[IGSREPORT-21086] Wk 1699 IGLOS Final Orbits

IGS ACC igs.acc at noaa.gov
Fri Aug 17 15:24:22 PDT 2012


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1699   (Jul 29, 2012 - Aug 04, 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 2.1699.
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:
                                                                               
 igl1699[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1699 in the SP3 format.
 igl16997.sum      Combination Report for GPS Week 1699.


    
    
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  |    178.3 ns
                1  |    190.1 ns
                2  |    193.4 ns
                3  |    194.1 ns
                4  |    193.7 ns
                5  |    194.9 ns
                6  |    196.6 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 1.1699, 1a.1699).
        
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 2.1699.0-6)                                                                                
    
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 3.1699.0-6). 
        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 1699 summary.                      (Jul 29, 2012 - Aug 04, 2012)

Table 1.1699.a     GPS week : 1699   MJD: 56137.0-56143.0

         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|   -2     0    -7    71   -26  -215  -.25   30   30 |     ---     ---    ---    ---
        |    1     2     2    20    28    13   .03           |     ---     ---
emx  130|    1     1    -5   -20    28    65  -.23   28   27 |  190455    -444   3943   6615
        |    1     1     2    19    26    15   .05           |    6187    1852
esx  170|    0    -1     0   -16    -3   -35   .38   16   15 |  191877   -1939   3940   4120
        |    0     1     2    23    40    35   .04           |    6167    2041
gfz  194|   -1     0    -3    -9   -13    37  -.25   21   20 |       0   -1412   3943   6422
        |    1     0     2    26    43    25   .05           |       0    1877
grg  120|   -2     2     3    39   -57   118  -.02   41   38 |  147984   -1241   3952  23914
        |    0     1     5    28    19    31   .07           |    8414    2069
iac  n/a|    1     0    13     1    43    65   .01   25   25 |  192510    -636   3938   6528
        |    1     0     6    31    28    62   .04           |    6112    1235
mcc  n/a|   -2     1     9    44   -22   238  -.62  156  156 |     ---     ---    ---    ---
        |   10     6    16    77    80   211   .31           |     ---     ---


Table 1.1699.b     GPS week : 1699   MJD: 56137.0-56143.0   

         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  |   14   12   13   11   16   17   15 |
 R02  |   11   16   12   17   11   10   13 |
 R03  |    8   13   11   11    9    9   13 |
 R04  |   10    9    8   15    8   13   11 |
 R05  |    7   11    8   11   12    7   11 |
 R06  |   10   10   12   11    8   10    9 |
 R07  |    8    9    8   10    9   12   15 |
 R08  |    8    9   10   11    9    7    7 |
 R09  |    9   12   14   11    9    8   12 |
 R10  |    9   11    9    9    7   10    9 |
 R11  |   13   16   18   17   16   18   14 |
 R12  |    7    9   10    9   10   11    9 |
 R13  |    8    8    8   10    9    9    9 |
 R14  |   12   11   12   12   11   13   12 |
 R15  |   10    9    9    9    8   11    9 |
 R16  |   11   11   11   13    9   14   12 |
 R17  |   13   13   12   10   14   11   11 |
 R18  |   10   17    0  ---  ---   21   17 |
 R19  |   33   15    9   12    9    9    9 |
 R20  |   32   22   14   16   16   17   13 |
 R21  |   15   15  282  ---  ---    0   30 |
 R22  |   12   11   12   10   10   11   10 |
 R23  |   14    9   11   10    9    8    9 |
 R24  |   11   12    9   13   13   11   10 |
 R26  |    0    0    0    0  ---  ---  --- |


