[IGSREPORT-30449] Wk 2365 IGLOS Final Orbits
acc
acc at igs.org
Fri May 23 07:31:17 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2365 (May 04, 2025 - May 10, 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 2.2365.
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:
igl2365[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2365 in the SP3 format.
igl23657.sum Combination Report for GPS Week 2365.
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 | 6.2 ns
1 | 2.9 ns
2 | 5.4 ns
3 | 3.6 ns
4 | 3.9 ns
5 | 1.9 ns
6 | 3.3 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
1 | ESA | R20
4 | ESA | R20
5 | ESA | R20
6 | ALL | R22
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 1.2365, 1a.2365).
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 2.2365.0-6)
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 3.2365.0-6).
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 2365 summary. (May 04, 2025 - May 10, 2025)
Table 1.2365.a GPS week : 2365 MJD: 60799.0-60805.0
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 1 -5 -15 27 .13 18 15 | 3915 50 3501 8802
| 0 0 2 12 17 15 .04 | 922 2426
esa n/a| -3 -1 2 5 -2 52 -.11 38 35 | 5110 -19 3443 8346
| 1 1 2 13 16 29 .03 | 1316 3306
gfz n/a| 0 0 6 11 4 -1 -.06 17 15 | 0 -30 3484 8241
| 0 1 2 17 16 39 .07 | 0 2785
grg n/a| 2 0 -2 -25 4 -21 .35 22 20 | 3620 -163 3428 7946
| 0 1 2 21 18 55 .04 | 1113 3048
iac n/a| 0 -1 -1 0 2 -47 -.12 18 17 | 4754 52 3488 8649
| 1 3 3 17 25 68 .03 | 1486 1261
jgx n/a| 0 0 -8 10 11 -5 -.19 24 24 | 5356 -269 3399 7844
| 0 1 1 16 12 26 .03 | 1236 3039
Table 1.2365.b GPS week : 2365 MJD: 60799.0-60805.0
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 | 5 7 6 7 5 6 9 |
R03 | 5 7 8 5 5 5 7 |
R04 | 8 8 9 8 6 6 7 |
R05 | 5 5 7 6 6 5 7 |
R07 | 6 6 7 10 7 8 10 |
R08 | 7 7 6 8 9 8 8 |
R09 | 6 7 6 9 6 8 8 |
R11 | 7 7 8 7 8 8 9 |
R12 | 7 7 8 7 7 6 6 |
R14 | 6 6 7 8 8 7 8 |
R15 | 8 6 7 7 7 7 7 |
R16 | 8 8 7 8 8 9 8 |
R17 | 8 7 9 8 6 8 9 |
R18 | 6 8 7 8 9 8 9 |
R19 | 18 17 21 22 21 17 16 |
R20 | 17 17 24 24 24 23 24 |
R21 | 7 7 7 7 6 7 7 |
R22 | 6 7 6 7 5 20 --- |
R24 | 9 8 8 9 8 8 9 |
R26 | 30 31 29 33 35 38 33 |
R27 | 52 63 58 52 58 53 29 |
Table 1.2365.c GPS week : 2365 MJD: 60799.0-60805.0
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 2365 0 | 75 61 171 -134 2150 5471 78.8 2020 2020 | 6161 0
brd 2365 1 | -50 11 161 -499 2598 6383 79.0 1829 1829 | 2891 0
brd 2365 2 | -31 -89 206 -468 562 3937 82.5 1595 1595 | 5396 0
brd 2365 3 | -70 -18 313 181 260 4153 82.1 1567 1567 | 3605 0
brd 2365 4 | 55 198 175 62 -639 -473 80.0 2308 2308 | 3944 0
brd 2365 5 | -40 54 218 -456 -660 9834 79.6 2378 2378 | 1942 0
brd 2365 6 | -13 55 210 -466 -1621 9743 81.4 2024 2024 | 3318 0
