[IGSREPORT-20262] Wk 1657 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Oct 27 05:43:31 PDT 2011


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1657   (Oct 09, 2011 - Oct 15, 2011) 
                                                                               
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
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 2.1657.
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:
                                                                               
 igl1657[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1657 in the SP3 format.
 igl16577.sum      Combination Report for GPS Week 1657.


    
    
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  |    160.3 ns
                1  |    165.8 ns
                2  |    160.4 ns
                3  |    160.0 ns
                4  |    163.3 ns
                5  |    163.6 ns
                6  |    161.8 ns

 5. The following orbit solutions were excluded from the combination
    because they were biasing the weighted average (generally indicated
    by long arc RMS).
    
               Day | Centre | PRN list
               ----+--------+---------------
                0  |  GRG   | R03 R04
                1  |  GRG   | R03 R04
                2  |  GRG   | R03
                3  |  GRG   | R03
                4  |  GFZ   | R17
                4  |  GRG   | R17

    
         
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 1.1657, 1a.1657).
        
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 2.1657.0-6)                                                                                
    
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 3.1657.0-6). 
        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 1657 summary.                      (Oct 09, 2011 - Oct 15, 2011)

Table 1.1657.a     GPS week : 1657   MJD: 55843.0-55849.0

         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  259|    0     0    -3    30   -57    34  -.24   28   27 |     ---     ---    ---    ---
        |    1     2     3    19    28    45   .03           |     ---     ---
emx  147|    2     0    -5   -20    -8    65  -.18   33   31 |  162396   -1203   5567   9688
        |    1     2     1    43    54    82   .04           |    1854    1563
esx  125|    0     0    -3    27    53   -20   .42   20   19 |  162298    -493   5761   5933
        |    2     1     2    30    39    26   .04           |    1746    2614
gfz  200|    0     0    -6    -3   -12    66  -.22   23   21 |   49732 1427906   5320   9072
        |    2     2     3    27    51    40   .06           |  131578 3779938
grg  132|   -4     1    -4   -22    -9   -29   .19   61   49 |     ---     ---    ---    ---
        |    3     1     5    72    43    73   .12           |     ---     ---
iac  n/a|    1     0    20   -17    -7  -129  -.14   26   26 |  162921    -863   5742  10103
        |    1     1     9    32    27   100   .07           |    2114    1254
mcc  n/a|    1     3    30    -3   -20   580   .18  142  142 |     ---     ---    ---    ---
        |    4     6    13    72    87   532   .25           |     ---     ---


Table 1.1657.b     GPS week : 1657   MJD: 55843.0-55849.0   

         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  |    7    9   11   10    9   14   13 |
 R02  |    9   10   10   10   11   10    9 |
 R03  |   11   12   11   19    0  ---  --- |
 R04  |   16  138  ---  ---  ---  ---  --- |
 R05  |   12   11   10   11   10   11   10 |
 R06  |    7    9   11    9    9   12    9 |
 R07  |   22   12   13   13   15   14   12 |
 R08  |    9    9    9    9    8   11   11 |
 R09  |   11   13   10   12   12   12   11 |
 R10  |   14   10   11    9   12   12   10 |
 R11  |   22   22   18   16   21   16   18 |
 R12  |   12   11   11   11   12   10   11 |
 R13  |   12   11   14   12   12   10   12 |
 R14  |  ---  ---  ---  ---   20   17   13 |
 R15  |   11   10   12   12   10   13   11 |
 R16  |   12    9   10   10   10   16   11 |
 R17  |   15   17   13   13   96   19   13 |
 R18  |   10   12   14   14   13   14    9 |
 R19  |   10   11   12   14   15   16   13 |
 R20  |   19   16   13   19   21   22   19 |
 R21  |   11   12   10   10   10   11   11 |
 R22  |   12   11   10   11   12   12   12 |
 R23  |   11    9   10   10   11   13   12 |
 R24  |   13   13   10   13   11   13   11 |


