[IGSREPORT-30296] Wk 2349 IGLOS Final Orbits
acc
acc at igs.org
Fri Jan 31 01:55:16 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2349 (Jan 12, 2025 - Jan 18, 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 2.2349.
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:
igl2349[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2349 in the SP3 format.
igl23497.sum Combination Report for GPS Week 2349.
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 | 12.2 ns
1 | 4.3 ns
2 | 3.3 ns
3 | -0.0 ns
4 | 3.1 ns
5 | 3.3 ns
6 | 2.0 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 1.2349, 1a.2349).
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 2.2349.0-6)
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 3.2349.0-6).
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 2349 summary. (Jan 12, 2025 - Jan 18, 2025)
Table 1.2349.a GPS week : 2349 MJD: 60687.0-60693.0
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 6 -8 -14 70 .25 22 18 | 5285 -202 3337 8792
| 0 1 2 15 18 28 .08 | 3618 1942
esa n/a| 0 0 0 -8 -18 -1 -.20 29 22 | 5022 -136 3377 7599
| 2 1 1 3 15 31 .10 | 4518 2229
gfz n/a| 0 1 0 13 -6 25 -.07 25 16 | 0 -268 3367 10654
| 1 1 2 14 12 47 .09 | 0 1890
grg n/a| 2 0 1 -27 -15 -9 .39 29 21 | 3562 -318 3337 8488
| 1 2 4 21 31 63 .08 | 3677 1863
iac n/a| 0 0 -4 21 36 -25 -.12 19 19 | 4655 -377 3338 8503
| 1 1 3 14 40 59 .12 | 3863 808
jgx n/a| 0 0 -1 -10 -3 -19 -.18 22 22 | 7017 -253 3315 7654
| 1 1 2 18 15 39 .08 | 3546 1816
Table 1.2349.b GPS week : 2349 MJD: 60687.0-60693.0
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 | 15 15 15 18 16 16 18 |
R02 | 7 7 7 9 13 10 7 |
R03 | 6 7 7 7 11 9 6 |
R04 | 8 7 7 6 16 17 7 |
R05 | 7 6 8 7 11 12 8 |
R07 | 6 7 7 8 15 10 8 |
R08 | 9 6 10 9 16 10 8 |
R09 | 7 6 6 6 6 5 7 |
R11 | 8 7 7 9 8 8 8 |
R12 | 6 6 7 7 7 7 7 |
R14 | 6 5 6 8 6 6 7 |
R15 | 7 7 7 8 8 6 9 |
R16 | 8 8 7 10 8 8 8 |
R17 | 10 8 7 8 9 8 9 |
R18 | 7 9 7 7 6 8 9 |
R19 | 25 21 17 16 14 15 16 |
R20 | 26 25 25 26 26 25 25 |
R21 | 8 11 7 8 8 8 7 |
R22 | 7 7 7 6 7 7 7 |
R24 | 11 9 6 7 6 7 9 |
R26 | 34 35 35 37 30 32 36 |
Table 1.2349.c GPS week : 2349 MJD: 60687.0-60693.0
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 2349 0 | 24 76 -52 454 2338 4119 78.5 2140 2140 | 12241 0
brd 2349 1 | -58 8 -42 516 -623 -1517 81.2 2386 2386 | 4313 0
brd 2349 2 | -30 -26 -3 245 -243 -1549 80.9 1974 1974 | 3308 0
brd 2349 3 | -40 -40 48 -647 1012 -346 83.9 2343 2343 | -3 0
brd 2349 4 | -114 63 -23 -1556 -140 887 79.6 1996 1996 | 3065 0
brd 2349 5 | 37 17 3 -1164 -2364 -3439 79.0 1671 1671 | 3331 0
brd 2349 6 | 91 -5 47 -1320 -883 -11960 79.5 1808 1808 | 1960 0
-------------+------------------------------------------------------------+----------------
