[IGSREPORT-27641] Wk 2133 IGLOS Final Orbits
acc
acc at igs.org
Mon Dec 14 01:15:23 UTC 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2133 (Nov 22, 2020 - Nov 28, 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 2.2133.
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:
igl2133[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2133 in the SP3 format.
igl21337.sum Combination Report for GPS Week 2133.
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 | 1.3 ns
1 | -0.4 ns
2 | 1.6 ns
3 | -0.4 ns
4 | 0.0 ns
5 | 1.0 ns
6 | 0.5 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
----+--------+---------------
3 | GFZ | R23
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 1.2133, 1a.2133).
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 2.2133.0-6)
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 3.2133.0-6).
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 2133 summary. (Nov 22, 2020 - Nov 28, 2020)
Table 1.2133.a GPS week : 2133 MJD: 59175.0-59181.0
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 -12 3 21 .06 25 21 | 18087 194 3004 7792
| 0 1 1 19 17 24 .03 | 661 1433
emx n/a| 0 0 -8 -29 29 -52 .10 36 36 | -6161 117 2995 7947
| 1 0 4 26 17 42 .07 | 10709 960
esx n/a| 0 2 -1 28 -31 -38 -.06 32 24 | 1475 -810 2996 10213
| 3 2 1 15 15 32 .05 | 9464 1422
gfz n/a| 0 0 0 -12 -15 -62 -.02 29 17 | 0 471 3033 7664
| 0 1 2 11 13 29 .05 | 0 1552
iac n/a| 0 0 2 13 15 112 -.02 25 22 | 2257 83 2996 8101
| 2 3 3 13 14 49 .08 | 854 1379
Table 1.2133.b GPS week : 2133 MJD: 59175.0-59181.0
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 | 15 18 17 18 20 20 16 |
R02 | 7 6 7 11 8 5 7 |
R03 | 8 8 7 9 8 7 7 |
R04 | 11 11 12 12 13 13 7 |
R05 | 9 10 13 14 8 9 10 |
R07 | 8 8 7 9 7 8 6 |
R08 | 11 8 9 8 10 9 10 |
R09 | 8 7 8 10 8 7 7 |
R12 | 12 11 10 11 10 10 10 |
R13 | 16 15 18 25 17 17 18 |
R14 | 9 9 9 11 9 9 7 |
R15 | 10 10 11 10 9 9 12 |
R16 | 14 18 12 10 14 15 13 |
R17 | 9 8 10 11 13 11 9 |
R18 | 10 9 6 7 10 7 10 |
R19 | 35 34 28 27 33 36 32 |
R20 | 24 26 30 33 31 31 31 |
R21 | 11 9 9 11 13 9 12 |
R22 | 10 15 19 22 16 11 15 |
R23 | 12 13 13 23 --- --- --- |
R24 | 11 11 11 10 10 10 11 |
R25 | 40 39 44 44 31 --- --- |
Table 1.2133.c GPS week : 2133 MJD: 59175.0-59181.0
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 2133 0 | -38 -4 28 805 -2258 2424 83.3 1468 1468 | 1300 0
brd 2133 1 | 24 0 65 -325 -1653 -1570 82.3 1513 1513 | -443 0
brd 2133 2 | 68 33 105 -1091 537 -1265 84.0 1593 1593 | 1606 0
brd 2133 3 | 36 2 -39 -227 1069 -2823 83.0 2005 2005 | -431 0
brd 2133 4 | -20 34 -38 -992 832 -4436 82.5 14760 14760 | 35 0
brd 2133 5 | -12 15 43 -723 1487 -5548 80.5 1861 1861 | 1047 0
