[IGSREPORT-30517] Wk 2372 IGLOS Final Orbits
acc
acc at igs.org
Fri Jul 11 04:55:11 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2372 (Jun 22, 2025 - Jun 28, 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 2.2372.
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:
igl2372[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2372 in the SP3 format.
igl23727.sum Combination Report for GPS Week 2372.
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 | 5.6 ns
1 | 8.6 ns
2 | 3.7 ns
3 | 7.6 ns
4 | 5.5 ns
5 | 3.5 ns
6 | 5.0 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 | R19
0 | GFZ | R19
1 | ESA | R19 R20
2 | ESA | R19 R20
3 | ESA | R19
4 | ESA | R19 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 1.2372, 1a.2372).
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 2.2372.0-6)
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 3.2372.0-6).
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 2372 summary. (Jun 22, 2025 - Jun 28, 2025)
Table 1.2372.a GPS week : 2372 MJD: 60848.0-60854.0
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 5 0 -17 20 .11 16 16 | 850 308 3347 11041
| 0 1 2 16 17 22 .05 | 1594 1835
esa n/a| -1 -2 0 -13 0 -53 -.12 37 40 | 856 -1449 3342 10820
| 1 1 2 24 32 43 .08 | 2541 2665
gfz n/a| 0 0 -1 17 6 29 -.07 17 14 | 0 77 3416 9180
| 1 1 1 17 13 21 .05 | 0 2045
grg n/a| 1 1 2 -30 24 -65 .44 19 15 | 5030 30 3466 8083
| 1 1 1 20 14 51 .07 | 1277 2218
iac n/a| 0 0 -4 13 2 5 -.13 14 14 | 5049 -322 3474 10969
| 1 0 3 8 22 71 .03 | 1352 1332
jgx n/a| 0 0 -2 -3 -10 23 -.28 19 18 | 4301 -47 3501 8218
| 0 0 1 15 12 28 .06 | 1720 2307
Table 1.2372.b GPS week : 2372 MJD: 60848.0-60854.0
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 6 8 8 8 8 9 |
R03 | 7 7 7 7 8 8 7 |
R04 | 7 6 7 6 8 7 6 |
R05 | 5 6 5 6 8 6 7 |
R07 | 8 6 6 6 8 9 7 |
R08 | 7 7 7 6 7 13 7 |
R09 | 9 7 7 7 7 7 6 |
R11 | 7 8 6 8 8 6 7 |
R12 | 7 6 8 7 7 6 7 |
R14 | 6 6 6 7 5 5 7 |
R15 | 5 5 7 8 8 10 8 |
R16 | 6 6 6 9 8 7 7 |
R17 | 6 7 7 7 8 6 6 |
R18 | 8 8 7 7 9 7 8 |
R19 | 17 8 14 26 10 8 9 |
R20 | 20 20 17 21 21 22 17 |
R21 | 6 6 8 7 9 8 8 |
R22 | 6 7 8 9 8 7 8 |
R24 | 8 7 7 6 8 9 7 |
R25 | 60 42 44 49 48 94 74 |
R26 | 29 31 30 26 27 20 28 |
R27 | 34 34 32 31 31 34 30 |
Table 1.2372.c GPS week : 2372 MJD: 60848.0-60854.0
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 2372 0 | 141 113 182 974 -113 16520 80.3 1856 1856 | 5624 0
brd 2372 1 | 2 260 315 -1900 3187 15360 80.1 1636 1636 | 8566 0
brd 2372 2 | 173 24 90 2449 1469 21310 81.3 1727 1727 | 3721 0
brd 2372 3 | 5 20 62 1795 1678 19760 79.9 1781 1781 | 7594 0
brd 2372 4 | -38 41 247 -2587 801 14450 77.9 1731 1731 | 5542 0
brd 2372 5 | 82 171 201 1521 -726 8811 79.0 1623 1623 | 3495 0
brd 2372 6 | 52 9 85 -68 698 10370 81.8 1636 1636 | 4972 0
