[IGSREPORT-27519] Wk 2124 IGLOS Final Orbits
acc
acc at igs.org
Sun Oct 11 16:54:01 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2124 (Sep 20, 2020 - Sep 26, 2020)
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 2.2124.
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:
igl2124[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2124 in the SP3 format.
igl21247.sum Combination Report for GPS Week 2124.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://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 | -2.4 ns
1 | -0.2 ns
2 | -1.4 ns
3 | -0.3 ns
4 | -0.7 ns
5 | -3.0 ns
6 | -1.4 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 1.2124, 1a.2124).
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 2.2124.0-6)
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 3.2124.0-6).
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 2124 summary. (Sep 20, 2020 - Sep 26, 2020)
Table 1.2124.a GPS week : 2124 MJD: 59112.0-59118.0
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 -17 0 -6 .11 26 21 | 19617 -519 3953 13589
| 0 1 2 21 31 24 .03 | 4046 1102
emx n/a| 0 0 15 -29 -7 -31 .12 37 34 | 627 -863 3043 7778
| 1 1 2 17 41 40 .06 | 5228 816
esx n/a| 0 0 6 41 -4 12 .15 34 30 | 2312 -1000 3958 13681
| 1 1 4 19 11 26 .06 | 6864 1727
gfz n/a| -1 0 -8 -16 -7 6 .10 24 16 | 0 -1055 3059 7064
| 2 0 3 15 18 23 .03 | 0 1680
grg n/a| 1 1 3 18 18 -85 -.35 26 21 | -985 -722 3078 7122
| 1 1 4 9 13 85 .03 | 902 1191
iac n/a| -1 0 -8 5 -5 83 -.05 21 19 | 589 -683 4084 13978
| 1 1 3 16 34 67 .03 | 4637 1247
mcc n/a| 0 -4 34 -4 34 1034 -.25 193 193 | --- --- --- ---
| 9 9 33 79 90 470 .56 | --- ---
Table 1.2124.b GPS week : 2124 MJD: 59112.0-59118.0
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 | 21 19 20 23 35 27 20 |
R02 | 12 13 11 12 14 13 16 |
R03 | 10 13 10 11 15 9 10 |
R04 | 12 11 11 11 12 12 10 |
R05 | 12 12 11 11 11 9 12 |
R07 | 8 8 10 10 12 11 10 |
R08 | 8 10 12 12 17 14 12 |
R11 | 9 4 7 6 7 8 7 |
R12 | 8 9 6 7 9 9 8 |
R13 | 17 16 18 21 21 17 12 |
R14 | 6 7 6 7 6 6 6 |
R15 | 10 7 7 8 6 6 8 |
R16 | 17 16 16 13 14 16 15 |
R17 | 10 7 8 8 11 10 9 |
R18 | 10 7 8 7 7 8 8 |
R19 | 18 20 18 21 33 24 21 |
R20 | 21 19 23 22 37 28 23 |
R21 | 9 9 9 10 14 11 10 |
R22 | 13 18 14 14 12 11 14 |
R23 | 10 11 12 10 8 11 10 |
R24 | 10 10 10 8 11 8 8 |
R26 | 12 11 26 21 17 19 14 |
Table 1.2124.c GPS week : 2124 MJD: 59112.0-59118.0
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 2124 0 | 63 -40 7 -126 1731 2427 82.2 1033 1033 | -2402 0
brd 2124 1 | 35 36 46 505 356 3133 83.0 1097 1097 | -228 0
brd 2124 2 | -46 -39 29 -1564 803 5822 82.2 1239 1239 | -1419 0
brd 2124 3 | -32 -24 15 -1022 -412 3797 83.3 1415 1415 | -300 0
