[IGSREPORT-28462] Wk 2193 IGLOS Final Orbits
acc
acc at igs.org
Mon Feb 7 04:37:17 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2193 (Jan 16, 2022 - Jan 22, 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 2.2193.
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:
igl2193[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2193 in the SP3 format.
igl21937.sum Combination Report for GPS Week 2193.
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 | -2.7 ns
1 | -3.6 ns
2 | -1.7 ns
3 | -2.6 ns
4 | -2.2 ns
5 | -0.7 ns
6 | -2.2 ns
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 1.2193, 1a.2193).
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 2.2193.0-6)
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 3.2193.0-6).
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 2193 summary. (Jan 16, 2022 - Jan 22, 2022)
Table 1.2193.a GPS week : 2193 MJD: 59595.0-59601.0
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 -4 62 .16 24 19 | 14759 -997 3051 7933
| 1 0 2 17 14 16 .04 | 1120 1077
emx n/a| 0 1 9 42 25 -4 .01 48 37 | -3092 -587 3056 7981
| 1 1 3 20 24 30 .03 | 6330 687
esx n/a| 0 2 3 1 11 -35 -.15 40 35 | 3056 -1515 3050 8246
| 1 1 2 13 14 33 .02 | 6139 1509
gfz n/a| 0 0 2 -2 -12 -21 -.04 26 17 | 0 -964 2994 7550
| 1 0 3 20 15 27 .05 | 0 1565
grg n/a| 0 -2 -6 -19 -3 -16 .29 34 24 | -1958 -871 3036 7406
| 1 1 3 26 15 34 .10 | 458 1236
iac n/a| -1 0 0 -6 18 -1 -.29 29 27 | -288 -491 3038 8484
| 1 1 4 38 59 111 .06 | 835 902
Table 1.2193.b GPS week : 2193 MJD: 59595.0-59601.0
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 | 22 19 18 17 16 19 19 |
R02 | 9 9 12 12 10 8 7 |
R03 | 9 13 12 9 10 10 9 |
R04 | 13 14 10 10 8 8 9 |
R05 | 15 11 11 8 9 9 8 |
R07 | 9 12 16 12 9 9 8 |
R08 | 8 12 12 10 9 8 8 |
R09 | 8 7 7 6 8 7 6 |
R11 | 14 14 9 9 8 8 10 |
R12 | 9 8 7 10 8 7 8 |
R13 | 15 14 15 14 15 14 13 |
R14 | 7 7 8 7 7 6 6 |
R15 | 7 8 7 8 9 7 7 |
R17 | 9 8 10 10 8 8 6 |
R18 | 10 9 9 9 11 9 8 |
R19 | 29 22 26 27 23 21 26 |
R20 | 25 26 27 28 28 25 23 |
R21 | 9 8 10 11 8 10 10 |
R22 | 23 30 34 34 29 26 26 |
R24 | 14 13 13 12 13 13 13 |
Table 1.2193.c GPS week : 2193 MJD: 59595.0-59601.0
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 2193 0 | 65 -23 -56 -2023 -1544 1280 81.2 4994 4994 | -2675 0
brd 2193 1 | -19 -67 24 -410 1 3066 80.4 1612 1612 | -3631 0
brd 2193 2 | -22 -68 58 2441 1070 -2321 82.1 1562 1562 | -1732 0
brd 2193 3 | -20 28 111 1704 2489 -3140 82.7 1554 1554 | -2579 0
brd 2193 4 | -13 43 171 1468 814 -1008 80.4 1836 1836 | -2225 0
brd 2193 5 | -9 68 146 2151 -2471 -3414 81.5 1805 1805 | -745 0
brd 2193 6 | 65 18 16 -761 -741 -2591 79.3 1853 1853 | -2198 0
-------------+------------------------------------------------------------+----------------
