[IGSREPORT-27943] Wk 2156 IGLOS Final Orbits
acc
acc at igs.org
Fri May 21 06:19:27 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2156 (May 02, 2021 - May 08, 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 2.2156.
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:
igl2156[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2156 in the SP3 format.
igl21567.sum Combination Report for GPS Week 2156.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -1.1 ns
1 | -6.2 ns
2 | -5.0 ns
3 | -7.6 ns
4 | -5.9 ns
5 | -4.6 ns
6 | -6.7 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 1.2156, 1a.2156).
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 2.2156.0-6)
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 3.2156.0-6).
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 2156 summary. (May 02, 2021 - May 08, 2021)
Table 1.2156.a GPS week : 2156 MJD: 59336.0-59342.0
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 -3 8 -30 7 .26 28 21 | -5418 -1346 3342 8226
| 1 1 1 22 27 29 .05 | 3346 2046
emx n/a| -1 1 10 -17 -13 -15 -.03 33 27 | -7264 -286 3334 8643
| 0 1 1 24 14 39 .05 | 10116 1475
esx n/a| 1 0 2 14 5 -69 -.02 30 21 | -3382 -894 3334 7775
| 1 2 1 12 18 39 .04 | 9450 1659
gfz n/a| 1 0 1 -18 -10 -30 -.12 36 17 | 0 -1539 3373 7919
| 1 2 1 33 17 21 .06 | 0 2068
grg n/a| 1 0 -9 -1 43 -38 .30 32 23 | -4510 -1697 3393 7830
| 1 0 3 35 27 49 .10 | 2081 2114
iac n/a| 0 -2 -1 5 -3 118 -.31 26 23 | -3319 -505 3335 8656
| 2 1 2 31 20 42 .11 | 1946 1646
mcc n/a| 0 0 -23 -16 -125 -492 -.25 180 180 | --- --- --- ---
| 7 6 8 71 97 287 .26 | --- ---
Table 1.2156.b GPS week : 2156 MJD: 59336.0-59342.0
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 19 13 11 13 13 12 |
R02 | 7 7 6 6 6 10 8 |
R03 | 6 6 6 5 6 8 7 |
R04 | 7 9 8 7 8 10 8 |
R05 | 10 8 9 8 10 11 8 |
R07 | 9 8 6 7 7 6 8 |
R08 | 8 9 6 7 9 8 7 |
R09 | 16 14 17 16 15 14 15 |
R11 | 9 11 8 11 9 10 11 |
R12 | 12 12 10 10 9 8 10 |
R13 | 17 20 19 18 18 18 15 |
R14 | 8 9 8 7 6 8 7 |
R15 | 8 9 10 7 8 9 8 |
R16 | 13 12 13 11 14 14 12 |
R17 | 9 14 9 9 8 8 9 |
R18 | 10 13 9 9 7 8 8 |
R19 | 22 16 17 23 29 25 25 |
R20 | 23 22 23 25 23 25 23 |
R21 | 10 12 11 10 10 9 10 |
R22 | 24 26 24 29 28 31 28 |
R24 | 9 9 8 11 10 10 9 |
Table 1.2156.c GPS week : 2156 MJD: 59336.0-59342.0
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 2156 0 | -51 -33 199 593 -1738 6657 81.6 1419 1419 | -1089 0
brd 2156 1 | -48 0 157 152 -470 7254 84.2 1449 1449 | -6234 0
brd 2156 2 | -26 -17 104 -707 852 -22 81.0 1493 1493 | -4986 0
brd 2156 3 | -64 19 119 -1505 -1827 2661 83.4 1559 1559 | -7573 0
brd 2156 4 | 82 -26 172 267 -64 -1218 81.0 1646 1646 | -5861 0
