[IGSREPORT-30042] Wk 2326 IGLOS Final Orbits
acc
acc at igs.org
Mon Aug 26 07:55:18 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2326 (Aug 04, 2024 - Aug 10, 2024)
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 2.2326.
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:
igl2326[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2326 in the SP3 format.
igl23267.sum Combination Report for GPS Week 2326.
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 | 7.8 ns
1 | 7.6 ns
2 | 6.4 ns
3 | 5.7 ns
4 | 5.3 ns
5 | 4.3 ns
6 | 6.9 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2326, 1a.2326).
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 2.2326.0-6)
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 3.2326.0-6).
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 2326 summary. (Aug 04, 2024 - Aug 10, 2024)
Table 1.2326.a GPS week : 2326 MJD: 60526.0-60532.0
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 1 -14 40 .11 17 14 | 604 -430 3273 9833
| 0 0 1 13 16 11 .03 | 889 1114
esa n/a| -1 0 5 -9 22 -1 -.15 31 22 | 8453 179 3287 8106
| 1 1 1 7 16 38 .05 | 4256 1153
gfz n/a| 0 0 -2 37 4 -14 -.07 29 16 | 0 -563 3274 8283
| 0 0 2 17 16 27 .07 | 0 1521
grg n/a| 1 0 5 -28 8 -26 .43 23 17 | 5938 -648 3272 8955
| 1 1 2 11 23 56 .08 | 1457 1410
iac n/a| 0 0 -7 -1 -5 -14 -.16 19 16 | 7206 -429 3258 9578
| 0 1 1 23 21 65 .05 | 1461 1026
jgx n/a| 0 0 -1 -4 -5 -2 -.18 26 26 | 4694 -583 3275 8445
| 1 0 1 17 17 31 .05 | 1315 1389
Table 1.2326.b GPS week : 2326 MJD: 60526.0-60532.0
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 | 22 20 17 16 16 18 22 |
R02 | 7 8 7 6 8 7 10 |
R03 | 9 8 8 7 7 7 6 |
R04 | 8 8 6 6 6 6 7 |
R05 | 7 7 7 7 7 7 7 |
R07 | 8 8 8 9 9 8 8 |
R08 | 7 8 8 7 10 8 7 |
R09 | 7 6 6 6 6 5 7 |
R11 | 8 7 8 7 8 7 7 |
R12 | 9 7 7 8 6 6 6 |
R14 | 7 6 6 6 5 5 5 |
R15 | 7 7 5 5 6 6 7 |
R16 | 9 9 8 7 6 8 6 |
R17 | 7 8 7 6 6 7 7 |
R18 | 7 7 6 7 6 5 6 |
R19 | 16 16 15 20 18 17 15 |
R20 | 27 25 32 27 28 26 28 |
R21 | 8 7 8 10 7 7 8 |
R22 | 7 7 6 6 6 5 6 |
R24 | 8 7 8 11 10 9 10 |
R25 | 12 10 8 9 8 9 13 |
R26 | 34 34 37 38 32 36 37 |
Table 1.2326.c GPS week : 2326 MJD: 60526.0-60532.0
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 2326 0 | -41 -28 -5 -238 215 7112 80.8 1364 1364 | 7752 0
brd 2326 1 | 0 -33 5 -701 2443 7929 80.7 1444 1444 | 7627 0
brd 2326 2 | -7 -50 62 301 3023 4415 82.1 1409 1409 | 6407 0
brd 2326 3 | -104 2 18 -152 3047 5261 80.8 1689 1689 | 5726 0
brd 2326 4 | -23 25 -14 1743 121 -3974 82.8 1829 1829 | 5311 0
brd 2326 5 | -40 -14 114 901 576 -3679 81.8 1672 1672 | 4259 0
brd 2326 6 | 47 81 101 -697 390 -388 81.8 1543 1543 | 6884 0
-------------+------------------------------------------------------------+----------------
brd 2326 mean| -24 -2 40 165 1402 2382 81.5 1564 1564 | 6280 0
