[IGSREPORT-28634] Wk 2205 IGLOS Final Orbits
acc
acc at igs.org
Tue May 3 02:13:24 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2205 (Apr 10, 2022 - Apr 16, 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 2.2205.
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:
igl2205[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2205 in the SP3 format.
igl22057.sum Combination Report for GPS Week 2205.
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 | -8.8 ns
1 | -0.1 ns
2 | -8.1 ns
3 | -6.8 ns
4 | 0.6 ns
5 | 0.4 ns
6 | -8.1 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2205, 1a.2205).
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 2.2205.0-6)
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 3.2205.0-6).
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 2205 summary. (Apr 10, 2022 - Apr 16, 2022)
Table 1.2205.a GPS week : 2205 MJD: 59679.0-59685.0
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| -1 0 0 2 -26 35 .12 19 15 | 30393 76 3408 8993
| 1 0 1 20 20 27 .02 | 4438 908
emx n/a| 0 3 5 15 27 -36 -.07 36 30 | -15781 527 3328 8790
| 1 0 1 22 18 22 .05 | 16562 863
esx n/a| 0 -1 -1 -14 27 -22 -.12 27 20 | 3504 -359 3421 9589
| 1 0 1 13 14 52 .05 | 7144 1346
gfz n/a| 0 0 0 -31 12 -6 -.01 32 18 | 0 -308 3363 8616
| 1 1 1 24 18 26 .03 | 0 1230
grg n/a| 0 0 -3 -4 -13 48 .30 25 19 | -4360 -219 3354 8279
| 1 2 3 16 23 45 .05 | 4188 942
iac n/a| 3 0 1 10 -19 -47 -.32 26 23 | -2313 -81 3362 9450
| 1 2 4 15 22 75 .07 | 4573 627
Table 1.2205.b GPS week : 2205 MJD: 59679.0-59685.0
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 | 15 17 14 12 12 11 15 |
R02 | 7 5 8 6 6 6 6 |
R03 | 7 8 5 6 5 7 7 |
R04 | 8 9 8 10 7 11 9 |
R05 | 9 9 9 10 11 7 7 |
R07 | 5 7 6 6 7 8 6 |
R08 | 10 11 8 7 11 8 6 |
R09 | 7 8 8 8 8 9 9 |
R11 | 12 10 10 12 16 12 12 |
R12 | 10 9 10 10 10 8 8 |
R13 | 17 13 18 20 16 17 16 |
R14 | 9 8 10 10 8 9 10 |
R15 | 7 7 14 8 7 8 9 |
R17 | 8 8 9 8 8 9 8 |
R18 | 7 8 7 8 7 8 9 |
R19 | 19 22 17 17 22 19 19 |
R20 | 22 19 21 23 18 20 22 |
R21 | 7 7 7 8 8 9 9 |
R22 | 24 22 23 25 32 25 26 |
R24 | 7 7 8 9 7 8 9 |
Table 1.2205.c GPS week : 2205 MJD: 59679.0-59685.0
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 2205 0 | -188 -121 137 -267 -1984 -2459 83.2 1543 1543 | -8776 0
brd 2205 1 | -18 -31 158 247 1594 3665 81.3 1412 1412 | -123 0
brd 2205 2 | 59 0 123 -324 1677 4109 81.5 1517 1517 | -8101 0
brd 2205 3 | 9 32 101 -1344 164 67 80.4 1644 1644 | -6801 0
brd 2205 4 | -16 24 148 -848 -151 -2658 81.6 1309 1309 | 632 0
brd 2205 5 | 7 -73 67 -1398 -214 -5969 82.4 1482 1482 | 398 0
brd 2205 6 | -29 70 127 -2419 -1893 -2795 79.0 1639 1639 | -8141 0
-------------+------------------------------------------------------------+----------------
