[IGSREPORT-27547] Wk 2126 IGLOS Final Orbits
acc
acc at igs.org
Thu Oct 22 22:14:08 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2126 (Oct 04, 2020 - Oct 10, 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 2.2126.
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:
igl2126[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2126 in the SP3 format.
igl21267.sum Combination Report for GPS Week 2126.
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 | -2.1 ns
1 | -1.1 ns
2 | -0.2 ns
3 | -3.1 ns
4 | -0.4 ns
5 | -0.2 ns
6 | 0.4 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 1.2126, 1a.2126).
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 2.2126.0-6)
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 3.2126.0-6).
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 2126 summary. (Oct 04, 2020 - Oct 10, 2020)
Table 1.2126.a GPS week : 2126 MJD: 59126.0-59132.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -3 -12 -7 -22 .07 19 15 | 18369 -1435 3424 9054
| 0 1 0 11 14 13 .02 | 2177 1826
emx n/a| -2 0 11 -22 -4 -53 .15 32 28 | -8153 -1004 3186 8292
| 1 1 1 15 21 35 .04 | 8025 1167
esx n/a| 0 0 5 34 30 5 .10 35 31 | 2497 -1535 3477 7458
| 2 0 1 11 20 39 .03 | 3601 1960
gfz n/a| 0 -1 -6 -4 -15 9 .16 27 18 | 0 -1316 3225 7813
| 1 1 2 22 17 37 .06 | 0 1874
grg n/a| 1 0 5 5 -7 -82 -.39 26 21 | -340 -1318 3216 7639
| 0 1 4 21 28 57 .05 | 839 1792
iac n/a| -1 1 -6 15 17 115 -.05 23 20 | 625 -312 3431 9151
| 2 1 1 18 31 33 .03 | 1869 1213
Table 1.2126.b GPS week : 2126 MJD: 59126.0-59132.0
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 18 18 18 18 19 |
R02 | 11 11 10 9 9 7 7 |
R03 | 9 7 8 9 11 9 9 |
R04 | 10 9 10 12 9 9 9 |
R05 | 11 11 11 10 10 10 9 |
R07 | 9 9 8 8 10 9 7 |
R08 | 13 9 10 11 10 9 8 |
R09 | 8 6 8 8 9 6 6 |
R11 | 9 7 6 5 5 7 7 |
R12 | 10 9 8 9 11 11 8 |
R13 | 17 15 15 13 17 17 15 |
R14 | 10 8 7 8 8 6 7 |
R15 | 9 10 9 10 11 8 9 |
R16 | 18 14 15 14 15 15 12 |
R17 | 10 8 8 8 8 8 9 |
R18 | 10 8 9 7 6 7 7 |
R19 | 17 19 18 17 16 17 17 |
R20 | 22 23 24 19 24 20 24 |
R21 | 10 10 11 10 10 8 9 |
R22 | 11 11 11 10 13 9 11 |
R23 | 9 10 11 10 12 9 9 |
R24 | 12 11 11 9 9 11 10 |
R26 | 15 16 14 9 13 11 12 |
Table 1.2126.c GPS week : 2126 MJD: 59126.0-59132.0
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 2126 0 | 5 46 88 1483 -449 1267 82.1 1751 1751 | -2058 0
brd 2126 1 | -135 29 139 -1330 -2284 -2064 83.0 1721 1721 | -1079 0
brd 2126 2 | -13 -56 136 472 455 -988 83.2 1948 1948 | -160 0