brd 2133 6 | 6 48 39 -238 1027 -3259 81.1 1513 1513 | 544 0
-------------+------------------------------------------------------------+----------------
brd 2133 mean| 9 18 29 -398 148 -2353 82.4 3530 3530 | 522 0
brd 2133 sdev| 37 20 52 638 1475 2588 1.2 4955 4955 | 829 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 2.2133.0 GPS week: 2133 Day: 0 MJD: 59175
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 9 7 13 .11 25 23 | 17307 2859 3277 8223
emx n/a| 0 0 -14 -82 -3 -107 .15 33 33 | 4078 1724 3258 8428
esx n/a| 2 3 0 12 -23 -79 -.07 30 24 | 9927 1265 3264 10643
gfz n/a| 0 0 3 -26 -19 -91 -.03 30 16 | 0 2230 3298 8159
iac n/a| -1 1 5 33 20 207 -.05 21 18 | 1880 2183 3265 8641
Table 2.2133.1 GPS week: 2133 Day: 1 MJD: 59176
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 2 -4 -15 -6 .09 26 21 | 17900 -1642 2813 8096
emx n/a| -1 0 -12 -29 37 -10 .09 33 33 | -23668 -969 2801 8367
esx n/a| 0 1 1 34 -4 5 -.08 30 22 | 15302 -2704 2808 10201
gfz n/a| 0 -1 0 -17 -20 -32 -.01 29 17 | 0 -1855 2835 8025
iac n/a| 2 -1 6 21 -5 52 .02 23 20 | 1554 -768 2804 8429
Table 2.2133.2 GPS week: 2133 Day: 2 MJD: 59177
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 -3 2 16 .05 26 23 | 18042 869 2685 6996
emx n/a| 2 0 -8 -30 42 0 .15 36 36 | -10750 334 2680 7089
esx n/a| -5 5 0 46 -23 -56 -.02 33 21 | -5428 502 2677 9228
gfz n/a| 0 0 1 -25 1 -63 .05 27 16 | 0 2237 2712 6830
iac n/a| 3 -3 4 9 15 88 -.16 21 18 | 2821 612 2680 7139
Table 2.2133.3 GPS week: 2133 Day: 3 MJD: 59178
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 5 -30 7 0 .05 21 17 | 18792 -594 3322 8321
emx n/a| 2 0 -6 5 16 -48 .12 37 37 | -5250 -783 3319 8448
esx n/a| -3 1 -2 39 -46 4 -.09 36 25 | -13444 -2065 3314 10863
gfz n/a| -1 0 1 -2 5 -17 -.08 33 17 | 0 -591 3370 8266
iac n/a| 2 -4 0 21 7 125 -.04 35 33 | 2836 -1916 3314 8487
Table 2.2133.4 GPS week: 2133 Day: 4 MJD: 59179
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 4 6 -3 27 .07 25 26 | 17215 -667 2934 7938
emx n/a| 1 0 -5 -14 43 -92 .17 38 38 | 4515 -516 2934 8031
esx n/a| -1 1 -2 4 -30 -33 -.07 31 28 | 364 -1597 2911 10475
gfz n/a| -1 -3 -2 -5 -20 -98 -.08 33 20 | 0 -400 2973 7710
iac n/a| 1 3 1 -7 10 92 -.04 25 22 | 811 1159 2908 8261
Table 2.2133.5 GPS week: 2133 Day: 5 MJD: 59180
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 -25 -13 68 .06 24 19 | 18794 163 2946 7320
emx n/a| 0 0 -4 -24 40 -81 .06 41 41 | -14422 195 2921 7419
esx n/a| 0 1 -3 23 -48 -55 .01 33 27 | 3070 -236 2941 9588
gfz n/a| 0 -1 0 4 -32 -77 -.05 29 16 | 0 1425 2940 7259
iac n/a| 0 1 1 6 39 94 .04 22 19 | 3080 146 2949 7685
Table 2.2133.6 GPS week: 2133 Day: 6 MJD: 59181
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 3 -40 36 28 .01 26 20 | 18559 372 3054 7655
