[IGSREPORT-30338] Wk 2353 IGLOS Final Orbits
acc
acc at igs.org
Fri Feb 28 03:27:24 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2353 (Feb 09, 2025 - Feb 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 2.2353.
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:
igl2353[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2353 in the SP3 format.
igl23537.sum Combination Report for GPS Week 2353.
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 | -1.3 ns
1 | 3.2 ns
2 | 2.0 ns
3 | 3.3 ns
4 | 0.6 ns
5 | 1.0 ns
6 | 1.1 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
1 | ESA | R26
2 | ESA | R26
3 | COD | R20
3 | ESA | R26
3 | GFZ | R26
4 | ESA | R26
4 | GFZ | R26
5 | ESA | R26
5 | GFZ | R26
6 | GFZ | 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 1.2353, 1a.2353).
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 2.2353.0-6)
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 3.2353.0-6).
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 2353 summary. (Feb 09, 2025 - Feb 15, 2025)
Table 1.2353.a GPS week : 2353 MJD: 60715.0-60721.0
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 0 -7 3 33 .11 20 15 | 5127 -340 3250 8387
| 0 0 0 14 11 21 .04 | 1760 1418
esa n/a| -2 -1 0 -33 0 63 -.13 28 26 | 6817 -2997 3300 8174
| 1 1 2 24 9 66 .05 | 2145 3552
gfz n/a| 0 1 2 24 13 -29 .02 20 16 | 0 -536 3350 7600
| 0 1 2 16 10 53 .05 | 0 1486
grg n/a| 1 0 0 -7 -9 3 .31 19 14 | 1477 -448 3276 7055
| 0 1 1 21 13 40 .04 | 1588 1503
iac n/a| 0 0 -5 -3 2 2 -.14 17 16 | 1923 -121 3251 8208
| 1 1 2 22 16 72 .04 | 1544 838
jgx n/a| 0 0 4 2 -8 -23 -.21 18 18 | 6574 -349 3278 7528
| 1 1 2 14 8 41 .04 | 1792 1594
Table 1.2353.b GPS week : 2353 MJD: 60715.0-60721.0
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 | 14 16 13 14 13 12 12 |
R02 | 6 7 6 7 6 5 8 |
R03 | 7 6 7 7 7 7 8 |
R04 | 9 7 7 7 7 7 6 |
R05 | 7 7 6 7 6 7 7 |
R07 | 8 7 9 7 8 7 9 |
R08 | 8 8 8 8 7 7 7 |
R09 | 7 6 6 5 7 6 6 |
R11 | 7 7 7 9 8 7 8 |
R12 | 8 6 8 7 7 7 8 |
R14 | 6 7 5 5 7 7 6 |
R15 | 9 6 7 9 9 7 8 |
R16 | 8 10 8 8 8 8 8 |
R17 | 9 8 8 8 5 6 9 |
R18 | 7 9 6 6 6 7 7 |
R19 | 6 6 8 12 9 8 8 |
R20 | 19 18 16 24 20 19 17 |
R21 | 9 9 8 8 9 9 9 |
R22 | 9 9 6 7 7 7 9 |
R24 | 11 7 8 8 9 7 9 |
R26 | 50 46 50 44 48 53 39 |
Table 1.2353.c GPS week : 2353 MJD: 60715.0-60721.0
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 2353 0 | 2 15 12 -1 -515 -10860 79.4 1439 1439 | -1324 0
brd 2353 1 | -32 -29 -38 -526 -2472 -9341 79.1 1336 1336 | 3153 0
brd 2353 2 | 32 -11 19 -1238 -3459 -13260 78.2 1613 1613 | 1976 0
brd 2353 3 | 73 70 1 -1064 -1369 -4946 80.0 1654 1654 | 3256 0
brd 2353 4 | 99 29 69 -2899 436 1103 79.5 1520 1520 | 646 0
brd 2353 5 | 4 -6 -23 -639 -1415 3747 80.5 1454 1454 | 970 0
brd 2353 6 | 13 -25 111 -1163 -721 4842 80.5 1588 1588 | 1131 0
