[IGSREPORT-27632] Wk 2132 IGLOS Final Orbits

acc acc at igs.org
Thu Dec 3 18:36:07 PST 2020


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2132   (Nov 15, 2020 - Nov 21, 2020) 
                                                                               
Contact: acc at igs.org
                                                                               
                                                                               
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 2.2132.
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:
                                                                               
 igl2132[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2132 in the SP3 format.
 igl21327.sum      Combination Report for GPS Week 2132.


    
    
REMARKS concerning the IGL Orbit Combination:                                  
---------------------------------------------

Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.

 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
    
    Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
    model file has been updated to igs14.atx to be consistent with IGS14.
    See IGSMAIL #7399 for more information
        ftp://igs.org/pub/station/general/igs14.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  |      0.3 ns
                1  |      1.0 ns
                2  |      1.5 ns
                3  |      0.6 ns
                4  |     -0.0 ns
                5  |      0.5 ns
                6  |     -0.1 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
               ----+--------+---------------
                0  |  IAC   | R23
                1  |  IAC   | R23

    
         
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 1.2132, 1a.2132).
        
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 2.2132.0-6)                                                                                
    
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 3.2132.0-6). 
        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 2132 summary.                      (Nov 15, 2020 - Nov 21, 2020)

Table 1.2132.a     GPS week : 2132   MJD: 59168.0-59174.0

         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  n/a|    0    -1     3     3    14    15   .26   26   22 |   18112    -869   3069   7704
        |    1     1     1    14    15    17   .07           |    1192    1406
emx  n/a|    0     0   -10   -37     0    -7   .18   33   32 |   -1368    -815   3062   7789
        |    1     1     1    34    24    43   .07           |    9920     856
esx  n/a|    0     2     0    18   -45    26   .08   31   26 |     596   -1721   3066   9982
        |    2     1     1    17    17    25   .09           |   10960    1487
gfz  n/a|   -1    -1     0   -12   -17   -37   .00   32   19 |       0    -261   3071   7457
        |    2     1     1    18    14    16   .06           |       0    1264
grg  n/a|    2     0     2    13     7   -61  -.37   24   20 |     772    -525   3064   7071
        |    1     1     3    19    24    34   .08           |     640    1408
iac  n/a|   -1     0     2    18    38    96  -.05   98   71 |    2616    -464   3065   7934
        |    2     1     3    40    38    78   .28           |    1039     809
mcc  n/a|    5    -2    -8    53    46   -14  -.30  204  204 |     ---     ---    ---    ---
        |    7    15     8   124   190   755   .50           |     ---     ---


Table 1.2132.b     GPS week : 2132   MJD: 59168.0-59174.0   

         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  |   15   18   18   14   16   14   16 |
 R02  |    7    7    7    7    7    9    8 |
 R03  |    6    8    9    8    6    8    5 |
 R04  |   10   10    8    9   10    9   10 |
 R05  |   11   12   10    8   12   11   11 |
 R07  |    9    8    9    8    8    7    7 |
 R08  |    9    8    8   10    9    8    7 |
 R09  |    8    9   12    8    8    7    9 |
 R11  |    7    7    9   10    0  ---  --- |
 R12  |    8    8   11   11    9   10   11 |
 R13  |   15   16   18   17   17   15   16 |
 R14  |    7    8   11   16    9    8    8 |
 R15  |   10   11   13   10   10    9    8 |
 R16  |   12   13   17   11   12   13   13 |
 R17  |   12    8    9    9    9    9    9 |
 R18  |   10    8    7    7    9    8    9 |
 R19  |   26   25   26   28   29   24   28 |
 R20  |   25   25   26   24   24   21   23 |
 R21  |    8   10   10   10   10   11    9 |
 R22  |   17   18   22   23   17   13   10 |
 R23  |   13   15   11   12   14   12   11 |
 R24  |   12    9    9    8    9    8   12 |
 R25  |  ---    0    0    0   23   18   43 |


