[IGSREPORT-20220] Wk 1655 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Oct 13 09:37:06 PDT 2011


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1655   (Sep 25, 2011 - Oct 01, 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 2.1655.
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:
                                                                               
 igl1655[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1655 in the SP3 format.
 igl16557.sum      Combination Report for GPS Week 1655.


    
    
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  |    164.4 ns
                1  |    166.5 ns
                2  |    165.9 ns
                3  |    167.3 ns
                4  |    168.0 ns
                5  |    167.2 ns
                6  |    164.8 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
               ----+--------+---------------
                1  |  IAC   | R07

    
         
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 1.1655, 1a.1655).
        
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 2.1655.0-6)                                                                                
    
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 3.1655.0-6). 
        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 1655 summary.                      (Sep 25, 2011 - Oct 01, 2011)

Table 1.1655.a     GPS week : 1655   MJD: 55829.0-55835.0

         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  253|    0    -1    -3    25   -78    46  -.11   31   32 |     ---     ---    ---    ---
        |    1     1     5    17    36    41   .07           |     ---     ---
emx  139|    1     0     0   -20   -16   -23  -.09   32   32 |  165447    -818   5028   8873
        |    1     1     5    48    42    23   .08           |    1051    1707
esx  137|    0     0     3    26    74   -62   .45   20   19 |  166722    -842   4940   5117
        |    1     1     1    33    18    19   .04           |    2075    2342
gfz  193|   -1     0    -1     9     3    37  -.18   23   20 |       0     241   4851   8431
        |    1     1     2    23    46    24   .05           |       0    1691
grg  127|   -3    -1    -5   -37   -47    -2   .13   48   47 |     ---     ---    ---    ---
        |    1     3     4    35    22    60   .08           |     ---     ---
iac  n/a|    0     0     2   -32    -8    18  -.27   23   23 |  167121    -531   4933   8839
        |    1     1    11    24    22    62   .05           |    1633     916
mcc  n/a|   -1    -5    15    34    56   281   .31  174  174 |     ---     ---    ---    ---
        |    8    11    40   173    74   371   .32           |     ---     ---


Table 1.1655.b     GPS week : 1655   MJD: 55829.0-55835.0   

         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  |    9   12   13   16   14   11   12 |
 R02  |   10    9   11   11   10   10   11 |
 R03  |   11   10   11   12   10   11   11 |
 R04  |   16   15   12   14   13   16   17 |
 R05  |   11   11   12   10   10    8   10 |
 R06  |   12   10    9   12   11   11    9 |
 R07  |   13  173   15   17   13   13    9 |
 R08  |    8   11   12   12   10   10    7 |
 R09  |    9   13    9   14   13   13   13 |
 R10  |   11   12   12   11   12   10   11 |
 R11  |   17   18   15   18   19   22   23 |
 R12  |   12   10   11   13   11    9   10 |
 R13  |   10   11   12   14   10   10   10 |
 R15  |   10   10    9   11   14   10   11 |
 R16  |    9   10   11   14    9   10   11 |
 R17  |   16   16   15   17   16   16   18 |
 R18  |   13   10   11   10   12   13   11 |
 R19  |   10   12   13   11   11   10   11 |
 R20  |   12   17   16   16   15   25   19 |
 R21  |   10   12   10   13    9   10   12 |
 R22  |   11   13   13   13   15   13   12 |
 R23  |   12   11   12   10   11   10    9 |
 R24  |   12   11   14   14   10   10   11 |


