[IGSREPORT-30901] Wk 2413 IGLOS Final Orbits

acc acc at igs.org
Fri Apr 24 00:28:07 UTC 2026


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2413   (Apr 05, 2026 - Apr 11, 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 2.2413.
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:
                                                                               
 igl2413[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2413 in the SP3 format.
 igl24137.sum      Combination Report for GPS Week 2413.


    
    
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  |      4.3 ns
                1  |      6.8 ns
                2  |      5.4 ns
                3  |      7.9 ns
                4  |      3.0 ns
                5  |      3.4 ns
                6  |      5.7 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
                1  |  ESA   | R06
                2  |  ESA   | R06
                3  |  ESA   | R06
                3  |  GRG   | R12
                4  |  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 1.2413, 1a.2413).
        
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 2.2413.0-6)                                                                                
    
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 3.2413.0-6). 
        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 2413 summary.                      (Apr 05, 2026 - Apr 11, 2026)

Table 1.2413.a     GPS week : 2413   MJD: 61135.0-61141.0

         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    14     3     2   .09   14   14 |    2286    -444   3444   9681
        |    0     1     1    13     7    16   .04           |    1265    3136
esa  n/a|   -2    -1     9    -5    -6    23   .00   30   29 |    3861    -850   3485  10151
        |    2     2     3    21    17    23   .04           |    1591    2989
gfz  n/a|    0     0     0    35     5     0  -.15   15   14 |       0    -768   3441   9405
        |    1     1     2    20    16    29   .06           |       0    3108
grg  n/a|    1     0     2   -47    -8   -32   .27   23   14 |    5386    -673   3581   9270
        |    1     0     1    16     7    28   .06           |     670    3032
iac  n/a|    1     0    -5     4     2   -24  -.06   18   18 |    6650    -796   3441  10033
        |    1     1     3    25    20    54   .05           |    1344    1785
jgx  n/a|    0     0    -5     4     1    24  -.12   14   14 |    5655    -874   3639   9826
        |    0     0     1     9    15    22   .03           |    1501    3227


Table 1.2413.b     GPS week : 2413   MJD: 61135.0-61141.0   

         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    8    6    5    6    6    5 |
 R03  |    7    7    6    5    8    6    6 |
 R04  |    8    6    8    6    7    6    6 |
 R05  |    7    6    5    7    6    6    5 |
 R06  |   32   34   34   34   23   26   34 |
 R07  |    6    7    6    7    6    6    5 |
 R08  |   11   11   12   11   10    9   11 |
 R09  |    6    8    6    7    7    7    6 |
 R11  |    9    9    7    6    6    7    7 |
 R12  |    7    6    7   24    9    7    6 |
 R14  |    8    7    7    7    7    6    6 |
 R15  |    8    7    8    7    9    6    6 |
 R16  |    7    9    9    8    8    8    8 |
 R17  |    7    7    6    7   10    9    6 |
 R18  |    7    7    7    8    8    8    6 |
 R19  |    7    6    7    6    7    7    6 |
 R20  |    6    6    6    7    6    5    7 |
 R21  |   11    9   10    9    9    7    9 |
 R22  |    9    6    5    6    7    7    7 |
 R24  |    7    6    8    6    7    8    5 |
 R26  |   23   31   26   32   28   28   26 |


Table 1.2413.c     GPS week : 2413   MJD: 61135.0-61141.0   

         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 2413 0   | -185   -18    55    -623   -3780    9403  77.3  3720  3720 |    4275       0
brd 2413 1   |   48   -98    75    2656    -891   10020  79.2  1821  1821 |    6766       0
brd 2413 2   |   89   -55   140    1426      91   14830  78.2  1612  1612 |    5377       0
brd 2413 3   |   48    36    88     287    1018   15250  77.4  2025  2025 |    7884       0
brd 2413 4   |  -67    48   -18       4     941   13650  79.3  2591  2591 |    3041       0
brd 2413 5   |  -11    45   -21   -1098    1621   11790  79.8  2383  2383 |    3392       0
brd 2413 6   |  113   -31   150    3504    2817    7508  81.7  2050  2050 |    5728       0
-------------+------------------------------------------------------------+----------------
brd 2413 mean|    5   -10    67     879     259   11778  79.0  2314  2314 |    5209       0
brd 2413 sdev|  103    56    68    1714    2125    2939   1.5   700   700 |    1767       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 2.2413.0  GPS week: 2413   Day: 0   MJD: 61135                            