Table 1.1699.c     GPS week : 1699   MJD: 56137.0-56143.0   

         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 1699 0   |  -46    33   216     289    1153   -9167  84.7  1985  1985 |  178263       0
brd 1699 1   |  -84     6   271    -431    -765   -9189  84.9  1468  1468 |  190136       0
brd 1699 2   | -146    36   148   -3121     545   -8374  85.7  1476  1476 |  193444       0
brd 1699 3   |    3   -72   131     550     823   -3734  84.4  1679  1679 |  194086       0
brd 1699 4   |   53    91   146    1304    -192   -7466  85.8  1481  1481 |  193687       0
brd 1699 5   |  -10   128    49    -247     522   -3106  84.8  1343  1343 |  194916       0
brd 1699 6   |  -29   -11   175     869    -432   -7111  83.9  1561  1561 |  196622       0
-------------+------------------------------------------------------------+----------------
brd 1699 mean|  -37    30   162    -112     236   -6878  84.9  1570  1570 |  191593       0
brd 1699 sdev|   64    66    69    1457     706    2494    .7   209   209 |    6193       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 2.1699.0  GPS week: 1699   Day: 0   MJD: 56137                            

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   102   -41  -216  -.23   31   31 |     ---     ---    ---    ---
emx  130|    1     0    -2     7    21    73  -.24   28   29 |  177599   -1428   3866   6725
esx  170|    0     0    -1    -8   -17   -68   .33   14   13 |  178830   -3118   3792   3984
gfz  194|   -1     1    -7   -48    -3    49  -.27   18   17 |       0   -3195   3800   6545
grg  120|   -2     4     1    79   -44   106  -.05   40   40 |  137651   -3401   3846  13136
iac  n/a|    1     0    17   -38    60   115  -.01   24   24 |  179436    -753   3788   6818
mcc  n/a|    1    -2    39    37   -37   391 -1.05  190  190 |     ---     ---    ---    ---

Table 2.1699.1  GPS week: 1699   Day: 1   MJD: 56138                            

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|   -4     0    -3    63   -73  -221  -.23   30   30 |     ---     ---    ---    ---
emx  130|    4     0    -6   -14   -23    56  -.16   34   29 |  188009     631   3970   6449
esx  170|    0     0     0   -43   -70   -58   .36   19   19 |  190955   -3632   3990   4169
gfz  194|    0     0     0    28    58    53  -.29   20   19 |       0   -1459   3981   6191
grg  120|   -1     2    -2     1   -64   111   .02   50   47 |  156874   -1258   4077  68669
iac  n/a|    0     0    10    25    79    44   .05   24   24 |  191206   -1377   3988   6308
mcc  n/a|    6     2    -3    73    92    82  -.89  160  160 |     ---     ---    ---    ---

Table 2.1699.2  GPS week: 1699   Day: 2   MJD: 56139                            

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    -8    91   -44  -226  -.27   32   35 |     ---     ---    ---    ---
emx  130|    2     2    -6     3    35    36  -.20   26   24 |  190976    2419   3535   7203
esx  170|    0    -2     0   -19   -35    -5   .38   16   15 |  191458    1997   3527   3703
gfz  194|    0    -1    -1   -40     4    60  -.26   22   21 |       0    2401   3523   6847
grg  120|   -2     2    -3    49   -32   126  -.09   35   34 |  150338    2872   3519  21335
iac  n/a|    2     1    11    10    72    21   .01   24   24 |  192922    1545   3518   6667
mcc  n/a|    8     3    10    82   -20   118  -.24  191  191 |     ---     ---    ---    ---

Table 2.1699.3  GPS week: 1699   Day: 3   MJD: 56140                            

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     4    -7    62    11  -235  -.22   32   34 |     ---     ---    ---    ---
emx  130|    1     2    -3   -41    17    70  -.23   25   27 |  192729    -187   3910   7088
esx  170|    0    -2     1    14    -3   -78   .36   18   16 |  193788    -811   3906   4050
gfz  194|    0     0    -1     0     6    17  -.24   24   21 |       0   -1423   3927   6737
grg  120|   -2     2     4    50   -71   102  -.06   42   39 |  160038    -995   3900  20581
iac  n/a|    0     1     7   -34    35   119   .00   26   26 |  196162   -1020   3906   6705
mcc  n/a|    2    -8    -5  -111    -5   553  -.60  132  132 |     ---     ---    ---    ---

