[IGSREPORT-30698] Wk 2392 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 28 00:38:25 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2392 (Nov 09, 2025 - Nov 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 2.2392.
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:
igl2392[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2392 in the SP3 format.
igl23927.sum Combination Report for GPS Week 2392.
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 | 4.2 ns
1 | 3.0 ns
2 | 3.9 ns
3 | 1.5 ns
4 | 3.6 ns
5 | 1.2 ns
6 | 3.8 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESA | R26
0 | GFZ | R20
1 | ESA | R26 R27
1 | GFZ | R02 R20
2 | GFZ | R20
3 | GFZ | R20
4 | ESA | R26
4 | GFZ | R20
5 | GFZ | R20
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 1.2392, 1a.2392).
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 2.2392.0-6)
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 3.2392.0-6).
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 2392 summary. (Nov 09, 2025 - Nov 15, 2025)
Table 1.2392.a GPS week : 2392 MJD: 60988.0-60994.0
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 3 9 4 .18 13 13 | -318 -1099 3176 11114
| 0 0 0 14 14 15 .02 | 1128 1991
esa n/a| -2 -1 2 -27 -21 44 -.13 19 18 | -745 -655 3171 11060
| 1 0 1 18 17 31 .04 | 1605 1926
gfz n/a| 0 1 -4 23 5 25 -.06 15 15 | 0 -476 3134 6735
| 1 1 2 17 22 20 .03 | 0 1941
grg n/a| 1 0 6 -25 -30 -5 .30 16 14 | 1220 -834 3250 11615
| 1 0 2 15 16 46 .04 | 1808 2092
iac n/a| 0 -1 -9 19 28 -24 -.17 17 17 | 4469 -1112 3290 11003
| 1 1 3 19 25 43 .07 | 1939 1210
jgx n/a| 1 0 8 4 8 -38 -.18 19 18 | 2261 -409 3247 7302
| 0 1 2 24 11 15 .06 | 1012 2236
Table 1.2392.b GPS week : 2392 MJD: 60988.0-60994.0
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 43 --- --- --- --- --- |
R03 | 8 7 7 7 7 6 6 |
R04 | 8 7 7 7 8 8 8 |
R05 | 5 8 6 7 6 9 7 |
R07 | 9 6 6 8 9 10 6 |
R08 | 6 7 7 7 6 7 7 |
R09 | 7 7 7 7 7 8 7 |
R11 | 7 9 7 7 8 9 9 |
R12 | 8 5 9 8 9 8 9 |
R14 | 7 10 7 8 6 7 6 |
R15 | 7 9 6 9 7 8 8 |
R16 | 8 6 8 9 8 7 7 |
R17 | 6 5 6 9 7 8 6 |
R18 | 7 7 7 8 8 7 7 |
R19 | 8 9 9 10 9 8 8 |
R20 | 8 9 10 12 13 8 10 |
R21 | 8 9 5 7 6 6 7 |
R22 | 8 8 6 6 7 9 10 |
R24 | 7 6 8 9 11 7 8 |
R26 | 39 33 32 36 38 36 31 |
R27 | 32 32 34 31 30 29 36 |
R28 | 70 44 72 56 73 86 90 |
Table 1.2392.c GPS week : 2392 MJD: 60988.0-60994.0
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 2392 0 | 1 11 -90 2501 -472 3999 80.3 1647 1647 | 4195 0
brd 2392 1 | -99 138 -117 -1535 -1719 4081 78.5 1483 1483 | 3008 0
brd 2392 2 | -21 21 -41 -2982 -2396 1101 81.7 3213 3213 | 3852 0
brd 2392 3 | 104 18 -114 -992 1039 2786 79.4 1631 1631 | 1546 0
brd 2392 4 | 50 38 -78 -170 2407 3201 79.3 1828 1828 | 3574 0
brd 2392 5 | -216 -63 101 -1140 -600 7518 80.9 1884 1884 | 1250 0
brd 2392 6 | 14 36 35 1206 3048 10310 83.6 1980 1980 | 3824 0
