[IGSREPORT-30525] Wk 2373 IGLOS Final Orbits
acc
acc at igs.org
Fri Jul 18 03:51:57 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2373 (Jun 29, 2025 - Jul 05, 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 2.2373.
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:
igl2373[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2373 in the SP3 format.
igl23737.sum Combination Report for GPS Week 2373.
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 | 5.7 ns
1 | 2.1 ns
2 | 6.4 ns
3 | 1.6 ns
4 | -0.4 ns
5 | 5.0 ns
6 | 4.2 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 | ESA | R20 R22
4 | ESA | R20
5 | ESA | R20
6 | ESA | 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 1.2373, 1a.2373).
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 2.2373.0-6)
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 3.2373.0-6).
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 2373 summary. (Jun 29, 2025 - Jul 05, 2025)
Table 1.2373.a GPS week : 2373 MJD: 60855.0-60861.0
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 1 -22 -16 13 .10 17 15 | 3450 -1334 3671 8439
| 1 0 2 12 14 26 .04 | 889 3109
esa n/a| -2 -2 4 16 10 29 .00 38 42 | 218 -1123 3643 8965
| 1 0 1 16 12 33 .07 | 1376 2522
gfz n/a| 0 0 0 28 4 10 .01 18 15 | 0 -1572 3736 8463
| 0 1 2 13 15 23 .08 | 0 3138
grg n/a| 1 0 1 -2 18 -38 .39 20 15 | 4025 -1583 3708 8055
| 1 1 2 10 27 23 .03 | 1828 3642
iac n/a| 0 0 -4 -4 -12 -1 -.15 16 15 | 5519 -616 3796 9329
| 0 1 2 18 27 34 .05 | 2032 1719
jgx n/a| 1 0 0 0 9 0 -.27 19 19 | 4431 -2025 3693 8293
| 0 0 1 11 12 20 .04 | 1132 4061
Table 1.2373.b GPS week : 2373 MJD: 60855.0-60861.0
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 | 8 7 6 8 7 7 7 |
R03 | 6 6 6 5 6 7 7 |
R04 | 6 6 6 6 7 6 7 |
R05 | 7 6 6 6 7 6 7 |
R07 | 7 7 8 7 8 5 7 |
R08 | 7 6 6 8 6 7 6 |
R09 | 6 6 6 8 7 5 5 |
R11 | 9 7 6 6 8 8 6 |
R12 | 8 7 8 7 8 7 7 |
R14 | 6 6 8 5 5 7 6 |
R15 | 7 6 7 6 8 8 7 |
R16 | 5 8 6 6 10 15 6 |
R17 | 7 7 9 7 7 8 7 |
R18 | 7 7 7 6 7 7 7 |
R19 | 9 8 10 7 7 9 8 |
R20 | 24 23 25 20 23 23 26 |
R21 | 6 7 8 9 7 8 8 |
R22 | 8 8 10 11 9 8 10 |
R24 | 9 9 6 9 9 7 8 |
R25 | 82 55 47 44 53 69 93 |
R26 | 29 31 31 32 30 31 30 |
R27 | 30 27 28 29 30 30 30 |
Table 1.2373.c GPS week : 2373 MJD: 60855.0-60861.0
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 2373 0 | 101 13 20 561 1630 13340 82.2 1671 1671 | 5716 0
brd 2373 1 | -11 34 154 -1437 583 8962 81.0 1692 1692 | 2060 0
brd 2373 2 | -100 91 169 -2352 233 16360 80.2 2091 2091 | 6407 0
brd 2373 3 | -16 44 276 1239 576 10930 81.7 2444 2444 | 1628 0
brd 2373 4 | 3 75 274 -927 1381 12240 79.9 2110 2110 | -397 0
brd 2373 5 | 77 76 65 1006 878 2874 80.8 1994 1994 | 5006 0
brd 2373 6 | 7 55 178 777 498 8829 82.0 2013 2013 | 4185 0
-------------+------------------------------------------------------------+----------------