brd 2124 4 | 20 -3 82 -1389 1485 3034 81.4 1108 1108 | -737 0
brd 2124 5 | 36 34 18 -742 2159 3119 81.5 1102 1102 | -2952 0
brd 2124 6 | 71 16 25 -352 741 -443 82.3 1108 1108 | -1370 0
-------------+------------------------------------------------------------+----------------
brd 2124 mean| 21 -3 32 -670 980 2984 82.3 1157 1157 | -1344 0
brd 2124 sdev| 45 33 25 732 877 1862 .7 129 129 | 1034 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 2.2124.0 GPS week: 2124 Day: 0 MJD: 59112
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 -1 -31 35 -12 .14 28 21 | 19803 -783 3176 7915
emx n/a| -1 0 15 -42 0 23 .07 37 34 | -1938 -978 2918 7718
esx n/a| 2 -1 3 8 -6 33 .13 33 27 | 12259 -2369 3270 7411
gfz n/a| 0 -1 -1 -28 8 15 .07 22 15 | 0 -2720 2921 6779
grg n/a| 0 0 3 11 15 -96 -.35 31 28 | -1183 -2087 2891 7121
iac n/a| -2 1 -10 35 -38 29 -.05 20 19 | 445 -1646 3446 8062
mcc n/a| -6 0 0 -93 145 885 -.41 137 137 | --- --- --- ---
Table 2.2124.1 GPS week: 2124 Day: 1 MJD: 59113
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 0 -41 -4 22 .13 24 19 | 19616 -381 2874 7721
emx n/a| 2 -1 16 -17 -4 -32 .12 39 35 | 10891 -390 2755 7643
esx n/a| 0 1 12 46 18 0 .15 35 30 | -3456 -397 2864 6776
gfz n/a| -1 -1 -7 -16 -24 10 .08 24 20 | 0 756 2741 6746
grg n/a| 2 2 -2 27 35 -10 -.35 24 17 | -113 -122 2700 6922
iac n/a| -3 0 -9 -7 -43 22 -.01 23 22 | 169 1327 2831 7764
mcc n/a| 5 0 6 14 -77 636 -.39 126 126 | --- --- --- ---
Table 2.2124.2 GPS week: 2124 Day: 2 MJD: 59114
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 3 -6 7 .15 27 25 | 26588 -930 6069 26600
emx n/a| -1 1 14 -20 -71 -70 .18 40 37 | 4488 -501 3122 7449
esx n/a| 0 2 12 37 -17 54 .20 37 37 | 593 -1634 6138 27249
gfz n/a| -2 -1 -7 -9 23 50 .14 29 16 | 0 -1983 3161 6637
grg n/a| 3 0 5 7 15 -76 -.32 22 18 | -819 -1259 3126 6375
iac n/a| -2 -1 -8 9 38 38 -.06 19 18 | 8698 -750 6184 27625
mcc n/a| 12 -2 12 -112 38 635 .41 135 135 | --- --- --- ---
Table 2.2124.3 GPS week: 2124 Day: 3 MJD: 59115
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 -9 -37 -50 .11 26 20 | 18624 -548 3001 7706
emx n/a| 0 -2 19 -39 11 20 .18 45 40 | -3127 -885 2838 7566
esx n/a| 0 0 7 46 -15 25 .21 38 33 | 3267 -573 3014 9311
gfz n/a| -4 0 -10 -7 -2 -16 .13 25 15 | 0 -254 2837 6672
grg n/a| 3 0 3 9 14 -68 -.34 25 20 | 121 -840 2765 6337
iac n/a| 0 0 -4 5 -3 78 -.08 21 19 | 1644 -535 2929 7804
mcc n/a| 8 -1 32 74 -36 1201 .36 175 175 | --- --- --- ---
Table 2.2124.4 GPS week: 2124 Day: 4 MJD: 59116
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 17 -38 -13 .13 18 16 | 22086 223 3136 10765
emx n/a| 0 -4 15 -41 56 -27 .05 30 30 | -3310 -790 2695 7041
esx n/a| -1 0 2 24 0 6 .04 28 31 | 3895 292 3088 9749
gfz n/a| -4 0 -11 -36 -14 10 .08 20 20 | 0 185 2692 6537
