[IGSREPORT-29450] Wk 2272 IGLOS Final Orbits

acc acc at igs.org
Mon Aug 14 04:00:17 UTC 2023


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2272   (Jul 23, 2023 - Jul 29, 2023) 
                                                                               
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 2.2272.
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:
                                                                               
 igl2272[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2272 in the SP3 format.
 igl22727.sum      Combination Report for GPS Week 2272.


    
    
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.

Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.

 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).
    
    The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
    until TBA, therefore the iac orbits are not used in the orbit combinations but
    are inlcuded for statistics only from GPS week 2238 until TBA.
    
    JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
    are currently excluded from the combinations until the IGS ACC assessments
    are completed. However, they are included for comparison statistics only.

 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:
        https://files.igs.org/pub/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:
        https://files.igs.org/pub/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
        https://files.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  |      0.6 ns
                1  |     -2.0 ns
                2  |    -14.8 ns
                3  |      0.9 ns
                4  |      0.4 ns
                5  |      0.3 ns
                6  |     -1.7 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 1.2272, 1a.2272).
        
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 2.2272.0-6)                                                                                
    
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 3.2272.0-6). 
        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 2272 summary.                      (Jul 23, 2023 - Jul 29, 2023)

Table 1.2272.a     GPS week : 2272   MJD: 60148.0-60154.0

         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|   -1     0     0     0   -25    20  -.00   18   15 |   34456    -643   2911   8894
        |    0     0     0    12    15    23   .02           |    7164    2194
esa  n/a|    0     0     1    -4     3    24  -.24   33   24 |   -3393     240   2897   7081
        |    0     1     1     8    10    14   .07           |    8155    2236
gfz  n/a|    0     0    -1     7     6    36  -.15   21   15 |       0    -482   2875   8348
        |    0     0     0    10     7    15   .05           |       0    2411
grg  n/a|    2     0     0    -6    15   -76   .32   21   17 |   -2366    -193   2863   7846
        |    1     1     1    10    11    35   .03           |    5737    2565
iac  n/a|    0     0    -3   -14   -11    25  -.23   25   21 |     365   -1033   2897   8979
        |    2     1     2    17    25    94   .06           |    5721     599
jgx  n/a|   -1     0     2    40     9   -30  -.23   31   31 |   35294    -387   2828   8444
        |    1     1     1    21    17    40   .08           |    7178    2824


Table 1.2272.b     GPS week : 2272   MJD: 60148.0-60154.0   

         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  |   19   20   20   18   21   20   15 |
 R02  |    8    8   10    8    7    6    7 |
 R03  |    7    8    9    8    7    8    8 |
 R04  |    9    8    9    9    9    7    8 |
 R05  |    8   11    8    7    9    9    7 |
 R07  |    7    9   10    8    8    8    8 |
 R08  |   10    8    8   10    9    8   10 |
 R09  |    7    6    7    7    6    9    8 |
 R11  |   11    6    7    9    7    8    8 |
 R12  |   10    8    8    7    9    8    8 |
 R13  |   19   22   13   21   21   15   16 |
 R14  |    6    6    6    6    7    6    8 |
 R15  |    9    7   12   11   10    7    7 |
 R16  |    8   11   11    9    9    9    9 |
 R17  |    9    9    7    7    8    8    9 |
 R18  |    9    9   12   10   12   11   12 |
 R19  |   28   27   24   29   29   32   25 |
 R20  |   31   35   30   33   35   32   38 |
 R21  |    9    9    8    9   10   10    7 |
 R22  |    7    7    8    8   11    8    7 |
 R24  |   11    9    9   11   11   10   12 |
 R25  |   13   13   14   11   15    0   16 |