brd 2193 mean| 6 0 67 652 -54 -1161 81.1 2173 2173 | -2255 0
brd 2193 sdev| 40 53 80 1707 1684 2457 1.1 1250 1250 | 888 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 2.2193.0 GPS week: 2193 Day: 0 MJD: 59595
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 -28 10 50 .14 23 18 | 16678 -587 2826 8243
emx n/a| 2 0 9 43 5 -34 -.00 46 33 | -596 487 2810 8105
esx n/a| 0 1 6 8 19 -89 -.16 44 38 | 1920 -1260 2851 8582
gfz n/a| 0 0 2 -7 4 -60 -.07 30 17 | 0 -215 2858 8022
grg n/a| 0 -3 -3 1 -31 -43 .28 30 23 | -2608 -426 2830 7364
iac n/a| -4 2 -4 -8 5 171 -.34 28 27 | -286 -300 2827 8708
Table 2.2193.1 GPS week: 2193 Day: 1 MJD: 59596
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 -13 -3 63 .18 23 15 | 13751 -2331 3220 7551
emx n/a| 0 0 9 48 69 3 .01 46 38 | -2821 -897 3246 7589
esx n/a| 0 4 5 -19 19 0 -.17 40 40 | -3877 -2918 3217 7794
gfz n/a| 1 0 -1 -18 -1 15 -.06 26 16 | 0 -3417 3040 7400
grg n/a| -1 0 -9 -17 6 40 .23 35 26 | -2622 -2186 3203 6942
iac n/a| 0 0 0 24 -82 -105 -.23 32 29 | -1710 -1291 3197 8110
Table 2.2193.2 GPS week: 2193 Day: 2 MJD: 59597
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 12 -17 48 .20 22 17 | 15070 168 2905 9830
emx n/a| -1 0 10 35 21 49 .02 47 40 | -16820 112 2934 10075
esx n/a| 1 2 3 9 0 -14 -.12 43 46 | -3180 -579 2901 7743
gfz n/a| 2 -1 0 31 -12 -40 -.00 27 19 | 0 -104 2896 8873
grg n/a| 0 -3 -3 21 -17 -45 .10 38 27 | -1685 -322 2901 9269
iac n/a| 0 0 0 -88 77 -49 -.37 45 41 | 551 -877 2898 10396
Table 2.2193.3 GPS week: 2193 Day: 3 MJD: 59598
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 -6 15 -20 64 .20 23 18 | 15745 -2148 3047 7673
emx n/a| 1 2 13 43 16 -42 -.06 54 44 | -3707 -1119 3111 7905
esx n/a| 0 1 0 16 -8 -74 -.16 42 45 | 8130 -2806 3049 7734
gfz n/a| -1 0 7 -18 -11 -30 -.08 27 17 | 0 -896 2859 7452
grg n/a| 1 -2 -3 -20 11 -19 .36 36 23 | -1866 -1773 3027 7284
iac n/a| -2 -2 -6 12 98 128 -.29 36 33 | 263 -1318 3032 8201
Table 2.2193.4 GPS week: 2193 Day: 4 MJD: 59599
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 -2 10 5 93 .17 25 24 | 13749 -1168 3126 7386
emx n/a| 1 2 14 8 0 -13 .01 49 40 | 1034 -1414 3116 7357
esx n/a| 0 1 0 5 33 -26 -.18 38 27 | -146 -2137 3115 9523
gfz n/a| 1 -1 -1 -20 0 9 -.07 26 20 | 0 -1625 3083 7072
grg n/a| 0 -2 -10 -24 -4 19 .39 34 24 | -1736 -1358 3076 6876
iac n/a| -1 2 6 -11 4 -118 -.23 23 22 | -1144 202 3089 7960
Table 2.2193.5 GPS week: 2193 Day: 5 MJD: 59600
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 -12 14 45 .09 26 19 | 14290 472 2933 7519
emx n/a| 0 2 6 79 19 9 .05 45 35 | 118 -396 2898 7463
esx n/a| 0 1 5 -15 2 -24 -.15 34 20 | 5768 1344 2928 7018
gfz n/a| 0 -1 1 19 -39 -30 .04 21 16 | 0 1475 2908 7005
