[IGSREPORT-27619] Wk 2131 IGLOS Final Orbits
acc
acc at igs.org
Mon Nov 30 19:04:06 PST 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2131 (Nov 08, 2020 - Nov 14, 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 2.2131.
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:
igl2131[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2131 in the SP3 format.
igl21317.sum Combination Report for GPS Week 2131.
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 | -2.5 ns
1 | -3.1 ns
2 | -1.1 ns
3 | -1.9 ns
4 | -1.3 ns
5 | -2.5 ns
6 | -1.5 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 1.2131, 1a.2131).
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 2.2131.0-6)
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 3.2131.0-6).
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 2131 summary. (Nov 08, 2020 - Nov 14, 2020)
Table 1.2131.a GPS week : 2131 MJD: 59161.0-59167.0
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 -1 1 -7 -1 -1 .17 22 16 | 20058 -1413 3170 7941
| 1 0 2 8 15 16 .04 | 1424 1380
emx n/a| 0 0 -5 -36 -24 -28 .09 32 30 | -8002 -867 3142 8017
| 1 0 3 8 26 21 .05 | 6534 732
esx n/a| -1 1 0 26 -12 -4 .16 29 21 | -413 -3035 3171 10011
| 0 1 1 14 20 25 .05 | 7880 1105
gfz n/a| -1 0 -2 4 -15 -28 .12 31 18 | 0 -1341 3194 7562
| 1 1 2 21 18 35 .09 | 0 1444
grg n/a| 0 0 2 -13 34 -49 -.39 24 19 | -1306 -1343 3173 7274
| 0 1 3 17 12 45 .08 | 854 1432
iac n/a| 0 0 0 14 9 114 -.06 26 24 | -422 9 3148 8129
| 2 0 2 14 21 27 .10 | 874 934
mcc n/a| -3 -6 40 147 -4 32 -.84 206 206 | --- --- --- ---
| 8 5 28 72 208 625 .38 | --- ---
Table 1.2131.b GPS week : 2131 MJD: 59161.0-59167.0
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 14 12 16 18 17 12 |
R02 | 5 8 8 5 7 6 6 |
R03 | 6 6 7 9 6 5 7 |
R04 | 11 11 10 8 10 9 12 |
R05 | 9 10 7 9 10 10 11 |
R07 | 6 8 8 7 6 6 9 |
R08 | 6 9 8 5 6 7 7 |
R09 | 7 9 8 7 7 8 9 |
R11 | 7 7 8 7 7 8 7 |
R12 | 11 10 10 7 8 8 9 |
R13 | 15 20 22 18 16 17 15 |
R14 | 10 10 10 8 9 8 9 |
R15 | 9 9 8 8 8 8 9 |
R16 | 13 15 12 13 12 14 10 |
R17 | 7 10 9 8 13 15 13 |
R18 | 8 7 7 8 10 12 11 |
R19 | 21 24 22 25 23 24 27 |
R20 | 20 23 21 22 22 21 23 |
R21 | 9 9 11 9 10 11 8 |
R22 | 12 20 18 15 14 13 13 |
R23 | 9 10 10 10 17 12 15 |
R24 | 9 8 8 10 8 9 11 |
Table 1.2131.c GPS week : 2131 MJD: 59161.0-59167.0
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 2131 0 | 2 47 110 -1439 388 91 83.2 1880 1880 | -2468 0
brd 2131 1 | -46 -21 120 -1261 1234 -228 82.7 1771 1771 | -3075 0
brd 2131 2 | -50 98 28 -134 -41 -2420 82.7 1912 1912 | -1143 0
brd 2131 3 | -60 37 130 -575 1616 -450 80.9 1618 1618 | -1920 0
brd 2131 4 | -46 -41 133 1639 180 308 80.3 1463 1463 | -1270 0
brd 2131 5 | 26 -16 127 8 1338 344 82.2 1332 1332 | -2541 0