grg n/a| 1 0 0 34 39 35 -.32 23 17 | -615 34 2765 6417
mcc n/a| 4 4 83 14 2 673 -.21 215 215 | --- --- --- ---
Table 2.2124.5 GPS week: 2124 Day: 5 MJD: 59117
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 -26 7 15 .09 28 21 | 16931 -2407 3975 9278
emx n/a| -2 0 12 1 -45 -57 .07 33 30 | -1584 -2541 3687 8033
esx n/a| -2 1 6 64 -7 -19 .21 28 26 | 7928 -3746 3927 10036
gfz n/a| 0 0 -10 -26 -26 -9 .10 24 14 | 0 -3563 3700 7546
grg n/a| 2 2 11 20 8 -216 -.40 31 25 | -2225 -2006 3935 7797
iac n/a| 0 0 -13 -5 31 187 -.07 21 20 | -2392 -2284 3900 9162
mcc n/a| -13 -6 77 -25 166 1301 -.21 274 274 | --- --- --- ---
Table 2.2124.6 GPS week: 2124 Day: 6 MJD: 59118
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 -34 43 -12 .05 32 24 | 13672 1188 5445 25143
emx n/a| 0 0 17 -43 0 -77 .15 37 33 | -1026 40 3288 8999
esx n/a| 0 0 4 58 -5 -15 .09 37 30 | -8300 1422 5408 25240
gfz n/a| 1 0 -10 8 -19 -15 .12 24 13 | 0 192 3361 8532
grg n/a| 0 1 2 16 1 -163 -.35 27 24 | -2061 1222 3364 8890
iac n/a| -2 2 -5 -7 -20 142 -.02 20 18 | -5029 -211 5219 23455
mcc n/a| -7 -24 30 98 3 1907 -1.27 291 291 | --- --- --- ---
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 3.2124.0 GPS week: 2124 Day: 0 MJD: 59112
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1266 69 58 75 20 17 21 --- 20 | 124 35 38 86 67 74 --- 68
R02 | 705 18 45 31 14 10 30 194 11 | 93 47 54 84 41 101 78 79
R03 | 504 18 32 32 17 14 19 91 9 | 90 56 46 83 80 93 103 78
XR04 | 647 16 36 24 --- 26 21 --- 12 | 97 89 80 --- 86 93 --- 90
R05 | 1198 14 49 37 24 12 18 --- 11 | 82 41 50 92 76 81 --- 73
R07 | 930 23 25 24 11 15 11 64 8 | 90 54 52 76 74 73 59 71
R08 | 1483 10 28 25 9 19 15 --- 7 | 71 39 49 79 79 82 --- 69
R11 | 560 11 21 16 27 20 18 161 9 | 40 37 47 56 33 34 107 39
R12 | 588 14 13 32 14 21 14 --- 8 | 58 51 41 57 18 54 --- 50
R13 | 984 35 59 34 12 65 10 --- 17 | 68 47 41 65 64 57 --- 56
R14 | 966 18 15 14 10 12 9 --- 5 | 43 42 40 41 45 34 --- 39
R15 | 489 13 18 30 30 18 21 --- 10 | 48 49 38 55 53 40 --- 45
R16 | 744 16 21 40 20 77 18 --- 16 | 36 33 39 42 74 34 --- 40
R17 | 693 17 29 24 10 23 25 --- 9 | 73 63 53 68 55 70 --- 62
R18 | 683 20 20 24 19 24 24 --- 10 | 73 74 82 86 69 69 --- 74
R19 | 1038 52 49 45 26 30 36 --- 17 | 86 76 61 59 50 42 --- 52
R20 | 1061 29 64 44 55 51 26 --- 20 | 78 51 57 92 67 65 --- 65
R21 | 1496 22 29 22 20 15 12 133 9 | 92 70 68 93 26 78 80 80
R22 | 883 31 48 9 28 22 27 --- 13 | 86 78 94 115 98 102 --- 96
R23 | 865 24 14 36 16 27 15 --- 10 | 197 193 194 194 180 173 --- 189
R24 | 2052 23 33 14 17 21 16 --- 9 | 83 63 67 71 73 67 --- 69
XR26 | 4325 21 --- 18 --- --- 11 --- 12 | 58 --- 68 --- --- 67 --- 67