Table 1.2272.c     GPS week : 2272   MJD: 60148.0-60154.0   

         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 2272 0   |   39   -14    81     -12    -643    6035  80.7  1570  1570 |     627       0
brd 2272 1   |  -33    -8    62    1201    -534    9878  82.1  1518  1518 |   -1996       0
brd 2272 2   |  -12   -94    64    -860     193    7268  81.1  1594  1594 |  -14778       0
brd 2272 3   |  -12   -78   101    -598   -1152    6134  82.8  1454  1454 |     902       0
brd 2272 4   |   48   -86   203     753   -1128    6069  80.9  1367  1367 |     370       0
brd 2272 5   |    0   -81   156    -231     123    5601  81.8  1405  1405 |     320       0
brd 2272 6   |   18    -1   280     375    1485    5122  81.4  1461  1461 |   -1741       0
-------------+------------------------------------------------------------+----------------
brd 2272 mean|    6   -52   135      89    -236    6586  81.5  1481  1481 |   -2328       0
brd 2272 sdev|   29    41    81     735     927    1591    .8    83    83 |    5611       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 2.2272.0  GPS week: 2272   Day: 0   MJD: 60148                            

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    11   -34    -1   .02   16   13 |   34711    1296   3102   9996
esa  n/a|    0    -1     0     0     8    43  -.25   34   27 |    8393    1951   3099   6746
gfz  n/a|   -1    -1    -2     2     0    40  -.08   19   15 |       0    1225   3159   9185
grg  n/a|    3     2     0   -16    38   -87   .30   23   17 |    -679    2782   3129   8973
iac  n/a|    2     0    -2     4    -7   213  -.26   27   24 |    2788    -226   3089   9990
jgx  n/a|    0     1     0    34    14    32  -.26   30   30 |   35714    2427   3015   9477

Table 2.2272.1  GPS week: 2272   Day: 1   MJD: 60149                            

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     1    13   -20    20   .00   18   16 |   34427   -4204   3272   8710
esa  n/a|    0     0     0   -12   -10    19  -.13   31   22 |     743   -2587   3298   7410
gfz  n/a|    0     0     0   -12     8    20  -.16   21   14 |       0   -3783   3304   8340
grg  n/a|    3     0    -2   -14    16   -55   .34   25   17 |    -266   -3709   3278   7831
iac  n/a|   -4     1    -5    -6    37    11  -.15   24   20 |     893   -1434   3266   8763
jgx  n/a|    0    -1     2    14   -25     9  -.38   32   32 |   36553   -4898   3281   8431

Table 2.2272.2  GPS week: 2272   Day: 2   MJD: 60150                            

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     0    -6    35  -.01   19   15 |   18851     290   3020   9074
esa  n/a|    0     0     3    -8    -4    26  -.21   28   24 |  -15930     208   3034   7078
gfz  n/a|    0     2    -1     7    15    18  -.19   23   19 |       0     733   2697   8686
grg  n/a|    1     0    -1   -17    11   -64   .31   17   13 |  -15363     854   2679   8203
iac  n/a|    0    -1    -3   -20   -28   -89  -.17   24   22 |  -12449   -1263   3024   9244
jgx  n/a|    0     0     2    20    13   -82  -.21   31   31 |   19383    1636   2613   8786

Table 2.2272.3  GPS week: 2272   Day: 3   MJD: 60151                            

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   -21   -18    40  -.03   18   13 |   36624     662   2883   7866
esa  n/a|   -1     1     3     3     2    32  -.21   33   26 |   -1684    1632   2860   6173
gfz  n/a|    0     1     0    12     2    27  -.14   22   16 |       0    1455   2894   6808
grg  n/a|    1    -1    -1     1     7   -94   .36   22   18 |      32    1701   2900   6224
iac  n/a|    0     1     0     5   -22     6  -.30   26   23 |    3270    -668   2875   7640
jgx  n/a|   -4     1     4    37     9   -43  -.14   30   30 |   37391    1503   2876   6878

