[IGSREPORT-29992] Wk 2322 IGLOS Final Orbits
acc
acc at igs.org
Fri Jul 26 07:17:09 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2322 (Jul 07, 2024 - Jul 13, 2024)
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 2.2322.
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:
igl2322[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2322 in the SP3 format.
igl23227.sum Combination Report for GPS Week 2322.
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.
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 | 15.0 ns
1 | 11.7 ns
2 | 14.5 ns
3 | 10.8 ns
4 | 14.8 ns
5 | 10.8 ns
6 | 11.1 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 | ALL | R26
1 | ALL | R26
2 | ALL | R26
3 | ALL | R26
4 | ALL | R26
5 | ALL | R26
6 | ALL | R26
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 1.2322, 1a.2322).
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 2.2322.0-6)
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 3.2322.0-6).
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 2322 summary. (Jul 07, 2024 - Jul 13, 2024)
Table 1.2322.a GPS week : 2322 MJD: 60498.0-60504.0
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 -23 -20 20 .10 21 17 | -4272 -200 3175 8680
| 0 0 1 12 13 54 .01 | 1255 1518
esa n/a| 0 -1 4 -18 12 19 -.08 32 23 | 12369 255 3171 7571
| 1 1 1 15 17 53 .03 | 5637 1333
gfz n/a| 1 0 -1 16 30 12 .01 25 16 | 0 -287 3175 8077
| 1 1 2 13 30 49 .04 | 0 1870
grg n/a| 2 0 4 7 9 -90 .41 26 22 | 12641 -360 3173 7782
| 1 1 1 17 14 53 .04 | 1695 1696
iac n/a| 0 0 -3 9 -15 -39 -.12 17 15 | 14411 -512 3172 8926
| 1 0 2 10 22 180 .08 | 1687 580
jgx n/a| 0 0 -1 -6 21 34 -.28 27 27 | -1089 -345 3135 8148
| 1 1 3 19 12 52 .04 | 1220 1639
Table 1.2322.b GPS week : 2322 MJD: 60498.0-60504.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 13 18 16 17 17 21 18 |
R02 | 9 11 7 7 9 9 6 |
R03 | 6 10 7 8 8 7 8 |
R04 | 6 8 8 7 9 11 5 |
R05 | 6 8 8 8 8 7 6 |
R07 | 6 8 6 6 7 6 7 |
R08 | 7 7 7 6 7 7 6 |
R09 | 6 6 6 6 6 8 6 |
R11 | 7 7 6 8 6 6 7 |
R12 | 7 7 7 6 8 5 6 |
R13 | 12 15 13 14 16 16 14 |
R14 | 5 6 5 6 6 7 7 |
R15 | 6 6 6 8 7 9 7 |
R16 | 7 7 8 10 7 8 8 |
R17 | 8 7 6 8 7 8 7 |
R18 | 8 8 7 8 11 9 9 |
R19 | 22 19 16 17 18 20 25 |
R20 | 30 25 27 32 27 24 25 |
R21 | 7 10 7 8 9 8 8 |
R22 | 8 5 7 7 7 7 7 |
R24 | 7 9 7 7 10 7 9 |
R25 | 11 12 9 11 10 11 12 |
Table 1.2322.c GPS week : 2322 MJD: 60498.0-60504.0
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 2322 0 | -94 -92 155 -2593 2261 7450 81.0 1679 1679 | 14984 0
brd 2322 1 | -60 -18 149 -962 2341 8625 79.9 1654 1654 | 11739 0
brd 2322 2 | 16 14 179 -77 1568 2456 80.0 1817 1817 | 14530 0
brd 2322 3 | 44 61 213 1490 1539 -8019 80.9 1784 1784 | 10825 0
brd 2322 4 | 32 51 204 -1571 -380 -6923 82.3 2047 2047 | 14760 0
brd 2322 5 | -4 9 77 -191 55 -10720 80.5 1796 1796 | 10840 0
