[IGSREPORT-26200] Wk 2022 IGLOS Final Orbits
acc
acc at igs.org
Thu Oct 25 23:40:59 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2022 (Oct 07, 2018 - Oct 13, 2018)
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 2.2022.
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:
igl2022[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2022 in the SP3 format.
igl20227.sum Combination Report for GPS Week 2022.
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 | 13.1 ns
1 | 13.5 ns
2 | 6.9 ns
3 | 6.3 ns
4 | 6.1 ns
5 | 4.9 ns
6 | 5.3 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 1.2022, 1a.2022).
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 2.2022.0-6)
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 3.2022.0-6).
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 2022 summary. (Oct 07, 2018 - Oct 13, 2018)
Table 1.2022.a GPS week : 2022 MJD: 58398.0-58404.0
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| -3 0 -9 -1 -34 15 .00 42 35 | 1337 733 3212 9861
| 1 1 3 10 27 35 .04 | 1318 1199
cof n/a| -3 0 -12 5 -36 23 .03 43 36 | 1333 743 3210 9861
| 1 1 3 21 19 45 .04 | 1319 1195
esx n/a| 0 0 2 19 11 59 .13 15 12 | 10566 1229 3235 11760
| 0 0 1 7 9 28 .03 | 7790 2656
gfz n/a| 0 0 13 -5 16 21 .07 37 35 | -272 991 3215 9689
| 1 1 1 26 24 17 .02 | 803 1371
grg n/a| 1 1 -5 -32 -4 -170 -.35 32 29 | 7122 903 3278 9493
| 1 1 3 22 18 86 .03 | 3030 1303
Table 1.2022.b GPS week : 2022 MJD: 58398.0-58404.0
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 | 34 28 34 32 30 28 31 |
R02 | 12 11 9 14 17 14 15 |
R03 | 12 14 12 11 12 14 15 |
R04 | 12 12 11 10 11 11 19 |
R05 | 13 11 12 13 11 12 20 |
R07 | 18 16 14 11 17 14 13 |
R08 | 12 11 13 11 13 13 14 |
R09 | 11 7 7 6 9 10 9 |
R10 | 7 9 12 11 11 14 16 |
R11 | 9 8 9 8 10 11 14 |
R13 | 10 16 11 12 13 17 11 |
R14 | 10 9 10 11 9 9 9 |
R15 | 17 13 13 16 19 22 17 |
R16 | 21 21 25 22 16 22 25 |
R17 | 16 12 12 14 17 13 17 |
R18 | 12 9 11 10 11 9 10 |
R19 | 35 33 27 24 28 29 32 |
R20 | 12 15 17 18 17 13 17 |
R21 | 13 14 15 14 14 10 13 |
R22 | 42 13 13 14 19 13 13 |
R23 | 8 9 12 12 12 12 13 |
R24 | 24 23 15 16 13 15 16 |
R26 | 0 0 0 0 0 0 0 |
Table 1.2022.c GPS week : 2022 MJD: 58398.0-58404.0
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 2022 0 | 336 -234 192 605 -4111 -2047 163.4 >>>>> >>>>> | 13135 0
brd 2022 1 | 1155 4886 -272 249 -18620 -40950 -24.1 >>>>> >>>>> | 13473 0
brd 2022 2 | 91 2053 -64 -211 -948 1904 63.4 >>>>> >>>>> | 6854 0
brd 2022 3 |-6338 549 -436 2364 -545 11090 10.7 >>>>> >>>>> | 6320 0
brd 2022 4 | -139 122 21630 5818 12680 5735 94.2 >>>>> >>>>> | 6112 0
brd 2022 5 | -130 1231 -6974 -1024 -4105 4227 -30.8 >>>>> >>>>> | 4941 0
brd 2022 6 | 164 13860 -3347 -12550 -634 -8447 <<<< >>>>> >>>>> | 5311 0
