[IGSREPORT-28308] Wk 2182 IGLOS Final Orbits
acc
acc at igs.org
Sat Nov 20 08:42:15 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2182 (Oct 31, 2021 - Nov 06, 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 2.2182.
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:
igl2182[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2182 in the SP3 format.
igl21827.sum Combination Report for GPS Week 2182.
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 | -1.7 ns
1 | -1.8 ns
2 | -2.4 ns
3 | -3.5 ns
4 | -2.1 ns
5 | -2.0 ns
6 | -3.0 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 1.2182, 1a.2182).
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 2.2182.0-6)
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 3.2182.0-6).
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 2182 summary. (Oct 31, 2021 - Nov 06, 2021)
Table 1.2182.a GPS week : 2182 MJD: 59518.0-59524.0
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 4 -17 -6 38 .12 26 19 | 14293 -1152 3127 8212
| 1 1 2 14 15 14 .04 | 966 1744
emx n/a| 0 0 -10 -15 12 -18 .04 37 29 | -6283 -940 3127 8439
| 0 1 2 27 25 14 .04 | 9357 1316
esx n/a| 0 2 0 -3 -8 40 .02 30 21 | 1286 -1150 3115 8992
| 1 1 2 9 16 24 .05 | 9199 1703
gfz n/a| 0 0 2 -1 -23 26 -.07 36 18 | 0 -1277 3181 8061
| 1 1 1 17 19 17 .10 | 0 1355
grg n/a| 0 -5 1 -1 9 -54 .20 28 21 | -1970 -1009 3119 7693
| 0 1 5 15 16 45 .07 | 381 1604
iac n/a| -2 2 0 16 14 -20 -.32 30 29 | -144 -827 3118 8740
| 2 1 3 27 39 39 .14 | 565 753
mcc n/a| 4 2 -1 50 98 -363 -.17 251 251 | --- --- --- ---
| 12 8 33 153 134 1379 .52 | --- ---
Table 1.2182.b GPS week : 2182 MJD: 59518.0-59524.0
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 | 12 10 13 16 13 15 17 |
R02 | 7 5 5 8 7 7 7 |
R03 | 7 8 8 7 7 8 8 |
R04 | 9 10 9 8 10 6 8 |
R05 | 9 8 10 10 9 10 9 |
R07 | 8 6 6 8 7 6 6 |
R08 | 8 8 8 7 8 7 9 |
R09 | 7 7 9 9 9 10 8 |
R11 | 7 7 9 8 9 10 11 |
R12 | 9 8 10 11 10 9 11 |
R13 | 13 13 13 17 19 16 18 |
R14 | 9 8 9 9 10 10 8 |
R15 | 8 9 8 8 8 9 10 |
R16 | 13 11 13 16 18 14 13 |
R17 | 8 8 9 9 10 8 8 |
R18 | 10 10 9 10 10 11 9 |
R19 | 27 28 26 26 23 27 25 |
R20 | 22 23 22 24 23 23 21 |
R21 | 8 9 8 11 14 22 8 |
R22 | 29 25 25 34 32 33 36 |
R24 | 10 10 9 8 8 10 9 |
Table 1.2182.c GPS week : 2182 MJD: 59518.0-59524.0
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 2182 0 | 37 12 74 -942 -948 -1146 81.5 1832 1832 | -1735 0
brd 2182 1 | 17 31 98 666 -291 -8080 81.8 1621 1621 | -1824 0
brd 2182 2 | 45 -6 -1 1560 -90 -6588 83.5 1480 1480 | -2385 0
brd 2182 3 | 14 16 -25 464 -1413 -5803 82.7 1401 1401 | -3506 0
brd 2182 4 | -30 96 30 -780 -1586 -3176 82.0 1360 1360 | -2056 0
