[IGSREPORT-28002] Wk 2160 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 21 02:59:26 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2160 (May 30, 2021 - Jun 05, 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 2.2160.
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:
igl2160[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2160 in the SP3 format.
igl21607.sum Combination Report for GPS Week 2160.
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 | -5.8 ns
1 | -5.7 ns
2 | -3.6 ns
3 | -4.6 ns
4 | -5.6 ns
5 | -2.4 ns
6 | -3.8 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 1.2160, 1a.2160).
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 2.2160.0-6)
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 3.2160.0-6).
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 2160 summary. (May 30, 2021 - Jun 05, 2021)
Table 1.2160.a GPS week : 2160 MJD: 59364.0-59370.0
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| -1 1 -1 -4 -9 -25 .12 23 18 | -8954 -596 3089 7552
| 0 1 2 8 16 10 .05 | 1143 1969
emx n/a| -1 0 3 17 -46 -10 -.10 47 33 | -8562 -190 3077 8157
| 1 1 2 18 20 46 .04 | 9160 1291
esx n/a| 0 0 0 61 2 -24 -.09 39 27 | -7933 -132 3078 6252
| 1 1 1 12 12 23 .04 | 3003 1942
gfz n/a| 0 1 0 -16 5 -31 -.09 32 17 | 0 -663 3116 7371
| 1 2 1 18 26 28 .08 | 0 1933
grg n/a| 1 0 1 -29 20 -39 .31 33 24 | -4312 -534 3087 7133
| 2 0 1 8 17 43 .04 | 775 1619
iac n/a| 0 -1 -4 -18 12 148 -.16 28 25 | -2657 -116 3088 8065
| 1 2 3 39 33 43 .03 | 1176 1894
mcc n/a| -2 2 -26 -68 -28 117 -.24 132 132 | --- --- --- ---
| 12 5 5 106 93 264 .47 | --- ---
Table 1.2160.b GPS week : 2160 MJD: 59364.0-59370.0
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 | 15 16 14 17 16 15 16 |
R02 | 9 7 6 8 4 5 8 |
R03 | 9 6 8 5 6 5 6 |
R04 | 9 10 10 11 11 8 10 |
R05 | 12 10 9 10 8 8 8 |
R07 | 6 6 8 12 6 7 8 |
R08 | 8 8 6 6 6 8 7 |
R09 | 11 11 10 10 12 13 12 |
R11 | 10 10 9 10 9 10 9 |
R12 | 7 7 7 8 9 8 9 |
R13 | 18 13 17 17 15 20 18 |
R14 | 8 9 8 8 7 7 8 |
R15 | 8 9 9 8 10 7 7 |
R16 | 15 13 12 13 14 13 14 |
R17 | 7 9 9 6 8 7 9 |
R18 | 9 10 10 11 10 7 8 |
R19 | 26 26 25 26 25 23 28 |
R20 | 30 28 27 29 31 33 28 |
R21 | 11 9 8 8 8 8 9 |
R22 | 33 33 30 27 29 28 31 |
R24 | 10 13 13 11 12 13 10 |
Table 1.2160.c GPS week : 2160 MJD: 59364.0-59370.0
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 2160 0 | 41 -29 195 -346 -998 6245 84.1 1740 1740 | -5823 0
brd 2160 1 | -15 17 220 -1463 -3 5238 83.6 1607 1607 | -5681 0
brd 2160 2 | 15 4 246 -1193 586 2009 82.3 1300 1300 | -3592 0
brd 2160 3 | -11 4 153 -186 732 -798 82.7 1359 1359 | -4648 0
brd 2160 4 | -5 -89 120 175 906 -3500 84.8 1734 1734 | -5552 0
