[IGSREPORT-30927] Wk 2415 IGLOS Final Orbits

acc acc at igs.org
Fri May 8 03:51:44 UTC 2026


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2415   (Apr 19, 2026 - Apr 25, 2026) 
                                                                               
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 2.2415.
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:
                                                                               
 igl2415[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2415 in the SP3 format.
 igl24157.sum      Combination Report for GPS Week 2415.


    
    
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.

Starting 02-Feb-2025 (GPS week 2352) the IGS Analysis Centers started using 
the IGS realization of the updated ITRF2020-u2023, called IGb20. The combined
GLONASS orbits from this date are therefore in IGb20 frame.

Starting 11-Jan-2026 (GPS Week 2401, day 0, MJD 61051), all IGS products
are based on the IGS realization of the second yearly update of ITRF2020
called ITRF2020-u2024. This IGS realization is called IGc20.
For more information see IGSMAIL #8634.

 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:
        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
    
    Starting 28-Nov-2022, the absolute antenna model file has been updated to
    igs20.atx to be consistent with IGS20.
    See IGSMAIL #8238 and #8256 for more information
        https://files.igs.org/pub/station/general/igs20.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  |      7.6 ns
                1  |      6.2 ns
                2  |      7.9 ns
                3  |      7.0 ns
                4  |      8.0 ns
                5  |      8.2 ns
                6  |      8.5 ns

 5. The following orbit solutions were excluded from the combination
    because they were biasing the weighted average (generally indicated
    by long arc RMS).
    
               Day | Centre | PRN list
               ----+--------+---------------
                0  |  ESA   | R06
                3  |  ALL   | R06
                4  |  ALL   | R06
                5  |  ALL   | R06
                6  |  ALL   | R06

    
         
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 1.2415, 1a.2415).
        
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 2.2415.0-6)                                                                                
    
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 3.2415.0-6). 
        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 2415 summary.                      (Apr 19, 2026 - Apr 25, 2026)

Table 1.2415.a     GPS week : 2415   MJD: 61149.0-61155.0

         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     2     1    -2    -1   .13   13   13 |    1746       2   3128   8988
        |    0     0     1    13     7    12   .03           |     854    1464
esa  n/a|   -2     0     4    -5   -13    60  -.03   22   21 |    3106    -271   3139   9240
        |    1     1     2    13    18    17   .04           |    1007    1746
gfz  n/a|    0     0     2     5    12    17  -.18   16   15 |       0     -22   3126   8827
        |    1     1     2    18    16    28   .03           |       0    1630
grg  n/a|    2     0     0   -13     9   -42   .32   14   14 |    7343     206   3172   8549
        |    1     0     2    19    12    42   .04           |     563    1666
iac  n/a|    0     0    -2     1    -3   -13  -.10   16   16 |    8729    -308   3121   9482
        |    1     1     1    15    20    48   .06           |     802    1316
jgx  n/a|    1     0    -7    -1    -4     3  -.14   15   15 |    3856      88   3142   8793
        |    0     0     2    18    12    33   .03           |     697    1399


Table 1.2415.b     GPS week : 2415   MJD: 61149.0-61155.0   

         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
------+------------------------------------+------------------------------------------
 R02  |    7    7    6    8    6    5    7 |
 R03  |    5    6    7    8    7    6    6 |
 R04  |    9    8    6    6    6    6    9 |
 R05  |    7    7    6    6    5    6    6 |
 R06  |   29   35 1120  ---  ---  ---  --- |
 R07  |    8    6    7    6    7    7    7 |
 R08  |   13   12   10   10   10    9   10 |
 R09  |    8    9    7    7    6    6    7 |
 R11  |    6    8    8    5    8    9    7 |
 R12  |    7    8    7    7    7    7    7 |
 R14  |    6    7    5    6    7    6    7 |
 R15  |    7    6    6    7    7    7    7 |
 R16  |    8   11    8    8    7    7    7 |
 R17  |    6    7    6    5    7    5    5 |
 R18  |    5    7    7    6    8    9    8 |
 R19  |    8    6    6    7    6    7    6 |
 R20  |    7    5    6    6    6    6    7 |
 R21  |   11    7    7    8   10    9    7 |
 R22  |    6    7    6    5    8    7    7 |
 R24  |    7    6    6    8    8    6    7 |
 R26  |   24   27   31   32   33 1658  --- |