brd 2182 5 | 13 -14 43 422 -344 3981 81.4 1316 1316 | -1994 0
brd 2182 6 | -21 -9 59 -259 2305 7137 82.4 1558 1558 | -2991 0
-------------+------------------------------------------------------------+----------------
brd 2182 mean| 10 17 39 161 -338 -1953 82.2 1509 1509 | -2355 0
brd 2182 sdev| 28 38 42 880 1299 5683 .7 178 178 | 660 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 2.2182.0 GPS week: 2182 Day: 0 MJD: 59518
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 1 2 0 13 .10 28 20 | 15215 -383 2928 8900
emx n/a| 0 0 -14 -4 17 -26 -.02 37 31 | -15005 237 2909 9200
esx n/a| 1 4 -1 -6 -26 5 .04 26 16 | 4369 -554 2890 8581
gfz n/a| 0 0 3 -6 7 -2 .12 34 17 | 0 -351 2972 8598
grg n/a| 0 -7 9 -6 11 -51 .18 28 22 | -1644 -538 2905 8212
iac n/a| 0 3 -6 1 27 28 -.35 24 19 | -18 -489 2913 9565
mcc n/a| 0 3 26 232 -50 196 -1.06 277 277 | --- --- --- ---
Table 2.2182.1 GPS week: 2182 Day: 1 MJD: 59519
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 4 -27 0 22 .10 25 17 | 15061 689 3251 8531
emx n/a| 2 0 -11 33 -20 -31 .03 36 28 | 5662 44 3246 8825
esx n/a| 0 0 2 2 -30 42 .01 30 19 | 1919 168 3245 10688
gfz n/a| 0 0 2 20 -17 41 -.06 32 22 | 0 -122 3311 8407
grg n/a| 0 -4 -1 -9 28 -26 .19 30 21 | -2047 197 3228 7926
iac n/a| 0 2 0 -7 11 -5 -.22 19 18 | 637 -287 3242 9174
mcc n/a| 7 19 53 25 112 1258 .18 266 266 | --- --- --- ---
Table 2.2182.2 GPS week: 2182 Day: 2 MJD: 59520
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 -44 -28 47 .15 27 21 | 15346 -2267 3406 9482
emx n/a| 0 -1 -10 -22 -7 -37 .04 37 29 | -17512 -1474 3400 9649
esx n/a| -1 3 0 -1 16 31 .11 30 20 | 6800 -2364 3412 11257
gfz n/a| 0 -1 2 0 -49 17 -.18 32 15 | 0 -1765 3464 9387
grg n/a| 1 -4 3 -13 -2 15 .22 29 21 | -1610 -1766 3430 8851
iac n/a| -1 0 -1 19 47 -41 -.22 18 15 | 210 -1373 3410 10067
mcc n/a| -3 5 10 8 305 -2250 .62 278 278 | --- --- --- ---
Table 2.2182.3 GPS week: 2182 Day: 3 MJD: 59521
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 5 -16 18 49 .13 24 20 | 13702 -3925 3285 6724
emx n/a| 1 0 -7 -40 38 -9 .02 37 30 | 19 -3526 3280 6837
esx n/a| -1 1 2 -8 -3 56 .02 33 21 | 12558 -3843 3263 8118
gfz n/a| -1 0 1 -26 -17 41 -.06 45 16 | 0 -3799 3324 6579
grg n/a| 0 -6 0 0 0 -43 .30 27 21 | -1696 -3706 3255 6410
iac n/a| 0 4 -4 67 -11 -39 -.43 30 30 | -1176 -1800 3251 7058
mcc n/a| 8 -4 -7 -114 166 -2009 -.03 229 229 | --- --- --- ---
Table 2.2182.4 GPS week: 2182 Day: 4 MJD: 59522
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 9 -14 -3 40 .17 25 20 | 12768 871 2727 7678
emx n/a| 0 0 -6 -44 42 -22 .07 35 27 | -15331 -233 2707 7860
