[IGSREPORT-30388] Wk 2358 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 4 00:51:01 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2358 (Mar 16, 2025 - Mar 22, 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 2.2358.
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:
igl2358[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2358 in the SP3 format.
igl23587.sum Combination Report for GPS Week 2358.
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 | 6.0 ns
1 | 4.6 ns
2 | 6.6 ns
3 | 4.9 ns
4 | 7.1 ns
5 | 4.5 ns
6 | 6.5 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 1.2358, 1a.2358).
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 2.2358.0-6)
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 3.2358.0-6).
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 2358 summary. (Mar 16, 2025 - Mar 22, 2025)
Table 1.2358.a GPS week : 2358 MJD: 60750.0-60756.0
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 2 6 -9 29 .13 21 16 | 15244 305 4224 46905
| 0 0 1 19 14 20 .04 | 1266 1687
esa n/a| -2 0 1 -6 -40 21 .01 34 26 | 16755 -1825 4138 47952
| 1 1 2 14 27 70 .02 | 1305 3000
gfz n/a| 0 0 -3 13 -10 -14 -.01 25 20 | 0 249 3704 8222
| 1 1 2 22 11 25 .04 | 0 1838
grg n/a| 1 0 6 -13 -4 32 .29 21 18 | 5563 95 3699 7808
| 1 0 1 12 10 45 .06 | 506 1816
iac n/a| 0 0 -7 -9 4 -37 -.22 17 16 | 17457 210 4141 48477
| 1 0 2 22 21 67 .07 | 1104 1130
jgx n/a| 0 0 3 13 21 -8 -.15 27 26 | 5169 203 3698 8273
| 1 1 2 21 17 20 .03 | 855 1832
Table 1.2358.b GPS week : 2358 MJD: 60750.0-60756.0
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 | 11 10 16 12 13 16 11 |
R02 | 8 7 8 7 7 6 8 |
R03 | 8 7 7 8 8 6 8 |
R04 | 8 7 7 7 6 6 5 |
R05 | 6 8 9 8 7 6 7 |
R07 | 7 6 8 10 7 7 6 |
R08 | 9 9 7 7 6 7 6 |
R09 | 7 8 7 7 6 7 7 |
R11 | 6 7 8 6 7 8 7 |
R12 | 8 8 9 11 8 8 7 |
R14 | 6 8 7 6 9 8 7 |
R15 | 7 8 9 8 8 9 11 |
R16 | 8 9 11 9 8 11 12 |
R17 | 7 9 7 6 9 7 7 |
R18 | 7 7 7 6 6 11 10 |
R19 | 19 20 24 18 20 22 20 |
R20 | 23 24 24 22 26 24 23 |
R21 | 10 10 10 8 10 9 10 |
R22 | 7 8 8 6 7 7 9 |
R24 | 10 10 13 8 9 12 11 |
R26 | 33 36 35 29 30 30 28 |
Table 1.2358.c GPS week : 2358 MJD: 60750.0-60756.0
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 2358 0 | 17 67 65 -392 807 3308 81.7 1748 1748 | 6032 0
brd 2358 1 | 55 23 97 41 -1180 4649 79.3 1943 1943 | 4600 0
brd 2358 2 | -87 143 -20 -1791 -1094 3958 79.1 1858 1858 | 6593 0
brd 2358 3 | -41 26 11 93 -709 4521 81.4 1754 1754 | 4887 0
brd 2358 4 | -8 -19 -129 519 422 2613 83.3 1635 1635 | 7123 0
brd 2358 5 | 39 -8 -54 -306 782 1030 82.6 1592 1592 | 4483 0
brd 2358 6 | 12 31 -44 297 2793 3244 80.7 1628 1628 | 6520 0
-------------+------------------------------------------------------------+----------------
