 R16  | 1157   18    7   17   19   27  ---   10 |    26  ---   31   31   24  ---     0
XR17  | ----  ---    2  ---  ---  ---  ---    0 |   ---  ---  ---  ---  ---  ---     0
 R18  | 4722   19   10   26   31   15  313   10 |    41  ---   21   54   43  143     0
 R19  | 1323   30    9   22   48   21  ---   11 |    26  ---   52   51   54  ---     0
 R20  | 1795   40   25   55   42   30  ---   21 |    20  ---   68   64   37  ---     0
 R21  | 1150   19   20   20   26   25  ---   12 |    31  ---   58   55   43  ---     0
 R22  | 2006   25   21   20   35   19  ---   12 |    34  ---   62   71   58  ---     0
 R23  | 1419   20   16   25   31   25   60   12 |    40  ---   60   62   61   48     0
 R24  | 1794   32    7   24   28   11  ---   10 |    22  ---   52   50   41  ---     0
------+-----------------------------------------+-------------------------------------
 RMS  | 2184   33   17   31   45   29  177      |T   31  ---   46   53   43   83   ---
 WRMS | 2184   30   13   29   45   29  177      |NE  31  ---   46   53   43   83   ---
 MEDI | 1794   28   16   25   34   25   97      |MD  26  ---   39   51   43   48   ---

Table 3.1614.3  GPS week: 1614   Day: 3   MJD: 55545                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1046   28   18   21   30   45  ---   16 |    32  ---   37   43   52  ---     0
 R02  |  947   34   20   26   34   36  ---   16 |    81  ---   84   81   80  ---     0
 R05  | 1453   37   22   31   51   40   67   18 |   125  ---  135  122  134   60     0
 R06  | 2955   37   11   33   39   31  ---   16 |    26  ---   46   39   44  ---     0
 R07  | 1539   20   12   26   36   29  ---   12 |    43  ---   37   59   37  ---     0
 R08  | 2810   24   23   24   35   35  352   15 |    53  ---   32   53   54   65     0
 R09  |  641   16    6   27   35   17  ---   10 |    33  ---   35   40   33  ---     0
 R10  | 1598   14   10   22   35   23  ---   10 |    19  ---   32   37   25  ---     0
 R11  | 1002   32   25   36   56   29   83   17 |    34  ---   61   86   52   28     0
 R12  | 1761   23   13   21   39   15  ---   10 |    18  ---   35   45   29  ---     0
 R13  | 2066   20   14   36   32   14  ---   12 |    28  ---   37   37   30  ---     0
 R15  | 3712   38   13   19   26   22   89   13 |    36  ---   34   40   29   38     0
 R16  |  655   21   16   12   21   22  ---   10 |    30  ---   34   31   24  ---     0
XR17  | ----  ---    3  ---  ---  ---  ---    0 |   ---  ---  ---  ---  ---  ---     0
 R18  | 1665   19   15   38   39   18  304   13 |    54  ---   86   90   46   82     0
 R19  | 1323   14   12   23   21   21  ---   10 |    38  ---   62   68   51  ---     0
 R20  | 1368   23   20   33   51   32  ---   15 |    32  ---   66   86   51  ---     0
 R21  | 1128   28   15   19   39   15  ---   11 |    46  ---   70   72   67  ---     0
 R22  |  925   22   21   19   27   23  ---   12 |    40  ---   43   36   32  ---     0
 R23  | 1138   14   11   12   22   21   61    8 |    27  ---   41   45   51   31     0
 R24  | 3271   13   11   25   23   12  ---    9 |    39  ---   58   54   40  ---     0
------+-----------------------------------------+-------------------------------------
 RMS  | 1859   25   16   26   36   27  200      |T   41  ---   53   58   48   50   ---
 WRMS | 1859   24   14   25   34   27  200      |NE  41  ---   53   58   48   50   ---
 MEDI | 1368   22   14   24   35   22   83      |MD  34  ---   41   45   44   38   ---