brd 2156 5 | 14 75 196 -2313 -36 -3380 81.9 1615 1615 | -4594 0
brd 2156 6 | 41 -26 189 -1891 768 -2959 82.2 1524 1524 | -6688 0
-------------+------------------------------------------------------------+----------------
brd 2156 mean| -7 -1 162 -771 -359 1284 82.2 1529 1529 | -5289 0
brd 2156 sdev| 54 38 37 1152 1080 4361 1.2 83 83 | 2105 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 2.2156.0 GPS week: 2156 Day: 0 MJD: 59336
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 -4 -18 -53 42 .21 25 20 | 1564 -2209 3305 8953
emx n/a| -2 3 8 -10 3 6 -.05 29 24 | 3420 -616 3302 9329
esx n/a| 0 -1 2 2 22 -37 -.07 29 20 | 1155 -1704 3303 8150
gfz n/a| -1 0 0 -38 -5 -18 -.10 35 17 | 0 -2769 3354 8600
grg n/a| 1 0 -8 14 17 -83 .38 30 23 | 73 -2695 3368 8500
iac n/a| 3 -4 0 30 9 114 -.42 32 29 | 287 -1168 3281 9366
mcc n/a| -2 7 -29 -86 -120 -411 .05 239 239 | --- --- --- ---
Table 2.2156.1 GPS week: 2156 Day: 1 MJD: 59337
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 -2 19 -34 35 .24 27 22 | -5999 -642 3401 7874
emx n/a| -1 -1 10 -4 5 17 -.04 30 26 | -4357 -511 3388 8405
esx n/a| 0 0 1 1 14 -15 .03 29 19 | 1139 -32 3379 5969
gfz n/a| 0 0 0 -65 7 -52 -.09 40 18 | 0 -1134 3438 7600
grg n/a| 2 0 -4 39 20 -65 .33 29 21 | -5479 -1284 3379 7459
iac n/a| -3 -1 -3 -32 -25 74 -.47 31 29 | -5799 1820 3392 8392
mcc n/a| 9 0 -27 -99 -170 -435 -.22 171 171 | --- --- --- ---
Table 2.2156.2 GPS week: 2156 Day: 2 MJD: 59338
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| -4 1 -4 0 -10 17 .30 27 21 | -5042 1872 3387 8283
emx n/a| 0 1 9 -44 -26 -74 -.00 31 27 | -17336 2270 3404 8719
esx n/a| 3 -4 0 15 6 -124 .02 29 22 | -21854 1660 3385 10163
gfz n/a| 0 -3 1 -41 5 -50 -.16 31 16 | 0 2042 3440 8202
grg n/a| 0 1 -8 24 27 -2 .24 30 19 | -5784 1615 3612 7990
iac n/a| -2 -1 1 -4 -16 187 -.36 23 20 | -2395 -371 3394 8656
mcc n/a| 10 -10 -20 62 -218 -167 -.13 214 214 | --- --- --- ---
Table 2.2156.3 GPS week: 2156 Day: 3 MJD: 59339
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 0 -2 -13 12 -35 .28 28 18 | -5155 -3595 3227 8135
emx n/a| -1 1 11 12 -28 27 .03 33 25 | -13018 -838 3212 8581
esx n/a| 3 0 2 6 -27 -37 -.05 30 21 | 8570 -2797 3218 7577
gfz n/a| 2 -1 0 -11 -29 -8 -.10 33 15 | 0 -2992 3248 7962
grg n/a| 0 0 -12 -29 30 10 .14 35 27 | -5779 -3845 3281 7792
iac n/a| 0 -3 0 27 30 65 -.21 25 19 | -4468 -1898 3220 8477
mcc n/a| -4 7 -7 -46 -111 -305 -.48 127 127 | --- --- --- ---
Table 2.2156.4 GPS week: 2156 Day: 4 MJD: 59340
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 -1 8 -70 22 .20 30 22 | -6902 -1357 3088 7963
emx n/a| 0 2 10 -36 -3 4 -.08 39 28 | 2843 -539 3067 8418