Table 1.1657.c     GPS week : 1657   MJD: 55843.0-55849.0   

         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 1657 0   |  -24    22    68   -2079   -1342    1873  83.8  2218  2218 |  160311       0
brd 1657 1   |    3    24   167   -1053    -194   -6718  89.9  2032  2032 |  165815       0
brd 1657 2   |  103    78   195     970    1966  -11890  86.9  2074  2074 |  160420       0
brd 1657 3   |  -84     6    67    -237    2102   -5683  83.7  2460  2460 |  159992       0
brd 1657 4   |  -87  -121   178   -1094    -235  -11880  82.4  1974  1974 |  163306       0
brd 1657 5   |  217   -54   262    1538      97   -5675  86.2  1738  1738 |  163575       0
brd 1657 6   |   53    94   113     953     460    2948  84.7  1715  1715 |  161805       0
-------------+------------------------------------------------------------+----------------
brd 1657 mean|   25     7   150    -143     407   -5289  85.4  2030  2030 |  162174       0
brd 1657 sdev|  109    74    71    1339    1240    5894   2.5   261   261 |    2158       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 2.1657.0  GPS week: 1657   Day: 0   MJD: 55843                            

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  259|   -1     0     1    24   -51    63  -.27   29   27 |     ---     ---    ---    ---
emx  147|    2     3    -6     0    32   -22  -.20   35   27 |  161697   -3091   4853  13045
esx  125|    0     0     0    50    94   -32   .38   18   17 |  161448   -2881   4750   4939
gfz  200|    1     0     0   -13   -99    28  -.14   33   31 |       0   -3852   4722  11768
grg  132|    0     2    -8   -16   -58   -66  -.03   71   51 |     ---     ---    ---    ---
iac  n/a|    0     0     9   -45   -54   -45  -.28   24   24 |  164298   -1938   4746  11821
mcc  n/a|    7     4     4   -79  -169    99   .25  126  126 |     ---     ---    ---    ---

Table 2.1657.1  GPS week: 1657   Day: 1   MJD: 55844                            

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  259|    0     2    -8    48   -27    49  -.23   28   27 |     ---     ---    ---    ---
emx  147|    0     0    -6   -31    23   144  -.16   33   34 |  166135    -395   7024   9497
esx  125|   -1     0    -6   -24   102   -27   .46   20   20 |  165611    1143   7035   7278
gfz  200|    3    -2    -6    33   -49    64  -.19   21   17 |  348125 9999999   7100   9451
grg  132|   -5     3    -4   -85   -50    27   .28   76   47 |     ---     ---    ---    ---
iac  n/a|    1     0    24    14     3  -176  -.20   23   23 |  166009   -1834   7041   9729
mcc  n/a|    1     5    21    19   -61   348  -.28  159  159 |     ---     ---    ---    ---

Table 2.1657.2  GPS week: 1657   Day: 2   MJD: 55845                            

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  259|   -2     4    -8     7   -23   105  -.28   29   30 |     ---     ---    ---    ---
emx  147|    3    -2    -8    -4   -65   173  -.17   32   29 |  160415    -687   6329   8682
esx  125|    0    -3    -6    -2    51   -36   .43   18   18 |  160656   -1098   6310   6577
gfz  200|    2     1   -11    24   -11    39  -.21   18   18 |       0   -1890   5382   7874
grg  132|   -5     1     0   -19     2    57   .26   78   45 |     ---     ---    ---    ---
iac  n/a|    0     0    36    10     3  -220  -.13   26   26 |  160533    1648   6283   8727
mcc  n/a|   -3    10    34   119   104   254   .41  172  172 |     ---     ---    ---    ---