esx n/a| -3 3 1 -10 -12 84 .01 33 26 | -12688 1143 2710 7720
gfz n/a| 0 1 3 4 -14 22 -.07 40 16 | 0 -91 2822 7542
grg n/a| 0 -6 -7 -2 11 -52 .22 27 21 | -2702 1089 2715 7158
iac n/a| -1 4 0 11 -51 -54 -.54 33 33 | -25 177 2722 8162
mcc n/a| 28 -3 -12 -101 69 -940 -.25 298 298 | --- --- --- ---
Table 2.2182.5 GPS week: 2182 Day: 5 MJD: 59523
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 2 -7 -22 54 .13 28 19 | 14287 -830 2969 7530
emx n/a| 0 1 -10 -32 28 -8 .10 39 28 | -1655 -293 2964 7770
esx n/a| 0 3 -2 -13 4 30 -.06 31 26 | 5892 -494 2969 6992
gfz n/a| 1 -2 5 -18 -31 19 -.16 37 20 | 0 -778 2996 7360
grg n/a| 2 -6 0 31 33 -126 .23 27 20 | -1987 -315 2982 7255
iac n/a| -5 2 3 33 7 32 -.37 49 49 | -200 -426 2987 7991
mcc n/a| -8 -7 -40 285 -84 531 -.27 176 176 | --- --- --- ---
Table 2.2182.6 GPS week: 2182 Day: 6 MJD: 59524
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 -18 -9 42 .05 26 19 | 13676 -2221 3328 8643
emx n/a| 0 -1 -10 1 -10 4 .05 39 30 | -159 -1335 3388 8934
esx n/a| 1 2 -5 13 -8 35 -.00 27 19 | -9847 -2106 3318 9590
gfz n/a| -1 1 0 16 -42 43 -.07 35 17 | 0 -2039 3381 8556
grg n/a| 0 -2 7 -6 -12 -95 .07 30 21 | -2110 -2028 3322 8041
iac n/a| -6 3 1 -11 69 -62 -.14 36 36 | -438 -1594 3307 9166
mcc n/a| -4 5 -35 20 170 670 -.34 237 237 | --- --- --- ---
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 3.2182.0 GPS week: 2182 Day: 0 MJD: 59518
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 | 670 25 33 36 16 18 18 --- 11 | 38 38 50 40 33 34 --- 35
R02 | 1054 9 11 14 20 11 20 --- 6 | 32 34 35 31 30 42 --- 31
R03 | 859 6 11 10 17 19 18 435 6 | 32 31 34 29 41 29 162 30
XR04M | 531 17 14 21 --- 14 17 --- 8 | 33 31 26 --- 28 22 --- 26
R05 | 737 28 20 17 23 10 11 253 8 | 31 32 31 32 28 21 138 24
R07 | 1042 11 14 18 17 21 17 70 7 | 34 32 32 30 30 30 143 27
R08 | 2377 12 10 21 18 22 22 --- 8 | 34 33 42 45 37 43 --- 36
R09 | 2945 18 13 9 13 16 23 --- 7 | 87 82 90 90 84 88 --- 87
R11 | 1290 15 15 8 14 21 16 --- 7 | 61 55 64 65 59 71 --- 61
R12 | 1026 25 26 13 15 10 19 --- 8 | 91 56 79 79 82 71 --- 76
R13 | 2903 35 41 24 25 18 23 --- 12 | 75 32 37 63 58 53 --- 49
R14M | 2255 16 27 22 21 13 18 --- 8 | 52 40 64 58 55 57 --- 53
R15 | 1166 12 28 9 15 13 23 72 7 | 62 43 57 64 60 72 89 59
R16M | 1493 18 35 24 46 35 14 --- 13 | 64 39 72 64 75 63 --- 61
R17 | 2580 19 32 14 14 14 15 --- 8 | 74 53 59 63 69 69 --- 64
R18M | 616 16 38 13 13 23 23 --- 9 | 65 55 74 67 78 79 --- 69
R19M | 2596 55 77 38 85 56 52 --- 27 | 103 87 94 109 97 96 --- 88
R20M | 2824 60 65 50 42 39 39 --- 22 | 151 128 124 135 137 134 --- 131
R21M | 671 18 33 13 11 16 15 348 8 | 77 55 64 62 70 76 180 66