brd 2373 mean| 8 55 162 -161 825 10504 81.1 2002 2002 | 3515 0
brd 2373 sdev| 66 27 96 1398 506 4260 .9 264 264 | 2478 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 2.2373.0 GPS week: 2373 Day: 0 MJD: 60855
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 4 -15 -39 -11 .11 18 16 | 3065 617 3203 8869
esa n/a| -3 -2 6 40 4 78 .04 39 51 | 1203 -189 3210 8345
gfz n/a| 0 -1 -4 52 28 12 .01 20 16 | 0 63 3262 7968
grg n/a| 2 0 0 -7 16 -24 .38 18 13 | 4835 202 3316 8075
iac n/a| 1 0 -3 -19 -15 34 -.22 16 14 | 6715 -1976 3595 8694
jgx n/a| 0 0 0 10 18 -19 -.30 19 19 | 5749 -33 3408 7727
Table 2.2373.1 GPS week: 2373 Day: 1 MJD: 60856
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 2 1 1 -24 0 .10 18 14 | 2480 -1959 4434 8946
esa n/a| -2 -2 3 0 4 35 -.06 36 50 | -9 -2414 4407 8860
gfz n/a| 0 0 0 9 13 -30 -.02 15 13 | 0 -2206 4519 8658
grg n/a| 1 0 2 -6 -7 -53 .40 17 14 | 2643 -2852 4520 7984
iac n/a| 0 1 -7 -15 35 24 -.11 16 15 | 3427 -997 4805 8839
jgx n/a| 1 0 0 -3 -5 13 -.28 20 20 | 4650 -4274 4783 8412
Table 2.2373.2 GPS week: 2373 Day: 2 MJD: 60857
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 -21 -6 9 .12 16 15 | 4889 3469 4386 10370
esa n/a| -4 -4 1 14 5 8 -.11 32 47 | 1736 2758 4414 10263
gfz n/a| 0 2 2 38 -5 41 .08 19 18 | 0 3137 4471 10558
grg n/a| 0 0 0 -14 41 -30 .33 19 15 | 3886 4332 4203 10184
iac n/a| 0 0 -2 -7 -42 -30 -.11 16 16 | 7204 1558 4414 11115
jgx n/a| 1 0 1 8 27 4 -.34 22 22 | 5460 5141 4287 10854
Table 2.2373.3 GPS week: 2373 Day: 3 MJD: 60858
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 -30 -29 -4 .17 14 14 | 3311 -753 3366 6618
esa n/a| -1 -4 6 12 11 -28 -.01 37 46 | -233 -1320 3381 7789
gfz n/a| 0 0 1 20 -3 14 -.02 16 12 | 0 -620 3430 6957
grg n/a| 2 3 2 6 54 3 .40 21 18 | 2012 -1293 3358 6425
iac n/a| 1 0 -5 21 -35 -17 -.09 16 15 | 3690 -159 3410 8137
jgx n/a| 0 0 -1 8 13 14 -.25 16 16 | 4683 -2241 3439 7302
Table 2.2373.4 GPS week: 2373 Day: 4 MJD: 60859
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 -23 -1 58 .10 16 15 | 2510 -5016 3522 7560
esa n/a| -3 -2 3 -5 -1 20 .08 43 35 | -2309 -4448 3571 9165
gfz n/a| 1 0 0 28 13 21 -.02 16 13 | 0 -6042 3556 7987
grg n/a| 0 -1 4 8 29 -67 .38 26 20 | 2595 -5973 3500 7249
iac n/a| 0 1 -6 17 -16 -58 -.17 16 15 | 2994 -2792 3571 8623
jgx n/a| 0 0 0 -19 -2 27 -.23 19 19 | 2667 -6190 3379 7551
Table 2.2373.5 GPS week: 2373 Day: 5 MJD: 60860
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 -40 -12 43 .02 17 15 | 4256 -374 3384 7906
esa n/a| -3 -1 2 31 14 37 .03 43 35 | 1348 1052 3127 8872
gfz n/a| 0 1 0 21 5 -8 .14 18 18 | 0 -375 3447 8178
grg n/a| 0 0 0 9 21 -45 .44 18 13 | 4929 226 3604 7837
iac n/a| 0 -1 -1 -28 -26 23 -.23 17 16 | 7455 1647 3377 9318
jgx n/a| 1 0 -3 10 18 -30 -.25 20 20 | 4657 -291 2955 7532
