[IGSREPORT-20758] Wk 1682 IGLOS Final Orbits

IGS ACC igs.acc at noaa.gov
Thu Apr 19 08:50:07 PDT 2012


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1682   (Apr 01, 2012 - Apr 07, 2012) 
                                                                               
Contact: J. Griffiths (jake.griffiths at noaa.gov)            
         K. Choi (kevin.choi 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
center's 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 2.1682.
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:
                                                                               
 igl1682[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1682 in the SP3 format.
 igl16827.sum      Combination Report for GPS Week 1682.


    
    
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. The grg orbits are introduced for the first time
    starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
    22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
    21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
    for the first time starting 11-Sep-2011 (GPS Week 1653).

 3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
    BKG, ESA, and CODE referred their GLONASS orbit products to the following
    satellite antenna offset (SAO) values (expressed in the spacecraft body
    frame):
    
      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.
    
    Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
    (GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
    (IGSMAIL #5438). The antenna phase center offsets and phase center variations
    are given in the file:
        ftp://igs.org/igscb/station/general/igs05.atx
    These antenna calibrations are also used in the homogeneously reprocessed IGS
    products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
    Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
    model is updated (IGSMAIL #6255 & #6374) as given in the file:
        ftp://igs.org/igscb/station/general/igs08.atx
    

 4. The satellite clock values in the combined orbit files are taken from the
    broadcast files. The following gps/glonass time offsets were added to the
    broadcast clocks. Before GPS Week 1637, the time offsets were derived
    from the bkg summary files; starting Week 1637 the offsets are derived
    from the gfz summary files.
    
               Day | applied clock offset
               ----+---------------------
                0  |    165.2 ns
                1  |    164.0 ns
                2  |    166.1 ns
                3  |    164.1 ns
                4  |    164.7 ns
                5  |    170.8 ns
                6  |    166.4 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 1.1682, 1a.1682).
        
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 2.1682.0-6)                                                                                
    
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 3.1682.0-6). 
        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 1682 summary.                      (Apr 01, 2012 - Apr 07, 2012)

Table 1.1682.a     GPS week : 1682   MJD: 56018.0-56024.0

         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]
--------+----------------------------------------------------+------------------------------
cod  258|   -1     1    -4    65    -8  -111  -.27   34   33 |     ---     ---    ---    ---
        |    1     2     3    31    35    45   .03           |     ---     ---
emx  138|    1     0    -5   -42   -52    17  -.30   32   31 |  165706    -169   4415   7434
        |    2     1     2    29    10    50   .05           |    1501    3464
esx  173|    0    -1     2     0    19   -28   .33   18   17 |  165951    -214   4252   4453
        |    1     1     2    24    18    18   .04           |    1472    4295
gfz  192|    0    -1     0   -18    14    15  -.30   21   18 |       0    -929   4414   7431
        |    1     1     2    24    36    14   .04           |       0    3920
grg  124|   -1     3     2    42   -57   104   .12   39   34 |  162533    -742   4418  39768
        |    1     3     3    30    38    43   .07           |   48491    4141
iac  n/a|    1     1     2    -9    28    18   .12   24   24 |  167688    -908   4424   8092
        |    0     1     6    19    30    35   .05           |    2480    2138
mcc  n/a|    2    -5    12   -23   -22   798   .44  177  177 |     ---     ---    ---    ---
        |    7     8    13   124    94   824   .35           |     ---     ---


Table 1.1682.b     GPS week : 1682   MJD: 56018.0-56024.0   

         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   10    8   11   11 |
 R02  |   10   11   11    8   13   10    9 |
 R03  |   15   14   12   13   10   10   11 |
 R04  |   12   12   11   11    9    8   10 |
 R05  |   12   11   11   13   12   11   12 |
 R06  |   10    9   12   12   28   14   10 |
 R07  |   10    9    9   12   13   13   14 |
 R08  |   13   10   10    9   11   11   14 |
 R09  |   10    9    9   10    9   12   12 |
 R10  |    8    8   11   11   11    7    9 |
 R11  |   19   17   19   17   25   19   18 |
 R12  |    9    9    8    9   13   13    9 |
 R13  |    9    8    8    8   10   13   11 |
 R14  |   18   11   15   15   10   12   14 |
 R15  |   11   12   12   11   12   10   15 |
 R16  |   12    9   10    9   10   12   12 |
 R17  |   11   11   13   11    9   11   10 |
 R18  |    9    8   12   10   11   10   14 |
 R19  |   10   10    9   10   10    9   11 |
 R20  |   24   16   15   16   23   19   19 |
 R21  |   12   16   16   16   14   14   16 |
 R22  |   10    9    9   10   10   10   11 |
 R23  |   10   11    8    9   11    9    9 |
 R24  |   11   10   10    9    9   12   12 |
 R26  |    0    0    0    0    0    0    0 |