esx n/a| 1 3 3 16 7 -82 -.02 30 20 | -6236 -259 3080 7754
gfz n/a| 2 0 1 -14 6 -13 -.03 30 15 | 0 -1602 3073 7706
grg n/a| 1 0 -10 8 44 23 .28 34 26 | -5381 -1143 3091 7439
iac n/a| 0 -3 -4 54 5 100 -.28 29 23 | -4487 733 3078 8443
mcc n/a| -8 0 -20 62 -244 -1048 -.00 182 182 | --- --- --- ---
Table 2.2156.5 GPS week: 2156 Day: 5 MJD: 59341
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 -4 50 -40 -10 .33 30 21 | -7845 275 3270 8537
emx n/a| -2 2 9 -44 -22 -42 -.09 33 27 | -21779 741 3260 8834
esx n/a| 3 0 4 26 23 -97 -.02 33 21 | -2085 -212 3252 8556
gfz n/a| 2 1 4 28 -26 -15 -.18 40 18 | 0 -125 3285 7990
grg n/a| 4 0 -13 0 84 -45 .46 34 25 | -4742 -132 3305 8171
iac n/a| 0 -2 -1 -23 -20 138 -.25 23 23 | -3161 343 3260 8968
mcc n/a| -5 -2 -24 45 -43 -664 -.29 144 144 | --- --- --- ---
Table 2.2156.6 GPS week: 2156 Day: 6 MJD: 59342
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 11 -19 -19 .24 29 22 | -8551 -3766 3717 7843
emx n/a| -1 1 10 8 -24 -50 .04 35 29 | -626 -2510 3705 8218
esx n/a| 1 0 5 35 -6 -93 -.04 31 21 | -4364 -2920 3721 6261
gfz n/a| 2 4 1 18 -30 -57 -.20 40 17 | 0 -4194 3779 7378
grg n/a| 1 -1 -10 -66 80 -105 .29 32 22 | -4481 -4401 3715 7464
iac n/a| 0 -2 0 -9 -3 146 -.19 20 18 | -3211 -2997 3726 8295
mcc n/a| 1 -5 -36 -55 33 -419 -.69 185 185 | --- --- --- ---
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 3.2156.0 GPS week: 2156 Day: 0 MJD: 59336
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 | 967 37 37 42 46 26 39 --- 17 | 60 62 66 68 51 61 --- 56
R02 | 1181 13 11 17 12 14 26 234 7 | 39 43 46 44 39 59 231 43
R03 | 1554 8 14 12 11 18 13 99 5 | 45 40 43 46 48 40 41 42
XR04 | 1048 14 8 19 --- 11 15 --- 7 | 46 44 37 --- 38 38 --- 38
R05 | 1788 16 14 28 30 18 19 98 9 | 31 39 51 49 30 35 47 33
R07 | 1036 7 8 17 13 29 33 190 8 | 51 55 49 61 44 62 177 51
R08 | 702 16 13 17 18 18 22 --- 7 | 51 55 56 62 50 61 --- 54
R09 | 3007 18 32 17 21 57 51 --- 15 | 89 103 95 94 43 111 --- 86
XR11 | 2554 17 19 13 11 --- 26 --- 9 | 39 41 41 42 --- 39 --- 38
R12 | 1404 22 35 23 24 20 35 --- 12 | 105 88 96 101 95 106 --- 96
R13 | 1382 51 38 45 29 22 22 --- 17 | 97 64 63 78 75 64 --- 67
R14 | 1293 11 18 17 15 17 21 --- 7 | 63 48 68 64 59 49 --- 56
R15 | 706 16 21 14 16 15 19 233 7 | 79 52 61 72 73 72 126 67
R16 | 2151 14 28 20 43 40 21 --- 13 | 70 60 80 71 88 73 --- 71
R17E | 894 21 25 11 27 15 17 --- 9 | 78 67 65 75 70 75 --- 70
R18E | 1092 12 22 16 20 24 29 --- 9 | 51 47 49 58 59 51 --- 50
R19E | 1076 31 43 45 86 33 39 --- 21 | 39 72 77 103 55 39 --- 54
R20E | 1257 44 50 63 58 34 46 --- 22 | 51 58 83 73 64 62 --- 53
R21E | 889 23 27 23 23 15 17 422 10 | 78 63 65 79 71 76 137 70