brd 2349 mean| -12 13 -3 -495 -129 -1972 80.3 2045 2045 | 4030 0
brd 2349 sdev| 68 43 40 889 1483 5003 1.8 263 263 | 3872 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 2.2349.0 GPS week: 2349 Day: 0 MJD: 60687
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 4 7 -21 83 .19 21 17 | 12420 442 3851 7314
esa n/a| 2 -1 0 -13 -14 8 .01 31 27 | 3308 927 3926 7208
gfz n/a| -2 1 -1 1 -11 113 .07 28 17 | 0 275 3838 6312
grg n/a| 3 0 2 -10 -1 -64 .43 19 20 | 11697 275 3848 7027
iac n/a| 1 -2 -7 20 11 -50 -.35 18 17 | 12489 -135 3853 7143
jgx n/a| -1 -1 1 -13 -5 -19 -.23 19 20 | 13854 224 3909 6538
Table 2.2349.1 GPS week: 2349 Day: 1 MJD: 60688
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 -10 4 95 .28 20 15 | 6305 1544 3389 9637
esa n/a| 2 1 -1 -12 4 -49 -.27 29 21 | 12010 2396 3428 8319
gfz n/a| 0 0 1 5 -3 27 -.15 26 15 | 0 1263 3425 8517
grg n/a| 1 0 3 -1 -5 -110 .40 23 16 | 3012 1615 3400 9075
iac n/a| 0 0 -5 42 -9 62 -.11 16 15 | 5762 -601 3391 9320
jgx n/a| -2 -2 -2 -46 9 -59 -.28 18 18 | 7224 1358 3459 9148
Table 2.2349.2 GPS week: 2349 Day: 2 MJD: 60689
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 7 6 -44 94 .16 22 18 | 5535 -209 3167 9532
esa n/a| 0 -1 0 -7 -44 36 -.21 29 23 | 9683 -1480 3214 6740
gfz n/a| 0 0 -3 42 -15 61 .03 29 16 | 0 -105 3218 8253
grg n/a| 0 0 4 -36 -16 -30 .44 20 21 | 2751 -379 3157 9262
iac n/a| 0 0 -3 10 103 -47 -.08 16 14 | 3919 -345 3168 9300
jgx n/a| 1 1 -4 -14 -17 -23 -.27 21 21 | 8005 -972 3058 8506
Table 2.2349.3 GPS week: 2349 Day: 3 MJD: 60690
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 9 -3 -28 68 .28 27 22 | 2398 -3201 3034 8028
esa n/a| -2 -2 2 -2 -29 -14 -.17 27 20 | 3497 -2755 3067 9276
gfz n/a| 0 1 0 13 -5 0 -.17 25 18 | 0 -3325 3046 6888
grg n/a| 2 0 -1 -18 8 42 .50 24 16 | 1003 -3206 3037 7841
iac n/a| 0 0 -7 29 27 -72 -.19 19 17 | 1085 -1232 3021 7739
jgx n/a| 0 0 0 -2 8 -19 -.16 22 22 | 3733 -2572 2883 7163
Table 2.2349.4 GPS week: 2349 Day: 4 MJD: 60691
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 9 -10 3 23 .39 24 19 | 1798 2413 3336 8279
esa n/a| 1 -1 0 -9 -13 -25 -.25 27 21 | -1707 2973 3354 6127
gfz n/a| 0 0 0 14 17 -14 -.05 20 15 | 0 2323 3365 7022
grg n/a| 1 -1 -7 -21 12 28 .31 52 27 | 1224 2030 3287 8016
iac n/a| 2 -1 0 6 3 47 -.11 25 29 | 2671 1224 3355 8032
jgx n/a| 0 0 -2 -4 9 -55 -.07 22 22 | 3942 2601 3274 7007
Table 2.2349.5 GPS week: 2349 Day: 5 MJD: 60692
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 3 -15 -10 41 .31 20 17 | 5681 -383 3364 9841
esa n/a| 0 0 -1 -6 -11 38 -.31 29 22 | 4140 -1202 3387 8712
gfz n/a| 1 2 0 14 -2 7 -.15 22 14 | 0 -402 3415 8116
grg n/a| 4 -5 3 -66 -29 0 .38 36 24 | 2988 -565 3414 9410
iac n/a| 0 0 -1 7 40 -26 .02 19 20 | 5096 -1090 3375 9467
jgx n/a| 0 0 -2 -8 0 -21 -.09 27 27 | 7920 -462 3369 7979
