[IGSREPORT-30431] Wk 2363 IGLOS Final Orbits
acc
acc at igs.org
Thu May 8 06:15:03 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2363 (Apr 20, 2025 - Apr 26, 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 2.2363.
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:
igl2363[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2363 in the SP3 format.
igl23637.sum Combination Report for GPS Week 2363.
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 | 5.8 ns
1 | 3.8 ns
2 | 1.2 ns
3 | 3.8 ns
4 | 2.3 ns
5 | 4.8 ns
6 | 4.3 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
----+--------+---------------
0 | ESA | R20
4 | ESA | R20
5 | ESA | R20
6 | ESA | R20
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 1.2363, 1a.2363).
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 2.2363.0-6)
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 3.2363.0-6).
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 2363 summary. (Apr 20, 2025 - Apr 26, 2025)
Table 1.2363.a GPS week : 2363 MJD: 60785.0-60791.0
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| -2 0 4 10 -10 31 .11 17 15 | 4141 714 4280 15773
| 0 0 1 12 21 28 .05 | 1754 1818
esa n/a| -4 -1 1 -2 -24 41 -.08 37 38 | 5802 -177 4050 14554
| 0 2 1 13 13 32 .04 | 1674 2015
gfz n/a| 1 0 -1 20 -1 -5 .06 18 15 | 0 536 4053 14048
| 1 0 3 12 15 34 .04 | 0 1631
grg n/a| 1 0 2 -41 -5 -11 .25 24 18 | 3184 528 3449 7337
| 1 2 2 14 14 25 .06 | 1791 2227
iac n/a| 0 0 -1 9 25 -28 -.15 16 16 | 2169 -397 4223 14803
| 1 1 2 13 20 40 .05 | 3561 1425
jgx n/a| 0 -1 -7 0 11 -20 -.19 24 24 | 7781 575 3432 7529
| 1 0 2 12 11 19 .03 | 2765 2204
Table 1.2363.b GPS week : 2363 MJD: 60785.0-60791.0
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
------+------------------------------------+------------------------------------------
R02 | 6 6 6 7 7 6 6 |
R03 | 6 8 7 7 6 6 5 |
R04 | 6 7 7 7 7 7 7 |
R05 | 5 6 6 6 8 6 7 |
R07 | 5 7 7 6 8 8 6 |
R08 | 6 6 7 6 7 9 8 |
R09 | 6 6 7 8 6 7 14 |
R11 | 7 6 6 7 7 7 6 |
R12 | 8 7 8 7 7 7 8 |
R14 | 8 5 6 7 6 6 6 |
R15 | 8 7 7 8 7 6 8 |
R16 | 8 10 7 8 8 8 9 |
R17 | 7 8 8 9 7 6 6 |
R18 | 8 10 8 10 9 7 8 |
R19 | 21 20 24 19 18 23 21 |
R20 | 18 26 23 21 15 17 19 |
R21 | 9 8 7 6 7 6 6 |
R22 | 9 7 7 8 6 8 8 |
R24 | 10 9 9 7 9 8 9 |
R26 | 27 26 29 29 28 31 30 |
R27 | 47 41 33 43 47 46 54 |
Table 1.2363.c GPS week : 2363 MJD: 60785.0-60791.0
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 2363 0 | 17 89 123 -2016 -1541 5926 81.4 2141 2141 | 5781 0
brd 2363 1 | 24 29 115 -1273 251 1198 84.1 2099 2099 | 3813 0
brd 2363 2 | 83 -60 185 2361 1012 2967 80.9 2088 2088 | 1169 0
brd 2363 3 | 62 96 194 536 1430 8845 81.3 2084 2084 | 3769 0
brd 2363 4 | 51 104 114 -183 867 9383 80.8 1945 1945 | 2283 0
brd 2363 5 | 46 51 18 -1485 -1045 9874 78.9 2292 2292 | 4799 0
