[IGSREPORT-27164] Wk 2096 IGLOS Final Orbits

acc acc at igs.org
Fri Mar 27 21:47:36 PDT 2020


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2096   (Mar 08, 2020 - Mar 14, 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 2.2096.
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:
                                                                               
 igl2096[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2096 in the SP3 format.
 igl20967.sum      Combination Report for GPS Week 2096.


    
    
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  |     -3.5 ns
                1  |     -3.7 ns
                2  |     -5.7 ns
                3  |     -4.0 ns
                4  |     -3.5 ns
                5  |     -4.2 ns
                6  |     -4.0 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
               ----+--------+---------------
                4  |  IAC   | R24
                5  |  IAC   | R24
                6  |  IAC   | R24

    
         
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 1.2096, 1a.2096).
        
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 2.2096.0-6)                                                                                
    
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 3.2096.0-6). 
        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 2096 summary.                      (Mar 08, 2020 - Mar 14, 2020)

Table 1.2096.a     GPS week : 2096   MJD: 58916.0-58922.0

         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     2     0   -23    77   .04   23   19 |   19080      21   3165   8083
        |    1     1     1    19    10    23   .04           |     926     855
cof  n/a|    0     0     4     0    -7    83   .06   25   21 |   19081       6   3166   8082
        |    1     1     2    19    25    22   .04           |     926     861
emx  n/a|    0    -1    -9    46    34   -49   .02   33   32 |   -8904     417   3150   8136
        |    1     0     1    11    34    26   .05           |   10144     823
esx  n/a|   -1     0    -7     5   -26   -31   .15   33   28 |     266     237   3159   9716
        |    1     1     2    17    21    67   .04           |    8164    1485
gfz  n/a|    0     0     3   -40    10   -39   .04   22   17 |       0    -383   3196   7633
        |    1     0     2    26    23    34   .05           |       0    1329
iac  n/a|    0     0     6     5     4    13  -.15   20   18 |   -2483     -81   3164   8168
        |    1     1     3    19    29    57   .05           |     510     821
mcc  n/a|    6     0   -21   117   -22   225  -.42  190  190 |     ---     ---    ---    ---
        |    4    14    27   112   164   864   .26           |     ---     ---


Table 1.2096.b     GPS week : 2096   MJD: 58916.0-58922.0   

         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  |   22   24   20   20   18   21   25 |
 R02  |   11    9    9    9    7    8    9 |
 R03  |   10   10   11   11    9   11   12 |
 R04  |   18   11   10   13   13   13   13 |
 R05  |   17    9   12   10   11   10   12 |
 R07  |   13   11   10   10   12   11   11 |
 R08  |   12   11   11    9   11   10    9 |
 R09  |    6    7    9    6    8    7   12 |
 R11  |    7    6    5    5    7    9   13 |
 R12  |    8    7    6    9    8    7   12 |
 R13  |   11   10   11   13   14   13   18 |
 R14  |    8    8    5    6    5    5    7 |
 R15  |    7    6    9    9    8    9    9 |
 R16  |   15   15   14   14    8   10   14 |
 R17  |   11   12   11   11    9    8   10 |
 R18  |   12    8    8   10    9    6    8 |
 R19  |   23   23   19   19   19   21   21 |
 R20  |   15   14   17   22   31   36   37 |
 R21  |   12   11   12   13   11   12   13 |
 R22  |   12   14   12   10   12   13   12 |
 R23  |   10    9    9   10   11   13   12 |
 R24  |  ---  ---    0    0   45   20   23 |
 R26  |   17   24   19   21   15   19   20 |


