[IGSREPORT-30663] Wk 2388 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 31 01:00:41 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2388 (Oct 12, 2025 - Oct 18, 2025)
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 2.2388.
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:
igl2388[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2388 in the SP3 format.
igl23887.sum Combination Report for GPS Week 2388.
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.
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
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 | 3.7 ns
1 | 4.9 ns
2 | 3.4 ns
3 | 6.0 ns
4 | 4.4 ns
5 | 4.1 ns
6 | 4.7 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 | R20
1 | ESA | R20
3 | GFZ | R26
5 | ALL | R26
5 | ESA | R20
6 | ALL | R26
6 | GFZ | R20
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 1.2388, 1a.2388).
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 2.2388.0-6)
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 3.2388.0-6).
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 2388 summary. (Oct 12, 2025 - Oct 18, 2025)
Table 1.2388.a GPS week : 2388 MJD: 60960.0-60966.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 0 0 5 12 .17 14 13 | -567 -812 3484 8766
| 1 0 2 8 6 14 .04 | 453 2077
esa n/a| -2 -2 1 13 -4 49 -.07 25 30 | 841 -578 3481 8491
| 1 1 2 18 19 31 .06 | 873 1820
gfz n/a| 0 0 -1 28 -6 -12 .01 16 15 | 0 -652 3470 7959
| 1 1 2 14 14 24 .06 | 0 2028
grg n/a| 0 0 -1 -28 -7 7 .24 17 14 | 4248 -861 3488 8648
| 0 2 0 16 15 31 .03 | 700 1771
iac n/a| 1 1 -6 9 3 -21 -.15 15 15 | 5225 -204 3491 8708
| 0 2 3 22 24 39 .04 | 588 1241
jgx n/a| 0 0 5 -25 -5 -23 -.22 14 14 | 1511 -647 3529 8256
| 0 0 2 18 17 32 .04 | 522 1852
Table 1.2388.b GPS week : 2388 MJD: 60960.0-60966.0
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 | 5 5 6 7 6 6 6 |
R03 | 6 6 7 7 7 7 7 |
R04 | 7 6 5 6 6 8 5 |
R05 | 7 6 6 6 6 8 6 |
R07 | 7 8 6 6 7 7 5 |
R08 | 6 7 7 7 6 7 7 |
R09 | 9 6 11 7 7 7 6 |
R11 | 8 6 6 6 5 7 8 |
R12 | 6 7 6 6 6 5 7 |
R14 | 5 6 8 6 6 6 7 |
R15 | 10 7 7 7 8 6 8 |
R16 | 12 7 10 10 10 8 9 |
R17 | 7 8 6 5 7 6 6 |
R18 | 7 7 6 6 7 7 8 |
R19 | 8 8 8 9 10 9 9 |
R20 | 13 20 22 20 --- 57 15 |
R21 | 8 6 6 7 7 8 6 |
R22 | 7 7 7 9 8 8 9 |
R24 | 6 8 8 11 8 8 9 |
R26 | 32 28 24 23 60 --- --- |
R27 | 24 23 26 22 26 26 29 |
R28 | --- --- --- --- 0 0 52 |
Table 1.2388.c GPS week : 2388 MJD: 60960.0-60966.0
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 2388 0 | 56 61 -114 -440 848 -8196 82.9 2252 2252 | 3664 0
brd 2388 1 | 30 205 -297 -2675 809 -6964 81.9 2228 2228 | 4945 0
brd 2388 2 | -130 19 -177 -3436 -1265 -5563 81.9 2619 2619 | 3410 0
brd 2388 3 | 13 -101 -302 1142 2518 -8296 81.9 2013 2013 | 5973 0
brd 2388 4 | -15 70 -316 -37 1075 -7681 82.4 1683 1683 | 4401 0
