[IGSREPORT-29480] Wk 2275 IGLOS Final Orbits

acc acc at igs.org
Tue Sep 5 00:01:04 UTC 2023


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2275   (Aug 13, 2023 - Aug 19, 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 2.2275.
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:
                                                                               
 igl2275[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2275 in the SP3 format.
 igl22757.sum      Combination Report for GPS Week 2275.


    
    
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  |    -11.3 ns
                1  |    -11.5 ns
                2  |    -14.5 ns
                3  |    -12.7 ns
                4  |    -13.5 ns
                5  |    -10.8 ns
                6  |    -14.9 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 1.2275, 1a.2275).
        
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 2.2275.0-6)                                                                                
    
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 3.2275.0-6). 
        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 2275 summary.                      (Aug 13, 2023 - Aug 19, 2023)

Table 1.2275.a     GPS week : 2275   MJD: 60169.0-60175.0

         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     1   -29    20   .03   18   15 |   17869    -814   3009   8853
        |    1     0     1    14    17    15   .03           |    2187    1371
esa  n/a|   -2     0     4     0     5    13  -.21   33   24 |  -11690    -100   3007   7921
        |    1     2     2    10    14    20   .04           |   11236    1391
gfz  n/a|    0     0    -4    20     5    -3  -.22   25   16 |       0    -902   2968   8118
        |    1     0     1    14     9    19   .05           |       0    1527
grg  n/a|    2     0    -1   -25    18   -46   .36   28   19 |  -12311   -1161   2969   7665
        |    1     2     1    19    25    37   .02           |    1634    1819
iac  n/a|    0     1   -15     1    -2     3 -1.43   40   40 |  -10423    -613   2990   8816
        |    2     2    11    33    27    99  1.45           |    1579    1109
jgx  n/a|    0     0     4     8    -5    46  -.20   32   32 |   18539   -1137   2981   8062
        |    1     1     3    26    17    22   .08           |    1676    1766


Table 1.2275.b     GPS week : 2275   MJD: 60169.0-60175.0   

         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  |   24   25   26   28   26   24   31 |
 R02  |    9    7    7   10    9    8    8 |
 R03  |   12    9    8    7    9   10    9 |
 R04  |    8    9    8    8    7    8    8 |
 R05  |    8    8   12    7    7    9    9 |
 R07  |    9    9    9   11   10    9    9 |
 R08  |    8    8   10    8    8   10    8 |
 R09  |    8   11    8    8   10    7    7 |
 R11  |    9    9    8    7    6    8    8 |
 R12  |   11    8   10    9    7    8    8 |
 R13  |   18   18   14   21   19   18   19 |
 R14  |    9    7    8    7    5    7    8 |
 R15  |    8    8    9   10   10   10   10 |
 R16  |   11   12   10    9   10    9   10 |
 R17  |    9   15   16   12   10    9    8 |
 R18  |   11   11   12   16   12    8    8 |
 R19  |   27   26   28   16   16   24   22 |
 R20  |   34   36   40   36   41   41   42 |
 R21  |   10    8   13   25    9    9   10 |
 R22  |    9    8    8    8   10   16    8 |
 R24  |    9   17   22    9   11   10    9 |
 R25  |   14   11   18   14   17   16   19 |


Table 1.2275.c     GPS week : 2275   MJD: 60169.0-60175.0   

         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 2275 0   |   80    -6   102    -930    1603    6948  79.0  1869  1869 |  -11297       0
brd 2275 1   |  -20     8   115   -1472    1272    5455  81.1  1396  1396 |  -11462       0
brd 2275 2   |  -38   -13    58    -785     559    1986  78.9  1423  1423 |  -14515       0
brd 2275 3   |  -57   -22    72   -1400   -1187     803  79.9  3667  3667 |  -12745       0
brd 2275 4   |   60   -73    62     641     332    -690  79.4  1518  1518 |  -13507       0
brd 2275 5   |  -22    28   100    -111    -504     493  80.3  1454  1454 |  -10765       0
brd 2275 6   |  -42    33   227    1158   -1623    -706  80.1  1566  1566 |  -14908       0
-------------+------------------------------------------------------------+----------------
brd 2275 mean|   -5    -6   105    -414      64    2041  79.8  1841  1841 |  -12742       0
brd 2275 sdev|   53    36    57    1014    1216    3018    .8   820   820 |    1635       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 2.2275.0  GPS week: 2275   Day: 0   MJD: 60169                            