Table 1.2096.c     GPS week : 2096   MJD: 58916.0-58922.0   

         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 2096 0   |  -52    79   188     272     798   -3435  81.4  1355  1355 |   -3503       0
brd 2096 1   |  -80    43    81    -186     576   -4294  81.9  1304  1304 |   -3656       0
brd 2096 2   |  -48    -6   165    -232     932   -5635  80.9  1572  1572 |   -5744       0
brd 2096 3   |  -42   -31   173    -681    -681   -4887  80.9  1479  1479 |   -3966       0
brd 2096 4   |    9    16   180    -562    -172   -2501  81.2  1408  1408 |   -3535       0
brd 2096 5   |   76    66   153     148    -330   -2655  81.8  1555  1555 |   -4159       0
brd 2096 6   |    9    66   210   -1679   -1497    -461  82.7  1804  1804 |   -4025       0
-------------+------------------------------------------------------------+----------------
brd 2096 mean|  -18    33   164    -417     -53   -3409  81.5  1496  1496 |   -4084       0
brd 2096 sdev|   53    41    41     654     881    1732    .7   167   167 |     774       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 2.2096.0  GPS week: 2096   Day: 0   MJD: 58916                            

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   -13   -28    74  -.00   25   17 |   19075    1675   3178   7223
cof  n/a|    1    -1     6    35   -26   119   .05   26   22 |   19068    1665   3181   7221
emx  n/a|   -1     0    -9    60    84   -73   .02   31   28 |  -14957    1934   3161   7230
esx  n/a|    0     0    -3    11    -3    96   .17   30   28 |     345    2809   3155   9079
gfz  n/a|    0     0     6   -36    31    28   .03   21   14 |       0    1368   3214   6873
iac  n/a|    1     0     0   -15   -33  -112  -.11   22   21 |   -1830      71   3168   7290
mcc  n/a|    6    15    10    74  -207  -877  -.79  319  319 |     ---     ---    ---    ---

Table 2.2096.1  GPS week: 2096   Day: 1   MJD: 58917                            

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     1    -3   119   .10   25   23 |   20599     351   3006   7841
cof  n/a|    2     0     0   -23    15    82   .10   29   27 |   20597     349   3003   7836
emx  n/a|   -3     0    -6    27    33   -70   .11   29   29 |  -13531     796   2981   7965
esx  n/a|   -2    -1    -8     3   -30  -106   .13   30   28 |   -2739   -1314   2996   9619
gfz  n/a|    0    -1     2   -37   -22   -69   .06   20   16 |       0    1114   3005   7472
iac  n/a|    1     2     6    13    19    58  -.24   18   17 |   -2131     113   3011   8045
mcc  n/a|    4    -5   -27    86   -15   215  -.50  229  229 |     ---     ---    ---    ---

Table 2.2096.2  GPS week: 2096   Day: 2   MJD: 58918                            

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     4   -35    60   .07   23   20 |   19804   -1065   3059   9200
cof  n/a|    1     0     1   -14   -33    60   .06   26   21 |   19815   -1099   3056   9196
emx  n/a|    2    -2   -10    45    -2   -31   .02   30   30 |    1871    -426   3044   9331
esx  n/a|    0     0    -8   -29   -19   -90   .10   29   26 |   -4979   -1667   3071  11237
gfz  n/a|    0    -1     5   -17    29   -63   .04   22   19 |       0   -2316   3113   8666
iac  n/a|    0     2     5    -9     8    42  -.14   15   13 |   -3128   -1427   3065   9291
mcc  n/a|    8   -26   -48   307  -100  1057  -.29  167  167 |     ---     ---    ---    ---

Table 2.2096.3  GPS week: 2096   Day: 3   MJD: 58919                            

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   -12   -17    43   .02   21   19 |   18961      63   3345   7979
cof  n/a|    0     0     6    -4     3    86   .12   23   20 |   18973      37   3350   7980
emx  n/a|    2     0    -7    43    65   -76   .07   31   31 |    -278     450   3318   8000
esx  n/a|   -1    -1    -9    21   -51   -13   .20   32   30 |   10910     427   3333   9751
gfz  n/a|   -2    -1     1   -24    16   -19   .06   19   17 |       0    -445   3376   7640
iac  n/a|    1     0     8    -3   -13    29  -.16   18   16 |   -3206    1339   3338   7994
mcc  n/a|    9    -5   -66   178   227  1523  -.45  165  165 |     ---     ---    ---    ---

