[IGSREPORT-29030] Wk 2233 IGLOS Final Orbits
acc
acc at igs.org
Thu Nov 17 02:17:36 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2233 (Oct 23, 2022 - Oct 29, 2022)
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 2.2233.
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:
igl2233[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2233 in the SP3 format.
igl22337.sum Combination Report for GPS Week 2233.
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.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -5.9 ns
1 | -6.9 ns
2 | -7.5 ns
3 | -6.1 ns
4 | 0.1 ns
5 | -2.1 ns
6 | 2.0 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 | ESX | R22
1 | ESX | R22
2 | ESX | R22
3 | ESX | R22
4 | ESX | R22
4 | GRG | R11
5 | ESX | R22
6 | ESX | 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 1.2233, 1a.2233).
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 2.2233.0-6)
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 3.2233.0-6).
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 2233 summary. (Oct 23, 2022 - Oct 29, 2022)
Table 1.2233.a GPS week : 2233 MJD: 59875.0-59881.0
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 5 -23 7 26 .16 27 18 | 28912 -36 3238 8600
| 1 0 1 18 18 25 .05 | 5217 2419
emx n/a| 0 0 -9 17 1 -21 .16 43 41 | -12255 -217 3229 8520
| 2 1 2 26 18 40 .09 | 11636 1852
esx n/a| 0 2 0 -10 -5 10 .01 30 20 | 102 653 3219 9682
| 0 1 1 33 15 33 .05 | 9625 2294
gfz n/a| 0 1 0 3 -9 10 -.13 29 16 | 0 103 3283 8515
| 1 0 1 13 17 16 .10 | 0 2516
grg n/a| 0 -4 1 5 9 -50 .12 34 21 | -4110 161 3214 7848
| 2 0 3 6 15 19 .06 | 3657 1908
iac n/a| 0 1 -2 5 10 24 -.27 31 28 | -1594 -617 3194 9008
| 2 2 2 44 37 78 .19 | 3662 980
Table 1.2233.b GPS week : 2233 MJD: 59875.0-59881.0
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 | 16 14 12 15 15 13 12 |
R02 | 7 8 6 8 9 7 9 |
R03 | 7 7 6 6 5 7 6 |
R04 | 8 7 8 8 8 7 9 |
R05 | 10 10 9 9 10 10 10 |
R07 | 5 6 6 8 6 7 6 |
R08 | 9 9 8 8 8 7 7 |
R09 | 13 15 15 20 14 11 12 |
R11 | 9 8 8 8 22 11 12 |
R12 | 8 8 8 8 8 8 12 |
R13 | 15 14 15 15 18 17 18 |
R14 | 8 8 9 8 9 13 14 |
R15 | 8 11 8 9 8 14 8 |
R17 | 9 10 9 10 9 8 11 |
R18 | 9 13 13 12 10 10 9 |
R19 | 25 28 30 31 30 27 28 |
R20 | 25 23 24 32 36 37 32 |
R21 | 9 9 8 9 10 12 10 |
R22 | 22 17 24 28 20 25 28 |
R24 | 12 10 9 9 11 9 10 |
Table 1.2233.c GPS week : 2233 MJD: 59875.0-59881.0
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 2233 0 | 17 52 136 -1192 -97 17 79.3 1222 1222 | -5910 0
brd 2233 1 | -30 35 22 62 -1394 -3059 79.6 1254 1254 | -6919 0
brd 2233 2 | 92 5 66 -190 -1098 -2499 79.7 1148 1148 | -7531 0
brd 2233 3 | 20 -9 35 284 -1355 2016 78.3 1200 1200 | -6055 0
brd 2233 4 | 97 -13 65 1204 976 2316 81.2 1321 1321 | 91 0
