[IGSREPORT-28016] Wk 2161 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 28 05:22:03 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2161 (Jun 06, 2021 - Jun 12, 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 2.2161.
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:
igl2161[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2161 in the SP3 format.
igl21617.sum Combination Report for GPS Week 2161.
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 | -3.2 ns
1 | -4.5 ns
2 | -5.1 ns
3 | -4.3 ns
4 | -3.4 ns
5 | -3.1 ns
6 | -1.5 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 1.2161, 1a.2161).
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 2.2161.0-6)
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 3.2161.0-6).
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 2161 summary. (Jun 06, 2021 - Jun 12, 2021)
Table 1.2161.a GPS week : 2161 MJD: 59371.0-59377.0
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 -1 -7 -23 -41 .14 23 18 | -11093 -828 3369 7967
| 1 1 1 8 17 20 .03 | 2197 2261
emx n/a| 0 0 -2 15 -8 -26 -.10 47 32 | -8381 -273 3374 8553
| 0 1 3 15 14 49 .03 | 8387 1434
esx n/a| 0 0 0 48 -2 -31 -.10 40 26 | -2611 -406 3360 7553
| 1 1 2 19 19 27 .03 | 2320 1803
gfz n/a| 0 1 3 -24 -15 -48 -.09 30 18 | 0 -1177 3393 7717
| 0 1 2 9 11 28 .06 | 0 1714
grg n/a| 2 0 1 -15 24 -58 .34 36 27 | -3217 -953 3409 7584
| 1 1 3 7 27 23 .06 | 952 2142
iac n/a| -2 0 -5 9 16 199 -.20 29 28 | -1570 -219 3370 8491
| 3 1 5 25 46 60 .05 | 1547 1483
mcc n/a| -1 3 -9 -17 -45 -555 -.58 174 174 | --- --- --- ---
| 6 5 20 76 64 700 .32 | --- ---
Table 1.2161.b GPS week : 2161 MJD: 59371.0-59377.0
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 | 16 17 17 15 17 20 17 |
R02 | 7 7 7 6 7 8 8 |
R03 | 6 7 7 7 6 6 7 |
R04 | 10 11 9 9 12 7 11 |
R05 | 8 8 8 7 10 8 8 |
R07 | 7 5 6 7 6 7 8 |
R08 | 8 7 8 9 6 5 9 |
R09 | 12 11 9 10 12 16 22 |
R11 | 8 10 10 11 9 10 8 |
R12 | 8 8 10 9 10 12 10 |
R13 | 17 17 17 20 20 21 21 |
R14 | 6 8 9 9 9 10 10 |
R15 | 6 7 8 8 8 10 10 |
R16 | 12 15 11 12 16 18 16 |
R17 | 8 7 7 8 9 9 8 |
R18 | 7 7 8 9 12 11 9 |
R19 | 27 27 26 23 26 24 22 |
R20 | 27 27 29 26 28 34 34 |
R21 | 8 10 8 8 8 11 9 |
R22 | 30 30 31 29 26 27 27 |
R24 | 11 11 13 10 12 11 12 |
Table 1.2161.c GPS week : 2161 MJD: 59371.0-59377.0
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 2161 0 | 1 -83 193 1924 -1383 -6039 81.8 1430 1430 | -3218 0
brd 2161 1 | -41 -18 109 1493 306 -3909 82.3 1648 1648 | -4494 0
brd 2161 2 | 44 -40 220 -747 -1388 -4281 83.7 1437 1437 | -5120 0
brd 2161 3 | 69 9 186 -829 -1460 -463 82.1 1484 1484 | -4290 0
brd 2161 4 | 45 71 128 -1668 -668 3873 82.0 1538 1538 | -3443 0