-------------+------------------------------------------------------------+----------------
brd 2372 mean| 59 91 169 311 999 15225 80.0 1712 1712 | 5644 0
brd 2372 sdev| 77 94 94 1919 1278 4557 1.3 87 87 | 1876 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 2.2372.0 GPS week: 2372 Day: 0 MJD: 60848
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 14 -10 -11 .11 17 16 | -1270 -806 3433 13071
esa n/a| -3 -3 2 -14 -3 -85 -.17 36 36 | -750 -1604 3419 13847
gfz n/a| 2 1 1 21 -16 17 -.15 13 12 | 0 -591 3506 11951
grg n/a| 0 1 1 -47 28 -112 .42 17 17 | 3889 -541 3611 11259
iac n/a| -1 0 -4 18 15 111 -.11 15 14 | 3887 -1790 3533 12245
jgx n/a| 0 0 -3 -11 0 -11 -.19 19 19 | 1401 -494 3595 11740
Table 2.2372.1 GPS week: 2372 Day: 1 MJD: 60849
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 5 -3 -27 47 .08 17 16 | 2551 1899 4089 12978
esa n/a| 0 -1 -2 -27 -41 -40 -.26 36 33 | 3271 67 4126 13128
gfz n/a| 0 1 0 38 0 -6 -.03 15 12 | 0 2077 4173 10944
grg n/a| 3 3 2 -48 36 25 .42 17 12 | 7068 1608 4296 9139
iac n/a| 0 -1 -2 20 1 -35 -.13 11 11 | 7215 885 4125 11845
jgx n/a| 1 0 -4 1 -30 41 -.25 20 20 | 6272 1673 4388 9662
Table 2.2372.2 GPS week: 2372 Day: 2 MJD: 60850
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 6 17 -9 16 .11 13 13 | -635 -1366 2911 11141
esa n/a| -2 -3 -2 -48 -2 -20 -.12 36 34 | -565 -2255 2870 10841
gfz n/a| 0 0 -3 11 -2 45 -.05 17 14 | 0 -2115 2961 8727
grg n/a| 2 0 0 -40 39 -51 .53 22 18 | 4427 -1924 3011 6525
iac n/a| 0 -1 -3 12 -14 -63 -.14 13 13 | 3323 -1970 3198 9917
jgx n/a| 1 0 -1 17 3 47 -.24 15 15 | 3429 -2037 3020 7092
Table 2.2372.3 GPS week: 2372 Day: 3 MJD: 60851
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 -7 13 -4 .14 16 16 | 1943 3017 3456 11010
esa n/a| 0 -1 -4 -16 -31 -139 -.15 35 33 | 1659 1723 3486 10463
gfz n/a| 0 -2 0 30 7 38 -.13 16 14 | 0 2934 3521 8771
grg n/a| 3 1 3 -28 25 -88 .52 20 16 | 5770 3156 3574 7396
iac n/a| 0 0 -2 -3 -11 60 -.07 14 13 | 6052 1457 3646 10032
jgx n/a| 0 0 -2 -14 -5 13 -.29 21 21 | 5334 3152 3646 8050
Table 2.2372.4 GPS week: 2372 Day: 4 MJD: 60852
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 10 -25 -39 43 .22 18 18 | 2744 -437 3160 9886
esa n/a| 0 0 2 -25 22 -23 -.12 40 56 | 5084 -6151 3118 9383
gfz n/a| -1 1 -1 17 14 14 -.04 22 19 | 0 -646 3233 7720
grg n/a| 1 1 5 -36 31 -113 .43 20 17 | 5703 -697 3244 6698
iac n/a| 0 0 -6 19 34 41 -.11 13 13 | 5437 405 3234 10379
jgx n/a| -1 0 -2 9 -18 -17 -.27 20 20 | 6031 -78 3213 6531
Table 2.2372.5 GPS week: 2372 Day: 5 MJD: 60853
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 6 -14 -31 30 .05 16 14 | -80 -1726 3087 9893
esa n/a| -2 -2 0 14 6 -26 -.07 38 35 | -1503 -2837 3094 9447
gfz n/a| 2 0 -2 -15 24 47 -.04 20 15 | 0 -2341 3146 8053
grg n/a| 1 -1 4 10 6 -25 .42 24 14 | 5047 -3097 3166 7048
iac n/a| -2 0 -10 15 25 -87 -.17 16 17 | 4177 -1093 3227 11945
