[IGSREPORT-30937] Wk 2416 IGLOS Final Orbits
acc
acc at igs.org
Fri May 15 02:32:34 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2416 (Apr 26, 2026 - May 02, 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 2.2416.
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:
igl2416[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2416 in the SP3 format.
igl24167.sum Combination Report for GPS Week 2416.
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 | 7.2 ns
1 | 6.6 ns
2 | 4.9 ns
3 | 7.7 ns
4 | 6.3 ns
5 | 10.8 ns
6 | 8.8 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
----+--------+---------------
3 | IAC | R06
4 | IAC | 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 1.2416, 1a.2416).
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 2.2416.0-6)
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 3.2416.0-6).
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 2416 summary. (Apr 26, 2026 - May 02, 2026)
Table 1.2416.a GPS week : 2416 MJD: 61156.0-61162.0
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 12 3 -5 .11 13 13 | 1669 -921 3431 9232
| 1 0 1 4 12 13 .02 | 879 1799
esa n/a| -2 -1 1 -5 -25 41 -.04 19 18 | 4240 -1252 3463 9295
| 1 0 2 14 11 45 .04 | 1615 1543
gfz n/a| -1 0 3 3 13 -30 -.21 17 17 | 0 -1095 3434 9369
| 1 1 4 21 20 24 .03 | 0 1863
grg n/a| 2 0 1 -13 -4 -3 .30 15 15 | 7810 -1095 3523 9120
| 1 0 2 15 20 32 .04 | 1460 1714
iac n/a| 1 0 0 8 8 -23 -.09 14 14 | 8973 -880 3431 10006
| 1 0 2 30 26 33 .02 | 1872 902
jgx n/a| 0 1 -8 -2 1 25 -.10 15 15 | 4049 -1136 3479 9335
| 0 1 1 13 15 30 .04 | 1140 1886
Table 1.2416.b GPS week : 2416 MJD: 61156.0-61162.0
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 7 6 6 6 5 |
R03 | 6 7 7 5 6 8 7 |
R04 | 8 7 7 9 7 8 7 |
R05 | 8 7 5 6 6 5 7 |
R06 | 31 37 34 13 15 40 37 |
R07 | 7 7 7 5 5 7 10 |
R08 | 11 12 11 11 11 11 11 |
R09 | 6 7 8 7 7 7 6 |
R11 | 7 7 7 9 6 6 7 |
R12 | 5 7 7 7 8 7 7 |
R14 | 6 6 6 7 7 8 7 |
R15 | 6 9 6 5 6 7 6 |
R16 | 8 8 7 7 8 8 8 |
R17 | 7 7 6 6 6 7 5 |
R18 | 8 6 8 6 6 8 8 |
R19 | 5 6 7 9 9 7 7 |
R20 | 6 5 6 7 7 8 7 |
R21 | 7 7 7 6 7 8 8 |
R22 | 5 5 7 5 6 5 7 |
R24 | 7 5 6 8 7 7 7 |
Table 1.2416.c GPS week : 2416 MJD: 61156.0-61162.0
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 2416 0 | 28 8 170 -991 -291 500 77.8 2162 2162 | 7162 0
brd 2416 1 | 138 23 87 2815 1819 5291 79.0 1969 1969 | 6577 0
brd 2416 2 | 47 5 175 -2176 2454 5539 79.8 1808 1808 | 4890 0
brd 2416 3 | -35 43 115 2111 1410 28 78.5 1673 1673 | 7656 0
brd 2416 4 | -32 90 215 1643 3193 3833 78.8 1843 1843 | 6303 0
brd 2416 5 | -13 50 160 501 1114 -1062 80.2 2062 2062 | 10757 0
brd 2416 6 | 37 -25 132 -251 1852 -2484 80.5 1830 1830 | 8810 0
