[IGSREPORT-27350] Wk 2110 IGLOS Final Orbits
acc
acc at igs.org
Sat Jul 4 19:31:22 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2110 (Jun 14, 2020 - Jun 20, 2020)
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 2.2110.
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:
igl2110[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2110 in the SP3 format.
igl21107.sum Combination Report for GPS Week 2110.
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 | -0.2 ns
1 | -2.4 ns
2 | -4.4 ns
3 | -3.6 ns
4 | -1.7 ns
5 | -2.6 ns
6 | -2.2 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 1.2110, 1a.2110).
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 2.2110.0-6)
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 3.2110.0-6).
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 2110 summary. (Jun 14, 2020 - Jun 20, 2020)
Table 1.2110.a GPS week : 2110 MJD: 59014.0-59020.0
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 0 -5 -9 5 .09 16 13 | 22875 -256 3269 9026
| 0 1 1 13 13 18 .02 | 1956 2135
cof n/a| 0 0 0 -1 3 6 .08 21 16 | 22863 -253 3265 9024
| 1 1 1 11 24 20 .04 | 1947 2133
emx n/a| 0 0 2 32 9 -32 .04 44 41 | -4254 -137 2937 8305
| 1 1 3 25 24 21 .03 | 7412 1371
esx n/a| 0 0 -1 46 0 4 .09 44 32 | -6493 807 2944 10465
| 1 0 2 16 12 22 .03 | 6333 2489
gfz n/a| 0 -1 -1 -17 -4 -23 .13 28 17 | 0 -378 2964 7756
| 0 1 1 14 14 18 .07 | 0 1937
grg n/a| 0 0 1 -25 5 -6 -.36 23 18 | -2333 -287 2931 7373
| 1 1 2 22 11 8 .05 | 435 2144
iac n/a| 0 0 -3 0 4 41 .03 23 23 | -2161 1200 17735 28016
| 1 1 2 19 12 51 .04 | 7322 8115
mcc n/a| 4 0 -20 -10 18 33 -.18 151 151 | --- --- --- ---
| 7 11 18 191 84 452 .24 | --- ---
Table 1.2110.b GPS week : 2110 MJD: 59014.0-59020.0
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 | 14 14 17 18 16 15 16 |
R02 | 6 5 5 7 6 8 6 |
R03 | 7 8 6 7 7 6 6 |
R04 | 6 10 11 9 9 10 8 |
R05 | 7 8 7 7 8 7 8 |
R07 | 5 8 8 6 6 7 7 |
R08 | 5 7 6 5 6 7 6 |
R09 | 7 7 8 7 8 8 7 |
R11 | 6 7 6 6 7 6 6 |
R12 | 7 8 8 7 8 8 8 |
R13 | 21 17 18 17 18 14 16 |
R14 | 7 7 7 7 8 7 7 |
R15 | 8 6 7 9 8 7 7 |
R16 | 11 11 14 13 12 12 12 |
R17 | 7 9 9 7 9 10 10 |
R18 | 6 7 8 7 8 8 8 |
R19 | 21 23 23 24 26 28 30 |
R20 | 32 32 30 31 37 26 28 |
R21 | 11 10 10 9 10 11 11 |
R22 | 0 0 0 0 0 0 0 |
R23 | 9 9 8 8 8 8 11 |
R24 | 12 13 12 13 14 12 15 |
R26 | 19 23 20 15 13 18 13 |
Table 1.2110.c GPS week : 2110 MJD: 59014.0-59020.0
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 2110 0 | 17 40 173 208 586 3947 83.0 1418 1418 | -219 0
brd 2110 1 | 18 -8 174 623 1295 2749 83.0 1401 1401 | -2372 0