Table 1.2415.c     GPS week : 2415   MJD: 61149.0-61155.0   

         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 2415 0   |   58    -3   -76    1152    1298    2697  80.7  1805  1805 |    7574       0
brd 2415 1   |  -10    -4   -39     974   -1103   -1857  78.7  1633  1633 |    6210       0
brd 2415 2   |   78    79   -44   -1572   -1805    -812  79.4  1777  1777 |    7855       0
brd 2415 3   |  102    65    20    -488    1608    2774  79.3  1648  1648 |    7016       0
brd 2415 4   |   12    38    88   -1586    3997   11150  76.7  1859  1859 |    8011       0
brd 2415 5   |  -95   -44   109    -155    -671   -2750  76.6  2141  2141 |    8249       0
brd 2415 6   |  -24  -129   220    -348   -1667   -2448  80.7  2310  2310 |    8542       0
-------------+------------------------------------------------------------+----------------
brd 2415 mean|   17     0    39    -289     236    1250  78.9  1881  1881 |    7636       0
brd 2415 sdev|   68    71   105    1084    2143    4933   1.7   253   253 |     796       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 2.2415.0  GPS week: 2415   Day: 0   MJD: 61149                            

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     9    -3   -14   .08   13   13 |    1023     577   2985   8397
esa  n/a|    0    -2     9    -4     3    49   .03   39   36 |    3444   -1549   3033   9245
gfz  n/a|    1     0     2    12    -9    41  -.13   14   12 |       0     245   2983   8089
grg  n/a|    0     0     4   -15    19   -36   .29   15   14 |    6969     866   3030   7981
iac  n/a|   -1     1    -4    -3     4    -3  -.07   16   16 |    8482    -349   2979   8872
jgx  n/a|    1     0   -10    -3    -5   -16  -.10   15   15 |    2883     321   3099   8312

Table 2.2415.1  GPS week: 2415   Day: 1   MJD: 61150                            

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     3    -9     8   -16   .13   14   14 |    1236   -2126   2899   8812
esa  n/a|   -3     0     4    22   -38    51  -.02   23   20 |    2417   -3203   2948   8568
gfz  n/a|    0     1     0    38    -3    -1  -.21   17   15 |       0   -2619   2902   8569
grg  n/a|    2     0     0   -45     4    22   .37   16   14 |    7312   -2518   3064   8426
iac  n/a|    3    -1     0     2     4    44  -.09   16   15 |    8200   -2697   2900   9232
jgx  n/a|    1     0    -6    -2   -13   -62  -.11   16   16 |    3570   -2188   3004   8646

Table 2.2415.2  GPS week: 2415   Day: 2   MJD: 61151                            

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    22   -14    14   .11   14   14 |    1889     961   2951  10034
esa  n/a|   -3    -2     1    -8    -8    57  -.04   21   20 |    1572     936   2964  10062
gfz  n/a|    0     0     3    -1    30    -9  -.14   13   12 |       0    1067   2953   9625
grg  n/a|    2     0     0   -20     9  -113   .34   14   13 |    6985    1435   2994   8779
iac  n/a|    2     1    -2    32    -8    32  -.03   14   14 |    8416    -658   2950  10253
jgx  n/a|    0     0    -9   -17   -20    26  -.14   16   16 |    4080    1107   2967   8976