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|   -3     0     1    20   -11    28   .01   21   17 |   20394   -1015   3045   9216
esa  n/a|   -2     0     3     6    16    14  -.23   33   24 |   -7914    -155   3046   7219
gfz  n/a|    0     0    -4     0     4    -5  -.24   22   16 |       0   -1253   3075   8585
grg  n/a|    4     0     1   -14    -6   -27   .35   21   18 |  -10759   -1520   3070   8159
iac  n/a|   -1     0    -6     5    24    83  -.39   27   22 |   -9179   -1636   3033   9187
jgx  n/a|    0    -1     9   -40     6    48  -.30   33   33 |   19833   -1644   3142   8224

Table 2.2275.1  GPS week: 2275   Day: 1   MJD: 60170                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
cod  n/a|   -2     0    -1    -2   -27    19   .04   18   14 |   20506   -1944   2875   8639
esa  n/a|   -5    -3     8     3    14    19  -.19   37   25 |   -7138   -1397   2882   7068
gfz  n/a|    0     0     0    20   -10    -2  -.28   23   18 |       0   -1674   2907   7595
grg  n/a|    4     1    -3   -21    34   -43   .36   24   19 |  -10497   -2090   2912   7390
iac  n/a|    2     0   -10    42   -10     5  -.24   27   24 |   -9331     677   2874   8390
jgx  n/a|    0     0     5    21     6    63  -.22   33   33 |   20467   -1430   2764   7583

Table 2.2275.2  GPS week: 2275   Day: 2   MJD: 60171                            

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     2     3   -35    11   .06   19   15 |   16095   -2840   3510   9269
esa  n/a|    0    -3     5    11    19    -5  -.19   35   23 |  -32472   -2572   3506  11116
gfz  n/a|    0     1    -4    14    17   -15  -.17   24   13 |       0   -3437   3410   9184
grg  n/a|    1     2     0   -59   -17     4   .39   33   22 |  -12642   -4108   3378   8883
iac  n/a|    0     0    -3   -13    15    -3  -.20   28   25 |  -11634   -2338   3490   9642
jgx  n/a|    2     0     1   -13   -39    55  -.13   30   30 |   17332   -3943   3440   9202

Table 2.2275.3  GPS week: 2275   Day: 3   MJD: 60172                            

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   -22   -38    36   .08   17   13 |   16809    1117   3635   8791
esa  n/a|   -2     0     1    -1     9    -5  -.15   31   18 |  -14218     977   3635   7982
gfz  n/a|    0     1    -5    47    12    17  -.27   24   15 |       0    1190   3371   8214
grg  n/a|    3    -2    -1   -25    11  -103   .39   36   23 |  -13808    1744   3448   7809
iac  n/a|    0     3    -7   -64   -33    58  -.23   24   23 |  -10392    -217   3625   8867
jgx  n/a|    2     0     1    20   -15    68  -.07   35   35 |   17223    1898   3428   8359

Table 2.2275.4  GPS week: 2275   Day: 4   MJD: 60173                            

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    17   -10    13  -.01   16   14 |   15793      -2   2901   9312
esa  n/a|   -1     0     4     6   -15    31  -.24   31   23 |   -7163     942   2902   6453
gfz  n/a|    0     0    -4    19    -4   -35  -.22   29   14 |       0     429   2949   8718
grg  n/a|    2     0    -2   -39    27   -16   .33   24   18 |  -13500    -291   2922   7934
iac  n/a|    0     2   -32     1    34  -195 -2.86   61   62 |  -11396    -270   2864   9132
jgx  n/a|    0     1     2    34   -10    56  -.21   32   32 |   17596    -680   2998   8551

