[IGSREPORT-28112] Wk 2168 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 13 01:57:33 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2168 (Jul 25, 2021 - Jul 31, 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 2.2168.
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:
igl2168[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2168 in the SP3 format.
igl21687.sum Combination Report for GPS Week 2168.
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 | 1.0 ns
1 | -1.6 ns
2 | 0.8 ns
3 | 0.6 ns
4 | 0.3 ns
5 | -2.5 ns
6 | 1.8 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 1.2168, 1a.2168).
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 2.2168.0-6)
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 3.2168.0-6).
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 2168 summary. (Jul 25, 2021 - Jul 31, 2021)
Table 1.2168.a GPS week : 2168 MJD: 59420.0-59426.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 2 -3 -24 -31 .15 24 20 | 13965 198 3428 8579
| 1 0 2 20 8 18 .03 | 1344 3191
emx n/a| -3 0 -6 1 -12 -44 -.07 42 30 | -9051 130 3475 9150
| 1 2 3 33 33 12 .07 | 8309 2050
esx n/a| 0 0 0 16 -1 -6 -.08 31 26 | -759 905 3423 9425
| 1 1 2 17 10 43 .03 | 7524 2939
gfz n/a| 0 1 1 -1 -10 25 -.07 24 17 | 0 -63 3455 8212
| 1 0 2 20 18 26 .05 | 0 3058
grg n/a| 3 1 5 -1 28 -132 .34 33 27 | -160 132 3490 8286
| 1 2 3 15 17 36 .05 | 251 3139
iac n/a| -1 1 -6 -4 28 196 -.20 32 29 | 2442 -545 3426 9073
| 1 2 5 37 37 43 .05 | 1377 1228
mcc n/a| 2 5 7 -106 17 251 -.62 208 208 | --- --- --- ---
| 11 8 20 233 94 629 .41 | --- ---
Table 1.2168.b GPS week : 2168 MJD: 59420.0-59426.0
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 | 23 18 20 22 19 19 19 |
R02 | 10 9 10 8 7 7 8 |
R03 | 10 8 9 8 8 8 8 |
R04 | 12 11 12 8 9 7 9 |
R05 | 11 9 10 9 9 10 7 |
R07 | 11 10 9 8 7 8 8 |
R08 | 11 10 10 8 7 7 7 |
R09 | 14 12 10 11 9 10 9 |
R11 | 11 13 13 11 11 10 11 |
R12 | 10 8 8 10 7 10 8 |
R13 | 14 14 16 15 15 14 17 |
R14 | 8 8 11 7 8 7 6 |
R15 | 8 8 7 8 7 6 7 |
R16 | 14 12 14 14 12 12 13 |
R17 | 12 8 8 7 7 7 7 |
R18 | 8 10 10 10 9 9 8 |
R19 | 28 24 27 25 21 23 28 |
R20 | 24 20 20 22 24 23 19 |
R21 | 9 7 9 8 6 9 7 |
R22 | 26 26 24 21 20 17 19 |
R24 | 12 10 10 11 11 11 7 |
Table 1.2168.c GPS week : 2168 MJD: 59420.0-59426.0
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 2168 0 | -24 -48 171 -198 574 8334 81.0 1677 1677 | 1031 0
brd 2168 1 | -13 0 191 66 2001 6890 82.1 1498 1498 | -1557 0
brd 2168 2 | -48 -118 234 1511 2001 2449 83.4 1342 1342 | 834 0
brd 2168 3 | 120 0 271 1223 -56 1840 81.1 1301 1301 | 592 0
brd 2168 4 | -5 57 275 2631 -671 -1643 83.9 1274 1274 | 335 0