------+----------------------------------------------+------------------------------------------
RMS | 1033 28 37 33 22 31 20 137 |T 80 61 61 79 67 71 85 70
WRMS | 1033 21 34 27 15 28 19 137 |NE 80 61 61 79 67 71 85 70
MEDI | 883 18 29 25 17 21 18 133 |MD 78 51 52 76 67 69 80 68
Table 3.2124.1 GPS week: 2124 Day: 1 MJD: 59113
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 929 52 61 74 25 10 23 --- 19 | 85 31 22 69 60 46 --- 51
R02 | 924 21 46 41 13 13 33 161 12 | 65 33 35 63 37 76 48 54
R03 | 613 9 43 50 15 13 31 119 12 | 65 41 32 77 74 89 67 65
XR04 | 1103 16 30 26 --- 16 18 --- 10 | 74 68 61 --- 54 70 --- 64
R05 | 1882 17 51 33 17 10 25 --- 11 | 65 33 40 64 58 70 --- 56
R07 | 1046 18 26 25 15 8 15 81 7 | 70 50 46 52 60 64 43 57
R08 | 841 9 40 33 17 22 12 --- 10 | 57 34 40 67 71 62 --- 57
R11 | 605 6 12 8 10 7 12 130 4 | 21 20 27 23 19 19 33 19
R12 | 732 15 12 10 26 19 21 --- 8 | 35 26 42 41 21 19 --- 27
R13 | 1785 31 44 39 15 49 28 --- 16 | 38 33 32 40 39 50 --- 37
R14 | 955 13 17 13 20 9 12 --- 6 | 33 30 26 20 33 23 --- 24
R15 | 757 8 15 24 15 11 19 --- 7 | 31 32 25 29 28 30 --- 27
R16 | 1040 11 27 31 28 61 20 --- 15 | 28 26 25 28 46 18 --- 24
R17 | 673 16 26 20 12 10 16 --- 7 | 60 57 56 61 65 53 --- 58
R18 | 593 13 18 19 12 8 24 --- 7 | 80 79 82 78 80 78 --- 79
R19 | 1320 51 67 53 31 36 25 --- 19 | 71 61 64 71 60 52 --- 58
R20 | 940 29 56 54 50 24 35 --- 18 | 66 61 64 83 57 58 --- 63
R21 | 608 14 27 24 19 18 18 127 8 | 61 52 48 66 23 61 52 56
R22 | 1585 34 53 20 58 32 31 --- 18 | 80 72 79 109 83 91 --- 83
R23 | 1091 26 26 41 15 13 17 --- 10 | 186 197 192 189 184 178 --- 187
R24 | 1559 25 31 14 11 19 25 --- 9 | 63 48 47 55 62 40 --- 51
XR26 | 3626 16 --- 15 --- --- 15 --- 11 | 65 --- 72 --- --- 70 --- 70
------+----------------------------------------------+------------------------------------------
RMS | 1096 24 39 35 24 24 23 126 |T 63 51 52 64 57 59 48 57
WRMS | 1096 19 35 30 20 17 22 126 |NE 63 51 52 64 57 59 48 57
MEDI | 940 16 30 25 15 13 20 127 |MD 65 41 42 63 58 58 48 56
Table 3.2124.2 GPS week: 2124 Day: 2 MJD: 59114
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 732 52 62 76 39 14 20 --- 19 | 104 33 26 94 62 78 --- 66
R02 | 1372 25 46 32 15 9 17 142 10 | 79 30 41 68 30 72 57 59
R03 | 586 17 32 41 14 12 23 151 10 | 77 48 53 73 65 83 83 67
XR04 | 463 16 22 33 --- 17 18 --- 10 | 81 72 65 --- 82 72 --- 76
R05 | 1482 23 40 38 18 11 19 --- 10 | 78 41 51 76 55 70 --- 62
R07 | 605 20 27 27 24 13 19 113 9 | 68 44 46 81 51 65 64 60
R08 | 623 11 48 38 19 14 25 --- 11 | 70 39 46 81 80 93 --- 72
R11 | 716 8 10 12 13 18 18 159 6 | 31 30 39 33 42 29 80 30
R12 | 1144 14 16 16 15 8 16 --- 6 | 41 36 48 38 20 30 --- 34
R13 | 2956 47 53 23 17 50 28 --- 17 | 52 30 38 51 38 55 --- 40
