[IGSREPORT-30364] Wk 2356 IGLOS Final Orbits
acc
acc at igs.org
Thu Mar 20 04:01:05 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2356 (Mar 02, 2025 - Mar 08, 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 2.2356.
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:
igl2356[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2356 in the SP3 format.
igl23567.sum Combination Report for GPS Week 2356.
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 | 2.5 ns
1 | 1.0 ns
2 | 3.5 ns
3 | 0.4 ns
4 | 2.7 ns
5 | 4.2 ns
6 | 0.6 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 1.2356, 1a.2356).
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 2.2356.0-6)
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 3.2356.0-6).
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 2356 summary. (Mar 02, 2025 - Mar 08, 2025)
Table 1.2356.a GPS week : 2356 MJD: 60736.0-60742.0
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 5 -17 31 .14 20 16 | 15173 -341 3691 46221
| 1 1 1 16 13 22 .04 | 1148 1541
esa n/a| -1 -1 1 -10 -16 63 -.02 27 24 | 17447 -2041 3701 46920
| 1 1 1 5 10 39 .03 | 2005 2453
gfz n/a| 1 1 -2 13 17 -48 .06 22 17 | 0 -84 3284 7778
| 0 1 2 17 12 22 .04 | 0 1627
grg n/a| 2 -1 7 -15 -16 0 .25 24 17 | 1998 -256 3282 7397
| 0 1 3 10 15 40 .03 | 1519 1542
iac n/a| 0 0 -6 -8 9 -26 -.22 17 16 | 13580 -607 3711 47551
| 1 1 3 14 21 44 .04 | 1475 706
jgx n/a| 0 -1 3 22 3 10 -.12 22 22 | 6307 -237 3277 7822
| 1 0 2 9 16 17 .01 | 1235 1584
Table 1.2356.b GPS week : 2356 MJD: 60736.0-60742.0
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 | 12 13 12 14 12 15 11 |
R02 | 7 7 6 7 9 8 7 |
R03 | 8 7 6 7 6 6 6 |
R04 | 6 6 6 8 5 8 7 |
R05 | 8 7 8 7 6 9 7 |
R07 | 7 6 9 7 7 7 8 |
R08 | 7 5 7 7 8 8 6 |
R09 | 6 6 7 6 7 7 8 |
R11 | 7 6 7 6 6 8 7 |
R12 | 9 9 10 7 9 8 7 |
R14 | 8 7 7 8 8 6 5 |
R15 | 8 8 7 8 8 9 7 |
R16 | 9 9 9 11 10 11 9 |
R17 | 7 8 9 9 9 10 8 |
R18 | 8 7 6 8 9 10 7 |
R19 | 9 14 18 23 19 20 19 |
R20 | 20 25 22 19 20 17 21 |
R21 | 8 9 10 10 10 8 9 |
R22 | 11 8 8 7 8 8 8 |
R24 | 8 11 10 10 10 10 10 |
R26 | 38 44 32 34 36 35 33 |
Table 1.2356.c GPS week : 2356 MJD: 60736.0-60742.0
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 2356 0 | 59 10 106 -914 2101 8449 78.9 1801 1801 | 2462 0
brd 2356 1 | -28 49 82 -1307 2739 5104 79.4 1693 1693 | 1038 0
brd 2356 2 | -33 24 79 -197 412 -905 78.9 1561 1561 | 3540 0
brd 2356 3 | 7 -33 63 -611 394 -3288 79.5 1768 1768 | 368 0
brd 2356 4 | 4 88 -35 -1539 584 -2750 79.8 1643 1643 | 2700 0
brd 2356 5 | -47 98 -6 -1798 265 -833 81.5 1750 1750 | 4222 0
brd 2356 6 | -102 -25 52 -1690 -1342 -1075 81.0 1728 1728 | 624 0
-------------+------------------------------------------------------------+----------------