brd 2110 2 | 72 -20 117 1230 169 -890 82.1 1327 1327 | -4377 0
brd 2110 3 | 89 64 151 1238 -763 -2299 80.3 1495 1495 | -3648 0
brd 2110 4 | -63 -19 142 -91 -952 -2665 83.2 1453 1453 | -1695 0
brd 2110 5 | -25 -4 167 113 -2244 132 82.2 1444 1444 | -2621 0
brd 2110 6 | -19 -15 160 1376 -1137 586 82.6 1645 1645 | -2243 0
-------------+------------------------------------------------------------+----------------
brd 2110 mean| 12 5 155 671 -435 222 82.4 1454 1454 | -2453 0
brd 2110 sdev| 54 33 20 610 1193 2460 1.0 98 98 | 1340 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 2.2110.0 GPS week: 2110 Day: 0 MJD: 59014
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 -18 -21 -31 .07 19 16 | 20758 2483 3172 8961
cof n/a| 2 1 -3 -14 -3 -18 .14 21 18 | 20761 2473 3163 8957
emx n/a| -1 -1 2 36 19 -34 .07 43 43 | -4513 1359 2949 8614
esx n/a| 3 1 1 72 7 -17 .08 43 31 | -7640 4595 2956 10917
gfz n/a| 0 0 0 -7 -6 -36 .22 28 17 | 0 2273 2963 7845
grg n/a| 0 0 2 -29 4 -12 -.38 20 18 | -1495 2601 2938 7502
iac n/a| 0 -2 -3 4 3 89 .03 20 20 | -1527 -2963 8971 19990
mcc n/a| 5 0 -44 -83 148 441 -.53 156 156 | --- --- --- ---
Table 2.2110.1 GPS week: 2110 Day: 1 MJD: 59015
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 11 -4 .09 16 14 | 23458 726 3229 8763
cof n/a| -1 0 -2 9 23 -18 .11 23 18 | 23427 765 3230 8765
emx n/a| 0 -2 2 4 -35 -53 -.01 42 33 | -109 107 3014 8828
esx n/a| 0 2 1 63 5 -14 .09 44 28 | -17676 250 3020 11076
gfz n/a| 0 -1 0 0 -14 -14 .16 27 18 | 0 508 3077 8131
grg n/a| 0 -2 2 -3 19 1 -.35 25 23 | -2753 659 3008 7702
iac n/a| 1 3 -3 -19 0 67 .00 20 20 | 172 -7086 14870 20119
mcc n/a| 17 -2 -41 -237 -29 628 -.11 165 165 | --- --- --- ---
Table 2.2110.2 GPS week: 2110 Day: 2 MJD: 59016
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 -12 -20 5 .10 16 12 | 26221 -3823 3569 12020
cof n/a| 0 0 0 -20 -19 1 .03 19 15 | 26199 -3813 3568 12014
emx n/a| 1 0 6 -7 -15 -51 .04 41 34 | -17893 -2065 2962 8291
esx n/a| 0 0 -1 28 -13 -23 .06 45 29 | -3360 -2573 2964 10039
gfz n/a| -1 1 0 -40 12 -25 .02 32 19 | 0 -2813 3025 7736
grg n/a| 2 -1 4 1 2 -13 -.35 22 17 | -2627 -3826 2959 7150
iac n/a| -2 0 -6 30 13 68 .11 21 21 | 5833 2022 15257 38609
mcc n/a| 4 9 -10 -194 20 -324 -.04 129 129 | --- --- --- ---
Table 2.2110.3 GPS week: 2110 Day: 3 MJD: 59017
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 -20 -4 14 .07 15 10 | 22999 -2365 3284 9224
cof n/a| -1 2 0 7 31 21 .08 21 14 | 22988 -2369 3284 9218
emx n/a| 0 -2 4 66 19 -7 .06 41 42 | -9508 -2031 2887 8676
esx n/a| 1 0 -3 43 -13 17 .05 42 29 | 859 -1857 2930 10875
gfz n/a| 1 0 -5 -28 16 -13 .18 27 16 | 0 -3052 2982 8088