-------------+------------------------------------------------------------+----------------
brd 2392 mean| -23 28 -43 -444 186 4713 80.5 1952 1952 | 3035 0
brd 2392 sdev| 105 59 83 1820 2049 3139 1.7 581 581 | 1178 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 2.2392.0 GPS week: 2392 Day: 0 MJD: 60988
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 0 -6 10 24 .21 15 15 | 275 -273 3351 7195
esa n/a| 0 -1 3 -20 -43 43 -.09 20 19 | 1615 -830 3340 6530
gfz n/a| -2 2 -3 29 12 32 -.07 15 15 | 0 -10 3266 7385
grg n/a| 2 -1 6 -36 -34 -4 .33 15 14 | 3992 -251 3364 7110
iac n/a| 1 1 -10 9 15 -40 -.19 13 13 | 7230 -1318 3415 8356
jgx n/a| 2 0 7 6 -7 -29 -.18 15 15 | 1172 174 3339 7863
Table 2.2392.1 GPS week: 2392 Day: 1 MJD: 60989
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 -5 -9 15 .20 12 12 | 258 -2011 3337 7555
esa n/a| -3 -2 4 -40 -10 42 -.14 19 18 | 536 -1970 3193 7723
gfz n/a| 0 0 -3 30 22 11 -.08 16 17 | 0 -1098 3263 6766
grg n/a| 3 0 3 -36 -2 -7 .25 14 14 | 3555 -1870 3418 7633
iac n/a| -2 -3 -10 0 9 -5 -.21 18 16 | 6028 -1894 3591 8078
jgx n/a| 3 1 10 45 9 -56 -.19 17 17 | 2129 -1890 3182 7118
Table 2.2392.2 GPS week: 2392 Day: 2 MJD: 60990
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 10 28 -7 .19 11 11 | 137 1176 3122 9329
esa n/a| -2 -1 3 -15 -34 82 -.16 19 18 | 638 1120 3129 9737
gfz n/a| 0 1 -4 10 -37 43 -.01 14 14 | 0 1795 3109 6997
grg n/a| 1 0 5 -30 -23 -47 .28 13 12 | 1189 1465 3235 9819
iac n/a| 2 -1 -14 26 33 -6 -.26 20 20 | 6162 -1274 3224 9674
jgx n/a| 1 2 6 4 10 -14 -.28 18 18 | 2715 1662 3354 7702
Table 2.2392.3 GPS week: 2392 Day: 3 MJD: 60991
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 -2 -11 2 -8 .15 15 14 | 835 -2489 3042 10710
esa n/a| -2 -2 1 2 -2 1 -.13 17 15 | -2032 -2028 3065 10782
gfz n/a| 0 0 -3 40 18 -4 -.03 15 15 | 0 -1387 3027 6325
grg n/a| 1 0 7 -33 -36 -17 .32 15 13 | 97 -2464 3115 11357
iac n/a| 0 0 -13 47 12 55 -.15 20 20 | 3340 -1638 3127 9900
jgx n/a| 1 0 12 0 -6 -50 -.22 22 22 | 4151 -2237 3159 6742
Table 2.2392.4 GPS week: 2392 Day: 4 MJD: 60992
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 1 -1 -12 .16 13 13 | -128 481 3561 12234
esa n/a| -1 0 2 -22 -3 88 -.19 20 19 | -2141 1937 3599 11953
gfz n/a| 0 0 -9 21 16 22 -.05 15 15 | 0 1383 3554 5784
grg n/a| 0 -1 11 -15 -46 27 .25 17 16 | -29 1383 3667 12937
iac n/a| 0 0 -5 21 15 -50 -.18 14 14 | 2900 1361 3597 11389
jgx n/a| 1 0 11 2 20 -50 -.15 22 22 | 2014 2316 3831 6368
Table 2.2392.5 GPS week: 2392 Day: 5 MJD: 60993
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 2 -1 6 7 -1 .15 13 13 | -1107 -4508 2838 14885
esa n/a| -3 0 3 -44 -19 29 -.14 19 18 | -1944 -3360 2850 14334
gfz n/a| 2 2 -7 40 19 14 -.10 16 17 | 0 -3994 2860 6993
grg n/a| 0 -1 7 5 -50 76 .34 17 16 | -243 -4178 2843 15581
iac n/a| 2 -4 -4 -6 81 -78 -.15 21 21 | 2347 -2347 2932 14468
