[IGSREPORT-30441] Wk 2364 IGLOS Final Orbits
acc
acc at igs.org
Thu May 15 06:42:33 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2364 (Apr 27, 2025 - May 03, 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 2.2364.
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:
igl2364[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2364 in the SP3 format.
igl23647.sum Combination Report for GPS Week 2364.
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 | 3.2 ns
1 | 1.8 ns
2 | 1.4 ns
3 | 4.2 ns
4 | 3.0 ns
5 | 3.1 ns
6 | 8.8 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
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 1.2364, 1a.2364).
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 2.2364.0-6)
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 3.2364.0-6).
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 2364 summary. (Apr 27, 2025 - May 03, 2025)
Table 1.2364.a GPS week : 2364 MJD: 60792.0-60798.0
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 0 3 -4 -15 34 .13 16 14 | 3656 -834 3740 11641
| 1 0 0 7 5 12 .02 | 1926 1358
esa n/a| -3 0 1 -9 -5 44 -.07 37 36 | 5127 -2026 3779 11494
| 1 1 2 11 22 34 .04 | 2588 1815
gfz n/a| 0 0 2 20 0 -23 -.01 18 17 | 0 -1392 3771 10861
| 1 1 2 12 21 25 .05 | 0 1722
grg n/a| 3 -1 0 -31 22 -7 .32 27 23 | 4092 -1404 3307 7122
| 1 1 3 17 21 37 .05 | 2078 1756
iac n/a| -1 -1 -1 11 -1 -38 -.17 18 18 | 3316 -372 3717 11034
| 0 1 3 15 20 70 .05 | 2550 783
jgx n/a| 1 0 -10 11 21 -7 -.16 23 23 | 6467 -1406 3312 7402
| 0 0 2 18 14 42 .03 | 2303 1744
Table 1.2364.b GPS week : 2364 MJD: 60792.0-60798.0
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 7 9 5 7 7 6 |
R03 | 6 8 8 8 6 6 5 |
R04 | 6 8 8 7 7 7 6 |
R05 | 7 7 9 6 7 7 6 |
R07 | 7 6 7 5 6 8 8 |
R08 | 6 7 7 7 8 9 8 |
R09 | 8 7 6 8 6 8 9 |
R11 | 9 9 6 8 6 8 8 |
R12 | 9 14 11 7 7 8 6 |
R14 | 14 9 7 6 6 8 7 |
R15 | 7 13 6 7 6 9 8 |
R16 | 7 10 9 7 7 8 8 |
R17 | 7 7 7 9 7 6 8 |
R18 | 8 7 9 8 7 9 8 |
R19 | 14 16 20 23 18 21 20 |
R20 | 15 25 22 23 22 24 15 |
R21 | 8 6 9 6 8 7 9 |
R22 | 10 8 7 9 9 7 7 |
R24 | 8 6 9 8 6 9 8 |
R26 | 28 26 29 32 34 32 27 |
R27 | 44 46 49 46 46 40 53 |
Table 1.2364.c GPS week : 2364 MJD: 60792.0-60798.0
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 2364 0 | -20 41 45 -1065 560 6100 78.4 1800 1800 | 3180 0
brd 2364 1 | 22 38 62 -1167 -885 2610 79.6 1735 1735 | 1758 0
brd 2364 2 | -7 -46 19 1337 1668 3071 81.7 2143 2143 | 1423 0
brd 2364 3 | 20 5 110 1541 1987 1438 81.6 2767 2767 | 4223 0
brd 2364 4 | 3 -74 223 1149 469 4003 81.9 2849 2849 | 2996 0
brd 2364 5 | 217 -4 158 -1968 1230 7400 84.9 2556 2556 | 3098 0
brd 2364 6 | 143 -2 234 -752 1208 7425 83.3 2274 2274 | 8782 0
-------------+------------------------------------------------------------+----------------
