[IGSREPORT-30378] Wk 2357 IGLOS Final Orbits
acc
acc at igs.org
Fri Mar 28 01:09:22 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2357 (Mar 09, 2025 - Mar 15, 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 2.2357.
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:
igl2357[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2357 in the SP3 format.
igl23577.sum Combination Report for GPS Week 2357.
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 | 2.3 ns
1 | 0.2 ns
2 | -0.2 ns
3 | 2.4 ns
4 | 3.2 ns
5 | 1.5 ns
6 | 4.3 ns
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 1.2357, 1a.2357).
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 2.2357.0-6)
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 3.2357.0-6).
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 2357 summary. (Mar 09, 2025 - Mar 15, 2025)
Table 1.2357.a GPS week : 2357 MJD: 60743.0-60749.0
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 -14 22 .14 21 17 | 15286 -1513 3800 45944
| 1 1 1 16 18 27 .03 | 1475 1632
esa n/a| -2 -1 1 -16 -19 30 -.05 30 25 | 16740 -2842 3819 46556
| 1 0 1 21 25 78 .04 | 2215 3276
gfz n/a| 1 0 -1 25 -2 -40 .04 25 18 | 0 -1436 3321 8085
| 1 0 2 23 19 29 .07 | 0 1571
grg n/a| 2 0 6 -23 6 47 .27 21 18 | 2500 -1537 3312 7637
| 1 1 1 22 18 13 .05 | 2122 1571
iac n/a| 0 0 -6 4 3 -24 -.20 16 15 | 13420 -392 3825 47172
| 0 1 2 22 14 50 .05 | 2395 1066
jgx n/a| 0 0 3 17 21 -19 -.14 23 23 | 6064 -1463 3314 8082
| 0 1 2 15 11 29 .04 | 1674 1541
Table 1.2357.b GPS week : 2357 MJD: 60743.0-60749.0
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
------+------------------------------------+------------------------------------------
R01 | 11 12 12 11 14 14 15 |
R02 | 7 6 7 8 6 9 8 |
R03 | 6 6 6 6 6 6 7 |
R04 | 7 7 8 7 6 8 7 |
R05 | 7 6 8 7 6 7 7 |
R07 | 8 7 7 10 8 6 6 |
R08 | 7 7 7 8 8 7 7 |
R09 | 6 7 7 7 7 6 7 |
R11 | 8 7 8 8 7 7 7 |
R12 | 8 9 9 8 8 8 7 |
R14 | 7 6 6 7 7 7 6 |
R15 | 7 9 8 9 9 7 8 |
R16 | 8 8 8 9 9 9 11 |
R17 | 8 7 8 7 7 7 7 |
R18 | 6 7 8 6 8 8 9 |
R19 | 16 20 23 20 22 19 20 |
R20 | 22 21 19 17 19 23 21 |
R21 | 8 8 8 9 10 10 8 |
R22 | 9 7 9 9 6 8 8 |
R24 | 8 9 10 9 13 11 11 |
R26 | 33 34 32 33 35 34 34 |
Table 1.2357.c GPS week : 2357 MJD: 60743.0-60749.0
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 2357 0 | -106 52 17 -409 -1324 2201 80.9 1387 1387 | 2266 0
brd 2357 1 | 35 -33 17 -1494 -163 4652 79.7 1548 1548 | 246 0
brd 2357 2 | 29 70 -46 -2052 -683 10150 80.1 1565 1565 | -238 0
brd 2357 3 | 68 100 -2 -2129 1033 4757 80.8 1516 1516 | 2397 0
brd 2357 4 | -62 58 45 -2378 151 4794 80.1 1637 1637 | 3213 0
brd 2357 5 | 76 -70 -22 -407 3003 3472 79.9 1722 1722 | 1548 0
brd 2357 6 | 72 -43 37 -539 368 2467 82.2 1576 1576 | 4316 0
