[IGSREPORT-29071] Wk 2236 IGLOS Final Orbits
acc
acc at igs.org
Wed Dec 7 04:15:28 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2236 (Nov 13, 2022 - Nov 19, 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 2.2236.
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:
igl2236[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2236 in the SP3 format.
igl22367.sum Combination Report for GPS Week 2236.
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 | 0.2 ns
1 | 1.5 ns
2 | 1.3 ns
3 | -0.4 ns
4 | 1.4 ns
5 | 0.2 ns
6 | 1.3 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 1.2236, 1a.2236).
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 2.2236.0-6)
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 3.2236.0-6).
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 2236 summary. (Nov 13, 2022 - Nov 19, 2022)
Table 1.2236.a GPS week : 2236 MJD: 59896.0-59902.0
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 5 -12 4 41 .10 24 17 | 35324 711 3074 8571
| 1 0 2 16 5 13 .04 | 2280 2253
emx n/a| 0 0 -1 22 -5 -32 -.03 46 28 | -8303 229 3067 8479
| 0 1 4 11 23 33 .03 | 4859 1135
esx n/a| 0 0 4 -25 -1 0 -.05 35 23 | 7199 576 3108 10406
| 1 1 1 6 21 29 .04 | 19192 1947
gfz n/a| 0 1 2 11 5 -4 -.02 25 16 | 0 848 3105 8357
| 1 1 3 33 22 42 .07 | 0 1879
grg n/a| 0 -4 -11 4 1 -10 .22 29 21 | -1192 750 3130 11424
| 1 1 5 19 11 42 .04 | 1661 1952
iac n/a| 2 2 0 7 -11 2 -.22 24 23 | 924 -142 3072 12299
| 2 2 3 19 56 52 .06 | 1896 861
Table 1.2236.b GPS week : 2236 MJD: 59896.0-59902.0
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 | 17 12 16 17 12 13 17 |
R02 | 8 6 5 6 6 5 9 |
R03 | 7 6 6 5 7 7 6 |
R04 | 10 7 7 8 6 7 9 |
R05 | 8 8 9 9 9 10 10 |
R07 | 6 7 6 6 7 6 7 |
R08 | 6 8 9 9 8 7 7 |
R09 | 10 10 12 14 13 13 11 |
R11 | 8 8 10 11 7 12 11 |
R12 | 10 8 8 8 8 8 8 |
R13 | 20 21 16 13 14 14 17 |
R14 | 8 7 8 10 6 8 8 |
R15 | 9 9 10 7 8 8 8 |
R17 | 8 10 7 7 8 7 7 |
R18 | 8 10 9 8 9 9 9 |
R19 | 32 30 28 26 29 33 31 |
R20 | 31 28 29 29 27 29 34 |
R21 | 10 8 9 6 7 8 7 |
R22 | 12 12 18 23 17 11 15 |
R24 | 8 10 10 8 9 8 8 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2236.c GPS week : 2236 MJD: 59896.0-59902.0
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 2236 0 | 43 14 26 941 -1305 5840 83.0 1629 1629 | 210 0
brd 2236 1 | 62 57 -57 390 -1942 4445 81.0 1863 1863 | 1456 0
brd 2236 2 | -47 16 146 -571 -3461 -1423 82.4 1735 1735 | 1292 0
brd 2236 3 | 0 20 29 -1372 -3444 -3545 81.6 1592 1592 | -421 0
brd 2236 4 | 51 -41 118 -2765 -1251 1335 82.1 1342 1342 | 1396 0
brd 2236 5 | 49 -56 -19 -1486 1243 4054 82.0 1443 1443 | 179 0
brd 2236 6 | 29 31 -7 -1374 2246 1593 81.4 1416 1416 | 1294 0
-------------+------------------------------------------------------------+----------------
brd 2236 mean| 26 6 33 -891 -1130 1757 81.9 1574 1574 | 772 0