brd 2126 3 | -45 26 119 -1445 2471 2230 85.0 1987 1987 | -3057 0
brd 2126 4 | -40 18 181 -1748 1339 2809 83.7 1869 1869 | -364 0
brd 2126 5 | 34 -9 163 598 287 1902 83.4 1669 1669 | -177 0
brd 2126 6 | 18 105 231 -281 1970 1096 81.2 1568 1568 | 366 0
-------------+------------------------------------------------------------+----------------
brd 2126 mean| -25 22 151 -321 541 893 83.1 1787 1787 | -932 0
brd 2126 sdev| 56 49 46 1228 1604 1776 1.2 152 152 | 1223 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 2.2126.0 GPS week: 2126 Day: 0 MJD: 59126
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 -5 -24 -17 -37 .06 25 19 | 20670 -1639 3527 9061
emx n/a| -4 0 13 -28 -28 -81 .18 35 34 | 24 -1637 3431 9037
esx n/a| -1 0 6 40 11 -32 .13 40 37 | 8646 -1683 3599 8789
gfz n/a| 2 -1 -7 20 -34 -4 .16 27 21 | 0 -1991 3467 8660
grg n/a| 1 0 12 4 -48 0 -.42 28 24 | -1208 -2132 3407 8526
iac n/a| 0 3 -9 -3 57 107 -.06 20 20 | -15 1265 3571 9186
Table 2.2126.1 GPS week: 2126 Day: 1 MJD: 59127
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 9 -4 .08 19 15 | 15643 -1809 3744 10691
emx n/a| -1 0 12 -16 12 -95 .18 33 28 | -13336 -938 3348 8873
esx n/a| 1 -1 4 24 54 -66 .03 36 28 | 4687 -1583 3665 9641
gfz n/a| 2 0 -7 -24 -18 -3 .12 22 17 | 0 -1155 3397 8324
grg n/a| 1 1 7 -21 -19 -17 -.38 29 26 | -90 -1809 3313 8436
iac n/a| -4 0 -4 46 -31 141 -.08 25 20 | -2337 -357 3688 10492
Table 2.2126.2 GPS week: 2126 Day: 2 MJD: 59128
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 -24 -13 -20 .06 18 14 | 20791 1903 3472 8615
emx n/a| -3 2 11 -14 17 -43 .16 33 27 | -14699 1381 3228 7629
esx n/a| 3 0 8 40 17 11 .09 36 30 | -2387 1440 3549 8480
gfz n/a| -2 0 -1 -21 -2 92 .08 27 18 | 0 1705 3284 7028
grg n/a| 2 -1 -2 31 -10 -159 -.30 30 22 | -1123 1952 3225 7151
iac n/a| -1 0 -6 4 2 61 -.08 22 19 | 2852 -133 3560 9191
Table 2.2126.3 GPS week: 2126 Day: 3 MJD: 59129
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 -3 -6 -1 -38 .10 18 15 | 18962 -3863 2931 8277
emx n/a| -2 -1 10 -6 17 -70 .16 29 27 | -19383 -2274 2678 7969
esx n/a| -2 0 3 37 43 29 .14 32 29 | 1905 -4688 2811 7222
gfz n/a| 0 0 -8 -3 0 0 .11 26 17 | 0 -4485 2665 7479
grg n/a| 1 1 9 -20 -7 -71 -.38 23 19 | -1279 -3581 2657 7354
iac n/a| -1 1 -7 6 23 162 -.06 24 20 | -924 -1746 2834 8367
Table 2.2126.4 GPS week: 2126 Day: 4 MJD: 59130
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 -3 2 5 -22 .07 21 16 | 19682 -2893 3120 8760
emx n/a| 0 0 9 -6 -18 -61 .14 33 27 | -3057 -1590 3044 8500
