[IGSREPORT-28351] Wk 2185 IGLOS Final Orbits
acc
acc at igs.org
Mon Dec 13 02:32:47 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2185 (Nov 21, 2021 - Nov 27, 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 2.2185.
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:
igl2185[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2185 in the SP3 format.
igl21857.sum Combination Report for GPS Week 2185.
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 | -0.6 ns
1 | -1.8 ns
2 | -1.2 ns
3 | -0.8 ns
4 | -1.9 ns
5 | 0.3 ns
6 | 0.2 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 1.2185, 1a.2185).
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 2.2185.0-6)
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 3.2185.0-6).
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 2185 summary. (Nov 21, 2021 - Nov 27, 2021)
Table 1.2185.a GPS week : 2185 MJD: 59539.0-59545.0
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 -5 51 .08 23 18 | 16049 -839 3636 8812
| 0 1 3 17 15 12 .05 | 1527 1892
emx n/a| 0 0 -2 5 38 -34 -.07 41 29 | -2799 -436 3586 8799
| 1 1 1 22 27 57 .03 | 11252 1178
esx n/a| 0 0 4 -5 -3 -11 -.06 35 24 | 375 -1270 3632 9476
| 1 1 1 25 14 25 .02 | 6581 2157
gfz n/a| 0 2 2 -10 -1 -31 -.04 29 18 | 0 -753 3693 8544
| 1 1 1 22 16 35 .07 | 0 1667
grg n/a| 0 -3 -15 -7 -10 31 .23 31 24 | -817 -581 3635 8322
| 1 0 3 14 23 60 .04 | 931 1622
iac n/a| 0 0 4 15 -4 -6 -.13 29 26 | 1054 -735 3633 9281
| 1 2 2 57 34 70 .11 | 1164 1169
mcc n/a| 3 0 6 73 -8 332 -.61 162 162 | --- --- --- ---
| 9 2 17 141 87 560 .28 | --- ---
Table 1.2185.b GPS week : 2185 MJD: 59539.0-59545.0
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 18 13 14 14 15 17 |
R02 | 6 6 7 6 8 7 8 |
R03 | 9 7 10 7 7 7 7 |
R04 | 9 11 9 10 9 8 8 |
R05 | 10 11 10 10 10 8 10 |
R07 | 7 7 7 8 9 6 6 |
R08 | 14 9 7 9 9 6 8 |
R09 | 8 10 8 9 8 8 8 |
R11 | 8 11 9 8 8 10 9 |
R12 | 10 8 9 8 7 8 7 |
R13 | 18 14 16 12 16 21 16 |
R14 | 8 7 8 11 8 7 8 |
R15 | 9 11 8 8 8 8 9 |
R16 | 15 14 12 12 14 10 12 |
R17 | 7 8 9 8 8 8 9 |
R18 | 10 9 11 11 10 8 9 |
R19 | 33 28 28 32 31 29 27 |
R20 | 24 20 20 23 27 27 23 |
R21 | 10 8 8 8 8 8 8 |
R22 | 27 30 30 29 26 26 28 |
R24 | 12 11 12 9 11 9 9 |
Table 1.2185.c GPS week : 2185 MJD: 59539.0-59545.0
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 2185 0 | -24 81 100 -4067 495 2382 82.5 1991 1991 | -555 0
brd 2185 1 | -33 25 35 -715 1373 752 82.5 2071 2071 | -1766 0
brd 2185 2 | -65 -73 15 -536 -1616 -11260 83.2 1813 1813 | -1204 0
brd 2185 3 | 24 -72 -27 2906 -913 -7043 84.4 1762 1762 | -774 0
brd 2185 4 | 176 72 4 2128 -1528 -3822 81.5 1837 1837 | -1946 0
