[IGSREPORT-26563] Wk 2050 IGLOS Final Orbits
acc
acc at igs.org
Sun May 12 17:15:23 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2050 (Apr 21, 2019 - Apr 27, 2019)
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 2.2050.
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:
igl2050[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2050 in the SP3 format.
igl20507.sum Combination Report for GPS Week 2050.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://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 | -0.2 ns
1 | -1.2 ns
2 | -0.6 ns
3 | -0.1 ns
4 | -1.3 ns
5 | -0.6 ns
6 | 1.1 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 1.2050, 1a.2050).
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 2.2050.0-6)
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 3.2050.0-6).
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 2050 summary. (Apr 21, 2019 - Apr 27, 2019)
Table 1.2050.a GPS week : 2050 MJD: 58594.0-58600.0
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 6 33 15 -4 .09 28 21 | 10796 175 3060 9249
| 1 1 1 18 18 27 .04 | 850 1427
cof n/a| 0 0 7 27 20 0 .12 29 24 | 10787 185 3059 9249
| 1 0 1 21 19 18 .07 | 853 1420
emx n/a| 0 0 -1 -12 -43 76 .07 25 25 | -6042 475 3048 9267
| 1 0 2 28 34 44 .05 | 11400 962
esx n/a| 0 0 -6 23 2 -31 .13 21 18 | 806 803 3053 11666
| 0 1 2 18 14 26 .04 | 6186 1421
gfz n/a| 0 0 3 -8 19 -23 .06 26 19 | 0 -176 3064 9111
| 1 1 2 20 19 22 .06 | 0 1643
grg n/a| 1 0 3 -57 6 -68 -.37 27 23 | -356 -35 3063 8564
| 1 0 3 17 15 62 .07 | 441 1613
iac n/a| 1 0 -3 16 8 44 -.07 30 30 | 799 -267 3053 9102
| 1 1 4 36 33 39 .03 | 739 838
mcc n/a| -5 -2 -3 81 -42 110 -.23 152 152 | --- --- --- ---
| 14 11 5 121 103 210 .16 | --- ---
Table 1.2050.b GPS week : 2050 MJD: 58594.0-58600.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 21 21 20 20 18 21 24 |
R02 | 9 8 7 6 8 8 8 |
R03 | 9 12 10 9 12 10 10 |
R04 | 11 9 8 7 7 9 7 |
R05 | 12 10 11 10 11 11 9 |
R07 | 12 10 9 9 8 10 8 |
R08 | 8 8 9 6 6 8 8 |
R09 | 9 6 7 6 8 7 8 |
R10 | 7 12 10 8 8 11 8 |
R11 | 7 7 8 6 5 7 6 |
R13 | 13 9 9 9 12 10 12 |
R14 | 9 9 9 10 9 8 8 |
R15 | 8 9 13 10 8 8 9 |
R16 | 17 15 16 18 18 20 17 |
R17 | 10 11 10 44 7 8 7 |
R18 | 8 10 9 12 8 8 7 |
R19 | 19 21 20 20 21 18 17 |
R20 | 14 17 15 18 15 15 16 |
R21 | 10 9 11 11 10 9 10 |
R22 | 9 9 11 14 10 9 10 |
R23 | 10 9 10 11 10 10 10 |
R24 | 13 13 16 19 14 13 11 |
R26 | 19 18 43 44 17 18 23 |
Table 1.2050.c GPS week : 2050 MJD: 58594.0-58600.0
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 2050 0 | -23 -48 190 -565 303 1876 82.0 1143 1143 | -231 0
brd 2050 1 | 20 29 186 -151 112 992 81.4 1155 1155 | -1218 0