Table 3.1614.4  GPS week: 1614   Day: 4   MJD: 55546                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1763   25   16   31   31   51  ---   18 |    28  ---   24   22   40  ---     0
 R02  | 1073   27   17   32   27   35  ---   15 |    42  ---   72   69   63  ---     0
 R05  | 1540   37   25   23   33   39   79   17 |    79  ---   87   98   88   45     0
 R06  | 2094   34   20   24   30   33  ---   15 |    50  ---   28   35   38  ---     0
 R07  | 4030   28   17   32   42   27  ---   14 |    45  ---   42   45   48  ---     0
 R08  | 2994   43   15   32   26   40  388   18 |    37  ---   78   59   71   43     0
 R09  | 1606   15   16   30   25   20  ---   11 |    30  ---   45   42   26  ---     0
 R10  | 3517   20   16   28   25   19  ---   12 |    25  ---   37   29   26  ---     0
 R11  |  839   34   16   29   28   25   94   14 |    22  ---   51   50   36   21     0
 R12  | 1463   14   10   21   24   11  ---    8 |    17  ---   40   27   18  ---     0
 R13  | 1739   13   12   20   25   13  ---    8 |    20  ---   39   36   19  ---     0
 R15  | 1374   22   19   23   24   28   92   13 |    29  ---   36   25   28   27     0
 R16  |  621   18   12   27   34   18  ---   11 |    23  ---   50   36   27  ---     0
XR17  | ----  ---    4  ---  ---  ---  ---    0 |   ---  ---  ---  ---  ---  ---     0
 R18  |  761   23    7   21   38   21  366   10 |    58  ---   58   51   39   50     0
 R19  | 1311   24   15   18   37   20  ---   11 |    22  ---   52   65   26  ---     0
 R20  | 3048   33   10   32   22   31  ---   15 |    33  ---   46   48   33  ---     0
 R21  | 1438   15   12   14   39   20  ---    8 |    42  ---   50   81   37  ---     0
 R22  |  982   12   16   20  ---   33  ---   12 |    39  ---   32  ---   31  ---     0
 R23  |  728   14   14   31   55   26  120   12 |    25  ---   47   66   36   18     0
 R24  | 3194   29   11   15   45   19  ---   10 |    28  ---   37   56   40  ---     0
------+-----------------------------------------+-------------------------------------
 RMS  | 2057   25   15   26   33   28  232      |T   34  ---   47   49   38   34   ---
 WRMS | 2057   25   13   25   32   28  232      |NE  34  ---   47   49   38   34   ---
 MEDI | 1463   23   15   24   30   25   94      |MD  29  ---   45   48   36   27   ---

Table 3.1614.5  GPS week: 1614   Day: 5   MJD: 55547                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  986   23   17   33   48   55  ---   18 |    21  ---   39   52   48  ---     0
 R02  | 1148   22   12   35   40   37  ---   14 |    66  ---   76   77   67  ---     0
 R05  | 1059   22   15   28   40   40  210   14 |   139  ---  150  133  150   69     0
 R06  | 1439   33   14   36   34   40  ---   17 |    42  ---   37   37   35  ---     0
 R07  | 5554   25   15   31   40   23  ---   13 |    39  ---   45   39   36  ---     0
 R08  | 1624   28   18   37   36   36  315   16 |    54  ---   67   65   64   35     0
 R09  | 1707   11    8   28   37   19  ---    9 |    29  ---   50   49   28  ---     0
 R10  | 5127   21   11   27   40   18  ---   10 |    21  ---   41   48   27  ---     0
 R11  | 1365   28   20   35   40   41  112   17 |    15  ---   46   38   38   21     0
 R12  | 1010   10    8   14   19   18  ---    7 |    15  ---   25   22   23  ---     0
 R13  | 1745   17    6   27   33   18  ---    9 |    23  ---   43   52   27  ---     0
 R15  | 1350   29   11   26   21   24   87   12 |    17  ---   36   27   22   32     0
 R16  |  798   14   17   28   24   17  ---   11 |    18  ---   38   35   21  ---     0
XR17  | ----  ---    4  ---  ---  ---  ---    0 |   ---  ---  ---  ---  ---  ---     0
 R18  | 1963   17    7   23   25   15  417    8 |    19  ---   41   51   39   53     0
 R19  | 3294   20   13   24   31   22  ---   11 |    24  ---   57   61   19  ---     0
 R20  | 4012   15   14   26   39   42  ---   13 |    24  ---   45   47   27  ---     0
 R21  | 1446   17    9   20   30   14  ---    8 |    26  ---   41   41   40  ---     0
 R22  | 1990   24   10   32   19   18  ---   12 |    18  ---   54   38   22  ---     0
 R23  | 1653   20    8   14   31   27  169   10 |    30  ---   18   47   29   15     0
 R24  | 1158   13    6   19   27   12  ---    7 |    21  ---   32   37   26  ---     0
------+-----------------------------------------+-------------------------------------
 RMS  | 2424   21   13   28   34   29  247      |T   33  ---   49   49   39   37   ---
 WRMS | 2424   21   11   26   33   29  247      |NE  33  ---   49   49   39   37   ---
 MEDI | 1446   20   11   27   33   22  169      |MD  23  ---   41   47   28   32   ---

