[IGSREPORT-28927] Wk 2226 IGLOS Final Orbits
acc
acc at igs.org
Mon Sep 26 01:09:16 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2226 (Sep 04, 2022 - Sep 10, 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 2.2226.
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:
igl2226[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2226 in the SP3 format.
igl22267.sum Combination Report for GPS Week 2226.
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 | 0.0 ns
1 | -6.8 ns
2 | -5.5 ns
3 | -5.9 ns
4 | -7.0 ns
5 | 0.0 ns
6 | 1.8 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 | BKG | R02
0 | COD | R02
0 | COF | R02
0 | EMX | R02
0 | ESX | R02
0 | GFZ | R02
0 | GRG | R02
0 | IAC | R02
0 | MCC | R02
1 | BKG | R02
1 | COD | R02
1 | COF | R02
1 | EMX | R02
1 | ESX | R02
1 | GFZ | R02
1 | GRG | R02
1 | IAC | R02
1 | MCC | R02
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 1.2226, 1a.2226).
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 2.2226.0-6)
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 3.2226.0-6).
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 2226 summary. (Sep 04, 2022 - Sep 10, 2022)
Table 1.2226.a GPS week : 2226 MJD: 59826.0-59832.0
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 0 -18 -34 28 .07 18 15 | 29424 288 3090 8315
| 1 0 1 18 14 9 .02 | 5163 1506
emx n/a| 0 0 11 16 -40 -3 -.04 36 31 | -2389 221 3098 8428
| 1 1 2 10 14 38 .08 | 8852 1333
esx n/a| 0 1 3 6 34 12 -.11 27 21 | -3625 908 3099 11030
| 1 1 1 17 19 16 .04 | 9522 1731
gfz n/a| 0 0 -7 24 -6 19 .04 29 18 | 0 252 3133 8182
| 1 1 2 18 20 24 .04 | 0 1498
grg n/a| 1 -2 2 -6 58 -131 .31 25 22 | -3739 367 3093 7813
| 1 2 1 22 27 53 .02 | 3647 1584
iac n/a| 0 0 -7 -11 -20 62 -.31 26 25 | -26 -570 3140 10190
| 2 2 2 15 36 52 .06 | 3716 842
Table 1.2226.b GPS week : 2226 MJD: 59826.0-59832.0
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 21 20 20 21 19 21 |
R02 | --- --- 13 7 8 8 8 |
R03 | 8 8 7 8 9 9 8 |
R04 | 12 9 9 11 10 8 9 |
R05 | 11 11 8 9 10 10 9 |
R07 | 9 9 8 8 8 9 7 |
R08 | 8 11 9 9 8 9 11 |
R09 | 9 8 8 11 9 10 10 |
R11 | 8 8 10 8 9 11 12 |
R12 | 7 8 8 5 6 7 7 |
R13 | 10 14 14 14 11 11 14 |
R14 | 8 7 6 7 6 6 6 |
R15 | 6 7 7 7 9 7 8 |
R17 | 10 8 9 7 8 8 8 |
R18 | 8 9 8 8 8 9 8 |
R19 | 21 21 24 18 17 20 18 |
R20 | 22 25 24 24 22 19 23 |
R21 | 8 9 8 9 10 9 8 |
R24 | 9 8 9 9 10 10 8 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2226.c GPS week : 2226 MJD: 59826.0-59832.0
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 2226 0 | 7 42 12 351 382 7 80.8 1652 1652 | 16 0
brd 2226 1 | 70 -42 -51 -280 -281 -431 79.9 1800 1800 | -6808 0