R22 | 2460 49 73 70 83 69 42 --- 29 | 65 87 107 75 89 79 --- 73
R24 | 890 24 32 11 16 26 15 --- 9 | 67 54 54 57 67 50 --- 55
------+----------------------------------------------+------------------------------------------
RMS | 1832 28 37 26 34 28 24 277 |T 63 52 61 62 62 60 142 57
WRMS | 1832 20 31 16 17 22 19 277 |NE 55 47 55 54 54 53 133 50
MEDI | 1166 18 28 17 17 18 18 253 |MD 64 43 59 63 60 63 143 59
Table 3.2182.1 GPS week: 2182 Day: 1 MJD: 59519
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 | 1001 21 33 22 24 22 18 --- 10 | 24 22 27 26 26 23 --- 20
R02 | 833 7 7 18 15 12 9 --- 5 | 21 19 28 20 25 29 --- 21
R03 | 747 11 13 9 27 11 20 --- 7 | 22 23 22 28 14 22 --- 16
XR04M | 656 21 19 15 --- 10 23 --- 9 | 20 21 21 --- 18 18 --- 16
R05 | 689 20 23 19 18 10 14 325 8 | 15 20 30 29 17 19 239 15
R07 | 931 12 13 16 12 12 10 107 5 | 19 20 22 17 17 16 151 14
R08 | 1722 11 17 15 25 18 14 --- 7 | 22 21 32 46 30 24 --- 26
R09 | 2063 14 15 14 17 19 16 --- 7 | 64 65 66 66 60 62 --- 62
R11 | 2004 14 12 18 14 19 15 --- 7 | 57 50 64 59 53 60 --- 55
R12 | 601 18 39 11 12 14 10 --- 8 | 77 44 68 65 71 68 --- 66
R13 | 1305 37 34 34 25 22 13 --- 12 | 55 34 38 34 52 40 --- 38
R14M | 1355 12 28 25 11 13 13 --- 7 | 41 31 54 47 45 41 --- 41
R15 | 924 13 35 12 23 15 14 106 8 | 47 38 55 68 47 56 154 51
R16M | 1716 16 26 27 32 34 14 --- 11 | 46 34 53 36 57 34 --- 40
R17 | 2633 16 32 15 11 21 13 --- 8 | 48 37 41 43 52 41 --- 42
R18M | 858 15 30 23 22 15 21 --- 9 | 43 39 51 45 51 58 --- 46
R19M | 3246 58 85 59 86 69 20 --- 28 | 62 55 72 80 57 57 --- 52
R20M | 2192 41 67 71 47 49 39 --- 23 | 69 70 45 66 80 43 --- 55
R21M | 727 17 38 18 15 16 19 393 9 | 52 39 49 46 51 48 253 46
R22 | 1217 52 50 57 65 74 29 --- 24 | 55 61 73 63 65 62 --- 53
R24 | 2234 20 27 12 20 21 27 --- 10 | 44 43 44 48 47 37 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1621 25 36 30 32 30 19 266 |T 43 37 45 46 44 40 199 38
WRMS | 1621 17 28 19 22 21 18 266 |NE 40 35 43 43 41 39 181 37
MEDI | 1217 16 28 18 20 18 15 107 |MD 46 37 45 46 51 41 154 41
Table 3.2182.2 GPS week: 2182 Day: 2 MJD: 59520
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 | 701 28 44 30 20 25 21 --- 12 | 25 26 28 27 26 29 --- 19
R02 | 1094 10 12 10 10 16 10 459 5 | 23 25 30 29 23 24 231 23
R03 | 640 14 14 27 17 19 15 171 8 | 22 22 41 39 26 27 94 25
XR04M | 605 8 11 19 --- 19 20 --- 8 | 26 23 32 --- 18 38 --- 24
R05 | 985 28 19 31 22 8 15 165 9 | 26 29 44 37 28 23 173 24
R07 | 1064 11 11 12 15 12 12 231 5 | 22 20 22 26 23 21 98 18
R08 | 760 12 15 13 18 12 22 --- 7 | 26 28 33 35 23 30 --- 25
R09 | 2265 15 17 11 19 28 20 --- 8 | 39 41 42 54 35 52 --- 42
