[IGSREPORT-30397] Wk 2359 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 11 06:16:17 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2359 (Mar 23, 2025 - Mar 29, 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 2.2359.
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:
igl2359[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2359 in the SP3 format.
igl23597.sum Combination Report for GPS Week 2359.
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 | 5.7 ns
1 | 5.0 ns
2 | 5.4 ns
3 | 4.9 ns
4 | 4.6 ns
5 | 5.9 ns
6 | 1.3 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
----+--------+---------------
3 | GFZ | R11
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 1.2359, 1a.2359).
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 2.2359.0-6)
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 3.2359.0-6).
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 2359 summary. (Mar 23, 2025 - Mar 29, 2025)
Table 1.2359.a GPS week : 2359 MJD: 60757.0-60763.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 4 -3 -16 42 .17 19 15 | 16118 1310 6405 59244
| 1 0 1 14 17 15 .03 | 3668 6928
esa n/a| -2 -2 1 -1 -35 34 -.06 36 35 | 17216 -542 6416 59886
| 1 1 2 11 9 58 .05 | 3676 7333
gfz n/a| 1 0 -1 7 0 -29 .00 20 17 | 0 -1027 3048 7390
| 1 1 3 16 20 27 .05 | 0 2696
grg n/a| 2 0 5 -10 3 9 .25 22 20 | 5067 -1189 3021 6947
| 1 1 1 23 14 38 .06 | 1080 2959
iac n/a| 0 1 -8 0 19 -11 -.25 17 15 | 18139 1276 6429 60606
| 1 1 2 23 28 25 .04 | 3447 6315
jgx n/a| 0 -1 1 15 26 -26 -.15 27 27 | 4480 -945 3046 7491
| 1 1 2 16 14 39 .03 | 1295 2659
Table 1.2359.b GPS week : 2359 MJD: 60757.0-60763.0
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 | 13 10 12 13 13 12 15 |
R02 | 8 7 6 5 6 6 6 |
R03 | 5 6 7 5 6 6 6 |
R04 | 6 7 7 6 6 7 6 |
R05 | 5 7 7 5 6 7 7 |
R07 | 5 6 6 8 7 8 7 |
R08 | 7 6 6 6 6 7 10 |
R09 | 7 7 7 8 8 8 10 |
R11 | 8 9 7 32 --- 0 0 |
R12 | 7 7 8 8 9 6 8 |
R14 | 6 5 7 8 8 8 11 |
R15 | 8 7 7 9 8 8 11 |
R16 | 9 9 8 10 9 10 8 |
R17 | 7 8 10 7 8 7 7 |
R18 | 7 7 8 8 9 7 8 |
R19 | 22 22 20 20 21 22 23 |
R20 | 23 20 21 19 22 21 24 |
R21 | 10 9 8 9 7 8 9 |
R22 | 7 7 7 6 6 6 7 |
R24 | 9 8 9 10 8 9 10 |
R26 | 32 34 29 30 38 36 36 |
R27 | --- --- --- --- --- --- 0 |
Table 1.2359.c GPS week : 2359 MJD: 60757.0-60763.0
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 2359 0 | -10 63 69 -553 411 5745 82.5 1644 1644 | 5680 0
brd 2359 1 | -16 56 79 184 1089 5668 83.4 1682 1682 | 4956 0
brd 2359 2 | 49 51 -92 -1061 -979 3622 80.0 7212 7212 | 5389 0
brd 2359 3 | -35 -3 -68 -847 -1431 611 82.3 1352 1352 | 4933 0
brd 2359 4 | 3 41 -6 -2645 70 4604 81.8 1496 1496 | 4610 0
brd 2359 5 | 20 -43 -64 -981 1252 7076 81.2 1668 1668 | 5940 0
brd 2359 6 | 52 -3 42 -436 1946 7319 80.7 1785 1785 | 1330 0