brd 2205 mean| -24 -14 123 -907 -115 -862 81.4 1506 1506 | -4416 0
brd 2205 sdev| 77 66 30 894 1464 3689 1.4 120 120 | 4457 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 2.2205.0 GPS week: 2205 Day: 0 MJD: 59679
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 8 -6 50 .13 19 14 | 26943 -1179 3535 9734
emx n/a| -1 3 5 18 34 -42 .01 37 28 | -15932 -1347 3531 9443
esx n/a| 0 -2 1 -5 18 28 -.09 28 18 | -8472 -1381 3535 11696
gfz n/a| -3 1 0 -39 32 28 .01 35 19 | 0 -2050 3535 9513
grg n/a| 0 -2 -2 -20 -36 23 .27 24 18 | -8430 -1388 3550 9147
iac n/a| 1 2 0 17 -27 -103 -.35 25 22 | -7084 -396 3535 10221
Table 2.2205.1 GPS week: 2205 Day: 1 MJD: 59680
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 0 33 -13 59 .11 20 15 | 34495 310 3177 8629
emx n/a| -2 2 3 -11 34 -46 -.08 36 30 | 6147 1270 3133 8437
esx n/a| 1 -2 -3 -7 18 -34 -.12 27 18 | 6578 -450 3118 7973
gfz n/a| 2 0 0 -29 6 -28 .02 33 15 | 0 175 3151 7965
grg n/a| 0 -2 -4 -17 -25 18 .27 24 17 | -277 267 3118 7821
iac n/a| 0 1 7 13 -14 -34 -.29 22 19 | 2186 -76 3127 8998
Table 2.2205.2 GPS week: 2205 Day: 2 MJD: 59681
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 -30 -14 33 .11 20 16 | 27124 -714 3224 7897
emx n/a| 0 3 6 45 22 -6 -.09 35 31 | -20749 532 3187 7819
esx n/a| 2 -1 0 -19 34 1 -.11 31 24 | 7218 -2708 3640 8015
gfz n/a| 0 0 1 -42 -18 0 -.01 31 20 | 0 -1550 3206 7629
grg n/a| -4 3 -10 20 -1 71 .20 26 19 | -7272 -1714 3188 7205
iac n/a| 2 -2 6 -8 -4 -139 -.25 23 20 | -5599 -551 3193 8307
Table 2.2205.3 GPS week: 2205 Day: 3 MJD: 59682
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 1 0 -3 -27 31 .15 20 16 | 27499 443 3048 9777
emx n/a| 0 4 6 29 22 -27 -.05 35 31 | -27197 1055 3001 9471
esx n/a| 0 -1 -1 -40 14 -97 -.05 27 24 | 12861 173 2994 12018
gfz n/a| 0 -2 -1 1 20 -21 .05 35 17 | 0 870 3009 9582
grg n/a| -1 -3 0 -14 -30 69 .34 27 22 | -7054 507 2987 8916
iac n/a| 2 1 0 6 3 23 -.33 26 24 | -5033 244 3022 10233
Table 2.2205.4 GPS week: 2205 Day: 4 MJD: 59683
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 -22 9 .09 14 13 | 35953 -180 3178 7696
emx n/a| 0 3 7 -18 55 -46 -.08 37 29 | 2621 650 2837 7380
esx n/a| -1 -1 -2 -17 19 -51 -.20 24 19 | -3324 1270 3120 10112
gfz n/a| 1 -1 2 1 8 -48 -.04 30 19 | 0 441 3156 7303
grg n/a| 0 -1 -2 -13 -31 108 .33 21 18 | 424 245 3086 7160
iac n/a| 5 0 -3 -3 -19 43 -.28 27 26 | 3052 -464 3118 8215
Table 2.2205.5 GPS week: 2205 Day: 5 MJD: 59684
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 -1 16 -31 -6 .14 19 15 | 34811 1651 3936 9574
emx n/a| 1 2 3 15 28 -74 -.14 37 33 | -13750 767 3927 9564
esx n/a| -1 0 -1 -3 56 50 -.18 26 20 | 3877 805 3868 8625