brd 2050 2 | 78 -7 200 -1844 508 1536 81.3 1202 1202 | -573 0
brd 2050 3 | -25 6 200 217 -721 473 83.7 1086 1086 | -74 0
brd 2050 4 | -20 68 171 -768 1076 2476 83.4 1261 1261 | -1332 0
brd 2050 5 | -56 84 185 543 -633 5469 84.7 1456 1456 | -559 0
brd 2050 6 | -47 51 160 80 -482 4773 84.3 1491 1491 | 1073 0
-------------+------------------------------------------------------------+----------------
brd 2050 mean| -10 26 185 -355 23 2513 83.0 1256 1256 | -416 0
brd 2050 sdev| 46 46 14 795 667 1900 1.4 158 158 | 805 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 2.2050.0 GPS week: 2050 Day: 0 MJD: 58594
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 9 43 -17 32 .15 25 21 | 10008 1763 2842 9165
cof n/a| -1 0 9 47 12 33 .15 26 22 | 9998 1767 2841 9169
emx n/a| 0 0 -4 -36 -49 41 .07 22 22 | -4945 1666 2820 9093
esx n/a| 0 -1 -4 52 15 21 .11 23 20 | -2785 1918 2851 11877
gfz n/a| 0 0 3 14 53 -27 -.05 27 21 | 0 1214 2859 8922
grg n/a| 0 1 2 -90 5 -142 -.36 26 25 | -1069 1751 2833 8641
iac n/a| 2 -1 -8 57 -3 13 -.08 32 32 | 257 1115 2843 8933
mcc n/a| -10 8 -10 291 -43 -130 -.00 179 179 | --- --- --- ---
Table 2.2050.1 GPS week: 2050 Day: 1 MJD: 58595
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 6 66 23 32 .08 29 24 | 10546 -752 2929 9323
cof n/a| 0 0 8 35 18 0 .10 31 27 | 10528 -722 2930 9320
emx n/a| 0 0 -2 -48 -65 78 .05 23 23 | -7220 -627 2920 9325
esx n/a| 0 -1 -5 31 22 -24 .19 21 18 | 13210 171 2915 11846
gfz n/a| 0 0 2 -26 37 -19 .04 25 17 | 0 -1145 2929 9094
grg n/a| 2 0 5 -48 -9 -133 -.39 29 28 | -447 -1300 2945 8488
iac n/a| 0 0 -7 0 -23 21 -.07 30 31 | 114 -157 2918 9119
mcc n/a| -27 -14 -5 -20 -85 65 -.02 206 206 | --- --- --- ---
Table 2.2050.2 GPS week: 2050 Day: 2 MJD: 58596
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 35 40 -36 .06 30 22 | 10026 -673 3328 9924
cof n/a| 0 0 8 44 61 -13 .07 32 25 | 10022 -676 3316 9925
emx n/a| 2 0 -4 -24 -27 99 .07 22 22 | -16751 424 3320 10045
esx n/a| 0 0 -7 33 -15 -44 .18 23 20 | -3496 229 3315 12441
gfz n/a| 1 0 8 22 20 1 .07 26 19 | 0 -1251 3309 9833
grg n/a| 0 1 8 -54 -3 -98 -.46 28 24 | -27 -928 3315 9201
iac n/a| 0 0 -9 -41 -16 20 -.02 30 30 | 484 -825 3319 9817
mcc n/a| -18 0 -6 -40 -166 409 -.33 161 161 | --- --- --- ---
Table 2.2050.3 GPS week: 2050 Day: 3 MJD: 58597
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 8 34 16 -8 .09 28 19 | 10929 808 3190 8925
cof n/a| 0 -1 9 36 4 -15 .21 30 22 | 10913 838 3197 8923
emx n/a| 0 0 1 -6 -30 83 .01 25 25 | 7845 1419 3151 8928
esx n/a| -1 -2 -10 14 4 -32 .14 23 19 | -1449 1133 3150 11187
gfz n/a| 0 2 0 -24 0 -17 .12 29 21 | 0 296 3203 8796
