[IGSREPORT-27071] Wk 2089 IGLOS Final Orbits
acc
acc at igs.org
Thu Feb 6 18:48:23 PST 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2089 (Jan 19, 2020 - Jan 25, 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 2.2089.
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:
igl2089[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2089 in the SP3 format.
igl20897.sum Combination Report for GPS Week 2089.
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 | -11.5 ns
1 | -0.4 ns
2 | -0.1 ns
3 | 0.0 ns
4 | 0.3 ns
5 | -0.5 ns
6 | -1.1 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
----+--------+---------------
6 | GFZ | R08
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 1.2089, 1a.2089).
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 2.2089.0-6)
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 3.2089.0-6).
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 2089 summary. (Jan 19, 2020 - Jan 25, 2020)
Table 1.2089.a GPS week : 2089 MJD: 58867.0-58873.0
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 -7 19 -14 54 .09 31 26 | 22742 -962 2883 7818
| 1 2 1 23 19 26 .03 | 4848 1307
cof n/a| -1 0 -9 9 3 57 .10 32 27 | 22737 -962 2885 7820
| 1 0 2 16 26 23 .03 | 4851 1310
emx n/a| 0 -1 5 48 22 -10 .09 26 26 | -2859 -495 2876 7961
| 0 1 0 19 26 40 .04 | 12996 847
esx n/a| 0 0 1 0 -21 -3 .15 26 22 | -2180 -456 2882 10079
| 1 1 1 19 10 41 .04 | 9027 1652
gfz n/a| 0 -1 -4 1 -11 -10 .17 26 21 | 0 -587 2930 7582
| 1 1 1 16 22 30 .04 | 0 1042
grg n/a| 0 2 1 -67 0 -57 -.36 31 27 | -1556 -556 2885 7080
| 1 0 4 11 16 64 .04 | 4715 1238
iac n/a| -1 0 5 19 31 14 -.28 31 28 | -389 -336 2877 8053
| 2 1 2 20 32 126 .05 | 4280 836
mcc n/a| 2 7 -32 90 52 112 -.45 214 214 | --- --- --- ---
| 3 8 11 94 109 678 .51 | --- ---
Table 1.2089.b GPS week : 2089 MJD: 58867.0-58873.0
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 21 21 19 20 22 20 |
R02 | 7 7 8 6 6 6 8 |
R03 | 10 11 12 10 11 9 10 |
R04 | 13 11 12 11 11 11 12 |
R05 | 11 10 10 9 9 9 9 |
R07 | 11 10 12 11 9 9 12 |
R08 | 9 10 8 8 9 9 54 |
R09 | 10 11 12 12 9 8 10 |
R11 | 6 8 8 7 7 7 5 |
R12 | 13 12 12 10 10 11 10 |
R13 | 16 21 19 15 16 15 15 |
R14 | 8 7 9 9 9 8 9 |
R15 | 8 8 8 9 10 11 10 |
R16 | 12 11 11 10 13 11 11 |
R17 | 11 9 9 10 11 8 8 |
R18 | 6 5 6 8 9 9 8 |
R19 | 28 29 27 26 25 22 26 |
R20 | 18 23 20 18 18 16 22 |
R21 | 12 11 12 11 13 12 9 |
R22 | 9 11 11 12 11 12 12 |
R23 | 11 7 9 10 9 8 10 |
R26 | 17 12 18 15 17 18 17 |
Table 1.2089.c GPS week : 2089 MJD: 58867.0-58873.0