Table 2.1699.4  GPS week: 1699   Day: 4   MJD: 56141                            

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     3    -6    80    -8  -200  -.30   28   28 |     ---     ---    ---    ---
emx  130|   -1     0    -4   -36    53    70  -.29   28   28 |  194329   -3637   3939   5785
esx  170|    0     0     1     3    36   -42   .42   13   11 |  195234   -3736   3939   4137
gfz  194|   -1     0    -2     0   -66    -8  -.32   22   19 |       0   -3227   3941   5733
grg  120|   -1     2     7     5   -36   127  -.02   42   38 |  142255   -3242   3938  14093
iac  n/a|    2     0     4     3     0   144  -.06   25   25 |  195387   -2409   3939   6134
mcc  n/a|   -5     6    19    53  -164   279  -.45  130  130 |     ---     ---    ---    ---

Table 2.1699.5  GPS week: 1699   Day: 5   MJD: 56142                            

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|   -3     1    -8    53    -5  -203  -.28   26   26 |     ---     ---    ---    ---
emx  130|    1     0    -7   -29    48    62  -.19   28   28 |  194192    -537   4140   6822
esx  170|    2    -1    -3   -48    38    10   .41   18   17 |  195961   -2721   4181   4392
gfz  194|   -2     0    -6    -6   -56    34  -.18   23   19 |       0   -1729   4192   6630
grg  120|   -1     4    10    55   -74    78  -.03   41   38 |  140545   -1453   4172  14714
iac  n/a|   -1     0    21    -3    31    37   .06   25   25 |  195214      95   4171   6849
mcc  n/a|  -13    -3     9    33    39   -76  -.83  139  139 |     ---     ---    ---    ---

Table 2.1699.6  GPS week: 1699   Day: 6   MJD: 56143                            

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|   -3    -1   -10    47   -25  -204  -.25   29   29 |     ---     ---    ---    ---
emx  130|    2     1    -8   -35    45    87  -.28   25   24 |  195354    -375   4246   6238
esx  170|    1     0     1   -14    27    -4   .42   16   14 |  196916   -1552   4247   4408
gfz  194|   -2     0    -4     1   -39    56  -.23   21   24 |       0   -1257   4243   6275
grg  120|   -2     0     3    32   -77   179   .11   39   33 |  148190   -1214   4218  14876
iac  n/a|    2     1    20    48    27   -26   .03   26   26 |  197246    -539   4256   6218
mcc  n/a|  -20    11    -6   142   -58   317  -.30  153  153 |     ---     ---    ---    ---

       
       
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 3.1699.0  GPS week: 1699   Day: 0   MJD: 56137                            

        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  | 1142   42   32   15   24   68   21  ---   13 |    81   43   60   65   69   48  ---    55
 R02  | 1049   45   34    6   17   21   24  ---   10 |    70   30   41   46   31   33  ---    38
 R03  | 1022   32   22   13   12   26   10  ---    8 |    60   73   73   58   48   55  ---    61
 R04  | 1042   18   16   10    9   53   25  ---    9 |    54   39   46   50   43   56  ---    46
 R05  | 1198   13   12   10   15   24   19   77    6 |    60   53   60   64   53   54   19    57
 R06  | 2055   22   28   13   11   34   28  ---    9 |    94   82   83   81   96   80  ---    82
 R07  | 1038   29   27   12   19   17   11  ---    8 |    76   65   60   67   62   56  ---    61
 R08  | 1491   21   29    7   12   20   21  174    7 |    60   60   57   52   50   49   24    53
 R09  | 1008   37   16   14   11   30   22  ---    9 |    28   30   37   33   46   37  ---    30
 R10  | 3081   18   22   18   18   34   17  ---    9 |    24   26   26   23   32   23  ---    20
 R11  | 1926   55   26   20   19   38   31  238   13 |    26   46   51   52   38   38   73    39
 R12  | 1129   20   17    7   18   23   14  ---    7 |    18   17   19   29   28   14  ---    15
 R13  | 1152   26   19    7   17   11   20  ---    7 |    25   19   21   29   27   18  ---    18
 R14  | 2451   45   32   12   17   25   31  ---   11 |    23   39   35   43   39   24  ---    31
 R15  | 2043   21   21   14   23   44   22   74   10 |    26   25   30   26   25   20   50    21
 R16  | 1694   44   22   14   18   41   23  ---   11 |    23   42   34   35   44   23  ---    26
 R17E | 2371   32   34   18   18   49   38  192   13 |    31   42   54   46   41   37   37    41
 R18E | 4597   19   34   18   16   32   21  285   10 |  9999   10    5   29   23 9999   10  9999
XR19E | 2757   43  ---   40   87  ---   39  ---   33 |    38  ---   39   88  ---   26  ---    36
XR20E | 3506   44  ---   28   95   90   57  ---   32 |    42  ---   53  107   81   55  ---    51
 R21E | 1635   34   56   19   36   40   27  ---   15 |  9999   39   36   48   44 9999  ---  9999
 R22E | 1705   33   33   19   18   34   30  ---   11 |    32   30   42   42   46   30  ---    32
 R23E | 2690   25   19    9   18   92   22  ---   14 |    24   30   30   39   79   27  ---    28
 R24E | 1935   20   38   11   15   44   32  ---   11 |    96   75   94   99  133   76  ---    91
XR26E | ----  ---  ---  ---  ---  ---   13  ---    0 |   ---  ---  ---  ---  --- 9999  ---  9999
------+----------------------------------------------+------------------------------------------
 RMS  | 1985   31   28   14   18   40   24  190      |T   45   41   45   52   51   39   35    42
 WRMS | 1985   31   29   13   17   40   24  190      |NE  46   43   45   47   45   39   41    40
 MEDI | 1694   29   26   13   18   34   22  174      |MD  32   39   41   46   44   37   24    38