Table 2.2415.3  GPS week: 2415   Day: 3   MJD: 61152                            

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     2     3    -7     6   .11   12   12 |    3252    -595   3163   9902
esa  n/a|   -1     0     3   -13    13    86  -.01   20   20 |    2759     734   3158   9958
gfz  n/a|   -1     1     4   -13     5    58  -.20   15   14 |       0     456   3162   9678
grg  n/a|    4     0     0   -10    25   -28   .33   14   15 |    6792    -105   3180   9476
iac  n/a|    2     1    -3   -13     1  -102  -.10   17   17 |    7750    1660   3149  10313
jgx  n/a|    1     0    -8    18    -2    29  -.14   15   15 |    4945    -364   3126   9628

Table 2.2415.4  GPS week: 2415   Day: 4   MJD: 61153                            

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     2    -7     2    -8   .14   12   12 |    1800   -1641   3142   9138
esa  n/a|    0     0     4    -2   -25    59  -.09   17   16 |    3678   -1266   3136   9727
gfz  n/a|    0     0     0    13    10    22  -.20   18   19 |       0   -2007   3138   8964
grg  n/a|    3     1     0   -23    -9   -75   .30   15   15 |    8492   -1515   3169   8773
iac  n/a|    0     0    -1     0    19    -9  -.04   18   18 |    8800    -283   3129   9590
jgx  n/a|    2     0    -6    28    -7    27  -.15   16   16 |    4121   -1155   3115   9014

Table 2.2415.5  GPS week: 2415   Day: 5   MJD: 61154                            

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     0   -16     0    -2   .17   14   14 |     740    1477   3269   7839
esa  n/a|   -2     0     2   -22   -26    79  -.01   16   14 |    3123    1489   3263   8198
gfz  n/a|    0     0     1    -8    17   -19  -.18   16   17 |       0    1294   3264   7889
grg  n/a|    4    -1     1     0    16   -27   .33   14   14 |    7440    1399   3321   7580
iac  n/a|   -1    -1    -4     4     3   -35  -.16   16   16 |    9247     528   3269   8548
jgx  n/a|    1     1    -4   -20    -5     9  -.14   15   15 |    3180    1329   3266   8009

Table 2.2415.6  GPS week: 2415   Day: 6   MJD: 61155                            

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     7     0    13   .16   14   14 |    2288    1363   3488   8795
esa  n/a|   -3     0     1    -6   -13    37  -.08   20   19 |    4749     960   3475   8925
gfz  n/a|   -2     0     5    -6    35    32  -.19   18   17 |       0    1408   3482   8979
grg  n/a|    1     1    -2    17    -2   -36   .26   12   12 |    7413    1885   3452   8832
iac  n/a|    0    -2     0   -14   -46   -23  -.20   17   17 |   10210    -357   3473   9566
jgx  n/a|    0     1    -5   -15    19    11  -.18   15   15 |    4215    1566   3417   8969

       
       