brd 2236 sdev| 38 40 73 1253 2180 3356 .7 186 186 | 762 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 2.2236.0 GPS week: 2236 Day: 0 MJD: 59896
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 -6 -1 36 .06 26 18 | 31212 498 3027 9471
emx n/a| 0 0 3 32 -15 20 -.08 44 27 | -1871 -210 3007 9143
esx n/a| -3 3 4 -28 -27 25 .04 37 23 | 1799 -104 3017 6384
gfz n/a| -2 0 6 6 -5 35 -.07 25 18 | 0 4 3038 9315
grg n/a| 0 -5 -17 21 -4 -70 .24 30 19 | -301 540 3017 8778
iac n/a| 2 4 -1 12 59 6 -.22 28 27 | 783 878 2946 9953
Table 2.2236.1 GPS week: 2236 Day: 1 MJD: 59897
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 -2 5 5 4 36 .08 23 17 | 33359 1987 2840 8328
emx n/a| 0 2 -1 29 -36 -45 -.04 44 28 | -3235 372 2849 8316
esx n/a| 0 2 7 -25 -3 9 -.03 35 27 | 4062 2715 2935 6557
gfz n/a| 0 2 3 -29 28 -12 -.01 27 15 | 0 2487 2903 8068
grg n/a| -2 -7 -17 20 -8 16 .23 29 22 | -383 3221 2966 7903
iac n/a| 3 1 0 2 25 -24 -.18 24 23 | 2343 351 2919 8963
Table 2.2236.2 GPS week: 2236 Day: 2 MJD: 59898
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 3 -41 6 35 .16 26 19 | 36128 1900 3034 8149
emx n/a| -1 0 -2 34 -9 -7 -.05 45 28 | -6959 884 3013 8127
esx n/a| -1 0 5 -17 12 35 -.05 35 27 | 1404 851 3136 7011
gfz n/a| 0 1 1 42 -35 -70 .03 24 15 | 0 2151 3040 8029
grg n/a| 0 -5 -13 0 -13 21 .15 29 21 | 509 1268 3159 7868
iac n/a| 0 0 2 12 23 16 -.11 21 20 | 4092 -507 3100 9169
Table 2.2236.3 GPS week: 2236 Day: 3 MJD: 59899
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 0 7 -20 6 69 .13 26 18 | 36052 -3384 3269 8396
emx n/a| 0 3 2 2 12 -24 .00 46 26 | -15707 -1373 3267 8325
esx n/a| 0 0 2 -20 30 -14 -.06 32 23 | -1238 -2802 3234 6807
gfz n/a| 0 0 -1 -5 24 -37 .03 23 16 | 0 -2220 3349 7833
grg n/a| -1 -4 -6 16 -1 -70 .23 26 22 | 541 -2499 3239 7919
iac n/a| 3 0 -1 27 -71 26 -.25 21 19 | 1064 -1399 3200 8913
Table 2.2236.4 GPS week: 2236 Day: 4 MJD: 59900
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 4 0 10 26 .07 22 17 | 35763 2879 2943 8346
emx n/a| 0 -1 0 26 13 -56 -.03 47 28 | -7794 2003 2956 8264
esx n/a| 1 0 5 -20 10 -3 -.09 31 19 | 49599 2740 2959 15361
gfz n/a| 1 1 5 -16 20 -4 .04 22 15 | 0 2454 2957 8261
grg n/a| 0 -4 -8 -20 18 0 .27 25 19 | -2532 2302 2961 13607
iac n/a| 3 5 -6 32 -91 14 -.29 27 25 | 682 -375 2951 14221
Table 2.2236.5 GPS week: 2236 Day: 5 MJD: 59901
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 4 0 10 36 .13 21 16 | 37938 -1163 3331 8756
emx n/a| 1 0 -9 19 28 -83 .02 52 30 | -11446 -822 3318 8724
esx n/a| 0 -1 3 -32 -27 -54 -.09 35 20 | 3548 -521 3317 14009
gfz n/a| 2 3 -1 19 -5 2 -.14 24 16 | 0 -865 3339 8628
grg n/a| 0 -3 -2 -21 9 28 .18 32 22 | -2758 -994 3377 15784
iac n/a| 0 3 1 -12 -40 75 -.23 25 22 | -1205 -790 3269 16377
Table 2.2236.6 GPS week: 2236 Day: 6 MJD: 59902
