[IGSREPORT-30281] Wk 2348 IGLOS Final Orbits
acc
acc at igs.org
Fri Jan 24 02:00:21 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2348 (Jan 05, 2025 - Jan 11, 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 2.2348.
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:
igl2348[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2348 in the SP3 format.
igl23487.sum Combination Report for GPS Week 2348.
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.
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 | 2.4 ns
1 | 4.3 ns
2 | 11.4 ns
3 | 6.9 ns
4 | 2.5 ns
5 | 5.9 ns
6 | 9.2 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
----+--------+---------------
6 | IAC | R26
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 1.2348, 1a.2348).
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 2.2348.0-6)
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 3.2348.0-6).
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 2348 summary. (Jan 05, 2025 - Jan 11, 2025)
Table 1.2348.a GPS week : 2348 MJD: 60680.0-60686.0
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| 0 0 5 12 -4 70 .12 21 18 | 7357 -334 3311 8587
| 1 1 1 17 13 23 .05 | 2995 1234
esa n/a| -1 0 0 -15 -10 -2 -.08 33 23 | 13388 -748 3343 7469
| 1 1 2 10 20 31 .06 | 4429 1382
gfz n/a| 0 0 2 20 3 20 .08 26 16 | 0 -349 3354 7886
| 1 0 2 9 18 24 .08 | 0 1327
grg n/a| 3 0 0 -33 -36 -49 .32 24 20 | 5784 -338 3310 8122
| 1 1 2 32 15 62 .03 | 3119 1149
iac n/a| 0 0 -4 11 31 -15 -.13 17 15 | 6760 -64 3353 8527
| 0 1 1 24 25 45 .04 | 3667 904
jgx n/a| -1 0 0 -21 4 -15 -.23 24 24 | 9184 -334 3244 7951
| 1 1 1 17 15 25 .05 | 2827 1363
Table 1.2348.b GPS week : 2348 MJD: 60680.0-60686.0
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 | 16 14 18 14 17 15 17 |
R02 | 6 6 5 7 6 8 5 |
R03 | 6 6 7 6 6 6 7 |
R04 | 6 7 7 8 6 7 7 |
R05 | 6 7 8 7 6 7 7 |
R07 | 7 7 7 7 8 7 6 |
R08 | 6 8 8 8 7 7 8 |
R09 | 6 7 8 6 5 6 7 |
R11 | 10 11 9 8 10 8 11 |
R12 | 7 7 9 8 8 6 8 |
R14 | 5 8 7 6 7 7 6 |
R15 | 7 9 7 10 7 10 8 |
R16 | 8 7 8 8 8 7 9 |
R17 | 9 7 9 8 9 8 7 |
R18 | 7 8 8 7 6 8 7 |
R19 | 23 18 17 15 16 17 20 |
R20 | 27 23 26 30 28 24 23 |
R21 | 8 8 8 8 8 7 9 |
R22 | 6 6 7 6 7 8 7 |
R24 | 10 9 10 10 8 8 10 |
R26 | 36 39 41 35 39 55 19 |
Table 1.2348.c GPS week : 2348 MJD: 60680.0-60686.0
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 2348 0 | 51 -53 7 1485 941 8283 81.2 1166 1166 | 2398 0
brd 2348 1 | -16 37 -13 -39 538 -10420 81.8 1374 1374 | 4341 0
brd 2348 2 | 21 51 -105 -153 -25 -6199 80.7 1480 1480 | 11368 0
brd 2348 3 | 18 93 -65 -2687 3417 -4022 80.6 1270 1270 | 6886 0
brd 2348 4 | -29 -69 -9 1148 1619 3050 79.7 1551 1551 | 2529 0
brd 2348 5 | -100 -6 -106 378 297 1550 79.6 1731 1731 | 5884 0
