[IGSREPORT-28220] Wk 2176 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 8 01:05:38 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2176 (Sep 19, 2021 - Sep 25, 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 2.2176.
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:
igl2176[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2176 in the SP3 format.
igl21767.sum Combination Report for GPS Week 2176.
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 | -2.1 ns
1 | -2.0 ns
2 | -3.9 ns
3 | -1.6 ns
4 | -1.0 ns
5 | -1.1 ns
6 | -1.4 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 1.2176, 1a.2176).
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 2.2176.0-6)
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 3.2176.0-6).
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 2176 summary. (Sep 19, 2021 - Sep 25, 2021)
Table 1.2176.a GPS week : 2176 MJD: 59476.0-59482.0
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 1 -3 -6 2 -30 .11 22 17 | 14345 -1298 3274 8307
| 1 0 2 13 17 19 .04 | 1104 1732
emx n/a| 0 2 15 22 -8 -51 -.02 36 32 | -7204 -1036 3305 8872
| 2 1 1 18 16 50 .04 | 8516 1246
esx n/a| 0 2 4 32 10 19 -.15 29 22 | -2002 -425 3276 8728
| 0 1 1 12 19 24 .04 | 3295 2267
gfz n/a| 0 0 -6 17 -3 7 .00 31 19 | 0 -1406 3346 8114
| 1 1 3 15 17 24 .04 | 0 1667
grg n/a| 2 -1 4 -27 6 -94 .29 26 20 | -1441 -1252 3335 7994
| 0 1 3 18 18 39 .05 | 872 1642
iac n/a| -1 -5 -11 -22 -23 210 -.28 29 29 | 363 -706 3279 8864
| 3 2 3 24 39 63 .06 | 1270 570
mcc n/a| 1 -4 21 -16 -92 193 -.47 167 167 | --- --- --- ---
| 10 7 13 84 104 768 .44 | --- ---
Table 1.2176.b GPS week : 2176 MJD: 59476.0-59482.0
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 | 21 22 21 20 18 19 19 |
R02 | 8 9 14 8 9 8 8 |
R03 | 8 7 8 10 11 12 7 |
R04 | 10 9 9 12 10 10 13 |
R05 | 9 9 11 9 8 10 11 |
R07 | 10 7 7 9 8 6 8 |
R08 | 9 11 10 9 8 8 8 |
R09 | 7 9 7 7 8 7 9 |
R11 | 14 17 11 8 9 9 11 |
R12 | 10 12 8 9 10 9 8 |
R13 | 13 15 17 15 14 17 15 |
R14 | 8 9 6 6 6 6 7 |
R15 | 8 8 8 8 9 7 7 |
R16 | 17 19 15 13 13 15 16 |
R17 | 10 8 8 8 8 7 7 |
R18 | 10 11 9 8 7 7 7 |
R19 | 22 20 18 18 20 18 21 |
R20 | 21 24 21 22 19 22 22 |
R21 | 10 10 11 10 10 9 8 |
R22 | 24 17 19 19 19 19 23 |
R24 | 10 8 8 10 10 9 9 |
Table 1.2176.c GPS week : 2176 MJD: 59476.0-59482.0
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 2176 0 | -35 8 58 1889 -1364 -2623 81.0 1215 1215 | -2090 0
brd 2176 1 | -24 -49 24 1544 -516 -18 82.8 1202 1202 | -2043 0
brd 2176 2 | -3 30 49 1246 -1016 1679 84.5 1273 1273 | -3936 0
brd 2176 3 | -3 17 81 449 -2748 -1969 83.4 1454 1454 | -1569 0
brd 2176 4 | -28 45 45 441 -1152 -2703 82.6 1676 1676 | -1008 0