grg n/a| 1 -4 -6 -35 0 -18 .35 34 23 | -1620 1473 2946 7075
iac n/a| 0 0 1 5 -2 -4 -.29 22 20 | 292 1136 2932 8117
Table 2.2193.6 GPS week: 2193 Day: 6 MJD: 59601
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 -4 -17 -17 71 .12 23 19 | 14030 -1390 3305 7331
emx n/a| 0 1 6 39 48 -4 .04 47 33 | 1148 -888 3282 7376
esx n/a| -2 2 2 3 11 -16 -.13 39 30 | 12782 -2249 3295 9334
gfz n/a| 0 0 5 -6 -24 -12 -.01 27 18 | 0 -1966 3314 7026
grg n/a| 1 0 -12 -62 10 -51 .32 33 24 | -1570 -1509 3269 7036
iac n/a| 0 -1 2 21 25 -32 -.24 18 16 | 13 -989 3291 7896
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 3.2193.0 GPS week: 2193 Day: 0 MJD: 59595
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 808 43 52 52 70 37 40 22 | 73 73 94 107 73 68 73
R02E | 1553 10 20 23 11 24 25 8 | 69 65 75 72 78 77 70
R03E | 1051 16 40 20 17 11 18 9 | 92 80 83 90 89 89 86
XR04E | 1125 29 27 14 --- 19 35 13 | 91 84 90 --- 82 92 86
R05E | 760 22 42 23 32 30 48 15 | 68 51 68 69 63 63 60
R07E | 670 21 29 15 13 17 21 8 | 172 161 167 166 168 163 166
R08E | 1642 12 34 12 17 12 22 8 | 131 122 127 139 138 127 131
R09 | 1066 14 17 10 11 16 28 7 | 29 33 31 30 29 41 28
R11 | 1769 18 18 66 18 23 27 13 | 20 23 26 30 27 33 21
R12 | 2039 24 19 20 15 16 19 8 | 88 66 66 77 72 81 75
R13 | 874 20 23 50 29 46 24 15 | 73 50 49 61 42 63 55
R14 | 506 11 18 18 9 11 21 6 | 64 44 63 54 52 67 56
R15 | 1411 9 14 13 9 12 26 6 | 75 66 66 66 66 57 65
R17 | 1036 18 22 14 12 19 25 8 | 36 25 30 34 43 39 32
R18 | 1266 9 35 11 27 16 27 10 | 36 28 36 44 41 41 35
R19 | 1294 46 126 70 33 73 21 28 | 63 47 41 68 71 56 55
R20 | 1098 29 81 89 64 46 25 25 | 79 48 34 98 70 80 69
R21 | 621 11 38 21 12 12 26 9 | 44 34 39 47 53 56 45
R22 |21153 36 25 104 48 34 35 22 | 46 44 62 40 58 44 33
R24 | 1094 14 63 25 21 24 30 13 | 65 54 55 61 65 64 59
------+-----------------------------------------+-------------------------------------
RMS | 4994 23 46 44 30 30 28 |T 70 59 65 71 69 70 65
WRMS | 4994 18 33 38 17 23 27 |NE 55 43 46 54 53 55 48
MEDI | 1094 18 27 20 17 19 25 |MD 68 50 62 66 65 63 59
Table 3.2193.1 GPS week: 2193 Day: 1 MJD: 59596
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 795 49 36 31 46 52 25 18 | 79 71 64 58 75 85 66
R02E | 3090 11 23 19 15 15 37 9 | 48 47 45 53 54 44 46
R03E | 765 10 46 26 30 40 31 13 | 97 87 85 100 93 109 93
XR04E | 1098 21 28 13 --- 32 41 14 | 93 86 92 --- 104 100 92
R05E | 1729 20 41 14 22 28 29 11 | 46 32 45 52 53 41 40
R07E | 676 19 36 15 10 41 31 11 | 153 144 153 150 150 158 151
R08E | 1482 19 36 16 16 38 32 11 | 121 109 117 121 133 125 120
R09 | 763 10 11 16 13 12 23 6 | 47 48 51 43 45 51 45
XR11 | 1607 21 --- 17 18 13 55 14 | 36 --- 31 44 44 63 37