-------------+------------------------------------------------------------+----------------
brd 2359 mean| 9 23 -5 -905 336 4949 81.7 2405 2405 | 4691 0
brd 2359 sdev| 33 40 70 874 1219 2309 1.2 2124 2124 | 1552 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 2.2359.0 GPS week: 2359 Day: 0 MJD: 60757
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 2 17 -17 57 .17 19 15 | 15484 -437 3089 48193
esa n/a| -4 -2 3 -1 -38 -54 -.03 34 30 | 15568 -1542 3106 48982
gfz n/a| 1 0 0 30 -4 -34 -.04 19 17 | 0 -583 2715 7824
grg n/a| 2 1 5 -15 -17 -35 .34 21 15 | 5930 -699 2724 7268
iac n/a| -1 -2 -9 -33 56 15 -.32 19 16 | 18212 -1412 3112 49667
jgx n/a| 0 0 2 3 17 1 -.20 28 28 | 4938 -729 2715 7869
Table 2.2359.1 GPS week: 2359 Day: 1 MJD: 60758
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 4 -4 19 34 .13 18 16 | 16024 -916 3263 48801
esa n/a| -1 -1 -1 0 -27 11 -.13 37 33 | 15869 -1266 3248 48974
gfz n/a| 5 -1 -3 2 -6 -38 -.07 22 16 | 0 -1213 2896 7558
grg n/a| 2 0 6 -28 3 -10 .30 17 17 | 5492 -1315 2883 7160
iac n/a| -1 0 -5 13 -10 -8 -.18 16 14 | 17762 -1019 3259 50259
jgx n/a| 0 -1 0 0 0 -13 -.10 27 27 | 5500 -1349 2911 7705
Table 2.2359.2 GPS week: 2359 Day: 2 MJD: 60759
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 4 -28 -10 54 .15 18 15 | 14703 -1487 3499 49474
esa n/a| -1 0 -2 -12 -22 4 -.06 35 39 | 18550 -8173 3551 50989
gfz n/a| 0 0 -5 -20 -8 -4 .09 21 18 | 0 -1091 2873 8890
grg n/a| 2 -1 1 30 22 -14 .20 19 19 | 5798 -1438 2868 8636
iac n/a| 0 1 -5 30 -18 -27 -.27 16 14 | 16879 -889 3542 50836
jgx n/a| -1 1 4 18 32 -4 -.12 25 25 | 4356 -1389 2857 9039
Table 2.2359.3 GPS week: 2359 Day: 3 MJD: 60760
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 3 -13 -31 21 .19 16 13 | 13264 3398 4419 48810
esa n/a| -3 -1 0 -10 -40 8 -.11 40 41 | 13274 3411 4439 49247
gfz n/a| 1 1 -2 14 36 11 .00 19 18 | 0 3167 2915 6992
grg n/a| 0 -1 6 -9 -11 3 .24 21 21 | 2970 3471 2919 6478
iac n/a| 0 2 -8 8 47 13 -.29 17 17 | 16269 1062 4484 50138
jgx n/a| 2 -1 2 7 22 -70 -.17 25 25 | 3085 3479 2922 6994
Table 2.2359.4 GPS week: 2359 Day: 4 MJD: 60761
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 6 3 -27 24 .20 20 15 | 16415 -2307 4244 49997
esa n/a| -2 -4 2 12 -41 79 -.05 34 39 | 17593 -4172 4249 50619
gfz n/a| 2 -2 -5 10 -29 -35 .04 24 22 | 0 -2356 3230 6967
grg n/a| 2 0 6 -15 15 30 .18 20 17 | 5671 -2641 3230 6532
iac n/a| -1 4 -9 0 30 -11 -.23 16 14 | 17174 -1812 4278 51335
jgx n/a| -1 -1 0 16 33 -47 -.17 25 24 | 5735 -2594 3216 7010
Table 2.2359.5 GPS week: 2359 Day: 5 MJD: 60762
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 0 5 0 -29 48 .19 18 16 | 13039 15955 22695 72364
esa n/a| -3 -2 1 -13 -26 107 -.05 36 30 | 15063 13805 22712 73501
gfz n/a| 2 0 1 15 5 -73 -.03 17 13 | 0 553 3025 5665