grg n/a| 0 0 4 -35 13 -64 -.44 28 24 | -375 623 3206 8259
iac n/a| -1 3 1 29 37 39 -.10 33 32 | 1480 -955 3177 8796
mcc n/a| -4 -17 3 149 159 48 -.35 122 122 | --- --- --- ---
Table 2.2050.4 GPS week: 2050 Day: 4 MJD: 58598
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 6 29 26 -13 .14 29 22 | 11532 -960 3072 9048
cof n/a| -1 0 5 24 27 -15 .20 29 21 | 11526 -944 3070 9045
emx n/a| 0 1 -1 31 -106 156 .16 29 28 | 10555 -132 3067 9078
esx n/a| -2 -1 -5 6 -16 -39 .09 20 20 | -2639 -350 3088 11633
gfz n/a| -1 1 1 -29 9 -11 .04 23 14 | 0 -1801 3086 9008
grg n/a| 3 0 3 -55 11 -36 -.30 23 19 | -731 -1266 3079 8630
iac n/a| 2 0 0 54 70 23 -.08 31 30 | 424 90 3060 8980
mcc n/a| 9 -11 -5 60 0 37 -.24 114 114 | --- --- --- ---
Table 2.2050.5 GPS week: 2050 Day: 5 MJD: 58599
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 7 9 10 -8 .07 30 25 | 10254 -1241 3095 9081
cof n/a| 1 0 8 -14 11 13 .03 31 29 | 10245 -1230 3095 9082
emx n/a| -1 0 1 14 -10 22 .07 26 26 | -16284 -605 3095 9091
esx n/a| -1 1 -5 -1 8 -34 .09 18 14 | 5059 -774 3088 11074
gfz n/a| -1 0 6 0 14 -69 .07 26 21 | 0 -1235 3090 8988
grg n/a| 1 1 1 -53 -3 37 -.28 28 22 | 200 -1517 3103 8379
iac n/a| 1 -1 0 -12 4 67 -.07 29 29 | 696 -1347 3090 9024
mcc n/a| 8 14 -4 -13 -110 394 -.24 117 117 | --- --- --- ---
Table 2.2050.6 GPS week: 2050 Day: 6 MJD: 58600
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 6 -30 .02 25 18 | 12282 2280 2968 9278
cof n/a| 0 0 5 16 4 -1 .05 27 21 | 12283 2267 2967 9280
emx n/a| 0 -1 -2 -17 -12 49 .07 26 26 | -15496 1181 2967 9309
esx n/a| -1 1 -3 28 0 -63 .11 20 16 | -2252 3297 2968 11609
gfz n/a| 2 1 5 -13 1 -21 .12 25 19 | 0 2685 2972 9141
grg n/a| 0 0 -2 -66 36 -44 -.34 25 21 | -48 2392 2964 8356
iac n/a| 2 -1 -1 27 -11 123 -.09 29 27 | 2143 205 2968 9045
mcc n/a| 4 0 6 147 -49 -52 -.40 163 163 | --- --- --- ---
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 3.2050.0 GPS week: 2050 Day: 0 MJD: 58594
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 680 51 55 28 51 34 44 69 --- 20 | 92 101 72 69 95 70 26 --- 63
R02 | 800 12 19 20 17 20 21 24 154 8 | 55 59 56 59 68 54 37 99 54
R03 | 743 19 20 15 21 12 21 30 113 9 | 77 79 60 49 75 76 40 36 62
R04 | 1506 22 22 17 29 12 31 23 --- 10 | 73 73 53 59 65 79 54 --- 61
R05 | 480 17 25 15 34 15 30 34 --- 11 | 59 67 55 62 61 70 49 --- 55
R07 | 825 17 20 21 20 38 18 40 189 11 | 77 78 60 59 89 72 38 46 64
R08 | 527 18 20 18 10 16 14 29 --- 8 | 69 70 56 56 61 63 37 --- 56
R09 | 2602 12 13 16 10 33 18 23 --- 8 | 35 33 30 33 48 28 34 --- 32
R10 | 1384 13 10 17 15 15 13 11 --- 6 | 47 45 43 50 58 46 36 --- 45
R11 | 1401 8 11 14 12 16 18 22 273 6 | 52 54 54 57 59 48 41 120 51
