[IGSREPORT-29010] Wk 2232 IGLOS Final Orbits
acc
acc at igs.org
Sat Nov 5 09:51:38 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2232 (Oct 16, 2022 - Oct 22, 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 2.2232.
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:
igl2232[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2232 in the SP3 format.
igl22327.sum Combination Report for GPS Week 2232.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -5.0 ns
1 | 0.8 ns
2 | -1.3 ns
3 | -7.8 ns
4 | -7.4 ns
5 | -5.6 ns
6 | -6.8 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESX | R22
1 | ESX | R22
2 | ESX | R22
3 | ESX | R22
4 | ESX | R22
5 | ESX | R22
6 | ESX | R22
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 1.2232, 1a.2232).
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 2.2232.0-6)
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 3.2232.0-6).
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 2232 summary. (Oct 16, 2022 - Oct 22, 2022)
Table 1.2232.a GPS week : 2232 MJD: 59868.0-59874.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 6 -19 10 29 .19 27 19 | 27129 -774 2893 8191
| 0 2 2 7 14 39 .04 | 4437 2303
emx n/a| 0 0 -10 37 -1 -55 .07 40 29 | -10432 -636 2876 8100
| 2 0 2 25 24 33 .05 | 11775 1777
esx n/a| 0 1 0 -10 -2 15 .00 27 20 | -5520 -71 2886 7390
| 1 1 1 17 23 46 .04 | 7239 2151
gfz n/a| 0 0 1 12 -16 5 -.09 31 16 | 0 -552 2935 8009
| 1 1 1 24 21 25 .07 | 0 2528
grg n/a| 1 -3 4 0 1 -28 .19 30 22 | -4716 -434 2891 7533
| 1 1 5 21 15 71 .05 | 3133 2208
iac n/a| 0 0 -4 0 13 3 -.28 25 22 | -2593 -387 2892 8715
| 2 2 4 30 51 79 .10 | 3202 978
Table 1.2232.b GPS week : 2232 MJD: 59868.0-59874.0
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 15 15 13 14 14 14 |
R02 | 6 7 6 6 7 6 6 |
R03 | 7 7 6 5 6 5 6 |
R04 | 7 5 9 9 9 10 10 |
R05 | 8 9 7 9 9 7 9 |
R07 | 7 8 6 7 6 5 8 |
R08 | 8 8 7 8 7 8 8 |
R09 | 18 16 19 15 18 13 13 |
R11 | 9 9 8 7 8 11 11 |
R12 | 9 9 9 9 10 9 9 |
R13 | 15 15 16 13 17 17 17 |
R14 | 10 9 9 8 10 11 8 |
R15 | 8 8 8 8 7 8 8 |
R17 | 8 9 8 9 9 9 8 |
R18 | 11 9 8 7 9 10 9 |
R19 | 22 30 31 25 26 27 27 |
R20 | 24 28 31 31 33 31 31 |
R21 | 8 8 8 8 8 9 7 |
R22 | 18 13 35 13 21 12 14 |
R24 | 9 9 9 9 10 8 12 |
Table 1.2232.c GPS week : 2232 MJD: 59868.0-59874.0
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 2232 0 | 21 -16 -6 -1431 761 -3761 80.7 2120 2120 | -4956 0
brd 2232 1 | 19 0 20 -1102 109 -11800 82.4 1813 1813 | 758 0
brd 2232 2 | -54 13 93 1145 158 -4583 82.2 1759 1759 | -1291 0
brd 2232 3 | -60 52 176 1301 -1721 -5367 82.5 1455 1455 | -7827 0
brd 2232 4 | 19 -17 82 121 -951 -5436 81.7 1217 1217 | -7397 0
brd 2232 5 | -44 -15 55 132 681 116 81.7 1175 1175 | -5634 0
