[IGSREPORT-29126] Wk 2241 IGLOS Final Orbits
acc
acc at igs.org
Thu Jan 12 05:17:03 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2241 (Dec 18, 2022 - Dec 24, 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 2.2241.
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:
igl2241[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2241 in the SP3 format.
igl22417.sum Combination Report for GPS Week 2241.
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.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
3. 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).
4. 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
5. 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 | 0.9 ns
1 | -0.7 ns
2 | 0.3 ns
3 | -1.0 ns
4 | -15.9 ns
5 | 1.0 ns
6 | 1.0 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 1.2241, 1a.2241).
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 2.2241.0-6)
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 3.2241.0-6).
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 2241 summary. (Dec 18, 2022 - Dec 24, 2022)
Table 1.2241.a GPS week : 2241 MJD: 59931.0-59937.0
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| -1 0 -1 -4 -3 47 .15 22 18 | 41073 139 3080 8805
| 1 1 1 11 22 26 .03 | 6713 2082
esa n/a| 0 0 0 -8 -5 -17 -.23 38 28 | 723 -90 3075 8970
| 1 0 2 13 12 44 .01 | 5925 2286
gfz n/a| 0 1 -1 22 7 -27 -.14 18 12 | 0 263 3082 8831
| 1 0 2 14 15 18 .03 | 0 1909
grg n/a| 2 -3 5 -17 -16 -8 .24 32 24 | 21294 -1648 15011 125011
| 1 1 3 25 12 65 .05 | 65815 6186
iac n/a| 1 0 1 7 -16 37 -.16 26 23 | 22338 -2436 14460 123085
| 2 1 6 22 24 80 .06 | 62775 4766
Table 1.2241.b GPS week : 2241 MJD: 59931.0-59937.0
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 | 19 18 19 19 22 19 21 |
R02 | 8 8 10 8 8 8 10 |
R03 | 5 8 7 10 8 10 11 |
R04 | 8 8 9 8 11 13 10 |
R05 | 7 10 7 8 8 8 10 |
R07 | 7 9 10 11 12 11 9 |
R08 | 7 6 10 8 13 9 10 |
R09 | 19 20 16 13 13 12 13 |
R11 | 10 10 9 7 8 8 7 |
R12 | 6 10 7 8 10 9 9 |
R13 | 14 18 18 18 18 18 19 |
R14 | 8 8 8 9 9 10 11 |
R15 | 9 6 15 8 7 8 10 |
R16 | 0 0 0 34 24 25 23 |
R17 | 5 7 8 6 9 5 7 |
R18 | 10 9 9 8 8 8 8 |
R19 | 27 27 34 26 29 28 32 |
R20 | 27 34 42 40 44 35 39 |
R21 | 7 8 12 9 9 10 8 |
R22 | 134 142 0 0 0 --- --- |
R24 | 12 11 10 10 12 9 11 |
Table 1.2241.c GPS week : 2241 MJD: 59931.0-59937.0
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 2241 0 | 4 22 81 1987 1232 -5116 79.4 1183 1183 | 893 0
brd 2241 1 | -24 -76 52 1754 128 -3667 80.5 1291 1291 | -684 0
brd 2241 2 | -21 -6 27 1123 -777 -6433 82.4 1257 1257 | 322 0
brd 2241 3 | 42 31 99 -217 -3171 -6472 82.6 1329 1329 | -956 0
brd 2241 4 | 0 66 -2 -229 -106 -7510 81.9 2196 2196 | -15926 0
brd 2241 5 | 5 92 -2 -1434 -532 -8702 83.0 1995 1995 | 951 0
brd 2241 6 | -13 81 46 -571 1939 2274 83.1 1348 1348 | 955 0
-------------+------------------------------------------------------------+----------------
brd 2241 mean| 0 30 43 344 -183 -5089 81.9 1514 1514 | -2063 0