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     7    13     0    23   .07   13   14 |    1533   -1895   3727  10472
esa  n/a|   -2    -1    12    10   -16   -18  -.06   35   35 |    4234   -2383   3765  10689
gfz  n/a|    0     0    -1    36   -11    12  -.24   14   11 |       0   -2475   3716  10218
grg  n/a|    1     0     3   -32     0   -78   .32   14   13 |    5056   -1659   3913  10211
iac  n/a|    3     0   -10    38    29    72   .01   23   24 |    7275   -2750   3711  10854
jgx  n/a|    0     0    -6    -3   -21    25  -.10   14   14 |    4616   -2591   3926  10932

Table 2.2413.1  GPS week: 2413   Day: 1   MJD: 61136                            

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     1    14     3     9   .04   13   12 |    2709    1507   3084   9193
esa  n/a|   -3    -2    10    19   -16    19  -.00   33   33 |    6403   -1011   3139   9153
gfz  n/a|    1     1     0    64   -18    20  -.18   16   16 |       0    1087   3079   9074
grg  n/a|    2     0     1   -36     0    -7   .22   14   12 |    6141     828   3249   9171
iac  n/a|    0    -1    -6   -24   -15   -74  -.05   19   18 |    8406    -645   3088   9754
jgx  n/a|   -1     1    -5    -6     0    43  -.10   13   13 |    5425    1411   3281   9688

Table 2.2413.2  GPS week: 2413   Day: 2   MJD: 61137                            

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    29     9   -27   .10   14   14 |    1795    -938   3376   8605
esa  n/a|   -2    -5    13    -7    17    18   .07   34   32 |    4008   -2210   3395   8844
gfz  n/a|    1     0     0    25     4   -48  -.20   16   16 |       0   -1031   3376   8184
grg  n/a|    0     1     3   -68   -14    -3   .33   15   12 |    5568    -958   3524   7678
iac  n/a|    0    -2    -2     8     4     7  -.04   14   14 |    6167   -1043   3370   8851
jgx  n/a|    0     0    -5     9    10    33  -.12   13   13 |    5542   -1050   3642   8150

Table 2.2413.3  GPS week: 2413   Day: 3   MJD: 61138                            

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    21     9     0   .11   14   11 |    3729    4328   3784  10227
esa  n/a|    2    -2     9   -33    19    19   .01   38   34 |    4658    3368   3819  11418
gfz  n/a|    0     1     0     8     7   -17  -.16   13   14 |       0    4075   3787   9944
grg  n/a|   -1     1     3   -49   -19   -17   .18   69   14 |    5735    3668   3889   9488
iac  n/a|    0     0    -4    -3    10   -15  -.04   17   16 |    8160    1295   3788  10553
jgx  n/a|    0    -1    -6    -5    -3    20  -.11   26   26 |    7314    3938   3967  10136

Table 2.2413.4  GPS week: 2413   Day: 4   MJD: 61139                            

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   -14   -11     5   .14   15   16 |    3962   -1795   3210  10771
esa  n/a|   -1     2     9    16   -17    57  -.03   32   33 |    3989   -1425   3241  11704
gfz  n/a|    0    -1     4    56    21    -7  -.14   12   10 |       0   -2569   3203  10466
grg  n/a|    2     0     3   -72   -12   -51   .32   18   15 |    4355   -2968   3346  10379
iac  n/a|    3     0    -5   -10     0   -78  -.11   19   20 |    5797   -1413   3208  11002
jgx  n/a|   -1     0    -5    14    12    54  -.10   11   11 |    8004   -3156   3414  11087