brd 2363 6 | -10 53 99 -1620 50 7960 79.0 1946 1946 | 4335 0
-------------+------------------------------------------------------------+----------------
brd 2363 mean| 39 51 121 -525 146 6593 80.9 2085 2085 | 3707 0
brd 2363 sdev| 31 56 58 1553 1095 3371 1.7 119 119 | 1547 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 2.2363.0 GPS week: 2363 Day: 0 MJD: 60785
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 17 -12 27 .02 18 17 | 4884 2906 4218 8729
esa n/a| -3 -1 4 -7 -36 59 -.06 36 44 | 6463 387 4215 8508
gfz n/a| 1 0 -4 12 -6 38 .06 19 18 | 0 3123 4213 8955
grg n/a| 2 2 0 -66 -5 -1 .17 22 22 | 3239 4399 3976 8859
iac n/a| 1 0 -2 9 29 -67 -.08 16 15 | 8159 -1522 4214 9112
jgx n/a| 0 0 -5 8 36 -23 -.17 23 23 | 4372 4399 4019 8924
Table 2.2363.1 GPS week: 2363 Day: 1 MJD: 60786
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 5 -13 -11 25 .10 17 15 | 6339 387 3370 8368
esa n/a| -4 -4 0 -8 -6 69 -.05 38 40 | 8096 911 3156 7375
gfz n/a| 3 0 -2 36 -9 3 .12 17 15 | 0 443 3139 7402
grg n/a| 0 1 5 -23 9 -41 .20 27 24 | 3667 -349 2759 7338
iac n/a| 0 0 -2 9 5 -30 -.15 18 17 | 5386 -653 3365 8065
jgx n/a| 2 -2 -7 9 7 -11 -.20 23 23 | 7927 -328 2747 7468
Table 2.2363.2 GPS week: 2363 Day: 2 MJD: 60787
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 -40 21 .17 19 16 | 1872 949 4744 10432
esa n/a| -4 0 3 18 -42 59 -.16 37 41 | 3322 1587 4347 8361
gfz n/a| 1 1 -5 22 0 33 .04 17 12 | 0 916 4484 7964
grg n/a| 1 1 3 -52 7 -41 .23 27 18 | -378 2523 3522 7121
iac n/a| 0 -1 0 8 41 -25 -.15 16 15 | 110 534 4735 9498
jgx n/a| 1 -1 -6 -26 5 -10 -.16 26 26 | 3655 2427 3515 7303
Table 2.2363.3 GPS week: 2363 Day: 3 MJD: 60788
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 4 2 -29 56 .14 14 13 | 5358 639 3321 13119
esa n/a| -3 -4 0 2 -32 14 -.09 34 35 | 7009 409 3371 11933
gfz n/a| 1 0 -1 19 30 1 .03 16 13 | 0 748 3341 10975
grg n/a| 0 -1 1 -30 -14 -21 .25 23 15 | 3089 845 3224 7455
iac n/a| 2 -1 0 36 50 -71 -.17 20 21 | 2936 -1129 3291 11928
jgx n/a| -1 -1 -6 3 7 2 -.26 22 22 | 8350 1121 3090 7637
Table 2.2363.4 GPS week: 2363 Day: 4 MJD: 60789
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 3 12 -14 61 .09 17 15 | 4628 -2548 4714 16747
esa n/a| -4 0 1 7 -11 1 -.02 37 45 | 6436 -4136 4485 14820
gfz n/a| 0 0 0 0 -5 -46 .11 19 18 | 0 -2466 4466 13737
grg n/a| 2 -1 2 -35 -25 -11 .26 18 14 | 2864 -1569 3799 6336
iac n/a| 1 3 0 1 43 -8 -.24 14 13 | 408 -2015 4363 14663
jgx n/a| 3 -2 -12 8 10 -29 -.18 23 23 | 9110 -1577 3800 6616
Table 2.2363.5 GPS week: 2363 Day: 5 MJD: 60790
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 26 14 -21 .07 17 15 | 1648 2649 5492 28986
esa n/a| -3 2 0 -20 -22 76 -.10 39 31 | 5121 -1566 4766 27281
gfz n/a| 2 -1 3 33 -19 -47 .03 20 16 | 0 319 4766 26343
grg n/a| 1 -3 4 -45 7 24 .30 22 22 | 5290 -1514 3351 7499