brd 2160 5 | -64 -7 61 18 218 -4505 81.6 1550 1550 | -2417 0
brd 2160 6 | -39 -45 140 509 -457 -6808 80.5 1500 1500 | -3829 0
-------------+------------------------------------------------------------+----------------
brd 2160 mean| -11 -20 162 -355 140 -302 82.8 1541 1541 | -4506 0
brd 2160 sdev| 34 36 63 721 685 4989 1.5 170 170 | 1283 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 2.2160.0 GPS week: 2160 Day: 0 MJD: 59364
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 -5 -14 -25 -43 .12 27 23 | -7401 -29 3235 6845
emx n/a| -1 2 0 2 -48 3 -.09 48 35 | -5382 -255 3226 7445
esx n/a| 0 0 0 80 2 -13 -.12 36 30 | -11324 1498 3218 6582
gfz n/a| 0 3 1 10 -12 -14 -.05 31 17 | 0 -796 3248 6720
grg n/a| 3 -1 3 -36 52 31 .29 31 23 | -5756 -139 3262 6685
iac n/a| -1 0 -2 -59 -28 131 -.17 34 31 | -4470 1082 3227 7363
mcc n/a| -9 4 -19 -185 -153 -336 -.11 130 130 | --- --- --- ---
Table 2.2160.1 GPS week: 2160 Day: 1 MJD: 59365
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 -4 -10 10 -18 .09 22 17 | -7359 -2898 3071 7338
emx n/a| 1 -2 0 53 -32 40 -.13 46 33 | -5047 -1285 3049 8103
esx n/a| 0 0 1 63 -19 -19 -.05 39 32 | -7738 -2326 3080 5720
gfz n/a| -1 2 0 -14 -35 0 .02 30 17 | 0 -2310 3106 7201
grg n/a| 2 0 2 -43 9 -84 .27 33 22 | -4696 -2298 3026 7168
iac n/a| 2 2 0 -32 73 117 -.13 30 26 | -3284 -1278 3085 7903
mcc n/a| -19 2 -32 112 47 215 -.17 116 116 | --- --- --- ---
Table 2.2160.2 GPS week: 2160 Day: 2 MJD: 59366
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 -1 -2 -14 7 -27 .06 20 18 | -9506 1061 3041 7671
emx n/a| 0 -1 1 13 -70 39 -.15 45 34 | -10725 770 3047 8236
esx n/a| -1 1 3 63 -5 13 -.04 40 27 | -2606 1272 3034 5878
gfz n/a| 0 3 2 -34 40 6 -.03 32 21 | 0 414 3059 7558
grg n/a| 2 -1 1 -25 36 -46 .32 32 22 | -4113 575 3006 7009
iac n/a| 0 0 0 51 -15 80 -.17 27 27 | -2840 1448 3043 8242
mcc n/a| 11 3 -23 -148 78 135 -1.09 124 124 | --- --- --- ---
Table 2.2160.3 GPS week: 2160 Day: 3 MJD: 59367
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 1 -4 -26 .08 22 17 | -8841 -1774 2940 7847
emx n/a| -1 0 4 6 -60 -28 -.09 46 34 | -12088 -1241 2924 8494
esx n/a| 0 0 0 47 7 -30 -.07 37 29 | -6144 -1097 2929 5817
gfz n/a| -1 1 0 -42 28 -48 -.18 33 16 | 0 -1351 2985 7594
grg n/a| 3 0 2 -30 16 3 .36 31 24 | -4132 -1299 2992 7052
iac n/a| -1 -3 -9 15 17 170 -.11 28 24 | -1370 -1927 2940 8457
mcc n/a| -14 6 -20 -131 -13 -126 -.48 163 163 | --- --- --- ---
Table 2.2160.4 GPS week: 2160 Day: 4 MJD: 59368
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 0 -2 -28 -13 .19 25 20 | -9690 -3027 3102 7393
emx n/a| -3 1 8 2 -53 0 -.03 43 29 | -26451 -1580 3078 8019