-------------+------------------------------------------------------------+----------------
brd 2357 mean| 16 19 6 -1344 340 4641 80.5 1564 1564 | 1964 0
brd 2357 sdev| 72 66 32 876 1395 2659 .9 103 103 | 1599 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 2.2357.0 GPS week: 2357 Day: 0 MJD: 60743
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 -29 22 27 .20 19 16 | 17568 -467 3099 45365
esa n/a| -1 -3 0 -30 -20 -5 -.12 29 25 | 18410 -164 3097 46287
gfz n/a| 0 0 1 4 14 -83 .02 25 18 | 0 -456 3157 7771
grg n/a| 1 0 6 -26 -8 54 .31 20 17 | 2548 -829 3135 7172
iac n/a| 0 0 -6 29 -7 10 -.23 15 14 | 13571 -683 3107 46558
jgx n/a| 0 1 1 28 2 6 -.07 21 21 | 8318 -761 3135 7748
Table 2.2357.1 GPS week: 2357 Day: 1 MJD: 60744
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 0 12 -27 -8 .12 16 14 | 14722 1567 4441 43709
esa n/a| -1 0 0 -18 -25 80 -.09 29 25 | 14172 1385 4510 44985
gfz n/a| 1 1 0 15 0 0 .08 29 17 | 0 1621 3279 7386
grg n/a| 0 -2 5 -29 2 52 .28 18 17 | -717 1533 3271 6896
iac n/a| -1 1 -5 18 3 -56 -.25 19 16 | 10361 1506 4496 44931
jgx n/a| 0 0 2 5 27 11 -.13 24 24 | 6265 1542 3286 7379
Table 2.2357.2 GPS week: 2357 Day: 2 MJD: 60745
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 3 0 13 -16 49 .13 20 17 | 14507 -1465 4583 43680
esa n/a| -4 -1 0 -17 -32 -26 -.03 31 25 | 15349 -1198 4603 44186
gfz n/a| 1 1 -1 50 -38 -31 .07 26 18 | 0 -1302 3436 7967
grg n/a| 3 0 3 -25 -15 25 .22 21 19 | 82 -1159 3438 7590
iac n/a| -1 -1 -2 -16 25 0 -.21 16 16 | 10164 420 4644 44920
jgx n/a| -1 0 4 30 29 -34 -.15 24 24 | 6255 -1091 3438 7953
Table 2.2357.3 GPS week: 2357 Day: 3 MJD: 60746
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| -3 0 0 -15 -20 -21 .12 21 17 | 16509 -2708 3220 46240
esa n/a| -4 -1 0 -7 -19 158 -.05 31 25 | 20221 -6862 3235 46134
gfz n/a| 2 0 -3 64 -14 -13 .15 22 17 | 0 -2412 2911 7271
grg n/a| 3 0 6 -66 18 55 .21 20 18 | 3604 -2663 2891 6817
iac n/a| 0 0 -6 4 14 -63 -.24 17 18 | 13981 -370 3227 47485
jgx n/a| -1 0 7 37 13 -24 -.10 22 22 | 7226 -2643 2893 7235
Table 2.2357.4 GPS week: 2357 Day: 4 MJD: 60747
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 1 14 -29 31 .15 23 16 | 15991 -1717 3301 47859
esa n/a| -2 -1 4 -21 20 6 -.05 28 27 | 17904 -3309 3333 47938
gfz n/a| 3 0 0 4 21 -67 -.00 29 19 | 0 -2202 3319 8203
grg n/a| 1 0 6 7 40 35 .32 23 21 | 3954 -2032 3326 7917
iac n/a| 0 0 -5 0 -17 31 -.15 14 12 | 15978 -763 3312 49074
jgx n/a| 0 0 3 15 37 -55 -.14 22 22 | 6537 -1940 3312 8274
Table 2.2357.5 GPS week: 2357 Day: 5 MJD: 60748
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -1 -24 48 .11 25 19 | 13209 -3119 3975 47587
esa n/a| 0 -2 3 23 1 73 -.03 31 25 | 16539 -7328 3952 48136
gfz n/a| 1 0 -1 26 4 -33 .04 20 20 | 0 -2661 3388 9615
grg n/a| 2 -1 8 -10 3 41 .22 22 17 | 2813 -2912 3380 9052