iac n/a| -1 0 -5 -5 0 46 -.15 15 13 | -2137 2212 5489 27702
jgx n/a| 0 -1 -7 1 7 -58 -.16 24 24 | 10673 -1421 3371 7719
Table 2.2363.6 GPS week: 2363 Day: 6 MJD: 60791
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 6 14 18 53 .16 17 15 | 4261 19 4105 24031
esa n/a| -5 -1 2 -11 -17 6 -.10 42 34 | 4173 1168 4010 23602
gfz n/a| 1 0 1 17 2 -22 .05 18 16 | 0 673 3968 22960
grg n/a| 3 -2 0 -38 -19 10 .33 28 15 | 4521 -638 3517 6754
iac n/a| 1 0 -3 9 9 -42 -.14 16 14 | 325 -210 4104 22659
jgx n/a| 0 -1 -9 0 3 -11 -.18 26 26 | 10380 -595 3484 7039
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 3.2363.0 GPS week: 2363 Day: 0 MJD: 60785
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1401 16 13 12 7 16 7 5 | 62 70 62 67 73 59 65
R03 | 976 10 10 13 14 13 13 5 | 62 74 68 70 60 55 63
R04 | 916 14 11 12 7 7 22 5 | 63 58 58 60 56 50 56
R05 | 863 11 17 12 6 12 10 5 | 61 57 60 61 53 58 57
R07 | 999 8 11 12 7 13 9 4 | 66 54 61 65 66 58 61
R08 | 678 15 12 13 8 7 18 5 | 61 62 68 66 66 61 63
R09E | 2126 13 18 12 15 13 10 6 | 30 36 35 39 32 26 31
R11E | 6950 12 12 20 16 12 11 6 | 23 29 34 30 28 25 26
R12E | 1069 11 27 22 17 15 16 8 | 255 247 249 263 256 254 254
R14E | 988 16 18 19 23 9 11 7 | 57 54 58 64 58 58 57
R15E | 824 10 18 25 23 9 13 7 | 44 45 52 52 50 42 45
R16E | 1369 14 15 20 25 15 16 8 | 78 82 75 85 75 77 77
R17 | 1203 7 21 17 10 15 17 6 | 56 48 53 50 58 47 52
R18 | 1329 25 16 13 13 24 12 8 | 49 61 52 52 56 47 51
R19 | 1609 46 56 28 52 29 64 21 | 66 45 72 68 74 79 66
R20 | 1713 15 128 37 51 12 48 18 | 100 56 108 123 99 92 103
R21 | 1181 15 24 26 13 14 22 8 | 56 52 64 63 58 47 55
R22 | 3363 17 28 15 23 11 19 8 | 74 84 81 75 79 80 77
R24 | 1479 23 27 14 18 30 15 10 | 59 46 57 55 63 52 54
XR26 |10939 46 62 36 --- 41 --- 26 | 85 122 89 --- 118 --- 100
XR27 | 7545 49 --- --- --- 45 --- 47 | 76 --- --- --- 133 --- 106
------+-----------------------------------------+-------------------------------------
RMS | 2141 18 36 19 22 16 23 |T 70 69 72 74 76 66 72
WRMS | 2141 17 44 18 22 15 23 |NE 66 63 68 67 74 60 68
MEDI | 1329 15 18 15 15 13 15 |MD 62 56 61 64 63 58 61
Table 3.2363.1 GPS week: 2363 Day: 1 MJD: 60786
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1356 7 20 14 9 19 11 6 | 42 48 36 37 43 27 36
R03 | 819 18 30 15 24 11 11 8 | 42 67 62 53 51 49 51
R04 | 699 14 23 15 13 16 15 7 | 50 53 54 47 44 43 47
R05 | 817 16 15 11 13 12 16 6 | 48 38 47 43 37 33 40
R07 | 1044 10 23 16 9 22 14 7 | 46 38 45 38 50 40 42
R08 | 870 10 16 13 9 23 8 6 | 40 41 37 43 49 47 41
R09E | 3886 14 19 13 8 15 11 6 | 23 25 28 25 27 21 22
R11E | 5796 14 16 13 13 10 14 6 | 24 26 36 26 26 23 25
R12E | 1694 15 18 17 11 16 11 6 | 277 278 274 283 273 277 277
R14E | 1004 9 15 8 16 10 12 5 | 42 40 37 49 37 39 39
R15E | 1215 9 19 16 18 16 14 7 | 51 51 51 57 52 54 51
