[IGSREPORT-28290] Wk 2181 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 12 04:35:42 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2181 (Oct 24, 2021 - Oct 30, 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 2.2181.
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:
igl2181[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2181 in the SP3 format.
igl21817.sum Combination Report for GPS Week 2181.
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 | 7.1 ns
1 | 14.3 ns
2 | -1.3 ns
3 | -2.6 ns
4 | -3.0 ns
5 | -1.5 ns
6 | -2.3 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 1.2181, 1a.2181).
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 2.2181.0-6)
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 3.2181.0-6).
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 2181 summary. (Oct 24, 2021 - Oct 30, 2021)
Table 1.2181.a GPS week : 2181 MJD: 59511.0-59517.0
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 3 5 0 22 .15 24 17 | 12855 -1080 6211 37814
| 0 1 1 14 13 20 .04 | 3829 2492
emx n/a| 0 0 -6 -20 0 -42 -.01 36 30 | 2901 -63 3537 8844
| 1 1 5 17 25 41 .05 | 9494 1355
esx n/a| 0 1 0 -12 -18 15 -.02 30 21 | -1404 -794 6188 37684
| 1 1 2 20 25 39 .04 | 10216 1852
gfz n/a| 0 0 3 7 -8 33 -.03 36 17 | 0 -1136 6320 38337
| 1 0 1 15 21 33 .08 | 0 2317
grg n/a| 1 -3 2 -8 11 -54 .21 28 21 | -3978 -963 6210 37469
| 2 0 2 20 14 35 .07 | 3573 2319
iac n/a| 0 0 -5 17 23 5 -.27 24 24 | -1593 -1228 6205 38097
| 2 1 2 33 70 87 .10 | 3471 2513
mcc n/a| 6 1 9 20 -10 50 -.70 181 181 | --- --- --- ---
| 9 3 21 86 99 302 .22 | --- ---
Table 1.2181.b GPS week : 2181 MJD: 59511.0-59517.0
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 12 13 11 15 13 14 |
R02 | 6 8 8 7 6 7 6 |
R03 | 6 6 7 6 6 5 7 |
R04 | 9 7 8 10 9 8 7 |
R05 | 10 9 10 8 9 9 9 |
R07 | 7 7 7 6 7 6 6 |
R08 | 8 7 7 8 8 7 7 |
R09 | 8 7 8 9 8 8 9 |
R11 | 10 9 9 10 9 10 9 |
R12 | 11 11 12 12 9 8 8 |
R13 | 18 15 21 20 17 15 15 |
R14 | 10 7 8 10 8 8 7 |
R15 | 11 9 10 11 10 10 9 |
R16 | 13 14 15 15 12 15 15 |
R17 | 6 8 8 8 16 13 10 |
R18 | 8 8 8 10 10 10 10 |
R19 | 21 23 19 20 25 21 25 |
R20 | 18 21 22 23 22 19 20 |
R21 | 8 8 7 9 8 9 9 |
R22 | 24 21 30 29 28 32 28 |
R24 | 8 8 8 10 8 9 9 |
Table 1.2181.c GPS week : 2181 MJD: 59511.0-59517.0
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 2181 0 | -13 51 50 1833 1157 1147 82.9 1744 1744 | 7138 0
brd 2181 1 | 54 -17 107 0 1888 4467 82.0 1617 1617 | 14283 0
brd 2181 2 | 42 -10 37 -1186 645 2805 82.4 1646 1646 | -1256 0
brd 2181 3 | -10 81 10 -1904 -944 -3127 81.8 1626 1626 | -2629 0
brd 2181 4 | -31 -7 84 -186 1175 635 82.4 1930 1930 | -2984 0