brd 2241 sdev| 22 58 39 1287 1633 3625 1.4 404 404 | 6163 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 2.2241.0 GPS week: 2241 Day: 0 MJD: 59931
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 0 8 -43 60 .14 21 14 | 41751 1858 3079 9311
esa n/a| 1 1 -1 -3 8 -30 -.25 39 39 | -46 2640 3071 8240
gfz n/a| 0 0 0 10 30 -39 -.16 14 13 | 0 2083 3099 9355
grg n/a| 1 -1 1 -21 -34 1 .20 22 17 | -492 2495 3093 8567
iac n/a| 3 2 3 25 -7 200 -.18 22 21 | 2236 458 3074 9816
Table 2.2241.1 GPS week: 2241 Day: 1 MJD: 59932
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 -1 -4 -2 17 .16 22 19 | 42233 -1029 2741 8321
esa n/a| 0 0 0 -16 -3 -40 -.22 37 24 | 12029 -972 2727 7102
gfz n/a| 1 3 -2 41 5 -1 -.13 15 13 | 0 -709 2740 8385
grg n/a| 1 -4 8 -40 -12 23 .23 29 24 | -317 -965 2742 7726
iac n/a| 1 -1 6 -19 -23 -14 -.13 26 24 | 1418 -1529 2745 8826
Table 2.2241.2 GPS week: 2241 Day: 2 MJD: 59933
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 8 -2 35 .15 22 19 | 44173 330 2813 9135
esa n/a| 1 0 -2 -24 -12 -76 -.24 38 21 | -6559 -377 2806 8356
gfz n/a| -2 1 -2 36 17 -57 -.17 20 13 | 0 756 2818 9159
grg n/a| 0 -2 9 -52 -2 59 .29 38 28 | -4497 -123 2923 22279
iac n/a| 4 0 9 35 16 -42 -.08 30 24 | -2390 -1628 2941 22644
Table 2.2241.3 GPS week: 2241 Day: 3 MJD: 59934
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 0 2 -22 33 .22 24 19 | 44692 -1462 2759 8298
esa n/a| 0 0 1 -21 -19 -49 -.22 36 22 | 1457 -1784 2747 7096
gfz n/a| 0 1 -1 15 17 -26 -.16 14 9 | 0 -1470 2744 8311
grg n/a| 2 -2 6 -30 -7 73 .24 35 23 | 170068 -14959 86161 810950
iac n/a| 0 2 5 1 -5 42 -.09 27 24 | 163916 -13099 82285 792072
Table 2.2241.4 GPS week: 2241 Day: 4 MJD: 59935
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 -16 16 47 .13 23 18 | 26381 -2941 2887 8597
esa n/a| 0 1 -1 1 11 38 -.24 38 24 | -4491 -3498 2882 11528
gfz n/a| 0 2 1 5 -15 -11 -.10 21 12 | 0 -2668 2874 8465
grg n/a| 2 -2 7 1 -33 -98 .30 37 28 | -14831 -2500 2891 8407
iac n/a| 0 0 -5 -9 -1 66 -.26 26 21 | -15313 59 2885 9216
Table 2.2241.5 GPS week: 2241 Day: 5 MJD: 59936
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 -1 -14 12 37 .12 21 19 | 41775 3071 3525 8785
esa n/a| 0 1 0 -5 -20 41 -.22 39 28 | 719 2757 3515 12081
gfz n/a| 0 1 1 32 0 -22 -.15 18 10 | 0 2275 3507 8852
grg n/a| 4 -4 -1 5 -13 -71 .28 33 26 | -698 3072 3522 8605
iac n/a| 3 1 -5 31 -54 -12 -.16 25 23 | 2720 -319 3526 9364
Table 2.2241.6 GPS week: 2241 Day: 6 MJD: 59937
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 -16 16 99 .15 22 17 | 46510 1147 3756 9190
esa n/a| 0 0 4 11 -3 -6 -.22 38 36 | 1956 601 3777 8388
gfz n/a| 0 1 -4 13 -2 -30 -.10 22 14 | 0 1577 3793 9296
grg n/a| 5 -5 4 15 -8 -48 .16 32 23 | -174 1438 3746 8549
iac n/a| 0 0 -1 -11 -41 22 -.19 26 27 | 3779 -996 3764 9660
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 3.2241.0 GPS week: 2241 Day: 0 MJD: 59931
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01M | 1076 41 53 17 30 27 19 | 126 76 103 88 88 100
R02M | 723 8 22 13 11 27 7 | 85 97 86 87 87 86
R03 | 1491 6 12 5 11 18 5 | 104 98 107 109 103 105
R04 | 797 15 12 9 17 19 7 | 91 81 84 74 85 83
