[IGSREPORT-28250] Wk 2178 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 22 02:09:34 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2178 (Oct 03, 2021 - Oct 09, 2021)
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 2.2178.
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:
igl2178[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2178 in the SP3 format.
igl21787.sum Combination Report for GPS Week 2178.
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 | -3.9 ns
1 | -0.7 ns
2 | -3.5 ns
3 | -0.4 ns
4 | -3.2 ns
5 | -1.3 ns
6 | -1.6 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 1.2178, 1a.2178).
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 2.2178.0-6)
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 3.2178.0-6).
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 2178 summary. (Oct 03, 2021 - Oct 09, 2021)
Table 1.2178.a GPS week : 2178 MJD: 59490.0-59496.0
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 -8 2 -10 .09 20 15 | 16793 -318 3305 8816
| 0 1 0 13 21 11 .04 | 674 2808
emx n/a| 0 0 4 14 -20 -34 -.15 33 29 | -5154 -226 3342 8933
| 1 1 1 17 18 41 .03 | 10469 1742
esx n/a| 0 3 2 20 11 -21 -.13 26 20 | -9511 -50 3305 9664
| 1 1 1 21 11 26 .05 | 12669 2741
gfz n/a| 0 0 0 6 -2 -15 .08 35 22 | 0 -263 3367 8689
| 1 1 4 21 21 39 .05 | 0 3018
grg n/a| 2 -2 -1 -26 7 -81 .20 32 23 | -1900 -284 3304 8031
| 0 1 3 22 11 36 .05 | 607 2645
iac n/a| -1 -5 -9 -27 -10 195 -.18 34 34 | 225 -534 3318 9152
| 2 2 4 26 45 77 .05 | 1219 2077
mcc n/a| 12 -6 13 1 40 265 -.38 176 176 | --- --- --- ---
| 10 12 15 177 192 869 .48 | --- ---
Table 1.2178.b GPS week : 2178 MJD: 59490.0-59496.0
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 14 16 19 17 16 14 |
R02 | 9 8 8 8 7 8 9 |
R03 | 7 6 6 7 9 9 8 |
R04 | 9 8 7 9 11 11 10 |
R05 | 7 7 8 11 11 8 9 |
R07 | 8 7 8 7 9 6 9 |
R08 | 7 9 11 10 8 9 11 |
R09 | 10 8 9 9 10 10 8 |
R11 | 17 20 12 10 10 10 6 |
R12 | 11 14 9 8 11 9 10 |
R13 | 16 15 15 16 15 19 18 |
R14 | 10 8 7 8 8 7 9 |
R15 | 8 9 7 9 8 8 10 |
R16 | 16 17 18 17 16 14 16 |
R17 | 8 8 7 8 8 7 7 |
R18 | 8 9 9 11 11 10 10 |
R19 | 21 20 25 22 19 22 31 |
R20 | 22 22 19 20 22 19 17 |
R21 | 7 8 9 9 10 10 10 |
R22 | 27 23 28 22 25 25 26 |
R24 | 10 10 7 8 10 10 9 |
Table 1.2178.c GPS week : 2178 MJD: 59490.0-59496.0
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 2178 0 | 14 68 61 24 987 521 82.3 1723 1723 | -3946 0
brd 2178 1 | -44 40 73 -1506 2342 2853 81.1 1686 1686 | -737 0
brd 2178 2 | -27 -41 -58 424 2982 6663 83.2 1910 1910 | -3511 0
brd 2178 3 | 112 -2 -47 720 4451 5845 81.5 1970 1970 | -426 0
brd 2178 4 | -48 12 -27 1971 837 -10860 83.2 1568 1568 | -3227 0