brd 2226 2 | -30 39 -45 -336 -13 1004 81.1 1591 1591 | -5495 0
brd 2226 3 | -11 15 65 -591 -423 -5751 82.7 1688 1688 | -5949 0
brd 2226 4 | -53 1 53 2433 763 -3047 82.4 1721 1721 | -7023 0
brd 2226 5 | 9 2 6 785 1048 -2237 83.3 1580 1580 | 7 0
brd 2226 6 | -47 -22 -24 2992 796 1440 81.1 1437 1437 | 1752 0
-------------+------------------------------------------------------------+----------------
brd 2226 mean| -7 5 2 764 324 -1287 81.6 1638 1638 | -3357 0
brd 2226 sdev| 42 30 45 1417 574 2550 1.2 116 116 | 3773 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 2.2226.0 GPS week: 2226 Day: 0 MJD: 59826
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 6 -19 22 .07 19 13 | 32953 -37 3259 8392
emx n/a| -1 0 14 17 -44 39 -.01 37 33 | -16808 -749 3274 8326
esx n/a| -2 0 4 6 72 13 -.13 27 21 | -10513 -1 3261 11534
gfz n/a| 0 -1 -8 12 -20 4 .08 30 14 | 0 -331 3293 8364
grg n/a| 3 0 0 -47 45 -83 .27 24 24 | -186 140 3283 7782
iac n/a| -5 0 -6 -5 -46 43 -.33 26 23 | 4130 -68 3318 10559
Table 2.2226.1 GPS week: 2226 Day: 1 MJD: 59827
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 -18 -37 32 .09 20 15 | 25270 -2140 2755 8769
emx n/a| -1 0 10 10 -62 14 .03 38 35 | -874 -1873 2764 8801
esx n/a| -1 0 4 -16 28 3 -.03 26 17 | 8292 -1043 2758 11695
gfz n/a| 1 -1 -11 0 -7 -20 .05 34 21 | 0 -1931 2835 8885
grg n/a| 2 -1 1 21 106 -206 .30 25 23 | -5957 -1997 2755 8132
iac n/a| 1 0 -7 11 -12 158 -.25 26 25 | -3586 -460 2824 10873
Table 2.2226.2 GPS week: 2226 Day: 2 MJD: 59828
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 -42 -12 32 .10 20 15 | 23978 2018 3179 7792
emx n/a| 0 2 10 26 -45 25 .09 41 32 | -5488 1809 3202 7871
esx n/a| 0 1 4 30 16 25 -.09 28 18 | 5389 2671 3223 10939
gfz n/a| 0 -1 -8 32 -7 11 .01 28 16 | 0 1362 3217 7426
grg n/a| 0 0 3 -6 23 -164 .35 31 24 | -6642 1700 3172 7486
iac n/a| 3 1 -7 -17 8 -4 -.31 24 22 | -2473 -234 3270 10282
Table 2.2226.3 GPS week: 2226 Day: 3 MJD: 59829
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 2 2 -39 -41 17 .04 19 16 | 26261 -109 3599 7920
emx n/a| 0 3 15 22 -51 -42 -.14 37 29 | 285 326 3583 7867
esx n/a| 0 1 5 26 25 -17 -.11 27 18 | -6030 1155 3597 7253
gfz n/a| 2 0 -8 12 27 20 .06 22 17 | 0 616 3611 7773
grg n/a| 1 -4 0 10 46 -105 .32 26 19 | -6234 74 3602 7511
iac n/a| -1 0 -7 -20 -64 98 -.40 25 24 | -2507 -1112 3630 9799
Table 2.2226.4 GPS week: 2226 Day: 4 MJD: 59830
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 1 -7 -38 21 .09 16 14 | 26081 802 3098 7989
emx n/a| 0 0 13 13 -32 23 -.04 33 29 | -8917 939 3106 7972
esx n/a| 0 3 0 9 52 34 -.11 26 17 | -19376 35 3094 11539
gfz n/a| 1 1 -8 47 14 50 -.01 29 15 | 0 402 3162 7819
grg n/a| 0 -5 2 -13 43 -186 .32 26 22 | -7685 915 3100 7553