R05 | 758 14 15 8 13 27 7 | 97 89 94 87 82 92
R07M | 1198 13 14 7 12 24 6 | 115 100 113 108 103 110
R08M | 957 12 21 10 9 12 7 | 119 107 126 118 113 120
R09M | 1744 29 38 20 48 18 19 | 117 119 109 78 102 101
R11 | 1521 12 24 17 16 22 9 | 89 95 93 96 87 92
R12 | 1203 9 13 9 9 16 5 | 117 117 111 113 108 113
R13M | 828 15 37 22 26 26 14 | 112 102 109 98 90 104
R14M | 526 12 17 9 16 18 7 | 103 112 102 101 100 103
R15M | 1005 19 16 8 15 23 8 | 115 109 110 106 104 110
XR16M | ---- 5 --- --- --- --- 0 | 187 --- --- --- --- 191
R17 | 666 7 11 6 9 14 4 | 35 41 39 40 34 38
R18 | 796 14 31 9 16 14 9 | 32 44 38 33 29 34
R19 | 1077 52 81 24 41 24 26 | 47 48 52 42 38 44
R20 | 1178 32 106 25 29 35 26 | 42 38 37 48 37 33
R21 | 528 9 27 5 12 20 7 | 38 46 41 42 38 41
XR22 | 1691 --- 182 --- 99 108 134 | --- 85 --- 37 29 51
R24 | 2535 12 34 13 28 21 12 | 40 53 48 40 45 43
------+------------------------------------+--------------------------------
RMS | 1183 21 39 14 22 22 |T 90 82 84 77 75 85
WRMS | 1183 14 39 13 17 21 |NE 66 69 67 63 59 64
MEDI | 1005 12 22 9 16 21 |MD 97 89 94 87 87 92
Table 3.2241.1 GPS week: 2241 Day: 1 MJD: 59932
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01M | 1691 43 48 12 23 18 18 | 85 44 63 63 67 64
R02M | 958 14 6 14 15 24 7 | 62 65 77 62 67 68
R03 | 1226 8 23 6 21 22 8 | 74 64 71 89 87 74
R04 | 467 13 15 8 18 17 7 | 62 64 59 51 68 58
R05 | 582 13 11 15 26 24 9 | 71 77 81 58 74 73
R07M | 788 13 14 11 22 21 8 | 85 76 85 77 87 81
R08M | 724 7 10 7 15 19 5 | 84 84 85 77 86 83
R09M | 2045 19 32 19 65 22 20 | 83 91 82 67 75 75
R11 | 2107 16 19 16 13 33 9 | 59 57 61 58 62 58
R12 | 935 13 29 14 12 27 9 | 83 82 71 75 71 75
R13M | 601 32 25 22 43 32 17 | 69 69 64 56 58 61
R14M | 1008 10 18 11 13 19 7 | 63 66 59 65 65 62
R15M | 702 14 15 5 8 29 6 | 74 73 73 67 79 71
XR16M | ---- 3 --- --- --- --- 0 | 169 --- --- --- --- 173
R17 | 1188 8 17 7 19 18 7 | 26 29 28 29 33 26
R18 | 705 16 22 8 20 15 9 | 27 30 28 27 25 26
R19 | 1076 52 71 23 50 22 27 | 36 41 25 50 40 27
R20 | 2031 40 114 32 52 52 33 | 28 51 50 48 33 36
R21 | 546 9 24 10 13 17 8 | 30 28 26 31 37 27
XR22 | 1100 --- 158 --- 128 123 142 | --- 85 --- 28 27 66
R24 | 2414 16 22 12 25 34 10 | 26 27 25 36 32 25
------+------------------------------------+--------------------------------
RMS | 1291 22 37 15 29 26 |T 64 60 58 55 58 62
WRMS | 1291 19 24 13 24 24 |NE 47 52 47 48 49 47
MEDI | 958 13 22 12 20 22 |MD 63 64 63 58 65 64
Table 3.2241.2 GPS week: 2241 Day: 2 MJD: 59933
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01M | 862 34 44 17 34 32 18 | 82 40 66 51 56 62
R02M | 1027 8 16 11 33 20 10 | 64 71 68 39 45 61
R03 | 800 6 15 11 14 9 6 | 71 59 70 62 61 66
R04 | 611 13 12 17 17 22 8 | 70 68 65 71 81 67
R05 | 1070 8 16 8 20 15 7 | 52 62 53 46 48 52
R07M | 1216 12 25 9 20 26 9 | 80 56 76 74 49 72
R08M | 1558 11 12 19 25 16 9 | 78 77 94 64 76 79
R09M | 2196 13 25 14 54 24 15 | 53 62 58 44 53 49
R11 | 2358 13 14 18 14 19 9 | 28 23 33 31 28 27
R12 | 1101 7 12 9 20 17 6 | 71 77 73 65 70 71
R13M | 704 26 30 26 48 42 18 | 63 60 68 30 43 56