brd 2322 6 | -120 -38 38 -956 -892 -8520 79.5 1764 1764 | 11067 0
-------------+------------------------------------------------------------+----------------
brd 2322 mean| -26 -1 145 -694 927 -2235 80.6 1791 1791 | 12677 0
brd 2322 sdev| 65 53 64 1285 1312 8171 .9 128 128 | 1973 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 2.2322.0 GPS week: 2322 Day: 0 MJD: 60498
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 -15 -24 36 .12 22 20 | -2921 -564 3131 8084
esa n/a| -1 -3 3 -35 5 -15 -.09 34 26 | 11609 184 3114 7223
gfz n/a| 0 0 -2 36 -14 -10 .05 22 14 | 0 -869 3177 7281
grg n/a| 1 0 4 -17 24 -155 .42 26 20 | 15047 -398 3163 7046
iac n/a| 0 0 0 8 -2 87 -.05 14 12 | 16529 -30 3120 8155
jgx n/a| 1 1 -7 -37 33 -10 -.33 29 29 | -454 224 3146 7441
Table 2.2322.1 GPS week: 2322 Day: 1 MJD: 60499
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 2 -3 -22 22 .10 20 18 | -6408 -114 3092 9287
esa n/a| -2 -1 4 -30 -11 -19 -.03 32 23 | 12482 938 3090 7800
gfz n/a| 1 -1 0 6 4 -22 .05 27 21 | 0 -249 3155 8904
grg n/a| 5 0 6 27 31 -145 .47 34 24 | 11487 -101 3169 8365
iac n/a| 1 0 0 11 2 29 -.08 13 12 | 13459 -1073 3099 9484
jgx n/a| 0 0 -4 -32 33 24 -.28 22 22 | -3547 263 3145 8582
Table 2.2322.2 GPS week: 2322 Day: 2 MJD: 60500
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 -35 -17 -34 .08 19 17 | -2648 1316 3018 8317
esa n/a| 0 -1 2 -15 12 -41 -.06 29 18 | 11081 271 3022 6883
gfz n/a| 1 -1 -3 19 19 -71 -.03 23 16 | 0 1712 3068 7786
grg n/a| 2 1 4 25 9 -114 .42 26 21 | 13762 938 3063 7678
iac n/a| -3 0 -1 2 10 161 -.11 16 14 | 16504 -805 3027 8666
jgx n/a| 2 -1 -1 2 6 9 -.34 26 26 | 166 868 3035 8172
Table 2.2322.3 GPS week: 2322 Day: 3 MJD: 60501
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 -24 5 84 .08 19 16 | -4510 -2902 3727 8304
esa n/a| 0 0 4 4 0 93 -.12 30 23 | 5447 -2123 3717 6842
gfz n/a| 1 0 -3 34 44 55 -.03 25 15 | 0 -3525 3464 7551
grg n/a| 2 0 2 -13 -5 -54 .42 22 19 | 12570 -3533 3463 7553
iac n/a| 0 2 -4 16 -34 -329 -.22 23 21 | 12666 245 3721 8648
jgx n/a| 1 0 -1 5 2 124 -.28 32 32 | -1319 -3601 3371 7716
Table 2.2322.4 GPS week: 2322 Day: 4 MJD: 60502
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 2 -16 -25 -36 .09 22 17 | -4613 1344 3241 8734
esa n/a| 0 0 5 -27 14 67 -.11 27 24 | 22183 1526 3241 8358
gfz n/a| -1 0 -2 3 72 66 -.05 25 17 | 0 1154 3292 8421
grg n/a| 3 0 2 14 0 -79 .41 25 23 | 13911 1059 3297 7978
iac n/a| 0 1 -4 0 -15 -16 -.03 18 16 | 15308 -63 3239 9136
jgx n/a| 0 -1 -1 4 17 3 -.28 27 27 | -164 31 3154 8285
Table 2.2322.5 GPS week: 2322 Day: 5 MJD: 60503
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 -35 -19 94 .10 21 16 | -4743 683 3009 8988
esa n/a| -1 -1 6 -22 22 64 -.10 34 24 | 16569 1681 3000 8252
gfz n/a| 0 0 -2 4 34 43 .05 24 17 | 0 1303 3015 8163
grg n/a| 1 1 4 9 -4 -3 .36 25 24 | 10195 1061 3035 7726