brd 2181 5 | -13 -73 95 -1988 -270 -2166 81.7 2106 2106 | -1496 0
brd 2181 6 | -47 -49 -39 -533 -352 18 81.3 2011 2011 | -2277 0
-------------+------------------------------------------------------------+----------------
brd 2181 mean| -2 -3 49 -566 471 540 82.1 1811 1811 | 1539 0
brd 2181 sdev| 37 54 52 1317 1019 2644 .6 201 201 | 6622 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 2.2181.0 GPS week: 2181 Day: 0 MJD: 59511
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 9 -11 20 .20 24 18 | 5022 -2024 13306 97104
emx n/a| 0 0 1 -20 -44 -121 -.09 34 31 | -5080 1912 3258 8794
esx n/a| 0 2 0 -52 -37 -32 -.03 25 20 | -15087 -1703 13254 96358
gfz n/a| -2 1 2 -1 -17 15 .06 29 15 | 0 -3057 13693 100213
grg n/a| 2 -2 1 -10 -10 -68 .21 29 18 | -11071 -2176 13319 97189
iac n/a| -1 0 -7 62 124 95 -.38 23 23 | -8244 -3723 13290 97044
mcc n/a| 14 -1 19 24 204 -175 -1.09 214 214 | --- --- --- ---
Table 2.2181.1 GPS week: 2181 Day: 1 MJD: 59512
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 -2 -12 16 .17 21 18 | 10508 -5491 12173 123737
emx n/a| 1 0 -2 -19 -5 -20 -.00 38 32 | 19367 -2085 3592 7806
esx n/a| 3 1 -3 -13 23 -28 -.01 30 25 | 3308 -4374 12127 122907
gfz n/a| 1 0 5 6 24 44 -.08 36 20 | 0 -4930 12335 124367
grg n/a| 4 -4 1 -47 13 -28 .26 23 17 | -6635 -5152 12184 123903
iac n/a| -5 0 -5 42 -11 51 -.28 21 21 | -4555 -5520 12174 123722
mcc n/a| 16 7 14 43 -10 -310 -.53 131 131 | --- --- --- ---
Table 2.2181.2 GPS week: 2181 Day: 2 MJD: 59513
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 36 18 2 .15 21 15 | 15265 1869 3391 8108
emx n/a| -2 -3 -3 -2 14 -49 -.03 38 34 | -102 665 3462 8526
esx n/a| 0 4 0 -15 -8 64 .01 34 21 | 4845 1215 3394 6698
gfz n/a| 3 0 4 -19 -3 94 -.12 40 18 | 0 1866 3427 8048
grg n/a| 0 -3 3 -6 0 -28 .24 28 23 | -2120 1624 3381 7409
iac n/a| 1 0 -6 -13 -46 -51 -.29 25 25 | 572 1188 3386 8487
mcc n/a| 6 -3 34 -48 -88 -212 -.85 114 114 | --- --- --- ---
Table 2.2181.3 GPS week: 2181 Day: 3 MJD: 59514
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 13 7 .12 23 15 | 14853 -538 3581 9703
emx n/a| 1 1 -7 5 34 -41 -.02 37 32 | 10541 -712 3489 9926
esx n/a| 0 1 2 -18 -20 52 .01 32 20 | 16053 537 3558 11256
gfz n/a| 0 0 4 18 -14 21 .08 39 17 | 0 -465 3627 9877
grg n/a| 2 -5 2 19 10 -89 .26 29 21 | -2344 73 3577 9008
iac n/a| -1 -1 -9 -8 -8 40 -.36 24 24 | -182 951 3581 10149
mcc n/a| -7 -1 27 -56 -40 137 -.58 136 136 | --- --- --- ---
Table 2.2181.4 GPS week: 2181 Day: 4 MJD: 59515
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 3 0 -17 12 .15 23 16 | 14610 -2068 3626 10004
emx n/a| 0 0 -12 -22 -18 -58 .05 38 29 | -4985 -1174 3603 10322