Table 1.1655.c     GPS week : 1655   MJD: 55829.0-55835.0   

         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 1655 0   |  -38     3   121    -290     318  -16079  86.4  1818  1818 |  164359       0
brd 1655 1   |   -2    19    21    -748     332  -15160  85.7  1537  1537 |  166532       0
brd 1655 2   |  -53    76   -54    1042    2292  -22980  88.8  1871  1871 |  165929       0
brd 1655 3   |   -1   -54  -116     377    1685  -24350  84.8  2258  2258 |  167285       0
brd 1655 4   |  -21    12   -12     976   -1946  -25310  81.2  2804  2804 |  167964       0
brd 1655 5   |   63    46    12     106   -1947  -20560  86.1  1725  1725 |  167170       0
brd 1655 6   |   67    86   149      15   -1845  -12970  86.1  2366  2366 |  164843       0
-------------+------------------------------------------------------------+----------------
brd 1655 mean|    1    27    17     211    -158  -19630  85.6  2054  2054 |  166297       0
brd 1655 sdev|   47    47    93     648    1784    4891   2.3   440   440 |    1327       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 2.1655.0  GPS week: 1655   Day: 0   MJD: 55829                            

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  253|   -2     1    -5     6   -67    15  -.05   30   30 |     ---     ---    ---    ---
emx  139|    0    -1    -4     0   -57    -5  -.01   23   24 |  163227     420   5282   7340
esx  137|    0     0     1    34    96   -75   .51   21   19 |  163880     106   5114   5255
gfz  193|    0     0     0    -8   -57    22  -.19   22   24 |       0     401   5035   6982
grg  127|   -3    -1   -11   -29   -17   -78   .05   41   43 |     ---     ---    ---    ---
iac  n/a|    0     0     8   -24    20    51  -.33   22   22 |  165200    -164   5101   6930
mcc  n/a|  -12   -22   -48   303   176   -89   .73  252  252 |     ---     ---    ---    ---

Table 2.1655.1  GPS week: 1655   Day: 1   MJD: 55830                            

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  253|   -1    -2    -7    37   -46     0  -.04   31   32 |     ---     ---    ---    ---
emx  139|    4    -1    -5    31     8   -49  -.03   34   34 |  165903    -509   4968   7144
esx  137|    0     0     3   -43    77   -45   .44   19   18 |  166640    -432   4887   5127
gfz  193|    0     0    -2   -24   -26    -2  -.16   20   18 |       0     606   4877   7109
grg  127|   -4    -4    -6   -16   -31   -60   .09   49   42 |     ---     ---    ---    ---
iac  n/a|    1     2     7     6    -7   108  -.31   22   22 |  166777    -177   4890   7667
mcc  n/a|    6    -9    16     7    32   -62  -.25  237  237 |     ---     ---    ---    ---

Table 2.1655.2  GPS week: 1655   Day: 2   MJD: 55831                            

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  253|   -2    -3    -7    22   -49    57  -.16   30   32 |     ---     ---    ---    ---
emx  139|    0    -1    -2   -52   -23     9  -.21   33   32 |  166004   -3349   4739   8485
esx  137|    1    -2     3    26    91   -88   .43   17   16 |  165468    -222   4701   4873
gfz  193|   -1     3    -1     3   -13    36  -.25   24   21 |       0   -1400   4675   8113
grg  127|   -1     5    -6    16   -68    45   .19   46   46 |     ---     ---    ---    ---
iac  n/a|   -2    -1     3   -35   -34    13  -.24   23   23 |  166043    -195   4661   8438
mcc  n/a|   10    -1    18  -265    30    52   .30  221  221 |     ---     ---    ---    ---

Table 2.1655.3  GPS week: 1655   Day: 3   MJD: 55832                            

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  253|    0    -1    -4    37  -127    94  -.10   30   31 |     ---     ---    ---    ---
emx  139|    1     1     1   -40   -37   -36  -.07   30   31 |  166157   -1522   4211   9155
esx  137|   -1     0     0    58    40   -33   .40   24   23 |  170133   -3333   4167   4433
gfz  193|   -2     0    -6    14    81    58  -.11   24   19 |       0   -1176   4109   7984
grg  127|   -3    -2    -3   -95   -79    57   .16   54   56 |     ---     ---    ---    ---
iac  n/a|    0     1    17   -18     1   -76  -.28   25   25 |  166906     982   4153   8760
mcc  n/a|   -6     6    10   -61   -55   154   .42  119  119 |     ---     ---    ---    ---