esx n/a| 2 1 4 54 0 20 .11 33 29 | 3382 -2941 3636 5344
gfz n/a| 0 0 -6 -29 -44 8 .25 27 20 | 0 -1571 3096 8013
grg n/a| 1 -1 1 4 15 -108 -.47 25 20 | 678 -2464 3015 7359
iac n/a| -6 3 -5 10 42 133 -.04 26 24 | 1762 795 3145 8956
Table 2.2126.5 GPS week: 2126 Day: 5 MJD: 59131
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 -11 -4 -28 .06 17 14 | 16722 -716 3823 8564
emx n/a| -2 -2 10 -38 -31 13 .11 32 28 | -8353 -734 3383 7417
esx n/a| 2 1 6 25 43 44 .11 35 34 | -647 -55 3763 3846
gfz n/a| 0 -1 -10 -5 -9 -6 .21 30 18 | 0 -1548 3422 7028
grg n/a| 1 0 3 4 -21 -86 -.42 22 16 | 242 -911 3390 6560
iac n/a| 0 0 -6 37 37 90 .02 21 18 | 2393 -2024 3902 8600
Table 2.2126.6 GPS week: 2126 Day: 6 MJD: 59132
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 -3 -22 -32 -5 .03 18 13 | 16118 -1031 3352 9414
emx n/a| -3 0 12 -45 1 -35 .09 30 26 | 1733 -1237 3194 8624
esx n/a| 0 0 5 21 43 28 .09 36 30 | 1897 -1236 3317 8887
gfz n/a| -1 -4 -6 30 1 -22 .20 31 19 | 0 -171 3250 8163
grg n/a| 0 0 5 33 40 -131 -.39 22 19 | 400 -282 3510 8093
iac n/a| 0 0 -7 4 -12 115 -.03 20 17 | 650 11 3321 9269
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 3.2126.0 GPS week: 2126 Day: 0 MJD: 59126
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1736 55 48 93 22 25 23 20 | 124 67 53 96 94 90 86
R02 | 1981 10 36 39 23 15 19 10 | 78 48 50 89 73 82 72
R03 | 1020 10 27 42 14 14 17 9 | 83 66 56 83 85 85 78
XR04 | 719 15 21 35 --- 16 10 9 | 96 84 78 --- 92 94 90
R05 | 2227 19 31 36 26 12 18 10 | 84 56 44 83 66 83 71
R07 | 1108 16 27 35 12 27 8 9 | 87 68 56 82 91 74 77
R08 | 838 14 41 43 24 27 21 12 | 83 59 55 106 98 105 87
R09 | 2470 11 22 17 20 12 17 7 | 35 42 41 43 38 36 36
R11 | 1570 12 20 21 21 27 15 8 | 55 49 46 68 67 55 56
R12 | 2033 8 24 43 15 27 15 10 | 72 65 50 70 93 80 72
R13 | 4604 31 50 64 37 21 18 16 | 74 54 35 90 79 82 70
R14 | 954 8 17 32 16 14 34 10 | 50 53 40 50 52 70 52
R15 | 802 8 25 31 12 26 15 8 | 86 76 75 88 102 92 87
R16 | 796 29 53 34 24 70 16 18 | 47 34 55 56 96 61 56
R17E | 1083 25 37 15 15 16 21 10 | 110 102 103 108 105 107 105
R18E | 1082 12 24 13 27 27 20 9 | 84 79 82 89 84 82 82
R19E | 771 52 41 31 36 38 25 17 | 89 97 100 96 114 94 93
R20E | 1115 38 59 66 66 43 31 22 | 92 87 85 90 90 69 77
R21E | 1133 15 37 23 21 13 20 9 | 105 99 107 107 107 115 106
R22E | 1563 21 33 21 31 27 18 11 | 68 60 60 83 67 65 64
R23E | 1849 18 20 30 21 16 16 9 | 122 123 128 124 131 129 125
R24E | 1428 25 29 13 18 35 25 11 | 80 93 85 89 97 88 86
XR26E | 6058 18 --- 30 --- --- 19 15 | 54 --- 47 --- --- 55 51
