[IGSREPORT-30915] Wk 2414 IGLOS Final Orbits

acc acc at igs.org
Fri May 1 03:04:16 UTC 2026


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2414   (Apr 12, 2026 - Apr 18, 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 2.2414.
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:
                                                                               
 igl2414[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2414 in the SP3 format.
 igl24147.sum      Combination Report for GPS Week 2414.


    
    
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  |      6.4 ns
                1  |      8.9 ns
                2  |      7.2 ns
                3  |      6.9 ns
                4  |     10.8 ns
                5  |      5.9 ns
                6  |      8.0 ns

 5. The following orbit solutions were excluded from the combination
    because they were biasing the weighted average (generally indicated
    by long arc RMS).
    
               Day | Centre | PRN list
               ----+--------+---------------
                0  |  IAC   | R06
                1  |  ESA   | R06
                2  |  ESA   | R06
                3  |  ESA   | R06
                4  |  ESA   | R06
                5  |  ESA   | R06
                6  |  ESA   | 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 1.2414, 1a.2414).
        
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 2.2414.0-6)                                                                                
    
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 3.2414.0-6). 
        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 2414 summary.                      (Apr 12, 2026 - Apr 18, 2026)

Table 1.2414.a     GPS week : 2414   MJD: 61142.0-61148.0

         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     3     2     2     7   .12   13   13 |      99    -519   3239   9445
        |    0     1     2    14    15    18   .03           |     922    2279
esa  n/a|   -2    -2     7   -17   -37    33  -.05   33   31 |    5511    -714   3270   9720
        |    1     2     2    28    29    36   .08           |    1838    2591
gfz  n/a|    0     0     1    19     7    -5  -.11   15   15 |       0    -650   3235   9212
        |    1     0     1    11    14    28   .04           |       0    2440
grg  n/a|    1     0     2   -34     5   -21   .29   23   15 |    7893    -700   3367   9064
        |    0     1     4    16    17    30   .05           |     436    2709
iac  n/a|    1     0    -4    14    21    -8  -.12   18   18 |    8554    -429   3239   9867
        |    1     1     2    25    21    56   .03           |     995    1518
jgx  n/a|    0     0    -5    -1    -5    -2  -.13   13   13 |    2841    -681   3356   9370
        |    1     0     1     9    12    16   .05           |     792    2832


Table 1.2414.b     GPS week : 2414   MJD: 61142.0-61148.0   

         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  |    6    5    8    6    7    5    6 |
 R03  |    5    4    6    6    8    5    6 |
 R04  |    7    7    6    7    9    7    7 |
 R05  |    7    6    6    6    6    6    8 |
 R06  |   20   31   30   32   33   29   30 |
 R07  |    7    7    5    6    6    7    7 |
 R08  |   11   11   12   12   13   13   12 |
 R09  |    7    7    6   15    9    7    7 |
 R11  |    6    7    6    7    6    8    9 |
 R12  |    5    7    6    6    8   12   12 |
 R14  |    5    7    6    7   17   12    7 |
 R15  |    7    6    8    7    6   14   11 |
 R16  |    7    7    7    9    9   11   11 |
 R17  |    7    7    7    7    7    7    6 |
 R18  |    6    5    6    7    7    7    6 |
 R19  |    7    8    8    7    8    7    7 |
 R20  |    7    8    9    6    7    7    8 |
 R21  |    7   10    9   11   10    9    9 |
 R22  |    5    8    5    7    6    8    7 |
 R24  |    7    6    6    8    8    7    8 |
 R26  |   29   29   27   28   27   33   32 |