Table 2.2413.5  GPS week: 2413   Day: 5   MJD: 61140                            

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     4    21    10    13   .14   13   13 |    1880   -5504   3807   8883
esa  n/a|   -3    -3     5   -21   -12    31  -.02   17   16 |    1919   -5090   3874   9299
gfz  n/a|    1     0     2    17     4    -3  -.08   17   18 |       0   -5440   3807   8680
grg  n/a|    1     0     2   -40    -7   -53   .28   17   17 |    6057   -5360   3977   8858
iac  n/a|    1    -1    -8    37    16   -19  -.07   16   15 |    4714   -2780   3811   9311
jgx  n/a|    0     0    -4     5   -10     0  -.15   11   11 |    4926   -5626   3998   9281

Table 2.2413.6  GPS week: 2413   Day: 6   MJD: 61141                            

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     4    14     2    -9   .05   14   16 |     398    1188   3122   9620
esa  n/a|   -4    -1     3   -22   -21    37   .04   20   17 |    1822    2795   3162   9951
gfz  n/a|    3     0    -1    42    27    42  -.06   16   14 |       0     971   3119   9272
grg  n/a|    0    -1     0   -35    -3   -15   .27   13   12 |    4791    1733   3175   9108
iac  n/a|    0     2    -1   -15   -32   -65  -.16   17   16 |    6032    1761   3113   9908
jgx  n/a|    0     0    -2    17    24   -10  -.18   11   11 |    3761     954   3247   9509

       
       
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 3.2413.0  GPS week: 2413   Day: 0   MJD: 61135                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  738    8   19   10   12   31    7    6 |    61   61   63   63   68   62    62
 R03  | 1396   12   21   10    9   33   17    7 |    64   77   73   74   83   62    69
 R04  |  826    9   25   15    9   18   25    7 |    66   76   66   65   63   55    62
 R05  | 2999   13   29   10   14   31    9    7 |    57   63   53   59   49   51    53
XR06  |  967   26  614   21  ---   91  ---   31 |    24  128   38  ---   93  ---    41
 R07  | 2483   10   33    9   11   14    8    5 |    61   68   63   65   58   62    62
 R08  | 5242   23   74   14   15   13   13   10 |    44   99   55   59   50   53    53
 R09E | 1187   12   30    9   11   15   14    6 |    57   64   54   53   56   57    55
 R11E | 2407   14   36   17   24   15   11    8 |    41   66   42   63   42   50    47
 R12E | 1493    9   25   16   15   10   12    6 |   772  769  773  778  773  764   773
 R14E | 3188   11   19   18   22   17   11    7 |    43   50   45   62   42   45    46
XR15E | 2088   13   24   14   17   14  ---    7 |    54   62   58   64   58  ---    57
 R16E |11953   13   35   11   18   14   13    7 |   140  150  141  146  136  141   141
XR17  | 1412    8   28    9   15   12  ---    6 |    43   38   41   48   42  ---    42
 R18  |  774   18   16   10   16   17   15    7 |    40   43   42   47   42   34    40
XR19  | 1060   11   18   17  ---   18    9    7 |    19   26   33  ---   32   27    24
 R20  | 1512    7   35    9    8   27    8    6 |    26   32   27   29   47   27    27
 R21  | 1063    9   60    8   14   39   23   10 |    51   37   49   53   59   44    47
 R22  | 1452   21   29   25   11   24    7    8 |    23   30   50   34   46   32    31
 R24  | 2647    9   24   18   11   20    9    6 |    49   42   53   45   54   46    47
XR26  | 7801   25   72   28  ---   59  ---   23 |    35   60   55  ---   80  ---    49
------+-----------------------------------------+-------------------------------------
 RMS  | 3720   13   35   14   14   23   14      |T   84   97   89  100   93   94    87
 WRMS | 3720   14   35   11   13   24   14      |NE  44   58   50   53   57   46    47
 MEDI | 1493   12   29   14   14   18   11      |MD  49   62   53   59   56   51    49

