[IGSREPORT-26983] Wk 2082 IGLOS Final Orbits
acc
acc at igs.org
Sun Dec 22 20:59:39 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2082 (Dec 01, 2019 - Dec 07, 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 2.2082.
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:
igl2082[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2082 in the SP3 format.
igl20827.sum Combination Report for GPS Week 2082.
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 | -10.8 ns
1 | -4.4 ns
2 | -3.9 ns
3 | -3.9 ns
4 | -4.1 ns
5 | -3.9 ns
6 | -3.5 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
----+--------+---------------
6 | GFZ | R19
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 1.2082, 1a.2082).
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 2.2082.0-6)
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 3.2082.0-6).
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 2082 summary. (Dec 01, 2019 - Dec 07, 2019)
Table 1.2082.a GPS week : 2082 MJD: 58818.0-58824.0
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 0 22 22 29 .20 25 22 | 18202 62 3967 11321
| 1 0 1 18 18 31 .05 | 3720 1206
cof n/a| 1 -1 1 15 8 28 .11 27 24 | 18199 54 3966 11330
| 1 1 1 16 17 29 .05 | 3732 1181
emx n/a| 2 -1 -13 20 12 46 .14 31 30 | -14954 -384 2991 7822
| 1 1 1 13 22 57 .04 | 4038 658
esx n/a| -1 1 -2 0 -18 -11 .06 22 19 | -387 -1345 2995 9628
| 1 1 1 11 18 18 .06 | 5951 1386
gfz n/a| -1 0 3 -8 -23 -46 .06 31 19 | 0 -18 2991 7686
| 1 0 1 22 16 15 .13 | 0 730
grg n/a| 0 1 5 -38 -23 -36 -.24 23 19 | -4847 -249 2988 7030
| 1 1 2 26 20 35 .05 | 2561 760
iac n/a| -2 0 4 6 26 30 -.12 22 20 | -3474 -17 3992 10952
| 1 1 1 22 22 28 .03 | 3388 835
mcc n/a| 2 3 11 152 88 77 -.05 210 210 | --- --- --- ---
| 11 9 17 159 57 490 .50 | --- ---
Table 1.2082.b GPS week : 2082 MJD: 58818.0-58824.0
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 18 16 19 20 17 15 |
R02 | 5 7 8 6 6 6 5 |
R03 | 5 5 7 7 6 5 6 |
R05 | 12 11 9 9 8 8 10 |
R07 | 7 5 7 6 7 6 7 |
R08 | 8 10 7 8 10 8 9 |
R09 | 7 7 8 7 7 7 6 |
R11 | 7 7 6 8 6 7 7 |
R12 | 10 10 8 9 10 8 7 |
R13 | 8 9 8 9 8 7 9 |
R14 | 9 11 10 8 8 7 8 |
R15 | 12 9 9 11 8 8 9 |
R16 | 13 12 10 13 15 17 13 |
R17 | 9 9 11 8 9 10 11 |
R18 | 7 5 6 8 8 8 6 |
R19 | 30 27 33 29 25 27 30 |
R20 | 15 13 12 11 11 11 13 |
R21 | 9 9 9 9 11 10 10 |
R22 | 7 10 9 10 9 10 11 |
R23 | 11 12 12 13 11 11 8 |
R26 | 17 16 11 13 17 17 21 |
Table 1.2082.c GPS week : 2082 MJD: 58818.0-58824.0