-------------+------------------------------------------------------------+----------------
brd 2353 mean| 27 5 21 -1075 -1359 -4102 79.6 1514 1514 | 1401 0
brd 2353 sdev| 45 35 52 913 1290 7375 .8 112 112 | 1586 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 2.2353.0 GPS week: 2353 Day: 0 MJD: 60715
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 -9 0 30 .08 19 15 | 4210 -1671 2900 6668
esa n/a| -1 -1 -2 -25 -1 88 -.08 28 26 | 4719 -1661 2981 6655
gfz n/a| 0 1 0 11 8 -54 .05 21 15 | 0 -1807 2936 6043
grg n/a| 1 -1 -1 -43 -17 -39 .36 21 16 | -675 -1595 2923 5656
iac n/a| 0 2 -1 25 13 59 -.16 16 15 | -717 -496 2919 6560
jgx n/a| 0 -1 6 4 -9 -45 -.27 19 19 | 5371 -1590 2930 6021
Table 2.2353.1 GPS week: 2353 Day: 1 MJD: 60716
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 -9 0 36 .09 17 15 | 7136 614 3215 8597
esa n/a| -3 -3 -3 4 4 166 -.18 28 26 | 9971 -2385 3271 8459
gfz n/a| 0 3 2 16 9 40 .04 21 14 | 0 514 3254 7977
grg n/a| 1 -1 1 -29 -15 -39 .36 18 13 | 2633 601 3249 7533
iac n/a| 0 1 -4 0 6 -90 -.18 16 15 | 3473 571 3218 8570
jgx n/a| 1 -3 5 -5 8 8 -.24 21 21 | 8904 583 3244 7926
Table 2.2353.2 GPS week: 2353 Day: 2 MJD: 60717
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 1 12 9 57 .16 18 15 | 7528 -2813 3425 8750
esa n/a| -1 0 -2 -32 -3 11 -.22 25 23 | 7645 -2483 3482 8311
gfz n/a| 0 0 7 49 26 -131 .01 19 14 | 0 -3302 3444 7807
grg n/a| 1 1 0 6 -22 28 .30 18 15 | 3317 -3082 3440 7550
iac n/a| 0 0 -7 -36 1 95 -.11 16 14 | 3214 -1761 3420 8626
jgx n/a| 0 0 1 6 -15 -68 -.15 14 14 | 8548 -3002 3525 8072
Table 2.2353.3 GPS week: 2353 Day: 3 MJD: 60718
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 6 12 54 .12 44 16 | 5997 5 2887 8282
esa n/a| 0 -2 0 -32 -15 105 -.15 28 27 | 6228 -1848 2938 7929
gfz n/a| 1 1 4 36 15 -39 .02 17 16 | 0 -30 3067 7433
grg n/a| 2 1 -3 18 15 33 .29 20 15 | 3260 -375 2881 7135
iac n/a| 0 0 -4 -14 0 -75 -.13 20 17 | 3377 55 2872 8128
jgx n/a| 0 -1 3 -23 -15 27 -.20 18 18 | 7877 -293 2890 7498
Table 2.2353.4 GPS week: 2353 Day: 4 MJD: 60719
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 1 -34 19 43 .13 14 13 | 2953 96 3228 8376
esa n/a| -2 -3 -2 -20 2 10 -.08 27 23 | 9092 -10896 3289 8668
gfz n/a| 0 1 2 36 0 -12 -.03 21 16 | 0 14 3369 7532
grg n/a| 2 0 0 -5 0 -41 .23 18 14 | 472 110 3265 6841
iac n/a| 0 0 -9 24 -28 -39 -.19 21 19 | 970 -91 3227 8194
jgx n/a| 1 1 5 1 -14 21 -.24 18 18 | 4847 58 3259 7350
Table 2.2353.5 GPS week: 2353 Day: 5 MJD: 60720
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 -12 -9 0 .16 15 13 | 3821 44 3198 8800
esa n/a| -5 0 4 -62 15 -23 -.13 32 30 | 5626 -1298 3265 8000
gfz n/a| 2 2 4 18 27 -6 -.04 22 16 | 0 -57 3360 7990
grg n/a| 3 0 0 4 -11 38 .31 19 13 | 1050 -316 3239 7014
