[IGSREPORT-27680] Wk 2136 IGLOS Final Orbits
acc
acc at igs.org
Mon Jan 4 08:11:16 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2136 (Dec 13, 2020 - Dec 19, 2020)
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 2.2136.
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:
igl2136[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2136 in the SP3 format.
igl21367.sum Combination Report for GPS Week 2136.
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 | -1.3 ns
1 | 1.2 ns
2 | 0.9 ns
3 | 0.5 ns
4 | 0.4 ns
5 | 0.6 ns
6 | 0.1 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
2 | IAC | R11
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 1.2136, 1a.2136).
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 2.2136.0-6)
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 3.2136.0-6).
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 2136 summary. (Dec 13, 2020 - Dec 19, 2020)
Table 1.2136.a GPS week : 2136 MJD: 59196.0-59202.0
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 -2 1 -5 14 .07 26 21 | 16270 -485 3073 7718
| 1 0 2 22 12 18 .02 | 1784 1855
emx n/a| 0 -1 0 -19 23 -51 .14 40 40 | -2930 -346 3079 8002
| 1 1 2 26 22 18 .05 | 12473 1462
esx n/a| 1 0 1 6 0 -36 .12 36 27 | 315 -540 3080 10274
| 1 0 1 18 16 33 .04 | 7135 1849
gfz n/a| 0 0 0 -16 -2 -54 .08 25 15 | 0 -24 3125 7491
| 0 1 1 14 20 31 .02 | 0 1769
grg n/a| 0 0 1 20 -2 6 -.42 30 23 | 371 -194 3086 7237
| 1 0 4 15 27 36 .07 | 353 1885
iac n/a| 0 0 1 2 0 152 .05 33 30 | 2323 -84 3079 8069
| 2 2 2 13 36 61 .02 | 1060 727
mcc n/a| 2 -2 0 77 -9 -51 -.84 146 146 | --- --- --- ---
| 7 4 8 86 143 177 .27 | --- ---
Table 1.2136.b GPS week : 2136 MJD: 59196.0-59202.0
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 | 19 17 15 15 22 18 18 |
R02 | 7 7 9 6 8 8 6 |
R03 | 7 9 7 8 6 9 7 |
R04 | 10 9 11 11 12 11 13 |
R05 | 8 9 9 13 10 9 10 |
R07 | 8 7 8 7 8 6 6 |
R08 | 7 7 7 8 7 7 10 |
R09 | 7 10 8 8 9 8 7 |
R11 | 17 19 61 0 --- --- --- |
R12 | 9 9 10 8 9 12 9 |
R13 | 18 15 13 15 18 17 18 |
R14 | 9 8 8 9 12 9 8 |
R15 | 9 9 9 9 9 10 7 |
R16 | 13 11 12 14 17 14 13 |
R17 | 8 10 11 9 8 10 10 |
R18 | 8 8 8 7 7 8 9 |
R19 | 33 30 29 30 33 29 34 |
R20 | 25 25 19 23 32 26 25 |
R21 | 9 11 11 10 10 12 13 |
R22 | 15 21 16 13 16 18 19 |
R24 | 11 11 11 11 14 11 10 |
Table 1.2136.c GPS week : 2136 MJD: 59196.0-59202.0
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 2136 0 | 75 67 116 -2203 108 -2900 79.6 1914 1914 | -1290 0
brd 2136 1 | -57 28 114 -631 216 -2302 81.1 1540 1540 | 1245 0
brd 2136 2 | 11 44 224 -1144 -15 -4238 81.9 1609 1609 | 856 0
brd 2136 3 | -92 -38 234 -70 -974 -961 82.6 1712 1712 | 474 0