------+-----------------------------------------+-------------------------------------
RMS | 1750 25 35 40 27 28 20 |T 80 70 66 85 87 82 77
WRMS | 1750 19 34 37 21 24 20 |NE 75 58 52 77 80 77 70
MEDI | 1133 16 29 32 21 25 18 |MD 83 66 56 89 91 82 77
Table 3.2126.1 GPS week: 2126 Day: 1 MJD: 59127
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 2070 41 45 83 25 34 16 18 | 83 58 46 67 77 57 62
R02 | 3199 9 41 34 27 14 15 10 | 55 34 34 76 60 62 54
R03 | 856 11 18 24 13 14 11 6 | 56 47 38 53 55 45 48
XR04 | 785 7 21 27 --- 12 23 9 | 69 66 64 --- 72 81 70
R05 | 2281 18 35 31 20 25 18 10 | 67 49 37 61 59 68 56
R07 | 1162 19 22 33 18 21 14 9 | 65 53 47 66 72 46 58
R08 | 770 8 32 28 16 23 15 9 | 55 36 41 62 67 60 54
R09 | 2929 11 19 11 17 10 12 6 | 22 28 26 30 24 25 23
R11 | 2064 8 20 9 17 18 12 6 | 44 35 43 50 52 39 43
R12 | 2123 11 26 31 12 16 27 9 | 53 48 39 49 54 69 51
R13 | 1664 27 28 50 30 48 24 15 | 50 33 22 35 34 46 34
R14 | 493 10 15 22 18 11 23 7 | 39 32 35 42 37 44 36
R15 | 601 7 17 47 18 22 16 9 | 57 53 51 63 67 51 56
R16 | 1726 27 34 34 16 53 20 14 | 33 30 40 51 78 47 42
R17E | 1989 11 29 19 19 13 9 7 | 76 72 77 80 77 81 76
R18E | 1852 14 21 19 15 19 14 7 | 54 48 56 58 56 57 54
R19E | 1148 38 50 40 37 47 44 18 | 72 81 88 83 74 75 72
R20E | 650 25 65 62 43 60 63 23 | 83 79 102 92 85 89 79
R21E | 779 18 37 19 16 24 17 9 | 77 71 78 80 70 75 74
R22E | 681 21 29 23 19 22 27 10 | 51 52 56 58 49 52 50
R23E | 1467 13 15 30 26 22 23 9 | 88 84 83 84 93 93 85
R24E | 1934 12 39 20 15 27 31 11 | 61 64 57 64 64 78 62
XR26E | 6404 15 --- 34 --- --- 20 15 | 43 --- 31 --- --- 45 38
------+-----------------------------------------+-------------------------------------
RMS | 1721 19 33 36 22 29 25 |T 58 52 51 62 62 60 55
WRMS | 1721 15 28 28 17 26 20 |NE 53 43 40 54 57 52 49
MEDI | 1664 13 28 30 18 22 18 |MD 56 49 46 62 64 57 54
Table 3.2126.2 GPS week: 2126 Day: 2 MJD: 59128
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 2018 35 30 89 20 32 18 17 | 91 58 52 75 87 74 71
R02 | 3480 10 32 35 13 13 22 9 | 68 47 47 65 68 73 61
R03 | 2203 10 19 31 12 21 12 7 | 70 60 47 66 75 62 64
XR04 | 975 21 18 27 --- 17 15 10 | 79 67 67 --- 57 66 68
R05 | 2162 21 30 32 30 17 16 11 | 71 43 52 80 49 66 61
R07 | 794 17 20 28 13 13 18 8 | 72 57 53 61 59 68 62
R08 | 1114 9 26 34 17 23 21 9 | 66 49 48 73 70 78 65
R09 | 3180 14 15 11 17 29 14 7 | 44 49 43 54 50 33 43
R11 | 1836 5 17 19 12 15 14 6 | 40 35 55 45 39 48 42
R12 | 2314 11 30 19 14 16 18 8 | 57 50 67 73 68 63 62