grg n/a| 0 0 2 -8 -13 -4 -.41 21 16 | -2431 -2408 2916 7621
iac n/a| 0 0 0 -18 16 -20 .04 22 22 | 1887 -1790 14541 18965
mcc n/a| 0 0 -3 26 -45 -444 -.43 119 119 | --- --- --- ---
Table 2.2110.4 GPS week: 2110 Day: 4 MJD: 59018
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 1 3 -19 15 .06 17 15 | 21108 880 3071 8551
cof n/a| 0 0 0 0 9 12 .04 21 18 | 21108 869 3064 8547
emx n/a| -2 -1 -1 41 19 2 .08 49 46 | 1421 910 2920 8207
esx n/a| 0 0 -1 41 -5 26 .12 46 33 | -7469 2449 2910 10720
gfz n/a| 0 -2 -1 -13 -2 -7 .14 25 14 | 0 655 2903 8232
grg n/a| 0 0 1 -41 13 -1 -.43 27 21 | -2101 716 2909 7661
iac n/a| 0 0 -3 -19 9 -35 .05 27 27 | -17454 14564 30432 52532
mcc n/a| -6 -22 -12 338 -6 -406 -.25 129 129 | --- --- --- ---
Table 2.2110.5 GPS week: 2110 Day: 5 MJD: 59019
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 1 17 -15 20 .13 15 13 | 21412 373 3129 8166
cof n/a| 2 1 0 1 19 37 .11 21 16 | 21407 376 3122 8167
emx n/a| -1 0 -1 44 31 -44 .02 44 41 | -2982 546 2970 8248
esx n/a| 0 0 -3 44 19 11 .08 45 35 | -9856 835 2982 10139
gfz n/a| 0 -2 -1 -25 -18 -9 .09 26 17 | 0 -565 2966 7719
grg n/a| -1 0 -2 -49 0 4 -.34 19 16 | -2660 105 2961 7492
iac n/a| -1 1 0 2 9 35 .02 26 26 | -1099 -5923 17261 22046
mcc n/a| 11 -4 -30 22 -73 416 .04 207 207 | --- --- --- ---
Table 2.2110.6 GPS week: 2110 Day: 6 MJD: 59020
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 5 20 .08 16 12 | 24169 -66 3430 7501
cof n/a| 2 0 0 9 -34 7 .08 19 14 | 24157 -75 3428 7502
emx n/a| 0 2 0 39 25 -41 .05 47 47 | 3804 210 2861 7271
esx n/a| -1 0 -3 31 -4 31 .11 43 38 | -314 1953 2850 9492
gfz n/a| 1 0 0 -9 -15 -60 .10 30 19 | 0 345 2835 6542
grg n/a| 0 0 3 -50 14 -18 -.27 22 17 | -2268 142 2830 6486
iac n/a| -2 0 -5 13 -19 87 -.00 27 27 | -2945 9580 22819 23857
mcc n/a| 1 13 1 55 119 -76 .09 156 156 | --- --- --- ---
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 3.2110.0 GPS week: 2110 Day: 0 MJD: 59014
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 712 38 38 22 45 16 33 28 --- 14 | 89 90 63 46 66 50 80 --- 66
R02 | 1131 14 13 10 9 24 10 10 109 6 | 49 52 49 50 61 48 46 87 49
R03 | 914 15 16 15 9 15 19 18 105 7 | 57 55 57 61 69 64 68 19 61
XR04 | 517 11 10 18 8 --- 10 11 --- 6 | 56 53 58 44 --- 46 46 --- 49
R05 | 826 13 9 14 20 17 17 16 --- 7 | 41 42 40 40 45 38 49 --- 40
R07 | 1244 11 14 10 13 11 11 10 217 5 | 63 64 54 57 71 61 61 106 61
R08 | 508 10 13 21 8 12 11 8 --- 5 | 53 57 46 56 61 62 55 --- 55
R09E | 4225 12 10 19 16 13 13 18 --- 6 | 53 56 54 62 62 55 54 --- 55
R11E | 1572 7 12 16 14 13 13 13 127 5 | 69 68 66 61 67 71 68 78 66