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 2082 0 | -25 45 38 -974 -1675 6803 84.6 2013 2013 | -10783 0
brd 2082 1 | -35 8 -65 -1178 1317 5184 85.2 2139 2139 | -4443 0
brd 2082 2 | -29 33 -50 -769 905 2655 84.1 2098 2098 | -3881 0
brd 2082 3 | -55 23 -73 -1109 1859 1209 83.1 1805 1805 | -3939 0
brd 2082 4 | -19 20 49 564 1367 1161 81.3 1738 1738 | -4118 0
brd 2082 5 | -66 73 67 -388 -260 -77 82.9 1928 1928 | -3915 0
brd 2082 6 | 19 12 83 -125 -376 -1159 84.7 1838 1838 | -3517 0
-------------+------------------------------------------------------------+----------------
brd 2082 mean| -30 31 7 -568 448 2253 83.7 1937 1937 | -4942 0
brd 2082 sdev| 27 22 67 629 1257 2852 1.3 152 152 | 2590 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 2.2082.0 GPS week: 2082 Day: 0 MJD: 58818
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 -1 -1 27 0 11 .24 26 23 | 13045 -482 3714 7998
cof n/a| 3 -2 2 1 2 11 .10 28 25 | 13019 -493 3674 7978
emx n/a| 1 -4 -13 23 -10 116 .07 33 33 | -17717 -605 3170 7792
esx n/a| -2 2 -1 -9 2 -44 .12 21 17 | -799 -3230 3157 9655
gfz n/a| -1 0 2 11 -49 -50 -.06 30 20 | 0 -114 3160 7608
grg n/a| 0 0 8 -49 -3 -26 -.15 24 20 | -10624 -375 3158 6965
iac n/a| -1 0 3 17 35 66 -.16 23 20 | -8595 -729 3843 8479
mcc n/a| 16 12 -7 395 36 -9 .17 259 259 | --- --- --- ---
Table 2.2082.1 GPS week: 2082 Day: 1 MJD: 58819
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 1 50 11 -8 .17 24 22 | 18944 -1108 3658 9141
cof n/a| 1 -1 1 26 -16 16 .15 27 25 | 18943 -1095 3654 9172
emx n/a| 2 -2 -11 24 -14 98 .13 29 27 | -13178 -1246 3106 8340
esx n/a| -3 2 -1 -4 -13 13 .14 22 18 | -9033 -699 3128 9917
gfz n/a| 0 0 4 -24 -32 -40 .04 32 19 | 0 -778 3115 8280
grg n/a| 0 3 3 -82 -1 -65 -.28 24 21 | -3906 -1186 3122 7537
iac n/a| -2 -2 2 17 20 44 -.14 24 21 | -2451 -1483 3752 8758
mcc n/a| 1 7 16 -61 111 179 .57 239 239 | --- --- --- ---
Table 2.2082.2 GPS week: 2082 Day: 2 MJD: 58820
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 21 23 6 .18 23 23 | 19975 497 4006 9254
cof n/a| 1 -1 0 46 3 -11 .09 27 24 | 19996 445 4011 9332
emx n/a| 4 0 -12 35 18 27 .11 31 31 | -19014 -768 3082 8462
esx n/a| -1 1 0 8 -4 -12 .06 23 18 | -2767 -239 3075 10096
gfz n/a| -1 2 3 15 -3 -34 -.07 31 19 | 0 7 3075 8260
grg n/a| 0 1 1 -47 -34 5 -.22 26 22 | -3946 -30 3052 7908
iac n/a| -2 0 4 -28 8 4 -.09 24 20 | -1384 513 3981 9995
mcc n/a| 9 6 14 142 20 -318 -.29 180 180 | --- --- --- ---
Table 2.2082.3 GPS week: 2082 Day: 3 MJD: 58821