brd 2168 5 | -48 86 165 1364 -1732 -3474 83.9 1184 1184 | -2522 0
brd 2168 6 | -64 5 60 -912 -2136 -3495 83.8 1228 1228 | 1793 0
-------------+------------------------------------------------------------+----------------
brd 2168 mean| -11 -2 195 812 -2 1557 82.8 1357 1357 | 72 0
brd 2168 sdev| 62 67 74 1212 1651 4766 1.3 172 172 | 1537 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 2.2168.0 GPS week: 2168 Day: 0 MJD: 59420
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 3 10 -8 -32 .15 29 23 | 12523 2921 3694 8822
emx n/a| -4 -1 -5 46 58 -65 -.12 40 29 | -12439 1792 3698 9264
esx n/a| 1 1 -2 -9 7 49 -.05 31 24 | -8818 3115 3675 9857
gfz n/a| 0 0 1 -12 -45 20 -.12 24 15 | 0 2124 3728 8705
grg n/a| 2 4 5 -11 56 -92 .27 36 34 | -441 2478 3736 8525
iac n/a| -1 6 -9 24 -37 185 -.13 57 57 | 3002 -177 3641 9321
mcc n/a| 21 8 24 28 60 975 -.82 241 241 | --- --- --- ---
Table 2.2168.1 GPS week: 2168 Day: 1 MJD: 59421
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 -17 -18 -27 .15 24 21 | 14269 -3668 3629 8557
emx n/a| -2 0 -4 -37 -34 -40 -.19 39 30 | -12123 -2820 3648 9031
esx n/a| -2 1 -1 35 0 50 -.03 31 25 | 13280 -2063 3639 9954
gfz n/a| -1 3 1 33 -11 27 -.15 25 18 | 0 -3492 3706 8098
grg n/a| 4 -1 6 -9 34 -130 .28 31 26 | 16 -3327 3693 8164
iac n/a| -1 0 -15 -19 57 176 -.19 32 32 | 1788 -2696 3639 9049
mcc n/a| 2 20 18 -40 -172 1123 -.26 198 198 | --- --- --- ---
Table 2.2168.2 GPS week: 2168 Day: 2 MJD: 59422
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 3 -37 -31 -12 .16 26 25 | 13486 568 3008 8879
emx n/a| -2 0 -3 37 -35 -47 -.02 37 29 | -5516 721 3018 9248
esx n/a| 0 0 0 19 0 -1 -.09 31 24 | -1669 1440 2998 7289
gfz n/a| 1 2 4 17 3 35 -.01 26 20 | 0 1422 3038 8724
grg n/a| 6 0 0 28 38 -209 .32 36 32 | 203 861 3089 8339
iac n/a| -1 2 -3 -46 75 175 -.16 31 31 | 1626 1254 3018 9332
mcc n/a| -17 2 -26 -620 64 384 -.62 241 241 | --- --- --- ---
Table 2.2168.3 GPS week: 2168 Day: 3 MJD: 59423
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 -2 3 -7 -26 -55 .11 21 19 | 13788 2478 4010 8436
emx n/a| -1 2 -12 -17 -15 -43 -.05 42 30 | -10190 2067 4103 9098
esx n/a| 0 0 0 29 -13 -17 -.09 32 29 | -5366 2603 4004 10227
gfz n/a| 2 0 0 -12 8 65 -.05 24 22 | 0 1447 3972 7551
grg n/a| 4 3 0 5 15 -122 .40 32 27 | -487 2157 4061 8245
iac n/a| -3 0 -2 -38 26 292 -.24 35 25 | 3560 -636 4007 8916
mcc n/a| 3 9 -6 -115 55 -438 -.21 233 233 | --- --- --- ---
Table 2.2168.4 GPS week: 2168 Day: 4 MJD: 59424
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 13 -25 -4 .16 24 19 | 16775 -45 3264 9053
emx n/a| -2 -2 -7 -34 -16 -37 -.00 46 33 | 7523 29 3329 9806
esx n/a| 1 -2 0 33 -15 -69 -.10 31 30 | -2166 1153 3244 11013