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 2089 0 | 8 -25 136 264 -899 690 81.4 1578 1578 | -11471 0
brd 2089 1 | 41 62 116 -377 457 1297 82.4 1199 1199 | -376 0
brd 2089 2 | -63 -40 105 929 316 -248 81.8 1357 1357 | -52 0
brd 2089 3 | 35 27 169 -115 -1101 -2888 81.2 1306 1306 | 17 0
brd 2089 4 | -39 111 82 -1549 -272 -2109 81.1 1287 1287 | 261 0
brd 2089 5 | 0 -73 88 333 495 -2841 82.2 1425 1425 | -497 0
brd 2089 6 | -3 0 89 -85 -560 -394 83.2 1501 1501 | -1067 0
-------------+------------------------------------------------------------+----------------
brd 2089 mean| -3 9 112 -85 -223 -927 81.9 1379 1379 | -1883 0
brd 2089 sdev| 37 63 31 769 660 1693 .7 131 131 | 4249 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 2.2089.0 GPS week: 2089 Day: 0 MJD: 58867
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 -6 7 26 55 .09 34 26 | 11896 948 3122 7884
cof n/a| -3 0 -9 -11 2 78 .11 37 28 | 11885 961 3125 7887
emx n/a| 2 -2 5 49 13 4 .10 27 27 | -26137 621 3121 7975
esx n/a| 0 0 2 -17 -15 8 .13 24 20 | -13819 2636 3127 10148
gfz n/a| -2 -1 -4 9 -19 -24 .21 29 24 | 0 1231 3206 7538
grg n/a| 0 1 0 -48 2 -106 -.37 30 24 | -12237 1551 3127 7257
iac n/a| 0 1 6 3 34 14 -.33 27 25 | -9808 285 3119 8048
mcc n/a| 2 -8 -17 84 -91 -197 -1.17 185 185 | --- --- --- ---
Table 2.2089.1 GPS week: 2089 Day: 1 MJD: 58868
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 -6 -15 -10 16 .09 31 27 | 24676 -1704 2806 7456
cof n/a| -2 0 -11 9 -9 18 .13 34 29 | 24678 -1712 2808 7453
emx n/a| 1 -2 4 69 27 56 .04 27 27 | 11771 -1205 2810 7730
esx n/a| 0 0 0 29 -22 -9 .11 28 22 | -4118 -1779 2814 9604
gfz n/a| -1 0 -4 -18 -34 -38 .17 31 29 | 0 -1168 2863 7150
grg n/a| 0 2 2 -67 -14 -110 -.37 33 35 | 360 -1451 2805 6529
iac n/a| -4 0 5 36 50 62 -.28 31 27 | 1855 -1348 2808 7760
mcc n/a| 7 1 -35 -4 105 43 -.06 128 128 | --- --- --- ---
Table 2.2089.2 GPS week: 2089 Day: 2 MJD: 58869
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 1 -8 14 -20 59 .04 29 23 | 25014 -1313 2562 7125
cof n/a| -2 -1 -12 2 3 46 .09 31 24 | 25012 -1322 2558 7131
emx n/a| 0 -2 5 49 46 -53 .03 28 28 | 2796 -638 2553 7231
esx n/a| 0 0 2 2 -19 -6 .21 29 23 | 7202 -663 2568 9521
gfz n/a| 0 0 -7 -20 -35 42 .15 28 19 | 0 -1206 2611 6625
grg n/a| 1 3 8 -84 -13 -141 -.32 29 26 | 214 -472 2575 6117
iac n/a| -2 0 5 34 23 132 -.25 34 30 | 2405 -1403 2565 7413
mcc n/a| 6 4 -32 168 214 314 .03 143 143 | --- --- --- ---
Table 2.2089.3 GPS week: 2089 Day: 3 MJD: 58870
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 -10 28 -26 83 .13 30 26 | 25028 -1621 2848 8237
