[IGSREPORT-28909] Wk 2225 IGLOS Final Orbits
acc
acc at igs.org
Mon Sep 19 01:45:06 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2225 (Aug 28, 2022 - Sep 03, 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 2.2225.
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:
igl2225[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2225 in the SP3 format.
igl22257.sum Combination Report for GPS Week 2225.
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 | 0.1 ns
1 | 1.3 ns
2 | 0.5 ns
3 | -1.2 ns
4 | -8.7 ns
5 | -7.5 ns
6 | -5.5 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
----+--------+---------------
1 | COD | R11
1 | GFZ | R11
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 1.2225, 1a.2225).
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 2.2225.0-6)
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 3.2225.0-6).
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 2225 summary. (Aug 28, 2022 - Sep 03, 2022)
Table 1.2225.a GPS week : 2225 MJD: 59819.0-59825.0
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 -2 6 -16 7 .11 22 18 | 30436 -725 3290 8620
| 0 1 3 20 15 32 .05 | 4934 2113
emx n/a| -2 0 15 9 -64 -12 -.04 38 33 | -9041 -385 3269 8374
| 2 1 0 24 25 45 .07 | 14895 1505
esx n/a| -1 0 3 10 29 -20 -.10 27 21 | 1362 -222 3268 11673
| 1 1 1 28 16 25 .05 | 11827 2299
gfz n/a| 0 0 -6 9 -2 7 -.05 30 19 | 0 -882 3066 8159
| 2 1 2 14 21 38 .04 | 0 2107
grg n/a| 5 -1 1 -29 30 7 .37 27 22 | -2898 -669 3265 7995
| 2 1 2 9 9 37 .06 | 3728 2116
iac n/a| -2 0 -5 -11 -14 18 -.28 25 24 | -238 -897 3418 10474
| 2 2 3 32 48 42 .06 | 3898 1180
Table 1.2225.b GPS week : 2225 MJD: 59819.0-59825.0
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 | 23 25 22 22 22 24 21 |
R02 | 8 10 9 11 15 11 17 |
R03 | 8 8 8 8 10 12 10 |
R04 | 9 8 9 11 10 9 9 |
R05 | 9 9 8 10 10 9 10 |
R07 | 8 9 9 8 8 8 9 |
R08 | 9 11 12 10 9 7 8 |
R09 | 7 9 8 10 9 9 9 |
R11 | 10 32 7 9 7 10 10 |
R12 | 9 8 6 6 7 6 6 |
R13 | 14 17 19 14 11 15 14 |
R14 | 6 6 7 6 6 9 7 |
R15 | 7 7 8 6 8 7 6 |
R17 | 9 11 13 9 13 11 9 |
R18 | 9 8 11 9 10 8 7 |
R19 | 21 22 17 15 18 21 20 |
R20 | 26 25 23 27 26 27 22 |
R21 | 12 8 9 9 11 10 8 |
R24 | 11 10 11 11 10 10 10 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2225.c GPS week : 2225 MJD: 59819.0-59825.0
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 2225 0 | -115 -53 24 -375 211 551 80.8 1346 1346 | 79 0
brd 2225 1 | -55 -16 28 166 -1148 -1068 82.4 1648 1648 | 1251 0
brd 2225 2 | -34 -71 15 -454 -188 -1430 81.4 1863 1863 | 471 0
brd 2225 3 | 113 -25 -55 523 794 -3138 82.3 1894 1894 | -1209 0
brd 2225 4 | 14 -73 101 179 -255 -1996 85.9 2025 2025 | -8738 0