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 3.2415.0  GPS week: 2415   Day: 0   MJD: 61149                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  | 1266    8   34   15    9   19   17    7 |    77   66   87   83   80   66    77
 R03  |  696    8   24   10   10   13    8    5 |    71   65   73   73   78   67    71
 R04  | 1275   21   43    7   24   17   10    8 |    68   74   59   52   50   51    56
 R05  | 2081   14   29    8   15   11   17    6 |    61   62   53   45   46   47    50
XR06  |  888   39  570   22  ---   56  ---   28 |    42   15  332  ---   79  ---    60
 R07  |  777    9   45   15   11   20   13    7 |    70   65   78   72   82   63    72
 R08  | 1138   29   58   18   26   31   27   13 |    50  101   69   72   78   59    65
 R09  | 2502   17   33   17   17   13   13    7 |    28   50   45   28   37   37    34
 R11  | 1402   14   19   15   11   13   14    6 |    46   44   43   40   40   34    38
 R12  | 1960   13   21   12   17    8   23    7 |    67   67   71   66   63   56    63
 R14  | 2864    9   20   15   16   11   15    6 |    66   73   77   79   75   57    70
 R15  | 1221    8   23   14   16   16   15    6 |    70   76   69   73   72   56    67
 R16  | 3334   13   29   21   11   19   16    7 |    66   62   70   62   57   49    60
 R17  | 1074    8   28   11   13   11   14    5 |    22   30   23   29   20   22    22
 R18  | 1141    8   16    7   14   12    7    4 |    28   41   32   35   29   24    29
XR19  | 1239    7   29   13  ---   16   16    7 |    16   33   15  ---   26   23    17
 R20  | 1690    9   44   14    9   17    8    6 |    19   44   23   24   23   23    20
 R21  |  802   10   91   10   12   21    9   10 |    18   78   25   35   24   17    21
 R22  | 1642    8   35   13   13   10   15    6 |    10   31   23   25   21   16    16
 R24  | 2674    9   25   14   12   20   21    7 |    23   37   23   26   24   23    21
XR26  | 8742   37   64   19  ---   53  ---   23 |    33   71  416  ---   59  ---   186
------+-----------------------------------------+-------------------------------------
 RMS  | 1805   13   39   14   15   16   15      |T   45   56   81   51   50   41    53
 WRMS | 1805   13   36   12   14   16   15      |NE  45   56   81   51   50   41    53
 MEDI | 1275    9   29   14   13   16   15      |MD  46   62   59   45   50   47    56

Table 3.2415.1  GPS week: 2415   Day: 1   MJD: 61150                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  | 1152    9   23   24   13    9   16    7 |    57   47   73   64   55   53    58
 R03  |  893   10   15   14   17   17    7    6 |    52   46   47   58   61   52    52
 R04  |  994   20   26    8   15   17   11    7 |    50   48   40   41   33   37    39
 R05  | 1223   18   13   10   18   15   12    6 |    42   38   39   35   32   38    35
XR06  |  991   38  ---   32  ---   68  ---   34 |    58  ---  373  ---   86  ---   107
 R07  |  794    8   17   16   11   17    9    6 |    45   56   31   45   48   44    43
 R08  | 1016   24   33   19   25   20   35   11 |    39   59   44   52   50   23    41
 R09  | 2730   14   23   28   21   19    7    8 |    22   38   39   20   30   28    25
 R11  | 1469   14   23   22   12   20   14    8 |    35   42   34   32   34   31    31
 R12  | 1276   14   20   11   19   16   19    7 |    54   47   43   39   48   40    43
 R14  | 1738   11   13   14   24   17   14    7 |    44   47   41   67   56   39    48
 R15  |  975   10   17   14   13   12   18    6 |    48   40   48   53   45   31    43
 R16  | 2119   18   50   18   22   17   16   10 |    45   71   46   42   48   41    43
 R17  | 1691    6   12   25   12    9   20    6 |    20   23   30   24   17   20    18
 R18  | 1299   13   23   11    9    9   20    6 |    27   38   34   30   22   26    27
XR19  | 1236    9   10   15  ---   11   11    5 |    14   19   14  ---   17   23    15
 R20  | 1730   11   16   11    7   13   11    5 |    13   33   14   20   20   19    16
 R21  |  768    7   17   13   13   20   16    6 |    21   30   16   21   24   16    16
 R22  | 2036   16   21   21    9    7    8    6 |    12   22   28   27   17   17    16
 R24  | 3115    8   21   13   11   16   12    6 |    20   23   21   23   17   17    18
XR26  | 6579   38   71   38  ---   44  ---   27 |    37   54  320  ---   39  ---   138
------+-----------------------------------------+-------------------------------------
 RMS  | 1632   14   23   17   16   16   16      |T   35   41   65   38   38   31    41
 WRMS | 1632   14   20   15   14   15   16      |NE  35   41   65   38   38   31    41
 MEDI | 1276   13   20   15   13   17   14      |MD  39   40   39   35   34   31    39