jgx n/a| 0 0 0 0 -15 52 -.33 20 20 | 4124 -3681 3188 7001
Table 2.2372.6 GPS week: 2372 Day: 6 MJD: 60854
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 4 14 -13 24 .09 17 16 | 702 1578 3298 9310
esa n/a| -2 -3 1 21 56 -35 .02 40 51 | -1202 911 3281 8634
gfz n/a| 0 1 0 15 16 51 -.02 17 13 | 0 1223 3374 8096
grg n/a| 2 0 0 -19 0 -93 .31 16 12 | 3307 1707 3363 8516
iac n/a| 0 0 -2 8 -28 12 -.15 17 16 | 5252 -149 3360 10424
jgx n/a| 0 0 0 -29 -3 38 -.38 14 14 | 3522 1133 3463 7450
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 3.2372.0 GPS week: 2372 Day: 0 MJD: 60848
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2706 8 20 15 12 17 --- 7 | 37 37 36 45 36 --- 36
R03E | 1214 12 26 8 23 19 11 7 | 60 52 61 72 59 62 60
R04E | 1695 10 32 14 14 13 12 6 | 46 45 37 49 43 34 40
R05E | 1502 10 27 9 12 8 10 5 | 81 87 79 82 78 78 80
R07E | 1067 12 15 13 24 17 17 7 | 53 50 60 65 52 56 55
R08E | 3820 8 15 12 17 17 17 6 | 38 42 34 47 32 38 35
R09 | 1511 26 41 20 9 13 10 8 | 40 42 52 46 48 42 43
R11 | 3279 15 33 12 16 15 11 7 | 39 42 32 39 33 34 33
R12 | 1593 17 32 9 11 10 15 6 | 39 63 39 35 35 31 36
R14 | 1171 9 16 16 11 14 7 5 | 41 45 38 38 45 45 40
R15 | 1618 13 21 7 8 11 11 5 | 51 36 48 46 46 41 45
R16 | 1216 14 21 14 11 9 12 6 | 47 40 47 36 45 42 42
R17 | 1253 11 27 9 15 9 8 5 | 75 65 68 60 74 61 67
R18 | 2038 8 43 14 13 16 16 7 | 53 76 56 49 46 41 50
XR19 | 4184 16 364 410 --- 18 --- 17 | 31 164 276 --- 42 --- 36
R20 | 1442 44 95 22 39 31 58 20 | 109 65 95 87 98 87 92
R21 | 878 9 22 10 14 7 14 5 | 73 68 71 70 68 70 69
XR22 | 2157 12 28 10 10 9 --- 6 | 28 38 35 34 34 --- 32
R24 | 1779 22 25 12 16 15 16 7 | 77 76 64 64 67 65 66
XR25 |18502 61 --- --- --- 58 --- 60 | 97 --- --- --- 136 --- 112
XR26E | 9597 40 50 43 --- 64 --- 29 | 42 58 51 --- 35 --- 39
XR27E | 6725 47 49 --- --- 48 --- 33 | 40 49 --- --- 32 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1856 17 36 13 17 15 19 |T 54 59 63 53 53 51 51
WRMS | 1856 16 36 12 17 14 19 |NE 57 63 70 50 58 50 54
MEDI | 1618 12 27 12 13 15 12 |MD 46 50 51 47 45 42 42
Table 3.2372.1 GPS week: 2372 Day: 1 MJD: 60849
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1950 9 16 12 13 8 --- 5 | 30 34 27 29 26 --- 26
R03E | 1262 12 19 14 20 13 10 6 | 56 56 55 59 54 54 53
R04E | 1307 9 19 12 14 10 11 5 | 31 32 27 36 27 22 26
R05E | 1614 14 23 10 9 9 10 5 | 61 69 61 61 61 59 61
R07E | 1476 7 19 14 19 8 13 6 | 65 55 68 67 62 71 64
R08E | 2707 12 20 12 17 12 15 6 | 53 66 50 54 40 56 50
R09 | 1217 21 21 13 8 7 20 6 | 41 38 40 43 43 44 41
R11 | 2237 16 29 8 12 21 12 7 | 27 46 35 42 32 35 32
R12 | 1635 11 29 11 10 8 14 6 | 28 56 28 30 34 26 30
R14 | 817 9 25 10 12 10 13 5 | 28 30 31 24 28 34 27
R15 | 1272 17 14 8 9 12 9 5 | 39 39 37 31 30 33 32
R16 | 1352 15 18 14 9 9 20 6 | 41 32 43 39 42 27 36