jgx n/a| 1 -1 6 12 16 -37 -.12 19 19 | 2427 -3713 2938 7635
Table 2.2392.6 GPS week: 2392 Day: 6 MJD: 60994
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 32 28 21 .20 14 14 | -2501 -69 2982 15890
esa n/a| -3 -1 1 -47 -40 22 -.08 20 19 | -1888 545 3027 16367
gfz n/a| 2 0 -2 -7 -15 55 -.07 12 12 | 0 -24 2861 6897
grg n/a| 1 0 5 -33 -21 -63 .33 19 16 | -15 72 3112 16872
iac n/a| 0 -1 -9 37 34 -47 -.05 16 16 | 3280 -678 3145 15156
jgx n/a| 0 1 6 -36 17 -27 -.09 18 18 | 1224 819 2932 7690
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 3.2392.0 GPS week: 2392 Day: 0 MJD: 60988
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 3186 14 18 14 20 9 12 6 | 29 14 49 35 15 10 27
R03 | 1685 15 28 11 14 10 20 7 | 56 41 51 56 53 36 48
R04 | 1280 27 23 13 11 10 16 7 | 64 49 49 53 53 43 50
R05 | 1260 11 19 13 9 10 7 5 | 53 51 53 53 46 45 49
R07 | 1796 23 15 20 21 19 15 8 | 54 37 42 46 48 37 41
R08 | 1205 12 14 16 10 12 8 5 | 57 52 60 53 57 53 54
R09 | 1607 17 10 19 11 16 15 7 | 47 56 55 43 61 45 50
R11 | 2663 16 17 16 17 10 9 6 | 59 67 65 49 56 53 58
R12 | 1011 14 17 18 25 11 11 7 | 111 103 110 95 106 98 103
R14 | 1115 9 23 10 23 12 14 7 | 103 112 104 84 110 89 99
R15 | 1084 14 16 18 10 13 19 7 | 129 113 123 118 126 105 119
R16 | 1261 12 17 18 11 14 24 7 | 118 110 119 114 115 94 111
R17 | 1326 12 24 8 13 12 11 6 | 42 54 46 44 39 45 43
R18 | 1041 13 19 17 11 10 15 6 | 53 47 47 50 52 51 49
XR19 | 2728 11 13 14 --- 12 --- 7 | 39 47 45 --- 40 --- 41
XR20 | 2503 8 --- 388 14 11 --- 8 | 124 --- 151 125 117 --- 122
R21 | 1551 8 34 10 12 14 18 7 | 47 43 48 48 53 36 46
XR22 | 2401 14 22 15 15 15 --- 8 | 44 48 50 47 56 --- 47
R24 | 1590 16 18 12 13 18 13 6 | 52 51 52 52 46 48 48
XR26 | 6509 38 94 48 --- 69 --- 38 | 60 148 64 --- 119 --- 81
XR27 | 7111 43 72 --- 56 50 --- 31 | 54 139 --- 61 117 --- 87
XR28 |16314 76 --- --- --- 63 --- 69 | 41 --- --- --- 64 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1646 15 20 15 15 13 15 |T 65 69 69 64 70 55 64
WRMS | 1646 15 19 15 14 13 15 |NE 65 69 69 64 70 55 64
MEDI | 1590 14 18 15 13 12 14 |MD 54 51 52 53 56 45 49
Table 3.2392.1 GPS week: 2392 Day: 1 MJD: 60989
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02 | 4993 40 --- 272 46 --- --- 43 | 29 --- 100 39 --- --- 29
R03 | 1395 17 18 14 11 11 11 6 | 42 45 39 38 42 32 38
R04 | 1248 16 21 16 9 10 16 6 | 46 38 46 43 41 35 40
R05 | 2068 10 13 29 11 12 16 7 | 32 26 47 34 27 22 30
R07 | 1780 14 14 8 12 16 14 6 | 38 24 31 39 28 24 30
R08 | 1947 10 15 18 15 15 15 6 | 45 31 39 31 46 40 37
R09 | 1142 13 18 18 9 18 8 6 | 37 44 45 36 41 30 37
R11 | 935 16 27 24 20 17 19 9 | 47 67 66 64 53 52 54
R12 | 931 11 17 10 9 14 9 5 | 84 81 84 85 82 82 82
R14 | 1430 9 27 13 28 30 18 9 | 77 84 71 57 94 59 71
R15 | 1441 13 14 14 15 30 24 8 | 102 90 97 92 109 77 94