iac n/a| 1 0 -6 29 -13 -246 -.08 18 17 | 13741 -1292 3006 9122
jgx n/a| 0 0 0 7 26 90 -.25 22 22 | -1114 1143 3071 8079
Table 2.2322.6 GPS week: 2322 Day: 6 MJD: 60504
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 0 -36 -39 -25 .10 20 17 | -4062 -1167 3013 9051
esa n/a| 0 -2 3 0 43 -9 -.07 36 27 | 7213 -690 3018 7645
gfz n/a| 3 1 1 12 56 28 .02 26 15 | 0 -1537 3056 8438
grg n/a| 1 -1 3 5 7 -77 .37 25 23 | 11515 -1551 3024 8132
iac n/a| 2 1 -6 0 -53 37 -.24 18 15 | 12672 -566 2995 9272
jgx n/a| 0 0 2 6 28 -4 -.23 28 28 | -1197 -1346 3023 8763
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 3.2322.0 GPS week: 2322 Day: 0 MJD: 60498
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01E | 2026 31 20 29 22 26 --- 13 | 110 96 106 107 93 --- 101
XR02E | 1081 10 14 28 16 15 --- 8 | 56 59 58 61 53 --- 56
R03E | 1476 9 11 15 21 9 17 6 | 120 124 126 125 117 121 121
R04E | 1981 9 11 17 14 12 16 6 | 94 95 95 102 87 101 94
R05E | 2786 14 18 13 13 11 16 6 | 55 57 49 55 47 56 51
R07E | 1605 8 16 15 16 11 15 6 | 59 73 61 58 58 71 62
R08E | 1526 8 14 15 25 13 20 7 | 49 51 47 58 45 48 47
R09 | 1194 17 14 14 13 13 8 6 | 27 33 34 30 32 27 28
R11 | 2226 13 23 18 11 9 12 6 | 47 42 44 48 43 46 43
R12 | 954 16 12 12 24 12 13 6 | 36 45 33 42 33 38 35
R13 | 1994 13 15 23 47 12 44 12 | 90 93 81 99 85 78 84
R14 | 1052 6 9 8 12 10 16 4 | 40 43 46 45 41 38 41
R15 | 743 12 11 21 8 10 13 5 | 46 36 33 43 39 43 39
R16 | 1209 12 17 11 21 13 12 6 | 50 48 41 40 44 47 43
R17 | 1053 13 15 15 26 11 20 7 | 79 65 73 63 72 62 69
R18 | 1693 10 31 12 22 9 25 8 | 65 85 62 55 56 46 60
R19 | 1488 45 93 37 40 28 43 21 | 124 48 130 115 114 78 104
R20 | 2498 69 95 66 65 22 91 29 | 135 53 152 122 92 76 103
R21 | 1329 21 12 12 13 12 23 7 | 96 90 93 87 87 84 88
R22 | 2112 15 23 13 16 18 16 7 | 37 47 45 41 41 44 39
R24 | 1305 11 17 18 23 10 15 7 | 63 71 64 71 65 58 63
XR25 |18040 15 13 --- --- 15 --- 10 | 36 42 --- --- 35 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1678 22 34 22 26 14 29 |T 68 63 70 69 62 61 63
WRMS | 1678 20 26 14 20 12 29 |NE 64 56 66 64 58 54 58
MEDI | 1488 13 15 15 21 12 16 |MD 56 53 61 58 53 56 56
Table 3.2322.1 GPS week: 2322 Day: 1 MJD: 60499
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01E | 2363 39 44 41 32 29 --- 18 | 56 66 82 65 65 --- 60
XR02E | 1133 13 17 40 22 15 --- 10 | 30 31 49 35 31 --- 29
R03E | 1913 13 11 28 52 11 16 9 | 70 67 65 85 63 66 65
R04E | 2239 9 14 19 38 15 13 8 | 54 59 62 64 54 57 56
R05E | 1314 12 13 24 29 11 17 7 | 30 29 30 33 32 34 29
R07E | 1174 9 14 16 42 13 15 8 | 30 30 32 44 25 36 27
R08E | 1070 6 21 17 31 11 12 7 | 27 30 30 52 27 29 28
R09 | 1357 12 14 16 13 10 13 5 | 31 34 36 29 33 37 32
R11 | 2216 14 28 12 15 11 10 6 | 42 33 41 40 39 33 36
R12 | 1035 15 13 26 17 9 12 6 | 26 28 33 30 28 28 25
R13 | 1951 28 26 18 68 12 50 15 | 59 59 62 65 53 45 51