brd 2358 mean| -1 37 -10 -219 260 3331 81.2 1736 1736 | 5748 0
brd 2358 sdev| 49 54 76 762 1406 1249 1.6 129 129 | 1075 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 2.2358.0 GPS week: 2358 Day: 0 MJD: 60750
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 2 -8 -13 25 .13 22 17 | 13775 1520 3936 45618
esa n/a| -2 -1 1 6 -47 61 -.00 35 28 | 17146 -4490 3935 46803
gfz n/a| -1 0 0 18 3 2 -.03 25 18 | 0 2013 3699 8247
grg n/a| 3 -1 9 -12 -13 62 .35 21 18 | 5049 1734 3688 7716
iac n/a| -1 0 -6 -16 24 -54 -.15 14 12 | 17029 608 3930 46834
jgx n/a| 0 0 0 35 26 -7 -.13 25 25 | 3983 1834 3696 8222
Table 2.2358.1 GPS week: 2358 Day: 1 MJD: 60751
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 -5 -9 49 .12 21 17 | 13358 144 4036 43430
esa n/a| -5 0 1 -27 -4 44 -.02 30 24 | 17974 -6850 4071 44951
gfz n/a| 1 -1 -5 20 -14 -16 .05 25 21 | 0 -288 3145 7606
grg n/a| 0 0 4 5 -7 41 .28 23 17 | 4814 -589 3131 7155
iac n/a| 0 1 -4 10 8 -82 -.24 16 16 | 15773 -551 4063 44577
jgx n/a| 0 0 4 -6 17 -1 -.16 26 26 | 5298 -465 3130 7787
Table 2.2358.2 GPS week: 2358 Day: 2 MJD: 60752
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 2 1 8 22 .12 20 16 | 15639 1903 4712 47383
esa n/a| 0 0 0 -15 -62 -29 .04 35 28 | 15646 1734 4750 48653
gfz n/a| 2 1 -7 6 -26 -53 -.03 28 19 | 0 1755 3778 8011
grg n/a| 0 1 5 -25 -9 107 .31 22 20 | 5631 1593 3772 7582
iac n/a| 0 0 -5 9 33 -40 -.29 19 18 | 17123 2005 4762 48656
jgx n/a| -1 1 1 -5 -9 -13 -.13 33 33 | 6528 1743 3741 8157
Table 2.2358.3 GPS week: 2358 Day: 3 MJD: 60753
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 2 42 -16 33 .10 22 17 | 15230 -1203 4619 48194
esa n/a| 0 -3 0 -21 -44 -28 .04 35 26 | 15989 -880 4625 48350
gfz n/a| 1 2 -2 35 -4 3 -.01 23 18 | 0 -1132 4182 8963
grg n/a| 2 0 3 -31 6 -35 .30 15 15 | 5680 -1110 4169 8548
iac n/a| -1 -1 -6 -23 -12 52 -.26 17 16 | 16867 -276 4644 49583
jgx n/a| -2 0 2 19 7 -44 -.13 22 22 | 4497 -1082 4180 8901
Table 2.2358.4 GPS week: 2358 Day: 4 MJD: 60754
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 2 -1 8 0 .10 20 16 | 16941 2088 4431 47789
esa n/a| -1 0 0 -3 -30 -73 .01 31 21 | 18964 422 4466 48434
gfz n/a| 0 0 -5 37 -12 -42 .01 24 17 | 0 2136 4235 7203
grg n/a| 1 0 6 -16 5 15 .20 23 18 | 5776 2106 4244 6821
iac n/a| -2 0 -9 -49 -21 60 -.16 18 15 | 18968 1347 4449 49447
jgx n/a| -1 -2 5 50 35 -7 -.13 25 25 | 5907 2213 4244 7269
Table 2.2358.5 GPS week: 2358 Day: 5 MJD: 60755
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 -8 -30 16 .11 21 17 | 15720 -2440 4313 47786
esa n/a| -1 -1 6 3 -11 138 -.01 35 26 | 15780 -2502 3553 49559
gfz n/a| 0 2 -2 11 2 -11 -.09 26 26 | 0 -2766 3650 8899
grg n/a| 2 0 6 -5 7 31 .22 20 18 | 5624 -2877 3639 8543
iac n/a| -1 0 -10 0 -17 -93 -.15 18 17 | 17785 -932 3598 50579