Table 1.2132.c     GPS week : 2132   MJD: 59168.0-59174.0   

         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 2132 0   |  -38    42   114      91    2856    3104  80.3  4774  4774 |     328       0
brd 2132 1   |   66    32   113     240    1608    1732  82.4  1843  1843 |    1028       0
brd 2132 2   |   17   -15   129    -800     730    2543  80.3  1660  1660 |    1472       0
brd 2132 3   |   17    97   168   -1357    1026      -4  80.8  1709  1709 |     567       0
brd 2132 4   |  -64    25    59    -262   -1268    1658  80.2  1667  1667 |     -30       0
brd 2132 5   |  -17   -43    98     715     611     713  80.9  1581  1581 |     486       0
brd 2132 6   |  -30   -15    64      89   -1465    3971  81.2  1532  1532 |    -148       0
-------------+------------------------------------------------------------+----------------
brd 2132 mean|   -7    17   107    -183     585    1959  80.9  2109  2109 |     529       0
brd 2132 sdev|   43    47    37     695    1530    1369    .8  1179  1179 |     570       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 2.2132.0  GPS week: 2132   Day: 0   MJD: 59168                            

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  n/a|    0     0     4    -9    17     9   .20   23   18 |   16637   -2167   2880   7661
emx  n/a|   -2    -1    -9   -62   -12    -4   .12   31   28 |  -10717   -1185   2892   7681
esx  n/a|    0     2     0    46   -33     0   .11   31   21 |   -9519   -2690   2897  10123
gfz  n/a|   -4     0     0     2     2   -21   .08   27   19 |       0   -1405   2928   7066
grg  n/a|    3     1    -3    28    20   -25  -.42   26   19 |    1041   -1300   2883   6856
iac  n/a|   -2     0     3   -17    19    47  -.06  454  265 |    1492     761   2894   7917
mcc  n/a|    1   -11   -17   -75   111  -885  -.50  185  185 |     ---     ---    ---    ---

Table 2.2132.1  GPS week: 2132   Day: 1   MJD: 59169                            

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  n/a|   -1    -3     4    -4    19    -1   .27   24   20 |   16749   -1116   3022   7725
emx  n/a|    0     1    -9   -24     2    12   .23   33   33 |    6093   -1271   3009   7616
esx  n/a|   -2     2     0    25   -60    42   .19   28   20 |    6732   -2460   3017   9450
gfz  n/a|    0    -3     0     2    -5   -41  -.07   28   17 |       0    -591   3082   7473
grg  n/a|    4     2     0    11    43   -59  -.29   25   22 |    1570    -778   3016   6622
iac  n/a|    0     0     6    29   -28    68  -.28   80   88 |    3636    -517   3021   7843
mcc  n/a|    2   -10     0    74    48  -187  -.70  202  202 |     ---     ---    ---    ---

Table 2.2132.2  GPS week: 2132   Day: 2   MJD: 59170                            

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  n/a|    2    -3     3    29    37    -2   .35   25   22 |   18113     114   3403   8211
emx  n/a|    0    -1   -10   -24    30    19   .27   32   33 |    5867    -401   3385   8342
esx  n/a|   -3     2    -2     1   -66    40   .18   34   29 |    6995   -1249   3390  10496
gfz  n/a|    0     0     0    -1   -35   -15   .07   35   16 |       0    1520   3277   8154
grg  n/a|    1     2     4    -5   -14   -44  -.42   26   22 |    1306     269   3406   7620
iac  n/a|   -2     0     5   -39    55    53  -.49   38   36 |    4237   -1011   3395   8353
mcc  n/a|   19   -20     0    34    22   739  -.10  159  159 |     ---     ---    ---    ---