iac n/a| 0 2 -9 -29 0 -104 -.12 17 15 | 13736 -1732 3989 48898
jgx n/a| 0 -2 0 8 13 12 -.18 27 27 | 3240 -2821 3395 9568
Table 2.2357.6 GPS week: 2357 Day: 6 MJD: 60749
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 5 -8 31 .13 23 17 | 14501 -2682 3984 47174
esa n/a| -3 -1 0 -45 -61 -75 -.02 31 26 | 14588 -2419 4003 48231
gfz n/a| 2 0 -5 8 -3 -54 -.05 24 19 | 0 -2641 3757 8383
grg n/a| 3 0 9 -16 7 65 .30 21 15 | 5222 -2699 3743 8017
iac n/a| 0 0 -9 25 10 13 -.17 17 15 | 16155 -1126 4001 48343
jgx n/a| -1 0 1 -5 24 -53 -.19 22 22 | 4611 -2529 3745 8418
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 3.2357.0 GPS week: 2357 Day: 0 MJD: 60743
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2174 22 34 34 29 20 11 11 | 82 50 71 70 67 69 68
R02 | 1038 23 18 14 10 10 16 7 | 51 43 44 39 36 34 40
R03 | 1163 8 14 14 18 14 9 5 | 64 62 65 71 56 56 61
R04 | 1218 7 21 9 18 10 20 6 | 63 51 56 64 53 51 56
R05 | 584 9 35 11 15 10 18 7 | 143 152 144 137 144 139 142
R07 | 680 11 25 20 18 17 15 7 | 48 41 49 54 46 41 45
R08 | 1333 7 27 18 13 9 18 6 | 43 56 51 52 49 45 47
R09 | 1118 14 18 14 13 14 9 6 | 42 47 51 42 45 36 42
R11 | 1732 16 25 20 15 14 9 7 | 43 48 55 48 45 43 44
R12 | 745 20 19 15 23 10 14 7 | 85 86 87 73 79 72 78
R14 | 1496 9 26 16 12 20 9 7 | 69 78 68 59 57 59 63
R15 | 2772 16 26 9 11 12 19 7 | 82 81 69 77 65 67 72
R16 | 1256 14 26 9 14 11 25 7 | 95 73 87 92 90 69 85
R17 | 638 11 26 21 10 8 31 8 | 74 57 77 71 66 56 66
R18 | 643 6 16 11 12 15 20 6 | 60 64 58 61 67 45 59
R19 | 1389 22 42 53 33 18 42 15 | 44 35 77 49 47 45 44
R20 | 966 54 65 71 43 22 39 21 | 53 58 65 55 42 47 34
R21 | 764 15 24 14 19 13 24 8 | 63 51 60 53 54 39 51
R22 | 2467 16 29 16 22 19 10 8 | 19 30 27 36 28 24 21
R24 | 742 15 27 16 16 14 22 8 | 67 57 81 63 75 54 65
XR26 |12537 54 45 --- --- 39 --- 32 | 200 213 --- --- 208 --- 204
------+-----------------------------------------+-------------------------------------
RMS | 1386 19 29 25 20 15 21 |T 70 68 67 63 67 54 66
WRMS | 1386 16 25 18 17 14 21 |NE 70 68 67 63 67 54 66
MEDI | 1163 15 26 15 15 14 18 |MD 63 57 65 59 56 47 59
Table 3.2357.1 GPS week: 2357 Day: 1 MJD: 60744
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1017 18 60 22 22 17 20 11 | 40 31 43 30 49 39 38
R02 | 971 7 22 11 14 10 10 5 | 27 35 33 25 29 29 27
R03 | 2021 10 22 16 13 11 15 6 | 36 46 37 34 37 28 35
R04 | 1389 12 16 12 15 21 8 6 | 36 32 35 33 29 38 32
R05 | 523 12 24 12 13 11 12 6 | 121 123 118 121 125 124 122
R07 | 699 5 27 18 18 7 13 6 | 28 23 39 36 26 28 29
R08 | 1428 12 15 14 15 10 24 7 | 26 24 36 36 29 28 28
R09 | 1108 14 27 20 10 10 20 7 | 30 43 50 35 34 31 33
R11 | 1494 10 17 16 24 15 11 7 | 39 39 43 34 48 42 38
R12 | 809 12 23 25 30 10 10 8 | 66 63 75 54 62 57 60
R14 | 1585 10 23 14 13 11 10 6 | 49 57 34 41 42 37 42
