[IGSREPORT-28997] Wk 2231 IGLOS Final Orbits
acc
acc at igs.org
Mon Oct 31 01:17:37 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2231 (Oct 09, 2022 - Oct 15, 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 2.2231.
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:
igl2231[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2231 in the SP3 format.
igl22317.sum Combination Report for GPS Week 2231.
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 | -1.1 ns
1 | -6.4 ns
2 | -6.3 ns
3 | -6.9 ns
4 | -7.0 ns
5 | -0.1 ns
6 | -6.0 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 1.2231, 1a.2231).
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 2.2231.0-6)
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 3.2231.0-6).
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 2231 summary. (Oct 09, 2022 - Oct 15, 2022)
Table 1.2231.a GPS week : 2231 MJD: 59861.0-59867.0
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 0 3 -17 -8 14 .16 21 15 | 26597 -896 3081 8385
| 0 0 1 22 16 15 .05 | 2778 1186
emx n/a| 0 -1 -6 19 0 -48 -.02 38 28 | 1537 -1003 3060 8307
| 2 1 3 14 33 18 .08 | 7646 885
esx n/a| 0 1 -2 -6 6 -16 -.05 26 17 | -4881 -238 3065 7831
| 1 0 2 12 17 36 .03 | 6444 1042
gfz n/a| 0 1 1 8 -18 19 -.02 27 16 | 0 -744 3135 8268
| 1 1 2 22 19 26 .09 | 0 1017
grg n/a| 2 -3 3 -4 12 -7 .18 29 22 | -4813 -459 3063 7748
| 1 0 3 23 14 25 .10 | 3170 915
iac n/a| -1 0 -5 -3 26 1 -.33 29 27 | -2783 -344 3069 8842
| 2 2 2 34 50 75 .06 | 2848 563
Table 1.2231.b GPS week : 2231 MJD: 59861.0-59867.0
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 | 12 13 12 12 11 17 17 |
R02 | 7 6 6 6 8 6 5 |
R03 | 6 9 8 7 8 7 6 |
R04 | 8 7 9 7 6 7 9 |
R05 | 9 8 8 7 7 8 7 |
R07 | 6 6 6 8 6 6 6 |
R08 | 7 8 8 6 9 8 9 |
R09 | 15 15 13 14 16 16 15 |
R11 | 8 7 11 9 8 9 9 |
R12 | 11 12 13 11 9 9 8 |
R13 | 14 14 14 18 18 16 14 |
R14 | 8 7 9 9 11 10 9 |
R15 | 8 9 7 8 8 9 9 |
R17 | 6 8 8 10 8 8 9 |
R18 | 9 9 8 10 12 10 10 |
R19 | 19 25 22 22 23 26 22 |
R20 | 27 26 25 28 29 26 26 |
R21 | 8 8 8 9 9 10 8 |
R22 | 23 22 20 11 13 29 41 |
R24 | 9 9 9 8 9 11 11 |
Table 1.2231.c GPS week : 2231 MJD: 59861.0-59867.0
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 2231 0 | -25 29 239 1900 -234 -3994 81.6 1799 1799 | -1102 0
brd 2231 1 | -87 15 132 -1360 153 644 78.0 2095 2095 | -6411 0
brd 2231 2 | 166 55 35 757 1745 -7296 82.1 1740 1740 | -6330 0
brd 2231 3 | 28 60 -33 -323 -1096 -6077 81.8 1569 1569 | -6881 0
brd 2231 4 | -84 141 24 -1268 2430 -5721 82.2 1871 1871 | -7026 0
brd 2231 5 | -70 -129 3 252 1370 -1683 81.3 1814 1814 | -51 0
brd 2231 6 | -7 -18 31 -1002 2742 -2756 80.6 2061 2061 | -6019 0
-------------+------------------------------------------------------------+----------------