Table 2.2132.3  GPS week: 2132   Day: 3   MJD: 59171                            

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  n/a|   -1     0     5    14    19     1   .34   25   23 |   17728     760   3456   8253
emx  n/a|    1     0    -9   -19   -34   -97   .26   33   33 |   12951     182   3462   8409
esx  n/a|   -1     3    -1    -6   -36    12   .07   32   33 |    2743     992   3448  10808
gfz  n/a|   -3     0     0   -32   -21   -45   .01   35   23 |       0     279   3340   8150
grg  n/a|    0     0     1    30    -4   -47  -.48   24   21 |     -92     938   3446   7846
iac  n/a|    4    -1     0    50    95   260   .02   35   35 |    2990    -536   3440   8429
mcc  n/a|    7    25   -20    38    23  1106   .73  199  199 |     ---     ---    ---    ---

Table 2.2132.4  GPS week: 2132   Day: 4   MJD: 59172                            

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  n/a|    0    -2     0    -2     8    36   .17   29   28 |   19165   -2061   3345   7763
emx  n/a|    1     0   -12   -54    -5   -13   .09   35   36 |  -13409   -1833   3323   7911
esx  n/a|   -1     1     1    14   -23    37  -.03   32   29 |  -14539   -2969   3335   9750
gfz  n/a|    0     0     1   -43    -6   -48   .02   32   19 |       0   -1176   3392   7530
grg  n/a|    1    -1     3     8    13  -105  -.39   21   16 |     681   -1868   3327   7200
iac  n/a|   -4     1     0    79    38   123   .36   31   29 |    2372   -1587   3329   8077
mcc  n/a|    0     4    -3   143  -336   320  -.62  160  160 |     ---     ---    ---    ---

Table 2.2132.5  GPS week: 2132   Day: 5   MJD: 59173                            

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  n/a|    2    -2     2     6   -11    35   .24   28   23 |   18535     783   2625   7325
emx  n/a|   -1    -2    -9    11    34    38   .14   32   32 |   -2358     338   2604   7361
esx  n/a|    1     3     0    20   -36    61  -.02   28   24 |   -5307    -694   2629   9334
gfz  n/a|    0    -2    -3    -5   -31   -27  -.01   32   20 |       0    1165   2673   7157
grg  n/a|    2     0     5   -16    22  -111  -.37   18   16 |     -52    1354   2622   6962
iac  n/a|   -3    -1     0    16    30    29   .17   26   25 |    1786     411   2608   7538
mcc  n/a|    0   -10   -12   261   227  -700  -.62  214  214 |     ---     ---    ---    ---

Table 2.2132.6  GPS week: 2132   Day: 6   MJD: 59174                            

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  n/a|    0     0     2    -6     8    25   .24   24   20 |   19862   -2401   2757   6990
emx  n/a|    0     0   -11   -92   -14    -9   .16   31   31 |   -8004   -1541   2760   7207
esx  n/a|    2     0    -2    28   -63    -8   .03   28   23 |   17068   -2983   2751   9915
gfz  n/a|    0     0     0    -6   -21   -61  -.08   33   19 |       0   -1619   2808   6674
grg  n/a|    0     1     7    36   -26   -35  -.23   27   21 |     951   -2295   2754   6391
iac  n/a|    0    -1     3     6    57    94  -.08   25   22 |    1800    -772   2773   7383
mcc  n/a|    4     2    -2  -103   227  -494  -.29  311  311 |     ---     ---    ---    ---

       
       
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 3.2132.0  GPS week: 2132   Day: 0   MJD: 59168                            