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 -2 4 -22 -4 46 .09 21 16 | 36817 2262 3075 8551
emx n/a| 0 0 -3 10 -27 -30 -.03 46 28 | -11112 751 3064 8457
esx n/a| 0 0 4 -35 -5 5 -.05 40 21 | -8777 1156 3163 16716
gfz n/a| 2 2 4 65 9 55 -.06 30 15 | 0 1931 3110 8366
grg n/a| 0 -3 -10 18 11 -3 .20 30 24 | -3421 1416 3191 18113
iac n/a| 3 3 0 -18 13 -96 -.25 25 21 | -1289 848 3120 18500
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 3.2236.0 GPS week: 2236 Day: 0 MJD: 59896
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 640 43 37 51 36 29 26 17 | 72 60 43 50 48 59 50
R02 | 1260 14 17 15 11 11 35 8 | 37 33 47 43 41 50 40
R03 | 578 11 8 15 14 10 30 7 | 55 57 61 55 65 70 59
XR04 | 933 20 17 22 --- 14 26 10 | 58 58 45 --- 54 52 51
R05 | 846 14 25 15 19 11 20 7 | 43 43 41 38 36 30 35
R07 | 793 5 12 17 13 12 14 5 | 52 52 47 50 55 56 50
R08 | 554 8 10 16 13 10 20 5 | 43 51 51 47 49 53 47
R09E | 3557 19 32 25 17 20 29 10 | 96 88 105 100 103 101 97
R11E | 2769 15 17 9 16 18 23 7 | 66 69 62 68 59 65 63
R12E | 1232 13 31 16 15 16 39 10 | 124 126 124 125 123 119 122
R13E | 1002 49 35 24 47 53 36 19 | 53 51 57 78 77 53 53
R14E | 2174 12 24 19 13 13 23 7 | 50 43 53 51 54 52 49
R15E | 2011 14 33 18 19 11 21 8 | 80 76 82 82 81 79 79
R17 | 2161 9 33 14 13 13 20 7 | 75 56 72 72 76 82 72
R18 | 1061 20 17 23 11 13 23 8 | 59 52 77 65 61 76 64
R19 | 768 39 124 63 56 93 25 31 | 120 50 63 139 112 118 102
R20 | 1899 60 97 117 38 44 41 30 | 140 71 79 138 132 122 111
R21 | 884 12 33 23 11 14 42 10 | 88 70 79 84 83 99 83
XR22 | 1099 --- 22 338 --- 15 13 12 | --- 15 701 --- 629 636 633
R24 | 1164 10 27 18 18 9 21 7 | 69 42 76 72 70 73 67
XR25 |13201 --- --- --- --- --- 5 0 | --- --- --- --- --- 70 71
------+-----------------------------------------+-------------------------------------
RMS | 1628 26 44 37 25 30 28 |T 72 58 98 75 100 100 95
WRMS | 1628 18 27 23 18 19 27 |NE 70 50 105 71 107 109 102
MEDI | 1099 14 25 18 15 13 23 |MD 66 52 62 68 65 70 64
Table 3.2236.1 GPS week: 2236 Day: 1 MJD: 59897
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 633 33 22 30 22 23 27 12 | 47 35 42 49 46 30 39
R02 | 1029 16 11 14 11 8 18 6 | 30 28 29 25 28 24 25
R03 | 594 8 8 13 12 21 17 6 | 41 42 43 40 58 43 43
XR04 | 599 9 17 11 --- 13 14 6 | 41 45 41 --- 37 41 39
R05 | 940 10 19 19 15 20 18 7 | 29 39 47 43 24 33 32
R07 | 592 11 16 20 15 16 12 6 | 40 39 31 33 45 43 36
R08 | 1110 18 19 15 16 8 20 7 | 32 32 32 46 43 50 37
R09E | 4687 22 24 20 21 22 22 10 | 92 89 97 95 97 83 91
R11E | 3071 16 18 9 15 25 17 7 | 44 45 47 49 39 46 44
R12E | 1143 16 27 12 8 14 28 8 | 97 98 97 95 102 104 98
R13E | 906 32 48 32 62 56 34 20 | 40 39 32 74 55 41 37
R14E | 2484 9 22 20 15 14 16 7 | 45 38 49 42 43 46 42
R15E | 2625 14 31 22 19 21 19 9 | 61 50 66 60 53 57 56