brd 2136 4 | 44 18 156 -587 1440 4074 83.3 1745 1745 | 366 0
brd 2136 5 | -43 67 132 -822 224 2561 84.1 1519 1519 | 627 0
brd 2136 6 | 9 45 112 -810 1277 1490 81.3 1610 1610 | 72 0
-------------+------------------------------------------------------------+----------------
brd 2136 mean| -7 33 155 -895 325 -325 82.0 1664 1664 | 335 0
brd 2136 sdev| 59 36 52 661 818 3088 1.5 137 137 | 807 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 2.2136.0 GPS week: 2136 Day: 0 MJD: 59196
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 1 -24 -15 -1 .09 25 19 | 14140 -3625 3607 8123
emx n/a| -1 -2 2 16 21 -35 .13 46 46 | -11510 -2944 3593 8388
esx n/a| 1 0 0 32 12 -54 .13 34 27 | -3974 -3858 3612 10812
gfz n/a| 0 0 -1 -36 -3 -46 .09 26 15 | 0 -3440 3709 7797
grg n/a| 1 1 -2 15 10 23 -.42 27 23 | 455 -3515 3642 8162
iac n/a| -3 1 -2 10 27 119 .05 31 29 | 321 -480 3622 8384
mcc n/a| 8 -1 -17 -2 24 -113 -.78 194 194 | --- --- --- ---
Table 2.2136.1 GPS week: 2136 Day: 1 MJD: 59197
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -1 26 -25 27 .08 25 19 | 13711 883 3045 7909
emx n/a| 0 -2 -4 -41 17 -53 .11 42 42 | -4852 1055 3088 8236
esx n/a| 0 -1 4 -2 -10 -38 .06 34 29 | -1718 1195 3070 10602
gfz n/a| 0 2 1 -9 -4 -41 .09 24 19 | 0 2145 3087 7637
grg n/a| 2 0 -2 0 3 -35 -.47 30 22 | 263 1763 3067 7187
iac n/a| 0 1 2 -8 40 134 .06 35 32 | 2337 693 3044 8319
mcc n/a| -8 -2 4 154 66 -2 -.80 148 148 | --- --- --- ---
Table 2.2136.2 GPS week: 2136 Day: 2 MJD: 59198
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 -2 2 3 26 .06 21 18 | 15677 2120 2929 7455
emx n/a| -1 0 -2 -48 64 -27 .20 34 34 | 9610 1505 2927 7846
esx n/a| 2 0 2 -5 3 13 .11 33 29 | 13967 1371 2920 10210
gfz n/a| 0 -2 0 5 0 -30 .07 27 15 | 0 1127 2957 7225
grg n/a| -2 1 -1 26 -43 -23 -.36 23 19 | -255 1959 2926 6875
iac n/a| 0 1 5 17 -52 63 .07 34 33 | 3219 -638 2923 7896
mcc n/a| 5 0 -2 -40 -59 16 -1.34 146 146 | --- --- --- ---
Table 2.2136.3 GPS week: 2136 Day: 3 MJD: 59199
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 31 3 43 .08 22 19 | 17589 -1449 3015 7036
emx n/a| 0 0 3 -28 32 -68 .20 37 37 | 9156 -451 3052 7261
esx n/a| 0 0 1 -14 11 -1 .13 34 27 | 6239 -1921 3042 9539
gfz n/a| 0 0 -1 -20 -9 -26 .10 25 14 | 0 -465 3106 6599
grg n/a| 0 1 0 23 -29 -26 -.32 27 21 | 948 -1130 3016 6572
iac n/a| -3 4 0 6 5 121 .08 35 31 | 1547 728 3012 7423
mcc n/a| 0 -5 -1 178 -59 -298 -1.05 160 160 | --- --- --- ---
Table 2.2136.4 GPS week: 2136 Day: 4 MJD: 59200
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 -26 3 0 .08 30 24 | 18242 -1244 2971 8018
emx n/a| 0 -1 0 17 23 -78 .15 39 39 | -12998 -1015 2956 8299