        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  |  622   31   42   38   39   26   21  ---   15 |    34   43   30   36   35   53  ---    32
 R02  |  979   10   12   14   10   14   29  ---    6 |    23   20   25   25   17   33  ---    20
 R03  |  956    8   12   11   10   16   16  104    5 |    20   19   25   21   22   23   74    18
XR04  |  911    7    6   19  ---   26   35  ---   10 |    27   29   26  ---   36   30  ---    25
 R05M | 1064   18   24   27   27   18   29  ---   10 |    23   24   36   32   30   32  ---    21
 R07  |  579   14   14   12   32   12   24  302    8 |    22   20   23   34   23   21  221    19
 R08M | 1198   15   19   22   18   20   32  ---    9 |    18   17   33   35   31   33  ---    21
 R09E | 3919   15   18   14   17   21   25  ---    8 |    93   93   96   96   93   87  ---    92
 R11E | 1655   17   12   10   11   18   24  130    7 |    27   25   24   25   29   44  103    27
 R12E | 1438   17   21   10   18   17   21  ---    8 |   130  126  127  132  125  128  ---   127
 R13E |  678   40   30   35   28   21   42  ---   14 |    66   53   61   61   63   71  ---    56
 R14E |  486   14   18   17   12   13   22  ---    7 |    57   55   70   66   64   68  ---    61
 R15E | 1115   18   30   23   18   13   23  ---    9 |    68   67   63   72   64   78  ---    65
 R16E | 2220   22   24   29   28   30   21  ---   11 |   119  108  111  106  122  105  ---   111
 R17M | 2138   14   33   23   16   15   48  ---   11 |    77   60   60   74   70   90  ---    70
 R18M | 1711   15   22   18   12   11   47  ---   10 |    65   61   71   69   70   93  ---    68
 R19M | 1311   53   69   69   61   44   56  ---   26 |    87   38   59   96   61   82  ---    59
 R20M |20681   28   68   82   37   56   46  ---   24 |    92   52   50   73   97   77  ---    64
 R21  |  478   18   25   15   18   11   18  135    8 |    75   55   57   72   67   71   56    65
 R22  | 1332   20   27   21   39   51   58  ---   17 |    63   58   74   66   78   67  ---    64
 R23M | 2285   24   24   29   27   21 2078  ---   12 |    69   54   81   53   74 9999  ---    64
 R24M | 1523   17   31   23   19   31   32  ---   11 |    62   49   48   65   67   69  ---    57
------+----------------------------------------------+------------------------------------------
 RMS  | 4774   23   31   31   27   26  454  185      |T   59   51   56   62   60   64  113    54
 WRMS | 4774   18   28   21   19   19  265  185      |NE  37   34   37   42   39   42  117    34
 MEDI | 1198   17   24   21   18   18   29  130      |MD  63   52   57   66   64   69   74    59

Table 3.2132.1  GPS week: 2132   Day: 1   MJD: 59169                            

        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  |  881   37   41   27   47   33   52  ---   17 |    28   32   26   63   25   56  ---    26
 R02  |  972   12   21   12   15   10   23  357    7 |    20   19   32   32   22   33  413    22
 R03  |  632   12   14   10   15   16   35   88    7 |    24   22   27   22   22   45   50    21
XR04  |  942   10    9   14  ---   22   34  ---    9 |    27   27   28  ---   35   32  ---    25
 R05M | 2770   29   24   21   31   11   42  ---   12 |    29   29   37   49   26   42  ---    27
 R07  | 1091    6   10   16   15   27   26  179    8 |    27   27   23   21   38   29   97    22
 R08M | 1411   11   17   10   15   15   35  ---    7 |    26   25   34   33   30   33  ---    26
 R09E | 3196   18   17   10   22   22   23  ---    8 |    75   77   77   81   75   77  ---    75
 R11E |  977   11   18   10   13   20   18  147    6 |    37   39   40   34   32   39   53    36
 R12E | 1568   20   27   14   15   15   18  ---    8 |   106   98  100  104   97  104  ---   100
 R13E |  786   40   38   36   37   31   30  ---   16 |    59   49   48   59   60   68  ---    50
 R14E |  924   14   22   19   12   13   23  ---    7 |    39   39   45   42   38   40  ---    37
 R15E | 1225   17   27   14   17   23   52  ---   11 |    83   82   86   84   89   66  ---    81
 R16E | 2083   23   28   20   19   39   44  ---   13 |   131  124  141  131  143  115  ---   130
 R17M | 3079   18   22   21   14   11   19  ---    8 |    48   44   42   49   48   50  ---    45
 R18M | 1741   18   21   16   16   15   27  ---    8 |    43   45   52   55   53   52  ---    48
 R19M | 2019   51   69   60   53   37   57  ---   24 |    53   48   49   52   47   80  ---    45
 R20M | 1754   38   80   69   48   34   52  ---   24 |    64   38   47   71   61   78  ---    52
 R21  |  567   10   30   19   19   20   32  125    9 |    52   40   47   55   45   68   30    48
 R22  | 1267   24   27   39   52   46   38  ---   17 |    51   48   64   44   55   60  ---    46
 R23M | 2335   29   15   36   31   27  332  ---   14 |    69   62   71   58   78  656  ---    66
 R24M | 3214   16   27   20   11   20   27  ---    9 |    43   40   43   38   46   39  ---    38
XR25E | ----    5  ---  ---  ---  ---  ---  ---    0 |   101  ---  ---  ---  ---  ---  ---   102
------+----------------------------------------------+------------------------------------------
 RMS  | 1842   24   33   28   28   25   80  202      |T   53   47   52   56   52   84  128    50
 WRMS | 1842   20   33   20   17   22   88  202      |NE  32   30   35   39   34   46  147    30
 MEDI | 1267   18   22   19   17   20   32  147      |MD  48   40   45   52   46   52   53    45