esx n/a| 2 -1 0 44 0 -59 -.10 40 26 | -9704 -2916 3078 6056
gfz n/a| 1 1 0 0 2 -56 -.11 33 17 | 0 -3336 3124 7143
grg n/a| 2 0 1 -16 18 -48 .29 34 25 | -4156 -2738 3124 7014
iac n/a| -2 0 -5 -30 27 142 -.20 22 19 | -2906 -1843 3102 7931
mcc n/a| -2 -4 -23 -99 26 257 -.37 130 130 | --- --- --- ---
Table 2.2160.5 GPS week: 2160 Day: 5 MJD: 59369
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 2 0 3 0 -16 .16 21 14 | -10140 1890 3195 8697
emx n/a| 0 0 6 24 -48 -33 -.12 49 32 | -970 1954 3188 9170
esx n/a| 2 0 -1 67 16 -46 -.15 41 24 | -10677 1699 3186 8287
gfz n/a| 0 -1 0 -23 -6 -64 -.10 32 18 | 0 2526 3233 8529
grg n/a| -1 1 1 -28 6 -39 .27 30 21 | -3192 1622 3169 7987
iac n/a| 0 -5 -5 -51 19 195 -.16 27 22 | -2766 2871 3194 9092
mcc n/a| 3 -5 -31 32 -31 220 .12 126 126 | --- --- --- ---
Table 2.2160.6 GPS week: 2160 Day: 6 MJD: 59370
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 0 5 -24 -32 .13 20 15 | -9743 601 3039 7076
emx n/a| -1 0 4 21 -8 -91 -.13 50 33 | 723 302 3030 7633
esx n/a| 2 1 0 64 15 -13 -.11 42 23 | -7338 944 3026 5424
gfz n/a| 1 -3 0 -12 21 -42 -.19 33 17 | 0 208 3058 6852
grg n/a| 0 0 -2 -25 3 -90 .37 36 28 | -4140 536 3036 7016
iac n/a| -2 -3 -5 -23 -9 198 -.18 27 22 | -966 -1169 3028 7470
mcc n/a| 13 7 -33 -58 -154 456 .39 137 137 | --- --- --- ---
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 3.2160.0 GPS week: 2160 Day: 0 MJD: 59364
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 | 1247 37 22 28 41 38 22 --- 15 | 93 74 63 87 57 63 --- 71
R02 | 2899 18 15 14 14 12 38 225 8 | 53 54 63 70 57 77 181 60
R03 | 802 17 11 16 13 15 36 146 8 | 62 68 76 74 64 84 52 69
XR04 | 675 13 16 16 --- 11 26 --- 8 | 64 64 46 --- 51 55 --- 54
R05 | 759 17 27 22 21 28 45 66 12 | 42 48 45 42 57 58 43 43
R07 | 1012 10 11 13 11 13 23 91 6 | 68 65 70 79 73 89 110 73
R08 | 1715 15 8 10 13 12 34 --- 7 | 52 54 58 60 62 52 --- 55
R09E | 4223 30 23 21 20 23 28 --- 11 | 113 113 118 121 109 112 --- 113
XR11E | 3781 17 15 14 18 --- 31 --- 9 | 38 45 42 51 --- 51 --- 43
R12E | 706 9 28 11 14 12 21 --- 7 | 46 40 48 54 52 51 --- 48
R13E | 2040 32 38 28 57 25 48 --- 17 | 56 42 59 81 71 51 --- 53
R14E | 709 15 28 20 7 12 26 --- 8 | 54 51 53 56 60 59 --- 54
R15E | 794 17 28 12 13 11 31 96 8 | 73 73 72 75 82 79 113 74
R16E | 1394 36 38 18 48 25 25 --- 15 | 55 50 64 87 76 57 --- 62
R17 | 1764 12 30 12 11 13 20 --- 7 | 69 48 58 69 73 63 --- 64
R18 | 1389 14 31 16 16 17 23 --- 8 | 62 46 71 59 71 66 --- 62
R19 | 606 48 114 28 47 61 43 --- 25 | 112 41 52 104 82 80 --- 79
R20 | 931 37 111 93 34 52 62 --- 29 | 123 65 52 133 139 131 --- 104
R21 | 1386 13 46 20 23 12 26 83 10 | 87 51 69 90 85 87 36 79