R14 | 1271 13 18 15 14 10 13 6 | 30 44 42 38 27 32 31
R15 | 663 11 8 18 17 9 13 5 | 32 39 50 31 37 35 35
R16 | 1077 10 19 16 21 10 15 6 | 37 49 44 27 36 28 34
R17 | 1392 15 14 11 14 14 20 6 | 51 43 38 44 51 44 45
R18 | 1612 14 27 19 14 10 19 7 | 44 45 29 36 37 32 36
R19 | 1373 31 72 50 58 24 34 19 | 66 41 82 55 59 57 57
R20 | 3289 55 94 67 58 22 43 24 | 74 41 95 61 51 76 57
R21 | 1596 20 17 38 12 12 28 10 | 60 53 77 58 51 48 55
R22 | 1617 14 10 13 13 8 11 5 | 35 35 35 39 33 32 33
R24 | 1334 16 30 23 28 16 12 9 | 43 67 54 63 41 55 47
XR25 |16549 21 9 --- --- 17 --- 12 | 26 25 --- --- 20 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1654 20 32 27 34 13 22 |T 43 43 50 47 40 42 40
WRMS | 1654 18 23 21 24 12 22 |NE 43 42 51 44 39 41 39
MEDI | 1373 14 17 19 22 11 15 |MD 37 41 44 44 37 36 35
Table 3.2322.2 GPS week: 2322 Day: 2 MJD: 60500
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1360 26 48 47 24 32 30 15 | 41 70 70 47 41 57 42
XR02E | 961 10 21 15 11 9 --- 6 | 33 43 37 34 27 --- 32
R03E | 1230 9 11 16 25 14 13 6 | 36 36 36 41 32 36 33
R04E | 2930 8 13 15 29 14 16 7 | 66 74 63 75 54 69 64
R05E | 966 9 12 12 32 20 17 8 | 39 43 43 47 37 42 37
R07E | 1514 9 13 14 15 11 19 6 | 30 34 36 38 29 35 30
R08E | 883 10 20 21 15 13 16 7 | 28 33 36 38 32 34 30
R09 | 1237 9 9 15 11 14 13 5 | 21 26 28 33 34 22 25
R11 | 2968 16 17 11 9 13 14 6 | 40 32 32 42 51 48 39
R12 | 1818 17 11 16 17 11 15 6 | 32 32 37 31 27 27 27
R13 | 2972 30 18 26 44 13 37 12 | 95 92 99 84 73 95 87
R14 | 663 7 12 14 10 10 12 4 | 31 40 39 33 29 33 32
R15 | 885 12 13 16 10 13 18 6 | 29 34 42 30 38 24 30
R16 | 1030 17 20 18 18 17 11 7 | 34 46 40 25 36 33 33
R17 | 1402 17 17 10 17 10 12 6 | 55 48 49 46 45 43 46
R18 | 1758 12 26 11 10 11 19 6 | 47 57 59 49 38 40 46
R19 | 948 19 62 45 31 18 37 16 | 77 54 96 81 80 52 72
R20 | 3754 54 81 42 70 29 81 26 | 93 53 81 74 71 67 67
R21 | 959 18 14 13 17 7 20 6 | 75 62 72 66 64 60 66
R22 | 1684 14 8 16 22 11 15 6 | 37 41 46 55 40 40 40
R24 | 1228 11 17 19 14 10 15 6 | 64 69 69 70 63 62 65
XR25 |10435 13 13 --- --- 10 --- 8 | 27 33 --- --- 33 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 1817 19 29 23 26 16 26 |T 46 47 52 49 44 45 44
WRMS | 1817 17 18 16 21 14 26 |NE 50 47 56 51 48 46 46
MEDI | 1237 12 14 16 17 13 16 |MD 37 43 43 46 38 40 37
Table 3.2322.3 GPS week: 2322 Day: 3 MJD: 60501
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 861 36 53 42 18 43 21 16 | 37 78 70 49 47 35 43
XR02E | 1372 9 13 18 12 18 --- 7 | 52 46 47 51 60 --- 49
R03E | 2111 12 13 12 18 27 19 8 | 37 33 36 36 45 34 33
R04E | 1186 15 16 17 13 17 18 7 | 49 40 52 47 56 45 47
R05E | 851 9 13 19 19 20 20 7 | 31 34 39 30 32 35 30
R07E | 1112 7 13 10 16 18 11 6 | 31 30 31 35 38 28 29
R08E | 908 7 14 13 9 17 12 5 | 31 33 34 36 40 28 31