iac n/a| -3 0 -4 -11 2 61 -.09 16 14 | 1533 72 3199 8505
jgx n/a| 0 0 1 20 -3 -41 -.18 14 14 | 5588 -228 3229 7616
Table 2.2353.6 GPS week: 2353 Day: 6 MJD: 60721
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 -7 -9 12 .07 16 16 | 4250 1340 3902 9241
esa n/a| -3 0 1 -64 -8 87 -.09 28 28 | 4442 -409 3877 9202
gfz n/a| 0 0 0 2 3 -7 .11 21 18 | 0 913 4026 8420
grg n/a| 0 0 0 -4 -16 40 .31 19 14 | 286 1519 3940 7657
iac n/a| -1 1 -5 -11 24 7 -.14 16 15 | 1616 797 3905 8875
jgx n/a| 2 -1 6 13 -9 -67 -.23 18 18 | 4887 2023 3871 8215
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 3.2353.0 GPS week: 2353 Day: 0 MJD: 60715
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 777 39 45 21 26 22 34 14 | 117 61 95 93 97 86 91
R02 | 1245 7 25 13 13 7 9 5 | 56 57 43 50 46 38 48
R03 | 1541 9 14 10 24 10 22 7 | 77 67 78 90 80 66 76
R04 | 1151 12 24 16 17 21 22 8 | 78 67 91 86 92 77 82
R05 | 1122 12 24 11 18 13 19 7 | 67 61 72 61 72 56 65
R07 | 1083 15 31 21 15 14 11 8 | 87 86 82 83 87 76 82
R08 | 1454 21 28 14 16 14 17 8 | 81 92 72 83 74 68 76
R09 | 1975 14 24 21 12 8 13 7 | 29 31 33 33 29 30 28
R11 | 814 10 31 16 15 8 14 7 | 26 34 34 37 32 29 29
R12 | 923 20 22 20 16 12 11 7 | 58 45 50 52 52 50 50
R14 | 1189 10 15 11 15 11 15 5 | 66 62 61 69 70 60 64
R15 | 711 12 25 23 15 15 28 9 | 74 61 84 68 76 48 68
R16 | 840 16 18 12 7 13 28 7 | 82 79 79 77 81 65 76
R17E | 2333 16 21 21 28 15 12 8 | 66 61 62 70 58 60 60
R18E | 637 14 18 16 15 16 16 7 | 41 44 42 42 43 41 40
R19E | 2146 10 17 14 17 12 13 6 | 36 41 36 47 28 30 34
R20E | 1634 40 59 55 44 30 30 19 | 64 65 74 67 56 51 50
R21E | 1581 14 17 16 22 23 19 8 | 55 55 51 58 68 54 55
R22E | 2512 17 34 16 13 17 16 8 | 39 55 45 44 32 48 41
R24E | 994 21 25 24 31 22 14 10 | 61 65 69 69 71 68 65
XR26 |19005 51 870 --- --- 47 --- 49 | 164 286 --- --- 170 --- 164
------+-----------------------------------------+-------------------------------------
RMS | 1438 19 28 21 21 16 19 |T 67 70 62 63 67 55 64
WRMS | 1438 15 26 15 16 15 19 |NE 75 77 67 67 75 57 71
MEDI | 1189 14 24 16 16 14 16 |MD 66 61 62 67 70 54 64
Table 3.2353.1 GPS week: 2353 Day: 1 MJD: 60716
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 939 39 57 25 33 13 47 16 | 76 56 76 78 67 76 70
R02 | 1292 10 23 10 20 13 14 6 | 41 45 38 35 40 25 35
R03 | 2038 7 20 9 11 13 13 5 | 51 49 51 54 54 55 51
R04 | 916 15 18 23 14 9 13 7 | 55 59 76 74 67 61 64
R05 | 1066 14 14 21 10 8 24 7 | 46 49 60 49 48 39 47
R07 | 468 11 21 10 14 11 25 7 | 69 68 69 69 72 53 66
R08 | 1670 18 20 14 15 13 22 7 | 64 63 51 58 57 51 56
R09 | 1769 9 18 14 12 15 11 6 | 26 36 26 36 31 33 29
R11 | 644 12 32 15 8 17 7 7 | 29 45 38 33 32 38 32
R12 | 1399 20 18 15 9 11 9 6 | 41 41 33 37 36 33 35
R14 | 803 7 21 13 15 17 16 6 | 55 66 49 61 65 56 57