iac n/a| 0 1 -5 -9 -60 33 -.37 26 26 | -3334 -1161 3141 10009
Table 2.2226.5 GPS week: 2226 Day: 5 MJD: 59831
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 -1 -55 31 .05 17 14 | 35319 -633 2749 8784
emx n/a| 1 0 9 25 -30 -60 -.09 30 28 | 8877 -468 2737 9596
esx n/a| 0 3 3 0 24 18 -.11 26 22 | 777 -219 2740 12381
gfz n/a| -1 0 -6 46 -29 17 .08 33 27 | 0 -952 2797 8507
grg n/a| 1 -1 4 -17 78 -73 .30 22 19 | 406 -968 2737 8144
iac n/a| 0 -5 -10 -38 31 42 -.28 25 24 | 3198 -1747 2747 9518
Table 2.2226.6 GPS week: 2226 Day: 6 MJD: 59832
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 -22 -33 44 .08 18 14 | 36107 2118 2996 8561
emx n/a| 0 0 9 -3 -17 -21 -.11 35 31 | 6198 1569 3022 8565
esx n/a| 0 0 3 -8 25 10 -.15 28 33 | -3920 3764 3024 11874
gfz n/a| -2 2 -2 23 -19 49 .02 27 15 | 0 2603 3017 8504
grg n/a| 2 -1 2 4 64 -101 .30 23 20 | 120 2707 3005 8087
iac n/a| 0 -4 -10 -1 -3 66 -.25 30 29 | 4385 792 3054 10292
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 3.2226.0 GPS week: 2226 Day: 0 MJD: 59826
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 576 37 64 76 55 16 20 21 | 127 46 37 126 107 96 92
R03 | 1154 10 35 17 9 25 13 8 | 84 52 69 78 97 84 78
XR04 | 875 7 26 12 --- 24 42 11 | 82 57 76 --- 81 80 76
R05 | 1129 13 47 20 23 22 26 11 | 78 43 75 93 94 92 79
R07 | 807 14 35 17 11 16 25 8 | 100 69 78 92 96 98 89
R08 | 2242 9 34 12 10 11 23 7 | 82 63 80 91 85 101 83
R09 | 722 10 10 15 18 32 23 8 | 51 51 56 60 35 49 48
R11 | 1822 16 14 17 10 23 21 8 | 30 35 36 33 40 33 31
R12 | 2823 8 22 16 22 16 16 7 | 48 59 47 54 47 45 48
R13 | 940 13 28 20 11 33 17 9 | 68 62 62 63 61 67 63
R14 | 1176 9 19 13 11 15 33 7 | 44 44 51 43 40 62 45
R15 | 1095 6 15 8 14 17 17 5 | 56 52 56 61 68 49 56
R17E | 2170 11 32 18 23 21 30 9 | 134 128 130 130 131 136 131
R18E | 3167 9 26 18 11 22 21 7 | 93 91 95 96 98 94 94
R19E | 1085 44 68 38 50 37 43 20 | 79 84 88 95 86 70 77
R20E | 1094 33 57 39 74 42 46 21 | 74 70 84 109 87 80 77
R21E | 1629 8 26 14 21 15 17 7 | 124 129 124 127 134 126 126
R24E | 1653 9 36 16 27 17 18 9 | 98 92 98 95 99 103 97
XR25 |11334 --- --- --- --- --- 8 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1652 19 37 27 30 24 26 |T 81 68 74 85 82 82 78
WRMS | 1652 13 33 21 14 24 23 |NE 72 52 60 72 70 73 67
MEDI | 1154 10 28 17 18 21 21 |MD 82 59 75 92 86 84 78
Table 3.2226.1 GPS week: 2226 Day: 1 MJD: 59827
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 570 44 64 65 23 32 29 20 | 81 30 39 63 78 58 56
R03 | 1091 13 31 15 13 18 19 8 | 57 35 44 58 56 53 50
XR04 | 918 11 28 11 --- 18 27 9 | 61 46 57 --- 57 60 56
R05 | 1042 10 49 21 12 13 36 11 | 51 36 49 50 61 73 51