R22E | 1404 41 51 41 55 66 62 --- 23 | 75 87 102 99 106 114 --- 87
R24E | 1235 18 21 12 15 19 33 --- 9 | 52 48 46 46 55 51 --- 47
------+----------------------------------------------+------------------------------------------
RMS | 1419 25 29 29 35 30 32 239 |T 61 58 63 69 60 63 126 58
WRMS | 1419 20 24 20 17 23 29 239 |NE 61 56 60 65 56 62 124 57
MEDI | 1235 17 22 17 21 19 26 190 |MD 52 55 63 68 55 61 126 54
Table 3.2156.1 GPS week: 2156 Day: 1 MJD: 59337
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 | 1329 42 31 59 36 35 32 --- 18 | 35 42 57 44 40 37 --- 32
R02 | 1725 13 9 12 13 13 24 286 6 | 26 27 32 30 25 34 122 24
R03 | 1021 7 11 12 21 12 14 83 5 | 25 28 26 32 27 22 30 22
XR04 | 700 13 15 19 --- 23 19 --- 9 | 27 27 21 --- 19 30 --- 21
R05 | 1170 12 19 24 20 17 14 66 8 | 24 28 40 24 15 21 63 21
R07 | 1375 12 12 10 14 25 26 139 8 | 28 29 30 26 21 38 76 24
R08 | 675 15 11 16 24 22 23 --- 8 | 30 34 35 30 24 37 --- 29
R09 | 2580 22 16 20 21 48 37 --- 13 | 78 78 88 92 33 83 --- 72
XR11 | 1943 18 23 14 20 --- 30 --- 11 | 33 41 39 36 --- 36 --- 33
R12 | 1133 23 36 23 10 13 42 --- 12 | 93 86 84 92 82 88 --- 84
R13 | 2391 42 52 38 52 45 32 --- 19 | 77 68 64 93 84 60 --- 66
R14 | 1086 12 19 17 26 17 22 --- 8 | 45 37 50 57 54 39 --- 44
R15 | 732 17 26 13 29 18 21 155 9 | 62 49 54 72 61 61 58 57
R16 | 1484 24 17 30 39 25 21 --- 11 | 56 56 67 57 58 62 --- 57
R17E | 1918 31 19 13 68 14 25 --- 14 | 66 60 60 83 62 69 --- 60
R18E | 1328 14 21 17 22 32 51 --- 12 | 63 64 68 68 82 76 --- 66
R19E | 1119 36 39 29 42 40 32 --- 16 | 48 56 42 58 65 46 --- 44
R20E | 927 51 67 51 50 27 38 --- 22 | 63 71 67 68 61 53 --- 56
R21E | 978 19 43 22 38 15 19 195 12 | 165 148 153 169 159 168 174 159
R22E | 1833 46 32 49 96 61 53 --- 25 | 90 97 122 103 110 143 --- 106
R24E | 954 23 21 14 18 13 22 --- 8 | 48 41 43 48 53 47 --- 44
------+----------------------------------------------+------------------------------------------
RMS | 1448 27 30 29 40 29 31 170 |T 56 55 59 64 56 59 87 53
WRMS | 1448 22 26 19 18 21 29 170 |NE 45 45 49 52 41 46 69 41
MEDI | 1170 19 21 19 24 22 25 139 |MD 48 49 54 57 54 47 63 44
Table 3.2156.2 GPS week: 2156 Day: 2 MJD: 59338
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 | 1787 36 20 31 33 27 15 --- 12 | 46 50 47 50 48 44 --- 43
R02 | 1994 7 13 14 10 13 16 466 5 | 30 36 33 41 35 40 304 34
R03 | 622 11 11 16 16 9 14 90 6 | 30 30 43 39 35 27 50 31
XR04 | 916 11 12 14 --- 23 15 --- 8 | 33 30 28 --- 19 35 --- 27
R05 | 932 22 22 21 26 14 12 73 9 | 25 33 44 53 24 29 90 30
R07 | 1366 12 14 15 12 10 15 114 6 | 36 35 36 39 41 35 88 35
R08 | 1051 11 10 18 16 17 11 --- 6 | 35 33 41 33 32 32 --- 33
R09 | 2312 35 27 16 35 69 24 --- 17 | 88 86 72 90 31 77 --- 67
