[IGSREPORT-26326] y

acc acc at igs.org
Thu Jan 3 19:09:17 PST 2019


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2032   (Dec 16, 2018 - Dec 22, 2018) 
                                                                               
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 2.2032.
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:
                                                                               
 igl2032[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2032 in the SP3 format.
 igl20327.sum      Combination Report for GPS Week 2032.


    
    
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  |      5.8 ns
                1  |      5.6 ns
                2  |      5.0 ns
                3  |      4.8 ns
                4  |      5.4 ns
                5  |      5.6 ns
                6  |      5.2 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 1.2032, 1a.2032).
        
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 2.2032.0-6)                                                                                
    
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 3.2032.0-6). 
        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 2032 summary.                      (Dec 16, 2018 - Dec 22, 2018)

Table 1.2032.a     GPS week : 2032   MJD: 58468.0-58474.0

         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     0     0    21    16     4   .15   24   22 |     551    -265   3128   9172
        |    0     1     1    15    12    23   .03           |     730    1003
cof  n/a|   -1     0     0    19     8    11   .02   27   24 |     533    -263   3127   9171
        |    1     1     1    16    13    33   .09           |     732    1002
emx  n/a|    0     0   -13     0   -25    -8   .12   27   27 |    -459    -158   3109   8768
        |    1     0     3    21    18    66   .06           |   10241     612
esx  n/a|    0     0    -3   -16    -7    39   .06   23   19 |    7169    -485   3113  11216
        |    0     1     1    14    14    23   .03           |   14121    1709
gfz  n/a|   -2     0     1    10    33    10   .05   28   22 |       0    -241   3114   9020
        |    1     0     2    19    14    37   .06           |       0     853
grg  n/a|    0     0     9   -61   -32   -86  -.31   23   20 |    4678    -319   3922  10323
        |    0     1     2    15    15    56   .07           |     924    1051
iac  n/a|    1     0     5    61    -8    58  -.05   26   27 |    6194    -202   3998  10535
        |    0     0     1    28    41    31   .04           |    1438     867


Table 1.2032.b     GPS week : 2032   MJD: 58468.0-58474.0   

         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   17   22   15   14   15   16 |
 R02  |    7    7    6    8    8    6    7 |
 R03  |    7    7    5    6    7    6    5 |
 R04  |    5    6    6    8    7    6    6 |
 R05  |    9    8   10   11   10   11   11 |
 R07  |    8    9    7    7    8    8    6 |
 R08  |    7    8    8   10    9   10   10 |
 R09  |    6    7    7    7    7    7    9 |
 R10  |    6    9    8    7    6    8    9 |
 R11  |    6    7    7    7    8    5    7 |
 R13  |    9    8    7    7    9    9    8 |
 R14  |    9    8    7    8    8    7    8 |
 R15  |    9   10    8    7   10    9    9 |
 R16  |   11   12   13   14   16   14   17 |
 R17  |    8    9    8    7   10   11   10 |
 R18  |    5    7    7    8    7    5    8 |
 R19  |   26   28   28   25   25   29   30 |
 R20  |   16   14   12   12   13   13   16 |
 R21  |   10   11   10   12   12   11    9 |
 R22  |    9    9   10   11   11   12   10 |
 R23  |   11   12   12   12   13   12   10 |
 R24  |   13   16   18   16   12   12   16 |
 R26  |   20   18   12   19   15   13   12 |