esx n/a| 3 0 -1 -9 -20 -67 .12 39 24 | -5500 -793 2963 10130
gfz n/a| 0 0 2 -5 -26 -46 .08 27 17 | 0 91 3036 7870
grg n/a| 0 1 6 50 -11 39 -.42 42 25 | 421 -82 2988 7269
iac n/a| 1 0 -1 -7 37 227 .02 33 28 | 3267 -1196 2980 8373
mcc n/a| 12 -9 2 155 260 267 -.71 123 123 | --- --- --- ---
Table 2.2136.5 GPS week: 2136 Day: 5 MJD: 59201
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 -3 7 -13 12 .03 28 22 | 17116 303 3016 7599
emx n/a| 3 -3 0 -17 -9 -40 .14 41 41 | 9930 51 3007 7764
esx n/a| 3 -1 1 15 -19 -78 .19 40 27 | -3311 238 3024 10129
gfz n/a| 0 0 0 -16 40 -78 .11 21 13 | 0 819 3040 7575
grg n/a| 0 0 0 18 19 4 -.54 29 24 | 337 513 3036 7132
iac n/a| 1 -2 2 -15 -23 235 .04 32 28 | 2722 372 3028 7881
mcc n/a| -4 0 -1 28 -170 -48 -.52 123 123 | --- --- --- ---
Table 2.2136.6 GPS week: 2136 Day: 6 MJD: 59202
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 -3 3 -8 .08 28 25 | 17421 -383 2934 7891
emx n/a| 2 -2 0 -31 11 -52 .07 42 42 | -19848 -629 2932 8225
esx n/a| 0 0 3 26 18 -26 .13 40 25 | -3498 -18 2933 10496
gfz n/a| 0 0 -2 -33 -12 -115 .04 23 14 | 0 -445 2944 7738
grg n/a| 0 0 7 8 34 61 -.44 34 26 | 433 -867 2931 7467
iac n/a| 0 0 0 16 -30 165 .05 29 26 | 2853 -70 2945 8209
mcc n/a| 5 2 10 65 -125 -181 -.67 129 129 | --- --- --- ---
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 3.2136.0 GPS week: 2136 Day: 0 MJD: 59196
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 | 1338 51 34 49 30 45 19 --- 18 | 86 66 52 66 47 67 --- 57
R02 | 607 7 10 13 12 11 35 186 7 | 48 40 43 47 46 43 148 43
R03M | 867 10 12 13 9 19 25 157 6 | 65 59 65 73 74 64 47 66
XR04 | 1120 13 18 20 --- 17 29 --- 10 | 77 73 58 --- 69 84 --- 70
R05 | 743 16 15 19 21 16 23 175 8 | 67 61 72 69 58 75 61 65
R07M | 1640 17 23 14 12 18 24 229 8 | 78 77 62 72 61 69 58 69
R08 | 938 18 13 14 18 15 13 --- 7 | 62 65 65 70 70 70 --- 66
R09E | 2888 12 13 11 16 14 23 --- 6 | 28 34 31 41 25 37 --- 31
XR11E | 4696 16 --- --- 19 --- 36 --- 17 | 22 --- --- 31 --- 106 --- 102
R12E | 1050 18 28 16 15 23 26 --- 9 | 78 80 86 85 72 78 --- 78
R13E | 4422 31 49 29 57 30 35 --- 18 | 58 51 50 85 55 61 --- 54
R14E | 542 13 30 11 15 22 24 --- 8 | 135 154 147 140 142 141 --- 141
R15E | 1305 11 32 23 11 14 32 285 9 | 58 59 64 59 60 61 123 57
R16E | 1636 13 45 22 43 19 20 --- 13 | 50 38 44 81 44 49 --- 48
R17M | 2008 16 26 17 10 16 24 --- 8 | 61 39 42 59 54 58 --- 52
R18 | 1437 9 18 16 8 18 28 --- 7 | 40 39 50 48 42 47 --- 42
R19 | 4259 49 143 85 48 65 52 --- 33 | 108 39 36 112 97 117 --- 82
R20M | 1307 46 70 86 44 48 36 --- 25 | 98 38 31 89 98 96 --- 68
R21 | 798 18 31 22 11 19 25 58 9 | 61 39 40 60 61 57 52 52