R11 | 2948 17 25 21 23 14 17 --- 8 | 48 53 60 40 52 52 --- 47
R12 | 505 21 44 17 17 20 8 --- 9 | 82 39 66 80 83 71 --- 70
R13 | 1188 32 39 24 33 31 11 --- 12 | 62 26 38 54 39 50 --- 42
R14M | 714 14 27 28 17 12 13 --- 8 | 45 28 57 42 44 38 --- 40
R15 | 913 9 34 14 16 15 14 312 7 | 55 39 47 61 67 49 241 52
R16M | 1254 19 31 25 39 42 16 --- 13 | 45 33 58 65 42 58 --- 47
R17 | 2610 20 27 16 16 18 17 --- 8 | 51 30 43 48 51 41 --- 41
R18M | 823 17 25 26 18 22 12 --- 8 | 36 29 52 35 52 49 --- 41
R19M | 2576 58 86 52 73 57 29 --- 25 | 50 59 54 63 57 49 --- 46
R20M | 821 54 68 63 47 39 21 --- 21 | 90 48 58 83 84 54 --- 65
R21M | 518 18 34 15 10 21 9 214 8 | 54 34 42 48 57 41 323 44
R22 | 858 48 34 60 78 64 40 --- 24 | 42 53 97 78 68 81 --- 61
R24 | 2189 21 36 18 16 19 13 --- 9 | 47 31 48 44 47 42 --- 40
------+----------------------------------------------+------------------------------------------
RMS | 1479 27 37 30 32 29 18 278 |T 43 34 47 49 45 43 193 39
WRMS | 1479 21 29 20 15 21 15 278 |NE 40 33 45 46 42 42 167 37
MEDI | 913 18 27 21 18 19 15 214 |MD 45 30 44 44 44 42 173 41
Table 3.2182.3 GPS week: 2182 Day: 3 MJD: 59521
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 | 1044 34 43 30 18 43 38 --- 16 | 34 33 35 38 39 33 --- 26
R02 | 777 11 8 15 12 12 34 322 7 | 21 21 29 29 18 37 99 21
R03 | 1040 10 13 9 16 11 29 94 7 | 23 27 34 33 25 49 48 28
XR04M | 583 10 8 13 --- 18 22 --- 7 | 24 24 30 --- 21 37 --- 24
R05 | 1232 20 16 31 28 9 23 106 10 | 20 17 38 33 21 35 111 19
R07 | 694 16 17 20 11 13 21 318 7 | 24 25 23 18 16 29 183 17
R08 | 624 14 13 12 15 14 22 --- 7 | 26 24 29 33 35 30 --- 26
R09 | 2139 15 13 12 16 17 39 --- 9 | 30 31 34 35 31 62 --- 33
R11 | 3657 18 19 12 21 14 15 --- 7 | 40 47 38 31 37 36 --- 35
R12 | 589 20 38 21 28 10 22 --- 10 | 92 54 77 93 85 74 --- 79
R13 | 834 30 57 38 43 23 36 --- 17 | 76 31 35 78 65 62 --- 55
R14M | 533 13 30 23 15 15 24 --- 9 | 50 25 60 54 54 44 --- 47
R15 | 1041 10 32 9 11 15 22 186 7 | 72 45 69 63 68 65 116 64
R16M | 1283 18 23 36 60 33 28 --- 15 | 40 34 53 54 37 41 --- 32
R17 | 1905 17 29 20 16 17 21 --- 9 | 50 29 37 44 54 39 --- 41
R18M | 790 19 20 24 15 18 29 --- 9 | 37 29 51 41 47 54 --- 40
R19M | 1789 32 82 43 88 59 35 --- 26 | 48 60 39 72 47 41 --- 39
R20M | 825 53 74 67 54 23 40 --- 23 | 81 37 47 70 61 70 --- 54
R21M | 508 17 44 21 7 11 36 236 11 | 58 29 46 53 59 76 200 53
R22 | 1172 44 38 85 139 70 43 --- 33 | 40 66 119 88 56 60 --- 55
R24 | 1524 14 30 16 18 15 18 --- 8 | 40 25 34 37 40 32 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 1401 24 37 33 45 27 30 229 |T 44 33 45 49 43 47 126 39
