[IGSREPORT-20554] Wk 1672 IGLOS Final Orbits

IGS ACC igs.acc at noaa.gov
Thu Feb 9 07:53:38 PST 2012


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1672   (Jan 22, 2012 - Jan 28, 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 2.1672.
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:
                                                                               
 igl1672[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1672 in the SP3 format.
 igl16727.sum      Combination Report for GPS Week 1672.


    
    
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  |    177.2 ns
                1  |    174.2 ns
                2  |    174.2 ns
                3  |    170.0 ns
                4  |    170.0 ns
                5  |    165.0 ns
                6  |    165.1 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   | R15
                3  |  GRG   | R15
                4  |  GRG   | R02 R15
                5  |  GRG   | R15
                6  |  GRG   | R15

    
         
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 1.1672, 1a.1672).
        
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 2.1672.0-6)                                                                                
    
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 3.1672.0-6). 
        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 1672 summary.                      (Jan 22, 2012 - Jan 28, 2012)

Table 1.1672.a     GPS week : 1672   MJD: 55948.0-55954.0

         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  251|    0     0    -3    -1   -49    -9  -.33   32   31 |     ---     ---    ---    ---
        |    1     1     3    14    25    45   .06           |     ---     ---
emx  137|    1     0     2  -128    25     0  -.32   32   32 |  170906    -757   3811   7208
        |    0     1     8    43    40    33   .03           |    4469    1944
esx  130|    0     0     0    56    77   -51   .29   21   18 |  172531   -1989   3825   3983
        |    0     2     4    25    39    20   .04           |    3878    2626
gfz  191|    0    -2    -8    13   -72     9   .21   25   22 |       0   -1091   3828   7314
        |    1     0     3    33    38    28   .05           |       0    2476
grg  123|   -1     3    -3    24   -65   130  -.07   48   43 |  167384    -867   3824  23663
        |    1     1     2    46    41    82   .09           |   15556    2517
iac  n/a|    0     0     7     5    16   -10  -.11   27   27 |  172152    -640   3824   8410
        |    1     2    10    34    37    51   .06           |    4413    2146
mcc  n/a|    0    -4    59   -33   -30  1230  -.20  180  180 |     ---     ---    ---    ---
        |   24    14    21   231   182   766   .52           |     ---     ---


Table 1.1672.b     GPS week : 1672   MJD: 55948.0-55954.0   

         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  |   16   12   14   10   16   12   11 |
 R02  |   10   12   10   10   12   10   10 |
 R03  |   18   11   15   12   12    9    9 |
 R04  |    9   13   14   12   12    9   12 |
 R05  |   12   15   15   10   14   10    9 |
 R06  |   10   13   10   11   10   12   11 |
 R07  |   11   11   12   11   18   11   11 |
 R08  |   10   12   21   16   13   17   13 |
 R09  |   12   15   12    9   10   10    9 |
 R10  |   12   10    8    8    9    9   11 |
 R11  |   18   17   20   22   17   18   12 |
 R12  |   11   12   12   13   14   10    9 |
 R13  |   11   13   13   11   10   10    9 |
 R14  |   10   10   11   15   12   10   11 |
 R15  |   10    0    0    0    0    0    0 |
 R16  |   11    8   12   10    9   12   10 |
 R17  |   18   11   12   16   13   13   13 |
 R18  |    9   15    9   13   10   12   12 |
 R19  |   11   14   21    9   10   10   12 |
 R20  |   18   19   24   21   18   18   17 |
 R21  |   13   15   16   17   15   12   18 |
 R22  |   15   31   13   11   14   14   11 |
 R23  |   16   11    9   12   12   10   13 |
 R24  |   13   14    9   11   11   12   14 |