Table 2.1655.4  GPS week: 1655   Day: 4   MJD: 55833                            

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  253|    1     0    -4    10  -129    75  -.04   30   33 |     ---     ---    ---    ---
emx  139|    0     0    -5   -92   -54   -33  -.06   29   30 |  166021    1414   5437   8444
esx  137|    2    -1     1    45    63   -68   .47   24   22 |  167997    -746   5360   5469
gfz  193|   -2    -1     0    52    38    65  -.20   23   16 |       0    1767   5005   8491
grg  127|   -2     1    -7   -31   -44     4   .26   45   45 |     ---     ---    ---    ---
iac  n/a|    0    -1     6   -34    17   -33  -.18   22   22 |  169842   -1727   5363   9667
mcc  n/a|   -1     2     0    78    20   365   .37  114  114 |     ---     ---    ---    ---

Table 2.1655.5  GPS week: 1655   Day: 5   MJD: 55834                            

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  253|    0     0     2    53   -86    87  -.21   31   31 |     ---     ---    ---    ---
emx  139|    1     0     6   -32   -10     0  -.16   41   36 |  165826     293   5965   8883
esx  137|    2     0     6    41    81   -52   .47   20   17 |  165285    2914   5836   6003
gfz  193|   -2     0     1    11    17    25  -.19   23   23 |       0    2922   5711   8485
grg  127|   -6    -5     0   -36   -30    66   .13   53   50 |     ---     ---    ---    ---
iac  n/a|    0     0   -10   -42   -29     2  -.21   21   21 |  168815   -1245   5847   8997
mcc  n/a|    5   -16    27   106   118   699   .53  116  116 |     ---     ---    ---    ---

Table 2.1655.6  GPS week: 1655   Day: 6   MJD: 55835                            

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  253|    1     0     5    10   -46    -2  -.16   32   32 |     ---     ---    ---    ---
emx  139|    0     0     7    42    63   -47  -.13   36   35 |  164994   -2476   4594  12665
esx  137|    0     0     4    20    69   -73   .40   18   15 |  167657   -4183   4516   4659
gfz  193|    0     0     0    15   -18    55  -.14   24   20 |       0   -1428   4547  11853
grg  127|   -3    -2     0   -67   -60   -49   .02   50   47 |     ---     ---    ---    ---
iac  n/a|    0     0   -13   -75   -25    64  -.30   22   22 |  166268   -1196   4519  11414
mcc  n/a|  -10     5    86    75    72   848   .08  160  160 |     ---     ---    ---    ---

       
       
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 3.1655.0  GPS week: 1655   Day: 0   MJD: 55829                            