R12E | 813 8 11 29 15 20 17 9 --- 7 | 39 42 36 42 47 43 38 --- 38
R13E | 1666 15 30 64 40 83 28 35 --- 20 | 41 58 26 41 113 44 53 --- 47
R14E | 728 14 15 22 17 18 16 12 --- 7 | 70 73 73 83 78 81 75 --- 76
R15E | 1058 10 10 26 12 25 14 13 --- 7 | 104 105 104 105 110 106 105 --- 105
R16E | 1060 21 22 24 22 29 26 17 --- 10 | 53 62 61 60 67 61 53 --- 56
R17 | 1313 18 18 26 19 10 9 11 --- 7 | 65 65 36 38 58 51 59 --- 52
R18 | 711 10 12 24 16 15 8 10 --- 6 | 47 48 36 48 55 46 51 --- 45
R19 | 705 38 33 82 76 29 33 20 --- 20 | 105 102 47 38 100 99 95 --- 83
R20 | 1931 32 44 125 137 47 37 49 --- 32 | 142 153 74 59 162 140 150 --- 123
R21 | 1060 10 11 39 42 24 13 26 189 11 | 77 75 58 52 85 70 90 48 73
XR22 | 3456 --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 401 --- 401
R23 | 834 11 7 18 47 16 15 12 --- 9 | 30 33 41 62 30 28 32 --- 32
R24 | 542 16 27 51 40 21 13 24 --- 12 | 76 86 44 55 80 75 83 --- 70
XR26 | 3399 18 46 --- --- --- --- 19 --- 18 | 47 81 --- --- --- --- 54 --- 49
------+---------------------------------------------------+-----------------------------------------------
RMS | 1418 19 21 43 43 28 20 20 156 |T 64 69 53 55 74 63 81 67 76
WRMS | 1418 16 18 43 31 17 18 20 156 |NE 66 70 50 50 72 62 88 65 81
MEDI | 1058 13 13 22 17 17 14 13 127 |MD 56 62 54 55 67 61 59 78 56
Table 3.2110.1 GPS week: 2110 Day: 1 MJD: 59015
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 691 28 36 25 50 41 22 25 --- 14 | 56 64 60 55 49 47 63 --- 52
R02 | 694 8 12 9 13 13 12 11 161 5 | 44 45 45 49 42 39 37 165 41
R03 | 645 13 13 10 11 19 25 17 107 7 | 47 51 50 54 66 68 44 33 52
XR04 | 598 17 21 27 26 --- 19 15 --- 10 | 40 42 44 25 --- 28 26 --- 31
R05 | 633 9 13 14 15 25 23 10 --- 7 | 33 32 34 32 44 25 31 --- 31
R07 | 764 11 11 15 21 19 21 18 215 8 | 46 46 43 38 49 34 47 138 41
R08 | 488 8 10 21 17 20 16 6 --- 6 | 37 43 29 47 47 43 38 --- 39
R09E | 4132 14 11 19 13 14 11 22 --- 7 | 37 38 35 35 37 35 41 --- 35
R11E | 1410 9 13 14 9 21 20 11 76 6 | 66 69 61 61 72 62 62 89 64
R12E | 543 8 12 34 13 14 23 11 --- 8 | 30 29 32 30 40 25 32 --- 29
R13E | 2476 22 27 48 44 53 26 33 --- 16 | 33 43 30 44 84 52 50 --- 43
R14E | 911 11 22 19 21 19 11 13 --- 7 | 69 64 74 69 71 67 68 --- 68
R15E | 1444 9 13 23 15 14 11 14 --- 6 | 78 76 79 85 82 82 81 --- 80
R16E | 1468 15 28 30 22 30 33 20 --- 11 | 39 40 47 42 47 50 39 --- 40
R17 | 1315 16 22 30 31 10 12 17 --- 8 | 38 40 30 29 31 23 36 --- 30
R18 | 945 11 8 19 21 15 16 11 --- 6 | 29 32 31 34 33 24 26 --- 27
R19 | 504 30 45 84 83 42 57 28 --- 23 | 50 70 36 42 50 64 44 --- 40
R20 | 831 31 41 122 138 51 44 42 --- 31 | 71 88 59 53 86 76 75 --- 63