Table 2.2096.4  GPS week: 2096   Day: 4   MJD: 58920                            

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     3   -29   -28    89   .04   21   15 |   18991    -510   2792   8648
cof  n/a|    0     3     2    -5   -27    71  -.00   22   17 |   18983    -514   2794   8651
emx  n/a|    0    -1    -8    49    55   -23   .00   32   32 |    2959    -408   2765   8692
esx  n/a|   -3     0    -6     0   -54   -63   .13   38   27 |   12021     612   2783  10206
gfz  n/a|    0    -1     0   -39   -21   -52   .06   20   18 |       0    -309   2824   8136
iac  n/a|    0    -1     7    25    52    39  -.14   20   17 |   -2246    -393   2785   8783
mcc  n/a|    8    13    -6   158   173   363  -.51  123  123 |     ---     ---    ---    ---

Table 2.2096.5  GPS week: 2096   Day: 5   MJD: 58921                            

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     3    21   -21    72   .09   22   18 |   18418    -129   3575   8200
cof  n/a|   -1     0     3     9    32    58   .06   25   21 |   18411    -138   3576   8199
emx  n/a|    0     0   -10    62     8   -56  -.03   39   39 |  -16346     -25   3589   8207
esx  n/a|    0     0    -8     8   -27   -28   .20   38   28 |   -9167     824   3597   9555
gfz  n/a|    0    -1     4   -98    29   -56   .10   25   18 |       0    -468   3644   7678
iac  n/a|    0     1     5    35    20    15  -.18   19   16 |   -2341      25   3605   8187
mcc  n/a|   12     3    -5    69   -74   -33  -.45  153  153 |     ---     ---    ---    ---

Table 2.2096.6  GPS week: 2096   Day: 6   MJD: 58922                            

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     5    26   -29    79  -.00   24   20 |   17718    -232   3200   7494
cof  n/a|    2     0     8     9   -14   104   .02   26   23 |   17723    -258   3206   7496
emx  n/a|    0    -1   -11    39     0   -12  -.04   37   37 |  -22047     601   3196   7533
esx  n/a|    0     1    -7    23     1   -14   .10   36   26 |   -4524     -29   3179   8567
gfz  n/a|    0     1     2   -32    12   -41  -.05   25   17 |       0   -1626   3201   6971
iac  n/a|    2     0    10    -6   -22    23  -.09   32   27 |   -2504    -300   3178   7591
mcc  n/a|   -3     3    -6   -54  -161  -672   .06  173  173 |     ---     ---    ---    ---

       
       
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 3.2096.0  GPS week: 2096   Day: 0   MJD: 58916                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  iac  mcc  IGL |   cod  cof  emx  esx  gfz  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  674   52   41   50   48   38   28  ---   21 |    82   82   47   69   76   54  ---    57
 R02E | 1133   11   19   27   15   27   20  500   10 |   100  103   86   92  108   92  151    96
 R03  | 1211   15   17   32   18    9   23  235   10 |    87   83   61   67   78   85  100    75
XR04  |  721   23   30   32   34  ---   32  ---   17 |   105   95   90   87  ---   86  ---    89
 R05  | 2910   40   22   40   25   36   15  ---   16 |   133  133  122  126  147  119  ---   128
 R07  | 1465   27   27   33   24   16   30  293   13 |   114  118   97  102  116   96  110   103
 R08  | 1797   26   16   35   18   22   19  ---   12 |    98  101   82   95  110  108  ---    99
 R09  |  785   11   20   17   12    8    7  ---    5 |    23   24   17   34   30   25  ---    24
 R11  |  884    7    8   12   10   15   20  323    7 |    28   32   28   31   30   28   90    25
 R12  | 1847   11   17   19   13   12   18  ---    7 |    34   36   31   37   35   32  ---    31
 R13  | 1064   27   25   18   22   22   16  ---   11 |    36   39   32   39   33   24  ---    28
 R14  |  683    7   11   14   14   15   22  ---    7 |    27   30   27   36   29   40  ---    29
 R15  |  608   10   10   12   22   10   10  ---    6 |    23   24   24   29   27   28  ---    24
 R16  | 1934   43   50   43   21   12   11  ---   14 |    32   33   29   42   37   28  ---    29
 R17  |  616   12   16   23   37   17   12  ---   10 |    72   73   62   43   76   75  ---    67
 R18  |  694   17   22   27   24   17   31  ---   11 |    45   46   42   46   66   67  ---    53
 R19  |  604   38   43   48   75   35   34  ---   23 |   100  103   50   41   87   86  ---    70
 R20  |  954   30   45   39   18   25   32  ---   14 |   183  175  181  183  182  179  ---   178
 R21  | 1501   11   12   28   37   17   24  113   12 |    69   68   47   43   81   82   63    66
 R22  | 2078   12   21   25   43   12   22  ---   12 |    73   76   50   40   81   81  ---    67
 R23  |  661   17   14   27   27   13   15  ---   10 |    46   52   42   68   60   59  ---    54
XR26  | ----   17   79  ---  ---  ---   16  ---   17 |    45   63  ---  ---  ---   53  ---    51
------+----------------------------------------------+------------------------------------------
 RMS  | 1355   25   26   31   30   21   22  319      |T   70   72   59   64   74   69  102    65
 WRMS | 1355   17   22   28   28   14   21  319      |NE  69   70   58   62   72   68   90    64
 MEDI |  954   17   20   27   22   16   20  293      |MD  69   68   47   43   76   67  100    57