brd 2185 5 | -47 14 -127 -1382 -1832 -423 82.6 1791 1791 | 342 0
brd 2185 6 | 26 21 -90 -3293 141 -1115 82.4 1828 1828 | 210 0
-------------+------------------------------------------------------------+----------------
brd 2185 mean| 8 10 -12 -708 -554 -2932 82.7 1870 1870 | -813 0
brd 2185 sdev| 81 62 77 2567 1234 4803 .9 114 114 | 893 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 2.2185.0 GPS week: 2185 Day: 0 MJD: 59539
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 6 9 4 70 .08 26 21 | 15322 1591 3793 8427
emx n/a| 0 0 -3 1 55 33 -.08 45 26 | -16488 938 3797 8621
esx n/a| 1 -1 4 14 -6 -50 -.07 33 24 | 6639 1994 3790 9944
gfz n/a| 0 4 0 -42 -16 -93 -.13 37 21 | 0 1975 3848 7984
grg n/a| -1 -4 -12 0 -2 48 .27 30 26 | -2002 1973 3810 8135
iac n/a| 1 3 3 3 35 28 .05 32 29 | -2 1370 3808 8934
mcc n/a| 8 -1 -11 -195 -26 1008 -.48 253 253 | --- --- --- ---
Table 2.2185.1 GPS week: 2185 Day: 1 MJD: 59540
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 7 12 6 50 -.00 27 21 | 15775 33 3568 7556
emx n/a| 0 0 0 -14 28 45 -.10 41 29 | 127 778 3555 7824
esx n/a| 2 0 2 36 19 10 -.08 32 22 | -7133 -299 3550 6057
gfz n/a| -2 1 0 10 20 -6 .02 30 25 | 0 145 3602 7411
grg n/a| 1 -4 -13 13 -53 -7 .18 28 23 | -1933 102 3566 7239
iac n/a| 1 0 1 -94 -50 -87 -.08 30 27 | 325 -1066 3528 8114
mcc n/a| -8 2 18 -19 38 397 -.93 96 96 | --- --- --- ---
Table 2.2185.2 GPS week: 2185 Day: 2 MJD: 59541
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 3 1 -8 44 .05 23 17 | 19027 -2860 3061 8020
emx n/a| -1 1 -3 -4 3 -38 -.06 38 29 | -8971 -1610 3052 8498
esx n/a| 0 0 5 5 -1 -9 -.02 34 24 | -8535 -3389 3042 7453
gfz n/a| 0 0 3 -12 16 -40 .03 31 17 | 0 -2776 3100 7838
grg n/a| 0 -3 -17 -23 -18 -46 .21 31 24 | -97 -2358 3036 7332
iac n/a| -2 0 7 47 11 73 -.15 27 27 | 2249 -2053 3049 8650
mcc n/a| -8 1 14 101 111 16 -1.05 108 108 | --- --- --- ---
Table 2.2185.3 GPS week: 2185 Day: 3 MJD: 59542
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 9 17 44 .15 24 19 | 16545 -1237 3852 8481
emx n/a| 0 0 -2 7 34 -63 -.08 44 33 | 5721 -87 3997 8953
esx n/a| 0 0 4 -35 -27 -12 -.05 34 27 | 988 -3229 3896 8616
gfz n/a| -1 4 2 -39 -23 -26 -.07 26 13 | 0 -1670 3964 8454
grg n/a| 1 -3 -14 -25 -22 61 .24 34 21 | 2 -1689 3879 7815
iac n/a| -1 0 5 68 11 14 -.12 31 31 | 989 304 3875 9063
mcc n/a| 14 -3 -5 245 71 -195 -.60 153 153 | --- --- --- ---
Table 2.2185.4 GPS week: 2185 Day: 4 MJD: 59543
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 2 -1 -2 -22 39 .05 20 18 | 14172 -3587 3314 8976
emx n/a| 0 -2 -3 17 84 -64 -.09 33 28 | 4069 -2255 3324 9403
esx n/a| 0 2 4 -16 -5 -22 -.09 32 21 | -2196 -3617 3298 10814