Table 1.2414.c     GPS week : 2414   MJD: 61142.0-61148.0   

         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 2414 0   |   77   156   165    -125    2995    6411  77.9  1857  1857 |    6370       0
brd 2414 1   |  171    58    47      39    2379    4870  78.2  1641  1641 |    8865       0
brd 2414 2   |   15    43    87     -69      -5    7969  78.1  1900  1900 |    7151       0
brd 2414 3   |  -27    56    43      78    -969   11800  77.6  1846  1846 |    6931       0
brd 2414 4   |  -42    49    95    -779     223    8458  76.7  2222  2222 |   10824       0
brd 2414 5   |  -48   -46   -30    -812    -652    6623  80.6  2062  2062 |    5894       0
brd 2414 6   |   37   -85    30    1234    1600    4387  80.5  1844  1844 |    8043       0
-------------+------------------------------------------------------------+----------------
brd 2414 mean|   26    33    62     -62     795    7216  78.5  1910  1910 |    7725       0
brd 2414 sdev|   78    78    61     682    1537    2504   1.5   184   184 |    1690       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 2.2414.0  GPS week: 2414   Day: 0   MJD: 61142                            

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     2     4    25    31    10   .10   14   15 |     721   -2714   2974   9204
esa  n/a|   -4    -3     3   -18   -66    15  -.02   20   19 |    2891   -1317   3029   9464
gfz  n/a|    2     0     2    28     7    12  -.07   14   13 |       0   -2285   2975   8843
grg  n/a|    1    -1     1   -21   -15   -69   .27   15   15 |    7349   -2235   3085   8798
iac  n/a|    2    -1    -2   -10    22    76  -.14   17   15 |    6945    -306   2979   9599
jgx  n/a|    0     1    -4     0     0   -11  -.13   10   10 |    3257   -2488   3135   9213

Table 2.2414.1  GPS week: 2414   Day: 1   MJD: 61143                            

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     2    16   -11     3   .09   11   11 |    -168     544   3080   9145
esa  n/a|   -2    -6    10   -32   -60    10  -.15   38   35 |    3805    1519   3119   8489
gfz  n/a|    0     0     1    12    -6    11  -.09   15   16 |       0     501   3076   8964
grg  n/a|    1     0     2   -45    -2   -15   .24   15   12 |    8618     359   3264   8805
iac  n/a|    1     1    -8    -5    40     7  -.07   15   15 |    8633     842   3072   9530
jgx  n/a|    0     0    -4    17   -12   -23  -.21   12   12 |    2507    1169   3227   9107

Table 2.2414.2  GPS week: 2414   Day: 2   MJD: 61144                            

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    -9     0   -18   .09   12   12 |    -759   -1023   3007   9020
esa  n/a|   -2    -3     6    -4   -58    85  -.03   36   31 |    5352    -529   3030   9566
gfz  n/a|    0     0     2    34    20    26  -.19   16   13 |       0   -1315   3007   8880
grg  n/a|    1     0     3   -17     2    21   .22   12   13 |    7779   -1803   3118   9019
iac  n/a|    4     1    -5    46     1   -90  -.10   18   19 |    8403    -118   3008   9560
jgx  n/a|    0     0    -6    -5    -4    16  -.17   13   13 |    3108   -2139   3121   9290

Table 2.2414.3  GPS week: 2414   Day: 3   MJD: 61145                            

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    -6     5     2   .16   12   12 |   -1372   -2405   3130   9741
esa  n/a|    0    -3    10    14   -12     2  -.15   33   33 |    6117   -2394   3167  10368
gfz  n/a|    1     0     3    22    15   -54  -.10   18   17 |       0   -2924   3125   9520
grg  n/a|    0     0     2   -32    13   -20   .35   24   15 |    7849   -2410   3302   9630
iac  n/a|    3     0     0    -7     0    38  -.16   16   17 |    8753   -2655   3134  10266
jgx  n/a|   -1     0    -7     3    -1     6  -.11   15   15 |    1920   -2610   3295   9903