grg n/a| 3 -1 3 5 10 82 .28 25 19 | 5376 532 3008 5343
iac n/a| 1 2 -10 -28 25 0 -.24 17 14 | 15075 15389 22717 73616
jgx n/a| 0 -2 0 49 30 -77 -.14 27 27 | 5383 936 3037 5779
Table 2.2359.6 GPS week: 2359 Day: 6 MJD: 60763
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 3 1 -17 55 .16 22 18 | 23903 -5034 3626 97075
esa n/a| -3 -4 4 13 -49 87 .04 38 31 | 24596 -5857 3611 96894
gfz n/a| 0 0 2 -3 3 -31 .03 17 13 | 0 -5667 3683 7837
grg n/a| 4 3 5 -39 0 8 .22 34 34 | 4238 -6235 3519 7216
iac n/a| -1 0 -13 12 3 -59 -.22 21 18 | 25607 -2385 3613 98392
jgx n/a| 0 -3 -1 12 45 26 -.15 29 29 | 2368 -4972 3669 8042
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 3.2359.0 GPS week: 2359 Day: 0 MJD: 60757
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 907 23 54 17 34 26 24 13 | 21 26 21 27 18 20 17
R02 | 2585 11 29 17 14 8 26 7 | 22 33 23 21 21 21 18
R03 | 1424 6 18 9 8 11 13 4 | 20 24 23 21 15 13 16
R04M | 607 15 13 15 14 14 11 6 | 23 24 25 22 20 16 19
R05M | 1603 7 13 12 7 9 13 4 | 22 23 18 21 16 23 17
R07M | 914 7 17 12 9 11 8 4 | 22 26 25 25 26 20 22
R08M | 2105 7 15 20 14 14 21 7 | 24 27 34 20 23 23 22
R09E | 1646 13 21 19 17 16 11 7 | 34 45 50 34 44 34 38
R11 | 2243 17 30 13 19 18 13 8 | 25 34 61 25 26 25 25
R12 | 2700 10 28 16 18 12 13 7 | 81 88 83 77 77 75 79
R14 | 1032 9 21 10 10 10 14 5 | 62 70 61 61 67 57 62
R15M | 1639 15 22 11 18 17 20 7 | 79 68 66 65 76 51 68
R16M | 1110 19 24 19 20 23 16 9 | 96 86 94 79 85 76 85
R17 | 1603 13 12 17 15 10 18 6 | 66 54 77 65 68 46 63
R18 | 929 10 15 15 12 16 25 7 | 52 71 66 58 67 46 58
R19M | 2023 54 42 38 52 42 63 22 | 45 44 66 50 62 45 45
R20 | 1163 38 101 30 35 29 70 22 | 105 61 96 73 87 61 80
R21 | 1136 10 27 25 11 17 38 9 | 75 56 83 71 79 56 71
R22M | 2392 19 19 10 14 18 14 7 | 39 39 39 47 48 38 40
R24 | 628 12 30 25 18 14 27 9 | 69 47 83 68 78 55 68
XR26M |14423 45 42 --- --- 44 --- 31 | 80 79 --- --- 83 --- 81
------+-----------------------------------------+-------------------------------------
RMS | 1644 19 34 19 21 19 28 |T 50 48 54 46 51 40 47
WRMS | 1644 15 30 17 15 16 28 |NE 54 51 61 51 54 43 50
MEDI | 1603 13 22 16 14 16 16 |MD 45 45 61 47 62 38 45
Table 3.2359.1 GPS week: 2359 Day: 1 MJD: 60758
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 640 21 31 28 24 19 9 10 | 20 34 23 15 24 18 18
R02 | 3026 10 30 8 10 11 28 7 | 24 30 20 25 29 20 22
R03 | 522 8 25 18 14 10 10 6 | 20 28 20 20 19 14 16
R04M | 684 12 32 17 13 12 18 7 | 23 27 25 22 15 19 18
R05M | 966 13 12 18 16 10 18 6 | 23 20 20 28 20 18 19
R07M | 1090 13 18 16 10 14 8 6 | 21 19 26 17 22 18 18
R08M | 2084 4 18 13 14 6 20 5 | 20 20 24 16 20 22 19
R09E | 1859 15 19 19 14 16 8 7 | 33 47 42 33 40 36 35
R11 | 1715 17 48 17 12 15 11 8 | 13 28 75 20 22 22 17
R12 | 1913 10 27 22 16 12 13 7 | 83 93 86 76 73 76 79