Table 3.2413.1  GPS week: 2413   Day: 1   MJD: 61136                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  591   12   17   26   10   31   14    8 |    45   45   64   51   62   49    51
 R03  | 1873   10   26   16   10   22   15    7 |    45   50   59   53   61   43    50
 R04  | 1178   11   23   10   14   11   14    6 |    47   56   49   51   43   42    46
 R05  | 2439   12   24   13    7   14   10    5 |    42   48   42   40   29   33    37
XR06  | 1062   30  605   26  ---   82  ---   33 |    31  133   29  ---   57  ---    30
 R07  | 1740   12   39   18   12   16   10    7 |    37   56   40   45   32   37    38
 R08  | 2706   25   62   15   13   16   18   10 |    31   54   33   34   21   33    29
 R09E | 2410   11   51   15   10   12   10    7 |    23   62   30   29   31   31    28
 R11E | 1736   13   20   17   28   18   13    8 |    16   33   23   39   19   20    19
 R12E | 1542   10   25   15   10   19   13    6 |   649  655  652  646  648  644   650
 R14E | 2398   11   22   12   18   15   11    6 |    26   35   28   38   27   26    27
XR15E | 1394    8   20    9   18   17  ---    7 |    36   37   41   49   45  ---    41
 R16E | 2219   19   26   23   20   18   14    8 |    79   89   87   91   80   77    82
XR17  | 1153   10   18   20   12   13  ---    7 |    23   27   21   25   16  ---    19
 R18  |  944   13   23   10   15   16   14    6 |    29   38   32   33   22   25    27
XR19  |  857   11   12   13  ---   12    9    5 |    15   20   17  ---   19   17    13
 R20  | 1480    9   32   14    8   15    8    5 |    17   25   32   25   29   22    21
 R21  | 1476   10   53   13   11   27   18    9 |    25   19   27   26   22   20    20
 R22  |  922    7   23   15   10   16   10    5 |    20   31   20   28   23   21    19
 R24  | 1873    6   19   16   11   23   12    6 |    26   24   30   25   29   26    24
XR26  | 9435   27  ---   26  ---   74  ---   30 |    35  ---   40  ---   49  ---    33
------+-----------------------------------------+-------------------------------------
 RMS  | 1821   13   33   16   14   19   13      |T   61   76   66   73   64   68    62
 WRMS | 1821   12   33   16   12   18   13      |NE  31   44   35   36   34   30    30
 MEDI | 1542   11   23   15   11   16   13      |MD  31   38   32   38   29   31    29