brd 2178 5 | 16 42 29 1975 339 -8555 80.9 1777 1777 | -1327 0
brd 2178 6 | -4 -42 100 -42 -1732 -5308 80.9 1668 1668 | -1581 0
-------------+------------------------------------------------------------+----------------
brd 2178 mean| 2 11 18 509 1458 -1262 81.9 1757 1757 | -2107 0
brd 2178 sdev| 54 42 63 1220 2004 7013 1.0 140 140 | 1425 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 2.2178.0 GPS week: 2178 Day: 0 MJD: 59490
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 -13 -12 -15 .12 17 13 | 17897 -3520 3751 10803
emx n/a| -2 0 5 24 -4 -58 -.09 32 28 | -13731 -2385 3765 11177
esx n/a| 0 5 2 21 28 -4 -.11 29 24 | -36963 -2847 3757 11133
gfz n/a| 0 0 -3 12 -29 14 .04 43 21 | 0 -3382 3805 10993
grg n/a| 3 -1 0 3 16 -152 .14 32 21 | -2540 -3356 3797 7746
iac n/a| 1 -5 0 -7 -13 240 -.24 31 31 | 235 -3077 3843 9844
mcc n/a| 11 0 28 -127 -91 1434 -.07 139 139 | --- --- --- ---
Table 2.2178.1 GPS week: 2178 Day: 1 MJD: 59491
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 -1 -14 -19 -14 .04 21 15 | 17523 3523 3575 11226
emx n/a| -1 1 6 -3 10 -85 -.17 32 29 | 9222 2241 3687 9636
esx n/a| 0 4 1 -1 18 -24 -.07 31 24 | -5871 2914 3550 11785
gfz n/a| 1 0 -2 9 6 -98 .16 38 27 | 0 3694 3657 11584
grg n/a| 1 -1 0 -11 12 -50 .17 25 18 | -901 3335 3580 10995
iac n/a| -1 -6 -10 17 -21 231 -.17 33 33 | 1545 1887 3597 11651
mcc n/a| 12 -6 31 112 -142 1381 .25 158 158 | --- --- --- ---
Table 2.2178.2 GPS week: 2178 Day: 2 MJD: 59492
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 -24 12 15 .07 24 17 | 16424 -3972 3134 8352
emx n/a| 0 0 5 15 -30 -9 -.14 32 26 | -18279 -2202 3126 8780
esx n/a| 0 0 4 43 9 16 -.06 23 18 | -4977 -3984 3133 10285
gfz n/a| 0 1 2 -3 23 -19 .06 34 19 | 0 -4231 3201 8116
grg n/a| 4 -2 -5 -30 4 -46 .15 31 23 | -1828 -3679 3091 7930
iac n/a| -2 0 -13 -49 -4 39 -.26 37 37 | -1596 -653 3116 8821
mcc n/a| 11 14 -6 -36 17 -721 -.21 119 119 | --- --- --- ---
Table 2.2178.3 GPS week: 2178 Day: 3 MJD: 59493
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 -10 36 -12 .07 20 17 | 16238 2184 2932 7922
emx n/a| 0 2 7 8 -39 -79 -.18 33 27 | 2071 1307 2956 7815
esx n/a| 1 3 2 54 17 -20 -.18 26 22 | 3080 3079 2923 10016
gfz n/a| -1 -2 -4 47 -14 6 .15 34 19 | 0 2609 2968 7963
grg n/a| 3 -1 2 -46 -11 -93 .26 32 27 | -1454 2016 2919 7694
iac n/a| -4 -6 -13 -49 -95 276 -.16 34 34 | 1568 691 2917 8432
mcc n/a| 18 -23 9 -292 -28 166 -.08 160 160 | --- --- --- ---
Table 2.2178.4 GPS week: 2178 Day: 4 MJD: 59494
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 1 -2 7 14 -14 .13 19 15 | 16489 -1465 3222 7021
emx n/a| 1 0 3 -3 -19 30 -.19 36 28 | -4604 -1079 3291 7666
esx n/a| 3 2 2 9 -4 -48 -.13 27 19 | -8357 -1176 3221 7907