-------------+------------------------------------------------------------+----------------
brd 2022 mean| -694 3209 1532 -678 -2326 -4069 23.4 >>>>> >>>>> | 8020 0
brd 2022 sdev| 2526 4999 9233 5704 9173 17387 91.5 15767 15767 | 3665 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 2.2022.0 GPS week: 2022 Day: 0 MJD: 58398
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 -7 0 -27 38 -.01 42 33 | 960 205 3410 8812
cof n/a| -3 0 -11 10 -33 59 .04 43 35 | 963 199 3409 8808
esx n/a| 1 0 5 21 -7 -1 .16 23 16 | 4421 -3823 3705 10299
gfz n/a| 0 0 12 -24 23 36 .08 40 36 | -910 284 3397 8712
grg n/a| 0 3 -9 -34 29 -18 -.36 31 31 | 12085 -20 3410 8437
Table 2.2022.1 GPS week: 2022 Day: 1 MJD: 58399
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 -8 -11 -75 -2 -.00 40 39 | 1486 2763 3087 10147
cof n/a| -2 0 -10 -29 -61 10 -.01 43 40 | 1486 2765 3082 10149
esx n/a| -1 0 2 10 20 78 .12 15 13 | 22953 4553 3092 12195
gfz n/a| 1 1 14 -3 60 22 .04 35 45 | -1371 3418 3083 9872
grg n/a| 1 1 -5 2 -9 -162 -.30 29 23 | 10812 3431 3080 9639
Table 2.2022.2 GPS week: 2022 Day: 2 MJD: 58400
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| -3 0 -5 9 -56 -48 .04 40 32 | -696 218 2916 9284
cof n/a| -3 -1 -8 28 -63 -42 .09 40 33 | -693 214 2910 9287
esx n/a| 0 -1 1 30 16 54 .15 15 11 | 9926 710 2924 11179
gfz n/a| -1 -1 15 -17 11 14 .10 37 32 | -656 838 2915 9105
grg n/a| 2 3 -4 -57 -18 -123 -.37 29 26 | 5929 435 3140 9028
Table 2.2022.3 GPS week: 2022 Day: 3 MJD: 58401
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 0 -8 3 -46 3 -.07 38 31 | 627 247 3168 8784
cof n/a| -2 1 -11 12 -31 -19 -.01 37 31 | 598 301 3171 8785
esx n/a| 0 0 1 15 11 80 .13 14 12 | 1770 1867 3176 10964
gfz n/a| 0 0 13 47 17 7 .06 36 30 | -1 490 3160 8793
grg n/a| 2 0 0 -47 -22 -228 -.39 30 27 | 6003 673 3170 8268
Table 2.2022.4 GPS week: 2022 Day: 4 MJD: 58402
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| -5 0 -8 7 6 43 .04 44 35 | 1670 1899 3458 9194
cof n/a| -5 1 -13 26 -14 59 .01 46 37 | 1666 1907 3455 9192
esx n/a| 0 0 2 9 5 57 .14 14 11 | 4710 3242 3455 11077
gfz n/a| 1 0 12 1 24 47 .05 37 40 | 0 1782 3463 9023
grg n/a| 1 1 -4 -7 0 -145 -.34 31 30 | 5385 1725 3632 8918
Table 2.2022.5 GPS week: 2022 Day: 5 MJD: 58403
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| -4 -3 -13 -18 -34 15 -.00 44 36 | 1650 -801 3559 11301
cof n/a| -4 -1 -18 -18 -16 12 .05 47 41 | 1648 -787 3561 11305
esx n/a| 0 0 1 22 14 70 .08 12 10 | 11932 331 3390 13206
gfz n/a| -1 2 13 -3 -15 27 .07 35 33 | -90 -1003 3574 10948
grg n/a| 2 0 -4 -49 7 -258 -.34 33 32 | 4282 -468 3645 11121
Table 2.2022.6 GPS week: 2022 Day: 6 MJD: 58404
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 -15 -3 -10 56 .03 42 36 | 3665 604 2889 11509