brd 2231 mean| -11 22 62 -149 1015 -3840 81.1 1849 1849 | -4831 0
brd 2231 sdev| 89 83 93 1201 1437 2782 1.5 182 182 | 2941 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 2.2231.0 GPS week: 2231 Day: 0 MJD: 59861
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 3 -27 7 0 .11 20 13 | 30998 -2645 3136 6706
emx n/a| -4 -1 -1 1 -34 -19 -.13 34 26 | 8738 -910 3138 6460
esx n/a| 0 1 -2 6 -7 -63 -.05 23 16 | -8892 -1498 3130 8691
gfz n/a| -1 0 -3 10 -17 18 .12 26 13 | 0 -2531 3199 6499
grg n/a| 2 -3 2 -10 8 6 .27 27 22 | -342 -1756 3126 6048
iac n/a| 1 2 -3 -1 79 71 -.36 29 27 | 967 -1393 3136 7144
Table 2.2231.1 GPS week: 2231 Day: 1 MJD: 59862
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 3 -51 1 -4 .08 22 15 | 25175 672 3319 9626
emx n/a| 2 -1 -7 33 -23 -73 -.10 37 28 | 6295 -407 3290 9629
esx n/a| 0 2 -1 0 -25 -12 -.08 26 17 | -3746 871 3256 8836
gfz n/a| -2 0 1 31 -47 -7 .03 26 16 | 0 570 3379 9588
grg n/a| 2 -2 4 -20 13 -6 .23 28 24 | -6802 310 3258 9066
iac n/a| -1 1 -6 28 51 67 -.30 31 28 | -4023 -402 3272 10178
Table 2.2231.2 GPS week: 2231 Day: 2 MJD: 59863
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 -30 -28 16 .17 17 14 | 26260 -635 3615 8853
emx n/a| 0 0 -2 22 -3 -49 .06 39 30 | -13974 -637 3580 8816
esx n/a| 0 2 -1 -25 6 35 -.02 28 20 | -3385 415 3587 7424
gfz n/a| 0 0 0 40 -3 69 -.13 28 15 | 0 -497 3676 8707
grg n/a| 3 -3 0 -26 0 -30 .29 25 18 | -6537 130 3605 8172
iac n/a| -4 0 -8 -30 82 -87 -.38 30 29 | -5041 412 3592 9469
Table 2.2231.3 GPS week: 2231 Day: 3 MJD: 59864
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 18 -35 6 .21 21 15 | 25998 -1773 3095 9481
emx n/a| 0 -2 -5 39 39 -68 .03 36 27 | 5142 -2291 3080 9387
esx n/a| 0 1 3 -7 28 -20 -.07 28 17 | -556 -834 3128 7595
gfz n/a| 0 2 4 -27 6 9 -.06 29 19 | 0 -869 3142 9347
grg n/a| 0 -3 -1 -6 30 -13 .21 28 20 | -6666 -1005 3148 8749
iac n/a| 2 1 -9 2 -40 82 -.41 29 26 | -4867 67 3146 9704
Table 2.2231.4 GPS week: 2231 Day: 4 MJD: 59865
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 -7 2 33 .19 23 15 | 24016 -1571 3027 8232
emx n/a| 0 0 -6 3 42 -45 .02 37 27 | 3155 -2181 3010 8302
esx n/a| 0 0 -3 1 15 8 -.08 26 18 | -10457 -1205 2970 6927
gfz n/a| 0 1 3 -1 -34 37 .06 29 17 | 0 -1371 3082 8318
grg n/a| 4 -2 1 33 -11 -45 .11 35 24 | -6706 -1114 2934 7710
iac n/a| 0 -4 -3 -42 -3 17 -.30 28 27 | -4519 -196 2969 8661
Table 2.2231.5 GPS week: 2231 Day: 5 MJD: 59866
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 3 -6 -1 12 .19 25 18 | 29838 -692 2776 8128
emx n/a| 0 0 -11 20 -36 -38 -.04 40 30 | 3762 -588 2755 8129
esx n/a| -2 1 -5 -2 6 0 -.04 27 16 | 5823 -555 2792 8065
gfz n/a| 0 2 2 1 -27 0 -.08 25 16 | 0 -676 2836 8064