R15 | 966 16 13 12 13 15 15 6 | 54 55 59 45 60 42 52
R16 | 760 12 37 22 13 23 22 9 | 60 47 63 58 72 52 58
R17E | 1827 15 18 16 24 21 13 8 | 63 57 65 52 61 59 58
R18E | 779 20 24 17 24 12 18 8 | 27 44 40 44 32 27 31
R19E | 1550 9 18 14 13 13 14 6 | 37 43 47 45 39 39 39
R20E | 1820 28 56 57 30 29 40 18 | 58 60 82 54 46 51 45
R21E | 1039 19 25 24 19 20 10 9 | 32 41 27 42 51 36 34
R22E | 2160 18 31 13 19 17 21 8 | 31 26 34 34 26 38 28
R24E | 972 14 19 15 17 13 13 6 | 36 38 36 43 44 43 38
XR26 |23020 46 857 --- --- 44 --- 45 | 119 287 --- --- 111 --- 114
------+-----------------------------------------+-------------------------------------
RMS | 1336 17 28 21 18 16 21 |T 50 60 51 50 52 45 49
WRMS | 1336 15 26 14 13 15 21 |NE 56 69 53 52 58 47 54
MEDI | 1066 15 21 15 14 13 14 |MD 51 49 49 45 51 42 47
Table 3.2353.2 GPS week: 2353 Day: 2 MJD: 60717
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 736 38 50 17 31 19 22 13 | 103 56 77 89 75 68 77
R02 | 1195 10 20 12 11 7 12 5 | 48 47 51 50 42 34 45
R03 | 719 10 32 15 21 6 8 7 | 67 60 78 63 65 64 65
R04 | 1156 9 15 19 16 15 14 6 | 65 61 82 71 63 69 67
R05 | 1304 12 13 12 14 13 8 5 | 55 63 68 61 61 56 59
R07 | 447 13 37 16 19 13 20 8 | 70 50 75 69 70 56 64
R08 | 1715 12 20 19 25 19 13 8 | 67 71 71 68 53 61 63
R09 | 639 11 21 12 13 9 12 5 | 30 26 35 30 38 22 29
R11 | 978 16 34 11 9 7 9 6 | 14 41 25 22 26 26 23
R12 | 2494 22 28 12 15 11 13 7 | 42 49 35 26 30 32 32
R14 | 887 7 19 12 8 10 8 4 | 58 66 70 69 58 62 63
R15 | 1012 24 11 13 6 8 19 7 | 61 56 51 48 52 45 49
R16 | 800 11 18 20 13 15 19 7 | 72 72 83 65 73 60 69
R17E | 718 14 19 12 17 27 14 8 | 59 55 50 54 47 52 50
R18E | 1160 10 22 13 18 11 11 6 | 41 49 39 42 42 39 39
XR19E | 1257 9 20 11 24 11 --- 7 | 24 31 27 34 23 --- 21
R20E | 3074 40 28 55 19 35 21 16 | 63 59 93 60 46 55 52
R21E | 1045 12 24 13 20 20 12 7 | 35 41 33 40 33 36 32
R22E | 3598 15 15 14 15 14 10 6 | 30 38 32 33 25 25 27
R24E | 2315 14 17 14 23 15 15 7 | 40 42 48 48 33 46 40
XR26 |29848 53 745 --- --- 46 --- 50 | 55 227 --- --- 90 --- 72
------+-----------------------------------------+-------------------------------------
RMS | 1612 18 25 19 18 16 14 |T 52 60 56 52 49 47 49
WRMS | 1612 15 23 14 15 14 14 |NE 57 67 61 56 56 50 55
MEDI | 1156 12 20 13 16 13 13 |MD 55 55 51 50 47 52 50
Table 3.2353.3 GPS week: 2353 Day: 3 MJD: 60718
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1210 40 61 17 22 28 11 13 | 102 39 77 89 70 81 78
R02 | 3207 10 27 13 15 10 13 6 | 51 52 42 55 46 32 46
R03 | 1153 13 28 10 15 15 14 7 | 69 48 57 68 58 51 58
R04 | 1354 15 23 14 16 11 10 6 | 59 47 58 51 56 57 54
R05 | 1066 15 17 9 20 15 8 6 | 55 53 54 44 61 47 51
R07 | 505 9 26 21 9 6 16 6 | 66 55 83 67 70 60 67
R08 | 909 10 18 18 15 19 23 8 | 56 69 76 60 58 45 59
R09 | 713 12 15 12 10 11 9 5 | 17 24 19 17 21 22 17