brd 2131 6 | 5 47 146 -449 936 410 82.2 1527 1527 | -1481 0
-------------+------------------------------------------------------------+----------------
brd 2131 mean| -24 21 113 -315 807 -277 82.0 1643 1643 | -1985 0
brd 2131 sdev| 34 49 39 1016 635 996 1.0 219 219 | 731 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 2.2131.0 GPS week: 2131 Day: 0 MJD: 59161
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 0 -13 -1 22 .20 16 14 | 21883 -1483 3833 7677
emx n/a| -1 0 -6 -18 -35 -46 .10 30 30 | -8634 -576 3697 7805
esx n/a| 0 2 1 53 -16 -42 .23 29 22 | 3946 -2841 3855 9400
gfz n/a| 0 0 0 0 5 -91 .13 26 18 | 0 -694 3901 7473
grg n/a| 1 0 4 -13 17 44 -.37 22 18 | -2188 -638 3845 6616
iac n/a| 1 0 0 -4 17 81 -.10 25 22 | -1086 235 3667 7874
mcc n/a| -7 1 15 243 -100 488 -.91 155 155 | --- --- --- ---
Table 2.2131.1 GPS week: 2131 Day: 1 MJD: 59162
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 2 0 0 -15 12 -21 .11 20 16 | 20721 -2294 3104 7869
emx n/a| -1 0 0 -46 -42 -57 .06 34 34 | -12319 -1932 3093 7930
esx n/a| -2 3 1 17 -14 26 .07 31 23 | -12613 -3514 3098 9973
gfz n/a| 0 0 -4 23 0 19 .15 32 21 | 0 -2174 3114 7668
grg n/a| 0 0 4 -7 54 -58 -.39 29 22 | -1849 -2401 3106 7315
iac n/a| 1 -1 1 2 -11 118 -.03 25 21 | -1746 -613 3099 8014
mcc n/a| 4 -3 24 146 -359 969 -.55 265 265 | --- --- --- ---
Table 2.2131.2 GPS week: 2131 Day: 2 MJD: 59163
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 0 -17 -6 8 .19 20 15 | 20049 530 3004 8283
emx n/a| 0 0 -1 -39 -19 2 .02 33 30 | -6293 75 2992 8416
esx n/a| -2 2 0 20 -24 8 .14 31 22 | -145 -1261 3022 10292
gfz n/a| -2 0 -4 -16 -16 2 .25 33 21 | 0 -348 3034 7938
grg n/a| 0 0 5 11 39 -91 -.36 24 19 | -1298 115 3011 7336
iac n/a| 1 -1 -1 41 12 104 -.22 23 21 | -252 1250 2998 8477
mcc n/a| -7 -5 63 19 -87 275 -1.44 284 284 | --- --- --- ---
Table 2.2131.3 GPS week: 2131 Day: 3 MJD: 59164
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 0 -23 12 .22 25 18 | 19964 -404 3324 7788
emx n/a| 0 0 -6 -36 -24 -31 .05 31 29 | -4580 -493 3321 7824
esx n/a| -1 0 2 36 -22 -37 .16 30 20 | -7177 -2761 3324 9609
gfz n/a| 0 0 -5 -30 -38 -14 .12 33 17 | 0 -567 3395 7269
grg n/a| 1 1 0 0 21 -46 -.26 20 16 | -1778 -496 3338 7668
iac n/a| 2 0 0 10 47 88 -.09 21 20 | 603 -651 3336 7925
mcc n/a| -14 -2 60 157 209 -247 -1.25 195 195 | --- --- --- ---
Table 2.2131.4 GPS week: 2131 Day: 4 MJD: 59165
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 5 -3 0 -11 .18 26 17 | 20615 -409 2806 7858
emx n/a| -2 0 -3 -36 -36 -36 .12 31 31 | -4708 -388 2790 7893
esx n/a| -1 0 1 15 -3 6 .20 26 18 | 4437 -2526 2789 9878
gfz n/a| -3 -2 2 13 -14 -37 -.03 31 18 | 0 517 2772 7542
grg n/a| 1 0 -1 -42 29 -38 -.36 23 20 | -1261 11 2791 7649