Table 1.1682.c     GPS week : 1682   MJD: 56018.0-56024.0   

         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 1682 0   |   49   136   135   -1495    -259   -4991  85.1  1788  1788 |  165201       0
brd 1682 1   |  -32    44    36    -928    1292     234  84.7  1998  1998 |  163985       0
brd 1682 2   |  -92   -69   171    -702    -222   -5710  83.5  2495  2495 |  166085       0
brd 1682 3   |  -78    75    64    -134   -1846   -1977  83.6  2492  2492 |  164136       0
brd 1682 4   |  -40    -7    96     180   -1254   -1113  84.0  1998  1998 |  164704       0
brd 1682 5   |  -47    -4    86    -395   -1936    -303  82.2  2044  2044 |  170809       0
brd 1682 6   |  -41   -39   159    -742   -3239   -1640  84.9  1661  1661 |  166366       0
-------------+------------------------------------------------------------+----------------
brd 1682 mean|  -40    19   107    -602   -1066   -2214  84.0  2068  2068 |  165898       0
brd 1682 sdev|   45    70    50     548    1474    2279   1.0   320   320 |    2346       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 2.1682.0  GPS week: 1682   Day: 0   MJD: 56018                            

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]
--------+----------------------------------------------------+------------------------------
cod  258|    0    -1     0    88    41  -100  -.21   33   34 |     ---     ---    ---    ---
emx  138|    0    -2    -1   -66   -51    33  -.29   33   27 |  165008     412   3841   6989
esx  173|    1    -1     1    10    11    -6   .41   21   19 |  166065   -2055   3851   4106
gfz  192|    0    -1     0   -61   -41    32  -.36   22   19 |       0   -1026   3838   7213
grg  124|   -2     3     3    47     2    60   .12   38   38 |  157155    -214   3841  29414
iac  n/a|    0     0    -3    10    51   -14   .11   23   23 |  167110    -261   3872   8321
mcc  n/a|   -1    -4    21   125    57   459   .84  130  130 |     ---     ---    ---    ---

Table 2.1682.1  GPS week: 1682   Day: 1   MJD: 56019                            

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]
--------+----------------------------------------------------+------------------------------
cod  258|   -3     0    -1    93   -24   -80  -.29   34   33 |     ---     ---    ---    ---
emx  138|    0     0    -5   -42   -43   110  -.22   31   33 |  165630   -3283   5404   9600
esx  173|   -1     0     6    29     6   -18   .33   16   15 |  163924    -646   4429   4726
gfz  192|    2    -1    -1   -35    14     6  -.30   18   17 |       0   -3292   5389   9290
grg  124|    0     3     3    17   -94    29   .09   34   30 |  139563   -4044   5384  21654
iac  n/a|    0     2    -4   -10    66   -16   .14   24   24 |  164962   -1932   5394   9727
mcc  n/a|    7    -4    19   -15   -54  1081   .26  152  152 |     ---     ---    ---    ---

Table 2.1682.2  GPS week: 1682   Day: 2   MJD: 56020                            

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]
--------+----------------------------------------------------+------------------------------
cod  258|   -1     4    -3   100     0  -163  -.26   33   34 |     ---     ---    ---    ---
emx  138|    2     0    -3   -19   -56    -6  -.30   28   29 |  164719    2102   4677   6868
esx  173|    1    -1     1   -11    20   -10   .33   20   18 |  165817    1381   4479   4643
gfz  192|    0    -2     4   -29    11    -7  -.29   19   16 |       0    2934   4670   6823
grg  124|    0     4     3    30   -63   104   .18   35   34 |  122388    3619   4758  14442
iac  n/a|    0     1    -4   -10    44    36   .19   22   22 |  166258    1226   4667   7445
mcc  n/a|   -8   -16    15  -169   -36  1458   .75  205  205 |     ---     ---    ---    ---