jgx n/a| 1 -2 6 1 42 23 -.22 31 25 | 5165 -2783 3655 8980
Table 2.2358.6 GPS week: 2358 Day: 6 MJD: 60756
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 23 -16 60 .23 21 16 | 16049 124 3524 48141
esa n/a| -1 3 2 10 -83 35 -.00 34 26 | 15788 -211 3567 48917
gfz n/a| 1 0 -1 -31 -19 17 .03 23 19 | 0 30 3239 8627
grg n/a| 2 0 7 -8 -20 5 .36 23 19 | 6368 -191 3255 8297
iac n/a| 0 0 -9 4 13 -103 -.30 16 15 | 18660 -727 3541 49667
jgx n/a| -1 0 4 1 27 -7 -.14 29 24 | 4809 -38 3243 8595
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 3.2358.0 GPS week: 2358 Day: 0 MJD: 60750
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 776 26 40 27 28 11 23 11 | 69 45 59 62 57 64 58
R02 | 1470 13 25 19 20 7 26 8 | 45 45 48 53 47 40 44
R03 | 1293 14 36 16 17 15 13 8 | 44 56 53 56 52 46 49
R04 | 974 23 28 15 13 13 20 8 | 48 40 42 48 50 42 45
R05 | 1414 10 19 17 16 8 6 5 | 44 36 38 47 38 39 40
R07 | 1277 9 21 16 13 13 25 7 | 52 53 56 52 56 47 52
R08 | 811 8 18 16 28 17 21 8 | 53 54 62 66 57 51 55
R09 | 2343 12 28 14 17 9 15 6 | 60 63 57 52 54 65 57
R11 | 1126 12 17 20 13 7 12 6 | 42 43 50 41 41 39 41
R12 | 1583 13 32 14 21 13 17 8 | 78 79 71 59 75 71 70
R14 | 2218 8 25 13 11 9 18 6 | 98 102 100 97 97 88 96
R15 | 841 21 18 12 8 9 21 6 | 87 81 79 82 75 71 78
R16 | 1429 23 27 20 16 10 20 8 | 84 72 86 76 66 54 71
R17 | 586 9 17 20 13 11 22 6 | 83 72 96 81 89 66 82
R18 | 607 10 31 17 19 9 15 7 | 68 82 80 72 79 70 73
R19 | 2530 46 46 30 54 29 54 19 | 60 50 81 48 71 54 57
R20 | 3188 58 100 68 29 24 51 23 | 102 83 112 61 60 45 63
R21 | 1044 13 37 14 16 20 30 9 | 80 63 83 70 76 53 71
R22 | 3820 18 15 19 17 8 15 6 | 39 52 59 48 47 38 45
R24 | 1225 19 31 41 13 12 23 10 | 91 72 110 87 90 69 86
XR26 |10987 60 56 --- --- 32 --- 33 | 323 321 --- --- 327 --- 324
------+-----------------------------------------+-------------------------------------
RMS | 1747 22 35 25 21 14 25 |T 78 74 71 62 76 55 74
WRMS | 1747 17 28 18 18 12 25 |NE 78 74 71 62 76 55 74
MEDI | 1293 13 28 17 16 11 20 |MD 68 63 62 59 60 53 58
Table 3.2358.1 GPS week: 2358 Day: 1 MJD: 60751
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 651 25 34 16 26 14 10 9 | 41 41 40 40 29 41 36
R02 | 930 18 19 12 11 9 20 6 | 32 30 25 34 27 31 28
R03 | 791 10 25 21 16 9 14 7 | 29 28 34 34 30 29 29
R04 | 690 14 21 18 12 13 12 6 | 32 31 32 28 33 29 29
R05 | 1887 13 29 16 17 13 15 7 | 31 37 29 31 27 26 27
R07 | 1590 10 11 10 12 14 19 6 | 32 39 32 37 36 28 33
R08 | 886 15 23 23 21 13 24 8 | 35 43 40 41 44 36 37
R09 | 1588 16 24 22 15 13 19 8 | 78 62 68 64 69 78 69
R11 | 1264 15 18 18 14 10 15 6 | 54 47 60 49 49 49 50
R12 | 1016 15 22 19 23 17 15 8 | 67 67 66 61 61 52 61
R14 | 3199 13 24 18 12 20 16 7 | 105 101 101 102 95 94 98
R15 | 830 16 24 15 19 12 19 7 | 108 96 107 108 101 101 103