Table 3.2096.1  GPS week: 2096   Day: 1   MJD: 58917                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  iac  mcc  IGL |   cod  cof  emx  esx  gfz  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  974   59   66   61   44   47   26  ---   24 |    59   60   35   45   52   41  ---    37
 R02E |  687   15   11   33    9   16   14  343    9 |    58   56   47   50   55   67  144    55
 R03  |  813   18   29   31   18   15   13  174    9 |    62   70   46   46   55   58   88    53
XR04  |  493   15   32   27   22  ---   14  ---   11 |    57   63   36   44  ---   53  ---    46
 R05  | 1527   17   16   26   21   17   11  ---    9 |    66   56   56   60   57   56  ---    57
 R07  |  752   17   14   34   23   12   21  160   10 |    64   60   51   46   55   62   91    54
 R08  | 2669   16   21   34   15   11   26  ---   11 |    58   58   46   50   61   73  ---    57
 R09  | 1040   16   16   13   16    7   14  ---    6 |    20   17   19   21   17   19  ---    16
 R11  |  723    8   11   11   12   12   10  279    5 |    16   18   14   26   24   24   49    18
 R12  | 1391   15   14   12   23    9   11  ---    7 |    19   20   16   27   24   22  ---    18
 R13  | 2247   23   36   25   22   20   11  ---   10 |    18   31   24   42   31   21  ---    22
 R14  | 1134   11   11   14   15   15   17  ---    7 |    22   24   17   30   27   25  ---    20
 R15  |  567    9   10   11   14    9   11  ---    5 |    18   20   13   28   20   21  ---    16
 R16  | 2097   50   57   19   15   30   18  ---   15 |    27   32   35   21   28   22  ---    21
 R17  |  769   17   17   22   40   19   14  ---   11 |    43   42   38   28   51   49  ---    41
 R18  |  856    8   11   22   15   18   11  ---    7 |    27   29   24   21   35   35  ---    28
 R19  |  689   46   58   37   84   26   27  ---   23 |    62   76   47   36   57   53  ---    46
 R20  |  745   30   39   38   19   28   22  ---   14 |   129  114  142  139  116  127  ---   128
 R21  | 1509   10   10   28   32   21   15  107   11 |    41   37   30   32   51   46   48    40
 R22  | 1545   13   12   33   45   21   27  ---   14 |    51   51   36   40   66   67  ---    52
 R23  |  542   17   16   20   24   10   15  ---    8 |    35   39   35   45   38   46  ---    39
XR26  | ----   25   47  ---  ---  ---   23  ---   24 |    26   61  ---  ---  ---   42  ---    34
------+----------------------------------------------+------------------------------------------
 RMS  | 1304   25   29   29   30   20   18  229      |T   44   47   38   41   46   46   84    40
 WRMS | 1304   23   27   29   28   16   17  229      |NE  43   46   38   41   45   45   69    40
 MEDI |  856   16   16   26   21   16   14  174      |MD  41   42   35   40   51   46   88    39