emx n/a| 0 0 -4 -31 29 -28 -.02 35 35 | 2368 834 3058 7851
esx n/a| 2 -1 -2 37 -40 -52 -.13 29 25 | 538 -841 3058 10498
gfz n/a| 0 0 2 -11 -23 -53 .05 25 15 | 0 251 3105 7401
iac n/a| -2 3 -2 6 21 130 .08 29 25 | 2822 -834 3057 8067
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 3.2133.0 GPS week: 2133 Day: 0 MJD: 59175
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz iac IGL | cod emx esx gfz iac IGL
------+------------------------------------+--------------------------------
R01 | 1012 38 27 26 29 27 15 | 80 82 45 52 44 57
R02 | 1594 9 9 16 15 13 6 | 44 47 32 38 45 40
R03 | 670 9 11 11 18 19 7 | 53 54 46 45 52 49
XR04 | 1691 18 11 21 --- 21 10 | 52 53 41 --- 39 44
R05 | 600 20 16 20 18 17 9 | 42 46 48 38 45 40
R07 | 814 15 17 13 15 15 7 | 57 60 64 56 64 58
R08 | 1286 20 17 32 16 21 11 | 49 53 69 54 50 53
R09E | 3056 17 19 13 15 18 8 | 105 106 115 111 112 109
R12E | 2543 17 39 25 20 14 11 | 81 70 80 84 82 78
R13E | 710 22 34 30 34 34 15 | 47 40 63 62 51 46
R14E | 920 20 24 19 17 11 9 | 94 93 103 99 104 98
R15E | 1677 18 31 11 16 18 9 | 50 55 48 58 57 52
R16E | 1591 21 31 28 40 20 14 | 39 40 58 44 47 38
R17 | 1429 19 26 21 11 11 9 | 63 42 44 59 64 54
R18 | 825 11 29 16 12 24 9 | 45 38 51 46 65 47
R19 | 2069 59 86 75 95 28 35 | 82 43 52 111 79 60
R20 | 1855 47 57 66 28 37 24 | 96 51 43 83 76 61
R21 | 592 19 29 23 15 22 11 | 68 44 45 58 66 56
R22 | 1393 15 22 16 28 15 10 | 49 44 67 60 58 53
R23 | 939 18 22 36 26 10 11 | 43 37 30 9999 48 39
R24 | 509 29 34 17 14 14 11 | 72 52 51 59 65 58
XR25E | ---- 40 --- --- --- 39 39 | 133 --- --- --- 129 134
------+------------------------------------+--------------------------------
RMS | 1467 25 33 30 30 21 |T 65 54 56 64 65 60
WRMS | 1467 23 33 24 16 18 |NE 59 49 48 58 57 51
MEDI | 1286 19 26 21 17 18 |MD 53 51 51 58 58 53
Table 3.2133.1 GPS week: 2133 Day: 1 MJD: 59176
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz iac IGL | cod emx esx gfz iac IGL
------+------------------------------------+--------------------------------
R01 | 959 44 39 31 35 24 17 | 52 46 40 39 28 36
R02 | 1038 10 9 12 8 15 5 | 32 33 25 29 25 26
R03 | 669 7 10 12 12 24 7 | 37 40 34 36 43 36
XR04 | 2389 21 12 25 --- 10 10 | 38 35 31 --- 30 30
R05 | 654 21 23 15 17 17 9 | 27 36 35 35 30 27
R07 | 771 17 14 11 19 13 7 | 41 44 47 37 41 40
R08 | 2536 13 21 18 12 14 8 | 36 37 40 35 39 36
R09E | 4196 14 14 7 14 18 7 | 77 84 82 88 73 80
R12E | 2406 16 34 20 18 20 11 | 67 64 70 68 60 64
R13E | 605 20 43 25 26 32 15 | 43 39 45 56 41 39
R14E | 1170 16 26 20 11 9 8 | 67 71 68 67 67 66
R15E | 1217 11 29 12 24 12 9 | 49 45 50 59 47 48
R16E | 1146 20 24 26 58 33 17 | 39 40 52 75 40 40