R13 | 1812 15 13 24 24 22 52 18 --- 13 | 58 63 52 65 81 102 57 --- 67
R14 | 711 21 26 9 15 23 10 36 --- 8 | 61 66 50 51 72 60 37 --- 54
R15 | 529 12 12 14 8 15 8 42 --- 8 | 85 83 83 78 89 86 63 --- 80
R16 | 1004 31 31 49 29 41 42 32 --- 17 | 78 80 61 68 86 82 66 --- 70
R17 | 983 16 13 21 19 37 16 24 --- 10 | 141 139 128 129 146 147 143 --- 141
R18 | 635 12 13 18 17 15 21 15 --- 7 | 106 112 108 118 120 123 114 --- 114
R19 | 736 65 51 30 28 36 36 46 --- 18 | 69 76 50 47 51 41 46 --- 41
R20 | 1498 27 26 35 22 44 20 34 --- 13 | 91 90 65 76 105 84 68 --- 79
R21 | 753 10 18 22 18 39 12 24 116 10 | 99 101 93 93 104 97 94 136 94
R22 | 1312 28 38 22 16 16 13 22 --- 9 | 80 85 75 72 76 78 67 --- 74
R23 | 912 28 26 14 30 19 16 22 --- 10 | 199 197 196 204 203 200 203 --- 199
R24 | 794 25 32 21 16 35 39 36 --- 13 | 51 56 48 58 69 74 52 --- 54
XR26 | ---- 14 19 --- --- --- --- 25 --- 19 | 61 64 --- --- --- --- 67 --- 63
------+---------------------------------------------------+-----------------------------------------------
RMS | 1143 25 26 22 23 27 26 32 179 |T 78 81 70 73 85 80 63 87 72
WRMS | 1143 21 22 22 20 21 25 32 179 |NE 78 81 70 73 85 80 63 87 72
MEDI | 800 17 20 18 18 20 18 25 154 |MD 73 76 56 59 75 74 52 99 63
Table 3.2050.1 GPS week: 2050 Day: 1 MJD: 58595
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 846 57 62 41 57 23 44 42 --- 20 | 64 76 53 52 57 51 25 --- 42
R02 | 874 11 15 12 19 11 20 31 202 8 | 41 40 43 50 42 35 22 156 39
R03 | 540 19 23 15 24 25 37 43 109 12 | 56 63 40 37 62 72 25 30 46
R04 | 1384 20 20 15 12 21 12 37 --- 8 | 52 54 40 47 58 52 44 --- 46
R05 | 493 20 16 16 20 12 21 37 --- 9 | 53 51 52 50 51 56 39 --- 48
R07 | 935 24 22 13 16 15 12 42 251 9 | 52 51 43 35 45 43 23 77 38
R08 | 612 21 26 13 15 24 12 20 --- 8 | 44 47 36 42 30 35 26 --- 33
R09 | 2319 13 15 12 11 18 11 15 --- 6 | 27 26 27 29 35 26 30 --- 27
R10 | 817 17 13 25 18 38 20 28 --- 11 | 28 33 26 47 67 41 26 --- 38
R11 | 1502 12 16 10 13 12 14 30 261 6 | 36 39 41 45 30 37 26 101 35
R13 | 2818 16 19 15 15 21 27 17 --- 8 | 42 45 47 47 50 55 35 --- 44
R14 | 569 18 13 12 18 9 23 35 --- 8 | 41 39 40 37 39 49 23 --- 37
R15 | 516 21 25 20 21 9 21 25 --- 9 | 63 66 61 53 55 70 57 --- 57
R16 | 1239 38 49 30 14 32 56 28 --- 15 | 63 66 63 60 66 49 53 --- 57
R17 | 682 18 22 21 20 27 30 21 --- 10 | 125 130 116 116 128 134 124 --- 125
R18 | 887 18 19 24 16 15 37 22 --- 10 | 82 82 77 83 91 109 82 --- 85
R19 | 721 75 73 41 23 30 58 40 --- 20 | 51 53 40 39 44 58 40 --- 33
R20 | 782 20 26 33 29 56 31 38 --- 16 | 62 64 49 57 90 56 52 --- 58
R21 | 616 22 15 20 12 18 20 22 171 8 | 85 84 78 74 81 80 75 182 78