brd 2326 sdev| 46 44 52 895 1364 5006 .8 171 171 | 1270 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 2.2326.0 GPS week: 2326 Day: 0 MJD: 60526
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 -4 28 .11 19 16 | 1910 -659 3198 9918
esa n/a| -2 -1 7 -1 7 -45 -.21 32 26 | 12003 283 3214 8975
gfz n/a| 2 0 -5 34 5 -38 -.14 27 17 | 0 -1743 3122 8837
grg n/a| 2 -2 6 -34 29 -25 .42 25 18 | 8126 -1537 3099 8566
iac n/a| 0 1 -9 -28 -12 54 -.15 18 14 | 8742 113 3184 9832
jgx n/a| -2 0 0 1 17 -24 -.19 28 27 | 7365 -1736 3091 9152
Table 2.2326.1 GPS week: 2326 Day: 1 MJD: 60527
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 2 -21 -20 53 .07 18 13 | 1362 -567 3642 8780
esa n/a| -2 1 3 -10 16 17 -.21 34 23 | 14344 317 3696 7763
gfz n/a| 0 0 -4 65 2 7 -.14 25 17 | 0 -260 3701 7929
grg n/a| 0 0 6 -29 28 -6 .32 21 16 | 7156 -437 3642 7955
iac n/a| -1 -2 -9 -1 -8 -116 -.10 20 16 | 8976 -593 3638 8693
jgx n/a| 0 0 0 11 -14 18 -.14 23 23 | 4944 -227 3742 8058
Table 2.2326.2 GPS week: 2326 Day: 2 MJD: 60528
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 2 0 4 13 23 .11 17 14 | -760 549 3608 10027
esa n/a| -2 0 6 -10 6 11 -.12 33 23 | 4419 1040 3649 7998
gfz n/a| 0 0 -1 27 -14 7 -.02 32 17 | 0 845 3726 8494
grg n/a| 2 0 6 -14 23 -35 .35 22 15 | 5467 745 3689 9321
iac n/a| -1 0 -6 12 -21 -41 -.13 19 16 | 6837 -173 3604 9585
jgx n/a| 0 0 -1 -25 -21 44 -.22 25 25 | 3067 713 3684 8580
Table 2.2326.3 GPS week: 2326 Day: 3 MJD: 60529
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 2 13 -16 34 .15 19 15 | 740 531 3179 9742
esa n/a| -1 0 4 0 14 -7 -.09 28 18 | 8131 757 3188 7463
gfz n/a| 1 0 0 47 10 -53 -.15 30 16 | 0 386 3231 8494
grg n/a| 3 0 0 -44 24 28 .50 21 15 | 5027 391 3225 8839
iac n/a| 0 1 -5 -29 -18 -9 -.23 19 17 | 7337 -1060 3159 9496
jgx n/a| 0 0 -1 13 -21 -4 -.16 28 28 | 4493 424 3218 8552
Table 2.2326.4 GPS week: 2326 Day: 4 MJD: 60530
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 5 -11 44 .12 17 14 | 585 644 3065 10133
esa n/a| 0 -2 6 -9 24 -24 -.13 29 20 | 11392 1132 3038 8329
gfz n/a| 0 0 -2 12 -20 -17 .01 33 19 | 0 1280 3019 8185
grg n/a| 1 1 5 -29 -27 34 .48 25 19 | 4340 816 3081 9140
iac n/a| 0 -1 -6 -6 34 -57 -.15 17 13 | 6136 133 3038 9882
jgx n/a| 1 0 -2 10 -16 14 -.11 25 25 | 4518 981 3060 8306
Table 2.2326.5 GPS week: 2326 Day: 5 MJD: 60531
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 0 -13 -38 49 .11 16 13 | -158 -1110 2949 10863
esa n/a| -1 -1 5 -14 50 -32 -.11 29 21 | 2994 -14 2949 9615
gfz n/a| 0 0 -2 51 16 -26 -.01 26 13 | 0 -1681 2817 9203
grg n/a| 0 2 7 -10 -15 -49 .50 23 18 | 4549 -1649 2844 9998
iac n/a| 0 1 -5 4 14 76 -.23 20 15 | 4789 878 2935 10578
jgx n/a| 0 0 -2 -20 17 -47 -.21 22 22 | 4086 -1756 2831 9298
Table 2.2326.6 GPS week: 2326 Day: 6 MJD: 60532
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 15 -24 50 .10 15 12 | 550 -2399 3272 9370