Table 3.2132.2  GPS week: 2132   Day: 2   MJD: 59170                            

        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  | 1786   43   43   37   49   23   33  ---   17 |    24   38   46   61   38   44  ---    32
 R02  | 1323   10   11   12   10   17   30  208    7 |    23   22   33   30   34   25  221    24
 R03  |  525    9   12   25   21   15   33   85    8 |    18   20   41   22   26   44   59    21
XR04  |  840   14   13   14  ---   13   22  ---    7 |    18   21   23  ---   16   29  ---    14
 R05M | 2250   20   17   28   21   16   37  ---   10 |    22   19   37   34   15   44  ---    18
 R07  | 1435   13   12   25   12   15   34  138    8 |    21   26   37   26   33   42   59    22
 R08M |  892   16   12   17   11   19   35  ---    8 |    20   24   34   22   37   36  ---    22
 R09E | 2622   19   23   23   14   21   53  ---   11 |    52   56   60   60   65   78  ---    56
 R11E |  467   11   26   16   12   16   40  197    9 |    46   44   32   36   42   57   89    41
 R12E | 1345   14   29   22   18   27   34  ---   10 |   129  123  126  124  136  137  ---   127
 R13E | 1133   42   46   40   35   32   40  ---   17 |    60   53   60   54   60   64  ---    51
 R14E | 2024   14   26   23   21   19   40  ---   10 |    71   69   78   74   79   66  ---    70
 R15E | 1771   17   22   15   19   44   46  ---   13 |   140  143  145  148  129  153  ---   139
 R16E | 1027   28   22   48   47   43   32  ---   17 |    92  100  115  121   88   99  ---    96
 R17M | 3069   22   24   20   15   12   27  ---    9 |    53   37   37   46   40   57  ---    42
 R18M | 1044   10   16   19   18   13   21  ---    7 |    42   39   54   58   42   59  ---    46
 R19M | 1021   39   60   58   80   47   57  ---   25 |    61   59   45   73   38   80  ---    47
 R20M | 1175   48   77   80   57   33   42  ---   26 |    75   58   40   61   43   62  ---    46
 R21  |  575   19   31   20    9   22   34  137   10 |    57   39   40   44   59   65   34    48
 R22  | 1349   29   38   48   79   37   44  ---   21 |    48   44   76   66   71   60  ---    51
 R23M | 1930   27   21   29   23   22   28  ---   11 |    29   37   55   49   53  277  ---    42
 R24M | 2723   19   24   14   14   13   31  ---    8 |    42   27   27   31   26   40  ---    28
XR25E | ----    7  ---  ---  ---  ---  ---  ---    0 |    81  ---  ---  ---  ---  ---  ---    82
------+----------------------------------------------+------------------------------------------
 RMS  | 1659   25   32   34   35   26   38  159      |T   53   49   56   59   53   73   92    50
 WRMS | 1659   22   33   29   16   22   36  159      |NE  29   30   42   41   39   44   93    30
 MEDI | 1323   19   23   23   19   19   34  138      |MD  48   39   41   54   42   59   59    46