R22 | 1080 34 36 17 12 15 17 20 --- 8 | 51 51 43 42 40 37 38 --- 39
R23 | 813 24 30 16 23 19 20 20 --- 9 | 181 181 177 187 185 185 186 --- 183
R24 | 1099 26 37 35 15 34 29 20 --- 12 | 35 43 38 41 49 60 37 --- 39
XR26 | ---- 15 43 --- --- --- --- 19 --- 17 | 40 56 --- --- --- --- 41 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1155 29 31 23 21 25 29 30 206 |T 59 62 55 57 63 63 49 109 55
WRMS | 1155 24 27 23 18 17 28 31 206 |NE 59 62 55 57 63 63 49 109 55
MEDI | 817 20 22 16 16 19 21 28 202 |MD 52 53 43 47 51 52 38 101 42
Table 3.2050.2 GPS week: 2050 Day: 2 MJD: 58596
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1071 66 71 29 60 18 30 54 --- 20 | 75 80 37 34 47 46 29 --- 32
R02 | 631 11 13 15 18 11 16 20 195 7 | 45 48 42 51 49 45 37 191 43
R03 | 746 27 23 16 18 18 15 38 105 10 | 68 64 57 50 65 49 36 35 53
R04 | 775 22 23 8 15 6 18 32 --- 7 | 56 56 45 45 45 50 30 --- 44
R05 | 560 20 22 22 29 19 16 29 --- 10 | 51 53 44 36 40 41 47 --- 39
R07 | 1142 16 22 11 18 20 23 30 181 8 | 62 63 53 43 66 58 33 71 51
R08 | 660 17 19 14 22 22 20 24 --- 9 | 55 59 38 35 53 43 25 --- 39
R09 | 2189 14 16 10 7 16 23 15 --- 6 | 26 28 29 25 32 25 30 --- 24
R10 | 1711 14 17 20 13 31 24 21 --- 9 | 34 37 31 45 62 41 32 --- 38
R11 | 1409 10 16 8 15 16 17 32 101 7 | 40 44 38 48 38 38 31 137 37
R13 | 2957 8 7 14 13 27 29 23 --- 9 | 49 51 43 43 48 54 37 --- 43
R14 | 709 15 19 14 21 23 18 28 --- 9 | 48 52 47 39 54 38 32 --- 42
R15 | 720 14 20 17 32 34 28 36 --- 12 | 67 69 63 52 75 80 47 --- 62
R16 | 953 38 56 27 16 46 50 31 --- 16 | 62 74 65 56 72 47 48 --- 54
R17 | 961 32 17 23 16 15 29 21 --- 10 | 202 201 157 163 200 214 202 --- 203
R18 | 1277 35 15 18 15 14 21 16 --- 9 | 130 158 152 161 160 158 147 --- 152
R19 | 645 74 77 37 37 32 30 47 --- 19 | 75 83 47 45 54 35 34 --- 41
R20 | 617 23 26 29 24 51 28 29 --- 14 | 73 78 48 56 90 63 56 --- 60
R21 | 730 26 36 25 17 27 23 32 192 11 | 111 114 108 110 118 112 91 135 108
R22 | 646 36 26 21 14 24 26 27 --- 11 | 102 101 96 95 104 111 88 --- 97
R23 | 909 24 19 25 24 18 21 17 --- 10 | 216 212 222 219 215 212 217 --- 216
R24 | 1228 24 22 38 14 32 63 24 --- 16 | 58 68 50 61 77 99 53 --- 62
XR26 | ---- 38 29 --- --- --- --- 46 --- 42 | 71 76 --- --- --- --- 94 --- 80
------+---------------------------------------------------+-----------------------------------------------
RMS | 1202 30 32 22 23 26 28 30 160 |T 77 81 68 68 80 75 64 113 70
WRMS | 1202 22 25 22 20 19 24 30 160 |NE 77 81 68 68 80 75 64 113 70
MEDI | 775 23 22 18 17 20 23 29 181 |MD 62 68 47 48 62 49 37 135 51
Table 3.2050.3 GPS week: 2050 Day: 3 MJD: 58597
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 762 67 67 20 52 20 28 51 --- 19 | 83 85 40 29 47 53 18 --- 36