Table 3.1699.1  GPS week: 1699   Day: 1   MJD: 56138                            

        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  |  664   43   37   16   20   45   16  ---   12 |    50   42   34   32   63   34  ---    34
 R02  |  857   50   39   22   20   77   26  ---   16 |    52   33   28   42   58   28  ---    28
 R03  |  922   22   35   23   12   65   22  ---   12 |    49   56   58   47   35   44  ---    44
 R04  |  997   23   18   24   14   19   15  ---    8 |    48   37   25   44   49   42  ---    35
 R05  |  953   22   24   16   24   39   25   57   10 |    41   32   41   51   34   41   24    37
 R06  | 2809   21   15   28   14   21   20  ---    9 |    66   68   76   77   83   73  ---    73
 R07  |  847   11   24   13   13   22   29  ---    8 |    48   50   59   56   43   41  ---    49
 R08  |  782   28   22   14   19   22   22  145    9 |    45   38   37   38   42   41   26    35
 R09  | 1210   32   26   23   25   43   18  ---   11 |    28   32   34   50   63   37  ---    35
 R10  | 1918   20   21   15    9   71   18  ---   11 |    21   29   32   21   64   24  ---    19
 R11  | 1855   57   29   29   18   55   28  237   15 |    19   49   60   45   52   34   73    39
 R12  | 1220   24   17   19   17   33   17  ---    9 |    23   24   38   34   27   16  ---    23
 R13  | 1420   23   21   10   16   28   18  ---    8 |    24   28   25   22   43   17  ---    19
 R14  | 1074   33   40   12   17   23   26  ---   11 |    20   40   28   26   24   21  ---    19
 R15  | 1270   15   24   15   14   38   22  146    9 |    30   21   30   23   28   19   49    17
 R16  | 1397   36   26   15   13   42   20  ---   10 |    21   27   29   20   37   20  ---    19
 R17E | 1727   22   51   20   22   38   30  161   13 |    41   58   51   48   49   39   43    42
XR18E |14150   16   34  ---   21   75   24  297   16 |  9999   18  ---   33   32 9999   10  9999
 R19E |  976   25   47   17   20   75   32  ---   15 |    35   62   48   53   77   29  ---    39
 R20E |  872   40   68   21   35  115   36  ---   21 |    41   59   69   78  119   53  ---    59
 R21E | 1255   34   54   25   27   46   26  ---   15 |  9999   24   37   39   41 9999  ---  9999
 R22E | 1341   30   30   16   22   29   21  ---   10 |    35   30   49   45   43   27  ---    35
 R23E | 3074   19   24   10   17   36   22  ---    9 |    19   29   30   38   64   22  ---    24
 R24E | 1433   25   31   13   25   45   31  ---   12 |    61   45   69   80   94   43  ---    62
XR26E | ----  ---  ---  ---  ---  ---    8  ---    0 |   ---  ---  ---  ---  --- 9999  ---  9999
------+----------------------------------------------+------------------------------------------
 RMS  | 1467   30   34   19   20   50   24  160      |T   37   38   42   43   52   33   37    35
 WRMS | 1467   30   29   19   19   47   24  160      |NE  36   37   39   39   46   33   43    32
 MEDI | 1220   24   26   16   18   39   22  146      |MD  35   33   37   42   43   34   26    35