Table 1.2032.c     GPS week : 2032   MJD: 58468.0-58474.0   

         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 2032 0   |   47    67    87     493    2237   -2000  84.8  1689  1689 |    5755       0
brd 2032 1   |   60    11    49     730    1136   -3200  83.0  1994  1994 |    5556       0
brd 2032 2   |  -55   -65   -11     688    -732   -2551  84.1  1891  1891 |    4991       0
brd 2032 3   |    7    -5    10     813     233   -3448  84.5  1780  1780 |    4765       0
brd 2032 4   |   -1   -48   -51     945   -1471   -6241  83.2  1903  1903 |    5442       0
brd 2032 5   |   79    14    78    -244     495  -13270  80.9  2097  2097 |    5640       0
brd 2032 6   |  131    98   117     254    1492  -13090  82.5  2158  2158 |    5206       0
-------------+------------------------------------------------------------+----------------
brd 2032 mean|   38    10    40     525     484   -6257  83.3  1930  1930 |    5336       0
brd 2032 sdev|   60    58    60     407    1283    4915   1.3   166   166 |     362       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 2.2032.0  GPS week: 2032   Day: 0   MJD: 58468                            

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     0    23    18   -25   .18   23   20 |     -74     159   2652   9035
cof  n/a|    0     0     0    44    18    29  -.10   27   23 |     -94     143   2654   9040
emx  n/a|    1    -1   -16    14    -9   -50   .20   27   27 |     906    -235   2560   8417
esx  n/a|   -1     1    -2   -31   -11    10   .05   22   17 |   -2740    1276   2561  10940
gfz  n/a|   -2     0     0    10    43   -10   .06   25   25 |       0     191   2562   8645
grg  n/a|    0     1     8   -65   -17     3  -.32   20   18 |    5687     215   2560   8280
iac  n/a|    0     0     4    73   -45    47  -.06   25   27 |    8196   -1450   3335   8917

Table 2.2032.1  GPS week: 2032   Day: 1   MJD: 58469                            

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    20    39   -11   .13   27   23 |    1250    1648   3061   9061
cof  n/a|    0    -1     0    27    29   -45  -.01   28   25 |    1219    1665   3064   9074
emx  n/a|    4     0   -14     4    -5   -59   .15   27   27 |   -7806     887   3064   8832
esx  n/a|    0    -2    -3   -10    -8     9   .10   23   17 |   24135    2232   3070  11380
gfz  n/a|   -2     0     0     6    59   -21   .07   27   23 |       0    1308   3054   8910
grg  n/a|   -1     1     9   -68   -39   -39  -.27   25   22 |    3060    1011   3596  12443
iac  n/a|    1     0     7    45   -38    82  -.14   25   25 |    6005     -10   3589  11929

Table 2.2032.2  GPS week: 2032   Day: 2   MJD: 58470                            

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     0    23     0   -15   .15   28   23 |    1227   -1215   3351   9262
cof  n/a|   -2    -1     0    34    -1    -2   .02   30   24 |    1194   -1194   3344   9258
emx  n/a|    0     0    -7     8   -27    72   .16   29   29 |   19215    -838   3338   8791
esx  n/a|   -1     0    -3    -8   -31    30   .08   23   19 |   19056   -1219   3332  11091
gfz  n/a|   -4     0    -1    18    19   -39  -.04   30   20 |       0    -803   3352   9203
grg  n/a|    0     1     8   -60   -17   -87  -.25   21   20 |    4724    -478   4639   9119
iac  n/a|    2     0     3    34    49   102  -.03   25   25 |    5462     935   4631   9566

Table 2.2032.3  GPS week: 2032   Day: 3   MJD: 58471                            

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     0    35    14    36   .18   26   22 |    1348    -224   3411   9264
cof  n/a|   -3     1     1     6    -8    63   .17   29   24 |    1355    -255   3415   9265
emx  n/a|    0     0   -13   -33   -59    65   .11   24   24 |    5099    -198   3417   8959
esx  n/a|    0     0    -1     5     2    65   .06   22   19 |  -15633    -381   3427  11469
gfz  n/a|   -2     0     0    30    25     7   .07   30   23 |       0    -550   3433   9114
grg  n/a|    0     0     7   -84   -35  -135  -.41   20   18 |    4909       2   3830   8821
iac  n/a|    2     0     5   110    37    43  -.04   26   27 |    6578     527   3869   9011

