[IGSREPORT-28617] Wk 2204 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 22 02:21:49 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2204 (Apr 03, 2022 - Apr 09, 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 2.2204.
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:
igl2204[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2204 in the SP3 format.
igl22047.sum Combination Report for GPS Week 2204.
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 | -9.2 ns
1 | 1.4 ns
2 | -0.9 ns
3 | -0.7 ns
4 | 0.8 ns
5 | 0.9 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
----+--------+---------------
0 | GRG | R08 R17
1 | GRG | R08 R17
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 1.2204, 1a.2204).
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 2.2204.0-6)
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 3.2204.0-6).
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 2204 summary. (Apr 03, 2022 - Apr 09, 2022)
Table 1.2204.a GPS week : 2204 MJD: 59672.0-59678.0
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 15 -23 28 .11 21 15 | 35599 59 3284 8649
| 0 1 2 18 15 16 .02 | 3615 2379
emx n/a| 0 0 5 33 36 -24 -.10 36 30 | -1257 646 3226 8541
| 1 1 1 12 19 24 .06 | 15686 1281
esx n/a| 1 0 0 -12 20 -17 -.05 26 21 | -2098 -501 3220 9762
| 1 2 2 23 21 24 .04 | 7555 2297
gfz n/a| 1 1 1 -12 11 -22 .03 31 17 | 0 -114 3189 8252
| 1 1 1 18 15 23 .07 | 0 2054
grg n/a| -1 -1 -15 -10 -3 36 .23 357 25 | -879 -336 3399 8317
| 1 1 4 28 17 86 .07 | 2362 2981
iac n/a| 0 -3 0 -6 -13 -22 -.34 28 24 | 1053 -142 3235 9053
| 2 3 3 30 55 60 .06 | 3728 946
Table 1.2204.b GPS week : 2204 MJD: 59672.0-59678.0
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 | 14 16 11 10 10 16 18 |
R02 | 8 8 7 8 15 8 7 |
R03 | 8 7 6 8 6 8 5 |
R04 | 13 24 9 6 9 22 8 |
R05 | 7 9 9 9 9 8 8 |
R07 | 7 7 8 7 9 5 6 |
R08 | 9 7 6 7 9 7 6 |
R09 | 8 8 9 7 7 10 8 |
R11 | 11 13 15 19 11 10 12 |
R12 | 8 9 9 11 7 8 9 |
R13 | 15 20 21 16 19 16 17 |
R14 | 11 10 9 11 9 8 8 |
R15 | 7 9 7 8 8 8 8 |
R17 | 8 9 7 6 7 7 8 |
R18 | 8 7 7 8 7 8 8 |
R19 | 19 16 20 22 20 21 18 |
R20 | 24 21 26 23 23 23 23 |
R21 | 28 16 7 26 8 8 7 |
R22 | 28 27 26 30 22 25 29 |
R24 | 9 9 9 9 9 8 9 |
Table 1.2204.c GPS week : 2204 MJD: 59672.0-59678.0
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 2204 0 | 25 -15 274 -3704 3884 -1392 80.3 1384 1384 | -9156 0
brd 2204 1 | 28 -83 291 558 -2577 -4986 83.2 1928 1928 | 1385 0
brd 2204 2 | 62 40 230 -1266 140 2505 83.6 1486 1486 | -871 0
brd 2204 3 | 48 5 281 -144 1024 5882 82.0 1486 1486 | -709 0
brd 2204 4 | -41 -41 240 -354 1676 3936 82.9 1499 1499 | 803 0
brd 2204 5 | -62 -44 99 608 -1392 -3333 82.7 1585 1585 | 918 0
brd 2204 6 | 22 97 88 -1673 -2690 -6751 84.3 1638 1638 | 496 0