grg n/a| 2 -4 8 23 22 6 .04 30 21 | -11 -613 2768 7386
iac n/a| -2 2 -3 -31 45 -74 -.33 32 29 | 1672 -547 2781 8563
Table 2.2231.6 GPS week: 2231 Day: 6 MJD: 59867
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 -20 -7 36 .16 23 16 | 23895 368 2601 7674
emx n/a| 0 -2 -10 14 11 -41 .05 40 30 | -2358 -7 2569 7430
esx n/a| 0 0 -3 -21 19 -62 -.01 25 17 | -12957 1136 2592 7284
gfz n/a| 0 3 0 2 -6 7 -.04 26 13 | 0 161 2632 7357
grg n/a| 2 -2 6 -23 24 30 .09 32 27 | -6632 829 2606 7107
iac n/a| -2 0 -2 52 -27 -66 -.25 26 25 | -3674 -354 2593 8177
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 3.2231.0 GPS week: 2231 Day: 0 MJD: 59861
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 3187 22 28 29 19 29 31 11 | 98 100 88 83 75 91 87
R02 | 1180 9 9 10 13 14 32 7 | 62 64 68 62 59 85 65
R03 | 1487 6 11 12 10 15 23 5 | 68 67 70 69 79 80 71
XR04 | 1375 8 15 18 --- 10 24 7 | 66 63 57 --- 67 66 63
R05 | 1544 16 19 25 22 16 25 9 | 65 55 62 53 53 64 56
R07 | 1348 6 14 11 14 16 23 6 | 68 71 69 65 63 60 65
R08 | 2317 15 9 12 18 16 20 7 | 66 67 76 87 75 81 74
R09 | 3208 32 27 19 19 62 28 15 | 95 88 88 85 41 78 76
R11 | 1204 16 15 16 13 22 20 7 | 47 49 50 47 57 51 47
R12 | 1110 7 34 10 17 14 49 10 | 54 40 50 51 63 86 53
R13 | 589 25 47 29 17 33 42 14 | 78 43 41 59 74 73 57
R14 | 599 14 27 17 15 12 21 7 | 63 40 66 62 57 56 57
R15 | 899 11 26 17 19 18 17 7 | 68 48 57 76 78 59 65
R17E | 1329 9 23 10 11 16 9 5 | 119 121 120 116 114 123 118
R18E | 961 9 20 25 13 16 28 8 | 48 56 57 55 56 51 51
R19E | 1509 30 65 35 50 43 28 18 | 72 53 71 97 85 57 68
R20E | 1541 48 81 59 73 51 55 27 | 94 85 87 126 90 88 86
R21E | 1092 9 32 12 11 18 16 7 | 50 42 46 49 54 47 46
XR22E | 2210 --- 45 365 --- 22 29 23 | --- 32 142 --- 37 37 35
R24E | 3449 15 34 15 13 18 20 8 | 59 61 54 58 66 58 57
------+-----------------------------------------+-------------------------------------
RMS | 1799 20 34 23 25 27 29 |T 70 62 70 72 67 69 64
WRMS | 1799 13 26 16 13 22 27 |NE 69 61 64 66 64 71 64
MEDI | 1348 14 26 17 15 16 24 |MD 66 56 66 62 63 64 63
Table 3.2231.1 GPS week: 2231 Day: 1 MJD: 59862
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 3295 15 43 31 25 27 27 12 | 54 64 47 63 52 77 55
R02 | 866 10 11 12 11 14 24 6 | 33 36 43 34 34 49 36
R03 | 854 6 9 15 15 15 44 8 | 37 36 34 37 40 52 36
XR04 | 1300 8 14 17 --- 13 17 6 | 34 35 34 --- 39 31 33
R05 | 1903 23 17 18 13 9 26 8 | 43 30 43 42 38 40 36
R07 | 721 12 15 9 18 13 15 6 | 46 47 42 41 38 43 41
R08 | 1820 13 20 19 17 19 24 8 | 45 41 59 50 55 54 49
R09 | 4180 30 16 20 27 56 24 14 | 67 56 68 71 22 58 53
R11 | 1756 12 12 11 15 28 11 7 | 27 29 38 28 49 36 32
R12 | 723 14 48 14 16 16 51 12 | 46 29 51 54 55 85 50