brd 2225 5 | -81 20 85 594 -634 -268 85.0 1968 1968 | -7548 0
brd 2225 6 | -24 45 20 1334 161 3293 84.9 1656 1656 | -5485 0
-------------+------------------------------------------------------------+----------------
brd 2225 mean| -26 -25 31 281 -151 -579 83.2 1771 1771 | -3025 0
brd 2225 sdev| 74 45 51 613 627 2077 2.0 236 236 | 4134 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 2.2225.0 GPS week: 2225 Day: 0 MJD: 59819
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 -9 -47 29 .09 23 15 | 33283 -374 3211 8805
emx n/a| 0 0 15 11 -62 33 -.04 41 34 | -16227 -1692 3203 8745
esx n/a| -2 0 6 57 11 -30 -.06 31 20 | 19869 367 3210 11699
gfz n/a| 0 1 -3 0 -9 -56 -.13 32 18 | 0 -258 3254 8887
grg n/a| 6 -2 0 -28 35 7 .40 23 19 | 105 -182 3228 8207
iac n/a| -2 0 -8 -12 18 15 -.33 24 23 | 3671 -2197 3369 9731
Table 2.2225.1 GPS week: 2225 Day: 1 MJD: 59820
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 2 2 1 -23 51 .04 21 16 | 33247 2126 2916 8052
emx n/a| -5 0 16 -25 -51 -24 -.11 39 34 | -10876 1658 2993 7792
esx n/a| -2 0 1 9 15 -28 -.01 26 17 | -696 2382 2921 11917
gfz n/a| -4 0 -5 24 -5 6 -.04 27 15 | 0 1712 2887 7762
grg n/a| 8 -1 0 -27 44 -4 .38 26 21 | 44 1767 2907 7508
iac n/a| 0 1 -9 -19 8 33 -.29 28 26 | 1793 -1307 3562 12676
Table 2.2225.2 GPS week: 2225 Day: 2 MJD: 59821
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 34 -7 -7 .05 24 19 | 36006 -267 3153 8293
emx n/a| -6 1 15 6 -100 26 -.14 36 33 | -17182 664 3186 8270
esx n/a| 0 -2 2 -11 30 -36 -.10 29 20 | -980 1518 3163 11358
gfz n/a| 2 -1 -8 -7 -24 6 -.04 26 15 | 0 590 3153 8303
grg n/a| 7 0 2 -33 25 29 .32 27 20 | 22 388 3153 7723
iac n/a| -4 -1 -4 -2 23 33 -.29 27 26 | 3247 -474 3144 8914
Table 2.2225.3 GPS week: 2225 Day: 3 MJD: 59822
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 37 0 4 .13 23 22 | 34515 -2602 3366 7952
emx n/a| 1 0 16 -6 -91 26 .03 36 32 | 8088 -1157 3362 7910
esx n/a| -1 0 4 -15 39 -56 -.12 25 18 | 14053 -3300 3367 11193
gfz n/a| 0 0 -8 11 2 9 -.07 32 17 | 0 -2844 3424 7811
grg n/a| 6 -1 2 -47 30 28 .28 27 22 | 102 -2925 3350 7721
iac n/a| -7 0 -5 19 -56 -11 -.16 24 22 | 2491 -1161 3381 10425
Table 2.2225.4 GPS week: 2225 Day: 4 MJD: 59823
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 0 -14 -26 .19 21 22 | 26420 -4345 3079 9167
emx n/a| 0 0 15 56 -33 -30 -.07 38 34 | 15686 -2613 3094 8980
esx n/a| 0 2 4 40 60 18 -.18 25 24 | -9182 -3530 3076 12410
gfz n/a| 0 1 -5 31 42 5 -.07 35 31 | 0 -3936 3081 8150
grg n/a| 4 0 2 -30 33 49 .37 26 23 | -6836 -4221 3081 8531
iac n/a| -2 -3 -9 -77 -105 -44 -.36 29 28 | -4706 -2092 3117 11043
Table 2.2225.5 GPS week: 2225 Day: 5 MJD: 59824
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 -8 -3 -7 34 .13 23 20 | 23655 101 4243 9223