gfz n/a| 0 0 1 -54 7 14 -.02 29 17 | 0 1017 3912 9191
grg n/a| -1 0 -3 17 10 74 .32 28 20 | 112 634 3873 8929
iac n/a| 5 -2 -1 40 -65 -127 -.26 24 22 | 2332 1187 3861 10026
Table 2.2205.6 GPS week: 2205 Day: 6 MJD: 59685
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 -2 -9 -68 70 .10 22 14 | 25926 201 3763 9648
emx n/a| 0 1 6 28 -4 -13 -.05 33 29 | -41613 767 3683 9418
esx n/a| 1 0 0 -3 29 -54 -.08 25 17 | 5793 -224 3673 8685
gfz n/a| 0 0 -1 -59 33 6 -.04 29 16 | 0 -1065 3576 9129
grg n/a| 0 0 -2 0 23 -28 .36 26 21 | -8023 -88 3678 8781
iac n/a| 3 0 3 9 -7 7 -.46 32 27 | -6046 -512 3683 10153
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 3.2205.0 GPS week: 2205 Day: 0 MJD: 59679
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 629 27 30 43 36 34 21 14 | 72 75 68 76 61 82 69
R02 | 4014 13 24 12 15 10 20 7 | 36 38 41 36 37 50 37
R03 | 1054 10 11 7 20 15 23 6 | 46 42 43 50 50 37 43
XR04 | 1240 15 8 10 --- 11 24 7 | 49 44 38 --- 41 36 40
R05 | 1177 21 16 19 25 15 25 9 | 33 35 45 38 42 40 35
R07 | 648 6 9 13 16 11 14 5 | 59 57 58 70 58 61 59
R08 | 963 12 14 14 31 33 27 10 | 55 55 60 74 41 64 55
R09 | 2549 12 16 10 17 22 17 7 | 41 41 50 50 37 48 42
XR11 | 2388 --- 25 14 19 32 23 12 | --- 51 58 57 64 65 58
R12 | 1616 16 37 17 13 21 21 9 | 90 57 85 81 79 90 81
R13 | 1237 28 55 52 38 24 22 16 | 118 69 71 118 111 97 97
R14 | 750 9 30 19 18 17 27 8 | 83 52 91 88 82 63 76
R15 | 818 7 25 8 19 13 21 7 | 98 76 98 102 90 97 93
R17E | 621 13 25 11 14 14 26 7 | 85 87 81 81 91 79 83
R18E | 1125 9 26 17 14 14 11 6 | 25 21 27 24 34 23 23
R19E | 1308 19 67 36 66 39 36 19 | 25 25 44 69 36 28 27
R20E | 1689 39 63 47 78 32 46 22 | 98 107 115 134 108 105 105
R21E | 1074 13 26 15 14 13 15 7 | 33 32 36 37 37 30 32
R22E | 1181 34 67 62 68 49 42 23 | 38 59 89 85 45 52 47
R24E | 1356 8 33 11 17 12 14 7 | 71 75 70 74 79 68 72
------+-----------------------------------------+-------------------------------------
RMS | 1542 19 37 28 35 24 25 |T 60 54 63 70 61 60 58
WRMS | 1542 14 28 18 19 18 22 |NE 65 53 62 70 61 63 60
MEDI | 1177 13 25 14 19 15 22 |MD 55 52 58 74 50 61 55
Table 3.2205.1 GPS week: 2205 Day: 1 MJD: 59680
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 627 34 19 50 41 40 24 16 | 51 48 46 48 51 54 45
R02 | 2725 8 10 14 8 12 10 4 | 31 30 33 32 28 34 30
R03 | 562 14 11 12 19 13 28 8 | 34 27 33 39 33 25 29
XR04 | 687 19 14 9 --- 14 26 9 | 34 31 31 --- 21 25 25
R05 | 1156 15 12 25 22 14 20 8 | 25 26 41 34 26 20 25
R07 | 596 8 15 10 10 10 25 6 | 40 40 42 39 39 56 42
R08 | 1324 15 15 14 38 35 11 10 | 36 35 35 55 24 38 34
R09 | 2108 12 24 10 22 14 22 7 | 34 34 43 48 33 48 38
XR11 | 2660 --- 25 13 11 26 15 9 | --- 45 42 42 49 42 42