brd 2364 mean| 54 -5 121 -132 891 4578 81.6 2303 2303 | 3637 0
brd 2364 sdev| 90 42 86 1431 954 2405 2.2 443 443 | 2454 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 2.2364.0 GPS week: 2364 Day: 0 MJD: 60792
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 6 -13 51 .15 13 12 | 3411 411 4293 18495
esa n/a| -2 0 3 -1 -41 72 -.03 38 34 | 5205 426 4343 17287
gfz n/a| 0 1 4 12 38 -3 .04 19 19 | 0 443 4363 16816
grg n/a| 5 0 -1 -31 55 12 .32 30 21 | 3370 -854 3946 7214
iac n/a| 0 -2 -2 -10 -14 -88 -.19 15 16 | -782 632 4278 17055
jgx n/a| 1 0 -8 17 24 -20 -.14 18 18 | 8707 -874 3984 7397
Table 2.2364.1 GPS week: 2364 Day: 1 MJD: 60793
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 4 1 -11 34 .12 16 13 | 6461 -2052 3563 8805
esa n/a| -1 0 0 -8 -2 56 -.09 34 42 | 7510 -3490 3491 8369
gfz n/a| 1 0 2 14 -21 -57 .02 18 19 | 0 -2917 3451 7739
grg n/a| 3 0 -3 -55 32 30 .25 35 24 | 3388 -3560 3317 7342
iac n/a| 0 0 4 10 14 -33 -.22 23 23 | 2739 283 3557 8362
jgx n/a| 1 1 -10 -25 1 -13 -.12 19 19 | 8534 -3507 3281 7653
Table 2.2364.2 GPS week: 2364 Day: 2 MJD: 60794
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 3 -5 -18 34 .10 16 14 | 2030 -355 3195 7614
esa n/a| -3 1 -2 -12 -4 40 -.02 34 41 | 3558 -298 3090 7789
gfz n/a| -1 1 -1 36 9 -13 .05 20 18 | 0 -352 3142 7072
grg n/a| 4 -3 6 -48 40 -50 .25 29 30 | 1387 -813 3075 6860
iac n/a| 0 -1 0 3 -6 -22 -.11 19 18 | 1437 381 3156 7441
jgx n/a| 0 0 -11 30 8 44 -.15 22 22 | 3768 -935 3098 7174
Table 2.2364.3 GPS week: 2364 Day: 3 MJD: 60795
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 -8 -10 20 .14 16 15 | 5330 311 3324 9495
esa n/a| -6 -2 0 -17 -16 65 -.09 37 31 | 9067 -4111 3365 8805
gfz n/a| 0 1 0 21 -29 13 -.02 19 15 | 0 127 3358 8100
grg n/a| 4 -2 1 -14 20 -45 .36 26 23 | 3691 604 3019 7803
iac n/a| -1 0 0 16 36 -10 -.12 16 16 | 5795 -964 3300 8972
jgx n/a| 0 0 -8 17 24 -46 -.16 26 26 | 7334 699 3002 8101
Table 2.2364.4 GPS week: 2364 Day: 4 MJD: 60796
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 1 -27 48 .14 16 14 | 4149 -2906 3299 9331
esa n/a| -3 -1 3 -29 -13 62 -.11 37 37 | 5721 -3436 3284 8198
gfz n/a| -2 -1 5 11 2 -34 -.02 16 17 | 0 -3661 3347 7947
grg n/a| 4 0 3 -27 10 34 .33 23 25 | 4640 -3584 3342 7570
iac n/a| 0 0 -5 20 -3 -68 -.13 15 14 | 4225 -832 3282 8662
jgx n/a| 1 0 -10 27 29 -35 -.18 25 25 | 6706 -3535 3414 7886
Table 2.2364.5 GPS week: 2364 Day: 5 MJD: 60797
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 -11 -12 35 .11 19 15 | 718 -1652 3874 8951
esa n/a| -2 0 1 -7 28 41 -.04 37 33 | 1555 -2635 3930 9462
gfz n/a| 0 0 5 6 0 -21 -.09 16 15 | 0 -2997 3825 8211
grg n/a| 2 0 0 -7 1 11 .32 19 19 | 3941 -2177 3352 6783
iac n/a| -2 -2 -2 3 -14 -133 -.25 24 24 | 3117 -750 3904 8505
jgx n/a| 3 1 -15 3 15 59 -.23 29 29 | 2790 -2213 3328 7071
Table 2.2364.6 GPS week: 2364 Day: 6 MJD: 60798