-------------+------------------------------------------------------------+----------------
brd 2416 mean| 24 28 151 521 1650 1663 79.3 1906 1906 | 7450 0
brd 2416 sdev| 60 37 42 1789 1096 3202 1.0 167 167 | 1894 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 2.2416.0 GPS week: 2416 Day: 0 MJD: 61156
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 16 -5 -11 .08 14 14 | 2596 -267 3066 9562
esa n/a| -1 0 0 -11 -12 37 -.00 19 15 | 4598 -796 3052 10358
gfz n/a| 0 0 3 15 8 -33 -.18 14 14 | 0 -443 3070 9728
grg n/a| 0 0 3 -6 8 45 .30 14 14 | 6966 -111 3076 9532
iac n/a| 0 0 2 2 12 -28 -.08 17 17 | 8898 -1278 3062 10465
jgx n/a| 0 0 -9 2 2 -14 -.10 15 15 | 4830 -118 3050 9714
Table 2.2416.1 GPS week: 2416 Day: 1 MJD: 61157
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 1 0 19 12 -10 .13 14 14 | 2780 -1279 3558 9436
esa n/a| -2 0 3 -22 -9 53 -.06 17 16 | 5056 -1981 3636 9627
gfz n/a| 0 -1 3 30 -4 -48 -.22 22 23 | 0 -1113 3560 9661
grg n/a| 3 0 0 -30 33 -10 .32 15 14 | 7170 -1465 3704 9172
iac n/a| 0 0 0 -10 -38 -26 -.05 13 13 | 8583 -1330 3560 10099
jgx n/a| 0 0 -5 21 16 31 -.15 15 15 | 5533 -1518 3638 9409
Table 2.2416.2 GPS week: 2416 Day: 2 MJD: 61158
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 3 7 19 -9 .14 13 11 | 677 -3928 3512 8582
esa n/a| -4 0 -1 -1 -37 42 -.09 20 19 | 1711 -3799 3581 8049
gfz n/a| -1 1 2 13 29 9 -.17 14 14 | 0 -4272 3510 8643
grg n/a| 2 -1 -1 -9 -23 -32 .33 16 15 | 6867 -4107 3622 8559
iac n/a| 2 0 0 -15 6 -6 -.08 13 13 | 6354 -2512 3510 9407
jgx n/a| 0 0 -9 -4 -12 0 -.04 18 18 | 3205 -4391 3573 8782
Table 2.2416.3 GPS week: 2416 Day: 3 MJD: 61159
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 13 -5 -8 .10 14 14 | 1157 1225 3206 8930
esa n/a| -1 -1 4 22 -41 31 -.05 21 21 | 3233 735 3184 8305
gfz n/a| 0 0 2 -34 25 -22 -.17 13 14 | 0 1151 3202 8994
grg n/a| 1 0 0 4 -6 -3 .34 12 12 | 6911 1079 3316 9087
iac n/a| 1 0 -6 -11 8 -11 -.10 15 15 | 8376 153 3212 9826
jgx n/a| 1 0 -6 -13 -19 19 -.15 13 13 | 2125 1229 3251 9245
Table 2.2416.4 GPS week: 2416 Day: 4 MJD: 61160
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 4 12 16 18 .11 13 13 | 602 -2525 4432 9712
esa n/a| -1 -1 -1 -14 -29 -20 -.05 18 19 | 3487 -2363 4511 9412
gfz n/a| 0 0 4 -13 -8 -31 -.22 16 16 | 0 -2757 4444 9775
grg n/a| 3 1 2 -35 -24 -50 .27 16 16 | 7202 -2365 4631 9705
iac n/a| 2 -1 -1 69 31 13 -.11 15 14 | 7849 -133 4439 10421
jgx n/a| 0 2 -8 -20 -8 25 -.10 14 14 | 3658 -2669 4532 9778
Table 2.2416.5 GPS week: 2416 Day: 5 MJD: 61161
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 10 -4 -22 .10 12 12 | 2032 553 3343 9191
esa n/a| -3 -1 -1 -7 -21 130 -.03 18 20 | 6806 -315 3361 9694