esx n/a| -2 0 1 -4 -57 -9 -.10 33 22 | -5703 -979 3616 9814
gfz n/a| 0 1 3 5 -41 -15 -.08 34 17 | 0 -1632 3655 10123
grg n/a| 0 -3 3 -7 13 -55 .24 27 20 | -1849 -1410 3607 9625
iac n/a| 3 0 -3 -5 125 87 -.23 27 27 | 634 -1158 3627 10481
mcc n/a| -5 2 10 78 -59 370 -.48 176 176 | --- --- --- ---
Table 2.2181.5 GPS week: 2181 Day: 5 MJD: 59516
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 -7 -2 37 .08 28 19 | 14599 1547 3554 8445
emx n/a| 0 1 -8 -34 8 2 -.02 34 28 | 5889 838 3538 8736
esx n/a| 0 0 1 9 -8 27 .01 27 19 | -6730 199 3541 9373
gfz n/a| 0 1 0 21 -17 43 -.08 35 17 | 0 909 3632 8259
grg n/a| 0 -2 0 2 37 -105 .15 28 23 | -2127 1337 3560 7726
iac n/a| -1 0 -2 53 -9 -40 -.06 27 27 | 761 297 3538 8918
mcc n/a| 15 3 -19 -66 -69 56 -.79 210 210 | --- --- --- ---
Table 2.2181.6 GPS week: 2181 Day: 6 MJD: 59517
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 5 4 4 61 .15 25 17 | 15134 -859 3852 7597
emx n/a| 0 -1 -10 -47 8 -9 .03 32 27 | -5320 114 3822 7804
esx n/a| 1 1 -1 4 -17 35 -.02 27 18 | -6520 -457 3830 7387
gfz n/a| 0 0 0 23 12 32 .00 35 15 | 0 -646 3873 7478
grg n/a| -2 -4 7 -7 12 -7 .07 31 23 | -1705 -1039 3846 7424
iac n/a| 1 3 -4 -10 -13 -142 -.27 24 20 | -141 -633 3845 7881
mcc n/a| 2 0 -21 172 -7 484 -.59 288 288 | --- --- --- ---
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 3.2181.0 GPS week: 2181 Day: 0 MJD: 59511
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 | 1381 27 27 24 28 27 22 --- 11 | 83 82 59 66 62 75 --- 69
R02 | 1475 7 9 11 13 9 20 413 5 | 51 51 52 46 46 66 280 51
R03 | 643 9 11 11 18 13 17 126 6 | 55 58 57 53 61 55 101 56
XR04 | 665 22 14 18 --- 12 21 --- 9 | 59 55 44 --- 47 51 --- 49
R05 | 660 20 20 18 35 16 23 99 10 | 58 45 47 46 48 54 52 47
R07 | 466 12 15 9 15 10 22 225 6 | 56 58 60 51 57 73 172 58
R08 | 2048 20 19 14 15 14 22 --- 8 | 58 57 73 74 63 81 --- 67
R09 | 2534 21 15 10 15 17 20 --- 7 | 79 73 79 74 62 80 --- 74
XR11 |10914 18 --- 16 17 19 28 --- 10 | 47 --- 53 54 44 43 --- 45
R12 | 522 10 50 22 26 19 19 --- 11 | 85 36 66 95 96 89 --- 79
R13 | 2464 47 48 41 36 33 30 --- 18 | 107 68 71 86 106 100 --- 86
R14 | 677 15 36 22 10 13 33 --- 10 | 82 66 78 80 82 94 --- 79
R15 | 746 13 45 9 13 20 32 147 10 | 79 42 68 80 80 78 45 70
R16 | 1270 17 41 31 30 34 20 --- 13 | 89 70 100 88 107 102 --- 93
R17E | 2127 12 22 10 15 15 12 --- 6 | 101 109 105 104 101 95 --- 101
R18E | 1431 11 22 25 13 12 13 --- 7 | 49 46 53 50 52 57 --- 50
R19E | 3106 41 52 39 51 61 28 --- 20 | 56 48 60 75 54 47 --- 49
R20E | 1613 26 56 39 57 30 32 --- 18 | 144 132 154 148 148 131 --- 140
R21E | 848 10 31 11 16 18 20 79 8 | 49 38 44 50 49 49 65 45