brd 2233 5 | 8 -5 90 649 1002 3232 83.1 1287 1287 | -2147 0
brd 2233 6 | -20 -23 78 190 1310 6007 82.0 1472 1472 | 1999 0
-------------+------------------------------------------------------------+----------------
brd 2233 mean| 26 5 70 144 -93 1147 80.5 1272 1272 | -3781 0
brd 2233 sdev| 50 27 37 742 1197 3223 1.7 104 104 | 3756 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 2.2233.0 GPS week: 2233 Day: 0 MJD: 59875
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 7 -20 -5 18 .14 25 18 | 24440 799 2774 7686
emx n/a| -3 3 -9 -9 -5 -84 .02 44 46 | -19473 845 2752 7603
esx n/a| 0 0 -2 -37 -18 -53 .06 26 20 | -2539 1422 2763 9595
gfz n/a| 0 1 0 9 -26 -3 -.07 27 16 | 0 1145 2840 7421
grg n/a| -1 -4 0 15 -10 -71 .16 23 19 | -6447 705 2794 6811
iac n/a| 1 1 0 20 76 158 -.30 26 24 | -3451 -843 2780 8175
Table 2.2233.1 GPS week: 2233 Day: 1 MJD: 59876
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 -19 -8 36 .09 25 17 | 24218 -399 2731 7660
emx n/a| 1 0 -7 -19 4 -2 .11 40 42 | -16327 336 2717 7571
esx n/a| 0 1 -1 4 0 18 -.04 25 20 | -5942 698 2685 9688
gfz n/a| 1 0 -1 14 21 18 -.28 31 16 | 0 167 2734 7495
grg n/a| -1 -4 4 8 0 -68 .13 24 18 | -7043 -73 2706 6777
iac n/a| 1 3 -2 -52 13 -7 .14 29 28 | -4520 -1162 2693 8114
Table 2.2233.2 GPS week: 2233 Day: 2 MJD: 59877
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 -21 28 32 .13 28 18 | 24989 -977 3335 7788
emx n/a| -1 0 -7 11 -14 -6 .15 38 30 | -20227 -654 3350 7896
esx n/a| 0 2 0 -32 -30 41 -.06 27 21 | 3968 -1212 3274 8703
gfz n/a| 0 1 0 18 -15 28 -.01 21 12 | 0 -1178 3300 7842
grg n/a| 0 -6 7 12 3 -49 .15 33 21 | -7629 -557 3263 7230
iac n/a| 1 2 -4 20 15 -6 -.27 27 23 | -4959 -408 3252 8289
Table 2.2233.3 GPS week: 2233 Day: 3 MJD: 59878
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 -26 9 -22 .23 27 19 | 25314 1741 3350 8956
emx n/a| 1 0 -12 22 -3 -22 .30 42 36 | -2232 1123 3330 8813
esx n/a| 0 1 0 -61 3 11 -.02 34 20 | -15859 2072 3271 9604
gfz n/a| -1 0 0 6 5 -4 -.13 36 20 | 0 1688 3406 8625
grg n/a| 3 -3 2 6 3 -13 .19 31 21 | -6955 1412 3261 8150
iac n/a| -4 4 -3 36 -50 70 -.43 30 27 | -4651 -738 3268 9199
Table 2.2233.4 GPS week: 2233 Day: 4 MJD: 59879
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 -7 -16 21 .20 29 20 | 34780 -21 3124 8541
emx n/a| -2 0 -9 60 -11 -69 .22 42 38 | 9868 -281 3120 8349
esx n/a| 0 3 0 14 -6 10 .06 34 19 | -727 711 3095 10451
gfz n/a| -1 0 2 -21 -13 8 -.11 30 15 | 0 234 3262 8519
grg n/a| 5 -4 1 4 40 -53 .13 75 29 | -211 -2 3034 7756
iac n/a| -2 -2 -5 -43 -8 69 -.45 35 31 | 3089 -1463 2934 9005
Table 2.2233.5 GPS week: 2233 Day: 5 MJD: 59880
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 3 -6 9 46 .19 26 16 | 34321 -4532 3190 9662
emx n/a| 3 -1 -12 26 2 22 .18 49 45 | -16790 -4105 3188 9499