iac n/a| 1 -1 -2 12 12 142 -.09 28 28 | 531 267 2818 7996
mcc n/a| -10 -11 79 203 171 25 -.74 160 160 | --- --- --- ---
Table 2.2131.5 GPS week: 2131 Day: 5 MJD: 59166
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 5 -11 -10 .20 23 16 | 19962 -2512 3030 7437
emx n/a| 0 1 -7 -41 31 -22 .15 30 30 | 399 -1044 3029 7578
esx n/a| 0 0 0 31 27 -4 .16 28 20 | -2396 -3467 3032 9671
gfz n/a| -1 -1 -1 31 -41 -44 .05 31 16 | 0 -2584 3033 7281
grg n/a| 0 1 2 -27 33 -68 -.47 23 20 | -1223 -2473 3034 6682
iac n/a| -4 0 1 19 -20 156 .08 30 28 | -61 -1366 3027 7717
mcc n/a| 0 -15 36 165 -61 -316 -.55 244 244 | --- --- --- ---
Table 2.2131.6 GPS week: 2131 Day: 6 MJD: 59167
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 1 -3 21 -10 .12 23 17 | 17215 -3321 3090 8676
emx n/a| 0 0 -9 -34 -44 -4 .13 32 24 | -19881 -1711 3078 8677
esx n/a| 0 2 -1 11 -35 10 .11 27 19 | 11056 -4877 3079 11255
gfz n/a| -1 0 0 7 -3 -31 .14 29 15 | 0 -3539 3115 7766
grg n/a| 2 -1 -2 -12 42 -85 -.50 25 18 | 449 -3519 3092 7655
iac n/a| -2 0 4 21 10 108 .01 32 31 | -946 941 3097 8903
mcc n/a| 8 -9 0 97 193 -968 -.46 140 140 | --- --- --- ---
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 3.2131.0 GPS week: 2131 Day: 0 MJD: 59161
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 | 994 44 --- 34 32 43 --- --- 23 | 75 --- 56 59 53 --- --- 59
R02 | 716 7 6 11 15 13 17 114 5 | 45 52 54 50 49 47 157 48
R03 | 1013 9 14 6 12 17 22 179 6 | 56 57 59 54 64 49 22 56
XR04 | 699 13 15 31 --- 25 21 --- 10 | 60 64 40 --- 66 44 --- 53
R05 | 1062 18 20 23 25 7 19 --- 8 | 58 54 52 47 47 49 --- 49
R07 | 2145 7 8 11 12 14 22 219 5 | 58 56 48 51 52 51 217 52
R08M | 1037 6 10 12 17 12 15 --- 5 | 54 55 62 66 53 49 --- 55
R09 | 4633 17 17 20 14 7 19 --- 7 | 79 81 75 73 78 76 --- 76
R11 | 992 11 25 11 16 18 18 150 7 | 56 36 50 62 55 56 60 51
R12 | 1968 11 35 36 24 18 20 --- 10 | 61 25 33 70 58 63 --- 51
R13 | 4098 28 43 50 24 18 32 --- 14 | 82 50 41 59 66 79 --- 59
R14 | 1915 14 24 22 20 29 26 --- 10 | 70 63 53 65 53 78 --- 62
R15 | 731 15 26 24 16 14 23 --- 8 | 59 31 31 52 43 56 --- 45
R16 | 925 17 21 31 41 36 24 --- 13 | 72 68 89 94 56 80 --- 73
R17E | 1104 12 26 15 12 14 14 --- 7 | 97 95 98 100 100 105 --- 98
R18E | 613 12 15 20 17 19 23 --- 7 | 52 58 61 48 48 62 --- 52
R19E | 1942 31 65 60 49 44 40 --- 21 | 63 55 66 73 70 62 --- 56
R20E | 679 19 59 58 56 34 47 --- 20 | 145 152 163 174 142 161 --- 151
R21E | 495 7 30 17 23 19 25 67 9 | 53 47 54 60 55 57 78 51
R22E | 2060 21 25 27 23 29 30 --- 11 | 88 89 108 106 85 102 --- 92
R23E | 698 19 20 21 20 20 16 --- 8 | 110 120 113 124 109 115 --- 113
R24E | 1827 12 31 22 19 18 14 --- 8 | 41 35 43 44 37 42 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1879 16 30 29 26 22 25 155 |T 69 63 65 72 65 70 106 65