R07 | 539 10 31 19 13 23 20 8 | 69 46 54 66 78 65 63
R08 | 3264 16 40 12 35 16 27 10 | 60 47 69 90 69 67 65
R09 | 1011 13 10 11 20 26 25 8 | 42 39 43 48 26 44 37
R11 | 1264 16 9 17 19 22 12 7 | 20 21 31 28 38 29 23
R12 | 3128 13 15 15 26 14 21 7 | 35 46 33 46 43 38 36
R13 | 1018 16 57 23 26 33 29 13 | 40 52 26 25 44 46 34
R14 | 1760 7 11 11 14 14 27 6 | 30 28 33 23 25 44 29
R15 | 1682 4 9 13 17 24 14 6 | 41 34 50 31 48 42 40
R17E | 2415 9 27 10 19 21 15 7 | 86 85 88 86 82 93 85
R18E | 3255 10 23 18 18 18 28 8 | 63 64 64 64 69 78 65
R19E | 1266 38 67 40 54 40 47 20 | 53 43 68 69 63 48 49
R20E | 1311 37 55 49 100 46 33 24 | 57 53 56 100 62 60 53
R21E | 1302 9 29 16 28 15 20 8 | 83 84 83 85 86 91 84
R24E | 827 7 40 11 22 13 12 8 | 55 50 61 62 59 63 56
XR25 |15430 --- --- --- --- --- 10 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1799 20 38 26 34 25 26 |T 54 46 52 58 64 59 53
WRMS | 1799 15 35 17 21 23 25 |NE 48 38 44 48 62 52 47
MEDI | 1266 11 29 15 20 18 25 |MD 55 46 50 62 61 60 53
Table 3.2226.2 GPS week: 2226 Day: 2 MJD: 59828
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 527 48 60 67 21 32 17 20 | 101 45 57 78 93 67 73
XR02 | 1268 23 46 --- 16 22 23 13 | 57 32 --- 49 44 44 43
R03 | 784 10 29 14 10 11 19 7 | 60 38 47 59 49 61 53
XR04 | 578 18 24 18 --- 15 18 9 | 65 44 54 --- 59 53 56
R05 | 1649 15 31 15 14 19 20 8 | 61 44 55 61 66 47 55
R07 | 607 13 30 18 11 23 15 8 | 78 53 64 71 84 78 71
R08 | 2405 9 36 16 19 14 28 9 | 68 57 62 84 73 90 72
R09 | 808 18 19 11 9 26 24 8 | 40 39 29 30 20 35 29
R11 | 1265 20 15 19 15 32 24 9 | 20 19 26 19 36 21 14
R12 | 3078 14 11 25 12 16 16 7 | 34 38 39 34 38 34 32
R13 | 695 14 38 33 23 51 22 13 | 33 51 26 27 52 36 30
R14 | 1124 9 12 11 13 13 17 5 | 33 28 34 35 31 28 30
R15 | 1488 8 13 9 18 24 19 7 | 43 42 42 44 53 34 40
R17E | 2258 10 29 18 23 15 26 9 | 57 59 47 57 54 61 54
R18E | 2723 10 25 15 16 18 20 7 | 39 37 41 40 41 40 37
R19E | 1472 27 71 45 78 48 57 24 | 38 46 47 86 48 38 36
R20E | 1308 38 93 47 53 73 24 24 | 47 76 59 73 54 36 42
R21E | 697 11 34 16 22 16 14 8 | 58 56 69 73 72 59 63
R24E | 823 11 41 12 18 18 19 8 | 32 37 32 37 41 38 32
XR25 |18676 --- --- --- --- --- 6 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1591 20 41 28 28 31 24 |T 50 44 46 53 53 47 45
WRMS | 1591 15 32 18 16 24 22 |NE 53 40 44 49 53 48 46
MEDI | 1265 14 30 16 16 19 19 |MD 47 44 47 49 52 40 42
Table 3.2226.3 GPS week: 2226 Day: 3 MJD: 59829
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 844 46 53 75 18 20 27 19 | 117 58 63 89 93 104 85
R02 | 1106 13 30 12 13 14 18 7 | 72 30 39 43 69 66 63
R03 | 1208 11 30 22 13 14 14 7 | 66 35 56 63 66 63 59