R15 | 2951 19 18 19 13 31 7 9 | 60 63 43 54 40 52 50
R16 | 1318 16 27 12 17 15 20 8 | 66 64 55 67 62 48 59
R17 | 866 11 19 13 10 13 22 6 | 44 32 41 51 43 31 40
R18 | 637 8 24 13 12 17 20 7 | 39 41 43 48 51 26 41
R19 | 961 25 49 62 32 43 60 19 | 37 34 76 37 64 27 37
R20 | 3180 35 53 87 18 33 58 21 | 42 31 77 35 45 36 30
R21 | 1300 17 20 17 18 14 19 7 | 38 36 30 31 29 26 29
R22 | 2170 15 27 19 15 8 9 6 | 24 27 27 36 26 24 23
R24 | 1189 15 22 30 16 21 19 9 | 44 40 50 45 50 33 42
XR26 |15395 47 63 --- --- 38 --- 33 | 153 149 --- --- 151 --- 150
------+-----------------------------------------+-------------------------------------
RMS | 1547 16 29 29 18 19 24 |T 49 49 49 44 51 39 46
WRMS | 1547 14 25 17 17 16 24 |NE 49 49 49 44 51 39 46
MEDI | 1300 12 23 16 15 14 15 |MD 39 39 43 36 43 31 38
Table 3.2357.2 GPS week: 2357 Day: 2 MJD: 60745
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 883 21 58 28 10 15 19 11 | 55 29 55 46 60 52 48
R02 | 1126 12 24 11 9 22 12 7 | 38 28 36 36 45 32 35
R03 | 1708 10 20 15 14 8 15 6 | 39 41 34 40 34 31 35
R04 | 967 16 16 14 12 24 12 7 | 38 34 37 34 33 32 31
R05 | 1576 12 19 22 15 17 15 7 | 126 121 123 128 138 135 129
R07 | 927 12 18 10 16 6 26 7 | 39 37 31 33 29 22 30
R08 | 955 16 16 11 9 14 22 6 | 36 39 45 43 48 37 40
R09 | 1229 12 25 16 10 12 12 6 | 38 41 48 37 35 37 38
R11 | 1619 19 37 15 16 12 10 8 | 37 64 39 36 34 36 36
R12 | 1017 20 21 13 30 12 10 8 | 72 73 63 57 66 57 62
R14 | 1503 11 23 12 13 10 14 6 | 57 59 51 50 53 39 50
R15 | 2724 14 21 16 17 19 16 7 | 61 48 57 64 44 44 52
R16 | 1350 15 31 13 19 15 10 7 | 68 51 59 73 60 57 61
R17 | 1109 9 26 26 12 10 19 7 | 62 56 76 64 59 49 60
R18 | 611 11 21 18 13 21 16 7 | 47 55 44 54 62 42 49
R19 | 944 39 48 73 61 25 57 23 | 31 39 60 41 34 31 25
R20 | 3232 43 60 50 29 16 60 19 | 38 49 44 42 27 55 25
R21 | 1250 20 18 16 10 14 23 7 | 46 30 40 40 31 27 35
R22 | 2622 19 30 22 20 13 9 8 | 24 31 36 32 26 23 21
R24 | 861 19 22 21 21 20 22 9 | 59 52 69 60 66 54 59
XR26 |12047 50 62 --- --- 29 --- 32 | 61 76 --- --- 64 --- 61
------+-----------------------------------------+-------------------------------------
RMS | 1564 20 31 26 21 16 24 |T 51 50 52 50 49 44 46
WRMS | 1564 17 25 18 19 16 24 |NE 51 50 52 50 49 44 46
MEDI | 1229 16 23 16 14 15 15 |MD 46 48 45 42 45 37 40
Table 3.2357.3 GPS week: 2357 Day: 3 MJD: 60746
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 974 29 40 13 19 19 27 11 | 59 32 48 49 45 60 47
R02 | 978 9 20 15 13 26 11 7 | 37 45 43 35 33 39 35
R03 | 1024 9 16 10 16 14 8 5 | 46 40 42 50 40 39 42
R04 | 1062 12 33 13 16 10 14 7 | 49 28 44 50 41 38 41
R05 | 1618 11 31 17 13 10 17 7 | 77 74 80 73 70 77 73
R07 | 1115 16 47 14 13 10 25 9 | 39 43 38 40 25 26 31
R08 | 591 17 21 15 11 12 31 8 | 29 40 36 37 36 43 34