brd 2232 6 | -20 -34 42 -105 2015 1618 81.3 1199 1199 | -6818 0
-------------+------------------------------------------------------------+----------------
brd 2232 mean| -16 -2 66 8 150 -4173 81.8 1534 1534 | -4737 0
brd 2232 sdev| 37 28 59 1025 1214 4348 .7 369 369 | 3262 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 2.2232.0 GPS week: 2232 Day: 0 MJD: 59868
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 5 -12 21 41 .24 26 18 | 25464 2263 3058 8167
emx n/a| 0 0 -9 53 -11 -58 .16 36 30 | -2600 2070 3065 8076
esx n/a| 0 0 0 10 1 -60 -.02 23 16 | -15406 3150 3055 6111
gfz n/a| 0 2 2 51 -27 -14 -.21 28 14 | 0 3058 3104 7747
grg n/a| 1 -4 9 -34 27 18 .27 28 23 | -6349 2424 3082 7582
iac n/a| -2 0 -11 -44 -25 36 -.27 27 23 | -3333 -101 3081 8721
Table 2.2232.1 GPS week: 2232 Day: 1 MJD: 59869
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 2 -11 13 0 .23 28 18 | 33797 1302 2649 8055
emx n/a| -4 0 -12 14 -15 -18 .03 38 28 | -6575 1390 2648 7923
esx n/a| 1 1 0 -5 -13 10 -.08 27 20 | 6189 2449 2644 6272
gfz n/a| -2 2 1 33 -9 -1 -.04 33 17 | 0 1772 2691 8091
grg n/a| 0 -5 5 -21 13 -183 .19 32 26 | -499 1846 2627 7539
iac n/a| 1 0 -3 -24 13 110 -.29 24 19 | 2595 654 2649 8844
Table 2.2232.2 GPS week: 2232 Day: 2 MJD: 59870
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 -3 5 -23 -16 -40 .15 28 19 | 33348 -3473 2869 7967
emx n/a| 0 -1 -14 76 -46 -86 .02 41 28 | 6865 -2161 2817 7732
esx n/a| 0 1 -1 -24 -33 -24 -.01 28 19 | -1337 -2186 2820 10121
gfz n/a| 0 0 2 6 -51 23 -.06 35 16 | 0 -3318 2902 7978
grg n/a| 3 -2 10 9 -6 19 .21 32 24 | 136 -3280 2832 7117
iac n/a| 0 5 -2 18 107 69 -.22 26 21 | 1136 -1722 2800 8380
Table 2.2232.3 GPS week: 2232 Day: 3 MJD: 59871
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 7 -26 21 64 .18 26 19 | 24821 -2102 2713 8562
emx n/a| -1 0 -9 36 19 -36 .10 44 28 | -22757 -1980 2713 8472
esx n/a| 0 2 0 -11 34 46 .04 28 22 | -1301 -669 2744 6366
gfz n/a| 1 -1 3 -21 -8 2 -.16 29 18 | 0 -2239 2716 8278
grg n/a| 1 -2 6 1 10 -18 .22 31 23 | -7476 -1070 2740 7827
iac n/a| 0 -1 -8 49 -49 -37 -.13 20 17 | -5725 354 2766 9032
Table 2.2232.4 GPS week: 2232 Day: 4 MJD: 59872
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 -4 4 -16 3 19 .21 27 17 | 23879 -2429 3013 9286
emx n/a| 0 1 -9 45 5 -25 .07 39 30 | -27816 -1848 2969 9323
esx n/a| 0 1 0 13 20 79 .03 28 20 | -6482 -1841 3012 9392
gfz n/a| 0 1 3 -8 20 37 -.04 32 15 | 0 -2714 3053 9304
grg n/a| 0 -1 0 19 -12 -26 .18 32 22 | -6308 -2461 3042 8521
iac n/a| 5 0 -3 -17 -10 -92 -.40 29 25 | -4945 -1430 3031 9667
Table 2.2232.5 GPS week: 2232 Day: 5 MJD: 59873
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 9 -18 23 54 .17 31 22 | 24679 1290 2817 8015
emx n/a| -1 0 -4 38 17 -110 .08 39 27 | -9027 -37 2809 7967