R13 | 552 34 43 27 30 26 24 14 | 59 34 35 33 54 41 38
R14 | 2207 8 34 16 14 12 13 7 | 46 32 56 47 46 49 45
R15 | 1195 7 29 16 10 25 24 8 | 46 33 41 51 62 45 46
R17E | 1492 13 22 13 16 15 26 7 | 109 104 111 114 109 108 108
R18E | 1006 8 23 29 17 18 18 8 | 36 40 39 45 47 46 39
R19E | 936 52 81 49 49 66 37 25 | 52 40 47 67 44 44 38
R20E | 1750 41 73 64 71 33 64 25 | 72 59 90 97 74 61 66
R21E | 868 9 29 12 16 15 27 8 | 32 24 27 36 41 41 30
XR22E | 2508 --- --- 361 --- 18 26 21 | --- --- 110 --- 34 39 35
R24E | 4854 15 34 17 15 14 25 8 | 45 34 40 39 48 45 39
------+-----------------------------------------+-------------------------------------
RMS | 2094 22 37 26 26 28 31 |T 48 42 52 52 49 52 45
WRMS | 2094 15 28 17 16 24 28 |NE 44 38 45 45 44 50 42
MEDI | 1300 13 23 17 16 16 24 |MD 46 36 43 45 46 45 39
Table 3.2231.2 GPS week: 2231 Day: 2 MJD: 59863
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1909 27 31 28 19 30 22 11 | 74 72 57 65 56 76 65
R02 | 1193 9 13 11 9 12 29 6 | 49 50 60 53 51 71 54
R03 | 1008 15 21 17 13 14 29 8 | 53 53 71 67 63 82 62
XR04 | 975 13 12 14 --- 12 32 8 | 53 49 48 --- 48 43 47
R05 | 1056 15 15 17 14 11 29 7 | 46 44 47 46 47 41 42
R07 | 639 5 13 10 15 15 16 5 | 55 55 56 65 55 53 55
R08 | 866 16 17 13 10 13 31 7 | 49 48 60 58 60 71 55
R09 | 3011 25 16 26 29 45 22 13 | 66 54 60 59 42 51 50
R11 | 1605 12 12 25 33 29 29 11 | 42 40 64 60 67 34 48
R12 | 1704 15 53 18 18 12 57 13 | 50 32 50 62 47 84 50
R13 | 1333 22 60 38 18 34 19 14 | 63 39 41 59 68 54 52
R14 | 2590 10 34 20 11 15 32 8 | 49 32 49 44 41 65 44
R15 | 677 6 27 13 13 11 21 6 | 49 34 43 57 51 46 47
R17E | 1215 14 30 16 9 16 28 8 | 154 147 153 151 145 147 150
R18E | 1223 10 18 23 20 19 13 7 | 33 31 34 31 44 32 31
R19E | 694 26 87 44 54 58 32 22 | 52 47 51 73 49 47 43
R20E | 2006 34 70 71 76 31 53 25 | 61 48 86 109 67 73 64
R21E | 939 7 35 14 26 12 19 8 | 36 27 37 46 39 33 33
XR22E | 3665 --- --- 332 --- 17 23 20 | --- --- 104 --- 36 41 36
R24E | 3774 11 37 22 15 18 21 8 | 42 36 45 47 47 39 40
------+-----------------------------------------+-------------------------------------
RMS | 1739 17 39 28 28 25 30 |T 56 49 60 64 56 59 53
WRMS | 1739 14 30 20 15 18 29 |NE 53 46 54 57 53 59 51
MEDI | 1215 14 27 18 15 15 28 |MD 50 47 51 59 49 51 48
Table 3.2231.3 GPS week: 2231 Day: 3 MJD: 59864
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 751 29 24 23 30 19 23 11 | 79 71 58 56 65 76 66
R02 | 1180 6 8 9 20 12 21 6 | 52 50 52 42 52 66 51
R03 | 612 6 14 15 18 13 27 7 | 60 56 68 57 67 81 64
XR04 | 651 10 9 12 --- 17 23 7 | 53 51 44 --- 48 53 49
R05 | 779 16 13 20 15 14 13 7 | 48 47 52 46 45 48 45
R07 | 670 14 12 14 12 13 31 7 | 56 49 46 47 57 53 49
R08 | 935 9 14 11 10 16 17 5 | 54 51 57 53 57 66 55