brd 2161 5 | -25 114 169 878 2535 2979 82.6 1616 1616 | -3080 0
brd 2161 6 | 0 37 113 -77 1166 -1964 82.5 1597 1597 | -1456 0
-------------+------------------------------------------------------------+----------------
brd 2161 mean| 13 12 160 139 -127 -1400 82.4 1535 1535 | -3585 0
brd 2161 sdev| 40 67 43 1329 1537 3748 .6 87 87 | 1198 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 2.2161.0 GPS week: 2161 Day: 0 MJD: 59371
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 0 -24 -41 .15 19 15 | -9330 2048 3190 7857
emx n/a| 0 1 5 15 -6 -95 -.11 47 30 | -8716 1513 3177 8596
esx n/a| -1 2 0 45 -38 -16 -.10 44 29 | -4346 1238 3178 6172
gfz n/a| 0 1 -1 -27 -30 -80 -.19 28 18 | 0 246 3224 7410
grg n/a| 2 -2 -2 -10 21 -49 .43 37 24 | -3970 1073 3264 7593
iac n/a| 0 -1 -2 -3 91 255 -.17 24 20 | -2345 1703 3187 8464
mcc n/a| 4 13 -41 -19 0 804 -.31 173 173 | --- --- --- ---
Table 2.2161.1 GPS week: 2161 Day: 1 MJD: 59372
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 -8 -49 -78 .14 22 14 | -8526 -196 3301 8116
emx n/a| -1 0 0 8 -21 -74 -.14 50 27 | -20430 -116 3321 8838
esx n/a| 0 -1 -3 38 13 -75 -.06 42 24 | 385 425 3300 7631
gfz n/a| 1 3 3 -21 -19 -19 -.10 30 19 | 0 -115 3352 7595
grg n/a| 3 -1 -2 -27 24 -63 .38 32 27 | -4399 -308 3341 7676
iac n/a| -1 1 -1 -6 55 269 -.27 24 22 | -138 -3052 3303 8678
mcc n/a| -8 0 -19 108 -53 -895 -.12 186 186 | --- --- --- ---
Table 2.2161.2 GPS week: 2161 Day: 2 MJD: 59373
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 -18 -43 .11 23 17 | -8912 -2431 3183 7201
emx n/a| 0 1 -4 -4 -15 6 -.05 47 34 | 4335 -1420 3231 7865
esx n/a| -2 2 3 75 -11 -24 -.15 42 30 | -5840 -2079 3177 6292
gfz n/a| 0 0 3 -32 -9 -23 -.02 29 16 | 0 -2987 3211 6937
grg n/a| 3 0 1 -16 36 -22 .32 32 29 | -3948 -2646 3178 6985
iac n/a| 0 -2 -2 59 11 118 -.14 26 25 | -3772 -71 3183 7740
mcc n/a| 5 0 0 52 -122 -1115 -.52 130 130 | --- --- --- ---
Table 2.2161.3 GPS week: 2161 Day: 3 MJD: 59374
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 -1 -13 1 -18 .09 18 13 | -11384 -2465 2868 8688
emx n/a| 0 0 -3 38 -16 50 -.11 46 37 | -4467 -1388 2891 9224
esx n/a| -1 0 2 56 21 -20 -.12 41 24 | -2378 -1549 2873 10376
gfz n/a| 0 1 4 -5 -5 -88 -.09 30 19 | 0 -2958 2914 8398
grg n/a| 2 -2 4 -15 31 -61 .37 32 21 | -3233 -2744 2911 8213
iac n/a| -1 -1 -1 26 -47 128 -.17 30 30 | -2926 -198 2895 9322
mcc n/a| -9 4 2 -23 -72 -1343 -.76 144 144 | --- --- --- ---
Table 2.2161.4 GPS week: 2161 Day: 4 MJD: 59375
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -14 -9 -50 .13 26 23 | -12163 -1657 3742 8729
emx n/a| 0 1 -4 -1 -20 -38 -.12 44 35 | -14091 -585 3719 9266