R16E | 868 12 22 16 31 23 22 9 | 66 76 65 73 63 74 66
R17 | 1485 8 18 13 13 23 27 8 | 27 33 30 26 29 25 25
R18 | 1384 16 28 26 21 26 10 9 | 27 39 31 27 29 30 25
R19 | 2040 53 73 24 58 26 30 19 | 48 37 28 27 29 47 27
R20 | 1662 12 115 26 81 19 74 25 | 40 32 43 64 39 42 38
R21 | 526 12 34 22 17 11 17 8 | 29 27 33 35 25 23 26
R22 | 2234 13 20 8 19 10 18 6 | 51 56 61 47 60 64 55
R24 | 2651 14 35 13 13 23 16 8 | 31 27 24 29 35 26 26
XR26 |11333 32 79 32 --- 45 --- 25 | 61 97 68 --- 75 --- 69
XR27 | 8885 36 --- --- --- 45 --- 40 | 64 --- --- --- 92 --- 75
------+-----------------------------------------+-------------------------------------
RMS | 2098 17 38 17 27 18 23 |T 53 56 54 54 55 51 52
WRMS | 2098 15 40 15 24 17 23 |NE 43 45 42 39 45 38 41
MEDI | 1384 14 20 15 13 19 14 |MD 42 39 37 43 43 40 40
Table 3.2363.2 GPS week: 2363 Day: 2 MJD: 60787
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 881 11 20 12 19 10 16 6 | 46 49 49 38 37 50 43
R03 | 680 17 31 11 12 13 14 7 | 46 67 57 56 55 43 52
R04 | 683 17 18 12 15 15 8 6 | 54 48 54 52 50 47 50
R05 | 1611 15 23 11 11 9 12 6 | 51 55 51 51 51 42 49
R07 | 745 5 12 12 12 23 15 6 | 52 44 47 60 64 48 52
R08 | 610 12 20 10 13 24 16 7 | 45 49 50 55 57 41 49
R09E | 4192 15 24 14 11 13 12 6 | 18 31 32 25 31 22 24
R11E | 5607 14 18 17 12 10 11 6 | 23 25 34 24 30 26 25
R12E | 2024 15 25 12 23 12 16 7 | 138 144 132 126 133 133 133
R14E | 1495 9 21 13 17 14 11 6 | 30 31 30 36 28 23 27
R15E | 1858 11 20 9 25 11 12 6 | 56 58 55 54 59 51 54
R16E | 1124 10 20 15 23 16 8 7 | 56 58 53 64 55 51 54
R17 | 1962 8 25 16 10 21 26 8 | 38 36 41 35 43 34 37
R18 | 1296 12 19 11 14 16 32 8 | 37 40 37 32 29 31 32
R19 | 1855 62 80 41 67 22 58 24 | 49 50 65 44 55 51 46
R20 | 2229 21 106 27 70 28 63 23 | 69 48 75 98 72 71 71
R21 | 699 7 20 11 22 11 19 6 | 38 32 30 50 40 30 35
R22 | 929 18 21 8 19 9 11 6 | 61 70 69 80 70 72 69
R24 | 1507 14 29 19 13 18 32 9 | 42 37 42 35 38 30 36
XR26 |14172 25 68 50 --- 60 --- 29 | 121 147 120 --- 138 --- 126
XR27 |12167 31 --- --- --- 34 --- 33 | 64 --- --- --- 78 --- 70
------+-----------------------------------------+-------------------------------------
RMS | 2088 19 37 17 27 16 26 |T 54 55 56 53 57 47 54
WRMS | 2088 16 41 12 18 15 26 |NE 54 55 56 52 58 45 54
MEDI | 1507 14 21 12 15 15 15 |MD 49 48 50 51 55 43 49
Table 3.2363.3 GPS week: 2363 Day: 3 MJD: 60788
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 885 13 20 12 14 19 7 6 | 43 35 37 47 53 37 41
R03 | 514 13 24 17 9 21 14 7 | 49 53 42 49 51 36 44
R04 | 714 16 16 10 12 26 9 7 | 43 43 39 37 50 39 40
R05 | 1215 8 13 14 12 20 8 6 | 41 41 33 43 50 34 38
R07 | 1131 7 20 14 13 9 9 5 | 59 52 52 58 50 50 53
R08 | 1159 8 30 10 10 12 8 6 | 50 47 53 54 54 49 50
R09E | 3528 13 17 17 21 20 12 7 | 25 22 30 29 33 23 23
