[IGSREPORT-29092] Wk 2238 IGLOS Final Orbits
acc
acc at igs.org
Tue Dec 20 23:58:05 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2238 (Nov 27, 2022 - Dec 03, 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 2.2238.
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:
igl2238[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2238 in the SP3 format.
igl22387.sum Combination Report for GPS Week 2238.
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 | -12.1 ns
1 | -14.7 ns
2 | -0.7 ns
3 | 0.3 ns
4 | -0.2 ns
5 | 0.7 ns
6 | -0.4 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 1.2238, 1a.2238).
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 2.2238.0-6)
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 3.2238.0-6).
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 2238 summary. (Nov 27, 2022 - Dec 03, 2022)
Table 1.2238.a GPS week : 2238 MJD: 59910.0-59916.0
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| -2 1 0 8 -8 58 .14 24 19 | 27983 -465 3096 8700
| 1 1 1 9 11 13 .03 | 7128 1531
esx n/a| 1 0 1 -29 3 -27 -.21 35 24 | -3115 -691 3284 9422
| 1 1 2 10 24 8 .07 | 8612 1661
gfz n/a| 0 3 -2 32 14 -32 -.14 29 23 | 0 -43 3088 8713
| 2 3 1 18 24 20 .06 | 0 1303
grg n/a| 2 -5 0 -4 -8 -13 .17 32 23 | -3530 -116 3294 8875
| 2 1 3 17 32 32 .05 | 6056 1257
iac n/a| 1 0 -4 19 -8 -4 -.27 26 24 | -1402 -475 3286 9955
| 1 2 1 31 61 99 .07 | 5767 959
Table 1.2238.b GPS week : 2238 MJD: 59910.0-59916.0
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 | 22 23 21 19 27 22 18 |
R02 | 10 11 10 8 13 10 7 |
R03 | 9 10 7 9 9 11 7 |
R04 | 11 12 12 11 9 9 10 |
R05 | 7 9 10 11 9 9 8 |
R07 | 13 10 8 8 13 14 10 |
R08 | 14 10 9 9 6 10 6 |
R09 | 22 22 21 22 22 23 27 |
R11 | 19 17 17 15 17 16 15 |
R12 | 12 11 11 11 10 9 10 |
R13 | 25 25 22 23 18 20 16 |
R14 | 21 16 13 9 10 8 9 |
R15 | 26 12 14 13 11 9 8 |
R17 | 9 11 10 9 7 8 8 |
R18 | 10 10 10 10 13 12 11 |
R19 | 34 31 31 34 31 30 29 |
R20 | 46 51 38 37 37 32 29 |
R21 | 14 15 10 12 9 10 11 |
R22 | 147 149 155 150 151 143 146 |
R24 | 15 12 8 9 11 11 8 |
Table 1.2238.c GPS week : 2238 MJD: 59910.0-59916.0
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 2238 0 | 75 29 -1 -354 4200 2416 81.8 1583 1583 | -12079 0
brd 2238 1 | -6 -71 134 -54 2969 1937 81.1 1790 1790 | -14670 0
brd 2238 2 | -108 60 131 1062 1480 -560 80.1 1770 1770 | -736 0
brd 2238 3 | -23 -36 115 -243 -189 -7078 81.0 1954 1954 | 291 0
brd 2238 4 | 21 -21 4 -570 -296 -9026 80.3 1878 1878 | -244 0
brd 2238 5 | 2 0 42 -213 -1269 -8669 79.5 1699 1699 | 654 0
brd 2238 6 | 19 -39 10 385 -875 -10950 79.7 1534 1534 | -391 0
-------------+------------------------------------------------------------+----------------
brd 2238 mean| -2 -11 62 1 859 -4561 80.5 1744 1744 | -3882 0
brd 2238 sdev| 56 44 62 552 2080 5640 .8 151 151 | 6543 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 2.2238.0 GPS week: 2238 Day: 0 MJD: 59910