R17 | 1816 10 33 17 13 25 28 9 | 42 31 42 49 54 40 40
R18 | 730 13 20 26 16 17 30 9 | 35 36 41 34 36 42 34
R19 | 1175 43 118 73 61 74 33 30 | 66 46 54 78 43 55 53
R20 | 1715 56 98 100 42 41 25 28 | 72 51 54 78 67 55 56
R21 | 1314 9 28 18 12 15 24 8 | 49 44 51 50 49 57 49
XR22 | 1799 --- --- 349 --- 11 11 11 | --- --- 521 --- 490 492 491
R24 | 1314 12 45 17 18 15 25 10 | 40 28 46 37 45 49 38
XR25 | 9564 --- --- --- --- --- 3 0 | --- --- --- --- --- 54 56
------+-----------------------------------------+-------------------------------------
RMS | 1863 23 44 35 27 29 24 |T 49 45 73 54 72 70 68
WRMS | 1863 17 28 27 15 22 23 |NE 43 38 76 46 76 73 71
MEDI | 1175 14 22 19 15 17 20 |MD 42 39 46 49 45 46 42
Table 3.2236.2 GPS week: 2236 Day: 2 MJD: 59898
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 445 43 26 41 30 41 22 15 | 52 34 27 40 39 27 30
R02 | 926 11 9 12 11 9 10 4 | 28 27 29 34 35 21 27
R03 | 704 13 10 14 15 15 13 6 | 48 49 42 44 57 48 47
XR04 | 612 10 13 16 --- 18 14 7 | 53 57 44 --- 66 50 52
R05 | 858 18 10 26 26 18 15 9 | 38 36 51 39 34 41 35
R07 | 1001 8 16 12 12 13 12 5 | 51 54 41 49 41 54 47
R08 | 1007 23 22 18 18 16 21 9 | 39 37 46 50 39 52 43
R09E | 4271 22 23 30 30 25 23 11 | 88 92 111 111 93 92 95
R11E | 3602 25 23 10 16 35 19 10 | 34 35 43 44 68 46 42
R12E | 1121 12 28 15 10 12 21 7 | 142 136 145 147 142 138 141
R13E | 751 26 46 27 40 40 30 15 | 47 31 48 61 53 40 41
R14E | 2080 9 17 20 15 22 18 7 | 48 50 57 54 54 49 50
R15E | 2124 25 26 21 14 19 26 10 | 61 58 59 55 68 60 57
R17 | 764 5 31 10 11 9 17 6 | 56 51 59 57 56 65 57
R18 | 758 14 26 32 19 15 16 9 | 47 44 65 55 50 60 53
R19 | 1330 52 125 70 40 64 26 28 | 101 46 67 104 98 91 84
R20 | 1019 58 102 98 45 57 31 29 | 104 46 55 105 107 87 81
R21 | 941 13 25 18 14 16 24 8 | 61 48 58 51 53 68 56
XR22 | 3073 --- --- 339 --- 20 14 17 | --- --- 678 --- 634 661 649
R24 | 1772 11 44 16 13 21 21 9 | 59 42 64 60 65 56 56
XR25 | 7228 --- --- --- --- --- 2 0 | --- --- --- --- --- 51 51
------+-----------------------------------------+-------------------------------------
RMS | 1735 26 45 35 24 29 21 |T 60 51 89 64 92 88 85
WRMS | 1735 19 28 27 15 21 20 |NE 56 43 94 57 98 95 91
MEDI | 1007 14 25 18 15 18 19 |MD 52 46 55 54 56 54 52
Table 3.2236.3 GPS week: 2236 Day: 3 MJD: 59899
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 603 39 17 52 35 28 36 16 | 59 45 39 48 46 66 44
R02 | 701 12 15 14 9 14 18 6 | 33 31 24 27 29 33 28
R03 | 806 9 9 8 10 13 9 4 | 47 36 45 41 49 44 43
XR04 | 951 16 16 14 --- 10 16 7 | 45 41 33 --- 37 37 37
R05 | 1040 29 22 18 22 12 17 9 | 38 30 38 36 25 22 28
R07 | 1047 11 9 12 14 15 12 5 | 53 49 60 68 48 49 54
R08 | 528 17 13 23 14 24 20 8 | 41 44 61 59 36 62 50
R09E | 4366 23 36 31 31 32 29 13 | 94 83 95 96 94 84 87