-------------+------------------------------------------------------------+----------------
brd 2365 mean| -10 39 208 -254 378 5578 80.5 1960 1960 | 3893 0
brd 2365 sdev| 55 88 51 287 1539 3593 1.5 318 318 | 1450 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 2.2365.0 GPS week: 2365 Day: 0 MJD: 60799
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 -3 -29 27 .15 17 13 | 5278 2854 3255 7680
esa n/a| -3 -1 5 -3 -4 54 -.13 37 48 | 4670 4017 3302 7713
gfz n/a| 1 2 4 7 3 36 -.01 16 13 | 0 3445 3276 7570
grg n/a| 2 -2 -1 -41 -7 -93 .29 19 16 | 4421 3194 3304 7602
iac n/a| 0 0 -4 6 8 -33 -.13 17 14 | 7276 1397 3237 8109
jgx n/a| 0 -1 -8 18 14 4 -.15 21 21 | 5986 3012 3265 7879
Table 2.2365.1 GPS week: 2365 Day: 1 MJD: 60800
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 -3 -28 46 .12 19 15 | 4777 -3483 3792 8440
esa n/a| -3 -1 3 -21 10 54 -.10 36 26 | 6833 -4786 3848 8502
gfz n/a| 1 0 7 23 -15 -20 -.05 16 15 | 0 -3481 3869 8781
grg n/a| 2 0 0 -39 -6 5 .33 19 19 | 3983 -3215 3854 8648
iac n/a| 0 -1 -7 11 20 -59 -.11 17 18 | 5426 -2519 3805 8855
jgx n/a| 1 0 -6 -6 1 -15 -.22 19 19 | 5560 -3216 3880 8797
Table 2.2365.2 GPS week: 2365 Day: 2 MJD: 60801
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 -12 -23 7 .08 21 17 | 3790 1714 3421 7280
esa n/a| -6 0 0 15 0 79 -.07 36 30 | 5557 2667 3535 7094
gfz n/a| 1 0 9 25 6 44 .01 14 14 | 0 1332 3488 7441
grg n/a| 3 0 -4 -36 31 27 .33 25 28 | 4242 862 3503 7363
iac n/a| 0 -1 0 -1 -26 -162 -.13 19 18 | 5821 557 3409 7538
jgx n/a| 0 0 -9 7 32 -1 -.19 24 24 | 5333 772 3521 7512
Table 2.2365.3 GPS week: 2365 Day: 3 MJD: 60802
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 -18 17 32 .15 15 13 | 3411 2361 4154 8559
esa n/a| -4 0 -1 10 20 44 -.10 38 34 | 4681 2863 3983 8419
gfz n/a| 0 1 2 6 0 -46 -.19 19 14 | 0 3042 3970 7318
grg n/a| 2 0 -4 7 -10 -92 .42 26 19 | 1211 3971 3729 6885
iac n/a| -1 0 4 -15 -37 64 -.15 22 20 | 4373 -333 4134 7953
jgx n/a| 0 -1 -7 31 1 -35 -.19 24 24 | 3588 3911 3641 6825
Table 2.2365.4 GPS week: 2365 Day: 4 MJD: 60803
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 -20 -21 24 .15 17 13 | 4345 -41 3025 9985
esa n/a| -2 -3 1 20 0 89 -.08 38 47 | 6681 -920 2983 9621
gfz n/a| 0 0 8 -22 0 24 -.03 16 16 | 0 -975 2986 8421
grg n/a| 3 1 0 2 10 -1 .35 26 23 | 4090 -857 3060 7493
iac n/a| -1 0 0 28 4 -66 -.06 14 13 | 3390 883 3016 9103
jgx n/a| 0 -1 -8 25 12 -41 -.20 27 27 | 7556 -927 3044 7702
Table 2.2365.5 GPS week: 2365 Day: 5 MJD: 60804
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 11 -22 45 .20 19 18 | 2970 -557 3342 10749
esa n/a| -4 -2 4 10 -17 45 -.17 39 30 | 3315 -865 3026 8206
gfz n/a| 0 -1 7 23 39 1 -.08 17 18 | 0 -341 3340 9431
grg n/a| 3 2 -3 -35 -9 -39 .37 21 16 | 3349 -946 3352 8934
iac n/a| 0 0 0 -25 17 -65 -.12 14 13 | 3231 207 3294 9995