Table 2.2373.6 GPS week: 2373 Day: 6 MJD: 60861
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 2 -26 -1 3 .08 17 14 | 3639 -5326 3403 8804
esa n/a| 0 -2 6 21 36 52 .05 38 32 | -205 -3305 3397 9462
gfz n/a| 1 1 -4 27 -18 21 -.09 23 15 | 0 -4966 3472 8937
grg n/a| 0 0 -1 -12 -24 -48 .39 19 13 | 7275 -5729 3456 8635
iac n/a| -1 0 0 4 13 14 -.15 15 15 | 7150 -1597 3402 10582
jgx n/a| 1 0 -2 -8 0 -8 -.27 17 17 | 3156 -6291 3601 8677
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 3.2373.0 GPS week: 2373 Day: 0 MJD: 60855
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1871 10 15 23 18 10 --- 7 | 37 46 44 45 39 --- 40
R03E | 1483 7 24 18 11 11 9 5 | 45 43 43 50 41 41 43
R04E | 2023 8 16 20 13 18 9 6 | 48 53 50 50 37 47 45
R05E | 1702 6 23 13 18 17 9 6 | 56 59 51 64 53 52 54
R07E | 1470 14 25 16 19 16 10 7 | 46 51 46 55 45 44 45
R08E | 1516 9 13 22 22 11 11 6 | 64 65 66 71 63 62 64
R09 | 2534 12 20 16 8 11 9 5 | 30 32 32 28 31 25 27
R11 | 1821 12 21 25 28 14 16 8 | 29 32 29 34 31 25 27
R12 | 911 18 25 22 10 11 20 8 | 40 45 43 41 33 31 35
R14 | 1210 8 17 15 9 19 10 5 | 42 41 51 43 43 40 42
R15 | 1887 19 19 11 9 13 16 6 | 53 43 52 48 44 47 47
R16 | 2083 9 11 16 11 10 8 5 | 56 57 63 55 61 57 58
R17 | 1298 13 24 14 15 10 16 6 | 82 74 78 70 72 62 72
R18 | 1148 8 31 13 17 13 10 6 | 94 101 93 100 94 90 94
XR19 | 2991 12 21 14 --- 14 --- 8 | 30 35 37 --- 34 --- 31
R20 | 2227 52 132 40 39 36 59 23 | 131 85 125 99 91 107 108
R21 | 1474 13 24 13 12 8 11 6 | 79 70 81 72 75 66 73
XR22 | 2729 14 18 15 20 11 --- 8 | 47 93 63 52 58 --- 53
R24 | 977 19 29 30 17 14 15 9 | 106 107 112 98 93 91 99
XR25 |15898 76 --- --- --- 88 --- 82 | 118 --- --- --- 164 --- 129
XR26E | 9372 47 41 43 --- 59 --- 28 | 31 44 55 --- 24 --- 26
XR27E |11917 38 39 --- 43 73 --- 30 | 26 35 --- 33 28 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1671 18 39 20 18 16 19 |T 58 57 60 58 57 55 56
WRMS | 1671 16 51 16 13 14 19 |NE 66 62 66 61 66 58 63
MEDI | 1821 12 23 16 17 13 10 |MD 47 51 51 52 44 47 45
Table 3.2373.1 GPS week: 2373 Day: 1 MJD: 60856
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1829 9 13 13 16 13 --- 6 | 46 54 46 53 47 --- 47
R03E | 2993 9 22 14 18 13 7 6 | 47 52 50 52 52 48 48
R04E | 1567 9 14 10 12 18 9 5 | 47 41 45 46 47 38 42
R05E | 1288 10 13 19 14 18 6 6 | 49 52 50 55 48 44 47
R07E | 1257 17 12 16 17 14 12 6 | 39 44 44 52 40 40 41
R08E | 1067 12 16 12 13 19 8 6 | 59 58 59 63 68 57 59
R09 | 2731 18 17 13 8 11 8 5 | 13 26 27 17 14 18 16
R11 | 2671 10 23 11 15 16 11 6 | 23 36 22 22 18 23 21
R12 | 857 11 17 9 17 10 18 6 | 27 37 35 35 32 29 30
R14 | 1230 12 11 10 12 16 11 5 | 32 32 35 29 22 31 28
R15 | 1152 13 14 17 12 16 5 5 | 39 31 49 32 33 38 36
R16 | 1575 12 21 17 9 30 11 7 | 41 39 36 40 55 39 39
R17 | 1117 13 18 20 16 13 14 7 | 51 39 63 44 56 39 47
