[IGSREPORT-29133] Wk 2242 IGLOS Final Orbits
acc
acc at igs.org
Tue Jan 17 01:10:41 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2242 (Dec 25, 2022 - Dec 31, 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 2.2242.
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:
igl2242[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2242 in the SP3 format.
igl22427.sum Combination Report for GPS Week 2242.
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 | -1.2 ns
1 | -1.4 ns
2 | -3.1 ns
3 | -0.8 ns
4 | -0.1 ns
5 | 0.5 ns
6 | 0.9 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 1.2242, 1a.2242).
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 2.2242.0-6)
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 3.2242.0-6).
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 2242 summary. (Dec 25, 2022 - Dec 31, 2022)
Table 1.2242.a GPS week : 2242 MJD: 59938.0-59944.0
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 1 0 -11 4 64 .16 21 18 | 40370 -1542 2963 8487
| 1 0 1 12 23 23 .03 | 3574 2765
esa n/a| 0 1 1 -10 -6 -16 -.22 37 26 | 156 -2037 2974 9948
| 1 0 1 11 10 26 .02 | 13577 2524
gfz n/a| 1 1 -2 13 2 -23 -.13 22 15 | 0 -1398 2958 8486
| 1 1 2 13 18 19 .03 | 0 2695
grg n/a| 0 -4 5 11 -10 -29 .19 33 24 | -136 -1495 2963 7902
| 1 1 2 26 23 41 .06 | 271 2382
iac n/a| 0 1 -2 0 -18 21 -.16 27 24 | 1152 -551 2972 8974
| 1 2 2 31 64 51 .02 | 1204 812
Table 1.2242.b GPS week : 2242 MJD: 59938.0-59944.0
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 | 26 18 19 15 17 22 23 |
R02 | 11 8 8 10 7 10 9 |
R03 | 9 7 8 9 8 13 13 |
R04 | 10 12 8 10 10 11 13 |
R05 | 11 11 9 9 8 9 10 |
R07 | 12 9 12 9 11 9 10 |
R08 | 6 9 11 11 12 10 8 |
R09 | 13 14 14 13 14 15 13 |
R11 | 8 8 6 9 9 8 9 |
R12 | 5 6 11 11 10 8 8 |
R13 | 20 16 22 19 18 16 19 |
R14 | 6 7 6 6 5 7 8 |
R15 | 9 9 8 10 8 7 7 |
R16 | 23 25 21 24 26 26 26 |
R17 | 7 7 8 5 8 7 8 |
R18 | 9 10 7 8 8 10 9 |
R19 | 32 27 30 31 24 26 29 |
R20 | 36 35 39 42 45 45 36 |
R21 | 8 11 8 10 10 8 11 |
R22 | --- --- --- --- 152 153 145 |
R24 | 9 13 13 9 11 11 12 |
Table 1.2242.c GPS week : 2242 MJD: 59938.0-59944.0
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 2242 0 | -17 8 9 403 4043 10030 80.2 1219 1219 | -1247 0
brd 2242 1 | 12 -61 -92 2493 2343 2570 81.4 1531 1531 | -1355 0
brd 2242 2 | 10 -70 -148 1684 1537 -2914 78.9 1283 1283 | -3149 0
brd 2242 3 | 12 78 -142 989 337 -12760 78.3 1489 1489 | -842 0
brd 2242 4 | -3 -25 -84 994 168 -10810 80.3 1439 1439 | -52 0
brd 2242 5 | 0 74 -180 -509 346 -4723 80.1 1402 1402 | 512 0
brd 2242 6 | 9 -75 -112 44 2039 -4911 80.6 1370 1370 | 897 0
-------------+------------------------------------------------------------+----------------
brd 2242 mean| 3 -10 -107 871 1545 -3359 80.0 1390 1390 | -748 0
brd 2242 sdev| 11 66 61 1010 1409 7775 1.0 110 110 | 1364 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 2.2242.0 GPS week: 2242 Day: 0 MJD: 59938
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 -11 52 105 .13 22 17 | 45943 -2497 2970 8858