Table 3.2413.2  GPS week: 2413   Day: 2   MJD: 61137                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  526   14   25   11   10   14    8    5 |    55   62   49   56   50   51    52
 R03  | 2037   11   20   15   12   12    8    5 |    47   58   55   52   57   54    52
 R04  | 1291   14   28   22   21   11   16    8 |    48   60   61   51   53   43    49
 R05  | 1624    8   24   14   11   12    8    5 |    46   55   52   50   55   47    49
XR06  | 1125   40  595   34  ---   62  ---   34 |    31  147   30  ---   67  ---    40
 R07  | 1461   10   24   16   14    9    8    5 |    43   45   38   38   36   33    36
 R08  | 1241   27   65   25   22   12   26   12 |    36   70   32   48   43   51    41
 R09E | 2156   11   24   15   18   11    9    6 |    21   26   17   31   27   25    21
 R11E | 1737   14   33   13   16    8    9    6 |    23   35   25   27   24   27    23
 R12E | 1688    9   32   16   16   12   10    6 |   631  630  639  634  634  627   632
 R14E | 2052   17   32   12   16   16   12    7 |    26   45   38   43   34   29    31
XR15E | 1745    9   28   17   18   10  ---    7 |    34   34   32   31   33  ---    30
 R16E | 2167   14   30   17   25   15   16    8 |    49   45   47   50   49   40    43
XR17  |  997    6   27   12    9   10  ---    5 |    31   29   36   34   28  ---    30
 R18  | 1227   17   17   15    9   21    7    6 |    26   27   31   30   30   28    26
XR19  | 1203   11   29   14  ---   13   12    7 |    16   33   18  ---   20   26    19
 R20  | 1368   12   29   13   15   10   10    6 |    21   36   27   25   25   28    24
 R21  | 1891   11   67   20   12   17   19   10 |    35   34   38   35   31   24    29
 R22  | 1108   11   30    9    8   10    5    5 |    16   30   21   27   22   23    20
 R24  | 1245   12   28   21   10   20   15    7 |    36   42   41   39   52   39    40
XR26  | 5601   39   53   31  ---   56  ---   26 |    27   56   33  ---   57  ---    40
------+-----------------------------------------+-------------------------------------
 RMS  | 1612   14   34   16   15   14   13      |T   61   76   64   72   67   70    63
 WRMS | 1612   14   32   16   12   14   13      |NE  34   52   37   40   41   37    36
 MEDI | 1461   12   29   15   14   12   10      |MD  34   45   36   38   36   33    36

Table 3.2413.3  GPS week: 2413   Day: 3   MJD: 61138                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  625    7   17   10    5   11   12    4 |    37   45   40   38   30   41    36
 R03  | 1314    7   34    7   10   10    8    5 |    53   70   53   60   49   54    54
 R04  |  823   10   29   11   15   10   10    5 |    47   63   50   42   50   43    47
 R05  | 2939   11   49   13   14    9   11    6 |    50   82   47   47   49   44    48
XR06  | 1128   32  597   33  ---   73  ---   33 |    26  146   49  ---   64  ---    38
 R07  | 2075   11   39    8   14   16   14    6 |    58   57   52   62   61   46    54
 R08  | 1028   21   42   14   14   33   29   11 |    40   65   51   49   60   33    43
 R09E | 2067   12   30   14   19   16   12    7 |    22   28   19   27   27   23    19
 R11E | 2781    9   25   14   12   11   10    5 |    19   32   21   23   25   22    19
 R12E | 4029   30   43   21  271   32   86   23 |  9999 9999 9999 9999 9999 9999  9999
 R14E | 1803   16   28   13   20    8   11    6 |    32   43   33   43   31   28    30
XR15E | 1727    9   21   13   22    9  ---    7 |    32   32   35   39   35  ---    32
 R16E | 2378   11   32   15   26   21   10    8 |    38   46   43   53   35   36    38
XR17  | 1371    8   27   11   14   16  ---    6 |    30   29   22   29   31  ---    26
 R18  | 1220   13   23    9   14   24   19    7 |    27   33   31   28   33   19    26
XR19  | 1165   10   24    8  ---   15   12    6 |     9   18   14  ---   23   22    13
 R20  | 2104    9   43   14   15   10   12    6 |    12   44   17   18   20   19    13
 R21  | 1975    9   72   20   17    9   14    9 |    31   34   48   46   33   33    36
 R22  | 1079   10   27   14   11   11   15    6 |    12   24   17   25   20   23    15
 R24  |  815   11   34    8    9   13   16    6 |    31   44   28   30   29   27    27
XR26  | 4681   38   72   38  ---   81  ---   32 |    19   73   31  ---   74  ---    34
------+-----------------------------------------+-------------------------------------
 RMS  | 2025   14   38   13   69   17   26      |T   31   50   35   38   38   32    32
 WRMS | 2025   11   34   14   14   16   26      |NE  32   55   36   39   41   33    34
 MEDI | 1727   11   32   13   14   13   12      |MD  31   44   33   39   33   28    32