R02 | 729 14 25 14 14 13 16 11 155 6 | 45 59 43 30 30 43 36 119 36
R03 | 791 12 16 16 20 25 12 33 102 9 | 66 67 57 44 76 66 40 24 57
R04 | 989 15 18 11 14 9 19 29 --- 7 | 56 60 41 43 46 57 32 --- 45
R05 | 659 16 23 21 22 26 20 31 --- 10 | 45 58 39 36 56 42 25 --- 38
R07 | 1264 15 10 14 19 18 22 31 163 8 | 71 67 56 44 71 77 39 41 59
R08 | 606 13 17 9 9 14 11 21 --- 5 | 57 62 53 46 57 51 36 --- 50
R09 | 1971 13 21 14 8 15 13 8 --- 5 | 16 25 17 20 26 21 18 --- 16
R10 | 1854 13 11 17 18 16 15 26 --- 8 | 39 38 35 54 51 48 30 --- 42
R11 | 948 6 11 10 11 10 16 27 94 6 | 40 38 38 45 46 48 26 80 40
R13 | 2174 15 18 21 9 15 27 35 --- 9 | 44 45 44 50 51 63 31 --- 46
R14 | 617 18 17 14 20 33 18 27 --- 10 | 50 47 40 39 64 44 28 --- 42
R15 | 923 21 23 23 24 24 17 29 --- 10 | 58 57 53 39 60 50 34 --- 47
R16 | 542 38 24 34 40 47 46 30 --- 18 | 65 67 37 36 77 60 36 --- 46
XR17 | 5034 36 134 --- --- 97 61 101 --- 44 | 192 238 --- --- 227 172 158 --- 180
R18 | 906 29 24 35 16 18 26 31 --- 11 | 117 130 130 131 131 132 117 --- 125
R19 | 755 57 69 38 41 45 32 57 --- 20 | 81 98 68 55 91 79 53 --- 65
R20 | 664 21 31 41 29 49 55 32 --- 17 | 95 99 77 85 108 113 83 --- 89
R21 | 999 27 25 21 12 20 22 39 73 10 | 85 82 86 82 91 79 94 82 84
R22 | 653 46 36 30 12 25 28 46 --- 14 | 130 129 134 129 135 137 95 --- 126
R23 | 1102 15 24 29 21 18 24 35 --- 10 | 204 200 200 201 203 192 195 --- 199
R24 | 830 25 27 43 13 65 58 29 --- 19 | 57 64 59 54 106 79 62 --- 62
XR26 | ---- 34 75 --- --- --- --- 55 --- 43 | 45 97 --- --- --- --- 110 --- 66
------+---------------------------------------------------+-----------------------------------------------
RMS | 1086 28 30 25 23 29 28 33 122 |T 75 83 64 61 84 77 60 69 69
WRMS | 1086 19 22 25 19 21 24 32 122 |NE 75 83 64 61 84 77 60 69 69
MEDI | 830 18 24 21 18 20 22 31 102 |MD 58 67 53 45 64 60 36 80 50
Table 3.2050.4 GPS week: 2050 Day: 4 MJD: 58598
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 612 69 66 32 39 12 15 49 --- 17 | 82 79 53 30 45 43 28 --- 39
R02 | 1679 17 13 19 12 15 14 26 118 7 | 51 46 50 40 44 57 32 55 43
R03 | 467 24 22 22 25 11 30 38 88 11 | 62 58 58 38 40 65 31 26 46
R04 | 649 10 11 14 11 13 15 30 --- 7 | 56 50 48 48 57 53 39 --- 49
R05 | 794 23 11 22 28 21 21 29 --- 10 | 45 39 44 44 50 42 37 --- 39
R07 | 1017 22 24 10 17 15 13 31 136 8 | 60 62 52 42 56 47 31 37 47
R08 | 767 18 17 16 7 9 12 20 --- 6 | 55 51 51 43 45 51 39 --- 46
R09 | 2352 11 12 28 22 15 14 8 --- 8 | 23 23 29 22 35 33 29 --- 24
R10 | 2240 15 16 16 16 15 19 27 --- 8 | 39 41 32 41 38 40 25 --- 33
R11 | 866 5 8 15 6 12 16 15 117 5 | 39 39 39 40 36 47 38 74 38