brd 2356 mean| -20 30 49 -1151 736 671 79.9 1706 1706 | 2136 0
brd 2356 sdev| 50 51 51 597 1332 4384 1.0 82 82 | 1492 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 2.2356.0 GPS week: 2356 Day: 0 MJD: 60736
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 -6 -9 40 .16 16 13 | 15252 -1757 4076 45812
esa n/a| -3 -3 1 -15 -27 16 -.05 27 25 | 17386 -3299 4114 46915
gfz n/a| 1 -1 -3 5 3 -33 .08 21 18 | 0 -1607 3018 7751
grg n/a| 2 -1 4 0 -10 -55 .22 23 18 | 3196 -1832 3018 7273
iac n/a| 0 2 -6 -25 42 -8 -.21 16 15 | 12712 -406 4127 47285
jgx n/a| 1 0 5 26 -32 30 -.15 21 21 | 6728 -1958 2996 7844
Table 2.2356.1 GPS week: 2356 Day: 1 MJD: 60737
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 -13 -19 10 .09 18 14 | 13464 -1841 4807 45438
esa n/a| -1 0 2 -4 -31 47 .01 22 22 | 14256 -1288 4844 46080
gfz n/a| 2 0 -1 17 19 -70 .04 19 14 | 0 -1340 3796 8050
grg n/a| 2 -2 5 -17 -4 25 .20 30 16 | 1273 -1489 3818 7693
iac n/a| -1 0 -7 -7 25 9 -.18 23 19 | 12559 -1931 4858 46697
jgx n/a| 0 0 4 20 6 -20 -.12 21 21 | 4971 -1454 3796 8009
Table 2.2356.2 GPS week: 2356 Day: 2 MJD: 60738
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 0 36 -9 4 .07 20 15 | 16392 746 3590 47333
esa n/a| -4 -1 0 -6 -13 144 -.02 29 21 | 17678 526 3566 47802
gfz n/a| 1 2 -5 0 29 -42 .04 20 17 | 0 1090 3646 7604
grg n/a| 1 0 4 -17 -10 48 .24 26 16 | 2857 896 3642 7205
iac n/a| 0 2 0 -26 -20 -59 -.21 18 16 | 15483 84 3594 48726
jgx n/a| -1 -1 3 26 17 3 -.12 21 21 | 7205 1000 3644 7635
Table 2.2356.3 GPS week: 2356 Day: 3 MJD: 60739
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 1 -3 -2 -35 31 .17 22 18 | 13724 -300 2965 46857
esa n/a| -3 0 0 -5 -3 62 -.03 28 24 | 15285 -373 2960 47044
gfz n/a| 2 3 0 30 29 -22 .01 27 19 | 0 -531 2999 6586
grg n/a| 1 0 5 -15 -22 40 .28 21 16 | 370 -621 2977 6281
iac n/a| -1 -1 -5 1 -11 -82 -.27 17 16 | 12179 -594 2966 48163
jgx n/a| 0 -1 5 29 6 25 -.13 24 24 | 4399 -616 2974 6578
Table 2.2356.4 GPS week: 2356 Day: 4 MJD: 60740
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 11 -34 69 .19 22 17 | 15715 -2012 3516 45960
esa n/a| 1 -1 0 -12 -5 68 -.07 28 26 | 19124 -5795 3546 46622
gfz n/a| 0 0 0 42 15 -65 .10 21 15 | 0 -1850 2885 7473
grg n/a| 0 -1 8 -34 -24 6 .22 24 17 | 3401 -1807 2883 7153
iac n/a| -2 0 -10 0 17 -75 -.28 17 17 | 14221 -1126 3554 47270
jgx n/a| 0 0 4 27 6 16 -.11 22 22 | 7274 -1768 2874 7577
Table 2.2356.5 GPS week: 2356 Day: 5 MJD: 60741
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 2 -9 47 .16 22 17 | 16174 1548 3575 46329
esa n/a| -1 0 3 -19 -13 46 .00 28 25 | 18845 259 3567 46879
gfz n/a| 1 0 -1 2 -1 -78 .11 23 16 | 0 1695 3303 8300
grg n/a| 1 -2 12 -16 -44 -34 .27 25 22 | 3169 1655 3295 7921
iac n/a| -1 0 -8 -12 9 23 -.21 16 16 | 15535 -246 3572 47587