esa n/a| 0 0 6 -20 38 67 -.19 30 25 | 5891 -2257 3278 6601
gfz n/a| 0 0 0 25 28 20 -.06 27 13 | 0 -2773 3308 6845
grg n/a| 0 1 7 -36 -6 -132 .48 23 17 | 6905 -2870 3325 8868
iac n/a| 0 1 -8 35 -24 -9 -.15 21 17 | 7627 -2302 3253 8985
jgx n/a| 0 0 -3 -23 3 -19 -.25 31 31 | 4388 -2484 3299 7174
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 3.2326.0 GPS week: 2326 Day: 0 MJD: 60526
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1595 40 97 26 23 33 48 21 | 110 33 93 91 93 51 78
R02 | 1536 9 11 14 15 17 18 6 | 45 45 52 52 51 38 46
R03 | 670 15 21 26 12 17 25 8 | 64 50 73 59 56 45 56
R04 | 786 13 15 12 15 12 29 7 | 72 65 70 70 67 54 65
R05 | 1047 18 12 10 23 12 21 7 | 75 55 64 56 67 54 61
R07 | 693 23 9 13 20 14 23 8 | 75 59 62 59 61 48 60
R08 | 649 14 12 15 23 14 17 7 | 62 55 68 56 64 48 57
R09 | 713 18 16 16 14 15 16 7 | 50 58 63 59 58 51 55
R11 | 1271 7 15 14 11 19 29 7 | 61 63 57 60 66 54 58
R12 | 1087 15 21 15 18 18 35 9 | 41 52 36 48 47 44 42
R14 | 1256 13 11 18 11 19 13 6 | 47 46 45 45 45 43 44
R15 | 1213 15 12 19 9 16 19 7 | 56 52 51 53 46 50 50
R16 | 1863 18 17 24 11 14 27 8 | 54 58 54 51 46 61 50
R17E | 980 8 18 13 24 13 15 7 | 86 81 85 96 84 82 85
R18E | 1017 11 16 16 19 13 11 6 | 36 38 34 46 33 33 34
R19E | 1015 25 50 47 33 26 33 16 | 42 54 83 54 43 48 44
R20E | 1137 39 68 79 71 29 68 26 | 57 76 97 59 52 61 53
R21E | 1276 14 26 21 21 11 12 8 | 87 85 94 94 89 92 89
R22E | 3558 15 16 15 19 15 11 7 | 24 28 37 39 32 27 29
R24E | 891 13 24 21 25 9 16 8 | 136 135 135 144 134 139 136
XR25E |16599 15 21 --- --- 12 --- 11 | 27 39 --- --- 31 --- 31
XR26 |20112 43 --- --- 35 59 --- 34 | 92 --- --- 96 122 --- 101
------+-----------------------------------------+-------------------------------------
RMS | 1364 19 32 27 25 18 28 |T 63 58 67 66 63 56 60
WRMS | 1364 16 26 17 18 14 27 |NE 64 53 60 61 63 49 58
MEDI | 1087 15 16 16 19 15 19 |MD 57 55 63 59 56 50 55
Table 3.2326.1 GPS week: 2326 Day: 1 MJD: 60527
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1762 44 91 39 20 19 30 19 | 83 44 80 50 51 39 54
R02 | 1025 7 10 15 22 21 19 7 | 31 31 37 37 40 22 30
R03 | 1234 7 23 24 17 18 20 8 | 40 33 55 36 49 29 38
R04 | 878 12 16 16 13 18 30 8 | 44 40 50 47 49 30 41
R05 | 1024 12 17 17 11 11 20 6 | 52 40 48 54 48 36 45
R07 | 560 16 14 14 15 16 28 8 | 54 44 51 47 50 29 44
R08 | 584 12 11 17 21 17 19 7 | 48 43 47 37 48 34 41
R09 | 1345 6 13 15 7 19 10 5 | 45 52 53 48 53 42 47
R11 | 870 12 18 14 9 17 15 6 | 48 50 53 52 55 46 49
R12 | 784 8 13 17 18 16 16 6 | 23 30 32 36 26 22 25
R14 | 1816 9 12 21 13 13 10 6 | 31 26 36 28 21 31 27
R15 | 1688 11 12 10 17 13 19 6 | 36 31 26 32 22 39 29
R16 | 1031 15 22 29 14 17 24 9 | 34 33 29 39 19 41 27
R17E | 819 8 21 21 26 12 8 7 | 81 85 78 86 74 77 79
R18E | 893 12 19 14 15 16 13 6 | 35 37 38 39 29 32 33