gfz n/a| -3 2 12 8 45 -17 -.21 23 22 | 0 428 3360 9230
grg n/a| 3 0 3 -20 -6 0 .27 17 18 | 10739 -382 3436 9327
iac n/a| 1 0 0 27 -6 -91 -.12 13 14 | 12025 -550 3349 9907
jgx n/a| 0 1 -10 -5 23 79 -.06 17 17 | 4387 -383 3399 8995
Table 2.2416.6 GPS week: 2416 Day: 6 MJD: 61162
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 8 -7 3 .11 13 13 | 1840 -232 2905 9211
esa n/a| -4 -2 3 -4 -25 17 .01 18 18 | 4791 -245 2917 9624
gfz n/a| 0 -1 -3 1 -2 -68 -.26 18 18 | 0 -662 2895 9558
grg n/a| 3 0 3 2 -12 25 .24 15 16 | 8821 -318 2878 8459
iac n/a| -1 0 0 -5 45 -10 -.07 14 12 | 10728 -514 2887 9917
jgx n/a| 1 2 -10 0 6 37 -.06 16 16 | 4606 -103 2916 9425
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 3.2416.0 GPS week: 2416 Day: 0 MJD: 61156
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 991 6 10 11 15 21 18 6 | 76 72 76 86 76 68 75
R03 | 891 8 10 8 16 19 13 5 | 80 70 81 70 75 69 77
R04 | 806 19 16 14 9 24 14 7 | 78 72 61 64 74 52 67
R05 | 2869 19 17 14 12 26 17 8 | 70 64 53 57 69 50 60
XR06 | 996 32 --- 28 --- 66 --- 30 | 113 --- 105 --- 138 --- 113
R07 | 1263 10 32 8 13 18 9 7 | 79 79 79 74 81 73 79
R08 | 2221 30 35 16 21 19 16 10 | 67 103 89 94 93 82 86
R09 | 1309 10 20 14 14 16 9 6 | 29 42 40 29 31 32 31
R11 | 3667 12 17 21 11 13 13 6 | 29 27 38 19 34 20 25
R12 | 917 9 11 10 12 12 15 5 | 75 68 76 75 73 56 70
R14 | 4314 13 11 10 14 13 15 5 | 63 74 76 80 75 60 70
R15 | 1745 10 20 11 11 14 17 6 | 76 77 77 74 80 61 73
R16 | 1788 16 20 16 20 12 15 7 | 72 64 79 64 72 57 66
R17 | 2126 11 16 10 13 18 22 7 | 24 25 26 28 30 26 25
R18 | 1150 12 21 18 14 16 23 8 | 23 31 24 27 34 25 24
XR19 | 2848 10 9 11 --- 9 9 5 | 19 24 23 --- 28 25 23
R20 | 1359 14 12 17 11 10 10 5 | 11 23 34 24 19 20 18
R21 | 2725 14 22 17 14 17 14 7 | 28 27 39 36 32 30 30
R22 | 892 7 9 12 11 17 11 5 | 17 23 21 25 24 23 20
R24 | 3190 12 17 19 11 12 18 7 | 32 30 33 30 31 25 28
------+-----------------------------------------+-------------------------------------
RMS | 2162 14 19 14 14 17 15 |T 53 52 56 53 58 44 53
WRMS | 2162 14 15 14 14 17 15 |NE 53 52 56 53 58 44 53
MEDI | 1359 12 17 14 13 16 15 |MD 63 64 53 57 69 50 60
Table 3.2416.1 GPS week: 2416 Day: 1 MJD: 61157
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1658 9 21 14 18 8 16 6 | 50 43 60 65 50 49 51
R03 | 883 7 17 29 14 9 8 6 | 51 42 59 40 58 52 51
R04 | 857 19 14 18 11 10 12 6 | 54 47 42 43 50 42 45
R05 | 2079 16 17 22 12 12 17 7 | 42 48 24 38 45 37 39
XR06 | 953 51 --- 29 --- 60 --- 36 | 85 --- 80 --- 95 --- 88
R07 | 1383 9 24 12 16 14 8 6 | 53 65 49 54 48 56 55
R08 | 2202 36 19 29 31 20 19 12 | 47 65 70 72 68 62 62
R09 | 1696 9 20 19 23 9 13 7 | 20 31 31 20 25 27 21
R11 | 1222 14 15 19 15 14 12 6 | 25 24 27 21 32 20 21