-------------+------------------------------------------------------------+----------------
brd 2204 mean| 11 -5 215 -853 9 -591 82.7 1572 1572 | -1019 0
brd 2204 sdev| 46 60 85 1519 2407 4785 1.3 176 176 | 3684 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 2.2204.0 GPS week: 2204 Day: 0 MJD: 59672
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 0 -17 -29 36 .11 23 14 | 27780 -3702 3294 7791
emx n/a| -3 2 7 21 67 -24 -.15 37 26 | -20912 -1383 3253 7525
esx n/a| 2 0 0 -19 47 -17 -.02 27 20 | -2885 -3798 3243 9625
gfz n/a| 0 0 1 -31 32 -42 .03 29 17 | 0 -3236 3230 7411
grg n/a| -2 0 -7 30 -25 37 .12 1157 29 | -6164 -5535 3860 8102
iac n/a| 3 -8 -2 52 -62 -56 -.25 32 26 | -7205 -1642 3263 8083
Table 2.2204.1 GPS week: 2204 Day: 1 MJD: 59673
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 10 -1 19 .11 20 14 | 35767 3746 3099 9329
emx n/a| 0 2 4 46 41 -54 -.16 34 31 | 14378 2865 3036 9013
esx n/a| 2 -4 1 -22 46 -65 -.03 29 21 | -4426 2986 3019 8547
gfz n/a| 3 0 1 -30 -3 -45 -.02 32 16 | 0 3059 2970 8999
grg n/a| -1 1 -19 23 -5 50 .26 1163 28 | -613 4250 3513 9717
iac n/a| -4 0 1 -31 -87 41 -.38 32 26 | 2985 767 3057 9687
Table 2.2204.2 GPS week: 2204 Day: 2 MJD: 59674
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 7 -36 21 .12 20 13 | 37146 -1562 3101 8977
emx n/a| 0 -2 2 37 38 -14 -.13 33 28 | 12113 291 3020 8814
esx n/a| 2 1 2 -14 18 -8 -.00 26 22 | -1675 -1897 3020 7977
gfz n/a| 2 2 0 19 16 14 -.08 38 20 | 0 -1134 3033 8582
grg n/a| -1 -2 -17 -40 -10 -2 .23 30 22 | 57 -1738 3080 8265
iac n/a| -4 -1 3 -13 20 -22 -.30 32 26 | 2062 -640 3023 9281
Table 2.2204.3 GPS week: 2204 Day: 3 MJD: 59675
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 36 -31 26 .10 24 18 | 35268 -871 3413 8352
emx n/a| 2 0 7 30 24 -7 .01 41 34 | -20341 127 3429 8426
esx n/a| 1 3 -3 -49 -12 10 -.07 25 23 | -5849 -2349 3358 10181
gfz n/a| 1 2 -1 -1 5 6 -.00 33 18 | 0 -1642 3232 8058
grg n/a| -2 -2 -20 -17 -16 69 .19 50 25 | -352 -1033 3422 7913
iac n/a| 0 -5 3 -8 34 -111 -.33 26 25 | 788 -755 3353 8674
Table 2.2204.4 GPS week: 2204 Day: 4 MJD: 59676
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 0 18 -32 0 .12 21 16 | 37136 1383 3404 9174
emx n/a| -2 1 5 51 4 -2 -.13 37 31 | 9274 899 3426 9141
esx n/a| 1 0 -3 -11 18 0 -.06 26 22 | 14014 828 3352 10759
gfz n/a| 2 1 1 -1 -4 -37 .15 27 16 | 0 536 3314 8320
grg n/a| -2 -3 -17 -39 28 201 .36 42 29 | 72 1047 3337 8695
iac n/a| 0 -4 2 3 62 -75 -.38 27 26 | 2894 521 3373 9653
Table 2.2204.5 GPS week: 2204 Day: 5 MJD: 59677
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 0 16 -1 41 .10 19 13 | 37609 984 3472 9040
emx n/a| 0 1 4 21 28 -63 -.07 37 33 | -11442 499 3483 9064