WRMS | 1879 14 30 22 18 18 22 155 |NE 63 53 52 61 56 60 114 56
MEDI | 1013 13 24 22 20 18 22 150 |MD 60 56 54 62 55 62 78 55
Table 3.2131.1 GPS week: 2131 Day: 1 MJD: 59162
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 | 699 29 38 23 17 47 19 --- 13 | 43 57 57 47 37 46 --- 39
R02 | 1349 9 31 10 13 17 21 312 7 | 27 42 30 35 20 20 58 24
R03 | 519 6 14 20 14 13 15 136 6 | 35 38 43 30 31 26 18 31
XR04 | 988 23 26 23 --- 16 23 --- 11 | 37 41 28 --- 30 24 --- 29
R05 | 940 21 23 27 25 13 14 --- 9 | 32 30 32 26 24 21 --- 23
R07 | 1822 13 17 15 16 19 18 455 7 | 30 23 24 27 39 33 331 27
R08M | 1008 13 10 29 24 20 21 --- 9 | 26 29 50 45 33 25 --- 31
R09 | 2988 14 10 27 28 13 19 --- 8 | 59 62 63 70 64 65 --- 61
R11 | 631 9 22 15 18 14 18 128 7 | 40 30 38 44 35 38 39 36
R12 | 1157 17 41 28 15 17 16 --- 10 | 48 23 28 46 42 50 --- 38
R13 | 3924 32 61 52 41 47 41 --- 20 | 62 44 33 41 72 67 --- 45
R14 | 2379 17 26 22 18 24 22 --- 9 | 40 41 56 55 53 61 --- 48
R15 | 1155 16 23 19 16 21 19 --- 8 | 42 26 26 37 28 49 --- 34
R16 | 995 19 29 30 52 39 25 --- 14 | 45 56 52 64 32 59 --- 45
R17E | 2359 12 27 21 22 25 23 --- 9 | 93 90 81 95 86 89 --- 88
R18E | 665 12 17 15 16 25 13 --- 7 | 37 37 44 43 47 38 --- 38
R19E | 3079 30 62 51 64 54 57 --- 23 | 47 42 43 84 64 60 --- 49
R20E | 594 35 69 70 61 37 35 --- 23 | 135 130 134 134 135 124 --- 128
R21E | 763 10 27 22 17 17 19 108 8 | 40 33 43 46 46 48 77 40
R22E | 1111 34 33 52 60 40 39 --- 19 | 75 76 80 67 62 79 --- 65
R23E | 491 18 15 18 26 33 15 --- 9 | 112 111 109 108 126 106 --- 110
R24E | 2468 10 32 16 13 25 12 --- 8 | 39 39 39 43 34 36 --- 36
------+----------------------------------------------+------------------------------------------
RMS | 1770 20 34 31 32 29 25 265 |T 52 50 51 56 51 52 104 48
WRMS | 1770 16 34 23 21 22 21 265 |NE 41 39 39 43 39 43 111 36
MEDI | 1008 16 26 22 18 21 19 136 |MD 40 41 43 46 39 48 58 38
Table 3.2131.2 GPS week: 2131 Day: 2 MJD: 59163
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 | 669 27 29 38 23 19 21 --- 12 | 58 38 47 55 62 29 --- 53
R02 | 2395 15 14 17 18 17 19 463 7 | 35 40 49 49 41 32 166 38
R03 | 620 6 10 16 20 17 18 121 6 | 46 45 56 49 46 49 26 46
XR04 | 1273 19 24 22 --- 18 20 --- 10 | 47 46 34 --- 31 29 --- 35
R05 | 711 14 14 16 12 11 20 --- 6 | 42 41 44 40 40 31 --- 37
R07 | 1029 11 11 13 13 27 17 --- 7 | 48 42 51 53 45 48 --- 45
R08M | 600 14 10 13 29 13 17 --- 7 | 48 49 56 71 51 47 --- 51
R09 | 3617 14 12 20 16 19 21 --- 7 | 58 60 57 57 57 54 --- 55
R11 | 584 15 19 12 11 26 22 111 8 | 40 30 36 39 28 44 58 33
R12 | 952 15 39 27 15 16 15 --- 10 | 49 27 35 50 47 44 --- 40
R13 | 4024 29 69 63 71 26 23 --- 21 | 69 40 37 115 65 51 --- 55