R22E | 2942 55 43 47 58 71 25 --- 23 | 60 66 74 103 78 56 --- 62
R24E | 2201 14 28 14 12 15 18 --- 7 | 36 37 36 37 43 45 --- 35
------+----------------------------------------------+------------------------------------------
RMS | 1744 24 34 25 29 29 23 214 |T 70 61 68 73 70 72 119 66
WRMS | 1744 18 31 20 15 18 23 214 |NE 70 58 64 68 68 74 130 65
MEDI | 1431 17 27 18 16 17 22 126 |MD 59 57 60 74 62 73 65 62
Table 3.2181.1 GPS week: 2181 Day: 1 MJD: 59512
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 | 912 30 34 38 23 22 15 --- 12 | 49 53 30 37 36 44 --- 40
R02 | 1449 13 14 14 10 14 25 241 7 | 40 30 35 34 29 46 267 34
R03 | 538 6 6 13 22 12 15 105 6 | 34 31 39 23 36 41 40 33
XR04 | 487 12 8 17 --- 12 12 --- 6 | 34 29 31 --- 35 32 --- 31
R05 | 596 20 13 31 22 18 12 78 9 | 32 23 30 29 33 31 63 26
R07 | 987 10 10 19 13 12 22 94 7 | 34 35 47 39 32 39 65 35
R08 | 2762 14 15 21 10 11 15 --- 6 | 34 34 54 37 41 42 --- 39
R09 | 2544 19 15 14 17 11 18 --- 7 | 45 45 50 52 42 50 --- 45
XR11 |10781 16 --- 22 25 17 13 --- 9 | 38 --- 46 36 38 31 --- 33
R12 | 847 12 55 27 24 14 17 --- 11 | 69 28 45 79 68 73 --- 62
R13 | 1333 21 56 50 26 22 31 --- 15 | 93 61 66 80 99 97 --- 83
R14 | 515 11 29 18 17 15 9 --- 7 | 86 70 92 79 89 83 --- 83
R15 | 498 14 45 12 13 13 19 79 9 | 62 34 52 58 58 51 63 54
R16 | 1996 20 41 29 36 40 19 --- 13 | 72 61 85 84 74 68 --- 73
R17E | 2337 12 32 14 14 16 20 --- 8 | 109 110 110 106 113 102 --- 107
R18E | 1202 13 20 19 27 14 13 --- 7 | 27 27 26 24 34 35 --- 25
R19E | 2685 32 83 47 72 52 33 --- 23 | 34 56 45 72 46 37 --- 29
R20E | 1479 30 59 57 81 25 30 --- 21 | 124 115 121 144 115 123 --- 118
R21E | 670 8 38 19 17 16 13 111 8 | 31 20 31 37 43 36 65 31
R22E | 2131 49 24 49 76 45 30 --- 21 | 35 48 55 73 45 47 --- 36
R24E | 1639 13 31 16 18 15 15 --- 8 | 35 25 32 37 41 41 --- 34
------+----------------------------------------------+------------------------------------------
RMS | 1616 21 38 30 36 23 21 131 |T 53 46 53 58 54 54 93 50
WRMS | 1616 18 32 25 20 17 21 131 |NE 51 41 50 51 50 52 99 47
MEDI | 1333 14 29 19 22 15 17 94 |MD 38 34 46 39 42 44 63 36
Table 3.2181.2 GPS week: 2181 Day: 2 MJD: 59513
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 | 955 29 36 28 24 38 17 --- 13 | 61 65 38 45 40 51 --- 48
R02 | 1782 9 16 14 17 22 25 119 8 | 39 42 38 32 24 44 161 34
R03 | 1066 12 14 9 15 21 21 132 7 | 42 42 47 47 58 63 33 49
XR04 | 540 10 12 11 --- 18 20 --- 7 | 43 47 40 --- 35 48 --- 41
R05 | 811 21 18 29 21 22 18 82 10 | 39 37 41 41 28 46 39 35
R07 | 686 7 11 10 20 11 24 143 6 | 41 39 43 38 41 58 39 42
R08 | 1868 11 12 16 18 16 15 --- 6 | 40 40 49 49 44 44 --- 41