R17 | 1457 17 23 13 18 9 8 | 42 36 38 44 37 38
R18 | 830 11 23 23 9 22 9 | 30 26 39 26 42 31
R19 | 1493 67 78 79 70 46 34 | 47 45 58 60 44 34
R20 | 987 46 55 70 55 33 26 | 51 34 38 64 36 39
R21 | 565 20 25 12 13 18 9 | 42 39 37 42 36 38
R22 | 748 30 38 19 27 28 14 | 43 39 41 40 48 36
R23 | 630 18 16 37 21 27 12 | 35 36 34 9999 25 29
R24 | 800 24 31 18 18 18 11 | 45 48 36 46 43 40
XR25E | ---- 38 --- --- --- 39 39 | 70 --- --- --- 63 70
------+------------------------------------+--------------------------------
RMS | 1512 26 33 30 29 23 |T 45 43 44 49 42 41
WRMS | 1512 21 33 22 17 20 |NE 39 38 38 41 36 34
MEDI | 987 18 24 19 18 18 |MD 42 39 40 44 41 38
Table 3.2133.2 GPS week: 2133 Day: 2 MJD: 59177
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz iac IGL | cod emx esx gfz iac IGL
------+------------------------------------+--------------------------------
R01 | 999 46 39 34 27 18 16 | 63 64 35 43 42 46
R02 | 923 15 14 13 14 12 7 | 38 43 39 36 47 37
R03 | 665 11 10 15 15 17 7 | 45 45 51 44 48 45
XR04 | 671 21 13 17 --- 26 12 | 50 44 40 --- 33 37
R05 | 1010 29 30 33 23 10 12 | 41 48 42 40 30 32
R07 | 597 13 13 12 16 14 7 | 48 49 52 58 52 51
R08 | 925 18 20 16 13 22 9 | 45 46 53 43 48 45
R09E | 4543 18 18 12 16 14 8 | 63 68 61 59 63 61
R12E | 2046 17 34 16 13 19 10 | 58 47 51 56 59 53
R13E | 774 29 49 29 42 33 18 | 54 49 59 70 41 47
R14E | 2496 17 27 21 15 10 9 | 68 65 71 71 75 69
R15E | 1081 12 33 22 21 16 10 | 61 58 53 62 57 56
R16E | 1199 21 29 24 25 17 11 | 37 39 55 60 41 42
R17 | 2269 19 26 22 16 16 9 | 49 43 36 49 43 42
R18 | 501 10 14 18 11 9 6 | 30 36 38 28 40 33
R19 | 1009 47 78 68 51 36 27 | 53 58 47 74 52 47
R20 | 720 51 76 84 47 36 29 | 81 47 45 80 70 57
R21 | 486 19 26 16 10 18 9 | 54 40 45 48 53 47
R22 | 1152 34 36 38 53 27 19 | 45 36 61 41 50 38
R23 | 588 25 15 31 19 29 12 | 28 28 21 9999 40 29
R24 | 1768 22 33 21 14 20 11 | 62 50 52 56 55 53
XR25E | ---- 48 --- --- --- 40 44 | 55 --- --- --- 68 65
------+------------------------------------+--------------------------------
RMS | 1593 26 36 33 27 21 |T 51 47 47 53 50 46
WRMS | 1593 23 36 21 16 18 |NE 48 45 43 49 46 42
MEDI | 999 19 27 21 16 18 |MD 50 47 51 56 48 46
Table 3.2133.3 GPS week: 2133 Day: 3 MJD: 59178
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz iac IGL | cod emx esx gfz iac IGL
------+------------------------------------+--------------------------------
R01 | 706 38 28 33 36 37 17 | 77 75 63 67 58 66
R02 | 1000 11 13 24 13 43 10 | 41 41 53 35 39 36
R03 | 803 8 10 19 19 28 8 | 44 43 53 43 44 43
XR04 | 578 12 11 15 --- 40 11 | 50 50 57 --- 37 49
R05 | 667 15 17 19 28 52 13 | 45 47 35 38 72 40
R07 | 676 8 15 14 10 37 8 | 48 46 53 58 77 53