R13 | 932 21 25 30 9 22 35 46 --- 12 | 43 46 47 56 77 75 30 --- 55
R14 | 543 20 17 18 16 11 23 36 --- 9 | 51 52 40 43 47 60 25 --- 43
R15 | 1070 25 22 17 13 16 14 28 --- 8 | 64 61 56 49 54 49 40 --- 50
R16 | 677 43 53 51 29 44 42 32 --- 18 | 66 86 69 58 85 66 44 --- 62
R17 | 1894 15 16 19 12 18 8 20 --- 7 | 143 155 168 174 154 144 138 --- 144
R18 | 739 19 13 34 9 14 16 12 --- 8 | 103 95 101 96 101 101 101 --- 99
R19 | 686 59 71 45 33 45 46 54 --- 20 | 72 83 76 85 85 73 76 --- 70
R20 | 858 32 35 38 22 40 31 33 --- 14 | 105 126 90 105 125 112 115 --- 106
R21 | 1475 18 17 29 17 31 13 21 106 10 | 83 81 88 84 88 83 86 60 83
R22 | 880 34 23 28 13 21 12 22 --- 9 | 74 80 79 70 77 79 78 --- 74
R23 | 1967 18 17 36 20 17 11 23 --- 9 | 252 253 264 251 252 254 258 --- 254
R24 | 1626 25 24 45 18 40 26 28 --- 13 | 59 63 66 61 72 58 58 --- 58
XR26 | ---- 15 47 --- --- --- --- 18 --- 17 | 69 75 --- --- --- --- 72 --- 69
------+---------------------------------------------------+-----------------------------------------------
RMS | 1260 29 29 29 20 23 23 31 114 |T 73 75 72 69 75 74 63 50 68
WRMS | 1260 22 21 28 20 14 19 30 114 |NE 73 75 72 69 75 74 63 50 68
MEDI | 866 20 17 22 16 15 15 28 117 |MD 62 62 53 48 56 58 39 55 50
Table 3.2050.5 GPS week: 2050 Day: 5 MJD: 58599
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 738 70 71 39 44 42 18 54 --- 20 | 79 83 44 35 73 35 18 --- 38
R02 | 2656 13 13 16 14 15 15 27 97 7 | 42 41 38 37 46 51 28 58 38
R03 | 598 22 26 13 19 18 18 37 103 9 | 54 59 43 40 55 51 28 30 43
R04 | 955 17 21 13 14 24 15 37 --- 9 | 50 57 47 44 54 51 42 --- 45
R05 | 692 18 23 22 24 27 19 36 --- 11 | 47 50 44 47 56 58 45 --- 46
R07 | 839 16 18 21 18 21 21 34 140 9 | 53 55 46 51 62 54 35 56 48
R08 | 819 16 19 10 11 16 19 29 --- 7 | 52 54 46 50 53 40 35 --- 45
R09 | 2066 13 12 15 8 27 10 11 --- 6 | 30 32 28 37 40 25 33 --- 31
R10 | 2497 13 20 19 15 19 44 29 --- 11 | 31 37 21 26 31 54 14 --- 24
R11 | 993 14 20 12 10 15 21 22 120 7 | 36 40 32 32 36 34 25 95 31
R13 | 1015 19 21 26 7 23 36 23 --- 10 | 31 33 39 41 40 52 32 --- 37
R14 | 1110 24 27 18 11 15 14 29 --- 8 | 44 45 41 41 44 44 29 --- 39
R15 | 848 25 33 18 11 11 11 30 --- 8 | 59 64 56 46 50 51 41 --- 49
R16 | 1143 54 65 55 22 53 55 29 --- 20 | 56 60 51 54 61 51 47 --- 49
R17 | 2383 15 18 20 10 21 14 19 --- 7 | 118 126 125 126 125 119 117 --- 120
R18 | 833 16 16 25 10 10 24 10 --- 7 | 71 74 70 72 77 76 73 --- 72
R19 | 817 66 49 44 18 43 39 31 --- 18 | 80 88 64 61 74 96 66 --- 67
R20 | 737 31 24 30 22 40 44 28 --- 14 | 113 109 98 97 110 110 101 --- 101
R21 | 1956 27 25 24 16 19 19 18 119 9 | 64 63 61 62 70 62 63 107 62