R14 | 2454 10 32 20 17 14 32 --- 9 | 49 38 48 49 44 54 --- 43
R15 | 1687 12 24 19 19 14 21 --- 8 | 47 35 36 49 42 58 --- 44
R16 | 569 15 26 27 33 30 26 --- 11 | 27 35 38 32 29 37 --- 23
R17E | 2184 14 29 23 14 17 16 --- 8 | 126 125 116 124 118 124 --- 122
R18E | 745 12 19 15 15 17 14 --- 7 | 37 37 40 44 39 35 --- 36
R19E | 3651 37 64 53 69 41 32 --- 22 | 61 51 46 81 61 48 --- 51
R20E | 544 46 65 59 50 25 32 --- 21 | 104 104 96 103 106 103 --- 97
XR21E | 2211 15 37 --- 14 15 22 127 10 | 39 34 --- 40 38 43 134 37
R22E | 2004 24 22 48 49 50 40 --- 17 | 73 68 65 68 79 55 --- 63
R23E | 699 13 18 21 38 21 23 --- 10 | 101 109 106 105 111 104 --- 104
R24E | 1184 7 27 19 22 20 16 --- 8 | 38 37 31 45 44 37 --- 37
------+----------------------------------------------+------------------------------------------
RMS | 1911 20 33 31 33 24 23 284 |T 56 51 53 62 55 52 96 52
WRMS | 1911 15 30 22 21 19 21 284 |NE 47 39 43 53 44 43 83 42
MEDI | 1029 14 24 20 19 18 21 121 |MD 48 40 47 50 45 47 58 44
Table 3.2131.3 GPS week: 2131 Day: 3 MJD: 59164
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 | 1616 42 33 42 51 13 30 --- 15 | 63 47 62 79 62 39 --- 56
R02 | 1489 10 9 11 9 10 15 169 5 | 38 43 39 49 49 51 155 43
R03 | 1363 14 12 7 13 22 32 74 9 | 43 44 35 37 51 33 62 37
XR04 | 723 12 17 17 --- 13 16 --- 7 | 46 48 36 --- 40 43 --- 41
R05 | 776 20 17 10 22 19 21 --- 8 | 48 44 43 49 36 32 --- 38
R07 | 747 17 13 15 10 12 21 262 7 | 45 50 39 41 37 34 226 38
R08M | 1296 14 8 7 15 6 16 --- 5 | 41 44 42 44 43 40 --- 40
R09 | 3130 17 13 19 18 13 16 --- 7 | 23 34 29 38 24 31 --- 25
R11 | 758 15 21 13 17 12 19 105 7 | 39 22 32 36 27 32 35 29
R12 | 661 18 24 15 9 11 14 --- 7 | 41 24 23 27 29 39 --- 29
R13 | 1569 41 60 53 45 19 26 --- 18 | 75 36 34 76 48 54 --- 44
R14 | 1520 11 27 18 19 11 20 --- 8 | 42 29 44 49 41 53 --- 41
R15 | 1928 25 21 16 12 13 10 --- 7 | 52 32 28 33 29 37 --- 34
R16 | 472 15 17 45 43 17 22 --- 12 | 30 38 50 42 24 43 --- 31
R17E | 1787 13 26 15 19 14 12 --- 7 | 102 108 103 108 103 97 --- 102
R18E | 962 13 21 15 15 15 19 --- 7 | 84 86 84 86 75 80 --- 81
R19E | 3972 56 69 59 69 50 23 --- 24 | 51 54 54 67 34 35 --- 29
R20E | 696 44 63 65 61 25 30 --- 21 | 177 165 179 186 164 170 --- 170
R21E | 1045 19 28 13 22 18 16 278 8 | 32 30 30 36 24 33 200 26
R22E | 1518 24 28 38 60 27 19 --- 15 | 100 107 97 91 92 89 --- 90
R23E | 1180 18 16 34 22 13 23 --- 9 | 130 133 132 134 130 118 --- 128
R24E | 864 6 29 16 20 27 24 --- 9 | 45 42 50 56 42 44 --- 44
------+----------------------------------------------+------------------------------------------
RMS | 1618 25 31 30 33 20 21 195 |T 61 57 57 64 54 55 135 54
WRMS | 1618 18 29 20 17 16 20 195 |NE 45 37 38 46 38 40 119 37