R18 | 1138 11 30 13 15 11 10 6 | 63 72 64 71 74 64 67
XR19 | 2030 11 16 15 --- 9 --- 7 | 21 25 31 --- 23 --- 24
R20 | 2053 52 122 23 43 17 64 23 | 80 54 57 63 68 56 61
R21 | 972 15 23 15 16 15 15 7 | 56 54 50 52 53 50 50
XR22 | 2714 15 22 10 18 14 --- 8 | 31 92 34 33 34 --- 31
R24 | 1279 23 28 13 16 12 22 9 | 87 91 83 89 76 76 82
XR25 |13016 48 --- --- --- 61 --- 54 | 108 --- --- --- 146 --- 120
XR26E |12331 49 50 45 --- 68 --- 30 | 18 49 50 --- 25 --- 24
XR27E |10627 39 46 --- 32 66 --- 27 | 26 47 --- 29 31 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1691 18 36 15 17 16 20 |T 45 48 46 46 48 43 44
WRMS | 1691 14 50 13 14 15 20 |NE 48 48 45 43 50 42 46
MEDI | 1567 12 18 13 16 15 11 |MD 41 47 46 46 47 39 41
Table 3.2373.2 GPS week: 2373 Day: 2 MJD: 60857
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1127 7 20 13 14 11 --- 6 | 36 35 33 38 38 --- 34
R03E | 3042 7 18 13 22 13 8 6 | 33 43 32 44 35 33 33
R04E | 2016 7 11 17 21 12 9 6 | 32 37 27 40 35 34 31
R05E | 1809 9 12 17 18 14 12 6 | 45 44 44 46 43 44 43
R07E | 2962 9 15 19 21 24 9 7 | 44 49 49 55 41 44 44
R08E | 1574 11 16 11 14 8 15 5 | 50 56 58 57 55 53 53
R09 | 2842 12 14 12 16 13 8 5 | 14 20 22 16 15 18 14
R11 | 3416 14 26 16 8 13 7 6 | 25 23 25 24 23 25 20
R12 | 1106 14 16 19 20 14 15 7 | 30 33 33 41 26 31 30
R14 | 1425 8 27 22 16 15 13 7 | 29 23 47 30 22 36 28
R15 | 1005 8 17 26 11 20 11 7 | 40 51 66 41 36 53 45
R16 | 1797 10 23 8 16 19 7 6 | 48 60 61 50 61 51 54
R17 | 1727 22 26 16 20 19 13 8 | 62 54 43 49 61 40 50
R18 | 1144 6 28 16 19 14 13 7 | 84 88 93 76 90 74 83
XR19 | 2474 11 15 23 --- 18 --- 9 | 15 23 35 --- 20 --- 19
R20 | 2802 46 102 43 36 24 73 25 | 84 74 81 87 71 66 73
R21 | 1042 16 22 19 13 12 20 7 | 59 45 62 62 57 40 54
XR22 | 4193 16 14 27 22 14 --- 9 | 39 95 54 39 35 --- 39
R24 | 1277 16 18 10 13 15 10 6 | 83 72 80 80 72 79 77
XR25 |14547 43 --- --- --- 51 --- 47 | 77 --- --- --- 85 --- 63
XR26E | 9766 50 44 44 --- 69 --- 31 | 20 43 53 --- 17 --- 21
XR27E | 9160 38 46 --- 36 64 --- 27 | 33 54 --- 30 25 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2091 16 32 19 19 16 22 |T 44 48 49 47 43 45 42
WRMS | 2091 15 47 18 15 16 22 |NE 49 50 54 49 48 46 46
MEDI | 1809 11 18 17 18 14 11 |MD 39 45 47 44 36 40 39
Table 3.2373.3 GPS week: 2373 Day: 3 MJD: 60858
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1207 13 28 13 18 11 --- 8 | 59 78 59 70 59 --- 61
R03E | 4766 8 15 11 15 11 8 5 | 29 31 24 30 29 28 27
R04E | 3453 7 15 10 20 12 10 5 | 28 27 29 38 29 21 26
R05E | 1517 9 16 13 22 9 8 5 | 31 35 32 46 31 29 31
R07E | 4153 10 19 15 16 19 8 6 | 38 38 41 48 42 34 37
R08E | 803 9 25 14 27 18 12 7 | 37 51 38 52 43 41 39
R09 | 2331 18 34 9 19 11 9 7 | 14 35 24 33 21 16 19
R11 | 3643 12 12 13 9 15 12 5 | 28 31 27 32 25 34 27
R12 | 1016 10 12 13 15 22 14 6 | 26 27 29 36 17 39 27