Table 2.2032.4  GPS week: 2032   Day: 4   MJD: 58472                            

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     0    44    20    31   .15   21   19 |    -481    -529   3162   9618
cof  n/a|   -3     1     0    -2    -2    25   .00   21   21 |    -506    -505   3153   9610
emx  n/a|    0     0   -17   -26   -17    41   .11   27   27 |   -3911     338   3147   9118
esx  n/a|    0     0    -5   -30    16    63   .01   25   22 |    2778   -2701   3156  11760
gfz  n/a|    0     0     2   -23    30    32   .07   25   19 |       0    -733   3142   9477
grg  n/a|    0     0    14   -31   -34  -165  -.37   24   22 |    3823   -1856   5483  15951
iac  n/a|    1     0     8    36   -57     7  -.01   28   28 |    3700    -431   5222  15868

Table 2.2032.5  GPS week: 2032   Day: 5   MJD: 58473                            

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    -1     8     7    16   .12   20   19 |     418    -323   3081   9002
cof  n/a|   -2     0     0    19     6     7   .07   23   21 |     417    -333   3086   8998
emx  n/a|    0     0   -12     4   -22   -43   .02   26   26 |   -5295    -244   3063   8659
esx  n/a|    0     0    -2    -6    -7    48   .05   24   19 |    4373    -940   3063  11228
gfz  n/a|    0     0     6    -1    22    37   .13   26   20 |       0     130   3070   8802
grg  n/a|   -1     0     5   -58   -19   -90  -.36   27   23 |    5230     428   3842   8901
iac  n/a|    1     0     6    48   -10    76  -.02   30   30 |    7395     170   3836   9036

Table 2.2032.6  GPS week: 2032   Day: 6   MJD: 58474                            

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    16     2   .12   25   29 |     170   -1372   3181   8962
cof  n/a|    0     0    -2     6    19    -1  -.01   28   29 |     150   -1368   3176   8956
emx  n/a|    0     0    -9    23   -38   -88   .10   28   28 |  -11426    -816   3180   8604
esx  n/a|    1     1    -2   -31    -9    49   .07   25   20 |   18218   -1662   3187  10647
gfz  n/a|   -2     1     2    32    32    67   .00   29   22 |       0   -1236   3191   8992
grg  n/a|    0     0    10   -65   -61   -89  -.22   25   20 |    5314   -1555   3507   8749
iac  n/a|    2    -1     3    82     6    50  -.02   26   26 |    6022   -1156   3508   9419

       
       