        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  | 1833   17   18   16   18   40   15  ---    8 |    35   40   42   38   34   34  ---    32
 R02  | 1082   23   25   13   16   49   12  ---    9 |    43   30   31   39   45   39  ---    32
 R03E | 1619   17   22   20   25   36   21  ---   10 |    74   76   76   75   72   78  ---    73
XR04  | 2688   34  ---   32   34   30   30  ---   16 |    23  ---   49   55   25   21  ---    29
 R05  | 2243   41   17   23   14   39   14  146   10 |    62   47   42   40   46   42   18    41
 R06  | 1890   30   22   37    9   42   19  ---   12 |    46   43   35   35   28   39  ---    33
 R07  | 4020   43   13   25   23   50   24  ---   12 |   794  850  861  760  838  775  ---   814
 R08  | 1419   15   12   12   15   39   19   95    8 |    57   52   54   54   43   48   32    50
 R09E | 1151   15   16   13   21   44   16  ---    9 |    37   48   52   53   50   46  ---    45
 R10E | 1101   16   18   12   25   53   22  ---   10 |    73   81   74   70   81   72  ---    72
 R11E |  818   34   37   35   30   49   38  455   16 |    73   65   73   76   87   70  163    66
 R12E | 1274   20   17   28   23   51   25  ---   12 |    41   47   58   50   47   40  ---    44
 R13E | 2422   21   23   11   24   37   19  ---    9 |    36   47   46   47   49   32  ---    39
 R15E | 1831   29   21    9   18   40   16  ---    9 |    31   38   35   42   58   38  ---    36
 R16E |  938   22   20    8   18   39   18  ---    9 |    39   50   50   49   48   47  ---    45
 R17  | 3332   62   43   27   14   39   28  ---   16 |    24   51   69   55   50   66  ---    52
 R18  | 2099   45   25   14   28   38   23  130   12 |    54   40   36   50   34   20   55    32
 R19  |  885   32   12   19   21   30   18  ---    9 |    46   29   30   32   33   17  ---    24
 R20  |  813   28   31   22   22   32   21  ---   11 |    34   44   36   48   43   36  ---    36
 R21  | 1860   36   20   25   12   31   14  ---   10 |    47   33   29   30   30   27  ---    26
 R22  |  781   31   24   16   31   40   13  ---   11 |    55   25   26   50   30   20  ---    28
 R23  | 1433   18   28   17   29   29   35  ---   12 |    44   29   21   41   39   33  ---    28
 R24  |  851   21   19   29   24   45   22  ---   11 |    32   16   29   31   30   27  ---    20
------+----------------------------------------------+------------------------------------------
 RMS  | 1817   30   23   21   22   41   22  252      |T   78   80   80   79   80   72   67    73
 WRMS | 1817   30   24   19   24   43   22  252      |NE  93   94   92   90   89   82   35    85
 MEDI | 1433   28   20   19   22   39   19  130      |MD  44   44   42   49   45   39   32    36

Table 3.1655.1  GPS week: 1655   Day: 1   MJD: 55830                            

        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  | 2159   24   23   18   20   58   27  ---   11 |    34   32   31   35   40   24  ---    26
 R02  | 1160   29   21   15   18   28   18  ---    9 |    25   38   28   18   28   27  ---    21
 R03E | 1139   17   28   11   19   41   25  ---   10 |    86   94   93   95   76   82  ---    87
XR04  | 3074   28  ---   29   16   40   35  ---   14 |    36  ---   64   48   53   43  ---    44
 R05  |  894   38   21   18    9   46   18  129   10 |    48   56   42   42   26   39   20    39
 R06  | 2737   21   28   14   20   49   13  ---    9 |    39   35   33   52   30   42  ---    35
XR07  |13311  236  ---  ---  125  ---  439  ---  172 |   880  ---  ---  797  ---  720  ---   860
 R08  | 1959   35   23   16   11   47   21   49   10 |    44   39   41   47   50   33   37    38
 R09E |  918   23   21   13   23   81   20  ---   12 |    33   45   48   57   87   36  ---    41
 R10E | 1619   29   28   16   22   48   28  ---   11 |    53   54   48   58   53   41  ---    45
 R11E |  995   35   52   37   33   60   33  435   17 |    64   77   78   72   66   67  145    64
 R12E |  939   18   24   12   18   57   22  ---   10 |    46   52   50   54   68   40  ---    47
 R13E | 1248   17   22   22   16   57   19  ---   10 |    33   33   51   36   47   31  ---    33
 R15E | 1568   23   20   17   17   43   20  ---    9 |    43   46   47   50   48   41  ---    42
 R16E |  772   17   18    8   19   55   18  ---    9 |    43   59   41   53   56   42  ---    43
 R17  | 3083   63   58   15   17   39   28  ---   16 |    30   34   33   41   57   32  ---    28
 R18  | 1135   34   25   16   14   29   18  130    9 |    42   27   30   23   49   24   61    25
 R19  |  839   32   41   15   25   38   16  ---   11 |    41   36   36   32   41   26  ---    30
 R20  | 1130   48   74   28   24   29   22  ---   16 |    40   62   49   53   41   45  ---    43
 R21  | 2297   35   27   19   24   47   20  ---   11 |    38   38   40   39   53   38  ---    34
 R22  |  832   36   38   24   17   50   28  ---   13 |    34   41   37   36   30   32  ---    28
 R23  |  850   19   24   18   21   40   26  ---   10 |    37   26   23   55   56   32  ---    31
 R24  |  841   20   27   17   20   50   20  ---   10 |    24   34   35   47   54   14  ---    28
------+----------------------------------------------+------------------------------------------
 RMS  | 1536   31   34   19   20   49   22  237      |T   77   45   44   80   50   67   65    74
 WRMS | 1536   32   34   18   18   42   22  237      |NE  92   38   37   91   43   78   39    87
 MEDI | 1139   29   25   16   19   47   21  129      |MD  40   39   41   48   50   38   37    38