brd 2176 5 | 8 -54 32 -125 -1114 -1300 85.0 1752 1752 | -1100 0
brd 2176 6 | 43 -2 17 -159 1920 -1060 84.9 1650 1650 | -1442 0
-------------+------------------------------------------------------------+----------------
brd 2176 mean| -6 0 44 754 -855 -1142 83.5 1460 1460 | -1884 0
brd 2176 sdev| 27 38 21 811 1404 1558 1.4 234 234 | 996 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 2.2176.0 GPS week: 2176 Day: 0 MJD: 59476
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -1 -14 16 -34 .11 27 20 | 14529 569 3685 7941
emx n/a| 0 1 15 44 -42 -46 -.06 33 31 | -17584 736 3749 8473
esx n/a| 0 0 5 18 5 7 -.15 28 20 | -4287 1681 3671 9723
gfz n/a| 1 -1 -9 33 -25 18 -.03 33 19 | 0 274 3777 7673
grg n/a| 1 0 0 -34 30 -113 .32 25 18 | -2365 438 3760 7752
iac n/a| 1 0 -12 -43 -25 240 -.22 33 33 | 845 -1626 3671 8316
mcc n/a| 1 5 28 36 -10 -250 -.25 199 199 | --- --- --- ---
Table 2.2176.1 GPS week: 2176 Day: 1 MJD: 59477
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 -29 .05 24 19 | 16261 -196 3152 8365
emx n/a| 3 1 18 32 -11 45 -.02 43 37 | -4044 -296 3242 9072
esx n/a| 0 0 7 40 -19 27 -.13 31 21 | -4369 1184 3164 6584
gfz n/a| 0 0 -9 15 7 41 .05 25 15 | 0 293 3234 8176
grg n/a| 2 0 0 -44 -7 -66 .35 30 25 | -2468 295 3194 7990
iac n/a| -5 -7 -8 -41 -6 81 -.27 31 31 | 227 -875 3169 8950
mcc n/a| 11 -15 18 3 38 -870 -.87 194 194 | --- --- --- ---
Table 2.2176.2 GPS week: 2176 Day: 2 MJD: 59478
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 -3 -7 5 -15 .09 21 17 | 14956 -4731 3110 8009
emx n/a| 0 4 18 -5 -2 -30 -.06 39 32 | -1431 -2881 3154 8793
esx n/a| 1 4 2 51 18 5 -.19 29 21 | 2344 -5041 3096 10253
gfz n/a| 1 0 -11 6 14 26 -.03 26 17 | 0 -4443 3165 7878
grg n/a| 2 -1 10 -35 -11 -85 .35 30 25 | -1938 -4261 3137 7905
iac n/a| -6 -5 -7 -7 -70 175 -.25 32 32 | -2358 -671 3106 8653
mcc n/a| 0 -1 1 -193 13 -579 -1.13 176 176 | --- --- --- ---
Table 2.2176.3 GPS week: 2176 Day: 3 MJD: 59479
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 -6 -13 -28 -45 .17 20 15 | 13980 -637 3167 8330
emx n/a| -1 4 15 31 0 -83 -.01 32 29 | 1159 -548 3175 8856
esx n/a| 2 3 3 36 31 45 -.18 30 21 | -5141 279 3168 8330
gfz n/a| -2 1 -5 35 -9 8 .00 31 20 | 0 -1034 3234 7921
grg n/a| 2 -2 5 -49 8 -79 .29 26 20 | -1614 -505 3247 8126
iac n/a| 1 -7 -7 -43 -12 247 -.39 28 28 | 335 58 3175 8963
mcc n/a| -20 -2 5 -55 -194 375 -.38 152 152 | --- --- --- ---
Table 2.2176.4 GPS week: 2176 Day: 4 MJD: 59480
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 -6 -22 -8 0 .11 20 16 | 14061 -582 3243 7838
emx n/a| -3 1 13 32 3 -104 -.03 33 31 | -15541 -406 3240 8353