gfz n/a| 0 0 4 -19 -8 10 .02 30 21 | 0 -2027 3270 6668
grg n/a| 1 -2 0 -57 8 -80 .23 37 26 | -2586 -1399 3198 6551
iac n/a| 0 -6 -11 -38 3 160 -.15 33 33 | 271 -2745 3224 7654
mcc n/a| -7 -16 11 196 143 286 -.68 190 190 | --- --- --- ---
Table 2.2178.5 GPS week: 2178 Day: 5 MJD: 59495
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 -15 -23 -16 .15 18 13 | 16133 454 3113 8945
emx n/a| -2 1 2 16 -37 -14 -.16 32 30 | -14113 259 3114 9399
esx n/a| 1 3 3 18 13 -60 -.18 23 18 | -6232 1277 3114 9813
gfz n/a| -1 2 5 8 23 -23 .07 32 26 | 0 476 3198 8258
grg n/a| 2 -4 -7 -32 21 -89 .23 41 26 | -1762 411 3137 8310
iac n/a| -1 -8 -7 -15 -4 218 -.13 35 35 | -1131 1870 3121 9594
mcc n/a| 14 -1 -6 -25 -39 -655 -.69 281 281 | --- --- --- ---
Table 2.2178.6 GPS week: 2178 Day: 6 MJD: 59496
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 0 13 8 -12 .07 21 16 | 16852 566 3413 7445
emx n/a| 0 -3 3 46 -21 -21 -.14 35 34 | 3353 272 3459 8064
esx n/a| -1 4 3 -1 0 -6 -.17 21 18 | -7257 386 3439 6715
gfz n/a| -2 0 3 -8 -20 3 .07 31 19 | 0 1016 3470 7246
grg n/a| 3 0 1 -8 1 -56 .20 25 19 | -2231 679 3408 6993
iac n/a| 1 -4 -9 -48 58 200 -.14 36 36 | 689 -1711 3413 8073
mcc n/a| 25 -12 24 183 427 -32 -1.16 184 184 | --- --- --- ---
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 3.2178.0 GPS week: 2178 Day: 0 MJD: 59490
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1282 22 38 40 39 23 39 --- 14 | 105 69 60 108 91 90 --- 85
R02 | 1600 14 23 10 19 13 34 156 8 | 58 47 59 70 62 80 57 60
R03M | 1233 8 18 17 12 20 20 135 7 | 70 49 60 68 80 80 114 67
XR04M | 779 10 12 24 --- 15 30 --- 9 | 78 69 69 --- 76 74 --- 72
R05M | 719 12 16 24 13 11 18 120 7 | 69 57 72 67 66 61 102 65
R07 | 745 12 14 23 10 17 30 134 8 | 77 62 64 69 75 72 118 69
R08 | 731 13 19 8 15 16 26 --- 7 | 64 55 70 84 76 77 --- 69
R09 | 1524 14 11 13 16 34 33 --- 9 | 41 46 48 50 42 51 --- 43
XR11 | 2605 21 24 18 23 --- 68 --- 16 | 83 84 98 88 --- 108 --- 86
R12M | 1896 13 46 17 12 35 16 --- 11 | 78 54 71 82 99 82 --- 75
R13M | 2545 19 36 43 27 60 19 --- 15 | 89 61 59 88 118 74 --- 80
R14M | 700 11 30 19 18 11 35 --- 9 | 64 52 71 68 61 83 --- 65
R15M | 921 9 19 23 16 10 26 122 7 | 73 60 61 80 80 89 76 72
R16M | 2463 23 31 34 39 54 35 --- 15 | 53 44 67 78 75 89 --- 62
R17E | 862 10 30 12 20 15 18 --- 7 | 41 44 45 47 46 42 --- 42
R18E | 1108 14 25 17 16 19 21 --- 8 | 37 41 39 44 39 39 --- 36
R19E | 1866 27 53 32 90 42 41 --- 21 | 43 50 48 82 57 47 --- 41
R20E | 2355 22 52 54 77 38 63 --- 22 | 96 97 100 113 100 118 --- 96
R21E | 617 5 25 12 19 15 21 161 7 | 56 59 59 54 59 56 100 56
R22E | 3991 38 34 59 110 66 42 --- 26 | 61 68 114 81 95 75 --- 72