R22 | 992 31 46 17 20 22 58 --- 14 | 55 49 61 66 54 89 --- 57
R24M | 1131 10 37 26 15 20 38 --- 11 | 67 37 47 61 55 72 --- 55
------+----------------------------------------------+------------------------------------------
RMS | 1913 25 46 34 26 27 31 194 |T 66 56 57 70 64 73 81 64
WRMS | 1913 19 46 27 15 23 29 194 |NE 67 52 53 67 60 72 87 59
MEDI | 1305 16 28 17 15 19 26 175 |MD 62 49 50 66 58 69 58 57
Table 3.2136.1 GPS week: 2136 Day: 1 MJD: 59197
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 | 722 53 29 49 30 31 19 --- 17 | 62 42 43 44 34 50 --- 40
R02 | 672 14 13 14 10 11 28 105 6 | 41 43 38 42 39 35 66 38
R03M | 1199 8 15 21 19 26 30 115 9 | 42 42 40 52 41 49 40 41
XR04 | 1085 14 17 26 --- 11 17 --- 8 | 63 65 53 --- 63 66 --- 60
R05 | 1506 13 10 10 17 19 39 121 8 | 49 45 53 47 42 77 42 50
R07M | 1212 12 13 12 12 21 19 249 6 | 62 57 57 66 46 54 35 56
R08 | 863 14 13 16 17 12 13 --- 6 | 47 51 58 57 45 56 --- 51
R09E | 2860 15 20 10 16 11 47 --- 9 | 52 57 55 61 52 53 --- 53
XR11E | 3793 18 --- --- 22 --- 41 --- 18 | 26 --- --- 36 --- 106 --- 101
R12E | 579 11 30 12 12 16 33 --- 8 | 74 78 77 76 79 90 --- 77
R13E | 1765 28 44 32 39 16 41 --- 15 | 51 47 54 64 55 62 --- 51
R14E | 541 11 26 14 17 18 22 --- 8 | 139 139 135 133 138 138 --- 136
R15E | 1466 11 32 22 11 21 30 147 9 | 45 49 46 49 50 52 60 45
R16E | 1841 17 40 17 25 24 26 --- 11 | 49 45 48 52 47 64 --- 47
R17M | 988 14 25 22 11 9 43 --- 9 | 40 28 35 37 30 48 --- 34
R18 | 1134 14 25 21 11 13 20 --- 7 | 28 20 36 30 25 41 --- 27
R19 | 3686 51 121 73 43 56 47 --- 29 | 60 40 27 52 34 59 --- 40
R20M | 1529 49 78 82 21 63 30 --- 25 | 59 58 43 46 61 44 --- 39
R21 | 766 24 25 32 17 17 33 88 11 | 32 25 23 31 26 39 32 24
R22 | 1177 14 33 28 52 63 68 --- 20 | 40 39 42 48 26 47 --- 28
R24M | 708 21 35 30 16 19 28 --- 11 | 38 29 30 35 35 41 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 1539 25 42 34 24 30 35 148 |T 52 49 49 52 48 60 45 50
WRMS | 1539 19 42 29 19 22 32 148 |NE 46 41 41 43 37 52 46 39
MEDI | 1177 14 25 21 17 18 30 115 |MD 49 45 43 48 42 53 40 45
Table 3.2136.2 GPS week: 2136 Day: 2 MJD: 59198
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 | 1880 35 32 46 26 28 32 --- 15 | 71 67 36 58 55 35 --- 53
R02 | 718 19 21 30 8 10 31 101 9 | 32 32 39 30 24 38 72 27
R03M | 1164 14 15 11 13 12 34 94 7 | 47 44 43 51 38 43 36 43
XR04 | 1409 12 14 27 --- 24 28 --- 10 | 59 55 47 --- 54 73 --- 54
R05 | 1461 17 13 23 19 16 32 103 9 | 57 51 47 50 42 58 61 47
R07M | 1380 10 13 14 9 15 37 278 7 | 64 54 54 56 60 77 56 58
R08 | 887 14 13 17 19 10 22 --- 7 | 53 42 53 62 47 37 --- 49
R09E | 3053 12 15 14 18 10 35 --- 7 | 47 44 39 45 40 52 --- 42