Table 3.2415.2  GPS week: 2415   Day: 2   MJD: 61151                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  982    9   22    7   14   16   14    6 |    62   54   56   68   66   55    61
 R03  | 1212    5   29   12   14   20   14    7 |    59   53   60   60   69   54    59
 R04  | 1255   11   14   13    8    9   20    5 |    53   41   66   59   56   48    54
 R05  |  919   22    9    7   11   12   12    6 |    47   35   35   42   31   27    34
XR06  | 9854 1188  --- 1055  ---  ---  --- 1120 |    83  ---  944  ---  ---  ---   976
 R07  |  938   13   12   15   15   17   14    6 |    48   44   48   49   45   53    46
 R08  | 1418   30   33   17   16   10   20    9 |    34   65   60   50   44   42    47
 R09  | 2624   11   19   15   11   16   13    6 |    20   30   25   23   32   27    23
 R11  | 1776   10   19   19   26   19   13    8 |    29   36   40   33   28   28    28
 R12  | 1041   10   20   15   14   18   16    7 |    54   62   63   56   52   45    53
 R14  | 1500   10   12    9   11   11   14    5 |    65   64   65   72   68   51    64
 R15  |  838   10   19    9   17   11   18    6 |    57   47   51   63   50   39    51
 R16  | 1113   16   24   22   14   11   16    8 |    58   49   67   55   50   42    53
 R17  | 3264    8   25    8   13   11    9    5 |    20   28   27   28   24   20    22
 R18  | 1855   17   16    6   13    9   23    6 |    24   26   24   34   23   17    22
XR19  | 1374   17   10    8  ---   13   11    6 |    21   24   20  ---   26   26    22
 R20  | 1637   10   23    9    7   13    9    5 |    16   30   22   24   24   20    20
 R21  | 1082   11   25    8   12   14   27    7 |    23   31   21   24   21   20    19
 R22  | 2608   11   15   15   14    9   12    5 |    12   20   16   21   17   18    14
 R24  | 3001   15   19   11   11   12   17    6 |    22   26   30   24   22   28    22
XR26  |11327   45   72   38  ---   60  ---   30 |    26   65  460  ---   55  ---   209
------+-----------------------------------------+-------------------------------------
 RMS  | 1777   14   21   13   14   14   16      |T   39   41  104   43   40   34    90
 WRMS | 1777   14   20   12   13   14   16      |NE  39   41  104   43   40   34    90
 MEDI | 1418   11   19   12   13   12   14      |MD  34   36   48   42   32   28    46

Table 3.2415.3  GPS week: 2415   Day: 3   MJD: 61152                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  785   13   19   13   27   15   20    8 |    77   76   79   93   83   70    79
 R03  | 1187   11   28   15   14   27   13    8 |    65   61   75   77   86   61    69
 R04  |  720    8   18   17    9   16   12    6 |    62   61   72   69   53   55    61
 R05  | 1760   16   15   12   10   11   13    6 |    60   45   53   53   48   40    50
 R07  |  990    7   22   10   11   21    8    6 |    58   60   57   55   69   56    58
 R08  | 1516   28   28   13   17   14   27   10 |    41   68   55   60   46   60    52
 R09  | 2451   10   22   15   13   18   15    6 |    22   37   26   20   22   31    22
 R11  | 1732   11   16   12   13    9   11    5 |    28   34   30   24   32   25    25
 R12  |  985    5   19   17   14   10   19    6 |    52   52   57   58   48   34    49
 R14  | 2031    7   16   14   15   18   12    6 |    58   66   62   64   57   49    58
 R15  | 1259    9   14   14   18   19   13    6 |    63   59   68   53   70   51    59
 R16  |  805   15   21   19   13   18   19    7 |    66   58   70   64   55   45    58
 R17  | 2526   10   20   10    6   13   11    5 |    21   27   30   25   21   24    22
 R18  | 2147   14   17   13    8   15    9    5 |    24   26   27   29   19   21    21
XR19  | 1367   14   12   14  ---   16   13    7 |    19   27   24  ---   19   28    20
 R20  | 1114   11   14   19   11   15   12    6 |    19   28   32   19   21   25    20
 R21  | 1333    7   25   15   18   19   20    7 |    23   29   29   28   25   18    21
 R22  | 2166    8   16   12   10   12    9    5 |    20   30   16   23   22   26    19
 R24  | 2213    8   26   21   16   19   14    7 |    23   26   25   25   27   21    21
XR26  |12765   42   70   37  ---   75  ---   31 |    29   53  226  ---   53  ---   121
------+-----------------------------------------+-------------------------------------
 RMS  | 1647   12   20   15   14   17   15      |T   45   46   55   46   43   38    59
 WRMS | 1647   12   20   14   15   17   15      |NE  45   46   55   46   43   38    59
 MEDI | 1367   10   19   14   13   16   13      |MD  41   45   53   53   46   34    50