esx n/a| 1 1 3 16 -6 -11 -.09 24 19 | -4593 788 3250 10138
gfz n/a| -1 1 -3 27 -28 -13 .02 34 20 | 0 -781 3330 7601
grg n/a| 3 0 6 -5 12 -75 .29 24 18 | -752 -761 3286 7554
iac n/a| -2 -8 -11 0 44 260 -.33 30 30 | 1048 -406 3246 8404
mcc n/a| 11 -12 27 40 -135 670 -.65 137 137 | --- --- --- ---
Table 2.2176.5 GPS week: 2176 Day: 5 MJD: 59481
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 -10 -2 -28 .12 19 16 | 13994 -1478 3575 9018
emx n/a| -2 1 15 1 2 -90 .04 35 32 | -14971 -1894 3593 9535
esx n/a| 0 1 5 28 7 5 -.17 31 29 | 425 -822 3603 8801
gfz n/a| 0 3 -6 -2 13 -30 .05 31 20 | 0 -1678 3665 8926
grg n/a| 3 -1 5 -5 -13 -65 .23 24 16 | -320 -2026 3667 8244
iac n/a| -2 -6 -16 16 -22 220 -.26 28 28 | 1022 -266 3585 9633
mcc n/a| 3 0 37 14 -133 877 .09 148 148 | --- --- --- ---
Table 2.2176.6 GPS week: 2176 Day: 6 MJD: 59482
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 -3 19 13 -62 .13 21 16 | 12639 -2036 2991 8653
emx n/a| 0 0 14 22 -11 -50 -.03 35 31 | 1978 -1967 2986 9023
esx n/a| 1 4 5 31 35 55 -.10 33 23 | 1605 -1046 2981 7272
gfz n/a| 0 0 -2 4 2 3 -.04 38 22 | 0 -2478 3019 8626
grg n/a| 2 -2 5 -16 29 -176 .22 23 19 | -636 -1949 3059 8388
iac n/a| 0 -4 -12 -37 -69 247 -.23 23 23 | 1426 -1162 3002 9132
mcc n/a| 0 -3 32 37 -221 1135 -.10 165 165 | --- --- --- ---
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 3.2176.0 GPS week: 2176 Day: 0 MJD: 59476
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 | 641 57 58 58 15 32 33 --- 20 | 131 52 51 104 114 105 --- 91
R02 | 825 15 31 9 12 15 15 181 7 | 88 58 72 85 86 82 72 78
R03 | 535 9 28 15 11 16 23 156 7 | 93 63 76 92 92 96 29 85
XR04 | 911 12 26 12 --- 17 33 --- 10 | 97 72 91 --- 95 94 --- 90
R05 | 977 16 27 17 12 13 29 71 8 | 81 55 71 71 65 81 24 70
R07 | 680 18 24 17 14 24 34 183 10 | 98 68 78 85 100 81 97 85
R08 | 1313 14 34 11 14 10 36 --- 9 | 89 59 78 97 90 104 --- 85
R09 | 1623 14 9 10 14 14 28 --- 7 | 29 36 39 38 31 42 --- 33
XR11 | 1127 28 --- 21 12 --- 32 --- 14 | 29 --- 47 34 --- 43 --- 33
R12 | 476 14 16 28 9 27 24 --- 9 | 69 72 71 74 84 67 --- 70
R13 | 2909 28 21 38 23 33 20 --- 13 | 79 74 52 68 71 71 --- 66
R14 | 923 12 11 21 14 14 30 --- 7 | 54 51 62 51 58 58 --- 54
R15 | 882 11 21 11 24 11 30 166 8 | 74 73 81 93 85 71 67 79
R16 | 1104 32 34 29 29 42 53 --- 16 | 49 63 66 66 62 81 --- 58
R17E | 1316 15 31 14 23 14 28 --- 9 | 129 125 130 132 129 139 --- 129
R18E | 984 15 26 17 34 15 26 --- 10 | 75 74 79 90 74 76 --- 76
R19E | 998 36 54 33 68 38 60 --- 21 | 52 75 66 67 73 75 --- 57
R20E | 1074 45 52 41 58 50 35 --- 21 | 69 91 77 85 77 92 --- 73
R21E | 911 13 30 15 30 14 27 340 9 | 78 80 81 85 79 81 163 79