Table 1.1672.c     GPS week : 1672   MJD: 55948.0-55954.0   

         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 1672 0   | -108   -41    11    -796    3336   -5319  82.4  1943  1943 |  177198       0
brd 1672 1   |   35    58   -21    -210     213   -5856  85.0  1455  1455 |  174170       0
brd 1672 2   |  -39     0   138     682    -761  -10380  83.5  1330  1330 |  174235       0
brd 1672 3   |  -68    38    30    -270   -1059   -4683  84.3  1850  1850 |  170043       0
brd 1672 4   | -117    20   130   -1808    2372   -8598  84.9  1895  1895 |  169962       0
brd 1672 5   |  -34  -224    69    2093     712   -5345  83.3  1721  1721 |  165010       0
brd 1672 6   |  -23    40    13    -528     537   -7869  82.6  1488  1488 |  165057       0
-------------+------------------------------------------------------------+----------------
brd 1672 mean|  -50   -15    53    -119     764   -6864  83.7  1668  1668 |  170810       0
brd 1672 sdev|   52    97    62    1227    1592    2115   1.1   243   243 |    4688       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 2.1672.0  GPS week: 1672   Day: 0   MJD: 55948                            

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  251|   -1     2     2   -12   -99    56  -.22   33   33 |     ---     ---    ---    ---
emx  137|    1     0     8  -173   -25   -27  -.29   27   27 |  177011    1232   3473   7388
esx  130|   -2     1     4    31    -7   -53   .35   22   18 |  176544    1581   3521   3709
gfz  191|   -2     0   -13    70    -3   -19   .28   27   21 |       0    1038   3520   7632
grg  123|    2     2    -1    68    -8   159  -.08   43   43 |  143913    2032   3536  19329
iac  n/a|    1    -3    -2    59    89   -30  -.16   29   29 |  177526     882   3519   8638
mcc  n/a|   26     6    77   300   -86   320   .05  164  164 |     ---     ---    ---    ---

Table 2.1672.1  GPS week: 1672   Day: 1   MJD: 55949                            

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  251|   -2     0    -4   -23   -51    34  -.32   35   32 |     ---     ---    ---    ---
emx  137|    0     1    12  -105    35    38  -.32   33   33 |  175153   -1384   3736   7408
esx  130|    0     0     4    37    84   -55   .22   21   19 |  176460   -3115   3737   3887
gfz  191|    1    -2    -2    10  -110    63   .17   25   22 |       0   -1142   3743   7329
grg  123|    0     4    -4    98   -71   159  -.21   54   51 |  159617   -1594   3737  26291
iac  n/a|   -3     0    -7    31    35  -102  -.12   37   37 |  176626   -3695   3749   8197
mcc  n/a|   11    -9    69  -177    32   384  -.05  157  157 |     ---     ---    ---    ---

Table 2.1672.2  GPS week: 1672   Day: 2   MJD: 55950                            

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  251|    1     0    -4    -1   -43    10  -.32   32   32 |     ---     ---    ---    ---
emx  137|    1     1    10   -60     4    13  -.32   34   36 |  173337     734   3812   6754
esx  130|    0     1    -1    70   101    -9   .27   21   17 |  174050     920   3827   3968
gfz  191|    0    -1   -10   -34   -77    -3   .26   28   23 |       0    1888   3840   6841
grg  123|   -2     1     0   -19  -139    36  -.12   65   48 |  153108    1907   3828  21522
iac  n/a|   -1    -1     4   -46     4   -15  -.19   26   26 |  174459    1421   3834   7819
mcc  n/a|   -8   -26    58  -387    -4   636   .46  176  176 |     ---     ---    ---    ---

Table 2.1672.3  GPS week: 1672   Day: 3   MJD: 55951                            

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  251|    0     1    -2    10   -43   -64  -.32   32   31 |     ---     ---    ---    ---
emx  137|    2    -1     0  -152    48   -40  -.34   39   40 |  170711   -2554   3650   6646
esx  130|    0     2     2    28   107   -40   .33   21   19 |  174415   -5311   3628   3756
gfz  191|   -2    -3    -9    32  -108     3   .19   26   22 |       0   -2522   3630   6789
grg  123|   -3     5    -1     0   -59   157  -.06   41   39 |  171025   -2723   3627  20639
iac  n/a|    2     0     7    19    -7    56  -.12   24   24 |  172017    -749   3642   7985
mcc  n/a|  -48    -8    52  -192  -390  1395  -.89  250  250 |     ---     ---    ---    ---