XR11 | 2187 16 17 17 14 --- 15 --- 8 | 19 30 24 24 --- 21 --- 21
R12 | 965 22 30 26 16 15 24 --- 10 | 66 44 39 56 67 53 --- 52
R13 | 1541 30 58 50 49 23 31 --- 18 | 68 36 34 79 59 57 --- 49
R14 | 1761 13 26 19 14 16 15 --- 8 | 39 30 42 30 46 41 --- 35
R15 | 1149 23 27 10 24 14 24 109 9 | 55 38 40 55 47 34 47 41
R16 | 1066 26 19 38 32 28 25 --- 13 | 51 47 65 52 54 50 --- 47
R17E | 1430 22 29 20 12 16 18 --- 9 | 60 42 44 53 58 52 --- 50
R18E | 804 15 20 14 13 23 29 --- 9 | 60 54 59 54 60 64 --- 57
R19E | 1233 29 59 39 40 29 31 --- 17 | 75 89 88 102 96 79 --- 82
R20E | 1023 55 52 60 62 26 40 --- 22 | 66 77 75 86 68 65 --- 63
R21E | 1094 14 32 26 17 18 26 134 10 | 135 117 131 134 136 148 155 133
R22E | 3094 51 37 41 63 77 33 --- 23 | 66 92 97 92 121 93 --- 87
R24E | 821 17 24 13 19 19 16 --- 8 | 60 54 59 60 67 67 --- 59
------+----------------------------------------------+------------------------------------------
RMS | 1492 27 31 29 31 30 23 214 |T 54 51 54 61 57 54 122 51
WRMS | 1492 21 27 22 16 19 20 214 |NE 44 39 42 49 41 41 115 38
MEDI | 1149 22 24 19 17 18 18 109 |MD 55 42 44 53 48 50 88 47
Table 3.2156.3 GPS week: 2156 Day: 3 MJD: 59339
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 | 1299 29 17 21 27 27 16 --- 10 | 48 47 55 59 44 48 --- 48
R02 | 1653 10 15 11 12 15 15 --- 6 | 36 33 33 30 31 40 --- 33
R03 | 977 6 13 12 8 14 11 93 5 | 37 37 35 34 39 41 61 36
XR04 | 1210 11 16 11 --- 11 17 --- 7 | 31 34 30 --- 26 26 --- 26
R05 | 1381 22 19 20 14 12 18 95 8 | 22 34 40 37 29 36 124 28
R07 | 1221 7 12 11 22 18 16 149 6 | 45 47 47 56 39 54 172 46
R08 | 918 11 13 11 17 10 24 --- 7 | 39 38 46 48 37 53 --- 42
R09 | 2549 36 28 26 27 66 25 --- 16 | 92 78 83 83 23 68 --- 68
XR11 | 2336 20 17 18 29 --- 23 --- 11 | 27 26 26 35 --- 32 --- 24
R12 | 1185 20 30 18 20 32 18 --- 10 | 71 45 51 76 67 68 --- 61
R13 | 784 36 47 52 38 35 21 --- 17 | 73 37 24 67 61 60 --- 46
R14 | 2415 12 19 14 12 15 19 --- 7 | 50 28 44 36 50 49 --- 41
R15 | 1854 20 22 11 9 15 17 160 7 | 54 29 39 36 46 42 76 40
R16 | 945 16 20 30 28 23 21 --- 10 | 40 38 57 37 58 51 --- 43
R17E | 1224 24 26 16 19 16 17 --- 9 | 60 41 45 62 58 50 --- 51
R18E | 700 12 27 9 23 32 14 --- 9 | 46 41 48 52 66 48 --- 46
R19E | 1216 35 82 34 50 48 53 --- 23 | 122 119 133 170 131 107 --- 124
R20E | 1986 63 59 56 60 44 46 --- 24 | 135 135 144 148 121 129 --- 130
R21E | 714 22 32 19 12 22 20 123 9 | 88 61 67 85 86 79 81 76
R22E | 3075 49 35 77 85 88 36 --- 28 | 71 74 124 84 112 88 --- 83
R24E | 713 22 32 18 15 24 27 --- 10 | 89 86 82 81 94 83 --- 83
------+----------------------------------------------+------------------------------------------