brd 2388 5 | -14 171 -182 -4366 3534 -10680 81.5 1920 1920 | 4087 0
brd 2388 6 | -59 79 -186 -536 1393 -13560 78.8 1793 1793 | 4692 0
-------------+------------------------------------------------------------+----------------
brd 2388 mean| -16 72 -225 -1478 1273 -8705 81.6 2072 2072 | 4453 0
brd 2388 sdev| 62 100 78 2021 1502 2641 1.3 319 319 | 861 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 2.2388.0 GPS week: 2388 Day: 0 MJD: 60960
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 3 12 16 19 .17 14 15 | -730 -1755 2830 8051
esa n/a| -2 -2 0 30 -18 46 -.01 34 53 | 467 -2049 2809 7751
gfz n/a| -1 0 0 6 6 8 .00 18 15 | 0 -1791 2888 7466
grg n/a| -1 0 -2 -56 -13 -46 .28 22 16 | 4421 -2509 2870 7837
iac n/a| 1 1 -4 50 -6 -10 -.10 14 16 | 4876 -1593 2811 7848
jgx n/a| 1 0 1 -40 -7 -49 -.21 14 14 | 1970 -2298 2974 7766
Table 2.2388.1 GPS week: 2388 Day: 1 MJD: 60961
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 2 7 8 29 .21 17 13 | -582 652 3596 8123
esa n/a| -1 -1 2 -4 -8 84 -.06 31 41 | 390 860 3612 7915
gfz n/a| 0 0 0 39 2 12 -.10 16 14 | 0 867 3660 7308
grg n/a| 0 -3 0 -32 -17 -12 .23 16 16 | 3888 725 3702 8060
iac n/a| 1 3 -12 13 -22 -75 -.13 18 18 | 5391 223 3592 7732
jgx n/a| 0 0 2 -12 11 -19 -.25 15 15 | 1692 844 3809 7652
Table 2.2388.2 GPS week: 2388 Day: 2 MJD: 60962
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 -10 0 19 .23 17 14 | -421 -3651 4388 8904
esa n/a| -4 -1 5 6 -33 11 -.03 29 32 | 169 -2695 4360 8325
gfz n/a| 1 1 0 47 -28 -2 -.02 15 14 | 0 -3545 4452 8265
grg n/a| 0 -2 -1 -35 14 -1 .23 21 18 | 4649 -3387 4418 8834
iac n/a| 1 3 -7 -13 1 33 -.13 18 18 | 4549 -2096 4382 8640
jgx n/a| 2 0 4 -12 10 -60 -.18 17 17 | 1493 -3395 4590 8658
Table 2.2388.3 GPS week: 2388 Day: 3 MJD: 60963
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 0 3 9 21 .15 12 12 | -418 2102 3382 9325
esa n/a| -1 -3 1 1 21 53 -.06 17 15 | 1560 1669 3359 9066
gfz n/a| -1 0 0 17 -21 -22 .07 18 18 | 0 2486 3415 7974
grg n/a| 0 0 0 -2 -33 40 .26 15 12 | 5054 340 3252 8891
iac n/a| 2 1 -5 8 47 -43 -.17 14 15 | 6041 223 3365 9082
jgx n/a| 0 0 6 -24 -15 -31 -.17 12 12 | 776 1837 3506 8213
Table 2.2388.4 GPS week: 2388 Day: 4 MJD: 60964
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 -7 3 6 .11 14 14 | -221 912 3169 10276
esa n/a| -5 -1 -2 25 5 30 -.02 20 20 | 2178 1146 3155 9804
gfz n/a| 1 -1 -1 26 -6 -58 .08 15 15 | 0 466 3020 8975
grg n/a| 1 1 -1 -21 4 8 .20 15 12 | 2871 1404 3221 10480
iac n/a| 0 0 -3 -7 -14 -14 -.13 15 14 | 4799 1061 3155 10031
jgx n/a| 0 1 6 -22 -4 36 -.21 12 12 | 2295 465 3101 9131
Table 2.2388.5 GPS week: 2388 Day: 5 MJD: 60965
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| -4 0 1 -6 5 -5 .15 13 13 | -117 -2544 3943 9137
esa n/a| -3 -4 3 41 12 96 -.16 25 25 | 1376 -2352 3991 9370