Table 3.1699.2  GPS week: 1699   Day: 2   MJD: 56139                            

        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  |  609   55   23   24   25   15   22  ---   12 |    58   32   33   38   33   40  ---    31
 R02  | 1172   32   47    8   19   25   22  ---   11 |    57   44   47   41   49   53  ---    43
 R03  |  797   23   34   17   22   37   21  ---   11 |    54   58   64   70   37   44  ---    55
 R04  | 1022   17   15    6   21   29   14  ---    7 |    50   41   45   52   43   33  ---    42
 R05  | 1186   25   14   20   14   19   14   59    8 |    43   37   40   45   55   38   35    39
 R06  | 3076   30   22   13   28   37   30  ---   11 |   108   85   97   97  103   93  ---    94
 R07  | 1156   17   16   10   20   29   20  ---    8 |    56   58   72   69   45   79  ---    65
 R08  | 1021   15   18   26   14   20   29  125   10 |    51   48   82   60   67   41   53    59
 R09  | 1178   37   14   20   12   75   24  ---   14 |    32   28   32   36   88   30  ---    32
 R10  | 1902   24   19   12   16   34   19  ---    9 |    28   22   30   34   55   20  ---    25
 R11  | 1388   73   46   26   28   43   29  328   18 |    15   74   70   58   58   47  159    52
 R12  | 1440   27   18    8   21   37   23  ---    9 |    16   20   24   30   40   20  ---    18
 R13  | 1903   22   10   10   20   32   12  ---    7 |    21   19   27   31   25   14  ---    16
 R14  | 1424   27   35   17   22   38   26  ---   12 |    27   38   44   46   59   35  ---    36
 R15  | 1011   19   23   17   17   17   18  170    8 |    27   31   24   25   25   12  103    18
 R16  | 1080   45   27    8   20   23   21  ---   10 |    33   33   29   33   34   32  ---    24
 R17E | 1123   26   27   13   22   48   32  163   12 |    31   35   39   51   57   25   77    33
XR18E | ----  ---  ---  ---  ---  ---    9  ---    0 |   ---  ---  ---  ---  --- 9999  ---  9999
 R19E | 1025   17   24   11   23   25   26  ---    9 |    29   38   30   40   41   23  ---    25
 R20E |  984   28   34   24   33   38   35  ---   14 |    41   44   50   68   24   30  ---    36
XR21E | ----  227  ---  ---  ---  ---  313  ---  282 |  9999  ---  ---  ---  --- 9999  ---  9999
 R22E | 1946   28   30   14   23   35   28  ---   11 |    49   45   51   58   63   35  ---    45
 R23E | 2444   19   16   10   24   39   32  ---   10 |    18   27   36   43   47   27  ---    30
 R24E | 1170   27   24   13   21   21   22  ---    9 |    60   47   57   59   74   62  ---    56
XR26E | ----  ---  ---  ---  ---  ---    8  ---    0 |   ---  ---  ---  ---  --- 9999  ---  9999
------+----------------------------------------------+------------------------------------------
 RMS  | 1476   32   26   16   22   35   24  191      |T   41   41   46   49   51   37   85    39
 WRMS | 1476   35   24   15   21   34   24  191      |NE  42   41   47   47   51   39   87    40
 MEDI | 1170   27   23   13   21   32   22  163      |MD  33   38   40   45   47   33   77    36