Table 3.2096.2  GPS week: 2096   Day: 2   MJD: 58918                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  iac  mcc  IGL |   cod  cof  emx  esx  gfz  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1210   57   70   48   52   31   15  ---   20 |    70   84   30   30   50   32  ---    35
 R02E |  913   15   15   32   12   19   10  207    9 |    54   57   33   43   60   53  114    49
 R03  |  810   23   16   29   23   25    9  123   10 |    60   57   32   37   67   47   74    48
XR04  |  490   17   20   23   19  ---   12  ---   10 |    58   55   36   38  ---   48  ---    45
 R05  |  864   17   14   45   19   24   14  ---   12 |    55   60   39   56   67   60  ---    54
 R07  | 1613   15   17   32   20   19   12   51    9 |    67   68   35   46   62   63   79    56
 R08  | 3521   24   24   31   14   17   17  ---   10 |    59   55   39   54   64   59  ---    55
 R09  | 1358   18   15   22   14   17   15  ---    8 |    15   16   15   22   28   22  ---    16
 R11  |  634    9   14   10   12    8   10  255    5 |    18   25   17   21   19   27   76    16
 R12  | 1028   12   16   15   17    7    9  ---    6 |    27   30   32   27   29   27  ---    26
 R13  | 3415   31   35   13   19   26   10  ---   10 |    21   30   29   39   38   24  ---    26
 R14  | 1451    7   12   10   12    7    9  ---    4 |    27   29   28   38   33   37  ---    31
 R15  | 1025   12   17   10   26   20   17  ---    9 |    24   30   22   34   26   32  ---    24
 R16  | 2667   30   24   28   20   37   19  ---   13 |    29   41   25   36   52   29  ---    30
 R17  |  598   15   15   26   34   22   11  ---   10 |    52   54   41   36   67   58  ---    52
 R18  |  736   10   11   26   13   24    7  ---    8 |    37   37   31   42   55   39  ---    40
 R19  |  606   41   37   41   63   25   20  ---   19 |    69   65   51   35   41   50  ---    46
 R20  | 1033   23   36   50   37   34   28  ---   17 |   176  173  148  178  181  174  ---   170
 R21  |  822   11   16   30   40   14   20  117   12 |    44   50   32   30   47   55   46    42
 R22  | 1281   12   14   28   37   26   12  ---   11 |    51   51   35   32   59   54  ---    47
 R23  |  905   19   20   17   30   17   10  ---    9 |    32   32   33   50   46   37  ---    37
XR24  | ----    4 >>>>  ---  ---  ---  ---  ---    0 |   203 9999  ---  ---  ---  ---  ---   205
XR26  | ----   23   37  ---  ---  ---   16  ---   19 |    38   37  ---  ---  ---   47  ---    44
------+----------------------------------------------+------------------------------------------
 RMS  | 1572   23   26   30   29   22   15  167      |T   55   51   37   44   54   48   77    51
 WRMS | 1572   20   21   30   26   19   13  167      |NE  56   51   37   44   54   48   68    52
 MEDI | 1025   17   17   28   20   20   12  123      |MD  51   50   32   37   50   47   76    44