R19E | 1258 31 45 52 26 25 28 15 | 50 57 80 58 43 57 49
R20E | 2628 40 87 59 49 54 56 25 | 54 94 81 62 58 49 50
R21E | 1896 11 25 21 17 10 10 7 | 70 69 80 79 69 77 73
R22E | 2853 13 16 11 25 17 10 7 | 21 27 27 34 26 24 23
R24E | 1200 12 21 15 19 11 10 6 | 103 110 101 101 105 104 103
XR25E |14672 12 12 --- --- 17 --- 10 | 20 23 --- --- 20 --- 19
XR26 |17785 39 --- --- 30 67 --- 33 | 68 --- --- 74 80 --- 71
------+-----------------------------------------+-------------------------------------
RMS | 1443 18 34 25 21 20 23 |T 48 47 54 51 47 43 45
WRMS | 1443 13 23 17 16 16 23 |NE 45 38 45 44 43 33 40
MEDI | 1200 12 17 17 17 17 19 |MD 45 40 50 47 48 36 41
Table 3.2326.2 GPS week: 2326 Day: 2 MJD: 60528
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1374 26 80 29 22 27 28 16 | 78 30 69 69 79 44 60
R02 | 917 8 10 12 22 23 13 7 | 37 35 37 34 48 33 35
R03 | 1336 11 21 15 23 12 22 7 | 49 32 43 59 45 30 42
R04 | 979 7 13 18 10 11 16 5 | 50 54 65 55 55 51 53
R05 | 1196 9 15 16 18 12 16 6 | 50 45 59 56 50 44 49
R07 | 721 15 21 21 13 16 24 8 | 58 41 59 48 58 38 49
R08 | 845 10 17 24 14 19 23 8 | 47 43 56 40 49 36 43
R09 | 1366 14 16 18 8 7 10 5 | 38 44 49 44 40 44 41
R11 | 1323 19 24 16 10 15 14 7 | 47 49 53 45 49 43 46
R12 | 678 13 13 20 18 14 13 7 | 30 38 41 34 22 35 29
R14 | 1446 9 7 10 14 16 17 6 | 39 46 41 51 49 34 42
R15 | 1877 7 14 16 11 13 10 5 | 44 45 52 47 42 41 44
R16 | 961 23 32 21 10 10 8 8 | 46 43 42 38 37 37 36
R17E | 960 10 21 11 21 13 8 6 | 55 61 54 47 52 53 51
R18E | 698 12 17 13 14 11 13 6 | 35 38 34 39 30 34 33
R19E | 1553 25 45 50 17 31 28 14 | 44 44 68 46 48 42 40
R20E | 3094 35 85 112 66 49 82 32 | 55 89 135 55 60 61 57
R21E | 1810 18 26 18 19 10 16 8 | 67 66 64 69 63 62 63
R22E | 1380 14 10 12 14 11 12 5 | 32 33 38 48 31 38 35
R24E | 1529 19 19 13 25 11 16 8 | 127 124 125 142 132 120 128
XR25E | 9696 10 14 --- --- 8 --- 7 | 22 26 --- --- 23 --- 23
XR26 |15140 41 --- --- 34 71 --- 36 | 88 --- --- 80 106 --- 87
------+-----------------------------------------+-------------------------------------
RMS | 1408 17 33 32 22 19 25 |T 51 48 59 54 53 46 49
WRMS | 1408 14 23 17 15 16 25 |NE 50 41 51 50 52 39 46
MEDI | 1336 13 17 16 17 13 16 |MD 47 44 53 48 49 41 43
Table 3.2326.3 GPS week: 2326 Day: 3 MJD: 60529
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 833 26 69 44 24 9 31 16 | 80 27 96 82 61 42 62
R02 | 900 8 10 12 12 20 16 6 | 50 49 51 49 61 38 49
R03 | 1506 18 18 9 17 10 19 7 | 62 41 45 64 48 38 49
R04 | 1212 10 11 14 12 10 20 5 | 55 48 57 60 48 43 51
R05 | 1365 7 18 20 11 13 22 7 | 56 52 71 63 63 45 57
R07 | 523 21 17 11 11 18 30 8 | 66 47 54 61 64 38 55
R08 | 622 8 15 24 10 13 25 7 | 55 53 68 59 55 42 54
R09 | 1798 10 14 16 12 9 11 5 | 21 18 20 19 20 21 17
R11 | 808 22 13 18 12 13 8 6 | 29 15 25 20 25 18 19
R12 | 1281 13 22 20 19 14 14 7 | 36 32 37 41 31 23 30