Table 2.1672.4  GPS week: 1672   Day: 4   MJD: 55952                            

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  251|    1    -1    -7     0   -57   -56  -.36   28   27 |     ---     ---    ---    ---
emx  137|    1    -1    -5  -171    84   -28  -.28   33   34 |  168602    1649   3871   7709
esx  130|    0    -2    -6    96    81   -64   .28   21   21 |  171330    -591   3799   4017
gfz  191|    2    -1    -7    13   -44    13   .20   28   25 |       0     731   3809   7700
grg  123|    0     1    -6   -27   -76   273  -.09   51   42 |  176253    1019   3796  28775
iac  n/a|    0     3    18   -10   -22   -14  -.03   22   22 |  170905     963   3808   8891
mcc  n/a|    3   -12    85   123    47  2028   .27  243  243 |     ---     ---    ---    ---

Table 2.1672.5  GPS week: 1672   Day: 5   MJD: 55953                            

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  251|    0     0    -5    -5   -20   -10  -.37   30   28 |     ---     ---    ---    ---
emx  137|    0     2    -6  -142   -18    43  -.36   28   27 |  166259   -3229   3609   7221
esx  130|    0    -2    -4    78   100   -69   .29   22   18 |  167532   -3592   3601   3741
gfz  191|   -1    -1    -8    16   -65   -16   .16   22   20 |       0   -5072   3604   7409
grg  123|   -2     4    -4    15   -75    75   .10   40   35 |  184327   -4360   3610  21183
iac  n/a|    0     2    21    -5    21     0  -.05   24   24 |  168004   -3541   3594   8618
mcc  n/a|   -4    10    51    69   -15  1895  -.41  145  145 |     ---     ---    ---    ---

Table 2.1672.6  GPS week: 1672   Day: 6   MJD: 55954                            

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  251|    1     0     0    22   -26   -35  -.41   32   31 |     ---     ---    ---    ---
emx  137|    1     0    -6   -91    52     6  -.29   27   26 |  165274   -1747   4527   7336
esx  130|    0     0     4    55    73   -64   .33   19   16 |  167389   -3818   4663   4803
gfz  191|    0    -3    -7   -11   -98    24   .25   22   20 |       0   -2564   4655   7499
grg  123|   -1     3    -5    36   -26    54  -.05   41   40 |  183448   -2351   4634  27905
iac  n/a|    1     1    11    -9    -2    36  -.14   25   25 |  165529     233   4627   8726
mcc  n/a|   20    10    20    26   207  1953  -.80  125  125 |     ---     ---    ---    ---

       
       
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 3.1672.0  GPS week: 1672   Day: 0   MJD: 55948                            