Table 3.2096.3  GPS week: 2096   Day: 3   MJD: 58919                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  iac  mcc  IGL |   cod  cof  emx  esx  gfz  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  740   49   53   48   55   29   13  ---   19 |    76   82   38   28   55   40  ---    43
 R02E | 2065    7   14   30   19   10   15  172    8 |    59   62   40   51   64   74  140    59
 R03  |  952   16   22   32   26   23   13   94   11 |    66   72   37   38   72   61  102    56
XR04  |  549   17   18   27   22  ---   22  ---   12 |    51   53   37   36  ---   61  ---    46
 R05  |  780   16   22   34   22   15   16  ---   10 |    56   58   29   44   54   54  ---    47
 R07  | 2466   15   15   31   24   20   13  149   10 |    66   66   38   40   64   62  104    55
 R08  | 2367   17   18   28   12   12   14  ---    8 |    55   58   35   48   52   56  ---    49
 R09  | 1862   10   16   18   11   11   10  ---    6 |    21   21   16   27   26   20  ---    20
 R11  |  556    7    9    8    9   11   13  246    5 |    18   21   18   26   22   22   90    18
 R12  |  812   17   16   12   20   18   17  ---    8 |    21   19   24   21   21   22  ---    15
 R13  | 2788   31   25   30   26   20   21  ---   12 |    27   32   37   32   31   23  ---    24
 R14  |  959    7   11    8   12    8   15  ---    5 |    19   24   17   20   20   23  ---    16
 R15  | 1745   10   11   17   20   24   10  ---    8 |    16   18   14   25   39   23  ---    20
 R16  | 1421   32   32   35   28   27   15  ---   13 |    25   32   38   38   42   31  ---    28
 R17  |  734   18   18   24   40   10   15  ---   11 |    60   60   45   30   46   58  ---    48
 R18  |  745   14   18   28   15   14   22  ---    9 |    43   47   33   41   57   60  ---    47
 R19  |  567   32   26   43   62   23   31  ---   18 |    70   65   46   38   58   46  ---    46
 R20  |  979   24   32   62   57   29   44  ---   21 |    85  105   73   66   95  103  ---    82
 R21  |  579   10   11   32   42   23   17  119   12 |    55   53   38   32   64   59   31    50
 R22  | 1900   15   19   23   31   23    9  ---   10 |    51   55   34   29   57   45  ---    43
 R23  | 1100   25   25   21   31   12   10  ---   10 |    27   28   27   49   39   41  ---    35
XR24  |>>>>>    3   64  ---  ---  ---  ---  ---    0 |   164 9999  ---  ---  ---  ---  ---   170
XR26  | ----   23   58  ---  ---  ---   18  ---   20 |    46   82  ---  ---  ---   66  ---    56
------+----------------------------------------------+------------------------------------------
 RMS  | 1479   21   23   31   32   19   18  165      |T   51   50   34   36   48   47   93    46
 WRMS | 1479   19   20   31   30   17   16  165      |NE  50   50   33   35   48   46   81    46
 MEDI |  959   16   18   28   24   18   15  149      |MD  51   53   37   36   52   46  102    46