R12 | 2372 17 18 15 18 15 21 8 | 59 45 48 63 54 41 52
R13 | 1127 34 34 33 26 44 12 14 | 50 32 28 39 31 34 34
R14 | 706 9 19 11 8 18 29 7 | 42 27 42 44 33 60 41
R15 | 1536 10 18 15 12 11 31 7 | 43 37 39 47 43 56 41
R17 | 1661 12 33 16 16 19 17 8 | 26 21 26 24 27 29 23
R18 | 944 7 41 14 18 13 21 8 | 33 31 27 28 29 31 27
R19 | 3509 36 98 49 29 55 30 21 | 27 52 24 28 29 34 23
R20 | 936 32 73 93 53 43 39 25 | 39 36 42 54 30 46 35
R21 | 673 12 29 9 16 20 22 8 | 32 29 33 29 35 36 30
R22 | 845 32 65 110 47 67 72 30 | 45 33 38 62 49 73 39
R24 | 1423 13 73 20 16 25 25 13 | 52 41 47 46 51 52 47
------+-----------------------------------------+-------------------------------------
RMS | 1612 23 46 40 26 35 32 |T 58 53 53 57 58 63 54
WRMS | 1612 15 38 40 16 26 29 |NE 40 36 36 42 38 46 36
MEDI | 1098 17 36 16 18 25 29 |MD 46 41 42 47 45 51 41
Table 3.2193.2 GPS week: 2193 Day: 2 MJD: 59597
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 585 39 40 41 39 51 27 18 | 67 53 64 63 71 58 55
R02E | 3285 10 32 15 23 29 51 11 | 73 68 76 71 96 95 75
R03E | 465 14 35 27 30 22 42 12 | 85 88 90 89 93 91 86
XR04E | 683 21 27 18 --- 18 18 10 | 67 68 64 --- 67 64 64
R05E | 2051 12 32 23 21 25 40 10 | 93 81 99 96 83 87 89
R07E | 716 26 39 15 16 26 79 15 | 237 229 224 221 230 205 224
R08E | 921 16 60 16 29 21 21 12 | 203 188 201 211 202 189 199
R09 | 972 12 19 11 11 16 28 7 | 23 33 27 27 27 34 23
XR11 | 1468 16 --- 16 11 10 31 8 | 26 --- 38 22 26 41 26
R12 | 2242 13 17 9 13 11 31 7 | 82 73 76 77 67 62 74
R13 | 949 28 23 18 32 57 33 15 | 48 50 45 47 36 40 39
R14 | 1057 12 12 13 20 6 36 7 | 58 47 49 39 48 71 50
R15 | 1138 11 13 18 8 7 33 7 | 72 62 65 66 71 64 67
R17 | 1301 12 38 18 10 23 37 10 | 32 28 33 32 38 45 31
R18 | 854 9 40 12 19 16 17 8 | 50 37 39 38 41 40 41
R19 | 1893 45 100 64 32 66 53 26 | 61 47 51 59 57 54 51
R20 | 2701 42 73 93 48 44 50 26 | 57 53 40 58 51 61 47
R21 | 842 11 38 22 26 21 20 10 | 40 48 40 47 47 37 41
R22 | 735 23 61 120 45 93 97 33 | 51 55 50 62 78 110 53
R24 | 1776 16 72 16 16 26 27 13 | 66 73 63 68 67 64 64
------+-----------------------------------------+-------------------------------------
RMS | 1562 22 47 43 27 38 45 |T 74 72 71 73 74 75 69
WRMS | 1562 17 40 46 19 27 41 |NE 51 50 47 49 50 55 46
MEDI | 972 14 38 18 21 22 33 |MD 61 55 51 62 67 62 53
Table 3.2193.3 GPS week: 2193 Day: 3 MJD: 59598
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 465 38 46 27 40 43 25 16 | 70 69 75 77 75 71 68
R02E | 3057 8 30 15 27 32 48 12 | 46 51 52 56 64 60 48
R03E | 867 12 34 19 12 12 34 9 | 97 89 84 98 93 104 92
XR04E | 897 17 24 15 --- 23 22 10 | 76 68 69 --- 75 80 71
R05E | 1434 16 25 13 13 11 25 7 | 43 35 40 44 42 47 39
R07E | 662 23 39 16 32 16 31 11 | 223 207 215 206 217 238 215