        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  |  892   22   35   14   58   44   21  ---   15 |    52   68   67   71   39   45  ---    57
 R02  | 1090   20   21   13   31   27   24  ---   10 |    55   31   30   52   56   27  ---    34
 R03  |  792   18   30   46   44   64   19  ---   17 |    61   49   57   86   72   52  ---    54
 R04  |  722   27   18   16   18   27   21  ---    9 |    72   61   58   71   70   49  ---    59
 R05  | 1151   35   32   24   13   33   20  153   11 |    70   43   40   50   58   41   31    44
 R06  | 2599   38   25   11   20   24   21  ---   10 |    64   49   54   55   52   40  ---    49
 R07  | 1756   45   14   15   24   35   22  ---   11 |    75   38   46   56   54   40  ---    46
 R08  | 2138   27   16   17   24   26   24  186   10 |    63   42   40   48   43   31   55    39
 R09  | 2115   39   28   27   11   29   26  ---   12 |    21   50   50   42   42   35  ---    36
XR10  | 1967   24  ---   21   19   37   22  ---   12 |    19  ---   26   32   50   20  ---    24
 R11  | 1093   66   34   30   24   28   46  149   17 |    37   58   58   55   43   46   91    41
 R12  | 1265   29   18   15   24   50   16  ---   11 |    31   31   41   31   47   23  ---    29
 R13  | 1668   35   20   26   18   31   22  ---   11 |    17   24   48   36   46   26  ---    27
 R14  | 1396   32   21   18   18   26   25  ---   10 |    25   34   37   30   35   24  ---    25
 R15  | 5848   28   26   13   18   25   22  ---    9 |     7   10    5    6    6    8  ---    11
 R16  | 1142   42   17   20   20   19   19  ---   10 |    26   51   58   60   48   30  ---    44
 R17E | 1558   32   32   37   29   78   29  ---   17 |    56   79   88   80   77   48  ---    70
 R18E | 1769   19   19   16   15   24   23  ---    8 |    60   71   80   75   87   58  ---    71
 R19  | 1271   30   13    8   25   52   23  ---   11 |    85  101  105  108  133   84  ---    98
 R20  | 1662   30   53   19   31   41   53  ---   17 |    93  112  108  110  104   75  ---    97
 R21  |  788   31   26   15   24   52   27  ---   12 |    94  129  130  120  132  108  ---   117
 R22E |  834   27   19   20   28   49   56  ---   15 |   208  200  206  209  221  178  ---   200
 R23E | 1169   23   28   21   31   81   34  ---   16 |    80   86   95   92  109   76  ---    83
 R24E | 2797   21   38   18   25   39   26  ---   12 |    71   83   89   87   94   66  ---    79
------+----------------------------------------------+------------------------------------------
 RMS  | 1943   33   27   22   27   43   29  164      |T   60   65   67   69   71   51   59    59
 WRMS | 1943   33   27   18   21   43   29  164      |NE  38   40   43   46   48   32   61    36
 MEDI | 1271   29   25   18   24   33   23  153      |MD  60   51   57   56   54   41   55    46

Table 3.1672.1  GPS week: 1672   Day: 1   MJD: 55949                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01M | 1218   20   26   17   28   45   33  ---   12 |    51   61   65   59   44   42  ---    54
 R02  |  727   22   21   16   40   27   21  ---   11 |    33   19   26   49   48   33  ---    25
 R03  |  711   37   14   15   26   24   28  ---   11 |    46   38   44   70   37   39  ---    41
 R04  |  645   18   33   16   40   56   16  ---   13 |    37   29   37   74   81   50  ---    44
 R05  |  976   48   35   11   20   76   14  158   14 |    48   24   26   44   75   23   29    28
 R06  |  892   33   28   28   22   43   27  ---   12 |    44   41   34   49   72   38  ---    37
 R07M | 2094   40   35   16   12   36   19  ---   11 |    51   42   52   49   49   49  ---    45
 R08M | 1182   31   16   14   23   67   18  163   11 |    36   31   18   41   66   26   50    24
 R09  | 2650   33   19   17   24   88   27  ---   14 |    27   35   38   40   82   26  ---    31
 R10  | 1318   15   34   12   16   40   15  ---    9 |    20   25   30   33   36   23  ---    24
 R11  | 2311   54   49   21   25   42   42  150   16 |    36   65   56   61   39   42   36    46
 R12  | 1478   36   28   28   23   24   18  ---   12 |    32   33   39   39   29   18  ---    24
 R13  | 1681   43   21   29   19   49   16  ---   12 |    21   28   43   32   52   23  ---    25
 R14  | 1299   33   22   14   21   42   15  ---   10 |    33   42   39   33   40   31  ---    30
XR15  |13242    6  ---  ---  ---  ---   72  ---    0 |    34  ---  ---  ---  ---    7  ---    33
 R16  |  817   25   19   16   12   26   18  ---    8 |    29   45   43   45   59   24  ---    36
 R17E | 1303   26   32   21   15   38   21  ---   10 |    38   58   59   54   63   44  ---    49
 R18E | 1294   23   25   23   22   84   33  ---   14 |    33   53   64   60   90   47  ---    51
 R19E | 1012   25   26   20   19   71   41  ---   14 |    64   79   81   83   99   54  ---    72
 R20E | 1632   29   60   21   34   69   47  ---   18 |    48   65   75   89  100   48  ---    64
 R21E |  630   41   44   26   18   53   32  ---   15 |    58  106  106   91   88   84  ---    88
 R22E | 1538   76   48   37   38   56  127  ---   30 |   347  353  353  351  348  315  ---   339
 R23E | 1015   19   26   17   17   53   29  ---   11 |    54   66   62   58   93   45  ---    56
 R24E | 2427   27   41   17   23   69   26  ---   14 |    44   60   73   75  115   49  ---    63
------+----------------------------------------------+------------------------------------------
 RMS  | 1455   35   33   21   25   54   37  157      |T   52   60   63   68   78   49   38    55
 WRMS | 1455   32   33   19   22   51   37  157      |NE  33   35   37   47   54   29   32    32
 MEDI | 1294   29   28   17   22   49   26  158      |MD  37   42   44   54   66   39   36    41