esx n/a| 1 3 -2 25 18 -5 .05 33 22 | 12969 -3124 3333 11201
gfz n/a| -1 1 2 3 -20 -8 -.25 32 16 | 0 -4638 3206 9713
grg n/a| 3 -4 0 -3 15 -41 .06 27 20 | -800 -3272 3342 8990
iac n/a| -2 0 0 -12 10 -53 -.23 33 32 | 143 -1175 3335 9928
Table 2.2233.6 GPS week: 2233 Day: 6 MJD: 59881
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 8 -63 33 54 .11 30 22 | 34325 3133 4162 9912
emx n/a| 3 0 -7 33 41 8 .15 46 46 | -20605 1217 4148 9910
esx n/a| 0 3 2 14 -6 47 .01 29 21 | 8848 4005 4116 8537
gfz n/a| -1 2 0 -7 -19 33 -.05 29 16 | 0 3305 4233 9991
grg n/a| -2 -5 -4 -1 9 -55 .03 26 17 | 315 2920 4101 9222
iac n/a| 2 4 0 70 12 -56 -.32 34 33 | 3186 1466 4097 10350
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 3.2233.0 GPS week: 2233 Day: 0 MJD: 59875
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 788 48 31 28 36 20 37 15 | 139 138 118 117 131 152 129
R02M | 1795 10 20 11 15 15 19 6 | 18 21 22 16 17 23 15
R03M | 869 15 20 13 11 15 13 6 | 15 20 28 22 22 28 18
XR04 | 905 8 15 14 --- 17 24 8 | 17 21 24 --- 18 23 13
R05 | 901 16 22 24 9 12 36 9 | 18 19 43 28 23 32 23
R07 | 647 7 9 9 10 13 17 5 | 20 20 20 25 20 30 20
R08 | 1210 23 21 14 23 15 21 9 | 17 22 32 37 20 33 24
R09E | 1500 25 30 24 16 44 27 13 | 103 105 110 98 69 101 94
R11E | 881 17 13 20 17 21 24 8 | 33 35 51 40 72 42 37
R12M | 1881 8 36 19 9 16 24 8 | 79 58 77 81 88 84 78
R13E | 670 25 49 35 26 37 23 14 | 69 33 39 56 71 53 50
R14E | 650 14 28 19 12 14 15 7 | 63 41 65 58 67 61 59
R15E | 498 17 30 14 8 16 17 7 | 70 41 52 60 69 49 57
R17M | 905 11 41 19 15 16 22 9 | 71 42 57 67 78 68 64
R18M | 630 19 32 14 13 17 21 8 | 52 46 75 59 76 68 62
R19M | 2287 45 108 43 73 42 16 25 | 90 44 41 106 72 77 64
R20 | 1896 56 88 66 51 32 39 24 | 93 59 57 65 48 40 47
R21 | 586 15 31 12 19 20 19 8 | 67 43 57 63 78 71 63
XR22 | 1248 --- 54 375 --- 20 20 21 | --- 20 224 --- 69 62 60
R24 | 1230 15 48 17 13 15 45 11 | 73 47 65 69 73 89 68
------+-----------------------------------------+-------------------------------------
RMS | 1222 25 44 26 27 23 26 |T 58 43 62 59 59 59 52
WRMS | 1222 18 46 20 16 19 24 |NE 43 31 65 47 43 47 39
MEDI | 901 16 30 19 15 16 21 |MD 67 41 52 59 69 53 57
Table 3.2233.1 GPS week: 2233 Day: 1 MJD: 59876
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 602 38 32 33 28 27 21 13 | 140 143 136 138 138 142 137
R02M | 1186 14 13 15 16 12 30 7 | 23 21 34 30 26 43 27
R03M | 703 10 15 9 10 13 27 6 | 24 24 32 32 27 47 29
XR04 | 894 9 9 18 --- 14 19 7 | 22 20 30 --- 21 33 21
R05 | 845 19 26 26 18 10 25 9 | 26 28 50 44 30 33 30
R07 | 659 9 13 14 16 14 15 6 | 22 21 28 32 29 31 25
R08 | 1557 15 20 21 25 18 24 9 | 18 20 32 34 29 35 24
R09E | 1768 27 19 31 24 47 29 14 | 95 92 103 86 57 82 82
R11E | 959 15 11 16 14 22 20 7 | 39 42 56 47 78 45 45