Table 2.2349.6 GPS week: 2349 Day: 6 MJD: 60693
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 5 -37 -3 88 .18 21 17 | 2858 -2023 3223 8916
esa n/a| -2 0 0 -4 -19 -2 -.21 28 24 | 4227 -1816 3267 6817
gfz n/a| 0 2 2 1 -23 -18 -.05 23 17 | 0 -1909 3264 29470
grg n/a| 4 2 7 -39 -79 68 .28 29 27 | 2265 -1998 3220 8786
iac n/a| 0 -1 -5 32 75 -93 -.02 17 16 | 1569 -462 3205 8526
jgx n/a| 0 0 -1 13 -30 61 -.17 24 25 | 4441 -1953 3259 7237
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 3.2349.0 GPS week: 2349 Day: 0 MJD: 60687
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1776 38 54 28 24 32 23 15 | 84 90 82 77 74 80 75
XR02E | 1140 9 14 14 14 15 --- 6 | 60 56 60 57 52 --- 55
R03E | 1736 9 17 14 18 14 9 6 | 74 72 71 75 69 70 70
R04E | 1388 20 17 18 20 9 15 7 | 35 33 40 46 32 26 33
R05E | 1293 15 17 16 19 16 13 7 | 44 40 51 50 48 41 43
R07E | 800 12 20 14 12 14 10 6 | 44 49 52 45 44 47 45
R08E | 2014 11 21 17 28 16 19 8 | 49 47 54 56 50 43 48
R09 | 1359 18 14 18 9 16 16 7 | 24 25 29 28 28 29 23
R11 | 626 18 17 17 21 21 13 8 | 29 38 41 44 34 31 31
R12 | 1089 13 15 18 13 12 14 6 | 37 36 37 34 32 34 31
R14 | 1570 9 11 15 11 20 7 5 | 34 36 40 35 40 35 34
R15 | 648 16 11 18 9 19 16 7 | 35 32 36 31 35 27 29
R16 | 812 18 19 15 18 14 19 7 | 37 36 34 36 29 34 30
R17 | 1342 20 18 15 25 27 20 9 | 106 90 97 92 108 85 95
R18 | 535 8 26 23 12 13 11 7 | 108 114 100 115 109 100 107
XR19 | 1077 40 83 42 41 39 --- 24 | 197 171 208 166 168 --- 176
R20 | 6436 48 96 95 32 18 48 26 | 142 67 164 105 106 102 109
R21 | 1353 12 17 24 14 20 18 8 | 144 127 147 139 138 124 136
R22 | 3787 20 15 16 11 15 9 6 | 41 49 42 45 42 39 40
R24 | 1123 22 28 15 25 19 26 10 | 195 174 189 196 194 177 187
XR26E |86009 38 --- --- 34 66 --- 34 | 43 --- --- 52 46 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 2139 21 31 28 19 18 19 |T 74 69 78 72 70 62 68
WRMS | 2139 17 27 17 20 17 20 |NE 86 76 89 82 81 68 79
MEDI | 1342 18 17 17 18 16 15 |MD 44 49 52 52 48 41 45
Table 3.2349.1 GPS week: 2349 Day: 1 MJD: 60688
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1128 30 50 57 10 20 26 15 | 66 62 82 66 58 60 60
XR02E | 685 11 16 15 13 13 --- 6 | 42 39 41 43 33 --- 36
R03E | 1577 14 12 15 17 18 12 6 | 72 71 72 72 70 67 69
R04E | 1554 14 19 18 12 15 13 6 | 47 57 55 57 48 54 51
R05E | 2340 11 14 15 11 16 12 6 | 42 46 44 44 42 45 41
R07E | 1095 10 20 12 23 14 12 7 | 76 79 78 87 70 73 75
R08E | 1103 13 23 14 9 12 10 6 | 58 65 57 61 49 54 55
R09 | 3264 9 22 14 15 9 11 6 | 19 35 24 26 22 23 20
R11 | 1296 15 17 16 25 14 7 7 | 29 44 32 46 19 32 30
R12 | 1468 11 20 12 11 14 16 6 | 24 28 26 26 25 30 22
R14 | 1575 7 13 16 11 10 9 5 | 19 21 23 19 21 16 16
R15 | 828 16 15 11 8 16 21 7 | 20 27 30 23 31 24 23
R16 | 572 22 19 16 18 12 16 7 | 18 42 36 33 25 35 26