Table 3.1655.2  GPS week: 1655   Day: 2   MJD: 55831                            

        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  | 2662   18   38   18   22   56   31  ---   12 |    30   37   27   44   44   26  ---    25
 R02  |  963   24   16   17   21   48   22  ---   10 |    29   35   38   28   50   22  ---    27
 R03E | 2321   14   33   14   13   51   27  ---   10 |    64   81   66   67   90   57  ---    65
XR04  | 2850   28  ---   25   21   28   21  ---   12 |    25  ---   39   28   36   15  ---    19
 R05  | 1514   29   33   11   11   60   26   82   11 |    35   42   22   17   49   23   36    17
 R06  | 3244   21   18   13   18   36   16  ---    8 |    40   31   48   41   42   44  ---    40
XR07  | 9195   46   23   15   24  ---   38  ---   15 |   491  323  309  620  ---  436  ---   457
 R08  | 2198   23   33   17   17   56   22   64   11 |    46   54   45   49   49   39   27    42
 R09E | 1177   23   13   15   18   37   21  ---    9 |    22   48   36   45   45   34  ---    34
 R10E | 3428   20   31   19   29   53   19  ---   12 |    54   59   49   52   59   36  ---    45
 R11E | 1286   32   51   25   27   44   27  416   14 |    65   85   76   71   83   67  223    67
 R12E | 1511   17   29   22   20   42   24  ---   11 |    40   38   64   54   69   29  ---    46
 R13E | 1491   30   20   17   21   60   17  ---   11 |    59   56   57   65   65   49  ---    53
 R15E | 1161   19   23   12   23   23   23  ---    9 |    42   39   41   48   41   41  ---    39
 R16E |  833   16   27   16   24   46   21  ---   10 |    23   34   39   36   52   29  ---    30
 R17  | 1909   51   42   10   27   35   34  ---   14 |    37   38   43   59   73   60  ---    45
 R18  | 2449   35   19   19   22   40   16  105   10 |    47   39   25   44   47   22   79    28
 R19  | 1006   41   53    7   16   36   16  ---   12 |    44   21   27   23   33   20  ---    21
 R20  | 1485   53   58   21   24   34   26  ---   15 |    51   53   59   59   44   44  ---    47
 R21  | 2049   25   22   16   23   36   23  ---   10 |    45   45   39   28   46   38  ---    32
 R22  |  604   38   30   14   36   40   26  ---   13 |    45   38   37   52   55   45  ---    37
 R23  | 1284   30   19   21   33   55   16  ---   12 |    33   24   32   30   47   32  ---    21
 R24  | 1423   27   27   16   36   61   25  ---   13 |    37   29   38   46   76   30  ---    28
------+----------------------------------------------+------------------------------------------
 RMS  | 1871   30   33   17   24   46   23  221      |T   61   56   54   69   54   53   91    55
 WRMS | 1871   32   32   16   21   46   23  221      |NE  69   57   55   77   49   59   47    59
 MEDI | 1511   27   27   16   22   42   23   82      |MD  42   39   39   46   49   36   36    37