gfz n/a| 1 0 -1 28 -7 -7 .02 15 14 | 0 -1745 3794 8723
grg n/a| 0 1 -1 -21 -8 42 .26 13 11 | 4341 -1667 3804 8756
iac n/a| 2 -1 -4 -8 -4 -57 -.22 13 14 | 4953 -368 3943 9078
jgx n/a| 1 0 7 -6 1 -1 -.27 14 14 | 1267 -524 3527 9008
Table 2.2388.6 GPS week: 2388 Day: 6 MJD: 60966
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 6 -2 -7 .18 13 12 | -1485 -1404 3080 7552
esa n/a| -1 0 2 -4 -10 26 -.14 20 20 | -253 -630 3086 7212
gfz n/a| 2 0 -7 36 11 -20 .02 16 16 | 0 -1305 3061 7006
grg n/a| 0 2 -1 -28 -1 23 .24 14 12 | 4515 -933 3155 7681
iac n/a| 2 -2 -4 26 24 14 -.16 13 13 | 5966 1120 3190 8548
jgx n/a| 0 0 6 -57 -38 -35 -.22 16 16 | 1085 -1461 3200 7369
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 3.2388.0 GPS week: 2388 Day: 0 MJD: 60960
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1492 8 18 14 9 11 9 5 | 44 44 42 37 45 39 40
R03 | 2006 13 15 15 16 8 7 5 | 56 53 58 63 58 52 55
R04 | 2145 6 32 19 17 10 11 7 | 60 62 66 66 59 52 59
R05 | 1302 12 30 11 16 12 12 7 | 53 56 54 47 46 39 46
R07 | 2020 12 30 8 12 17 14 7 | 62 53 53 55 60 48 54
R08 | 1310 10 25 16 12 12 4 6 | 53 57 61 58 59 53 55
R09E | 1514 17 32 14 30 13 12 8 | 32 47 40 38 35 37 35
R11E | 2212 16 20 14 23 18 15 7 | 42 36 40 39 47 44 41
R12E | 1109 12 23 18 8 8 11 6 | 115 111 116 118 113 108 113
R14E | 1192 7 12 8 14 14 10 5 | 75 77 79 79 81 74 76
R15E | 1088 15 17 29 38 21 15 10 | 75 76 73 89 66 66 70
R16E | 1403 15 14 25 52 24 19 11 | 77 81 71 99 80 80 77
R17 | 1533 7 28 13 18 12 13 6 | 64 55 68 70 67 56 63
R18 | 1143 17 17 18 17 15 14 7 | 54 62 62 58 61 52 56
XR19 | 1436 13 11 16 --- 11 --- 7 | 28 31 35 --- 28 --- 28
R20 | 6796 31 108 31 22 15 24 12 | --- --- --- --- --- --- 0
R21 | 1763 17 25 15 11 11 24 8 | 68 61 64 68 61 57 62
XR22 | 1058 13 14 17 14 12 --- 7 | 45 46 59 57 49 --- 49
R24 | 1363 11 17 12 15 13 14 6 | 67 65 58 56 59 58 61
XR26 |10949 32 84 58 --- 52 --- 31 | 361 20 187 --- 354 --- 354
XR27 | 8279 34 46 --- 42 46 --- 24 | 90 129 --- 100 121 --- 105
------+-----------------------------------------+-------------------------------------
RMS | 2251 14 34 18 22 14 14 |T 76 61 67 66 77 57 74
WRMS | 2251 15 53 15 16 16 14 |NE 78 56 66 61 80 50 77
MEDI | 1492 13 23 15 16 13 13 |MD 60 56 61 58 59 52 56
Table 3.2388.1 GPS week: 2388 Day: 1 MJD: 60961
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1607 10 18 9 6 12 7 4 | 31 35 28 31 30 27 28
R03 | 2543 6 18 16 19 13 8 6 | 33 35 32 36 36 35 32
R04 | 1716 6 16 14 15 12 11 5 | 35 36 36 39 36 32 34
R05 | 1755 5 22 14 11 14 12 5 | 35 32 38 38 34 32 34
R07 | 1530 12 23 14 22 23 9 7 | 38 39 40 33 45 33 35
R08 | 1642 9 23 10 20 11 12 6 | 33 30 30 28 32 34 29
R09E | 2189 13 9 17 9 15 12 6 | 33 25 33 25 28 32 28
R11E | 2098 12 15 14 11 18 8 5 | 45 46 50 52 47 43 46