Table 3.1672.2  GPS week: 1672   Day: 2   MJD: 55950                            

        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  |  831   23   27   26   27   29   42  ---   13 |    45   57   69   63   50   30  ---    49
 R02  |  749   18   18    8   24   42   26  ---    9 |    49   40   43   52   62   38  ---    37
 R03  |  918   27   25   18   58   38   18  ---   14 |    53   38   43   85   59   36  ---    46
 R04  |  951   22   44   12   43   48   20  ---   13 |    50   32   52   84   85   38  ---    50
 R05  |  982   23   31   34   40   60   23  169   15 |    56   34   70   78   79   39   37    51
 R06  | 1325   27   23   13   16   52   20  ---   10 |    54   42   43   64   81   33  ---    45
 R07  | 2215   36   21   11   30   49   28  ---   12 |    59   35   43   46   60   39  ---    38
 R08  | 1268   33   21   12   23  165   25  183   21 |    47   43   31   41  141   35   72    36
 R09  | 1263   31   12   19   19   67   19  ---   11 |    32   27   28   33   77   23  ---    26
 R10  | 1209   15   25   13   15   19   17  ---    7 |    25   23   31   34   40   18  ---    23
 R11  | 2713   50   66   41   31   44   39  176   20 |    35   50   73   73   42   39   80    48
 R12  | 1640   34   19   21   21   29   33  ---   11 |    25   22   36   37   22   25  ---    23
 R13  | 1139   53   24   19   22   43   18  ---   13 |    31   25   41   48   52   32  ---    29
 R14  | 1071   34   26   15   13   51   17  ---   10 |    28   35   31   30   45   21  ---    23
XR15  | ----    5  ---  ---  ---  ---  ---  ---    0 |    26  ---  ---  ---  ---  ---  ---    27
 R16  |  895   37   29   27   23   35   13  ---   12 |    22   20   54   31   58   29  ---    30
 R17E |  973   27   30   27   22   50   16  ---   12 |    46   60   67   54   77   49  ---    53
 R18E | 1407   19   23   15   18   30   20  ---    8 |    47   55   53   59   70   45  ---    50
 R19E |  910   29   37   24   22  152   22  ---   20 |    58   65   78   71  153   62  ---    68
 R20E |  943   48   90   27   36   92   45  ---   23 |    50   77   73   76  107   51  ---    59
 R21E |  664   42   27   24   37   43   39  ---   15 |    58   80   91   98  105   61  ---    78
 R22E | 2301   24   33   14   30   49   31  ---   12 |   164  185  175  185  178  175  ---   175
 R23E | 1011   21   12   11   21   27   23  ---    8 |    41   45   48   54   61   46  ---    45
 R24E |  834   21   27   13   20   30   19  ---    9 |    45   66   67   72   66   46  ---    58
------+----------------------------------------------+------------------------------------------
 RMS  | 1330   32   34   21   28   65   26  176      |T   47   50   58   63   76   43   63    48
 WRMS | 1330   32   36   17   23   48   26  176      |NE  37   32   45   54   58   30   58    35
 MEDI | 1011   27   26   18   23   44   22  176      |MD  46   42   52   59   66   38   72    45