R24E | 1393 11 36 13 38 19 21 --- 10 | 96 93 91 98 90 94 --- 93
------+----------------------------------------------+------------------------------------------
RMS | 1722 17 32 29 43 32 31 139 |T 68 60 67 75 74 75 94 66
WRMS | 1722 13 28 24 21 21 31 139 |NE 71 60 66 78 69 79 87 68
MEDI | 1282 13 25 19 19 19 30 134 |MD 69 57 64 78 75 77 100 69
Table 3.2178.1 GPS week: 2178 Day: 1 MJD: 59491
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1129 20 34 44 40 15 34 --- 14 | 69 41 45 89 60 87 --- 63
R02 | 3203 13 22 19 12 7 31 181 8 | 39 30 51 47 42 47 71 40
R03M | 814 9 18 10 15 12 20 116 6 | 48 33 47 40 52 59 115 46
XR04M | 1032 9 13 18 --- 8 27 --- 7 | 60 53 57 --- 62 62 --- 58
R05M | 619 14 12 16 15 12 16 142 6 | 40 43 44 41 48 44 99 41
R07 | 1609 8 11 15 12 16 23 198 6 | 48 39 46 50 48 44 187 44
R08 | 1091 11 21 13 41 7 17 --- 9 | 41 33 45 66 39 46 --- 42
R09 | 992 16 9 14 13 27 22 --- 8 | 50 45 47 53 44 44 --- 45
R11 | 2716 38 35 76 17 14 61 --- 20 | 73 78 143 82 29 117 --- 93
R12M | 943 17 41 24 24 43 24 --- 13 | 53 47 53 69 84 74 --- 61
R13M | 944 28 43 31 31 36 35 --- 15 | 68 49 45 71 55 43 --- 53
R14M | 511 11 19 24 16 17 18 --- 8 | 47 44 65 56 40 49 --- 48
R15M | 1932 10 30 20 24 12 28 134 9 | 58 47 53 72 69 72 70 60
R16M | 2053 19 43 41 40 38 45 --- 16 | 43 43 59 61 50 79 --- 52
R17E | 710 8 24 12 25 12 22 --- 7 | 33 36 35 27 38 51 --- 35
R18E | 805 17 22 15 26 16 26 --- 9 | 32 32 37 48 35 31 --- 32
R19E | 2236 28 55 39 79 29 34 --- 20 | 33 41 58 68 54 37 --- 35
R20E | 3253 34 45 42 80 39 54 --- 21 | 64 63 87 109 88 94 --- 77
R21E | 1088 9 25 12 19 20 21 160 8 | 47 53 52 43 54 50 112 49
R22E | 1614 42 41 50 77 46 58 --- 23 | 62 52 90 98 79 77 --- 67
R24E | 1269 19 33 18 27 13 17 --- 9 | 61 63 60 63 53 70 --- 59
------+----------------------------------------------+------------------------------------------
RMS | 1686 21 32 31 38 25 33 158 |T 50 45 58 62 53 60 109 52
WRMS | 1686 15 29 24 27 18 33 158 |NE 53 44 62 64 43 64 129 54
MEDI | 1091 16 25 19 24 16 26 142 |MD 48 44 52 61 52 51 99 49
Table 3.2178.2 GPS week: 2178 Day: 2 MJD: 59492
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 473 45 36 41 12 25 24 --- 15 | 86 71 68 63 87 68 --- 70
R02 | 3028 10 23 13 16 12 35 141 8 | 53 41 49 59 60 73 74 53
R03M | 770 7 17 9 15 17 21 142 6 | 57 49 64 59 58 67 55 57
XR04M | 1205 14 11 7 --- 10 27 --- 7 | 64 57 64 --- 64 60 --- 61
R05M | 767 17 20 23 10 10 22 48 8 | 59 58 63 58 55 50 91 55
R07 | 1596 16 13 16 20 18 24 164 8 | 64 55 51 47 66 41 79 53
R08 | 795 19 28 10 34 14 36 --- 10 | 59 49 64 82 79 78 --- 66
R09 | 1900 22 9 12 19 26 29 --- 9 | 39 34 39 42 30 39 --- 34
R11 | 4566 18 27 20 12 14 57 --- 11 | 35 35 65 44 34 66 --- 41