Table 2.1682.3  GPS week: 1682   Day: 3   MJD: 56021                            

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]
--------+----------------------------------------------------+------------------------------
cod  258|   -2     0    -5    73    11  -109  -.30   33   33 |     ---     ---    ---    ---
emx  138|   -3     0    -6   -42   -47    10  -.36   30   30 |  164561   -1458   3984   6708
esx  173|    0     0     3     7    57   -49   .30   16   15 |  164959   -2007   3995   4159
gfz  192|    0    -3    -2     2    20    21  -.29   22   16 |       0   -2804   4002   6712
grg  124|   -1     6     6    27  -105   143   .05   35   32 |  141311   -1687   3929  27559
iac  n/a|    0     3     1    -8   -21    16   .15   23   23 |  166752   -1160   3994   7377
mcc  n/a|   13   -10    -1  -201   114   649   .05  189  189 |     ---     ---    ---    ---

Table 2.1682.4  GPS week: 1682   Day: 4   MJD: 56022                            

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]
--------+----------------------------------------------------+------------------------------
cod  258|   -1     4    -2    33     4   -71  -.24   34   34 |     ---     ---    ---    ---
emx  138|    0     1    -7   -71   -38    38  -.34   35   34 |  164378    -687   4463   7662
esx  173|    0     0     0   -39    28   -32   .29   19   16 |  165521   -1337   4444   4607
gfz  192|   -2     0     1     9    -6     5  -.24   23   21 |       0   -2543   4437   7693
grg  124|   -3    -2     1    66   -66   135   .25   47   37 |  142761   -1991   4469  20691
iac  n/a|    2     0     8    17    10    29   .06   31   31 |  166538   -2170   4457   8150
mcc  n/a|    7     8     8     9  -179   107   .03  181  181 |     ---     ---    ---    ---

Table 2.1682.5  GPS week: 1682   Day: 5   MJD: 56023                            

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]
--------+----------------------------------------------------+------------------------------
cod  258|   -2     2    -8    45   -73  -186  -.29   34   33 |     ---     ---    ---    ---
emx  138|    2     3    -6   -66   -58   -32  -.33   34   29 |  167828    6001   3971   6580
esx  173|   -1    -2     0   -15     4   -54   .32   18   18 |  166776    8425   3994   4195
gfz  192|   -1     0     2    -2    79    21  -.30   22   20 |       0    5742   4008   6615
grg  124|   -1     0    -3    95   -57   119   .09   35   31 |  267801    5478   3999 140253
iac  n/a|    1     1    11   -37     8    82   .07   24   24 |  171999    2109   4010   7125
mcc  n/a|    5    -1    31   -24   -59  -291   .76  196  196 |     ---     ---    ---    ---

Table 2.1682.6  GPS week: 1682   Day: 6   MJD: 56024                            

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]
--------+----------------------------------------------------+------------------------------
cod  258|    0    -1    -7    23   -17   -70  -.27   34   33 |     ---     ---    ---    ---
emx  138|    4     1   -10     8   -70   -33  -.25   34   33 |  167824   -4271   4567   7633
esx  173|    1    -2     3    23     7   -26   .36   18   18 |  168601   -5264   4575   4741
gfz  192|   -1     0     0   -14    23    26  -.35   23   20 |       0   -5520   4555   7674
grg  124|   -3     8     1    10   -18   137   .04   46   36 |  166753   -6361   4548  24363
iac  n/a|    1     0     7   -26    42    -7   .13   23   23 |  170201   -4171   4577   8501
mcc  n/a|   -3   -10    -5   109     2  2127   .39  187  187 |     ---     ---    ---    ---

       
       