R17 | 1599 17 19 16 20 13 19 8 | 91 95 92 96 89 80 89
R18 | 597 10 27 26 17 16 18 8 | 71 77 61 67 72 65 67
XR19 | 1458 35 77 44 28 23 --- 21 | 102 72 115 92 95 --- 93
R20 | 7013 54 83 69 70 22 43 25 | 95 51 78 65 75 70 67
R21 | 2709 15 26 21 33 25 20 10 | 101 86 105 90 104 86 94
R22 | 3194 17 12 13 18 19 13 7 | 30 37 44 48 36 30 34
R24 | 883 21 22 16 15 15 21 8 | 184 169 184 187 183 170 179
XR26E |>>>>> 36 --- --- 44 61 --- 34 | 50 --- --- 48 42 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 2386 20 29 26 23 16 18 |T 59 60 63 61 57 56 56
WRMS | 2386 15 21 15 16 15 18 |NE 61 60 65 62 61 55 58
MEDI | 1468 15 19 16 17 15 13 |MD 50 51 55 57 48 54 51
Table 3.2349.2 GPS week: 2349 Day: 2 MJD: 60689
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 956 25 43 56 19 33 25 15 | 73 81 78 76 60 68 65
XR02E | 1286 10 16 18 12 12 --- 6 | 55 58 64 53 50 --- 53
R03E | 1378 11 21 29 10 15 9 7 | 68 67 75 70 69 67 67
R04E | 1623 10 20 16 11 11 19 6 | 51 46 55 55 41 36 45
R05E | 2036 17 16 16 14 21 16 7 | 43 42 45 49 46 35 40
R07E | 2099 12 13 12 18 15 20 7 | 94 91 94 98 80 81 87
R08E | 1867 16 27 23 33 13 15 9 | 40 40 43 61 40 35 39
R09 | 2475 9 16 19 11 13 8 5 | 20 27 35 25 24 22 22
R11 | 2180 8 14 14 21 11 14 6 | 12 20 20 23 16 15 10
R12 | 1625 16 12 26 20 10 10 7 | 21 24 29 19 23 30 19
R14 | 942 14 17 12 12 12 13 6 | 20 38 30 27 25 25 24
R15 | 835 20 21 23 9 13 12 7 | 22 35 33 23 26 21 20
R16 | 625 18 16 18 11 16 6 6 | 27 31 36 26 24 28 24
R17 | 1268 17 15 15 10 13 21 7 | 89 77 82 85 85 80 83
R18 | 721 9 15 11 21 11 19 6 | 64 70 63 77 70 57 66
R19 | 1468 39 57 41 39 20 30 16 | 86 45 90 74 64 74 65
R20 | 3988 61 76 75 39 20 61 24 | 103 31 103 64 54 54 63
R21 | 2808 10 19 19 12 13 19 7 | 77 66 83 75 78 64 73
R22 | 3106 14 18 12 24 10 6 6 | 24 32 28 38 32 29 27
R24 | 1812 16 12 15 13 13 16 6 | 149 146 148 146 139 141 144
XR26E |>>>>> 38 --- --- 47 58 --- 35 | 55 --- --- 50 46 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1973 22 29 29 20 16 21 |T 56 53 61 57 52 50 51
WRMS | 1973 18 23 16 21 14 21 |NE 54 49 60 54 50 49 49
MEDI | 1625 16 16 18 14 13 16 |MD 55 42 55 55 46 36 47
Table 3.2349.3 GPS week: 2349 Day: 3 MJD: 60690
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1649 39 38 47 40 47 24 18 | 92 103 108 108 78 87 90
XR02E | 1519 15 18 13 14 22 --- 8 | 58 58 51 54 48 --- 51
R03E | 1170 11 16 21 16 12 10 6 | 72 70 71 73 73 69 70
R04E | 1932 12 20 13 17 6 12 6 | 71 66 74 78 70 66 70
R05E | 1387 16 11 14 18 13 11 6 | 51 47 53 54 47 48 48
R07E | 2397 14 18 24 18 14 13 7 | 73 79 70 77 71 77 72
R08E | 2164 14 28 17 20 19 18 9 | 60 67 60 63 57 61 58
R09 | 2494 13 17 18 9 13 11 6 | 21 26 28 23 17 21 19
XR11 | 1166 15 15 18 23 10 --- 8 | 11 22 16 29 19 --- 14
