[IGSREPORT-28608] Wk 2203 IGLOS Final Orbits
acc
acc at igs.org
Tue Apr 19 00:44:03 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2203 (Mar 27, 2022 - Apr 02, 2022)
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 2.2203.
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:
igl2203[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2203 in the SP3 format.
igl22037.sum Combination Report for GPS Week 2203.
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 | 0.5 ns
1 | -8.9 ns
2 | -6.4 ns
3 | -5.8 ns
4 | -7.3 ns
5 | -7.3 ns
6 | 2.1 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 1.2203, 1a.2203).
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 2.2203.0-6)
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 3.2203.0-6).
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 2203 summary. (Mar 27, 2022 - Apr 02, 2022)
Table 1.2203.a GPS week : 2203 MJD: 59665.0-59671.0
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 13 -33 21 .15 28 17 | 29079 513 3208 8712
| 1 1 1 19 17 22 .02 | 4866 2186
emx n/a| 0 0 3 23 54 7 -.15 36 30 | -13016 727 3206 8711
| 2 2 3 15 32 44 .04 | 9527 1342
esx n/a| 0 0 0 -13 -6 -17 -.06 29 21 | -4043 827 3467 9669
| 0 1 1 16 15 22 .04 | 6498 2448
gfz n/a| 0 0 1 -23 -2 -10 -.03 31 19 | 0 415 3175 8452
| 1 1 2 29 14 41 .04 | 0 2396
grg n/a| 0 -1 -9 -16 25 8 .20 31 20 | -4995 285 3207 8092
| 1 1 3 18 15 40 .04 | 3407 2365
iac n/a| 0 0 0 52 -10 -4 -.22 34 30 | -3690 433 3480 10273
| 2 2 5 24 30 106 .05 | 4886 1705
Table 1.2203.b GPS week : 2203 MJD: 59665.0-59671.0
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 | 17 17 12 12 14 17 15 |
R02 | 8 8 8 6 7 8 8 |
R03 | 6 6 6 8 6 7 7 |
R04 | 7 7 10 9 9 8 8 |
R05 | 11 10 9 10 13 12 9 |
R07 | 10 10 8 7 8 7 10 |
R08 | 10 8 8 11 9 9 6 |
R09 | 8 8 9 8 9 7 7 |
R11 | --- 0 12 12 8 12 12 |
R12 | 10 9 10 10 8 8 9 |
R13 | 15 20 16 20 20 17 18 |
R14 | 9 9 7 7 8 9 8 |
R15 | 8 8 7 7 8 9 9 |
R17 | 7 8 8 8 7 7 8 |
R18 | 10 11 9 9 9 7 8 |
R19 | 20 21 18 28 16 17 20 |
R20 | 23 22 28 35 29 24 22 |
R21 | 9 8 9 8 9 7 9 |
R22 | 24 34 40 34 25 24 26 |
R24 | 8 9 10 9 9 8 9 |
Table 1.2203.c GPS week : 2203 MJD: 59665.0-59671.0
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 2203 0 | 43 -143 76 2476 1115 2997 80.0 1497 1497 | 527 0
brd 2203 1 | 56 -14 80 1264 -346 -5286 80.9 1677 1677 | -8903 0
brd 2203 2 | 16 54 21 -1453 186 -2694 83.0 1860 1860 | -6429 0
brd 2203 3 | -4 -17 77 -1278 100 -2136 81.1 1635 1635 | -5835 0
brd 2203 4 | -19 10 135 -694 1014 6615 80.3 1527 1527 | -7316 0
brd 2203 5 | -29 37 57 -1993 3440 -5514 81.5 1535 1535 | -7304 0
brd 2203 6 | -96 11 262 -1596 2631 -5136 79.9 1620 1620 | 2126 0
-------------+------------------------------------------------------------+----------------