R09 | 2899 16 15 17 17 15 24 --- 8 | 25 28 27 29 32 37 --- 24
XR11 | 6250 16 --- 14 24 17 21 --- 9 | 64 --- 62 76 66 56 --- 62
R12 | 871 17 56 24 21 15 21 --- 11 | 84 41 57 86 85 83 --- 73
R13 | 1532 18 72 59 44 44 42 --- 20 | 77 42 40 92 96 103 --- 71
R14 | 1432 10 36 17 21 15 9 --- 8 | 76 63 89 91 80 81 --- 79
R15 | 487 11 52 17 16 16 14 105 10 | 63 31 47 62 64 61 40 54
R16 | 1131 10 28 29 52 48 29 --- 15 | 98 86 94 79 100 106 --- 93
R17E | 1386 12 32 16 15 15 17 --- 8 | 80 73 77 77 81 70 --- 75
R18E | 1333 16 22 17 18 18 16 --- 8 | 25 23 30 28 35 26 --- 24
R19E | 3589 24 59 38 66 43 24 --- 18 | 43 50 42 81 62 44 --- 43
R20E | 1545 43 61 59 59 38 44 --- 22 | 123 110 97 108 119 104 --- 106
R21E | 656 8 30 12 18 14 15 94 7 | 29 21 27 34 36 34 45 28
R22E | 1857 50 30 93 118 47 44 --- 30 | 33 43 105 93 46 42 --- 40
R24E | 1917 10 32 15 18 14 16 --- 7 | 36 30 30 33 41 35 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 1645 21 38 34 40 28 25 114 |T 55 47 53 61 57 58 59 52
WRMS | 1645 15 34 21 18 23 25 114 |NE 56 46 50 59 56 62 62 53
MEDI | 1386 12 30 17 20 18 21 105 |MD 43 42 43 49 46 51 39 43
Table 3.2181.3 GPS week: 2181 Day: 3 MJD: 59514
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 | 638 25 26 25 32 25 15 --- 11 | 71 77 80 63 59 66 --- 67
R02 | 967 10 15 10 12 27 12 155 6 | 45 48 41 39 32 45 162 39
R03 | 1012 7 6 12 16 14 15 122 5 | 53 55 51 44 58 54 69 52
XR04 | 771 13 15 19 --- 22 27 --- 10 | 48 51 33 --- 41 50 --- 42
R05 | 805 19 19 22 24 11 15 76 8 | 45 43 36 32 34 43 39 36
R07 | 910 8 12 18 13 17 11 210 6 | 47 49 44 41 43 51 107 45
R08 | 1475 16 17 15 15 17 25 --- 8 | 47 46 55 54 57 70 --- 53
R09 | 2934 17 10 20 17 17 26 --- 8 | 23 29 36 31 20 39 --- 25
R11 | 2374 20 34 12 27 20 22 --- 10 | 54 52 54 46 56 50 --- 49
R12 | 984 14 44 27 12 29 24 --- 11 | 84 52 65 78 91 80 --- 74
R13 | 2200 28 66 50 60 36 24 --- 19 | 100 40 55 122 93 82 --- 79
R14 | 1954 9 37 20 32 14 17 --- 9 | 89 75 93 111 97 101 --- 93
R15 | 529 9 47 18 21 19 23 114 10 | 71 44 57 79 79 85 31 69
R16 | 1102 21 21 35 50 34 31 --- 14 | 66 64 83 57 69 89 --- 69
R17E | 982 17 33 13 16 13 17 --- 8 | 157 160 155 157 154 145 --- 153
R18E | 873 19 19 23 28 17 27 --- 10 | 31 26 37 38 36 32 --- 28
R19E | 3400 27 67 33 72 52 21 --- 20 | 55 43 49 89 53 45 --- 47
R20E | 2105 57 65 48 64 36 37 --- 23 | 140 141 167 160 159 152 --- 149
R21E | 694 21 26 13 15 15 24 101 8 | 34 28 34 39 41 43 72 34
R22E | 1523 40 44 90 93 70 44 --- 29 | 32 38 90 58 40 54 --- 33
R24E | 974 7 39 14 25 16 27 --- 9 | 36 31 35 50 45 44 --- 37
------+----------------------------------------------+------------------------------------------