R16 | 1831 16 36 11 20 13 22 8 | 73 66 65 84 67 63 68
R17 | 915 9 22 27 10 17 28 8 | 57 52 76 69 63 44 60
R18 | 577 11 19 16 13 13 20 6 | 53 60 57 67 50 44 53
R19 | 2187 33 48 37 55 26 62 19 | 67 51 57 49 60 45 52
R20 | 4768 65 73 69 34 25 59 24 | 71 56 76 53 53 36 47
R21 | 2194 15 25 13 28 24 16 9 | 60 48 59 43 61 48 52
R22 | 3302 14 17 18 25 19 11 8 | 45 60 49 59 51 43 48
R24 | 1550 11 33 32 21 11 30 10 | 56 49 62 70 51 45 54
XR26 | 9650 60 52 --- --- 38 --- 35 | 288 286 --- --- 292 --- 289
------+-----------------------------------------+-------------------------------------
RMS | 1943 21 30 25 23 16 26 |T 67 64 56 56 64 48 63
WRMS | 1943 17 24 21 17 16 26 |NE 67 64 56 56 64 48 63
MEDI | 1550 15 24 18 17 13 19 |MD 56 51 57 49 51 44 52
Table 3.2358.2 GPS week: 2358 Day: 2 MJD: 60752
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1024 31 61 36 32 17 38 15 | 49 34 52 45 44 50 40
R02 | 1303 13 21 13 14 15 27 7 | 34 34 36 37 38 34 33
R03 | 854 15 16 18 17 8 20 7 | 31 31 30 36 36 27 31
R04 | 984 13 20 20 18 12 15 7 | 36 29 39 36 36 30 32
R05 | 2404 13 17 21 31 16 16 9 | 31 31 31 44 29 22 28
R07 | 907 13 35 7 16 6 19 7 | 41 42 39 44 37 32 37
R08 | 541 13 17 17 16 12 17 6 | 44 45 53 53 44 46 45
R09 | 2352 12 25 19 15 13 13 7 | 60 73 69 70 54 64 63
R11 | 1625 16 17 18 21 19 16 8 | 43 47 47 41 46 42 42
R12 | 1186 13 20 12 30 20 16 9 | 58 51 57 52 66 52 54
R14 | 1500 8 19 18 10 17 18 6 | 114 121 119 116 107 111 113
R15 | 1923 13 20 16 25 27 13 9 | 89 88 82 103 66 81 83
R16 | 2729 24 35 25 22 15 23 10 | 63 58 64 56 46 33 50
R17 | 806 12 14 17 18 12 19 7 | 55 54 66 50 56 45 53
R18 | 1021 10 20 14 13 11 22 6 | 49 62 63 59 57 42 54
R19 | 1404 45 58 43 39 44 87 23 | 47 51 79 57 65 42 50
R20 | 3953 42 85 71 22 22 78 24 | 70 36 98 45 65 32 49
R21 | 2438 9 35 19 20 26 24 10 | 58 48 60 49 66 39 52
R22 | 2926 14 27 17 20 17 9 8 | 21 39 24 32 26 26 21
R24 | 955 14 36 48 17 19 30 12 | 59 60 101 70 77 53 69
XR26 | 7153 55 48 --- --- 42 --- 34 | 204 217 --- --- 191 --- 200
------+-----------------------------------------+-------------------------------------
RMS | 1858 20 35 28 22 19 33 |T 59 59 60 54 59 45 57
WRMS | 1858 16 28 19 20 18 33 |NE 59 59 60 54 59 45 57
MEDI | 1404 13 21 18 18 17 19 |MD 49 48 57 49 54 42 50
Table 3.2358.3 GPS week: 2358 Day: 3 MJD: 60753
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1562 26 55 25 11 20 24 11 | 47 30 53 39 43 49 40
R02 | 1224 12 20 12 12 18 15 6 | 36 34 35 36 47 38 36
R03 | 689 19 12 18 9 11 25 7 | 35 35 41 37 30 26 32
R04 | 688 15 22 17 13 11 19 7 | 37 30 35 37 27 26 29
R05 | 2742 13 32 13 16 13 17 7 | 29 27 31 40 29 28 29
R07 | 609 22 38 23 14 18 18 9 | 41 50 47 44 35 37 37
R08 | 574 13 19 22 8 13 15 6 | 42 41 42 48 44 39 41