cof n/a| -1 0 -11 16 -13 77 .10 31 27 | 25025 -1622 2851 8237
emx n/a| 0 0 5 20 39 -2 .11 24 24 | -1892 -831 2836 8413
esx n/a| 0 2 1 9 -29 -35 .17 27 23 | -11910 -318 2837 10891
gfz n/a| 1 -3 -4 0 6 -38 .11 25 23 | 0 -609 2878 8224
grg n/a| -2 2 8 -78 3 -14 -.43 29 24 | 626 -1086 2837 7442
iac n/a| -3 -1 5 50 0 -43 -.20 30 27 | -686 786 2825 8604
mcc n/a| 2 9 -41 115 -45 465 -.46 183 183 | --- --- --- ---
Table 2.2089.4 GPS week: 2089 Day: 4 MJD: 58871
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 -6 24 -27 19 .09 30 24 | 23870 880 2734 7608
cof n/a| 0 0 -11 -3 7 72 .14 31 26 | 23867 873 2738 7610
emx n/a| 0 -1 4 77 -27 7 .13 25 25 | -12616 774 2725 7683
esx n/a| -2 1 0 9 -5 46 .18 27 26 | -5806 25 2731 9932
gfz n/a| 0 -1 -4 1 3 19 .24 25 19 | 0 319 2746 7447
grg n/a| 1 3 0 -66 -12 -4 -.39 28 27 | 50 666 2744 7267
iac n/a| 0 -1 9 0 74 -154 -.30 32 28 | 1782 81 2731 7742
mcc n/a| -3 12 -43 -56 32 1336 -1.07 264 264 | --- --- --- ---
Table 2.2089.5 GPS week: 2089 Day: 5 MJD: 58872
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 2 -5 62 -25 75 .11 30 26 | 25545 -1725 3224 8553
cof n/a| 1 -1 -4 37 -23 39 .07 31 25 | 25534 -1708 3220 8553
emx n/a| 0 0 7 36 15 -59 .10 25 25 | 8509 -869 3210 8818
esx n/a| 0 0 1 -26 -37 -70 .09 24 20 | 6664 -458 3214 10611
gfz n/a| 0 -1 -2 21 -24 -20 .15 19 14 | 0 -817 3267 8520
grg n/a| 0 0 0 -63 10 -53 -.33 32 27 | 172 -1232 3232 7859
iac n/a| -2 1 1 1 56 197 -.25 29 28 | 1342 -706 3213 8790
mcc n/a| 4 18 -40 215 148 -668 -.50 292 292 | --- --- --- ---
Table 2.2089.6 GPS week: 2089 Day: 6 MJD: 58873
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 -2 -6 12 -16 72 .08 30 26 | 23165 -2199 2891 7869
cof n/a| -3 0 -8 17 57 70 .05 32 26 | 23163 -2208 2896 7872
emx n/a| 0 0 6 36 45 -26 .10 27 27 | -2445 -1318 2881 7877
esx n/a| -1 2 4 -11 -20 42 .13 25 18 | 6521 -2641 2887 9846
gfz n/a| 2 -2 -4 19 22 -10 .18 26 16 | 0 -1859 2940 7570
grg n/a| 1 1 -4 -61 30 31 -.31 33 23 | -80 -1872 2875 7092
iac n/a| 2 3 6 9 -15 -106 -.33 30 29 | 383 -50 2882 8020
mcc n/a| 0 12 -13 112 1 -508 .05 303 303 | --- --- --- ---
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 3.2089.0 GPS week: 2089 Day: 0 MJD: 58867
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | 835 85 92 42 42 27 43 35 --- 21 | 115 118 43 46 69 64 39 --- 53
R02M | 1180 24 23 15 9 10 14 12 177 6 | 76 81 49 62 68 51 60 137 60
R03 | 567 28 30 22 17 22 19 26 81 10 | 96 95 64 57 89 82 49 83 71
XR04 | 1238 43 47 27 9 --- 23 25 --- 13 | 99 100 63 56 --- 54 47 --- 62
R05 | 818 25 20 22 20 33 18 27 --- 11 | 78 79 48 65 89 68 54 --- 65