emx n/a| -1 1 14 7 -75 -92 .01 39 33 | -21649 620 4156 9159
esx n/a| -2 1 3 -16 19 5 -.13 27 24 | -13196 722 4252 12272
gfz n/a| 1 1 -10 -2 -14 0 -.02 32 14 | 0 -2158 2705 8475
grg n/a| 2 0 4 -20 29 -67 .46 31 27 | -7647 -84 4249 8707
iac n/a| -1 -1 0 18 12 90 -.29 26 25 | -5233 1204 4301 11279
Table 2.2225.6 GPS week: 2225 Day: 6 MJD: 59825
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 -2 -2 -13 -15 -32 .12 22 16 | 25929 284 3066 8853
emx n/a| -1 3 14 16 -38 -28 .05 36 30 | -21129 -177 2891 7764
esx n/a| 0 0 4 7 29 -16 -.12 28 22 | -331 287 2892 10864
gfz n/a| 0 -1 -3 11 -8 77 .01 29 21 | 0 716 2958 7728
grg n/a| 2 -3 -2 -16 13 6 .37 26 23 | -6082 573 2887 7569
iac n/a| 1 3 -4 -3 -3 13 -.26 21 20 | -2933 -253 3052 9254
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 3.2225.0 GPS week: 2225 Day: 0 MJD: 59819
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1981 52 68 78 26 33 33 22 | 126 42 45 104 115 92 87
R02 | 3269 7 36 15 16 17 11 7 | 68 31 52 53 63 73 67
R03 | 834 16 28 14 10 15 20 7 | 81 47 58 68 71 77 68
XR04 | 913 16 22 15 --- 14 18 8 | 67 41 63 --- 61 54 58
R05 | 1047 9 39 25 14 12 23 9 | 67 39 54 59 59 70 58
R07 | 734 15 29 21 12 17 19 8 | 84 53 65 74 81 77 73
R08 | 976 13 36 12 28 14 19 9 | 83 56 71 97 80 88 79
R09 | 988 11 11 18 11 13 25 7 | 35 34 41 37 35 40 35
R11 | 1466 21 30 23 15 17 24 9 | 769 490 464 598 596 577 592
R12 | 802 12 18 19 27 12 27 9 | 32 38 38 44 31 41 32
R13 | 1468 16 35 29 24 52 17 14 | 47 55 32 43 47 44 41
R14 | 703 8 16 15 17 10 14 6 | 33 36 41 39 29 30 32
R15 | 760 9 18 12 20 13 19 6 | 42 39 40 59 43 46 43
R17E | 1441 15 28 15 21 21 15 8 | 141 139 133 140 136 135 137
R18E | 906 12 23 24 13 20 22 8 | 167 165 178 165 169 163 167
R19 | 1125 56 76 40 44 29 31 20 | 72 52 72 69 61 52 57
R20 | 1270 24 74 65 104 41 26 26 | 90 68 71 131 86 85 82
R21E | 847 9 38 28 25 16 36 11 | 149 136 139 151 148 155 146
R24E | 1096 23 46 14 18 20 28 11 | 82 77 78 80 82 84 78
XR25 |24559 --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1345 23 40 31 32 23 24 |T 117 86 91 111 104 104 101
WRMS | 1345 15 34 20 18 19 23 |NE 113 74 80 105 97 96 93
MEDI | 988 15 30 19 18 17 20 |MD 81 52 63 69 71 77 68
Table 3.2225.1 GPS week: 2225 Day: 1 MJD: 59820
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
XR01 | 1605 54 --- 79 20 33 24 25 | 95 --- 53 70 82 57 67
R02 | 5196 13 47 10 14 21 28 9 | 43 22 36 29 43 53 44
R03 | 760 16 28 11 15 14 25 8 | 60 37 46 57 52 46 49
XR04 | 798 15 25 13 --- 19 11 8 | 54 35 56 --- 44 44 47
R05 | 943 16 38 14 13 16 29 9 | 54 31 47 49 48 45 45
R07 | 900 13 32 22 11 20 17 8 | 56 30 42 58 67 55 52
R08 | 696 11 39 21 29 14 26 10 | 56 39 51 85 74 75 63