R09 | 2814 13 27 16 9 16 16 7 | 20 37 34 19 23 24 21
R11 | 1938 12 19 24 14 14 20 7 | 28 38 51 29 27 29 30
R12 | 1244 15 32 19 17 17 13 8 | 58 62 59 48 51 40 50
R14 | 1322 10 24 14 16 14 11 6 | 60 64 53 52 67 50 56
R15 | 2903 18 24 19 18 22 20 9 | 70 59 73 69 65 54 64
R16 | 677 18 37 27 13 10 20 9 | 78 49 84 69 72 53 68
R17 | 783 15 19 16 19 9 19 7 | 61 52 60 53 52 47 52
R18 | 584 11 20 15 13 15 10 6 | 56 61 68 59 57 49 57
R19 | 1392 54 30 57 48 26 41 19 | 40 40 64 37 41 41 32
R20 | 1417 42 58 33 36 20 42 17 | 36 48 51 41 25 34 24
R21 | 669 18 22 25 12 13 27 9 | 49 33 54 43 39 24 39
R22 | 2832 13 33 20 24 21 13 9 | 21 52 28 47 20 25 26
R24 | 666 14 28 17 18 20 20 8 | 50 33 48 43 53 37 43
XR26 |12416 51 66 --- --- 30 --- 33 | 49 90 --- --- 81 --- 68
------+-----------------------------------------+-------------------------------------
RMS | 1516 21 31 22 20 17 22 |T 48 48 52 47 45 41 44
WRMS | 1516 17 25 17 18 18 22 |NE 48 48 52 47 45 41 44
MEDI | 1115 15 28 16 16 15 19 |MD 49 45 51 47 41 39 42
Table 3.2357.4 GPS week: 2357 Day: 4 MJD: 60747
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1013 40 37 26 36 15 32 13 | 52 44 50 38 38 46 40
R02 | 936 13 14 10 24 9 12 6 | 33 35 31 33 28 34 29
R03 | 850 13 12 11 18 16 6 6 | 44 40 39 45 33 34 37
R04 | 1683 14 27 9 9 8 9 5 | 43 39 36 41 39 32 36
R05 | 1473 15 13 13 11 8 16 5 | 147 142 147 146 150 142 145
R07 | 758 11 36 17 17 13 17 8 | 38 34 37 40 38 30 33
R08 | 630 14 24 18 22 18 12 8 | 32 38 32 44 27 30 29
R09 | 2772 16 21 19 12 11 14 6 | 34 46 49 39 35 40 37
R11 | 2637 11 22 20 18 9 13 6 | 32 41 36 35 34 35 33
R12 | 1808 14 24 13 11 14 29 8 | 66 71 60 68 71 60 64
R14 | 1556 12 29 10 20 14 10 7 | 57 70 49 45 44 52 50
R15 | 2317 14 29 30 21 10 19 9 | 67 53 81 77 61 50 62
R16 | 598 20 34 23 19 8 18 8 | 74 48 72 58 64 52 61
R17 | 676 18 17 17 20 9 14 7 | 59 59 54 51 42 47 49
R18 | 547 12 27 17 32 10 10 8 | 47 56 49 46 45 44 45
R19 | 2551 56 37 93 37 18 37 21 | 39 46 111 49 34 45 45
R20 | 2097 47 54 41 22 30 52 18 | 50 36 49 39 28 35 27
R21 | 902 14 28 21 28 8 28 9 | 45 36 48 66 38 28 41
R22 | 2452 13 17 12 20 6 10 5 | 17 31 26 40 22 20 22
R24 | 642 17 27 38 37 23 29 12 | 58 65 79 53 62 50 57
XR26 |13688 70 43 --- --- 33 --- 34 | 100 109 --- --- 115 --- 108
------+-----------------------------------------+-------------------------------------
RMS | 1636 23 28 29 23 14 22 |T 54 54 56 52 49 45 50
WRMS | 1636 16 27 19 21 12 22 |NE 54 54 56 52 49 45 50
MEDI | 1473 14 27 17 20 11 14 |MD 47 46 49 45 38 40 41
Table 3.2357.5 GPS week: 2357 Day: 5 MJD: 60748
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 971 37 42 23 35 18 33 14 | 40 31 39 43 33 51 37
R02 | 1005 23 21 14 15 13 30 8 | 39 39 40 37 41 25 35
R03 | 1186 16 18 13 14 9 14 6 | 35 25 29 31 28 21 27