Table 2.2272.4  GPS week: 2272   Day: 4   MJD: 60152                            

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     1     0    -8   -33    47  -.01   21   15 |   37872     717   2962   8860
esa  n/a|    0     0     2   -15    17    -1  -.23   34   24 |   -1419    2544   2922   8299
gfz  n/a|    1     1    -2    17     0    61  -.11   19   16 |       0    1057   2969   8499
grg  n/a|    2     0    -1    -1    16  -140   .32   24   20 |    -325    1043   2961   7691
iac  n/a|    2     0    -2   -31   -25     8  -.24   24   20 |    2841    -408   2940   9078
jgx  n/a|   -3     1     5    56    24   -54  -.20   32   32 |   38730     484   2998   8203

Table 2.2272.5  GPS week: 2272   Day: 5   MJD: 60153                            

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   -12   -17  -.02   19   16 |   39517     112   2575   9770
esa  n/a|   -1     0     1     6    -1    16  -.35   36   25 |  -12127    1039   2557   7088
gfz  n/a|   -1     1    -3    16     2    43  -.15   21   13 |       0      50   2566   9318
grg  n/a|    4     0     0     9     3   -28   .28   19   15 |     151    -362   2552   8756
iac  n/a|   -3    -1    -2   -12     2   -29  -.19   25   21 |    3447   -1413   2542   9921
jgx  n/a|    0     0     0    42     5   -59  -.19   33   33 |   39952    -147   2504   9505

Table 2.2272.6  GPS week: 2272   Day: 6   MJD: 60154                            

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     6   -51    20   .03   17   15 |   39190   -3376   2564   7982
esa  n/a|   -1     0     4    -5    15    31  -.27   33   19 |   -1729   -3106   2515   6774
gfz  n/a|    0     1    -2     7    18    46  -.23   21   15 |       0   -4115   2541   7601
grg  n/a|    2     0     0    -8    16   -62   .36   21   18 |    -114   -3663   2548   7247
iac  n/a|    0     1    -6   -42   -37    53  -.32   23   21 |    1770   -1824   2547   8222
jgx  n/a|    0    -1     0    77    25   -18  -.25   32   32 |   39341   -3720   2512   7834

       
       
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 3.2272.0  GPS week: 2272   Day: 0   MJD: 60148                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01E |  672   28   51   27   29   35   48   19 |    98  120  107  101   92  105   101
 R02  |  832   11   12   10   17   23  ---    7 |    82   81   79   84   75  ---    80
 R03E | 1001    7   13   13   14   27   14    7 |   102   97  102  104   87   96   101
 R04E | 1246    9   16   15   19   25   20    8 |    93   92   89   96   89   88    91
 R05E | 1518    8   11   15   19   20   16    8 |    77   80   79   82   76   77    78
 R07E |  821   11   12   11   11   19   11    6 |    61   65   64   69   51   62    64
 R08E | 2755   12   18   17   19   32   12    9 |    58   62   57   71   51   57    60
 R09  |  833   12   10   16    9   34   14    7 |    18   15   19   14   31   15    14
 R11  | 1439   12   18   20   23   18    9   10 |    29   26   26   33   33   27    25
 R12  | 1254   14   12   21   16   26    9    9 |    35   42   42   41   39   39    37
 R13  |  756   15   37   30   45   25   81   18 |    56   47   51   44   50   50    47
 R14  | 1251   10    8   10   13   17   11    6 |    40   48   45   51   36   41    44
 R15  | 1184   18   17   13   14   13   10    9 |    48   41   43   50   42   39    44
 R16  | 1799   10   21   14   12   17   11    8 |    55   57   48   44   55   57    49
 R17  |  788   13   21    9   19   17  ---    9 |    64   54   56   55   54  ---    56
 R18  | 1342    7   24   11   16   18   20    8 |    48   66   44   49   47   40    49
 R19  | 1437   27   85   38   44   48   49   27 |   106   40  108   92   77   58    88
 R20  | 3569   36   99   38   41   48   54   31 |   113   44  116   99   75   60    92
 R21  |  768   13   11   16   16   35   24    8 |    78   65   71   69   63   55    71
 R22  | 2291   12   13    9   11   12   12    6 |    43   42   49   46   45   47    44
 R24  | 1815   17   19   16   20   20   12   10 |    55   62   60   66   58   51    58
XR25  |14014    8   18  ---  ---   37  ---   12 |    22   34  ---  ---   31  ---    26
------+-----------------------------------------+-------------------------------------
 RMS  | 1570   16   34   19   23   27   30      |T   62   58   64   64   57   56    59
 WRMS | 1570   13   27   15   17   24   30      |NE  55   47   57   55   50   44    51
 MEDI | 1251   12   17   15   17   23   14      |MD  56   54   57   66   51   55    56