R14 | 1224 6 10 16 18 15 13 6 | 35 32 32 44 39 30 34
R15 | 1002 9 15 13 13 9 9 5 | 42 56 48 48 40 45 45
R16 | 1147 15 19 21 13 11 10 6 | 46 54 59 43 44 47 45
R17E | 1250 8 19 14 15 9 11 5 | 42 48 47 50 37 41 42
R18E | 962 10 20 15 18 14 18 7 | 30 39 26 41 31 31 31
R19E | 2707 35 40 77 18 31 58 20 | 46 43 88 51 32 49 41
R20E | 4359 40 66 69 56 52 85 27 | 49 48 84 56 48 39 41
R21E | 2167 22 25 18 27 20 16 10 | 47 46 43 56 37 44 40
R22E | 2045 17 15 19 10 10 9 6 | 26 32 39 39 35 34 32
R24E | 1493 24 22 22 29 27 15 10 | 105 103 105 126 98 107 105
XR25E |11428 10 13 --- --- 13 --- 8 | 19 29 --- --- 25 --- 23
XR26 |13038 49 --- --- 32 70 --- 38 | 37 --- --- 61 93 --- 61
------+-----------------------------------------+-------------------------------------
RMS | 1689 19 28 30 21 19 28 |T 47 43 54 53 47 40 44
WRMS | 1689 15 18 16 15 17 28 |NE 47 40 51 51 49 36 44
MEDI | 1250 13 18 18 15 13 16 |MD 46 46 48 51 40 39 42
Table 3.2326.4 GPS week: 2326 Day: 4 MJD: 60530
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 650 35 65 30 35 22 28 16 | 87 38 79 85 59 48 62
R02 | 1136 9 14 23 15 8 29 7 | 61 47 70 65 52 37 54
R03 | 2025 15 13 18 15 7 18 6 | 61 43 64 57 51 40 52
R04 | 897 10 12 9 15 14 17 6 | 60 55 52 53 53 45 52
R05 | 1377 8 15 18 15 13 20 6 | 62 60 73 63 67 48 61
R07 | 618 10 28 26 16 16 21 8 | 73 60 86 67 81 58 70
R08 | 942 14 21 37 13 18 33 10 | 57 55 93 78 78 47 65
R09 | 1796 12 14 21 19 12 4 6 | 37 43 52 45 35 37 38
R11 | 1088 22 12 25 16 10 10 7 | 50 44 45 41 40 43 42
R12 | 1696 14 18 15 14 7 12 6 | 28 26 23 31 24 19 22
R14 | 1525 9 11 15 8 9 9 4 | 34 37 38 33 27 35 32
R15 | 1068 11 8 19 17 11 15 6 | 38 44 37 46 44 35 39
R16 | 1194 12 18 17 9 7 10 5 | 39 55 57 41 45 37 43
R17E | 932 7 22 12 19 7 14 6 | 50 53 44 43 47 37 44
R18E | 1044 7 16 19 16 12 10 6 | 29 32 28 37 31 26 28
R19E | 3647 21 50 67 28 38 35 17 | 35 45 79 36 45 30 34
R20E | 4285 34 68 94 75 42 75 27 | 50 55 117 49 60 41 48
R21E | 1832 14 26 16 20 10 14 7 | 43 52 50 48 46 49 45
R22E | 2386 14 17 17 19 8 7 6 | 22 33 25 36 22 22 23
R24E | 1485 18 29 24 38 9 12 9 | 125 130 123 125 118 123 122
XR25E |13834 10 16 --- --- 8 --- 8 | 16 27 --- --- 21 --- 20
XR26 |10376 41 --- --- 38 52 --- 32 | 88 --- --- 89 93 --- 90
------+-----------------------------------------+-------------------------------------
RMS | 1828 17 29 33 25 17 25 |T 52 49 61 55 51 42 49
WRMS | 1828 14 20 19 19 13 25 |NE 55 46 59 56 53 40 51
MEDI | 1377 12 17 19 16 10 14 |MD 50 45 52 48 46 37 44
Table 3.2326.5 GPS week: 2326 Day: 5 MJD: 60531
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 753 29 73 36 27 15 46 17 | 71 35 80 70 54 37 55
R02 | 769 8 20 18 17 11 17 6 | 51 44 59 44 47 40 46
R03 | 2699 14 15 15 16 12 22 7 | 55 43 54 55 38 36 46
R04 | 959 14 13 8 14 11 16 5 | 53 51 44 48 46 45 47
R05 | 890 11 12 11 22 16 12 6 | 58 52 48 53 55 45 51