Table 3.2415.4  GPS week: 2415   Day: 4   MJD: 61153                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  801   10   10   10   11   17   14    5 |    65   67   63   69   59   62    64
 R03  | 1777    6   12   12   17   21   20    6 |    66   68   69   70   72   52    64
 R04  |  846   12   16   12    9   12   16    6 |    68   59   52   63   69   54    61
 R05  | 3316    6   11   10   12   16   12    5 |    56   59   56   57   45   49    53
 R07  | 1109    9   17   19   12   23    8    6 |    59   57   66   54   72   58    59
 R08  | 1656   28   23   12   21   19   25   10 |    39   65   49   61   61   48    50
 R09  | 1416    9   16   13   10   15   14    5 |    21   27   20   22   24   22    19
 R11  | 3430   14   17   23   15   23   14    8 |    32   28   41   33   25   29    28
 R12  | 1219    8   17   23   14   12   18    7 |    43   43   59   51   43   34    43
 R14  | 2184    9   23   10   22    9   13    7 |    48   51   47   60   45   38    47
 R15  |  847   10   18   10   17   18   13    6 |    54   45   51   47   52   38    47
 R16  | 1121   16   19   13   13   16   18    7 |    57   45   43   48   51   40    46
 R17  | 1742    6   19   18   15   20   10    6 |    20   33   26   23   25   18    20
 R18  | 1814   13   16   21   19   24    9    7 |    24   22   34   26   33   20    22
XR19  | 1241   10   11   14  ---   14   13    6 |    18   23   18  ---   28   19    18
 R20  | 1038    7   17   14   12    9   13    5 |    22   26   28   18   30   25    22
 R21  | 2014    9   25   28   24   17   21    9 |    18   21   25   22   31   18    16
 R22  | 1886   10   13   26   15   27    9    7 |    13   24   23   24   31   17    16
 R24  | 2376    8   16   25   10   19   26    8 |    22   26   28   23   20   24    19
XR26  | 7391   45   65   43  ---   73  ---   32 |    25   69  805  ---   67  ---   360
------+-----------------------------------------+-------------------------------------
 RMS  | 1858   12   17   18   15   18   16      |T   39   42   80   42   44   35    59
 WRMS | 1858   12   16   19   15   18   16      |NE  39   42   80   42   44   35    59
 MEDI | 1656    9   17   14   14   17   14      |MD  39   43   43   47   43   34    46