R09 | 841 15 16 12 13 23 31 8 | 31 36 40 35 28 39 31
XR11 |22409 915 --- --- 306 30 34 32 | 9999 --- --- 636 538 539 541
R12 | 640 19 27 17 10 9 22 8 | 22 25 31 27 22 31 21
R13 | 1170 27 38 36 20 54 47 17 | 29 34 32 25 47 41 19
R14 | 840 8 18 15 13 15 15 6 | 21 30 22 23 21 19 18
R15 | 613 8 18 13 14 16 23 6 | 28 27 25 28 19 27 22
R17E | 2267 24 29 9 21 19 37 10 | 115 115 111 118 115 117 114
R18E | 1235 12 30 18 12 19 16 7 | 133 133 134 125 136 121 130
R19 | 683 45 70 54 46 44 37 21 | 47 51 71 44 49 38 42
R20 | 1268 39 69 62 75 47 32 25 | 52 64 63 64 73 51 50
R21E | 515 13 33 12 18 18 14 7 | 96 87 93 97 96 94 93
R24E | 1058 16 44 11 14 23 29 10 | 50 39 51 50 64 51 48
XR25 |17786 --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1648 21 39 26 27 26 28 |T 57 49 55 90 85 81 78
WRMS | 1648 16 34 17 15 21 26 |NE 46 35 43 87 80 77 74
MEDI | 900 16 32 14 14 19 25 |MD 52 36 47 50 52 51 48
Table 3.2225.2 GPS week: 2225 Day: 2 MJD: 59821
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1170 54 58 80 26 26 30 22 | 107 58 58 93 89 85 77
R02 | 6150 11 50 10 16 10 16 9 | 61 25 49 51 54 68 57
R03 | 703 18 33 12 13 13 21 8 | 64 30 48 57 56 47 50
XR04 | 699 13 30 16 --- 17 18 9 | 56 31 51 --- 42 60 48
R05 | 961 16 27 10 17 17 12 7 | 64 39 52 60 52 48 52
R07 | 527 17 28 17 18 14 21 8 | 73 53 54 69 71 61 63
R08 | 1361 9 39 19 15 18 45 11 | 66 47 61 79 69 98 69
R09 | 773 12 26 10 16 17 26 8 | 27 33 34 39 27 53 33
R11 | 2132 13 11 21 17 10 15 7 | 210 464 457 317 319 322 318
R12 | 1136 8 14 17 11 11 19 6 | 27 29 30 31 31 36 27
R13 | 827 45 33 38 40 52 31 18 | 39 35 34 35 34 37 27
R14 | 821 10 21 13 13 12 20 6 | 24 33 31 33 30 32 25
R15 | 717 12 12 26 15 9 23 8 | 34 31 26 38 31 31 29
R17E | 1503 17 41 23 15 44 25 12 | 112 106 118 113 118 108 110
R18E | 1521 14 25 23 15 27 34 10 | 153 140 160 153 160 150 153
R19 | 1150 21 44 38 50 31 32 16 | 41 44 59 51 44 37 36
R20 | 1560 45 67 37 62 49 43 22 | 61 69 66 76 47 43 49
R21E | 650 22 26 14 16 15 22 8 | 124 113 112 115 121 113 116
R24E | 1623 13 40 16 15 39 17 11 | 64 70 68 68 85 63 66
XR25 |15601 --- --- --- --- --- 6 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1862 24 36 29 26 27 27 |T 74 76 82 82 77 78 73
WRMS | 1862 19 33 20 15 20 26 |NE 63 68 74 73 66 70 64
MEDI | 1136 14 30 17 16 17 21 |MD 64 44 54 60 54 60 52
Table 3.2225.3 GPS week: 2225 Day: 3 MJD: 59822
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 818 44 58 77 32 28 33 22 | 126 55 52 116 104 114 92
R02 | 4560 12 46 19 22 16 26 10 | 71 32 55 48 62 88 72
R03 | 1383 20 32 9 12 12 21 8 | 78 40 57 68 68 62 63
XR04 | 1062 11 32 12 --- 23 26 10 | 67 38 61 --- 64 74 61
R05 | 1569 18 39 17 21 25 17 10 | 71 37 55 75 45 71 59