Table 2.1657.3  GPS week: 1657   Day: 3   MJD: 55846                            

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  259|   -1    -1    -4    21   -75    11  -.23   28   26 |     ---     ---    ---    ---
emx  147|    0     1    -5   -67    -9   126  -.21   31   32 |  161382   -3585   5087   7905
esx  125|   -3    -2    -2    41    59     6   .42   19   18 |  161459   -3944   5180   5283
gfz  200|    2     3    -6    14    -9   121  -.20   20   15 |       0   -3283   5176   7811
grg  132|    0    -1   -12   -62   -41    53   .10   54   54 |     ---     ---    ---    ---
iac  n/a|    2     0    23     5   -29  -256  -.11   24   24 |  160176   -1601   5096   8700
mcc  n/a|   -4     3    35    55   -63   188   .47  179  179 |     ---     ---    ---    ---

Table 2.1657.4  GPS week: 1657   Day: 4   MJD: 55847                            

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  259|    1    -2    -4    11   -48    43  -.27   25   26 |     ---     ---    ---    ---
emx  147|    2    -1    -5   -15   -70    24  -.10   38   39 |  162661     817   4862   8920
esx  125|    0     0     0    24    59   -26   .37   18   16 |  161295    3827   4870   4994
gfz  200|   -3    -2    -6   -22     5   125  -.32   22   21 |       0     215   4764   9185
grg  132|   -2     1    -5   100    27   -72   .23   48   46 |     ---     ---    ---    ---
iac  n/a|    3     4    14   -57    -6  -169  -.08   30   30 |  163253    -318   4889  10177
mcc  n/a|    2     0    39   -22    23   504   .15  156  156 |     ---     ---    ---    ---

Table 2.1657.5  GPS week: 1657   Day: 5   MJD: 55848                            

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  259|    0     2    -3    57   -76   -27  -.22   28   30 |     ---     ---    ---    ---
emx  147|    5    -1    -6   -75    74   -34  -.23   31   29 |  162986    -705   5721  10751
esx  125|    3     0    -6    52     5    24   .46   26   25 |  163727   -1137   6900   7056
gfz  200|    0    -2    -7   -30    10    52  -.24   26   22 |       0    3526   5937   9004
grg  132|   -8     0    -2    35    61   -77   .26   50   48 |     ---     ---    ---    ---
iac  n/a|    0     0    18     1     0   -39  -.09   27   27 |  164086   -1286   6863  11804
mcc  n/a|    5     8    46   -44    28  1242   .22   99   99 |     ---     ---    ---    ---

Table 2.1657.6  GPS week: 1657   Day: 6   MJD: 55849                            

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  259|    1    -1     0    44  -102    -7  -.20   27   27 |     ---     ---    ---    ---
emx  147|    2    -1    -3    53   -43    49  -.16   33   30 |  161501    -778   5093   9016
esx  125|    0     0    -4    49    -1   -51   .40   18   18 |  161892     633   5286   5408
gfz  200|    0    -1    -8   -32    64    36  -.26   20   19 |       0     629   4159   8415
grg  132|   -7     0     3  -108    -6  -127   .26   53   53 |     ---     ---    ---    ---
iac  n/a|    0     3    13   -53    33     3  -.10   26   26 |  162098    -712   5281   9764
mcc  n/a|    0    -8    33   -70    -5  1425   .03  104  104 |     ---     ---    ---    ---

       
       
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 3.1657.0  GPS week: 1657   Day: 0   MJD: 55843                            