R04 | 1632 17 22 19 8 21 9 7 | 40 35 47 37 32 43 37
R05 | 1064 12 29 10 14 14 10 6 | 64 68 63 63 60 67 63
R07 | 823 11 19 13 13 14 16 6 | 26 21 22 26 29 19 22
R08 | 1002 10 11 21 13 19 16 7 | 30 29 45 33 25 21 29
R09 | 2329 12 21 13 15 11 8 6 | 31 36 44 31 42 37 36
R11 | 2966 15 20 13 13 12 14 6 | 30 36 36 30 29 29 28
R12 | 2283 10 31 17 14 13 18 7 | 64 78 70 62 61 48 62
R14 | 1710 8 29 14 15 14 13 7 | 49 61 46 49 42 40 45
R15 | 1553 21 15 16 15 11 11 6 | 59 54 44 46 54 47 49
R16 | 604 18 41 14 13 13 26 9 | 66 54 58 58 64 49 56
R17 | 690 15 15 12 22 15 12 7 | 64 55 55 58 59 57 57
R18 | 573 11 26 15 22 12 20 8 | 39 41 31 40 38 34 34
R19 | 2040 62 55 31 47 28 34 19 | 47 24 44 34 43 29 29
R20 | 3343 55 64 37 35 31 83 23 | 59 39 38 34 34 68 35
R21 | 800 12 30 29 16 17 30 10 | 40 30 57 41 36 26 37
R22 | 2707 21 20 18 14 16 22 8 | 17 31 40 38 34 24 27
R24 | 1091 21 20 26 36 12 17 10 | 53 39 52 42 50 46 45
XR26 |12527 66 34 --- --- 38 --- 34 | 59 75 --- --- 78 --- 68
------+-----------------------------------------+-------------------------------------
RMS | 1721 25 31 20 22 17 27 |T 45 42 45 41 43 39 40
WRMS | 1721 19 25 20 17 15 27 |NE 45 42 45 41 43 39 40
MEDI | 1186 16 22 15 15 14 16 |MD 40 39 44 38 41 37 37
Table 3.2357.6 GPS week: 2357 Day: 6 MJD: 60749
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 961 29 51 23 42 22 25 14 | 78 40 58 81 56 66 62
R02 | 1684 11 37 18 14 10 22 8 | 56 43 46 58 53 48 50
R03 | 1579 15 18 21 13 13 12 7 | 64 54 54 64 54 51 55
R04 | 892 22 28 12 11 8 16 7 | 66 47 61 63 54 54 57
R05 | 970 10 32 10 12 15 7 6 | 90 97 92 86 99 89 91
R07 | 965 8 20 12 13 11 13 5 | 47 40 48 54 51 42 47
R08 | 1761 9 20 20 16 16 15 7 | 40 45 52 47 40 34 41
R09 | 1793 17 21 19 13 12 10 6 | 38 45 54 39 50 45 44
R11 | 1844 13 22 17 11 7 20 6 | 39 51 47 34 39 37 38
R12 | 1914 9 31 16 15 10 12 7 | 77 92 77 74 70 67 73
R14 | 1384 10 21 20 11 9 13 6 | 62 76 71 68 63 57 64
R15 | 663 16 17 15 12 15 22 7 | 75 69 68 69 57 51 63
R16 | 710 20 31 31 20 22 15 10 | 86 71 93 68 76 64 73
R17 | 662 20 14 14 21 10 13 7 | 85 69 80 68 73 71 73
R18 | 490 10 21 22 31 15 16 9 | 59 67 68 54 64 50 58
R19 | 1711 48 47 50 38 38 47 20 | 56 47 86 48 74 52 55
R20 | 2267 62 70 42 33 30 48 21 | 89 45 64 42 53 60 48
R21 | 571 8 27 10 9 20 26 8 | 60 46 63 61 68 40 56
R22 | 3639 18 15 19 14 19 11 7 | 20 28 24 33 30 23 24
R24 | 1473 24 20 37 21 11 23 10 | 77 53 80 58 68 55 64
XR26 |12674 62 44 --- --- 36 --- 34 | 84 124 --- --- 115 --- 103
------+-----------------------------------------+-------------------------------------
RMS | 1575 23 31 24 21 17 22 |T 64 59 64 58 62 52 59
WRMS | 1575 17 26 19 15 15 22 |NE 64 59 64 58 62 52 59
MEDI | 1473 16 22 19 14 15 15 |MD 64 51 63 58 57 51 57
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