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 4 -11 -13 16 .15 16 15 | 3495 405 4638 18800
esa n/a| -2 0 4 7 14 -28 -.12 39 36 | 3276 -639 4952 20549
gfz n/a| 0 1 0 38 0 -49 -.08 17 15 | 0 -393 4912 20145
grg n/a| 2 -1 -3 -38 -1 -44 .38 24 20 | 8227 553 3098 6287
iac n/a| -1 -1 -2 38 -24 88 -.15 18 16 | 6685 -1360 4548 18245
jgx n/a| 0 0 -7 13 45 -39 -.15 22 22 | 7430 523 3082 6533
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 3.2364.0 GPS week: 2364 Day: 0 MJD: 60792
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 644 6 13 16 14 12 11 5 | 100 93 102 103 102 88 97
R03M | 2220 5 25 15 14 10 11 6 | 94 97 104 105 96 87 96
R04M | 845 15 16 13 14 8 8 5 | 88 73 78 80 80 72 78
R05M | 808 13 22 10 13 11 16 6 | 83 72 83 83 81 76 79
R07 | 724 9 14 21 22 15 10 6 | 95 93 84 98 99 93 93
R08M | 1984 11 13 13 16 15 13 6 | 95 105 106 101 106 91 100
R09 | 2436 13 15 17 34 10 13 7 | 42 43 48 45 41 41 40
R11E | 2191 12 18 19 36 21 11 8 | 56 69 58 68 56 60 58
R12E | 2362 13 22 16 28 21 20 8 | 295 301 291 276 299 282 291
R14E | 1165 16 24 24 74 31 11 13 | 70 67 72 105 86 65 72
R15E | 772 6 20 25 16 11 12 6 | 130 126 125 136 127 131 128
R16E | 2684 10 20 24 22 11 11 7 | 73 74 78 76 71 70 72
R17 | 684 8 26 16 19 9 14 6 | 34 43 34 38 35 37 34
R18 | 641 13 25 12 22 10 19 7 | 37 32 31 41 36 36 33
R19 | 804 28 47 17 53 14 31 14 | 30 36 23 33 27 35 25
R20 | 4128 17 131 22 38 17 45 14 | 38 32 37 41 30 32 31
R21M | 944 11 12 16 8 17 27 7 | 33 36 30 35 29 36 31
R22 | 2184 16 37 27 28 10 11 9 | 38 42 47 44 32 35 36
R24 | 806 13 25 23 10 15 10 7 | 49 47 38 42 39 44 42
XR26M | 8484 40 72 31 --- 47 --- 27 | 69 97 69 --- 86 --- 71
XR27M |11914 40 --- --- --- 47 --- 43 | 41 --- --- --- 79 --- 54
------+-----------------------------------------+-------------------------------------
RMS | 1799 13 38 19 30 15 18 |T 75 78 76 81 77 74 74
WRMS | 1799 12 34 19 20 16 18 |NE 45 46 42 47 42 44 41
MEDI | 1165 13 22 17 22 14 12 |MD 69 69 69 76 79 65 71
Table 3.2364.1 GPS week: 2364 Day: 1 MJD: 60793
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1141 6 15 11 12 20 18 6 | 73 72 82 78 81 66 74
R03M | 1189 11 28 25 17 13 15 8 | 70 71 90 84 70 64 73
R04M | 1453 14 16 19 12 14 20 7 | 71 58 74 67 61 52 63
R05M | 986 15 13 9 9 16 19 6 | 69 56 58 63 67 54 60
R07 | 2105 9 11 16 10 21 9 6 | 66 60 56 62 73 63 62
R08M | 1372 13 23 12 13 17 19 7 | 62 70 60 67 65 60 62
R09 | 3700 12 20 17 18 13 6 6 | 42 52 43 48 49 43 44
R11E | 2171 12 19 13 44 18 16 9 | 32 39 43 56 36 36 36
R12E | 2509 12 31 15 70 43 13 14 | 188 194 186 181 213 189 190
R14E | 1034 14 24 13 46 16 13 9 | 57 74 56 87 61 54 59
R15E | 1100 14 23 22 59 39 15 13 | 105 110 107 136 111 111 108
R16E | 2474 18 14 18 53 19 10 10 | 142 136 133 177 145 133 141
R17 | 668 5 20 20 13 11 16 6 | 28 28 22 37 26 29 26