R14 | 1085 9 13 10 11 11 7 4 | 25 33 30 29 29 23 26
R15 | 1298 11 11 21 15 11 12 6 | 38 41 51 33 41 36 38
R16 | 1547 10 14 11 19 14 7 5 | 44 53 50 37 50 46 44
R17 | 1648 16 25 10 18 11 14 7 | 66 55 58 55 62 54 58
R18 | 1363 5 28 15 17 8 7 6 | 65 78 63 69 59 64 64
XR19 | 3671 11 15 11 --- 9 --- 6 | 15 23 31 --- 24 --- 21
R20 | 2729 32 118 37 50 27 46 19 | 103 71 100 71 87 71 85
R21 | 1262 14 32 18 18 18 18 8 | 63 59 67 72 66 53 61
XR22 |10993 17 476 20 22 18 --- 11 | 41 377 51 50 47 --- 44
R24 | 1456 22 40 10 16 20 14 9 | 60 40 40 59 48 43 46
XR25 |13927 38 --- --- --- 49 --- 43 | 96 --- --- --- 105 --- 84
XR26E | 7140 43 58 60 --- 62 --- 32 | 39 53 61 --- 25 --- 30
XR27E | 9584 40 40 --- 36 69 --- 28 | 33 38 --- 28 27 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 2444 14 37 16 21 16 16 |T 44 60 45 46 43 39 41
WRMS | 2444 14 46 12 18 15 16 |NE 48 71 47 48 48 43 46
MEDI | 1648 11 25 13 18 14 10 |MD 38 40 40 46 41 36 37
Table 3.2373.4 GPS week: 2373 Day: 4 MJD: 60859
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1357 10 16 15 16 17 --- 7 | 62 64 63 56 54 --- 59
R03E | 3010 12 15 13 12 11 16 6 | 41 43 43 47 38 40 40
R04E | 2175 10 13 16 24 15 11 6 | 45 42 43 38 45 47 42
R05E | 1620 8 15 19 24 12 8 6 | 48 45 50 43 46 42 44
R07E | 1749 13 28 10 23 18 11 7 | 43 48 45 54 38 41 42
R08E | 1209 15 14 14 16 10 12 6 | 53 60 53 62 56 55 54
R09 | 1335 14 21 20 18 15 7 7 | 18 26 24 29 20 20 17
R11 | 4492 15 34 12 28 11 10 8 | 32 46 33 44 23 29 29
R12 | 1755 17 19 16 17 26 12 8 | 39 34 39 39 30 42 34
R14 | 1129 6 18 8 12 16 8 5 | 33 26 36 37 36 24 30
R15 | 1524 13 20 16 15 13 22 7 | 38 30 37 38 30 27 30
XR16 | 7918 14 --- 19 22 10 --- 9 | 45 --- 51 28 33 --- 39
R17 | 1454 17 25 15 17 13 9 7 | 73 73 64 61 72 67 67
R18 | 1828 6 24 15 18 11 13 6 | 108 109 108 102 108 103 106
XR19 | 3816 10 14 10 --- 13 --- 6 | 27 30 34 --- 30 --- 28
R20 | 2293 39 146 26 67 29 56 22 | 95 85 86 85 75 73 81
R21 | 1199 14 20 11 13 8 19 6 | 57 50 51 51 49 33 47
XR22 | 3144 15 21 17 17 16 --- 8 | 37 150 52 58 39 --- 43
R24 | 2238 10 22 15 25 23 21 8 | 105 112 112 107 100 114 107
XR25 |12409 47 --- --- --- 59 --- 52 | 114 --- --- --- 106 --- 105
XR26E | 8829 34 52 55 --- 66 --- 30 | 24 47 53 --- 25 --- 26
XR27E | 5485 39 39 --- 47 71 --- 30 | 33 39 --- 32 28 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2109 16 43 16 26 16 19 |T 53 57 53 53 49 50 49
WRMS | 2109 15 35 13 20 15 19 |NE 58 64 55 56 53 53 54
MEDI | 1828 14 20 15 18 15 12 |MD 43 46 50 47 38 42 42
Table 3.2373.5 GPS week: 2373 Day: 5 MJD: 60860
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 3445 9 21 10 9 16 --- 6 | 50 57 48 53 46 --- 49
R03E | 1639 12 17 21 13 16 15 7 | 44 49 40 47 46 44 42
R04E | 900 11 22 16 10 10 13 6 | 36 46 40 39 36 37 37
R05E | 1695 10 21 13 17 11 10 6 | 49 58 52 58 54 46 51