R08 | 689 11 10 22 17 18 8 | 44 50 58 57 47 49
R09E | 4849 11 13 24 12 40 10 | 33 39 50 44 45 36
R12E | 1368 14 31 20 17 24 10 | 40 24 37 42 42 34
R13E | 2732 18 71 42 75 36 25 | 49 37 48 121 64 56
R14E | 4287 11 29 22 17 35 11 | 34 31 52 48 49 39
R15E | 1724 9 31 15 17 27 10 | 39 27 37 51 55 39
R16E | 1502 12 20 22 23 25 10 | 31 33 41 33 24 27
R17 | 2912 15 28 29 19 21 11 | 44 22 26 47 44 36
R18 | 662 9 12 18 16 16 7 | 28 24 40 33 38 30
R19 | 1427 28 81 50 57 60 27 | 45 70 29 66 59 38
R20 | 743 47 77 101 56 50 33 | 77 36 46 73 81 48
R21 | 570 14 34 22 10 29 11 | 49 23 33 41 52 38
R22 | 923 42 27 51 55 31 21 | 36 52 78 54 34 44
XR23 | 565 14 --- --- 316 35 22 | 45 --- --- 9999 39 48
R24 | 1936 15 28 17 12 26 9 | 34 31 27 33 47 31
XR25E |13153 26 --- --- --- 69 43 | 64 --- --- --- 85 60
------+------------------------------------+--------------------------------
RMS | 2005 21 37 36 33 35 |T 45 40 45 51 51 42
WRMS | 2005 17 37 25 17 33 |NE 47 43 46 49 51 43
MEDI | 923 14 27 22 17 35 |MD 44 37 46 47 47 39
Table 3.2133.4 GPS week: 2133 Day: 4 MJD: 59179
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz iac IGL | cod emx esx gfz iac IGL
------+------------------------------------+--------------------------------
R01 | 1030 52 37 41 22 37 20 | 75 72 60 63 52 61
R02 | 1209 18 8 15 17 16 8 | 41 47 46 53 51 45
R03 |63698 11 11 15 17 21 8 | 50 52 57 67 40 50
XR04 | 883 13 14 21 --- 33 13 | 49 51 57 --- 36 45
R05 | 519 15 21 13 18 14 8 | 49 45 55 69 64 54
R07 | 1250 9 12 11 18 14 6 | 46 48 50 41 47 45
R08 | 578 20 15 24 20 19 10 | 42 45 46 60 56 47
R09E | 4319 14 19 9 16 17 7 | 66 71 69 71 71 67
R12E | 785 15 29 19 18 16 9 | 56 48 58 65 63 56
R13E | 3178 20 43 35 37 33 16 | 55 43 49 81 51 51
R14E | 4938 16 27 16 15 11 8 | 62 61 68 66 67 64
R15E | 2102 14 30 12 14 15 8 | 57 56 56 62 67 58
R16E | 1249 13 28 26 38 29 13 | 41 34 52 52 51 40
R17 | 3032 11 33 30 22 28 12 | 46 33 36 52 55 42
R18 | 930 11 21 12 29 23 10 | 30 25 29 46 31 28
R19 | 2268 22 98 65 87 55 33 | 41 54 37 85 62 35
R20 | 583 64 78 79 54 24 31 | 78 36 39 60 41 38
R21 | 737 20 29 20 24 31 12 | 45 34 36 38 57 40
R22 | 701 34 28 33 43 17 16 | 43 43 67 60 52 49
R24 | 1294 15 34 12 21 12 9 | 52 44 42 50 51 46
XR25E |23421 16 --- --- --- 42 31 | 88 --- --- --- 141 87
------+------------------------------------+--------------------------------
RMS |14761 25 38 31 33 25 |T 52 47 50 60 57 49
WRMS |14761 26 38 28 20 22 |NE 49 44 46 57 49 44
MEDI | 1249 15 28 19 21 21 |MD 49 45 50 60 52 47
Table 3.2133.5 GPS week: 2133 Day: 5 MJD: 59180
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz iac IGL | cod emx esx gfz iac IGL
------+------------------------------------+--------------------------------