Table 3.1614.6  GPS week: 1614   Day: 6   MJD: 55548                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 2303   29   15   18   27   39  ---   14 |    34  ---   16   31   35  ---     0
 R02  | 1401   33   29   24   39   39  ---   18 |    62  ---   71   56   70  ---     0
 R05  |  658   24   15   27   45   34  ---   14 |   115  ---  125  149  135  ---     0
 R06  | 1206   46   21   34   32   31  ---   18 |    81  ---   57   52   69  ---     0
 R07  | 3981   32   11   43   32   27  ---   16 |    45  ---   56   55   70  ---     0
 R08  | 2897   22   12   35   40   19  274   12 |    41  ---   51   45   41   56     0
 R09  | 1327   16   13   40   45   24  ---   13 |    27  ---   50   47   37  ---     0
 R10  | 4645   25   14   22   28   13  ---   10 |    23  ---   28   30   31  ---     0
 R11  | 2536   28   22   31   27   22  144   15 |    23  ---   53   46   51   24     0
 R12  | 1379   20    5   22   21   17  ---    9 |    18  ---   35   32   26  ---     0
 R13  | 1345    9    5   16   20   22  ---    7 |    21  ---   25   31   31  ---     0
 R15  | 1887   18   12   14   29   26   81   10 |    24  ---   27   34   24   38     0
 R16  |  705   16   16   20   24   25  ---   11 |    25  ---   39   33   26  ---     0
XR17  | ----  ---    4  ---  ---  ---  ---    0 |   ---  ---  ---  ---  ---  ---     0
 R18  | 1538   18   11   23   25   22  457   10 |    35  ---   58   59   55   87     0
 R19  | 3563   15   11   17   28   12  ---    7 |    46  ---   73   65   55  ---     0
 R20  | 2795   31   14   28   54   34  ---   15 |    27  ---   65   83   55  ---     0
 R21  |  994   20    9   36   34   31  ---   13 |    39  ---   75   65   39  ---     0
 R22  | 1753   16   12   21   22   22  ---   10 |    37  ---   56   43   38  ---     0
 R23  | 2490   19    7   15   36   17  229    8 |    34  ---   48   56   34   26     0
 R24  | 2134   26   11   26   38   17  ---   11 |    18  ---   57   66   36  ---     0
------+-----------------------------------------+-------------------------------------
 RMS  | 2330   25   14   27   34   26  270      |T   38  ---   53   53   47   46   ---
 WRMS | 2330   23   12   24   27   26  270      |NE  38  ---   53   53   47   46   ---
 MEDI | 1753   20   12   23   29   22  229      |MD  34  ---   53   47   38   38   ---




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