R09 | 1280 15 15 11 11 13 13 6 | 23 24 21 21 20 19 18
R11 | 3225 19 18 15 16 26 14 8 | 23 32 23 28 26 31 21
R12 | 1808 12 10 15 9 22 13 6 | 31 26 24 26 27 32 25
R13 | 3708 29 16 23 41 24 37 13 | 62 58 50 48 76 62 59
R14 | 454 10 12 15 10 18 15 6 | 27 24 27 23 30 22 22
R15 | 944 6 22 17 15 24 13 7 | 29 24 32 35 30 25 26
R16 | 1048 19 21 27 16 26 19 9 | 39 43 53 28 30 28 31
R17 | 847 21 16 20 9 19 12 7 | 64 50 46 54 55 49 51
R18 | 1650 11 31 16 12 17 15 7 | 47 60 37 46 38 38 42
R19 | 1526 30 69 32 33 34 28 17 | 94 50 89 89 82 70 76
R20 | 2168 36 74 68 66 31 121 31 | 96 58 146 104 98 70 91
R21 | 834 13 23 21 7 16 21 7 | 87 68 96 82 82 67 80
R22 | 3202 16 14 14 12 15 15 6 | 37 45 54 46 41 50 43
R24 | 1257 11 21 16 11 18 12 6 | 61 63 52 67 72 53 59
XR25 |12169 14 12 --- --- 18 --- 10 | 27 35 --- --- 41 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 1784 19 30 25 22 23 32 |T 46 43 50 46 48 41 42
WRMS | 1784 16 23 15 19 21 32 |NE 49 44 53 49 49 44 45
MEDI | 1257 13 16 17 13 18 15 |MD 37 40 46 46 41 35 33
Table 3.2322.4 GPS week: 2322 Day: 4 MJD: 60502
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01E | 778 32 35 39 30 36 --- 17 | 51 60 69 64 43 --- 50
XR02E | 1262 18 11 16 16 19 --- 8 | 50 46 52 47 41 --- 44
R03E | 3575 11 12 28 19 14 13 7 | 56 68 79 65 64 56 62
R04E | 875 32 18 12 16 16 14 9 | 62 59 62 64 54 54 55
R05E | 852 12 13 23 17 18 17 7 | 46 50 50 47 47 55 46
R07E | 838 12 20 16 17 14 11 6 | 35 49 44 33 40 39 37
R08E | 1348 13 13 19 15 12 12 6 | 37 45 44 45 45 45 41
R09 | 1502 11 8 15 11 15 15 6 | 19 26 34 23 29 28 23
R11 | 2446 10 13 17 13 12 9 5 | 38 48 36 36 31 38 36
R12 | 1613 22 14 12 13 18 18 7 | 30 40 36 34 40 31 32
R13 | 4486 25 23 17 51 28 56 16 | 101 95 98 92 104 96 96
R14 | 653 6 11 17 14 15 9 5 | 34 40 37 39 45 38 36
R15 | 1332 14 17 18 18 17 8 7 | 32 27 28 35 31 27 26
R16 | 1185 19 16 15 15 19 12 7 | 36 39 35 23 41 23 30
R17 | 1470 19 12 16 11 17 15 7 | 56 56 47 56 42 41 48
R18 | 1546 11 46 25 13 24 12 11 | 42 64 32 46 38 36 39
R19 | 1513 29 61 45 43 20 35 17 | 73 66 101 82 73 68 73
R20 | 1719 58 66 64 65 23 79 27 | 79 41 100 67 74 40 60
R21 | 736 20 19 19 15 16 27 8 | 76 65 66 69 81 58 69
R22 | 3956 16 11 16 14 19 11 7 | 37 49 60 49 56 42 46
R24 | 1504 27 22 22 17 11 24 9 | 72 82 69 76 77 75 73
XR25 | 9733 14 12 --- --- 13 --- 9 | 19 33 --- --- 41 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 2047 22 27 25 25 18 27 |T 49 52 56 52 51 46 47
WRMS | 2047 17 24 17 23 16 27 |NE 49 51 55 51 53 45 47
MEDI | 1470 16 14 17 16 17 14 |MD 42 49 50 47 43 41 44
Table 3.2322.5 GPS week: 2322 Day: 5 MJD: 60503
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01E | 1019 26 32 69 40 28 --- 20 | 60 58 101 70 57 --- 60
XR02E | 1902 16 14 16 22 19 --- 9 | 74 74 65 76 64 --- 68
R03E | 3450 12 14 16 17 17 13 6 | 57 54 49 60 50 59 52
R04E | 913 44 15 19 17 18 15 11 | 84 70 72 74 70 69 70