R07M | 1179 24 29 19 21 21 29 24 152 10 | 88 91 55 49 78 78 48 199 64
R08M | 1631 14 17 23 15 19 25 19 --- 9 | 82 82 50 48 79 81 58 --- 69
R09 | 2604 17 24 14 12 17 10 43 --- 9 | 32 37 32 38 43 38 48 --- 34
R11 | 2109 11 11 13 11 17 11 14 287 6 | 61 60 50 49 62 63 48 145 54
R12 | 727 32 32 29 19 26 32 29 --- 12 | 89 83 51 50 75 77 50 --- 61
R13 | 2501 61 70 26 27 37 23 33 --- 16 | 92 96 58 51 73 64 44 --- 59
R14 | 1700 22 19 20 8 19 16 17 --- 7 | 77 76 50 52 66 60 50 --- 57
R15M | 869 25 27 15 15 14 12 17 --- 7 | 92 93 71 72 77 79 70 --- 75
R16M | 811 27 28 22 26 27 32 17 --- 11 | 53 55 49 76 62 79 73 --- 64
R17 | 574 23 24 16 32 30 19 21 --- 11 | 35 33 27 29 43 32 23 --- 28
R18M | 3950 8 8 17 5 15 13 12 --- 5 | 23 22 17 24 25 26 18 --- 20
R19M | 401 60 58 54 56 75 67 53 --- 27 | 52 57 48 33 64 51 30 --- 41
R20M | 836 41 52 50 19 29 60 30 --- 18 | 37 54 33 31 40 35 24 --- 29
R21M | 1081 17 22 18 30 34 23 28 165 11 | 35 37 30 35 44 40 30 125 33
R22M | 918 15 17 16 15 23 20 29 --- 9 | 39 39 30 34 42 40 31 --- 34
R23M | 1225 16 22 31 29 17 27 12 --- 10 | 19 26 23 34 30 27 25 --- 23
XR26 | ---- 16 95 --- --- --- --- 16 --- 16 | 28 67 --- --- --- --- 28 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1577 34 37 27 24 29 30 27 185 |T 63 67 44 47 60 56 43 137 49
WRMS | 1577 26 28 27 20 24 24 25 185 |NE 68 72 49 49 67 59 44 114 51
MEDI | 1081 24 24 22 19 22 23 24 165 |MD 61 67 49 49 64 60 47 137 54
Table 3.2089.1 GPS week: 2089 Day: 1 MJD: 58868
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | 1140 76 84 35 55 24 30 45 --- 21 | 87 94 31 37 52 53 21 --- 38
R02M | 1681 16 25 16 10 16 16 14 103 6 | 54 62 39 51 58 39 41 113 46
R03 | 632 30 28 19 19 17 23 35 86 10 | 74 74 55 51 67 69 36 148 57
XR04 | 1748 33 29 15 14 --- 16 24 --- 10 | 76 73 55 51 --- 55 42 --- 55
R05 | 747 22 23 23 11 30 16 25 --- 10 | 58 59 40 45 66 38 36 --- 45
R07M | 1706 29 25 19 23 17 22 24 118 10 | 67 63 42 37 55 59 36 159 48
R08M | 601 20 22 20 20 27 25 20 --- 10 | 61 64 31 31 57 58 42 --- 49
R09 | 1867 18 22 13 9 26 21 47 --- 10 | 26 28 21 27 38 35 35 --- 25
R11 | 1453 7 13 14 14 12 28 18 104 7 | 39 42 32 35 46 54 30 115 37
R12 | 1306 30 30 29 21 36 16 23 --- 12 | 61 61 37 43 68 47 36 --- 45
R13 | 1471 58 61 25 33 57 50 51 --- 20 | 77 83 55 48 87 58 31 --- 55
R14 | 1909 23 31 23 9 12 11 11 --- 7 | 57 64 40 46 51 40 41 --- 44
R15M | 787 21 21 14 19 10 19 14 --- 7 | 64 66 56 51 51 57 60 --- 55
R16M | 776 24 26 22 21 28 26 28 --- 11 | 43 43 43 54 51 43 56 --- 44
R17 | 705 25 24 13 22 15 20 27 --- 9 | 21 22 18 18 20 21 15 --- 16