Table 2.2275.5  GPS week: 2275   Day: 5   MJD: 60174                            

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     2     0    -2   -59    39   .03   17   15 |   19583     293   2586   9022
esa  n/a|    0     2     5   -19   -12    -2  -.26   32   29 |    3762    1006   2585   8530
gfz  n/a|    0     0    -6    21     8    -5  -.25   30   19 |       0    -202   2617   7825
grg  n/a|    0    -2    -1     4    56   -57   .34   25   15 |  -10683    -266   2615   7274
iac  n/a|    0    -2   -25     9   -26   -23 -3.18   58   62 |   -8302   -1018   2553   8898
jgx  n/a|    0     2     3    20     1    27  -.17   34   33 |   20581    -346   2631   7858

Table 2.2275.6  GPS week: 2275   Day: 6   MJD: 60175                            

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     0   -23    -3   .01   20   14 |   15903   -1311   2514   7724
esa  n/a|   -2     0     5    -3     3    45  -.24   31   27 |  -16691     495   2496   7080
gfz  n/a|    2     1    -5    19    12    23  -.14   22   13 |       0   -1369   2449   6711
grg  n/a|    1    -3     0   -25    21   -79   .38   30   17 |  -14290   -1602   2439   6212
iac  n/a|   -4     1   -25    27   -24   100 -2.90   57   60 |  -12727     509   2495   7596
jgx  n/a|    0     3     7    16    11     4  -.27   27   27 |   16746   -1818   2466   6660

       
       
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 3.2275.0  GPS week: 2275   Day: 0   MJD: 60169                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1984   33   74   28   17   19   29   23 |   100   36   94   79   76   48    75
 R02  |  825   12   12   16   21   20   19    9 |    57   48   62   52   66   39    53
 R03  | 3183   13   19   24   22   22   34   11 |    62   39   61   54   62   31    52
 R04  | 2071   14   12   12   14   12   25    7 |    61   50   52   57   59   42    54
 R05  | 1426   12   12   10   18   15   12    8 |    57   55   59   61   68   48    57
 R07  | 1665   16   15   13   15   19   23    8 |    79   58   68   70   81   50    68
 R08  | 1612   11   17   11   14   17   34    7 |    67   55   65   59   68   41    60
 R09  |  641   11   15   12   15   25  ---    8 |    34   42   35   34   38  ---    34
 R11  |  775   12   22   10   14   29   17    8 |    39   56   47   43   50   38    44
 R12  |  831   17   15   21   17   20   16   10 |    31   33   32   36   31   32    30
 R13  | 1012   33   42   21   25   26   57   17 |    61   37   35   43   38   54    42
 R14  | 1785    9   14   18   15   26   13    8 |    33   32   41   36   45   31    35
 R15  | 1065   14    8   15   12   17   27    7 |    44   50   55   50   51   36    48
 R16  |  896   29   13   19    8   26   15   11 |    49   47   47   38   51   48    42
 R17  | 1531   15   14   14   19   18  ---    9 |   127  125  130  123  125  ---   126
 R18E | 1397   16   22   12   24   17   14   11 |   123  130  121  132  127  122   125
 R19E | 3800   38   61   51   35   63   71   27 |   106   55  117   70   52   43    86
 R20  | 3816   40   91   55   48   51   65   34 |   110   62  121   86   93   83    89
 R21E |  602   13   13   16   22   27   18    9 |   169  162  164  167  163  163   165
 R22E | 2101   13   17    9   17   14   20    8 |    39   48   42   46   41   46    41
 R24E |  976   15   16   13   16   20   21    9 |    92   94   91   98   89   83    92
XR25  |15641   11   15  ---  ---   45  ---   13 |    39   39  ---  ---   31  ---    38
------+-----------------------------------------+-------------------------------------
 RMS  | 1868   21   33   22   21   27   33      |T   71   61   73   68   68   56    66
 WRMS | 1868   17   24   16   18   22   33      |NE  61   50   62   57   60   44    55
 MEDI | 1426   14   15   15   17   20   21      |MD  61   50   61   57   59   46    53