        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  | 1021   17   19   13   15   24   14  ---    7 |    48   54   42   48   30   46  ---    44
 R02  | 1710   20   14   14   17   36   24  ---    8 |    51   44   50   42   34   41  ---    41
 R03E | 1222   27   32   16   16  242   24  ---   11 |    23   40   32   29  108   20  ---    24
XR04  | 1612   41  ---   21   14  241   28  ---   15 |   145  ---    5    5  185    5  ---   164
 R05  |  835   36   16   21   20   56   22  132   12 |    68   41   47   50   44   50   42    46
 R06  | 1401   20   11    8   14   29   16  ---    7 |    58   47   42   51   42   46  ---    44
 R07  | 5830   25   29   26  106   47   21  ---   22 |    43   49   33   85   55   40  ---    44
 R08  | 1560   20   21    8   22   42   15  107    8 |    50   36   39   40   38   51   43    39
 R09E |  702   17   26   20   34   36   23  ---   11 |    20   27   35   30   29   22  ---    20
 R10E | 1702   16   47   16   34   50   28  ---   13 |    36   38   38   30   52   46  ---    33
 R11E | 1124   51   80   32   35   63   47   75   22 |    31   48   79   73   45   34   43    49
 R12E | 1936   18   31   14   20   71   21  ---   12 |    30   45   38   40   64   29  ---    32
 R13E | 1645   23   26   14   19   67   30  ---   12 |    45   52   57   49   62   32  ---    44
 R15E | 3390   20   24   17   22   51   21   58   10 |    27   20   26   31   56   22   35    18
 R16E |  721   24   27   27   23   43   20  ---   11 |    30   25   38   37   50   26  ---    26
 R17  | 4714   39   27   31   33   37   35  ---   15 |   186  128  150  204  154  186  ---   185
 R18  | 2490   27   15   10   15   66   11  205   10 |    56   39   35   43   40   30  135    35
 R19  | 1166   27   22   13   19   50   13  ---   10 |    53   43   37   47   30   27  ---    37
 R20  | 2591   41   90   17   22   64   20  ---   19 |    44   52   48   58   47   28  ---    41
 R21  |  778   31   15   13   22   54   20  ---   10 |    61   36   47   53   41   29  ---    42
 R22  |  831   40   28   12   14   54   28  ---   12 |    67   45   43   44   30   34  ---    40
 R23  | 1291   29   22   18   30   35   21  ---   11 |    57   35   40   45   32   23  ---    35
 R24  | 1054   34   13   16   40   53   24  ---   12 |    45   34   48   56   45   26  ---    37
------+----------------------------------------------+------------------------------------------
 RMS  | 2218   29   35   18   33   71   24  126      |T   55   44   45   51   57   38   59    48
 WRMS | 2218   27   27   17   31   51   24  126      |NE  68   48   47   58   56   44   73    58
 MEDI | 1401   27   24   16   22   51   21  107      |MD  48   41   40   45   45   30   43    40

Table 3.1657.1  GPS week: 1657   Day: 1   MJD: 55844                            

        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  |  967   17   19   25   18   28   17  ---    9 |    43   48   45   46   38   38  ---    40
 R02  | 1000   25   23   15   13   42   26  ---   10 |    35   37   34   24   32   38  ---    26
 R03E |  844   20   39   13   21  288   24  ---   12 |    28   44   33   36   97   20  ---    29
XR04  |27773  105  ---  ---  --- 2456  157  ---  138 |    65  ---  ---  ---  131    4  ---   126
 R05  | 1668   42   15   16   12   44   22  137   11 |    63   47   48   51   38   43   30    46
 R06  | 1658   24   15   17   19   39   12  ---    9 |    41   44   32   40   62   48  ---    40
 R07  | 4758   16   22   23   32   47   20  ---   11 |    40   35   38   58   61   39  ---    37
 R08  | 1956   15   23   12   18   37   19   63    8 |    38   29   32   34   39   30   33    30
 R09E | 1019   26   30   31   15   49   22  ---   12 |    22   23   53   39   46   26  ---    28
 R10E | 2009   19   23   16   18   42   20  ---    9 |    33   29   37   24   48   30  ---    25
 R11E | 2313   56   90   22   26   60   35  122   21 |    29   68   68   60   76   40   65    46
 R12E | 1963   24   26   15   22   25   29  ---   10 |    34   46   37   43   42   36  ---    34
 R13E | 1015   16   29   16   21   36   26  ---   10 |    39   40   37   45   54   40  ---    38
 R15E | 2674   18   23   19   16   32   22   31    9 |    25   24   36   34   39   30   33    26
 R16E |  752   23   18   19   14   42   18  ---    9 |    22   24   40   34   36   32  ---    26
 R17  | 1667   38   38   22   37   78   26  ---   16 |   165  131  135  173  156  157  ---   162
 R18  | 3394   31   28   17   12   44   29  297   11 |    42   38   34   26   46   26   61    27
 R19  | 1527   32   23   24   16   39   24  ---   11 |    44   51   45   41   35   28  ---    35
 R20  | 3083   36   48   32   29   49   29  ---   16 |    41   53   35   32   39   36  ---    28
 R21  |  991   21   35   24   31   38   17  ---   12 |    48   34   58   46   43   32  ---    40
 R22  |  710   25   23   15   25   49   17  ---   10 |    40   24   38   49   39   27  ---    32
 R23  | 1639   25   17   14   14   42   12  ---    8 |    36   27   41   39   34   24  ---    30
 R24  | 1690   24   28   20   13   72   24  ---   13 |    29   27   26   25   54   15  ---    17
------+----------------------------------------------+------------------------------------------
 RMS  | 2032   28   33   20   21   76   23  159      |T   43   41   44   45   55   36   44    42
 WRMS | 2032   27   34   20   17   47   23  159      |NE  51   44   45   48   56   39   41    47
 MEDI | 1667   24   23   17   18   42   22  122      |MD  39   37   37   39   43   32   33    32