Table 3.1672.3  GPS week: 1672   Day: 3   MJD: 55951                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1386   19   22   23   14   38   23  ---   10 |    63   79   73   65   72   58  ---    65
 R02  |  937   26   28   16   24   22   25  ---   10 |    43   43   35   43  116   18  ---    28
 R03  |  542   22   30   23   33   27   23  ---   11 |    69   68   56   75   54   62  ---    60
 R04  | 1340   25   45   18   27   41    9  ---   12 |    53   40   42   63   54   47  ---    45
 R05  |  844   39   17   11   20   26   22  173   10 |    65   47   54   79   84   42   72    56
 R06  | 1868   13   23   10   24   53   24  ---   11 |    54   45   51   69   85   56  ---    54
 R07  | 1334   28   17   15   15   50   18  ---   10 |    84   76   88   93  115   68  ---    83
 R08  |  695   43   28   18   40   54   38  200   16 |    51   41   27   48   41   50  123    29
 R09  | 1023   29   17   11   24   23   16  ---    9 |    22   39   43   35   56   47  ---    36
 R10  | 1162   18   11   11   14   27   20  ---    7 |    30   19   31   32   50   24  ---    26
 R11  | 1970   54   87   49   37   46   21  244   22 |    27   52   71   57   31   30  148    37
 R12  | 1557   43   19   21   31   26   27  ---   12 |    35   32   39   57   37   30  ---    33
 R13  | 2637   39   14   24   16   27   17  ---   10 |    25   23   31   28   35   23  ---    21
 R14  | 4663   32   51   32   18   32   28  ---   14 |    27   40   49   47   42   20  ---    31
XR15  | ----    6  ---  ---  ---   61  ---  ---    0 |    28  ---  ---  ---   32  ---  ---    28
 R16  | 1048   30   24   14   18   38   15  ---   10 |    36   44   51   45   57   33  ---    40
 R17E |  779   36   49   30   22   53   29  ---   15 |    37   52   92   72  106   44  ---    62
 R18E | 4258   22   26   16   14   71   15  348   12 |    29   46   42   39   78   32    6    35
 R19E | 1219   21   22   14   17   38   11  ---    9 |    66   83   81   75   87   74  ---    75
 R20E | 1309   41   87   24   44   49   31  ---   20 |    34   49   53   77   75   50  ---    49
 R21E |  834   40   61   26   22   57   27  ---   16 |    52   65   86   84  101   62  ---    71
 R22E | 2150   26   25   16   30   29   27  ---   11 |   176  176  180  190  202  171  ---   179
 R23E |  959   24   34   15   26   33   32  ---   12 |    38   50   43   50   53   33  ---    38
 R24E |  813   23   25   13   31   36   21  ---   11 |    33   49   48   49   59   36  ---    41
------+----------------------------------------------+------------------------------------------
 RMS  | 1850   32   39   21   26   41   24  250      |T   49   54   59   64   71   48   87    50
 WRMS | 1850   31   40   19   22   39   24  250      |NE  39   41   46   52   56   36  110    38
 MEDI | 1219   26   25   16   24   38   23  200      |MD  37   47   51   57   57   44   72    40