Table 3.2275.1  GPS week: 2275   Day: 1   MJD: 60170                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1941   25   89   28   12   31   51   24 |    81   46   77   74   51   45    68
 R02  |  648    8    9   13   14   24   20    6 |    52   51   47   53   54   38    49
 R03  | 2943   16   18    6   17   12   21    8 |    54   42   44   47   48   39    45
 R04  | 1659   13   12   11   20   25   23    8 |    53   43   49   48   56   42    47
 R05  | 1101   10   17   15   12   22   17    7 |    43   42   47   49   43   37    44
 R07  |  907    8   27   16   11   31   34    9 |    59   48   70   67   66   42    61
 R08  |  979   10   21   10   11   13   33    7 |    55   43   54   54   44   33    51
 R09  | 1315   16   17   20   19   26  ---   10 |    34   43   39   43   37  ---    37
 R11  |  769   17   11   19    9   17   15    8 |    36   46   42   48   43   34    40
 R12  |  787   10   20    9   13   15   23    7 |    28   39   39   31   32   28    32
 R13  |  968   24   32   24   41   17   46   17 |    46   41   44   41   39   41    41
 R14  | 1338    5    9   15   13   16   16    6 |    28   36   28   35   26   27    29
 R15  |  795   12   22   12   12   16   11    8 |    32   50   48   40   39   41    40
 R16  |  799   21   23   20   18   18   25   12 |    35   63   64   40   37   33    47
 R17  | 1591   20   20   19   37   41  ---   14 |    93   95   95  104   96  ---    93
 R18E | 1390   14   24   10   26   23   24   11 |    96  104   98  100  106   98    97
 R19E | 1609   26   65   49   40   64  ---   25 |    72   55   99   61   37  ---    69
 R20  | 1810   42  102   63   43   35   78   36 |    72   33   93   79   62   47    65
 R21E |  727   12   17   12   15   30   19    8 |   132  130  133  126  124  125   130
 R22E | 1733   12   14    9   17   18   20    7 |    24   32   29   38   30   35    28
 R24E | 1240   20   22   22   44   29   36   16 |    98  104  102  123   95   91   102
XR25  |12693    8   15  ---  ---   28  ---   11 |    38   42  ---  ---   38  ---    39
------+-----------------------------------------+-------------------------------------
 RMS  | 1396   18   37   23   24   27   33      |T   57   55   63   61   54   48    57
 WRMS | 1396   14   25   18   19   24   33      |NE  49   47   55   53   47   37    48
 MEDI | 1240   13   20   15   17   23   23      |MD  52   43   49   49   43   39    47