R12E | 2186 13 14 14 15 30 8 7 | 98 95 95 88 87 91 92
R14E | 1577 10 14 11 15 20 10 6 | 66 70 66 71 69 65 67
R15E | 1311 11 19 10 18 14 14 6 | 56 57 57 58 55 57 55
R16E | 1367 12 15 15 15 28 11 7 | 76 81 79 80 73 75 76
R17 | 1232 7 28 13 16 15 20 7 | 40 37 46 46 47 33 40
R18 | 1209 17 18 12 11 22 14 7 | 35 34 43 39 43 37 37
XR19 | 1940 13 13 14 --- 15 --- 8 | 26 23 24 --- 30 --- 23
R20 | 6220 53 105 41 26 20 36 19 | --- --- --- --- --- --- 0
R21 | 1180 11 21 13 14 11 9 5 | 47 46 49 52 40 46 45
XR22 | 892 15 12 14 9 16 --- 7 | 58 62 74 63 63 --- 62
R24 | 1067 16 25 14 16 16 19 8 | 35 36 39 40 37 33 36
XR26 | 8468 33 75 40 --- 55 --- 28 | 313 23 233 --- 289 --- 298
XR27 | 8494 35 45 --- 25 56 --- 23 | 74 94 --- 80 103 --- 82
------+-----------------------------------------+-------------------------------------
RMS | 2228 17 31 16 16 18 15 |T 60 46 57 49 61 44 58
WRMS | 2228 13 41 14 16 18 15 |NE 59 40 54 43 61 34 58
MEDI | 1642 12 18 14 15 16 11 |MD 38 36 43 40 43 34 37
Table 3.2388.2 GPS week: 2388 Day: 2 MJD: 60962
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2310 8 15 16 14 8 12 5 | 31 30 33 19 27 18 24
R03 | 1742 11 18 10 21 17 13 6 | 43 36 32 43 36 33 34
R04 | 1566 8 11 6 7 17 13 5 | 40 41 34 38 38 27 34
R05 | 2499 10 15 11 10 17 12 5 | 29 22 27 30 23 21 23
R07 | 1346 15 18 9 12 20 11 6 | 48 42 42 44 48 49 44
R08 | 1431 13 31 9 18 12 8 7 | 38 52 40 34 36 38 37
R09E | 2676 24 28 16 37 24 9 10 | 43 54 45 56 36 41 42
R11E | 1312 11 11 13 13 15 6 5 | 25 28 30 27 28 27 26
R12E | 3631 10 20 9 18 13 12 6 | 86 94 84 82 92 75 83
R14E | 2932 14 21 18 19 17 14 7 | 60 71 61 78 63 64 63
R15E | 1232 12 17 8 16 20 15 6 | 61 59 63 70 57 59 60
R16E | 1207 19 17 29 29 16 15 10 | 58 54 67 56 54 50 53
R17 | 1194 7 17 14 14 14 16 6 | 43 44 50 49 53 43 46
R18 | 1612 13 17 13 11 19 11 6 | 34 41 43 38 44 35 38
XR19 | 1662 15 11 12 --- 17 --- 8 | 54 58 54 --- 54 --- 54
R20 | 7398 43 87 33 46 27 53 21 | --- --- --- --- --- --- 0
R21 | 1508 16 22 12 10 14 10 6 | 55 59 43 50 41 42 46
XR22 | 815 15 16 8 14 17 --- 7 | 40 40 35 40 35 --- 37
R24 | 978 18 29 8 12 25 10 7 | 42 61 44 48 27 46 40
XR26 | 7919 27 60 36 --- 47 --- 24 | 295 31 217 --- 297 --- 292
XR27 | 8034 45 58 --- 27 48 --- 26 | 60 96 --- 71 91 --- 75
------+-----------------------------------------+-------------------------------------
RMS | 2618 17 29 15 21 18 17 |T 59 50 54 48 59 41 57
WRMS | 2618 14 32 14 18 18 17 |NE 60 46 53 42 60 35 58
MEDI | 1612 14 18 12 14 17 12 |MD 43 44 43 44 41 41 42
Table 3.2388.3 GPS week: 2388 Day: 3 MJD: 60963
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2322 7 15 24 16 15 15 7 | 26 28 40 20 36 20 25
R03 | 1631 10 18 28 6 19 10 7 | 40 33 55 34 31 28 34
R04 | 1372 7 13 15 12 19 6 5 | 35 27 40 40 36 29 33
R05 | 2231 14 13 13 12 16 12 6 | 27 18 23 24 18 26 19