MEDI | 1180 17 21 16 19 13 19 169 |MD 45 44 42 49 41 40 155 40
Table 3.2131.4 GPS week: 2131 Day: 4 MJD: 59165
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 | 787 49 44 47 31 28 29 --- 17 | 48 43 59 50 27 34 --- 36
R02 | 2292 14 13 10 11 13 25 233 7 | 34 40 41 34 45 39 51 37
R03 | 1514 8 11 11 13 10 17 68 5 | 37 36 45 49 43 40 27 40
XR04 | 906 17 26 9 --- 21 26 --- 10 | 45 51 43 --- 34 34 --- 38
R05 | 824 15 22 21 20 18 31 --- 9 | 37 42 43 49 34 39 --- 36
R07 | 771 13 11 10 17 13 17 164 6 | 43 41 48 53 40 48 141 44
R08M | 1004 7 11 14 15 16 16 --- 6 | 36 41 44 36 32 46 --- 38
R09 | 3302 13 12 20 16 19 15 --- 7 | 55 61 63 61 59 58 --- 58
R11 | 636 10 17 8 12 17 27 86 7 | 40 33 39 46 33 39 29 36
R12 | 1085 15 27 16 22 13 16 --- 8 | 47 31 41 56 35 34 --- 38
R13 | 913 43 47 39 28 29 18 --- 15 | 69 40 31 38 51 45 --- 39
R14 | 935 21 25 12 19 27 14 --- 9 | 52 41 47 56 22 43 --- 40
R15 | 1167 23 21 15 14 16 19 --- 8 | 52 40 31 42 31 40 --- 36
R16 | 615 21 32 21 42 14 20 --- 11 | 33 49 48 33 34 45 --- 35
R17E | 2255 16 34 19 20 21 49 --- 12 | 119 112 115 121 113 112 --- 112
R18E | 932 12 39 17 13 21 18 --- 9 | 161 155 171 169 169 167 --- 164
R19E | 2599 52 57 41 73 51 27 --- 23 | 53 48 57 78 51 46 --- 42
R20E | 1417 51 58 60 56 28 38 --- 22 | 112 114 121 110 116 101 --- 106
R21E | 760 12 33 17 30 18 20 185 9 | 44 41 43 61 39 54 93 44
R22E | 1533 24 27 28 47 35 24 --- 14 | 116 108 124 129 111 116 --- 116
R23E | 724 23 30 28 40 29 64 --- 17 | 101 98 97 93 104 98 --- 94
R24E | 604 12 26 16 16 16 14 --- 7 | 38 35 35 32 37 34 --- 33
------+----------------------------------------------+------------------------------------------
RMS | 1462 26 31 26 31 23 28 160 |T 62 59 63 66 57 59 68 57
WRMS | 1462 17 31 18 18 20 28 160 |NE 45 42 44 47 37 41 62 39
MEDI | 932 15 26 17 20 18 20 164 |MD 47 41 45 53 39 45 51 39
Table 3.2131.5 GPS week: 2131 Day: 5 MJD: 59166
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 | 593 41 38 49 30 34 24 --- 16 | 44 36 52 36 29 27 --- 34
R02 | 893 9 12 11 13 11 20 484 5 | 32 33 31 28 34 27 144 29
R03 | 1139 5 12 9 12 9 22 107 5 | 36 32 37 37 28 46 31 34
XR04 | 754 13 20 23 --- 16 13 --- 8 | 40 45 34 --- 37 33 --- 37
R05 | 768 22 24 24 27 11 25 --- 10 | 40 44 47 55 36 34 --- 39
R07 | 694 13 12 9 11 9 25 101 6 | 41 40 42 39 36 29 83 36
R08M | 597 14 11 26 15 12 16 --- 7 | 40 43 59 52 41 50 --- 46
R09 | 3282 13 9 19 15 23 14 --- 7 | 68 71 64 68 66 73 --- 66
R11 | 1502 9 16 11 18 17 29 136 7 | 40 36 36 32 31 52 30 35
R12 | 1414 12 30 16 13 16 20 --- 8 | 43 28 44 44 31 49 --- 37
R13 | 651 20 52 40 54 16 32 --- 16 | 43 28 44 77 36 51 --- 38
R14 | 992 9 20 11 30 13 21 --- 8 | 37 33 38 48 40 40 --- 36
R15 | 668 20 25 13 8 17 16 --- 8 | 44 33 34 32 43 40 --- 36