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 3.1682.0  GPS week: 1682   Day: 0   MJD: 56018                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1994   22   20   11   18   44   17  ---    9 |    56   57   58   66   76   61  ---    59
 R02  |  960   21   22   14   15   48   11  ---    9 |    65   51   42   54   55   52  ---    48
 R03  |  684   40   16   17   24   73   24  ---   14 |    88   65   67   70   69   73  ---    67
 R04  |  543   48   22   15   23   30   17  ---   11 |    79   53   43   47   41   38  ---    45
 R05  | 2618   43   24   18   15   35   23  237   11 |    83   61   49   53   50   44   58    51
 R06  | 2227   30   18   17   14   29   22  ---    9 |   107  101  103   98   94   95  ---    98
 R07  | 1965   34   15   21   14   35   14  ---    9 |    74   58   41   53   41   58  ---    51
 R08  | 1626   28   31   22   22   44   27   84   12 |    63   51   46   46   40   55   52    45
 R09E | 1181   19   23   23   16   30   19  ---    9 |    43   46   46   41   44   43  ---    40
 R10E | 1361   20   16   11   12   30   16  ---    7 |    35   33   38   40   40   32  ---    34
 R11E | 3062   59   57   39   33   50   28   70   19 |    42   39   73   62   76   49   26    52
 R12E |  608   11   17   11   20   29   27  ---    9 |    51   48   47   53   53   57  ---    49
 R13E | 2238   19   19   16   18   25   22  ---    9 |    21   37   36   36   29   26  ---    28
 R14E | 2897   33   39   30   58   44   30  ---   18 |    47   63   47   77   61   38  ---    49
 R15E | 1932   28   22   21   26   26   22  132   10 |    27   32   35   48   44   38   89    32
 R16E | 1642   18   29   20   22   38   27  ---   11 |    22   33   31   29   42   26  ---    23
 R17  | 1670   29   20   23   13   32   30  103   11 |    59   58   72   63   58   34   24    56
 R18  | 2491   33   22   12   18   21   21   77    9 |    52   37   41   35   44   30   51    36
 R19  | 1382   33   17   23   23   21   14  ---    9 |    50   41   41   45   28   24  ---    34
 R20  | 2183   47  107   35   20   35   37  ---   23 |    53   38   44   48   27   35  ---    35
 R21  | 1221   46   21   18   16   51   16  ---   12 |    74   39   28   44   27   33  ---    33
 R22  | 1306   32   27   25   13   15   21  ---   10 |    52   52   29   41   29   31  ---    34
 R23  |  590   23   23   14   18   39   22  ---   10 |    37   18   22   34   25   33  ---    22
 R24  |  828   25   23   21   17   44   15  ---   10 |    40   26   32   36   47   29  ---    30
XR26  | ----  ---  ---  ---  ---  ---    4  ---    0 |   ---  ---  ---  ---  ---  120  ---   121
------+----------------------------------------------+------------------------------------------
 RMS  | 1788   33   33   21   22   38   23  130      |T   55   47   46   50   47   46   50    46
 WRMS | 1788   34   27   19   19   38   23  130      |NE  64   50   47   52   46   49   46    50
 MEDI | 1626   29   22   18   18   35   22   84      |MD  52   46   42   47   44   38   51    45

Table 3.1682.1  GPS week: 1682   Day: 1   MJD: 56019                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 2027   13   17   19   14   22   22  ---    8 |    38   32   40   41   43   47  ---    36
 R02  |  826   28   19   17   14   53   12  ---   10 |    45   41   29   42   60   34  ---    34
 R03  |  782   46   24   10   10   68   26  ---   13 |    78   62   63   68   82   53  ---    60
 R04  |  680   44   26   13   23   46   19  ---   12 |    61   51   33   40   51   33  ---    37
 R05  | 2124   53   21    8   19   31   20  268   10 |    52   43   29   32   32   22   42    28
 R06  | 1616   29   30   15   11   22   18  ---    9 |    81   85   82   72   80   80  ---    77
 R07  | 1498   37   21    9   11   29   17  ---    8 |    63   48   48   46   50   37  ---    45
 R08  | 1560   31   29   11   11   41   23  102   10 |    51   49   42   51   31   51   75    42
 R09E | 1142   22   25   12   16   19   27  ---    8 |    32   44   56   57   51   56  ---    49
 R10E | 1610   36   19   12   13   22   14  ---    8 |    29   35   34   46   42   30  ---    33
 R11E | 3592   47   67   23   24   38   31   88   16 |    25   35   66   70   70   45   34    51
 R12E |  672   22   24   11   15   21   26  ---    8 |    37   36   37   43   31   33  ---    33
 R13E | 2122   14   21   11   14   28   14  ---    7 |    18   27   26   25   32   23  ---    19
 R14E | 4801   21   35   18   20   31   24  ---   10 |    60   74   77   80   79   66  ---    71
 R15E | 3041   26   33   12   29   35   26  160   11 |    38   39   42   51   61   40   76    39
 R16E | 2184   23   29   12   15   28   21  ---    9 |    33   37   31   31   42   27  ---    26
 R17  | 1532   19   15   11   31   22   35  127   10 |    40   45   34   56   60   24   49    38
 R18  | 1825   26   17   15   13   13   22   86    7 |    42   45   54   49   45   34   96    45
 R19  |  854   39   26   14   11   17   33  ---   10 |    39   26   27   23   19   26  ---    17
 R20  | 2871   49   73   22   12   40   21  ---   16 |    40   36   31   28   21   30  ---    25
 R21  | 1443   63   28   29   27   50   25  ---   15 |    46   33   40   36   34   40  ---    27
 R22  |  922   22   21   17   17   16   25  ---    8 |    39   32   31   38   28   29  ---    29
 R23  | 1104   30   25   24   16   33   26  ---   11 |    26   24   21   21   42   24  ---    14
 R24  |  720   19   26   11   21   27   24  ---    9 |    36   31   40   52   41   29  ---    37
XR26  | ----  ---  ---  ---  ---  ---    5  ---    0 |   ---  ---  ---  ---  ---  102  ---   103
------+----------------------------------------------+------------------------------------------
 RMS  | 1998   34   31   16   18   34   24  152      |T   43   42   42   45   46   40   62    40
 WRMS | 1998   33   33   15   17   30   24  152      |NE  48   42   40   43   44   40   65    40
 MEDI | 1532   28   25   12   15   28   23  102      |MD  39   37   37   43   42   34   49    37