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 3.2032.0  GPS week: 2032   Day: 0   MJD: 58468                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  IGL |   cod  cof  emx  esx  gfz  grg  iac   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  684   35   50   37   43   25   32   13   14 |    91   96   90   54   69   49   59    65
 R02  |  629   12   17    8   10   19   18   22    7 |    52   53   50   48   47   38   33    43
 R03  | 2919    8   13   12   10   14   15   25    6 |    59   62   65   58   57   58   46    56
 R04  | 1103    7    8    9    8   13    6   15    4 |    57   59   61   58   57   56   47    55
 R05  | 1082   16   18   28   20   22   20   14    9 |    48   55   65   52   51   36   48    46
 R07  |  770   14   15   22    7   19   16   19    7 |    61   62   67   57   53   44   46    53
 R08  | 1323   11   15   12   21   15   13   21    7 |    58   61   63   63   63   54   47    57
 R09E | 3432   12   13   17    8   19   14   10    6 |    55   59   59   60   64   59   64    59
 R10E | 1250   14   14   18   10   13   10   13    5 |    38   39   42   43   46   44   40    40
 R11E | 2655    8   10   18   11   16   13   13    6 |    81   83   84   82   81   86   84    82
 R13E | 1460   18   21   29   18   13   23   16    9 |   112  113  114  110  111  118  116   112
 R14E | 2734   14   13   32   18   16   25    9    9 |    47   50   49   61   58   51   52    51
 R15E | 1657   13   11   26   20   23   18   17    9 |    35   33   24   36   46   24   37    30
 R16E | 1421   17   45   37   21   23   17   30   11 |    54   60   51   59   58   53   61    52
 R17  | 1519   23   28   20   14   18   12   23    8 |    72   76   48   52   63   58   42    55
 R18  |  781   14   12   14   10   10   13   10    5 |    52   50   44   54   48   43   50    47
 R19  | 1830   65   60   56   51   70   27   66   25 |    76   78   44   57   78   52   58    38
 R20  | 2102   24   41   45   25   44   40   41   16 |    79   91   47   59   89   84   44    64
 R21  |  779   28   29   23   20   15   16   23    9 |    72   73   45   51   65   58   41    54
 R22  |  646   23   23   23   15   10   18   30    9 |    74   75   48   59   65   61   38    56
 R23  | 1186   20   25   21   31   27   24   21   11 |    69   68   72   96   62   71   86    74
 R24  |  870   28   25   26   22   30   29   37   13 |    48   53   60   68   66   42   61    54
XR26  | 3100   18   39  ---  ---  ---  ---   21   19 |    50   64  ---  ---  ---  ---   54    48
------+----------------------------------------------+------------------------------------------
 RMS  | 1689   23   27   27   22   25   20   25      |T   62   65   58   60   63   56   54    56
 WRMS | 1689   20   23   27   17   25   18   27      |NE  63   67   57   59   62   53   50    54
 MEDI | 1323   16   18   22   18   18   17   21      |MD  58   62   51   58   62   53   48    54

Table 3.2032.1  GPS week: 2032   Day: 1   MJD: 58469                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  IGL |   cod  cof  emx  esx  gfz  grg  iac   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  756   47   55   43   38   33   33   35   17 |    68   81   71   57   69   34   33    51
 R02  | 1182   20   18   11   12   17   17   13    7 |    39   37   34   36   36   25   22    29
 R03  | 3285   11   10    7   14   13   16   20    6 |    42   42   46   49   50   39   34    42
 R04  | 1061    9   11   11   11   15   14   19    6 |    38   42   41   44   46   33   26    36
 R05  |  675   11   12   22   17    8   29   11    8 |    41   37   48   54   45   36   39    42
 R07  | 1180   24   23   27   10   27   13   20    9 |    43   41   47   36   32   32   27    32
 R08  | 1976   18   19   20   14   24   16   12    8 |    39   39   39   38   40   31   33    33
 R09E | 4360   14   13   18   12   19   10   15    6 |    43   44   40   43   49   44   43    42
 R10E | 1305   14   12   29   19   21   15   20    9 |    29   30   28   39   40   29   31    29
 R11E | 1732    7    8   20   10   13   20   17    7 |    71   71   73   73   77   81   68    73
 R13E | 1946   19   18   17   16   21   19   12    8 |    94   95   99   99  103   99   97    97
 R14E | 4144   19   15   24   13   16   17   14    7 |    60   60   54   55   57   64   50    55
 R15E | 1777   14   11   29   17   24   21   21    9 |    26   28   16   25   38   32   28    23
 R16E |  984   19   27   22   24   36   29   31   12 |    33   31   41   53   40   38   43    38
 R17  | 1700   27   33   20   14   21   20   19    9 |    42   47   28   31   39   20   29    28
 R18  | 1052   16   20   15   13   12   22   17    7 |    35   37   31   33   34   17   34    28
 R19  | 2469   77   76   56   53   75   31   65   27 |    74   80   50   50   78   54   45    48
 R20  | 1389   27   20   42   19   17   40   27   13 |    46   38   31   40   37   56   34    35
 R21  |  931   26   36   26   19   30   14   30   11 |    44   54   34   35   53   34   26    34
 R22  |  695   29   31   23   15   14   11   28    9 |    45   46   32   32   33   28   26    30
 R23  | 1878   19   15   17   40   27   29   19   12 |    60   62   64   76   47   60   63    60
 R24  | 1441   27   27   31   37   37   56   19   16 |    30   40   38   55   45   23   34    31
XR26  | 3941   25   54  ---  ---  ---   23   27   17 |    43   66  ---  ---  ---   47   38    39
------+----------------------------------------------+------------------------------------------
 RMS  | 1993   27   28   27   23   27   25   25      |T   47   49   44   47   49   41   39    41
 WRMS | 1993   23   25   27   17   23   22   25      |NE  45   49   42   44   45   35   33    37
 MEDI | 1441   19   19   22   15   21   20   19      |MD  43   42   40   43   45   34   34    36