Table 3.2272.1  GPS week: 2272   Day: 1   MJD: 60149                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01E |  747   24   45   42   20   41   26   19 |    80   90  100   86   78   76    85
 R02  | 1108   12   14   15   14   21  ---    8 |    93   91   94   92   89  ---    91
 R03E |  799    8   17   17   12   16   18    8 |    95   98   94  101   93   97    96
 R04E | 1421   11   13   10   17   17   20    7 |    76   76   74   79   82   74    75
 R05E | 1479    7   18   16   29   19   12   10 |    75   73   72   86   79   71    75
 R07E | 1105   12   20   12   15   21   15    8 |    61   62   66   60   66   60    61
 R08E | 2472   11   18   11   11   23   14    7 |    58   62   65   64   54   52    61
 R09  |  890   10    7   14    7   23   10    6 |    18   22   25   24   31   23    21
 R11  | 2049    8    9   13   10   14  ---    6 |    30   31   42   32   34  ---    32
 R12  | 1163    7   10   13   22   16   16    8 |    29   38   41   47   34   44    36
 R13  |  776   31   37   31   50   12   53   21 |    40   49   45   45   38   37    37
 R14  |  764    7   10   12   13   24    8    6 |    36   38   31   39   42   31    35
 R15  | 1445   13   12   13    9   24   26    7 |    38   41   52   42   45   33    42
 R16  | 1370   17   20   19   20   11   14   11 |    41   59   55   42   47   47    46
 R17  |  856   15   19   10   18   19  ---    9 |    40   42   32   36   32  ---    35
 R18  | 1371   10   22   13   12   16   16    8 |    35   44   36   34   34   32    35
 R19  | 1143   23   77   43   33   29   49   26 |    57   32   70   53   55   29    50
 R20  | 2827   46   83   40   70   57   95   34 |    62   45   35   67   52   34    43
 R21  | 1187   14   14   18   14   17   19    8 |    42   43   48   48   39   37    44
 R22  | 2804   12    9   12   14   18   10    7 |    31   34   33   38   37   30    32
 R24  | 1324   21   14    9   15   19    7    9 |    33   40   40   48   42   42    37
XR25  |10383    9   16  ---  ---   26  ---   12 |    21   31  ---  ---   38  ---    23
------+-----------------------------------------+-------------------------------------
 RMS  | 1518   18   31   21   25   24   32      |T   49   51   54   55   51   47    49
 WRMS | 1518   16   22   14   17   20   32      |NE  40   42   45   45   43   34    39
 MEDI | 1187   12   16   13   15   19   16      |MD  40   43   48   48   42   37    42