R05E | 2267 11 12 13 16 18 19 7 | 33 36 33 37 37 38 33
R07E | 913 10 14 13 18 17 9 6 | 30 32 23 38 27 32 27
R08E | 1609 9 21 13 17 20 10 7 | 33 43 34 41 33 35 33
R09 | 1354 12 16 14 14 22 17 7 | 26 24 25 36 46 33 30
R11 | 1338 8 14 15 14 16 11 6 | 54 51 50 63 62 62 56
R12 | 1302 11 11 10 10 12 9 4 | 26 32 26 28 24 25 25
R13 | 3390 26 26 22 53 21 51 16 | 125 131 135 126 116 136 128
R14 | 1007 15 17 14 14 19 8 6 | 38 29 36 39 30 29 30
R15 | 2044 16 15 35 20 11 10 8 | 32 29 39 38 31 32 28
R16 | 912 19 21 26 12 18 10 8 | 28 31 34 27 28 28 23
R17 | 1509 21 16 14 11 17 22 8 | 48 43 43 47 40 30 38
R18 | 954 9 37 20 17 21 12 9 | 35 52 34 49 35 32 35
R19 | 945 28 87 33 53 21 39 19 | 70 33 75 70 65 63 60
R20 | 2437 43 96 66 45 21 47 24 | 69 45 95 63 52 60 58
R21 | 743 20 18 17 14 16 21 8 | 52 46 54 41 50 43 45
R22 | 2224 13 16 11 26 13 12 7 | 32 35 41 43 43 34 35
R24 | 1276 12 12 21 13 15 10 6 | 59 53 58 55 52 46 52
XR25 |13176 13 16 --- --- 16 --- 10 | 15 25 --- --- 29 --- 20
------+-----------------------------------------+-------------------------------------
RMS | 1796 21 34 24 25 18 22 |T 49 46 53 53 47 46 45
WRMS | 1796 16 24 17 24 17 22 |NE 47 43 53 51 46 46 44
MEDI | 1338 13 16 16 17 18 12 |MD 38 43 43 47 43 35 35
Table 3.2322.6 GPS week: 2322 Day: 6 MJD: 60504
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1295 23 41 62 35 22 45 17 | 69 72 101 86 75 49 73
XR02E | 1819 10 15 13 14 12 --- 6 | 42 42 41 46 48 --- 42
R03E | 2795 12 15 18 22 18 18 7 | 73 73 74 83 74 70 72
R04E | 1660 8 13 13 16 11 8 5 | 89 91 90 92 91 89 89
R05E | 1506 11 11 21 15 11 10 6 | 31 36 34 34 35 37 32
R07E | 1052 10 17 15 19 17 12 7 | 27 42 27 43 31 38 31
R08E | 2118 8 14 16 17 14 7 6 | 26 33 30 31 27 29 26
R09 | 2230 17 11 14 12 12 11 6 | 39 40 39 38 42 37 38
R11 | 989 10 19 12 18 15 21 7 | 63 56 57 62 66 68 61
R12 | 896 15 13 15 10 13 13 6 | 43 51 54 42 43 39 43
R13 | 2633 25 21 17 43 15 47 13 | 142 145 143 136 127 148 139
R14 | 1821 7 14 13 14 23 11 6 | 51 53 50 51 45 46 47
R15 | 1026 14 20 14 12 18 8 6 | 52 45 49 52 47 50 47
R16 | 1083 14 28 23 11 12 18 8 | 50 54 49 48 43 53 45
R17 | 1684 16 10 11 21 17 15 7 | 86 71 76 69 77 67 74
R18 | 1164 8 32 23 20 19 19 9 | 63 84 52 71 57 57 61
R19 | 1733 44 90 61 45 35 61 25 | 135 59 151 127 119 87 113
R20 | 3180 42 105 36 53 31 65 25 | 121 68 134 111 99 90 99
R21 | 874 24 18 21 16 8 15 8 | 100 87 93 86 83 77 86
R22 | 1824 14 15 14 13 15 13 6 | 55 60 64 59 53 55 56
R24 | 1208 26 18 20 24 16 14 9 | 91 90 87 88 81 78 84
XR25 | 8481 15 20 --- --- 17 --- 12 | 31 49 --- --- 39 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1763 20 36 26 25 18 28 |T 67 63 71 69 63 63 63
WRMS | 1763 17 27 15 23 15 28 |NE 74 67 78 74 68 68 68
MEDI | 1660 14 17 16 17 15 14 |MD 55 56 57 62 53 55 56
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