Table 3.2413.4  GPS week: 2413   Day: 4   MJD: 61139                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  735   11   33   15   11    9    9    6 |    55   61   66   64   53   58    58
 R03  | 2842   11   26    9   25   24   11    7 |    52   59   56   69   41   48    52
 R04  |  864   18   30    6   20   18   10    7 |    56   68   49   49   44   44    48
 R05  | 3730   15   19   10    9   14   12    5 |    52   50   50   47   46   40    45
XR06  | 1060   30  592   15  ---   53  ---   23 |    25  218   37  ---   44  ---    31
 R07  | 2932    9   31   13   11   17   12    6 |    58   70   67   59   67   54    60
 R08  | 1800   34   44   12   19   16   12    9 |    43   71   56   58   59   54    53
 R09E | 1307   14   20   11   17   25    9    6 |    37   36   40   37   39   35    35
 R11E | 1931   12   21    8   14   13   12    5 |    34   36   35   31   34   36    33
 R12E | 4581   13   28   16   25   32   10    8 |   693  688  688  705  688  687   689
 R14E | 4462   14   23   13   24   16    7    7 |    35   43   39   46   32   35    35
XR15E | 2796   10   31   13   19   19  ---    8 |    41   49   42   47   39  ---    40
 R16E | 2417   17   27   14   25   16   12    7 |    79   80   81   76   75   70    75
XR17  | 2210   16   24   20   15   24  ---    9 |    29   25   35   25   31  ---    25
 R18  | 1113   15   28   11   16   27   15    7 |    27   32   26   26   33   28    25
XR19  | 1101    8   28   13  ---   19    9    7 |    18   23   23  ---   27   23    21
 R20  | 3663    9   34   11   11   18   11    6 |    24   39   29   24   33   37    28
 R21  | 1802    8   67   10   12   23    7    8 |    30   32   31   37   35   32    30
 R22  | 1106   11   32   16   16    8    9    6 |    21   35   26   28   24   26    22
 R24  |  982   14   19    8   11   20   16    6 |    31   32   30   33   32   29    28
XR26  | 5943   28   52   34  ---   83  ---   28 |    32   48   27  ---   70  ---    34
------+-----------------------------------------+-------------------------------------
 RMS  | 2590   15   32   12   18   19   11      |T   70   85   73   81   73   78    69
 WRMS | 2590   16   33   10   15   20   11      |NE  36   57   40   43   42   39    37
 MEDI | 1931   14   28   13   16   19   11      |MD  35   48   39   46   39   37    35