R16 | 1540 13 16 14 9 16 16 6 | 89 74 82 83 93 71 82
R17 | 1304 10 14 11 9 9 13 5 | 27 22 30 31 25 21 24
R18 | 1093 9 20 18 7 12 25 7 | 30 30 26 28 30 34 28
XR19 | 1673 12 19 19 --- 12 --- 9 | 23 31 33 --- 32 --- 27
XR20 | 2626 10 --- 358 9 19 --- 9 | 100 --- 91 95 92 --- 95
R21 | 1079 6 29 16 18 21 21 8 | 34 30 35 34 42 26 32
XR22 | 2036 14 11 21 11 14 --- 7 | 23 31 36 30 33 --- 26
R24 | 2149 10 15 6 17 17 13 6 | 38 40 31 45 36 31 34
XR26 | 8512 27 97 30 --- 76 --- 32 | 41 98 49 --- 86 --- 51
XR27 |10550 27 104 --- 27 77 --- 32 | 35 103 --- 35 71 --- 41
XR28 |21125 33 --- --- --- 56 --- 43 | 22 --- --- --- 122 --- 58
------+-----------------------------------------+-------------------------------------
RMS | 1482 12 19 16 14 18 17 |T 47 52 53 49 58 42 47
WRMS | 1482 12 18 17 14 16 17 |NE 47 52 53 49 58 42 47
MEDI | 1540 13 18 16 11 16 16 |MD 38 40 45 39 42 34 37
Table 3.2392.2 GPS week: 2392 Day: 2 MJD: 60990
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R03 | 1473 15 19 9 12 24 18 7 | 45 39 41 45 37 35 38
R04 | 953 16 18 17 12 18 18 7 | 51 43 55 46 49 38 46
R05 | 1981 10 15 18 10 14 16 6 | 46 44 53 51 52 43 47
R07 | 1844 9 22 14 7 18 9 6 | 44 32 49 46 54 41 42
R08 | 2254 14 12 16 17 20 16 7 | 49 42 51 62 47 53 49
R09 | 1279 11 13 17 12 31 10 7 | 52 48 46 44 75 54 50
XR11 | 1381 12 15 15 12 15 --- 6 | 54 55 55 47 59 --- 52
R12 | 775 13 25 16 15 31 20 8 | 96 104 101 100 73 85 93
R14 | 1284 9 24 14 18 20 8 7 | 77 80 78 60 83 72 73
R15 | 1092 11 13 8 16 18 11 5 | 106 104 98 91 109 97 100
R16 |10818 12 16 13 17 17 27 7 | 103 110 103 94 102 91 99
R17 | 1073 6 15 17 8 16 18 6 | 40 45 37 41 35 39 37
R18 | 1206 9 27 11 10 12 25 7 | 43 39 38 42 36 43 39
XR19 | 2260 13 15 15 --- 19 --- 8 | 41 44 39 --- 40 --- 38
XR20 | 2294 9 --- 346 9 22 --- 9 | 108 --- 124 121 108 --- 112
R21 | 815 6 9 10 14 15 14 5 | 47 45 48 44 50 37 45
XR22 | 1559 13 11 12 12 12 --- 6 | 39 45 51 42 42 --- 42
R24 | 1908 11 22 11 15 14 27 7 | 53 56 51 48 52 58 51
XR26 | 8909 37 74 41 --- 74 --- 31 | 66 116 66 --- 104 --- 78
XR27 |10521 50 73 --- 33 85 --- 34 | 45 123 --- 64 116 --- 75
XR28 |15641 49 --- --- --- 104 --- 72 | 53 --- --- --- 86 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 3213 11 19 14 13 20 18 |T 59 63 62 60 67 56 59
WRMS | 3213 11 18 14 12 20 18 |NE 59 63 62 60 67 56 59
MEDI | 1559 12 16 15 12 18 16 |MD 51 45 51 47 54 43 50
Table 3.2392.3 GPS week: 2392 Day: 3 MJD: 60991
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R03 | 2367 7 18 19 10 16 24 7 | 41 29 52 44 42 24 37
R04 | 943 21 14 9 10 16 20 6 | 48 37 41 42 42 35 39
R05 | 838 16 9 16 15 13 22 7 | 60 57 49 57 65 62 56
R07 | 1571 19 25 14 9 15 15 7 | 46 26 37 40 36 34 34
R08 | 2166 12 10 20 6 16 19 6 | 46 50 41 49 49 38 44
R09 | 1224 11 16 11 13 23 9 6 | 60 66 62 53 66 52 59
R11 | 729 15 13 13 13 25 9 6 | 56 61 56 51 60 51 54