R07 | 2224 8 17 23 8 8 11 5 | 31 39 24 31 30 23 27
R08 | 1349 12 31 14 13 9 10 7 | 32 45 32 40 37 31 33
R09E | 2621 17 14 19 12 12 11 6 | 35 48 40 49 33 36 37
R11E | 1829 13 10 14 13 13 13 5 | 36 35 47 38 39 36 37
R12E | 3107 9 17 11 15 8 13 5 | 139 131 135 127 137 139 135
R14E | 2943 9 12 12 19 16 10 6 | 60 61 64 66 58 54 59
R15E | 1136 12 14 17 17 14 14 6 | 70 66 67 78 71 60 67
R16E | 1941 15 20 24 28 23 13 9 | 64 72 61 81 60 64 64
R17 | 1182 13 9 11 9 11 14 5 | 59 57 62 59 53 50 56
R18 | 1117 13 19 15 12 11 13 6 | 48 58 50 52 49 45 49
XR19 | 1836 16 16 13 --- 13 --- 8 | 46 47 50 --- 38 --- 44
XR20 | 5939 27 69 32 --- 35 31 20 | --- --- --- --- --- --- 0
R21 | 1706 16 22 9 17 11 12 6 | 66 55 59 67 60 61 60
XR22 | 1240 15 12 22 16 20 --- 8 | 83 90 93 80 85 --- 84
XR24 | 1339 30 11 12 --- 18 26 11 | 69 59 54 --- 46 52 55
XR26 |19000 21 --- 1580 --- 24 --- 22 | 81 --- 730 --- 116 --- 91
XR27 | 9309 21 71 --- 9 31 --- 21 | 38 87 --- 43 83 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 2014 12 17 18 15 14 12 |T 54 55 90 54 55 47 53
WRMS | 2014 12 15 18 12 15 12 |NE 48 49 100 44 51 36 47
MEDI | 1836 13 15 15 13 15 13 |MD 46 55 54 49 46 36 49
Table 3.2388.4 GPS week: 2388 Day: 4 MJD: 60964
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1634 9 28 14 12 10 7 6 | 23 40 16 24 19 23 20
R03 | 1790 8 26 13 11 15 14 6 | 32 33 29 31 35 22 28
R04 | 844 16 23 11 12 10 8 6 | 40 32 31 24 31 25 28
R05 | 1984 12 24 10 5 10 15 5 | 26 18 24 23 21 17 19
R07 | 2162 10 17 14 11 14 17 6 | 39 42 40 41 39 41 38
R08 | 789 14 20 13 15 11 11 6 | 30 42 33 29 32 31 30
R09E | 2184 14 16 18 10 19 15 7 | 35 46 43 37 40 42 38
R11E | 1282 14 12 14 11 7 8 5 | 43 45 46 40 44 40 41
R12E | 1743 10 13 14 13 16 11 5 | 97 88 98 95 91 101 94
R14E | 2196 15 18 10 14 14 10 6 | 62 67 65 67 65 57 62
R15E | 1374 13 15 17 23 24 12 8 | 72 70 80 78 68 66 70
R16E | 1757 21 19 16 33 21 11 9 | 70 72 70 77 68 70 68
R17 | 1438 17 10 16 13 15 11 6 | 64 56 60 60 56 55 58
R18 | 996 20 22 19 15 8 14 7 | 49 60 57 50 52 50 52
XR19 | 2469 14 26 11 --- 13 --- 9 | 41 54 44 --- 39 --- 42
R21 | 2085 13 29 17 10 15 10 7 | 69 58 66 60 67 61 63
XR22 | 1823 14 13 14 16 14 --- 7 | 55 50 61 58 48 --- 53
XR24 | 1155 23 15 12 --- 18 10 8 | 63 55 58 --- 54 55 56
XR26 | 9876 60 --- --- --- 58 --- 59 | 289 --- --- --- 282 --- 278
XR27 | 9041 43 68 --- 32 43 --- 26 | 76 127 --- 88 108 --- 94
XR28 |20507 2 --- --- --- --- --- 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1683 14 20 15 15 15 12 |T 63 55 51 51 62 47 61
WRMS | 1683 14 20 15 12 14 12 |NE 64 51 43 44 63 38 61
MEDI | 1790 14 19 14 13 14 11 |MD 49 54 46 50 48 42 52
Table 3.2388.5 GPS week: 2388 Day: 5 MJD: 60965
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 4511 12 26 10 14 10 10 6 | 27 29 26 29 27 24 25