esx n/a| 0 -1 1 58 -9 9 -.13 34 21 | -1472 -1429 3702 7012
gfz n/a| 0 1 3 -30 2 -52 -.07 27 14 | 0 -1635 3757 8478
grg n/a| 1 0 -1 -3 8 -88 .33 37 32 | -2064 -2573 3733 8103
iac n/a| -6 0 -6 1 -24 244 -.25 32 32 | -1259 -72 3714 9201
mcc n/a| -3 -4 25 -107 74 -531 -.58 200 200 | --- --- --- ---
Table 2.2161.5 GPS week: 2161 Day: 5 MJD: 59376
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 0 -15 -37 -21 .18 26 23 | -13741 -3369 4270 7644
emx n/a| -1 0 -4 27 15 -25 -.08 46 31 | -1901 -1730 4250 8032
esx n/a| -1 0 0 50 0 -45 -.09 41 30 | -4360 -1969 4272 7894
gfz n/a| 0 0 5 -33 -28 -55 -.14 34 21 | 0 -2216 4343 7805
grg n/a| 4 0 0 -18 68 -38 .26 39 30 | -1977 -2121 4341 7172
iac n/a| -6 0 -7 -11 13 177 -.17 31 31 | -1167 -716 4293 8047
mcc n/a| 0 6 -12 -46 -61 -361 -1.12 162 162 | --- --- --- ---
Table 2.2161.6 GPS week: 2161 Day: 6 MJD: 59377
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 -3 -26 -32 .19 29 20 | -13597 2274 3034 7536
emx n/a| 0 -1 -6 22 7 -7 -.13 48 31 | -13397 1812 3035 8053
esx n/a| 1 1 1 11 5 -46 -.07 36 20 | -271 2515 3024 7496
gfz n/a| 0 1 6 -21 -16 -19 -.05 28 16 | 0 1422 2951 7401
grg n/a| 0 0 8 -14 -20 -84 .27 39 26 | -2929 2648 3098 7349
iac n/a| -5 -2 -17 1 18 204 -.22 37 37 | 614 872 3016 7986
mcc n/a| 1 1 -18 -86 -81 -445 -.62 224 224 | --- --- --- ---
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 3.2161.0 GPS week: 2161 Day: 0 MJD: 59371
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 412 33 26 57 32 44 17 --- 16 | 126 107 98 113 104 105 --- 109
R02 | 881 5 10 17 10 20 21 266 6 | 53 46 48 59 51 60 173 52
R03 | 1044 7 11 6 12 15 23 157 6 | 59 57 61 62 57 70 143 60
XR04 | 710 16 18 8 --- 19 30 --- 10 | 67 68 56 --- 64 44 --- 58
R05 | 1122 9 22 10 22 30 15 119 8 | 44 48 47 47 57 42 63 43
R07 | 917 5 12 6 22 17 21 201 6 | 64 56 66 77 66 60 268 64
R08 | 889 8 17 29 16 11 21 --- 8 | 52 48 76 63 58 53 --- 57
R09E | 3732 28 22 19 19 26 33 --- 11 | 98 99 90 94 76 92 --- 90
XR11E | 3469 14 23 13 17 --- 15 --- 8 | 47 43 50 58 --- 43 --- 48
R12E | 901 7 32 16 13 16 20 --- 7 | 59 59 58 66 66 58 --- 59
R13E | 1248 28 40 35 53 39 29 --- 16 | 43 36 52 67 56 52 --- 44
R14E | 1343 9 22 15 13 14 13 --- 6 | 63 68 74 74 69 67 --- 67
R15E | 1735 7 27 15 14 13 10 114 6 | 27 25 32 31 35 29 57 27
R16E | 1364 25 22 26 32 15 27 --- 11 | 61 61 67 73 72 71 --- 63
R17 | 1675 10 31 17 13 16 19 --- 7 | 66 49 61 68 79 79 --- 67
R18 | 717 15 25 15 9 11 19 --- 7 | 50 43 60 51 55 57 --- 51
R19 | 1588 30 128 51 30 83 38 --- 26 | 98 32 56 94 77 88 --- 76
R20M | 831 25 103 102 48 48 32 --- 26 | 112 28 37 119 127 109 --- 92
R21M | 1385 8 34 16 12 15 16 132 7 | 79 67 71 75 79 71 64 73