brd 2348 6 | -29 36 -117 -176 2005 3891 78.1 2078 2078 | 9170 0
-------------+------------------------------------------------------------+----------------
brd 2348 mean| -12 12 -58 -6 1256 -552 80.2 1521 1521 | 6082 0
brd 2348 sdev| 49 58 52 1350 1192 6538 1.2 307 307 | 3351 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 2.2348.0 GPS week: 2348 Day: 0 MJD: 60680
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 3 6 -24 57 .15 21 19 | 4829 -2479 3360 8878
esa n/a| -1 1 -3 -6 -19 11 -.18 34 28 | 11227 -3612 3391 7790
gfz n/a| 1 0 6 18 37 18 -.03 32 17 | 0 -3083 3362 8174
grg n/a| 1 0 0 -73 -32 -8 .33 22 19 | 3299 -2655 3371 8460
iac n/a| -1 0 -2 57 39 -74 -.10 16 13 | 3175 -389 3349 8721
jgx n/a| 0 0 3 -34 -9 21 -.23 24 24 | 7862 -2824 3377 8255
Table 2.2348.1 GPS week: 2348 Day: 1 MJD: 60681
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 0 -17 74 .15 22 19 | 3966 854 3188 8761
esa n/a| -1 -1 -1 -15 19 -51 -.06 34 23 | 11563 36 3230 8496
gfz n/a| 0 0 1 15 -5 -12 .01 24 20 | 0 508 3229 8047
grg n/a| 4 0 0 -47 -47 23 .31 22 21 | 3543 486 3206 8345
iac n/a| 0 0 -2 20 39 -16 -.13 15 14 | 4167 1148 3205 8692
jgx n/a| 0 0 2 -7 4 13 -.17 22 22 | 6400 514 3199 8224
Table 2.2348.2 GPS week: 2348 Day: 2 MJD: 60682
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 5 19 -4 79 .11 20 16 | 11591 -5 3040 9246
esa n/a| -3 -1 0 -38 -9 35 -.15 33 21 | 20856 -232 3045 7866
gfz n/a| 0 1 0 36 -5 67 .14 28 19 | 0 -494 3060 8556
grg n/a| 3 0 -1 -24 -57 -171 .27 25 21 | 11115 -273 3027 8947
iac n/a| 0 0 -4 -8 41 30 -.17 17 16 | 12370 -1488 3028 9227
jgx n/a| 0 1 0 -8 9 -23 -.26 26 26 | 13952 -740 2957 8914
Table 2.2348.3 GPS week: 2348 Day: 3 MJD: 60683
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 8 26 14 63 .03 22 16 | 7727 937 3415 8261
esa n/a| 0 0 0 -13 -15 -25 -.03 31 20 | 15042 504 3497 7310
gfz n/a| 0 -1 2 6 8 2 .22 26 13 | 0 1001 3581 7557
grg n/a| 3 -1 -3 -43 -14 -66 .28 23 17 | 5862 878 3399 7830
iac n/a| 0 1 -6 23 1 50 -.18 19 18 | 7580 -242 3410 8097
jgx n/a| 0 -1 -1 -1 12 -52 -.29 25 25 | 9534 1515 3083 7653
Table 2.2348.4 GPS week: 2348 Day: 4 MJD: 60684
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 -1 5 27 5 29 .12 20 16 | 5166 -1467 3202 8171
esa n/a| 0 0 -1 -4 8 21 -.03 35 24 | 7436 -1088 3216 6738
gfz n/a| 0 0 5 27 8 24 .07 22 16 | 0 -627 3228 7326
grg n/a| 4 -2 -1 -55 -21 -69 .33 29 24 | 2502 -773 3194 7528
iac n/a| 0 1 -3 -1 -12 -3 -.12 16 14 | 3120 -30 3196 7944
jgx n/a| -1 0 0 -42 30 -31 -.16 26 27 | 6256 -907 3130 7206
Table 2.2348.5 GPS week: 2348 Day: 5 MJD: 60685
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 4 -18 1 102 .17 21 19 | 7253 -90 3208 7762
esa n/a| -1 0 3 -12 -41 -21 -.06 31 20 | 11019 71 3235 6461
gfz n/a| -2 0 0 20 -20 24 .08 23 14 | 0 137 3241 7212