brd 2203 mean| -4 -8 101 -467 1163 -1593 81.0 1621 1621 | -4733 0
brd 2203 sdev| 51 64 78 1680 1397 4681 1.1 123 123 | 4271 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 2.2203.0 GPS week: 2203 Day: 0 MJD: 59665
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 21 -25 52 .16 22 15 | 35436 981 2934 8750
emx n/a| 0 2 -1 11 41 37 -.14 34 24 | 5629 1186 2936 8910
esx n/a| 0 -2 0 -5 -23 -27 -.04 27 20 | -8981 807 2927 11036
gfz n/a| 0 -1 3 -40 -3 5 .02 30 18 | 0 932 2928 8524
grg n/a| 0 -2 -10 23 11 57 .21 31 22 | 229 450 2912 7907
iac n/a| 0 -1 0 35 43 -128 -.27 32 29 | 2165 193 2950 9474
Table 2.2203.1 GPS week: 2203 Day: 1 MJD: 59666
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 -17 -25 -8 .16 24 16 | 25598 -2597 2651 7719
emx n/a| 2 1 1 42 61 -34 -.23 35 30 | -19006 -738 2629 7801
esx n/a| 0 0 -2 0 -6 -39 -.07 28 23 | 3336 -3369 2631 10699
gfz n/a| 0 0 5 -14 -21 -18 -.04 33 18 | 0 -3579 2596 7799
grg n/a| 0 -3 -9 -16 22 -10 .22 40 23 | -7055 -3590 2617 7131
iac n/a| -4 1 2 46 -6 116 -.20 33 30 | -8029 -1306 2680 11154
Table 2.2203.2 GPS week: 2203 Day: 2 MJD: 59667
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 -1 -21 26 .18 36 18 | 26115 -1199 3359 9488
emx n/a| -2 3 5 -3 90 54 -.17 46 42 | -16861 -432 3381 9448
esx n/a| -1 2 -1 -12 -13 -20 -.04 30 21 | -8425 389 3293 13743
gfz n/a| -1 0 0 8 19 49 -.08 24 22 | 0 -412 3380 9299
grg n/a| 0 0 -6 -20 39 -37 .16 32 18 | -6486 9 3398 9078
iac n/a| 1 0 -5 38 -37 -50 -.18 36 33 | -7335 426 3304 12727
Table 2.2203.3 GPS week: 2203 Day: 3 MJD: 59668
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 44 -65 37 .14 44 19 | 26504 1607 3403 8350
emx n/a| -3 -3 6 27 102 46 -.17 41 34 | -22735 1201 3386 8566
esx n/a| 0 0 -2 -18 -4 29 -.06 30 23 | -10651 3864 5485 9350
gfz n/a| -1 0 2 -46 -10 17 .01 31 17 | 0 2353 3356 7914
grg n/a| 1 0 -5 -19 21 55 .23 36 19 | -6729 1523 3347 7738
iac n/a| 3 -2 -7 72 -35 -136 -.19 34 31 | -6525 3414 5495 10615
Table 2.2203.4 GPS week: 2203 Day: 4 MJD: 59669
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 4 10 -14 -6 .15 23 19 | 26770 326 3077 7559
emx n/a| 1 0 2 24 7 -2 -.15 30 26 | -11616 577 3082 7547
esx n/a| -1 2 0 -44 0 -16 -.01 30 21 | -8822 681 3007 5790
gfz n/a| 1 0 2 10 6 -42 -.05 31 17 | 0 -451 3085 7422
grg n/a| 1 -1 -15 -25 42 -40 .21 31 19 | -7271 -400 3065 6919
iac n/a| 2 -6 5 47 -35 101 -.33 38 33 | -5240 190 3004 7976
Table 2.2203.5 GPS week: 2203 Day: 5 MJD: 59670
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 15 -42 27 .10 25 17 | 26256 156 3113 9842
emx n/a| -1 0 2 38 35 -64 -.08 32 28 | -18252 41 3106 9624
esx n/a| 0 1 -1 6 -21 -28 -.09 23 17 | 2597 -207 3078 8795
gfz n/a| -1 -1 -1 -13 3 -80 -.03 32 21 | 0 57 2972 9405