Table 2.2414.4  GPS week: 2414   Day: 4   MJD: 61146                            

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     6    -9    -2    -5   .10   14   15 |     773    3770   3607   9598
esa  n/a|    0     2     8   -27   -59    46   .03   35   36 |    7556    3851   3617  10217
gfz  n/a|   -1     0    -2    24     1     5  -.08   16   16 |       0    4191   3601   9325
grg  n/a|    2    -2     0   -22   -10   -40   .34   33   21 |    8251    4740   3752   8862
iac  n/a|    0     2    -4     4    59   -14  -.15   24   25 |   10298    1637   3608   9865
jgx  n/a|    1     0    -5    -5     4     2  -.11   12   12 |    2808    4787   3723   9131

Table 2.2414.5  GPS week: 2414   Day: 5   MJD: 61147                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
cod  n/a|    0     1     7   -10   -15    23   .16   14   15 |    1221   -2070   3385  10790
esa  n/a|   -2    -1     9    12     0    79  -.05   33   32 |    7886   -3372   3424  11342
gfz  n/a|    0    -1     2    11    28   -30  -.06   14   13 |       0   -2279   3377  10490
grg  n/a|    2     0    -3   -34    35     8   .27   40   17 |    7473   -3281   3451  10096
iac  n/a|    0     0    -5    47    12   -61  -.08   19   20 |    8755   -2121   3380  11119
jgx  n/a|    0     0    -4    -8     3    12  -.06   12   12 |    4234   -3059   3393  10377

Table 2.2414.6  GPS week: 2414   Day: 6   MJD: 61148                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
cod  n/a|    0     0     2     8    11    36   .12   12   13 |     277     261   3494   8619
esa  n/a|   -4    -2     4   -67    -5    -2   .03   37   34 |    4970   -2759   3507   8595
gfz  n/a|   -1     0     0     0   -13   -12  -.14   15   14 |       0    -441   3486   8463
grg  n/a|    1    -2    10   -65    12   -33   .31   25   15 |    7933    -274   3597   8244
iac  n/a|    1     0    -6    24    13   -17  -.11   15   14 |    8093    -287   3497   9132
jgx  n/a|    1     0    -8   -13   -30   -22  -.10   18   18 |    2053    -432   3604   8574

       
       
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 3.2414.0  GPS week: 2414   Day: 0   MJD: 61142                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02M |  944   10   13   14   14   19    8    5 |    57   58   67   66   68   57    61
 R03M | 1339    6   15    9   12   16   10    5 |    68   67   65   72   75   61    66
 R04  |  740   22   18    7    9   16   14    6 |    66   73   58   60   54   48    57
 R05  | 2644   14   22   19   11   13   11    6 |    61   59   51   57   56   49    54
XR06  | 1021   18  ---   21  ---  101  ---   20 |    27  ---   55  ---   98  ---    44
 R07  |  911   13   29   11   17   19    7    7 |    68   88   67   69   76   65    69
 R08  | 1691   28   37   17   28   20   13   10 |    47   93   65   63   61   55    58
 R09E | 2216   11   16   19   15   18   10    6 |    47   55   54   43   54   46    47
 R11E | 2315   10   17   13   13   15    9    5 |    46   51   50   53   48   51    49
 R12E | 1137    7   16   11   17    8    8    5 |    71   71   73   78   68   72    71
 R14E | 1460   10   13    9   14    9   10    5 |    73   78   79   86   76   72    76
 R15E | 1551   11   18   16   16   16   10    6 |    38   43   40   51   42   38    39
 R16E | 2898   15   19   17   17   13   11    6 |    63   82   71   76   66   68    69
XR17  | 1507    8   20   15   12   13  ---    7 |    51   42   49   52   45  ---    47
 R18  | 1345   12   12   14    8   19    8    5 |    33   41   36   35   32   33    33
XR19  |  954   11   16   15  ---   17    9    6 |    23   26   27  ---   22   24    22
 R20  | 1112   18   15   22    8   14   10    6 |    28   36   40   30   31   31    28
 R21  | 3023    8   23   12   10   27    9    6 |    37   60   35   42   46   39    38
 R22  |  978    6   19   12   13   10    8    5 |    21   31   25   33   28   25    24
 R24  | 2652   14   16   14   13   19   12    6 |    44   46   45   40   48   47    44
XR26  | 7396   44   66   33  ---   57  ---   28 |    24   87   34  ---   83  ---    46
------+-----------------------------------------+-------------------------------------
 RMS  | 1856   14   20   14   15   17   10      |T   47   59   51   55   56   48    49
 WRMS | 1856   15   19   13   15   15   10      |NE  40   56   45   48   52   41    43
 MEDI | 1460   11   17   14   13   16   10      |MD  47   58   51   53   54   48    47