R12 | 2140 18 43 18 12 18 12 9 | 69 45 61 64 59 62 60
R13 | 1107 24 42 40 23 24 15 12 | 81 58 71 80 68 70 70
R14 | 1162 11 40 21 11 12 10 8 | 66 43 76 72 70 56 64
R15 | 1149 16 23 10 10 14 14 6 | 85 67 72 76 65 65 72
R17E | 860 12 32 14 10 14 17 7 | 56 62 52 56 57 48 53
R18E | 1159 13 25 19 11 20 14 7 | 25 31 27 24 33 25 24
R19E | 1152 32 73 35 70 47 36 21 | 24 39 42 79 38 35 27
R20E | 1842 29 60 40 50 28 44 18 | 77 83 80 93 76 71 75
R21E | 1259 10 28 12 11 15 19 7 | 32 31 31 31 39 28 30
R22E | 1572 38 55 52 76 38 28 21 | 36 50 67 63 51 43 39
R24E | 713 15 29 14 16 13 13 7 | 49 50 44 49 57 50 48
------+-----------------------------------------+-------------------------------------
RMS | 1411 20 36 27 33 24 22 |T 46 43 48 53 45 44 43
WRMS | 1411 15 30 18 15 17 19 |NE 48 40 48 52 43 45 44
MEDI | 1156 15 25 14 16 14 17 |MD 36 40 42 49 39 43 39
Table 3.2205.2 GPS week: 2205 Day: 2 MJD: 59681
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 543 37 27 42 40 23 8 14 | 64 60 54 42 54 51 52
R02 | 1804 14 10 25 15 14 19 7 | 42 37 33 40 39 56 39
R03 | 538 7 10 12 13 11 13 5 | 39 37 43 43 36 47 39
XR04 | 600 15 15 14 --- 15 20 8 | 44 44 34 --- 31 40 36
R05 | 1264 20 15 23 25 20 13 9 | 29 31 49 48 35 50 35
R07 | 799 10 17 10 12 11 14 5 | 51 44 55 62 49 59 52
R08 | 2382 13 5 25 20 23 12 7 | 43 43 46 45 27 41 40
R09 | 1639 9 24 9 26 17 20 8 | 37 32 44 50 46 48 40
XR11 | 2790 --- 29 17 9 17 21 9 | --- 57 47 53 58 69 55
R12 | 1998 15 42 14 17 23 19 10 | 75 37 66 59 83 71 66
R13 | 890 22 63 48 34 48 24 17 | 86 52 50 97 92 90 77
R14 | 1715 16 35 24 16 15 21 9 | 60 34 68 48 55 71 56
R15 | 1421 29 30 59 16 25 13 13 | 78 62 113 80 74 74 77
R17E | 683 11 30 15 22 15 25 9 | 56 46 54 57 55 63 53
R18E | 1212 11 17 18 10 23 14 7 | 27 24 29 26 40 30 27
R19E | 1822 27 51 38 49 31 30 16 | 36 45 43 54 42 36 31
R20E | 2839 29 69 40 58 30 49 20 | 72 101 97 104 75 80 81
R21E | 1440 9 26 16 10 12 15 6 | 35 37 34 39 43 35 35
R22E | 1240 31 48 57 69 52 48 22 | 35 35 68 68 53 79 44
R24E | 540 12 23 17 11 24 15 7 | 51 50 54 54 51 58 51
------+-----------------------------------------+-------------------------------------
RMS | 1516 20 35 31 31 26 23 |T 50 45 54 56 51 57 49
WRMS | 1516 16 31 24 20 19 20 |NE 54 43 54 55 52 59 51
MEDI | 1264 15 26 18 17 20 19 |MD 44 43 49 53 49 56 44
Table 3.2205.3 GPS week: 2205 Day: 3 MJD: 59682
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 619 25 19 33 37 25 18 12 | 64 66 41 56 64 60 56
R02 | 1924 12 11 10 14 19 13 6 | 37 26 32 32 25 33 30
R03 | 660 7 13 12 10 21 15 6 | 41 40 43 38 58 51 44
XR04 | 519 18 22 17 --- 18 26 10 | 37 40 27 --- 23 39 30
R05 | 1487 20 18 28 21 22 24 10 | 29 41 49 48 33 36 33
R07 | 1065 7 11 15 16 17 16 6 | 52 50 45 59 62 40 50