R22E | 1301 52 35 58 77 33 42 --- 23 | 43 53 76 67 66 83 --- 50
R24E | 1402 14 37 11 26 12 25 --- 9 | 100 99 100 101 100 109 --- 100
------+----------------------------------------------+------------------------------------------
RMS | 1214 27 33 28 33 25 33 199 |T 76 69 73 79 81 82 75 73
WRMS | 1214 20 31 20 19 18 33 199 |NE 75 61 66 73 79 76 57 69
MEDI | 984 15 28 17 15 15 30 166 |MD 78 68 76 85 79 81 67 76
Table 3.2176.1 GPS week: 2176 Day: 1 MJD: 59477
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 | 875 46 57 75 23 38 42 --- 21 | 96 49 53 72 100 100 --- 74
R02 | 794 10 45 18 14 13 27 178 9 | 67 56 55 64 66 73 35 62
R03 | 618 16 22 15 10 10 25 150 7 | 73 55 55 68 66 54 26 62
XR04 | 595 11 25 15 --- 22 19 --- 9 | 74 59 78 --- 73 74 --- 72
R05 | 794 14 35 20 21 20 16 63 9 | 71 53 68 72 57 64 25 64
R07 | 1104 9 26 19 13 17 16 185 7 | 68 58 58 66 77 67 61 65
R08 | 683 14 47 15 22 12 35 --- 11 | 66 46 64 86 80 92 --- 72
R09 | 2551 15 24 8 14 18 38 --- 9 | 31 36 41 44 36 54 --- 37
XR11 | 790 30 --- 19 18 --- 44 --- 16 | 30 --- 48 38 --- 52 --- 36
R12 | 1189 9 20 30 15 30 46 --- 11 | 60 70 57 59 62 77 --- 58
R13 | 2085 19 33 37 25 53 24 --- 14 | 53 52 27 46 62 35 --- 43
R14 | 817 10 15 20 11 19 37 --- 8 | 44 48 40 46 37 59 --- 43
R15 | 773 13 15 8 12 9 38 132 7 | 58 57 57 58 58 36 50 53
R16 | 1117 36 68 28 31 62 21 --- 18 | 40 86 62 66 68 40 --- 55
R17E | 843 10 28 11 19 15 25 --- 8 | 114 115 122 120 117 116 --- 116
R18E | 1134 15 26 18 25 24 31 --- 10 | 80 78 82 87 79 77 --- 79
R19E | 1382 27 58 38 58 36 46 --- 19 | 65 77 71 76 72 56 --- 61
R20E | 1151 50 99 50 43 55 29 --- 24 | 78 102 81 81 73 62 --- 68
R21E | 1020 19 37 20 27 15 18 340 10 | 87 86 86 94 91 84 128 86
R22E | 1026 45 37 51 29 27 30 --- 17 | 61 72 76 85 77 71 --- 68
R24E | 1117 13 37 14 16 14 18 --- 8 | 91 99 99 99 100 93 --- 95
------+----------------------------------------------+------------------------------------------
RMS | 1202 24 43 31 25 30 31 194 |T 67 67 65 71 72 68 54 65
WRMS | 1202 19 37 21 15 25 31 194 |NE 59 55 54 60 64 62 39 56
MEDI | 1020 15 33 19 19 19 29 150 |MD 67 58 62 68 72 67 35 64
Table 3.2176.2 GPS week: 2176 Day: 2 MJD: 59478
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 | 773 34 67 70 16 30 48 --- 20 | 101 53 67 93 92 106 --- 82
R02 | 1133 9 48 30 15 15 59 192 14 | 69 40 55 87 82 124 62 75
R03 | 582 11 28 16 14 17 23 145 8 | 72 44 58 76 70 61 34 64
XR04 | 875 13 23 16 --- 17 21 --- 8 | 71 47 62 --- 48 81 --- 63
R05 | 1356 15 32 19 25 26 24 66 10 | 67 39 68 80 43 43 34 58
R07 | 1264 12 23 15 14 14 19 188 7 | 74 50 64 61 68 82 70 66
R08 | 1051 11 37 19 21 16 26 --- 9 | 69 43 63 86 67 72 --- 68