R17 | 1403 16 20 12 22 9 9 6 | 49 48 41 39 49 40 43
R18 | 1690 9 34 21 14 7 15 7 | 35 47 42 35 41 26 36
XR19 | 5115 13 354 7 --- 12 --- 8 | 22 127 116 --- 25 --- 25
R20 | 1894 43 116 34 38 11 62 19 | 64 43 66 64 57 44 54
R21 | 1210 17 17 13 10 6 16 6 | 50 47 39 49 41 39 42
XR22 | 2684 13 24 12 16 12 --- 7 | 28 34 32 34 30 --- 29
R24 | 2060 22 12 16 20 9 14 7 | 57 52 58 43 50 47 49
XR25 |19227 52 --- --- --- 34 --- 42 | 51 --- --- --- 68 --- 54
XR26E | 9940 55 45 55 --- 56 --- 31 | 37 54 73 --- 26 --- 37
XR27E |12234 53 49 --- --- 43 --- 33 | 24 49 --- --- 21 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1636 17 36 15 17 11 20 |T 41 50 48 43 40 41 39
WRMS | 1636 16 33 12 12 11 20 |NE 40 49 46 39 40 35 37
MEDI | 1635 14 21 12 13 10 13 |MD 39 47 41 39 40 39 36
Table 3.2372.2 GPS week: 2372 Day: 2 MJD: 60850
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1670 13 17 11 22 14 --- 7 | 30 34 35 39 30 --- 30
R03E | 1218 9 23 11 21 15 14 6 | 42 46 45 43 53 48 45
R04E | 1144 11 30 11 14 18 8 6 | 31 34 28 24 32 24 25
R05E | 2047 7 19 10 12 14 11 5 | 50 58 52 61 54 46 51
R07E | 2016 9 17 13 17 13 10 5 | 44 50 46 41 41 44 42
R08E | 2054 9 23 15 22 14 13 6 | 39 46 36 50 35 40 37
R09 | 2417 12 28 6 17 15 18 7 | 31 38 33 39 26 32 30
R11 | 2234 8 21 20 14 9 11 6 | 26 25 28 26 22 25 21
R12 | 1129 15 21 27 14 9 7 7 | 27 32 28 28 25 25 23
R14 | 1290 11 26 12 15 12 7 6 | 32 26 27 31 26 29 27
R15 | 1597 16 24 17 14 9 9 6 | 40 29 35 34 33 36 33
R16 | 1302 10 21 12 21 7 10 5 | 40 41 41 36 39 45 39
R17 | 1152 10 25 13 25 10 11 6 | 52 41 56 52 54 43 49
R18 | 1578 12 26 14 19 11 8 6 | 43 48 46 40 40 38 40
XR19 | 4114 11 356 26 --- 22 --- 14 | 25 157 84 --- 33 --- 29
R20 | 2084 26 113 34 53 19 40 17 | 73 45 79 72 68 62 67
R21 | 1508 13 19 16 25 10 19 7 | 60 48 59 76 55 43 55
XR22 | 2519 11 30 9 22 12 --- 8 | 28 33 36 35 35 --- 30
R24 | 1994 15 18 17 14 16 11 6 | 56 51 51 56 38 46 47
XR25 |15278 40 --- --- --- 47 --- 43 | 91 --- --- --- 82 --- 68
XR26E | 7087 36 44 65 --- 58 --- 30 | 50 49 45 --- 26 --- 30
XR27E |11981 39 52 --- --- 48 --- 32 | 30 60 --- --- 28 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1726 13 36 17 22 13 15 |T 42 47 44 43 39 39 38
WRMS | 1726 13 34 14 18 13 15 |NE 44 47 46 43 41 38 39
MEDI | 1994 11 24 13 17 14 11 |MD 40 45 41 39 35 40 33
Table 3.2372.3 GPS week: 2372 Day: 3 MJD: 60851
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1663 14 18 15 15 14 --- 7 | 30 41 42 41 38 --- 34
R03E | 1125 10 20 12 13 16 18 6 | 30 29 34 33 35 34 30
R04E | 1353 9 24 12 10 15 17 6 | 33 30 30 35 33 27 29
R05E | 2560 13 27 10 15 13 11 6 | 37 44 40 42 45 36 38
R07E | 2490 9 26 12 14 13 13 6 | 55 50 63 57 57 55 55
R08E | 1231 9 13 17 16 9 13 5 | 29 26 28 36 25 28 25
XR09 | 2265 12 28 9 16 11 --- 7 | 18 27 17 23 17 --- 17
R11 | 1458 18 24 12 17 20 11 7 | 32 46 28 37 25 25 27