jgx n/a| -1 0 -8 10 20 19 -.17 25 25 | 4688 -1142 3126 7117
Table 2.2365.6 GPS week: 2365 Day: 6 MJD: 60805
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 3 11 2 10 .08 15 14 | 2840 -2497 3521 8927
esa n/a| -3 0 3 3 -29 -2 -.14 39 31 | 4035 -3109 3427 8872
gfz n/a| 0 1 3 19 -2 -54 -.08 18 13 | 0 -3235 3464 8730
grg n/a| 2 2 1 -37 26 45 .37 20 16 | 4044 -4155 3200 8701
iac n/a| 3 -8 -3 3 30 -9 -.14 24 23 | 3762 174 3526 8991
jgx n/a| -1 2 -12 -13 -2 29 -.22 25 25 | 4782 -4299 3317 9078
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 3.2365.0 GPS week: 2365 Day: 0 MJD: 60799
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1134 7 9 9 11 8 17 4 | 56 56 60 60 51 45 54
R03 | 1283 6 15 11 15 10 14 5 | 65 64 62 69 65 52 63
R04 | 1309 25 22 15 12 14 11 7 | 61 49 47 48 49 46 48
R05 | 940 13 14 9 10 14 6 5 | 54 43 49 44 45 44 46
R07 | 752 7 16 8 20 14 8 5 | 60 63 59 64 56 53 58
R08 | 1389 13 16 13 17 20 15 7 | 51 58 66 73 66 50 60
R09 | 1385 11 13 18 11 13 14 6 | 57 57 61 52 61 49 55
R11 | 4432 13 24 15 13 15 6 6 | 64 78 64 64 60 60 62
R12 | 2062 9 22 12 21 9 17 6 | 64 72 55 65 56 46 58
R14 | 1801 13 11 10 18 12 14 6 | 71 77 78 90 80 67 77
R15 | 1072 8 25 21 12 8 20 7 | 87 85 95 84 84 68 83
R16 | 1619 12 24 22 14 13 24 8 | 84 69 98 84 89 68 82
R17 | 1404 9 25 14 18 21 22 8 | 44 47 46 46 43 27 44
R18 | 836 9 19 13 13 8 19 6 | 35 38 42 45 40 37 38
R19 | 3047 44 47 17 50 26 45 17 | 63 53 61 52 53 56 54
R20 | 3656 31 134 30 26 28 49 16 | 52 40 52 54 52 46 48
R21 | 2074 10 20 18 7 16 18 7 | 39 35 41 42 40 35 37
R22 | 2305 14 12 18 9 10 10 5 | 46 29 60 55 44 19 49
R24 | 1303 10 28 18 11 32 17 9 | 50 42 41 47 46 48 43
XR26 | 9296 44 63 42 --- 59 --- 29 | 74 133 78 --- 131 --- 96
XR27 |11960 48 --- --- --- 56 --- 52 | 65 --- --- --- 134 --- 94
------+-----------------------------------------+-------------------------------------
RMS | 2019 17 37 16 19 17 21 |T 59 59 60 59 64 48 59
WRMS | 2019 13 48 13 16 14 21 |NE 59 59 60 59 64 48 59
MEDI | 1404 12 20 15 13 14 17 |MD 60 56 60 55 56 48 55
Table 3.2365.1 GPS week: 2365 Day: 1 MJD: 60800
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 828 10 20 13 10 26 12 7 | 36 33 48 45 45 40 40
R03 | 791 7 22 15 12 13 18 6 | 46 43 53 54 38 31 43
R04 | 1234 22 22 17 14 11 9 7 | 45 38 47 38 39 32 38
R05 | 1599 10 15 12 7 8 6 4 | 34 30 43 38 43 38 37
R07 | 860 10 11 8 12 25 7 6 | 35 36 32 42 26 33 30
R08 | 1093 13 10 9 15 21 22 7 | 32 38 31 42 34 25 32
R09 | 2883 16 12 18 12 13 9 6 | 43 44 39 42 50 32 41
R11 | 3769 13 15 11 17 17 18 7 | 47 59 55 52 50 44 49
R12 | 1186 9 31 8 16 11 17 7 | 52 69 56 60 52 46 54
R14 | 1529 14 15 15 17 9 11 6 | 61 62 80 74 63 61 67
R15 | 1036 13 16 11 13 10 19 6 | 67 63 63 64 54 48 59