esx n/a| -2 2 2 -32 -2 19 .03 25 21 | -9664 367 2763 7753
gfz n/a| 0 0 0 10 -20 -36 -.03 30 14 | 0 1292 2869 7873
grg n/a| 0 -3 -3 22 -9 16 .14 27 18 | -6283 1021 2749 7258
iac n/a| 4 0 -2 4 14 28 -.41 27 23 | -3165 514 2739 8499
Table 2.2232.6 GPS week: 2232 Day: 6 MJD: 59874
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 7 -31 9 67 .15 26 19 | 23916 -2272 3132 7285
emx n/a| 2 0 -10 0 18 -51 .02 45 30 | -11119 -1887 3116 7213
esx n/a| 0 1 -2 -22 -21 38 .03 29 24 | -10640 -1771 3166 5720
gfz n/a| 1 0 0 13 -14 25 -.10 29 18 | 0 -1720 3214 6795
grg n/a| 0 -3 2 4 -12 -24 .14 27 20 | -6234 -1520 3166 6890
iac n/a| -1 0 1 6 47 -94 -.22 26 26 | -4716 -979 3178 7868
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 3.2232.0 GPS week: 2232 Day: 0 MJD: 59868
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 514 49 49 41 37 30 39 18 | 72 81 71 64 51 44 59
R02 | 863 10 14 16 12 14 15 6 | 40 44 43 36 39 42 38
R03 | 742 6 15 7 8 22 22 6 | 44 43 44 46 53 53 45
XR04 | 597 9 7 15 --- 18 18 7 | 43 44 38 --- 38 48 40
R05 | 1062 18 13 23 12 15 23 8 | 43 42 52 45 37 55 42
R07 | 896 13 11 9 10 15 26 6 | 53 55 52 48 48 55 49
R08 | 810 20 16 11 20 15 21 8 | 49 52 62 67 55 67 57
R09 | 3877 28 18 29 27 73 37 17 | 139 142 145 140 116 132 132
R11 | 919 23 11 22 20 25 11 9 | 34 38 38 42 52 46 38
R12 | 2145 13 29 22 13 18 16 8 | 45 35 52 46 52 44 42
R13 | 625 34 51 25 26 19 36 14 | 86 42 51 58 68 61 56
R14 | 875 13 42 10 10 21 26 9 | 66 51 77 77 83 87 72
R15 | 526 13 32 17 16 15 12 8 | 92 70 86 101 97 95 90
R17 | 2743 12 34 10 14 19 21 8 | 71 45 58 65 74 69 63
R18 | 664 19 37 19 12 32 20 10 | 58 48 72 60 82 69 63
R19 | 1236 34 61 35 74 38 47 22 | 113 121 116 136 117 104 110
R20 | 5807 61 72 49 61 31 42 24 | 111 66 84 100 79 55 75
R21 | 658 13 27 13 15 22 13 7 | 66 50 60 63 65 60 59
XR22E | 3527 --- --- 381 --- 18 16 17 | --- --- 299 --- 294 295 297
R24 | 3341 17 32 14 17 21 13 8 | 73 60 60 64 72 67 64
------+-----------------------------------------+-------------------------------------
RMS | 2119 26 36 23 28 28 27 |T 68 59 78 69 78 77 74
WRMS | 2119 18 30 16 14 23 23 |NE 68 59 66 69 67 65 62
MEDI | 875 17 29 17 15 19 21 |MD 66 50 60 63 65 60 59
Table 3.2232.1 GPS week: 2232 Day: 1 MJD: 59869
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 567 36 49 27 19 26 38 15 | 37 46 47 33 35 25 29
R02 | 738 9 18 14 20 14 18 7 | 27 36 32 28 18 19 22
R03 | 1114 7 10 25 10 18 11 6 | 21 21 23 21 29 24 19
XR04 | 676 6 9 8 --- 12 9 4 | 22 22 31 --- 30 31 25
R05 | 860 23 16 17 24 16 14 8 | 26 24 40 32 35 34 27
R07 | 1147 7 9 23 22 16 19 8 | 29 29 32 23 28 28 24
R08 | 621 22 16 20 20 16 13 8 | 25 33 36 33 24 28 27
R09 | 3245 35 20 18 25 68 28 16 | 120 122 111 120 90 111 109