cof n/a| -4 -2 -18 10 -33 83 .01 45 37 | 3663 605 2886 11507
esx n/a| 0 1 3 26 19 72 .10 15 13 | 18250 1726 2904 13402
gfz n/a| 0 0 15 -36 -7 -3 .10 37 30 | 1119 1130 2917 11371
grg n/a| 2 0 -9 -33 -16 -258 -.35 40 35 | 5359 546 2870 11044
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 3.2022.0 GPS week: 2022 Day: 0 MJD: 58398
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg IGL | cod cof esx gfz grg IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 112 107 37 56 20 33 | 107 105 54 69 43 38
R02 |>>>>> 21 30 12 31 24 11 | 77 85 60 51 72 62
R03 | ---- 29 37 13 29 19 12 | 84 87 56 50 68 61
R04 | ---- 31 29 10 24 19 11 | 96 96 78 68 73 77
R05 | ---- 33 29 14 33 16 13 | 99 100 86 71 93 86
R07 |>>>>> 35 39 17 48 32 17 | 90 94 58 52 87 66
R08 |>>>>> 22 23 9 35 19 11 | 78 78 57 38 68 59
R09 |>>>>> 15 17 8 23 27 10 | 26 28 35 31 43 33
R10 |>>>>> 12 12 6 19 15 7 | 27 31 36 41 39 34
R11 |>>>>> 12 18 7 31 15 9 | 35 36 38 40 42 37
R13 |>>>>> 9 9 5 31 22 10 | 36 34 42 39 44 40
R14 |>>>>> 12 18 13 22 20 9 | 38 39 48 40 35 39
R15 |>>>>> 37 40 15 51 27 17 | 50 52 42 45 33 39
R16 | ---- 30 24 23 27 56 20 | 46 55 50 41 39 43
R17 |>>>>> 33 38 16 42 26 15 | 84 87 49 29 70 55
R18 |>>>>> 19 21 7 34 24 11 | 58 55 59 38 69 57
R19 |>>>>> 96 100 41 72 44 34 | 112 115 39 48 72 47
R20 |>>>>> 24 30 10 26 24 11 | 66 70 60 52 79 62
R21 |>>>>> 32 32 8 40 15 13 | 73 72 41 33 61 47
R22 |>>>>> 64 65 77 70 67 41 | 128 127 102 134 129 112
R23 |>>>>> 19 21 8 17 10 7 | 52 53 72 55 70 66
R24 |>>>>> 27 42 24 50 61 23 | 92 111 85 70 97 84
XR26 | ---- 5 74 --- --- --- 0 | 573 521 --- --- --- 573
------+------------------------------------+--------------------------------
RMS |>>>>> 42 43 23 40 31 |T 92 92 56 51 64 79
WRMS |>>>>> 33 35 16 36 31 |NE 92 92 56 51 64 79
MEDI |>>>>> 27 30 12 31 22 |MD 77 78 54 45 68 57
Table 3.2022.1 GPS week: 2022 Day: 1 MJD: 58399
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg IGL | cod cof esx gfz grg IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 102 116 25 55 21 28 | 85 92 44 54 52 43
R02 |>>>>> 26 27 10 29 21 11 | 60 62 50 51 47 49
R03 |>>>>> 30 30 13 34 27 13 | 67 67 55 44 58 53
R04 | ---- 26 26 12 29 23 11 | 93 91 81 70 72 78
R05 | ---- 28 23 10 32 16 11 | 76 78 74 54 81 72
R07 |>>>>> 33 29 15 41 32 15 | 68 65 47 42 72 53
R08 |>>>>> 27 30 7 37 16 11 | 64 65 47 30 47 46
R09 | ---- 18 17 4 17 10 6 | 20 22 24 28 27 23
R10 |>>>>> 14 12 9 20 23 9 | 27 28 29 32 24 26
R11 |>>>>> 11 11 8 22 19 8 | 31 32 31 36 35 32
R13 |>>>>> 12 16 14 41 41 15 | 28 29 37 32 29 31
R14 |>>>>> 24 23 6 23 14 8 | 34 38 40 41 31 36
R15 |>>>>> 37 40 14 33 18 13 | 31 38 28 37 22 26
R16 |>>>>> 28 35 24 23 60 21 | 43 53 46 49 42 43
R17 |>>>>> 39 38 9 31 14 12 | 72 72 60 57 57 59
R18 |>>>>> 13 15 11 28 13 8 | 53 54 57 45 51 52