R22M | 1485 38 51 118 61 97 38 --- 30 | 39 67 86 48 56 47 --- 37
R24 | 547 11 50 28 18 27 11 --- 10 | 66 30 66 73 84 66 --- 64
------+----------------------------------------------+------------------------------------------
RMS | 1430 19 47 44 28 37 24 173 |T 65 54 62 70 69 64 128 61
WRMS | 1430 15 30 29 18 24 20 173 |NE 61 47 59 66 64 61 161 59
MEDI | 1122 11 25 17 17 17 21 132 |MD 61 49 61 67 66 60 64 60
Table 3.2161.1 GPS week: 2161 Day: 1 MJD: 59372
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 682 42 28 40 43 48 20 --- 17 | 93 75 71 84 78 81 --- 78
R02 | 885 7 10 19 12 19 18 137 6 | 41 35 37 46 30 52 93 39
R03 | 666 7 10 11 27 21 10 109 7 | 43 40 39 61 42 50 42 45
XR04 | 690 22 25 17 --- 11 30 --- 11 | 50 48 37 --- 48 31 --- 40
R05 | 956 12 24 19 16 16 23 63 8 | 32 35 41 42 30 32 26 31
R07 | 1437 8 15 6 16 8 11 391 5 | 43 39 43 49 39 44 299 42
R08 | 1205 11 13 14 20 11 16 --- 6 | 36 34 31 28 38 34 --- 31
R09E | 3817 21 17 25 23 27 31 --- 11 | 102 86 84 88 89 102 --- 92
XR11E | 4346 16 23 14 23 --- 25 --- 10 | 44 42 53 53 --- 54 --- 49
R12E | 1091 11 31 12 18 15 19 --- 8 | 55 52 58 64 58 54 --- 56
R13E | 1532 35 32 24 53 32 36 --- 16 | 35 34 40 83 49 64 --- 42
R14E | 2201 11 26 18 12 19 17 --- 7 | 65 61 68 64 67 75 --- 65
R15E | 2617 9 28 17 15 16 14 76 7 | 26 23 28 33 34 31 47 27
R16E | 1588 32 28 32 54 26 21 --- 15 | 62 55 61 82 67 48 --- 57
R17 | 2162 6 29 17 13 12 9 --- 6 | 35 31 33 40 44 33 --- 35
R18 | 746 10 27 17 8 17 11 --- 6 | 28 25 32 27 42 31 --- 29
R19 | 1534 28 147 39 33 63 38 --- 27 | 43 64 29 48 51 46 --- 38
R20M | 844 36 103 102 42 42 35 --- 27 | 53 43 45 54 53 47 --- 42
R21M | 1275 10 33 21 16 12 36 117 10 | 56 50 58 58 60 66 68 56
R22M | 1584 40 64 120 56 81 32 --- 30 | 37 46 58 39 43 33 --- 31
R24 | 835 11 48 32 14 18 21 --- 10 | 30 20 46 40 38 31 --- 31
------+----------------------------------------------+------------------------------------------
RMS | 1648 22 50 42 30 32 24 186 |T 48 44 47 54 50 49 95 45
WRMS | 1648 14 27 24 19 27 22 186 |NE 38 37 36 42 40 38 115 36
MEDI | 1275 11 28 19 18 18 21 109 |MD 43 42 43 49 44 47 47 42
Table 3.2161.2 GPS week: 2161 Day: 2 MJD: 59373
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 741 47 24 64 19 25 24 --- 16 | 111 90 94 105 94 102 --- 97
R02 | 1257 11 21 10 19 17 16 166 7 | 46 36 57 61 49 49 40 49
R03 | 597 9 13 9 21 22 15 123 7 | 49 47 57 69 46 61 40 54
XR04 | 1049 17 19 13 --- 16 18 --- 8 | 55 55 45 --- 49 43 --- 48
R05 | 618 20 13 21 13 8 20 83 7 | 43 35 49 35 39 46 36 38
R07 | 1422 9 14 11 9 9 20 185 5 | 47 35 48 47 48 54 127 46
R08 | 1013 9 14 15 13 25 28 --- 8 | 42 32 53 45 60 32 --- 42
R09E | 3146 22 14 21 18 18 27 --- 9 | 98 95 79 93 85 109 --- 93