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 10 65 .15 25 23 | 17578 1494 3509 9244
esx n/a| 2 0 1 -39 10 -28 -.08 34 21 | -13224 1672 4998 16836
gfz n/a| 0 6 -1 17 44 -9 -.19 37 27 | 0 2022 3534 9361
grg n/a| 0 -8 -3 23 -64 -61 .21 47 31 | -10132 1775 4928 15277
iac n/a| 0 2 -5 -22 -2 -130 -.25 35 33 | -8242 805 4924 15900
Table 2.2238.1 GPS week: 2238 Day: 1 MJD: 59911
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 1 1 6 -16 44 .11 25 18 | 17809 -888 2950 8869
esx n/a| 2 1 2 -47 -18 -27 -.19 37 24 | -11259 -1637 2993 8192
gfz n/a| 1 4 -3 32 47 -58 -.20 38 32 | 0 -790 2913 8797
grg n/a| 4 -8 -4 9 -3 -1 .24 35 32 | -14291 -1128 3039 7751
iac n/a| 0 0 -6 22 80 121 -.39 27 23 | -11212 -1596 2995 9129
Table 2.2238.2 GPS week: 2238 Day: 2 MJD: 59912
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 3 -2 48 .17 22 17 | 31234 -2251 3099 9284
esx n/a| -2 0 2 -31 -29 -39 -.16 38 24 | -3407 -2185 3060 8126
gfz n/a| 1 4 -4 18 0 -3 -.20 27 24 | 0 -1747 3097 9204
grg n/a| 3 -5 3 -7 28 -30 .16 30 19 | -140 -1377 3046 8383
iac n/a| 2 0 -5 60 -39 26 -.21 23 21 | 1342 -796 3075 9636
Table 2.2238.3 GPS week: 2238 Day: 3 MJD: 59913
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 3 -1 2 -22 66 .15 21 17 | 30065 947 3048 7908
esx n/a| 0 3 2 -20 -10 -35 -.26 37 28 | -884 574 2965 7035
gfz n/a| -3 -2 0 27 3 -45 -.08 25 23 | 0 683 3023 7884
grg n/a| 5 -4 1 1 13 -9 .12 33 20 | -548 1258 3016 7257
iac n/a| 3 0 -4 34 -63 -140 -.32 22 20 | 1841 201 3000 8238
Table 2.2238.4 GPS week: 2238 Day: 4 MJD: 59914
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 2 0 -13 72 .09 22 19 | 32472 -1621 3133 9170
esx n/a| 0 -1 0 -19 3 -15 -.24 38 28 | -7716 -1121 3114 10855
gfz n/a| -1 5 0 34 -11 -41 -.10 29 16 | 0 -472 3127 9185
grg n/a| 3 -5 2 -16 17 -11 .14 28 22 | -140 -438 3110 8510
iac n/a| 1 -2 -2 -15 43 82 -.27 25 24 | 2601 -1728 3117 9552
Table 2.2238.5 GPS week: 2238 Day: 5 MJD: 59915
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 28 -1 40 .15 28 20 | 33117 861 2713 8134
esx n/a| 0 1 2 -26 32 -21 -.29 31 21 | 3365 629 2710 7382
gfz n/a| -1 1 -3 70 -6 -47 -.09 27 18 | 0 940 2701 8208
grg n/a| 3 -4 1 -22 -31 44 .19 24 19 | 343 285 2748 7236
iac n/a| 3 3 -3 8 13 18 -.26 22 22 | 2311 233 2726 8599
Table 2.2238.6 GPS week: 2238 Day: 6 MJD: 59916
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 0 12 -14 73 .14 23 16 | 33611 -1800 3225 8291
esx n/a| 2 0 -3 -20 35 -23 -.24 32 21 | 11319 -2771 3151 7531
gfz n/a| 2 1 -3 24 24 -22 -.09 22 21 | 0 -937 3226 8353
grg n/a| 0 -3 5 -21 -21 -27 .12 26 18 | 192 -1188 3176 7715
iac n/a| 0 2 -2 48 -93 -6 -.18 25 23 | 1544 -450 3168 8637
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 3.2238.0 GPS week: 2238 Day: 0 MJD: 59910
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 706 41 28 30 52 27 22 | 104 74 80 63 83 80
R02 | 1557 9 12 23 26 19 9 | 76 82 87 67 69 77
R03 | 955 10 15 24 11 12 9 | 73 64 80 72 73 70
R04 | 854 15 20 24 16 18 10 | 85 73 82 84 77 79