gfz n/a| 1 2 3 11 3 11 -.11 30 18 | 0 -2448 3350 8696
grg n/a| 1 -3 -10 1 1 141 .26 29 22 | -680 -2371 3291 8469
iac n/a| 0 -2 6 -7 -48 -108 -.11 25 23 | -213 -1341 3306 9365
mcc n/a| 8 0 -16 113 -89 -460 -.37 208 208 | --- --- --- ---
Table 2.2185.5 GPS week: 2185 Day: 5 MJD: 59544
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 -21 -15 68 .13 20 17 | 16294 -711 4405 10264
emx n/a| 1 -1 -2 -17 13 -120 -.02 46 31 | 12200 -693 4182 10328
esx n/a| 0 0 7 -20 -11 -25 -.06 40 23 | 7932 -408 4382 11965
gfz n/a| 1 1 4 -1 -6 -55 -.03 25 15 | 0 -8 4478 10020
grg n/a| 0 -3 -17 -14 -2 27 .19 33 24 | 253 -172 4393 9596
iac n/a| 0 2 3 70 28 58 -.22 30 22 | 2909 -1378 4393 10671
mcc n/a| 0 2 15 142 -30 677 -.51 128 128 | --- --- --- ---
Table 2.2185.6 GPS week: 2185 Day: 6 MJD: 59545
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 2 -33 -20 43 .08 21 16 | 15212 896 3464 9962
emx n/a| 3 0 -1 49 53 -32 -.03 43 31 | -16252 -129 3196 7971
esx n/a| 0 0 4 -24 5 29 -.07 39 24 | 4933 54 3472 11484
gfz n/a| 0 2 3 3 -7 -11 .03 25 15 | 0 -490 3510 9406
grg n/a| 0 -4 -20 -4 21 -4 .27 33 25 | -1263 445 3476 9671
iac n/a| 2 0 5 19 -17 -26 -.30 28 26 | 1123 -984 3473 10176
mcc n/a| 8 4 27 124 -132 879 -.32 189 189 | --- --- --- ---
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 3.2185.0 GPS week: 2185 Day: 0 MJD: 59539
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 | 542 43 36 32 48 35 18 --- 16 | 79 69 42 61 48 55 --- 55
R02 | 3291 9 12 11 11 9 25 454 6 | 41 40 35 32 39 29 219 35
R03 | 1142 10 9 17 11 25 38 241 9 | 54 57 61 59 75 61 140 59
XR04 | 761 8 10 19 --- 13 31 --- 9 | 62 66 59 --- 67 57 --- 61
R05 | 987 13 17 21 26 29 27 125 10 | 58 56 73 75 46 67 62 59
R07 | 764 13 8 17 13 20 19 154 7 | 59 64 57 61 58 64 78 59
R08 | 1142 27 23 13 22 28 56 --- 13 | 52 53 64 69 52 87 --- 60
R09E | 3322 16 13 10 27 23 17 --- 8 | 50 52 51 61 52 47 --- 50
R11E | 3251 15 14 15 17 22 24 --- 8 | 29 26 36 38 45 33 --- 33
R12E | 1039 8 28 16 24 27 24 --- 9 | 55 52 58 61 55 58 --- 55
R13E | 2945 33 32 15 76 25 36 --- 17 | 46 37 49 93 58 51 --- 46
R14E | 839 16 20 21 10 11 20 --- 7 | 57 59 68 66 62 66 --- 61
R15E | 4279 10 24 17 16 16 33 265 9 | 56 56 60 57 64 63 226 57
R16E | 2403 19 24 35 53 38 28 --- 15 | 36 38 49 61 55 51 --- 39
R17 | 708 9 26 14 11 11 20 --- 7 | 71 48 66 71 69 72 --- 66
R18 | 958 12 23 29 24 20 21 --- 9 | 56 45 76 52 67 68 --- 59
R19 | 533 41 143 62 62 76 42 --- 33 | 114 56 55 114 99 114 --- 85
R20 | 903 47 92 58 47 30 34 --- 24 | 105 40 39 98 88 99 --- 75
R21 | 850 17 24 13 14 22 34 96 9 | 70 51 58 62 65 83 75 64
R22 | 1961 56 34 90 72 40 47 --- 27 | 48 92 130 63 69 85 --- 73