RMS | 1559 28 33 30 33 35 25 127 |T 60 52 59 65 60 59 102 55
WRMS | 1559 18 25 21 15 27 19 127 |NE 47 39 43 48 42 47 108 41
MEDI | 1221 20 22 18 20 22 19 123 |MD 50 41 47 56 50 51 81 46
Table 3.2156.4 GPS week: 2156 Day: 4 MJD: 59340
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 | 658 37 32 23 28 32 19 --- 13 | 36 42 39 39 22 36 --- 31
R02 | 2701 8 14 12 7 15 22 273 6 | 30 30 35 29 29 42 276 30
R03 | 588 11 12 10 13 11 19 133 6 | 33 34 34 33 26 40 111 31
XR04 | 883 17 22 14 --- 17 11 --- 8 | 27 27 21 --- 23 20 --- 20
R05 | 918 26 25 28 18 14 20 225 10 | 20 27 51 39 38 32 168 29
R07 | 1612 11 15 13 18 14 15 215 6 | 31 34 42 44 29 31 117 33
R08 | 704 18 15 20 22 15 23 --- 8 | 30 31 40 43 29 36 --- 32
R09 | 2564 36 25 21 17 62 28 --- 15 | 96 86 78 78 23 85 --- 72
XR11 | 2956 18 18 12 15 --- 25 --- 9 | 26 31 32 34 --- 38 --- 29
R12 | 1132 17 28 12 23 24 18 --- 9 | 68 61 57 71 61 59 --- 60
R13 | 1666 34 61 41 45 25 23 --- 17 | 69 45 38 79 61 44 --- 49
R14 | 2203 15 18 9 10 14 15 --- 6 | 45 29 37 32 43 40 --- 36
R15 | 1803 9 28 12 13 14 22 53 7 | 51 31 41 50 50 60 79 46
R16 | 828 22 28 18 39 39 38 --- 14 | 42 50 71 67 79 76 --- 58
R17E | 1801 22 21 12 15 20 13 --- 7 | 54 34 37 46 46 44 --- 42
R18E | 684 11 24 11 8 13 15 --- 6 | 50 52 57 62 54 56 --- 54
R19E | 1371 52 112 42 53 60 67 --- 29 | 70 84 71 98 99 114 --- 79
R20E | 1768 55 56 60 51 33 50 --- 23 | 97 87 78 98 95 96 --- 84
R21E | 1032 23 26 21 10 19 33 79 10 | 68 50 52 56 56 72 93 57
R22E | 3108 60 38 76 71 81 20 --- 28 | 40 65 99 65 76 69 --- 60
R24E | 742 13 28 15 11 35 21 --- 9 | 71 67 67 69 88 82 --- 71
------+----------------------------------------------+------------------------------------------
RMS | 1645 30 39 30 30 34 29 182 |T 50 47 51 56 51 55 140 47
WRMS | 1645 22 28 20 15 26 23 182 |NE 43 39 44 49 39 45 150 39
MEDI | 1371 18 25 15 17 19 21 133 |MD 45 42 42 50 46 44 111 46
Table 3.2156.5 GPS week: 2156 Day: 5 MJD: 59341
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 | 533 36 25 22 28 38 23 --- 13 | 29 36 50 57 26 38 --- 32
R02 | 3480 14 21 12 24 15 33 138 9 | 25 22 40 40 26 56 92 33
R03 | 799 10 13 14 13 20 23 105 7 | 24 19 21 26 21 35 40 21
XR04 | 732 14 21 14 --- 27 16 --- 9 | 19 24 21 --- 16 27 --- 17
R05 | 584 13 20 35 27 23 21 177 10 | 17 15 42 29 29 23 98 14
R07 | 1352 8 7 10 7 18 21 242 6 | 26 22 24 24 18 31 83 22
R08 | 742 22 9 13 17 18 23 --- 8 | 25 20 26 31 28 24 --- 20
R09 | 2932 30 22 18 23 59 24 --- 14 | 83 58 70 77 41 69 --- 61
XR11 | 2496 17 16 13 27 --- 25 --- 10 | 29 30 27 30 --- 38 --- 28
R12 | 1063 16 24 10 17 17 17 --- 8 | 58 56 55 62 60 52 --- 55
R13 | 2431 41 42 52 41 22 30 --- 17 | 63 46 56 62 65 43 --- 47