Table 3.1657.2  GPS week: 1657   Day: 2   MJD: 55845                            

        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  | 1716   20   35   14   17   38   26  ---   10 |    32   44   30   25   35   38  ---    26
 R02  |  554   27   19   21   13   34   27  ---   10 |    45   39   43   39   54   50  ---    38
 R03E | 1507   16   27   13   15  304   34  ---   11 |    24   32   29   31   98   21  ---    28
 R05  | 1243   38   18   19   12   38   16  165   10 |    59   45   45   48   58   48   29    46
 R06  | 1855   36   15   18   22   37   25  ---   11 |    46   33   33   42   50   62  ---    39
XR07  | 4158   24   19   28  ---   41   23  ---   13 |    41   28   42  ---   39   38  ---    31
 R08  | 3184   19   21   13   13   33   24   46    8 |    37   31   41   33   36   55   35    36
 R09E | 1665   19   30   15   18   31   25  ---   10 |    22   18   29   29   40   33  ---    21
 R10E | 1496   24   27   21   13   37   27  ---   10 |    37   39   39   39   56   43  ---    34
 R11E |  939   49   70   28   22   42   28  109   17 |    40   53   67   67   43   41   44    48
 R12E | 1258   26   26   25   18   36   21  ---   11 |    42   33   50   33   68   39  ---    36
 R13E |  774   23   31   20   22   51   44  ---   14 |    60   55   68   76   74   45  ---    59
 R15E | 2120   20   43   10   21   50   20   33   11 |    31   37   31   37   58   29   33    29
 R16E | 1095   20   20   14   17   38   28  ---   10 |    19   25   37   33   50   26  ---    26
 R17  | 1981   31   43   24   16   47   28  ---   13 |   250  148  191  281  171  253  ---   251
 R18  | 5695   47   23   20   27   33   32  326   13 |    48   40   45   35   60   38   77    32
 R19  | 2212   37   21   26   20   33   26  ---   12 |    49   57   50   39   24   21  ---    35
 R20  | 2333   27   44   16   16   65   23  ---   13 |    55   48   46   46   43   42  ---    40
 R21  |  722   28   23   18   19   33   14  ---    9 |    54   38   33   53   25   31  ---    37
 R22  |  570   24   30   13   15   47   17  ---   10 |    53   36   57   60   50   38  ---    47
 R23  | 1546   23   25   12   15   50   15  ---    9 |    45   31   35   41   35   16  ---    28
 R24  | 2442   26   23   10   15   49   19  ---   10 |    48   25   40   41   51   17  ---    30
------+----------------------------------------------+------------------------------------------
 RMS  | 2074   29   32   18   18   78   26  172      |T   51   42   49   53   55   46   43    45
 WRMS | 2074   30   29   18   18   45   26  172      |NE  61   45   52   60   52   53   47    51
 MEDI | 1546   24   25   18   17   38   25  109      |MD  45   37   41   39   50   38   35    35