R22 | 2782 53 77 101 64 81 35 --- 32 | 38 74 100 54 53 45 --- 46
R24 | 916 13 44 18 20 14 24 --- 9 | 75 42 66 79 77 73 --- 69
------+----------------------------------------------+------------------------------------------
RMS | 1739 27 48 36 31 31 34 130 |T 68 57 64 76 72 70 89 65
WRMS | 1739 23 35 30 17 23 31 130 |NE 71 56 63 76 71 73 84 66
MEDI | 1247 17 28 18 18 14 28 91 |MD 62 51 63 74 71 63 52 62
Table 3.2160.1 GPS week: 2160 Day: 1 MJD: 59365
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 35 29 49 30 33 21 --- 15 | 71 60 44 82 38 56 --- 57
R02 | 2361 11 9 14 24 14 21 144 7 | 48 49 60 69 48 46 84 52
R03 | 556 9 10 17 11 10 19 152 6 | 54 56 63 57 54 60 41 56
XR04 | 630 18 17 19 --- 8 30 --- 9 | 54 55 45 --- 49 41 --- 48
R05 | 471 16 16 23 24 10 40 84 10 | 43 44 46 40 46 57 23 41
R07 | 519 8 11 15 13 13 16 89 5 | 52 54 47 58 64 63 133 55
R08 | 1394 10 13 9 16 22 26 --- 7 | 43 43 47 53 57 35 --- 45
R09E | 4438 21 16 21 22 21 36 --- 10 | 93 101 102 97 90 118 --- 97
XR11E | 4539 14 --- 16 18 --- 21 --- 10 | 22 --- 30 34 --- 35 --- 27
R12E | 644 9 27 14 12 16 21 --- 7 | 31 29 35 38 42 33 --- 32
R13E | 1960 24 34 31 34 27 30 --- 13 | 49 37 37 53 41 43 --- 35
R14E | 797 16 20 23 19 15 20 --- 8 | 31 28 41 42 41 39 --- 33
R15E | 799 12 29 21 17 14 23 102 8 | 73 78 82 83 81 77 99 77
R16E | 2775 23 30 20 36 32 25 --- 12 | 35 30 38 46 54 32 --- 34
R17 | 1312 14 30 17 19 19 28 --- 9 | 45 42 38 42 41 42 --- 40
R18 | 822 13 24 17 15 26 30 --- 9 | 41 34 41 49 36 42 --- 37
R19 | 578 36 106 36 49 71 43 --- 25 | 61 45 38 56 47 42 --- 41
R20 | 682 39 104 94 44 48 33 --- 27 | 64 52 57 72 68 52 --- 52
R21 | 732 8 41 22 16 14 22 107 9 | 42 28 33 44 46 49 39 39
R22 | 1368 45 81 108 75 84 48 --- 33 | 33 64 54 41 29 48 --- 31
R24 | 1131 13 57 15 19 21 38 --- 12 | 48 28 46 44 40 60 --- 43
------+----------------------------------------------+------------------------------------------
RMS | 1606 22 46 39 30 33 30 116 |T 49 47 48 55 50 50 69 46
WRMS | 1606 17 33 32 17 22 26 116 |NE 49 46 47 54 47 49 64 45
MEDI | 822 14 27 20 19 19 26 102 |MD 48 44 45 49 46 46 41 41
Table 3.2160.2 GPS week: 2160 Day: 2 MJD: 59366
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 | 720 27 27 56 26 16 18 --- 13 | 60 65 45 70 62 60 --- 56
R02 | 700 8 12 11 16 11 22 96 6 | 43 43 44 39 40 34 74 38
R03 | 631 7 11 20 25 13 28 162 8 | 54 51 69 77 54 48 38 56
XR04 | 598 18 19 15 --- 14 28 --- 9 | 50 52 40 --- 43 30 --- 42
R05 | 552 18 18 24 16 15 25 133 9 | 35 42 57 57 33 47 42 41
R07 | 879 15 24 14 19 14 25 129 8 | 55 49 71 76 60 80 132 63
R08 | 676 12 14 15 11 10 15 --- 5 | 39 42 50 49 45 59 --- 45
R09E | 3980 22 24 16 23 20 27 --- 10 | 83 83 88 96 79 89 --- 83