jgx n/a| 1 -1 2 26 9 16 -.13 23 23 | 7610 1781 3308 8375
Table 2.2356.6 GPS week: 2356 Day: 6 MJD: 60742
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 0 7 -1 19 .14 21 17 | 15493 1227 3309 45820
esa n/a| -1 -1 0 -11 -18 61 -.01 30 26 | 19559 -4322 3315 47103
gfz n/a| 1 2 -3 -2 23 -29 .03 24 18 | 0 1951 3345 8688
grg n/a| 3 0 9 -3 2 -32 .28 19 16 | -276 1401 3341 8259
iac n/a| -1 0 -3 14 6 8 -.17 14 12 | 12374 -35 3310 47135
jgx n/a| 0 0 0 2 7 3 -.10 23 23 | 5963 1355 3348 8737
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 3.2356.0 GPS week: 2356 Day: 0 MJD: 60736
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 462 21 50 27 27 20 21 12 | 82 38 69 77 75 64 69
R02 | 1530 15 27 15 19 9 8 7 | 86 72 91 86 87 81 84
R03 | 1997 8 19 21 17 10 28 8 | 65 62 60 71 61 49 60
R04 | 527 9 19 14 20 9 8 6 | 79 80 78 82 77 78 78
R05 | 787 11 36 16 18 17 8 8 | 64 68 68 73 63 58 63
R07 | 1505 12 17 19 13 18 15 7 | 95 88 87 95 88 90 90
R08 | 1142 10 20 16 11 15 19 6 | 51 58 55 50 44 47 49
R09 | 2095 11 19 18 11 7 17 6 | 34 34 50 37 43 34 37
R11 | 1337 12 26 10 12 15 13 6 | 35 52 43 31 41 31 37
R12 | 1346 12 23 23 27 18 17 8 | 79 84 81 60 83 62 74
R14 | 1746 9 18 32 16 16 15 8 | 68 71 83 52 55 51 62
R15 | 2025 18 17 13 13 28 12 8 | 87 78 78 77 63 74 75
R16 | 899 13 34 25 14 11 15 8 | 89 76 99 80 85 74 83
R17 | 1168 14 15 15 16 12 19 7 | 76 70 80 72 74 61 71
R18 | 843 10 18 17 32 11 20 8 | 53 61 52 61 55 44 52
R19E | 2291 15 29 23 26 10 12 8 | 100 90 90 110 92 97 95
R20E | 4853 45 45 43 33 30 66 20 | 74 74 70 68 55 70 59
R21 | 1201 13 16 19 28 16 14 8 | 56 44 50 48 53 37 45
R22 | 747 15 20 13 50 18 13 10 | 50 60 59 85 68 52 59
R24 | 2233 12 25 19 14 16 18 7 | 57 53 59 53 61 42 52
XR26 |13234 58 62 --- --- 42 --- 38 | 20 86 --- --- 77 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1800 16 27 21 23 16 21 |T 66 66 70 68 66 59 63
WRMS | 1800 13 25 18 18 15 21 |NE 64 65 69 66 65 57 62
MEDI | 1346 12 20 18 17 16 15 |MD 68 70 69 71 63 58 62
Table 3.2356.1 GPS week: 2356 Day: 1 MJD: 60737
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 579 27 44 25 19 24 22 12 | 53 32 54 44 46 52 45
R02 | 2603 14 19 16 23 12 11 7 | 62 46 64 64 55 62 58
R03 | 2251 8 12 11 9 20 21 6 | 43 46 42 43 55 30 42
R04 | 535 8 13 18 17 9 15 6 | 52 55 62 54 52 51 53
R05 | 1490 13 24 12 13 12 14 7 | 41 45 48 40 42 38 41
R07 | 860 15 9 13 15 12 16 6 | 58 55 54 62 62 61 57
R08 | 1162 13 13 8 13 9 14 5 | 32 36 34 35 30 41 33
R09 | 1172 10 16 11 12 14 13 5 | 31 35 36 35 47 31 35
R11 | 1463 11 15 13 19 11 9 5 | 26 33 34 29 31 27 28
R12 | 1918 20 23 17 34 14 11 9 | 60 70 49 50 57 49 53
R14 | 2168 8 21 18 11 10 20 7 | 51 59 59 49 54 35 50
R15 | 2357 19 20 10 13 19 17 7 | 65 69 61 63 45 61 59