Table 3.1682.2  GPS week: 1682   Day: 2   MJD: 56020                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1968   19   22   20   22   16   20  ---    9 |    47   63   52   60   61   58  ---    55
 R02  | 1425   31   27   11   20   47   20  ---   11 |    49   48   35   32   37   37  ---    30
 R03  | 1205   35   22   16   17   50   25  ---   11 |    79   60   57   68   69   46  ---    56
 R04  |  825   38   19   13   19   46   15  ---   10 |    61   44   46   58   45   34  ---    42
 R05  | 1230   47   11   22   14   36   19  280   11 |    68   41   48   46   57   55   44    48
 R06  |  993   32   23   13   22   48   23  ---   11 |   143  131  157  143  171  150  ---   147
 R07  | 1459   31   18   17   13   32   14  ---    8 |    65   57   47   52   41   43  ---    47
 R08  | 1553   29   13   12   14   44   18  102    9 |    60   50   44   54   33   44   74    45
 R09E |  987   16   22   13   15   30   20  ---    8 |    41   40   46   44   60   45  ---    41
 R10E | 2296   18   36   19   23   20   22  ---   10 |    38   33   52   53   47   31  ---    40
 R11E | 2593   48   60   43   29   46   31  116   19 |    48   49   95   83   71   48   31    63
 R12E | 2097   26   18   14   12   22   18  ---    7 |    39   42   36   41   40   28  ---    32
 R13E | 1758   18   20   13   10   23   20  ---    7 |    24   25   30   31   39   26  ---    25
 R14E | 4342   42   31   28   39   37   30  ---   15 |    50   75   68   81   65   56  ---    60
 R15E | 7893   19   42   17   22   33   20  287   11 |    35   22   33   37   47   36   75    29
 R16E | 1367   17   27   19   18   37   21  ---   10 |    26   36   26   35   36   26  ---    25
XR17  | 1823   30   24   21   22  ---   29  121   12 |    55   49   51   56  ---   36   54    46
 R18  | 2015   28   25    9   18   23   41  164   11 |    44   43   33   41   49   24   93    34
 R19  | 1130   27   21   13   18   31   17  ---    9 |    47   42   48   55   33   41  ---    43
 R20  | 3819   43   55   18   20   40   19  ---   14 |    51   37   39   54   30   36  ---    38
 R21  | 1005   67   27   41   19   35   24  ---   16 |    64   31   49   55   55   39  ---    39
 R22  |  802   21   18    8   18   23   26  ---    8 |    44   40   41   51   48   24  ---    38
 R23  | 1445   28   12   12    7   28   18  ---    7 |    35   28   35   33   32   31  ---    29
 R24  |  940   27   20   22   15   29   18  ---    9 |    38   37   28   41   57   23  ---    32
XR26  | ----  ---  ---  ---  ---  ---    4  ---    0 |   ---  ---  ---  ---  ---  117  ---   118
------+----------------------------------------------+------------------------------------------
 RMS  | 2494   33   28   20   19   35   22  205      |T   52   46   49   54   53   45   61    48
 WRMS | 2494   34   29   18   16   34   22  205      |NE  59   50   50   56   54   49   66    52
 MEDI | 1445   28   22   16   18   33   20  121      |MD  47   42   46   52   47   37   54    41