R16 | 1035 17 21 25 11 12 17 8 | 65 64 85 73 65 57 68
R17 | 2169 11 25 9 7 28 12 7 | 23 24 20 23 24 23 17
R18 | 844 17 20 10 15 11 24 7 | 24 25 24 29 20 19 21
R19 | 2068 49 42 19 53 12 29 16 | 27 30 28 29 29 36 24
R20 | 2973 36 130 33 34 17 41 16 | 45 23 54 32 42 38 33
R21 | 2046 11 23 13 9 14 16 6 | 27 29 27 26 20 20 22
R22 | 1697 16 27 12 11 17 13 7 | 42 34 47 54 39 19 44
R24 | 1484 13 14 15 16 28 16 8 | 34 25 33 30 29 29 27
XR26 | 9391 55 68 31 --- 59 --- 30 | 49 92 64 --- 96 --- 70
XR27 | 5977 60 --- --- --- 66 --- 63 | 48 --- --- --- 117 --- 76
------+-----------------------------------------+-------------------------------------
RMS | 1829 19 36 16 19 17 19 |T 42 43 46 44 46 35 42
WRMS | 1829 15 26 15 19 18 19 |NE 42 43 46 44 46 35 42
MEDI | 1529 13 20 13 13 14 16 |MD 43 36 47 42 42 33 40
Table 3.2365.2 GPS week: 2365 Day: 2 MJD: 60801
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 705 11 18 10 9 17 16 6 | 49 56 52 51 49 42 48
R03 | 1392 11 21 17 17 16 19 7 | 56 58 77 72 55 51 62
R04 | 860 27 25 14 17 17 18 8 | 56 55 57 49 40 42 48
R05 | 1154 18 14 15 11 24 8 7 | 46 43 52 43 34 38 41
R07 | 1020 11 14 13 8 28 7 7 | 48 43 46 47 61 45 47
R08 | 908 18 19 13 12 9 14 6 | 44 60 58 55 44 48 50
R09 | 3874 14 18 13 13 12 10 6 | 51 59 54 55 51 57 53
R11 | 2630 11 11 11 15 24 23 7 | 56 61 67 54 79 56 62
R12 | 551 9 26 13 15 17 22 7 | 57 61 67 64 67 54 60
R14 | 1398 13 16 13 17 18 12 6 | 63 71 69 66 65 58 64
R15 | 1231 13 17 14 19 14 18 7 | 78 74 77 62 76 63 71
R16 | 948 7 18 11 15 17 20 6 | 78 72 87 89 90 67 81
XR17 | 1875 11 23 11 14 25 --- 8 | 33 35 38 39 30 --- 32
R18 | 1131 15 28 18 10 14 8 7 | 30 31 44 36 26 29 31
R19 | 896 65 73 19 66 18 31 21 | 43 40 37 44 37 45 36
R20 | 2235 26 110 22 56 30 71 24 | 40 36 52 39 31 34 35
R21 | 1440 13 19 14 15 16 14 6 | 30 31 29 33 26 23 26
R22 | 1559 11 11 9 18 13 10 5 | 47 31 56 64 47 28 52
R24 | 1114 14 21 12 17 17 25 8 | 32 38 46 43 33 43 37
XR26 | 9695 44 80 25 --- 55 --- 28 | 90 112 87 --- 113 --- 95
XR27 | 6623 58 --- --- --- 57 --- 57 | 92 --- --- --- 146 --- 115
------+-----------------------------------------+-------------------------------------
RMS | 1595 21 36 14 25 19 24 |T 53 53 57 52 57 45 54
WRMS | 1595 17 30 14 28 18 24 |NE 53 53 57 52 57 45 54
MEDI | 1231 13 19 13 15 17 16 |MD 49 55 54 51 49 45 50
Table 3.2365.3 GPS week: 2365 Day: 3 MJD: 60802
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 590 8 18 13 9 26 12 6 | 44 45 41 41 58 39 42
R03 | 1790 6 17 13 10 10 14 5 | 52 55 54 54 57 48 52
R04 | 1176 20 14 13 19 20 6 7 | 43 36 36 31 33 35 35
R05 | 850 12 14 13 10 21 7 6 | 33 25 31 29 29 23 26
R07 | 1555 13 23 10 9 41 17 9 | 44 45 45 49 69 34 44
R08 | 763 17 22 15 22 19 13 8 | 37 49 43 59 52 46 45
XR09 | 4762 13 14 24 13 16 --- 8 | 38 45 39 45 50 --- 39