R12M | 1707 13 21 17 19 28 14 --- 8 | 63 60 55 70 79 60 --- 63
R13M | 2585 26 24 36 35 44 30 --- 15 | 77 59 45 59 80 51 --- 59
R14M | 735 8 22 8 13 10 31 --- 7 | 59 54 60 55 57 66 --- 57
R15M | 1155 9 23 12 12 10 23 106 6 | 65 57 59 66 65 64 38 62
R16M | 2839 23 44 25 42 53 63 --- 18 | 53 51 62 72 54 96 --- 59
R17E | 1010 8 24 10 17 14 19 --- 6 | 41 48 40 45 40 45 --- 41
R18E | 886 14 18 13 28 14 28 --- 8 | 30 30 33 42 29 31 --- 29
R19E | 1730 29 75 37 79 62 38 --- 24 | 45 50 65 76 66 38 --- 44
R20E | 2871 24 49 37 55 47 37 --- 18 | 59 53 67 64 71 53 --- 55
R21E | 769 9 25 9 18 26 33 67 8 | 39 45 44 37 49 29 54 39
R22E | 965 68 42 42 73 59 82 --- 27 | 56 70 81 118 87 115 --- 67
R24E | 811 10 22 10 19 11 29 --- 7 | 103 106 107 109 100 116 --- 105
------+----------------------------------------------+------------------------------------------
RMS | 1910 24 32 23 34 31 37 119 |T 57 53 59 63 62 62 65 55
WRMS | 1910 17 26 18 19 23 37 119 |NE 56 47 56 56 59 60 76 52
MEDI | 1155 16 23 13 19 17 29 106 |MD 59 53 62 59 64 60 55 57
Table 3.2178.3 GPS week: 2178 Day: 3 MJD: 59493
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 997 42 24 61 31 32 33 --- 18 | 89 64 66 78 78 64 --- 68
R02 | 3361 7 25 11 14 12 30 174 7 | 54 39 56 59 48 67 38 52
XR03M | 855 6 --- 10 19 10 20 176 6 | 56 --- 49 47 56 62 50 52
XR04M | 1744 12 13 23 --- 16 25 --- 9 | 51 41 65 --- 41 49 --- 49
R05M | 870 16 29 22 26 18 37 85 10 | 51 41 74 79 46 78 72 58
R07 | 1170 8 21 15 14 12 21 209 6 | 64 45 56 71 59 73 43 60
R08 | 840 18 23 9 20 14 49 --- 10 | 54 45 61 77 60 95 --- 61
R09 | 2590 18 16 15 15 27 25 --- 8 | 40 34 43 47 35 35 --- 36
R11 | 4705 15 23 23 21 18 34 --- 10 | 38 53 52 48 31 55 --- 42
R12M | 1227 16 21 16 24 15 17 --- 8 | 89 73 79 98 93 98 --- 87
R13M | 2041 19 48 41 22 46 26 --- 15 | 76 63 55 74 80 87 --- 69
R14M | 1007 12 21 14 15 14 29 --- 7 | 88 78 83 81 86 90 --- 84
R15M | 1146 7 24 20 16 13 40 183 9 | 70 60 54 75 75 88 51 68
R16M | 3133 16 40 29 40 64 28 --- 16 | 69 48 63 74 89 66 --- 66
R17E | 1271 12 26 13 23 17 21 --- 8 | 37 39 39 37 37 39 --- 34
R18E | 1299 17 20 23 25 15 44 --- 10 | 36 34 47 36 33 31 --- 33
R19E | 678 20 63 40 73 45 54 --- 21 | 29 53 53 75 58 64 --- 37
R20E | 2257 33 70 33 42 49 40 --- 19 | 54 48 68 71 62 57 --- 51
R21E | 726 7 27 9 34 13 28 120 9 | 30 31 32 40 38 36 42 31
R22E | 1389 41 27 31 75 66 44 --- 22 | 59 62 73 86 90 69 --- 62
R24E | 787 10 26 10 31 13 18 --- 8 | 59 54 54 66 63 62 --- 58
------+----------------------------------------------+------------------------------------------
RMS | 1970 20 33 26 34 32 34 160 |T 56 50 58 65 59 65 49 55
WRMS | 1970 17 27 22 19 27 34 160 |NE 56 46 55 63 51 64 40 53