Table 3.1672.4  GPS week: 1672   Day: 4   MJD: 55952                            

        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  | 1760   34   43   19   32   73   28  ---   15 |    38   76   41   37   55   53  ---    40
XR02  | 1031   29  ---   12   19  599   20  ---   11 |    43  ---   39   40  495   31  ---    32
 R03  | 1406   27   16   16   35   43   24  ---   11 |    51   49   41   59   30   33  ---    38
 R04  | 1413   19   22   10   32   71   19  ---   12 |    56   50   55   69   63   36  ---    46
 R05  |  671   24   24   28   50   28   21  204   13 |    51   52   28   66   45   38  180    38
 R06  | 1921   18   18   20   21   39   17  ---    9 |    51   42   55   66   36   42  ---    47
 R07  | 1357   18   45   27   38   82   42  ---   18 |    61   44   80   94  125   45  ---    62
 R08  | 2397   25   16   13   16   91   17  324   13 |    46   40   50   34   78   32  267    36
 R09  | 1252   27   19   23   17   38   20  ---   10 |    23   34   44   28   47   22  ---    24
 R10  | 2885   16   20   21   24   25   18  ---    9 |    20   28   44   25   33   17  ---    22
 R11  | 3412   52   52   27   26   45   23  172   16 |    30   35   54   47   37   27   81    31
 R12  | 1527   31   22   29   23   69   16  ---   13 |    26   32   40   40   58   19  ---    22
 R13  | 4132   32   22   13   23   24   18  ---    9 |    18   33   33   45   32   27  ---    25
 R14  | 2817   26   39   12   28   44   20  ---   12 |    34   31   36   41   42   23  ---    28
XR15  | ----    8  ---  ---  ---   45  ---  ---    0 |    22  ---  ---  ---   21  ---  ---    25
 R16  | 1113   32   11   16   12   42   13  ---    9 |    25   20   21   20   42   19  ---    13
 R17E |  863   29   30   23   26   44   26  ---   12 |    34   49   57   50   66   38  ---    42
 R18E |  896   21   21   19   16   42   16  ---    9 |    26   44   44   42   58   35  ---    36
 R19E | 1023   23   27   19   21   31   18  ---   10 |    38   41   44   43   58   47  ---    40
 R20E | 1613   36   70   19   34   42   33  ---   17 |    35   62   57   64   45   44  ---    46
 R21E |  760   32   52   26   19   56   18  ---   14 |    47   68   82   71   70   64  ---    65
 R22E | 1457   26   36   29   29   51   26  ---   14 |    93  102  122  112  118   88  ---   102
 R23E | 1139   24   31   24   31   22   22  ---   11 |    30   39   52   57   52   39  ---    40
 R24E |  935   29   26   15   28   45   20  ---   11 |    40   39   52   63   70   46  ---    45
------+----------------------------------------------+------------------------------------------
 RMS  | 1895   28   33   21   28   51   22  243      |T   39   45   50   52   74   37  176    39
 WRMS | 1895   27   34   21   25   42   22  243      |NE  34   36   40   45   75   27  130    30
 MEDI | 1406   26   24   19   26   44   20  204      |MD  35   41   44   47   52   36  180    38

Table 3.1672.5  GPS week: 1672   Day: 5   MJD: 55953                            

        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  | 1190   35   28   13   12   57   23  ---   12 |    42   63   60   50   49   50  ---    49
 R02  | 1102   26   22   14   21   31   18  ---    9 |    36   22   26   30  102   26  ---    22
 R03  | 1802   27   15   12   12   31   27  ---    9 |    45   46   51   45   38   41  ---    41
 R04  | 1444   18   14   12   18   25   26  ---    8 |    54   60   56   53   52   31  ---    48
 R05  |  853   30   22   28   13   20   18   90   10 |    58   64   47   41   47   55   63    48
 R06  | 1738   15   24   17   34   57   14  ---   12 |    49   44   36   69   68   40  ---    45
 R07  | 1280   28   26   18   19   33   31  ---   11 |    53   52   59   64   59   39  ---    50
 R08  | 2650   20   34   55   34   48   25  125   17 |    39   33   70   45   63   33   98    38
 R09  | 1199   27   16   15   14   36   25  ---    9 |    15   17   23   24   25   29  ---    16
 R10  | 2794   14   12   21   17   30   18  ---    8 |    16   20   32   20   30   16  ---    16
 R11  | 3086   44   54   34   22   43   43  199   17 |    29   27   57   35   50   36   51    30
 R12  |  769   33   12   16   20   37   16  ---    9 |    35   34   24   30   56   26  ---    25
 R13  | 2896   27   21   12   19   40   15  ---    9 |    33   33   32   37   26   22  ---    27
 R14  | 2752   35   27   11   17   36   14  ---   10 |    28   46   34   37   35   25  ---    29
XR15  | ----    6  ---  ---  ---   44  ---  ---    0 |    22  ---  ---  ---   24  ---  ---    22
 R16  |  791   42   28   19   20   33   19  ---   11 |    30   32   49   45   49   24  ---    33
 R17E |  789   32   34   30   21   28   22  ---   12 |    29   35   54   49   55   37  ---    38
 R18E | 1657   31   38   15   17   33   25  ---   11 |    33   49   40   41   54   28  ---    34
 R19E |  944   30   18   15   19   34   22  ---   10 |    60   74   74   75   86   71  ---    71
 R20E | 1299   44   48   25   37   52   35  ---   17 |    38   36   54   67   70   45  ---    47
 R21E | 1490   31   24   20   14   54   21  ---   11 |    67   59   80   69   96   62  ---    68
 R22E |  919   27   29   23   19   72   19  ---   13 |   126  125  137  121  179  132  ---   132
 R23E |  925   23   24   18   23   33   19  ---   10 |    32   41   41   40   44   34  ---    33
 R24E | 1367   31   31   17   27   25   26  ---   11 |    33   38   47   57   59   37  ---    41
------+----------------------------------------------+------------------------------------------
 RMS  | 1720   30   28   22   22   40   24  145      |T   41   45   51   49   59   40   70    41
 WRMS | 1720   28   27   18   20   35   24  145      |NE  34   37   38   38   46   30   57    30
 MEDI | 1299   28   24   17   19   34   22  125      |MD  35   41   49   45   52   36   63    38