R18M | 930 7 9 12 8 14 9 14 --- 5 | 18 21 18 19 21 14 20 --- 15
R19M | 707 42 47 46 72 83 73 62 --- 29 | 23 33 37 36 60 36 30 --- 30
R20M | 675 39 42 69 24 25 82 32 --- 23 | 21 27 32 25 24 33 14 --- 17
R21M | 1255 16 18 18 21 23 31 32 197 10 | 21 20 18 23 26 28 20 86 21
R22M | 1325 17 20 16 32 33 17 25 --- 11 | 20 24 18 27 29 21 21 --- 20
R23M | 638 13 11 14 24 11 14 17 --- 7 | 17 21 21 22 21 23 17 --- 17
XR26 | ---- 10 42 --- --- --- --- 12 --- 11 | 22 40 --- --- --- --- 32 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1199 31 34 27 28 31 33 31 128 |T 45 49 35 37 47 41 32 124 36
WRMS | 1199 27 29 27 22 29 35 27 128 |NE 51 54 39 40 55 46 33 131 40
MEDI | 1140 22 25 19 21 23 21 24 104 |MD 43 43 37 37 51 40 32 115 38
Table 3.2089.2 GPS week: 2089 Day: 2 MJD: 58869
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | 1729 72 62 32 49 33 32 55 --- 21 | 90 87 36 44 67 48 35 --- 44
R02M | 2119 17 17 18 15 13 23 11 79 7 | 57 58 36 53 54 35 37 66 45
R03 | 744 29 30 26 25 29 13 34 73 12 | 75 78 47 43 80 59 41 118 56
XR04 | 2460 36 37 17 18 --- 21 12 --- 11 | 80 84 57 57 --- 60 55 --- 61
R05 | 975 26 38 29 14 25 21 17 --- 10 | 70 82 46 49 65 62 47 --- 53
R07M | 2218 28 33 21 24 33 13 31 186 11 | 71 76 48 35 72 46 34 135 50
R08M | 642 16 13 15 17 22 19 20 --- 8 | 65 63 40 38 67 58 45 --- 55
R09 | 1694 14 13 14 14 24 25 52 --- 11 | 20 20 23 28 30 29 42 --- 21
R11 | 700 10 9 17 14 14 30 15 125 8 | 45 50 35 39 52 65 43 68 44
R12 | 1538 21 21 23 29 25 28 29 --- 11 | 59 59 40 36 60 57 33 --- 44
R13 | 921 54 65 44 32 32 45 36 --- 18 | 77 90 43 37 72 50 39 --- 48
R14 | 1009 23 24 24 12 22 13 22 --- 9 | 62 65 37 44 66 50 36 --- 48
R15M | 1006 19 23 15 17 14 17 23 --- 8 | 64 69 54 46 63 56 52 --- 54
R16M | 1347 25 38 18 24 28 18 36 --- 11 | 48 48 43 64 51 49 69 --- 50
R17 | 1099 18 21 19 14 12 23 33 --- 9 | 23 24 24 25 25 27 19 --- 20
R18M | 1281 11 14 15 12 14 16 12 --- 6 | 20 21 23 27 27 29 13 --- 21
R19M | 1223 47 45 39 81 61 60 63 --- 26 | 41 40 43 33 56 49 24 --- 38
R20M | 875 27 23 67 17 41 54 37 --- 20 | 31 30 34 29 36 31 23 --- 24
R21M | 1427 24 25 14 32 18 27 36 202 11 | 27 30 28 27 35 32 27 114 27
R22M | 2157 11 11 20 24 34 21 31 --- 11 | 27 29 23 27 40 36 31 --- 28
R23M | 517 11 19 22 24 10 22 26 --- 9 | 18 23 21 25 26 28 21 --- 18
XR26 | ---- 17 40 --- --- --- --- 18 --- 18 | 26 54 --- --- --- --- 22 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS | 1356 29 31 28 29 28 29 34 143 |T 49 53 37 38 52 45 35 100 39
WRMS | 1356 23 24 28 23 19 26 30 143 |NE 53 60 39 39 56 51 37 93 41