R12M | 1437 15 28 16 9 14 26 8 | 85 84 90 88 92 85 86
R13E | 608 19 50 30 33 20 37 14 | 57 42 47 69 51 64 51
R14E | 2156 10 34 14 14 18 17 8 | 56 37 60 55 67 57 55
R15E | 743 21 32 15 27 13 40 11 | 56 35 46 63 51 45 46
R17M | 896 14 35 16 17 21 27 9 | 43 28 34 32 50 50 38
R18M | 459 25 30 21 24 32 37 12 | 44 41 52 50 60 56 47
R19M | 2357 32 103 50 95 51 32 28 | 57 41 50 92 50 52 48
R20 | 1437 71 69 50 44 24 41 23 | 46 56 45 44 52 45 41
R21 | 715 9 31 18 13 21 28 9 | 37 28 36 38 45 57 37
XR22 | 2147 --- --- 388 --- 14 20 17 | --- --- 117 --- 45 40 42
R24 | 1278 14 40 11 14 16 37 10 | 50 36 43 47 49 70 47
------+-----------------------------------------+-------------------------------------
RMS | 1254 25 40 25 31 24 29 |T 49 44 56 56 52 55 47
WRMS | 1254 17 42 20 16 18 28 |NE 31 29 47 39 37 43 33
MEDI | 896 15 30 18 17 18 27 |MD 44 36 46 47 50 47 42
Table 3.2233.2 GPS week: 2233 Day: 2 MJD: 59877
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 817 32 34 31 19 22 27 12 | 100 97 126 109 99 92 104
R02M | 691 12 10 12 8 11 20 5 | 27 27 34 28 29 23 25
R03M | 852 8 10 9 10 17 20 6 | 16 18 19 20 17 17 14
XR04 | 637 12 10 15 --- 10 22 7 | 20 27 21 --- 19 31 19
R05 | 734 22 19 23 17 21 18 9 | 28 31 46 40 23 39 28
R07 | 509 10 7 16 12 12 17 6 | 18 18 22 18 19 23 16
R08 | 1126 17 21 20 10 15 23 8 | 19 19 30 30 19 26 22
R09E | 2090 32 18 21 19 55 38 14 | 97 92 94 88 48 102 83
R11E | 993 18 21 22 11 22 14 8 | 24 28 30 25 37 23 19
R12M | 696 10 25 21 13 18 23 8 | 107 99 109 107 112 103 106
R13E | 582 35 39 24 39 28 23 14 | 54 28 34 55 55 37 34
R14E | 1856 12 37 12 12 25 15 8 | 50 40 57 56 74 50 53
R15E | 530 19 28 12 10 22 20 8 | 58 40 50 51 59 39 48
R17M | 1032 16 29 16 21 20 23 9 | 53 33 48 35 60 54 44
R18M | 485 14 20 37 31 31 26 12 | 54 51 68 52 69 44 51
R19M | 1828 48 105 53 39 91 67 29 | 72 47 79 82 113 97 70
R20 | 1672 74 64 60 39 42 28 23 | 71 65 59 59 41 39 44
R21 | 1083 11 29 12 12 22 14 7 | 53 40 44 51 60 42 47
XR22 | 2039 --- --- 394 --- 26 21 24 | --- --- 165 --- 61 52 52
R24 | 1127 15 32 13 14 17 24 8 | 54 34 42 51 48 55 46
------+-----------------------------------------+-------------------------------------
RMS | 1148 28 38 27 21 33 27 |T 51 43 58 53 53 49 46
WRMS | 1148 18 30 21 12 21 23 |NE 37 33 53 41 36 38 34
MEDI | 852 16 25 20 13 22 22 |MD 53 34 46 51 48 39 44
Table 3.2233.3 GPS week: 2233 Day: 3 MJD: 59878
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 604 34 37 32 38 38 21 15 | 66 71 62 57 70 61 62
XR02M | 1031 13 --- 15 14 11 21 7 | 56 --- 69 65 63 82 65
R03M | 779 8 8 11 11 17 21 6 | 20 23 30 28 26 38 24
XR04 | 625 17 10 18 --- 13 17 8 | 20 23 32 --- 24 30 21
R05 | 1401 16 19 24 25 16 20 9 | 22 29 47 44 23 35 28
R07 | 631 13 14 20 13 9 28 7 | 24 26 29 26 22 35 21