esx n/a| 0 0 2 11 0 -27 -.05 27 19 | -9749 215 3408 11124
gfz n/a| 1 1 4 -23 5 -24 .09 30 17 | 0 880 3386 8508
grg n/a| 1 -1 -13 -6 0 -59 .20 37 26 | 563 439 3445 8293
iac n/a| 0 -2 -4 -6 -16 41 -.41 25 22 | 2845 -216 3411 9550
Table 2.2204.6 GPS week: 2204 Day: 6 MJD: 59678
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 5 35 -33 52 .14 21 16 | 38488 439 3205 7886
emx n/a| 0 0 8 23 49 -6 -.03 36 30 | 8125 1225 2940 7805
esx n/a| 0 0 1 20 23 -11 -.13 24 17 | -4118 505 3145 10122
gfz n/a| 1 0 0 -18 32 -31 .02 30 16 | 0 733 3164 7890
grg n/a| -1 -2 -10 -22 5 -38 .26 21 17 | 283 215 3136 7240
iac n/a| 0 1 -4 -43 -47 23 -.33 23 20 | 3006 969 3167 8444
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 3.2204.0 GPS week: 2204 Day: 0 MJD: 59672
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 949 32 22 41 26 35 21 14 | 85 78 75 74 62 71 72
R02 | 2391 10 13 18 15 20 32 8 | 52 44 57 50 50 42 48
R03 | 783 10 22 9 14 15 33 8 | 70 66 77 80 77 83 74
XR04 | 727 9 19 28 --- 48 22 13 | 88 78 81 --- 88 85 80
R05 | 694 10 17 17 17 14 18 7 | 53 52 64 53 60 61 56
R07 | 1641 8 20 15 16 21 18 7 | 74 67 68 80 69 78 72
R08 | 801 15 16 18 22 3957 18 9 | 68 62 61 70 9999 63 64
R09 | 1551 12 18 20 15 20 25 8 | 37 37 43 47 37 52 39
XR11 | 1577 --- 22 17 11 --- 23 10 | --- 31 39 35 --- 35 33
R12 | 2557 12 27 20 13 20 14 8 | 69 46 75 71 65 68 66
R13 | 1388 24 44 37 38 28 28 14 | 95 50 68 109 91 89 81
R14 | 843 12 23 19 16 54 17 11 | 56 32 62 55 45 62 49
R15 | 1084 13 22 7 15 19 17 7 | 79 61 70 67 77 71 71
R17E | 677 9 28 13 15 2899 12 7 | 113 109 114 114 9999 108 111
R18E | 1006 11 23 19 15 19 22 8 | 81 76 88 87 89 86 83
R19E | 1723 28 60 34 43 52 45 19 | 54 46 58 67 66 63 49
R20E | 1150 38 82 36 67 40 53 23 | 74 76 85 112 82 75 78
R21E | 1266 26 32 26 33 161 29 27 | 77 64 74 83 170 67 69
R22E | 947 63 72 63 57 39 79 28 | 46 83 108 92 85 81 66
R24E | 1547 9 32 16 11 20 28 8 | 75 86 77 78 85 88 79
------+-----------------------------------------+-------------------------------------
RMS | 1384 23 37 27 29 1157 32 |T 70 62 72 74 76 71 67
WRMS | 1384 14 26 20 17 29 26 |NE 68 54 64 65 65 66 61
MEDI | 1084 12 22 19 16 28 22 |MD 74 62 70 74 77 71 69
Table 3.2204.1 GPS week: 2204 Day: 1 MJD: 59673
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 641 36 17 50 30 28 33 15 | 58 37 46 44 37 56 41
R02 | 5188 19 11 14 15 19 27 8 | 41 36 38 35 32 31 33
R03 | 626 14 18 17 15 12 17 7 | 49 44 65 62 54 58 54
XR04 | 891 21 21 26 --- 105 34 24 | 60 58 69 --- 84 63 51
R05 | 1321 12 19 22 26 12 30 9 | 39 37 52 45 31 53 40
R07 | 629 6 18 16 12 11 26 6 | 47 39 47 52 46 53 46
R08 | 769 12 14 16 15 2497 17 7 | 43 38 46 49 9999 40 43
R09 | 1276 12 15 17 18 22 23 8 | 34 35 38 45 38 37 35