grg n/a| 1 1 3 22 -34 -31 .35 24 24 | 5568 10 3200 7125
iac n/a| 0 -1 -4 -12 58 -32 -.07 14 13 | 6217 998 3336 7954
jgx n/a| -1 0 0 -17 -16 -11 -.28 26 26 | 8531 -80 3226 7242
Table 2.2348.6 GPS week: 2348 Day: 6 MJD: 60686
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 27 -5 90 .10 25 20 | 10972 -94 3770 9035
esa n/a| -1 -1 0 -16 -19 14 -.06 34 27 | 16579 -916 3792 7626
gfz n/a| 0 0 1 19 1 18 .08 24 13 | 0 110 3778 8330
grg n/a| 3 0 4 -9 -46 -24 .36 21 17 | 8602 -39 3773 8619
iac n/a| 0 -2 -7 0 48 -58 -.16 19 17 | 10691 -450 3949 9056
jgx n/a| -2 0 -1 -40 -1 -23 -.24 22 22 | 11754 182 3742 8163
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 3.2348.0 GPS week: 2348 Day: 0 MJD: 60680
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 716 26 48 48 36 29 26 15 | 85 94 106 90 83 89 85
XR02E | 1076 11 14 11 15 9 --- 6 | 59 62 61 63 57 --- 59
R03E | 1564 7 12 16 18 9 12 5 | 59 60 65 63 62 56 59
R04E | 1267 11 15 16 16 9 11 5 | 56 58 54 62 57 57 56
R05E | 701 13 10 9 21 7 11 5 | 49 47 48 61 48 46 49
R07E | 992 16 23 13 14 11 10 6 | 49 51 49 48 47 44 46
R08E | 755 14 12 16 9 10 15 5 | 67 61 76 64 67 58 65
R09 | 735 11 15 22 9 11 15 6 | 21 35 34 28 19 20 22
R11 | 1662 18 10 18 39 14 14 9 | 40 43 42 63 47 40 45
R12 | 1179 11 18 16 10 17 13 6 | 47 34 37 37 48 37 40
R14 | 1026 9 10 16 14 11 9 5 | 49 55 62 51 49 49 51
R15 | 804 27 12 17 6 11 16 7 | 55 42 48 47 48 38 44
R16 | 1080 26 12 19 13 14 17 8 | 60 53 57 52 54 47 52
R17 | 1375 18 17 13 15 15 29 8 | 75 58 67 68 67 54 64
R18 | 927 14 15 18 14 8 17 6 | 69 85 87 77 77 68 75
R19 | 1368 41 82 67 32 28 53 22 | 120 63 141 106 102 72 97
R20 | 1361 40 90 96 49 31 56 26 | 150 67 153 116 127 93 115
R21 | 794 13 29 19 15 16 19 8 | 61 46 67 58 63 44 55
R22 | 1788 14 10 9 16 14 9 5 | 35 34 37 50 32 39 36
R24 | 1159 20 35 16 16 12 26 9 | 82 53 69 78 75 58 69
XR26E |16235 46 --- --- 43 57 --- 35 | 49 --- --- 32 72 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1165 21 34 32 22 16 24 |T 63 55 68 62 61 53 58
WRMS | 1165 19 27 17 19 13 24 |NE 66 51 69 63 62 50 58
MEDI | 1080 14 15 16 15 12 15 |MD 59 53 61 62 57 49 55
Table 3.2348.1 GPS week: 2348 Day: 1 MJD: 60681
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1814 27 50 46 21 15 23 13 | 85 85 98 89 74 77 80
XR02E | 900 6 13 15 11 8 --- 5 | 58 57 56 60 56 --- 56
R03E | 2714 8 18 11 20 12 8 6 | 55 64 57 59 56 49 55
R04E | 1014 11 18 22 12 13 13 6 | 39 37 37 42 33 31 33
R05E | 746 10 14 18 19 14 13 6 | 41 40 46 48 42 38 40
R07E | 613 16 25 14 17 13 14 7 | 44 51 47 49 45 41 43
R08E | 690 13 15 27 25 13 12 8 | 65 65 67 74 60 68 64
R09 | 1825 13 13 22 14 14 16 7 | 16 19 26 15 16 19 13
R11 | 1132 15 29 17 39 20 14 10 | 28 43 29 77 44 29 39
R12 | 905 18 11 14 20 15 9 7 | 33 26 18 25 30 24 23