R09 | 3716 10 32 18 13 12 10 7 | 31 52 38 35 29 43 33
R11 | 1936 13 24 12 14 14 7 6 | 28 43 29 22 27 28 26
R12 | 1357 23 29 15 31 24 12 10 | 57 56 44 48 59 48 46
R14 | 1060 14 19 13 10 13 14 6 | 70 75 65 67 63 59 65
R15 | 1568 18 19 16 12 21 19 8 | 94 83 95 90 81 73 85
R16 | 3192 17 40 21 12 24 13 9 | 65 50 62 64 40 43 52
R17 | 912 9 18 19 8 8 15 5 | 64 60 80 71 71 59 67
R18 | 1396 13 20 11 10 16 11 6 | 55 72 68 62 71 56 62
R19 | 717 51 47 52 25 23 44 18 | 58 47 68 49 50 30 41
R20 | 1513 53 89 48 23 28 59 21 | 76 72 67 60 50 22 41
R21 | 1322 15 20 24 7 12 21 7 | 68 57 69 61 64 48 60
R22 | 2698 14 21 16 14 9 9 6 | 23 34 30 34 22 23 23
R24 | 770 13 27 21 13 19 15 7 | 59 50 72 70 74 58 64
XR26 | 8405 45 55 --- --- 28 --- 29 | 95 95 --- --- 95 --- 91
------+-----------------------------------------+-------------------------------------
RMS | 1753 22 35 23 15 17 22 |T 52 52 53 50 50 41 47
WRMS | 1753 17 26 18 15 16 22 |NE 52 52 53 50 50 41 47
MEDI | 1357 15 24 18 12 16 15 |MD 55 50 47 48 47 39 41
Table 3.2358.4 GPS week: 2358 Day: 4 MJD: 60754
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2367 37 32 14 25 23 29 12 | 45 45 41 39 42 47 39
R02 | 979 15 12 13 15 18 18 7 | 44 42 48 46 37 40 40
R03 | 1318 11 15 14 23 20 10 7 | 40 40 42 49 43 45 41
R04 | 717 7 16 11 13 11 14 5 | 39 38 38 41 44 42 39
R05 | 1263 12 18 11 23 7 12 6 | 32 35 28 39 28 29 29
R07 | 1017 11 26 18 9 11 15 7 | 40 43 36 37 26 37 34
R08 | 700 16 10 14 11 15 16 6 | 37 41 39 41 26 41 35
R09 | 3933 12 19 18 11 12 11 6 | 74 79 85 71 68 75 74
R11 | 1939 12 27 15 12 12 17 7 | 57 73 65 51 44 46 54
R12 | 1619 16 26 17 20 11 11 7 | 66 61 57 61 52 56 57
R14 | 876 11 15 23 32 11 18 8 | 96 87 103 93 92 90 92
R15 | 901 14 19 20 20 11 26 8 | 102 92 102 105 95 87 96
R16 | 2143 21 26 20 11 9 21 8 | 71 67 75 68 61 52 64
R17 | 590 10 10 10 25 24 23 8 | 64 62 57 58 74 48 59
R18 | 1265 12 14 11 13 13 20 6 | 59 68 67 63 63 58 61
R19 | 726 50 24 60 42 36 42 19 | 51 65 93 52 49 35 49
R20 | 1733 35 103 52 47 36 69 25 | 77 81 90 89 41 44 62
R21 | 1261 12 29 26 13 12 31 9 | 68 56 75 73 63 51 63
R22 | 2463 14 9 17 23 17 10 7 | 38 50 51 37 48 35 41
R24 | 589 10 33 22 17 17 16 8 | 67 57 70 66 71 59 64
XR26 | 6528 48 38 --- --- 39 --- 30 | 214 210 --- --- 212 --- 213
------+-----------------------------------------+-------------------------------------
RMS | 1635 20 31 24 23 18 25 |T 65 66 63 58 60 50 62
WRMS | 1635 16 21 17 18 15 25 |NE 65 66 63 58 60 50 62
MEDI | 1263 12 19 17 17 13 17 |MD 59 61 57 52 49 46 57
Table 3.2358.5 GPS week: 2358 Day: 5 MJD: 60755
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1729 27 55 16 30 32 47 15 | 25 36 29 28 27 44 23
R02 | 724 10 19 17 17 8 9 6 | 19 30 24 21 20 24 19
R03 | 1583 15 10 11 8 15 14 5 | 20 35 37 24 29 24 25