esa n/a| -2 0 0 0 -15 -33 -.22 36 38 | 13155 -3277 2944 11825
gfz n/a| 1 1 -1 25 -25 -39 -.13 24 13 | 0 -2155 2939 8917
grg n/a| 0 -5 5 -13 -37 2 .18 30 21 | -210 -2391 2952 8236
iac n/a| -1 2 -5 -25 67 -41 -.17 23 23 | 943 -1235 2942 9301
Table 2.2242.1 GPS week: 2242 Day: 1 MJD: 59939
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 2 -1 -2 -3 63 .21 22 20 | 44691 -3791 2942 8232
esa n/a| 2 1 -1 4 -9 -50 -.22 36 29 | -21478 -3304 2958 10717
gfz n/a| 1 0 0 11 28 -48 -.15 20 16 | 0 -3259 2956 8265
grg n/a| 0 -2 4 -20 -35 16 .19 28 21 | 12 -2909 2929 7539
iac n/a| -2 5 -6 61 -17 -44 -.17 29 26 | 1138 -681 2946 8674
Table 2.2242.2 GPS week: 2242 Day: 2 MJD: 59940
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 -15 -12 73 .15 22 18 | 40148 -5959 3072 8006
esa n/a| 0 0 3 -5 -3 -11 -.22 32 20 | 19171 -5841 3077 10946
gfz n/a| 1 2 -2 35 23 2 -.13 23 14 | 0 -5825 3063 8046
grg n/a| 0 -3 4 -8 -5 -103 .17 33 25 | -602 -5509 3083 7369
iac n/a| 0 1 -1 -34 -10 66 -.14 28 25 | -811 -1827 3083 8423
Table 2.2242.3 GPS week: 2242 Day: 3 MJD: 59941
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 -4 13 35 .20 23 18 | 38039 -1641 3161 8688
esa n/a| 0 2 2 -22 -25 -18 -.27 41 23 | -9405 -2557 3151 11734
gfz n/a| 1 1 0 12 -5 -7 -.14 19 17 | 0 -1408 3153 8595
grg n/a| 0 -5 0 12 -15 -20 .31 32 25 | -133 -1559 3095 8066
iac n/a| 1 0 -1 -16 50 3 -.19 28 26 | 312 162 3143 9056
Table 2.2242.4 GPS week: 2242 Day: 4 MJD: 59942
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 1 -2 5 0 74 .17 18 17 | 37245 562 2749 9818
esa n/a| 1 0 3 -24 -1 -34 -.21 39 22 | -3264 95 2753 11901
gfz n/a| 2 2 0 0 0 -43 -.15 21 15 | 0 -289 2742 9765
grg n/a| 2 -5 7 34 -19 -2 .13 39 27 | -214 31 2773 9345
iac n/a| 0 0 -2 -1 -64 42 -.17 28 24 | 1957 454 2761 10351
Table 2.2242.5 GPS week: 2242 Day: 5 MJD: 59943
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 0 -27 -17 60 .13 20 17 | 37076 941 3001 7641
esa n/a| 0 3 2 -3 6 19 -.24 39 27 | 2182 -1238 2978 6006
gfz n/a| 2 2 -7 0 0 -18 -.09 22 18 | 0 848 3003 7652
grg n/a| 1 -6 9 39 7 -53 .15 37 25 | 301 226 2969 7102
iac n/a| -2 1 1 7 -118 88 -.18 26 23 | 1567 -733 2988 8168
Table 2.2242.6 GPS week: 2242 Day: 6 MJD: 59944
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 -24 -2 41 .14 20 17 | 39448 1589 2851 8167
esa n/a| 0 1 2 -19 2 16 -.20 38 25 | 735 1857 2960 6507
gfz n/a| 0 0 -6 8 -1 -12 -.08 21 14 | 0 2301 2855 8165
grg n/a| 2 -5 6 38 29 -44 .21 34 26 | -111 1642 2941 7660
iac n/a| 0 0 0 8 -39 32 -.13 24 24 | 2963 -3 2943 8848
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 3.2242.0 GPS week: 2242 Day: 0 MJD: 59938
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1130 49 45 35 47 17 25 | 81 40 67 38 51 54
R02 | 1292 10 20 18 24 19 10 | 71 85 78 69 78 74
R03 | 933 8 18 19 12 27 8 | 87 81 100 90 101 90
R04 | 915 18 14 9 27 23 10 | 118 112 109 100 102 109
R05 | 1695 19 17 8 25 11 10 | 109 106 100 94 106 101