Table 3.2032.2  GPS week: 2032   Day: 2   MJD: 58470                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  IGL |   cod  cof  emx  esx  gfz  grg  iac   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  843   68   65   53   34   51   39   37   21 |    68   69   70   42   67   22   27    39
 R02  | 2375   10   13   10   14   16   13   18    6 |    39   45   44   43   44   38   33    38
 R03  | 1262   11   16   13    9   14   13    8    5 |    47   50   48   53   62   55   56    52
 R04  | 1399    9   11   15    8   16   15   16    6 |    40   42   47   42   47   29   31    37
 R05  |  576   16   24   34   14   22   27   17   10 |    39   48   46   35   40   20   39    31
 R07  | 1368   11   16   15    9   17   12   22    6 |    53   55   52   50   45   51   35    46
 R08  | 2223   17   18   18   24   14    7   20    8 |    41   40   46   58   49   45   38    46
 R09E | 3874   12   14   18   13   21   12   15    6 |    42   39   45   49   52   47   55    47
 R10E | 1215   13   16   28   14   14   20   19    8 |    28   31   27   35   34   30   32    28
 R11E | 1440   13   14   21   16   13   13   12    6 |    43   45   46   40   44   38   44    40
 R13E |  956    7   11   18   15   25   15   15    7 |    58   59   55   56   78   61   55    58
 R14E | 4100   16   18   23   12   14   13   15    7 |    48   52   49   46   48   50   44    46
 R15E | 1826   13   14   23   13   24   15   16    7 |    31   34   27   31   41   32   28    29
 R16E | 1500   23   34   42   17   39   21   30   13 |    49   48   41   45   48   61   49    44
 R17  | 1809   20   16   19   12   12   16   20    7 |    56   51   45   45   39   53   35    44
 R18  | 1146   12   12   23   16   10   14   19    7 |    39   43   31   45   41   33   39    36
 R19  | 2461   83   84   62   56   75   22   64   27 |    75   80   50   44   70   28   35    29
 R20  |  925   19   27   41   20   23   32   26   12 |    48   52   32   37   46   53   33    37
 R21  |  733   26   23   22   16   21   14   30    9 |    54   50   41   34   54   47   36    41
 R22  |  697   25   29   24   19   27   13   27   10 |    53   55   35   35   53   37   28    37
 R23  |  795   20   21   14   35   33   20   27   11 |    39   39   51   62   39   41   58    46
 R24  | 2557   26   32   27   47   57   45   24   18 |    51   71   53   79   62   38   48    50
XR26  | 3998   20   62  ---  ---  ---   13   16   11 |    38   71  ---  ---  ---   41   42    43
------+----------------------------------------------+------------------------------------------
 RMS  | 1890   28   30   29   23   30   21   25      |T   46   50   44   45   50   41   40    41
 WRMS | 1890   23   24   29   19   20   20   25      |NE  48   53   46   46   50   39   38    40
 MEDI | 1399   16   18   22   15   21   15   19      |MD  47   50   46   44   47   41   38    41