R14 | 1216 17 19 12 20 17 14 --- 7 | 44 32 40 32 48 39 --- 36
R15 | 1209 16 22 18 17 16 21 54 8 | 51 37 35 39 52 53 74 43
R16 | 611 25 20 23 55 38 20 --- 13 | 38 41 53 45 55 55 --- 43
R17E | 2243 17 23 15 13 17 16 --- 7 | 43 34 36 44 52 46 --- 40
R18E | 1152 15 19 15 24 21 13 --- 8 | 36 21 35 31 37 33 --- 29
R19E | 1922 31 74 33 85 51 45 --- 24 | 48 49 50 81 46 40 --- 39
R20E | 919 64 55 64 72 39 31 --- 24 | 59 47 65 75 49 37 --- 41
R21E | 956 27 25 20 22 13 13 45 9 | 72 59 54 72 63 59 119 61
R22E | 1197 65 59 87 91 84 18 --- 30 | 41 54 81 63 44 40 --- 37
R24E | 1268 18 38 19 16 16 11 --- 9 | 58 50 58 57 70 49 --- 55
------+----------------------------------------------+------------------------------------------
RMS | 1615 30 33 33 40 34 23 144 |T 42 36 44 48 42 42 84 36
WRMS | 1615 21 27 21 18 25 23 144 |NE 37 32 40 42 37 41 77 33
MEDI | 1197 17 22 18 23 20 21 105 |MD 41 36 42 44 44 40 83 37
Table 3.2156.6 GPS week: 2156 Day: 6 MJD: 59342
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 | 1204 29 30 33 27 32 16 --- 12 | 52 57 68 71 39 46 --- 51
R02 | 2295 11 14 17 22 16 21 243 8 | 36 37 47 46 41 50 232 41
R03 | 550 12 15 18 16 12 16 91 7 | 40 41 51 45 41 45 51 42
XR04 | 559 10 15 19 --- 15 15 --- 7 | 36 38 31 --- 29 38 --- 33
R05 | 888 17 22 17 21 12 11 138 7 | 24 36 39 36 33 29 49 28
R07 | 901 10 8 22 14 15 23 330 8 | 45 47 41 45 36 55 158 44
R08 | 833 17 17 12 17 14 15 --- 7 | 42 46 47 51 46 53 --- 46
R09 | 3764 21 26 18 31 65 27 --- 15 | 85 79 80 87 30 81 --- 71
XR11 | 2148 22 21 9 25 --- 23 --- 10 | 37 36 33 45 --- 50 --- 38
R12 | 951 16 30 12 15 27 27 --- 10 | 91 80 81 91 81 86 --- 82
R13 | 1695 30 52 35 29 36 24 --- 15 | 88 69 63 76 70 67 --- 65
R14 | 1223 12 20 15 21 22 10 --- 7 | 58 48 50 57 62 50 --- 51
R15 | 1257 17 25 17 13 26 11 66 8 | 70 56 58 69 73 69 87 63
R16 | 1198 15 18 26 45 34 15 --- 11 | 56 59 73 62 85 67 --- 63
R17E | 2033 24 23 20 16 21 13 --- 8 | 76 54 52 65 72 65 --- 62
R18E | 1410 11 23 17 11 23 16 --- 7 | 55 47 61 53 65 52 --- 52
R19E | 1255 33 76 43 105 41 34 --- 25 | 74 56 65 123 76 70 --- 66
R20E | 585 76 61 55 51 35 26 --- 23 | 86 75 69 81 78 70 --- 64
R21E | 754 27 26 22 25 15 14 73 9 | 89 64 65 84 82 75 134 74
R22E | 1029 58 59 78 93 69 25 --- 28 | 53 81 102 67 75 75 --- 64
R24E | 1630 25 33 14 16 17 13 --- 9 | 69 60 63 66 79 65 --- 65
------+----------------------------------------------+------------------------------------------
RMS | 1523 29 35 31 40 32 20 185 |T 60 55 59 66 59 59 118 55
WRMS | 1523 22 29 21 17 22 18 185 |NE 54 52 54 60 51 56 115 51
MEDI | 1204 17 23 18 21 22 16 91 |MD 56 56 61 65 65 65 87 62
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