XR04 | 769 19 22 17 --- 16 37 11 | 59 33 50 --- 48 58 49
R05 | 1366 24 28 14 10 15 21 8 | 69 36 54 59 51 52 54
R07 | 1262 14 26 17 11 23 23 8 | 77 54 71 81 93 57 74
R08 | 3015 12 37 16 24 13 22 9 | 70 47 69 96 84 92 77
R09 | 1571 16 21 9 14 36 38 10 | 38 33 35 37 33 58 32
R11 | 1785 19 16 13 11 13 28 7 | 20 24 27 21 24 33 18
R12 | 2571 12 11 13 9 10 15 5 | 37 37 39 39 36 29 34
R13 | 1479 17 34 38 27 40 21 13 | 35 52 40 41 46 45 37
R14 | 899 11 15 12 8 16 24 6 | 34 37 35 35 36 33 32
R15 | 2813 12 16 12 11 12 26 6 | 51 47 40 47 52 42 45
R17E | 2245 10 26 14 19 17 12 7 | 48 45 54 61 65 55 53
R18E | 1646 12 18 18 15 18 24 7 | 37 31 37 36 42 43 35
R19E | 934 23 61 40 48 31 40 18 | 29 61 48 64 41 36 31
R20E | 1628 30 87 40 51 71 34 23 | 46 71 68 71 52 50 49
R21E | 709 14 32 13 20 16 24 8 | 50 47 45 64 55 48 49
R24E | 624 10 34 16 17 16 25 8 | 32 34 33 41 42 41 33
XR25 |20067 --- --- --- --- --- 10 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1688 19 37 27 22 26 25 |T 51 42 47 54 54 52 47
WRMS | 1688 16 29 18 17 19 24 |NE 57 40 47 54 56 56 50
MEDI | 1366 14 28 16 14 16 24 |MD 48 37 45 47 51 50 49
Table 3.2226.4 GPS week: 2226 Day: 4 MJD: 59830
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1244 34 52 81 20 28 42 21 | 109 60 49 98 103 111 87
R02 | 943 14 36 15 11 12 16 7 | 63 28 35 53 55 70 58
R03 | 792 10 36 11 15 14 38 9 | 67 34 59 54 61 92 61
XR04 | 628 11 25 20 --- 17 25 9 | 66 44 64 --- 65 49 58
R05 | 861 19 34 25 20 17 22 10 | 68 38 54 75 51 67 59
R07 | 1074 13 21 14 13 15 34 8 | 69 55 57 70 74 44 62
R08 | 2294 9 28 14 16 15 20 7 | 68 54 65 76 75 78 68
R09 | 1933 17 18 18 12 31 24 9 | 44 37 38 39 20 44 33
R11 | 2067 13 17 15 16 31 19 8 | 17 20 31 30 38 37 21
R12 | 1643 12 13 15 12 12 21 6 | 41 37 49 39 42 39 39
R13 | 2482 15 27 27 28 35 19 11 | 45 57 48 42 39 41 42
R14 | 1239 9 12 18 12 14 11 5 | 28 26 35 37 35 26 28
R15 | 2529 13 22 16 19 20 31 8 | 40 39 34 47 50 46 39
R17E | 1810 10 26 14 16 16 22 7 | 62 62 58 65 76 65 63
R18E | 833 13 24 18 13 18 25 8 | 47 43 43 45 54 48 44
R19E | 1555 27 40 26 65 31 29 16 | 41 39 46 76 49 36 39
R20E | 3223 20 69 31 76 60 25 21 | 40 41 38 88 58 31 39
R21E | 660 13 33 11 32 22 28 10 | 64 61 61 69 65 67 62
R24E | 1028 14 32 17 22 27 30 10 | 38 33 48 46 53 54 42
XR25 |17897 --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1721 16 33 26 29 26 26 |T 53 42 48 58 55 55 49
WRMS | 1721 14 29 17 15 22 26 |NE 55 40 47 55 54 57 50
MEDI | 1244 13 27 17 16 18 24 |MD 47 39 48 53 54 48 44
Table 3.2226.5 GPS week: 2226 Day: 5 MJD: 59831
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1007 34 50 73 37 16 25 19 | 104 69 49 110 88 98 86
R02 | 830 11 33 11 24 10 20 8 | 65 33 35 62 49 56 57