Table 3.1655.3  GPS week: 1655   Day: 3   MJD: 55832                            

        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  | 2688   23   50   16   23   85   25  ---   15 |    52   73   56   56   89   48  ---    49
 R02  |  819   27   17   27   18   38   25  ---   11 |    35   24   32   35   37   35  ---    23
 R03E | 5270   20   21   17   20   57   30  ---   11 |   107  129  114  116  126  100  ---   111
XR04  | 1906   29  ---   18   14   66   27  ---   14 |    33  ---   48   49   41   53  ---    41
 R05  | 1588   34   25   19   17   28   16  106   10 |    58   53   57   41   42   36   53    44
 R06  | 2402   32   23   16   26   56   13  ---   11 |    42   36   27   26   38   26  ---    21
XR07  | 8802   31   18   19  ---   65   42  ---   17 |   538  343  344  ---  310  541  ---   529
 R08  | 1797   18   24   20   18   71   14   62   11 |    50   58   54   46   46   44   40    45
 R09E | 1049   23   46   23   25   47   24  ---   13 |    28   42   43   56   56   36  ---    37
 R10E | 4477   22   24   14    8   54   25  ---   10 |    62   61   59   55   47   51  ---    52
 R11E |  948   42   26   39   31   70   44  120   18 |    53   79   97   80   77   68  174    68
 R12E | 1447   12   30   16   30   43   37  ---   12 |    58   60   58   70   78   51  ---    57
 R13E | 1453   42   26   36   26   38   17  ---   13 |    49   35   51   52   38   39  ---    37
 R15E | 1651   18   27   15   24   25   28  125   10 |    42   46   42   42   42   38   70    37
 R16E | 1098   21   49   18   26   54   24  ---   13 |    39   61   53   59   59   43  ---    46
 R17  | 1104   57   32   39   30   42   32  ---   17 |    39   57   86   81   45   60  ---    61
 R18  | 3825   27   30   23   15   29   16  159   10 |    53   35   51   50   43   28   39    39
 R19  | 1132   35   31   21   13   46   11  ---   11 |    68   51   56   54   80   44  ---    52
 R20  | 2530   41   43   26   20   63   29  ---   15 |    36   53   38   29   45   36  ---    22
 R21  | 1887   29   20   20   14   78   24  ---   13 |    61   50   52   52   56   41  ---    45
 R22  |  926   38   20   20   26   33   30  ---   12 |    60   55   54   41   49   23  ---    40
 R23  |  902   18   12   17   27   48   13  ---    9 |    50   44   50   60   65   49  ---    49
 R24  |  941   16   16   27   45   65   18  ---   14 |    38   36   20   75   55   33  ---    35
------+----------------------------------------------+------------------------------------------
 RMS  | 2257   30   30   24   24   54   25  119      |T   71   67   67   55   68   66   75    66
 WRMS | 2257   31   31   23   19   56   25  119      |NE  80   69   68   49   69   73   44    73
 MEDI | 1588   27   25   20   23   54   25  120      |MD  50   53   53   52   49   43   53    45