Table 3.1657.3  GPS week: 1657   Day: 3   MJD: 55846                            

        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  | 2100   19   20   17   13   61   18  ---    9 |    56   49   57   57   68   57  ---    53
 R02  |  908   24   24   11   22   46   18  ---    9 |    40   37   37   31   33   38  ---    31
XR03E | 5147   10   37  ---  ---  386   25  ---   18 |    26   31  ---  ---  109   25  ---    23
 R05  | 1196   31   13   20   17   66   20  181   11 |    83   77   77   86   47   75   40    76
 R06  | 3072   28   21   15    9   37   16  ---    8 |    58   59   42   47   59   48  ---    47
 R07  | 2786   29   43   21   23   58   24  ---   13 |    66   78   48   44   63   45  ---    52
 R08  | 2538   27   19   20   14   31   19   47    9 |    49   44   37   40   29   36   22    35
 R09E |  941   39   30   18   13   51   20  ---   11 |    39   33   37   34   34   28  ---    28
 R10E | 1848   15   16   10   13   52   21  ---    8 |    32   36   34   32   44   29  ---    29
 R11E | 1344   38   48   31   31   63   23  113   16 |    35   34   61   63   67   42   30    44
 R12E | 1268   19   19   23   17   53   22  ---   10 |    45   38   51   50   62   40  ---    43
 R13E | 1753   17   19   27   26   52   26  ---   11 |    44   51   53   49   60   36  ---    43
 R15E | 2139   23   36   11   20   66   24   50   12 |    30   28   30   38   49   31   27    26
 R16E | 1167   25   17   15   16   51   22  ---    9 |    30   30   42   42   64   35  ---    33
 R17  | 2591   35   28   27   13   49   27  ---   12 |   206  244  229  243  191  203  ---   209
 R18  | 7095   35   35   19   18   66   34  332   13 |    55   35   40   45   64   25   87    33
 R19  | 2290   27   44   15   14   71   32  ---   13 |    61   60   63   53   29   34  ---    48
 R20  | 2524   48   75   22   29   41   43  ---   19 |    44   41   58   64   74   35  ---    43
 R21  |  538   31   12   16   13   63   16  ---   10 |    71   58   58   55   85   52  ---    57
 R22  | 1286   28   17   17   22   56   20  ---   10 |    69   58   55   65   52   40  ---    54
 R23  | 1061   14   17   19   16   49   24  ---    9 |    60   58   70   54   63   40  ---    54
 R24  | 2883   17   29   19   40   40   25  ---   12 |    43   38   52   70   51   28  ---    43
------+----------------------------------------------+------------------------------------------
 RMS  | 2460   28   31   19   20   54   24  179      |T   56   55   58   60   63   46   41    50
 WRMS | 2460   26   32   18   15   54   24  179      |NE  68   66   65   68   64   54   49    59
 MEDI | 1848   27   21   19   17   52   22  113      |MD  45   41   52   50   60   36   30    43