R11 | 1418 19 37 13 17 11 21 8 | 20 35 36 46 44 42 35
R12 | 1534 25 23 10 11 6 14 7 | 34 23 25 20 23 21 22
R14 | 1838 11 15 12 13 12 8 5 | 42 34 34 30 36 29 33
R15 | 1059 19 15 16 13 15 29 8 | 54 49 56 53 36 24 43
R16 | 1888 14 19 15 10 20 24 8 | 66 66 68 57 61 43 59
R17E | 1562 10 14 16 14 28 12 7 | 73 70 77 80 67 68 71
R18E | 1468 10 21 16 13 10 10 6 | 99 95 98 101 102 101 99
R19E | 797 16 28 18 43 23 26 12 | 43 44 42 74 35 36 40
R20E | 1684 185 52 40 44 57 40 23 | 228 61 97 70 121 67 78
R21E | 1397 11 22 24 21 14 13 8 | 34 36 33 44 34 34 32
R22E | 3706 16 25 13 16 15 14 7 | 25 39 38 40 35 32 32
R24E | 941 16 21 16 22 14 16 7 | 34 36 35 37 30 36 31
XR26 |34746 45 769 1109 --- 43 --- 44 | 47 233 351 --- 70 --- 55
------+-----------------------------------------+-------------------------------------
RMS | 1654 44 28 17 20 20 18 |T 60 57 69 55 54 46 50
WRMS | 1654 16 27 16 15 17 18 |NE 52 59 74 50 50 42 48
MEDI | 1397 15 23 16 15 15 14 |MD 54 48 56 53 56 42 51
Table 3.2353.4 GPS week: 2353 Day: 4 MJD: 60719
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 613 22 64 20 20 17 17 12 | 97 51 105 98 87 82 88
R02 | 2344 14 21 15 11 11 10 6 | 52 45 39 47 45 27 44
R03 | 680 10 17 16 8 15 22 6 | 72 59 75 66 66 58 65
R04 | 686 10 24 12 17 13 17 7 | 69 49 67 66 56 58 60
R05 | 1174 10 22 16 13 16 9 6 | 53 46 54 47 51 47 48
R07 | 735 10 22 22 10 20 16 7 | 76 62 88 73 75 64 73
R08 | 625 11 18 17 16 16 21 7 | 68 67 70 56 64 58 63
R09 | 967 15 14 15 8 18 18 6 | 30 29 33 28 35 28 27
R11 | 1682 12 28 8 12 19 20 7 | 27 32 25 22 42 26 26
R12 | 1783 18 19 15 11 17 13 7 | 49 41 39 31 37 29 37
R14 | 2665 7 12 18 17 18 10 6 | 53 49 61 42 62 52 52
R15 | 1140 17 27 23 14 17 16 8 | 53 45 60 51 47 37 48
R16 | 1285 15 17 8 10 23 30 8 | 71 62 64 66 70 56 65
R17E | 862 6 16 12 9 13 15 5 | 33 36 29 35 30 34 31
R18E | 1542 11 22 11 15 15 10 6 | 139 132 124 144 132 124 131
R19E | 858 12 14 20 17 34 22 9 | 76 76 84 83 65 84 77
R20E | 2058 28 50 63 49 43 38 20 | 52 78 86 63 79 47 56
R21E | 1039 15 26 14 25 16 18 8 | 36 36 39 49 35 41 36
R22E | 3161 16 16 17 16 21 13 7 | 22 34 28 34 23 24 23
R24E | 954 10 25 25 23 25 11 9 | 43 63 52 58 44 55 49
XR26 |43707 38 837 1039 --- 59 --- 47 | 80 306 261 --- 110 --- 89
------+-----------------------------------------+-------------------------------------
RMS | 1519 14 27 21 18 21 18 |T 59 66 70 57 59 51 56
WRMS | 1519 13 23 16 14 19 18 |NE 60 67 74 53 60 47 56
MEDI | 1140 12 22 16 14 17 16 |MD 53 49 61 51 56 47 52
Table 3.2353.5 GPS week: 2353 Day: 5 MJD: 60720
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 885 20 63 31 23 16 16 11 | 79 53 85 86 81 70 76
R02 | 2238 10 27 13 8 8 8 5 | 47 43 43 44 43 39 43
R03 | 591 12 25 17 13 9 19 7 | 62 59 69 70 60 51 60