Table 3.1682.3  GPS week: 1682   Day: 3   MJD: 56021                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1386   20   22   10   34   31   17  ---   10 |    55   70   57   60   51   52  ---    55
 R02  | 2368   28   16   17   17   20   13  ---    8 |    64   60   50   56   60   54  ---    53
 R03  | 1013   39   32   21   20   41   22  ---   12 |    73   73   62   46   40   51  ---    54
 R04  |  708   38   28   14   19   37   22  ---   11 |    68   43   52   59   63   36  ---    48
 R05  | 1471   46   14   10   18   59   22  293   12 |    64   47   40   44   67   48   21    44
 R06  |  927   23   23   22   23   51   10  ---   11 |   130  135  125  120  169  132  ---   130
 R07  | 1436   38   25   27   25   29   18  ---   12 |    71   57   57   52   52   46  ---    50
 R08  |  619   34   11    9   14   23   21  104    8 |    57   47   45   43   38   30   49    39
 R09E |  860   15   21   14   20   43   18  ---    9 |    22   31   35   36   54   35  ---    30
 R10E | 2895   17   24   17   29   42   20  ---   11 |    27   37   38   49   49   30  ---    33
 R11E | 1882   52   45   25   39   33   40  173   17 |    39   53   77   89   87   50   32    61
 R12E | 2348   26   21   12   17   35   13  ---    9 |    57   50   36   53   63   50  ---    45
 R13E | 1735   23   27    9   12   21   15  ---    7 |    21   31   28   30   32   21  ---    23
 R14E | 2671   17   37   23   34   45   39  ---   14 |    51   56   70   77   66   27  ---    52
 R15E | 8887   20   36   16   16   31   24  250   10 |    38   48   42   44   41   40   94    37
 R16E | 1472   19   24   14   15   25   21  ---    8 |    34   32   34   39   40   26  ---    29
 R17  | 1600   26   34   16   21   22   28  100   10 |    45   62   58   61   62   32   29    51
 R18  | 1862   28   27    8   14   30   28  123    9 |    48   55   49   48   37   43   58    44
 R19  | 1146   23   21    9   16   45   16  ---    9 |    45   57   51   52   51   45  ---    47
 R20  | 3879   43   75   10   20   29   28  ---   16 |    50   25   36   38   41   20  ---    30
 R21  |  651   67   40   18   28   26   38  ---   16 |    69   34   33   42   51   25  ---    28
 R22  |  788   34   22   19   11   26   16  ---    9 |    57   57   46   53   36   55  ---    47
 R23  |  912   21   16    8   18   30   23  ---    8 |    33   29   32   30   21   39  ---    27
 R24  |  896   32   16   14   17   20   15  ---    8 |    49   27   47   42   38   36  ---    37
XR26  | ----  ---  ---  ---  ---  ---    3  ---    0 |   ---  ---  ---  ---  ---  215  ---   215
------+----------------------------------------------+------------------------------------------
 RMS  | 2492   33   30   16   22   35   23  189      |T   52   50   50   52   54   49   47    52
 WRMS | 2492   33   30   15   16   32   23  189      |NE  61   54   52   52   54   56   39    58
 MEDI | 1436   26   24   14   18   30   21  123      |MD  50   48   46   48   51   40   32    45