R24 | 857 16 47 12 14 21 35 --- 11 | 76 55 76 71 71 77 --- 70
------+----------------------------------------------+------------------------------------------
RMS | 1991 26 45 33 37 30 32 253 |T 60 52 60 66 62 66 133 58
WRMS | 1991 21 26 24 21 26 29 253 |NE 67 56 63 68 65 72 114 62
MEDI | 987 16 24 17 22 23 28 154 |MD 56 53 58 61 62 64 78 59
Table 3.2185.1 GPS week: 2185 Day: 1 MJD: 59540
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 | 511 54 33 37 37 41 21 --- 17 | 64 47 41 54 43 44 --- 44
R02 | 3316 6 14 15 8 13 17 113 5 | 29 31 24 27 28 33 220 27
R03 | 1408 12 12 12 15 13 23 91 6 | 39 37 51 39 54 57 82 45
XR04 | 636 19 28 15 --- 15 28 --- 10 | 49 53 44 --- 55 48 --- 47
R05 | 1093 24 29 21 26 21 25 70 11 | 42 47 52 49 48 59 53 46
R07 | 882 13 12 19 11 19 17 124 7 | 48 46 40 53 48 49 77 45
R08 | 1998 21 13 14 23 18 24 --- 8 | 47 47 50 51 51 56 --- 49
R09E | 3206 15 16 14 26 30 28 --- 10 | 32 44 30 48 46 35 --- 36
R11E | 3536 18 20 18 23 30 36 --- 11 | 21 27 28 32 37 40 --- 24
R12E | 1377 9 24 20 10 20 23 --- 8 | 57 53 56 52 58 70 --- 56
R13E | 2933 31 18 30 32 42 20 --- 13 | 43 35 33 41 69 58 --- 42
R14E | 738 7 13 20 23 15 15 --- 7 | 54 52 67 62 57 60 --- 57
R15E | 4705 14 28 12 18 14 48 94 11 | 49 51 47 50 52 60 98 49
R16E | 1663 27 20 35 38 24 34 --- 13 | 38 36 48 56 44 58 --- 39
R17 | 680 10 26 12 14 11 28 --- 8 | 38 31 39 41 38 46 --- 37
R18 | 1200 14 27 29 14 14 18 --- 8 | 40 34 44 33 42 53 --- 39
R19 | 696 56 112 54 62 53 15 --- 28 | 76 58 59 72 54 49 --- 54
R20 | 1113 51 72 56 27 18 25 --- 20 | 58 27 31 43 42 46 --- 36
R21 | 853 12 23 16 11 17 25 68 8 | 38 32 33 40 38 50 50 37
R22 | 1265 38 76 82 76 54 74 --- 30 | 43 69 56 42 47 43 --- 37
R24 | 1353 10 47 18 13 22 27 --- 10 | 42 42 47 43 50 64 --- 45
------+----------------------------------------------+------------------------------------------
RMS | 2070 27 41 32 30 28 30 96 |T 45 42 43 46 47 51 96 42
WRMS | 2070 21 29 22 25 23 27 96 |NE 46 42 43 45 45 49 96 42
MEDI | 1265 15 24 19 23 19 25 91 |MD 43 44 44 43 48 50 77 44
Table 3.2185.2 GPS week: 2185 Day: 2 MJD: 59541
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 | 519 34 19 35 25 32 18 --- 12 | 74 60 42 59 51 55 --- 56
R02 | 1890 8 8 25 12 12 24 188 7 | 35 33 23 26 36 52 90 32
R03 | 1725 12 16 25 14 25 32 71 9 | 37 36 40 41 63 69 66 45
XR04 | 813 8 12 12 --- 15 31 --- 8 | 42 49 43 --- 55 41 --- 44
R05 | 683 16 20 19 21 17 32 82 9 | 41 39 45 39 36 27 26 35
R07 | 815 12 11 16 15 18 15 116 6 | 49 50 53 38 44 44 37 45
R08 | 955 9 8 15 21 19 19 --- 7 | 43 46 45 51 45 51 --- 45
R09E | 3600 15 13 9 18 16 25 --- 7 | 33 35 33 39 29 34 --- 31