Table 3.2096.4  GPS week: 2096   Day: 4   MJD: 58920                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  iac  mcc  IGL |   cod  cof  emx  esx  gfz  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1089   42   45   42   57   24   21  ---   18 |    60   62   37   44   39   43  ---    37
 R02E | 3251    7    9   26   10   10   14  112    7 |    58   61   49   62   62   73  139    61
 R03  | 2189   18   18   29   14   11   12   93    8 |    65   64   39   45   53   59   66    54
XR04  |  557   22   31   24   29  ---   12  ---   12 |    59   64   34   34  ---   49  ---    44
 R05  |  943   15   12   32   25   22   15  ---   11 |    50   46   26   44   58   44  ---    44
 R07  | 1383    9   10   38   26   23   14  104   11 |    68   63   41   45   79   72   94    64
 R08  | 1474    8   12   39   17   20   17  ---   10 |    60   62   39   49   66   70  ---    58
 R09  | 1127   16   17   15   19   16   16  ---    8 |    19   21   15   31   29   20  ---    17
 R11  |  614   10   10   15   14   12   16  183    6 |    24   23   19   22   26   25  109    21
 R12  |  587    8   20   24   29    9   12  ---    8 |    26   30   32   30   29   28  ---    25
 R13  | 1672   33   29   23   30   31   17  ---   14 |    17   22   31   30   26   20  ---    19
 R14  |  745   13   11    9    7    8   12  ---    5 |    19   22   17   32   27   28  ---    23
 R15  |  963   11   14   14   19   13   18  ---    7 |    24   23   18   24   15   28  ---    18
 R16  |  635   17   24   17   23   13   12  ---    8 |    23   26   24   40   37   28  ---    27
 R17  | 1313   14   13   23   32   11   10  ---    8 |    49   45   38   28   46   46  ---    42
 R18  |  945   13   11   28   10    9   24  ---    9 |    36   36   34   38   42   54  ---    40
 R19  | 1990   33   40   41   68   25   31  ---   19 |    40   51   44   49   55   30  ---    35
 R20  |  939   42   42   81   97   48   52  ---   31 |   208  193  163  160  172  194  ---   178
 R21  |  628   10   14   27   45   18   12   99   11 |    48   50   37   25   48   51   66    43
 R22  | 1623   15   15   28   37   16   24  ---   11 |    55   54   47   41   57   71  ---    55
 R23  |  969   21   23   24   41   12   13  ---   11 |    26   27   27   55   37   36  ---    32
XR24  |>>>>>   46   48  ---  ---   43 4109  ---   45 |    69 9999  ---  ---   53 9999  ---    73
XR26  | ----   14   68  ---  ---  ---   15  ---   15 |    49  107  ---  ---  ---   46  ---    46
------+----------------------------------------------+------------------------------------------
 RMS  | 1407   21   22   32   38   20   20  123      |T   50   52   38   44   50   50   94    45
 WRMS | 1407   15   17   32   27   18   17  123      |NE  49   51   38   43   49   49   83    45
 MEDI |  969   15   17   26   26   16   15  104      |MD  49   46   34   40   46   44   94    42

Table 3.2096.5  GPS week: 2096   Day: 5   MJD: 58921                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  iac  mcc  IGL |   cod  cof  emx  esx  gfz  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1527   39   34   47   51   51   27  ---   21 |    62   53   33   43   75   42  ---    45
 R02E | 3355   11   12   23   10   18   14  147    8 |    54   56   49   55   60   58  157    54
 R03  | 1884   11    8   35   30   17   17  124   11 |    66   63   53   52   74   75   80    65
XR04  | 1210   17   21   33   26  ---   18  ---   13 |    65   62   41   40  ---   69  ---    56
 R05  | 1431   20   17   31   25   13   15  ---   10 |    60   57   41   47   55   61  ---    52
 R07  |  719   15   21   35   31   20   14  127   11 |    68   68   46   47   69   67   85    60
 R08  | 1581   16   20   36   16   21   12  ---   10 |    64   66   42   53   66   64  ---    59
 R09  |  668   12    9   16   12   14   12  ---    6 |    15   16   20   20   18   18  ---    14
 R11  |  546   15   11   25   11   16   21  228    9 |    16   18   16   20   27   22   86    17
 R12  |  629   15    9   16   15   14    8  ---    7 |    30   27   22   30   33   24  ---    25
 R13  | 1847   36   43   21   35   18    8  ---   12 |    36   43   29   45   48   30  ---    35
 R14  | 1377    7   23   10   12    8   10  ---    4 |    22   22   20   26   21   21  ---    19
 R15  |  659   20   20   19   10   22   13  ---    8 |    19   16   12   20   39   27  ---    20
 R16  |  731   22   28   12   22   18   18  ---    9 |    26   35   37   34   31   34  ---    29
 R17  | 1635   11   10   24   22   15   13  ---    8 |    44   43   36   43   46   48  ---    43
 R18  | 1723    7   10   18   12   12    9  ---    5 |    30   28   25   28   33   30  ---    28
 R19  | 2758   40   33   52   72   27   21  ---   21 |    47   54   44   36   41   33  ---    34
 R20  |  551   32   57  122  100   61   47  ---   36 |   165  176  121  162  181  154  ---   155
 R21  |  501   11    9   32   39   25   15  108   12 |    36   33   30   31   47   37   46    34
 R22  | 1979   11   13   32   43   25   16  ---   12 |    34   39   28   24   49   42  ---    35
 R23  |  995   30   38   18   34   19   21  ---   12 |    26   34   27   38   33   42  ---    30
XR24  |>>>>>   20   41  ---  ---   20 1427  ---   20 |   122 9999  ---  ---   35  750  ---   108
XR26  | ----   20   69  ---  ---  ---   17  ---   18 |    25   62  ---  ---  ---   33  ---    26
------+----------------------------------------------+------------------------------------------
 RMS  | 1554   22   25   39   38   25   19  153      |T   49   48   36   42   51   77   90    45
 WRMS | 1554   18   21   39   28   18   16  153      |NE  49   48   36   41   51   78   74    44
 MEDI | 1377   16   20   25   25   18   15  127      |MD  36   43   33   38   46   42   85    35