R12 | 917 17 27 12 16 8 7 6 | 31 29 18 32 22 24 23
R14 | 2230 13 37 16 14 10 13 7 | 23 27 29 24 22 20 19
R15 | 1115 21 29 17 14 14 8 7 | 32 26 28 27 19 23 23
R16 | 1242 22 21 18 32 11 11 8 | 41 37 37 18 30 29 28
R17 | 1189 16 22 14 16 11 12 6 | 55 43 49 42 49 42 46
R18 | 1627 13 37 12 13 11 13 7 | 40 55 35 40 30 28 34
XR19 | 4063 26 360 53 --- 25 --- 25 | 16 184 68 --- 30 --- 29
R20 | 3223 28 97 32 48 22 65 20 | 93 50 89 76 71 76 76
R21 | 1620 8 30 15 14 7 19 6 | 58 50 63 61 59 46 56
XR22 | 2639 14 28 21 15 10 --- 8 | 23 30 44 40 25 --- 29
R24 | 1541 13 15 13 12 15 10 5 | 51 45 39 52 40 50 44
XR25 |17436 50 --- --- --- 47 --- 48 | 113 --- --- --- 93 --- 93
XR26E | 9971 38 43 39 --- 53 --- 25 | 42 50 46 --- 31 --- 34
XR27E | 6756 43 48 --- --- 43 --- 31 | 27 48 --- --- 34 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 1780 16 35 16 20 14 21 |T 41 46 41 39 37 36 37
WRMS | 1780 16 33 14 16 13 21 |NE 44 49 41 39 38 36 38
MEDI | 1627 14 27 14 15 13 13 |MD 32 43 37 37 31 29 29
Table 3.2372.4 GPS week: 2372 Day: 4 MJD: 60852
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2120 12 27 13 15 11 --- 7 | 41 48 43 36 32 --- 37
R03E | 1254 16 19 23 17 10 20 7 | 67 72 72 74 67 76 69
R04E | 1219 13 28 25 15 14 13 7 | 32 42 38 37 28 32 29
R05E | 2495 13 24 25 20 14 12 7 | 37 41 42 41 39 33 35
R07E | 2024 13 24 22 20 13 13 7 | 58 52 63 73 60 69 61
R08E | 1210 12 17 13 15 10 19 6 | 31 29 25 30 24 34 25
R09 | 1970 17 28 12 12 14 9 6 | 34 31 39 45 32 35 34
R11 | 1163 16 24 19 21 21 10 8 | 33 24 18 38 18 30 22
R12 | 1021 17 17 21 12 9 14 6 | 32 34 27 32 27 21 24
R14 | 1128 8 17 6 12 6 17 5 | 30 31 29 32 28 31 28
R15 | 919 25 29 15 13 15 15 8 | 32 26 31 25 28 28 24
R16 | 764 20 23 24 15 16 12 8 | 37 40 45 28 24 25 27
R17 | 1024 15 27 26 17 10 10 7 | 53 51 34 48 48 45 45
R18 | 1347 18 47 27 11 11 14 9 | 43 55 34 41 33 32 35
XR19 | 5010 14 386 20 --- 9 --- 10 | 27 225 60 --- 26 --- 30
R20 | 4186 38 124 31 51 12 61 21 | 77 47 76 69 69 52 65
R21 | 904 16 34 29 15 10 12 8 | 58 45 62 46 50 49 50
XR22 | 3560 18 17 13 19 12 --- 8 | 24 29 31 30 31 --- 25
R24 | 1702 13 20 14 27 12 11 7 | 54 55 50 67 47 44 51
XR25 |23401 54 --- --- --- 42 --- 48 | 101 --- --- --- 112 --- 107
XR26E |11914 38 43 50 --- 49 --- 26 | 34 50 37 --- 34 --- 29
XR27E | 8426 42 48 --- --- 42 --- 30 | 23 51 --- --- 28 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 1730 18 40 22 20 13 20 |T 43 51 42 44 40 39 39
WRMS | 1730 18 56 19 17 13 20 |NE 45 53 41 41 40 35 40
MEDI | 1347 16 27 21 15 12 13 |MD 34 45 38 38 32 33 30
Table 3.2372.5 GPS week: 2372 Day: 5 MJD: 60853
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1956 9 22 16 7 23 --- 8 | 39 44 50 42 46 --- 41
R03E | 2577 6 18 16 28 14 13 7 | 47 45 50 50 52 47 46
R04E | 1326 9 16 18 21 12 20 7 | 39 41 49 47 37 32 38
R05E | 1586 10 14 10 13 11 16 5 | 51 55 56 65 49 56 54