XR11E | 9695 58 --- --- 64 --- 561 --- 61 | 31 --- --- 69 --- 239 --- 292
R12E | 651 10 32 14 20 16 34 --- 9 | 65 62 59 69 56 79 --- 62
R13E | 1465 25 36 32 34 25 25 --- 13 | 49 48 50 63 58 52 --- 49
R14E | 684 14 24 22 14 15 21 --- 8 | 95 100 81 84 101 93 --- 91
R15E | 3064 14 28 12 16 13 30 80 8 | 32 26 28 38 28 44 60 29
R16E | 1597 18 27 17 21 33 40 --- 11 | 42 40 56 61 46 69 --- 47
R17M | 642 20 28 30 13 10 41 --- 10 | 140 131 134 145 146 164 --- 142
R18 | 1096 12 22 15 14 16 30 --- 8 | 32 26 35 33 33 41 --- 29
R19 | 2058 30 97 78 77 47 35 --- 28 | 74 57 67 113 68 76 --- 68
R20M | 2180 43 50 66 20 28 48 --- 19 | 68 52 36 48 57 69 --- 47
R21 | 1194 15 26 37 14 21 36 118 11 | 47 32 35 47 48 61 53 43
R22 | 1287 14 31 16 44 46 49 --- 16 | 29 33 28 50 29 66 --- 30
R24M | 960 27 33 26 13 18 26 --- 10 | 73 56 58 64 53 61 --- 59
------+----------------------------------------------+------------------------------------------
RMS | 1608 21 34 33 27 23 34 146 |T 57 52 51 61 54 72 56 64
WRMS | 1608 18 34 29 15 19 33 146 |NE 50 43 43 55 44 53 62 44
MEDI | 1380 15 26 22 18 16 34 101 |MD 53 48 47 56 48 61 56 49
Table 3.2136.3 GPS week: 2136 Day: 3 MJD: 59199
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 | 2055 37 39 33 22 25 51 --- 15 | 77 67 40 54 45 33 --- 51
R02 | 902 7 13 11 9 12 27 146 5 | 36 34 36 43 35 49 140 36
R03M | 671 10 19 14 15 15 40 78 8 | 68 72 71 75 54 51 72 65
XR04 | 1465 14 14 31 --- 14 38 --- 11 | 53 44 32 --- 44 73 --- 46
R05 | 1405 20 21 30 35 24 34 118 12 | 47 43 28 30 49 58 57 36
R07M | 765 12 12 25 11 13 24 290 7 | 65 54 44 58 64 72 103 58
R08 | 675 15 11 17 11 17 34 --- 7 | 54 43 55 47 47 46 --- 48
R09E | 4099 13 14 11 22 20 26 --- 8 | 97 94 96 98 91 95 --- 93
XR11E | ---- --- --- --- --- --- 9 --- 0 | --- --- --- --- --- 141 --- 437
R12E | 989 15 30 16 18 10 21 --- 8 | 71 76 77 77 73 86 --- 74
R13E | 2025 22 48 26 39 25 39 --- 14 | 86 99 76 94 94 89 --- 85
R14E | 980 15 25 16 22 15 27 --- 8 | 188 192 186 194 177 174 --- 185
R15E | 2693 13 29 12 19 23 25 102 9 | 54 54 53 54 42 51 94 49
R16E | 1379 30 33 25 39 29 34 --- 14 | 49 42 68 78 51 77 --- 55
R17M | 1127 15 28 25 7 16 27 --- 8 | 319 317 309 319 323 307 --- 316
R18 | 997 8 23 16 13 18 18 --- 7 | 32 33 42 40 33 33 --- 33
R19 | 1582 45 98 84 56 72 47 --- 30 | 89 47 45 98 80 88 --- 68
R20M | 1356 33 60 84 32 40 62 --- 23 | 88 56 48 82 74 98 --- 68
R21 | 1140 17 26 28 11 14 38 134 10 | 47 39 34 52 38 65 86 43
R22 | 2215 23 40 24 23 31 33 --- 12 | 35 38 33 45 43 48 --- 33
R24M | 1528 24 35 24 14 15 35 --- 10 | 100 82 86 91 98 94 --- 90
------+----------------------------------------------+------------------------------------------