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 30 33 19 .29 26 23 | 12963 1481 5323 26538
cof n/a| 2 -3 0 2 -1 30 .14 28 26 | 12946 1476 5320 26531
emx n/a| 1 0 -13 31 38 -52 .19 35 29 | -10011 -123 2804 7711
esx n/a| 0 0 -1 -14 -19 5 .06 22 20 | 5069 -536 2807 9444
gfz n/a| 0 0 3 -19 -10 -69 -.04 28 18 | 0 181 2800 7506
grg n/a| -1 1 5 -21 -60 -63 -.25 25 21 | -4174 295 2795 7088
iac n/a| -1 0 2 23 14 66 -.15 20 18 | -7604 700 4970 23150
mcc n/a| 2 13 20 259 157 -280 -.35 126 126 | --- --- --- ---
Table 2.2082.4 GPS week: 2082 Day: 4 MJD: 58822
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 23 46 46 .21 27 22 | 21748 664 4038 9569
cof n/a| 1 0 4 15 27 68 .17 28 23 | 21761 621 4035 9571
emx n/a| 0 0 -12 0 0 80 .14 33 33 | -18205 -422 3039 7089
esx n/a| 0 1 -4 15 -54 -22 -.03 20 18 | -2781 -558 3063 9168
gfz n/a| -1 0 0 -5 -36 -28 .27 26 17 | 0 2 3062 6909
grg n/a| 2 -1 6 -26 -17 -7 -.30 24 19 | -4035 -272 3041 6373
iac n/a| -4 -2 4 -9 74 3 -.09 20 19 | -809 630 4402 9221
mcc n/a| 9 -7 6 14 31 -206 -.29 181 181 | --- --- --- ---
Table 2.2082.5 GPS week: 2082 Day: 5 MJD: 58823
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 15 3 83 .19 23 21 | 19081 -1762 3444 8116
cof n/a| -1 0 1 0 5 66 .07 27 24 | 19083 -1705 3481 8099
emx n/a| 1 -1 -14 3 40 25 .14 26 26 | -17150 -408 2700 6996
esx n/a| 0 0 -1 10 -13 -11 .03 26 25 | -1742 -3490 2708 8655
gfz n/a| -1 0 3 -45 -9 -35 .19 31 19 | 0 -808 2704 6892
grg n/a| -1 1 3 -43 -23 -86 -.25 21 16 | -3315 -1133 2705 5909
iac n/a| 0 0 5 34 18 23 -.14 23 21 | -3621 -250 3504 8124
mcc n/a| -20 0 -9 64 138 71 -.71 310 310 | --- --- --- ---
Table 2.2082.6 GPS week: 2082 Day: 6 MJD: 58824
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 -9 40 47 .12 24 23 | 21659 1147 3591 8633
cof n/a| 1 0 -1 12 36 18 .03 24 22 | 21648 1135 3587 8628
emx n/a| 2 -2 -13 27 15 30 .17 28 28 | -9409 879 3037 8369
esx n/a| 0 0 -4 -6 -28 -11 .01 24 19 | 9339 -667 3032 10461
gfz n/a| -1 -1 4 7 -22 -62 .10 39 20 | 0 1378 3024 8348
grg n/a| 0 1 7 0 -21 -11 -.23 21 16 | -3930 956 3045 7433
iac n/a| -2 0 5 -6 16 4 -.08 23 20 | 140 498 3494 8943
mcc n/a| 1 -11 41 251 123 1108 .58 176 176 | --- --- --- ---
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 3.2082.0 GPS week: 2082 Day: 0 MJD: 58818
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 | 1100 47 54 37 30 17 35 18 --- 14 | 70 79 87 58 59 44 57 --- 58
R02 | 1216 10 21 13 7 17 13 9 412 5 | 50 55 48 45 54 38 46 307 45
R03 | 1477 6 11 14 8 16 10 11 167 5 | 62 59 61 59 53 58 61 79 58