R11 | 1422 15 24 19 19 24 16 8 | 37 48 35 39 23 46 35
R12 | 2027 12 25 26 13 20 15 8 | 40 36 45 31 41 46 37
R13 | 540 45 47 24 27 37 20 15 | 64 21 33 38 67 33 37
R14 | 971 9 33 17 16 20 17 8 | 68 63 78 67 83 72 70
R15 | 616 10 34 14 13 14 15 7 | 77 60 65 78 67 80 72
R17 | 1943 14 35 14 10 24 20 9 | 43 33 34 35 48 51 39
R18 | 774 12 21 24 21 25 13 8 | 41 34 45 37 50 38 39
R19 | 924 44 92 59 91 79 38 30 | 91 86 104 123 99 84 89
R20 | 4910 71 72 60 75 26 54 27 | 49 67 53 38 48 43 39
R21 | 887 18 28 12 10 22 12 7 | 44 35 42 39 42 38 38
XR22E | 2636 --- --- 395 --- 16 10 13 | --- --- 354 --- 287 281 283
R24 | 2487 23 28 18 11 24 13 8 | 48 40 34 40 46 45 40
------+-----------------------------------------+-------------------------------------
RMS | 1812 28 38 27 33 32 24 |T 47 45 63 47 59 57 55
WRMS | 1812 18 28 20 17 26 19 |NE 47 45 48 47 47 46 43
MEDI | 924 15 25 19 19 20 15 |MD 41 36 40 37 42 38 37
Table 3.2232.2 GPS week: 2232 Day: 2 MJD: 59870
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 960 34 47 37 33 29 15 14 | 51 63 40 45 39 43 42
R02 | 1785 9 10 14 14 12 15 5 | 31 40 42 39 32 25 32
R03 | 970 8 7 11 12 12 21 6 | 35 37 35 26 30 43 33
XR04 | 909 15 11 22 --- 14 17 8 | 31 29 26 --- 25 27 25
R05 | 701 21 19 15 15 14 11 7 | 31 35 38 34 27 26 28
R07 | 839 7 11 12 15 14 19 6 | 34 40 32 32 37 47 35
R08 | 1157 11 11 21 17 16 15 7 | 36 39 52 50 42 43 41
R09 | 2800 37 34 23 25 78 33 18 | 127 120 120 112 103 122 111
R11 | 1545 14 15 17 14 26 17 8 | 59 65 74 62 69 64 64
R12 | 2223 16 36 12 27 15 13 9 | 37 36 45 56 47 48 40
R13 | 821 53 34 23 30 29 30 15 | 85 41 48 53 82 54 56
R14 | 749 20 31 18 15 17 15 8 | 63 53 59 61 70 59 59
R15 | 736 11 31 12 13 22 13 7 | 59 49 67 64 79 67 63
R17 | 1646 14 33 12 14 19 16 8 | 48 28 38 47 46 59 44
R18 | 758 8 24 23 23 18 10 8 | 38 38 45 31 51 48 39
R19 | 1630 40 112 55 93 77 29 30 | 41 59 55 73 58 28 32
R20 | 4773 68 75 75 85 30 73 31 | 67 43 72 73 46 50 43
R21 | 1229 14 33 16 14 13 15 8 | 49 36 41 46 44 47 42
XR22E | 2068 --- 86 401 --- 27 31 35 | --- 21 373 --- 379 369 386
R24 | 950 19 34 15 10 15 26 9 | 57 36 51 48 52 45 46
------+-----------------------------------------+-------------------------------------
RMS | 1758 28 41 28 35 32 26 |T 51 45 67 52 67 65 63
WRMS | 1758 19 28 19 16 24 21 |NE 51 46 51 52 51 49 46
MEDI | 970 15 31 17 15 17 16 |MD 48 39 45 48 46 47 42
Table 3.2232.3 GPS week: 2232 Day: 3 MJD: 59871
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 911 37 36 34 21 29 15 13 | 55 49 42 43 38 52 43
R02 | 2001 10 12 15 11 15 12 5 | 34 39 49 41 33 38 37
R03 | 775 10 12 7 13 11 14 5 | 33 44 44 36 40 49 40
XR04 | 509 11 15 19 --- 17 20 8 | 38 34 34 --- 31 55 38
R05 | 663 25 19 25 24 12 11 9 | 30 34 45 34 31 31 29