Table 3.2413.5  GPS week: 2413   Day: 5   MJD: 61140                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  949    9   13   18   10   12   10    5 |    59   53   55   60   55   54    54
 R03  | 3133   12    8    8   12   22    5    5 |    36   32   35   36   34   32    32
 R04  |  657   13    6   17   14   15    8    5 |    48   44   34   52   41   41    42
 R05  | 2763   14   16    7    7   14   13    5 |    41   48   40   44   42   44    42
XR06  | 1079   33  ---   19  ---   51  ---   26 |    21  ---   37  ---   40  ---    28
 R07  | 2165    7   22   18   12   15    8    6 |    40   38   49   33   43   36    37
 R08  | 2430   25   29   17   10   21    9    8 |    28   38   43   32   21   38    32
 R09E | 2279   12   17   18   25   17    8    7 |    23   35   21   30   34   24    23
 R11E | 1786   15   10   18   20   12   11    6 |    18   20   25   25   23   20    18
 R12E | 5175   14   16   14   20   15    9    6 |   680  674  680  653  673  665   674
 R14E | 3153   11   16   13   16   10    8    5 |    29   33   29   32   26   26    26
 R15E | 2187    8   15   19   18   17    9    6 |    32   33   39   40   35   23    31
 R16E | 1343   15   17   15   28   20   12    8 |    79   85   85   86   83   83    82
XR17  | 1503    9   18   25   18   14  ---    8 |    26   21   42   21   26  ---    24
 R18  | 1201   17   23   18   10   15   19    8 |    23   24   18   25   23   21    19
XR19  |  970    7   16   19  ---   15   11    6 |    16   23   13  ---   21   21    15
 R20  | 2626   13   15   13    7    8   11    5 |    19   24   19   21   21   19    17
 R21  | 2155    6   21   15   10   25    9    6 |    26   43   31   34   24   24    25
 R22  | 1064   12    8   21   25   15    8    7 |    17   23   26   24   19   17    16
 R24  | 1160    6   23   31   17    9   19    8 |    31   22   34   31   32   39    29
XR26  | 5468   40   45   42  ---   63  ---   27 |    33   55   34  ---   49  ---    40
------+-----------------------------------------+-------------------------------------
 RMS  | 2383   13   17   17   17   16   11      |T   63   68   66   71   65   68    62
 WRMS | 2383   13   16   18   17   15   11      |NE  30   34   34   34   32   32    30
 MEDI | 2155   12   16   18   14   15    9      |MD  29   33   34   32   34   26    29

Table 3.2413.6  GPS week: 2413   Day: 6   MJD: 61141                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R02  |  750    9   11    9   10   17   10    5 |    77   76   74   78   77   70    74
 R03  | 1715   11   13   15   11   19    6    5 |    68   70   69   74   64   62    66
 R04  | 1260   21   12   15    6   18    6    6 |    69   77   62   68   64   58    64
 R05  | 1085   13   17   12    8   11    8    5 |    66   71   62   65   65   60    63
XR06  | 1108   33  ---   30  ---   74  ---   34 |    32  ---   36  ---   88  ---    45
 R07  | 1135    8   27    9    8   11    7    5 |    74   71   72   72   76   70    72
 R08  | 2591   36   37   18   18   22   14   11 |    61   93   74   64   58   71    66
 R09E | 2917    8   14   14   11   22   11    6 |    30   35   32   35   32   30    30
 R11E | 2458    9   13   16   21   15   14    7 |    22   25   30   27   28   22    22
 R12E | 3045    8   17   18   17   13    7    6 |   781  783  792  769  785  773   781
 R14E | 1982    9   18   12   15   15    6    5 |    29   35   32   35   26   25    27
 R15E | 1652    8   15   17   14   14   11    5 |    45   41   50   47   42   20    42
 R16E | 1953   17   29   17   16   15    9    7 |   108  120  116  122  112  108   113
XR17  | 1184    7   19   16   11    8  ---    6 |    39   28   44   39   38  ---    37
 R18  | 1445   14   21   10   12   14    9    6 |    30   36   31   31   36   28    30
XR19  | 1195    8   18   12  ---   13   10    6 |    14   19   15  ---   22   21    16
 R20  | 1951   12   21   15   13   12   15    6 |    27   22   26   28   29   30    25
 R21  | 3379    9   27   28   10   23   20    9 |    42   40   54   49   48   34    41
 R22  | 1688    7   13   25   15   19   11    7 |    12   22   26   25   23   17    15
 R24  | 1637   11   17   13    8   15    9    5 |    47   40   40   44   47   48    43
XR26  | 7911   35   50   40  ---   57  ---   26 |    32   72   45  ---   83  ---    47
------+-----------------------------------------+-------------------------------------
 RMS  | 2049   14   20   16   13   17   11      |T   81   88   84   92   87   85    81
 WRMS | 2049   16   17   14   12   16   11      |NE  46   52   48   53   54   47    46
 MEDI | 1688    9   17   15   11   15    9      |MD  42   40   45   47   48   34    43



More information about the IGSREPORT mailing list