R16 | 888 20 33 16 19 10 8 8 | 68 52 68 57 58 62 60
R17 | 947 10 18 19 25 16 12 7 | 56 54 59 53 62 49 55
R18 | 676 11 18 15 14 16 11 6 | 33 36 31 43 43 30 34
R19E | 1063 15 19 12 61 48 17 14 | 106 97 108 121 103 96 100
R20E | 2959 43 35 43 83 67 66 25 | 95 66 79 113 79 74 73
R21 | 858 15 15 26 14 22 23 9 | 37 29 40 34 40 26 31
R22 | 1687 19 15 11 31 14 12 7 | 26 30 34 46 37 28 29
R24 | 2737 17 18 31 38 18 25 11 | 44 40 43 46 41 28 36
XR26 | 7863 71 69 --- --- 35 --- 43 | 41 72 --- --- 40 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1693 18 22 19 30 23 21 |T 51 50 52 54 51 46 48
WRMS | 1693 14 22 14 16 19 21 |NE 46 47 48 47 47 42 44
MEDI | 1463 15 18 15 17 14 14 |MD 51 46 49 46 47 41 45
Table 3.2356.2 GPS week: 2356 Day: 2 MJD: 60738
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 701 33 43 16 12 20 24 11 | 65 34 39 52 42 49 44
R02 | 2409 8 10 15 10 18 13 6 | 90 86 101 93 93 90 92
R03 | 2316 7 16 11 13 10 16 5 | 55 55 45 55 53 43 50
R04 | 751 13 17 12 14 13 14 6 | 61 59 59 65 58 54 59
R05 | 745 13 23 21 22 11 13 7 | 51 51 40 56 51 44 46
R07 | 840 14 32 21 14 19 16 8 | 85 86 83 90 76 83 82
R08 | 1457 14 27 13 12 12 18 7 | 37 57 36 37 42 39 39
R09 | 1736 11 21 13 13 18 11 6 | 19 30 32 27 23 23 22
R11 | 1667 11 22 19 9 15 11 6 | 27 29 35 25 24 22 24
R12 | 1457 23 29 15 23 24 10 9 | 66 65 55 56 56 60 57
R14 | 1944 9 25 16 11 11 14 6 | 52 68 63 63 55 51 56
R15 | 1837 14 22 16 8 11 16 6 | 72 60 59 64 70 65 64
R16 | 820 22 36 16 14 8 12 8 | 80 65 72 70 65 60 67
R17 | 625 17 16 15 31 15 16 8 | 55 49 47 48 56 46 48
R18 | 696 7 19 14 14 11 15 6 | 45 51 55 46 45 45 46
R19E | 687 34 47 34 60 36 22 17 | 128 151 128 166 132 139 136
R20E | 3239 43 61 45 63 32 55 22 | 115 135 109 124 102 104 105
R21 | 648 20 13 24 19 15 36 10 | 49 38 44 46 40 30 37
R22 | 1570 13 20 21 23 15 16 8 | 26 44 50 53 28 29 34
R24 | 1621 21 20 15 36 18 20 10 | 43 37 36 41 37 30 33
XR26 | 7840 51 38 --- --- 42 --- 31 | 49 77 --- --- 71 --- 61
------+-----------------------------------------+-------------------------------------
RMS | 1560 20 29 20 26 18 21 |T 60 63 59 63 58 55 57
WRMS | 1560 15 21 17 16 16 21 |NE 54 54 52 54 51 47 50
MEDI | 1457 14 22 16 14 15 16 |MD 55 57 50 55 55 46 50
Table 3.2356.3 GPS week: 2356 Day: 3 MJD: 60739
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 748 36 42 25 22 21 37 13 | 67 42 60 56 49 60 51
R02 | 1908 16 16 15 16 13 16 7 | 58 45 47 52 46 50 48
R03 | 1910 17 15 13 15 16 10 6 | 56 52 49 61 49 47 51
R04 | 970 20 29 17 11 11 10 7 | 56 44 60 59 54 52 53
R05 | 720 9 26 14 11 13 20 7 | 53 41 63 58 60 47 54
R07 | 1574 7 20 16 17 12 17 6 | 56 49 45 59 54 46 50
R08 | 816 20 21 8 10 13 15 6 | 47 49 49 48 45 48 46
R09 | 2499 13 15 16 11 15 11 6 | 17 23 26 19 15 20 16