R19 |>>>>> 103 107 33 72 42 32 | 79 84 44 54 55 45
R20 |>>>>> 19 28 14 42 31 14 | 58 63 50 51 60 50
R21 |>>>>> 34 35 14 31 26 13 | 60 61 49 48 61 52
R22 |>>>>> 46 47 8 33 13 13 | 91 90 78 103 93 83
R23 |>>>>> 24 29 9 21 15 9 | 56 59 59 58 60 58
R24 |>>>>> 22 28 26 35 65 23 | 77 79 74 76 81 75
XR26 | ---- 6 65 --- --- --- 0 | 794 658 --- --- --- 794
------+------------------------------------+--------------------------------
RMS |>>>>> 40 43 15 35 29 |T 89 86 50 49 52 81
WRMS |>>>>> 39 40 13 45 23 |NE 89 86 50 49 52 81
MEDI |>>>>> 26 29 11 31 21 |MD 60 63 47 48 52 50
Table 3.2022.2 GPS week: 2022 Day: 2 MJD: 58400
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg IGL | cod cof esx gfz grg IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 103 96 40 61 49 33 | 88 89 77 61 50 53
R02 |>>>>> 25 26 5 32 9 9 | 61 63 51 45 52 50
R03 |>>>>> 35 37 11 31 19 12 | 63 66 42 48 57 47
R04 |>>>>> 34 29 7 33 12 10 | 68 63 43 29 48 44
R05 |>>>>> 23 15 10 33 26 11 | 90 90 87 84 95 88
R07 | ---- 38 42 12 36 22 13 | 71 74 49 53 60 53
R08 |>>>>> 16 16 10 38 30 12 | 63 65 53 41 79 58
R09 |>>>>> 15 16 7 21 13 7 | 22 24 29 32 31 26
R10 |>>>>> 11 11 5 41 28 11 | 29 30 32 36 37 31
R11 |>>>>> 15 16 6 27 18 8 | 28 27 34 35 40 33
R13 |>>>>> 11 19 11 24 30 11 | 32 33 31 37 36 31
R14 |>>>>> 32 31 6 26 13 9 | 32 28 30 32 31 28
R15 | ---- 34 28 11 37 22 13 | 34 32 38 42 22 32
R16 |>>>>> 31 47 24 47 69 24 | 45 62 47 39 37 42
R17 |>>>>> 42 37 7 35 12 12 | 68 66 51 42 48 50
R18 |>>>>> 15 16 14 27 26 11 | 54 54 60 51 54 54
R19 |>>>>> 95 101 24 58 27 26 | 84 91 53 55 43 48
R20 |>>>>> 34 31 15 46 38 17 | 61 51 40 41 64 45
R21 |>>>>> 35 36 12 41 27 14 | 62 61 41 39 60 45
R22 |>>>>> 36 36 10 36 21 12 | 146 145 136 142 131 137
R23 |>>>>> 29 28 7 30 26 11 | 47 50 61 42 74 59
R24 |>>>>> 24 21 16 25 39 14 | 48 60 61 57 69 59
XR26 | ---- 5 810 --- --- --- 0 | 375 741 --- --- --- 374
------+------------------------------------+--------------------------------
RMS |>>>>> 40 40 15 37 29 |T 72 89 52 49 55 64
WRMS |>>>>> 32 33 11 32 26 |NE 72 89 52 49 55 64
MEDI |>>>>> 31 29 10 33 26 |MD 61 62 47 42 50 48
Table 3.2022.3 GPS week: 2022 Day: 3 MJD: 58401
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg IGL | cod cof esx gfz grg IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 101 97 33 64 42 31 | 88 92 61 63 44 43
R02 |>>>>> 24 23 10 40 32 13 | 61 58 41 37 63 45
R03 |>>>>> 32 28 7 32 13 10 | 65 66 41 28 39 41
R04 |>>>>> 29 26 7 27 19 10 | 82 77 65 60 65 65
R05 |>>>>> 32 38 9 35 27 13 | 60 72 52 41 64 51
R07 |>>>>> 31 31 6 32 15 10 | 75 77 51 44 58 53
R08 |>>>>> 23 28 9 38 20 11 | 69 73 53 36 59 53
R09 |>>>>> 12 13 6 18 10 6 | 12 17 20 26 22 18
R10 |>>>>> 18 18 11 30 27 11 | 23 23 27 20 32 23
R11 |>>>>> 13 15 5 27 15 7 | 19 20 22 19 27 19