R07 | 1550 12 12 11 13 22 15 6 | 39 41 44 41 43 37 38
R08 | 926 10 21 15 24 18 19 8 | 38 35 47 56 45 33 39
R09 | 2250 27 24 18 22 72 23 15 | 62 75 68 74 52 71 59
R11 | 1957 17 16 11 12 24 16 7 | 70 74 70 69 64 68 68
R12 | 1475 21 38 12 13 19 21 9 | 39 39 39 50 58 57 45
R13 | 595 36 42 25 30 26 19 13 | 84 60 60 69 63 60 62
R14 | 598 17 29 21 11 16 13 8 | 80 65 89 73 77 73 76
R15 | 703 11 27 10 17 22 19 8 | 64 55 64 62 69 48 58
R17 | 1171 22 31 13 18 13 16 8 | 62 35 54 63 55 48 52
R18 | 725 11 19 24 14 18 11 7 | 43 37 60 42 51 51 47
R19 | 2066 40 102 55 64 63 18 25 | 48 59 51 76 40 36 40
R20 | 2340 61 112 74 80 46 52 31 | 86 58 49 93 49 52 50
R21 | 1552 11 41 15 11 16 12 7 | 57 27 49 56 60 53 51
XR22E | 1837 --- --- 375 --- 17 9 12 | --- --- 312 --- 249 239 240
R24 | 1626 23 36 12 16 27 15 9 | 64 35 48 41 57 39 45
------+-----------------------------------------+-------------------------------------
RMS | 1455 26 44 28 29 31 20 |T 54 47 65 56 60 59 57
WRMS | 1455 19 28 22 18 23 17 |NE 54 47 52 56 50 50 48
MEDI | 1171 17 27 15 16 18 15 |MD 55 41 49 56 51 51 45
Table 3.2232.4 GPS week: 2232 Day: 4 MJD: 59872
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 837 37 39 21 21 44 25 14 | 58 64 54 46 46 46 47
R02 | 663 10 13 19 11 13 23 7 | 41 41 55 45 39 48 43
R03 | 561 8 14 11 13 15 16 5 | 45 50 53 45 51 49 47
XR04 | 596 17 16 14 --- 20 23 9 | 45 46 41 --- 39 37 39
R05 | 1068 20 20 21 19 13 20 8 | 42 45 54 47 48 45 43
R07 | 1180 9 11 11 9 17 15 5 | 45 47 46 47 52 43 45
R08 | 1088 12 19 15 13 16 19 7 | 44 51 50 48 44 50 46
R09 | 2243 23 12 31 32 71 39 17 | 123 119 121 119 117 114 114
R11 | 1937 16 13 12 24 20 22 8 | 59 60 67 66 64 57 61
R12 | 745 15 40 15 16 21 24 9 | 56 54 47 49 57 62 50
R13 | 1028 34 55 32 40 25 39 16 | 82 54 55 87 75 67 65
R14 | 533 15 38 24 12 16 30 10 | 52 43 78 65 59 72 59
R15 | 609 11 24 11 13 15 21 7 | 74 60 73 70 76 65 69
R17 | 1040 15 32 17 14 20 19 8 | 56 41 50 55 56 45 49
R18 | 838 14 22 21 16 20 30 9 | 44 40 62 56 51 63 51
R19 | 1383 26 80 44 81 65 40 25 | 61 71 42 83 53 64 47
R20 | 2244 84 87 80 77 47 59 33 | 80 65 86 82 49 52 53
R21 | 1003 15 36 10 15 14 14 8 | 62 50 62 58 60 53 56
XR22E | 3181 --- --- 392 --- 21 19 20 | --- --- 354 --- 330 323 327
R24 | 818 18 37 17 15 26 23 10 | 47 35 42 35 57 45 40
------+-----------------------------------------+-------------------------------------
RMS | 1216 27 39 28 32 32 29 |T 58 54 74 61 71 70 67
WRMS | 1216 17 30 20 15 22 25 |NE 58 54 59 61 57 56 53
MEDI | 1003 15 24 17 15 20 23 |MD 56 50 54 55 53 52 49
Table 3.2232.5 GPS week: 2232 Day: 5 MJD: 59873
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1392 43 33 25 21 19 34 13 | 40 28 53 42 33 34 35
R02 | 542 13 13 15 8 11 14 5 | 25 22 20 21 25 26 19