R14 | 1792 8 26 9 13 7 9 5 | 37 50 32 39 34 33 35
R15M | 2077 15 15 12 14 11 25 7 | 51 40 45 46 45 33 43
R16M | 1399 22 31 15 16 15 19 8 | 62 68 62 59 45 46 54
R17 | 1667 13 27 17 15 12 24 7 | 41 33 48 53 43 33 42
R18 | 822 10 18 13 10 15 24 6 | 35 38 30 35 38 22 32
R19M | 1121 40 60 30 41 41 88 22 | 42 32 42 37 29 62 32
R20 | 2182 38 102 56 29 24 35 19 | 61 42 83 34 46 47 47
R21 | 1094 7 41 18 12 18 31 9 | 45 41 48 41 44 34 40
R22M | 2935 17 22 19 10 10 12 6 | 23 31 39 35 27 30 28
R24 | 988 16 38 26 11 10 17 8 | 45 31 45 45 38 32 38
XR26M |13473 54 44 --- --- 42 --- 33 | 81 77 --- --- 73 --- 75
------+-----------------------------------------+-------------------------------------
RMS | 1682 18 37 22 17 16 27 |T 38 39 41 34 35 31 34
WRMS | 1682 16 33 16 17 14 27 |NE 38 40 46 36 37 31 35
MEDI | 1667 13 27 17 14 12 18 |MD 35 33 39 34 34 30 32
Table 3.2359.2 GPS week: 2359 Day: 2 MJD: 60759
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1579 14 38 42 24 29 11 12 | 20 26 40 24 29 30 19
R02 | 934 11 19 17 10 9 16 6 | 18 18 30 18 17 19 17
R03 | 1547 11 19 20 8 10 18 6 | 16 25 24 17 20 13 15
R04M | 829 18 19 17 12 7 18 6 | 20 25 32 18 19 22 19
R05M | 939 10 29 14 14 14 13 6 | 20 35 32 21 15 25 19
R07M |31640 11 13 12 21 9 11 6 | 20 23 17 17 17 21 16
R08M | 1487 7 21 14 14 12 18 6 | 23 29 25 18 26 23 22
R09E | 1519 14 22 16 11 19 11 7 | 27 48 48 36 34 34 33
R11 | 1451 13 27 10 16 15 9 6 | 16 25 64 19 21 18 18
R12 | 880 20 19 15 21 15 9 7 | 66 59 69 68 60 59 62
R14 | 2138 6 22 14 19 16 16 7 | 54 61 53 49 58 43 51
R15M | 1980 18 19 12 14 11 17 6 | 58 47 44 47 45 31 45
R16M | 820 19 22 11 16 10 25 7 | 68 54 64 60 54 44 57
R17 | 1064 12 30 30 20 10 31 9 | 44 37 75 72 53 36 53
R18 | 576 17 16 13 12 15 24 7 | 37 51 56 59 53 36 47
R19M | 911 46 58 34 45 24 59 19 | 52 28 68 58 42 31 46
R20 | 1826 33 103 39 28 32 57 21 | 69 36 74 39 65 30 50
R21 | 829 11 31 16 16 11 21 7 | 53 37 63 62 49 43 51
R22M | 2809 13 20 11 19 11 12 6 | 32 36 34 48 31 29 33
R24 | 999 13 31 26 15 14 19 8 | 50 39 63 58 49 50 50
XR26M |15696 45 44 --- --- 35 --- 29 | 62 65 --- --- 67 --- 65
------+-----------------------------------------+-------------------------------------
RMS | 7211 18 35 21 19 16 25 |T 39 38 48 40 39 31 37
WRMS | 7211 15 39 18 19 14 25 |NE 40 37 55 44 43 34 39
MEDI | 1451 13 22 15 16 14 17 |MD 37 36 48 39 42 30 45
Table 3.2359.3 GPS week: 2359 Day: 3 MJD: 60760
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1405 15 72 28 24 18 22 12 | 20 26 22 20 32 29 19
R02 | 1552 8 24 8 9 11 12 5 | 14 26 17 16 22 22 15
R03 | 2749 8 23 7 9 10 18 5 | 18 27 16 16 18 19 15
R04M | 730 10 20 12 14 16 10 6 | 16 19 24 23 14 23 17
R05M | 1057 11 14 11 9 13 8 5 | 21 20 27 20 15 20 18
R07M | 890 7 33 10 22 15 19 7 | 17 38 21 15 19 19 14
R08M | 887 9 17 13 11 15 20 6 | 22 27 26 17 21 22 19