R08 | 2854 13 12 11 15 10 23 6 | 46 50 52 53 58 63 51
R09 | 1134 17 20 13 18 25 18 8 | 41 31 47 50 24 40 36
XR11 | 2633 --- 30 27 14 21 23 12 | --- 37 33 54 62 64 48
R12 | 1449 15 40 19 24 20 16 10 | 75 41 63 89 78 80 70
R13 | 601 18 68 53 41 51 34 19 | 86 42 42 98 110 106 78
R14 | 2535 15 32 22 24 14 20 9 | 63 35 72 47 65 76 60
R15 | 1557 14 25 13 13 22 18 7 | 69 47 73 61 61 65 62
R17E | 784 15 32 9 14 12 21 8 | 36 35 35 41 40 44 36
R18E | 703 9 19 19 19 23 12 7 | 25 26 27 28 30 24 23
R19E | 1512 26 58 37 52 28 30 17 | 29 45 46 53 45 30 30
R20E | 2649 32 62 47 82 32 51 23 | 54 64 72 99 52 56 53
R21E | 1544 10 29 12 15 19 16 7 | 31 33 33 37 39 31 30
R22E | 1933 47 52 48 77 57 58 25 | 26 32 60 49 50 59 27
R24E | 1861 18 29 21 15 23 18 9 | 30 34 27 34 40 30 27
------+-----------------------------------------+-------------------------------------
RMS | 1643 20 35 27 35 27 26 |T 45 40 45 54 50 51 43
WRMS | 1643 16 31 24 17 22 24 |NE 53 42 47 57 55 57 49
MEDI | 1487 15 25 19 18 21 18 |MD 41 40 43 50 50 44 36
Table 3.2205.4 GPS week: 2205 Day: 4 MJD: 59683
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 615 17 13 20 39 28 36 11 | 58 61 63 61 49 70 56
R02 | 1494 7 13 17 10 11 24 6 | 32 36 29 34 27 43 31
R03 | 520 10 6 9 10 11 18 5 | 45 40 38 43 37 31 39
XR04 | 557 9 15 18 --- 13 16 6 | 32 36 28 --- 34 28 30
R05 | 1587 17 21 34 28 17 31 11 | 25 36 50 43 35 30 28
R07 | 878 9 10 18 14 23 19 7 | 45 47 51 48 37 48 43
R08 | 2163 12 19 34 32 23 23 10 | 46 48 45 50 59 49 44
R09 | 1558 16 19 9 20 17 19 7 | 41 38 36 33 26 33 33
XR11 | 1602 --- 68 17 16 18 32 16 | --- 85 59 65 56 81 63
R12 | 827 10 43 18 17 29 26 10 | 76 59 70 86 88 97 77
R13 | 853 26 66 44 28 29 27 16 | 93 55 55 95 89 93 79
R14 | 1696 12 31 20 21 11 11 7 | 59 38 69 50 61 54 56
R15 | 1900 7 30 11 13 13 21 6 | 68 50 75 72 74 69 68
R17E | 679 15 28 17 20 13 17 8 | 30 29 30 36 36 37 28
R18E | 1300 7 19 17 21 12 14 6 | 25 25 28 25 34 28 25
R19E | 1214 16 87 31 76 33 56 21 | 36 58 46 81 42 36 35
R20E | 1711 26 62 43 50 30 37 17 | 50 48 58 70 70 70 53
R21E | 641 8 29 16 18 14 23 7 | 36 32 33 40 42 41 35
XR22E | 1063 39 --- 61 94 86 33 32 | 42 --- 56 56 65 37 33
R24E | 987 11 27 13 13 19 18 7 | 29 23 30 32 35 33 27
------+-----------------------------------------+-------------------------------------
RMS | 1309 14 37 24 30 21 27 |T 45 44 47 53 49 50 44
WRMS | 1309 13 29 19 19 18 26 |NE 51 48 51 56 51 55 49
MEDI | 1063 12 27 18 20 17 23 |MD 42 40 46 50 42 41 35
Table 3.2205.5 GPS week: 2205 Day: 5 MJD: 59684
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 751 23 29 18 23 32 27 11 | 46 46 59 52 29 40 41
R02 | 1332 15 10 10 10 13 20 6 | 27 34 37 39 36 41 34
R03 | 769 12 10 18 10 12 25 7 | 35 36 27 35 26 46 32