R07 | 1195 15 29 13 11 20 17 7 | 80 49 65 74 82 70 70
R08 | 2299 7 37 14 14 16 35 9 | 77 52 73 90 78 109 80
R09 | 1435 26 19 18 13 19 27 9 | 23 22 29 24 18 34 18
R11 | 2584 17 20 16 20 31 12 9 | 307 138 148 228 190 213 215
R12 | 1501 11 15 12 12 11 14 5 | 26 30 43 36 34 43 34
R13 | 888 41 21 35 27 32 19 14 | 46 47 37 42 43 45 37
R14 | 1572 12 15 13 10 14 17 6 | 23 23 25 22 25 24 19
R15 | 2875 13 13 13 17 12 13 6 | 34 35 35 46 37 37 35
R17E | 720 17 32 15 20 20 22 9 | 122 117 117 124 115 125 119
R18E | 1227 15 24 20 13 32 17 9 | 125 116 129 125 142 125 127
R19 | 1527 20 45 15 44 32 39 14 | 42 47 31 35 38 53 32
R20 | 1038 44 68 36 104 64 29 27 | 58 43 46 108 43 39 45
R21E | 1098 16 36 9 23 16 21 9 | 178 173 183 188 180 183 181
R24E | 1686 15 35 13 22 30 28 10 | 75 72 77 84 91 54 73
XR25 |17986 --- --- --- --- --- 6 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1894 23 36 25 32 27 24 |T 85 61 69 85 76 82 75
WRMS | 1894 22 32 18 17 22 22 |NE 75 45 54 72 62 71 62
MEDI | 1435 16 32 15 20 20 21 |MD 71 47 55 74 64 70 63
Table 3.2225.4 GPS week: 2225 Day: 4 MJD: 59823
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1501 37 60 70 33 36 38 21 | 122 57 62 121 128 106 98
R02 | 2199 9 55 20 61 20 33 15 | 69 33 48 101 51 102 77
R03 | 804 12 38 23 22 16 29 10 | 83 55 63 90 84 80 75
XR04 | 1177 15 30 16 --- 14 24 9 | 68 51 63 --- 59 70 61
R05 | 2224 21 39 21 16 21 17 10 | 72 39 62 69 58 70 60
R07 | 1954 13 28 14 13 16 25 8 | 73 47 65 63 72 68 64
R08 | 2187 6 37 14 15 20 23 8 | 74 49 68 79 88 88 74
R09 | 1758 17 21 19 20 20 21 8 | 39 43 39 44 37 46 37
R11 | 4674 19 16 11 10 18 14 7 | 365 265 267 323 338 327 323
R12 | 1629 12 20 15 14 9 25 7 | 31 26 48 42 34 52 36
R13 | 1266 13 19 28 24 32 20 10 | 43 47 49 51 41 49 42
R14 | 2613 10 12 11 12 16 23 6 | 29 28 31 32 34 39 29
R15 | 2649 7 16 24 17 17 18 7 | 31 30 28 36 44 36 31
R17E | 708 24 27 11 29 22 48 12 | 136 130 136 143 136 129 134
R18E | 801 14 21 22 17 24 32 10 | 181 184 195 185 184 195 186
R19 | 1185 35 72 18 41 37 33 17 | 32 54 40 36 53 40 31
R20 | 1162 47 61 36 104 61 34 26 | 61 33 46 96 63 54 46
R21E | 1845 18 43 17 21 21 31 11 | 206 192 205 211 205 184 201
R24E | 1460 10 34 11 29 24 29 10 | 44 39 38 50 48 49 40
XR25 |17998 --- --- --- --- --- 11 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 2024 21 38 25 35 26 29 |T 92 73 81 98 92 93 86
WRMS | 2024 22 34 24 31 23 28 |NE 79 57 65 84 78 81 72
MEDI | 1629 14 30 18 20 20 25 |MD 69 47 62 69 59 70 61
Table 3.2225.5 GPS week: 2225 Day: 5 MJD: 59824
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1565 44 71 78 50 26 22 23 | 112 46 49 126 106 97 87
XR02 | 1308 11 41 16 --- 16 27 11 | 68 44 67 --- 85 74 62