MEDI | 1227 16 24 20 23 16 29 174 |MD 54 48 56 71 59 64 43 58
Table 3.2178.4 GPS week: 2178 Day: 4 MJD: 59494
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1677 27 39 66 19 37 19 --- 17 | 79 81 62 73 97 62 --- 70
R02 | 2766 11 15 15 14 14 25 246 7 | 50 37 38 34 51 50 35 42
R03M | 989 8 17 12 11 22 43 237 8 | 54 42 55 55 56 45 88 48
XR04M | 1853 14 13 13 --- 12 47 --- 11 | 55 42 54 --- 43 40 --- 46
R05M | 1061 16 17 36 17 38 21 69 11 | 60 52 93 69 40 66 58 63
R07 | 692 11 17 16 13 19 42 228 9 | 63 59 52 60 69 89 48 62
R08 | 775 11 17 17 19 18 19 --- 7 | 57 49 52 61 66 68 --- 57
R09 | 1779 25 14 13 18 26 33 --- 10 | 44 35 36 38 24 44 --- 33
XR11 | 4201 14 --- 15 12 25 32 --- 9 | 28 --- 39 29 29 58 --- 31
R12M | 558 11 36 20 19 15 40 --- 10 | 316 318 310 322 317 334 --- 318
R13M | 3370 25 47 24 29 46 29 --- 14 | 249 249 230 249 248 248 --- 244
R14M | 1777 9 20 14 21 20 21 --- 7 | 384 383 374 392 389 381 --- 383
R15M | 1407 7 24 18 17 13 27 142 7 | 181 181 184 183 178 165 153 180
R16M | 2245 23 38 38 30 49 40 --- 15 | 67 53 67 82 72 64 --- 65
R17E | 1072 9 19 16 17 11 32 --- 8 | 43 43 38 43 41 48 --- 41
R18E | 1514 20 27 15 26 29 23 --- 10 | 45 50 49 52 59 45 --- 46
R19E | 1280 25 56 38 54 57 37 --- 19 | 36 62 61 70 75 72 --- 49
R20E | 820 37 90 35 41 42 50 --- 22 | 66 104 77 76 71 61 --- 63
R21E | 658 8 32 11 33 13 25 153 9 | 56 58 56 46 54 60 60 54
R22E | 961 31 31 38 74 101 47 --- 25 | 60 63 71 72 95 62 --- 59
R24E | 965 14 28 13 28 18 27 --- 9 | 81 74 83 85 80 96 --- 81
------+----------------------------------------------+------------------------------------------
RMS | 1568 19 36 27 30 37 33 190 |T 98 101 99 104 102 102 73 96
WRMS | 1568 15 28 19 21 26 33 190 |NE 53 52 46 49 56 61 41 49
MEDI | 1280 14 24 16 19 22 32 153 |MD 60 58 61 69 69 62 58 59
Table 3.2178.5 GPS week: 2178 Day: 5 MJD: 59495
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 683 23 40 42 37 32 36 --- 15 | 64 73 44 54 81 49 --- 56
R02 | 982 6 21 8 10 10 39 430 7 | 42 33 39 37 38 64 148 40
R03M | 955 7 14 16 13 30 40 423 9 | 42 34 41 44 63 33 196 39
XR04M | 2244 19 10 17 --- 17 43 --- 11 | 50 40 40 --- 36 26 --- 39
R05M | 2011 13 19 19 12 14 29 142 8 | 47 38 50 39 44 35 78 41
R07 | 743 8 12 9 22 11 21 222 6 | 62 58 60 67 57 69 63 60
R08 | 1475 12 20 21 14 22 38 --- 9 | 51 48 43 57 68 68 --- 52
R09 | 1797 18 17 12 30 32 26 --- 9 | 38 32 37 41 27 51 --- 33
R11 | 5198 13 13 22 15 26 46 --- 10 | 18 23 34 38 35 54 --- 23
R12M | 791 9 33 18 17 16 30 --- 9 | 621 615 627 630 623 627 --- 624
R13M | 1576 24 58 44 30 45 56 --- 18 | 500 500 507 500 500 496 --- 501
R14M | 680 9 17 17 18 11 20 --- 6 | 789 795 793 798 795 789 --- 793