R11E | 4764 12 16 16 12 15 16 6 | 21 28 36 25 29 26 25
R12E | 844 10 20 14 24 15 12 7 | 193 189 197 196 198 196 195
R14E | 3483 9 16 18 16 11 16 6 | 31 32 34 36 30 28 29
R15E | 3730 9 21 15 11 25 18 7 | 44 52 40 49 36 47 41
R16E | 2153 15 20 15 11 27 19 8 | 59 70 70 69 52 71 62
R17 | 1929 8 22 13 14 30 26 8 | 36 37 39 38 51 31 37
R18 | 887 19 18 19 7 30 30 9 | 39 44 48 41 44 32 39
R19 | 973 28 67 19 60 23 46 18 | 56 45 60 52 58 56 51
R20 | 1738 27 100 24 52 25 50 20 | 79 45 65 75 71 76 70
R21 | 827 10 21 6 10 11 16 5 | 49 37 45 54 50 40 46
R22 | 924 13 16 21 25 8 14 7 | 45 44 47 53 48 42 44
R24 | 557 12 27 15 10 10 13 6 | 47 39 42 41 47 42 42
XR26 | 9819 36 87 35 --- 56 --- 29 | 90 122 89 --- 106 --- 94
XR27 |13855 33 --- --- --- 54 --- 42 | 50 --- --- --- 90 --- 66
------+-----------------------------------------+-------------------------------------
RMS | 2084 14 34 16 23 20 22 |T 54 53 54 55 59 50 53
WRMS | 2084 13 35 13 15 21 22 |NE 51 48 49 49 58 43 50
MEDI | 1159 13 20 15 12 20 14 |MD 47 44 42 49 50 40 44
Table 3.2363.4 GPS week: 2363 Day: 4 MJD: 60789
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1054 12 8 9 16 15 20 6 | 38 41 42 52 50 28 42
R03 | 2205 9 20 17 10 11 15 6 | 38 44 31 39 40 27 35
R04 | 911 17 19 15 17 14 15 7 | 45 34 42 47 25 30 36
R05 | 539 18 22 24 11 15 10 7 | 39 35 43 40 36 29 35
R07 | 867 11 33 25 8 12 12 7 | 42 44 60 42 49 44 45
R08 | 2266 9 26 18 12 12 17 6 | 42 43 54 46 41 34 42
R09E | 4911 11 18 14 10 13 11 5 | 18 30 29 27 25 24 22
R11E | 3640 15 17 17 14 16 18 7 | 22 22 35 23 28 27 23
R12E | 1018 9 16 18 22 9 12 6 | 98 103 102 112 96 97 100
R14E | 1765 9 14 16 17 9 17 6 | 35 37 42 44 38 34 37
R15E | 1459 9 17 19 12 12 16 6 | 37 34 47 39 41 33 37
R16E | 2238 14 27 22 11 12 20 7 | 63 77 72 68 66 63 66
R17 | 889 6 18 21 14 9 22 6 | 38 36 47 37 34 34 36
R18 | 617 17 24 18 12 20 30 9 | 33 42 39 30 43 25 33
R19 | 1565 43 58 32 42 24 48 18 | 59 34 57 48 49 57 46
R20 | 1901 26 126 24 33 17 45 14 | 80 43 84 64 67 83 73
R21 | 852 10 22 14 15 10 17 6 | 46 45 50 41 44 45 43
R22 | 1386 14 13 16 7 10 17 5 | 76 70 81 76 81 84 77
R24 | 560 21 30 14 13 14 25 8 | 43 35 38 43 38 38 37
XR26 | 9390 42 67 45 --- 47 --- 28 | 119 143 128 --- 136 --- 129
XR27 | 9636 48 --- --- --- 44 --- 46 | 46 --- --- --- 92 --- 70
------+-----------------------------------------+-------------------------------------
RMS | 1944 17 37 19 18 14 23 |T 50 49 56 48 53 44 50
WRMS | 1944 15 45 18 14 13 23 |NE 52 49 56 46 55 42 51
MEDI | 1459 14 20 18 13 13 17 |MD 42 41 47 43 43 34 42
Table 3.2363.5 GPS week: 2363 Day: 5 MJD: 60790
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1401 7 22 9 12 9 12 5 | 56 52 53 51 49 46 50
R03 | 2759 8 13 19 10 13 8 5 | 53 43 41 44 50 52 47
R04 | 824 22 12 18 17 11 9 7 | 54 47 45 54 39 49 47