R14 | 646 6 9 32 15 9 19 7 | 29 33 53 33 29 22 31
R15 | 1116 26 11 23 16 13 20 8 | 32 24 39 34 21 22 24
R16 | 947 16 17 17 14 15 14 7 | 36 35 42 44 37 30 35
R17 | 1039 19 13 12 13 11 17 6 | 54 41 52 55 49 40 47
R18 | 725 17 21 14 17 9 22 7 | 65 86 80 74 73 68 72
R19 | 671 38 70 46 44 19 34 18 | 73 40 88 62 69 54 62
R20 | 2850 54 96 36 34 25 57 22 | 91 74 66 86 77 64 72
R21 | 501 14 27 24 8 9 22 8 | 56 42 63 56 52 45 51
R22 | 1564 13 16 10 11 16 11 6 | 28 35 34 40 34 30 31
R24 | 1369 28 24 13 18 14 19 8 | 68 44 45 67 53 43 52
XR26E |18647 43 --- --- 59 57 --- 38 | 40 --- --- 41 66 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1373 22 34 24 22 15 22 |T 49 47 52 53 48 41 45
WRMS | 1373 19 23 20 21 14 22 |NE 46 41 48 51 44 37 42
MEDI | 1014 16 17 17 17 14 16 |MD 44 41 47 55 49 40 43
Table 3.2348.2 GPS week: 2348 Day: 2 MJD: 60682
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 612 22 50 61 32 30 44 18 | 81 97 100 74 71 94 78
XR02E | 1564 7 13 14 11 9 --- 5 | 49 46 52 53 46 --- 48
R03E | 3549 9 18 19 13 16 12 6 | 50 54 61 62 56 47 53
R04E | 1086 10 25 14 15 14 18 7 | 42 45 48 46 42 43 41
R05E | 726 14 16 17 21 22 15 8 | 49 52 52 61 49 47 49
R07E | 756 13 17 15 20 9 16 6 | 66 51 54 75 53 53 57
R08E | 615 15 20 27 20 15 11 8 | 80 78 88 90 72 75 79
R09 | 1521 19 23 16 11 14 14 7 | 22 31 27 24 18 25 19
R11 | 807 11 12 26 25 13 24 8 | 29 32 52 33 38 28 33
R12 | 1169 17 11 13 28 18 24 8 | 39 28 43 31 43 24 33
R14 | 1227 8 16 11 21 13 18 6 | 34 41 38 47 43 35 38
R15 | 1523 11 18 15 16 11 20 6 | 38 42 47 54 39 43 42
R16 | 601 16 23 21 12 14 12 7 | 47 44 45 49 40 48 43
R17 | 909 21 15 25 20 15 16 8 | 102 90 107 86 89 91 93
R18 | 656 9 23 19 10 10 30 8 | 71 85 66 76 70 54 68
R19 | 737 33 64 33 50 13 37 17 | 108 81 102 80 95 90 91
R20 | 2871 55 95 67 48 26 63 26 | 101 50 104 75 91 50 75
R21 | 499 15 21 13 13 15 25 7 | 55 56 53 55 60 51 54
R22 | 2137 14 15 16 13 14 14 6 | 28 36 36 32 22 34 28
R24 | 1614 18 25 12 37 19 23 10 | 80 66 73 77 71 73 71
XR26E |24620 47 --- --- 53 66 --- 40 | 51 --- --- 52 58 --- 43
------+-----------------------------------------+-------------------------------------
RMS | 1480 20 33 28 25 17 26 |T 58 55 62 58 55 52 54
WRMS | 1480 16 21 19 21 16 26 |NE 58 52 61 55 55 49 52
MEDI | 1086 15 18 16 20 14 18 |MD 50 50 52 55 53 48 49
Table 3.2348.3 GPS week: 2348 Day: 3 MJD: 60683
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 771 27 40 44 15 27 31 14 | 81 62 93 69 73 61 70
XR02E | 1595 7 16 13 16 9 --- 6 | 38 37 38 44 34 --- 36
R03E | 1204 9 18 12 17 15 8 6 | 46 45 46 50 42 36 43
R04E | 897 14 23 15 15 19 11 7 | 53 64 54 53 42 55 51
R05E | 914 10 16 18 14 15 14 6 | 44 50 44 50 46 41 44
R07E | 759 14 15 10 14 19 16 7 | 47 44 43 44 44 38 41
R08E | 1255 23 25 15 14 11 20 8 | 58 47 45 59 54 53 51