R08 | 678 13 18 15 19 12 24 7 | 20 22 26 28 24 41 22
R09E | 1847 33 37 23 33 68 49 19 | 86 96 91 94 50 120 80
R11E | 1500 16 19 14 16 15 21 7 | 27 35 39 38 76 35 28
R12M | 478 11 32 16 12 13 17 7 | 91 77 93 97 96 107 93
R13E | 952 36 35 32 36 19 35 14 | 57 30 39 39 46 48 35
R14E | 1975 7 30 26 9 11 18 8 | 52 28 63 48 55 53 49
R15E | 672 9 36 16 23 17 22 9 | 51 36 54 65 59 46 51
R17M | 1642 12 29 19 25 20 28 10 | 50 30 36 34 58 61 44
R18M | 388 22 25 30 28 23 28 11 | 31 30 53 28 54 55 39
R19M | 966 61 99 64 82 65 48 31 | 76 43 62 108 73 79 60
R20 | 1533 52 92 93 87 56 47 32 | 97 50 54 120 85 42 65
R21 | 1587 14 31 14 13 13 32 9 | 57 42 48 52 51 64 51
XR22 | 1294 --- --- 384 --- 25 30 28 | --- --- 194 --- 48 29 36
R24 | 937 23 31 12 14 15 19 8 | 71 40 58 61 54 57 56
------+-----------------------------------------+-------------------------------------
RMS | 1200 27 42 34 36 31 30 |T 51 40 58 57 52 55 46
WRMS | 1200 19 36 20 20 21 27 |NE 44 33 61 55 41 41 37
MEDI | 952 16 30 19 19 16 22 |MD 52 30 53 48 54 48 44
Table 3.2233.4 GPS week: 2233 Day: 4 MJD: 59879
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 598 29 28 33 28 31 50 15 | 58 57 51 57 44 80 52
R02M | 568 11 15 9 10 22 42 9 | 128 133 121 125 115 117 122
R03M | 698 11 7 7 9 16 14 5 | 15 17 21 17 21 19 13
XR04 | 693 14 13 10 --- 17 20 7 | 15 21 20 --- 21 25 16
R05 | 928 31 17 21 18 16 23 10 | 24 34 39 35 19 34 24
R07 | 565 13 8 13 10 11 24 6 | 16 14 22 19 14 28 14
R08 | 1709 10 14 12 17 13 31 7 | 19 25 32 40 27 25 23
R09E | 1838 27 20 19 23 49 42 14 | 110 97 109 99 79 127 100
R11E | 2620 23 32 65 22 286 49 21 | 29 34 70 30 202 51 34
R12M | 489 14 26 14 13 15 22 7 | 102 96 108 104 107 96 102
R13E | 1702 33 51 23 52 47 31 18 | 61 31 42 79 52 44 43
R14E | 848 16 24 22 17 18 20 8 | 62 47 66 59 67 58 59
R15E | 993 15 31 13 9 15 21 8 | 52 41 48 46 60 58 49
R17M | 1679 14 27 19 10 23 27 9 | 48 39 40 47 54 50 44
R18M | 637 21 29 14 13 31 27 10 | 35 31 44 41 59 52 41
R19M | 1782 56 97 65 60 80 40 30 | 56 60 52 72 54 41 41
R20 | 1435 75 99 92 79 51 71 35 | 97 80 57 103 61 56 57
R21 | 1179 11 41 13 13 26 19 9 | 51 31 48 56 68 58 50
XR22 | 3085 --- --- 360 --- 19 20 20 | --- --- 174 --- 58 68 62
R24 | 1092 27 40 12 15 22 28 11 | 63 31 43 44 58 39 43
------+-----------------------------------------+-------------------------------------
RMS | 1320 29 42 34 30 75 35 |T 54 48 60 59 62 56 49
WRMS | 1320 20 38 19 15 29 31 |NE 40 33 54 49 40 41 36
MEDI | 993 16 27 14 15 22 27 |MD 52 34 48 47 58 51 43
Table 3.2233.5 GPS week: 2233 Day: 5 MJD: 59880
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 915 29 35 22 36 32 13 13 | 30 32 31 33 29 26 26
R02M | 598 9 11 14 13 10 30 7 | 164 175 165 164 173 163 166
R03M | 709 8 13 16 20 10 20 6 | 14 15 24 19 12 25 12