Table 3.1699.3  GPS week: 1699   Day: 3   MJD: 56140                            

        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  | 1216   42   22   12   28   24   15  ---   10 |    73   39   53   58   56   45  ---    49
 R02  |  873   56   17   44   25   16   39  ---   16 |    63   28   52   48   42   54  ---    36
 R03  | 1084   21   31   19   12   24   33  ---   10 |    62   65   68   59   71   36  ---    57
 R04  |  764   32   17   17   26   87   28  ---   15 |    57   50   47   60   58   54  ---    46
 R05  | 1096   17   27    8   33   22   34  130   11 |    52   68   59   75   64   43   36    55
 R06  | 1826   15   24   19   19   48   20  ---   10 |    55   49   61   61   48   45  ---    51
 R07  | 1515   23   30   11   21   30   16  ---    9 |    70   48   74   79   61   74  ---    67
 R08  | 1714   22   20   19   22   49   22  128   11 |    54   78   74   61   33   72   23    64
 R09  | 1613   33   11   18   20   47   17  ---   10 |    33   33   36   44   66   35  ---    35
 R10  | 1749   13   19   20   15   29   21  ---    8 |    40   36   45   43   45   26  ---    35
 R11  | 1229   59   39   29   29   44   28  118   16 |    17   63   71   66   50   35  105    47
 R12  | 1654   25   17    8   16   38   17  ---    8 |    18   27   29   31   36   21  ---    22
 R13  | 1783   29   13   11   25   41   15  ---    9 |    19   19   26   40   30   22  ---    19
 R14  | 1918   41   34   11   28   21   18  ---   11 |    29   43   44   52   47   35  ---    38
 R15  |  975   33   16   13   19   24   17  188    9 |    28   26   20   23   21   23  124    16
 R16  | 1169   51   27    7   21   41   23  ---   12 |    28   43   38   44   53   39  ---    32
 R17E | 1036   25   28   16   21   31   21   68   10 |    57   50   59   53   48   42   61    49
 R19E |  770   20   31   19   27   46   29  ---   12 |    26   32   39   46   48   20  ---    27
 R20E | 3165   21   29   19   36   66   44  ---   15 |    69   46   73   78   89   76  ---    67
 R22E | 1196   17   28   19   16   31   20  ---    9 |    29   34   41   40   43   33  ---    32
 R23E | 3558   20   27   11   19   42   17  ---    9 |    31   37   38   46   40   33  ---    34
 R24E | 1828   21   31   10   30   45   38  ---   12 |    67   48   66   75   87   48  ---    60
XR26E | ----  ---  ---  ---  ---  ---    8  ---    0 |   ---  ---  ---  ---  --- 9999  ---  9999
------+----------------------------------------------+------------------------------------------
 RMS  | 1678   32   25   18   24   42   25  132      |T   44   43   50   53   51   41   69    42
 WRMS | 1678   34   27   16   21   39   25  132      |NE  43   44   49   52   48   41   72    41
 MEDI | 1229   23   27   16   21   38   21  128      |MD  40   43   47   52   48   36   61    38