Table 3.2032.3  GPS week: 2032   Day: 3   MJD: 58471                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  IGL |   cod  cof  emx  esx  gfz  grg  iac   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  577   49   44   33   28   28   16   37   14 |    76   82   68   54   60   53   38    55
 R02  | 2342   15   15   19   15   20   24   11    8 |    43   41   46   41   39   24   35    35
 R03  | 1290   12   12   16   11   16    9   16    6 |    53   54   60   49   48   51   43    50
 R04  | 2046   11   12   14   17   19   17   22    7 |    45   46   55   34   47   57   32    44
 R05  |  580   15   19   18   21   28   33   12   10 |    42   42   48   52   58   23   34    38
 R07  |  738    7    9   10   22   16   17   16    7 |    58   59   59   77   74   54   54    61
 R08  | 1297   22   18   19   15   38   10   27    9 |    50   55   64   60   83   60   40    58
 R09E | 3290   15   16   18   17   18   13   17    7 |    34   40   34   38   39   35   41    34
 R10E | 1197   10   14   22   14   12   13   14    6 |    32   32   27   35   32   29   33    29
 R11E | 1129    8   12   24   11   19   13   14    6 |    37   39   37   41   45   33   36    36
 R13E | 2734   14   15   15   15   17   18   15    7 |   135  134  138  136  134  125  142   134
 R14E | 3222   16   16   26   14   23   15   17    8 |    43   45   41   48   50   44   46    41
 R15E | 1535   13   10   22   10   20   11   18    7 |    33   34   22   28   41   26   31    28
 R16E |  670   28   29   35   15   49   26   34   14 |    36   50   42   56   88   55   47    49
 R17  | 1858   16   18   19   12   17   11   22    7 |    60   63   44   55   59   57   42    52
 R18  |  998   14   18   21   21   13   10   16    7 |    40   39   37   57   42   48   40    43
 R19  | 3060   81   95   52   45   63   22   57   24 |    90  100   28   35   81   54   26    39
 R20  | 1128   16   27   34   17   34   26   30   11 |    49   59   30   37   63   57   25    40
 R21  |  583   25   26   21   27   36   13   34   11 |    61   62   42   35   70   48   34    45
 R22  |  753   28   29   23   19   29   15   38   11 |    62   61   37   35   62   50   26    43
 R23  |  466   26   30   16   32   37   12   30   11 |    30   29   36   56   27   35   51    35
 R24  | 2239   20   21   26   41   47   45   24   16 |    61   63   51   81   64   54   61    58
XR26  | 7095   25  116  ---  ---  ---   24   31   18 |    24  121  ---  ---  ---   25   29    15
------+----------------------------------------------+------------------------------------------
 RMS  | 1779   26   29   24   22   30   20   26      |T   51   58   47   51   59   47   42    46
 WRMS | 1779   22   24   24   19   23   18   26      |NE  52   61   47   50   58   46   38    44
 MEDI | 1290   16   18   21   17   20   15   22      |MD  45   54   42   48   58   50   38    43