XR11E | 5875 13 20 12 24 --- 21 --- 9 | 24 36 34 48 --- 32 --- 30
R12E | 1113 11 28 13 17 17 13 --- 7 | 34 31 34 40 43 37 --- 34
R13E | 1192 20 45 36 58 28 36 --- 16 | 32 30 55 72 61 48 --- 40
R14E | 1265 8 24 18 17 15 21 --- 7 | 31 28 36 39 42 35 --- 32
R15E | 799 11 28 16 24 9 27 60 8 | 73 71 81 84 78 66 94 74
R16E | 1259 15 31 27 37 31 25 --- 12 | 53 50 53 62 69 54 --- 52
R17 | 889 15 31 14 23 21 23 --- 9 | 55 36 43 57 51 43 --- 47
R18 | 703 11 32 20 18 21 31 --- 9 | 44 26 51 44 55 53 --- 45
R19 | 912 38 104 48 48 63 35 --- 24 | 75 42 57 83 64 60 --- 60
R20 | 615 36 94 93 40 56 36 --- 26 | 87 33 50 99 92 85 --- 75
R21 | 1271 11 34 14 20 17 14 139 8 | 58 39 48 62 61 52 66 54
R22 | 745 38 72 103 73 75 44 --- 30 | 46 59 67 47 48 33 --- 32
R24 | 1466 18 56 19 11 37 21 --- 12 | 58 28 50 51 72 40 --- 50
------+----------------------------------------------+------------------------------------------
RMS | 1299 20 45 40 32 32 27 124 |T 51 44 53 62 57 51 74 49
WRMS | 1299 18 34 27 21 22 27 124 |NE 54 43 53 62 55 51 70 50
MEDI | 879 15 28 18 23 17 25 129 |MD 53 42 50 57 55 48 66 47
Table 3.2160.3 GPS week: 2160 Day: 3 MJD: 59367
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 | 1636 40 43 49 40 25 21 --- 16 | 68 63 47 50 45 47 --- 49
R02 | 933 10 9 14 13 25 21 107 7 | 38 36 32 46 61 33 103 39
R03 | 926 6 8 12 10 11 19 182 5 | 49 47 55 53 54 34 104 48
XR04 | 745 23 21 18 --- 25 15 --- 10 | 50 49 27 --- 25 35 --- 36
R05 | 749 17 14 20 20 12 38 135 9 | 40 53 47 48 47 73 63 48
R07 | 1373 14 16 17 18 18 52 221 11 | 53 54 72 61 56 95 166 63
R08 | 596 11 14 11 15 11 18 --- 6 | 50 46 59 60 55 54 --- 53
R09E | 4240 18 21 18 29 24 26 --- 10 | 81 80 88 102 84 102 --- 87
XR11E | 3996 16 18 15 16 --- 29 --- 9 | 25 31 35 36 --- 33 --- 28
R12E | 915 14 22 15 15 17 22 --- 7 | 39 29 38 44 46 43 --- 38
R13E | 1374 30 33 29 72 23 29 --- 17 | 52 46 53 76 57 49 --- 49
R14E | 654 13 27 20 18 12 13 --- 7 | 30 28 36 37 35 30 --- 29
R15E | 665 10 27 19 14 14 18 149 7 | 70 73 59 66 77 77 102 69
R16E | 1158 14 22 27 40 33 30 --- 12 | 49 39 51 56 77 55 --- 50
R17 | 644 9 30 11 9 11 15 --- 6 | 56 35 55 51 53 57 --- 51
R18 | 670 9 41 21 21 21 33 --- 10 | 45 27 53 46 51 63 --- 46
R19 | 822 43 99 45 47 73 41 --- 25 | 81 45 56 91 72 76 --- 67
R20 | 682 30 106 97 57 49 45 --- 28 | 100 50 51 125 121 124 --- 95
R21 | 1034 14 29 17 18 16 17 163 8 | 65 46 51 66 60 53 71 57
R22 | 905 42 84 84 55 68 25 --- 27 | 29 68 66 46 30 33 --- 28
R24 | 1040 17 49 20 12 23 16 --- 10 | 55 24 46 49 59 46 --- 46
------+----------------------------------------------+------------------------------------------