Table 3.2275.2  GPS week: 2275   Day: 2   MJD: 60171                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1300   32   81   29   20   27   55   26 |    85   33   81   66   40   28    63
 R02  |  831    6   18   14   12   22   36    7 |    46   36   53   49   52   28    45
 R03  | 3013   12   15   16   13   22   29    8 |    51   38   46   47   50   28    44
 R04  | 1738   11    8   11   21   22   24    7 |    48   41   47   41   43   39    44
 R05  | 1062   15   16   25   27   21   23   12 |    35   45   60   40   47   28    42
 R07  |  637   11   21   12   14   19   23    8 |    60   51   69   70   69   50    61
 R08  |  894   12   22   20   10   19   29    9 |    49   47   67   60   55   41    54
 R09  |  728   11   10   10   19   19   20    7 |    23   28   28   21   33   21    22
 R11  | 1029   16   16   11   11   32   20    8 |    28   32   34   26   36   35    27
 R12  | 1782   14   20   14   18   16   14    9 |    22   33   32   30   27   20    25
 R13  | 1373   14   29   17   37   30   50   14 |    25   28   41   35   38   27    28
 R14  | 1307    7   12   15   18   13   14    7 |    25   26   35   21   25   26    25
 R15  |  857    6   12   17   21   15   11    8 |    35   39   28   43   31   38    34
 R16  |  750   19   26   11   12   16   21   10 |    36   59   46   41   41   38    43
 R17  | 1647   21   14   15   52   49  ---   16 |   163  160  161  162  162  ---   160
 R18E | 1088   16   22   15   27   14   18   11 |   130  140  132  147  127  129   135
 R19E | 1413   25   52   60   51   52  ---   27 |    49   55   93   48   35  ---    56
 R20  | 1735   54  102   55   66   39   60   40 |    81   62   76   59   64   63    57
 R21E |  827   10   22   15   42   20   23   13 |   194  194  190  210  199  195   195
 R22E | 2052   12   15    9   18   25   19    7 |    28   32   28   38   40   35    29
 R24E | 1492   22   18   27   76   40   19   22 |   147  143  142  158  129  135   143
XR25  |17333   13   22  ---  ---   20  ---   17 |    23   48  ---  ---   33  ---    31
------+-----------------------------------------+-------------------------------------
 RMS  | 1422   19   35   24   33   28   30      |T   62   62   70   67   62   52    61
 WRMS | 1422   15   23   13   22   25   30      |NE  49   47   56   50   49   34    47
 MEDI | 1300   13   18   15   20   21   23      |MD  46   41   53   47   41   35    44

Table 3.2275.3  GPS week: 2275   Day: 3   MJD: 60172                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  946   29   87   32   25   16   56   27 |    91   38   96   86   74   36    73
 R02  |  984    5   20   22   15   14   34    9 |    57   42   63   54   49   33    53
 R03  | 1909   11   16   10    9   27   37    7 |    58   39   45   54   62   33    49
 R04  |  975   14    9   11   17   21   25    7 |    53   41   40   39   43   32    43
 R05  | 1597    8    9   10   19   31   14    6 |    47   42   44   47   51   42    44
 R07  | 1036   16   25   12   23   20   24   11 |    72   58   67   60   54   56    63
 R08  | 1469    9   18   13   16   11   20    8 |    55   50   64   62   55   43    56
 R09  | 1023   14   13   13   17   16    9    8 |    18   17   15   15   26   13    14
 R11  |  967   12   13   10   10   20   20    6 |    27   23   24   25   35   25    23
 R12  | 1673   16   16   16   13   12   11    9 |    31   31   33   31   25   30    28
 R13  | 2084   21   30   35   63   19   83   21 |    36   32   46   42   37   47    34
 R14  | 1550    9   11   16   13   16   15    7 |    30   30   41   33   30   28    33
 R15  |  995   13   18   18   24   13   12   10 |    36   36   46   43   33   33    37
 R16  |  693   11   20    8   21   14   14    8 |    41   56   47   33   50   48    44
 R17  | 1103    8   18   19   37   23  ---   11 |   102   96  104   98  111  ---    98
 R18E |  860    9   25   13   57   20   15   15 |   130  131  130  128  128  125   127
 R19E | 1537   20   28   26   40   41   31   16 |    45   57   60   60   38   45    46
 R20  | 3674   43   75   65   68   59   85   35 |    92   73  114   49   53   45    73
 R21E |  677   14   18   46   86   24   28   25 |   216  219  232  228  207  222   219
 R22E |15419   12   10   13   19   20   15    7 |    40   42   50   52   39   43    43
 R24E | 1071   13   19   13   17   18   19    8 |    91   93   99   84   81   88    90
XR25  |12541   10   18  ---  ---   18  ---   14 |    41   54  ---  ---   40  ---    44
------+-----------------------------------------+-------------------------------------
 RMS  | 3667   17   31   24   36   24   35      |T   64   59   69   63   60   53    60
 WRMS | 3667   13   18   15   23   23   35      |NE  52   44   55   48   48   36    47
 MEDI | 1071   12   18   13   19   19   20      |MD  47   42   50   52   49   42    44