R11 | 3901 12 16 20 19 16 12 7 | 40 41 54 34 47 41 41
R12 | 719 4 23 18 15 18 15 6 | 70 78 74 65 79 63 70
R14 | 1528 11 21 14 24 18 15 7 | 69 72 67 86 70 64 70
R15 | 1528 10 22 13 20 19 9 7 | 79 72 78 70 79 67 74
R16 | 818 6 25 15 12 29 17 7 | 87 71 92 84 110 75 87
XR17 | 2468 12 24 13 16 19 --- 8 | 39 42 39 40 37 --- 37
R18 | 1499 9 22 18 21 16 24 8 | 36 40 43 40 39 34 36
R19 | 915 42 81 33 68 26 41 21 | 69 42 62 54 50 64 55
R20 | 1163 14 109 38 56 33 68 24 | 55 43 62 67 55 48 53
R21 | 1600 13 17 15 8 13 20 6 | 38 42 37 38 35 31 35
R22 | 1973 14 18 20 22 12 6 7 | 33 38 43 51 31 23 36
R24 | 1061 12 29 17 18 12 29 8 | 38 39 46 41 39 35 38
XR26 | 8584 36 89 47 --- 66 --- 32 | 62 124 84 --- 114 --- 84
XR27 | 8105 39 --- --- --- 67 --- 51 | 76 --- --- --- 118 --- 90
------+-----------------------------------------+-------------------------------------
RMS | 1567 15 38 19 26 22 24 |T 51 52 53 51 59 45 51
WRMS | 1567 13 34 14 19 20 24 |NE 51 52 53 51 59 45 51
MEDI | 1528 12 22 15 18 19 15 |MD 44 43 45 49 52 41 44
Table 3.2365.4 GPS week: 2365 Day: 4 MJD: 60803
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 856 8 7 10 12 10 13 4 | 34 32 30 40 29 39 32
R03 | 921 7 14 9 11 10 11 4 | 49 55 43 49 51 40 47
R04 | 809 16 14 9 12 16 6 5 | 48 45 34 46 42 38 41
R05 | 705 8 19 15 13 12 10 5 | 36 28 41 30 38 31 33
R07 | 2729 4 16 22 12 11 21 7 | 38 32 54 36 38 21 37
R08 | 917 12 23 13 24 16 27 8 | 36 35 49 60 49 31 42
R09 | 5288 12 12 15 13 14 9 5 | 50 48 59 50 56 56 52
R11 | 5363 15 23 16 14 14 20 7 | 58 60 71 59 72 53 62
R12 | 1057 6 14 22 14 13 13 6 | 71 74 92 76 65 66 73
R14 | 2251 14 24 16 17 17 16 7 | 72 73 75 87 86 71 76
R15 | 1239 8 21 16 20 8 16 6 | 77 73 80 86 76 65 75
R16 | 1518 14 17 18 28 8 14 7 | 81 75 88 58 76 65 75
R17 | 1917 10 19 16 9 7 17 6 | 43 37 42 35 40 27 38
R18 | 1408 17 13 14 21 21 30 9 | 43 39 46 40 44 40 40
R19 | 1896 45 70 24 64 24 52 20 | 49 57 52 38 42 56 44
R20 | 2016 31 132 32 67 26 76 23 | 46 37 52 62 49 55 46
R21 | 1593 8 17 7 21 10 16 6 | 31 29 25 42 32 26 29
R22 | 2610 11 12 10 15 8 14 5 | 73 40 86 85 77 40 79
R24 | 843 20 28 9 9 9 22 7 | 46 44 38 43 40 41 40
XR26 | 6290 53 84 50 --- 58 --- 34 | 82 129 81 --- 116 --- 95
XR27 | 7763 60 --- --- --- 55 --- 58 | 78 --- --- --- 116 --- 94
------+-----------------------------------------+-------------------------------------
RMS | 2307 17 38 16 26 14 27 |T 54 52 56 53 58 45 54
WRMS | 2307 13 47 16 23 13 27 |NE 54 52 56 53 58 45 54
MEDI | 1593 12 17 15 14 13 16 |MD 49 44 52 49 49 40 46
Table 3.2365.5 GPS week: 2365 Day: 5 MJD: 60804
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 792 16 11 10 16 14 11 6 | 29 25 30 38 29 21 27
R03 | 1370 11 12 16 12 10 7 5 | 38 38 29 43 39 36 35
R04 | 727 20 12 11 9 18 8 6 | 48 52 42 46 49 41 44