XR11 | 1240 --- 30 15 22 --- 21 13 | --- 20 29 34 --- 27 23
R12 | 2493 12 31 17 14 23 29 9 | 52 31 54 56 71 39 49
R13 | 1996 16 63 50 41 56 36 19 | 67 43 51 87 92 90 67
R14 | 1798 9 27 25 14 31 25 9 | 40 27 53 36 26 55 37
R15 | 1676 11 25 12 13 26 28 8 | 65 50 63 67 54 73 60
R17E | 1152 11 30 18 12 4252 15 8 | 94 84 84 95 9999 90 89
R18E | 1884 9 22 15 19 12 16 7 | 55 53 58 67 60 47 56
R19E | 1046 27 45 30 43 44 32 16 | 39 50 47 58 40 40 37
R20E | 1992 34 65 34 61 36 54 21 | 42 50 72 84 67 54 52
R21E | 1761 18 28 20 21 78 19 15 | 46 45 47 51 103 44 49
R22E | 1683 43 57 60 82 46 76 27 | 41 44 72 54 69 81 44
R24E | 1639 9 36 20 16 18 15 8 | 58 66 64 61 67 60 60
------+-----------------------------------------+-------------------------------------
RMS | 1927 20 34 29 32 1162 32 |T 51 44 54 56 57 54 48
WRMS | 1927 14 30 21 16 28 26 |NE 49 38 50 51 51 51 44
MEDI | 1321 12 25 18 18 28 26 |MD 47 43 52 54 54 53 46
Table 3.2204.2 GPS week: 2204 Day: 2 MJD: 59674
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 680 25 21 26 26 22 26 11 | 77 63 59 73 76 61 66
R02 | 1313 14 13 9 19 9 22 6 | 50 48 50 35 46 50 46
R03 | 886 8 11 9 19 19 12 6 | 63 62 63 63 70 70 64
XR04 | 659 17 13 11 --- 30 17 9 | 65 56 50 --- 59 53 55
R05 | 1147 16 23 19 22 24 19 9 | 44 56 61 64 48 56 50
R07 | 573 10 20 12 17 10 34 8 | 71 61 74 74 75 97 74
R08 | 916 8 14 12 16 16 17 6 | 62 55 60 63 687 64 58
R09 | 1451 13 16 11 17 39 20 9 | 31 38 30 36 41 38 31
XR11 | 1183 --- 27 15 21 --- 38 15 | --- 45 35 46 --- 41 36
R12 | 1799 14 33 16 17 21 15 8 | 58 40 59 57 55 52 53
R13 | 1216 22 59 54 42 69 24 20 | 80 37 31 72 109 65 62
R14 | 2124 8 28 22 18 11 23 8 | 46 31 52 39 59 51 44
R15 | 2068 10 22 10 14 21 15 6 | 66 60 60 54 56 64 60
R17E | 2350 9 27 10 16 13 16 6 | 73 65 70 71 434 68 70
R18E | 1031 10 20 17 11 15 22 7 | 64 61 70 61 65 67 64
R19E | 1989 28 61 40 60 43 46 20 | 41 51 55 60 53 51 40
R20E | 1519 37 60 48 91 42 66 25 | 59 86 97 109 72 77 72
R21E | 1544 11 25 10 23 12 19 7 | 66 56 64 73 92 54 65
R22E | 1397 44 45 48 87 47 70 25 | 44 54 78 50 91 74 54
R24E | 1208 14 34 15 17 19 19 8 | 64 64 62 61 67 52 60
------+-----------------------------------------+-------------------------------------
RMS | 1485 20 33 26 38 30 32 |T 59 54 59 61 118 60 56
WRMS | 1485 13 28 22 20 22 26 |NE 59 50 52 56 115 58 53
MEDI | 1216 14 23 15 19 21 20 |MD 63 56 60 61 67 56 58
Table 3.2204.3 GPS week: 2204 Day: 3 MJD: 59675
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 746 26 24 19 20 24 17 10 | 79 69 64 68 63 72 68
R02 | 779 19 11 18 18 15 11 7 | 61 51 39 45 52 44 47
R03 | 1303 11 9 18 9 14 27 7 | 61 61 48 55 53 78 58
XR04 | 711 7 9 11 --- 18 13 6 | 54 51 48 --- 48 59 52
R05 | 1151 21 21 16 22 13 24 9 | 40 42 46 44 35 50 39