R03 | 852 11 40 26 12 23 36 11 | 71 45 53 73 82 97 69
XR04 | 720 9 29 16 --- 16 22 9 | 58 41 50 --- 69 66 56
R05 | 2141 21 33 16 12 14 18 8 | 65 31 45 48 58 52 49
R07 | 1085 21 28 13 10 13 14 7 | 71 41 51 63 63 53 56
R08 | 1539 9 26 10 13 18 16 7 | 69 51 68 61 67 69 64
R09 | 2664 15 16 16 18 26 21 8 | 42 39 46 44 26 45 38
R11 | 4575 22 20 16 13 26 33 10 | 197 181 170 186 216 185 189
R12 | 2206 12 12 18 11 9 14 6 | 34 33 30 33 31 36 30
R13 | 1105 13 20 34 32 57 28 14 | 33 42 38 48 34 61 38
R14 | 1999 13 17 10 17 21 36 9 | 24 29 36 40 28 59 33
R15 | 1517 11 14 8 14 14 27 7 | 25 28 33 34 31 51 32
R17E | 791 17 37 17 21 21 33 11 | 130 124 125 128 124 135 126
R18E | 1603 12 24 17 20 16 19 8 | 171 156 166 157 160 173 164
R19 | 1511 42 85 28 48 35 40 20 | 49 61 50 56 60 58 44
R20 | 888 48 58 41 92 81 15 26 | 63 46 48 79 64 39 46
R21E | 2095 19 36 11 23 18 20 9 | 172 166 172 173 163 176 170
R24E | 1861 10 32 18 25 24 19 9 | 66 64 66 66 75 61 64
XR25 |13085 --- --- --- --- --- 6 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1968 23 39 27 32 31 26 |T 80 66 71 83 81 83 74
WRMS | 1968 20 33 24 14 27 25 |NE 65 50 55 68 68 69 59
MEDI | 1539 13 29 16 18 21 21 |MD 66 45 50 63 67 61 56
Table 3.2225.6 GPS week: 2225 Day: 6 MJD: 59825
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 966 48 64 74 35 17 19 20 | 153 66 58 139 125 116 111
XR02 | 2189 18 --- --- --- --- 15 16 | 100 --- --- --- --- 88 82
R03 | 592 9 33 23 15 11 35 10 | 99 65 79 89 98 120 93
XR04 | 489 9 25 15 --- 18 19 8 | 85 61 75 --- 78 88 78
R05 | 1546 11 36 26 17 19 22 9 | 84 49 69 87 88 94 79
R07 | 787 16 38 19 10 9 18 8 | 91 49 66 76 79 87 76
R08 | 1085 10 30 10 16 15 23 8 | 89 60 80 93 83 103 85
R09 | 1606 16 16 15 22 30 18 9 | 45 48 50 55 32 56 44
R11 | 3222 13 11 21 25 38 12 9 | 342 244 235 295 311 295 295
R12 | 2334 11 12 15 11 13 13 5 | 40 43 37 39 39 42 38
R13 | 1127 14 23 39 23 50 25 14 | 52 56 46 60 43 61 49
R14 | 1604 14 15 12 11 13 23 7 | 34 35 39 39 31 47 35
R15 | 773 8 10 10 20 12 11 5 | 39 40 35 52 40 46 41
R17E | 1292 15 30 14 13 21 25 9 | 145 141 142 146 141 143 142
R18E | 2380 9 22 21 18 16 13 7 | 212 207 212 209 208 209 209
R19 | 1739 49 75 35 49 30 26 20 | 94 87 62 82 91 76 75
R20 | 1324 38 52 42 79 52 28 22 | 84 74 69 110 72 55 69
R21E | 2144 12 29 16 18 13 14 7 | 187 182 190 189 185 184 186
R24E | 1257 15 34 13 31 22 17 10 | 81 74 78 84 91 80 79
XR25 | 8587 --- --- --- --- --- 5 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1656 22 36 28 29 26 21 |T 108 87 90 108 101 104 98
WRMS | 1656 16 30 22 21 23 20 |NE 95 69 71 93 86 91 83
MEDI | 1324 14 29 16 18 17 18 |MD 89 61 69 87 83 88 79
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