WRMS | 1401 20 30 21 16 21 30 229 |NE 42 33 45 46 42 45 111 37
MEDI | 1040 17 29 21 16 15 28 186 |MD 40 29 38 41 40 41 111 35
Table 3.2182.4 GPS week: 2182 Day: 4 MJD: 59522
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 | 1347 25 36 26 29 21 37 --- 13 | 40 38 44 48 38 35 --- 34
R02 | 1967 11 15 14 10 16 22 200 6 | 26 25 27 27 32 39 92 24
R03 | 1048 8 9 13 12 13 31 103 6 | 27 25 39 32 33 39 61 29
XR04M | 531 17 16 16 --- 11 35 --- 9 | 26 25 26 --- 23 44 --- 23
R05 | 1037 21 16 18 16 17 33 80 9 | 24 24 40 34 24 52 42 27
R07 | 847 13 7 14 8 12 33 434 7 | 28 26 28 28 30 39 262 25
R08 | 733 14 18 19 17 16 21 --- 7 | 30 33 42 40 40 30 --- 32
R09 | 2188 14 15 24 16 18 29 --- 8 | 44 50 55 45 37 47 --- 42
R11 | 2710 19 11 16 14 21 33 --- 9 | 76 75 82 69 69 79 --- 73
R12 | 852 19 29 19 17 19 30 --- 10 | 73 47 57 53 62 75 --- 59
R13 | 1054 29 55 50 58 31 27 --- 19 | 74 41 41 101 71 56 --- 59
R14M | 483 16 26 24 26 21 22 --- 10 | 46 41 65 66 60 54 --- 51
R15 | 848 12 31 13 13 14 17 78 8 | 70 56 58 66 61 72 81 62
R16M | 1231 20 19 40 70 26 50 --- 17 | 44 41 54 71 41 57 --- 37
R17 | 607 22 27 23 12 12 33 --- 9 | 50 32 36 37 40 41 --- 35
R18M | 734 18 20 24 17 15 37 --- 9 | 43 34 52 47 47 54 --- 43
R19M | 1817 27 76 42 55 55 43 --- 22 | 67 84 73 67 70 72 --- 66
R20M | 1139 66 70 55 40 18 39 --- 23 | 89 46 48 51 54 60 --- 53
R21M | 632 23 48 22 17 14 53 529 14 | 59 46 53 47 59 88 155 53
R22 | 2253 46 32 86 124 73 29 --- 32 | 38 61 116 72 60 68 --- 57
R24 | 655 13 27 16 16 15 23 --- 8 | 36 26 33 34 36 31 --- 29
------+----------------------------------------------+------------------------------------------
RMS | 1359 25 35 33 40 27 33 298 |T 48 41 50 51 47 53 115 43
WRMS | 1359 20 27 26 16 21 33 298 |NE 45 39 49 49 45 50 107 41
MEDI | 1037 19 26 22 17 17 33 103 |MD 44 41 48 47 41 54 81 42
Table 3.2182.5 GPS week: 2182 Day: 5 MJD: 59523
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 | 1401 36 35 44 37 17 26 --- 15 | 24 21 45 38 28 26 --- 24
R02 | 1628 6 11 13 11 10 38 220 6 | 19 22 22 21 20 36 220 17
R03 | 1438 13 13 16 20 15 31 89 8 | 28 26 26 30 37 32 61 24
XR04M | 697 10 9 11 --- 10 23 --- 6 | 22 24 25 --- 24 27 --- 21
R05 | 710 24 20 25 17 19 31 91 10 | 29 28 47 37 40 39 51 32
R07 | 689 14 8 13 15 10 21 --- 6 | 24 24 21 18 20 22 --- 18
R08 | 837 11 14 14 26 14 18 --- 7 | 20 20 33 38 23 22 --- 24
R09 | 2392 21 17 23 23 19 24 --- 9 | 61 58 60 59 56 52 --- 54
R11 | 1866 16 11 16 21 20 46 --- 9 | 51 48 53 44 58 73 --- 50
R12 | 784 10 33 13 20 18 33 --- 9 | 62 44 54 62 64 82 --- 58
R13 | 985 39 48 37 24 24 42 --- 16 | 65 40 36 55 46 56 --- 42
R14M | 692 10 29 20 23 17 45 --- 10 | 61 54 61 69 70 72 --- 62