R05 | 729 32 27 28 31 25 8 27 --- 12 | 50 51 57 49 52 39 28 --- 39
R07 | 1767 10 21 17 13 27 15 13 251 7 | 53 57 60 50 57 55 51 78 52
R08 | 727 14 18 17 21 14 14 23 --- 8 | 55 64 59 65 58 59 47 --- 55
R09E | 4294 15 15 21 13 21 14 13 --- 7 | 87 85 91 86 92 90 89 --- 88
R11E | 1864 13 17 26 7 14 17 16 --- 7 | 114 116 113 113 118 114 114 --- 114
R12E | 1994 18 21 38 16 23 22 21 --- 10 | 59 63 48 51 59 59 51 --- 52
R13E | 1962 14 15 30 14 20 19 12 --- 8 | 30 32 25 41 47 35 31 --- 32
R14E | 1989 15 12 33 21 25 18 11 --- 9 | 105 113 108 126 124 105 110 --- 112
R15E | 428 13 15 38 18 34 30 27 --- 12 | 97 98 96 100 108 101 90 --- 97
R16E | 502 24 29 35 26 23 40 24 --- 13 | 37 36 40 55 54 36 43 --- 38
R17 | 3520 22 25 21 17 23 14 22 --- 9 | 68 68 50 46 62 54 44 --- 52
R18 | 1699 15 15 22 13 19 13 12 --- 7 | 58 58 53 70 59 54 59 --- 58
R19 | 1810 67 68 86 51 90 54 51 --- 29 | 76 73 73 61 94 46 37 --- 44
R20 | 2498 29 39 39 22 38 34 38 --- 14 | 69 67 60 56 80 69 38 --- 57
R21 | 538 19 21 20 12 24 15 26 87 8 | 66 64 43 52 69 50 37 66 51
R22 | 2308 22 16 18 9 13 12 20 --- 7 | 109 109 88 91 104 94 77 --- 93
R23 | 2727 30 32 24 26 30 17 20 --- 11 | 40 36 39 71 36 50 64 --- 49
XR26 | 3497 16 25 --- --- --- --- 17 --- 17 | 36 42 --- --- --- --- 44 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 2013 26 28 33 21 30 24 23 259 |T 66 67 64 67 71 62 58 132 61
WRMS | 2013 23 25 33 17 20 20 20 259 |NE 61 63 59 59 64 54 49 132 53
MEDI | 1810 16 21 24 16 23 15 20 167 |MD 62 64 59 58 59 54 51 78 52
Table 3.2082.1 GPS week: 2082 Day: 1 MJD: 58819
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 | 707 39 32 55 39 55 33 16 --- 18 | 52 61 60 47 72 36 48 --- 47
R02 | 1780 14 15 7 18 11 23 13 363 7 | 29 32 28 43 43 24 38 249 32
R03 | 626 6 11 9 10 18 11 14 131 5 | 52 54 50 55 48 53 51 76 51
R05 | 805 18 32 29 23 37 19 25 --- 11 | 40 56 42 39 49 49 28 --- 35
R07 | 2183 10 15 13 11 18 10 9 263 5 | 33 34 35 31 33 33 34 176 31
R08 | 2663 19 29 16 21 30 17 23 --- 9 | 41 55 34 43 53 35 38 --- 36
R09E | 2767 15 15 16 15 15 21 13 --- 7 | 52 53 59 57 62 60 57 --- 56
R11E | 1148 12 13 21 8 13 16 18 --- 6 | 72 75 78 76 78 77 69 --- 74
R12E | 1331 20 28 35 12 14 22 26 --- 10 | 40 44 38 37 38 35 42 --- 35
R13E | 4764 16 19 32 16 16 21 12 --- 8 | 24 24 24 27 34 37 23 --- 25
R14E | 2430 21 20 34 22 27 22 20 --- 10 | 101 95 88 88 108 100 87 --- 93
R15E | 717 11 7 28 18 26 24 19 --- 9 | 73 74 73 75 80 73 74 --- 73