R21 | 756 11 16 34 35 18 12 21 215 9 | 56 57 56 43 56 49 55 60 52
XR22 | 3026 --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 243 --- 242
R23 | 867 18 25 13 31 19 22 12 --- 8 | 28 31 23 34 20 35 29 --- 24
R24 | 1081 15 22 52 41 16 34 19 --- 13 | 50 55 36 45 42 58 48 --- 45
XR26 | 3055 21 39 --- --- --- --- 25 --- 23 | 45 55 --- --- --- --- 37 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1400 16 23 42 44 27 25 20 165 |T 46 50 44 45 52 46 54 97 52
WRMS | 1400 14 18 33 28 18 23 20 165 |NE 44 50 41 41 47 43 54 99 53
MEDI | 867 13 16 23 21 19 21 17 161 |MD 44 45 43 43 47 47 44 89 41
Table 3.2110.2 GPS week: 2110 Day: 2 MJD: 59016
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 700 35 16 33 73 38 25 21 --- 16 | 66 56 60 54 50 61 44 --- 51
R02 | 934 8 12 15 16 11 10 10 134 5 | 40 46 45 33 42 42 35 99 38
R03 | 1325 5 10 11 13 8 16 21 100 6 | 46 51 49 54 47 57 36 40 46
XR04 | 629 20 24 30 17 --- 17 25 --- 11 | 44 45 46 31 --- 27 24 --- 32
R05 | 724 10 14 13 16 25 19 8 --- 7 | 30 34 34 38 47 28 35 --- 33
R07 | 1029 7 7 14 12 17 25 21 138 7 | 47 48 48 55 57 40 61 66 49
R08 | 691 9 11 13 16 20 11 17 --- 6 | 50 52 48 47 62 49 57 --- 51
R09E | 3044 11 19 24 15 23 22 18 --- 8 | 38 38 42 36 41 40 45 --- 38
R11E | 1355 7 11 26 21 15 8 12 174 6 | 49 46 43 63 52 47 48 85 48
R12E | 522 12 17 34 19 15 12 14 --- 7 | 39 40 37 40 44 31 34 --- 35
R13E | 1846 26 35 63 39 64 21 34 --- 18 | 43 46 53 45 73 46 37 --- 40
R14E | 1276 12 10 30 17 11 11 13 --- 7 | 47 45 49 38 44 38 41 --- 41
R15E | 852 11 10 23 19 13 12 16 --- 6 | 83 82 83 90 80 92 91 --- 86
R16E | 1237 19 23 26 27 55 37 22 --- 14 | 39 42 39 42 68 45 46 --- 38
R17 | 1463 10 16 28 25 21 18 20 --- 8 | 45 47 31 35 52 32 47 --- 39
R18 | 1108 7 13 24 18 20 19 23 --- 8 | 39 41 31 44 41 46 51 --- 40
R19 | 1534 34 23 77 89 48 46 25 --- 22 | 83 73 70 57 86 63 74 --- 67
R20 | 1347 24 42 106 130 66 39 46 --- 29 | 98 101 65 54 125 95 120 --- 92
R21 | 1552 12 12 36 34 30 19 16 80 10 | 57 58 45 47 71 57 62 81 55
XR22 | 2813 --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 434 --- 434
R23 | 1015 15 19 13 38 13 9 10 --- 7 | 23 24 21 40 23 19 29 --- 22
R24 | 622 7 12 54 40 12 22 24 --- 12 | 47 44 35 31 49 51 60 --- 45
XR26 | 4242 17 41 --- --- --- --- 23 --- 20 | 30 59 --- --- --- --- 42 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1327 16 19 41 45 32 22 21 129 |T 49 50 46 46 57 47 67 74 63
WRMS | 1327 12 15 34 29 19 17 21 129 |NE 49 51 44 44 57 47 75 71 70
MEDI | 1237 11 14 26 19 20 19 20 134 |MD 45 46 45 44 50 46 46 81 41
Table 3.2110.3 GPS week: 2110 Day: 3 MJD: 59017