R13 | 3757 21 26 53 24 37 38 14 | 53 48 49 60 52 72 54
R14 | 701 10 15 26 10 10 23 7 | 44 32 31 40 37 50 39
R15 | 1145 10 16 43 20 17 10 9 | 62 64 54 75 61 63 63
R16 | 1933 17 34 30 32 57 24 14 | 53 37 47 57 73 51 50
R17E | 2522 11 26 21 16 18 14 7 | 51 53 54 55 51 54 51
R18E | 1618 16 17 22 14 31 15 8 | 40 44 46 47 49 44 42
R19E | 795 36 53 33 41 41 40 18 | 47 63 67 70 59 54 50
R20E | 622 27 79 54 68 56 44 24 | 56 89 71 94 58 49 56
R21E | 791 10 40 25 35 21 15 11 | 66 63 60 76 63 62 63
R22E | 966 18 26 16 33 29 20 10 | 58 57 59 64 69 51 56
R23E | 837 19 21 21 22 41 17 10 | 61 58 69 66 68 57 59
R24E | 1153 11 49 18 21 27 18 11 | 42 44 48 44 48 43 40
XR26E | 2941 15 --- 27 --- --- 20 14 | 33 --- 29 --- --- 37 30
------+-----------------------------------------+-------------------------------------
RMS | 1948 18 33 36 27 30 22 |T 57 53 52 63 59 57 54
WRMS | 1948 14 27 30 18 22 19 |NE 62 49 50 63 60 61 57
MEDI | 1618 15 26 27 20 21 18 |MD 57 50 52 65 59 57 56
Table 3.2126.3 GPS week: 2126 Day: 3 MJD: 59129
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1149 40 39 75 17 26 29 17 | 105 51 26 73 77 92 74
R02 | 1858 12 27 30 17 17 13 8 | 71 40 51 72 65 66 61
R03 | 1798 9 22 35 12 17 25 9 | 69 50 51 69 75 72 65
XR04 | 1272 20 26 36 --- 14 19 11 | 64 46 38 --- 49 56 51
R05 | 775 29 23 29 13 16 18 10 | 69 34 44 48 37 58 48
R07 | 1379 11 22 26 14 16 16 7 | 62 43 39 51 58 63 53
R08 | 1669 9 33 33 21 26 29 11 | 62 42 44 86 79 93 68
R09 | 3522 15 15 17 18 20 20 8 | 27 29 30 31 25 30 24
R11 | 1023 6 10 10 14 14 10 4 | 43 43 39 38 49 42 41
R12 | 2130 8 36 14 16 17 20 8 | 56 37 55 70 68 70 59
R13 | 5855 16 37 45 23 17 36 13 | 61 64 42 77 76 85 65
R14 | 1036 9 16 26 13 17 27 8 | 49 37 34 46 47 60 44
R15 | 1125 18 17 47 16 11 14 9 | 56 44 37 57 60 56 51
R16 | 1279 14 35 29 33 43 28 14 | 41 41 40 51 55 55 44
R17E | 2556 12 26 19 15 22 18 8 | 32 29 27 34 37 32 29
R18E | 1140 12 18 21 16 17 14 7 | 24 24 28 20 26 30 21
R19E | 1514 32 40 29 49 30 39 16 | 56 69 65 70 82 67 61
R20E | 971 31 45 40 60 36 42 19 | 55 49 54 82 94 62 58
R21E | 629 10 33 20 34 13 16 10 | 61 54 48 63 50 49 53
R22E | 915 11 20 15 33 26 21 9 | 34 27 34 38 33 28 27
R23E | 829 19 22 23 22 33 12 10 | 33 31 42 41 36 31 31
R24E | 619 12 34 20 24 15 16 9 | 29 28 25 35 28 31 25
XR26E | 3955 8 --- 16 --- --- 16 9 | 21 --- 19 --- --- 29 19
------+-----------------------------------------+-------------------------------------
RMS | 1987 18 29 32 26 23 24 |T 51 41 39 54 54 54 46