XR11E | 4137 20 --- 10 17 --- 18 --- 10 | 46 --- 50 53 --- 63 --- 51
R12E | 721 16 29 16 16 18 33 --- 9 | 40 43 44 45 51 62 --- 45
R13E | 1252 30 41 27 56 24 38 --- 17 | 39 41 44 77 46 44 --- 40
R14E | 1365 16 26 21 17 15 24 --- 9 | 74 75 84 85 80 73 --- 76
R15E | 1540 13 27 21 16 13 13 89 7 | 25 21 26 29 35 28 61 24
R16E | 1303 23 25 22 27 24 19 --- 10 | 61 58 60 77 72 70 --- 63
R17 | 2177 12 30 14 9 14 15 --- 7 | 49 33 48 47 53 55 --- 46
R18 | 690 14 28 22 15 18 15 --- 8 | 39 29 44 36 49 45 --- 38
R19 | 731 44 108 39 27 74 45 --- 25 | 74 42 47 59 62 64 --- 54
R20M | 936 37 107 102 36 67 29 --- 28 | 82 42 44 79 93 67 --- 66
R21M | 1785 11 28 21 10 20 20 95 8 | 68 55 59 58 59 74 56 62
R22M | 2272 32 85 111 82 64 27 --- 31 | 42 65 44 67 43 44 --- 36
R24 | 652 14 56 20 17 26 39 --- 13 | 46 23 44 48 64 60 --- 45
------+----------------------------------------------+------------------------------------------
RMS | 1437 23 47 42 29 32 26 130 |T 56 47 53 60 58 59 60 53
WRMS | 1437 17 34 30 16 29 25 130 |NE 49 36 49 49 51 50 60 46
MEDI | 1252 16 26 21 17 18 20 95 |MD 47 42 48 58 51 60 40 48
Table 3.2161.3 GPS week: 2161 Day: 3 MJD: 59374
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 444 31 31 55 32 18 21 --- 14 | 94 99 95 96 93 89 --- 92
R02 | 1280 7 19 8 14 13 18 234 5 | 52 39 49 51 54 43 85 47
R03 | 465 6 16 16 22 11 24 132 7 | 55 48 67 73 56 44 44 56
XR04 | 929 15 12 13 --- 18 24 --- 8 | 50 45 43 --- 40 41 --- 44
R05 | 1022 12 19 14 18 12 21 97 7 | 42 42 51 60 49 64 38 48
R07 | 1897 11 17 18 18 9 20 96 7 | 52 44 50 66 57 63 111 53
R08 | 904 11 16 11 15 18 41 --- 9 | 46 44 48 53 59 39 --- 45
R09E | 3040 16 22 17 25 22 28 --- 9 | 98 102 103 106 90 105 --- 99
XR11E | 3254 13 22 17 21 --- 36 --- 11 | 53 75 60 62 --- 47 --- 53
R12E | 675 10 34 17 18 16 23 --- 8 | 56 40 51 55 58 71 --- 54
R13E | 1350 22 59 46 68 29 50 --- 20 | 44 40 46 75 63 70 --- 47
R14E | 1634 15 22 23 18 17 26 --- 9 | 79 79 88 87 93 88 --- 83
R15E | 1588 8 33 15 13 17 18 143 7 | 29 26 25 30 34 37 68 27
R16E | 1231 18 26 30 35 25 21 --- 11 | 71 70 86 97 83 75 --- 77
R17 | 909 9 30 15 10 18 24 --- 7 | 61 43 50 58 59 59 --- 56
R18 | 884 10 37 18 14 20 28 --- 9 | 57 39 54 51 54 45 --- 50
R19 | 1623 33 95 50 29 68 49 --- 23 | 90 57 65 83 66 87 --- 72
R20M | 783 27 100 96 45 49 41 --- 26 | 98 45 55 115 101 98 --- 86
R21M | 1445 9 34 20 13 24 15 116 8 | 69 52 60 69 70 68 55 65
R22M | 2950 30 76 102 62 79 34 --- 28 | 33 57 58 44 42 41 --- 29
R24 | 654 11 56 11 10 20 26 --- 10 | 56 31 52 52 60 53 --- 52
------+----------------------------------------------+------------------------------------------