Table 3.2032.4  GPS week: 2032   Day: 4   MJD: 58472                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  IGL |   cod  cof  emx  esx  gfz  grg  iac   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  686   37   45   38   35   17   24   33   14 |    73   81   74   42   51   46   42    53
 R02  | 1401   19   22   19   13   12   29   10    8 |    43   43   44   37   38   22   35    34
 R03  |  965    8    9   10   20   19   17   17    7 |    44   47   54   66   45   49   38    48
 R04  |  964    9   12   15   11   14   11   27    6 |    43   44   54   40   39   38   24    38
 R05  |  738   12   18   31   19   20   31   21   10 |    36   42   57   45   50   21   23    36
 R07  | 1063   11    7   12   10   14   29   18    7 |    54   50   57   52   52   28   50    48
 R08  |  566   17   22   11   29   17   11   25    8 |    45   42   55   67   57   42   37    49
 R09E | 3040   15   15   15   16   23   12   12    7 |    31   34   38   39   44   41   40    36
 R10E | 1608    9   11   24   13   11   13   11    6 |    26   29   28   36   34   26   34    28
 R11E | 1177   13    9   20   20   10   26    9    7 |    43   45   39   40   43   59   50    43
 R13E | 4767   16   16   23   19   20   18   18    8 |    89   95   91  110  106  107   94    98
 R14E | 2087   14   14   23   23   16   16   18    8 |    38   35   34   57   51   49   37    42
 R15E |  974   11   14   28   18   33   18   18    9 |    31   35   22   33   50   28   29    29
 R16E |  992   15   18   42   21   45   48   27   15 |    31   35   38   35   43   62   36    31
 R17  | 1356   24   28   22   23   14   17   24    9 |    58   61   39   39   51   52   35    45
 R18  | 1233   12   16   18   22   13   11   12    6 |    41   48   37   50   48   48   45    43
 R19  | 4106   55   38   58   56   55   36   73   25 |    84   79   34   59   84   76   26    55
 R20  | 2295   22   16   33   24   34   22   39   13 |    48   44   29   31   57   41   41    36
 R21  | 1295   23   25   23   28   32   17   32   11 |    55   57   39   35   67   46   33    44
 R22  |  915   22   24   26   21   16   25   34   11 |    54   56   29   38   52   59   27    42
 R23  |  660   21   23   21   37   27   27   34   12 |    64   70   73   73   59   66   61    62
 R24  | 1631   21   24   31   27   26   34   23   12 |    54   67   60   64   65   43   53    52
XR26  | 3942   24  104  ---  ---  ---   21   17   15 |    37   91  ---  ---  ---   26   44    37
------+----------------------------------------------+------------------------------------------
 RMS  | 1902   21   21   27   25   25   24   28      |T   48   53   46   49   53   46   40    44
 WRMS | 1902   19   21   27   22   19   22   28      |NE  52   57   49   49   54   43   38    45
 MEDI | 1233   16   18   23   21   17   21   21      |MD  44   47   39   40   51   46   37    43

Table 3.2032.5  GPS week: 2032   Day: 5   MJD: 58473                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  IGL |   cod  cof  emx  esx  gfz  grg  iac   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1279   40   35   33   36   21   34   31   15 |    58   60   59   40   43   41   42    47
 R02  | 2519    9   21    7    8   11   14   25    5 |    42   51   38   39   40   43   36    39
 R03  | 1141    9    7   13   13   14   17   20    6 |    38   37   33   35   36   49   36    36
 R04  | 1235    6   10   10   15   13    9   22    5 |    37   39   38   42   29   36   29    34
 R05  |  764   11   17   38   15   30   19   21   10 |    28   28   49   24   35   30   19    26
 R07  | 2190   11   14   12    9   12   36   20    8 |    46   47   47   42   44   26   55    41
 R08  | 1562   13   11   18   17   25   23   33    9 |    39   45   42   51   50   45   32    42
 R09E | 2823   10   16   15   10   15   13   23    6 |    49   50   52   47   56   53   56    50
 R10E | 2807   10   13   20   19   16   17   23    7 |    32   39   31   40   37   40   31    33
 R11E | 1062    9   16   17    9   10   12   13    5 |    47   50   51   50   50   48   48    48
 R13E |  879   17   18   24   20   19   17   27    9 |   215  223  219  226  222  224  221   220
 R14E | 2694    8   12   20   14   16   16   15    6 |    45   46   49   47   45   52   38    44
 R15E | 2834   11   11   25   17   26   15   21    8 |    25   27   24   32   41   28   30    26
 R16E | 2801   15   17   34   24   43   42   27   14 |    36   45   38   47   37   52   36    33
 R17  | 1043   21   25   25   21   26   12   34   10 |    48   50   33   32   55   37   21    38
 R18  | 1372    8   10   16   13    9   14    8    5 |    36   38   28   41   43   33   35    35
 R19  | 3452   46   62   62   67   78   55   80   28 |    58   74   32   43   91   80   25    47
 R20  | 3499   25   39   36   26   19   35   30   13 |    51   60   29   39   43   51   37    38
 R21  | 2170   30   28   20   16   19   28   21   10 |    50   48   36   31   42   21   34    35
 R22  | 1680   24   19   25   29   15   31   32   11 |    51   44   31   31   46   61   30    40
 R23  | 1193   17   23   16   33   22   32   30   11 |    37   45   37   47   33   39   44    35
 R24  | 1063   17   21   27   25   28   42   27   12 |    38   37   53   50   39   37   46    39
XR26  | 5081   16   48  ---  ---  ---   18   21   13 |    38   58  ---  ---  ---   32   44    39
------+----------------------------------------------+------------------------------------------
 RMS  | 2097   20   23   26   24   26   27   30      |T   49   53   47   48   52   50   44    46
 WRMS | 2097   19   21   26   19   20   23   30      |NE  43   47   39   39   44   41   35    38
 MEDI | 1680   13   17   20   17   19   18   23      |MD  42   46   38   41   43   41   36    39