R16E | 494 20 36 29 24 31 32 26 --- 12 | 29 39 38 45 52 29 30 --- 30
R17 | 3278 24 29 25 14 13 16 20 --- 8 | 43 47 30 30 35 37 29 --- 32
R18 | 1120 10 11 15 12 10 10 14 --- 5 | 40 42 37 43 43 39 43 --- 40
R19 | 2334 62 55 54 47 92 46 62 --- 27 | 58 58 61 41 75 32 35 --- 38
R20 | 2220 25 41 41 18 27 36 28 --- 13 | 49 61 50 37 50 47 29 --- 39
R21 | 574 22 25 18 11 22 20 24 105 9 | 42 44 31 37 42 26 29 32 33
R22 | 2648 18 20 24 11 23 22 30 --- 9 | 59 70 61 71 76 71 49 --- 63
R23 | 2247 29 36 25 36 26 15 18 --- 11 | 25 27 25 50 27 33 40 --- 31
XR26 | 3704 16 43 --- --- --- --- 15 --- 15 | 37 56 --- --- --- --- 37 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 2138 24 27 29 22 32 24 24 239 |T 47 52 47 48 54 46 43 133 44
WRMS | 2138 22 25 27 18 19 21 21 239 |NE 42 49 41 43 49 39 37 133 38
MEDI | 2183 18 25 25 16 22 21 19 131 |MD 42 54 38 43 49 37 38 76 36
Table 3.2082.2 GPS week: 2082 Day: 2 MJD: 58820
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 | 671 26 34 55 36 34 33 23 --- 15 | 52 62 70 70 71 50 47 --- 56
R02 | 2395 13 15 12 15 13 28 19 281 8 | 34 35 36 35 37 31 41 325 32
R03 | 1396 18 19 13 14 16 18 18 150 7 | 66 70 72 73 70 65 67 90 67
R05 | 607 22 16 22 13 21 9 22 --- 8 | 38 37 43 39 35 37 24 --- 32
R07 | 812 9 5 16 15 20 12 16 138 6 | 51 46 53 49 41 57 57 173 50
R08 | 3409 8 12 16 21 15 11 18 --- 7 | 45 49 45 56 55 51 44 --- 48
R09E | 2417 19 20 21 10 18 17 20 --- 8 | 40 41 41 42 41 42 42 --- 39
R11E | 1016 12 11 22 9 10 17 10 162 6 | 60 56 61 57 60 64 58 110 59
R12E | 1515 17 16 31 12 18 16 16 --- 8 | 41 38 36 32 37 38 33 --- 33
R13E | 4127 16 20 25 17 15 20 13 --- 8 | 34 39 36 42 39 42 34 --- 36
R14E | 3425 18 19 41 16 20 19 16 --- 9 | 71 73 62 65 74 71 63 --- 66
R15E | 1891 13 15 26 18 28 20 19 --- 9 | 94 95 91 101 104 86 97 --- 95
R16E | 992 15 27 22 21 26 24 28 --- 10 | 38 45 34 49 52 42 42 --- 38
R17 | 2611 31 32 30 19 18 20 20 --- 10 | 53 53 42 43 43 29 36 --- 38
R18 | 1176 11 14 17 14 11 12 11 --- 5 | 48 47 47 61 58 50 52 --- 52
R19 | 2185 59 77 80 63 101 76 69 --- 33 | 66 83 69 52 95 74 35 --- 43
R20 | 2180 34 36 36 7 23 34 18 --- 12 | 54 45 24 36 41 36 34 --- 34
R21 | 585 21 25 21 13 27 13 24 120 9 | 49 51 27 29 51 37 28 62 35
R22 | 2020 25 22 23 13 15 15 21 --- 8 | 91 89 74 79 86 73 67 --- 77
R23 | 1610 21 19 18 36 40 15 13 --- 11 | 36 33 35 60 27 38 43 --- 38
XR26 | 3337 12 25 --- --- --- --- 9 --- 11 | 30 44 --- --- --- --- 29 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 2098 23 27 31 23 31 26 24 179 |T 51 53 49 53 55 50 46 152 47