R12 | 826 16 14 13 9 18 32 7 | 97 90 94 87 92 74 89
R14 | 1770 7 14 11 17 31 17 7 | 88 94 88 81 118 83 90
R15 | 1029 20 20 24 20 17 20 9 | 97 83 108 75 98 73 88
R16 | 3520 20 17 14 21 25 20 8 | 96 97 87 73 102 74 86
R17 | 1475 13 27 10 27 21 19 9 | 39 56 45 48 36 47 42
R18 | 1218 14 18 12 15 21 27 8 | 51 58 48 53 52 60 51
XR19 | 2277 22 13 15 --- 20 --- 10 | 46 59 53 --- 48 --- 49
XR20 | 2948 10 --- 339 13 24 --- 11 | 30 --- 108 36 42 --- 34
R21 | 515 9 10 12 10 12 31 6 | 41 41 44 37 31 47 39
XR22 | 1890 11 14 10 11 18 --- 6 | 43 43 48 41 49 --- 42
R24 | 1525 13 23 16 15 21 29 8 | 46 56 49 43 34 54 45
XR26 | 9427 65 70 42 --- 68 --- 35 | 42 134 59 --- 122 --- 86
XR27 | 9756 52 51 --- 38 73 --- 30 | 65 126 --- 80 134 --- 96
XR28 |12559 45 --- --- --- 68 --- 56 | 76 --- --- --- 114 --- 90
------+-----------------------------------------+-------------------------------------
RMS | 1631 15 17 15 15 20 22 |T 57 66 61 55 68 53 59
WRMS | 1631 14 15 15 13 20 22 |NE 57 66 61 55 68 53 59
MEDI | 1571 15 16 14 13 21 20 |MD 48 58 52 49 52 52 51
Table 3.2392.4 GPS week: 2392 Day: 4 MJD: 60992
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R03 | 2390 7 17 13 12 20 17 6 | 43 42 40 37 58 32 41
R04 | 1495 18 21 19 12 12 20 7 | 52 39 49 39 42 38 42
R05 | 1491 13 15 8 9 13 19 6 | 43 39 36 41 43 35 38
R07 | 2622 10 23 30 12 12 22 8 | 40 35 61 38 36 28 38
R08 | 1910 16 18 12 8 14 7 6 | 42 30 42 36 42 42 38
R09 | 1340 13 12 18 12 12 16 6 | 36 34 40 26 40 44 35
R11 | 2175 11 22 16 24 16 9 7 | 46 63 63 38 56 44 51
R12 | 1285 16 20 14 29 19 16 8 | 88 91 78 69 90 72 81
R14 | 2476 9 17 11 10 13 20 6 | 82 87 94 91 93 73 87
R15 | 820 15 14 9 7 12 30 6 | 104 99 89 92 89 74 92
R16 | 3308 17 20 17 26 10 19 8 | 100 91 106 74 99 83 92
R17 | 969 10 15 10 15 12 32 7 | 33 34 33 30 35 37 32
R18 | 808 12 24 17 13 12 23 7 | 36 36 43 33 37 36 35
XR19 | 1796 13 19 17 --- 14 --- 9 | 32 29 40 --- 33 --- 32
XR20 | 4145 12 --- 350 17 23 --- 13 | 112 --- 133 112 99 --- 107
R21 | 579 10 16 9 14 11 19 6 | 44 35 39 43 50 33 42
XR22 | 1174 12 12 15 13 17 --- 7 | 35 43 47 37 43 --- 40
R24 | 1256 14 35 11 26 17 36 10 | 41 45 38 46 48 31 39
XR26 | 9620 50 105 33 --- 71 --- 38 | 45 133 74 --- 97 --- 64
XR27 | 7244 47 62 --- 42 55 --- 29 | 47 106 --- 62 93 --- 72
XR28 |12884 70 --- --- --- 75 --- 72 | 54 --- --- --- 183 --- 106
------+-----------------------------------------+-------------------------------------
RMS | 1828 13 20 15 17 14 22 |T 55 58 60 52 66 46 57
WRMS | 1828 13 19 15 16 14 22 |NE 55 58 60 52 66 46 57
MEDI | 1796 13 19 15 13 14 19 |MD 44 42 47 39 50 38 42
Table 3.2392.5 GPS week: 2392 Day: 5 MJD: 60993
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R03 | 2079 9 16 11 18 16 11 6 | 45 34 41 56 36 44 42
R04 | 1137 24 13 15 11 18 22 8 | 58 60 55 66 56 55 57
R05 | 1880 10 16 15 16 38 24 9 | 100 106 93 101 108 107 100