R07 | 612 11 14 18 16 17 20 7 | 57 59 46 59 57 69 57
R08 | 796 16 18 11 19 14 17 7 | 56 46 50 60 563 45 51
R09 | 2266 12 20 14 14 23 11 7 | 17 22 31 28 16 20 20
XR11 | 1481 --- --- 20 17 --- 37 18 | --- --- 21 27 --- 55 29
R12 | 1189 15 39 11 15 45 20 10 | 60 35 52 53 75 70 55
R13 | 968 39 56 39 22 39 10 16 | 90 30 43 77 78 64 63
R14 | 1549 19 27 24 16 15 35 10 | 51 22 52 35 51 33 37
R15 | 2226 12 30 11 12 21 14 7 | 58 47 53 49 68 48 52
R17E | 3004 9 24 11 14 15 12 6 | 48 46 45 49 266 43 46
R18E | 953 15 21 18 13 19 17 7 | 44 45 58 48 61 54 50
R19E | 1658 21 78 40 71 39 34 21 | 53 69 43 83 72 41 51
R20E | 979 31 75 48 73 38 42 23 | 57 58 74 96 53 56 58
R21E | 1585 21 39 21 21 157 29 26 | 69 63 67 70 127 78 60
R22E | 1329 60 80 45 69 98 51 29 | 32 50 69 52 129 48 44
R24E | 1329 11 27 15 16 17 25 8 | 34 37 40 42 41 37 36
------+-----------------------------------------+-------------------------------------
RMS | 1485 24 41 25 33 50 26 |T 53 47 49 54 100 53 48
WRMS | 1485 18 34 23 18 25 25 |NE 57 44 45 50 96 54 48
MEDI | 1189 16 24 18 17 19 20 |MD 56 47 48 52 61 50 51
Table 3.2204.4 GPS week: 2204 Day: 4 MJD: 59676
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 587 24 22 14 20 37 23 10 | 69 63 66 65 36 54 60
R02 | 941 18 23 13 9 92 28 14 | 48 40 53 54 136 55 56
R03 | 481 8 10 10 9 22 16 5 | 65 65 66 66 74 78 67
XR04 | 608 11 9 17 --- 32 23 9 | 78 77 70 --- 102 76 77
R05 | 1272 19 17 15 14 20 35 9 | 44 46 48 55 67 68 50
R07 | 806 15 9 19 19 33 27 9 | 58 54 49 59 60 45 52
R08 | 955 15 7 14 11 43 30 9 | 48 45 38 44 615 43 44
R09 | 3648 12 16 15 18 20 16 7 | 35 42 38 40 30 36 34
XR11 | 1399 --- 26 17 12 28 25 10 | --- 45 33 40 27 41 34
XR12 | 881 9 --- 10 15 28 11 7 | 63 --- 62 65 48 61 60
R13 | 716 27 67 42 17 74 28 18 | 80 31 48 75 119 83 66
R14 | 1715 17 24 23 18 22 21 9 | 51 35 55 29 59 34 40
R15 | 1571 10 23 14 16 24 20 7 | 72 59 71 56 84 64 65
R17E | 1497 9 24 15 14 21 15 7 | 69 59 73 69 204 60 67
R18E | 1359 12 18 18 13 19 19 7 | 60 61 68 66 79 59 63
R19E | 826 25 74 36 56 39 38 20 | 42 57 42 74 91 43 48
R20E | 999 41 64 54 56 59 40 23 | 56 58 84 82 81 59 58
R21E | 1054 11 27 15 18 18 17 7 | 78 67 78 76 75 59 71
R22E | 2003 37 67 48 53 59 44 22 | 59 52 68 68 76 43 47
R24E | 1850 12 26 15 17 24 26 8 | 47 46 47 50 54 42 45
------+-----------------------------------------+-------------------------------------
RMS | 1499 21 37 26 27 42 27 |T 59 52 57 59 105 55 55
WRMS | 1499 16 31 22 16 29 26 |NE 59 50 53 54 112 56 54
MEDI | 999 15 23 15 17 28 23 |MD 59 54 55 65 75 55 56
Table 3.2204.5 GPS week: 2204 Day: 5 MJD: 59677
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 764 33 42 38 26 58 22 16 | 57 69 58 66 31 44 49
R02 | 2213 13 11 13 19 22 24 7 | 43 41 47 44 35 34 39