R12 | 990 9 12 23 14 11 17 6 | 55 46 63 50 55 40 50
R14 | 2896 11 16 24 9 8 10 5 | 43 57 65 54 50 48 50
R15 | 2105 9 12 34 17 16 23 8 | 56 56 68 49 60 37 52
R16 | 1620 12 15 38 13 14 16 8 | 53 51 56 53 53 38 48
R17 | 2435 7 13 14 12 18 18 6 | 18 19 17 23 18 15 16
R18 | 1071 10 21 15 12 9 12 6 | 19 23 30 24 20 20 20
XR19 | 2888 11 11 18 --- 8 14 6 | 14 21 21 --- 20 26 17
R20 | 1859 11 16 13 6 9 9 5 | 8 31 25 18 18 16 14
R21 | 2482 10 16 18 7 20 20 7 | 20 30 27 29 25 19 21
R22 | 896 11 17 12 9 5 14 5 | 18 12 16 24 20 22 16
R24 | 4012 11 14 14 10 11 11 5 | 23 24 26 24 22 18 20
------+-----------------------------------------+-------------------------------------
RMS | 1968 14 17 22 15 13 15 |T 37 38 42 38 41 33 37
WRMS | 1968 14 16 23 14 13 15 |NE 37 38 42 38 41 33 37
MEDI | 1658 11 16 18 12 11 14 |MD 42 42 31 38 45 37 39
Table 3.2416.2 GPS week: 2416 Day: 2 MJD: 61158
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1438 6 22 10 13 18 18 6 | 56 40 55 63 67 43 55
R03 | 908 9 21 9 15 16 16 6 | 59 48 66 64 74 54 63
R04 | 792 18 21 9 8 15 11 6 | 60 53 51 53 47 48 51
R05 | 1656 15 7 12 13 8 9 5 | 50 41 43 45 45 43 44
XR06 | 1007 41 --- 31 --- 62 --- 33 | 37 --- 52 --- 75 --- 54
R07 | 1244 9 23 11 14 13 19 6 | 60 64 61 58 55 47 57
R08 | 814 30 32 16 28 14 27 11 | 51 84 73 71 70 52 64
R09 | 1636 13 20 21 15 18 12 7 | 33 43 42 28 35 39 33
R11 | 1962 12 24 17 15 11 15 7 | 23 26 27 20 23 28 21
R12 | 1075 10 20 15 18 7 19 6 | 64 60 65 58 56 47 58
R14 | 1070 10 13 11 14 17 11 6 | 50 55 52 62 66 48 55
R15 | 1598 12 16 15 15 6 12 5 | 61 52 61 49 51 46 53
R16 | 2210 12 23 19 13 10 12 6 | 62 47 68 66 61 56 60
R17 | 3252 6 19 9 17 4 25 6 | 24 29 23 29 24 23 22
R18 | 1218 13 16 17 15 8 34 8 | 25 31 32 33 21 24 24
XR19 | 2053 10 19 14 --- 15 5 6 | 16 22 21 --- 19 18 16
R20 | 1891 10 21 11 11 11 10 5 | 15 19 12 27 20 22 16
R21 | 2409 9 18 16 21 11 21 7 | 24 23 26 30 23 18 21
R22 | 1099 8 19 19 13 15 9 6 | 18 28 28 28 20 21 20
R24 | 3378 9 11 15 16 13 16 6 | 31 28 25 31 27 27 26
------+-----------------------------------------+-------------------------------------
RMS | 1807 13 20 14 16 13 18 |T 40 41 44 45 43 37 40
WRMS | 1807 11 19 14 15 13 18 |NE 40 41 44 45 43 37 40
MEDI | 1438 10 20 15 15 13 15 |MD 37 41 43 45 45 43 44
Table 3.2416.3 GPS week: 2416 Day: 3 MJD: 61159
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1003 9 15 12 10 16 11 5 | 71 70 78 71 75 67 71
R03 | 733 6 17 12 12 14 10 5 | 61 62 66 48 67 60 62
XR04 | 1244 14 10 25 9 18 --- 8 | 57 51 72 51 40 --- 54
R05 | 1306 17 13 10 7 16 15 6 | 50 42 47 46 33 36 41
XR06 | 1227 12 --- 13 --- 106 --- 12 | 24 --- 37 --- 91 --- 33
R07 | 1122 8 16 9 10 12 11 5 | 62 56 55 56 61 51 58