Table 3.2414.1  GPS week: 2414   Day: 1   MJD: 61143                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02M |  818    8   25   12   12   14    6    5 |    39   39   42   42   42   40    39
 R03M |  942    6   15    9   11   13    6    4 |    45   44   41   50   48   43    45
 R04  |  925   16   28   11    6   22   16    7 |    48   53   44   47   40   35    42
 R05  | 1094   11   29   18    6   10   11    6 |    39   40   53   43   37   38    40
XR06  |  928   30  571   24  ---   69  ---   30 |    24  112   27  ---   54  ---    32
 R07  | 1059    9   37   17   18    8    5    6 |    46   47   36   57   43   47    45
 R08  | 1133   18   76   17   23   18   12   10 |    36   73   37   49   32   43    38
 R09E | 2618   12   36   15   13   14   14    6 |    50   56   50   48   52   46    48
 R11E | 2400    8   23   20   19   16   12    7 |    52   54   56   52   55   58    53
 R12E | 1741    9   33   12   16   18    9    6 |    78   83   80   81   78   81    78
 R14E |  932    8   19   22   20   12   11    7 |    91   86   90   99   86   85    89
 R15E | 1458    8   23   15   15   13   13    6 |    48   56   50   54   49   47    48
 R16E | 3127   17   32   12   18    9    9    7 |    71   76   71   74   67   69    70
XR17  | 2278   10   23    9   12   15  ---    6 |    34   37   36   39   43  ---    35
 R18  | 1749   10   17   10    7   13   11    4 |    30   38   36   36   34   31    32
XR19  |  876   11   16   22  ---   16   10    7 |    32   37   31  ---   33   34    30
 R20  |  771    9   46   19   12   21   14    8 |    36   49   27   29   39   38    32
 R21  | 2177    8   79   15   20   21   14   10 |    31   51   35   33   31   32    31
 R22  |  883   13   32   18   16   19   13    7 |    30   37   33   34   35   33    30
 R24  | 1467    7   23   10   11    8   17    5 |    34   40   34   36   39   33    33
XR26  |10754   40   84   29  ---   68  ---   29 |    32   49   46  ---   61  ---    41
------+-----------------------------------------+-------------------------------------
 RMS  | 1640   11   38   15   15   15   12      |T   44   55   45   50   47   46    44
 WRMS | 1640   11   35   16   12   15   12      |NE  34   51   36   40   40   36    35
 MEDI | 1133   10   29   15   13   15   11      |MD  39   49   41   47   43   40    40