R11 | 2222 11 19 10 11 15 15 6 | 26 31 35 28 38 21 28
R12 | 1335 8 24 18 15 8 19 7 | 55 65 64 46 53 36 51
R14 | 1218 15 31 15 14 12 13 7 | 53 63 36 41 42 40 43
R15 | 2110 13 21 17 13 14 26 8 | 64 55 64 65 70 51 61
R16 | 932 26 42 27 17 21 16 11 | 78 39 67 50 77 54 61
R17 | 696 26 24 16 26 14 13 9 | 54 49 46 41 34 31 38
R18 | 993 13 25 14 23 15 16 8 | 51 57 44 46 52 36 45
R19E | 1515 40 36 89 39 24 59 23 | 69 67 118 68 71 73 66
R20E | 4921 43 56 43 44 25 43 18 | 67 71 94 59 53 50 54
R21 | 609 20 24 19 12 23 29 9 | 53 37 52 57 59 28 48
R22 | 1295 21 14 12 17 15 15 7 | 26 35 37 42 36 22 31
R24 | 493 14 17 19 30 19 22 9 | 46 32 45 35 41 30 34
XR26 | 8233 63 40 --- --- 37 --- 33 | 68 97 --- --- 92 --- 80
------+-----------------------------------------+-------------------------------------
RMS | 1768 22 28 27 21 17 24 |T 53 49 55 49 51 42 48
WRMS | 1768 18 24 19 16 16 24 |NE 51 47 49 47 50 39 46
MEDI | 1295 17 24 16 15 15 16 |MD 55 49 49 50 52 46 50
Table 3.2356.4 GPS week: 2356 Day: 4 MJD: 60740
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 723 27 44 17 42 13 19 12 | 64 44 52 79 55 58 57
R02 | 975 22 25 16 17 19 20 8 | 85 79 83 99 83 83 84
R03 | 2240 15 17 12 14 13 13 6 | 51 50 51 53 48 42 48
R04 | 778 7 17 12 9 14 9 5 | 63 56 59 64 58 62 59
R05 | 872 12 25 9 11 13 11 6 | 55 60 59 57 61 55 57
R07 | 2623 12 22 17 11 9 18 6 | 95 81 94 87 82 92 88
R08 | 1256 13 22 15 21 16 19 8 | 45 47 40 50 42 33 41
R09 | 2932 15 23 14 21 13 11 7 | 26 28 32 31 30 30 27
R11 | 1726 14 13 15 13 15 11 6 | 31 33 36 20 37 34 30
R12 | 2157 17 26 22 22 18 18 9 | 73 80 57 72 77 57 67
R14 | 1074 10 26 17 18 19 8 7 | 57 70 52 50 66 55 56
R15 | 1428 21 23 14 16 16 10 7 | 78 71 61 71 72 63 68
R16 | 1180 20 41 15 14 18 26 10 | 82 65 78 66 83 57 71
R17 | 632 17 13 25 24 20 12 8 | 62 63 68 55 49 52 56
R18 | 698 16 30 11 26 13 18 8 | 46 51 38 41 42 33 39
R19E | 1972 47 47 58 53 19 27 19 | 93 86 104 105 97 87 92
R20E | 2802 48 49 37 38 22 63 19 | 66 59 69 68 54 58 55
R21 | 679 18 28 12 15 24 27 9 | 52 30 45 52 60 37 45
R22 | 1850 17 23 13 20 17 17 8 | 29 39 33 44 35 30 31
R24 | 567 14 13 23 32 22 22 10 | 48 45 50 40 46 39 42
XR26 | 8766 62 46 --- --- 42 --- 35 | 54 77 --- --- 71 --- 61
------+-----------------------------------------+-------------------------------------
RMS | 1643 22 28 21 24 17 22 |T 59 57 58 60 59 52 55
WRMS | 1643 17 26 15 17 17 22 |NE 57 56 54 57 57 50 54
MEDI | 1256 17 25 15 18 17 18 |MD 57 59 52 55 58 55 56
Table 3.2356.5 GPS week: 2356 Day: 5 MJD: 60741
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 936 30 56 20 43 16 40 15 | 56 35 42 67 54 61 49
R02 | 1385 13 29 13 21 16 15 8 | 63 59 59 54 62 60 58
R03 | 1582 6 20 9 19 9 14 5 | 40 42 45 52 39 36 41
R04 | 1236 19 33 11 16 12 9 7 | 47 40 46 41 43 44 42