MEDI | 1223 21 23 20 18 24 22 29 125 |MD 48 54 37 37 54 49 35 114 44
Table 3.2089.3 GPS week: 2089 Day: 3 MJD: 58870
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | 1283 64 57 33 43 40 27 47 --- 19 | 86 82 32 32 66 34 26 --- 37
R02M | 1588 12 13 17 12 14 11 13 105 6 | 57 57 35 45 59 46 44 41 47
R03 | 1125 24 25 22 21 19 14 25 75 9 | 76 75 48 46 73 61 42 102 57
XR04 | 3021 31 34 20 19 --- 15 21 --- 11 | 80 85 61 47 --- 60 51 --- 59
R05 | 1316 26 23 21 19 11 24 19 --- 9 | 64 61 34 45 48 48 38 --- 43
R07M | 2118 32 36 24 15 24 24 24 291 10 | 77 79 44 46 71 39 40 234 51
R08M | 964 14 17 19 15 24 13 18 --- 8 | 62 63 34 40 63 55 52 --- 55
R09 | 977 17 24 17 6 23 25 53 --- 12 | 25 31 21 23 35 29 47 --- 21
R11 | 932 7 12 18 10 13 27 15 144 7 | 56 55 42 50 58 66 40 46 51
R12 | 815 28 21 26 20 15 20 24 --- 10 | 65 62 40 40 52 55 36 --- 44
R13 | 1086 47 38 28 24 24 45 30 --- 15 | 70 67 40 28 47 58 27 --- 40
R14 | 1386 27 34 23 17 14 13 13 --- 8 | 66 70 37 37 56 50 42 --- 46
R15M | 1635 22 22 17 19 21 15 27 --- 9 | 67 67 48 41 61 58 41 --- 51
R16M | 1671 18 21 16 25 19 28 17 --- 9 | 69 78 53 81 65 69 74 --- 66
R17 | 689 21 21 18 20 24 13 29 --- 9 | 30 30 27 34 36 25 23 --- 26
R18M | 745 16 18 19 15 18 21 19 --- 8 | 24 27 20 27 28 27 24 --- 21
R19M | 1121 52 73 36 71 50 65 67 --- 25 | 42 62 40 37 51 48 28 --- 35
R20M | 1518 40 37 44 17 46 59 20 --- 18 | 25 35 20 24 31 37 25 --- 19
R21M | 1086 24 25 12 27 18 29 34 212 11 | 29 32 23 23 27 26 19 102 22
R22M | 2100 22 15 18 35 25 25 27 --- 11 | 32 30 23 27 35 34 26 --- 27
R23M | 530 13 13 33 25 10 15 21 --- 9 | 20 26 19 35 32 27 23 --- 23
XR26 | ---- 13 60 --- --- --- --- 15 --- 14 | 24 51 --- --- --- --- 37 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1306 30 31 24 27 25 29 30 183 |T 52 55 35 38 49 45 36 105 39
WRMS | 1306 26 27 24 23 23 24 27 183 |NE 55 58 38 38 50 50 38 74 41
MEDI | 1125 22 23 20 19 19 24 21 144 |MD 57 61 35 37 51 48 37 102 40
Table 3.2089.4 GPS week: 2089 Day: 4 MJD: 58871
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | 818 66 67 37 47 37 24 50 --- 20 | 79 79 38 28 56 45 28 --- 35
R02M | 638 9 12 22 6 14 15 11 178 6 | 57 60 50 54 61 52 44 101 52
R03 | 803 17 18 25 23 27 26 29 119 11 | 72 75 52 50 85 78 40 165 62
XR04 | 2951 30 33 21 16 --- 14 25 --- 10 | 78 82 62 59 --- 66 46 --- 61
R05 | 1147 24 21 22 16 17 17 19 --- 8 | 67 70 53 55 60 61 48 --- 55
R07M | 2206 33 32 20 12 15 18 15 424 9 | 75 77 48 57 65 45 48 436 55
R08M | 1327 13 13 31 11 24 18 17 --- 9 | 67 68 45 44 61 58 57 --- 60
R09 | 1276 10 18 16 11 12 20 42 --- 9 | 35 42 36 35 41 41 47 --- 35