R18 | 728 15 21 16 18 11 15 7 | 31 37 36 31 31 26 31
R19 | 910 38 56 20 53 21 30 16 | 49 41 41 38 43 55 40
R20 | 1485 31 111 36 58 38 53 24 | 34 22 45 32 22 32 25
R21M | 1209 11 14 14 10 14 14 6 | 25 20 27 29 22 22 20
R22 | 2426 14 27 16 15 27 9 8 | 20 41 25 29 27 22 19
R24 | 787 12 18 11 12 18 11 6 | 30 29 31 33 23 25 26
XR26M | 9524 33 69 28 --- 49 --- 25 | 27 60 42 --- 49 --- 39
XR27M | 6398 36 --- --- --- 56 --- 45 | 84 --- --- --- 80 --- 78
------+-----------------------------------------+-------------------------------------
RMS | 1735 16 34 18 35 23 19 |T 62 63 62 70 64 59 60
WRMS | 1735 13 42 19 24 23 19 |NE 37 38 37 38 36 36 34
MEDI | 1372 14 20 16 17 18 15 |MD 57 56 45 62 61 54 59
Table 3.2364.2 GPS week: 2364 Day: 2 MJD: 60794
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1754 9 16 25 14 33 12 9 | 79 85 70 77 104 73 81
R03M | 1005 10 22 16 16 22 18 7 | 79 77 81 92 94 71 81
R04M | 1184 16 18 19 28 15 15 8 | 72 65 75 60 61 59 65
R05M | 2368 15 24 26 19 13 18 8 | 90 72 96 80 81 74 82
R07 | 2851 7 19 12 9 24 13 7 | 70 57 68 73 84 60 69
R08M | 821 15 19 11 13 12 21 7 | 65 65 68 78 78 80 71
R09 | 3701 14 18 19 13 10 11 6 | 16 26 34 20 20 22 19
R11E | 4555 13 18 13 17 10 13 6 | 40 47 47 38 43 45 41
R12E | 1659 16 21 21 41 27 16 10 | 208 213 219 223 186 210 208
R14E | 2678 12 25 18 15 13 15 7 | 34 48 36 44 40 32 35
R15E | 1544 8 18 12 22 9 17 6 | 41 51 49 47 42 41 42
R16E | 1784 10 24 23 29 9 18 8 | 74 80 86 101 80 73 79
R17 | 855 8 18 13 18 9 26 7 | 31 38 34 43 29 32 32
R18 | 720 18 26 17 21 18 16 8 | 29 25 27 34 30 22 24
R19 | 2121 46 71 31 67 26 33 20 | 63 35 46 39 24 48 39
R20 | 1782 13 98 30 59 32 55 21 | 35 21 25 43 32 31 30
R21M | 740 9 23 18 17 17 29 8 | 24 37 24 30 28 27 24
R22 | 2597 11 8 18 23 19 13 7 | 25 32 34 48 34 24 27
R24 | 1065 10 33 19 25 12 17 8 | 41 43 31 42 30 31 34
XR26M | 5385 34 84 41 --- 48 --- 28 | 20 76 29 --- 55 --- 35
XR27M | 9934 43 --- --- --- 54 --- 48 | 152 --- --- --- 162 --- 154
------+-----------------------------------------+-------------------------------------
RMS | 2142 16 34 20 29 19 22 |T 61 59 58 63 63 55 60
WRMS | 2142 14 41 18 30 18 22 |NE 38 34 37 42 35 33 34
MEDI | 1782 13 21 18 19 17 17 |MD 41 48 46 47 43 45 41
Table 3.2364.3 GPS week: 2364 Day: 3 MJD: 60795
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 2235 7 15 10 11 14 12 5 | 81 76 78 85 86 78 80
R03M | 743 10 21 13 16 23 17 7 | 88 100 83 99 105 79 91
R04M | 1273 11 19 20 24 11 7 7 | 81 80 89 67 83 76 79
R05M | 2700 13 18 14 15 14 8 6 | 110 99 102 102 104 103 104
R07 | 943 9 17 11 16 11 8 5 | 86 79 91 100 89 85 88
R08M | 671 13 17 12 21 14 14 6 | 83 86 93 102 86 86 88
R09 | 4156 17 18 17 25 17 9 8 | 24 32 27 32 26 24 22
R11E | 6876 11 20 24 25 14 13 8 | 25 35 36 34 26 25 25
R12E | 748 9 14 19 20 9 18 6 | 87 90 98 87 99 85 90