gfz n/a| 0 1 3 -25 -24 5 -.10 21 14 | 0 739 3245 8685
grg n/a| 1 0 8 1 25 -116 .37 31 25 | -259 617 3348 8762
iac n/a| -3 2 -8 4 33 162 -.18 21 17 | 3197 306 3267 9622
mcc n/a| -5 -4 30 -48 -40 295 -1.31 154 154 | --- --- --- ---
Table 2.2168.5 GPS week: 2168 Day: 5 MJD: 59425
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 -13 -24 -39 .19 22 17 | 13420 -4469 2888 8277
emx n/a| -4 4 -7 5 -9 -26 -.03 44 31 | -11660 -2560 2924 8903
esx n/a| 1 -1 3 -3 1 -35 -.12 29 27 | 4868 -4042 2881 7635
gfz n/a| 2 1 0 -10 0 38 -.07 25 15 | 0 -5290 2926 8130
grg n/a| 1 1 7 -18 0 -118 .32 31 25 | -139 -5084 2945 8040
iac n/a| 0 1 -5 59 0 179 -.22 23 21 | -1 -817 2899 8675
mcc n/a| 4 -1 15 30 49 -245 -.89 134 134 | --- --- --- ---
Table 2.2168.6 GPS week: 2168 Day: 6 MJD: 59426
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 23 -34 -47 .11 21 16 | 13494 3602 3507 8034
emx n/a| -3 0 0 7 -35 -50 -.07 43 31 | -18952 1681 3608 8702
esx n/a| 0 1 -1 12 13 -22 -.08 30 21 | -5448 4135 3521 10001
gfz n/a| 0 0 -1 0 -2 -17 -.02 25 13 | 0 2606 3570 7593
grg n/a| 1 0 7 -6 25 -138 .40 32 20 | -16 3228 3558 7933
iac n/a| -1 -2 0 -14 39 201 -.29 22 18 | 3923 -1051 3517 8599
mcc n/a| 6 2 -6 23 105 -337 -.23 256 256 | --- --- --- ---
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 3.2168.0 GPS week: 2168 Day: 0 MJD: 59420
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 1478 73 30 23 46 33 99 --- 23 | 89 115 111 119 102 115 --- 101
R02E | 4125 11 26 10 11 28 54 278 9 | 91 90 85 89 92 99 181 87
R03E | 1686 11 32 14 13 31 40 147 9 | 48 45 42 44 62 57 116 45
XR04E | 1064 14 27 14 --- 23 56 --- 12 | 106 105 100 --- 106 110 --- 103
R05E | 879 16 36 17 15 40 32 344 11 | 152 157 168 162 157 157 78 158
R07E | 1002 17 34 13 17 16 62 203 11 | 48 47 45 47 49 65 48 45
R08E | 1553 11 32 17 17 29 55 --- 10 | 68 69 69 69 77 76 --- 67
R09 | 918 18 28 24 16 43 71 --- 13 | 69 70 69 72 44 90 --- 64
XR11 | 2142 21 25 17 12 --- 42 --- 10 | 43 24 42 42 --- 52 --- 40
R12 | 906 13 29 14 18 21 57 --- 10 | 103 92 99 107 102 100 --- 100
R13 | 1610 23 32 24 22 55 34 --- 14 | 75 55 48 65 45 65 --- 57
R14 | 784 12 12 11 12 19 49 --- 7 | 54 53 66 60 64 45 --- 57
R15 | 1037 6 12 16 12 19 45 260 7 | 77 71 75 74 74 72 65 73
R16 | 1584 21 29 27 28 50 36 --- 14 | 52 57 69 60 63 60 --- 57
R17 | 1422 17 22 9 10 13 87 --- 11 | 48 41 42 44 47 69 --- 44
R18 | 1343 8 24 18 9 10 50 --- 8 | 37 34 41 31 37 45 --- 33
R19 | 1737 42 117 53 33 71 48 --- 27 | 55 42 44 63 60 65 --- 48
R20 | 824 69 55 53 37 46 71 --- 24 | 65 53 54 63 53 77 --- 54
R21 | 692 10 24 10 12 16 55 151 8 | 49 41 44 49 52 51 49 46
R22 | 1679 27 34 89 55 54 43 --- 25 | 46 48 51 54 36 48 --- 35