WRMS | 1987 15 27 29 17 19 20 |NE 59 42 40 59 58 64 53
MEDI | 1272 12 26 26 17 17 19 |MD 56 41 39 51 50 56 51
Table 3.2126.4 GPS week: 2126 Day: 4 MJD: 59130
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 801 37 47 73 20 15 33 17 | 103 61 57 97 80 101 82
R02 | 1739 15 21 24 20 17 18 8 | 74 59 56 70 72 60 64
R03 | 1217 13 18 45 12 23 28 10 | 76 59 48 71 81 82 69
XR04 | 1442 14 17 29 --- 13 15 9 | 80 71 69 --- 86 83 78
R05 | 848 25 19 35 16 21 16 10 | 78 58 55 62 74 69 65
R07 | 2346 8 24 36 11 18 26 9 | 77 67 60 74 84 84 74
R08 | 1022 15 27 29 18 18 29 10 | 64 57 53 73 71 84 66
R09 | 3300 11 12 13 27 17 28 8 | 57 65 63 70 44 44 55
R11 | 1599 7 12 12 12 11 11 5 | 48 47 44 48 48 48 46
R12 | 783 24 36 22 15 21 17 10 | 76 65 64 76 80 74 72
R13 | 5338 27 33 52 42 46 29 17 | 69 50 45 77 83 79 66
R14 | 1676 11 25 11 15 20 25 8 | 44 42 48 57 41 57 46
R15 | 692 9 24 39 16 18 32 10 | 70 66 58 78 82 90 73
R16 | 1371 18 27 23 41 53 25 15 | 40 36 44 48 56 42 41
R17E | 967 15 27 15 15 12 14 7 | 60 61 59 59 59 60 58
R18E | 789 10 15 18 12 17 11 6 | 56 52 52 58 51 53 52
R19E | 2648 39 37 30 38 27 42 16 | 47 47 55 71 44 54 46
R20E | 761 30 84 47 62 44 47 24 | 54 79 67 78 63 51 55
R21E | 1286 17 32 21 17 14 31 10 | 78 77 82 85 76 71 76
R22E | 1110 24 29 34 30 27 23 12 | 48 57 67 63 57 55 52
R23E | 914 24 29 19 40 19 17 11 | 81 83 87 97 87 84 83
R24E | 580 13 31 15 20 13 18 8 | 57 59 59 63 57 51 55
XR26E | 3919 13 --- 20 --- --- 20 12 | 39 --- 43 --- --- 47 41
------+-----------------------------------------+-------------------------------------
RMS | 1869 21 33 33 27 25 26 |T 64 59 58 70 67 66 61
WRMS | 1869 16 27 29 20 20 24 |NE 68 57 54 69 70 71 64
MEDI | 1217 15 27 24 18 18 25 |MD 64 59 57 71 71 60 64
Table 3.2126.5 GPS week: 2126 Day: 5 MJD: 59131
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 755 30 49 82 27 18 28 17 | 89 56 35 97 61 90 74
R02 | 2639 11 19 19 15 12 18 6 | 56 44 44 51 49 53 49
R03 | 638 10 22 36 21 21 12 9 | 68 55 43 66 74 69 64
XR04 | 943 15 16 28 --- 11 19 8 | 71 71 66 --- 67 60 66
R05 | 1895 19 13 34 15 13 28 9 | 56 44 44 51 54 32 45
R07 | 1163 9 24 40 19 16 12 8 | 64 50 44 80 74 70 64
R08 | 883 11 26 27 19 16 23 8 | 51 40 40 69 54 69 54
R09 | 2843 10 10 18 15 7 18 6 | 40 41 40 45 39 44 39
R11 | 1599 10 13 24 13 15 13 6 | 37 28 26 37 37 33 33
R12 | 728 13 36 34 15 31 14 10 | 61 42 45 61 73 55 57
R13 | 3364 16 55 49 26 56 14 16 | 63 50 46 60 88 60 61
R14 | 2228 8 16 8 14 10 21 6 | 26 27 32 27 35 36 29
R15 | 1150 6 18 37 13 16 14 7 | 46 38 30 47 44 51 43