R14E | 4320 6 21 15 11 13 13 6 | 41 45 45 45 38 33 39
R15E | 2329 9 27 10 15 10 22 6 | 54 57 61 63 54 66 56
R16E | 1892 14 20 15 14 11 16 6 | 49 52 48 51 38 42 44
R17 | 1221 13 23 26 13 16 28 9 | 39 41 48 42 39 44 39
R18 | 770 12 21 14 18 15 27 8 | 43 42 47 52 51 41 44
R19 | 1832 42 75 44 62 23 66 22 | 43 59 29 41 33 48 32
R20 | 4228 25 114 28 59 27 57 22 | 36 31 30 31 27 41 25
R21M | 806 8 11 14 24 11 13 6 | 32 31 37 29 30 32 29
R22 | 3295 12 33 7 24 23 13 8 | 33 43 36 40 42 36 34
R24 | 1429 15 30 11 11 16 27 8 | 40 48 43 44 37 45 40
XR26M | 7045 44 69 43 --- 69 --- 32 | 104 126 109 --- 133 --- 110
XR27M | 7089 41 --- --- --- 50 --- 45 | 288 --- --- --- 289 --- 287
------+-----------------------------------------+-------------------------------------
RMS | 2767 16 37 19 26 16 26 |T 69 62 61 60 72 56 68
WRMS | 2767 15 31 15 23 16 26 |NE 43 46 43 47 43 45 40
MEDI | 1892 12 20 14 18 14 14 |MD 49 52 48 51 51 45 44
Table 3.2364.4 GPS week: 2364 Day: 4 MJD: 60796
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 2706 12 11 22 12 20 12 7 | 69 67 63 69 76 63 67
R03M | 743 9 22 17 10 8 9 5 | 74 84 67 78 71 76 73
R04M | 663 12 16 14 15 15 17 6 | 78 78 76 88 76 66 76
R05M | 2746 13 30 16 15 12 10 7 | 100 99 91 100 99 100 97
R07 | 1101 7 20 14 18 11 15 6 | 81 70 89 83 71 69 77
R08M | 691 14 20 24 16 13 22 8 | 84 75 105 97 88 79 88
R09 | 4341 17 17 12 15 11 7 6 | 26 31 29 28 30 27 26
R11E | 7039 11 19 12 12 14 16 6 | 64 71 62 68 67 65 65
R12E | 1875 11 16 18 12 16 13 6 | 150 150 147 150 138 147 146
R14E | 5035 12 20 11 16 11 9 6 | 32 32 29 38 31 27 29
R15E | 2357 7 17 14 15 14 17 6 | 38 37 40 39 38 33 35
R16E | 2774 18 21 14 21 6 17 7 | 41 49 42 58 39 36 41
R17 | 1484 8 14 10 7 21 24 6 | 40 43 45 46 39 45 41
R18 | 727 14 22 12 13 14 22 7 | 33 41 31 40 38 39 35
R19 | 1221 42 64 18 48 14 52 18 | 39 42 28 38 31 35 29
R20 | 2362 22 122 28 62 19 74 22 | 44 34 46 26 31 54 36
R21M | 870 15 29 12 22 16 18 8 | 37 43 32 29 25 28 29
R22 | 3635 17 25 15 23 21 13 8 | 33 42 43 39 29 36 32
R24 | 1533 13 20 12 10 13 16 6 | 45 46 42 46 39 35 40
XR26M | 4575 42 76 56 --- 64 --- 34 | 269 273 256 --- 266 --- 263
XR27M | 6881 46 --- --- --- 46 --- 46 | 409 --- --- --- 422 --- 415
------+-----------------------------------------+-------------------------------------
RMS | 2849 16 37 16 23 15 25 |T 85 70 68 61 83 55 82
WRMS | 2849 14 37 17 25 14 25 |NE 42 43 44 43 38 42 39
MEDI | 2357 13 20 14 15 14 16 |MD 45 46 45 46 39 45 41
Table 3.2364.5 GPS week: 2364 Day: 5 MJD: 60797
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 2232 17 17 10 8 27 19 7 | 53 42 46 51 57 37 47
R03M | 1048 8 17 12 11 22 16 6 | 53 61 57 54 64 43 54
R04M | 1067 18 14 10 11 25 19 7 | 56 52 49 53 57 41 50
R05M | 2504 15 18 6 11 28 19 7 | 109 104 105 98 101 97 102