R07 | 1820 17 29 24 26 19 22 10 | 40 39 45 35 39 30 32
R08 | 1104 10 23 18 9 16 13 7 | 33 25 48 39 42 31 34
R09 | 2043 9 17 22 21 19 11 7 | 42 51 58 35 34 49 43
R11 | 3228 12 27 19 25 22 15 9 | 37 53 48 30 33 29 35
R12 | 2182 14 13 8 27 27 12 8 | 73 74 64 55 84 62 67
R14 | 2750 9 16 17 10 9 29 7 | 77 86 93 79 73 62 78
R15 | 1138 10 14 21 15 26 24 8 | 93 82 99 93 74 74 87
R16 | 2437 18 16 16 9 20 15 7 | 93 76 91 85 77 76 83
R17 | 1082 10 20 12 16 20 24 7 | 27 28 30 31 27 32 26
R18 | 892 14 18 13 9 14 19 6 | 28 33 21 28 24 25 25
XR19 | 1068 10 15 12 --- 21 --- 8 | 24 22 30 --- 26 --- 23
XR20 | 4513 9 --- 341 8 18 --- 8 | 100 --- 93 100 106 --- 102
R21 | 746 6 10 9 13 27 9 5 | 27 25 24 27 34 40 23
XR22 | 959 13 16 12 7 34 --- 8 | 17 25 28 28 32 --- 21
R24 | 1697 12 21 8 17 15 21 7 | 30 34 25 31 31 25 27
XR26 | 7440 43 84 50 --- 71 --- 35 | 34 101 36 --- 73 --- 56
XR27 |10034 45 63 --- 30 62 --- 29 | 60 110 --- 70 79 --- 75
XR28 |17672 63 --- --- --- 117 --- 85 | 43 --- --- --- 163 --- 70
------+-----------------------------------------+-------------------------------------
RMS | 1884 13 19 16 17 21 19 |T 51 56 53 54 59 49 52
WRMS | 1884 13 18 17 16 21 19 |NE 51 56 53 54 59 49 52
MEDI | 1880 12 16 15 15 20 19 |MD 42 51 48 39 42 44 43
Table 3.2392.6 GPS week: 2392 Day: 6 MJD: 60994
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R03 | 937 11 24 10 15 10 14 6 | 61 49 58 64 52 52 55
R04 | 1099 20 13 10 12 19 24 7 | 75 69 73 77 65 63 69
R05 | 3174 17 17 15 11 18 14 7 | 103 113 107 115 100 115 107
R07 | 1519 13 17 7 11 16 19 6 | 55 42 52 48 57 38 47
R08 | 1334 10 29 8 13 15 12 6 | 47 46 49 49 52 43 45
R09 | 2652 14 23 15 19 15 6 7 | 48 64 55 38 47 47 48
R11 | 1655 15 28 14 32 8 8 8 | 50 61 54 30 55 45 48
R12 | 2059 10 12 21 35 20 19 9 | 106 105 115 83 111 86 101
R14 | 2921 7 16 11 18 16 13 6 | 100 104 95 89 108 89 97
R15 | 811 23 11 12 17 21 21 8 | 122 105 112 107 96 90 106
R16 | 1734 15 17 14 12 19 19 7 | 120 99 116 109 100 97 107
R17 | 1165 8 18 9 14 11 21 6 | 38 46 40 36 40 44 38
R18 | 1033 13 19 9 18 15 13 6 | 47 42 43 45 43 47 43
XR19 | 1249 14 14 8 --- 16 --- 7 | 40 45 43 --- 49 --- 43
XR20 | 4755 11 --- 364 9 19 --- 10 | 123 --- 143 125 125 --- 123
XR21 | 845 17 21 9 11 11 --- 7 | 38 45 40 44 42 --- 39
XR22 | 2037 16 19 10 19 30 --- 9 | 37 38 45 37 48 --- 39
R24 | 3159 13 22 7 15 20 30 8 | 35 37 37 34 38 39 35
XR26 | 6469 43 63 40 --- 70 --- 30 | 59 142 68 --- 122 --- 86
XR27 | 8057 59 56 --- 51 75 --- 35 | 57 140 --- 64 134 --- 92
XR28 |17446 84 --- --- --- 96 --- 90 | 57 --- --- --- 139 --- 90
------+-----------------------------------------+-------------------------------------
RMS | 1979 14 20 12 19 16 18 |T 67 73 70 66 77 63 69
WRMS | 1979 14 19 12 16 16 18 |NE 67 73 70 66 77 63 69
MEDI | 1734 14 19 10 15 18 14 |MD 57 61 55 49 57 47 55
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