R03 | 1296 7 10 10 12 11 16 5 | 27 29 35 39 31 30 30
XR04 | 882 17 26 12 --- 26 15 10 | 26 33 29 --- 17 17 19
R05 | 1461 15 15 15 16 9 16 6 | 22 29 31 31 27 18 22
R07 | 1237 10 13 14 8 9 8 4 | 27 24 24 22 22 25 22
R08 | 1402 20 23 13 23 9 19 8 | 24 17 33 40 27 38 28
R09 | 2227 18 17 26 29 39 35 13 | 122 126 133 131 109 128 123
R11 | 1936 24 11 22 18 35 29 11 | 59 66 78 65 82 70 69
R12 | 525 15 34 18 17 21 20 9 | 49 45 44 41 34 52 40
R13 | 768 31 48 43 48 26 29 17 | 89 68 52 93 75 64 69
R14 | 589 11 40 20 13 25 27 10 | 73 63 75 79 91 89 77
R15 | 788 11 30 10 20 16 14 7 | 56 40 55 65 57 51 54
R17 | 619 19 27 21 10 21 20 9 | 46 35 42 44 48 42 40
R18 | 869 16 28 19 19 24 24 9 | 43 35 46 42 62 50 44
R19 | 1152 36 90 38 74 71 51 27 | 53 63 43 54 54 61 42
R20 | 1187 101 86 61 64 40 45 30 | 73 40 53 45 42 32 32
R21 | 610 18 34 11 12 14 25 8 | 55 35 45 42 47 54 45
XR22E | 3184 --- --- 389 --- 12 12 12 | --- --- 490 --- 464 452 461
R24 | 717 13 32 11 14 15 17 7 | 46 53 49 49 48 51 46
------+-----------------------------------------+-------------------------------------
RMS | 1175 31 39 25 30 27 27 |T 50 44 71 52 69 69 65
WRMS | 1175 22 27 21 14 18 23 |NE 50 44 49 52 49 49 45
MEDI | 882 17 28 18 17 19 20 |MD 46 35 45 42 47 50 40
Table 3.2232.6 GPS week: 2232 Day: 6 MJD: 59874
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 949 38 39 28 28 23 24 13 | 74 72 63 63 56 54 60
R02 | 1371 11 19 12 8 9 15 5 | 47 44 50 45 44 46 45
R03 | 1394 8 14 10 13 15 12 5 | 49 47 52 47 54 55 50
XR04 | 783 19 25 20 --- 17 15 9 | 48 51 43 --- 44 45 44
R05 | 1096 16 19 19 20 16 23 8 | 44 46 52 45 40 38 40
R07 | 507 11 15 19 11 8 30 7 | 55 54 47 47 51 66 51
R08 | 1511 14 21 18 18 14 22 8 | 52 52 61 70 57 64 58
R09 | 1960 21 16 30 24 45 19 12 | 144 153 156 151 146 149 147
R11 | 1165 14 13 25 21 28 35 11 | 72 75 85 76 82 79 75
R12 | 993 12 33 14 18 26 15 8 | 44 32 45 46 48 46 41
R13 | 655 39 41 30 31 29 48 16 | 96 72 69 88 86 75 77
R14 | 832 8 32 14 14 19 15 7 | 85 73 81 78 93 91 83
R15 | 649 12 31 15 10 17 16 7 | 82 59 74 78 81 79 76
R17 | 711 14 33 16 16 16 15 8 | 86 67 73 80 80 87 79
R18 | 642 18 28 22 14 26 18 9 | 80 72 92 83 94 91 85
R19 | 2393 37 116 34 59 70 41 26 | 92 76 71 114 81 91 79
R20 | 1267 69 97 85 81 23 34 30 | 106 54 61 96 78 68 66
R21 | 553 17 28 11 12 11 13 7 | 85 64 77 78 80 81 78
XR22E | 2710 --- --- 392 --- 13 15 14 | --- --- 499 --- 482 467 476
R24 | 1041 16 54 17 17 25 32 12 | 88 77 82 90 97 101 87
------+-----------------------------------------+-------------------------------------
RMS | 1198 26 45 29 29 27 26 |T 75 65 91 76 93 93 89
WRMS | 1198 19 30 24 18 20 26 |NE 75 65 70 76 73 74 69
MEDI | 993 16 28 19 17 17 18 |MD 80 64 69 78 80 75 75
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