R24 | 2816 28 39 13 12 24 50 --- 11 | 44 27 37 41 46 61 --- 37
------+----------------------------------------------+------------------------------------------
RMS | 1677 29 40 31 24 36 57 241 |T 67 63 66 67 68 75 89 64
WRMS | 1677 23 29 24 15 34 57 241 |NE 58 50 55 58 55 64 57 53
MEDI | 1422 17 29 17 15 28 50 203 |MD 55 53 54 60 60 65 65 57
Table 3.2168.1 GPS week: 2168 Day: 1 MJD: 59421
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 728 48 42 31 40 28 48 --- 18 | 48 59 69 66 59 66 --- 52
R02E | 3455 18 23 14 8 15 34 186 8 | 109 108 112 109 113 106 205 108
R03E | 1009 15 29 11 13 20 17 172 7 | 49 49 49 49 50 56 103 48
XR04E | 984 14 29 20 --- 24 29 --- 11 | 144 142 147 --- 140 132 --- 142
R05E | 634 15 36 16 13 21 23 180 9 | 180 186 175 181 182 184 85 181
R07E | 911 16 35 16 12 19 34 277 9 | 61 52 53 57 66 61 39 57
R08E | 1912 11 33 13 14 24 36 --- 10 | 81 84 84 82 86 67 --- 78
R09 | 1125 22 32 17 20 44 22 --- 12 | 52 55 42 49 29 41 --- 38
XR11 | 2346 17 27 21 17 --- 43 --- 12 | 21 18 28 24 --- 48 --- 24
R12 | 719 12 13 16 21 25 20 --- 8 | 75 73 69 86 67 55 --- 72
R13 | 2279 24 20 22 29 38 48 --- 14 | 49 41 39 55 31 49 --- 38
R14 | 1162 7 9 19 11 15 34 --- 7 | 31 32 39 40 36 35 --- 33
R15 | 908 10 16 16 8 18 33 194 7 | 54 53 47 45 48 47 34 48
R16 | 1661 27 32 25 23 34 26 --- 12 | 32 43 44 34 35 30 --- 33
R17 | 1063 14 23 13 8 16 30 --- 7 | 35 30 26 28 35 70 --- 31
R18 | 1630 11 31 23 25 15 28 --- 10 | 30 24 27 27 27 23 --- 22
R19 | 1115 40 90 42 26 76 33 --- 23 | 30 26 36 38 43 48 --- 29
R20 | 1120 49 66 54 29 27 44 --- 20 | 34 67 34 48 27 37 --- 32
R21 | 467 13 26 12 7 11 20 159 6 | 38 30 35 32 40 52 16 35
R22 | 1247 23 47 93 71 49 20 --- 26 | 40 44 37 77 49 29 --- 36
R24 | 2069 12 45 11 8 21 30 --- 9 | 30 23 24 27 30 28 --- 24
------+----------------------------------------------+------------------------------------------
RMS | 1498 24 39 31 25 31 32 198 |T 58 59 57 57 59 60 80 55
WRMS | 1498 21 30 25 18 26 32 198 |NE 39 39 37 43 38 42 25 35
MEDI | 1120 15 31 17 14 21 30 180 |MD 48 49 42 48 43 49 39 38
Table 3.2168.2 GPS week: 2168 Day: 2 MJD: 59422
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 825 48 51 41 49 38 41 --- 20 | 91 98 112 111 108 99 --- 98
R02E | 2005 10 29 12 26 23 24 273 9 | 95 97 99 106 92 89 352 95
R03E | 718 17 32 12 15 19 19 231 8 | 47 41 37 43 49 45 118 41
XR04E | 1595 14 31 19 --- 22 27 --- 11 | 76 81 78 --- 76 53 --- 72
R05E | 610 16 28 14 18 33 19 219 9 | 92 93 87 83 85 89 34 86
R07E | 1097 15 29 12 12 28 18 379 8 | 42 36 38 40 53 47 34 39
R08E | 2180 9 33 13 27 22 15 --- 9 | 58 56 50 61 62 54 --- 54
R09 | 1167 21 18 11 19 42 24 --- 10 | 49 50 46 54 29 42 --- 42