R11E | 3206 17 23 7 24 19 25 --- 9 | 25 24 33 38 28 41 --- 29
R12E | 768 7 19 23 20 15 31 --- 9 | 36 31 34 34 41 45 --- 33
R13E | 2812 35 23 36 55 24 31 --- 16 | 31 39 40 77 47 60 --- 40
R14E | 1472 14 14 22 18 16 20 --- 7 | 42 38 43 42 37 43 --- 38
R15E | 3048 15 22 14 16 14 27 80 8 | 37 40 37 47 43 42 61 39
R16E | 1528 14 25 19 37 33 25 --- 11 | 22 21 30 54 34 36 --- 24
R17 | 866 11 31 13 10 17 27 --- 8 | 55 41 52 52 47 65 --- 50
R18 | 1087 10 40 29 15 14 33 --- 11 | 44 27 58 44 51 54 --- 43
R19 | 1088 45 103 56 80 57 22 --- 28 | 81 38 65 111 70 65 --- 66
R20 | 1523 55 59 54 21 32 30 --- 20 | 75 37 29 48 55 59 --- 45
R21 | 893 14 30 19 14 9 18 57 8 | 55 38 46 52 55 55 39 49
R22 | 1408 36 77 91 61 89 37 --- 30 | 42 49 75 47 53 36 --- 37
R24 | 1760 9 43 23 17 24 32 --- 11 | 53 45 55 48 47 60 --- 49
------+----------------------------------------------+------------------------------------------
RMS | 1812 23 38 34 31 31 27 108 |T 45 38 43 49 46 49 53 41
WRMS | 1812 17 29 24 17 24 27 108 |NE 51 42 47 50 50 52 51 45
MEDI | 1408 14 22 22 18 18 27 80 |MD 42 38 43 47 47 51 39 43
Table 3.2185.3 GPS week: 2185 Day: 3 MJD: 59542
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 | 598 42 30 31 21 35 18 --- 14 | 80 65 40 42 33 48 --- 50
R02 | 1279 11 13 9 8 21 16 309 6 | 42 39 36 35 26 31 95 33
R03 | 830 7 11 14 10 14 29 103 6 | 41 41 39 40 50 62 50 43
XR04 | 851 12 12 36 --- 9 19 --- 10 | 45 38 29 --- 42 53 --- 37
R05 | 567 17 15 24 26 22 23 107 9 | 37 36 26 31 44 29 45 28
R07 | 837 10 12 14 13 16 32 138 7 | 53 55 46 48 56 49 40 49
R08 | 1114 21 14 23 15 16 21 --- 8 | 50 50 62 50 47 62 --- 52
R09E | 4266 15 19 10 15 19 32 --- 8 | 31 35 36 38 36 43 --- 34
XR11E | 2789 17 --- 17 15 11 19 --- 8 | 18 --- 29 26 29 29 --- 22
R12E | 986 10 28 13 21 14 16 --- 7 | 34 33 33 36 36 38 --- 32
R13E | 3093 17 32 22 29 29 29 --- 11 | 37 33 37 38 45 33 --- 33
R14E | 1421 16 20 27 28 15 30 --- 10 | 47 47 56 48 51 61 --- 47
R15E | 1498 12 26 14 15 15 24 51 7 | 39 43 41 45 46 45 69 39
R16E | 809 19 20 28 36 26 22 --- 12 | 33 32 42 44 35 34 --- 28
R17 | 1087 9 29 15 8 15 28 --- 7 | 57 35 53 50 58 62 --- 52
R18 | 653 12 32 34 26 12 23 --- 10 | 37 37 55 31 43 46 --- 38
R19 | 1867 41 114 77 58 85 48 --- 31 | 83 35 50 104 76 104 --- 70
R20 | 2670 40 77 60 28 43 63 --- 22 | 89 39 46 71 63 97 --- 62
R21 | 790 13 31 13 11 10 25 42 7 | 56 42 48 51 56 67 54 52
R22 | 1414 53 93 78 44 81 37 --- 29 | 35 70 87 47 51 47 --- 42
R24 | 2345 18 35 14 13 15 29 --- 9 | 52 35 52 41 48 62 --- 47
------+----------------------------------------------+------------------------------------------
RMS | 1761 24 44 34 26 34 31 153 |T 47 42 44 45 46 52 58 42