Table 3.2272.2  GPS week: 2272   Day: 2   MJD: 60150                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01E |  769   31   43   39   21   48   36   19 |    49   79   76   56   43   39    57
 R02  | 1894   12   21   23   14   20  ---   10 |    36   39   39   44   35  ---    36
 R03E | 1217   17   13   14   18   10   12    9 |    57   53   55   59   49   52    54
 R04E |  861   15   17   14   14   25   18    8 |    47   47   43   51   58   49    46
 R05E | 1687   10   12   14   16   23   22    7 |    32   31   33   31   38   32    29
 R07E |  942   16   19   18   14   19   17    9 |    32   39   36   38   35   33    33
 R08E | 2797   15   12   14   14   15   13    8 |    33   32   37   42   32   29    34
 R09  | 1336    7    8   14   12   12   16    6 |    16   16   20   22   16   21    16
 R11  | 1903   13    9    8   12   27   10    6 |    29   38   39   31   20   31    32
 R12  | 1732   14   12   17    9   20   19    7 |    26   24   34   22   28   33    23
 R13  | 1307   26   24   23   13   30   62   12 |    41   38   43   45   56   51    35
 R14  |  913    5    9   11   14   14   13    6 |    27   27   25   39   25   26    29
 R15  | 1639   13   19   28   18   38   19   11 |    33   39   30   43   19   25    34
 R16  |  875   20   14   20   17   18   13   10 |    39   42   52   28   39   33    37
 R17  | 1086   13   13   14    7   17  ---    7 |    46   39   35   50   35  ---    42
 R18  | 1224    7   26   32    9   16   15   11 |    35   39   21   41   26   27    32
 R19  | 1214   39   72   30   18   30   35   24 |    84   48   79   64   64   53    66
 R20  | 1970   40   75   49   43   31   87   29 |    78   50  102   63   69   64    70
 R21  | 1589    9   14   16   13   14   19    7 |    55   52   61   52   52   44    53
 R22  | 3092   14   11   15   16   23   15    8 |    40   42   46   48   39   52    42
 R24  |  937   17   18   18   10   18   26    9 |    50   48   35   51   33   31    44
XR25  |11262   10   17  ---  ---   32  ---   13 |    24   29  ---  ---   47  ---    24
------+-----------------------------------------+-------------------------------------
 RMS  | 1594   19   28   23   17   24   31      |T   41   40   44   43   39   38    39
 WRMS | 1594   15   24   19   13   22   31      |NE  41   38   44   42   37   37    38
 MEDI | 1307   14   14   17   14   20   18      |MD  36   39   39   44   35   33    35

Table 3.2272.3  GPS week: 2272   Day: 3   MJD: 60151                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01E |  923   21   37   40   21   50   37   17 |    47   50   80   59   48   42    54
 R02  | 1338   10   18   13   10   16  ---    7 |    44   43   42   48   39  ---    43
 R03E | 1101   12   14   14   16   21   14    8 |    84   81   80   82   76   78    81
 R04E | 1025   12   19   15   15   22   23    8 |    46   39   47   45   45   37    43
 R05E | 1636    9   12   14   11   21   19    6 |    41   41   44   45   49   42    42
 R07E |  855    7   18   14   17   21   14    8 |    44   44   49   50   49   47    44
 R08E | 1641   11   16   23   16   20   19   10 |    58   50   59   61   49   50    55
 R09  | 1870   13   10   11   13   20   17    7 |    28   28   35   25   30   29    26
 R11  | 1590   15   16   18   12   21   11    9 |    37   30   26   34   30   30    30
 R12  | 1521    9   13   12   12   21   12    6 |    36   37   39   37   42   35    35
 R13  | 1425   25   25   42   44   32   53   20 |    57   37   52   46   67   52    46
 R14  |  847    9    9   10   11   19   13    5 |    36   37   30   33   44   33    32
 R15  | 1567   11   19   18   23   30   15   10 |    43   44   43   55   35   47    44
 R16  |  601   15   17   14   12   30   10    8 |    48   53   51   40   60   47    46
 R17  |  827   11   13   13    9   25  ---    6 |    63   61   55   66   51  ---    61
 R18  |  945    6   30   21   10   17   19   10 |    45   62   39   47   40   47    46
 R19  | 1210   34   86   36   40   26   45   28 |    93   45   94   81   83   61    77
 R20  | 1587   49   93   37   47   38   73   33 |    93   49   79   65   49   52    67
 R21  | 1793   13   17   11   19   17   27    9 |    64   53   64   53   52   43    58
 R22  | 3158   12   18   11   17   11   15    8 |    44   44   44   54   38   46    44
 R24  |  849   14   23   18   20   30   37   10 |    62   59   62   69   48   42    61
XR25  |12030    6   15  ---  ---   32  ---   11 |    35   44  ---  ---   40  ---    36
------+-----------------------------------------+-------------------------------------
 RMS  | 1454   18   33   22   22   26   30      |T   52   46   53   52   48   45    48
 WRMS | 1454   13   26   16   18   23   30      |NE  51   45   50   50   46   43    47
 MEDI | 1338   12   17   14   16   21   19      |MD  45   44   49   50   48   46    44