Table 3.1657.4  GPS week: 1657   Day: 4   MJD: 55847                            

        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  | 1437   14   29   16   19   29   21  ---    9 |    41   39   48   36   39   47  ---    38
 R02  | 1200   26   24   15   20   44   22  ---   10 |    42   29   39   28   42   36  ---    31
XR03E | ----  ---  ---  ---  ---  ---   12  ---    0 |   ---  ---  ---  ---  ---   22  ---    25
 R05  | 2514   31   25   21   15   31   18  113   10 |    57   47   28   38   57   46   41    38
 R06  | 1650   23   22   13   19   40   16  ---    9 |    45   50   46   50   33   40  ---    41
XR07  | 2532   30   16   18  ---   62   24  ---   14 |    52   50   49  ---   33   47  ---    42
 R08  | 2483   23   25   12   14   28   15   69    8 |    54   41   44   52   42   37   33    42
 R09E | 1094   20   44   14   14   51   33  ---   12 |    28   40   46   44   48   36  ---    35
 R10E | 2079   19   23   22   28   58   21  ---   12 |    42   37   32   38   54   40  ---    32
 R11E | 1564   29   50   37   41   86   55  176   21 |    47   50   73   75   85   56   45    50
 R12E | 1538   19   32   22   21   57   18  ---   11 |    30   31   49   38   70   33  ---    34
 R13E | 1231   21   21   18   23   57   25  ---   11 |    43   56   62   53   52   40  ---    47
XR14E | 1862   25  ---   15  ---  ---  ---  ---   19 |    18  ---   24  ---  ---  ---  ---    20
 R15E | 2919   18   30   12   16   34   30   72    9 |    33   36   32   36   39   35   25    28
 R16E | 1294   24   30   14   20   31   20  ---    9 |    26   37   35   42   42   36  ---    30
XR17  | 6273   94  ---  ---  372  552   98  ---   96 |   464  ---  ---  637  179  383  ---   415
 R18  | 3985   28   31   13   26   54   33  260   13 |    59   51   35   48   58   51   99    43
 R19  | 1550   27   54   16   28   53   39  ---   15 |    41   40   31   53   43   34  ---    31
 R20  | 2274   32  100   14   27   62   47  ---   20 |    47   27   46   45   69   43  ---    39
 R21  | 1647   28   25   17   13   29   28  ---   10 |    58   35   52   44   38   38  ---    44
 R22  | 1783   32   23   20   18   50   22  ---   11 |    67   53   57   59   31   47  ---    52
 R23  | 1119   31   28   11   17   34   34  ---   11 |    55   54   39   36   32   25  ---    34
 R24  | 1629   19   24   14   21   37   32  ---   10 |    55   43   62   73   62   27  ---    52
------+----------------------------------------------+------------------------------------------
 RMS  | 1974   25   38   18   22   48   30  156      |T   63   42   44   76   54   54   48    54
 WRMS | 1974   26   39   16   21   46   30  156      |NE  81   43   44   92   54   64   57    67
 MEDI | 1647   25   25   15   20   50   24  113      |MD  45   40   46   44   43   38   41    38

Table 3.1657.5  GPS week: 1657   Day: 5   MJD: 55848                            

        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  | 1019   18   44   16   20   45   40  ---   14 |    46   42   45   35   29   45  ---    37
 R02  | 1207   29   16   21   15   37   21  ---   10 |    33   28   25   21   33   26  ---    19
 R05  | 1253   33    8   20   21   41   19   65   10 |    51   41   44   43   43   42   46    40
 R06  | 1250   28   31   32   18   41   15  ---   12 |    39   32   35   17   41   28  ---    22
XR07  | 8759   26   33   29  ---   33   21  ---   14 |    50   61   42  ---   33   47  ---    44
 R08  | 1987   26   22   20   28   37   23   96   11 |    45   51   41   50   37   39   33    39
 R09E | 2066   16   33   15   23   42   31  ---   11 |    25   29   30   33   37   24  ---    22
 R10E | 1912   16   19   26   18   62   28  ---   12 |    30   28   45   29   40   28  ---    24
 R11E | 2115   44   30   27   24   53   43   96   16 |    35   52   73   68   65   52   44    50
 R12E | 1938   15   31   14   14   45   20  ---   10 |    35   41   35   40   64   38  ---    34
 R13E | 1349   17   22   31   17   25   21  ---   10 |    42   40   65   46   44   31  ---    41
XR14E | 3259   25  ---   27  ---   47   25  ---   16 |    18  ---   30  ---   26   18  ---    17
 R15E | 1545   22   34   24   29   51   24   63   13 |    26   25   35   32   48   25   25    20
 R16E | 1145   27   35   43   17   64   24  ---   15 |    29   40   63   34   63   33  ---    32
XR17  | 5173   35  ---   31   21  ---   39  ---   18 |   270  ---  248  283  ---  267  ---   260
 R18  | 1872   23   20   13   46   65   23  150   14 |    47   31   38   71   33   40  149    38
 R19  | 1462   34   18   36   32   57   38  ---   15 |    41   53   42   45   37   18  ---    29
 R20  | 2270   43   77   24   33   76   43  ---   22 |    43   38   43   50   29   22  ---    29
 R21  | 2845   25   27   21   21   30   26  ---   11 |    52   34   60   55   48   38  ---    45
 R22  | 1513   33   19   25   23   49   22  ---   12 |    59   48   55   33   58   26  ---    40
 R23  | 1562   32   25   27   27   51   19  ---   13 |    48   56   45   39   41   40  ---    38
 R24  | 1590   28   22   29   37   46   15  ---   13 |    50   45   37   61   44   36  ---    38
------+----------------------------------------------+------------------------------------------
 RMS  | 1738   28   31   26   26   50   27   99      |T   50   40   53   54   42   43   59    43
 WRMS | 1738   30   29   25   22   48   27   99      |NE  62   43   57   61   38   51   76    51
 MEDI | 1590   26   25   25   21   46   23   96      |MD  42   40   42   40   41   33   44    37