Table 3.2096.6  GPS week: 2096   Day: 6   MJD: 58922                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  iac  mcc  IGL |   cod  cof  emx  esx  gfz  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  556   37   47   56   60   53   39  ---   24 |    90   96   55   63   98   54  ---    66
 R02E | 2843    9   13   26   14   17   15  177    8 |    74   70   51   72   79   69  204    69
 R03  | 1302   16   20   34   31   22   13  110   12 |    97   99   68   72  100   93  126    87
XR04  | 1317   22   26   27   25  ---   18  ---   13 |    92   94   60   63  ---   88  ---    76
 R05  | 1842   24   26   26   28   17   19  ---   11 |    85   90   57   61   78   85  ---    73
 R07  | 1490   22   22   26   26   21   16  131   11 |    93   93   63   62   91   75  146    78
 R08  |  685   16   19   25   16   15   14  ---    8 |    88   86   68   75   85   89  ---    81
 R09  |  820   13   19   12   15   13   49  ---   12 |    21   26   17   31   26   58  ---    27
 R11  |  795   13   18   20   12   13   54  269   13 |    24   27   20   22   22   51  114    24
 R12  |  726    9   16   35   22   17   34  ---   12 |    33   33   36   36   37   47  ---    32
 R13  | 5241   34   33   20   43   43   33  ---   18 |    41   49   54   49   53   47  ---    45
 R14  | 1152   14   17   11   13    9   21  ---    7 |    27   31   30   35   33   41  ---    31
 R15  |  691   16   21   11   20   12   27  ---    9 |    27   32   24   33   27   45  ---    29
 R16  | 1599   39   38   25   18   24   17  ---   13 |    29   28   46   38   50   49  ---    39
 R17  |  793   16   16   21   34   11   20  ---   10 |    73   71   54   40   69   75  ---    63
 R18  | 1834    7   11   24   12   18   18  ---    8 |    49   51   40   46   61   52  ---    50
 R19  | 2470   34   44   45   68   32   25  ---   21 |    78   78   50   39   71   71  ---    59
 R20  |  660   42   32  113   85   52   77  ---   37 |   210  201  169  189  204  206  ---   192
 R21  |  635   11   15   28   40   29   15  131   13 |    67   66   43   40   76   68   66    60
 R22  | 1739   17   16   27   38    9   23  ---   11 |    68   68   45   41   66   72  ---    59
 R23  | 1124   32   35   20   21   12   29  ---   12 |    36   38   36   61   45   63  ---    45
XR24  |>>>>>   23   57  ---  ---   23 3059  ---   23 |    95 9999  ---  ---   47 9999  ---    97
XR26  | ----   16   80  ---  ---  ---   22  ---   19 |    41   72  ---  ---  ---   51  ---    45
------+----------------------------------------------+------------------------------------------
 RMS  | 1803   24   26   37   36   25   32  173      |T   66   68   51   55   67   70  131    62
 WRMS | 1803   20   23   37   26   17   27  173      |NE  66   68   51   54   66   70  113    61
 MEDI | 1152   16   21   26   25   17   22  131      |MD  68   68   50   46   66   63  126    59



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