XR11 | 1561 21 29 25 19 --- 35 --- 13 | 35 17 49 43 --- 57 --- 41
R12 | 1397 14 19 23 10 16 25 --- 8 | 81 90 91 87 91 80 --- 85
R13 | 2116 38 21 24 43 52 20 --- 15 | 52 36 30 38 26 29 --- 30
R14 | 1156 19 13 25 11 11 45 --- 10 | 30 23 39 31 28 44 --- 26
R15 | 794 17 13 7 10 16 26 87 7 | 45 37 43 44 45 37 73 39
R16 | 1287 33 23 37 18 35 29 --- 13 | 45 40 59 53 56 46 --- 47
R17 | 1096 14 24 8 11 21 30 --- 8 | 30 25 28 28 37 26 --- 26
R18 | 1845 8 25 29 20 19 25 --- 9 | 23 19 26 18 30 35 --- 19
R19 | 1691 50 95 41 28 80 64 --- 26 | 46 40 48 59 35 40 --- 40
R20 | 1083 45 51 45 48 48 32 --- 20 | 46 49 34 42 37 46 --- 33
R21 | 758 16 25 8 23 19 29 143 9 | 46 36 43 47 40 32 29 39
R22 | 717 28 43 85 39 56 51 --- 24 | 39 37 38 42 45 60 --- 31
R24 | 1223 14 37 10 11 34 13 --- 9 | 26 20 28 23 48 33 --- 25
------+----------------------------------------------+------------------------------------------
RMS | 1341 26 37 30 26 36 31 241 |T 52 48 52 52 53 51 106 48
WRMS | 1341 25 29 24 20 32 31 241 |NE 42 37 43 43 42 43 51 37
MEDI | 1167 17 29 19 19 23 26 219 |MD 46 40 43 43 45 46 34 40
Table 3.2168.3 GPS week: 2168 Day: 3 MJD: 59423
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 867 40 50 48 60 31 64 --- 22 | 109 114 139 135 121 137 --- 118
R02E | 1074 13 24 13 15 15 23 --- 7 | 49 43 40 45 54 47 --- 44
R03E | 744 12 30 16 20 14 17 259 8 | 36 26 29 36 41 28 158 31
XR04E | 2543 10 26 13 --- 14 18 --- 8 | 111 110 119 --- 116 108 --- 112
R05E | 622 16 32 15 20 22 15 220 9 | 103 106 104 103 106 111 49 104
R07E | 1093 14 26 12 15 16 22 340 7 | 29 26 27 35 34 26 65 26
R08E | 1833 8 30 11 19 17 19 --- 7 | 27 25 31 35 45 31 --- 29
R09 | 1787 21 15 20 18 38 27 --- 10 | 52 51 56 55 20 43 --- 44
XR11 | 1475 20 --- 16 19 --- 16 --- 10 | 25 --- 33 31 --- 29 --- 25
R12 | 1774 14 12 19 26 24 31 --- 9 | 67 52 66 61 69 73 --- 62
R13 | 2921 26 30 34 21 51 39 --- 15 | 56 40 34 50 37 61 --- 43
R14 | 577 9 20 22 12 18 16 --- 7 | 30 24 48 30 42 37 --- 33
R15 | 747 15 22 10 16 19 26 155 8 | 40 34 33 40 23 25 174 31
R16 | 954 18 25 43 21 46 24 --- 13 | 36 36 61 38 51 51 --- 42
R17 | 1200 6 28 13 20 14 14 --- 7 | 26 20 27 37 36 28 --- 26
R18 | 1686 12 23 32 25 20 23 --- 10 | 23 24 29 25 27 27 --- 21
R19 | 869 33 106 49 26 52 73 --- 24 | 37 32 36 41 49 66 --- 33
R20 | 872 44 73 43 31 59 46 --- 21 | 68 38 57 59 50 62 --- 51
R21 | 557 12 22 7 11 16 36 130 8 | 46 42 43 43 47 37 42 41
R22 | 1066 30 35 79 22 48 49 --- 20 | 31 42 40 46 32 37 --- 24
R24 | 911 9 63 15 20 11 18 --- 11 | 28 21 31 40 34 41 --- 28
------+----------------------------------------------+------------------------------------------