R05 | 1234 11 23 25 20 20 19 9 | 37 40 45 41 34 37 35
R07 | 1956 11 12 13 13 10 23 6 | 75 72 83 77 76 66 74
R08 | 641 12 23 12 20 15 19 7 | 39 45 46 42 26 29 35
R09 | 3984 17 19 11 15 15 8 6 | 19 27 33 29 38 29 28
R11 | 982 16 25 10 26 15 15 8 | 23 47 33 48 28 30 31
R12 | 2334 16 26 13 24 16 14 8 | 57 65 55 42 46 53 51
R14 | 732 8 21 14 13 11 17 6 | 46 58 56 54 56 46 51
R15 | 1054 27 23 13 14 15 19 8 | 67 56 57 52 53 39 52
R16 | 1423 22 23 31 30 14 20 10 | 68 57 83 51 64 51 61
R17 | 471 17 16 34 33 17 12 10 | 54 46 67 44 52 44 49
R18 | 729 12 25 19 40 15 12 9 | 38 48 45 39 33 30 34
R19E | 2691 49 46 58 43 24 41 19 | 77 79 85 94 70 69 74
R20E | 2762 45 41 39 29 25 47 17 | 72 62 71 70 58 68 62
R21 | 807 19 24 17 15 10 20 8 | 39 31 38 38 38 31 34
R22 | 2268 18 17 16 15 21 13 7 | 22 35 27 34 36 24 27
R24 | 1120 20 22 24 18 16 34 10 | 51 44 43 47 48 43 44
XR26 | 9996 66 39 --- --- 39 --- 35 | 80 96 --- --- 91 --- 85
------+-----------------------------------------+-------------------------------------
RMS | 1749 22 28 23 25 16 23 |T 50 51 52 50 49 44 48
WRMS | 1749 17 25 16 22 16 23 |NE 48 49 50 47 48 41 46
MEDI | 1236 17 23 14 20 15 17 |MD 51 47 46 47 48 43 49
Table 3.2356.6 GPS week: 2356 Day: 6 MJD: 60742
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2609 28 46 25 28 12 15 11 | 90 49 67 87 68 72 72
R02 | 1301 15 33 11 13 7 8 6 | 89 70 84 86 83 81 82
R03 | 991 7 30 10 11 9 9 5 | 65 62 58 70 63 55 62
R04 | 1044 16 30 14 8 9 11 6 | 75 65 74 70 75 69 71
R05 | 1230 13 26 12 14 6 16 6 | 59 55 60 63 61 63 59
R07 | 1729 16 19 18 15 21 14 8 | 98 101 102 103 102 96 99
R08 | 732 8 14 18 12 11 12 5 | 56 55 50 60 59 52 55
R09 | 3034 14 36 15 21 10 7 7 | 36 47 45 38 38 37 36
R11 | 1508 13 17 17 14 15 12 6 | 41 49 48 51 49 43 45
R12 | 1783 15 26 14 17 14 8 7 | 82 87 76 67 65 73 72
R14 | 1111 10 18 9 15 9 7 5 | 63 76 65 71 64 57 64
R15 | 2133 19 21 14 12 13 13 6 | 94 84 88 86 83 76 84
R16 | 1692 25 28 15 15 12 20 8 | 103 81 95 83 88 75 86
R17 | 574 19 11 25 17 9 22 8 | 74 66 76 58 70 55 65
R18 | 723 8 17 26 17 12 15 7 | 58 63 69 48 56 42 54
R19E | 1253 35 47 30 47 26 62 18 | 94 96 106 100 94 94 93
R20E | 2971 55 58 70 25 24 53 21 | 87 108 109 73 70 77 77
R21 | 857 15 32 26 19 11 20 8 | 59 51 62 55 57 37 52
R22 | 2709 17 20 20 14 17 14 7 | 29 42 36 43 41 32 35
R24 | 1205 15 35 25 18 13 25 9 | 56 40 57 53 57 45 49
XR26 | 7396 64 42 --- --- 31 --- 32 | 83 120 --- --- 113 --- 99
------+-----------------------------------------+-------------------------------------
RMS | 1727 21 30 24 19 14 23 |T 71 69 71 68 69 61 67
WRMS | 1727 17 26 18 16 12 23 |NE 68 66 67 66 68 58 65
MEDI | 1301 15 28 17 15 12 14 |MD 74 65 67 67 65 57 65
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