R08 | 639 29 24 19 24 20 26 10 | 46 76 72 70 68 54 62
R09 | 1185 10 24 13 12 18 16 6 | 39 51 33 45 42 42 40
XR11 | 2765 20 --- 20 16 13 16 8 | 37 --- 41 25 36 25 31
R12 | 867 11 28 11 15 15 12 6 | 64 71 53 59 55 49 56
R14 | 1525 18 10 16 11 20 11 6 | 60 71 86 74 86 64 73
R15 | 1491 12 15 10 11 11 12 5 | 69 62 64 64 61 57 62
R16 | 2780 18 21 16 12 11 11 6 | 68 61 72 67 60 56 64
R17 | 2079 10 29 11 8 17 9 6 | 21 34 25 27 25 18 21
R18 | 1910 16 22 12 10 7 13 6 | 20 25 25 27 23 20 21
XR19 | 1451 14 29 20 --- 16 14 9 | 17 26 30 --- 19 22 18
R20 | 2634 14 31 20 6 11 9 7 | 17 24 31 21 22 21 20
R21 | 1722 12 26 8 12 12 12 6 | 27 18 25 29 26 28 24
R22 | 662 10 19 13 8 14 8 5 | 15 27 13 21 20 20 15
R24 | 2663 16 10 14 17 17 19 7 | 28 25 26 22 32 28 24
------+-----------------------------------------+-------------------------------------
RMS | 1673 14 21 13 12 15 13 |T 42 47 47 45 47 39 42
WRMS | 1673 14 21 14 12 15 13 |NE 42 47 47 45 47 39 42
MEDI | 1306 12 19 13 11 15 12 |MD 39 51 41 46 40 36 40
Table 3.2416.4 GPS week: 2416 Day: 4 MJD: 61160
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1046 14 11 15 17 12 9 6 | 61 52 53 59 64 50 56
R03 | 966 10 19 11 17 8 13 6 | 61 50 64 43 55 52 57
R04 | 2271 12 22 14 13 17 10 6 | 65 45 63 59 60 62 57
R05 | 1501 13 13 11 12 9 17 5 | 51 45 46 43 44 33 43
XR06 | 1004 11 --- 19 --- 118 --- 15 | 52 --- 69 --- 96 --- 62
R07 | 1438 10 17 12 14 8 10 5 | 55 58 53 43 59 53 55
R08 | 686 29 31 15 23 13 27 11 | 48 75 61 70 55 66 59
R09 | 1980 11 20 15 13 22 12 7 | 37 38 33 40 36 42 35
R11 | 1448 11 13 11 11 19 11 6 | 29 34 30 27 39 25 26
R12 | 813 7 18 25 19 16 24 8 | 59 64 81 63 64 43 60
R14 | 2069 8 17 12 22 14 17 7 | 60 68 63 61 65 47 59
R15 | 1293 12 9 20 18 11 12 6 | 68 56 75 56 60 51 60
R16 | 2732 18 22 22 13 10 12 7 | 67 49 76 65 57 54 60
R17 | 2369 6 11 11 14 22 12 6 | 17 20 18 21 19 15 14
R18 | 1555 16 20 15 10 9 9 6 | 17 19 20 21 19 19 17
XR19 | 1145 10 15 13 --- 28 12 8 | 15 20 24 --- 28 23 18
R20 | 3153 7 25 18 13 21 10 7 | 13 18 16 18 23 16 14
R21 | 1487 8 17 21 17 12 15 6 | 24 26 32 30 24 20 22
R22 | 1415 7 17 17 13 16 12 6 | 11 25 15 23 21 17 13
R24 | 2619 14 13 18 15 18 16 7 | 23 18 21 22 23 15 16
------+-----------------------------------------+-------------------------------------
RMS | 1843 13 18 16 16 15 14 |T 41 41 45 42 45 37 40
WRMS | 1843 13 19 16 16 14 14 |NE 41 41 45 42 45 37 40
MEDI | 1448 11 17 15 14 14 12 |MD 48 45 46 43 44 42 43
Table 3.2416.5 GPS week: 2416 Day: 5 MJD: 61161
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1055 10 11 14 10 15 13 5 | 66 58 62 60 70 54 61
R03 | 3904 8 18 19 22 12 22 7 | 57 45 46 71 60 40 53