R05 | 1064 5 8 19 16 21 7 | 58 60 62 63 55 59
R07 | 715 16 12 37 22 28 13 | 78 69 90 67 80 73
R08 | 1289 16 25 28 28 18 13 | 69 89 84 62 64 74
R09 | 1892 29 23 24 72 33 22 | 82 86 86 51 81 71
R11 | 2114 21 13 36 59 27 18 | 22 32 47 66 47 31
R12 | 507 14 12 37 17 78 12 | 118 120 117 116 103 116
R13 | 874 23 33 78 32 43 25 | 82 87 127 71 89 84
R14 | 1521 26 25 47 55 43 21 | 64 61 61 96 76 61
R15 | 1436 22 25 43 86 45 25 | 103 90 112 145 100 103
R17 | 1099 7 12 22 22 15 8 | 43 36 48 47 35 40
R18 | 441 13 20 21 14 18 10 | 35 42 38 40 32 36
R19 | 1219 55 60 40 79 44 34 | 77 63 104 79 79 75
R20 | 1643 51 111 44 96 57 46 | 103 86 104 104 92 86
R21 | 992 19 17 41 19 19 14 | 45 45 66 47 44 45
XR22 | 4007 --- 113 --- 191 197 147 | --- 90 --- 36 36 62
R24 | 4437 16 23 44 17 25 15 | 44 41 55 45 42 40
------+------------------------------------+--------------------------------
RMS | 1582 25 34 37 47 35 |T 71 69 80 71 67 68
WRMS | 1582 23 21 27 31 33 |NE 71 69 80 71 67 68
MEDI | 1099 16 20 36 26 27 |MD 76 69 82 66 73 71
Table 3.2238.1 GPS week: 2238 Day: 1 MJD: 59911
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 648 44 42 22 37 24 22 | 77 50 68 52 55 60
R02 | 727 12 17 20 23 22 10 | 57 57 45 45 51 50
R03 | 983 11 13 30 12 18 9 | 53 57 53 46 54 50
R04 | 731 19 24 22 17 16 12 | 62 46 70 51 52 55
R05 | 834 8 18 20 14 17 8 | 42 37 49 51 45 42
R07 | 844 7 16 23 24 17 10 | 52 57 57 51 48 52
R08 | 1254 9 21 23 18 17 10 | 49 59 53 45 47 49
R09 | 2670 27 22 33 59 31 21 | 95 95 95 31 91 77
R11 | 1841 19 15 37 43 20 17 | 24 47 43 87 47 42
R12 | 1950 11 14 31 14 21 10 | 48 42 45 50 38 44
R13 | 1775 40 44 57 33 29 25 | 73 42 77 50 55 51
R14 | 959 17 18 47 22 19 15 | 44 56 77 53 55 50
R15 | 2734 12 19 31 20 21 11 | 71 68 68 93 75 71
R17 | 807 11 21 31 10 17 11 | 25 28 39 24 28 23
R18 | 442 11 26 19 12 17 10 | 25 23 27 29 33 23
R19 | 3663 38 62 43 67 40 30 | 29 37 52 32 33 31
R20 | 1661 61 115 85 88 63 50 | 60 80 112 54 63 61
R21 | 1097 18 15 48 13 22 15 | 29 32 52 32 28 28
XR22 | 2028 --- 145 --- 151 158 148 | --- 68 --- 27 22 44
R24 | 3366 16 17 34 13 29 12 | 30 33 52 36 23 31
------+------------------------------------+--------------------------------
RMS | 1789 25 37 38 35 27 |T 49 50 59 46 47 46
WRMS | 1789 18 24 32 32 23 |NE 49 50 59 46 47 46
MEDI | 1097 16 19 31 20 21 |MD 49 47 53 46 47 49
Table 3.2238.2 GPS week: 2238 Day: 2 MJD: 59912
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 700 45 48 22 19 24 21 | 88 67 73 65 64 71
R02 | 855 11 17 21 20 17 10 | 72 78 88 71 67 75
R03 | 989 11 11 16 10 25 7 | 62 58 55 60 71 58
R04 | 831 19 15 28 14 18 11 | 73 65 77 60 64 68
R05 | 737 9 8 23 21 17 9 | 61 58 75 52 66 60
R07 | 653 12 14 13 12 11 7 | 57 39 44 52 49 48
R08 | 734 7 23 18 13 15 9 | 50 65 43 42 55 48
R09 | 3142 26 28 27 55 24 20 | 80 91 90 34 79 70
R11 | 1710 20 17 37 36 22 16 | 27 41 51 70 40 38
R12 | 3304 12 19 26 20 30 11 | 48 41 54 49 50 44
R13 | 1668 34 47 36 31 29 21 | 61 37 57 42 51 41