R09 | 2361 11 13 14 15 18 22 --- 7 | 26 31 28 34 41 41 --- 30
XR11 | 1542 12 --- 16 19 --- 31 --- 11 | 29 --- 44 42 --- 40 --- 35
R12 | 867 12 17 22 9 24 19 --- 7 | 59 67 51 55 70 64 --- 58
R13 | 2393 30 51 27 33 47 46 --- 17 | 49 47 43 48 48 44 --- 39
R14 | 581 11 14 15 13 16 13 --- 6 | 38 39 48 47 54 38 --- 42
R15 | 762 12 15 31 16 15 15 121 8 | 50 55 42 54 48 54 37 48
R16 | 1432 27 42 23 14 63 26 --- 15 | 36 37 56 49 89 33 --- 47
R17E | 827 10 26 12 21 13 28 --- 8 | 47 45 48 55 52 45 --- 46
R18E | 1588 16 24 20 21 20 21 --- 9 | 33 24 38 33 38 46 --- 32
R19E | 1023 28 54 29 53 39 31 --- 17 | 46 48 53 60 59 41 --- 42
R20E | 846 31 80 38 44 55 40 --- 21 | 46 48 61 56 51 45 --- 40
R21E | 702 15 33 16 26 21 39 271 11 | 43 38 40 46 45 43 68 39
R22E | 1612 42 32 46 50 27 38 --- 18 | 35 45 50 57 47 41 --- 38
R24E | 957 15 33 16 14 18 19 --- 8 | 42 45 41 42 51 43 --- 40
------+----------------------------------------------+------------------------------------------
RMS | 1272 21 39 29 26 30 32 176 |T 52 44 51 58 58 56 50 50
WRMS | 1272 17 32 21 17 25 32 176 |NE 57 45 53 62 63 63 47 55
MEDI | 1023 13 32 19 16 18 26 145 |MD 47 45 51 55 51 45 37 46
Table 3.2176.3 GPS week: 2176 Day: 3 MJD: 59479
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 | 948 34 58 69 33 34 24 --- 19 | 112 47 64 114 109 96 --- 90
R02 | 1171 9 33 15 10 16 25 155 8 | 84 56 71 80 81 93 73 78
R03 | 784 13 24 16 25 16 35 128 9 | 85 59 68 65 86 85 28 74
XR04 | 1600 16 26 32 --- 18 24 --- 11 | 78 57 72 --- 65 76 --- 68
R05 | 1183 15 28 25 19 21 17 76 9 | 72 50 77 77 54 66 23 65
R07 | 1428 12 25 16 25 12 29 184 9 | 82 53 66 82 75 78 36 73
R08 | 791 7 31 8 22 19 26 --- 8 | 80 53 76 95 81 84 --- 78
R09 | 2776 15 14 14 16 15 17 --- 6 | 25 24 34 33 30 28 --- 26
XR11 | 1141 11 18 17 14 --- 19 --- 7 | 28 29 37 41 --- 46 --- 33
R12 | 954 13 29 21 11 21 27 --- 9 | 60 53 64 64 78 81 --- 65
R13 | 2495 30 24 32 24 40 38 --- 14 | 60 45 58 56 57 55 --- 52
R14 | 704 7 13 22 13 6 16 --- 6 | 47 47 52 53 51 58 --- 50
R15 | 729 12 14 34 13 9 20 135 8 | 56 55 52 64 63 72 58 58
R16 | 1870 16 30 23 20 52 23 --- 13 | 46 55 51 44 53 48 --- 46
R17E | 2204 14 25 16 18 13 19 --- 7 | 37 35 37 38 44 41 --- 35
R18E | 2086 12 25 18 12 20 18 --- 8 | 38 38 41 42 49 53 --- 40
R19E | 1037 30 36 27 61 33 41 --- 17 | 56 53 61 85 70 53 --- 56
R20E | 910 26 61 43 76 44 35 --- 21 | 52 71 61 92 62 49 --- 54
R21E | 1156 12 33 19 26 18 27 200 10 | 47 41 39 50 49 44 94 43
R22E | 907 41 30 55 48 29 44 --- 19 | 32 37 61 54 58 49 --- 38
R24E | 751 8 33 16 19 20 31 --- 9 | 44 48 50 48 58 43 --- 45
------+----------------------------------------------+------------------------------------------