R16 | 952 22 28 31 44 38 34 14 | 26 36 32 48 29 40 28
R17E | 881 13 28 15 23 15 15 8 | 70 66 68 76 72 72 70
R18E | 1217 11 18 16 20 13 12 6 | 55 51 50 46 56 55 52
R19E | 2518 34 50 37 52 28 33 17 | 58 69 50 61 61 59 54
R20E | 953 26 61 55 73 24 33 20 | 57 63 62 97 56 47 55
R21E | 1935 7 27 18 18 14 18 7 | 80 79 83 84 78 78 79
R22E | 792 17 23 26 28 15 16 9 | 40 41 45 54 41 43 40
R23E | 856 20 23 15 22 17 17 8 | 90 88 90 93 91 93 90
R24E | 706 13 38 20 44 12 15 11 | 58 58 61 80 62 63 61
XR26E | 3687 13 --- 19 --- --- 16 11 | 39 --- 34 --- --- 34 33
------+-----------------------------------------+-------------------------------------
RMS | 1668 17 32 35 30 22 21 |T 56 51 48 63 58 56 53
WRMS | 1668 14 28 34 18 16 18 |NE 53 44 40 56 55 54 50
MEDI | 1150 13 23 27 20 15 17 |MD 57 50 44 61 56 55 54
Table 3.2126.6 GPS week: 2126 Day: 6 MJD: 59132
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 992 37 44 83 42 30 26 19 | 119 58 36 118 80 106 90
R02 | 2588 8 23 19 9 10 20 7 | 78 58 66 77 76 87 74
R03 | 750 14 20 24 33 22 8 9 | 92 71 61 76 97 92 83
XR04 | 560 20 18 26 --- 12 16 9 | 108 98 86 --- 96 87 96
R05 | 2199 21 14 34 13 14 20 9 | 82 64 62 66 70 57 66
R07 | 878 9 22 29 14 16 10 7 | 89 70 62 94 90 87 83
R08 | 1056 6 26 22 26 12 14 8 | 74 50 55 92 69 86 72
R09 | 1822 10 10 10 15 15 10 5 | 43 43 43 46 43 43 42
R11 | 1152 8 10 14 13 21 16 6 | 53 44 43 52 47 51 48
R12 | 899 9 19 33 20 21 11 8 | 75 61 58 86 90 86 76
R13 | 2491 20 45 65 29 29 19 15 | 96 59 51 103 99 98 86
R14 | 878 7 16 14 15 14 20 6 | 49 44 52 49 49 60 50
R15 | 1493 8 15 39 12 26 13 8 | 76 67 56 78 87 80 74
R16 | 797 26 20 45 26 27 21 12 | 45 34 45 57 60 54 47
R17E | 961 10 31 13 29 11 16 8 | 100 99 100 106 104 104 101
R18E | 2093 11 23 16 11 13 18 7 | 73 73 80 80 81 80 76
R19E | 2110 27 56 48 44 34 30 17 | 74 78 86 91 85 75 74
R20E | 1002 37 55 49 94 46 38 24 | 68 79 59 98 61 54 58
R21E | 2582 12 31 24 19 12 17 8 | 97 93 100 105 97 97 97
R22E | 1251 19 32 28 26 19 24 11 | 52 55 57 69 54 55 53
R23E | 1266 17 20 29 17 25 15 9 | 122 123 123 124 127 117 121
R24E | 846 10 39 20 25 19 17 10 | 83 86 83 92 87 88 84
XR26E | 3878 17 --- 17 --- --- 15 11 | 42 --- 36 --- --- 38 37
------+-----------------------------------------+-------------------------------------
RMS | 1567 18 30 36 31 22 20 |T 77 68 65 83 79 77 73
WRMS | 1567 13 26 30 19 19 17 |NE 77 58 55 76 75 76 70
MEDI | 1152 12 22 26 20 19 17 |MD 76 64 59 86 81 86 74
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