R07 | 1190 12 26 13 17 19 20 7 | 64 64 68 70 62 52 63
R08M | 1588 11 26 19 15 22 27 8 | 85 87 93 89 88 74 86
R09 | 4583 11 28 16 16 25 16 8 | 26 28 43 34 42 29 31
R11E | 5608 11 10 21 22 22 17 8 | 69 68 81 66 80 71 71
R12E | 2587 14 15 14 19 23 19 7 | 130 132 125 128 118 121 125
R14E | 3238 15 13 17 13 28 19 8 | 38 41 53 50 50 40 42
R15E | 2406 10 17 29 17 23 20 9 | 42 38 51 49 45 44 42
R16E | 3353 13 24 12 18 19 21 7 | 39 41 41 51 38 30 37
R17 | 674 13 10 13 12 15 21 6 | 37 32 36 36 32 28 32
R18 | 897 10 41 16 8 22 25 9 | 39 38 50 40 44 47 40
R19 | 914 56 58 15 53 39 48 20 | 55 41 37 41 28 54 40
R20 | 1642 29 117 30 33 29 76 23 | 44 31 43 43 23 38 27
R21M | 1303 6 32 9 10 22 19 7 | 29 42 30 32 23 29 27
R22 | 3472 13 19 10 11 16 25 6 | 31 26 33 31 25 39 29
R24 | 1187 15 31 17 9 18 30 8 | 44 42 46 48 32 48 42
XR26M | 5512 26 84 45 --- 72 --- 31 | 323 332 317 --- 313 --- 319
XR27M | 5923 30 --- --- --- 52 --- 40 | 546 --- --- --- 555 --- 550
------+-----------------------------------------+-------------------------------------
RMS | 2555 19 37 16 19 24 29 |T 91 67 70 56 89 50 88
WRMS | 2555 15 33 15 19 24 29 |NE 42 37 44 42 36 41 38
MEDI | 2232 13 19 14 13 23 20 |MD 53 42 49 50 50 43 42
Table 3.2364.6 GPS week: 2364 Day: 6 MJD: 60798
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1195 6 19 12 12 14 12 5 | 114 99 111 113 113 99 109
R03M | 1395 8 12 7 10 16 8 4 | 111 113 112 111 117 107 111
R04M | 1199 17 14 9 10 11 12 5 | 104 91 89 94 87 87 92
R05M | 1656 13 9 17 9 14 11 6 | 159 156 155 161 156 159 157
R07 | 1114 11 18 16 18 23 13 7 | 120 108 110 118 122 107 114
R08M | 1873 13 26 12 16 15 22 7 | 134 137 143 137 140 126 136
R09 | 3648 17 20 25 28 15 10 9 | 33 34 32 46 34 34 31
R11E | 4898 15 18 10 26 18 14 7 | 42 46 46 48 52 49 45
R12E | 2871 14 12 15 14 13 14 6 | 147 147 138 142 140 143 143
R14E | 2614 8 16 13 23 18 13 6 | 57 61 61 70 57 59 58
R15E | 1503 7 18 24 17 21 18 8 | 70 72 71 77 72 72 70
R16E | 2625 8 28 27 14 14 17 8 | 60 62 63 60 57 53 57
R17 | 952 10 18 11 27 10 23 7 | 59 61 60 62 58 60 59
R18 | 964 6 27 12 17 17 19 7 | 61 58 61 64 63 63 60
R19 | 1879 43 58 20 62 30 53 20 | 60 69 54 63 40 62 55
R20 | 2512 24 139 26 38 25 36 14 | 54 54 54 44 41 64 49
R21M | 1885 10 18 19 14 21 31 8 | 55 56 55 50 42 52 49
R22 | 2865 9 19 15 23 11 16 6 | 55 59 62 59 51 57 55
R24 | 998 13 31 14 20 17 16 8 | 65 68 65 68 58 62 63
XR26M | 7041 45 64 29 --- 51 --- 27 | 194 195 193 --- 197 --- 192
XR27M |11556 44 --- --- --- 61 --- 52 | 607 --- --- --- 601 --- 605
------+-----------------------------------------+-------------------------------------
RMS | 2274 16 39 17 24 18 22 |T 112 87 86 83 109 79 110
WRMS | 2274 15 36 15 20 16 22 |NE 63 63 62 65 58 63 60
MEDI | 1879 13 18 15 17 17 16 |MD 65 68 63 68 63 63 63
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