Table 3.2132.3  GPS week: 2132   Day: 3   MJD: 59171                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 2027   38   27   43   24   14   38  ---   14 |    50   59   62   66   47   46  ---    50
 R02  | 1879   14   11   13   19   14   25  256    7 |    37   45   42   43   41   39  100    38
 R03  |  609    9    8   18   19   18   33   89    8 |    41   41   43   37   40   47   49    39
XR04  |  937   11   12   13  ---   13   35  ---    8 |    46   48   51  ---   52   46  ---    46
 R05M | 1372   17   13   23   15   10   30  ---    8 |    45   45   56   51   47   47  ---    45
 R07  |  855   17   19   15   12   10   32  209    8 |    41   43   48   40   45   45  174    41
 R08M | 1531   13   15   24   23    8   48  ---   10 |    40   39   48   42   36   60  ---    39
 R09E | 2838   15   15   22   16   15   25  ---    8 |    61   67   66   66   64   59  ---    62
 R11E |  844   13   26   15   13   19   37  238    9 |    51   51   48   46   53   49  144    42
 R12E |  487   20   30   15   15   27   34  ---   11 |   133  131  128  125  135  136  ---   130
 R13E | 1159   48   43   35   34   22   32  ---   16 |    70   69   72   74   73   74  ---    66
 R14E | 2491   16   40   18   26   30   72  ---   16 |    89   81   81   82   99  101  ---    83
 R15E | 2149   14   27   19   26   23   16  ---    9 |   256  260  255  250  261  273  ---   258
 R16E | 2085   16   19   30   26   26   33  ---   11 |   130  122  120  128  139  129  ---   126
 R17M | 2390   22   25   22   19   12   17  ---    9 |    71   58   56   66   57   61  ---    60
 R18M | 1694   14   19   11   11   17   23  ---    7 |    69   64   68   64   73   73  ---    67
 R19M |  613   41   80   65   90   49   33  ---   28 |    91   88   74  120   83   87  ---    82
 R20M | 1135   51   70   72   57   21   35  ---   23 |    86   37   47   79   55   47  ---    52
 R21  |  564   27   28   22   10   11   36  158   10 |    73   53   52   64   56   72   64    59
 R22  | 2120   25   33   49   74   55   51  ---   22 |    56   79   89   71   70   89  ---    66
 R23M | 1642   26   19   36   37   20   23  ---   12 |    77   84   95   76   86  146  ---    81
 R24M | 2249   12   24   16   19   10   24  ---    7 |    60   53   55   57   49   57  ---    52
XR25E | ----    6  ---  ---  ---  ---  ---  ---    0 |    38  ---  ---  ---  ---  ---  ---    37
------+----------------------------------------------+------------------------------------------
 RMS  | 1708   25   33   32   35   24   35  199      |T   74   73   75   78   75   81  106    70
 WRMS | 1708   23   33   33   23   21   35  199      |NE  49   52   55   53   50   54   96    48
 MEDI | 1531   16   24   22   19   17   33  209      |MD  61   58   56   66   56   60  100    59