R11 | 1704 13 11 19 9 16 22 16 185 7 | 55 61 46 55 64 67 49 79 54
R12 | 819 18 25 24 19 18 25 27 --- 10 | 66 75 47 52 65 69 44 --- 55
R13 | 1557 30 32 24 42 33 42 38 --- 16 | 64 63 50 44 70 57 32 --- 48
R14 | 1616 29 29 20 14 12 17 18 --- 8 | 64 64 46 44 45 56 37 --- 47
R15M | 1873 25 26 17 22 15 16 30 --- 9 | 72 76 58 56 69 67 55 --- 60
R16M | 1378 36 26 35 20 26 27 14 --- 12 | 64 78 64 92 99 94 69 --- 79
R17 | 710 22 30 21 31 29 20 25 --- 11 | 37 40 43 47 43 33 28 --- 37
R18M | 1615 16 20 23 12 21 19 22 --- 8 | 31 34 33 35 42 43 24 --- 33
R19M | 1162 63 59 33 60 42 63 69 --- 24 | 49 49 39 41 53 38 29 --- 36
R20M | 1075 35 43 37 28 47 51 41 --- 18 | 34 41 60 46 54 34 40 --- 41
R21M | 574 21 14 20 30 32 29 35 298 12 | 41 44 40 39 50 45 29 242 39
R22M | 1266 24 26 16 23 19 27 38 --- 11 | 42 46 42 46 51 45 41 --- 43
R23M | 512 12 27 29 25 9 12 17 --- 8 | 28 36 34 35 35 36 23 --- 31
XR26 | ---- 14 50 --- --- --- --- 18 --- 16 | 25 57 --- --- --- --- 30 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1287 30 31 25 27 25 28 32 264 |T 54 59 46 48 58 53 40 204 47
WRMS | 1287 24 26 25 26 19 27 28 264 |NE 56 62 48 49 59 58 40 122 48
MEDI | 1266 22 26 22 20 19 20 25 185 |MD 57 61 46 46 56 52 40 165 47
Table 3.2089.5 GPS week: 2089 Day: 5 MJD: 58872
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | 817 70 76 42 42 40 41 56 --- 21 | 66 72 36 36 52 38 42 --- 34
R02M | 1094 14 17 15 5 8 16 14 113 5 | 52 51 37 42 43 33 58 58 42
R03 | 615 26 22 19 22 15 19 18 425 9 | 61 53 41 30 53 47 43 278 44
XR04 | 2176 34 28 16 19 --- 13 20 --- 10 | 66 60 42 44 --- 52 40 --- 47
R05 | 1273 31 26 18 17 14 13 19 --- 8 | 61 59 43 58 61 42 52 --- 51
R07M | 879 33 40 18 18 15 15 25 450 9 | 59 65 36 32 40 37 31 316 37
R08M | 963 21 20 28 14 19 21 18 --- 9 | 78 83 45 50 107 63 82 --- 70
R09 | 1897 15 19 12 12 13 20 34 --- 8 | 35 35 34 33 35 36 36 --- 32
R11 | 2197 6 10 22 9 12 17 13 161 6 | 53 52 39 48 54 53 48 64 48
R12 | 610 30 23 25 27 19 27 25 --- 11 | 67 62 45 43 58 64 45 --- 51
R13 | 3406 36 29 27 24 29 49 35 --- 14 | 56 57 46 50 50 64 41 --- 47
R14 | 1476 21 17 20 15 10 22 16 --- 7 | 48 44 30 35 37 48 30 --- 35
R15M | 1662 22 17 22 23 20 22 34 --- 10 | 62 56 44 42 64 61 44 --- 51
R16M | 529 23 26 27 20 14 39 19 --- 10 | 48 58 48 54 66 67 62 --- 55
R17 | 506 25 16 17 13 14 13 27 --- 8 | 19 18 17 19 20 14 14 --- 15
R18M | 1806 24 18 26 15 14 20 21 --- 9 | 18 19 23 23 21 28 15 --- 16
R19M | 1563 53 59 40 51 33 63 55 --- 21 | 31 34 21 40 66 34 33 --- 31
R20M | 755 30 36 36 16 23 64 30 --- 15 | 37 45 42 45 48 32 23 --- 33