grg n/a| -1 -3 -10 -36 36 26 .23 25 18 | -7363 -294 3190 9327
iac n/a| 0 1 7 29 10 82 -.21 34 30 | -5194 -1545 3082 10285
Table 2.2203.6 GPS week: 2203 Day: 6 MJD: 59671
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 4 17 -38 22 .16 19 13 | 36880 4320 3920 9276
emx n/a| 0 -1 8 24 40 19 -.12 34 25 | -8271 3255 3923 9084
esx n/a| 0 -1 0 -20 22 -15 -.12 31 24 | 2645 3628 3849 8275
gfz n/a| -1 0 1 -68 -14 -7 -.06 37 19 | 0 4009 3912 8802
grg n/a| 0 0 -10 -20 2 6 .14 24 19 | -294 4300 3922 8549
iac n/a| 1 1 -4 97 -11 -17 -.19 33 27 | 4322 1664 3846 9682
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 3.2203.0 GPS week: 2203 Day: 0 MJD: 59665
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 655 43 35 44 27 29 42 17 | 95 69 59 76 63 79 70
R02 | 2927 9 14 15 15 13 32 7 | 59 57 65 57 56 62 58
R03 | 454 12 14 14 11 11 22 6 | 77 65 77 72 70 72 72
XR04M | 595 8 14 15 --- 12 20 6 | 89 82 96 --- 90 83 88
R05M | 1401 21 25 32 28 14 20 10 | 45 41 63 58 43 51 46
R07M | 1149 12 22 16 14 8 45 9 | 64 51 60 75 65 94 66
R08M | 1967 13 15 21 16 16 43 9 | 61 56 56 67 60 82 61
R09M | 924 16 20 12 18 15 18 7 | 25 34 31 31 26 31 26
R12 | 1756 21 24 17 24 13 26 9 | 94 66 85 80 82 91 82
R13M | 1486 19 43 30 23 45 38 14 | 96 75 75 99 111 115 92
R14M | 2479 8 37 22 19 14 17 9 | 61 41 75 69 65 73 62
R15M | 1124 8 28 17 12 23 21 8 | 75 49 77 63 82 57 68
R17E | 1626 10 26 13 16 13 17 7 | 27 24 25 27 33 24 24
R18E | 768 8 14 18 36 31 18 10 | 34 24 34 38 43 34 30
R19E | 1484 22 86 35 40 31 42 19 | 41 49 31 50 47 35 32
R20E | 1464 35 49 55 70 59 33 23 | 63 46 81 78 72 60 57
R21E | 946 14 16 17 20 28 25 9 | 22 27 25 30 33 27 22
R22E | 1187 47 34 45 54 78 54 24 | 56 58 93 99 107 72 70
R24E | 716 14 22 17 19 15 17 7 | 44 40 52 48 49 50 45
------+-----------------------------------------+-------------------------------------
RMS | 1496 22 34 27 30 31 32 |T 59 50 61 62 63 62 56
WRMS | 1496 15 24 20 18 22 29 |NE 81 64 71 71 67 76 70
MEDI | 1187 14 24 17 19 15 25 |MD 61 49 63 63 63 62 61
Table 3.2203.1 GPS week: 2203 Day: 1 MJD: 59666
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 641 45 28 42 33 31 31 16 | 67 42 38 58 49 51 45
R02 | 3988 8 14 20 27 10 15 7 | 39 45 49 32 40 32 38
R03 | 523 8 13 10 16 13 19 6 | 59 52 52 62 53 57 55
XR04M | 525 9 12 15 --- 12 22 7 | 66 61 69 --- 68 66 65
R05M | 1904 19 23 28 21 17 24 10 | 31 38 54 50 33 39 36
R07M | 606 12 27 17 10 12 46 10 | 50 35 41 52 52 73 47
R08M | 2401 6 20 12 15 17 37 8 | 39 33 41 43 39 70 41
R09M | 2130 16 20 11 15 24 17 7 | 26 30 24 27 20 27 22
XR11M | 3454 --- --- --- --- --- 7 0 | --- --- --- --- --- 53 51
R12 | 1420 23 27 11 12 19 25 9 | 66 44 59 56 48 48 54
R13M | 960 22 48 41 30 78 36 19 | 71 44 51 68 105 71 65