R09 | 1268 11 5 5 12 13 20 5 | 18 19 24 22 22 34 20
R11 | 747 11 10 20 28 16 15 8 | 30 39 42 53 33 30 33
R12 | 1311 12 8 18 18 19 26 8 | 37 39 49 32 44 27 35
R14 | 1773 12 9 10 16 12 16 5 | 39 49 51 40 51 56 46
R15 | 2305 10 16 19 14 32 32 10 | 47 44 35 56 68 30 45
R16 | 788 16 18 25 14 19 16 8 | 52 49 45 57 64 45 50
R17 | 1051 19 15 19 18 17 17 8 | 76 60 70 58 69 57 64
R18 | 915 8 19 16 8 12 22 6 | 90 83 95 91 84 87 88
R19 | 884 31 54 36 33 19 22 15 | 98 88 88 97 82 87 85
R20 | 2244 57 96 75 63 37 71 30 | 113 64 129 61 97 63 81
R21 | 732 15 22 16 18 18 20 8 | 84 74 83 72 89 61 77
R22 | 1657 15 14 11 15 12 12 6 | 30 44 42 38 36 39 36
R24 | 892 32 26 15 24 13 18 10 | 99 70 85 69 84 68 78
XR26E |30856 46 --- --- 32 64 --- 35 | 41 --- --- 33 53 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 1270 22 31 26 23 19 25 |T 58 53 60 54 57 50 52
WRMS | 1270 16 20 13 17 18 25 |NE 62 55 64 57 63 52 56
MEDI | 1051 14 16 16 16 17 18 |MD 47 49 46 53 53 53 46
Table 3.2348.4 GPS week: 2348 Day: 4 MJD: 60684
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 924 28 58 35 23 38 41 17 | 57 81 71 58 45 70 54
XR02E | 740 8 16 11 18 12 --- 6 | 49 45 52 54 53 --- 50
R03E | 1519 7 19 12 19 14 12 6 | 47 53 52 57 51 48 49
R04E | 1662 14 15 13 9 9 14 5 | 33 33 40 41 40 30 35
R05E | 1501 11 20 9 15 13 15 6 | 40 43 45 48 45 40 42
R07E | 850 9 14 24 21 15 19 8 | 66 66 78 79 55 62 65
R08E | 1232 18 19 12 12 9 20 7 | 64 58 66 67 62 51 61
R09 | 778 13 10 9 15 10 13 5 | 22 20 15 29 18 20 18
R11 | 1620 17 30 20 37 13 12 9 | 37 19 41 22 40 38 30
R12 | 1025 12 12 14 38 14 9 8 | 34 35 38 26 38 34 32
R14 | 1355 11 11 19 21 17 14 7 | 36 48 44 35 52 34 41
R15 | 1418 16 16 18 13 11 20 7 | 44 38 26 45 45 29 37
R16 | 925 19 18 20 18 17 18 8 | 45 34 31 51 52 30 40
R17 | 1513 19 22 13 25 16 24 8 | 74 65 74 67 76 59 68
R18 | 1772 7 16 11 12 12 20 6 | 51 55 50 50 50 43 48
R19 | 1316 38 59 31 34 17 38 16 | 96 75 87 85 81 78 79
R20 | 3329 48 103 53 86 22 73 28 | 97 72 105 120 75 59 80
R21 | 1620 13 19 17 21 9 24 7 | 107 102 112 112 109 96 106
R22 | 2106 15 22 11 19 18 10 7 | 24 41 35 32 29 32 28
R24 | 991 14 26 19 12 13 20 7 | 80 68 86 76 81 72 77
XR26E |40118 53 --- --- 49 58 --- 38 | 50 --- --- 49 73 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1551 20 35 22 29 16 26 |T 54 52 57 57 55 48 51
WRMS | 1551 16 24 16 24 14 27 |NE 57 51 57 57 57 48 52
MEDI | 1418 14 19 14 19 14 19 |MD 49 48 50 51 52 43 48
Table 3.2348.5 GPS week: 2348 Day: 5 MJD: 60685
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1651 24 55 41 17 25 40 15 | 64 55 82 61 52 56 56
XR02E | 843 11 18 18 13 15 --- 7 | 47 49 48 54 46 --- 46
R03E | 1669 10 12 20 12 7 14 5 | 57 53 59 58 53 47 53
R04E | 1965 12 18 11 22 11 16 6 | 39 44 42 50 44 37 41