R16 | 608 21 26 30 41 38 29 --- 14 | 37 40 46 51 62 34 --- 38
R17E | 1798 12 36 27 24 31 57 --- 14 | 122 118 121 120 113 117 --- 115
R18E | 1069 19 28 13 32 36 27 --- 12 | 128 125 130 119 135 124 --- 126
R19E | 1689 34 53 59 81 34 58 --- 24 | 70 75 74 100 62 77 --- 66
R20E | 2239 58 58 51 38 28 36 --- 21 | 167 159 168 167 158 158 --- 160
R21E | 644 15 29 22 12 27 31 150 10 | 61 59 54 58 63 57 87 57
R22E | 1607 16 17 20 37 32 39 --- 12 | 170 175 170 165 162 189 --- 170
R23E | 693 23 17 32 33 21 24 --- 11 | 132 141 137 143 136 125 --- 133
R24E | 628 20 26 14 13 14 24 --- 8 | 61 62 56 58 60 57 --- 57
------+----------------------------------------------+------------------------------------------
RMS | 1332 23 30 28 31 23 30 244 |T 68 66 69 72 65 67 75 64
WRMS | 1332 16 30 20 16 20 28 244 |NE 41 38 42 45 39 41 72 38
MEDI | 768 15 24 20 24 17 24 136 |MD 43 43 47 55 41 50 83 38
Table 3.2131.6 GPS week: 2131 Day: 6 MJD: 59167
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 | 584 21 26 29 33 30 14 --- 12 | 70 54 62 55 50 38 --- 56
R02 | 1939 14 8 17 12 10 20 --- 6 | 38 48 53 48 45 42 --- 44
R03 | 548 10 12 11 14 10 30 132 6 | 47 48 49 44 47 37 46 43
XR04 | 541 19 20 26 --- 13 34 --- 11 | 51 58 35 --- 42 47 --- 44
R05 | 862 23 18 30 16 22 33 --- 10 | 44 49 53 54 60 38 --- 46
R07 | 803 8 11 10 7 18 45 52 8 | 53 53 57 54 59 45 72 51
R08M | 1679 10 11 15 17 21 17 --- 7 | 43 48 56 53 49 45 --- 48
R09 | 3562 13 20 20 12 27 23 --- 8 | 78 88 79 82 78 84 --- 79
R11 | 1591 14 10 15 10 20 14 195 6 | 52 38 47 45 31 41 39 41
R12 | 1394 26 21 18 16 11 24 --- 9 | 53 28 37 45 29 43 --- 36
R13 | 1014 33 39 34 31 18 39 --- 14 | 72 36 40 69 49 58 --- 48
R14 | 739 14 28 15 24 10 22 --- 8 | 51 40 55 67 51 51 --- 50
R15 | 824 20 26 18 23 17 18 --- 9 | 60 31 35 54 38 55 --- 44
R16 | 797 13 27 27 26 17 20 --- 10 | 43 41 65 51 46 41 --- 45
R17E | 1606 13 34 23 15 14 57 --- 12 | 103 99 100 105 100 116 --- 101
R18E | 1663 16 30 17 20 26 40 --- 11 | 103 101 112 105 112 116 --- 106
R19E | 1269 33 83 66 77 50 48 --- 27 | 118 117 134 139 126 126 --- 119
R20E | 2796 56 61 57 43 44 33 --- 22 | 149 157 160 159 146 142 --- 147
R21E | 564 23 21 14 12 18 14 141 8 | 54 47 48 59 52 58 96 51
R22E | 1543 19 28 18 29 44 27 --- 13 | 136 132 126 137 130 135 --- 131
R23E | 1552 29 23 20 53 18 50 --- 15 | 129 130 129 132 139 132 --- 129
R24E | 610 17 34 19 23 22 24 --- 10 | 60 56 54 60 61 55 --- 55
------+----------------------------------------------+------------------------------------------
RMS | 1526 23 32 27 29 25 32 140 |T 73 68 72 77 70 70 63 68
WRMS | 1526 17 24 19 15 18 31 140 |NE 54 47 51 55 48 47 52 48
MEDI | 1014 17 23 18 20 18 24 132 |MD 54 49 55 59 51 51 46 50
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