Table 3.2032.6  GPS week: 2032   Day: 6   MJD: 58474                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  IGL |   cod  cof  emx  esx  gfz  grg  iac   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1551   53   52   35   37   30   20   25   16 |    86   84   80   53   58   52   49    61
 R02  | 2332   10   10   12   10   17   19   17    6 |    56   56   55   53   57   36   43    49
 R03  | 1938    9   15   10   12   13   11   14    5 |    60   62   58   66   61   60   50    58
 R04  |  796   10   11   12   12   14    9   16    5 |    53   56   59   54   51   50   41    50
 R05  | 1103   16   20   44   17   26   12   26   11 |    40   48   62   51   55   42   33    42
 R07  | 2535   13   12    7   10   13   14   15    5 |    66   67   68   63   65   56   62    62
 R08  | 1267   21   26   19   29   17   17   19    9 |    58   56   62   81   75   72   57    67
 R09E | 3288   14   13   19   16   32   14   11    8 |    74   75   74   77   84   76   79    76
 R10E | 3481   15   20   18   12   23   26   15    8 |    34   39   29   42   37   39   39    34
 R11E | 1435   11   12   18   11   19   14   13    6 |    71   71   71   75   77   73   78    73
 R13E | 1673   14   16   23   22   15   17   15    8 |   193  195  191  197  198  194  194   194
 R14E | 2623   12   16   22   22   17   17   16    8 |    58   55   60   50   51   64   46    53
 R15E | 1898   10    9   25   14   27   26   17    9 |    37   39   35   35   50   49   43    38
 R16E | 2520   17   34   36   29   60   41   31   16 |    53   58   46   63   61   58   58    51
 R17  | 1547   26   25   20   17   17   16   35   10 |    75   72   46   46   65   63   39    55
 R18  | 1311   15   14   23   19   18   18   12    8 |    54   53   44   60   63   44   52    52
 R19  | 3451   69   64   57   67   82   36   76   29 |   107  109   34   56  118   85   40    60
 R20  | 3008   37   49   36   42   23   37   32   16 |    84   92   45   63   77   81   50    63
 R21  | 2256   25   25   18   12   17   13   27    8 |    78   79   57   55   77   59   48    61
 R22  | 1976   28   33   20   22   16   16   23    9 |    80   84   58   56   71   68   46    61
 R23  |  847   21   22   21   22   21   20   28   10 |    41   43   47   64   38   37   57    44
 R24  | 1226   12   25   48   19   31   61   17   16 |    56   59   73   65   59   46   63    56
XR26  | 5320   18   93  ---  ---  ---   10   19   11 |    48   85  ---  ---  ---   38   55    48
------+----------------------------------------------+------------------------------------------
 RMS  | 2157   25   28   28   25   29   25   26      |T   67   71   61   64   70   62   57    61
 WRMS | 2157   29   29   28   20   22   20   26      |NE  65   69   56   59   66   55   49    55
 MEDI | 1938   15   20   20   17   18   17   17      |MD  58   62   58   56   61   58   50    56



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