WRMS | 2098 23 24 31 18 19 22 20 179 |NE 50 53 49 52 54 48 43 162 44
MEDI | 1891 18 19 22 15 18 17 18 150 |MD 49 47 43 49 51 42 42 110 39
Table 3.2082.3 GPS week: 2082 Day: 3 MJD: 58821
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 | 782 44 41 73 31 43 43 22 --- 19 | 57 68 73 50 62 43 45 --- 46
R02 | 1259 10 14 10 13 13 20 8 115 5 | 37 40 38 41 41 28 35 175 35
R03 | 1899 18 18 13 10 11 17 14 155 6 | 118 120 124 117 120 113 109 62 115
R05 | 541 15 15 28 15 23 16 21 --- 8 | 36 42 42 36 43 38 33 --- 33
R07 | 552 11 16 12 10 19 12 11 105 5 | 52 58 56 54 54 57 60 104 54
R08 | 1595 13 18 15 28 15 18 11 --- 8 | 48 54 51 60 49 45 44 --- 48
R09E | 1748 15 14 19 11 16 16 17 --- 7 | 20 22 25 26 33 27 34 --- 24
R11E | 2298 10 12 28 15 12 21 13 140 7 | 36 38 31 42 42 41 38 37 36
R12E | 2050 17 16 28 18 20 21 17 --- 9 | 35 34 23 37 41 35 29 --- 30
R13E | 1421 8 14 32 19 26 18 8 --- 8 | 26 28 31 28 32 28 22 --- 22
R14E | 3503 20 15 29 13 16 15 16 --- 8 | 84 83 84 94 93 86 87 --- 87
R15E | 2530 17 21 31 18 29 23 32 --- 11 | 90 96 90 93 103 100 74 --- 89
R16E | 1500 19 37 38 22 38 30 22 --- 12 | 36 38 42 54 52 59 41 --- 41
R17 | 1413 24 27 20 10 12 19 17 --- 8 | 57 59 40 45 48 35 32 --- 41
R18 | 2012 14 15 16 19 10 27 14 --- 7 | 36 37 33 48 43 27 46 --- 38
R19 | 1918 75 65 98 50 71 50 43 --- 28 | 78 81 88 41 77 47 24 --- 37
R20 | 2206 30 47 34 17 14 34 14 --- 10 | 47 59 36 34 35 30 29 --- 30
R21 | 671 27 29 19 9 18 17 22 104 8 | 53 53 30 34 48 33 26 44 35
R22 | 2187 28 34 19 14 24 21 17 --- 9 | 77 78 55 57 77 54 51 --- 60
R23 | 929 16 25 11 38 40 24 20 --- 12 | 35 33 38 67 25 29 50 --- 39
XR26 | 6826 14 75 --- --- --- --- 12 --- 13 | 38 75 --- --- --- --- 24 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1804 26 28 35 22 28 25 20 125 |T 52 56 51 52 55 47 44 84 46
WRMS | 1804 23 26 29 19 18 21 18 125 |NE 54 61 54 52 55 44 43 96 45
MEDI | 1748 17 18 20 15 18 20 17 115 |MD 47 54 40 45 48 38 38 62 38
Table 3.2082.4 GPS week: 2082 Day: 4 MJD: 58822
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 | 2031 40 39 81 39 32 53 22 --- 20 | 60 71 73 47 51 29 49 --- 43
R02 | 1933 8 10 15 15 15 10 12 213 5 | 35 35 44 38 32 37 34 203 34
R03 | 1559 13 13 10 11 20 16 11 65 6 | 71 72 78 72 76 78 76 48 73
R05 | 551 16 17 22 17 24 15 13 --- 8 | 35 32 39 39 40 32 31 --- 31
R07 | 989 13 14 13 18 11 14 19 281 7 | 64 63 58 77 67 52 54 108 61
R08 | 676 16 21 16 29 24 18 23 --- 10 | 45 42 45 60 57 37 31 --- 44