R05 | 542 17 8 14 12 9 7 5 | 48 49 47 50 39 45 45
R07 | 778 12 27 18 19 8 15 7 | 54 46 66 64 51 52 55
R08 | 2930 14 32 19 19 16 16 8 | 47 45 60 45 45 50 47
R09E | 5777 10 16 15 17 17 13 6 | 28 33 34 30 32 30 29
R11E | 3387 10 17 22 12 11 13 6 | 27 30 43 31 28 30 29
R12E | 1543 14 18 17 24 8 13 7 | 172 173 175 174 177 174 173
R14E | 1293 10 14 19 16 7 11 6 | 31 31 35 40 33 26 30
R15E | 1491 9 17 14 13 10 17 6 | 30 28 37 36 31 28 29
R16E | 3112 12 24 30 11 12 18 8 | 75 73 75 72 68 69 70
R17 | 593 10 15 10 12 15 15 6 | 38 35 35 38 24 36 32
R18 | 562 14 23 14 12 11 13 6 | 34 37 34 31 26 33 30
R19 | 1090 52 56 24 63 38 70 23 | 67 62 62 65 40 62 55
R20 | 2472 23 138 41 34 12 51 16 | 78 39 83 50 57 65 65
R21 | 1733 8 18 14 8 10 17 5 | 35 30 42 39 36 39 36
R22 | 2809 14 25 13 15 14 19 7 | 56 88 66 79 67 66 68
R24 | 633 11 19 13 16 17 25 7 | 44 37 33 35 32 36 34
XR26 |13324 42 67 55 --- 51 --- 30 | 161 165 143 --- 162 --- 157
XR27 | 9334 48 --- --- --- 43 --- 45 | 56 --- --- --- 77 --- 67
------+-----------------------------------------+-------------------------------------
RMS | 2292 17 39 20 22 15 24 |T 59 57 60 54 55 52 56
WRMS | 2292 15 31 16 22 13 24 |NE 58 55 57 49 52 48 55
MEDI | 1543 12 18 17 15 12 15 |MD 53 43 45 45 40 46 47
Table 3.2363.6 GPS week: 2363 Day: 6 MJD: 60791
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 732 8 20 11 14 10 16 5 | 59 54 52 59 57 49 54
R03 | 1590 7 11 12 14 13 11 5 | 60 60 53 60 59 51 56
R04 | 718 22 18 15 6 10 12 6 | 63 56 49 56 46 50 52
R05 | 434 11 16 20 10 16 15 6 | 51 44 43 48 42 44 43
R07 | 755 8 14 11 25 10 11 6 | 61 61 68 76 65 62 64
R08 | 2164 8 31 9 11 17 25 8 | 58 60 65 63 67 55 60
R09E | 3771 12 22 20 75 21 14 14 | 37 42 41 80 39 32 38
R11E | 3034 12 22 14 9 7 12 5 | 19 32 34 22 22 22 22
R12E | 2927 15 25 13 21 18 16 8 | 231 232 228 224 229 226 228
R14E | 1749 11 15 17 17 11 11 6 | 65 67 69 70 60 67 65
R15E | 1260 8 19 27 19 10 11 7 | 43 37 55 49 43 43 43
R16E | 2753 15 30 24 21 10 15 8 | 83 96 98 86 91 86 88
R17 | 700 8 19 14 15 12 12 6 | 59 56 60 58 55 53 56
R18 | 864 16 23 15 14 16 23 8 | 52 65 59 52 56 48 53
R19 | 948 46 66 17 67 28 61 21 | 83 63 80 81 70 67 72
R20 | 2672 24 143 32 26 29 69 19 | 111 68 121 113 113 97 109
R21 | 1940 6 21 15 10 11 19 6 | 67 57 70 69 68 65 66
R22 | 2273 21 30 14 19 14 12 8 | 82 98 89 90 91 91 88
R24 | 708 15 34 19 11 21 18 9 | 65 58 63 63 62 58 61
XR26 |10420 54 60 31 --- 59 --- 30 | 178 210 174 --- 208 --- 188
XR27 |10462 54 --- --- --- 52 --- 53 | 68 --- --- --- 129 --- 96
------+-----------------------------------------+-------------------------------------
RMS | 1946 17 42 18 28 16 26 |T 75 75 78 74 79 66 76
WRMS | 1946 15 34 16 15 14 26 |NE 74 72 74 68 79 60 74
MEDI | 1749 12 22 15 15 14 15 |MD 63 60 63 63 62 55 61
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