R14M | 2365 10 23 21 17 19 31 9 | 42 31 50 32 40 59 40
R15M | 1428 13 25 19 10 9 28 8 | 53 44 64 50 53 53 51
R17E | 842 9 17 16 14 14 29 7 | 25 26 27 28 33 50 27
R18E | 612 6 13 18 43 36 21 11 | 39 39 42 56 43 43 39
R19E | 1573 30 82 41 48 30 47 21 | 42 30 47 51 44 26 27
R20E | 1347 39 45 47 50 48 63 21 | 55 44 51 75 63 76 43
R21E | 1229 11 18 19 18 19 22 8 | 22 22 25 27 33 42 22
R22E | 1160 61 71 53 88 118 37 33 | 42 34 58 125 159 76 69
R24E | 959 10 21 22 17 21 26 8 | 45 46 54 44 50 44 44
------+-----------------------------------------+-------------------------------------
RMS | 1676 24 35 28 33 40 33 |T 46 38 47 52 53 52 44
WRMS | 1676 16 30 22 18 23 30 |NE 57 45 49 52 47 47 48
MEDI | 1229 12 23 19 17 19 26 |MD 42 39 50 50 48 51 43
Table 3.2203.2 GPS week: 2203 Day: 2 MJD: 59667
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 836 40 26 26 17 9 31 11 | 73 48 42 52 56 62 51
R02 | 4887 14 14 9 10 15 35 7 | 45 43 43 35 51 34 39
R03 | 736 15 15 11 14 8 21 6 | 61 60 66 46 61 67 58
XR04M | 629 10 18 13 --- 11 38 9 | 69 69 66 --- 74 86 70
R05M | 1165 21 25 21 9 12 30 9 | 38 38 54 45 43 53 43
R07M | 779 9 25 8 26 11 14 7 | 50 41 51 72 53 45 52
R08M | 964 13 18 13 20 20 19 7 | 52 38 40 47 63 46 46
R09M | 3491 25 22 13 14 21 24 8 | 30 24 30 30 21 30 23
XR11M | 3919 --- --- 9 --- --- 16 12 | --- --- 28 --- --- 38 34
R12 | 1372 10 35 11 15 18 40 9 | 81 61 75 89 76 98 79
R13M | 1100 24 58 38 24 34 42 16 | 90 52 48 90 86 95 74
R14M | 1363 9 22 11 10 22 18 7 | 48 33 50 41 56 54 46
R15M | 1360 12 19 13 16 14 22 7 | 53 43 55 40 57 48 48
R17E | 606 13 23 14 14 15 23 7 | 28 30 26 30 31 37 26
R18E | 681 14 20 14 22 31 14 9 | 45 42 43 48 51 46 44
R19E | 2091 40 80 26 30 27 44 18 | 38 42 40 55 55 46 40
R20E | 1321 49 65 42 50 90 72 27 | 57 64 75 74 105 69 57
R21E | 1553 17 17 21 23 23 18 9 | 36 31 29 30 41 42 30
R22E | 1890 118 133 96 45 62 70 39 | 229 41 61 143 148 166 124
R24E | 1510 12 25 15 19 21 39 9 | 50 48 44 51 57 41 46
------+-----------------------------------------+-------------------------------------
RMS | 1859 36 46 30 24 32 36 |T 61 44 48 56 62 60 51
WRMS | 1859 18 42 21 22 18 33 |NE 65 53 56 55 61 65 56
MEDI | 1321 14 23 13 17 20 24 |MD 50 42 44 47 56 46 46
Table 3.2203.3 GPS week: 2203 Day: 3 MJD: 59668
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 680 36 19 19 21 23 39 12 | 82 53 49 54 48 81 56
R02 | 3506 13 12 9 15 11 18 5 | 47 44 48 45 53 41 45
R03 | 1027 18 14 13 10 15 30 7 | 64 57 50 59 65 36 54
XR04M | 711 12 14 16 --- 14 30 9 | 59 58 50 --- 61 70 57
R05M | 1018 21 25 22 13 15 33 9 | 47 51 59 62 66 68 57
R07M | 812 12 18 12 13 14 27 7 | 58 49 52 58 53 58 53
R08M | 933 17 22 22 16 36 28 10 | 54 43 47 48 69 43 48