RMS | 1301 21 42 32 24 32 35 233 |T 49 45 51 49 51 52 97 46
WRMS | 1301 19 30 29 22 27 25 233 |NE 40 35 42 42 39 44 108 36
MEDI | 1066 14 26 16 20 19 23 220 |MD 37 36 40 40 42 41 65 33
Table 3.2168.4 GPS week: 2168 Day: 4 MJD: 59424
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 1012 44 44 40 47 41 29 --- 18 | 88 96 92 103 97 76 --- 87
R02E | 1157 9 24 11 12 17 19 219 6 | 50 53 51 49 54 51 246 48
R03E | 672 14 31 17 16 18 16 156 8 | 46 43 45 47 51 45 159 43
XR04E | 3373 11 28 13 --- 18 18 --- 8 | 54 46 50 --- 61 60 --- 54
R05E | 1094 14 38 17 16 13 19 45 8 | 55 45 60 63 58 67 107 58
R07E | 1287 17 23 11 9 20 14 148 6 | 39 30 39 39 46 38 78 36
R08E | 541 9 29 12 14 14 15 --- 6 | 37 32 43 49 48 42 --- 41
R09 | 1556 23 13 13 18 34 15 --- 9 | 44 40 47 55 24 51 --- 41
XR11 | 881 21 --- 28 15 --- 12 --- 11 | 43 --- 45 54 --- 48 --- 45
R12 | 1022 13 17 22 12 16 14 --- 7 | 95 98 96 107 99 92 --- 97
R13 | 2676 25 34 48 27 43 27 --- 15 | 48 34 36 47 52 51 --- 41
R14 | 796 11 13 18 15 23 22 --- 8 | 37 32 40 32 55 48 --- 38
R15 | 630 15 17 9 13 15 21 186 7 | 44 46 44 42 53 33 175 40
R16 | 1001 21 30 29 19 48 14 --- 12 | 30 38 59 55 39 45 --- 42
R17 | 1188 6 29 11 11 15 19 --- 6 | 31 21 33 33 33 41 --- 31
R18 | 1284 22 29 36 10 7 13 --- 9 | 30 25 34 30 28 31 --- 25
R19 | 1118 23 108 53 34 27 35 --- 20 | 49 40 31 46 42 48 --- 40
R20 | 996 52 105 49 34 57 34 --- 23 | 50 73 63 56 53 37 --- 46
R21 | 536 10 20 12 13 14 16 103 6 | 43 38 40 35 44 48 58 40
R22 | 2138 42 49 65 19 68 16 --- 19 | 40 49 52 46 47 47 --- 35
R24 | 1433 23 66 9 6 18 12 --- 10 | 34 32 28 27 36 32 --- 28
------+----------------------------------------------+------------------------------------------
RMS | 1274 24 46 31 21 31 21 154 |T 47 45 48 50 51 49 137 45
WRMS | 1274 19 33 30 14 25 17 154 |NE 44 43 46 47 46 46 116 42
MEDI | 1094 17 29 17 15 18 16 148 |MD 44 40 45 47 48 48 107 41
Table 3.2168.5 GPS week: 2168 Day: 5 MJD: 59425
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 795 33 40 27 51 42 55 --- 19 | 108 115 125 119 111 105 --- 109
R02E | 1288 10 25 16 11 16 18 121 7 | 30 28 27 29 35 28 111 26
R03E | 687 15 31 12 13 14 18 180 7 | 33 32 34 35 41 43 129 34
XR04E | 2428 8 26 11 --- 16 16 --- 7 | 82 79 87 --- 78 78 --- 81
R05E | 1615 16 40 13 26 16 16 45 9 | 76 76 75 86 75 81 70 77
R07E | 1229 12 33 12 17 20 19 177 8 | 31 25 26 31 33 32 38 27
R08E | 742 8 30 11 14 16 18 --- 7 | 28 21 31 29 41 32 --- 28
R09 | 2399 15 23 16 17 40 23 --- 10 | 39 39 38 46 21 34 --- 32
XR11 | 829 12 --- 13 16 --- 22 --- 9 | 24 --- 25 36 --- 27 --- 24
R12 | 858 13 29 22 23 23 29 --- 10 | 53 45 46 62 61 75 --- 55
R13 | 2167 18 29 34 29 47 24 --- 13 | 46 18 27 46 35 50 --- 36