Table 3.1682.4  GPS week: 1682   Day: 4   MJD: 56022                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1072   11   17   10   22   23   18  ---    7 |    44   56   50   54   38   48  ---    47
 R02  | 2206   31   20   19   25   67   22  ---   13 |    61   44   58   64   35   38  ---    46
 R03  | 1150   35   18   16   16   31   16  ---    9 |    66   57   49   43   49   45  ---    47
 R04  |  646   31   19   11   15   23   22  ---    8 |    55   35   41   34   51   26  ---    36
 R05  | 1419   38   16    7   25   59   22  297   12 |    57   40   38   46   74   33   20    39
 R06  | 1127   43   33   32   42  127   88  ---   27 |   360  360  363  363  393  330  ---   355
 R07  | 1656   45   33   20   19   49   22  ---   13 |    60   53   39   40   33   44  ---    38
 R08  | 1946   42   21   14   15   32   20  101   10 |    49   42   33   27   36   21   55    28
 R09E |  763   16   22   13   16   27   29  ---    9 |    29   34   34   42   59   31  ---    32
 R10E | 2062   24   19   15   15   51   22  ---   10 |    28   38   38   43   66   32  ---    35
 R11E | 2606   53   86   44   41   77   24  177   24 |    55   51   99  100   90   61   34    70
 R12E | 1587   19   32   20   23   50   29  ---   12 |    46   39   40   47   55   35  ---    35
 R13E | 1668   31   21   15   21   26   27  ---   10 |    39   43   33   41   50   31  ---    33
 R14E | 2612   22   18   17   20   34   27  ---   10 |    40   42   36   44   33   34  ---    32
 R15E | 4929   29   38   18   22   21   31  232   12 |    31   42   40   50   48   29  108    36
 R16E | 1625   30   24   16   14   25   28  ---   10 |    26   31   28   36   35   27  ---    25
 R17  |  851   20   13   20   12   42   16   82    9 |    60   42   48   48   44   42   33    45
 R18  | 2428   28   16   21   23   35   22   78   10 |    36   37   26   40   32   32   49    26
 R19  | 1145   15   13   11   30   42   13  ---    9 |    42   39   40   68   25   51  ---    44
 R20  | 4163   39  101   10   27   29   59  ---   22 |    46   35   38   51   28   46  ---    34
 R21  |  728   57   31   15   25   35   30  ---   14 |    77   47   63   61   57   43  ---    53
 R22  |  714   45   21   11   11   29   20  ---   10 |    55   39   26   32   36   27  ---    29
 R23  |  728   37   22   21   21   25   16  ---   10 |    38   30   40   49   52   40  ---    36
 R24  |  849   27   21   13   12   32   19  ---    8 |    35   26   35   36   28   30  ---    27
XR26  | ----  ---  ---  ---  ---  ---    5  ---    0 |   ---  ---  ---  ---  ---  125  ---   125
------+----------------------------------------------+------------------------------------------
 RMS  | 1998   34   35   19   23   47   31  181      |T   59   54   55   60   60   52   49    54
 WRMS | 1998   34   34   16   21   37   31  181      |NE  71   61   61   66   63   60   39    62
 MEDI | 1419   31   21   15   21   32   22  101      |MD  46   40   39   44   44   35   34    36

Table 3.1682.5  GPS week: 1682   Day: 5   MJD: 56023                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  935   13   46   17   17   27   26  ---   11 |    32   54   27   31   29   39  ---    31
 R02  | 2475   27   24   10   22   32   17  ---    9 |    40   34   31   31   42   33  ---    29
 R03  | 1057   30   19   12   26   30   22  ---   10 |    49   45   38   36   50   33  ---    35
 R04  |  774   28   11   14   16   19   22  ---    8 |    52   38   46   48   50   36  ---    42
 R05  | 1392   42   21   13   25   25   20  292   10 |    46   37   35   37   37   32   32    32
 R06  | 1055   42   18   18   24   59   30  ---   14 |   228  215  226  216  206  233  ---   221
 R07  | 2147   40   24   18   17   56   15  ---   12 |    51   55   33   37   60   30  ---    33
 R08  | 2288   45   18   18   17   38   14  207   11 |    42   36   29   36   37   30  141    26
 R09E | 1073   18   37   17   23   41   25  ---   12 |    23   35   43   47   57   45  ---    37
 R10E | 2590    9   14    9   16   26   17  ---    7 |    22   29   41   35   47   24  ---    29
 R11E | 2748   46   64   24   26   58   40  197   18 |    36   40   68   67   78   41   37    50
 R12E |  948   22   36   28   18   38   29  ---   12 |    69   50   64   66   55   47  ---    55
 R13E | 3801   27   33   17   32   29   31  ---   12 |    50   74   62   70   49   33  ---    53
 R14E | 4054   33   32   26   16   29   24  ---   11 |    34   28   43   39   43   29  ---    29
 R15E | 3893   21   39   15   16   29   21  216   10 |    36   38   37   40   35   39  132    33
 R16E |  922   31   24   18   27   33   29  ---   12 |    49   35   49   55   66   28  ---    41
 R17  | 1277   31   18   14   15   56   13   61   11 |    41   27   35   37   40   40   27    30
 R18  | 1803   15   26   15   20   33   25  113   10 |    30   37   39   47   18   64   60    38
 R19  |  627   16   17   19   25   16   15  ---    8 |    38   46   34   41   40   45  ---    37
 R20  | 2932   60   84   25   23   27   34  ---   19 |    43   25   45   50   42   42  ---    36
 R21  |  499   64   37   15   31   18   22  ---   14 |    67   42   48   53   55   39  ---    45
 R22  |  635   38   23   15   17   26   17  ---    9 |    51   29   46   44   30   42  ---    38
 R23  |  791   33   28   14   17   14   14  ---    8 |    41   36   35   51   41   35  ---    36
 R24  |  496   34   18   28   19   27   29  ---   11 |    38   27   36   37   32   43  ---    27
XR26  | ----  ---  ---  ---  ---  ---    8  ---    0 |   ---  ---  ---  ---  ---  104  ---   103
------+----------------------------------------------+------------------------------------------
 RMS  | 2043   34   34   18   22   35   24  196      |T   50   46   49   52   51   48   71    46
 WRMS | 2043   33   29   18   20   31   24  196      |NE  55   48   48   52   50   54   65    49
 MEDI | 1073   31   24   17   19   29   22  197      |MD  41   37   39   41   42   39   37    36