Table 3.1699.4  GPS week: 1699   Day: 4   MJD: 56141                            

        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  | 1404   34   36   13   23   95   23  ---   15 |    63   36   66   65  112   51  ---    57
 R02  |  795   27   36   14   23   21   25  ---   10 |    63   27   63   51   65   43  ---    51
 R03  | 1419   28   33   10   18   16   22  ---    9 |    56   64   46   49   49   43  ---    47
 R04  |  709   24   15    7   13   42   15  ---    8 |    45   43   46   46   30   39  ---    39
 R05  | 1024   20   40   16   24   52   24  145   12 |    53   57   60   59   83   44   27    53
 R06  | 1221   13   17    8   16   34   23  ---    7 |    58   63   56   58   44   60  ---    55
 R07  |  901   24   26    9   20   21   22  ---    8 |    58   38   51   63   71   35  ---    50
 R08  | 1290   23   19   10   19   38   25  110    9 |    47   42   55   59   40   57   25    49
 R09  | 1787   33   28    5   17   32   18  ---    9 |    22   24   24   26   47   28  ---    20
 R10  | 1309   13   12   12   15   26   20  ---    7 |    23   18   31   27   33   24  ---    22
 R11  | 1385   55   26   20   37   57   26   99   15 |    28   54   45   58   60   34   64    38
 R12  |  945   31   14   10   22   51   21  ---   10 |    17   24   32   36   57   18  ---    23
 R13  | 1266   27   15   15   12   34   17  ---    8 |    17   19   33   24   35   19  ---    18
 R14  | 2136   37   26   11   20   41   22  ---   10 |    18   36   42   42   57   28  ---    32
 R15  | 1077   22   15   11   18   19   22  182    7 |    18   23   26   33   21   13   52    17
 R16  | 1487   35   17   10   16   24   22  ---    9 |    18   29   32   35   24   21  ---    23
 R17E | 1288   30   36   18   36   33   38   89   13 |    46   58   81   90   75   53   38    68
 R19E | 1350   18   32   11   12   35   21  ---    9 |    24   27   27   31   31   19  ---    21
 R20E | 2930   22   39   20   36   54   46  ---   15 |    67   77   73   94   63   49  ---    68
 R22E |  794   20   25    9   22   36   26  ---    9 |    36   43   43   57   63   39  ---    43
 R23E | 2244   13   26   12   12   30   26  ---    8 |    29   30   31   28   38   28  ---    26
 R24E | 1768   21   43   16   20   46   32  ---   12 |    50   60   51   47   57   57  ---    48
------+----------------------------------------------+------------------------------------------
 RMS  | 1481   28   28   13   22   42   25  130      |T   38   40   46   49   52   36   41    39
 WRMS | 1481   28   28   11   19   38   25  130      |NE  37   37   44   45   51   34   42    37
 MEDI | 1290   24   26   11   19   34   22  110      |MD  36   36   45   47   49   35   38    39

Table 3.1699.5  GPS week: 1699   Day: 5   MJD: 56142                            

        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  |  966   34   65   19   28   42   25  ---   16 |    49   24   47   66   67   61  ---    45
 R02  | 1059   26   33   12   15   27   22  ---   10 |    45   28   52   44   52   39  ---    42
 R03  | 1109   23   14   21   12   26   26  ---    9 |    47   31   55   43   65   35  ---    43
 R04  |  886   36   20   34   21   19   29  ---   12 |    39   30   40   34   30   31  ---    24
 R05  | 1082   12   15   16   10   21   16  149    6 |    40   42   39   41   59   55   24    43
 R06  |  838   15   15   21   11   58   15  ---   10 |    46   50   47   57   81   58  ---    51
 R07  | 1179   31   19   27   13   41   23  ---   11 |    60   43   47   49   84   39  ---    47
 R08  | 1342   18   16   10   16   25   15  120    7 |    37   33   31   46   45   46   17    37
 R09  | 1434   24   12   10   18   31   19  ---    8 |    23   24   25   33   37   18  ---    22
 R10  | 1184   21   23   14   19   42   23  ---   10 |    33   30   31   32   38   35  ---    26
 R11  | 2195   51   44   25   45   43   31  102   18 |    22   34   47   58   43   22   31    29
 R12  | 1189   29   15   12   23   48   17  ---   10 |    25   34   28   32   57   27  ---    27
 R13  | 1003   15   11   15   20   42   15  ---    8 |    16   22   22   35   49   17  ---    19
 R14  | 1378   30   36   21   19   40   25  ---   12 |    28   54   49   48   47   33  ---    38
 R15  |  936   20   33   17   29   21   28  199   11 |    17   16   15   26   23   21   54    10
 R16  |  996   37   15   16   38   51   28  ---   13 |    24   27   33   54   37   24  ---    25
 R17E | 1231   15   20   19   23   41   34   98   11 |    58   60   70   74   67   55   33    61
XR18E | ----   21  ---  ---  ---  ---   20  ---   21 |  9999  ---  ---  ---  --- 9999  ---  9999
 R19E | 1348   25   19   16   17   23   20  ---    9 |    19   25   24   29   27   16  ---    18
 R20E | 2932   29   43   20   32   80   36  ---   17 |    62   66   55   61  105   45  ---    57
XR21E | ----   13  ---  ---  ---  ---  ---  ---    0 |  9999  ---  ---  ---  ---  ---  ---  9999
 R22E |  939   14   15   13   22   57   29  ---   11 |    26   38   36   41   66   30  ---    32
 R23E | 1571   14   19   12   18   25   23  ---    8 |    25   46   37   34   35   28  ---    31
 R24E |  885   19   31   12   21   37   26  ---   10 |    37   44   45   44   35   39  ---    36
------+----------------------------------------------+------------------------------------------
 RMS  | 1343   26   28   18   23   41   25  139      |T   35   36   39   44   52   35   31    34
 WRMS | 1343   26   28   17   19   38   25  139      |NE  34   32   38   43   50   35   31    33
 MEDI | 1109   21   19   16   19   40   23  120      |MD  33   33   39   43   47   33   31    32