R07E | 2032 13 29 18 19 31 9 9 | 54 43 60 60 72 60 57
R08E | 1602 11 18 21 63 14 23 13 | 26 36 32 57 26 29 24
R09 | 1537 13 19 18 11 14 13 6 | 26 46 35 26 35 27 29
R11 | 1233 12 13 17 12 16 8 6 | 22 28 23 29 14 18 19
R12 | 974 14 21 13 10 11 12 6 | 31 29 34 33 21 19 26
R14 | 2949 9 16 9 10 10 9 4 | 34 36 32 33 26 34 31
R15 | 1038 20 15 32 17 29 13 10 | 37 42 49 44 25 38 33
R16 | 1121 16 19 14 8 16 11 6 | 34 35 36 32 26 34 30
R17 | 1071 11 11 17 12 9 20 6 | 47 43 53 44 43 32 42
R18 | 1225 8 32 10 8 15 8 6 | 37 44 35 40 27 33 35
XR19 | 4168 12 14 12 --- 16 --- 7 | 46 133 60 --- 49 --- 46
R20 | 1579 43 130 42 41 18 57 21 | 72 43 68 47 56 31 51
R21 | 1505 14 28 14 22 9 12 7 | 51 46 44 49 46 38 43
XR22 | 3684 14 16 12 15 11 --- 6 | 20 30 28 29 28 --- 23
R24 | 1113 16 23 25 15 13 26 9 | 49 43 59 48 49 31 44
XR25 |21387 82 --- --- --- 108 --- 94 | 63 --- --- --- 170 --- 96
XR26E | 7723 29 26 20 --- 50 --- 19 | 49 48 61 --- 29 --- 41
XR27E |10981 35 34 --- --- 66 --- 33 | 48 38 --- --- 33 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 1623 16 38 20 24 16 20 |T 41 45 45 43 43 34 39
WRMS | 1623 14 35 15 14 17 20 |NE 40 46 42 37 43 30 39
MEDI | 1579 13 19 16 13 14 13 |MD 39 43 49 44 35 32 38
Table 3.2372.6 GPS week: 2372 Day: 6 MJD: 60854
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1756 7 25 19 18 16 --- 8 | 25 27 36 32 31 --- 26
R03E | 1588 8 18 18 10 19 12 6 | 58 56 63 66 59 66 61
R04E | 2455 9 18 16 14 10 7 5 | 50 53 54 50 52 50 50
R05E | 1103 11 19 17 21 14 14 7 | 68 67 73 79 69 67 70
R07E | 1499 16 21 14 18 11 11 7 | 77 90 80 84 84 80 81
R08E | 1584 13 16 9 23 16 8 6 | 32 35 33 35 35 31 31
R09 | 1792 13 14 11 11 17 14 6 | 37 44 44 42 45 42 40
R11 | 1835 17 20 12 10 16 15 6 | 24 31 26 25 21 21 19
R12 | 1003 12 13 12 10 21 17 6 | 40 40 39 42 27 47 37
R14 | 2200 10 20 13 14 18 14 6 | 43 37 44 42 42 38 39
R15 | 1668 20 24 23 11 11 7 7 | 49 38 46 46 37 42 42
R16 | 1395 16 15 15 12 13 15 6 | 45 40 45 36 41 51 41
R17 | 1247 15 17 8 10 13 12 5 | 66 52 61 58 61 48 57
R18 | 1258 10 41 11 12 15 12 7 | 47 65 42 45 38 39 43
XR19 | 3701 12 17 14 --- 20 --- 9 | 61 159 93 --- 70 --- 65
R20 | 1876 37 135 38 34 29 30 17 | 112 57 110 80 80 83 91
R21 | 1808 21 29 16 11 18 14 8 | 73 61 65 62 68 51 62
XR22 | 3566 15 21 7 20 12 --- 7 | 30 36 35 39 34 --- 32
R24 | 1092 15 22 14 13 14 13 6 | 69 58 62 68 61 51 60
XR25 |16303 69 --- --- --- 78 --- 74 | 90 --- --- --- 170 --- 120
XR26E | 8522 38 45 41 --- 65 --- 27 | 33 58 42 --- 38 --- 35
XR27E |12256 35 46 --- 39 77 --- 30 | 29 55 --- 10 32 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1635 17 40 17 16 17 14 |T 52 55 54 49 54 50 51
WRMS | 1635 16 51 13 12 16 14 |NE 56 55 54 48 56 46 53
MEDI | 1756 15 20 14 13 16 13 |MD 47 53 45 45 42 48 42
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