R03 | 1720 13 31 16 11 10 17 7 | 34 48 39 34 35 26 33
R04 | 1044 17 30 10 12 16 17 7 | 43 43 40 32 39 29 35
R05 | 1484 11 39 19 9 11 13 7 | 33 36 38 26 27 26 28
R07 | 1352 11 20 15 8 17 16 6 | 33 32 34 34 28 30 30
R08 | 1853 14 23 12 10 19 11 6 | 31 27 26 37 38 27 29
R09E | 1902 13 21 19 8 16 10 6 | 31 36 36 34 38 36 34
R11E | 1547 16 16 21 11 13 13 6 | 34 37 48 34 44 32 37
R12E | 1912 9 16 11 10 12 13 5 | 116 120 119 120 119 113 117
R14E | 1167 10 15 11 19 9 8 5 | 75 76 78 82 69 76 75
R15E | 1408 11 18 13 17 12 10 6 | 56 58 59 64 59 55 58
R16E | 1964 13 24 23 17 19 12 8 | 58 64 61 65 59 61 59
R17 | 1316 11 11 12 8 14 14 5 | 42 49 39 41 43 36 40
R18 | 1005 10 30 16 11 6 16 6 | 32 40 34 33 31 31 31
XR19 | 1292 14 20 15 --- 14 --- 8 | 33 37 37 --- 37 --- 34
XR20 | 1739 --- 404 62 52 --- --- 57 | --- --- --- --- --- --- 0
R21 | 2478 7 32 14 13 12 22 7 | 38 70 39 44 46 33 41
XR22 | 1692 12 28 16 17 14 --- 8 | 70 83 71 70 70 --- 71
R24 | 1152 22 31 11 21 12 9 8 | 38 52 40 48 30 34 33
XR27 |10785 43 67 --- 23 53 --- 26 | 44 78 --- 53 67 --- 54
XR28 |15865 3 --- --- --- --- --- 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1919 13 25 15 13 13 14 |T 60 53 48 48 62 41 60
WRMS | 1919 13 25 14 11 14 14 |NE 59 48 38 40 61 29 58
MEDI | 1692 12 24 15 12 13 13 |MD 38 48 39 37 39 32 35
Table 3.2388.6 GPS week: 2388 Day: 6 MJD: 60966
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 3389 8 17 14 11 10 22 6 | 31 33 28 27 28 30 27
R03 | 1757 14 24 9 14 9 17 6 | 47 45 40 48 42 36 41
R04 | 1117 7 21 12 9 9 10 5 | 50 51 48 46 45 46 46
R05 | 1523 7 21 13 10 12 13 5 | 44 42 47 37 42 32 39
R07 | 914 5 10 8 10 8 16 4 | 50 47 50 55 47 45 48
R08 | 2443 10 26 19 13 13 13 7 | 41 47 42 44 44 37 40
R09E | 1360 12 19 13 9 15 12 6 | 39 41 48 42 48 46 43
R11E | 1675 14 21 18 11 15 22 7 | 55 55 63 53 62 49 55
R12E | 1802 14 22 16 12 14 17 7 | 121 120 124 118 121 110 118
R14E | 2636 11 12 20 20 12 9 6 | 105 104 102 106 100 97 102
R15E | 1321 15 15 15 25 17 14 7 | 91 93 99 112 94 87 95
R16E | 1849 20 21 20 21 15 21 9 | 85 87 91 96 86 82 86
R17 | 1171 11 17 17 14 9 7 5 | 89 79 86 90 88 79 85
R18 | 649 13 29 20 16 12 16 7 | 75 88 78 77 76 75 76
XR19 | 1216 12 16 16 --- 15 --- 8 | 45 47 48 --- 47 --- 46
XR20 | 2028 14 --- 360 --- 15 --- 14 | --- --- --- --- --- --- 0
R21 | 1918 8 16 11 11 13 21 6 | 89 81 84 82 84 74 82
XR22 | 866 15 15 24 15 18 --- 9 | 74 74 79 68 65 --- 71
R24 | 979 22 26 25 15 15 19 9 | 85 82 81 58 75 73 78
XR27 | 7962 43 70 --- 40 51 --- 28 | 70 123 --- 71 108 --- 87
XR28 |14183 50 --- --- --- 53 --- 52 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1792 13 20 16 14 13 16 |T 84 70 68 68 85 62 83
WRMS | 1792 12 20 16 12 13 16 |NE 84 64 59 58 85 52 83
MEDI | 1675 13 21 16 13 14 16 |MD 70 74 63 58 65 49 71
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