RMS | 1711 22 37 34 25 26 35 160 |T 82 76 72 85 77 87 92 93
WRMS | 1711 19 37 27 14 21 31 160 |NE 52 43 38 51 46 54 94 43
MEDI | 1356 15 26 24 19 17 34 118 |MD 65 54 48 75 51 73 86 58
Table 3.2136.4 GPS week: 2136 Day: 4 MJD: 59200
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 | 885 61 51 38 43 62 28 --- 21 | 68 65 40 47 30 40 --- 39
R02 | 967 14 12 18 12 18 31 45 8 | 35 32 42 32 23 25 54 29
R03M | 530 12 10 19 7 16 16 90 6 | 103 94 90 100 106 113 82 100
XR04 | 632 19 23 38 --- 16 17 --- 12 | 61 58 29 --- 57 43 --- 48
R05 | 1059 23 23 24 23 23 19 139 10 | 49 41 41 39 47 47 94 40
R07M | 810 16 12 15 18 15 25 157 8 | 54 44 41 45 41 61 140 46
R08 | 912 15 12 15 19 19 16 --- 7 | 48 45 52 35 49 41 --- 43
R09E | 3801 19 12 15 14 29 29 --- 9 | 84 89 88 90 84 80 --- 84
R12E | 1554 10 29 16 15 15 25 --- 8 | 55 57 62 63 57 62 --- 57
R13E | 1006 42 35 35 39 50 35 --- 17 | 98 95 120 110 87 95 --- 97
R14E | 1164 19 34 21 16 30 36 --- 11 | 113 121 132 119 130 95 --- 116
R15E | 3925 11 26 13 16 21 28 151 9 | 38 40 44 51 45 40 110 39
R16E | 1118 42 45 18 33 48 28 --- 16 | 45 46 60 75 76 76 --- 57
R17M | 1311 20 23 20 9 19 18 --- 8 | 527 533 531 532 530 536 --- 532
R18 | 1132 13 23 18 10 15 12 --- 7 | 30 36 35 35 28 34 --- 31
R19 | 2539 63 95 89 38 108 55 --- 33 | 67 36 52 60 73 75 --- 46
R20M | 1167 33 74 116 63 57 70 --- 32 | 80 44 45 111 93 112 --- 73
R21 | 731 15 26 32 10 18 32 116 10 | 42 34 30 42 55 54 91 41
R22 | 2224 29 44 22 26 63 26 --- 16 | 43 42 37 47 39 41 --- 34
R24M | 1017 36 32 20 15 39 38 --- 13 | 151 161 159 160 146 162 --- 156
------+----------------------------------------------+------------------------------------------
RMS | 1744 30 39 39 27 42 33 123 |T 89 85 86 94 89 91 95 85
WRMS | 1744 24 39 24 17 25 28 123 |NE 49 43 39 42 44 44 79 39
MEDI | 1059 19 26 20 16 21 28 116 |MD 55 45 45 60 57 61 91 46
Table 3.2136.5 GPS week: 2136 Day: 5 MJD: 59201
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 | 496 59 34 59 21 17 39 --- 17 | 64 47 35 38 37 30 --- 33
R02 | 1006 9 19 20 14 22 14 106 7 | 30 26 42 36 17 29 53 28
R03M | 713 17 16 23 11 21 28 80 8 | 130 129 118 115 137 117 120 123
XR04 | 462 23 19 28 --- 16 19 --- 10 | 63 56 42 --- 42 58 --- 51
R05 | 538 24 18 26 16 15 21 140 9 | 47 45 40 50 31 33 49 39
R07M | 559 13 13 13 8 16 15 182 5 | 46 43 41 38 38 42 60 40
R08 | 2172 7 10 20 14 11 29 --- 7 | 42 37 46 35 34 29 --- 35
R09E | 3951 15 14 24 17 21 20 --- 8 | 42 44 50 54 54 44 --- 45
R12E | 1096 25 24 14 25 18 41 --- 11 | 66 71 68 74 70 76 --- 68
R13E | 1045 42 37 48 33 36 30 --- 17 | 89 75 75 88 91 83 --- 80