R09E | 1888 16 21 23 13 19 12 8 | 33 53 49 49 57 45 45
XR11 |10531 27 --- 427 35 --- --- 31 | 42 --- 221 36 --- --- 32
R12 | 729 13 30 9 25 17 10 7 | 70 64 64 60 59 57 60
R14 | 856 9 17 24 17 10 19 7 | 59 59 64 56 55 45 55
R15M | 1271 16 17 21 17 24 20 8 | 63 48 61 54 41 36 50
R16M | 1052 17 47 16 22 11 23 9 | 71 71 59 68 61 42 60
R17 | 573 10 21 13 15 16 19 6 | 47 43 56 46 56 39 47
R18 | 946 12 20 14 23 12 22 7 | 42 49 45 68 52 40 47
R19M | 1896 45 46 27 55 28 58 19 | 42 33 57 54 54 27 41
R20 | 1197 20 110 32 14 25 58 19 | 65 54 67 61 65 29 55
R21 | 710 14 28 23 16 23 20 9 | 51 38 51 38 59 32 45
R22M | 1970 14 19 9 18 15 8 6 | 19 26 25 27 24 22 19
R24 | 1159 15 34 30 11 17 26 10 | 46 36 71 54 60 44 52
XR26M |14682 40 43 --- --- 43 --- 29 | 68 68 --- --- 55 --- 62
------+-----------------------------------------+-------------------------------------
RMS | 1351 16 40 19 21 17 25 |T 40 41 52 39 41 32 37
WRMS | 1351 13 41 18 21 17 25 |NE 43 42 63 42 47 35 40
MEDI | 1159 14 23 14 16 16 19 |MD 42 38 49 38 52 29 45
Table 3.2359.4 GPS week: 2359 Day: 4 MJD: 60761
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 698 21 49 31 16 28 31 13 | 27 17 25 26 31 36 17
R02 | 853 9 12 16 17 10 9 5 | 20 21 24 17 16 22 17
R03 | 2812 9 20 20 11 8 7 5 | 17 21 22 16 17 15 13
R04M | 2544 12 9 19 9 13 16 6 | 22 19 27 19 22 19 19
R05M | 1331 8 9 21 11 9 14 5 | 24 16 23 18 20 21 19
R07M | 1437 9 32 14 11 13 20 7 | 17 39 29 22 15 25 19
R08M | 810 10 23 11 10 10 16 6 | 22 30 24 17 23 21 20
R09E | 3009 15 25 21 14 15 15 7 | 45 69 70 54 55 53 54
R12 | 817 15 22 16 29 14 13 8 | 85 80 83 81 79 79 80
R14 | 522 12 17 19 21 13 18 7 | 49 53 56 54 49 47 49
R15M | 711 21 17 18 15 19 16 8 | 54 45 52 45 38 39 43
R16M | 967 21 22 21 16 12 22 8 | 65 58 67 53 49 45 54
R17 | 765 7 20 30 13 13 23 8 | 47 35 61 44 51 30 44
R18 | 647 13 23 22 17 19 19 8 | 36 52 51 41 53 33 43
R19M | 837 63 45 42 53 24 49 21 | 36 33 49 37 30 29 25
R20 | 1920 32 105 38 23 28 61 21 | 57 43 51 50 47 24 41
R21 | 1024 8 19 16 20 11 23 7 | 50 41 51 50 45 38 45
R22M | 1950 13 14 18 14 10 7 5 | 32 35 40 42 40 32 35
R24 | 863 9 30 29 17 9 16 8 | 51 36 66 59 53 46 51
XR26M |14383 59 64 --- --- 42 --- 38 | 73 91 --- --- 80 --- 77
------+-----------------------------------------+-------------------------------------
RMS | 1496 20 34 24 20 16 25 |T 41 41 45 39 40 34 38
WRMS | 1496 15 39 22 17 14 24 |NE 43 39 49 43 44 37 40
MEDI | 863 12 22 20 16 13 16 |MD 36 36 51 42 40 32 41
Table 3.2359.5 GPS week: 2359 Day: 5 MJD: 60762
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 832 25 62 17 20 19 26 12 | 21 36 31 18 19 27 18
R02 | 1218 9 26 9 11 14 9 5 | 21 27 19 26 22 21 17
R03 | 2677 9 20 14 17 9 8 5 | 20 26 23 20 20 23 18
R04M | 2154 14 17 10 17 13 21 6 | 15 16 15 18 17 18 13