R08E | 639 14 44 13 23 12 33 10 | 160 151 154 164 159 150 156
R09 | 1383 13 14 10 12 16 21 6 | 22 29 27 31 23 21 23
XR11 | 1623 17 --- 16 12 16 24 8 | 24 --- 42 26 38 40 30
R12 | 2711 19 22 23 15 16 36 9 | 75 61 58 59 58 91 64
R13 | 712 27 34 18 25 42 36 13 | 63 58 53 51 41 40 48
R14 | 1608 11 15 7 17 8 25 6 | 52 35 49 39 47 56 45
R15 | 1538 12 16 15 9 15 31 7 | 63 49 60 58 45 54 54
R17 | 728 11 45 14 14 20 34 9 | 38 35 45 50 48 51 42
R18 | 1039 13 42 15 13 13 27 8 | 36 37 33 32 39 38 32
R19 | 1885 41 119 62 37 79 38 27 | 47 60 59 55 58 56 45
R20 | 2522 34 93 91 66 54 41 28 | 66 77 63 89 63 69 66
R21 | 675 11 40 30 21 17 38 11 | 47 39 39 51 54 59 47
R22 | 906 39 101 124 28 81 74 33 | 59 71 63 42 62 69 42
R24 | 1640 22 59 23 14 26 15 11 | 42 46 36 35 37 46 37
------+-----------------------------------------+-------------------------------------
RMS | 1553 23 54 42 27 36 36 |T 67 66 65 66 66 72 63
WRMS | 1553 18 44 45 17 23 33 |NE 48 49 48 47 47 53 44
MEDI | 1039 16 39 16 17 16 31 |MD 52 58 53 51 54 56 47
Table 3.2193.4 GPS week: 2193 Day: 4 MJD: 59599
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 753 40 48 35 43 33 17 16 | 65 53 69 83 65 62 63
R02E | 4126 15 26 16 22 17 30 9 | 43 39 42 39 47 48 39
R03E | 794 21 27 12 17 15 29 9 | 59 54 55 59 58 59 55
XR04E | 843 17 26 18 --- 15 9 8 | 48 41 41 --- 48 51 44
R05E | 839 15 32 15 29 16 17 9 | 54 49 58 66 64 52 55
R07E | 1220 16 31 15 20 14 21 8 | 178 175 182 185 179 180 179
R08E | 529 15 37 12 23 15 19 9 | 165 161 162 166 164 162 162
R09 | 2229 13 8 22 14 26 20 8 | 25 26 39 36 28 25 25
R11 | 1275 14 32 17 14 19 17 8 | 15 31 24 18 27 21 17
R12 | 3262 11 26 14 11 17 23 7 | 70 58 64 65 60 86 68
R13 | 1017 37 35 29 30 46 26 15 | 53 24 37 46 40 31 35
R14 | 1486 10 21 18 10 17 18 7 | 47 33 61 57 41 53 49
R15 | 1639 18 15 17 25 16 18 8 | 65 56 48 40 54 57 53
R17 | 1167 11 36 22 16 12 15 8 | 33 22 25 35 33 40 29
R18 | 1820 24 45 15 26 16 16 10 | 34 25 32 36 33 40 30
R19 | 1626 44 109 51 21 63 19 22 | 44 41 41 49 50 44 40
R20 | 3003 21 90 103 51 60 45 28 | 63 35 39 61 60 63 48
R21 | 705 16 30 18 11 14 20 8 | 37 35 38 41 35 33 34
R22 | 1634 59 82 94 29 85 21 28 | 40 48 44 37 34 42 24
R24 | 809 13 66 20 31 18 20 12 | 61 61 66 69 61 57 61
------+-----------------------------------------+-------------------------------------
RMS | 1835 25 49 38 26 34 23 |T 59 53 58 62 59 60 55
WRMS | 1835 24 40 27 20 24 22 |NE 45 38 42 45 42 45 39
MEDI | 1220 16 32 18 22 17 19 |MD 48 41 42 49 48 51 44
Table 3.2193.5 GPS week: 2193 Day: 5 MJD: 59600
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 643 44 62 35 39 40 32 18 | 51 37 44 61 44 55 43
R02E | 3289 9 30 15 18 13 24 8 | 32 27 35 36 42 36 32