R04 | 505 6 20 16 10 9 15 5 | 25 37 33 33 29 28 28
R05 | 839 7 17 13 10 17 14 6 | 27 32 27 28 24 29 25
R07 | 2030 9 26 9 17 12 13 6 | 26 32 31 40 22 34 28
R08 | 1008 13 20 11 13 9 27 7 | 29 36 20 28 23 33 25
R09 | 2704 13 16 21 16 11 15 7 | 24 23 39 30 31 28 26
R11 | 2867 14 29 20 8 14 16 7 | 31 44 41 34 30 31 30
R12 | 2268 15 19 14 22 12 18 7 | 89 96 84 92 83 89 87
R14 | 879 8 33 12 23 17 16 8 | 71 85 77 78 70 73 73
R15 | 735 15 24 29 20 11 20 9 | 71 73 83 70 70 67 70
R16 | 1401 18 35 40 16 9 25 10 | 59 35 77 51 53 38 51
R17 | 464 9 15 24 16 14 17 7 | 52 48 70 57 64 50 57
R18 | 606 19 16 12 23 32 24 10 | 45 52 56 55 76 42 54
R19 | 2242 64 37 67 37 27 53 22 | 34 30 71 39 50 32 37
R20 | 1890 37 104 38 31 27 87 24 | 63 72 58 71 61 36 56
R21 | 983 13 30 14 24 14 25 8 | 56 40 58 65 43 40 50
R22 | 2058 14 23 13 13 10 22 6 | 27 28 35 34 30 26 28
R24 | 443 21 32 38 22 20 23 11 | 54 50 76 56 70 51 59
XR26 | 9097 46 50 --- --- 34 --- 30 | 154 175 --- --- 155 --- 159
------+-----------------------------------------+-------------------------------------
RMS | 1591 21 35 26 20 18 31 |T 47 51 51 46 50 40 48
WRMS | 1591 17 26 26 18 17 25 |NE 47 51 51 46 50 40 48
MEDI | 1401 14 24 16 17 14 18 |MD 34 37 41 39 43 34 37
Table 3.2358.6 GPS week: 2358 Day: 6 MJD: 60756
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 809 24 27 27 33 14 28 11 | 64 55 62 60 61 55 58
R02 | 1431 16 29 11 11 13 24 7 | 52 52 46 49 46 40 46
R03 | 1806 6 18 16 27 9 24 7 | 47 45 47 56 43 49 46
R04 | 585 9 11 16 8 10 10 5 | 49 46 47 45 42 43 44
R05 | 1229 6 25 15 13 13 17 6 | 38 33 37 43 39 46 37
R07 | 1490 8 10 22 13 9 10 5 | 48 42 49 45 44 47 45
R08 | 1497 10 13 18 13 9 16 6 | 48 42 60 54 49 46 50
R09 | 2308 15 20 15 18 14 13 7 | 43 50 49 40 45 40 42
R11 | 2933 13 18 18 17 15 11 7 | 26 29 36 20 28 24 24
R12 | 2681 15 27 11 19 13 11 7 | 80 96 84 80 83 76 81
R14 | 958 9 19 17 14 11 18 6 | 86 93 92 87 83 80 85
R15 | 995 24 21 23 30 17 27 10 | 73 64 67 49 62 48 57
R16 | 918 17 39 37 25 13 26 11 | 74 56 86 61 68 44 63
R17 | 801 13 13 17 15 11 23 6 | 80 74 87 72 83 59 76
R18 | 607 18 23 18 20 26 25 10 | 67 84 73 79 93 66 76
R19 | 1853 59 53 36 57 14 35 19 | 60 50 80 48 60 40 53
R20 | 2812 36 94 42 18 32 85 23 | 106 69 100 78 90 46 79
R21 | 763 9 41 19 11 18 28 9 | 81 58 90 80 87 59 77
R22 | 1894 18 37 18 21 11 22 9 | 29 41 47 45 42 32 36
R24 | 567 24 24 22 24 20 28 10 | 87 63 93 72 85 60 77
XR26 |12486 48 40 --- --- 30 --- 27 | 229 239 --- --- 232 --- 231
------+-----------------------------------------+-------------------------------------
RMS | 1628 21 34 23 23 16 29 |T 69 65 66 58 69 50 65
WRMS | 1628 16 26 19 19 15 24 |NE 69 65 66 58 69 50 65
MEDI | 1431 15 24 18 18 13 23 |MD 64 55 62 54 61 46 57
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