Table 3.2415.5  GPS week: 2415   Day: 5   MJD: 61154                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  919    8    8   11    5   13   12    4 |    43   40   42   42   42   40    40
 R03  | 2267   10    8    9   21   12   15    6 |    59   63   58   70   65   51    60
 R04  |  833   17   12   11   14   12    6    5 |    66   59   60   60   57   55    59
 R05  | 3727   15   11   15    9   12   10    5 |    51   40   41   42   40   43    42
 R07  | 1171    6   12   11    8   25   18    6 |    43   42   48   47   55   29    42
 R08  | 1224   29   16   21   15   24   15    9 |    29   41   52   54   52   39    43
 R09  | 1166   11   13   13    9   22   10    6 |    24   33   27   34   37   30    29
 R11  | 4796   26   12   23   15   29   10    9 |    38   29   32   22   32   28    26
 R12  | 1114   10   14   23   14   10   17    7 |    49   46   53   44   42   33    43
 R14  | 1994    9   20   11   16    9   14    6 |    48   56   57   57   49   46    51
 R15  |  910    7   19    9   15   17   17    6 |    54   58   57   60   51   46    53
 R16  |  800   15   19   17   16   16   13    7 |    53   52   52   49   45   41    46
 R17  | 2457    9   14   11    7    9   15    5 |    18   18   17   20   15   17    15
 R18  | 1082   16   25   19   18   12   21    8 |    17   28   28   21   19   13    16
XR19  | 1645    8   16   17  ---    9   11    6 |    15   19   19  ---   20   20    15
 R20  |  851    9   12   15   14   15    9    5 |    22   28   28   36   27   25    26
 R21  | 2956   12   21   24   20   14   21    8 |    21   23   32   26   19   22    20
 R22  |  865   13   15   19   17   12   18    7 |    12   16   28   23   22   24    16
 R24  | 3253   12   19   12   10   13   15    6 |    19   24   25   20   21   17    16
XR26  | 9602 1505  --- 1825  ---  ---  --- 1657 |    58  --- 9999  ---  ---  ---   822
------+-----------------------------------------+-------------------------------------
 RMS  | 2141   14   16   16   14   16   15      |T   40   37   39   40   38   32    72
 WRMS | 2141   14   14   17   14   16   15      |NE  40   37   39   40   38   32    72
 MEDI | 1171   11   14   15   14   13   15      |MD  43   40   41   42   40   30    42

Table 3.2415.6  GPS week: 2415   Day: 6   MJD: 61155                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  884   10   25   17   10   22    8    7 |    77   71   82   86   88   74    80
 R03  | 1735    8    8   16   18   12   12    6 |    85   84   81  100   87   76    86
 R04  |  938   29   22   12   13   20   12    8 |    87   81   72   72   67   69    73
 R05  | 3173   11   11    7    8   18   16    5 |    77   73   67   73   70   61    70
 R07  | 1356    7   27   17   11   13   11    6 |    76   68   81   75   83   69    75
 R08  | 2103   32   14   26   14   20   16    9 |    54   85   89   83   79   72    74
XR09  | 1357    8   17   15   10   14  ---    6 |    19   32   17   17   25  ---    18
 R11  | 5028   16   14   22    9   20   16    7 |    40   35   47   30   38   29    34
 R12  |  860    8   14   25    9    9   21    6 |    62   60   75   64   64   48    61
 R14  | 3554    9   19   18   14   22   15    7 |    59   70   64   63   68   50    60
 R15  |  836    7   28   12   11   19   19    7 |    70   75   71   67   75   56    67
 R16  |  809   11   15   22   16   15   13    7 |    68   63   79   65   55   53    63
 R17  | 2824   12   16   14    8   11   11    5 |    20   21   29   20   21   21    18
 R18  | 1116   11   24   15    9   12   26    7 |    21   25   21   21   26   22    19
XR19  | 1915    9    9   13  ---   12   10    5 |    19   22   23  ---   24   20    20
 R20  | 1189   15   18   19   12   20   11    7 |    26   37   40   35   31   28    31
 R21  | 3547    8   30   11   10   14   11    6 |    20   22   21   24   17   19    18
 R22  |  998   13   16   16   13   18   15    6 |    21   21   29   23   18   26    20
 R24  | 2334   10   18   21   10   23   10    6 |    22   25   24   24   30   22    21
------+-----------------------------------------+-------------------------------------
 RMS  | 2309   14   20   18   12   17   15      |T   49   51   53   52   51   45    48
 WRMS | 2309   14   19   17   12   17   15      |NE  49   51   53   52   51   45    48
 MEDI | 1357   10   17   16   10   18   12      |MD  54   60   64   63   55   48    60



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