XR04 | 1537 15 15 15 22 11 --- 8 | 53 48 59 48 58 --- 52
R05 | 966 8 10 17 15 7 10 5 | 47 39 57 42 42 39 43
XR06 | 1008 51 --- 33 --- 68 --- 39 | 81 --- 78 --- 95 --- 84
R07 | 1085 6 20 22 9 15 19 6 | 43 33 62 65 54 40 45
R08 | 767 31 22 30 30 12 18 11 | 35 56 51 66 48 47 45
R09 | 1835 11 16 27 9 20 8 7 | 55 57 61 53 53 54 53
R11 | 1424 15 14 15 10 9 12 5 | 36 45 43 38 36 51 39
R12 | 1596 6 17 22 15 9 20 6 | 53 51 70 65 46 42 52
R14 | 2210 13 30 24 18 12 14 8 | 53 63 43 59 55 43 52
R15 | 1915 12 21 11 16 12 16 6 | 63 65 54 58 59 45 56
R16 | 1378 10 22 23 20 15 21 8 | 60 45 67 54 68 48 56
R17 | 1259 7 12 14 13 21 21 7 | 18 22 21 24 19 24 17
R18 | 1100 12 22 14 26 17 19 8 | 22 24 22 21 24 28 19
XR19 | 1403 12 12 20 --- 15 13 7 | 13 18 19 --- 17 20 14
R20 | 3831 10 19 38 16 10 16 8 | 12 19 26 20 18 20 13
R21 | 1096 9 19 25 22 7 25 8 | 21 24 26 27 18 17 19
R22 | 2218 6 15 22 11 9 7 5 | 15 26 21 23 16 21 16
R24 | 3347 12 12 32 11 7 15 6 | 22 30 40 33 23 23 25
------+-----------------------------------------+-------------------------------------
RMS | 2061 12 18 23 17 13 17 |T 41 40 46 45 43 36 40
WRMS | 2061 12 20 22 18 14 17 |NE 41 40 46 45 43 36 40
MEDI | 1403 10 17 22 15 12 16 |MD 43 45 46 48 46 40 45
Table 3.2416.6 GPS week: 2416 Day: 6 MJD: 61162
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 930 11 10 20 9 8 8 5 | 84 74 85 82 84 72 80
XR03 | 6104 9 11 17 --- 17 17 7 | 83 74 83 --- 87 69 80
R04 | 1245 16 20 12 13 9 22 7 | 77 69 77 63 74 43 68
R05 | 1103 12 10 20 16 9 20 6 | 68 60 71 55 62 44 59
XR06 | 1037 43 --- 35 --- 67 --- 36 | 91 --- 85 --- 131 --- 96
XR07 | 1642 9 27 34 --- 11 18 10 | 74 63 96 --- 82 65 75
R08 | 919 29 23 24 22 18 20 10 | 57 86 88 92 83 70 76
R09 | 1367 8 16 20 8 12 10 5 | 60 65 60 59 57 62 59
R11 | 1236 15 18 16 17 11 18 7 | 36 31 39 35 42 35 34
R12 | 1214 11 15 21 17 13 18 7 | 74 67 73 76 70 57 68
R14 | 1869 8 17 12 14 17 16 6 | 68 76 74 73 82 60 71
R15 | 2520 8 19 14 14 10 16 6 | 87 90 91 83 80 70 82
R16 | 837 15 17 26 25 10 11 8 | 89 76 97 72 79 72 80
R17 | 1310 6 17 15 9 8 10 5 | 25 30 27 24 24 21 23
R18 | 1549 12 25 20 17 15 16 8 | 22 32 29 22 28 25 22
XR19 | 993 7 16 19 --- 13 12 6 | 13 24 25 --- 20 22 17
R20 | 2658 8 20 15 18 16 8 6 | 16 27 19 30 20 21 19
R21 | 2384 10 20 19 13 23 22 8 | 31 25 39 36 30 25 29
R22 | 2032 11 20 16 14 17 13 7 | 15 19 23 24 23 18 15
R24 | 3561 10 19 19 11 9 16 6 | 32 36 41 41 35 35 32
------+-----------------------------------------+-------------------------------------
RMS | 1830 13 18 18 15 14 16 |T 55 53 61 54 59 46 54
WRMS | 1830 13 18 18 16 12 16 |NE 55 53 61 54 59 46 54
MEDI | 1310 10 18 19 14 12 16 |MD 60 63 71 55 62 44 59
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