R11E | 3290 17 20 6 16 42 22 10 | 47 52 46 49 62 50 45
R12E | 1435 12 23 20 15 15 20 7 | 129 125 143 135 123 129 130
R13E | 742 22 43 22 31 24 26 12 | 49 44 43 62 53 46 45
R14E | 817 14 29 16 15 22 28 9 | 58 51 71 70 65 67 62
R15E | 951 14 28 18 11 12 14 7 | 79 79 92 90 86 78 84
R17 | 490 10 30 10 12 10 18 7 | 65 43 61 55 65 70 60
R18 | 815 12 28 25 11 15 13 7 | 49 37 61 47 48 53 49
R19 | 852 52 117 62 52 44 20 26 | 103 51 64 114 101 93 88
R20 | 1465 64 119 88 33 58 23 29 | 105 43 40 86 110 67 69
R21 | 753 14 25 10 11 11 12 6 | 63 48 56 55 59 60 57
XR22 | 2659 --- --- 334 --- 25 19 22 | --- --- 266 --- 259 247 250
R24 | 1796 14 34 9 14 13 19 7 | 54 36 52 41 59 58 50
XR25 | 6983 --- --- --- --- --- 6 0 | --- --- --- --- --- 27 30
------+-----------------------------------------+-------------------------------------
RMS | 1592 26 46 32 23 26 21 |T 63 50 69 65 72 68 66
WRMS | 1592 18 26 23 16 22 19 |NE 58 41 64 56 69 65 62
MEDI | 951 14 25 18 14 15 19 |MD 54 44 56 55 59 60 50
Table 3.2236.4 GPS week: 2236 Day: 4 MJD: 59900
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 578 26 28 34 21 21 29 12 | 63 62 38 52 51 73 53
R02 | 854 11 15 12 12 12 22 6 | 39 42 34 37 40 43 37
R03 | 990 6 15 15 11 24 22 7 | 53 53 48 54 73 56 56
XR04 | 870 7 12 13 --- 11 15 6 | 53 58 51 --- 63 52 54
R05 | 1011 24 15 22 21 11 22 9 | 48 43 44 33 40 38 37
R07 | 772 10 11 14 13 20 22 7 | 51 45 58 49 48 67 51
R08 | 756 13 12 21 15 18 18 7 | 47 45 54 56 45 58 49
R09E | 3266 25 39 23 28 30 31 13 | 86 83 83 85 76 88 80
R11E | 2640 11 13 13 12 17 21 6 | 34 36 35 38 48 42 37
R12E | 908 8 26 13 9 17 35 8 | 105 105 102 107 115 88 103
R13E | 701 24 42 29 33 28 37 14 | 43 41 43 52 47 66 42
R14E | 684 9 21 12 15 13 17 6 | 50 51 53 56 57 55 52
R15E | 914 10 30 12 18 18 25 8 | 93 90 100 94 104 93 96
R17 | 644 9 32 17 10 17 23 7 | 56 44 48 51 68 66 55
R18 | 592 10 40 20 11 14 24 8 | 53 39 50 54 60 67 53
R19 | 551 38 122 68 60 70 30 29 | 79 50 74 108 93 76 78
R20 | 2004 63 111 83 25 28 45 27 | 92 60 46 72 64 78 62
R21 | 784 10 32 13 13 14 16 7 | 54 41 55 55 56 54 52
XR22 | 3408 --- --- 347 --- 14 20 17 | --- --- 671 --- 654 676 664
R24 | 1492 14 36 18 17 18 23 9 | 53 35 42 40 57 59 46
XR25 | 8717 --- --- --- --- --- 8 0 | --- --- --- --- --- 41 42
------+-----------------------------------------+-------------------------------------
RMS | 1342 22 47 31 22 25 27 |T 60 53 86 60 92 92 85
WRMS | 1342 17 28 19 15 19 25 |NE 57 47 93 55 100 100 92
MEDI | 870 11 28 17 15 17 22 |MD 53 45 50 54 57 66 53
Table 3.2236.5 GPS week: 2236 Day: 5 MJD: 59901
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 734 29 45 33 14 38 12 12 | 52 69 49 64 29 43 47
R02 | 942 10 9 10 8 7 16 4 | 35 39 41 41 36 37 37
R03 | 932 6 16 23 11 13 24 7 | 42 41 39 50 52 47 44
XR04 | 1065 7 19 17 --- 9 13 6 | 46 42 40 --- 44 46 43