Table 3.1655.4  GPS week: 1655   Day: 4   MJD: 55833                            

        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  | 1856   23   40   21   15   59   30  ---   13 |    41   70   60   52   52   35  ---    46
 R02  | 1315   31   23   18   16   40   14  ---   10 |    39   43   31   40   41   32  ---    32
 R03E | 5170   19   20   23   21   28   20  ---    9 |    88   96   97   99   89   80  ---    90
XR04  | 1894   30  ---   15   25   43   26  ---   13 |    27  ---   42   65   48   36  ---    37
 R05  | 1554   27   12   19   20   47   15   95   10 |    36   24   33   33   34   20   27    23
 R06  | 1662   34   25   16   21   32   19  ---   10 |    33   22   27   34   34   29  ---    21
 R07  | 7456   24   27   21   33   33   28  ---   12 |   269  198  213  323  220  275  ---   272
 R08  | 2065   24   28   14   13   40   17   92    9 |    38   52   40   42   45   35   28    38
 R09E |  901   24   39   22   29   29   25  ---   12 |    37   37   52   56   51   42  ---    42
 R10E | 5267   17   30   18   24   44   33  ---   12 |    57   57   58   65   70   49  ---    54
 R11E | 1351   38   46   48   40   38   42   84   19 |    49   82   95   82   60   59   97    64
 R12E | 1367   24   19   20   18   46   22  ---   10 |    43   46   61   60   47   47  ---    49
 R13E | 1200   17   21   22   18   36   21  ---    9 |    28   48   58   45   38   41  ---    40
 R15E | 1970   16   36   20   25   73   21  110   13 |    35   36   36   36   66   36   16    31
 R16E | 1412   15   21   23   17   38   14  ---    9 |    38   47   52   47   44   39  ---    41
 R17  | 2533   53   27   35   31   47   24  ---   16 |    26   55   63   63   28   49  ---    45
 R18  | 4725   38   24   29   16   46   12  169   12 |    56   34   31   39   46   33   48    34
 R19  | 1008   34   29   24   14   45   11  ---   11 |    54   27   39   37   65   33  ---    35
 R20  | 1071   26   51   32   15   61   25  ---   15 |    46   28   48   32   44   32  ---    30
 R21  | 1378   28   17   15   12   35   19  ---    9 |    44   33   38   35   46   15  ---    27
 R22  | 1249   49   27   15   36   69   14  ---   15 |    57   41   39   38   69   17  ---    27
 R23  | 1164   35   12   30   22   22   18  ---   10 |    44   31   52   34   35   24  ---    31
 R24  |  820   17   19   18   21   45   15  ---    9 |    48   45   34   38   34   32  ---    33
------+----------------------------------------------+------------------------------------------
 RMS  | 2803   30   29   24   23   45   22  114      |T   53   52   56   60   56   47   43    49
 WRMS | 2803   33   30   22   16   45   22  114      |NE  57   50   52   60   56   46   34    48
 MEDI | 1412   26   25   21   21   43   20   95      |MD  43   43   48   42   46   35   28    37

Table 3.1655.5  GPS week: 1655   Day: 5   MJD: 55834                            

        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  |  977   15   21   24   13   58   19  ---   10 |    35   39   45   42   54   33  ---    36
 R02  | 1045   29   15   12   17   59   16  ---   10 |    29   31   24   33   37   24  ---    21
 R03E | 1451   26   24   20   18   61   18  ---   11 |   130  139  132  120  140  116  ---   125
XR04  | 2165   31  ---   14   45   39   29  ---   16 |    25  ---   33   59   40   39  ---    27
 R05  |  999   22   15   16   19   28   14   98    8 |    45   41   46   51   55   44   21    44
 R06  | 2054   39   15   14   28   37   13  ---   10 |    30   19   23   32   34   18  ---    16
 R07  | 2466   29   19   26   39   54   16  ---   13 |   423  260  262  357  235  415  ---   417
 R08  | 1236   25   30   17   17   40   13  122    9 |    24   28   20   23   41   19   20    15
 R09E | 1635   20   30   22   25   69   23  ---   12 |    21   36   38   31   68   25  ---    24
 R10E | 3294   18   25   16   19   50   22  ---   10 |    48   53   49   48   62   33  ---    42
 R11E | 1284   42   96   40   29   47   43   85   22 |    28   59   54   50   65   38   50    37
 R12E |  897   25   25   10   22   44   12  ---    9 |    44   53   51   59   57   52  ---    50
 R13E | 1184   22   25   21   14   49   13  ---    9 |    29   28   44   39   42   33  ---    31
 R15E | 1720   17   31   11   25   51   15  112   10 |    16   30   25   34   45   21   14    21
 R16E | 1172   19   22   16   22   46   23  ---   10 |    31   39   44   45   37   38  ---    35
 R17  | 3632   48   32   28   17   78   26  ---   15 |    38   26   55   39   40   47  ---    39
 R18  | 1877   40   23   21   31   60   17  150   13 |    47   28   45   43   36   27   25    31
 R19  | 1091   29   25   19   16   36   20  ---   10 |    55   37   57   57   51   42  ---    47
 R20  |  913   49  127   11   23   83   36  ---   25 |    28   64   30   43   34   37  ---    28
 R21  | 1154   23   16   15   25   38   18  ---    9 |    40   39   31   46   30   32  ---    32
 R22  | 1059   51   17   11   25   43   32  ---   13 |    46   24   33   47   42   21  ---    25
 R23  | 2088   29   27   20   18   43   14  ---   10 |    41   28   32   51   47   33  ---    34
 R24  | 1097   24   19   15   18   55   12  ---    9 |    32   27   27   17   42   17  ---    17
------+----------------------------------------------+------------------------------------------
 RMS  | 1725   31   41   20   23   53   21  116      |T   55   51   52   59   58   52   26    51
 WRMS | 1725   31   36   17   23   50   21  116      |NE  62   49   50   62   54   56   22    55
 MEDI | 1236   26   24   16   22   49   18  112      |MD  35   36   44   45   42   33   21    32