R09E | 1849 17 19 16 12 22 13 13 --- 7 | 38 35 37 38 48 34 44 --- 39
R11E | 2943 12 9 23 11 12 13 9 160 6 | 50 50 53 55 55 51 52 33 51
R12E | 1832 20 12 29 21 12 29 14 --- 9 | 35 33 26 45 41 46 36 --- 35
R13E | 1426 15 13 24 19 18 14 10 --- 7 | 21 18 20 33 25 15 25 --- 20
R14E | 2397 18 11 35 13 12 13 12 --- 8 | 51 54 61 64 61 58 54 --- 57
R15E | 1842 16 17 28 12 22 16 16 --- 8 | 92 91 88 89 96 88 89 --- 89
R16E | 1479 21 41 38 15 28 53 31 --- 14 | 35 40 44 43 57 52 54 --- 39
R17 | 1302 20 18 20 12 14 21 24 --- 8 | 58 57 44 50 54 60 36 --- 48
R18 | 1688 12 18 19 24 17 18 11 --- 8 | 52 51 50 63 52 42 58 --- 53
R19 | 1497 82 72 75 31 68 30 41 --- 25 | 79 74 53 35 71 38 30 --- 35
R20 | 2371 31 46 28 12 36 16 19 --- 10 | 45 63 34 37 61 28 31 --- 35
R21 | 478 27 26 24 20 34 18 24 97 11 | 49 48 34 30 56 33 31 53 34
R22 | 2517 25 21 21 16 21 14 18 --- 8 | 51 47 37 38 50 40 38 --- 40
R23 | 772 22 29 19 28 23 20 23 --- 10 | 31 31 31 56 31 35 53 --- 40
XR26 | 4105 19 47 --- --- --- --- 13 --- 16 | 20 62 --- --- --- --- 31 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS | 1738 27 28 33 20 26 24 20 181 |T 48 50 47 50 54 44 44 89 43
WRMS | 1738 22 23 33 18 17 19 19 181 |NE 49 53 47 49 53 41 41 103 42
MEDI | 1688 18 18 22 16 21 16 16 160 |MD 49 50 44 45 54 38 38 53 40
Table 3.2082.5 GPS week: 2082 Day: 5 MJD: 58823
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 | 1661 24 39 60 49 28 36 20 --- 17 | 44 54 67 34 46 44 47 --- 43
R02 | 866 15 20 18 12 18 8 11 465 6 | 32 35 36 29 31 29 23 432 27
R03 | 746 6 7 12 10 9 9 12 115 4 | 90 92 94 89 92 89 92 121 91
R05 | 778 18 29 16 18 23 14 21 --- 8 | 32 46 34 39 35 35 17 --- 28
R07 | 1099 11 11 9 17 20 9 10 427 5 | 39 38 38 39 29 42 36 230 35
R08 | 767 14 12 16 16 21 15 22 --- 8 | 33 34 40 39 39 45 31 --- 34
R09E | 2195 13 15 17 14 20 16 8 --- 6 | 57 61 64 65 64 58 64 --- 60
R11E | 3921 8 9 26 17 10 11 15 240 6 | 83 86 90 83 88 93 83 49 86
R12E | 1842 11 12 25 14 19 22 15 --- 8 | 41 46 45 41 48 48 41 --- 41
R13E | 2046 14 15 16 19 18 12 12 --- 6 | 20 25 19 33 31 23 21 --- 20
R14E | 3142 9 7 26 20 12 11 11 --- 7 | 69 67 56 76 76 69 69 --- 68
R15E | 4261 13 14 30 11 19 14 14 --- 7 | 75 79 72 80 82 73 73 --- 75
R16E | 1206 16 24 31 31 56 53 23 --- 17 | 27 36 33 41 58 56 39 --- 29
R17 | 553 17 26 22 18 26 12 30 --- 9 | 46 54 41 42 56 42 32 --- 41
R18 | 969 12 12 14 27 14 14 14 --- 7 | 49 53 50 69 59 45 55 --- 52
R19 | 882 71 79 41 60 92 27 62 --- 27 | 71 83 44 69 98 34 24 --- 46
R20 | 1846 28 29 23 23 23 27 24 --- 11 | 43 33 42 39 43 35 33 --- 36