Table 3.2414.2  GPS week: 2414   Day: 2   MJD: 61144                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02M |  873   12   25   17   13   18   19    7 |    45   53   63   63   58   39    51
 R03M | 1782    6   25   19    9   12   11    5 |    52   45   63   58   52   49    53
 R04  | 1047   12   26   11    9   13   17    6 |    56   65   61   60   51   47    54
 R05  | 3341    9   23   16    9   12   16    6 |    48   56   52   54   51   41    48
XR06  |  919   32  579   21  ---   69  ---   29 |    25  152   44  ---   67  ---    38
 R07  | 1145   10   32    7    7   11   11    5 |    52   61   51   53   50   48    51
 R08  | 1238   27   77   13   18   22   20   12 |    36   92   47   57   31   46    44
 R09E | 1656    9   38   12   10   19    7    6 |    30   37   31   27   32   28    28
 R11E | 2904   13   19   14   11   19   11    6 |    32   35   32   37   38   36    33
 R12E | 1647    8   22   15    9   18   10    5 |    35   29   41   39   44   27    33
 R14E |  864    9   20   13   13   17   11    5 |    34   32   31   40   40   26    31
 R15E | 2589    8   24   18   15   23   16    7 |    40   36   46   51   35   41    41
 R16E | 2947   13   28   18   18   18   10    7 |    80   85   81   88   77   81    80
XR17  | 1892   13   23   16   10   10  ---    6 |    48   41   42   40   37  ---    40
 R18  | 1893   12   15   18    9   16    4    5 |    29   35   40   35   26   27    29
XR19  | 1127   13   16   21  ---    9   14    7 |    13   25   22  ---   20   22    16
 R20  |  812   14   54   26    8   17   10    8 |    20   53   43   25   26   27    25
 R21  | 1632    6   71   12   13   23    9    9 |    32   33   37   37   26   33    31
 R22  | 2107    6   22   16    8   15   10    5 |    21   31   28   24   25   28    23
 R24  |  959   10   21   16   11   20   11    6 |    35   40   45   39   35   41    37
XR26  | 9556   35   55   30  ---   74  ---   27 |    31   56   30  ---   73  ---    37
------+-----------------------------------------+-------------------------------------
 RMS  | 1899   12   36   16   12   18   13      |T   37   52   44   45   42   38    39
 WRMS | 1899   12   31   13   13   19   13      |NE  34   56   41   42   39   36    36
 MEDI | 1647   12   25   16   10   18   11      |MD  35   41   43   40   38   36    37

Table 3.2414.3  GPS week: 2414   Day: 3   MJD: 61145                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02M |  829    9   20   13   14   13   10    5 |    57   63   53   66   64   48    56
 R03M | 3203    7   21    9   25   11   14    6 |    61   67   66   83   70   57    65
 R04  | 1092    9   25   16   23   10   18    7 |    56   68   61   48   61   44    53
 R05  | 3166    6   22   16   15   12   13    6 |    53   60   63   56   62   48    55
XR06  | 1109   35  581   23  ---   66  ---   32 |    26  137   41  ---   76  ---    43
 R07  | 1317    7   25   13   11   12   12    5 |    57   68   63   57   63   50    57
 R08  | 1193   27   55   11   21   12   32   12 |    39   85   52   58   55   55    51
 R09E | 1250   10   34   43   69   21   16   14 |    31   45   51   68   33   32    29
 R11E | 2600   12   22   19   10   12   14    6 |    26   33   31   30   33   34    28
 R12E | 1891    7   21   17   15   15    9    6 |    54   50   62   55   63   53    55
 R14E | 1418   15   33   16   16   14    9    7 |    98   84   82   95  101   92    92
 R15E | 2212    9   18    9   18   18   17    6 |    35   33   34   44   40   34    34
 R16E | 1169   14   26   21   21   22   15    8 |    59   57   62   61   63   59    58
XR17  | 1287    8   23   13   24    9  ---    7 |    29   33   35   30   23  ---    27
 R18  | 1954   10   21   19   19   14   11    6 |    29   27   33   26   24   28    25
XR19  | 1160   13   20   12  ---   12   10    6 |    13   24   21  ---   21   22    17
 R20  | 1477   11   30   16   11    9   11    6 |    15   30   23   21   20   19    16
 R21  | 1751    6   78   17   26   11   14   11 |    23   32   28   35   21   21    21
 R22  | 1369    8   26   13    7   22   12    6 |    12   35   20   22   28   20    18
 R24  | 1220   13   21   11   16   29    9    8 |    31   36   31   28   32   30    28
XR26  |10722   38   59   31  ---   68  ---   28 |    13   60   21  ---   68  ---    32
------+-----------------------------------------+-------------------------------------
 RMS  | 1846   12   33   18   24   16   15      |T   38   53   44   49   48   41    40
 WRMS | 1846   12   33   17   15   17   15      |NE  30   53   37   38   42   33    34
 MEDI | 1369   10   25   16   16   13   12      |MD  31   50   41   48   55   34    34