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 614 41 50 51 68 42 27 17 --- 18 | 61 71 44 54 52 38 47 --- 43
R02 | 2089 6 15 8 33 11 18 19 99 7 | 38 38 35 35 36 49 37 50 36
R03 | 1409 5 10 13 22 14 23 11 96 6 | 45 47 47 33 37 55 39 39 42
XR04 | 731 12 17 30 19 --- 18 15 --- 9 | 42 41 56 42 --- 30 29 --- 36
R05 | 658 8 14 18 18 21 20 11 --- 7 | 27 28 42 42 44 20 35 --- 31
R07 | 639 8 8 14 18 9 13 16 141 5 | 50 49 56 48 52 45 64 41 51
R08 | 1372 7 11 12 7 11 11 20 --- 5 | 47 48 46 46 42 46 57 --- 46
R09E | 3342 8 14 16 12 22 16 17 --- 6 | 14 17 14 20 27 16 25 --- 15
R11E | 1326 9 13 23 13 11 14 10 160 5 | 93 93 93 97 91 98 89 54 93
R12E | 702 10 13 32 19 9 13 11 --- 6 | 28 33 23 31 33 29 32 --- 27
R13E | 2279 27 45 41 48 51 38 29 --- 17 | 42 44 39 46 56 68 41 --- 41
R14E | 1098 8 15 21 14 10 13 21 --- 6 | 79 83 82 85 83 82 74 --- 80
R15E | 749 14 16 34 24 15 16 17 --- 8 | 86 88 84 71 79 71 72 --- 76
R16E | 1538 22 21 42 19 43 24 23 --- 13 | 21 40 30 27 62 35 32 --- 27
R17 | 1582 9 13 24 28 11 10 20 --- 7 | 43 44 28 26 45 35 51 --- 39
R18 | 1429 12 9 27 12 14 12 21 --- 7 | 32 40 33 38 51 41 44 --- 38
XR19 | 1485 29 50 --- 100 52 35 24 --- 23 | 79 95 --- 51 82 52 71 --- 64
R20 | 1839 19 35 124 132 64 47 53 --- 31 | 105 115 68 54 136 106 133 --- 98
R21 | 993 6 7 36 35 26 11 15 81 9 | 64 67 54 49 78 63 72 52 63
XR22 | 2946 --- --- --- --- --- --- 2 --- 0 | --- --- --- --- --- --- 397 --- 397
R23 | 1028 11 11 13 39 8 13 12 --- 7 | 21 22 33 48 22 22 24 --- 24
R24 | 531 6 13 63 45 19 23 25 --- 13 | 54 54 33 32 60 68 65 --- 53
XR26 | 2609 11 80 --- --- --- --- 19 --- 14 | 37 73 --- --- --- --- 30 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1495 15 21 41 42 27 21 22 119 |T 50 55 47 46 58 50 67 47 63
WRMS | 1495 10 14 42 29 16 16 22 119 |NE 49 55 44 42 56 47 74 45 68
MEDI | 1372 9 14 24 22 14 16 17 99 |MD 43 47 42 46 52 46 47 50 42
Table 3.2110.4 GPS week: 2110 Day: 4 MJD: 59018
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 875 32 31 27 66 22 37 32 --- 16 | 66 65 46 53 63 46 64 --- 52
R02 | 1615 7 11 16 15 10 11 25 99 6 | 42 48 39 48 45 41 58 73 43
R03 | 708 9 11 10 16 17 25 14 87 7 | 46 40 43 42 48 62 45 30 47
XR04 | 738 13 17 18 30 --- 14 13 --- 8 | 47 49 49 32 --- 37 45 --- 42
R05 | 647 14 11 17 23 17 12 20 --- 7 | 37 37 43 48 46 35 40 --- 38
R07 | 1030 8 7 12 9 15 11 18 156 5 | 54 54 50 55 64 55 61 40 56
R08 | 1082 10 15 13 12 13 9 15 --- 5 | 54 60 50 58 58 55 58 --- 54
R09E | 3592 11 17 18 13 18 16 27 --- 7 | 48 53 48 52 44 50 47 --- 46
R11E | 1343 7 7 22 7 18 11 20 183 6 | 72 74 77 75 82 78 65 53 74