R14 | 577 12 15 13 16 13 23 --- 7 | 42 45 47 51 49 56 --- 47
R15 | 721 9 18 11 11 12 15 131 5 | 56 42 53 51 61 54 109 53
R16 | 1162 19 24 25 29 47 17 --- 12 | 31 37 43 39 38 31 --- 33
R17 | 974 10 30 15 18 12 13 --- 7 | 34 37 37 33 40 31 --- 32
R18 | 981 11 21 31 15 15 20 --- 8 | 28 22 24 23 35 23 --- 23
R19 | 600 45 100 58 45 42 26 --- 23 | 44 59 44 57 33 35 --- 39
R20 | 805 51 103 52 26 49 24 --- 22 | 35 69 52 50 30 36 --- 34
R21 | 626 11 22 21 23 16 20 100 8 | 36 40 40 32 38 37 24 34
R22 | 762 26 29 62 26 52 14 --- 17 | 41 37 38 66 51 47 --- 39
R24 | 1379 18 60 14 18 20 22 --- 11 | 33 25 34 37 39 36 --- 31
------+----------------------------------------------+------------------------------------------
RMS | 1183 22 44 29 25 31 23 134 |T 44 44 45 47 47 46 80 42
WRMS | 1183 17 31 27 15 25 21 134 |NE 38 39 39 44 40 40 66 36
MEDI | 858 13 29 16 18 16 20 121 |MD 36 37 38 39 39 36 70 34
Table 3.2168.6 GPS week: 2168 Day: 6 MJD: 59426
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 1240 33 44 37 60 33 37 --- 18 | 91 102 97 101 102 105 --- 94
R02E | 1642 15 24 15 17 20 19 265 8 | 45 53 47 54 49 56 112 48
R03E | 918 14 37 15 13 15 14 494 8 | 68 57 57 62 65 61 130 61
XR04E | 2535 14 31 16 --- 12 15 --- 8 | 87 84 74 --- 85 78 --- 80
R05E | 1290 10 34 14 14 13 13 71 7 | 87 92 83 85 91 84 83 85
R07E | 917 14 34 16 12 13 13 234 7 | 49 39 42 51 49 43 52 44
R08E | 1237 9 28 10 14 17 21 --- 7 | 30 25 29 34 38 29 --- 28
R09 | 2464 15 16 10 15 38 21 --- 9 | 57 50 52 50 48 43 --- 47
XR11 | 1065 18 --- 17 14 --- 22 --- 10 | 36 --- 36 36 --- 42 --- 34
R12 | 1550 7 33 8 8 33 16 --- 8 | 84 77 82 90 100 86 --- 86
R13 | 1304 35 45 40 29 47 28 --- 16 | 74 43 45 57 47 67 --- 55
R14 | 722 13 13 10 11 10 16 --- 5 | 53 55 57 54 56 61 --- 54
R15 | 1090 14 12 16 9 10 20 98 6 | 69 61 66 68 70 70 113 66
R16 | 970 27 22 18 24 48 27 --- 12 | 40 43 59 52 62 49 --- 46
R17 | 1183 11 26 10 7 15 17 --- 6 | 41 38 36 39 43 47 --- 39
R18 | 757 10 28 18 19 21 18 --- 8 | 30 23 38 27 42 31 --- 28
R19 | 976 32 128 76 50 58 29 --- 27 | 64 49 42 79 65 65 --- 56
R20 | 1007 43 55 47 42 37 25 --- 18 | 71 65 57 70 56 49 --- 57
R21 | 580 13 25 11 9 16 21 100 7 | 48 41 43 47 44 44 42 43
R22 | 666 28 39 59 20 62 35 --- 18 | 50 48 58 55 65 40 --- 41
R24 | 1400 16 33 11 9 11 12 --- 7 | 44 29 36 37 45 42 --- 37
------+----------------------------------------------+------------------------------------------
RMS | 1227 21 43 30 25 32 22 256 |T 58 53 54 57 61 56 88 53
WRMS | 1227 16 31 21 13 20 18 256 |NE 54 47 50 54 57 52 77 49
MEDI | 1090 14 31 16 14 17 20 100 |MD 53 49 52 54 56 49 83 48
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