R07 | 845 16 21 10 15 18 22 7 | 57 49 51 54 62 42 52
R08 | 728 11 24 24 16 16 15 8 | 49 42 65 57 58 45 51
R09 | 2072 10 7 11 11 13 10 4 | 43 50 51 40 52 48 46
R11 | 1081 18 15 13 14 17 14 7 | 46 45 43 48 42 39 42
R12 | 1973 10 14 17 19 9 15 6 | 25 29 24 32 21 30 24
R14 | 1449 12 12 11 10 10 11 5 | 30 27 27 25 24 22 24
R15 | 1631 8 11 18 15 17 14 6 | 32 30 30 41 40 28 31
R16 | 1270 11 31 19 18 14 11 7 | 32 56 29 32 40 25 32
R17E | 771 8 20 14 24 15 12 7 | 70 63 68 80 60 65 66
R18E | 1420 6 16 11 16 11 8 5 | 34 35 30 43 32 29 32
R19E | 1617 29 51 43 26 41 33 16 | 35 77 69 51 43 55 46
R20E | 3585 31 61 83 66 53 57 26 | 61 80 127 63 74 55 57
R21E | 1443 10 20 18 23 12 12 7 | 76 68 79 87 71 78 75
R22E | 2128 12 11 12 14 6 10 5 | 18 25 27 35 21 25 23
R24E | 2020 12 32 22 24 9 15 8 | 95 108 98 99 96 92 95
XR25E |12122 9 17 --- --- 12 --- 8 | 11 26 --- --- 22 --- 17
XR26 |10453 40 --- --- 36 69 --- 36 | 68 --- --- 73 100 --- 77
------+-----------------------------------------+-------------------------------------
RMS | 1672 16 29 26 23 20 22 |T 48 49 55 53 49 44 47
WRMS | 1672 13 21 13 18 15 22 |NE 47 42 46 48 48 37 44
MEDI | 1443 11 17 15 17 13 14 |MD 49 45 51 51 46 40 46
Table 3.2326.6 GPS week: 2326 Day: 6 MJD: 60532
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 622 16 92 33 38 51 50 21 | 113 41 131 119 131 71 100
R02 | 853 12 18 11 17 30 33 9 | 79 64 81 78 88 53 74
R03 | 2371 12 15 12 17 7 19 6 | 81 63 72 82 71 61 71
R04 | 682 11 16 11 17 14 22 6 | 77 69 76 75 70 59 71
R05 | 961 10 18 13 15 16 22 7 | 84 70 79 75 86 68 77
R07 | 786 16 22 11 16 13 29 8 | 93 69 85 87 90 61 82
R08 | 635 10 16 16 19 15 14 6 | 80 72 95 79 92 70 81
R09 | 1701 10 13 19 16 16 10 6 | 52 60 64 53 61 56 56
R11 | 977 11 15 12 11 25 9 6 | 60 67 62 62 60 58 60
R12 | 823 12 13 16 13 11 15 6 | 39 34 33 42 33 34 34
R14 | 1133 7 14 11 12 10 16 5 | 41 42 46 49 39 37 41
R15 | 1540 9 18 17 17 15 20 7 | 50 47 51 59 46 41 47
R16 | 1826 12 14 20 14 8 15 6 | 46 47 45 48 44 49 44
R17E | 893 9 20 17 25 12 15 7 | 98 106 102 100 101 98 99
R18E | 2222 5 19 14 14 11 10 5 | 47 49 51 57 47 41 47
R19E | 2060 25 42 49 23 33 28 15 | 57 72 81 77 66 66 63
R20E | 3326 38 55 88 55 39 101 28 | 80 76 132 83 80 86 77
R21E | 1330 14 15 16 23 16 17 7 | 123 120 123 136 122 128 124
R22E | 1195 14 10 10 19 11 16 6 | 34 34 40 52 42 42 39
R24E | 1646 13 22 20 35 16 24 9 | 124 123 123 143 124 125 125
XR25E |12121 16 20 --- --- 17 --- 12 | 20 33 --- --- 28 --- 24
XR26 | 9230 36 --- --- 31 79 --- 36 | 80 --- --- 80 119 --- 86
------+-----------------------------------------+-------------------------------------
RMS | 1543 15 30 27 23 21 31 |T 70 64 78 77 74 65 69
WRMS | 1543 12 25 13 17 17 31 |NE 69 57 70 70 73 55 66
MEDI | 1195 12 18 16 17 15 17 |MD 77 64 76 77 70 59 71
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