RMS | 1454 20 32 30 31 26 28 152 |T 58 47 56 63 63 61 52 55
WRMS | 1454 15 29 21 20 20 28 152 |NE 65 48 60 66 67 69 43 61
MEDI | 1141 13 28 21 19 19 25 135 |MD 56 50 61 56 58 55 36 54
Table 3.2176.4 GPS week: 2176 Day: 4 MJD: 59480
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 | 910 41 40 58 28 20 22 --- 17 | 110 58 44 97 87 79 --- 79
R02 | 1823 13 30 13 19 11 29 90 8 | 78 55 62 82 72 57 88 67
R03 | 643 10 35 23 20 20 36 97 10 | 77 53 68 70 83 99 43 74
XR04 | 1209 15 27 17 --- 20 22 --- 9 | 79 58 76 --- 62 79 --- 71
R05 | 1067 20 25 13 13 13 15 90 7 | 77 51 64 60 60 62 22 63
R07 | 2057 9 29 13 16 12 24 181 7 | 75 56 69 79 76 71 66 71
R08 | 1144 8 32 11 21 15 19 --- 7 | 74 49 69 86 78 77 --- 72
R09 | 2018 15 21 16 16 20 19 --- 8 | 24 32 26 29 20 35 --- 23
XR11 | 1732 13 16 16 15 --- 25 --- 8 | 24 19 40 36 --- 34 --- 29
R12 | 605 14 43 9 29 17 27 --- 10 | 49 40 62 80 61 72 --- 57
R13 | 3278 30 36 34 42 20 27 --- 14 | 55 51 50 62 53 70 --- 53
R14 | 742 9 21 7 9 9 22 --- 5 | 41 35 35 36 34 43 --- 36
R15 | 736 10 17 21 22 18 28 143 8 | 57 51 52 64 68 76 56 59
R16 | 3373 17 24 14 24 53 23 --- 12 | 35 47 48 43 47 47 --- 40
R17E | 2325 9 28 12 17 19 28 --- 8 | 53 54 54 59 54 48 --- 52
R18E | 1394 8 19 18 17 14 17 --- 6 | 33 30 40 37 40 37 --- 33
R19E | 824 37 40 26 75 34 47 --- 19 | 49 40 36 76 48 28 --- 35
R20E | 1146 26 53 28 61 38 52 --- 18 | 43 48 40 72 52 70 --- 39
R21E | 1632 12 32 17 34 19 22 185 10 | 45 44 43 56 47 51 103 44
R22E | 1314 32 35 46 57 32 51 --- 19 | 25 30 51 49 51 40 --- 28
R24E | 837 7 40 14 29 18 22 --- 9 | 40 39 37 46 45 47 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1675 20 33 24 34 24 30 137 |T 54 44 50 60 56 58 63 50
WRMS | 1675 16 31 19 20 18 30 137 |NE 61 46 54 63 61 64 55 56
MEDI | 1209 13 30 16 21 19 24 97 |MD 49 48 50 60 53 57 56 52
Table 3.2176.5 GPS week: 2176 Day: 5 MJD: 59481
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 | 1070 31 68 68 37 23 24 --- 19 | 109 56 63 123 103 100 --- 94
R02 | 1901 9 29 20 16 18 16 107 8 | 80 67 64 85 86 88 32 78
R03 | 589 8 34 31 14 19 43 114 11 | 76 57 65 72 87 98 22 75
XR04 | 716 12 24 17 --- 18 31 --- 10 | 77 70 74 --- 73 95 --- 77
R05 | 644 25 28 20 17 19 14 101 9 | 80 52 58 49 59 53 22 59
R07 | 1915 11 24 13 10 10 14 168 6 | 75 56 65 69 70 81 72 70
R08 | 1232 9 28 14 18 16 21 --- 7 | 71 54 77 77 75 69 --- 70
R09 | 1823 13 11 19 14 8 20 --- 6 | 21 28 34 34 31 42 --- 28
XR11 | 1309 13 17 19 20 --- 17 --- 8 | 22 23 36 33 --- 34 --- 26
R12 | 675 13 25 9 13 22 29 --- 8 | 55 47 61 56 61 65 --- 56
R13 | 4691 26 36 46 48 34 37 --- 16 | 47 46 32 64 32 69 --- 44
R14 | 705 7 24 16 10 11 8 --- 5 | 41 35 49 43 36 41 --- 39