Table 3.1672.6  GPS week: 1672   Day: 6   MJD: 55954                            

        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  |  825   31   20   14   26   45   22  ---   11 |    44   70   60   69   62   39  ---    54
 R02  |  684   22   25   24   15   39   15  ---   10 |    45   31   35   43   80   22  ---    31
 R03  | 2036   27   22   15   13   29   22  ---    9 |    59   50   37   49   56   26  ---    39
 R04  |  930   35   14   15   29   16   38  ---   11 |    66   49   43   60   44   22  ---    42
 R05  | 1474   23    9   18   20   26   28  114    9 |    67   63   61   68   73   37   92    58
 R06  |  955   28   26    8   19   41   25  ---   10 |    60   55   45   52   45   22  ---    41
 R07  | 1450   21   18   15   23   48   20  ---   10 |    93   86   89   98  102   73  ---    86
 R08  | 1952   41   23   19   40   26   21   67   13 |    57   39   40   51   45   30  119    37
 R09  |  956   27   21   17   19   18   19  ---    9 |    12   23   42   36   45   23  ---    26
 R10  | 1440   13   32   16   20   37   32  ---   11 |    22   25   36   25   32   28  ---    21
 R11  | 2375   38   26   13   23   41   21  172   11 |    20   54   56   48   64   33   35    41
 R12  | 1080   25   15   14   21   42   12  ---    9 |    23   29   33   27   44   22  ---    24
 R13  | 1642   24   18   13   20   35   13  ---    8 |    30   29   35   33   52   28  ---    27
 R14  | 1166   40   21   16   21   26   21  ---   10 |    31   40   41   44   40   28  ---    31
XR15  | ----    6  ---  ---  ---   35  ---  ---    0 |    37  ---  ---  ---   20  ---  ---    38
 R16  | 1170   38   15   16   17   21   20  ---    9 |    25   33   47   40   40   21  ---    31
 R17E | 1261   37   32   31   21   29   25  ---   13 |    24   33   66   51   50   39  ---    42
XR18E |  964   27  ---   14   17   45   26  ---   12 |    33  ---   49   49   60   38  ---    42
 R19E |  790   31   28   16   19   46   30  ---   12 |    91  107   99  100  119  105  ---   101
 R20E | 1500   34   52   24   31   60   37  ---   17 |    45   52   66   66   75   44  ---    53
 R21E |  695   37   29   29   24   94   27  ---   17 |    56   73   82   84  126   74  ---    76
 R22E | 2982   24   31   22   17   38   20  ---   11 |   171  164  172  169  183  176  ---   171
 R23E | 1063   28   34   21   18   32   36  ---   12 |    57   49   52   52   53   63  ---    49
 R24E | 1836   50   45   17   21   32   23  ---   14 |    34   38   49   43   57   46  ---    40
------+----------------------------------------------+------------------------------------------
 RMS  | 1488   32   27   19   22   41   25  125      |T   50   54   58   59   65   45   82    50
 WRMS | 1488   31   26   16   20   40   25  125      |NE  38   40   42   43   48   26   63    34
 MEDI | 1170   28   23   16   20   35   22  114      |MD  44   49   49   51   53   33   92    41




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