R05E | 1217 15 20 23 15 8 14 7 | 50 59 56 52 54 49 51
R07E | 872 11 20 16 16 13 14 6 | 54 58 60 58 48 43 51
R08E | 921 16 14 16 20 10 13 6 | 51 52 53 55 45 49 48
R09 | 754 11 11 11 19 6 14 5 | 15 20 23 27 13 14 14
R11 | 1482 11 18 13 31 11 15 7 | 17 21 22 45 24 22 22
R12 | 1314 13 13 9 20 12 9 6 | 26 22 21 16 27 22 21
R14 | 793 12 14 20 21 11 17 7 | 32 42 49 32 44 27 38
R15 | 1136 24 20 13 18 17 35 9 | 43 33 37 34 47 23 35
R16 | 713 22 14 17 11 10 16 7 | 43 42 45 38 42 36 40
R17 | 1180 25 12 16 14 12 20 7 | 102 91 87 95 92 94 92
R18 | 1844 13 14 15 19 21 21 8 | 78 80 73 86 88 75 79
R19 | 2607 41 58 25 28 27 46 16 | 107 82 84 93 97 73 89
R20 | 3883 38 86 61 61 13 66 24 | 81 48 92 84 59 52 65
R21 | 1245 20 16 12 13 7 18 6 | 69 64 65 61 65 59 63
R22 | 2684 22 23 15 24 10 12 7 | 21 27 32 34 26 23 22
R24 | 1450 18 21 10 28 8 19 7 | 57 46 51 66 48 47 51
XR26E |51425 71 --- --- 87 76 --- 55 | 39 --- --- 38 166 --- 54
------+-----------------------------------------+-------------------------------------
RMS | 1731 21 31 23 24 14 26 |T 52 49 54 54 56 44 49
WRMS | 1731 19 20 14 24 13 26 |NE 53 47 52 54 51 43 48
MEDI | 1314 16 18 16 19 11 16 |MD 50 48 51 54 48 47 51
Table 3.2348.6 GPS week: 2348 Day: 6 MJD: 60686
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1590 28 71 43 25 26 31 17 | 75 92 102 75 77 74 76
XR02E | 1553 10 11 10 9 11 --- 5 | 72 66 72 71 64 --- 68
R03E | 2403 17 17 21 12 10 10 6 | 75 78 88 79 75 73 77
R04E | 1762 9 23 12 15 14 12 6 | 52 51 53 61 54 48 52
R05E | 1365 13 17 17 15 18 12 7 | 54 54 63 64 60 52 56
R07E | 535 11 19 13 11 11 12 5 | 56 55 59 57 55 54 54
R08E | 712 27 19 13 14 15 9 7 | 77 70 74 70 66 67 69
R09 | 588 18 10 23 9 13 8 6 | 20 23 35 24 20 17 19
R11 | 1015 17 15 10 40 18 27 10 | 32 29 36 48 41 27 33
R12 | 807 22 11 23 12 19 13 7 | 40 33 40 25 41 27 31
R14 | 1218 8 12 9 15 10 18 5 | 48 55 52 42 54 58 50
R15 | 1147 19 11 16 14 17 25 8 | 56 41 50 41 55 30 44
R16 | 728 26 18 17 15 15 28 9 | 59 54 52 46 53 35 47
R17 | 719 18 18 12 12 14 19 7 | 89 77 81 84 82 77 80
R18 | 1087 13 18 13 14 13 17 6 | 81 82 80 90 85 67 80
R19 | 2403 53 76 43 26 40 27 20 | 127 81 111 100 115 87 100
R20 | 6746 48 83 56 42 32 52 23 | 122 60 124 108 76 87 91
R21 | 568 30 17 14 25 17 13 9 | 107 87 97 89 96 82 91
R22 | 2752 20 15 13 10 19 11 6 | 26 32 28 29 25 21 23
R24 | 1319 18 25 24 24 18 25 10 | 88 65 87 92 74 71 79
XR26E |69089 20 --- --- 17 473 --- 18 | 58 --- --- 51 231 --- 60
------+-----------------------------------------+-------------------------------------
RMS | 2078 25 34 24 21 19 22 |T 67 59 69 64 71 55 60
WRMS | 2078 20 27 13 17 17 22 |NE 68 55 67 62 62 52 59
MEDI | 1218 18 17 14 15 17 17 |MD 59 55 63 64 64 58 60
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