XR04 | 740 16 15 20 --- 12 34 10 | 27 28 25 --- 30 37 25
R05 | 941 12 20 16 15 14 16 6 | 17 27 38 35 30 18 23
R07 | 832 7 13 20 15 15 29 7 | 34 35 42 43 35 47 36
R08 | 874 18 16 22 14 14 11 7 | 28 33 30 30 31 29 27
R09 | 2832 18 25 11 16 24 24 8 | 41 30 42 34 40 48 37
XR11 | 1462 --- --- 26 13 14 24 11 | --- --- 33 44 38 48 38
R12 | 1171 14 29 16 11 15 18 7 | 60 42 58 47 50 59 52
R13 | 1021 25 59 49 39 32 26 17 | 79 57 47 80 75 71 66
R14 | 1070 13 33 23 16 18 14 8 | 54 27 59 40 43 49 45
R15 | 1643 9 35 11 16 11 16 7 | 60 40 63 64 64 61 58
R17E | 848 16 29 13 14 15 24 8 | 66 61 72 67 68 67 66
R18E | 972 10 23 17 27 15 17 8 | 22 22 27 26 30 25 22
R19E | 1510 29 64 31 44 47 41 18 | 26 54 44 60 46 35 30
R20E | 2646 39 56 51 46 40 40 20 | 76 74 108 106 81 82 83
R21E | 1434 16 28 15 27 13 16 8 | 39 29 34 38 38 36 31
R22E | 2475 30 72 49 71 72 31 24 | 41 68 58 55 48 51 40
R24E | 899 14 29 18 14 16 19 8 | 50 52 56 52 57 52 51
------+-----------------------------------------+-------------------------------------
RMS | 1481 19 37 26 29 28 24 |T 43 41 47 49 44 47 41
WRMS | 1481 15 33 20 17 20 22 |NE 42 36 43 45 40 45 39
MEDI | 1021 16 29 18 16 15 24 |MD 41 36 42 44 38 47 37
Table 3.2205.6 GPS week: 2205 Day: 6 MJD: 59685
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 989 31 38 40 22 33 34 14 | 71 82 73 76 50 60 63
R02 | 2709 8 10 13 14 12 23 6 | 44 44 45 51 45 51 45
R03 | 848 11 12 9 13 9 33 6 | 56 54 58 58 57 67 57
XR04 | 956 14 12 21 --- 21 22 9 | 45 42 29 --- 41 43 38
R05 | 522 20 9 17 8 17 17 7 | 31 29 38 32 32 37 29
R07 | 677 7 6 16 11 8 21 5 | 57 57 59 63 57 58 57
R08 | 917 10 8 12 15 11 19 5 | 50 53 48 59 55 52 52
R09 | 3888 18 22 11 15 15 31 8 | 54 37 48 50 40 55 45
XR11 | 1191 --- 27 12 28 18 27 11 | --- 42 46 64 50 61 49
R12 | 1132 16 29 11 14 7 24 7 | 90 58 81 83 80 81 79
R13 | 1147 31 56 31 30 22 35 15 | 104 66 64 104 92 89 85
R14 | 1037 9 32 20 16 25 20 9 | 74 46 81 76 64 72 68
R15 | 1287 14 30 10 18 21 23 8 | 84 61 86 90 82 79 79
R17E | 1800 15 23 13 16 17 26 8 | 97 100 96 99 99 98 97
R18E | 655 14 19 23 19 15 31 9 | 27 22 32 28 37 35 26
R19E | 1126 24 50 32 57 45 41 18 | 56 45 36 61 43 41 37
R20E | 2182 55 60 48 44 29 61 22 | 126 124 126 140 138 165 131
R21E | 1001 18 25 13 18 11 30 8 | 42 37 38 44 48 45 39
R22E | 2475 28 50 55 77 71 54 25 | 51 68 71 61 59 63 50
R24E | 684 18 31 17 12 19 20 8 | 94 104 90 97 97 89 94
------+-----------------------------------------+-------------------------------------
RMS | 1639 22 33 25 29 26 32 |T 65 58 62 70 63 67 61
WRMS | 1639 14 29 17 16 21 27 |NE 63 51 58 67 57 61 57
MEDI | 1037 16 25 16 16 17 26 |MD 56 53 58 63 55 60 52
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