R07E | 3138 9 16 12 15 11 7 5 | 38 38 35 43 35 36 36
R08E | 1485 11 20 12 19 14 10 6 | 51 53 56 62 50 54 53
R09 | 1031 15 14 12 11 8 9 5 | 15 30 22 20 15 15 15
R11 | 3842 12 27 9 17 20 14 7 | 24 29 27 20 28 31 21
R12 | 1546 17 24 21 9 17 6 7 | 32 34 26 26 30 23 24
R14 | 1309 8 11 16 10 27 13 6 | 29 31 29 27 35 30 26
R15 | 1408 14 27 19 11 22 13 7 | 29 30 34 25 34 23 25
XR16 | 7698 29 --- 36 19 17 --- 15 | 41 --- 63 47 35 --- 40
R17 | 1331 22 25 15 17 13 17 8 | 54 55 43 60 45 46 48
R18 | 1468 12 29 17 12 7 9 6 | 99 97 99 112 96 101 100
XR19 | 1863 11 18 17 --- 16 --- 9 | 14 33 26 --- 19 --- 18
R20 | 2936 41 143 30 48 29 64 23 | 86 74 90 85 74 64 77
R21 | 1064 15 31 20 13 12 12 7 | 50 45 56 53 44 42 46
XR22 | 1017 15 17 15 18 14 --- 8 | 64 123 58 63 64 --- 61
R24 | 2369 13 15 22 11 15 11 6 | 50 51 59 53 46 46 48
XR25 |11508 63 --- --- --- 74 --- 68 | 73 --- --- --- 102 --- 74
XR26E | 6223 38 48 54 --- 71 --- 31 | 17 43 52 --- 27 --- 25
XR27E | 4513 32 49 --- 40 76 --- 29 | 23 38 --- 25 20 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 1994 17 43 18 18 17 20 |T 44 50 47 48 44 42 42
WRMS | 1994 15 35 18 13 16 20 |NE 47 52 48 49 47 42 44
MEDI | 1639 13 21 16 13 16 12 |MD 41 45 43 47 36 42 40
Table 3.2373.6 GPS week: 2373 Day: 6 MJD: 60861
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2602 12 13 17 12 10 --- 6 | 47 55 58 60 49 --- 51
R03E | 1877 9 19 13 16 19 12 6 | 43 44 40 41 47 46 42
R04E | 1052 17 24 18 9 13 12 7 | 34 31 37 34 35 24 30
R05E | 1455 10 20 22 15 19 9 7 | 46 53 53 56 48 45 47
R07E | 3139 9 20 11 17 19 15 6 | 43 40 41 47 38 35 38
R08E | 1243 9 23 15 15 14 9 6 | 59 67 61 67 61 56 60
R09 | 1519 15 13 12 7 8 10 5 | 38 45 38 43 36 40 39
R11 | 3126 13 10 14 11 15 8 5 | 41 32 41 40 34 37 37
R12 | 1704 12 22 15 17 13 12 6 | 51 47 42 51 52 43 46
R14 | 1074 7 21 16 16 11 7 5 | 49 52 46 51 47 45 46
R15 | 1960 10 26 25 15 9 9 7 | 53 51 53 51 48 49 48
R16 | 1073 18 17 12 14 9 7 6 | 62 54 53 49 53 50 55
R17 | 1258 17 11 12 14 18 13 6 | 88 76 78 80 79 70 77
R18 | 1110 11 37 11 10 21 7 7 | 116 122 112 118 115 113 114
XR19 | 2145 13 18 8 --- 17 --- 8 | 38 45 41 --- 44 --- 40
R20 | 3965 48 126 68 48 19 56 25 | 138 100 147 100 108 99 113
R21 | 1238 12 41 12 19 12 16 8 | 89 82 89 80 86 73 82
XR22 | 1268 14 26 18 25 12 --- 9 | 75 111 73 71 72 --- 73
R24 | 2338 13 21 17 25 15 13 7 | 92 79 93 95 82 82 86
XR25 |14543 80 --- --- --- 107 --- 93 | 92 --- --- --- 192 --- 125
XR26E | 5709 39 49 45 --- 70 --- 29 | 33 52 61 --- 35 --- 38
XR27E | 4067 30 43 --- 49 75 --- 29 | 31 46 --- 33 27 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2013 17 38 22 19 15 17 |T 61 61 62 61 63 56 59
WRMS | 2013 14 32 15 13 15 17 |NE 73 68 69 69 74 63 70
MEDI | 1704 13 21 15 15 15 10 |MD 49 52 53 51 48 46 47
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