R21M | 650 24 24 20 33 18 34 26 79 11 | 16 17 20 19 17 19 21 156 14
R22M | 1236 26 25 15 37 15 38 30 --- 12 | 25 24 28 22 24 26 26 --- 20
R23M | 951 11 11 22 22 12 11 28 --- 8 | 22 24 23 21 25 19 21 --- 18
XR26 | ---- 16 68 --- --- --- --- 20 --- 18 | 26 53 --- --- --- --- 20 --- 18
------+---------------------------------------------------+-----------------------------------------------
RMS | 1424 30 31 25 24 19 32 29 292 |T 45 47 35 37 47 41 37 174 36
WRMS | 1424 26 25 25 20 14 27 28 292 |NE 49 49 37 40 46 46 36 171 38
MEDI | 1094 24 23 22 19 15 21 25 161 |MD 48 52 37 40 48 38 36 156 35
Table 3.2089.6 GPS week: 2089 Day: 6 MJD: 58873
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | 1211 72 69 34 45 35 25 34 --- 19 | 102 101 47 40 52 44 26 --- 42
R02M | 751 13 13 22 7 20 16 20 156 7 | 66 66 44 56 68 53 53 62 55
R03 | 608 26 33 20 17 26 14 30 403 10 | 82 86 50 44 80 65 43 263 59
XR04 | 1609 38 38 20 16 --- 12 21 --- 11 | 93 94 54 49 --- 63 51 --- 61
R05 | 1155 20 27 21 16 15 20 20 --- 8 | 80 85 52 72 79 70 61 --- 68
R07M | 1528 27 25 21 21 32 16 33 498 11 | 78 76 46 42 76 51 38 252 54
XR08M |14258 62 73 --- --- 228 99 55 --- 53 | 273 276 --- --- 237 144 267 --- 225
R09 | 1850 16 16 20 15 14 10 42 --- 9 | 33 36 33 31 41 36 47 --- 32
R11 | 1400 10 9 13 6 10 9 14 141 4 | 66 67 56 61 66 68 54 60 61
R12 | 863 26 36 21 15 23 17 34 --- 10 | 92 97 64 60 88 84 51 --- 71
R13 | 2952 42 53 22 29 42 27 25 --- 14 | 89 97 57 53 79 68 51 --- 62
R14 | 697 21 25 21 11 13 30 23 --- 9 | 71 74 45 51 54 69 39 --- 52
R15M | 911 21 21 20 24 13 28 27 --- 10 | 75 77 59 44 68 74 41 --- 58
R16M | 797 24 38 21 19 23 36 17 --- 10 | 72 69 69 84 81 94 89 --- 80
R17 | 1367 22 22 20 9 17 13 22 --- 8 | 34 34 28 30 37 33 24 --- 29
R18M | 983 21 23 19 17 15 16 13 --- 7 | 28 31 24 31 36 28 27 --- 27
R19M | 3050 49 40 33 63 56 73 64 --- 25 | 49 56 45 62 51 53 39 --- 42
R20M | 728 27 31 72 27 32 82 19 --- 22 | 34 38 32 25 37 34 31 --- 26
R21M | 689 23 25 18 12 14 20 32 58 9 | 35 35 30 34 41 40 28 124 32
R22M | 1486 25 29 18 32 23 29 23 --- 11 | 54 55 48 45 55 55 46 --- 49
R23M | 2143 11 18 21 14 16 22 38 --- 9 | 20 21 21 26 25 24 26 --- 20
XR26 | ---- 15 64 --- --- --- --- 18 --- 17 | 29 80 --- --- --- --- 33 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1501 30 32 27 25 26 33 30 303 |T 70 75 45 47 67 59 52 152 56
WRMS | 1501 26 26 27 18 16 23 29 303 |NE 66 75 48 50 65 61 45 161 52
MEDI | 1211 23 27 21 16 20 20 23 156 |MD 66 69 46 44 55 55 41 124 52
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