Table 3.2132.4  GPS week: 2132   Day: 4   MJD: 59172                            

        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  | 1872   53   26   44   38   16   25  ---   16 |    49   45   62   53   45   46  ---    45
 R02  | 2325   14   10   11   12   12   29  200    7 |    39   40   46   42   37   48   98    40
 R03  |  940   14   10   11    6    9   22   45    5 |    39   40   42   40   45   50   75    40
XR04  |  892   13   20   13  ---    9   39  ---   10 |    41   42   35  ---   41   51  ---    39
 R05M |  633   25   23   31   25   16   32  ---   11 |    42   46   58   44   50   41  ---    43
 R07  |  582   19   16    7   15   13   30  114    7 |    46   47   39   40   51   46  106    42
 R08M |  812   12   15   23   27   15   27  ---    9 |    42   38   48   50   51   53  ---    44
 R09E | 2698   16   13   10   22   19   25  ---    8 |    73   75   75   70   76   70  ---    71
XR11E |19186  ---  ---  ---  ---  ---    9   86    0 |   ---  ---  ---  ---  ---   47   72    42
 R12E |  533   12   30   20   19   21   18  ---    9 |   164  166  160  159  162  168  ---   162
 R13E | 1245   34   54   38   36   29   36  ---   17 |    51   57   49   59   61   57  ---    48
 R14E | 1572   16   25   13   21   18   30  ---    9 |    58   60   65   64   68   69  ---    61
 R15E | 2231   15   33   20   19   16   33  ---   10 |   379  378  384  378  380  367  ---   378
 R16E | 3105   22   26   26   39   19   23  ---   11 |    60   57   62   68   61   75  ---    59
 R17M | 2137   19   25   17   17   11   29  ---    8 |    63   54   56   63   57   65  ---    57
 R18M | 2007   19   15   16   23   13   33  ---    9 |    62   60   63   61   56   71  ---    59
 R19M | 1146   57   97   57   76   50   40  ---   28 |   104   63   86  102  104  125  ---    90
 R20M | 1510   61   65   70   52   18   48  ---   23 |    77   42   46   67   58   57  ---    47
 R21  |  462   30   21   18   13   12   33  218    9 |    70   51   54   57   53   62   44    55
 R22  | 1439   28   28   38   41   42   40  ---   16 |    62   57   77   65   78   58  ---    63
 R23M | 1067   25   14   48   44   19   28  ---   14 |    63   70  101   66   64  181  ---    68
 R24M | 1593   14   33   15   16   11   24  ---    8 |    58   53   56   61   53   61  ---    55
XR25E | ----   20  ---  ---  ---  ---   24  ---   22 |    45  ---  ---  ---  ---   45  ---    52
------+----------------------------------------------+------------------------------------------
 RMS  | 1666   29   35   32   32   21   31  160      |T   76   73   79   80   78   83   79    72
 WRMS | 1666   28   36   29   19   16   29  160      |NE  49   46   50   49   50   51   80    46
 MEDI | 1439   19   25   20   22   16   29  114      |MD  58   54   58   61   57   58   75    55

Table 3.2132.5  GPS week: 2132   Day: 5   MJD: 59173                            

        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  |  877   48   19   44   32   11   19  ---   14 |    24   35   51   53   40   35  ---    35
 R02  | 2392   11   12   17   12   12   37  348    8 |    16   16   26   21   20   31  182    16
 R03  | 1337   15   14   16   10   26   17   94    8 |    20   17   24   21   26   22   69    18
XR04  |  888   13   18   11  ---   14   27  ---    8 |    22   19   26  ---   19   19  ---    18
 R05M |  645   23   28   26   29   18   28  ---   11 |    23   28   49   46   30   30  ---    28
 R07  | 1233   10   12   17   10   13   28   44    7 |    17   21   25   22   14   28   65    16
 R08M | 1041   16   10   15   25   16   22  ---    8 |    19   26   23   31   22   33  ---    22
 R09E | 1320   15   16   11   18   14   18  ---    6 |    57   54   60   64   63   65  ---    59
 R12E | 1326   10   33   22   17   23   23  ---   10 |   112  110  118  116  112  117  ---   112
 R13E |  907   33   51   32   31   20   34  ---   14 |    45   36   47   50   45   48  ---    40
 R14E | 1019    8   28   10   14   15   22  ---    7 |    32   31   34   39   35   39  ---    32
 R15E | 2119   10   32   17   23   13   23  ---    9 |   395  410  402  400  401  405  ---   401
 R16E | 3459   25   40   18   32   16   38  ---   12 |    80   95   88   95   84   93  ---    85
 R17M | 2041   10   30   18   20   15   22  ---    8 |    45   37   45   52   54   44  ---    45
 R18M | 1704   15   24   10   20   14   17  ---    7 |    56   58   57   62   56   61  ---    56
 R19M | 1627   60   70   50   70   31   43  ---   24 |    85   87   85  109   63   92  ---    78
 R20M | 1884   58   54   65   59   15   23  ---   21 |    63   37   45   60   27   33  ---    33
 R21  |  536   22   25   25   35   16   28  225   11 |    49   35   36   55   34   32   32    35
 R22  | 1045   22   15   25   47   28   19  ---   12 |    41   56   52   52   51   41  ---    46
 R23M | 1371   25   24   37   35   12   22  ---   11 |    40   53   63   45   46  172  ---    48
 R24M |  591   27   27   14   15   10   14  ---    8 |    46   25   38   29   28   38  ---    32
XR25E | ----   17  ---  ---  ---  ---   18  ---   18 |    48  ---  ---  ---  ---   35  ---    45
------+----------------------------------------------+------------------------------------------
 RMS  | 1581   28   32   28   32   18   26  214      |T   60   61   66   71   60   68   80    59
 WRMS | 1581   23   32   24   20   16   25  214      |NE  27   28   34   37   29   29   87    26
 MEDI | 1320   16   25   18   23   15   22   94      |MD  45   36   47   52   40   38   65    35