XR04 | 690 9 15 13 --- 11 24 7 | 19 21 20 --- 17 30 15
R05 | 936 23 29 24 16 14 30 10 | 15 21 41 33 23 32 19
R07 | 619 9 19 14 16 11 24 6 | 13 18 24 27 13 25 15
R08 | 2077 12 14 11 21 20 11 7 | 20 17 28 32 18 17 18
R09E | 1065 23 22 17 23 27 33 10 | 182 173 177 188 181 176 180
R11E | 1854 15 12 15 28 23 42 10 | 23 30 33 29 80 54 27
R12M | 544 15 25 17 12 11 25 7 | 93 92 98 97 104 95 96
R13E | 2506 31 67 31 42 23 37 16 | 60 30 35 68 39 58 42
R14E | 674 16 36 30 23 22 50 13 | 91 86 112 101 81 76 89
R15E | 772 16 36 20 20 53 21 13 | 54 42 48 53 77 52 51
R17M | 1361 10 35 15 11 17 24 8 | 43 28 40 33 49 51 40
R18M | 924 15 32 23 11 19 31 9 | 37 33 43 36 44 51 37
R19M | 2026 28 103 54 81 58 27 26 | 51 60 37 81 55 48 44
R20 | 1432 81 127 104 67 42 61 36 | 85 59 69 76 51 53 50
R21 | 631 12 42 22 18 21 44 11 | 50 40 40 52 63 60 49
XR22 | 3097 --- --- 360 --- 20 29 24 | --- --- 108 --- 67 38 52
R24 | 1029 18 46 14 11 13 22 9 | 47 33 43 37 43 39 38
------+-----------------------------------------+-------------------------------------
RMS | 1286 26 49 33 32 27 33 |T 57 52 60 64 60 58 53
WRMS | 1286 16 45 22 16 20 32 |NE 35 29 46 42 36 36 32
MEDI | 924 15 32 17 20 20 27 |MD 47 33 40 37 49 51 40
Table 3.2233.6 GPS week: 2233 Day: 6 MJD: 59881
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 764 35 34 27 14 15 28 11 | 45 43 53 46 50 58 46
R02M | 731 11 20 18 20 14 30 8 | 205 221 205 205 202 208 204
R03M | 972 10 10 13 15 14 15 6 | 15 16 21 18 18 19 14
XR04 | 629 10 17 15 --- 20 28 9 | 15 25 21 --- 15 33 15
R05 | 1944 21 20 21 17 23 27 9 | 14 18 36 34 21 24 18
R07 | 450 9 8 18 11 9 23 6 | 17 16 28 23 19 20 17
R08 | 2397 16 15 11 19 9 19 6 | 18 15 22 24 15 21 15
R09E | 2168 20 57 18 21 17 34 12 | 137 130 137 130 119 150 132
R11E | 1416 20 11 18 18 32 44 11 | 39 37 44 34 44 60 36
R12M | 884 18 39 22 16 25 42 11 | 196 179 205 200 211 201 199
R13E | 2466 43 51 26 46 37 34 17 | 73 38 44 77 52 43 50
R14E | 601 27 50 13 20 23 52 13 | 127 100 125 120 127 130 121
R15E | 653 15 26 13 17 13 30 8 | 54 45 52 48 51 57 47
R17M | 1382 13 39 21 25 22 25 10 | 69 43 59 78 76 67 66
R18M | 911 19 37 18 8 19 23 9 | 45 39 63 47 64 62 52
R19M | 839 34 102 55 75 68 30 28 | 86 47 46 109 64 75 64
R20 | 2451 88 102 83 52 27 60 31 | 118 35 59 91 64 48 60
R21 | 638 16 29 16 12 20 39 9 | 73 47 59 60 76 74 65
XR22 | 3792 --- --- 383 --- 20 37 27 | --- --- 187 --- 73 62 66
R24 | 1731 13 38 19 14 19 28 9 | 72 44 66 66 68 67 63
------+-----------------------------------------+-------------------------------------
RMS | 1472 30 46 29 29 26 34 |T 74 59 76 78 71 73 67
WRMS | 1472 22 46 21 16 17 33 |NE 46 28 59 49 43 43 39
MEDI | 911 18 34 18 17 20 30 |MD 69 43 53 60 64 60 52
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