Table 3.1682.6  GPS week: 1682   Day: 6   MJD: 56024                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  834   16   38   18   25   31   18  ---   10 |    50   74   43   50   45   47  ---    47
 R02  | 2389   26   18   16   22   28   19  ---    9 |    50   34   30   31   33   38  ---    32
 R03  | 1339   39   24   21   23   20   24  ---   11 |    69   49   42   42   42   45  ---    42
 R04  | 1302   36   13   19   18   25   23  ---   10 |    63   46   41   44   45   28  ---    39
 R05  | 1427   41   26   18   24   45   17  ---   12 |    70   54   49   53   43   39  ---    46
 R06  | 1074   32   24   14   23   29   17  ---    9 |   227  217  223  221  231  221  ---   222
 R07  | 2222   41   34   21   21   53   24  ---   13 |    67   58   58   46   58   49  ---    49
 R08  | 1360   44   20   19   21   68   20  143   13 |    64   43   33   43   53   33   81    36
 R09E |  779   28   38   16   23   35   25  ---   11 |    21   33   46   44   54   36  ---    35
 R10E | 1408   22   34    9   17   31   19  ---    9 |    22   26   25   32   35   25  ---    22
 R11E | 1510   50   64   23   35   61   30  118   18 |    28   36   71   78   73   46   54    52
 R12E | 1663   19   30   11   20   31   18  ---    9 |    72   57   74   69   81   68  ---    68
 R13E | 1418   22   35   17   19   41   19  ---   10 |    41   59   48   50   42   35  ---    41
 R14E | 1964   23   31   19   19   75   20  ---   13 |    41   41   38   52   88   44  ---    41
 R15E | 3775   28   38   20   26   71   24  292   14 |    34   35   34   45   66   32  244    32
 R16E |  552   48   27   13   18   37   21  ---   11 |    38   35   32   44   45   30  ---    32
 R17  | 1408   41   23   11   17   22   20  143    9 |    68   61   56   57   52   54   45    55
 R18  | 3135   29   25   13   27   74   21  ---   13 |    50   41   43   38   34   48  ---    36
 R19  | 1531   14   24   13   32   39   21  ---   10 |    54   56   51   57   44   45  ---    50
 R20  | 1059   31   68   37   31   56   37  ---   19 |    55   38   33   52   27   53  ---    38
 R21  | 1247   67   36   17   21   69   18  ---   16 |    92   39   43   57   45   49  ---    47
 R22  |  693   32   36   14   21   22   24  ---   10 |    67   50   61   55   56   49  ---    54
 R23  |  831   20   18   19   17   16   24  ---    9 |    47   31   45   29   36   32  ---    32
 R24  |  540   26   34   20   20   39   30  ---   12 |    46   28   45   31   41   31  ---    31
XR26  | ----  ---  ---  ---  ---  ---    5  ---    0 |   ---  ---  ---  ---  ---  167  ---   167
------+----------------------------------------------+------------------------------------------
 RMS  | 1661   34   34   18   23   46   23  187      |T   59   51   52   55   57   53  106    53
 WRMS | 1661   33   33   18   20   36   23  187      |NE  71   57   56   56   55   60   63    60
 MEDI | 1360   29   30   17   21   37   21  143      |MD  50   41   43   46   45   45   54    41




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