R03 | 493 9 14 16 20 36 17 8 | 51 51 65 62 45 58 54
XR04 | 1071 19 14 24 --- 107 31 22 | 61 56 50 --- 82 65 52
R05 | 1040 11 13 16 15 14 27 7 | 40 38 38 50 34 45 39
R07 | 640 7 10 10 15 14 13 5 | 46 48 50 56 50 42 48
R08 | 2024 9 14 14 18 23 13 6 | 49 47 46 53 595 44 48
R09 | 3626 13 23 14 16 35 29 9 | 40 51 52 58 38 57 47
XR11 | 1023 --- --- 18 14 24 16 10 | --- --- 26 37 26 36 31
R12 | 834 16 27 14 19 16 20 8 | 55 46 49 44 44 51 47
R13 | 637 27 56 42 25 36 24 15 | 72 41 41 63 73 67 57
R14 | 1175 9 32 18 14 15 16 7 | 40 27 47 52 49 48 42
R15 | 1411 14 26 13 14 23 16 7 | 56 45 47 47 62 48 49
R17E | 1219 11 21 12 14 15 18 6 | 62 59 66 68 197 69 64
R18E | 908 10 19 18 18 25 20 8 | 49 42 53 54 48 54 49
R19E | 919 23 53 33 54 85 35 20 | 47 50 54 66 67 47 42
R20E | 1570 40 64 51 60 62 35 22 | 61 56 77 86 72 70 61
R21E | 1498 9 27 15 14 20 25 8 | 64 65 64 65 51 70 62
R22E | 1574 33 80 56 69 48 53 24 | 42 69 74 66 57 39 45
R24E | 2437 12 30 12 26 18 10 8 | 48 46 51 59 56 50 49
------+-----------------------------------------+-------------------------------------
RMS | 1585 19 37 27 30 37 25 |T 51 49 52 57 85 51 48
WRMS | 1585 13 33 19 17 26 22 |NE 50 46 47 52 89 49 46
MEDI | 1071 13 26 16 18 23 20 |MD 49 48 50 58 50 48 48
Table 3.2204.6 GPS week: 2204 Day: 6 MJD: 59678
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1073 44 47 41 27 41 28 17 | 79 89 86 82 56 56 69
R02 | 3566 15 20 14 15 15 15 7 | 51 52 44 53 50 34 45
R03 | 901 9 15 7 9 17 11 5 | 72 71 78 83 79 84 78
XR04 | 1173 13 15 14 --- 8 20 7 | 87 78 85 --- 70 87 81
R05 | 839 14 17 19 26 13 19 8 | 54 53 64 60 57 63 56
R07 | 652 12 11 16 14 11 19 6 | 67 66 60 67 62 62 63
R08 | 2148 14 13 8 13 10 20 6 | 59 65 62 70 671 69 63
R09 | 3243 16 22 12 17 12 27 8 | 47 47 49 53 40 53 45
XR11 | 1539 --- 28 17 23 18 29 11 | --- 28 42 36 23 59 39
R12 | 1676 15 39 13 19 15 22 9 | 75 38 75 75 69 78 69
R13 | 1158 37 55 45 31 24 25 16 | 101 38 52 93 99 82 76
R14 | 838 12 24 14 28 17 14 8 | 62 39 65 60 59 53 56
R15 | 933 10 33 12 10 20 16 7 | 79 52 75 69 85 81 74
R17E | 831 8 27 11 23 13 21 7 | 99 90 93 103 269 100 96
R18E | 860 11 27 17 16 15 20 7 | 68 67 74 74 76 69 70
R19E | 727 26 55 37 69 24 31 18 | 63 53 61 86 49 56 54
R20E | 917 44 71 51 68 41 40 23 | 92 64 96 118 82 77 82
R21E | 1378 10 27 17 12 15 17 7 | 74 65 67 75 63 75 70
XR22E | 1096 36 --- 55 86 71 33 29 | 65 --- 71 53 62 54 50
R24E | 2057 8 31 12 19 22 22 8 | 52 47 52 58 58 47 49
------+-----------------------------------------+-------------------------------------
RMS | 1638 21 36 24 30 21 23 |T 70 58 67 72 103 66 64
WRMS | 1638 16 30 17 16 17 20 |NE 69 55 64 66 109 66 62
MEDI | 1073 14 27 14 19 15 20 |MD 68 53 65 70 62 63 63
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