Table 3.1655.6  GPS week: 1655   Day: 6   MJD: 55835                            

        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  |  941   21   20   19   21   75   16  ---   11 |    26   36   37   39   44   28  ---    29
 R02  |  803   41   20    9   11   61   12  ---   10 |    42   22   21   31   39   19  ---    21
 R03E | 4910   28   17   17   15   48   27  ---   10 |   141  151  156  151  149  125  ---   144
XR04  | 2737   43  ---   20   39   53   26  ---   16 |    25  ---   42   45   40   29  ---    23
 R05  | 1475   28   15   16   18   41   22  164    9 |    55   42   41   37   34   37   27    37
 R06  | 2568   25   18   12   22   45   15  ---    9 |    43   26   27   31   32   19  ---    22
 R07  | 2157   18   24   12   25   33   15  ---    9 |   401  269  275  341  256  399  ---   396
 R08  |  841   24   19    9   11   26   10  126    6 |    38   43   31   27   21   25   21    27
 R09E |  913   19   40   19   23   65   19  ---   12 |    36   39   45   56   54   43  ---    40
 R10E | 3417   21   29   15   15   50   28  ---   11 |    70   78   71   75   99   72  ---    73
 R11E | 1550   45   85   38   40   63   52  204   23 |    48   57   89   81   64   50  115    60
 R12E | 1142   18   29   13   21   44   23  ---   10 |    49   71   57   62   75   47  ---    54
 R13E | 1030   25   22   12   24   36   21  ---    9 |    38   58   51   44   40   39  ---    42
 R15E | 4632   20   30   15   29   37   17  133   10 |    21   35   31   33   32   28   20    23
 R16E | 1140   23   34   16   30   42   15  ---   11 |    27   48   48   52   53   35  ---    38
 R17  | 2342   53   27   34   39   92   21  ---   18 |    30   46   64   56   54   62  ---    48
 R18  | 1214   44   18    8   17   44   18  160   10 |    68   39   43   37   42   31   41    38
 R19  | 1207   37   32   16   22   38   13  ---   10 |    71   37   43   46   42   43  ---    43
 R20  | 4942   43   95   23   19   42   31  ---   19 |    48   50   42   41   41   34  ---    33
 R21  | 1108   30   32   10   24   54   21  ---   11 |    58   41   41   50   59   31  ---    40
 R22  |  728   42   21   15   31   43   18  ---   12 |    70   39   39   60   42   33  ---    41
 R23  | 2218   28   30   12   14   33   18  ---    9 |    53   26   34   44   53   25  ---    32
 R24  | 1939   31   16   15   28   35   21  ---   10 |    42   33   26   26   34   24  ---    25
------+----------------------------------------------+------------------------------------------
 RMS  | 2365   32   36   18   24   50   22  160      |T   65   58   58   63   60   55   44    57
 WRMS | 2365   32   35   15   20   47   22  160      |NE  71   53   53   60   55   55   29    57
 MEDI | 1475   28   24   15   22   44   19  160      |MD  48   41   42   45   42   34   27    38




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