R04 | 768 13 25 24 8 17 12 7 | 54 47 74 55 63 50 56
R05 | 1419 7 31 15 17 10 15 6 | 51 46 62 67 57 44 53
R07 | 753 12 21 22 12 19 12 7 | 60 64 72 63 56 53 59
R08 | 657 10 26 22 8 10 18 7 | 54 66 67 52 57 47 54
R09 | 930 17 23 19 11 10 9 6 | 29 32 31 31 25 33 28
R11 | 1407 13 42 13 12 12 7 7 | 29 48 31 25 32 29 28
R12 | 1700 18 22 21 19 12 8 7 | 47 48 54 44 53 44 46
R14 | 1935 10 34 18 12 14 10 6 | 52 48 51 55 47 57 50
R15 | 730 17 26 13 9 17 11 6 | 44 39 39 45 37 42 40
R16 | 1052 14 33 17 10 15 16 7 | 60 64 65 62 68 53 60
R17E | 1269 10 17 19 15 8 8 5 | 44 36 45 47 44 46 42
R18E | 1522 12 26 15 16 12 16 7 | 182 180 180 182 184 195 183
R19E | 952 14 28 12 25 13 15 7 | 98 91 96 113 92 96 98
R20E | 1522 29 49 60 44 42 30 18 | 48 63 89 54 55 46 47
R21E | 811 16 30 14 30 14 13 8 | 34 43 31 48 32 33 33
R22E | 2955 15 36 11 19 13 10 7 | 25 53 24 42 19 25 26
R24E | 2210 13 18 14 20 12 13 6 | 34 39 45 46 42 46 40
XR26 |53040 54 856 1020 --- 51 --- 53 | 55 381 270 --- 95 --- 73
------+-----------------------------------------+-------------------------------------
RMS | 1454 15 32 22 19 16 14 |T 56 73 72 61 59 54 56
WRMS | 1454 13 30 16 13 14 14 |NE 51 74 72 53 55 47 51
MEDI | 1269 13 27 17 13 13 12 |MD 51 48 62 52 55 46 50
Table 3.2353.6 GPS week: 2353 Day: 6 MJD: 60721
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1235 25 61 33 14 15 14 12 | 120 64 111 113 108 104 105
XR02 | 2445 13 20 15 14 19 --- 8 | 61 56 55 63 67 --- 60
R03 | 783 17 27 21 15 10 19 8 | 89 79 82 86 84 69 80
R04 | 2316 9 26 13 13 10 9 6 | 80 66 85 81 82 79 79
R05 | 2376 12 20 24 11 12 15 7 | 67 62 77 62 72 62 66
R07 | 1063 17 28 11 17 16 24 8 | 91 80 88 86 94 75 85
R08 | 838 12 20 19 14 9 16 6 | 85 93 78 82 77 80 81
R09 | 1103 14 17 13 9 9 12 5 | 33 31 35 32 31 35 31
R11 | 1034 11 37 14 14 12 13 7 | 34 52 35 32 39 37 35
R12 | 1661 17 18 8 29 13 10 7 | 63 52 49 45 55 52 52
R14 | 1223 8 16 11 12 12 14 5 | 64 64 66 64 72 65 65
R15 | 1142 21 19 16 12 12 22 7 | 68 54 67 65 61 51 60
R16 | 1462 26 29 15 12 12 16 8 | 85 86 91 81 83 71 81
R17E | 1606 12 18 23 23 20 14 8 | 89 86 75 98 96 79 87
R18E | 1112 8 21 23 12 15 9 6 | 206 206 196 208 206 200 203
R19E | 1299 20 19 19 19 12 17 8 | 86 84 90 82 76 76 81
R20E | 1204 23 43 42 33 42 43 17 | 54 59 76 56 58 57 51
R21E | 1245 12 26 17 24 19 17 8 | 48 48 39 57 47 39 44
R22E | 2970 13 32 20 20 19 12 8 | 31 36 44 43 30 38 34
R24E | 2366 14 20 31 28 8 14 9 | 52 50 56 71 54 60 55
XR26 |65672 64 63 1023 --- 39 --- 39 | 68 517 334 --- 105 --- 88
------+-----------------------------------------+-------------------------------------
RMS | 1587 16 28 21 19 16 18 |T 74 91 87 75 76 69 72
WRMS | 1587 16 28 18 14 15 18 |NE 72 96 89 68 73 65 69
MEDI | 1245 14 21 19 14 12 14 |MD 68 64 76 65 72 65 66
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