R03E | 1333 15 37 13 24 14 25 9 | 56 49 51 62 57 56 54
XR04E | 647 12 28 14 --- 14 16 8 | 54 46 50 --- 50 50 49
R05E | 583 17 34 17 22 20 14 9 | 43 28 43 45 40 33 37
R07E | 2899 17 27 11 17 24 22 8 | 167 151 160 164 162 163 161
R08E | 1351 11 32 14 17 14 18 7 | 140 127 133 137 141 136 136
R09 | 1741 12 23 11 14 16 22 7 | 23 31 23 26 21 35 22
R11 | 1694 12 20 18 10 25 23 8 | 20 25 34 30 29 35 25
R12 | 2959 17 15 16 9 14 17 6 | 62 52 59 58 53 57 56
R13 | 1492 34 20 38 29 40 18 13 | 59 47 57 51 33 39 45
R14 | 882 15 14 11 15 11 15 6 | 44 35 42 33 41 41 38
R15 | 1504 16 24 8 13 16 14 6 | 60 56 56 51 46 49 51
R17 | 964 7 33 14 20 17 17 8 | 27 26 29 33 28 26 26
R18 | 1425 15 34 13 11 20 23 8 | 30 26 28 31 34 38 28
R19 | 804 47 97 48 27 46 26 21 | 50 46 34 41 38 44 36
R20 | 3561 40 95 79 32 63 30 24 | 44 29 46 44 38 35 31
R21 | 801 8 36 19 26 19 21 9 | 26 20 27 29 34 32 26
R22 | 906 59 39 89 25 84 20 25 | 42 64 44 52 44 71 40
R24 | 808 11 66 25 14 36 22 12 | 51 47 50 49 58 41 47
------+-----------------------------------------+-------------------------------------
RMS | 1805 26 45 34 21 34 22 |T 54 48 52 54 51 53 49
WRMS | 1805 19 35 20 16 23 20 |NE 41 38 40 40 38 41 36
MEDI | 1333 15 32 15 18 19 21 |MD 44 37 44 45 41 41 38
Table 3.2193.6 GPS week: 2193 Day: 6 MJD: 59601
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 623 28 68 46 53 40 25 18 | 60 52 71 76 65 48 54
R02E | 3117 6 29 13 20 12 15 7 | 30 32 30 35 34 28 28
R03E | 1657 11 36 18 25 16 17 9 | 76 75 75 82 77 67 73
XR04E | 895 8 39 15 --- 14 14 8 | 65 58 72 --- 72 76 68
R05E | 776 16 35 12 17 20 14 8 | 52 44 49 53 52 50 49
R07E | 3641 17 27 14 20 14 15 7 | 178 178 180 172 178 188 179
R08E | 2142 12 26 11 19 18 22 8 | 197 190 191 194 200 173 189
R09 | 866 12 17 13 16 16 10 6 | 27 30 31 31 28 27 26
R11 | 2263 13 14 19 13 38 24 9 | 18 19 25 27 32 32 21
R12 | 3293 20 16 26 18 10 17 8 | 83 62 61 70 74 71 70
R13 | 2087 23 29 24 22 46 26 12 | 68 63 61 64 43 54 57
R14 | 647 10 11 18 16 12 12 6 | 57 43 63 48 52 48 51
R15 | 659 20 17 18 9 12 17 7 | 80 71 64 63 69 60 67
R17 | 751 9 23 11 11 19 10 6 | 43 34 40 48 48 42 42
R18 | 1024 19 29 20 23 12 10 8 | 42 29 45 48 47 46 41
R19 | 1776 40 110 80 34 62 30 25 | 73 47 36 77 83 74 64
R20 | 2278 41 78 83 52 43 13 22 | 87 53 45 96 82 79 72
R21 | 794 10 38 23 33 23 13 10 | 49 40 43 61 59 47 48
R22 | 897 55 75 84 45 79 23 26 | 54 45 75 88 66 83 55
R24 | 755 15 58 40 14 25 20 12 | 62 50 56 61 72 64 59
------+-----------------------------------------+-------------------------------------
RMS | 1852 23 47 39 27 33 18 |T 70 60 65 73 71 67 65
WRMS | 1852 19 33 30 18 24 16 |NE 57 45 49 60 58 55 51
MEDI | 897 15 29 18 20 18 15 |MD 60 47 56 63 65 54 55
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