R07 | 1039 25 18 8 28 13 12 | 101 79 92 78 91 88
R08 | 1204 11 8 12 10 15 6 | 172 167 176 168 178 171
R09 | 945 24 18 17 29 29 13 | 40 42 39 34 37 33
R11 | 1103 10 13 14 16 22 7 | 23 36 29 28 31 27
R12 | 1588 7 8 8 11 25 5 | 87 86 82 78 95 82
R13 | 647 30 46 31 28 15 19 | 92 73 88 77 74 81
R14 | 2304 11 17 4 8 22 6 | 62 70 59 60 72 61
R15 | 955 14 17 11 22 27 9 | 84 73 76 71 81 76
R16 | 1539 30 24 57 28 31 22 | 213 203 210 209 211 209
R17 | 831 10 13 8 14 16 6 | 48 42 52 50 51 48
R18 | 1002 11 18 12 19 13 8 | 39 38 40 50 37 40
R19 | 1307 39 80 16 78 27 32 | 42 28 45 55 47 40
R20 | 1004 26 104 63 46 24 36 | 67 46 84 59 67 60
R21 | 697 8 19 16 10 21 7 | 38 42 52 48 44 44
R24 | 1056 15 20 11 19 37 9 | 58 44 47 59 48 51
------+------------------------------------+--------------------------------
RMS | 1219 22 36 24 30 23 |T 81 74 81 75 80 76
WRMS | 1219 17 38 13 21 23 |NE 81 74 81 75 80 76
MEDI | 1039 14 18 12 22 22 |MD 71 70 76 60 72 61
Table 3.2242.1 GPS week: 2242 Day: 1 MJD: 59939
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 767 40 42 17 20 25 18 | 67 45 52 50 54 50
R02 | 938 8 20 14 14 22 8 | 76 85 76 87 88 79
R03 | 1214 15 9 13 9 28 7 | 77 77 74 81 85 76
R04 | 718 18 16 13 30 25 11 | 103 104 104 90 98 99
R05 | 2011 18 11 11 30 27 11 | 114 111 111 100 103 108
R07 | 916 14 19 12 18 22 9 | 100 90 97 97 101 96
R08 | 1179 13 18 14 17 20 9 | 155 150 161 153 160 155
R09 | 1240 20 24 16 36 28 14 | 39 41 43 37 43 35
R11 | 1071 18 16 10 13 12 8 | 21 36 33 30 29 27
R12 | 2085 11 11 5 13 25 6 | 69 57 57 60 73 60
R13 | 1244 18 20 24 44 30 16 | 72 77 85 70 60 75
R14 | 2434 10 16 13 9 24 7 | 51 55 38 52 51 47
R15 | 877 13 18 14 15 26 8 | 64 54 68 62 53 62
R16 | 1424 37 32 55 38 33 25 | 180 175 178 170 176 175
R17 | 796 8 14 9 19 20 7 | 45 36 43 45 47 42
R18 | 1160 18 20 10 20 32 9 | 34 25 30 42 44 32
R19 | 1658 31 81 22 50 27 27 | 29 33 29 36 27 25
R20 | 2239 44 105 43 47 62 34 | 42 44 44 48 29 38
R21 | 728 12 29 9 23 25 10 | 31 43 37 34 33 34
R24 | 3089 20 34 12 28 30 13 | 47 36 31 53 33 38
------+------------------------------------+--------------------------------
RMS | 1530 22 36 20 28 29 |T 70 68 69 69 69 67
WRMS | 1530 20 29 16 21 26 |NE 70 68 69 69 69 67
MEDI | 1179 18 19 13 20 25 |MD 64 54 52 53 53 50
Table 3.2242.2 GPS week: 2242 Day: 2 MJD: 59940
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 990 40 37 22 23 27 18 | 62 48 54 51 42 49
R02 | 865 10 17 13 14 21 7 | 60 66 58 53 52 59
R03 | 849 7 16 10 20 27 7 | 108 105 118 118 120 112
R04 | 630 14 11 8 20 15 7 | 92 89 91 90 84 90
R05 | 980 11 10 15 26 15 9 | 95 93 105 99 101 97
R07 | 1054 11 22 23 24 18 11 | 107 99 117 103 107 106
R08 | 1895 15 15 24 17 19 10 | 112 105 123 104 98 111
R09 | 1141 17 17 21 39 30 13 | 39 41 50 27 45 36
R11 | 692 9 11 9 10 15 5 | 22 28 27 25 30 24
R12 | 1896 10 12 17 30 18 10 | 73 75 86 59 67 73
R13 | 941 35 27 29 60 23 22 | 70 47 50 46 49 50
R14 | 844 6 11 13 10 16 6 | 54 50 65 51 62 55
R15 | 1415 9 15 14 16 24 7 | 71 68 76 63 65 69