R12 | 1791 20 12 12 21 14 10 6 | 22 28 26 21 27 21 20
R14 | 874 15 17 12 12 25 14 7 | 15 26 17 22 36 20 19
R15 | 572 21 16 17 12 13 20 7 | 18 28 34 27 24 24 22
R16 | 766 32 24 18 18 25 9 9 | 22 48 45 25 41 37 31
R17 | 1447 23 17 19 10 7 21 7 | 117 99 116 104 105 91 104
R18 | 604 10 12 10 18 12 22 7 | 72 75 74 82 75 62 72
R19 | 1568 40 47 43 38 22 25 16 | 86 64 94 64 76 47 74
R20 | 6715 75 68 52 58 20 62 25 | 127 67 111 69 85 71 82
R21 | 1298 17 17 17 12 23 19 8 | 95 84 81 76 92 72 82
R22 | 2769 16 16 16 16 10 8 6 | 37 44 37 37 31 38 35
R24 | 2859 13 15 23 17 11 14 7 | 97 102 117 103 104 95 102
XR26E |>>>>> 34 --- --- 54 60 --- 36 | 58 --- --- 74 57 --- 60
------+-----------------------------------------+-------------------------------------
RMS | 2343 27 27 25 24 19 22 |T 60 60 64 60 58 55 56
WRMS | 2343 22 20 18 16 17 22 |NE 56 54 61 52 56 49 52
MEDI | 1568 16 17 17 18 14 14 |MD 60 64 60 64 57 61 60
Table 3.2349.4 GPS week: 2349 Day: 4 MJD: 60691
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 2599 48 35 29 45 19 32 15 | 66 80 72 66 61 79 66
XR02E | 1563 14 15 12 73 22 --- 13 | 79 83 90 116 90 --- 85
R03E | 2198 16 13 10 48 44 18 11 | 75 81 77 91 95 77 77
R04E | 1276 18 17 14 102 54 10 16 | 61 72 73 145 79 62 68
R05E | 794 12 17 18 69 20 15 10 | 91 100 96 128 88 89 92
R07E | 1276 22 16 14 92 42 18 14 | 82 82 91 145 81 83 84
R08E | 1036 21 17 14 112 38 20 16 | 52 50 52 119 53 47 47
R09 | 2815 12 13 13 14 8 14 5 | 19 27 29 17 18 23 20
R11 | 841 18 23 15 26 17 11 8 | 18 35 23 28 20 18 18
R12 | 956 13 15 17 18 12 20 7 | 17 24 24 18 22 17 16
R14 | 1232 12 14 12 20 19 11 6 | 22 20 22 22 22 20 17
R15 | 728 12 9 13 9 23 24 7 | 21 26 30 33 35 20 23
R16 | 724 22 17 20 16 17 13 8 | 16 32 40 27 24 23 22
R17 | 1063 20 12 19 25 15 23 8 | 114 100 115 97 109 90 104
R18 | 736 11 14 9 10 15 15 5 | 87 87 79 74 79 71 79
R19 | 1292 38 35 26 57 19 20 14 | 85 64 79 93 64 58 71
R20 | 4847 51 86 50 59 24 57 25 | 122 88 125 85 106 89 100
R21 | 935 15 19 17 20 14 21 8 | 97 77 96 89 88 74 86
R22 | 3298 18 17 12 19 13 11 6 | 45 48 41 39 42 41 41
R24 | 2898 15 10 14 21 9 15 6 | 137 141 141 132 136 139 138
XR26E |>>>>> 32 --- --- 46 48 --- 29 | 89 --- --- 101 108 --- 95
------+-----------------------------------------+-------------------------------------
RMS | 1995 24 27 20 52 25 22 |T 66 65 69 79 67 58 64
WRMS | 1995 19 21 15 27 29 22 |NE 61 59 64 58 58 52 56
MEDI | 1276 18 16 14 26 19 18 |MD 75 72 73 89 79 62 71
Table 3.2349.5 GPS week: 2349 Day: 5 MJD: 60692
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 2673 40 54 24 28 17 39 15 | 71 89 68 87 76 87 74
XR02E | 2888 15 11 12 49 12 --- 9 | 65 64 63 88 71 --- 66
R03E | 2537 13 15 13 46 14 20 8 | 83 84 88 89 83 88 83
R04E | 1523 21 22 25 68 51 26 16 | 124 126 128 132 114 121 118