Table 3.2275.4  GPS week: 2275   Day: 4   MJD: 60173                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1209   30   84   32   21   88   35   26 |    95   47   96   77  147   58    77
 R02  |  667   11   19   18   12   64   28    8 |    55   49   71   64  107   39    58
 R03  | 1275   10   21   18   16   75   24    9 |    61   48   68   54  120   43    57
 R04  |  702   10   15    8   13   73   32    6 |    61   55   51   62  116   42    56
 R05  | 1583   11    9   12   15   95   15    7 |    54   48   45   46  125   47    47
 R07  |  895   15   24   10   18   81   28   10 |    67   48   59   59  118   41    58
 R08  | 1590    9   16   13   17   57   21    8 |    57   54   65   55  102   51    57
 R09  |  612   10   14   22   19   47   14    9 |    24   33   32   28   24   19    25
 R11  | 1717    6    7   14    9   48    9    5 |    30   39   48   33   27   37    36
 R12  |  783    7   15   15   11   44   11    7 |    26   36   29   27   80   28    26
 R13  | 1913   27   34   35   35   46   49   18 |    34   39   37   34   78   21    29
 R14  | 2053    7   10    8   11   36   12    5 |    24   31   28   28   70   28    27
 R15  |  773   14   26   12   16   41   22   10 |    30   42   43   40   82   25    35
 R16  |  673   19   19   15   16   52   17   10 |    36   43   41   27   89   34    34
 R17  | 1407   11   19   13   23   38  ---    9 |   129  131  130  132  128  ---   129
 R18E |  840   19   23   25   17   31   17   12 |   136  133  124  127  123  131   129
 R19E | 1658   19   31   37   25   65   40   16 |    44   34   55   53   80   31    41
 R20  | 3735   31   80  102   69  101   91   41 |    82   57  147   53  134   60    78
 R21E |  906   13   17   14   19   35   14    9 |   184  181  178  179  182  184   180
 R22E | 2126   14   12   20   23   62   16   10 |    50   51   48   71   46   47    53
 R24E |  948   16   19   19   24   37   24   11 |    56   68   65   60   67   62    59
XR25  |11881   11   23  ---  ---   55  ---   16 |    31   31  ---  ---   21  ---    29
------+-----------------------------------------+-------------------------------------
 RMS  | 1517   16   31   29   24   61   32      |T   62   59   69   62   93   51    60
 WRMS | 1517   14   23   14   18   62   32      |NE  52   48   61   51   92   38    50
 MEDI | 1209   11   19   15   17   52   21      |MD  54   48   55   54   89   41    53