Table 3.1657.6  GPS week: 1657   Day: 6   MJD: 55849                            

        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  |  812   21   21   25   19   38   47  ---   13 |    44   48   50   50   38   43  ---    44
 R02  | 1188   19   22   17   15   36   18  ---    8 |    48   32   37   42   50   37  ---    37
 R05  |  728   33   10   16   20   32   23   48   10 |    63   46   38   47   38   36   43    40
 R06  | 1778   28   23   15   14   26   20  ---    9 |    53   49   31   34   38   43  ---    36
XR07  | 9468   19   40   18  ---   28   20  ---   12 |    49   55   33  ---   34   38  ---    38
 R08  | 2217   25   35   17   17   56   11   96   11 |    59   56   44   45   48   44   32    44
 R09E | 1227   32   23   16   21   29   25  ---   10 |    36   46   41   33   51   36  ---    35
 R10E | 1937   14   28   14   16   39   27  ---    9 |    37   47   32   31   49   25  ---    28
 R11E | 2819   49   45   22   40   50   40   79   17 |    27   50   61   77   51   46   40    48
 R12E | 1193   15   18   19   16   65   22  ---   10 |    38   44   35   39   58   36  ---    35
 R13E | 1797   19   20   19   21   44   41  ---   12 |    53   53   60   57   62   22  ---    47
XR14E | 2999   24  ---   16  ---   40   22  ---   13 |    15  ---   24  ---   31   15  ---    14
 R15E | 1329   26   19   13   21   61   24   58   11 |    31   39   33   31   58   35   28    27
 R16E |  939   30   36   18   16   37   24  ---   11 |    35   49   39   42   54   34  ---    35
 R17  | 2695   40   45   12   23   41   24  ---   13 |   270  159  192  304  201  257  ---   261
 R18  | 1285   17   28   11   16   50   13  181    9 |    64   38   60   65   35   43   99    52
 R19  | 1393   19   29   16   20   83   22  ---   12 |    58   41   60   66   52   33  ---    48
 R20  | 3290   25   83   22   21   93   23  ---   18 |    51   47   54   50   46   37  ---    42
 R21  | 1468   20   37   10   16   54   27  ---   11 |    64   48   58   64   46   43  ---    53
 R22  | 1179   35   25   25   16   51   16  ---   11 |    85   64   45   55   50   63  ---    56
 R23  |  928   28   23   30   23   44   17  ---   11 |    63   53   47   35   33   39  ---    41
 R24  | 1231   11   30   17   17   71   17  ---   11 |    57   52   50   51   49   45  ---    45
------+----------------------------------------------+------------------------------------------
 RMS  | 1714   27   33   18   20   53   26  104      |T   59   53   51   60   53   47   48    50
 WRMS | 1714   27   30   18   19   53   26  104      |NE  73   56   57   69   54   57   58    59
 MEDI | 1329   24   28   17   17   44   22   79      |MD  51   48   44   47   49   37   40    41




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