R05E | 935 19 15 16 54 25 28 11 | 66 79 78 95 82 77 74
R07E | 1265 11 15 18 55 20 23 10 | 44 46 50 60 37 42 39
R08E | 1100 15 17 15 56 14 26 10 | 71 67 64 93 59 67 65
R09 | 1208 8 14 7 22 9 13 5 | 19 21 20 26 23 19 18
R11 | 935 7 25 13 26 22 9 8 | 16 32 24 33 25 22 19
R12 | 618 13 10 14 26 12 15 6 | 19 27 27 24 17 24 20
R14 | 1913 15 7 12 10 9 20 5 | 22 27 36 29 31 31 27
R15 | 782 16 12 13 18 14 12 6 | 26 27 34 25 22 27 24
R16 | 576 22 21 16 24 17 11 8 | 25 39 34 37 29 25 26
R17 | 1083 15 18 18 27 10 21 7 | 78 67 76 68 69 64 70
R18 | 892 12 15 17 21 16 23 7 | 62 60 81 76 66 59 66
R19 | 1843 34 42 30 21 19 49 15 | 72 50 68 52 47 34 51
R20 | 2292 34 86 67 52 15 59 24 | 84 57 106 98 85 51 78
R21 | 737 16 21 13 20 13 24 7 | 75 62 66 79 71 57 68
R22 | 2904 19 14 13 23 14 11 7 | 36 39 40 46 28 33 33
R24 | 2549 12 13 14 17 12 19 6 | 110 99 107 116 108 102 106
XR26E |>>>>> 32 --- --- 63 46 --- 31 | 92 --- --- 110 90 --- 93
------+-----------------------------------------+-------------------------------------
RMS | 1670 20 29 22 36 19 27 |T 60 58 62 69 58 54 58
WRMS | 1670 17 22 14 24 20 27 |NE 49 46 55 54 47 42 46
MEDI | 1265 15 15 14 26 14 21 |MD 66 57 64 76 66 51 66
Table 3.2349.6 GPS week: 2349 Day: 6 MJD: 60693
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1735 42 64 35 34 15 37 17 | 79 87 78 87 74 79 73
R02E | 3901 10 13 14 30 13 16 7 | 50 52 50 62 52 13 49
R03E | 1743 12 16 11 22 10 16 6 | 84 77 84 92 83 80 82
R04E | 1775 9 13 11 32 8 15 6 | 119 119 126 148 124 123 124
R05E | 1832 10 13 17 22 25 13 8 | 42 43 40 49 57 42 43
R07E | 1960 13 17 16 22 12 20 7 | 37 36 41 47 34 39 35
R08E | 1164 21 8 10 24 11 22 7 | 63 65 66 71 61 68 64
R09 | 1638 13 16 8 35 11 16 7 | 28 35 32 34 32 31 29
R11 | 739 7 20 15 28 18 16 7 | 16 26 23 27 31 21 18
R12 | 821 13 9 20 22 8 12 6 | 25 29 30 33 28 28 26
R14 | 898 6 10 18 21 14 13 6 | 25 31 37 29 31 33 29
R15 | 1000 22 18 13 23 19 28 9 | 27 39 34 35 28 32 28
R16 | 972 24 17 10 20 16 9 7 | 23 44 37 43 32 37 31
R17 | 1038 13 18 14 28 24 23 9 | 125 117 115 108 130 104 117
R18 | 847 18 15 20 34 16 20 9 | 99 103 95 114 102 87 98
R19 | 1969 39 47 30 45 27 25 15 | 130 74 120 101 99 60 101
R20 | 2153 34 77 71 42 26 66 24 | 148 67 163 118 130 90 119
R21 | 1195 21 16 12 15 13 18 7 | 122 98 116 107 112 94 108
R22 | 3426 15 17 10 24 12 20 7 | 50 58 47 51 49 47 49
R24 | 1496 19 15 16 29 20 22 9 | 161 148 154 162 149 145 152
XR26E |>>>>> 44 --- --- 54 53 --- 35 | 107 --- --- 107 100 --- 103
------+-----------------------------------------+-------------------------------------
RMS | 1807 21 28 23 29 17 24 |T 74 67 74 77 73 62 70
WRMS | 1807 17 24 17 27 16 25 |NE 75 66 77 74 73 62 69
MEDI | 1638 15 16 14 28 15 18 |MD 63 58 50 71 61 47 64
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