RMS | 1483 18 46 41 30 32 30 144 |T 61 53 59 69 64 63 66 58
WRMS | 1483 13 37 24 19 21 30 144 |NE 56 43 52 60 55 53 69 52
MEDI | 1231 12 30 17 18 18 24 116 |MD 56 45 54 62 59 63 55 53
Table 3.2161.4 GPS week: 2161 Day: 4 MJD: 59375
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 1000 47 38 45 29 17 32 --- 16 | 93 97 112 100 98 83 --- 95
R02 | 1777 10 12 12 15 22 19 277 6 | 41 31 42 35 45 36 149 36
R03 | 665 10 12 9 13 14 20 118 5 | 53 44 44 49 47 37 73 45
XR04 | 658 27 15 13 --- 23 29 --- 11 | 56 46 47 --- 38 29 --- 42
R05 | 1228 14 24 18 18 31 31 89 10 | 35 41 48 54 29 71 44 43
R07 | 759 11 15 8 12 13 14 117 5 | 46 42 53 59 57 55 101 52
R08 | 816 6 10 14 18 11 19 --- 6 | 41 34 47 48 36 31 --- 38
R09E | 3612 19 26 19 18 27 48 --- 12 | 104 112 115 109 96 111 --- 105
XR11E | 3319 15 14 19 13 --- 25 --- 8 | 59 57 69 63 --- 52 --- 60
R12E | 644 12 31 16 22 22 29 --- 9 | 89 90 96 93 89 107 --- 92
R13E | 943 35 44 35 65 38 40 --- 20 | 38 31 38 63 51 51 --- 32
R14E | 2049 15 18 19 13 20 29 --- 8 | 56 53 55 52 55 58 --- 53
R15E | 1617 9 29 11 12 19 29 331 8 | 27 24 24 26 36 41 164 26
R16E | 1402 27 30 32 39 36 45 --- 15 | 53 54 68 74 57 69 --- 57
R17 | 863 11 29 15 11 18 29 --- 8 | 43 36 50 41 51 56 --- 44
R18 | 722 15 36 25 14 19 46 --- 12 | 44 31 47 37 44 44 --- 38
R19 | 2384 48 89 33 42 90 38 --- 25 | 75 37 52 80 57 58 --- 58
R20M | 1076 42 92 84 41 74 22 --- 27 | 92 51 50 81 107 76 --- 74
R21M | 1325 19 25 14 10 17 14 130 7 | 71 56 62 62 61 63 102 62
R22M | 1482 48 77 77 30 69 38 --- 25 | 36 75 62 66 36 48 --- 39
R24 | 1538 20 53 23 16 15 31 --- 12 | 55 27 49 48 45 60 --- 46
------+----------------------------------------------+------------------------------------------
RMS | 1537 26 44 34 27 37 32 199 |T 57 50 58 62 56 58 105 54
WRMS | 1537 23 35 21 14 32 32 199 |NE 48 36 47 50 44 47 91 44
MEDI | 1228 15 29 19 16 20 29 118 |MD 53 44 50 59 51 56 101 46
Table 3.2161.5 GPS week: 2161 Day: 5 MJD: 59376
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 733 55 32 58 37 32 34 --- 20 | 143 146 137 142 130 125 --- 133
R02 | 1214 11 19 9 10 20 30 211 8 | 40 33 44 46 55 45 193 41
R03 | 648 10 11 13 15 12 17 154 6 | 48 43 53 50 59 47 102 48
XR04 | 515 11 14 14 --- 12 13 --- 6 | 60 64 58 --- 55 59 --- 59
R05 | 1470 14 20 19 21 21 15 45 8 | 35 44 43 43 24 31 48 32
R07 | 1291 7 14 17 11 15 24 218 6 | 42 43 36 47 45 61 139 43
R08 | 999 10 9 8 15 9 16 --- 5 | 42 40 42 51 51 45 --- 43
R09E | 3163 34 38 28 20 41 52 --- 16 | 101 94 100 104 87 100 --- 94
XR11E | 3460 16 19 14 17 --- 27 --- 9 | 44 53 48 49 --- 52 --- 46
R12E | 971 13 35 17 31 31 36 --- 12 | 112 108 119 117 106 121 --- 111
R13E | 2358 47 37 33 67 33 46 --- 20 | 75 79 97 93 82 88 --- 79