R14 | 1007 8 13 15 10 13 13 --- 5 | 31 34 38 35 41 37 --- 35
R15 | 831 9 16 32 11 14 9 --- 7 | 43 38 38 47 45 40 --- 41
R16 | 587 29 53 33 32 48 14 --- 16 | 33 53 38 46 37 30 --- 34
R17 | 1020 25 25 21 13 11 14 --- 8 | 74 62 71 74 67 57 --- 68
R18 | 770 8 21 19 18 20 16 --- 8 | 42 45 46 42 46 49 --- 43
R19 | 748 47 60 57 36 22 27 --- 17 | 76 66 75 83 52 68 --- 68
R20 | 1367 30 68 74 80 29 27 --- 23 | 44 45 54 77 23 35 --- 31
R21 | 803 17 26 24 18 21 15 99 8 | 66 55 52 70 24 64 34 61
R22 | 1906 27 50 22 45 19 20 --- 13 | 60 58 66 96 70 79 --- 70
R23 | 1108 37 28 33 25 19 23 --- 12 | 58 67 58 59 69 73 --- 61
R24 | 1675 30 35 19 15 18 13 --- 9 | 59 45 46 49 48 41 --- 45
XR26 | 3328 43 --- 23 --- --- 36 --- 25 | 56 --- 60 --- --- 72 --- 62
------+----------------------------------------------+------------------------------------------
RMS | 1239 27 40 37 29 22 19 135 |T 60 46 49 63 49 58 63 53
WRMS | 1239 25 37 37 16 18 18 135 |NE 60 46 49 63 49 58 63 53
MEDI | 831 23 32 27 18 17 18 142 |MD 59 45 46 68 48 64 64 60
Table 3.2124.3 GPS week: 2124 Day: 3 MJD: 59115
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 409 49 68 94 37 16 30 --- 22 | 108 35 22 100 59 93 --- 70
R02 | 1165 9 57 35 25 23 8 147 12 | 75 25 45 93 55 73 69 71
R03 | 603 10 37 43 10 30 13 201 11 | 80 41 41 78 93 85 149 72
XR04 | 643 16 28 32 --- 12 21 --- 10 | 76 57 60 --- 59 82 --- 66
R05 | 1357 22 32 28 20 22 23 --- 10 | 73 45 55 66 74 53 --- 59
R07 | 541 17 32 31 13 10 26 139 9 | 70 33 40 66 56 77 90 58
R08 | 688 12 49 35 25 10 29 --- 12 | 62 33 37 83 64 87 --- 62
R11 | 847 12 13 9 18 14 13 246 6 | 34 30 32 33 45 39 154 32
R12 | 1461 13 21 14 19 13 15 --- 7 | 46 38 46 43 25 56 --- 44
R13 | 3682 44 86 39 14 64 29 --- 21 | 59 64 39 52 65 60 --- 52
R14 | 820 7 16 10 18 17 15 --- 6 | 37 28 40 49 44 35 --- 37
R15 | 959 8 14 18 18 25 13 --- 7 | 42 36 34 48 52 41 --- 41
R16 | 962 35 41 24 32 26 11 --- 12 | 38 48 37 44 48 30 --- 37
R17 | 1156 22 28 23 11 11 14 --- 8 | 87 79 70 83 81 62 --- 78
R18 | 911 7 23 16 8 14 17 --- 6 | 67 71 76 76 67 80 --- 69
R19 | 670 51 63 68 42 29 28 --- 20 | 98 83 76 88 68 62 --- 75
R20 | 1584 27 87 70 62 25 25 --- 22 | 68 65 62 75 48 69 --- 52
R21 | 494 20 28 21 17 25 21 106 9 | 52 28 34 47 34 52 45 39
R22 | 3023 30 39 18 30 28 32 --- 13 | 77 73 80 96 72 104 --- 82
R23 | 959 26 23 19 12 24 25 --- 10 | 66 86 72 69 76 90 --- 70
R24 | 1074 17 28 15 11 17 12 --- 7 | 52 31 49 43 45 40 --- 42
XR26 | 3756 28 --- 26 --- --- 32 --- 21 | 62 --- 75 --- --- 101 --- 71
------+----------------------------------------------+------------------------------------------
RMS | 1414 26 45 38 25 25 21 175 |T 64 49 51 66 58 66 101 58
WRMS | 1414 20 40 33 15 20 19 175 |NE 64 49 51 66 58 66 101 58