R14E | 745 16 22 13 21 23 14 --- 8 | 176 183 180 191 172 176 --- 180
R15E | 1948 13 23 13 12 29 31 98 9 | 78 75 72 76 80 70 87 73
R16E | 1055 34 35 13 35 25 25 --- 13 | 28 28 39 54 42 39 --- 35
R17M | 950 16 28 35 14 25 13 --- 10 | 745 748 755 754 733 746 --- 747
R18 | 813 14 13 15 14 15 28 --- 7 | 30 31 33 30 29 31 --- 28
R19 | 2198 42 119 81 30 49 54 --- 28 | 63 52 37 51 60 64 --- 44
R20M | 1432 48 76 106 24 40 53 --- 26 | 69 49 53 59 60 81 --- 51
R21 | 616 11 31 24 13 28 42 101 11 | 35 33 39 46 38 47 54 38
R22 | 1259 25 43 37 29 62 31 --- 17 | 32 40 50 42 36 44 --- 35
R24M | 1723 32 30 23 9 18 32 --- 11 | 207 209 207 206 214 215 --- 209
------+----------------------------------------------+------------------------------------------
RMS | 1519 28 41 40 21 29 32 123 |T 104 101 101 107 100 102 70 99
WRMS | 1519 22 41 27 13 24 28 123 |NE 45 40 40 41 36 40 52 36
MEDI | 1006 17 23 23 16 21 28 101 |MD 63 47 46 54 42 47 54 44
Table 3.2136.6 GPS week: 2136 Day: 6 MJD: 59202
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 | 897 57 29 62 20 24 28 --- 17 | 90 59 56 59 60 45 --- 55
R02 | 985 14 13 10 14 16 10 177 6 | 44 38 33 40 26 35 111 35
R03M | 793 14 13 13 11 18 21 81 6 | 158 154 156 162 151 156 159 156
XR04 | 480 30 24 18 --- 20 33 --- 13 | 80 68 49 --- 57 65 --- 63
R05 | 706 26 21 26 12 24 23 133 10 | 65 56 44 55 43 54 60 51
R07M | 871 14 13 19 10 11 14 178 6 | 73 63 55 69 59 65 60 64
R08 | 2471 14 12 17 18 23 39 --- 10 | 54 46 55 53 48 46 --- 49
R09E | 3573 20 10 16 12 12 22 --- 7 | 120 121 119 121 116 122 --- 119
R12E | 2148 18 31 17 19 20 16 --- 9 | 75 75 71 73 77 78 --- 73
R13E | 1017 53 51 39 35 29 31 --- 18 | 68 64 67 63 59 57 --- 55
R14E | 760 19 18 9 13 13 23 --- 7 | 173 175 162 165 166 153 --- 165
R15E | 825 13 24 11 11 17 18 60 7 | 69 67 64 63 67 65 96 64
R16E | 1584 29 44 16 21 23 31 --- 12 | 46 41 56 68 62 68 --- 54
R17M | 2285 16 25 32 10 18 25 --- 9 | 944 943 938 948 950 950 --- 946
R18 | 634 12 19 10 17 20 34 --- 9 | 46 38 45 46 47 42 --- 41
R19 | 2210 36 131 86 45 95 53 --- 34 | 104 51 42 114 108 119 --- 84
R20M | 1031 37 71 103 29 49 38 --- 25 | 107 41 44 104 114 107 --- 85
R21 | 721 15 35 44 17 23 42 96 13 | 60 43 41 65 63 73 63 57
R22 | 1405 33 25 30 50 65 21 --- 18 | 46 45 47 58 53 57 --- 49
R24M | 1797 28 25 17 16 16 27 --- 9 | 276 262 263 269 265 264 --- 267
------+----------------------------------------------+------------------------------------------
RMS | 1610 28 42 40 23 34 29 129 |T 134 122 120 136 129 131 91 126
WRMS | 1610 25 42 25 14 26 26 129 |NE 65 49 45 61 56 59 78 53
MEDI | 985 19 24 17 17 20 25 96 |MD 73 59 55 68 62 65 63 63
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