R14 | 1279 13 20 30 21 26 12 | 42 51 60 40 38 43
R15 | 3370 18 14 37 22 25 14 | 74 66 80 66 63 68
R17 | 701 12 17 23 12 15 9 | 41 39 49 42 38 40
R18 | 659 12 23 20 16 18 10 | 32 30 31 31 30 28
R19 | 2706 28 74 46 68 24 31 | 54 36 66 62 54 50
R20 | 1611 43 115 26 59 46 37 | 72 47 59 73 64 56
R21 | 891 10 20 19 16 21 9 | 37 38 51 40 36 39
XR22 | 977 --- 167 --- 143 151 154 | --- 53 --- 33 37 33
R24 | 2002 14 13 17 12 13 8 | 39 40 37 41 39 37
------+------------------------------------+--------------------------------
RMS | 1770 22 38 27 30 23 |T 56 52 60 51 52 50
WRMS | 1770 17 24 24 19 21 |NE 56 52 60 51 52 50
MEDI | 977 13 19 23 20 22 |MD 57 47 57 49 51 48
Table 3.2238.3 GPS week: 2238 Day: 3 MJD: 59913
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 758 35 40 25 25 29 18 | 73 34 54 58 37 54
R02 | 659 8 9 14 19 16 7 | 44 40 47 30 39 40
R03 | 1667 12 13 21 10 10 8 | 61 57 72 63 60 62
R04 | 932 23 13 19 16 13 10 | 66 42 48 42 53 49
R05 | 797 14 14 26 17 20 10 | 58 56 68 46 59 55
R07 | 857 10 16 15 13 13 8 | 61 44 63 54 58 56
R08 | 763 12 16 17 12 16 8 | 52 51 48 50 54 49
R09 | 3942 28 29 31 60 38 21 | 78 89 82 35 80 66
R11 | 2308 16 12 26 41 17 14 | 16 28 31 54 26 24
R12 | 3144 13 15 26 15 18 10 | 44 42 52 39 48 41
R13 | 914 40 39 42 37 32 23 | 49 38 57 39 54 40
R14 | 2111 9 19 15 18 15 9 | 44 52 54 43 41 45
R15 | 3217 19 12 24 28 18 12 | 60 55 58 46 47 51
R17 | 883 12 19 18 10 10 9 | 34 28 43 33 36 32
R18 | 941 18 18 17 15 15 10 | 24 32 34 33 30 28
R19 | 2732 33 77 34 83 31 33 | 73 58 82 70 67 67
R20 | 1629 28 113 34 61 27 36 | 76 35 89 97 67 72
R21 | 758 16 10 30 18 30 11 | 32 27 38 31 42 29
XR22 | 1184 --- 146 --- 154 161 150 | --- 49 --- 26 27 31
R24 | 2679 13 17 17 17 21 9 | 37 36 31 31 30 31
------+------------------------------------+--------------------------------
RMS | 1954 21 37 25 33 22 |T 51 44 55 46 47 46
WRMS | 1954 17 28 22 20 20 |NE 51 44 55 46 47 46
MEDI | 941 16 16 24 18 18 |MD 52 42 54 42 47 45
Table 3.2238.4 GPS week: 2238 Day: 4 MJD: 59914
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 847 57 52 31 31 32 26 | 90 60 63 54 72 64
R02 | 714 10 27 27 24 16 12 | 71 80 76 67 80 70
R03 | 1171 11 11 24 15 24 9 | 55 53 60 55 60 54
R04 | 877 18 11 17 13 19 9 | 64 60 59 56 64 59
R05 | 1122 16 7 20 12 12 8 | 58 53 50 43 48 50
R07 | 843 16 11 33 22 13 12 | 63 53 66 49 55 56
R08 | 780 9 10 10 9 22 5 | 52 55 58 62 49 56
R09 | 3028 28 26 36 57 42 22 | 76 77 93 27 68 62
R11 | 2134 27 12 28 43 20 17 | 15 34 38 72 33 32
R12 | 2153 12 16 18 21 23 9 | 46 48 50 42 40 43
R13 | 591 22 32 45 25 41 18 | 48 40 79 49 71 51
R14 | 2502 15 19 24 13 18 10 | 44 52 39 45 40 42
R15 | 3107 11 19 23 19 27 10 | 66 53 73 66 50 63
R17 | 971 7 15 17 10 16 7 | 34 30 39 30 39 31
R18 | 1256 19 29 25 12 29 12 | 23 30 41 26 36 26
R19 | 2531 36 86 38 50 24 31 | 62 31 73 62 50 54
R20 | 1732 24 108 56 51 23 36 | 63 48 95 82 65 67
R21 | 909 7 17 20 13 16 8 | 28 23 37 30 30 26