RMS | 1626 23 37 32 39 29 24 136 |T 63 56 64 69 64 67 80 60
WRMS | 1626 15 32 20 17 21 24 136 |NE 60 51 55 61 59 64 81 56
MEDI | 984 17 26 20 24 19 24 114 |MD 53 48 54 54 56 54 69 49
Table 3.2181.4 GPS week: 2181 Day: 4 MJD: 59515
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 | 536 40 30 35 37 21 24 --- 14 | 57 63 55 59 44 41 --- 48
R02 | 1167 5 15 11 9 17 15 257 5 | 30 43 41 33 37 31 237 33
R03 | 1327 8 11 10 17 14 14 98 5 | 42 47 37 38 38 40 95 39
XR04 | 794 15 20 16 --- 17 21 --- 9 | 48 57 37 --- 35 42 --- 42
R05 | 806 19 21 15 23 22 16 83 8 | 54 48 54 53 34 50 42 46
R07 | 1502 9 11 11 11 12 27 294 6 | 44 52 46 42 44 41 168 42
R08 | 1056 16 21 12 22 21 18 --- 8 | 41 43 45 49 62 49 --- 47
R09 | 3457 15 10 23 20 19 16 --- 8 | 33 33 37 38 33 32 --- 30
R11 | 6065 20 12 26 18 18 25 --- 9 | 79 31 76 75 82 66 --- 73
R12 | 694 8 32 14 14 27 16 --- 8 | 57 36 51 58 73 45 --- 52
R13 | 1226 44 50 47 27 26 22 --- 16 | 97 54 46 79 62 54 --- 62
R14 | 998 12 31 16 8 16 14 --- 7 | 77 54 65 72 78 77 --- 70
R15 | 512 13 37 21 23 22 18 69 10 | 68 39 49 73 67 65 37 60
R16 | 1482 16 24 30 36 22 28 --- 11 | 104 91 102 99 114 110 --- 102
R17E | 814 11 40 25 16 21 70 --- 16 | 118 124 124 122 119 93 --- 112
R18E | 722 14 29 24 24 19 27 --- 10 | 40 40 55 47 50 51 --- 44
R19E | 1831 33 101 33 50 69 32 --- 24 | 54 59 40 63 52 38 --- 35
R20E | 1429 48 66 59 53 25 41 --- 22 | 106 109 124 112 116 105 --- 107
R21E | 669 16 23 12 21 23 15 113 8 | 45 41 47 51 52 51 99 45
R22E | 2211 39 42 94 103 44 29 --- 28 | 42 52 90 100 65 60 --- 49
R24E | 986 8 32 17 15 18 15 --- 8 | 32 33 36 36 46 31 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 1930 23 38 33 34 27 27 176 |T 60 54 59 64 62 55 113 55
WRMS | 1930 16 29 22 17 20 27 176 |NE 59 49 52 59 57 53 115 53
MEDI | 1056 15 29 21 21 21 21 98 |MD 54 48 49 58 52 50 95 47
Table 3.2181.5 GPS week: 2181 Day: 5 MJD: 59516
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 | 535 43 20 31 30 21 17 --- 13 | 44 41 47 48 30 44 --- 37
R02 | 2292 12 14 8 20 22 11 321 7 | 29 31 28 24 45 30 136 27
R03 | 907 9 8 8 11 13 10 135 4 | 38 35 41 37 44 34 54 37
XR04 | 636 16 20 7 --- 15 20 --- 8 | 40 45 39 --- 43 26 --- 36
R05 | 615 25 21 21 14 19 16 118 9 | 45 39 51 43 31 39 60 38
R07 | 895 9 13 13 8 17 16 199 6 | 40 42 43 39 34 33 208 37
R08 | 869 16 11 12 20 16 17 --- 7 | 34 36 37 41 35 39 --- 35
R09 | 3452 18 16 12 18 21 21 --- 8 | 64 66 62 67 54 63 --- 61
R11 | 6396 21 24 24 16 21 22 --- 9 | 65 42 61 66 76 58 --- 63
R12 | 657 9 30 18 14 19 16 --- 8 | 52 41 59 56 52 52 --- 50
R13 | 2243 37 46 35 23 39 17 --- 15 | 73 43 41 54 71 48 --- 51
R14 | 751 11 29 18 16 21 9 --- 8 | 97 90 105 104 106 102 --- 100