R09 | 2748 20 13 26 15 62 29 14 | 59 51 59 58 46 65 48
R11 | 1039 17 16 12 29 11 22 8 | 27 31 28 40 24 31 25
R12 | 2471 12 40 18 19 13 44 11 | 51 30 48 58 48 72 48
R13 | 1416 25 55 46 50 38 33 18 | 72 40 33 97 57 74 57
R14 | 1778 8 39 20 20 17 13 9 | 46 28 59 59 46 37 44
R15 | 427 7 26 8 16 24 16 7 | 54 39 49 49 64 46 50
R17E | 784 13 33 20 20 13 34 10 | 127 132 137 145 133 127 132
R18E | 1364 13 24 19 16 28 28 9 | 29 33 33 28 46 35 29
R19E | 1164 30 82 42 58 52 34 22 | 41 54 48 86 55 57 43
R20E | 2157 57 70 76 66 43 55 27 | 58 47 82 86 68 45 50
R21E | 764 10 30 14 18 21 22 8 | 34 27 31 34 45 35 30
XR22E | 2927 --- --- 338 --- 10 12 11 | --- --- 133 --- 39 40 38
R24E | 3297 10 34 15 13 16 11 7 | 31 27 27 28 41 30 27
------+-----------------------------------------+-------------------------------------
RMS | 1569 21 36 28 29 28 29 |T 54 48 57 59 55 56 50
WRMS | 1569 15 27 17 19 20 26 |NE 54 45 50 55 52 59 50
MEDI | 1039 13 24 18 18 16 23 |MD 53 47 49 53 48 53 48
Table 3.2231.4 GPS week: 2231 Day: 4 MJD: 59865
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 905 26 28 20 26 23 19 10 | 70 65 79 61 57 65 66
R02 | 679 8 12 14 14 24 29 8 | 49 51 50 47 43 67 50
R03 | 995 9 7 15 11 17 35 8 | 58 59 62 65 63 53 59
XR04 | 728 5 13 9 --- 14 13 5 | 56 58 55 --- 55 49 54
R05 | 1194 17 13 15 14 21 15 7 | 47 43 53 44 38 40 44
R07 | 968 12 14 7 16 14 17 6 | 53 48 52 52 60 45 50
R08 | 1025 19 21 14 11 21 29 8 | 45 40 52 47 49 47 45
R09 | 2652 21 26 27 16 82 20 15 | 87 87 87 86 79 78 79
R11 | 894 16 19 13 18 24 17 7 | 43 41 60 47 71 47 50
R12 | 2253 14 35 12 15 25 16 8 | 58 44 54 55 69 55 54
R13 | 1166 32 50 47 35 40 34 17 | 81 35 34 78 78 72 59
R14 | 1103 15 45 21 21 23 22 11 | 49 32 54 62 67 64 52
R15 | 508 9 28 11 14 24 18 7 | 62 47 59 57 68 57 58
R17E | 1071 15 30 11 18 17 18 8 | 123 122 122 129 122 125 123
R18E | 640 16 29 18 14 18 47 11 | 52 56 51 50 55 77 54
R19E | 1188 29 82 36 71 57 32 23 | 57 53 37 87 51 48 45
R20E | 5394 63 76 69 65 66 52 29 | 50 44 80 77 80 57 48
R21E | 1007 15 29 12 18 26 20 8 | 53 46 47 58 63 54 51
XR22E | 2954 --- --- 350 --- 14 11 12 | --- --- 134 --- 40 35 37
R24E | 2909 15 29 12 26 18 16 8 | 53 55 55 56 58 52 52
------+-----------------------------------------+-------------------------------------
RMS | 1870 23 37 26 29 35 28 |T 60 54 63 64 63 59 56
WRMS | 1870 15 27 18 17 24 27 |NE 58 50 57 58 61 56 55
MEDI | 1025 15 28 14 16 23 19 |MD 53 48 54 57 60 54 52
Table 3.2231.5 GPS week: 2231 Day: 5 MJD: 59866
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1259 46 45 36 21 13 59 17 | 54 55 49 55 42 34 41
R02 | 788 10 9 10 15 9 24 6 | 33 34 39 32 35 46 34
R03 | 1002 9 8 11 15 17 25 6 | 42 42 39 38 47 38 40