WRMS | 1761 19 33 27 13 21 31 153 |NE 54 44 47 49 49 58 56 46
MEDI | 1114 16 26 22 15 16 25 103 |MD 42 38 42 42 46 48 50 42
Table 3.2185.4 GPS week: 2185 Day: 4 MJD: 59543
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 | 486 28 38 28 37 33 24 --- 14 | 60 64 58 62 39 44 --- 52
R02 | 1005 14 19 14 19 19 13 378 7 | 37 39 35 36 23 27 175 31
R03 | 642 8 15 11 12 12 26 209 6 | 45 46 38 38 38 57 102 42
XR04 | 823 16 9 28 --- 13 16 --- 9 | 46 38 22 --- 41 45 --- 37
R05 | 801 15 16 25 24 25 24 134 9 | 30 34 38 34 54 38 66 33
R07 | 825 15 16 15 13 16 32 201 8 | 49 49 42 42 40 28 81 40
R08 | 941 16 17 26 12 17 28 --- 9 | 48 48 63 53 64 43 --- 50
R09E | 4919 16 14 12 19 18 20 --- 7 | 30 35 32 37 30 35 --- 30
R11E | 2155 14 22 12 17 16 24 --- 8 | 15 23 26 34 28 30 --- 22
R12E | 638 8 25 9 16 16 15 --- 6 | 43 42 46 47 50 37 --- 42
R13E | 2439 22 41 31 51 38 25 --- 15 | 48 44 59 62 40 38 --- 41
R14E | 1628 10 16 25 17 17 23 --- 8 | 44 37 48 37 45 43 --- 39
R15E | 2039 10 25 16 12 18 20 117 7 | 33 35 33 38 45 39 87 34
R16E | 2070 19 32 23 53 26 26 --- 13 | 28 23 43 81 29 39 --- 34
R17 | 1311 7 31 14 11 14 25 --- 8 | 50 39 48 54 61 63 --- 51
R18 | 1111 18 25 30 16 14 20 --- 9 | 37 31 47 46 50 48 --- 41
XR19 | 3198 53 --- 84 42 81 36 --- 30 | 66 --- 54 78 59 75 --- 61
R20 | 2338 29 87 86 45 57 50 --- 26 | 82 30 40 101 113 89 --- 73
R21 | 832 19 25 10 14 15 19 39 8 | 47 33 44 35 43 48 81 41
R22 | 1363 50 43 75 64 75 23 --- 25 | 38 77 78 30 62 56 --- 47
R24 | 1723 22 36 13 22 20 25 --- 10 | 51 35 46 63 44 54 --- 47
------+----------------------------------------------+------------------------------------------
RMS | 1836 20 33 32 30 29 25 208 |T 44 40 44 50 47 46 98 42
WRMS | 1836 18 28 21 18 22 23 208 |NE 49 43 46 51 52 51 101 46
MEDI | 1311 16 25 23 17 18 24 134 |MD 45 37 44 42 44 43 81 41
Table 3.2185.5 GPS week: 2185 Day: 5 MJD: 59544
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 | 1031 36 43 36 28 20 33 --- 14 | 55 52 28 38 38 26 --- 36
R02 | 2234 10 14 20 9 16 21 138 6 | 30 29 31 21 25 24 125 23
R03 | 658 11 17 15 18 20 17 91 7 | 38 41 32 25 42 39 38 33
XR04 | 497 15 12 19 --- 14 19 --- 8 | 59 51 46 --- 45 48 --- 50
R05 | 568 13 23 17 22 15 16 67 8 | 35 35 37 39 38 37 64 34
R07 | 1758 7 11 13 14 8 22 213 6 | 38 41 47 41 49 50 77 41
R08 | 879 8 10 17 11 14 17 --- 5 | 40 39 41 37 43 41 --- 38
R09E | 4770 14 16 10 18 23 23 --- 8 | 28 33 29 37 37 32 --- 29
XR11E | 2797 15 --- 14 18 16 34 --- 10 | 18 --- 25 25 27 25 --- 20
R12E | 744 14 33 11 13 15 22 --- 8 | 46 44 43 43 41 48 --- 42
R13E | 2475 33 61 52 53 43 37 --- 20 | 50 28 50 85 49 50 --- 46