R15 | 811 16 32 18 11 19 20 65 8 | 68 49 53 61 65 61 184 58
R16M | 1217 18 27 29 33 24 54 --- 13 | 45 41 61 69 50 89 --- 50
R17 | 1152 12 31 12 19 15 23 --- 8 | 56 50 55 60 57 62 --- 54
R18M | 616 15 31 21 21 22 35 --- 10 | 56 50 64 66 68 54 --- 57
R19M | 982 37 101 38 70 59 47 --- 27 | 79 84 75 78 69 83 --- 66
R20M | 1360 60 71 59 44 15 54 --- 23 | 85 58 50 73 68 61 --- 61
R21M | 1200 34 33 24 20 11 142 293 22 | 86 76 79 76 76 73 342 71
R22 | 2499 58 35 77 113 72 61 --- 33 | 56 70 100 66 78 62 --- 60
R24 | 793 9 42 14 14 21 29 --- 10 | 45 42 45 52 61 68 --- 49
------+----------------------------------------------+------------------------------------------
RMS | 1315 28 39 31 37 27 49 176 |T 49 44 50 53 51 54 171 45
WRMS | 1315 19 28 26 20 20 49 176 |NE 43 38 46 45 46 49 129 40
MEDI | 985 16 31 20 21 18 33 91 |MD 56 44 53 59 57 61 184 50
Table 3.2182.6 GPS week: 2182 Day: 6 MJD: 59524
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 | 732 53 24 33 34 23 39 --- 16 | 37 43 48 43 30 40 --- 33
R02 | 1567 7 12 9 21 14 19 162 6 | 26 26 31 34 24 26 131 26
R03 | 1166 8 10 19 14 15 29 164 7 | 31 30 39 32 35 39 76 32
XR04M | 787 6 14 11 --- 14 28 --- 7 | 44 46 48 --- 46 49 --- 44
R05 | 797 21 23 18 13 18 27 52 9 | 33 33 33 28 28 24 42 25
R07 | 603 9 12 8 14 13 18 210 5 | 37 35 38 35 31 40 339 34
R08 | 727 20 15 16 19 10 37 --- 9 | 31 32 41 40 37 36 --- 33
R09 | 3165 10 17 12 17 23 20 --- 7 | 87 88 94 89 84 96 --- 88
R11 | 2272 16 24 20 13 21 47 --- 10 | 67 66 78 66 70 92 --- 70
R12 | 1365 12 36 21 11 23 40 --- 10 | 84 60 80 84 90 96 --- 81
R13 | 2516 36 45 29 31 58 36 --- 17 | 83 41 46 65 67 74 --- 58
R14M | 1476 10 32 16 8 14 30 --- 8 | 151 146 157 155 157 153 --- 153
R15 | 872 18 36 15 15 26 20 348 9 | 75 46 61 69 80 74 158 67
R16M | 1029 19 36 20 32 21 45 --- 12 | 57 47 65 50 54 80 --- 54
R17 | 2089 10 36 11 17 15 14 --- 8 | 82 63 73 80 81 76 --- 75
R18M | 468 15 30 17 13 16 29 --- 8 | 78 65 88 80 85 84 --- 80
R19M | 671 40 105 40 63 37 32 --- 24 | 154 140 144 160 150 146 --- 144
R20M | 843 57 59 46 39 23 43 --- 20 | 113 73 69 90 84 82 --- 81
R21M | 1187 18 27 12 10 24 9 340 8 | 129 119 121 122 126 171 296 127
R22 | 2692 42 52 78 117 82 85 --- 35 | 73 98 123 86 103 85 --- 81
R24 | 922 9 36 9 12 20 33 --- 9 | 67 55 67 65 73 70 --- 64
------+----------------------------------------------+------------------------------------------
RMS | 1557 26 39 27 35 30 36 237 |T 73 64 73 73 73 77 173 69
WRMS | 1557 19 30 19 17 21 36 237 |NE 58 51 60 58 59 62 149 54
MEDI | 1029 16 30 17 15 21 30 164 |MD 73 55 67 66 73 76 131 67
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