XR04 | 742 9 12 8 --- 17 21 7 | 47 53 47 --- 46 49 46
R05 | 1873 20 22 18 18 14 18 8 | 39 43 51 52 39 48 42
R07 | 897 12 11 10 13 14 18 6 | 44 46 37 36 40 40 38
R08 | 1088 21 17 9 17 8 28 7 | 42 36 46 45 39 42 41
R09 | 3010 25 17 37 17 62 21 15 | 94 89 94 84 46 78 77
R11 | 1483 14 18 16 17 17 30 8 | 64 67 72 73 80 68 68
R12 | 1831 15 37 11 10 21 32 9 | 38 31 43 43 58 58 43
R13 | 1131 37 46 47 25 33 24 16 | 86 54 58 76 86 75 69
R14 | 716 16 41 11 11 20 31 9 | 89 77 83 85 96 90 86
R15 | 673 10 26 17 14 27 20 8 | 54 41 40 46 60 53 47
R17E | 1454 16 33 12 14 17 19 8 | 122 119 118 121 117 119 119
R18E | 585 9 32 17 13 16 40 9 | 62 64 66 64 70 64 63
R19E | 2087 41 88 37 56 78 43 25 | 71 52 54 69 68 64 51
R20E | 4484 50 84 67 61 37 38 25 | 47 50 79 69 53 49 48
R21E | 1053 14 35 18 15 20 27 9 | 69 64 67 70 76 84 70
XR22E | 3033 --- --- 357 --- 25 33 28 | --- --- 127 --- 39 47 41
R24E | 2371 22 41 12 24 12 39 11 | 53 58 53 68 63 64 57
------+-----------------------------------------+-------------------------------------
RMS | 1814 25 40 27 25 30 32 |T 60 56 63 62 60 60 56
WRMS | 1814 18 30 16 16 21 29 |NE 55 51 53 55 54 55 51
MEDI | 1131 16 32 16 15 17 27 |MD 54 53 53 64 53 53 47
Table 3.2231.6 GPS week: 2231 Day: 6 MJD: 59867
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 591 48 34 32 36 24 44 17 | 84 84 75 67 71 65 68
R02 | 1203 6 11 7 10 18 13 4 | 49 49 51 43 54 62 49
R03 | 706 7 11 8 13 13 24 6 | 61 57 58 57 63 62 58
XR04 | 886 10 14 16 --- 12 28 8 | 63 64 55 --- 55 65 59
R05 | 1770 15 13 23 11 12 13 7 | 55 55 64 59 51 57 56
R07 | 632 7 13 9 12 13 22 5 | 62 64 65 61 61 71 63
R08 | 723 18 13 17 13 18 36 9 | 54 56 59 65 70 81 62
R09 | 3890 23 25 23 23 65 29 14 | 97 93 100 99 48 100 89
R11 | 2092 17 11 28 13 29 17 9 | 72 74 77 75 84 69 73
R12 | 1510 13 30 14 10 20 27 8 | 70 47 79 79 84 95 75
R13 | 932 30 52 28 17 36 31 14 | 110 76 81 100 116 95 95
R14 | 696 10 44 12 9 20 29 9 | 116 105 118 117 119 123 116
R15 | 788 16 32 17 11 21 20 8 | 78 60 71 77 93 82 76
R17E | 2547 7 39 17 14 27 19 9 | 119 118 119 120 125 121 119
R18E | 484 18 33 16 14 30 20 9 | 57 54 56 53 72 56 55
R19E | 2241 41 81 36 60 56 18 22 | 61 59 53 85 51 55 52
R20E | 5173 41 88 63 69 40 41 26 | 53 68 82 77 72 60 56
R21E | 855 14 28 15 13 30 13 8 | 52 43 47 47 60 54 47
XR22E | 2924 --- 93 370 --- 29 41 40 | --- 30 141 --- 38 30 35
R24E | 2662 16 35 13 16 37 31 10 | 53 56 52 48 57 45 48
------+-----------------------------------------+-------------------------------------
RMS | 2060 23 40 25 26 32 26 |T 71 65 75 73 72 72 67
WRMS | 2060 16 30 17 13 27 25 |NE 74 68 73 74 74 79 72
MEDI | 932 16 30 17 13 24 24 |MD 62 59 65 67 63 65 59
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