XR22 | 1232 --- 159 --- 142 151 150 | --- 42 --- 25 28 22
R24 | 3701 13 17 26 20 32 11 | 36 33 30 39 45 31
------+------------------------------------+--------------------------------
RMS | 1878 22 38 29 28 25 |T 52 47 58 49 51 47
WRMS | 1878 19 28 16 22 24 |NE 52 47 58 49 51 47
MEDI | 1171 16 17 25 20 23 |MD 55 48 59 49 49 51
Table 3.2238.5 GPS week: 2238 Day: 5 MJD: 59915
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 695 50 42 23 30 25 22 | 71 43 63 43 63 52
R02 | 651 9 14 28 13 16 10 | 57 65 56 60 57 57
R03 | 2044 12 13 29 13 18 10 | 50 57 58 58 60 53
R04 | 790 15 10 22 10 17 8 | 61 55 64 63 61 59
R05 | 1047 19 15 9 15 14 8 | 45 34 35 38 31 36
R07 | 914 15 17 34 21 23 13 | 54 43 76 41 61 51
R08 | 833 8 15 26 16 20 10 | 47 37 63 41 52 45
R09 | 2897 34 29 27 54 21 22 | 82 67 79 35 66 57
R11 | 1436 31 15 20 35 19 15 | 18 27 31 59 28 26
R12 | 1701 16 17 17 10 17 9 | 53 54 61 52 48 53
R13 | 988 21 35 53 23 21 20 | 42 38 70 38 47 39
R14 | 2384 14 11 13 13 16 7 | 39 45 51 50 39 46
R15 | 2749 17 15 15 15 25 9 | 65 56 61 58 49 58
R17 | 1117 10 14 17 13 14 8 | 25 27 30 29 29 25
R18 | 1051 20 28 21 11 23 12 | 25 35 40 31 37 29
R19 | 1553 63 63 43 36 22 30 | 41 40 71 31 31 41
R20 | 2568 52 80 42 37 43 31 | 53 42 60 40 42 41
R21 | 1404 17 21 20 12 18 10 | 25 32 31 27 25 25
XR22 | 747 --- 159 --- 128 142 143 | --- 54 --- 27 25 23
R24 | 2367 13 24 17 16 20 10 | 31 40 33 39 38 32
------+------------------------------------+--------------------------------
RMS | 1699 28 31 27 24 22 |T 46 44 54 43 44 42
WRMS | 1699 20 21 18 19 22 |NE 46 44 54 43 44 42
MEDI | 1117 17 17 22 15 20 |MD 47 42 60 40 42 41
Table 3.2238.6 GPS week: 2238 Day: 6 MJD: 59916
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 618 35 42 23 23 26 18 | 103 62 91 65 70 80
R02 | 882 8 9 16 10 16 6 | 81 90 87 79 82 84
R03 | 1804 9 13 14 11 26 7 | 71 72 78 76 79 74
R04 | 876 12 14 23 16 24 10 | 82 87 83 77 77 80
R05 | 1053 12 12 15 16 18 8 | 64 63 62 55 58 60
R07 | 721 9 11 16 24 23 9 | 78 70 77 60 82 71
R08 | 1184 11 10 12 9 24 6 | 65 67 68 60 70 64
R09 | 3460 38 43 32 65 30 26 | 80 84 73 45 70 57
R11 | 1139 22 21 27 32 14 15 | 23 37 42 30 33 26
R12 | 695 14 15 20 16 20 9 | 57 59 65 58 62 58
R13 | 759 19 31 34 20 23 15 | 64 46 82 52 53 58
R14 | 1315 12 16 19 15 11 9 | 52 58 51 59 46 53
R15 | 1515 14 18 14 12 19 8 | 84 70 76 80 67 77
R17 | 1028 12 13 18 8 12 7 | 44 35 46 44 38 41
R18 | 826 15 25 22 14 20 11 | 31 39 44 35 27 34
R19 | 727 44 67 31 59 27 29 | 77 61 82 76 72 69
R20 | 3062 51 87 21 27 66 29 | 95 66 92 101 91 81
R21 | 1623 9 20 24 22 19 11 | 41 37 48 50 38 41
XR22 | 1203 --- 162 --- 131 130 146 | --- 87 --- 24 28 41
R24 | 1957 14 17 11 12 16 8 | 43 42 39 41 43 39
------+------------------------------------+--------------------------------
RMS | 1533 23 32 22 26 25 |T 65 61 67 58 59 59
WRMS | 1533 16 21 21 18 23 |NE 65 61 67 58 59 59
MEDI | 1053 14 17 20 16 20 |MD 65 62 73 58 62 58
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