R15M | 756 9 19 14 21 14 27 107 7 | 356 357 352 360 361 371 340 358
R16M | 1546 17 39 25 41 38 33 --- 13 | 49 52 60 54 63 70 --- 52
R17E | 1246 8 19 13 19 13 27 --- 7 | 53 55 56 59 56 51 --- 53
R18E | 1880 17 31 8 27 34 22 --- 10 | 39 36 38 45 55 45 --- 37
R19E | 990 35 40 30 58 86 47 --- 21 | 32 35 50 75 92 52 --- 42
R20E | 1561 31 60 32 56 48 25 --- 18 | 65 69 67 65 72 71 --- 58
R21E | 578 12 33 12 39 16 19 174 10 | 43 44 50 48 51 43 80 44
R22E | 2182 38 42 31 55 115 57 --- 25 | 63 61 72 80 108 74 --- 64
R24E | 1911 14 24 11 40 24 17 --- 9 | 101 96 97 101 89 102 --- 97
------+----------------------------------------------+------------------------------------------
RMS | 1777 18 32 23 32 41 35 281 |T 148 147 150 159 157 154 150 147
WRMS | 1777 13 30 18 26 26 35 281 |NE 45 44 42 49 51 59 105 44
MEDI | 1475 13 21 17 22 24 30 174 |MD 51 52 50 57 63 64 80 52
Table 3.2178.6 GPS week: 2178 Day: 6 MJD: 59496
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 678 34 28 45 13 13 23 --- 13 | 105 94 61 91 93 95 --- 87
R02 | 1231 7 18 18 11 10 49 149 8 | 58 48 57 55 58 92 144 58
R03M | 1222 8 13 12 12 8 46 169 7 | 60 43 54 52 65 83 212 57
XR04M | 2059 18 12 14 --- 14 42 --- 10 | 127 121 128 --- 123 122 --- 124
R05M | 2068 21 21 21 15 16 24 144 8 | 66 55 58 54 64 51 85 57
R07 | 590 14 16 13 18 16 41 263 8 | 75 67 81 82 73 104 88 78
R08 | 1175 19 20 15 25 18 56 --- 11 | 66 63 67 89 75 108 --- 74
R09 | 1428 12 15 9 21 21 28 --- 7 | 43 52 44 41 32 57 --- 41
R11 | 3215 15 17 14 11 12 11 --- 6 | 23 26 39 31 40 41 --- 29
R12M | 855 13 33 17 30 17 23 --- 9 | 997 9999 995 9999 993 998 --- 997
R13M | 1210 22 63 39 27 32 63 --- 17 | 774 758 766 765 772 767 --- 767
R14M | 570 12 32 16 9 14 36 --- 8 | 9999 9999 9999 9999 9999 9999 --- 9999
R15M | 1091 13 29 18 25 19 28 166 9 | 605 597 603 604 604 602 593 603
R16M | 3064 21 62 14 27 54 22 --- 15 | 99 97 101 102 103 106 --- 98
R17E | 874 7 26 14 14 12 24 --- 7 | 63 72 61 62 62 58 --- 62
R18E | 1547 19 32 11 27 25 20 --- 9 | 50 57 51 54 48 54 --- 48
XR19E | 1392 52 --- 46 57 92 50 --- 30 | 50 --- 50 95 126 100 --- 67
R20E | 1212 35 46 27 49 40 35 --- 17 | 111 109 92 100 115 106 --- 101
R21E | 688 13 35 14 29 15 26 186 9 | 58 61 61 53 58 59 207 56
R22E | 3422 52 56 28 88 55 59 --- 25 | 113 57 76 71 112 65 --- 78
R24E | 1045 13 31 9 30 19 21 --- 9 | 118 118 116 118 119 115 --- 117
------+----------------------------------------------+------------------------------------------
RMS | 1668 21 35 21 31 25 36 184 |T 183 138 178 139 186 189 221 179
WRMS | 1668 16 34 18 19 19 36 184 |NE 61 58 58 64 61 82 116 61
MEDI | 1212 15 28 15 25 17 28 166 |MD 66 63 61 71 75 95 144 74
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