R22 | 545 26 23 22 13 24 17 18 --- 9 | 52 50 39 41 50 41 44 --- 42
R23 | 2678 18 15 34 14 20 24 15 --- 9 | 158 158 166 162 166 157 167 --- 162
R24 | 1114 22 27 33 20 20 45 35 --- 13 | 45 56 51 58 61 55 46 --- 49
XR26 | ---- 16 68 --- --- --- --- 20 --- 18 | 48 68 --- --- --- --- 54 --- 50
------+---------------------------------------------------+-----------------------------------------------
RMS | 1456 30 31 26 18 26 28 29 117 |T 61 65 56 57 65 62 51 69 56
WRMS | 1456 25 29 26 14 21 22 29 117 |NE 61 65 56 57 65 62 51 69 56
MEDI | 955 18 23 21 14 20 19 29 119 |MD 52 57 46 46 55 51 42 58 46
Table 3.2050.6 GPS week: 2050 Day: 6 MJD: 58600
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 761 72 76 51 62 35 33 44 --- 23 | 103 114 76 56 90 48 30 --- 58
R02 | 1798 12 13 16 10 17 11 34 89 7 | 60 62 58 51 65 60 39 96 55
R03 | 726 11 15 15 16 23 19 42 105 9 | 79 82 65 61 85 81 44 68 68
R04 | 1565 16 15 12 11 12 8 30 --- 7 | 71 68 58 64 68 67 50 --- 62
R05 | 601 14 24 24 14 12 13 35 --- 8 | 62 71 65 52 65 63 50 --- 57
R07 | 750 16 14 10 17 16 24 21 94 8 | 71 69 58 55 63 76 51 69 60
R08 | 834 19 19 13 15 14 21 22 --- 8 | 66 69 62 50 57 71 44 --- 58
R09 | 2767 10 14 16 7 21 30 12 --- 7 | 33 31 32 30 41 33 33 --- 30
R10 | 3075 11 14 15 8 29 10 26 --- 7 | 46 49 34 47 61 46 29 --- 43
R11 | 1080 13 15 15 11 11 14 21 322 6 | 51 51 42 49 49 52 38 148 46
R13 | 936 14 15 29 16 26 42 22 --- 11 | 60 65 56 63 76 87 48 --- 64
R14 | 733 17 20 18 13 19 8 24 --- 7 | 68 71 56 50 69 62 40 --- 57
R15 | 637 19 23 13 23 17 20 29 --- 9 | 87 89 77 66 84 91 61 --- 76
R16 | 1233 27 41 49 18 27 59 35 --- 16 | 85 98 69 76 90 98 62 --- 77
R17 | 1838 18 18 18 11 15 15 13 --- 7 | 130 132 130 129 132 130 127 --- 128
R18 | 1117 9 12 24 11 16 14 13 --- 6 | 77 76 72 78 72 80 76 --- 75
R19 | 879 48 43 41 27 28 29 47 --- 16 | 76 81 82 85 83 86 75 --- 77
R20 | 986 15 17 40 17 60 36 34 --- 16 | 86 88 78 84 114 81 79 --- 84
R21 | 1487 18 18 28 16 25 14 25 48 9 | 75 72 72 72 78 69 75 79 72
R22 | 556 29 33 27 16 25 17 18 --- 10 | 49 53 51 51 52 51 48 --- 48
R23 | 2560 21 22 23 22 21 18 19 --- 9 | 184 182 183 183 191 184 180 --- 183
R24 | 1840 22 19 19 21 26 26 27 --- 10 | 30 37 40 48 54 56 46 --- 40
XR26 | ---- 17 39 --- --- --- --- 29 --- 23 | 51 63 --- --- --- --- 64 --- 55
------+---------------------------------------------------+-----------------------------------------------
RMS | 1490 25 27 26 20 25 25 29 163 |T 73 77 68 68 79 76 60 92 68
WRMS | 1490 18 21 26 16 19 21 27 163 |NE 73 77 68 68 79 76 60 92 68
MEDI | 986 17 18 18 16 21 18 26 94 |MD 71 71 62 56 69 69 50 79 60
More information about the IGSREPORT
mailing list