R15 | 913 10 17 16 19 9 18 125 6 | 53 53 43 54 49 54 45 50
R16 | 2713 24 33 23 35 48 21 --- 14 | 41 34 41 37 40 48 --- 36
R17E | 2329 11 29 14 19 12 14 --- 7 | 109 106 107 108 112 112 --- 108
R18E | 1484 8 22 15 17 16 17 --- 7 | 78 78 80 84 75 80 --- 77
R19E | 966 42 49 29 44 31 48 --- 18 | 63 61 56 88 60 60 --- 57
R20E | 999 28 60 51 75 46 41 --- 22 | 64 69 74 84 66 57 --- 60
R21E | 1248 6 34 17 21 14 21 229 8 | 81 78 81 83 75 78 136 77
R22E | 1026 27 27 61 46 28 53 --- 18 | 46 52 78 75 75 65 --- 56
R24E | 980 9 37 15 17 16 18 --- 8 | 90 92 95 99 100 93 --- 93
------+----------------------------------------------+------------------------------------------
RMS | 1752 19 35 31 31 24 28 148 |T 65 57 63 70 68 70 54 63
WRMS | 1752 16 32 29 20 16 28 148 |NE 60 48 54 61 61 66 38 57
MEDI | 1070 12 28 19 18 18 21 114 |MD 71 56 64 72 70 69 32 60
Table 3.2176.6 GPS week: 2176 Day: 6 MJD: 59482
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 | 648 32 60 69 46 21 29 --- 19 | 142 72 65 146 117 132 --- 113
R02 | 2224 8 35 14 17 16 16 143 8 | 104 78 93 104 112 112 72 101
R03 | 758 13 24 19 10 15 16 138 7 | 106 79 85 98 107 102 35 97
XR04 | 611 9 27 28 --- 16 38 --- 12 | 111 90 93 --- 104 136 --- 107
R05 | 705 20 34 29 21 14 24 154 10 | 99 62 73 73 90 90 25 82
R07 | 1622 15 20 16 14 12 20 176 7 | 95 67 77 82 87 88 98 84
R08 | 2416 7 30 16 16 18 14 --- 7 | 90 61 84 104 98 99 --- 90
R09 | 1524 20 15 19 16 9 27 --- 8 | 33 42 44 44 41 52 --- 40
XR11 | 1006 16 13 26 16 --- 27 --- 10 | 31 22 45 42 --- 51 --- 36
R12 | 677 16 11 20 12 17 20 --- 7 | 71 70 67 76 86 83 --- 75
R13 | 4447 21 31 44 48 40 16 --- 15 | 75 61 54 79 77 74 --- 68
R14 | 848 11 22 19 18 9 13 --- 6 | 53 47 57 60 51 52 --- 51
R15 | 1210 11 17 13 28 11 10 137 6 | 72 66 66 87 76 70 57 72
R16 | 1319 31 44 22 36 43 29 --- 15 | 44 52 55 57 60 65 --- 52
R17E | 1110 10 30 15 14 13 12 --- 7 | 153 149 156 152 157 156 --- 153
R18E | 944 8 27 16 17 16 16 --- 7 | 107 100 102 95 101 107 --- 101
R19E | 1278 44 66 34 66 32 38 --- 20 | 93 87 85 97 94 87 --- 85
R20E | 1454 31 52 55 82 40 37 --- 21 | 88 87 80 113 78 69 --- 76
R21E | 1551 11 29 13 17 13 16 227 7 | 111 107 106 113 110 99 174 106
R22E | 999 35 35 76 77 35 39 --- 22 | 66 64 88 89 75 74 --- 65
R24E | 1005 11 33 15 29 13 18 --- 9 | 135 135 140 140 146 140 --- 138
------+----------------------------------------------+------------------------------------------
RMS | 1649 21 35 33 38 23 23 165 |T 89 76 81 92 93 92 76 85
WRMS | 1649 16 31 23 22 19 23 165 |NE 80 62 68 80 85 86 57 76
MEDI | 1110 15 30 19 17 16 20 143 |MD 93 70 80 89 90 88 57 84
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