R14E | 1045 12 22 18 10 12 21 --- 7 | 53 44 60 56 56 63 --- 54
R15E | 1394 12 27 13 17 17 22 81 7 | 52 51 51 44 51 60 135 50
R16E | 1131 11 23 25 28 25 22 --- 10 | 28 24 33 39 34 46 --- 29
R17 | 1601 8 32 23 16 12 17 --- 8 | 47 40 39 53 44 47 --- 44
R18 | 1346 12 29 25 9 16 22 --- 8 | 35 32 43 38 43 43 --- 37
R19 | 2505 40 122 68 39 83 31 --- 28 | 46 61 43 46 35 49 --- 35
R20 | 1478 24 94 105 27 55 55 --- 26 | 70 40 48 78 97 104 --- 70
R21 | 706 10 33 15 10 15 25 124 8 | 41 31 39 41 53 55 58 42
R22 | 1566 36 55 81 51 69 67 --- 26 | 41 54 74 54 42 57 --- 42
R24 | 861 18 38 11 20 15 18 --- 9 | 50 41 42 31 47 45 --- 41
------+----------------------------------------------+------------------------------------------
RMS | 1791 20 46 40 25 33 30 128 |T 42 40 41 43 44 47 82 39
WRMS | 1791 17 31 23 15 24 22 128 |NE 44 41 42 41 45 47 72 40
MEDI | 1346 13 27 18 18 16 22 91 |MD 41 40 42 39 43 47 64 41
Table 3.2185.6 GPS week: 2185 Day: 6 MJD: 59545
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 | 787 42 31 52 28 44 19 --- 17 | 88 74 45 56 51 54 --- 59
R02 | 1834 10 14 24 9 9 29 190 7 | 45 43 44 39 40 35 64 38
R03 | 768 8 17 19 12 18 17 92 6 | 61 59 59 55 71 62 56 59
XR04 | 719 15 14 16 --- 14 18 --- 7 | 86 77 73 --- 76 73 --- 77
R05 | 570 16 25 20 29 13 31 58 10 | 56 58 52 44 51 56 47 50
R07 | 1397 9 16 7 17 11 16 387 5 | 60 59 60 62 64 64 73 59
R08 | 947 14 17 29 15 14 16 --- 7 | 52 53 74 60 62 64 --- 59
R09E | 3994 15 16 13 14 24 26 --- 8 | 49 55 52 60 58 50 --- 52
XR11E | 4247 16 --- 11 13 17 30 --- 9 | 34 --- 37 46 43 48 --- 38
R12E | 618 9 28 14 8 12 22 --- 7 | 45 40 49 45 44 44 --- 43
R13E | 3469 31 49 30 40 34 31 --- 16 | 58 40 52 55 61 48 --- 47
R14E | 1287 12 24 11 18 18 20 --- 7 | 68 55 68 70 71 64 --- 66
R15E | 1273 12 30 19 22 11 18 67 8 | 57 55 51 60 57 64 96 56
R16E | 1591 15 30 24 31 23 31 --- 11 | 31 30 48 52 40 46 --- 35
R17 | 1266 9 33 19 12 11 31 --- 8 | 74 54 64 75 68 89 --- 70
R18 | 879 11 26 20 10 17 32 --- 8 | 58 46 70 54 62 71 --- 58
R19 | 1981 37 117 61 43 74 34 --- 27 | 101 44 40 105 85 96 --- 77
R20 | 1729 34 77 90 24 39 46 --- 23 | 117 55 50 100 112 122 --- 92
R21 | 3104 15 29 16 12 18 21 116 8 | 72 49 62 64 79 74 53 67
R22 | 1221 26 63 95 54 86 49 --- 28 | 49 79 114 55 53 57 --- 55
R24 | 1073 18 28 17 17 15 24 --- 8 | 80 63 81 73 67 73 --- 72
------+----------------------------------------------+------------------------------------------
RMS | 1828 21 43 39 25 33 28 189 |T 63 54 59 61 62 64 64 58
WRMS | 1828 16 31 24 15 25 26 189 |NE 71 58 63 64 67 70 58 63
MEDI | 1273 15 28 19 17 17 26 92 |MD 58 55 52 56 62 64 56 59
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