R14M | 1400 8 19 13 14 23 7 | 45 57 42 40 44 44
R15M | 863 27 12 31 14 28 14 | 59 41 41 45 50 43
XR16M |13346 3 --- --- --- --- 0 | 91 --- --- --- --- 99
R17 | 749 9 9 13 23 28 8 | 27 27 29 32 27 26
R18 | 505 13 15 9 24 20 8 | 28 27 28 31 27 26
R19 | 1310 53 87 22 74 23 33 | 55 62 42 36 45 44
R20 | 1478 45 114 50 96 81 42 | 39 99 84 39 38 59
R21 | 801 5 27 19 28 24 11 | 30 36 35 37 26 30
XR22 | 1714 --- --- --- 8 17 0 | --- --- --- 31 25 62
R24 | 1415 15 14 17 22 19 9 | 32 33 34 35 26 31
------+------------------------------------+--------------------------------
RMS | 1257 22 38 20 38 30 |T 55 54 55 45 45 53
WRMS | 1257 19 21 13 28 24 |NE 45 52 49 43 41 46
MEDI | 1101 12 16 17 22 22 |MD 55 59 58 39 45 56
Table 3.2241.3 GPS week: 2241 Day: 3 MJD: 59934
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01M | 1433 49 39 13 31 21 19 | 96 52 59 57 59 64
R02M | 693 11 16 8 19 26 7 | 79 83 72 65 86 74
R03 | 859 7 28 16 17 20 10 | 79 59 90 77 66 79
R04 | 630 14 21 8 11 19 7 | 74 52 68 63 68 66
R05 | 1140 12 11 8 21 13 7 | 56 63 55 71 64 59
R07M | 990 23 19 11 26 19 11 | 83 59 76 56 75 70
R08M | 1040 11 12 11 17 21 7 | 84 81 90 87 75 87
R09M | 2736 20 27 14 36 25 13 | 48 56 55 34 53 46
R11 | 1987 11 12 9 14 24 6 | 26 26 28 30 35 26
R12 | 1343 13 17 9 21 20 8 | 55 49 47 37 53 46
R13M | 1432 38 32 21 41 29 18 | 77 49 67 41 47 59
R14M | 1635 13 27 9 12 21 8 | 51 72 52 56 47 55
R15M | 1059 19 13 8 15 29 8 | 66 52 51 51 67 54
XR16M | 6870 46 53 45 --- 47 33 | 123 35 36 --- 38 139
R17 | 876 8 14 7 14 20 6 | 30 28 30 38 33 30
R18 | 790 12 17 11 19 14 8 | 27 28 28 35 27 27
R19 | 1843 45 69 18 59 43 26 | 42 54 56 50 38 46
R20 | 1115 41 111 38 104 56 40 | 33 68 52 46 37 40
R21 | 661 15 22 9 17 35 8 | 34 47 41 37 40 37
XR22 | 647 --- --- --- 6 25 0 | --- --- --- 27 28 28
R24 | 969 15 22 6 27 11 9 | 34 35 31 36 34 32
------+------------------------------------+--------------------------------
RMS | 1328 24 36 14 35 27 |T 59 52 54 49 50 55
WRMS | 1328 19 22 9 23 24 |NE 44 46 47 45 43 43
MEDI | 1059 14 21 9 19 21 |MD 55 52 52 46 47 54
Table 3.2241.4 GPS week: 2241 Day: 4 MJD: 59935
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01M | 811 44 52 15 38 25 22 | 97 51 75 55 56 70
R02M | 809 10 18 8 22 15 8 | 75 76 69 64 81 70
R03 | 903 15 10 6 20 19 7 | 80 70 64 65 79 69
R04 | 922 21 18 9 25 24 10 | 79 57 64 54 60 64
R05 | 1169 17 9 10 16 15 7 | 55 66 69 68 73 63
R07M | 962 7 15 20 34 13 11 | 83 78 96 73 80 83
R08M | 1468 20 18 28 12 25 12 | 82 78 108 85 91 89
R09M | 2758 16 22 16 35 25 12 | 65 71 71 44 62 62
R11 | 2133 11 14 11 17 13 7 | 52 58 51 56 53 53
R12 | 1394 9 15 8 32 15 9 | 76 75 74 65 74 72
R13M | 1599 29 35 21 38 19 17 | 77 64 62 61 67 65
R14M | 840 8 14 19 17 26 8 | 69 72 54 72 78 64
R15M | 864 13 10 11 13 19 7 | 74 73 58 62 71 66
R16M | 7833 35 28 57 29 44 24 | 126 23 19 32 29 130
R17 | 830 8 19 10 22 11 8 | 32 40 37 29 38 32
R18 | 976 12 18 13 13 10 8 | 30 33 34 30 30 30
R19 | 1918 33 80 16 70 50 28 | 45 44 35 45 53 36
R20 | 1397 53 116 43 102 58 44 | 41 73 61 40 41 43