R16 | 1144 23 24 56 25 46 20 | 142 146 150 144 151 148
R17 | 850 8 15 13 17 33 7 | 36 37 47 38 50 38
R18 | 955 11 14 6 17 18 7 | 32 32 31 32 29 30
R19 | 1506 38 64 33 76 37 30 | 33 32 38 37 28 29
R20 | 1943 56 100 48 60 54 39 | 45 56 56 57 35 45
R21 | 806 8 15 9 20 22 7 | 28 26 30 33 29 28
R24 | 2401 13 31 12 30 41 12 | 48 34 48 45 39 42
------+------------------------------------+--------------------------------
RMS | 1282 22 32 23 33 28 |T 66 63 71 63 63 64
WRMS | 1282 18 20 14 25 25 |NE 66 63 71 63 63 64
MEDI | 980 11 15 14 20 22 |MD 60 50 56 51 52 50
Table 3.2242.3 GPS week: 2242 Day: 3 MJD: 59941
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 736 24 39 20 27 28 15 | 69 44 60 53 55 55
R02 | 861 11 15 13 28 18 9 | 55 64 64 43 58 56
R03 | 549 13 23 12 14 20 8 | 84 67 87 87 82 82
R04 | 840 20 22 12 16 19 10 | 100 86 94 104 94 95
R05 | 722 11 13 11 24 30 8 | 93 99 100 106 113 98
R07 | 1054 16 17 7 20 25 8 | 97 83 84 80 95 86
R08 | 1497 17 19 17 19 31 10 | 83 79 95 98 107 89
R09 | 1089 16 14 14 42 28 13 | 48 49 50 28 59 41
R11 | 699 12 19 18 14 16 9 | 15 22 26 20 22 16
R12 | 902 13 22 9 33 25 11 | 55 65 50 33 61 49
R13 | 1163 32 26 16 52 31 18 | 79 60 61 32 50 57
R14 | 638 10 10 7 15 14 6 | 58 56 52 46 46 52
R15 | 1528 24 14 10 17 15 10 | 63 47 50 44 57 50
R16 | 1818 34 40 53 24 40 24 | 65 60 66 60 53 62
R17 | 1177 7 13 5 12 26 5 | 38 32 36 41 52 36
R18 | 762 9 13 11 19 16 7 | 30 28 28 35 28 27
R19 | 2875 55 83 21 58 27 30 | 45 56 41 54 54 38
R20 | 1123 39 135 38 80 63 41 | 49 94 82 47 65 62
R21 | 748 8 31 15 15 13 10 | 38 34 41 41 39 37
R24 | 4026 11 30 8 10 35 8 | 43 33 37 38 47 36
------+------------------------------------+--------------------------------
RMS | 1488 23 41 19 32 28 |T 60 57 60 54 60 56
WRMS | 1488 18 23 17 25 26 |NE 60 57 60 54 60 56
MEDI | 902 13 19 12 19 25 |MD 55 56 52 44 55 52
Table 3.2242.4 GPS week: 2242 Day: 4 MJD: 59942
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 821 26 45 19 31 29 17 | 71 36 53 56 41 54
R02 | 923 9 14 10 19 18 7 | 65 70 68 57 72 65
R03 | 901 10 23 9 14 14 8 | 119 114 120 110 123 116
R04 | 916 14 13 10 29 30 9 | 122 118 119 96 114 115
R05 | 1537 14 18 7 14 38 7 | 94 107 97 98 102 97
R07 | 884 14 22 13 29 26 11 | 111 103 114 96 119 108
R08 | 1038 15 22 26 20 24 12 | 87 75 103 84 96 89
R09 | 1373 16 20 14 47 29 14 | 55 64 56 14 67 49
R11 | 1106 13 17 18 12 10 9 | 14 20 32 28 22 20
R12 | 866 7 16 13 34 20 10 | 62 73 65 52 73 62
R13 | 1237 31 23 18 52 24 18 | 73 45 56 45 49 55
R14 | 762 6 13 7 12 12 5 | 53 56 50 46 56 51
R15 | 1767 16 15 7 13 17 7 | 67 56 55 53 51 58
R16 | 1599 33 31 61 31 30 25 | 140 146 145 138 150 142
R17 | 1165 7 20 14 11 19 7 | 43 42 49 40 50 43
R18 | 963 15 11 12 12 21 7 | 37 33 41 41 39 36
R19 | 1280 24 73 14 57 37 23 | 48 45 49 47 43 43
R20 | 2881 32 129 41 122 59 45 | 54 55 65 76 51 50
R21 | 900 10 28 9 23 26 9 | 32 39 36 35 40 33
XR22 | 3239 --- 144 --- 159 146 151 | --- 50 --- 29 25 26
R24 | 3047 15 22 10 28 26 10 | 48 39 48 47 43 44