R09M | 3965 21 25 8 13 19 18 7 | 34 29 30 33 30 28 27
XR11M | 3964 --- --- 9 --- --- 15 12 | --- --- 33 --- --- 32 29
R12 | 1632 18 29 12 13 17 36 9 | 71 44 60 56 55 84 59
R13M | 1169 30 54 49 22 56 53 20 | 84 47 50 86 102 119 77
R14M | 988 15 23 12 13 12 23 7 | 51 34 54 52 43 45 45
R15M | 874 13 29 11 10 11 21 7 | 60 44 52 51 60 62 52
R17E | 798 10 29 11 11 15 26 7 | 35 38 36 37 38 39 34
R18E | 808 26 21 18 18 16 19 8 | 43 60 58 61 50 65 53
R19E | 1472 42 84 51 35 100 44 27 | 38 35 42 79 139 48 55
R20E | 1512 137 70 84 49 51 51 35 | 217 52 49 123 87 131 97
R21E | 942 14 29 15 12 15 23 8 | 42 39 43 44 42 52 41
R22E | 1332 93 87 39 102 59 54 34 | 55 53 90 155 102 98 85
R24E | 1348 13 29 15 19 20 26 9 | 69 72 78 80 76 51 70
------+-----------------------------------------+-------------------------------------
RMS | 1634 44 41 30 31 36 34 |T 63 47 51 65 65 62 54
WRMS | 1634 19 34 23 17 19 31 |NE 66 49 51 53 55 60 53
MEDI | 1018 18 25 15 13 16 27 |MD 55 47 50 56 60 52 53
Table 3.2203.4 GPS week: 2203 Day: 4 MJD: 59669
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 884 32 31 27 21 42 33 14 | 68 63 40 47 26 68 48
R02 | 1672 12 10 9 19 10 24 6 | 46 39 44 47 35 50 41
R03 | 893 8 12 12 14 15 15 5 | 65 60 66 73 51 76 64
XR04M | 815 16 12 23 --- 15 20 8 | 77 71 64 --- 75 85 72
R05M | 642 9 12 26 28 16 68 13 | 41 43 44 40 41 87 41
R07M | 1194 18 15 10 16 9 29 7 | 55 43 51 51 47 43 47
R08M | 1418 21 16 20 17 12 25 8 | 47 33 54 41 36 39 41
R09M | 4355 20 17 16 15 17 29 8 | 21 30 27 26 22 31 22
XR11M | 3187 --- --- 6 --- --- 9 7 | --- --- 26 --- --- 36 31
R12 | 1059 20 21 12 11 15 25 8 | 71 51 50 57 58 66 58
R13M | 861 21 59 43 21 54 67 20 | 71 45 49 55 98 113 64
R14M | 715 9 21 23 11 17 20 7 | 49 33 60 43 48 56 46
R15M | 764 16 26 7 14 15 24 8 | 57 31 49 58 46 56 48
R17E | 683 11 25 12 14 16 17 7 | 40 41 43 44 52 39 42
R18E | 912 13 19 20 18 19 32 9 | 37 31 43 38 39 48 36
R19E | 2393 37 31 35 38 28 42 16 | 41 50 27 67 50 52 39
R20E | 1061 39 67 85 61 70 64 29 | 114 50 65 132 143 144 97
R21E | 1531 16 24 19 17 27 21 9 | 36 36 50 42 45 45 39
R22E | 639 49 44 36 87 56 53 25 | 62 44 63 92 81 57 54
R24E | 938 17 20 15 19 23 26 9 | 51 47 42 46 52 39 44
------+-----------------------------------------+-------------------------------------
RMS | 1526 23 30 30 31 31 38 |T 55 44 47 55 55 61 48
WRMS | 1526 19 26 21 17 19 33 |NE 62 53 50 56 42 65 52
MEDI | 912 17 21 19 17 17 25 |MD 51 43 49 47 48 52 44
Table 3.2203.5 GPS week: 2203 Day: 5 MJD: 59670
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 774 36 45 39 20 43 34 16 | 60 75 64 61 43 57 52
R02 | 1263 14 18 20 14 16 27 8 | 43 49 58 50 42 62 48
R03 | 549 8 11 14 20 14 18 6 | 60 58 61 70 61 75 62