Table 3.1699.6  GPS week: 1699   Day: 6   MJD: 56143                            

        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  | 1013   44   47   14   14   48   31  ---   14 |    83   35   58   64   64   75  ---    58
 R02  |  763   43   43   13   25   26   22  ---   13 |    78   36   47   60   54   50  ---    48
 R03  | 1210   41   33   21   16   22   36  ---   12 |    71   78   92   80   73   61  ---    77
 R04  |  811   19   24   21   18   34   28  ---   10 |    52   46   78   62   84   56  ---    60
 R05  | 1223   22   16   26   17   35   33  136   11 |    60   55   48   56   78   68   22    54
 R06  |  785   11   18    7   21   32   26  ---    8 |    65   54   62   66   84   75  ---    64
 R07  |  974   28   17   12   21   90   23  ---   14 |    81   64   68   69   86   57  ---    65
 R08  | 2888   17   12    7   18   27   14  162    6 |    64   77   72   77   64   73   26    71
 R09  | 1312   34    7   17   32   38   33  ---   12 |    16   29   33   42   35   22  ---    24
 R10  | 2350   12   18   12   18   34   22  ---    8 |    32   33   38   39   37   25  ---    32
 R11  | 1781   44   37   19   23   47   30  119   14 |    28   73   53   62   73   40   47    48
 R12  |  890   32   19    8   18   30   18  ---    9 |    18   29   24   31   46   20  ---    21
 R13  | 1466   22   18   12   28   27   17  ---    9 |    17   23   29   36   30   24  ---    22
 R14  | 1223   32   25   19   20   44   21  ---   11 |    25   39   41   34   49   24  ---    31
 R15  | 1357   20   19   12   12   27   29  216    8 |    19   24   18   22   25   18   50    13
 R16  | 1124   40   16   14   25   35   28  ---   11 |    16   27   37   43   38   25  ---    27
 R17E | 1576   28   26   15   28   24   24  105   10 |    41   53   46   49   38   39   38    40
XR18E | ----   17  ---  ---  ---  ---   17  ---   17 |  9999  ---  ---  ---  --- 9999  ---  9999
 R19E | 1188   26   16   14   17   32   18  ---    8 |    23   36   30   38   42   24  ---    27
 R20E | 3309   26   30   16   25   57   29  ---   13 |    36   41   38   37   69   33  ---    31
XR21E | ----   35  ---  ---  ---  ---   24  ---   29 |  9999  ---  ---  ---  --- 9999  ---  9999
 R22E | 1367   22   20   18   17   33   24  ---    9 |    31   44   39   40   41   34  ---    33
 R23E |  887   14   19   11   21   33   25  ---    9 |    25   38   30   33   43   28  ---    28
 R24E | 1726   20   22   20   19   35   19  ---    9 |    40   39   42   42   50   40  ---    37
------+----------------------------------------------+------------------------------------------
 RMS  | 1560   29   25   16   21   39   26  153      |T   41   44   46   49   54   41   36    41
 WRMS | 1560   29   24   14   24   33   26  153      |NE  45   45   49   52   57   44   36    44
 MEDI | 1223   26   19   14   19   33   24  136      |MD  32   39   41   42   49   34   38    33




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