Table 3.2414.4  GPS week: 2414   Day: 4   MJD: 61146                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02M |  720   10   16   20   10   15   12    6 |    47   38   35   42   45   38    39
 R03M | 3862   10   36   20   33   14   10    8 |    59   78   48   76   47   49    53
 R04  |  954   18   38   17   19   14   16    8 |    57   69   52   46   56   38    49
 R05  | 2316    8   26   10   13   12   11    5 |    58   65   59   52   53   51    55
XR06  | 1003   27  620   26  ---   87  ---   33 |    22  166   43  ---   70  ---    35
 R07  | 1092    7   27   11    9   13   12    5 |    56   63   55   55   59   53    55
 R08  | 1067   37   53   20   19   37   12   13 |    38   79   65   53   76   52    53
 R09E | 1248   11   36   11   49   15   16    9 |    28   27   26   65   26   29    26
 R11E | 5412   11   22   17   18   12   11    6 |    33   39   34   41   37   39    34
 R12E | 2348    9   21   23   25   11   14    7 |    56   60   60   69   59   61    58
 R14E | 2040   12   24   20  100   60   10   17 |    81   97   93  153   78   84    86
 R15E | 2199   10   25   11   19    9   11    6 |    39   46   40   48   42   40    39
 R16E | 1049   15   37   17   17   28   15    9 |    62   66   70   69   63   68    64
XR17  | 1192    9   25   12   15    9  ---    6 |    46   55   37   50   37  ---    41
 R18  | 1697   13   27   13   20   23   10    7 |    23   36   31   24   22   25    23
XR19  | 1085   14   19   23  ---   16   10    8 |    22   25   37  ---   22   18    18
 R20  | 2439    7   34   13   20   16    8    6 |    15   27   18   29   26   24    18
 R21  | 1426    6   75   13   27   15   10   10 |    24   36   26   32   18   18    20
 R22  |  840   11   26   11   13   21   10    6 |    10   30   18   20   22   19    14
 R24  | 1366    9   31    9   18   29   13    7 |    24   42   25   29   31   26    25
XR26  |11505   25   70   29  ---   76  ---   26 |    15   55   22  ---   61  ---    27
------+-----------------------------------------+-------------------------------------
 RMS  | 2222   14   35   16   33   24   12      |T   38   57   42   52   45   40    39
 WRMS | 2222   15   36   16   21   25   12      |NE  31   57   37   39   42   32    33
 MEDI | 1366   11   27   17   19   15   11      |MD  38   55   37   48   45   38    39