R21 | 957 9 17 9 27 19 9 | 37 35 38 39 38 35
XR22 |10208 --- --- --- 9 39 0 | --- --- --- 40 32 54
R24 | 1158 19 23 12 33 22 12 | 42 34 31 39 30 31
------+------------------------------------+--------------------------------
RMS | 2196 23 38 21 37 26 |T 65 58 58 53 57 61
WRMS | 2196 18 24 12 28 21 |NE 51 53 50 47 50 48
MEDI | 1158 15 18 12 25 19 |MD 69 64 61 55 60 64
Table 3.2241.5 GPS week: 2241 Day: 5 MJD: 59936
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01M | 891 37 52 18 27 23 19 | 92 49 72 64 58 71
R02M | 1297 8 20 7 21 16 7 | 72 83 68 71 73 71
R03 | 584 16 20 14 24 12 10 | 75 60 74 55 70 67
R04 | 1283 26 14 9 36 29 13 | 75 61 63 54 55 62
R05 | 577 17 10 8 21 14 8 | 58 48 44 44 45 47
R07M | 1448 15 21 17 28 14 11 | 72 57 60 85 63 65
R08M | 1898 10 13 8 28 31 8 | 66 63 63 84 84 66
R09M | 2569 20 19 13 29 24 11 | 68 68 66 61 73 64
R11 | 1984 14 12 8 18 28 7 | 54 59 59 61 57 57
R12 | 1907 12 15 12 28 18 9 | 86 85 87 76 80 84
R13M | 632 38 35 21 32 18 18 | 81 61 68 54 70 67
R14M | 768 14 14 9 30 25 9 | 87 92 92 101 98 90
R15M | 745 12 17 10 16 20 7 | 78 77 73 84 72 76
R16M | 6468 32 36 53 38 47 24 | 167 65 49 53 74 168
R17 | 680 6 14 5 13 16 5 | 23 19 20 25 18 21
R18 | 517 13 19 11 11 26 7 | 22 16 18 26 23 19
R19 | 2649 34 85 16 63 35 27 | 44 29 34 40 32 34
R20 | 826 22 112 34 81 40 35 | 28 56 50 33 41 35
R21 | 1415 8 31 11 22 19 10 | 23 30 28 31 28 25
R24 | 1054 13 22 10 23 18 9 | 30 29 21 26 18 23
------+------------------------------------+--------------------------------
RMS | 1995 21 39 18 33 25 |T 65 55 55 56 55 60
WRMS | 1995 19 28 10 26 23 |NE 47 44 45 42 41 43
MEDI | 1054 14 19 11 27 20 |MD 68 59 60 54 58 64
Table 3.2241.6 GPS week: 2241 Day: 6 MJD: 59937
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01M | 913 42 47 15 36 32 20 | 199 181 188 180 188 186
R02M | 1647 8 20 12 28 19 10 | 76 88 77 71 86 76
R03 | 946 13 26 18 20 24 11 | 97 78 102 89 107 93
R04 | 1078 19 16 6 22 18 9 | 96 89 83 75 88 85
R05 | 830 16 12 13 24 37 9 | 78 74 78 62 71 73
R07M | 1315 13 20 12 17 16 8 | 174 163 170 169 166 169
R08M | 2600 16 12 10 28 24 10 | 130 126 130 141 130 131
R09M | 2102 18 19 17 33 25 12 | 221 220 222 219 219 220
R11 | 1565 11 9 12 16 23 7 | 43 45 48 46 48 44
R12 | 1361 14 11 16 15 20 8 | 92 89 99 88 91 92
R13M | 640 38 35 29 27 26 19 | 89 70 78 58 72 75
R14M | 924 15 14 14 29 20 10 | 181 180 179 179 184 179
R15M | 1040 9 19 17 23 26 10 | 108 89 104 94 109 100
R16M | 981 31 32 52 25 28 22 | 108 72 77 71 80 105
R17 | 864 8 16 5 16 22 6 | 39 42 39 40 41 39
R18 | 746 13 18 6 13 21 7 | 39 40 37 39 35 37
R19 | 2064 36 80 15 84 18 31 | 45 43 46 59 41 45
R20 | 1474 36 117 59 60 39 39 | 38 44 61 47 40 43
R21 | 688 9 23 7 13 28 7 | 46 44 48 49 46 47
R24 | 1128 11 27 13 22 35 10 | 45 52 40 45 39 43
------+------------------------------------+--------------------------------
RMS | 1347 22 38 22 32 26 |T 97 91 95 91 94 94
WRMS | 1347 17 36 14 23 27 |NE 59 58 61 58 58 58
MEDI | 1040 14 19 13 23 24 |MD 89 74 78 71 80 76
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