------+------------------------------------+--------------------------------
RMS | 1438 18 39 21 39 28 |T 69 66 71 61 67 64
WRMS | 1438 17 22 15 27 24 |NE 69 66 71 61 67 64
MEDI | 1106 14 22 13 28 26 |MD 62 56 56 52 51 54
Table 3.2242.5 GPS week: 2242 Day: 5 MJD: 59943
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1267 31 50 30 46 32 22 | 66 38 71 34 44 51
R02 | 878 16 23 12 20 14 10 | 60 60 51 53 54 54
R03 | 902 9 28 26 21 21 12 | 79 64 96 70 62 79
R04 | 778 12 14 16 34 18 11 | 76 64 81 62 71 72
R05 | 2071 15 13 16 12 17 8 | 60 62 77 72 72 67
R07 | 1063 7 16 13 22 17 8 | 65 59 69 60 71 64
R08 | 1668 12 20 20 14 24 9 | 101 94 105 99 105 100
R09 | 1650 15 11 20 48 22 14 | 59 58 66 25 61 52
R11 | 722 12 14 10 20 22 8 | 18 22 24 22 25 18
R12 | 809 8 16 6 22 26 7 | 69 76 78 65 74 72
R13 | 668 30 32 18 34 11 16 | 69 65 54 58 57 60
R14 | 810 15 8 12 11 21 7 | 50 57 67 62 48 58
R15 | 1541 15 11 9 13 21 7 | 71 61 60 62 48 64
R16 | 1815 31 34 63 31 33 25 | 157 151 156 150 152 154
R17 | 813 9 15 7 13 21 6 | 33 28 30 28 33 29
R18 | 877 18 13 15 17 18 9 | 24 24 27 29 31 23
R19 | 1143 23 80 13 62 44 26 | 42 39 28 44 41 31
R20 | 3250 46 126 35 105 61 44 | 48 62 52 53 40 38
R21 | 657 6 16 9 22 21 7 | 24 24 21 31 27 22
XR22 | 4625 --- 146 --- 159 151 152 | --- 40 --- 34 23 34
R24 | 1698 13 24 12 29 14 10 | 35 25 30 38 26 31
------+------------------------------------+--------------------------------
RMS | 1401 20 39 22 37 26 |T 60 55 62 54 55 55
WRMS | 1401 17 27 18 25 23 |NE 60 55 62 54 55 55
MEDI | 1063 15 16 13 22 21 |MD 60 59 60 53 48 54
Table 3.2242.6 GPS week: 2242 Day: 6 MJD: 59944
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1441 40 45 22 54 24 23 | 88 44 76 52 65 63
R02 | 1205 12 11 16 17 14 8 | 78 88 80 78 78 79
R03 | 1126 16 30 21 24 19 13 | 97 77 102 80 92 90
R04 | 805 12 18 20 34 30 12 | 107 91 111 87 90 100
R05 | 1827 15 11 14 25 26 9 | 95 91 96 84 90 91
R07 | 1310 11 28 14 12 18 9 | 102 88 107 89 105 98
R08 | 1941 12 12 12 17 17 7 | 148 146 153 143 152 148
R09 | 2697 22 15 14 36 21 13 | 50 47 50 24 50 41
R11 | 1393 15 11 12 20 14 8 | 23 22 33 22 29 23
R12 | 1354 13 19 9 15 27 8 | 86 79 85 73 84 81
R13 | 839 26 28 29 46 22 18 | 86 75 80 68 70 76
R14 | 1063 12 20 9 13 13 7 | 65 73 66 67 67 67
R15 | 1108 13 12 8 12 25 6 | 93 83 84 82 79 86
R16 | 963 32 34 64 33 34 26 | 194 187 197 184 187 191
R17 | 874 5 10 14 24 17 8 | 54 46 51 57 52 51
R18 | 921 10 23 10 17 22 8 | 47 49 48 52 50 47
R19 | 1066 36 74 15 76 45 29 | 72 47 62 75 68 62
R20 | 1662 33 120 25 58 37 35 | 75 69 82 80 77 73
R21 | 1027 7 31 10 29 14 11 | 50 47 55 57 55 51
XR22 | 4379 --- 142 --- 147 152 145 | --- 43 --- 29 26 34
R24 | 1285 13 23 20 24 17 11 | 54 45 54 66 58 53
------+------------------------------------+--------------------------------
RMS | 1369 20 38 21 34 24 |T 83 73 83 73 77 76
WRMS | 1369 17 25 14 26 24 |NE 83 73 83 73 77 76
MEDI | 1205 13 23 14 24 22 |MD 78 73 80 73 70 73
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