MEDI | 959 17 32 24 18 22 21 147 |MD 66 41 45 66 59 62 90 59
Table 3.2124.4 GPS week: 2124 Day: 4 MJD: 59116
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg mcc IGL | cod emx esx gfz grg mcc IGL
------+-----------------------------------------+-------------------------------------
XR01 | 721 53 59 86 41 --- --- 34 | 99 30 28 98 --- --- 63
XR02 | 1017 21 35 24 17 --- 142 14 | 65 30 36 64 --- 78 49
R03 | 559 9 40 45 25 26 298 14 | 71 40 33 88 84 134 65
XR04 | 538 19 27 19 --- 14 --- 11 | 75 60 65 --- 66 --- 67
R05 | 967 22 24 27 18 14 --- 10 | 65 37 59 54 54 --- 53
R07 | 710 16 31 36 16 17 63 11 | 72 41 39 70 72 108 61
XR08 | 627 13 41 27 33 --- --- 16 | 64 32 41 77 --- --- 53
XR11 | 625 10 12 12 11 --- 200 6 | 28 30 28 33 --- 55 29
XR12 | 1156 10 15 25 14 --- --- 9 | 42 39 33 46 --- --- 39
R13 | 1694 41 48 32 24 52 --- 20 | 61 37 28 47 54 --- 43
R14 | 801 9 16 14 12 7 --- 6 | 33 33 40 31 31 --- 31
R15 | 1352 6 19 10 16 7 --- 6 | 46 35 48 53 44 --- 45
R16 | 665 18 24 41 26 28 --- 14 | 38 64 38 68 43 --- 48
R17 | 1423 17 29 30 22 15 --- 11 | 70 65 60 82 55 --- 65
R18 | 983 9 18 12 12 13 --- 6 | 56 56 51 55 52 --- 53
XR19 | 718 54 63 75 39 --- --- 33 | 83 46 42 71 --- --- 57
XR20 | 1724 41 82 63 73 --- --- 37 | 64 56 50 106 --- --- 61
XR21 | 540 17 33 27 19 --- 134 13 | 57 47 44 61 --- 40 51
R22 | 1464 17 27 22 26 21 --- 11 | 58 43 68 75 51 --- 57
R23 | 935 13 21 21 16 10 --- 8 | 74 73 74 70 70 --- 71
R24 | 1085 16 38 11 22 19 --- 11 | 30 41 35 43 37 --- 31
XR26 | 3537 13 --- 21 --- --- --- 17 | 57 --- 68 --- --- --- 60
------+-----------------------------------------+-------------------------------------
RMS | 1108 18 30 28 20 22 215 |T 59 44 45 64 54 83 52
WRMS | 1108 16 30 31 20 17 215 |NE 59 44 45 64 54 83 52
MEDI | 935 16 29 25 19 15 142 |MD 61 41 41 64 54 78 53
Table 3.2124.5 GPS week: 2124 Day: 5 MJD: 59117
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
XR01 | 909 64 60 79 26 --- 33 --- 27 | 94 23 37 60 --- 73 --- 51
XR02 | 1027 20 39 33 17 --- 24 148 13 | 61 33 43 63 --- 58 59 50
R03 | 1232 12 32 28 7 24 17 380 9 | 65 44 50 62 68 66 121 58
XR04 | 609 21 26 18 --- 30 21 --- 11 | 88 88 81 --- 99 101 --- 87
R05 | 854 23 27 22 14 14 10 --- 8 | 57 38 50 48 53 55 --- 46
R07 | 646 11 32 40 22 21 16 75 11 | 66 44 46 80 73 75 61 62
R08 | 1156 10 41 33 39 30 32 --- 14 | 56 35 40 90 54 89 --- 61
XR11 | 543 8 14 24 15 --- 16 183 8 | 21 25 21 27 --- 29 51 21
XR12 | 713 10 13 26 20 --- 14 --- 8 | 31 36 29 42 --- 40 --- 34
R13 | 1620 43 43 30 21 63 25 --- 17 | 43 38 33 43 57 37 --- 36
R14 | 854 5 10 14 9 20 12 --- 5 | 28 28 32 27 36 21 --- 26
R15 | 807 6 18 14 12 17 16 --- 6 | 37 26 38 39 39 41 --- 35
R16 | 602 35 16 23 49 53 16 --- 15 | 30 32 36 34 36 27 --- 24