Table 3.2132.6  GPS week: 2132   Day: 6   MJD: 59174                            

        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  |  536   31   45   27   34   31   48  ---   16 |    53   66   50   61   39   53  ---    46
 R02  | 3171   11   15   10   13   19   27  548    7 |    28   38   40   41   41   38  389    34
 R03  | 1084    6   11    9    8    8   20  125    5 |    30   31   36   31   45   43   93    34
XR04  | 1012    8   14   14  ---   29   29  ---   10 |    33   38   35  ---   54   42  ---    36
 R05M |  681   17   13   23   39   26   24  ---   11 |    36   40   52   66   49   38  ---    41
 R07  |  994    7   11   27   15   12   18  146    7 |    34   34   51   38   42   36  153    37
 R08M |  668   14   16   17   14   12   15  ---    6 |    32   35   33   33   34   41  ---    31
 R09E |  976   18   12    8   19   20   30  ---    8 |    62   68   67   63   62   77  ---    65
 R12E | 1864   10   36   24   24   26   15  ---   10 |   122  127  116  125  120  118  ---   120
 R13E |  574   22   41   31   50   34   28  ---   15 |    55   60   61   67   50   57  ---    50
 R14E | 1258   11   22   15   17   19   17  ---    7 |    36   42   35   38   37   43  ---    35
 R15E | 1522   15   23   11   13   16   18  ---    7 |   453  463  459  451  452  457  ---   455
 R16E | 3533   21   32   26   39   29   28  ---   13 |    97   95   88   86   94   97  ---    90
 R17M | 1358   20   28   17   11   15   23  ---    8 |    69   48   46   59   48   64  ---    55
 R18M | 1118   13   21   17   30   16   22  ---    9 |    73   72   76   58   71   88  ---    72
 R19M | 1680   43   72   68   97   41   33  ---   27 |   110   96   94  150  105   88  ---    98
 R20M | 1770   68   48   49   29   62   32  ---   23 |    87   39   42   64   70   42  ---    45
 R21  |  485   22   28   24   16   13   14  220    9 |    68   45   43   64   52   54   43    53
 R22  | 1311   17   15   23   35   24   19  ---   10 |    53   53   63   60   69   60  ---    55
 R23M | 1050   13   19   39   24   25   18  ---   11 |    65   79   93   59   53  209  ---    69
 R24M |  488   26   40   22   13   26   19  ---   11 |    62   41   39   46   34   57  ---    45
XR25E | ----   35  ---  ---  ---  ---   49  ---   42 |    54  ---  ---  ---  ---   49  ---    61
------+----------------------------------------------+------------------------------------------
 RMS  | 1531   24   31   28   33   27   25  311      |T   77   76   77   83   77   84  148    73
 WRMS | 1531   20   31   23   19   21   22  311      |NE  42   43   45   49   48   46  169    42
 MEDI | 1084   17   22   23   19   24   22  146      |MD  55   48   51   60   52   54   93    50



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