R03 | 853 9 31 15 16 14 28 8 | 64 48 57 55 67 83 62
XR04 | 800 12 19 14 --- 10 19 7 | 62 50 48 --- 55 71 56
R05 | 1485 21 31 18 21 17 16 9 | 69 36 59 45 54 51 53
R07 | 733 14 21 17 16 18 32 9 | 67 57 68 66 68 46 62
R08 | 1593 7 27 22 16 21 24 8 | 69 59 65 76 75 73 68
R09 | 1331 16 14 22 18 33 19 9 | 42 43 45 39 30 45 35
R11 | 2288 17 13 14 14 43 26 10 | 25 27 33 24 67 29 27
R12 | 1026 11 13 18 17 12 19 6 | 45 51 58 50 41 53 47
R13 | 2697 13 26 38 17 33 19 11 | 44 55 49 52 36 38 43
R14 | 1189 8 16 13 14 10 21 6 | 29 27 32 26 33 37 29
R15 | 1374 8 15 17 12 23 15 7 | 39 38 44 45 55 46 42
R17E | 798 6 31 14 14 16 27 8 | 102 97 107 104 103 116 104
R18E | 788 12 22 17 16 17 29 8 | 67 64 74 73 79 81 71
R19E | 1510 33 46 35 82 23 34 19 | 56 48 44 94 54 55 49
R20E | 3446 25 49 27 80 29 35 18 | 76 67 66 106 55 66 64
R21E | 1265 8 28 15 31 18 15 8 | 115 115 115 122 116 108 114
R24E | 1257 15 34 16 29 16 22 9 | 69 70 71 67 73 72 68
XR25 |22088 --- --- --- --- --- 9 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1580 17 30 26 33 22 24 |T 63 55 58 67 63 64 59
WRMS | 1580 14 28 22 27 19 24 |NE 55 45 49 54 55 55 51
MEDI | 1257 12 27 17 17 17 21 |MD 65 51 57 62 55 56 57
Table 3.2226.6 GPS week: 2226 Day: 6 MJD: 59832
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1118 34 69 80 27 19 43 21 | 152 77 62 144 133 151 122
R02 | 1522 10 31 15 12 20 23 8 | 89 47 42 64 81 80 83
R03 | 743 9 28 17 14 16 26 8 | 86 56 73 80 90 103 82
XR04 | 856 8 24 20 --- 13 22 8 | 79 61 74 --- 77 95 77
R05 | 1430 16 35 16 12 12 26 8 | 82 43 71 65 69 79 69
R07 | 798 17 21 8 8 11 25 7 | 87 64 78 81 82 66 77
R08 | 1687 11 30 10 10 16 56 10 | 90 71 93 100 94 129 94
R09 | 995 14 25 16 25 35 15 10 | 50 47 53 57 35 46 45
R11 | 2499 19 20 15 13 39 47 12 | 35 34 44 39 54 51 38
R12 | 965 10 14 20 12 13 22 6 | 57 62 62 58 53 51 56
R13 | 2360 15 24 35 35 41 21 13 | 61 73 64 76 58 63 63
R14 | 1424 8 21 13 16 10 12 6 | 45 41 53 48 48 42 46
R15 | 797 8 16 22 11 15 31 7 | 58 55 52 58 69 73 59
R17E | 1100 10 31 13 17 14 21 7 | 124 121 122 120 121 131 123
R18E | 1051 12 18 14 16 15 28 7 | 75 77 81 80 82 87 79
R19E | 1302 40 59 34 48 22 40 18 | 76 77 65 85 80 67 70
R20E | 1257 27 61 46 77 47 32 22 | 82 81 79 109 83 82 78
R21E | 2069 15 27 17 22 9 20 8 | 125 126 130 132 130 130 128
R24E | 1121 10 31 16 17 14 16 7 | 89 87 87 93 91 89 89
XR25 |30425 --- --- --- --- --- 8 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1437 18 35 28 27 23 30 |T 81 68 72 82 80 85 77
WRMS | 1437 14 31 33 15 20 29 |NE 74 56 63 72 72 79 70
MEDI | 1121 12 27 16 16 15 23 |MD 82 64 71 80 81 80 77
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