R01 | 992 53 26 40 42 21 19 | 55 45 50 60 44 45
R02 | 1165 6 9 13 10 10 5 | 28 38 30 39 32 31
R03 | 781 11 9 12 14 16 6 | 37 37 34 34 39 34
XR04 | 661 22 23 17 --- 26 13 | 35 38 26 --- 27 27
R05 | 542 14 18 16 21 18 8 | 36 32 50 49 44 39
R07 | 1601 4 11 19 16 22 8 | 42 43 36 37 57 42
R08 | 654 23 9 19 19 16 9 | 32 40 44 48 35 38
R09E | 4254 15 13 8 11 14 6 | 71 76 74 73 73 72
R12E | 677 12 26 20 21 23 10 | 60 58 61 64 67 60
R13E | 1879 26 35 31 34 39 16 | 45 32 51 57 51 41
R14E | 4574 10 28 16 9 19 8 | 74 72 77 75 72 73
R15E | 1799 16 30 15 14 14 9 | 53 50 52 56 58 52
R16E | 703 14 35 26 48 24 15 | 36 41 53 57 51 40
R17 | 1875 15 26 26 16 21 10 | 42 47 38 45 50 42
R18 | 754 12 20 13 12 10 6 | 28 29 30 34 31 29
R19 | 2364 38 129 72 62 52 35 | 52 54 36 64 56 35
R20 | 649 55 75 89 60 19 31 | 70 33 34 72 50 43
R21 | 929 21 21 20 12 15 9 | 43 34 32 34 40 36
R22 | 948 21 26 22 21 16 10 | 43 42 51 51 43 42
R24 | 963 14 38 17 18 16 10 | 49 56 49 53 45 48
------+------------------------------------+--------------------------------
RMS | 1860 24 41 33 29 22 |T 46 44 45 52 48 43
WRMS | 1860 19 41 27 16 19 |NE 42 40 38 47 42 37
MEDI | 948 15 26 19 18 18 |MD 43 41 44 53 45 41
Table 3.2133.6 GPS week: 2133 Day: 6 MJD: 59181
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz iac IGL | cod emx esx gfz iac IGL
------+------------------------------------+--------------------------------
R01 | 855 39 17 41 25 28 16 | 83 72 58 63 73 65
R02 | 1039 7 10 12 10 23 6 | 44 51 44 45 57 46
R03 | 552 6 12 18 13 16 6 | 53 58 50 48 54 50
XR04 | 635 9 14 14 --- 11 7 | 52 57 45 --- 48 48
R05 | 887 20 18 13 18 23 9 | 51 42 56 56 58 50
R07 | 1751 9 14 10 12 17 6 | 63 61 68 65 77 66
R08 | 644 25 16 19 19 18 10 | 56 60 74 70 66 64
R09E | 3174 14 13 10 13 19 7 | 100 106 107 105 107 105
R12E | 964 10 25 16 13 28 9 | 87 76 83 90 90 85
R13E | 1320 33 37 20 38 47 18 | 56 48 57 79 61 55
R14E | 3024 10 19 8 10 21 7 | 97 92 95 100 99 96
R15E | 1519 15 36 15 20 28 11 | 63 60 65 72 67 64
R16E | 880 19 28 18 23 35 12 | 46 41 51 58 79 52
R17 | 1631 11 25 19 12 20 8 | 57 46 46 56 58 51
R18 | 798 14 22 16 17 25 9 | 36 28 43 34 49 35
R19 | 2262 51 94 65 57 51 32 | 81 46 37 98 78 53
R20 | 930 61 75 77 46 37 30 | 85 40 40 74 71 47
R21 | 647 17 25 26 24 27 12 | 59 34 34 62 53 47
R22 | 1187 25 23 27 30 37 14 | 54 44 58 48 48 47
R24 | 1000 29 29 15 16 19 11 | 74 60 59 63 64 62
------+------------------------------------+--------------------------------
RMS | 1512 26 35 29 25 29 |T 64 56 58 67 67 59
WRMS | 1512 20 35 25 15 25 |NE 60 49 50 60 61 52
MEDI | 964 15 22 16 18 23 |MD 57 51 56 63 64 52
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