R21 | 728 21 24 22 23 21 19 28 106 10 | 44 44 34 28 45 46 25 65 34
R22 | 2052 28 27 23 20 21 16 27 --- 10 | 100 102 88 98 105 93 82 --- 93
R23 | 637 24 26 18 34 32 10 21 --- 10 | 29 31 35 49 26 24 39 --- 31
XR26 | 5152 16 70 --- --- --- --- 18 --- 17 | 41 80 --- --- --- --- 34 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1927 23 27 26 26 31 21 23 310 |T 50 56 51 54 57 51 45 179 47
WRMS | 1927 21 24 26 25 19 16 21 310 |NE 49 55 49 51 54 46 40 212 44
MEDI | 1206 15 20 22 18 20 14 18 240 |MD 44 53 42 41 48 45 39 121 41
Table 3.2082.6 GPS week: 2082 Day: 6 MJD: 58824
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 | 714 28 34 62 31 16 34 22 --- 15 | 72 80 101 50 65 36 51 --- 58
R02 | 1021 8 10 8 16 9 9 12 248 5 | 49 53 49 56 50 52 47 256 49
R03 | 646 12 7 10 11 16 11 14 141 5 | 91 95 97 101 97 99 94 162 96
R05 | 1256 21 21 31 19 27 18 16 --- 9 | 45 49 56 40 45 39 28 --- 37
R07 | 1257 20 20 12 10 16 17 17 84 7 | 63 62 60 61 57 59 51 221 57
R08 | 591 15 14 22 27 16 20 16 --- 9 | 58 63 57 79 69 61 59 --- 62
R09E | 3105 12 14 17 12 14 13 12 --- 6 | 83 82 87 81 84 84 86 --- 83
R11E | 4079 9 10 28 10 19 15 8 210 6 | 111 111 111 110 113 108 113 102 110
R12E | 1933 12 12 25 18 15 12 14 --- 7 | 58 58 63 53 65 56 64 --- 58
R13E | 980 14 22 33 17 21 16 15 --- 8 | 25 29 23 40 44 27 32 --- 28
R14E | 2893 7 9 25 19 20 14 14 --- 7 | 71 69 61 70 69 75 66 --- 67
R15E | 3342 11 10 28 17 23 19 17 --- 8 | 104 102 98 99 107 105 105 --- 102
R16E | 687 18 27 33 22 41 29 30 --- 13 | 35 40 46 55 45 51 47 --- 40
R17 | 459 19 18 22 25 29 13 30 --- 10 | 74 71 53 57 75 61 45 --- 60
R18 | 1051 12 11 15 14 13 10 9 --- 5 | 65 61 59 73 61 58 68 --- 64
R19 | 534 68 66 42 68 147 49 60 --- 30 | 105 104 45 68 144 88 31 --- 59
R20 | 1606 33 30 32 20 27 34 29 --- 13 | 63 60 45 50 62 50 41 --- 49
R21 | 957 27 21 22 14 22 16 26 149 9 | 69 68 45 43 66 48 39 83 50
R22 | 1775 28 26 24 20 28 14 32 --- 11 | 84 83 80 75 89 72 75 --- 77
R23 | 1677 18 28 18 26 16 17 14 --- 8 | 38 36 43 69 38 41 56 --- 46
XR26 | 5443 19 44 --- --- --- --- 23 --- 21 | 54 65 --- --- --- --- 54 --- 51
------+---------------------------------------------------+-----------------------------------------------
RMS | 1837 24 24 28 24 39 21 23 176 |T 67 68 63 66 72 63 59 164 62
WRMS | 1837 23 22 28 19 20 16 20 176 |NE 66 67 60 63 70 58 52 180 58
MEDI | 1256 18 20 24 18 19 16 16 149 |MD 65 65 57 61 65 58 54 162 58
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