R14E | 2217 10 29 20 23 19 31 --- 10 | 95 91 91 89 92 110 --- 93
R15E | 1282 13 27 14 26 23 32 148 10 | 28 26 29 37 36 42 149 28
R16E | 1348 30 44 25 50 63 29 --- 18 | 71 63 76 92 107 64 --- 73
R17 | 856 8 36 16 17 13 26 --- 8 | 37 26 36 43 41 47 --- 36
R18 | 799 21 25 21 13 20 38 --- 10 | 36 41 49 51 42 50 --- 42
R19 | 2839 38 107 50 44 52 24 --- 24 | 58 34 44 60 53 41 --- 41
R20M | 1484 32 113 105 66 88 38 --- 33 | 74 76 66 86 84 56 --- 64
R21M | 1367 18 31 12 9 30 36 134 10 | 63 53 58 58 68 61 45 57
R22M | 1522 25 39 102 59 74 24 --- 26 | 35 43 43 43 33 36 --- 28
R24 | 1267 18 52 18 14 22 22 --- 11 | 48 28 35 44 45 48 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1615 26 46 41 34 39 31 162 |T 61 58 62 67 64 63 112 58
WRMS | 1615 23 31 30 21 30 31 162 |NE 44 39 44 48 47 47 120 42
MEDI | 1291 16 31 18 20 22 29 148 |MD 48 44 49 51 55 52 102 46
Table 3.2161.6 GPS week: 2161 Day: 6 MJD: 59377
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01M | 1989 40 29 45 25 43 45 --- 17 | 155 149 136 148 140 140 --- 142
R02 | 1925 10 19 17 13 19 31 164 8 | 53 41 56 58 61 55 139 53
R03 | 567 10 12 13 13 12 27 119 6 | 59 52 62 66 59 58 44 59
XR04 | 693 14 24 13 --- 32 25 --- 10 | 66 67 57 --- 55 63 --- 60
R05 | 1279 13 21 21 10 11 24 47 7 | 45 48 49 45 44 49 48 44
R07 | 1864 16 17 7 11 12 36 479 7 | 61 53 66 76 72 85 209 67
R08 | 1391 18 14 9 13 25 30 --- 8 | 56 48 60 67 73 66 --- 60
R09E | 3126 50 42 24 29 87 45 --- 21 | 114 111 104 108 57 113 --- 96
XR11E | 2963 14 14 12 13 --- 25 --- 8 | 45 47 49 47 --- 49 --- 45
R12E | 615 15 25 12 13 35 37 --- 10 | 114 118 122 124 124 127 --- 119
R13E | 1742 37 42 40 54 45 53 --- 20 | 78 76 67 87 91 89 --- 74
R14E | 2068 19 34 17 19 18 27 --- 9 | 74 83 84 86 75 94 --- 81
R15E | 817 11 26 11 20 30 29 130 9 | 42 39 41 45 50 54 78 40
R16E | 1017 29 43 22 39 34 40 --- 15 | 74 69 81 96 103 80 --- 80
R17 | 842 14 32 9 11 18 25 --- 8 | 60 39 53 56 58 57 --- 53
R18 | 927 12 20 18 14 14 41 --- 9 | 48 46 61 49 52 62 --- 51
R19 | 3013 51 96 38 21 38 46 --- 22 | 114 36 60 92 82 96 --- 80
R20M | 1418 46 131 96 56 66 47 --- 34 | 133 80 59 136 141 122 --- 106
R21M | 721 16 38 18 10 23 14 102 9 | 81 60 67 71 79 75 52 72
R22M | 830 49 27 86 58 73 44 --- 27 | 46 34 78 45 48 50 --- 37
R24 | 629 19 57 10 16 27 27 --- 12 | 72 33 56 63 69 60 --- 58
------+----------------------------------------------+------------------------------------------
RMS | 1597 29 48 36 28 39 37 224 |T 75 63 69 78 76 78 95 70
WRMS | 1597 20 31 20 16 26 37 224 |NE 63 46 58 63 62 65 110 58
MEDI | 1279 16 27 17 14 27 31 119 |MD 66 52 61 67 69 66 52 60
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