Table 3.2272.4  GPS week: 2272   Day: 4   MJD: 60152                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01E |  879   25   30   44   40   58   47   20 |    51   50   74   55   47   51    50
 R02  | 1018    9   13   10   15   14  ---    7 |    40   41   36   44   34  ---    39
 R03E | 1663   10   15   11    9   18   19    6 |    44   52   46   54   37   44    47
 R04E | 1102   16   14   14   16   18   18    8 |    50   46   46   48   54   45    46
 R05E | 1341   13   17   11   18   19   28    8 |    38   36   37   45   39   36    37
 R07E |  912   13   14   11   12   11   13    7 |    36   35   35   38   33   35    34
 R08E | 1385   11   15   15   18   18   19    8 |    43   49   46   52   37   45    45
 R09  | 1555    8    8   11   10   32   24    5 |    23   25   30   27   28   24    25
 R11  | 1153   10   13   12   11   20   12    7 |    31   31   25   34   29   30    28
 R12  |  914   11   21   14   13   16   18    8 |    28   31   15   32   28   27    23
 R13  | 1334   28   33   29   52   21   62   21 |    46   38   37   24   31   43    33
 R14  |  694    9   12   12   13   14   22    6 |    32   26   37   27   37   36    30
 R15  | 1594   15   15   18   17   14   32    9 |    34   28   23   34   33   51    28
 R16  |  804   19   12   15   12   23   31    9 |    40   41   40   38   42   55    37
 R17  |  845   14   16   12   13   19  ---    8 |    54   45   55   51   41  ---    51
 R18  |  878    8   29   27   13   26   23   12 |    36   50   25   47   26   26    36
 R19  | 1859   33   90   29   36   25   45   28 |    85   32   77   80   62   61    67
 R20  | 1263   59   99   25   53   43   66   35 |    87   44   64   56   51   46    57
 R21  | 1246   11   23   15   16   19   25    9 |    51   42   59   47   38   35    49
 R22  | 3076   14   13   20   24   13   14   10 |    29   35   51   40   36   39    36
 R24  | 1146   22   15   15   23   23   26   11 |    61   41   45   46   37   33    46
XR25  |15734   10   20  ---  ---   27  ---   15 |    31   37  ---  ---   20  ---    34
------+-----------------------------------------+-------------------------------------
 RMS  | 1367   21   34   19   24   24   32      |T   44   38   43   43   37   40    39
 WRMS | 1367   15   24   16   20   19   32      |NE  44   36   41   41   35   38    38
 MEDI | 1153   13   15   15   16   19   24      |MD  40   38   40   45   37   39    37