R05 | 1133 25 25 16 19 13 24 9 | 38 38 41 35 31 33 32
R07 | 558 14 14 15 17 12 6 6 | 43 40 36 32 34 33 35
R08 | 810 16 13 24 10 14 13 7 | 39 35 48 35 37 33 37
R09E | 3422 23 27 23 32 26 37 12 | 82 79 90 80 75 83 78
R11E | 2779 23 24 8 23 45 17 11 | 57 55 47 54 43 45 45
R12E | 495 11 26 9 17 12 24 7 | 98 95 94 102 98 92 96
R13E | 723 15 48 27 39 28 26 13 | 36 28 32 56 47 44 35
R14E | 1555 16 28 22 19 14 12 8 | 65 64 61 66 68 63 62
R15E | 583 13 33 12 18 10 21 7 | 63 61 56 61 63 56 59
R17 | 1303 12 28 13 16 12 13 6 | 46 37 40 38 44 46 42
R18 | 563 10 42 18 16 12 26 9 | 43 35 47 44 48 56 45
R19 | 1578 43 147 84 50 95 40 33 | 58 62 62 78 83 68 60
R20 | 1758 40 112 99 45 54 48 29 | 68 73 81 92 68 81 71
R21 | 1318 12 32 16 13 17 23 8 | 49 48 51 52 56 47 49
XR22 | 5485 --- --- 335 --- 12 10 11 | --- --- 554 --- 515 521 517
R24 | 788 14 36 9 15 21 18 8 | 51 36 44 40 41 48 43
XR25 | 8860 --- --- --- --- --- 6 0 | --- --- --- --- --- 60 64
------+-----------------------------------------+-------------------------------------
RMS | 1442 21 52 35 24 32 25 |T 53 51 77 56 75 75 73
WRMS | 1442 16 30 20 16 22 22 |NE 46 45 83 50 79 79 77
MEDI | 1065 14 28 17 17 13 18 |MD 49 42 47 52 47 47 45
Table 3.2236.6 GPS week: 2236 Day: 6 MJD: 59902
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 527 40 40 38 39 40 22 16 | 82 71 48 57 52 61 59
R02 | 1288 13 10 12 14 27 34 9 | 45 48 50 49 43 66 48
R03 | 665 9 9 12 14 10 18 5 | 64 66 61 70 74 68 66
XR04 | 1056 13 17 27 --- 11 17 8 | 70 63 59 --- 69 68 65
R05 | 817 22 22 21 30 13 18 9 | 56 51 52 48 46 42 45
R07 | 1185 14 18 15 17 19 13 7 | 67 60 58 55 52 58 57
R08 | 730 14 13 24 12 11 15 7 | 54 52 71 60 58 63 59
R09E | 3156 22 19 18 22 24 29 10 | 85 81 78 90 75 71 77
R11E | 2879 19 25 11 26 45 11 11 | 53 54 54 64 59 61 55
R12E | 570 10 31 14 17 18 19 8 | 119 105 116 112 113 121 114
R13E | 623 26 49 31 58 31 23 16 | 53 38 37 84 50 52 48
R14E | 1979 14 24 21 12 14 21 8 | 57 60 80 72 68 74 67
R15E | 555 15 28 10 21 17 16 8 | 71 65 71 78 73 76 72
R17 | 1015 13 26 11 11 12 15 6 | 68 43 62 54 64 67 60
R18 | 432 7 23 28 9 16 24 8 | 59 45 74 57 58 73 60
R19 | 1589 39 135 87 46 62 49 31 | 110 55 73 119 110 117 94
R20 | 1214 36 95 124 73 69 51 33 | 122 97 81 143 138 135 107
R21 | 1074 9 33 13 16 9 14 7 | 76 62 71 77 74 74 72
XR22 | 6212 --- --- 329 --- 17 13 15 | --- --- 701 --- 642 644 642
R24 | 1229 16 32 15 17 17 15 8 | 73 40 63 60 59 68 61
XR25 | 8409 --- --- --- --- --- 7 0 | --- --- --- --- --- 71 73
------+-----------------------------------------+-------------------------------------
RMS | 1415 21 46 40 30 30 25 |T 72 60 98 74 98 101 95
WRMS | 1415 16 28 21 15 24 21 |NE 72 57 108 70 109 111 104
MEDI | 1074 14 25 18 17 17 18 |MD 68 60 63 64 64 68 65
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