R13 |>>>>> 16 16 9 30 31 11 | 28 28 33 30 41 32
R14 |>>>>> 18 17 7 29 29 11 | 30 31 31 40 32 30
R15 |>>>>> 34 39 17 38 37 16 | 36 39 31 27 37 27
R16 |>>>>> 31 37 24 37 63 22 | 47 58 35 27 50 32
R17 |>>>>> 38 39 12 34 25 13 | 67 66 37 34 47 41
R18 |>>>>> 19 25 4 22 25 9 | 46 50 47 34 61 48
R19 |>>>>> 83 48 24 43 26 23 | 83 68 44 45 45 42
R20 |>>>>> 29 33 17 48 45 18 | 68 78 61 43 53 55
R21 |>>>>> 34 31 12 40 27 14 | 66 63 42 26 58 45
R22 |>>>>> 42 44 9 41 15 13 | 90 93 98 106 90 93
R23 |>>>>> 29 26 17 15 22 12 | 38 41 61 46 40 49
R24 |>>>>> 27 50 12 34 46 16 | 56 53 65 52 82 65
XR26 | ---- 6 1130 --- --- --- 0 | 9999 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS |>>>>> 38 37 14 36 30 |T 54 56 46 40 50 44
WRMS |>>>>> 31 31 12 30 27 |NE 54 56 46 40 50 44
MEDI |>>>>> 29 31 9 34 26 |MD 60 58 42 36 47 43
Table 3.2022.4 GPS week: 2022 Day: 4 MJD: 58402
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg IGL | cod cof esx gfz grg IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 110 107 31 48 34 30 | 96 99 50 52 36 39
R02 |>>>>> 20 30 16 38 48 17 | 65 72 51 44 86 56
R03 |>>>>> 37 43 6 37 11 11 | 70 72 44 47 51 47
R04 |>>>>> 29 32 9 20 22 10 | 77 83 64 53 45 59
R05 |>>>>> 38 37 6 34 9 11 | 87 93 73 61 54 68
R07 |>>>>> 37 33 19 36 40 17 | 75 73 40 43 79 52
R08 |>>>>> 29 22 11 32 29 13 | 73 71 56 46 80 62
R09 |>>>>> 24 19 6 18 18 8 | 16 19 22 28 29 21
R10 |>>>>> 12 11 6 33 27 10 | 26 28 32 25 26 27
R11 |>>>>> 13 22 7 32 23 10 | 26 24 34 32 36 32
R13 |>>>>> 23 21 9 24 36 12 | 28 29 35 29 38 31
R14 |>>>>> 18 21 7 25 19 9 | 31 29 37 31 46 36
R15 |>>>>> 42 46 15 50 42 18 | 35 32 42 59 33 34
R16 |>>>>> 34 40 8 53 33 16 | 42 67 39 42 27 34
R17 |>>>>> 40 40 15 42 36 16 | 65 68 47 52 61 50
R18 |>>>>> 30 27 8 27 21 11 | 50 55 56 45 59 53
R19 |>>>>> 104 115 25 47 28 27 | 71 79 41 47 54 39
R20 |>>>>> 43 34 16 36 39 17 | 69 68 53 48 55 51
R21 |>>>>> 33 41 10 42 26 14 | 65 73 50 43 62 52
R22 |>>>>> 38 39 15 52 43 18 | 182 186 174 203 167 175
R23 |>>>>> 35 33 14 21 23 12 | 35 30 51 36 39 43
R24 |>>>>> 29 34 13 26 31 13 | 51 70 63 59 57 58
XR26 | ---- 6 145 --- --- --- 0 | 503 519 --- --- --- 502
------+------------------------------------+--------------------------------
RMS |>>>>> 44 46 14 37 31 |T 79 84 52 51 55 70
WRMS |>>>>> 35 37 11 40 30 |NE 79 84 52 51 55 70
MEDI |>>>>> 33 34 10 34 28 |MD 65 70 47 45 51 50
Table 3.2022.5 GPS week: 2022 Day: 5 MJD: 58403
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg IGL | cod cof esx gfz grg IGL
------+------------------------------------+--------------------------------
R01 | ---- 97 94 27 44 42 27 | 79 78 25 29 40 24
R02 |>>>>> 32 37 12 32 34 13 | 57 62 33 26 55 36
R03 |>>>>> 35 38 11 38 30 14 | 60 64 38 21 61 40
R04 |>>>>> 26 31 6 36 19 10 | 60 64 47 32 48 46