R12E | 744 8 7 29 22 11 15 20 --- 7 | 45 44 45 49 49 42 43 --- 43
R13E | 2059 20 28 44 39 60 29 38 --- 17 | 50 61 67 57 102 47 52 --- 57
R14E | 2077 10 11 29 24 20 16 18 --- 8 | 53 57 53 70 66 60 47 --- 56
R15E | 1110 12 14 27 22 15 14 13 --- 7 | 94 95 91 95 96 87 98 --- 93
R16E | 1656 20 23 32 20 30 33 24 --- 11 | 41 48 54 50 61 59 49 --- 48
R17 | 1482 8 10 31 35 12 17 20 --- 8 | 50 50 42 42 54 60 55 --- 50
R18 | 796 13 14 19 7 19 15 26 --- 7 | 35 38 39 37 38 45 48 --- 37
R19 | 600 40 46 103 79 51 47 42 --- 26 | 68 73 60 37 63 56 70 --- 51
R20 | 976 29 39 155 146 40 77 54 --- 36 | 99 101 127 60 106 130 110 --- 92
R21 | 1703 16 18 30 34 16 17 23 85 9 | 58 57 44 42 53 54 54 45 50
XR22 | 3990 --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 323 --- 322
R23 | 632 12 16 19 37 12 11 17 --- 8 | 33 34 38 47 40 34 32 --- 33
R24 | 675 10 25 65 51 15 23 31 --- 14 | 64 75 48 46 68 68 71 --- 60
XR26 | 2243 9 35 --- --- --- --- 18 --- 12 | 39 55 --- --- --- --- 41 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1453 17 21 49 46 25 27 27 129 |T 54 57 54 52 62 57 68 48 64
WRMS | 1453 15 18 46 33 14 21 27 129 |NE 52 55 51 46 57 55 73 47 66
MEDI | 1082 11 15 27 23 17 16 20 99 |MD 50 54 48 49 58 55 54 45 50
Table 3.2110.5 GPS week: 2110 Day: 5 MJD: 59019
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1450 25 26 29 58 32 30 25 --- 14 | 64 64 53 42 63 45 61 --- 53
R02 | 1531 9 10 14 17 12 16 33 135 7 | 37 38 32 37 33 32 55 136 34
R03 | 462 8 10 14 16 21 10 10 78 6 | 35 40 34 36 51 35 41 54 37
XR04 | 820 18 20 24 31 --- 12 19 --- 10 | 36 37 35 24 --- 24 33 --- 28
R05 | 631 7 10 24 19 16 9 18 --- 6 | 34 31 37 26 25 30 31 --- 27
R07 | 822 8 8 15 14 24 7 18 151 6 | 45 50 40 47 63 50 52 76 48
R08 | 1074 12 10 16 19 20 7 21 --- 7 | 45 45 47 45 58 51 61 --- 49
R09E | 3989 13 16 23 10 20 14 27 --- 8 | 48 46 48 47 48 51 50 --- 46
R11E | 1372 9 10 18 10 15 15 15 395 6 | 98 97 96 103 103 104 98 103 100
R12E | 649 10 11 27 17 18 15 23 --- 7 | 40 41 37 44 45 34 40 --- 37
R13E | 1556 21 24 43 42 39 16 38 --- 14 | 46 48 50 49 70 49 50 --- 47
R14E | 1559 8 13 26 19 15 12 15 --- 6 | 74 74 74 76 75 76 70 --- 73
R15E | 1491 14 15 28 13 13 12 16 --- 7 | 73 74 70 76 73 75 71 --- 72
R16E | 1604 26 38 27 21 27 25 34 --- 12 | 46 48 43 57 54 54 53 --- 48
R17 | 1084 7 15 39 41 15 12 22 --- 9 | 41 47 30 30 50 46 47 --- 41
R18 | 701 13 13 27 15 24 17 15 --- 8 | 29 30 29 37 42 33 32 --- 31
R19 | 668 27 31 128 86 50 53 53 --- 27 | 55 62 42 33 73 63 78 --- 55
R20 | 810 16 52 87 134 59 24 29 --- 25 | 79 108 89 48 106 77 72 --- 76
R21 | 1800 9 10 43 41 10 16 28 100 10 | 45 46 31 33 38 44 54 74 40