Table 3.2272.5  GPS week: 2272   Day: 5   MJD: 60153                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01E |  869   19   40   43   33   53   37   20 |    85   86  111   85   86   88    88
 R02  | 1586   10   12    9   12   19  ---    6 |    56   56   57   64   52  ---    58
 R03E | 1473   15   19   11   12   19   18    8 |    52   48   50   54   50   50    50
 R04E |  822   12   15   11   12   18   14    7 |    70   69   66   79   67   69    71
 R05E |  855   11   14   16   17   20   16    8 |    54   60   62   57   64   62    56
 R07E |  694   13   17   12   14   25   16    8 |    44   48   48   49   40   45    45
 R08E | 1236   15   17   11   15   16   23    8 |    41   42   39   47   39   41    40
 R09  | 1853   19   15   17    7   16   11    8 |    21   18   16   18   18   13    12
 R11  | 1176    8   20   13   12   15   16    7 |    24   33   24   26   23   23    24
 R12  |  645   19    9   15    8   20   16    8 |    22   28   33   24   22   20    24
 R13  | 1386   23   36   17   29   36   62   15 |    38   41   34   23   24   43    30
 R14  |  948    9    9   10   14   22   10    6 |    26   33   31   24   32   29    27
 R15  | 2001   12   17   10    8   16   14    6 |    27   26   34   23   35   25    26
 R16  | 1405   19   19   13    9   23   23    9 |    30   39   28   32   36   38    27
 R17  | 1141    9   23   13   12   11  ---    8 |    46   33   52   49   44  ---    45
 R18  |  966    6   27   23   13   21   19   10 |    32   39   30   38   26   27    32
 R19  | 1000   41   94   49   41   29   70   31 |    73   27   76   55   51   38    56
 R20  | 1947   42  104   42   33   43   83   32 |    82   64   90   80   67   84    73
 R21  |  890   15   23   15   13   18   29    9 |    43   44   36   47   44   30    40
 R22  | 3055   12    8   14   15   24    9    7 |    28   29   33   31   33   29    28
 R24  | 1175   22   13   11   16   11   11    9 |    48   38   32   35   34   35    36
XR25  |16303    1  ---  ---  ---   34  ---    0 |    31  ---  ---  ---   21  ---    31
------+-----------------------------------------+-------------------------------------
 RMS  | 1404   19   36   21   19   25   33      |T   44   42   46   44   41   41    41
 WRMS | 1404   16   25   13   15   21   33      |NE  39   36   40   37   35   33    35
 MEDI | 1175   13   17   13   13   20   16      |MD  41   39   36   47   36   38    36

Table 3.2272.6  GPS week: 2272   Day: 6   MJD: 60154                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01E |  911   19   35   26   22   45   52   14 |   100  101  109  106   93   94   101
 R02  | 1237    9   11   11   16   22  ---    7 |    65   69   70   69   63  ---    67
 R03E | 1999   16   17    9    9   14   13    7 |    49   54   53   58   49   53    52
 R04E | 2012   12   12   13   15   23   17    7 |    90   90   93  100   89   98    92
 R05E | 1305    8   14   14   13   17   20    7 |    71   74   69   74   73   78    70
 R07E | 1210   12   13   12   17   11   16    8 |    56   49   57   58   49   55    54
 R08E | 1299   14   14   20   16   14   15    9 |    47   45   45   49   41   46    45
 R09  |  935   16   17   10   10   18   20    8 |    27   23   23   24   19   28    22
 R11  | 1146   16   17   12    7   17   18    7 |    34   29   25   32   26   26    28
 R12  |  614   16   10   19    9   27   25    8 |    35   42   49   40   32   35    39
 R13  | 1174   16   32   21   38   31   52   16 |    59   56   51   48   48   46    51
 R14  |  488    7   13   21   10   16   19    7 |    41   46   40   43   42   48    40
 R15  | 1510   10   15   12    8   29   12    6 |    47   54   44   50   41   46    47
 R16  | 1199   16   13   17   11   12   13    8 |    51   60   60   49   55   56    53
 R17  | 1323   19   11   13   17   14  ---    9 |    73   58   58   63   61  ---    62
 R18  | 1028    7   33   23   17   23   14   11 |    50   69   41   56   43   44    50
 R19  |  922   20   75   44   30   32   54   25 |   110   49  118   89   86   68    92
 R20  | 2145   45  105   55   55   39   77   37 |   109   68  110   93   81   67    88
 R21  | 1450   13   15    9    8   19   27    6 |    76   67   75   72   71   51    72
 R22  | 3001   13   10   10   12   19   13    6 |    45   48   51   47   52   46    46
 R24  | 1503   16   25   15   24   14   23   11 |    65   64   57   63   61   51    60
XR25  |17788   10   21  ---  ---   15  ---   15 |    35   40  ---  ---   32  ---    35
------+-----------------------------------------+-------------------------------------
 RMS  | 1460   17   33   21   21   23   32      |T   60   57   61   61   54   54    57
 WRMS | 1460   15   19   15   18   21   32      |NE  57   52   58   55   50   47    53
 MEDI | 1237   14   15   14   15   18   19      |MD  51   54   57   58   49   51    52



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