R05 | 814 16 14 9 12 12 6 5 | 33 39 34 40 36 28 34
R07 | 3365 15 28 22 13 9 13 7 | 39 23 40 32 30 27 29
R08 | 697 16 22 26 10 12 18 8 | 31 26 57 43 43 28 37
R09 | 5213 14 19 16 25 14 7 7 | 41 43 51 27 40 36 38
R11 | 4916 17 23 21 10 9 21 7 | 62 65 77 61 65 58 64
R12 | 1127 16 13 15 12 12 9 6 | 61 54 53 56 48 48 51
R14 | 1206 14 13 11 11 16 19 6 | 71 67 69 61 70 66 66
R15 | 973 13 23 8 15 9 22 7 | 73 77 68 79 74 62 71
R16 | 1651 17 19 24 22 10 19 8 | 77 76 91 76 72 60 73
R17 | 1838 12 22 21 11 16 16 7 | 25 23 32 27 24 30 23
R18 | 1839 16 20 12 16 15 28 8 | 24 22 24 28 26 22 22
R19 | 1342 40 48 16 48 16 42 16 | 32 20 30 35 27 34 26
R20 | 3937 37 137 18 51 22 77 22 | 35 19 35 40 31 40 35
R21 | 1523 7 21 17 10 17 9 6 | 22 21 26 23 24 19 20
XR22 | 5563 21 --- 54 31 20 --- 19 | 48 --- 95 42 46 --- 51
R24 | 1462 21 19 16 17 10 15 7 | 33 25 25 32 30 27 25
XR26 | 7646 65 76 58 --- 62 --- 37 | 97 120 100 --- 117 --- 107
XR27 |10988 61 --- --- --- 45 --- 52 | 87 --- --- --- 106 --- 96
------+-----------------------------------------+-------------------------------------
RMS | 2378 19 39 17 21 14 25 |T 47 43 50 43 48 37 46
WRMS | 2378 18 30 18 16 13 25 |NE 47 43 50 43 48 37 46
MEDI | 1523 16 20 16 13 14 15 |MD 39 38 40 40 40 34 37
Table 3.2365.6 GPS week: 2365 Day: 6 MJD: 60805
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 623 10 22 10 26 29 18 8 | 52 47 53 67 46 40 49
R03 | 1336 9 13 8 17 29 6 6 | 58 54 57 68 55 51 56
R04 | 727 14 19 21 8 16 10 6 | 62 57 51 58 53 52 54
R05 | 657 13 10 11 18 20 14 6 | 51 45 50 46 51 46 47
R07 | 1983 10 43 21 12 31 15 9 | 60 39 63 54 70 48 55
R08 | 696 9 29 11 18 25 18 8 | 53 50 58 68 65 46 56
R09 | 3419 11 21 14 19 23 20 7 | 60 64 66 54 58 63 59
R11 | 4826 13 25 24 18 17 15 8 | 74 74 88 70 77 67 74
R12 | 927 7 20 9 12 18 12 5 | 92 102 90 91 93 81 90
R14 | 1294 14 15 20 13 27 14 7 | 96 100 115 99 112 92 101
R15 | 1133 7 20 17 14 19 18 7 | 107 106 111 98 101 86 101
R16 | 2186 19 25 13 17 22 14 8 | 110 99 109 95 96 89 100
XR17 | 2123 10 13 19 12 31 --- 8 | 52 49 56 51 61 --- 50
R18 | 1124 10 35 18 10 25 19 8 | 52 56 52 54 58 50 51
R19 | 1529 35 61 22 43 27 32 16 | 81 64 76 68 67 77 73
R20 | 3395 30 115 34 36 17 77 23 | 75 54 72 81 61 65 66
R21 | 1245 8 23 5 11 25 14 6 | 47 47 49 54 52 44 47
R24 | 1347 12 24 21 15 24 24 8 | 51 48 53 54 59 57 51
XR26 |10065 51 95 22 --- 70 --- 32 | 106 156 110 --- 153 --- 120
XR27 | 5294 20 --- --- --- 41 --- 29 | 101 --- --- --- 137 --- 113
------+-----------------------------------------+-------------------------------------
RMS | 2023 15 39 18 20 24 25 |T 74 69 74 71 78 62 73
WRMS | 2023 14 31 13 16 23 25 |NE 74 69 74 71 78 62 73
MEDI | 1336 11 23 18 15 25 15 |MD 62 56 63 68 65 57 59
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