Table 3.2414.5  GPS week: 2414   Day: 5   MJD: 61147                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02M |  798    6   13    6   11   16    9    4 |    33   33   29   35   37   27    30
 R03M | 3144    9   16   14   14   10    6    4 |    38   37   26   44   32   33    32
 R04  | 2024   12   31   11   22   16    9    6 |    55   66   49   55   53   53    53
 R05  | 1127   15   25   11   15   12    9    6 |    49   45   42   38   46   41    42
XR06  |  891   34  587   21  ---   65  ---   29 |    17  187   40  ---   48  ---    32
 R07  | 1142    5   31   13   12   16   14    6 |    43   46   49   35   40   32    39
 R08  | 1132   35   64   14   19   25   12   12 |    27   69   48   43   48   35    39
 R09E |  968   11   33   17   20   15   11    7 |    35   44   36   42   37   35    34
 R11E | 3499   10   28   13   42   15   15    8 |    47   49   50   58   49   51    47
 R12E | 2071   14   27   14   82   21   16   12 |    74   73   77  106   70   78    73
 R14E | 4627   15   25   15   64   35   14   11 |   116  121  119  128  112  112   114
 R15E | 1245   11   30   25   90   31   16   14 |    54   57   52  107   70   53    54
 R16E | 1757   10   35   17   71   18   10   11 |    70   65   70   96   74   66    67
 R17  | 1164   12   25   12   12    8   17    6 |    25   21   25   27   21   14    22
 R18  | 1320   20   19   15   13   11   10    6 |    23   19   27   26   23   19    19
XR19  | 1337   11   24   15  ---   15   13    7 |    14   23   21  ---   25   21    17
 R20  | 2476   10   43   10   15   11    8    6 |    12   30   10   12   13   19    11
 R21  | 1413    7   59   11   15   14   14    8 |    18   25   20   24   21   24    18
 R22  | 1302   17   33   11   14   22   11    7 |    15   35   29   26   23   24    20
 R24  | 1269   10   14   14   22   24   12    7 |    24   25   25   25   29   28    23
XR26  |11849   45   47   31  ---   96  ---   33 |    13   33   28  ---   69  ---    25
------+-----------------------------------------+-------------------------------------
 RMS  | 2062   14   33   14   40   19   12      |T   38   52   41   51   44   40    38
 WRMS | 2062   15   32   13   17   20   12      |NE  25   48   31   31   35   28    27
 MEDI | 1320   11   30   14   15   16   12      |MD  33   44   36   38   40   33    32

Table 3.2414.6  GPS week: 2414   Day: 6   MJD: 61148                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02M |  816    7   20   10   10   13   17    5 |    64   61   60   64   66   52    60
 R03M | 1758    5   20   17   10   10   16    5 |    70   77   76   81   71   62    71
 R04  | 1701   11   30   12   16   14   15    6 |    80   97   74   74   71   69    74
 R05  | 1995   16   31   17   16   15   14    7 |    75   75   69   67   75   65    70
XR06  |  824   35  529   25  ---   61  ---   30 |    29  170   30  ---   83  ---    39
 R07  |  958    7   48   11   16    7   11    6 |    79   83   81   76   76   74    77
 R08  | 1087   32   69   17   11   23   12   12 |    52  119   77   75   69   66    68
 R09E | 1419    8   36   12   17   17   12    6 |    44   50   48   44   51   45    45
 R11E | 2249   11   29   16   29   12   25    8 |    47   48   54   50   50   57    49
 R12E | 2054   12   27   25   57   13   21   11 |    93   88   93  118   97   97    94
 R14E | 4429   13   22    9   28   16   14    7 |   156  145  151  160  157  148   154
 R15E |  716   13   28   17   48   15   25   10 |    63   55   57   92   66   61    61
 R16E | 2503    9   42   18   46   16   28   11 |    62   63   63   80   64   64    61
 R17  |  820    8   12   14   15   16   11    5 |    39   37   36   37   34   14    34
 R18  | 1089   10   33   12   11    9   17    6 |    30   37   29   27   24   25    26
XR19  | 1340   11   25   13  ---   17   12    7 |    22   29   25  ---   26   22    21
 R20  | 1635    6   51   12   12   14   13    7 |    19   34   18   19   25   22    19
 R21  | 1209    7   67   20   13   12    8    9 |    31   29   32   41   34   29    30
 R22  | 1248   11   29   10   16   14   17    6 |    18   40   19   22   23   23    19
 R24  | 1793   11   17   15   14   19   25    7 |    34   38   36   32   38   32    33
XR26  | 8458   43   49   32  ---   79  ---   31 |    15   59   28  ---   93  ---    39
------+-----------------------------------------+-------------------------------------
 RMS  | 1843   12   37   15   25   15   18      |T   53   68   55   64   61   54    54
 WRMS | 1843   13   34   14   15   14   18      |NE  40   65   42   47   51   40    42
 MEDI | 1419   11   30   15   16   15   15      |MD  47   59   54   64   66   57    49



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