R17 | 1223 24 34 23 14 14 15 --- 9 | 104 99 95 95 104 111 --- 99
R18 | 1297 13 29 12 18 19 17 --- 8 | 63 62 71 75 70 67 --- 68
R19 | 787 74 61 61 37 34 35 --- 23 | 104 95 114 111 123 99 --- 98
XR20 | 855 51 65 58 68 --- 43 --- 28 | 75 91 73 71 --- 63 --- 66
XR21 | 892 15 31 22 18 --- 19 114 10 | 58 41 51 61 --- 63 48 54
R22 | 1280 17 29 18 23 27 27 --- 10 | 73 78 86 77 74 87 --- 76
R23 | 851 17 36 22 18 26 27 --- 11 | 71 66 76 78 61 89 --- 69
R24 | 1571 13 26 15 19 23 15 --- 8 | 53 47 56 62 53 55 --- 51
XR26 | 3303 18 --- 32 --- --- 28 --- 18 | 51 --- 30 --- --- 55 --- 46
------+----------------------------------------------+------------------------------------------
RMS | 1102 28 33 28 24 31 21 274 |T 60 50 54 62 66 63 68 55
WRMS | 1102 21 30 26 14 25 20 274 |NE 60 50 54 62 66 63 68 55
MEDI | 855 17 31 23 18 24 17 148 |MD 58 41 46 62 61 63 59 51
Table 3.2124.6 GPS week: 2124 Day: 6 MJD: 59118
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 943 66 55 80 24 22 18 --- 20 | 124 29 45 83 59 82 --- 68
XR02 | 759 12 52 35 12 --- 37 137 16 | 81 33 49 83 --- 95 73 72
R03 | 1119 8 31 41 15 15 21 472 10 | 86 54 55 93 91 88 124 81
XR04 | 814 20 26 20 --- 15 15 --- 9 | 121 118 108 --- 118 106 --- 114
R05 | 754 19 45 31 18 25 17 --- 11 | 89 59 62 85 87 65 --- 75
R07 | 771 10 32 39 12 22 20 113 10 | 91 61 57 94 87 94 67 84
R08 | 656 16 43 36 31 18 14 --- 12 | 77 50 57 112 90 95 --- 86
R11 | 1598 13 13 17 12 21 13 137 6 | 35 33 39 39 32 32 53 35
XR12 | 524 12 18 32 11 --- 11 --- 8 | 59 57 49 64 --- 54 --- 57
R13 | 1316 32 38 38 12 29 16 --- 12 | 72 40 41 66 70 55 --- 58
R14 | 757 9 15 19 8 9 15 --- 5 | 43 44 39 39 42 39 --- 41
R15 | 994 12 15 22 10 26 12 --- 7 | 62 48 46 54 69 45 --- 54
R16 | 1032 31 28 30 23 56 24 --- 15 | 40 51 64 52 75 30 --- 47
R17 | 735 26 28 19 11 20 14 --- 8 | 99 86 85 95 90 89 --- 90
R18 | 1671 14 25 15 20 20 13 --- 8 | 58 55 62 65 64 61 --- 59
R19 | 797 71 50 47 38 41 29 --- 20 | 108 79 103 99 88 89 --- 88
R20 | 1504 48 74 61 55 26 39 --- 22 | 79 97 104 97 70 73 --- 76
XR21 | 1363 11 31 26 15 --- 16 116 10 | 80 67 57 76 --- 76 81 72
R22 | 707 24 36 19 39 27 27 --- 13 | 87 84 101 116 93 97 --- 95
R23 | 1292 17 32 26 16 29 18 --- 10 | 98 102 109 106 93 100 --- 100
R24 | 1348 16 19 20 12 17 17 --- 7 | 80 80 77 78 69 74 --- 74
XR26 | 2929 25 --- 17 --- --- 17 --- 14 | 52 --- 61 --- --- 55 --- 53
------+----------------------------------------------+------------------------------------------
RMS | 1108 32 37 37 24 27 20 291 |T 78 63 66 79 77 72 79 71
WRMS | 1108 24 33 30 13 24 18 291 |NE 78 63 66 79 77 72 79 71
MEDI | 943 16 31 26 15 22 17 137 |MD 80 57 57 83 75 74 73 72
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