RMS | 1359 22 46 37 33 31 28 163 |T 53 46 51 60 58 57 101 51
WRMS | 1359 17 34 29 16 24 24 163 |NE 55 45 51 60 56 58 101 51
MEDI | 915 14 27 19 18 21 22 149 |MD 50 46 51 51 55 53 102 49
Table 3.2160.4 GPS week: 2160 Day: 4 MJD: 59368
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 | 1263 43 21 51 37 26 20 --- 15 | 63 49 47 49 43 44 --- 44
R02 | 1067 7 11 10 10 8 10 113 4 | 41 40 49 41 42 41 84 40
R03 | 1004 8 16 11 8 19 17 126 6 | 50 50 52 49 44 61 66 50
XR04 | 1268 26 21 19 --- 13 21 --- 10 | 56 52 39 --- 49 39 --- 45
R05 | 623 15 25 15 18 18 19 48 8 | 33 49 32 42 30 37 60 32
R07 | 1977 11 10 7 12 13 20 223 6 | 53 58 60 65 54 71 175 60
R08 | 1039 11 10 13 16 15 13 --- 6 | 51 54 59 57 62 60 --- 56
R09E | 5288 20 28 17 32 36 28 --- 12 | 82 70 90 97 88 91 --- 84
XR11E | 3997 16 16 15 16 --- 22 --- 9 | 23 28 30 33 --- 31 --- 26
R12E | 1172 17 27 14 24 13 16 --- 8 | 33 30 38 53 49 37 --- 37
R13E | 2361 30 30 29 56 23 22 --- 14 | 39 34 46 61 45 42 --- 37
R14E | 900 15 26 15 9 13 14 --- 7 | 35 31 32 31 37 35 --- 31
R15E | 764 18 23 29 27 20 19 87 10 | 83 80 84 84 90 86 93 82
R16E | 1367 29 27 23 46 24 28 --- 13 | 54 45 50 69 48 60 --- 49
R17 | 567 7 35 11 15 15 18 --- 8 | 53 46 47 52 47 62 --- 51
R18 | 1175 21 34 18 13 17 25 --- 9 | 38 44 54 46 51 58 --- 47
R19 | 2155 54 99 45 42 66 28 --- 25 | 75 40 53 73 57 52 --- 50
R20 | 716 30 108 108 53 69 44 --- 31 | 91 58 64 107 114 107 --- 84
R21 | 860 10 31 17 14 25 11 114 8 | 57 42 48 49 69 54 97 53
R22 | 1324 45 43 97 76 82 29 --- 28 | 38 67 66 48 51 25 --- 34
R24 | 657 19 51 25 18 16 21 --- 11 | 66 28 43 57 54 55 --- 51
------+----------------------------------------------+------------------------------------------
RMS | 1733 25 43 40 33 34 22 130 |T 53 47 51 58 56 54 95 49
WRMS | 1733 20 29 26 17 25 19 130 |NE 54 48 50 56 54 54 96 49
MEDI | 1172 18 27 17 18 18 20 113 |MD 53 46 49 52 49 54 84 49
Table 3.2160.5 GPS week: 2160 Day: 5 MJD: 59369
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 | 543 34 23 40 33 28 31 --- 14 | 58 44 43 45 35 56 --- 43
R02 | 1444 9 17 12 6 16 10 125 5 | 27 29 29 32 48 34 96 31
R03 | 807 8 10 8 13 14 14 144 5 | 32 33 28 26 38 38 70 30
XR04 | 1371 12 15 15 --- 6 23 --- 7 | 41 39 26 --- 35 32 --- 34
R05 | 550 9 20 23 9 12 25 63 7 | 29 36 35 28 32 29 35 26
R07 | 2506 10 10 11 22 14 22 192 7 | 38 38 36 51 35 46 113 39
R08 | 683 13 10 24 16 14 20 --- 7 | 35 34 35 29 33 49 --- 33
R09E | 4160 23 28 20 27 32 37 --- 12 | 96 106 93 97 103 111 --- 97
XR11E | 4239 16 24 18 21 --- 25 --- 10 | 31 35 42 46 --- 42 --- 35
R12E | 673 9 28 18 12 22 16 --- 7 | 39 31 41 39 41 44 --- 38
R13E | 1554 28 44 26 78 29 41 --- 19 | 39 36 45 93 45 59 --- 45