Table 3.2275.5  GPS week: 2275   Day: 5   MJD: 60174                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1146   29   81   27   14   81   40   24 |    92   52   91   78  136   64    78
 R02  | 1136   10   18   16   12   67   20    8 |    55   47   65   57  104   47    55
 R03  | 1783   11   28   20    9   58   26   10 |    62   47   77   68   99   52    63
 R04  |  728   11   19   10   10   59   26    7 |    65   61   65   66   96   54    63
 R05  | 1349   16   14   11   19   65   25    9 |    69   56   58   57   99   49    60
 R07  | 1358   15   19    7   18   81   25    9 |    70   52   65   60  110   50    62
 R08  | 1521   10   21   21   19   76   30   10 |    63   62   75   69  117   58    65
 R09  |  807    9   14   12   11   59   14    6 |    32   34   38   33   52   31    33
 R11  | 1197   11   18   11   13   55   15    7 |    46   56   46   56   60   46    49
 R12  | 1012   13   10   13   15   48   32    7 |    35   48   50   37   90   28    40
 R13  | 1158   30   40   33   23   58   61   18 |    38   37   30   41   95   29    32
 R14  | 1607   10   14   11   11   53   13    6 |    36   38   41   33   89   37    36
 R15  |  920   15   22   16   17   36    9   10 |    35   36   41   41   80   38    35
 R16  |  734   16   18   15   14   63   20    9 |    35   44   46   45  102   42    40
 R17  |  848    9   18   13   22   28  ---    9 |    92   95   92   89   99  ---    90
 R18E |  818    6   22   16   12   34   16    8 |    98  102  100  100  100   98    99
 R19E |  985   27   32   46   55   65   43   23 |    43   47   59   71   47   39    44
 R20  | 3159   28   84  103   60   43   97   40 |    69   42  134   65   62   43    68
 R21E |  813   10   17   14   18   41   14    8 |   112  115  113  107  113  107   110
 R22E | 3057   17   16   27   40   65   13   15 |    80   77   80  101   84   82    81
 R24E | 1144   15   20   14   16   36   17    9 |    45   55   53   56   54   47    49
XR25  |12415   10   23  ---  ---   64  ---   16 |    39   42  ---  ---   56  ---    39
------+-----------------------------------------+-------------------------------------
 RMS  | 1453   17   32   30   25   58   34      |T   59   56   67   63   88   52    58
 WRMS | 1453   15   29   19   15   62   33      |NE  54   49   63   55   90   44    53
 MEDI | 1144   11   19   15   16   58   20      |MD  55   48   65   60   95   47    55

Table 3.2275.6  GPS week: 2275   Day: 6   MJD: 60175                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  748   26   97   45   17   68   40   30 |   132   40  141  118  157   81   109
 R02  |  791    8   14   15   14   65   18    7 |    70   61   82   76  123   57    71
 R03  | 1074    9   22    9   16   68   28    8 |    79   58   82   79  131   51    75
 R04  |  877   11   20   11   11   49   29    7 |    73   59   79   76  106   48    71
 R05  | 1114   12   19   11   18   64   27    8 |    76   58   71   68  118   53    68
 R07  | 1586   17   15   14   13   73   22    9 |    85   64   71   74  125   55    74
 R08  |  997    8   17   14   15   83   20    8 |    82   74   89   86  141   66    82
 R09  |  818   11   11   14   13   49   11    7 |    39   45   47   44   47   32    42
 R11  | 1355    9   12   15   17   58   15    7 |    49   51   47   52   51   47    48
 R12  |  721   12   16   10   17   43   16    8 |    42   44   44   48   80   42    43
 R13  | 1131   17   30   31   48   62   60   18 |    62   59   63   49  101   51    56
 R14  |  763   10   18   16    9   58   10    8 |    47   39   43   44   89   46    42
 R15  |  752   10   14   21   21   47   12    9 |    51   47   46   57   86   51    49
 R16  | 1534   20   17   15   12   74   24    9 |    54   57   50   52  100   55    51
 R17  |  820   10   13   10   20   31  ---    8 |   132  125  128  137  132  ---   130
 R18E | 1192    9   18   13   17   28   13    8 |   111  108  106  114  106  106   108
 R19E | 1520   27   34   46   40   53   44   21 |    78   64  113   78   94   64    80
 R20  | 4011   68   60   47  105   68   49   41 |   122   94  143  122   98   90   107
 R21E |  842   12   19   17   18   31   11    9 |   150  144  143  151  146  147   147
 R22E | 3735   10   17   11   19   48   12    8 |    68   72   64   70   70   74    66
 R24E |  836   13   14   14   19   37   14    8 |    84   78   89   89   82   80    84
XR25  |12767   13   24  ---  ---   51  ---   18 |    39   46  ---  ---   35  ---    40
------+-----------------------------------------+-------------------------------------
 RMS  | 1566   20   31   22   30   57   27      |T   78   67   82   80  100   64    74
 WRMS | 1566   14   27   13   17   60   27      |NE  72   60   76   73  101   55    68
 MEDI |  997   11   17   14   17   53   18      |MD  73   59   79   76  100   55    71



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