R05 |>>>>> 34 32 9 32 21 11 | 85 83 67 54 73 68
R07 |>>>>> 37 41 10 39 29 14 | 63 68 41 29 59 43
R08 |>>>>> 31 26 12 28 32 13 | 61 61 41 36 64 45
R09 |>>>>> 21 31 5 23 26 9 | 12 17 19 25 31 19
R10 |>>>>> 15 21 6 40 45 14 | 17 17 20 23 30 18
R11 |>>>>> 13 14 5 35 30 10 | 22 24 26 28 29 24
R13 |>>>>> 14 17 13 32 55 16 | 16 18 20 19 32 15
R14 |>>>>> 25 31 6 22 16 8 | 17 23 20 22 23 17
XR15 |>>>>> 39 47 --- 37 18 22 | 22 34 --- 41 40 27
R16 |>>>>> 63 67 9 56 51 22 | 28 30 35 40 38 30
R17 |>>>>> 37 46 10 31 26 12 | 54 58 37 37 40 38
R18 |>>>>> 18 24 6 23 20 8 | 44 40 43 40 46 42
R19 |>>>>> 108 106 28 44 36 29 | 69 72 48 48 36 42
R20 |>>>>> 28 45 12 30 35 13 | 49 64 42 50 39 41
R21 | ---- 35 32 7 23 16 10 | 57 55 43 45 40 42
R22 |>>>>> 41 46 10 33 19 12 | 169 167 159 176 171 165
R23 |>>>>> 39 46 10 25 21 12 | 29 28 43 35 47 39
R24 |>>>>> 33 50 6 40 42 15 | 40 38 53 50 60 49
XR26 | ---- 8 125 --- --- --- 0 | 539 447 --- --- --- 539
------+------------------------------------+--------------------------------
RMS |>>>>> 44 47 12 35 33 |T 71 70 42 41 50 63
WRMS |>>>>> 36 41 10 33 32 |NE 71 70 42 41 50 63
MEDI |>>>>> 33 38 10 32 29 |MD 54 58 41 35 40 40
Table 3.2022.6 GPS week: 2022 Day: 6 MJD: 58404
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg IGL | cod cof esx gfz grg IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 92 99 33 55 51 31 | 121 127 33 38 70 42
R02 |>>>>> 27 28 15 31 40 14 | 83 87 55 41 93 63
R03 |>>>>> 38 39 12 39 25 14 | 85 85 46 30 69 52
R04 |>>>>> 27 20 17 41 55 18 | 80 77 50 30 95 57
R05 |>>>>> 34 37 19 41 56 19 | 105 106 76 66 113 82
R07 |>>>>> 38 39 10 36 17 13 | 86 87 49 37 70 55
R08 |>>>>> 30 35 12 41 29 14 | 86 92 59 38 86 64
R09 |>>>>> 20 15 7 22 17 8 | 14 14 18 26 27 17
R10 |>>>>> 16 20 11 37 53 16 | 25 27 29 29 34 25
R11 |>>>>> 13 12 11 28 48 14 | 32 33 37 39 46 35
R13 |>>>>> 15 22 8 33 31 11 | 26 27 34 22 40 29
R14 |>>>>> 22 20 8 22 19 9 | 31 30 30 21 32 27
R15 |>>>>> 46 38 10 48 28 17 | 48 50 36 34 45 37
R16 |>>>>> 54 58 10 47 78 25 | 39 44 42 42 55 41
R17 |>>>>> 39 39 13 44 35 16 | 87 87 53 43 79 60
R18 |>>>>> 21 23 7 31 19 9 | 64 68 65 52 68 63
R19 |>>>>> 104 110 30 60 33 32 | 110 118 52 61 62 53
R20 |>>>>> 25 35 19 27 53 17 | 74 78 63 56 67 63
R21 |>>>>> 37 37 12 28 19 12 | 84 85 54 46 66 58
R22 | ---- 41 39 7 25 21 13 | 181 178 170 202 180 177
R23 |>>>>> 35 27 14 20 23 12 | 49 52 68 52 77 63
R24 |>>>>> 28 39 10 35 48 15 | 70 71 80 71 103 79
XR26 | ---- 9 44 --- --- --- 0 | 476 438 --- --- --- 475
------+------------------------------------+--------------------------------
RMS |>>>>> 42 45 15 37 40 |T 89 89 54 48 71 74
WRMS |>>>>> 36 37 13 30 35 |NE 89 89 54 48 71 74
MEDI |>>>>> 30 37 11 35 31 |MD 80 78 50 39 68 57
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