R15 | 734 17 33 17 15 27 15 58 9 | 65 46 54 61 77 51 38 58
R16 | 2079 24 40 32 40 25 38 --- 15 | 101 92 103 90 96 98 --- 95
R17E | 845 19 37 16 12 38 41 --- 13 | 139 147 144 136 147 134 --- 139
R18E | 602 16 30 16 26 15 28 --- 10 | 52 50 56 54 46 72 --- 53
R19E | 1352 45 77 35 47 51 26 --- 21 | 57 56 54 72 51 44 --- 47
R20E | 1756 54 54 38 50 19 28 --- 19 | 115 108 108 118 123 113 --- 111
R21E | 685 20 28 17 12 19 22 293 9 | 68 68 64 62 65 64 99 62
R22E | 3054 57 37 70 114 59 70 --- 32 | 51 71 93 103 66 85 --- 62
R24E | 962 15 34 12 19 19 16 --- 8 | 44 50 37 37 54 41 --- 40
------+----------------------------------------------+------------------------------------------
RMS | 2106 28 34 27 35 28 27 210 |T 62 59 63 65 64 60 99 59
WRMS | 2106 19 28 19 17 23 27 210 |NE 56 49 55 56 56 51 99 51
MEDI | 895 18 29 17 18 21 17 135 |MD 52 46 54 56 54 51 60 51
Table 3.2181.6 GPS week: 2181 Day: 6 MJD: 59517
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 | 603 39 13 40 31 25 16 --- 13 | 68 75 64 61 55 60 --- 60
R02 | 3605 10 9 13 14 13 20 503 6 | 44 50 47 36 41 51 224 44
R03 | 923 7 12 10 13 27 21 277 7 | 52 55 57 48 68 47 88 53
XR04 | 535 12 12 11 --- 12 16 --- 6 | 56 61 47 --- 52 48 --- 50
R05 | 1097 26 19 22 18 17 19 166 9 | 60 51 59 47 41 44 72 48
R07 | 1321 8 11 11 20 12 14 169 6 | 56 63 59 46 57 59 131 55
R08 | 1000 9 16 20 16 17 13 --- 7 | 53 56 63 59 57 67 --- 58
R09 | 3704 17 20 10 14 24 25 --- 8 | 82 87 77 77 71 84 --- 79
R11 | 3042 18 20 25 10 27 20 --- 9 | 52 30 55 51 60 49 --- 49
R12 | 1025 11 29 14 13 25 17 --- 8 | 72 43 63 73 76 59 --- 63
R13 | 2558 34 46 23 44 22 27 --- 15 | 92 48 48 89 77 64 --- 67
R14 | 2110 11 22 20 16 13 11 --- 7 | 82 78 96 91 90 87 --- 86
R15 | 978 15 30 15 7 24 21 51 8 | 82 59 67 79 94 74 56 75
R16 | 2318 25 39 22 53 25 26 --- 14 | 111 96 116 114 123 122 --- 113
R17E | 1873 12 35 17 12 28 19 --- 9 | 128 126 126 124 125 122 --- 125
R18E | 809 15 32 21 23 27 16 --- 10 | 40 42 50 40 47 55 --- 43
R19E | 1646 32 59 43 82 63 49 --- 24 | 39 62 44 75 43 56 --- 36
R20E | 1693 56 58 32 51 29 25 --- 19 | 91 94 98 97 95 105 --- 93
R21E | 709 14 28 14 11 31 16 332 9 | 49 42 46 51 58 53 78 47
R22E | 3246 51 42 74 84 71 42 --- 28 | 82 93 86 100 86 75 --- 74
R24E | 730 16 32 13 17 20 23 --- 9 | 72 70 69 73 70 72 --- 70
------+----------------------------------------------+------------------------------------------
RMS | 2010 25 32 27 35 31 24 288 |T 69 65 68 71 70 69 108 66
WRMS | 2010 17 27 18 15 23 20 288 |NE 68 60 65 67 68 65 114 64
MEDI | 1321 15 28 20 16 25 20 169 |MD 68 61 63 73 68 60 78 60
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