R05M | 1527 10 13 14 16 11 23 6 | 22 29 20 21 14 17 16
R07M | 1335 11 34 18 21 12 19 8 | 18 36 26 20 21 18 19
R08M | 1268 14 23 13 10 13 15 6 | 21 27 30 19 21 25 19
R09E | 3315 12 20 17 34 11 10 8 | 80 88 88 92 79 82 82
XR11 | ---- 5 --- --- --- --- --- 0 | 34 --- --- --- --- --- 35
R12 | 820 14 18 9 15 8 15 5 | 53 51 47 46 48 48 48
R14 | 913 10 19 14 27 22 18 8 | 84 84 87 91 89 85 85
R15M | 704 18 22 12 23 15 16 7 | 59 49 50 56 55 58 51
R16M | 1127 24 22 22 18 12 26 9 | 67 60 67 58 55 48 58
R17 | 520 8 15 9 17 16 22 6 | 39 38 35 43 49 30 38
R18 | 679 10 21 11 20 16 19 7 | 35 44 37 36 40 33 36
R19M | 1147 47 42 26 53 43 73 21 | 34 33 45 34 48 43 31
R20 | 2680 23 105 32 57 22 56 21 | 44 42 45 62 34 23 37
R21 | 1420 12 31 18 18 6 20 7 | 38 26 48 52 36 37 40
R22M | 2670 12 16 18 12 9 11 6 | 28 24 32 30 28 30 27
R24 | 702 15 36 16 12 20 14 8 | 43 34 47 56 57 53 48
XR26M |13149 53 59 --- --- 45 --- 36 | 32 31 --- --- 26 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1667 18 36 17 25 17 27 |T 38 40 41 42 38 37 36
WRMS | 1667 16 30 13 19 14 27 |NE 39 40 41 45 41 38 38
MEDI | 1218 12 22 14 18 13 19 |MD 34 34 37 36 34 30 35
Table 3.2359.6 GPS week: 2359 Day: 6 MJD: 60763
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 838 35 53 25 43 13 37 14 | 18 28 29 27 21 45 24
R02 | 1448 14 30 10 10 10 9 6 | 19 29 23 20 23 20 20
R03 | 2561 11 13 9 15 14 18 6 | 19 27 18 22 17 23 17
R04M | 2500 12 24 11 11 11 15 6 | 17 21 24 19 25 19 19
R05M | 1021 14 16 11 9 16 18 6 | 23 25 30 27 31 22 25
R07M | 873 14 27 7 29 10 10 7 | 18 21 19 25 19 17 16
XR08M | 1394 20 22 15 --- 24 21 10 | 92 93 91 --- 93 94 92
R09E | 2781 17 16 11 52 16 11 9 | 100 102 103 112 101 100 100
XR11 | ---- 4 --- --- --- --- --- 0 | 16 --- --- --- --- --- 15
R12 | 889 14 18 18 18 12 28 8 | 88 84 85 77 78 68 80
R14 | 950 13 26 12 51 23 14 10 | 123 129 126 114 117 126 121
XR15M | 969 15 21 14 44 18 --- 11 | 116 120 121 118 115 --- 118
R16M | 964 20 27 12 27 14 18 8 | 82 80 75 80 78 71 75
R17 | 1303 9 21 10 14 23 20 7 | 65 53 72 62 81 49 65
R18 | 692 13 18 6 30 26 15 8 | 50 65 60 58 75 47 58
R19M | 993 59 58 35 61 42 58 22 | 46 34 64 61 72 37 48
R20 | 3345 33 99 34 63 32 75 24 | 80 49 86 89 75 35 67
R21 | 720 9 36 13 24 15 23 8 | 62 42 72 75 68 49 62
R22M | 3269 11 21 14 14 18 11 6 | 36 29 46 46 35 39 38
R24 | 916 19 32 15 22 27 22 10 | 71 49 80 65 84 62 70
XR26M |13835 57 36 --- --- 51 --- 36 | 76 76 --- --- 85 --- 78
XR27 |19083 4 --- --- --- --- --- 0 | 5 --- --- --- --- --- 5
------+-----------------------------------------+-------------------------------------
RMS | 1785 22 38 17 34 21 29 |T 55 57 64 60 64 51 55
WRMS | 1785 18 31 13 34 18 29 |NE 51 55 65 60 63 52 50
MEDI | 1021 14 24 12 24 16 18 |MD 50 49 72 61 75 45 58
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