XR04M | 887 14 11 19 --- 12 18 7 | 74 71 67 --- 71 70 69
R05M | 615 21 19 13 28 23 50 11 | 47 48 46 42 57 73 47
R07M | 1255 9 18 12 18 14 26 7 | 54 49 49 62 46 56 50
R08M | 1832 21 15 20 18 13 29 8 | 52 50 46 52 47 34 45
R09M | 3456 17 13 11 19 14 23 7 | 32 35 40 38 38 39 34
XR11M | 3012 --- --- 14 14 --- 20 11 | --- --- 37 22 --- 39 36
R12 | 1439 14 37 9 13 9 17 8 | 60 49 57 59 63 58 56
R13M | 653 42 48 24 28 39 39 16 | 107 91 104 106 122 109 103
R14M | 595 11 20 16 19 22 33 9 | 101 100 98 98 98 98 98
R15M | 872 8 27 8 23 11 40 9 | 68 58 64 56 66 86 64
R17E | 1240 7 25 11 19 14 15 7 | 30 37 37 39 35 30 33
R18E | 1596 13 22 12 13 16 14 6 | 38 39 40 45 41 35 38
R19E | 1979 24 50 31 58 23 41 17 | 29 64 41 60 47 31 33
R20E | 1246 59 54 41 61 45 63 24 | 63 63 54 106 88 88 62
R21E | 2402 13 24 15 13 13 16 7 | 28 29 35 31 28 27 27
R22E | 1309 46 46 51 76 46 56 24 | 69 65 83 98 73 84 66
R24E | 1424 14 23 18 14 18 22 8 | 46 52 48 43 56 43 46
------+-----------------------------------------+-------------------------------------
RMS | 1535 25 32 23 32 25 34 |T 55 56 56 59 59 59 53
WRMS | 1535 17 28 17 20 18 30 |NE 55 57 60 60 52 63 54
MEDI | 1255 14 23 15 19 16 26 |MD 54 52 49 56 56 57 48
Table 3.2203.6 GPS week: 2203 Day: 6 MJD: 59671
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 717 21 23 50 35 21 45 14 | 73 61 58 61 53 53 55
R02 | 1571 10 16 23 17 12 25 7 | 47 48 63 47 45 56 49
R03 | 592 11 10 18 12 8 34 7 | 74 67 68 80 68 71 70
XR04M | 610 10 10 19 --- 13 26 7 | 96 90 86 --- 90 104 92
R05M | 603 12 24 21 20 22 26 9 | 58 51 79 66 75 73 64
R07M | 2091 16 15 21 35 8 37 10 | 72 61 61 67 65 82 65
R08M | 1787 10 13 14 23 10 15 6 | 55 48 55 61 48 48 51
R09M | 2970 11 18 12 20 14 19 6 | 29 30 35 39 33 37 30
XR11M | 1714 --- --- 16 10 --- 23 12 | --- --- 35 18 --- 36 33
R12 | 1968 16 27 19 17 17 23 8 | 78 57 79 80 67 85 72
R13M | 910 31 49 48 62 30 21 18 | 250 248 235 255 247 248 245
R14M | 716 9 20 22 10 19 23 7 | 372 369 374 371 373 375 372
R15M | 850 7 28 11 20 18 32 8 | 177 170 179 177 177 179 176
R17E | 931 11 27 13 17 16 18 7 | 49 44 51 52 51 48 48
R18E | 1884 14 18 17 18 21 13 7 | 68 60 70 69 63 61 63
R19E | 2119 30 57 41 61 38 41 19 | 40 31 42 56 44 35 30
R20E | 1810 34 66 38 63 36 66 21 | 58 53 71 79 71 64 51
R21E | 1158 14 34 13 16 14 29 9 | 33 30 35 38 36 37 33
R22E | 2410 35 59 77 83 54 46 26 | 50 50 115 137 82 55 67
R24E | 1371 10 26 18 17 15 30 8 | 42 45 54 52 49 41 45
------+-----------------------------------------+-------------------------------------
RMS | 1620 19 34 31 37 24 33 |T 90 84 92 95 91 89 85
WRMS | 1620 13 25 24 19 19 27 |NE 68 58 67 67 58 66 61
MEDI | 1371 12 24 19 20 17 26 |MD 58 53 63 66 65 56 55
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