XR22 | 5852 --- --- --- --- --- --- 2 --- 0 | --- --- --- --- --- --- 239 --- 239
R23 | 605 14 14 19 39 14 9 12 --- 8 | 25 33 29 41 31 27 27 --- 26
R24 | 744 11 17 52 50 16 13 28 --- 12 | 54 53 43 45 58 45 55 --- 49
XR26 | 2079 12 49 --- --- --- --- 26 --- 18 | 43 66 --- --- --- --- 25 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1443 15 21 44 45 26 19 26 206 |T 49 53 47 46 57 49 60 88 56
WRMS | 1443 13 16 41 35 17 16 26 206 |NE 44 50 40 37 53 43 60 85 54
MEDI | 1084 12 14 27 19 18 14 22 135 |MD 45 47 42 44 54 46 53 76 47
Table 3.2110.6 GPS week: 2110 Day: 6 MJD: 59020
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1256 31 38 24 58 43 34 22 --- 16 | 82 87 52 33 71 52 73 --- 61
R02 | 1429 6 10 15 20 21 7 15 188 6 | 55 57 44 44 65 48 57 169 52
R03 | 566 8 12 11 14 16 10 20 150 5 | 54 52 52 51 54 61 60 70 54
XR04 | 1404 12 15 20 22 --- 16 11 --- 8 | 52 51 53 31 --- 35 39 --- 42
R05 | 763 9 12 18 21 27 15 16 --- 7 | 40 43 43 38 48 35 40 --- 38
R07 | 657 6 10 14 14 23 18 14 185 6 | 65 62 58 58 79 71 71 218 67
R08 | 1227 10 10 15 10 15 9 21 --- 6 | 62 64 56 59 73 65 75 --- 65
R09E | 4422 11 16 15 13 15 13 19 --- 6 | 38 40 42 41 43 39 42 --- 38
R11E | 2022 7 9 22 7 14 14 15 163 5 | 83 86 91 87 90 88 85 207 86
R12E | 567 12 9 29 17 15 16 23 --- 8 | 30 28 27 28 34 26 31 --- 26
R13E | 1548 20 25 50 48 55 23 35 --- 16 | 51 53 52 50 72 59 52 --- 51
R14E | 2380 12 9 23 12 19 11 10 --- 6 | 87 85 87 79 79 78 82 --- 82
R15E | 1897 9 9 25 21 14 12 17 --- 7 | 109 110 109 115 114 110 106 --- 110
R16E | 2001 25 27 17 24 33 23 32 --- 11 | 40 41 45 41 49 48 48 --- 41
R17 | 1014 13 11 36 39 21 16 20 --- 10 | 66 65 50 45 73 67 70 --- 62
R18 | 973 11 10 28 9 16 14 22 --- 7 | 45 44 39 45 48 48 58 --- 46
R19 | 699 24 16 145 79 49 61 49 --- 29 | 94 95 47 43 107 104 113 --- 85
R20 | 951 33 51 94 119 61 28 51 --- 27 | 137 146 57 45 162 138 144 --- 119
R21 | 861 9 13 39 45 21 13 21 55 10 | 69 70 42 51 78 69 78 83 65
XR22 | 8537 --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 402 --- 402
R23 | 1062 10 15 21 41 22 26 24 --- 10 | 32 31 43 57 33 36 41 --- 32
R24 | 1659 14 9 56 46 24 13 49 --- 14 | 76 78 48 65 90 84 90 --- 74
XR26 | 2880 10 52 --- --- --- --- 17 --- 13 | 48 59 --- --- --- --- 46 --- 46
------+---------------------------------------------------+-----------------------------------------------
RMS | 1644 16 19 47 43 30 22 27 156 |T 64 65 54 52 73 64 82 149 75
WRMS | 1644 12 14 47 38 19 17 27 156 |NE 65 66 48 47 75 65 91 135 81
MEDI | 1256 11 12 23 21 21 15 20 163 |MD 55 59 50 45 72 61 70 169 61
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