R14E | 834 9 21 18 13 14 19 --- 7 | 54 53 56 53 59 56 --- 54
R15E | 1359 12 25 18 13 10 14 89 6 | 57 65 68 64 66 63 73 62
R16E | 1188 27 31 25 42 26 17 --- 12 | 42 40 49 64 63 55 --- 49
R17 | 574 6 30 14 22 12 13 --- 7 | 35 26 31 45 40 30 --- 34
R18 | 1762 8 20 16 15 16 20 --- 7 | 30 29 33 25 34 37 --- 29
R19 | 2336 39 115 47 25 39 45 --- 23 | 70 38 36 42 52 72 --- 48
R20 | 883 34 128 117 47 67 45 --- 32 | 88 87 69 91 93 75 --- 76
R21 | 723 13 34 23 11 11 18 103 8 | 44 30 44 38 47 52 51 42
R22 | 967 40 60 94 72 71 18 --- 27 | 47 42 51 44 46 37 --- 36
R24 | 545 12 60 27 15 14 37 --- 12 | 55 32 37 47 52 70 --- 49
------+----------------------------------------------+------------------------------------------
RMS | 1550 21 49 41 32 30 27 126 |T 47 43 44 49 49 51 73 44
WRMS | 1550 14 32 24 18 21 22 126 |NE 44 38 38 41 44 46 73 39
MEDI | 967 12 25 20 16 14 20 103 |MD 41 36 41 45 45 49 70 39
Table 3.2160.6 GPS week: 2160 Day: 6 MJD: 59370
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 | 582 27 16 39 38 50 30 --- 15 | 87 67 54 73 52 80 --- 70
R02 | 1545 9 10 16 10 29 26 184 8 | 51 53 50 54 54 63 138 52
R03 | 1155 9 12 12 12 18 11 149 5 | 54 56 55 57 56 57 56 54
XR04 | 1146 17 24 11 --- 16 29 --- 10 | 58 62 44 --- 45 39 --- 47
R05 | 578 13 19 12 15 23 18 85 7 | 40 48 41 42 52 40 43 39
R07 | 1457 12 16 10 36 15 13 176 8 | 63 61 72 90 66 76 108 70
R08 | 751 10 16 15 17 11 19 --- 6 | 58 54 64 64 62 65 --- 61
R09E | 3727 25 22 23 23 29 33 --- 11 | 89 85 76 87 82 85 --- 81
XR11E | 3175 14 16 17 19 --- 22 --- 9 | 31 35 35 42 --- 39 --- 34
R12E | 680 9 28 29 17 14 23 --- 9 | 44 32 48 52 51 47 --- 45
R13E | 1383 31 48 32 59 24 41 --- 18 | 42 35 46 73 48 51 --- 41
R14E | 981 9 22 19 19 31 14 --- 8 | 56 54 62 68 64 61 --- 60
R15E | 1042 7 24 17 18 9 18 89 7 | 92 89 95 96 94 87 107 91
R16E | 2190 36 24 26 35 37 21 --- 14 | 41 35 51 52 62 54 --- 44
R17 | 1440 8 37 17 9 13 33 --- 9 | 65 40 56 60 63 80 --- 61
R18 | 1276 18 23 17 22 13 16 --- 8 | 48 39 63 54 51 61 --- 52
R19 | 2274 30 135 60 32 77 45 --- 28 | 106 48 56 108 121 106 --- 90
R20 | 947 23 106 101 61 50 33 --- 28 | 127 66 72 158 151 139 --- 117
R21 | 1138 9 35 17 17 23 20 101 8 | 75 46 62 71 87 77 51 71
R22 | 943 39 74 110 69 84 40 --- 30 | 42 58 104 47 51 29 --- 37
R24 | 744 11 54 17 15 18 18 --- 10 | 83 44 62 78 82 86 --- 74
------+----------------------------------------------+------------------------------------------
RMS | 1499 20 50 42 33 36 27 137 |T 64 52 60 71 69 67 83 61
WRMS | 1499 15 33 23 17 28 22 137 |NE 68 53 61 73 70 71 79 63
MEDI | 1146 13 24 17 19 23 22 101 |MD 58 53 56 64 62 63 56 60
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