[IGSREPORT-26957] Wk 2080 IGLOS Final Orbits
acc
acc at igs.org
Sun Dec 8 17:04:37 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2080 (Nov 17, 2019 - Nov 23, 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 2.2080.
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:
igl2080[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2080 in the SP3 format.
igl20807.sum Combination Report for GPS Week 2080.
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 | 1.1 ns
1 | 1.3 ns
2 | -1.0 ns
3 | 0.1 ns
4 | 0.7 ns
5 | 0.7 ns
6 | 0.5 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
----+--------+---------------
2 | GRG | R24
3 | GFZ | R24
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 1.2080, 1a.2080).
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 2.2080.0-6)
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 3.2080.0-6).
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 2080 summary. (Nov 17, 2019 - Nov 23, 2019)
Table 1.2080.a GPS week : 2080 MJD: 58804.0-58810.0
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 -1 0 23 17 28 .17 20 17 | 25506 22 3398 10194
| 1 0 1 14 11 24 .03 | 1974 2094
cof n/a| 0 0 0 27 23 14 .14 23 20 | 25492 24 3400 10198
| 2 1 2 24 23 35 .08 | 1979 2104
emx n/a| 0 -2 -1 11 -20 49 .01 26 26 | -486 -52 2815 7386
| 2 0 2 18 20 28 .04 | 10546 1399
esx n/a| 0 0 0 19 -14 -27 .14 24 20 | 1716 -1448 2777 9003
| 1 1 1 15 16 22 .04 | 11368 2162
gfz n/a| -1 0 0 11 -25 -17 .01 28 19 | 0 112 2766 7334
| 1 0 0 19 15 27 .09 | 0 1930
grg n/a| 1 0 4 -92 -2 -11 -.33 44 26 | 490 -50 2802 6527
| 1 2 4 26 23 54 .06 | 413 2237
iac n/a| -2 0 0 -10 27 1 -.15 23 21 | 1299 -31 3354 9712
| 1 1 3 24 17 30 .05 | 1189 1021
mcc n/a| 1 -5 16 158 21 298 -.19 202 202 | --- --- --- ---
| 10 13 13 225 161 559 .87 | --- ---
Table 1.2080.b GPS week : 2080 MJD: 58804.0-58810.0
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 22 20 19 15 18 15 |
R02 | 14 7 12 8 6 6 5 |
R03 | 15 6 10 6 6 7 6 |
R05 | 9 10 8 10 8 12 12 |
R07 | 15 6 14 7 7 5 6 |
R08 | 6 7 8 6 9 8 6 |
R09 | 8 7 7 8 6 7 7 |
R11 | 7 6 8 7 6 7 7 |
R12 | 11 10 11 12 10 9 11 |
R13 | 7 6 8 7 7 6 7 |
R14 | 10 8 8 7 8 10 8 |
R15 | 13 12 11 10 10 11 12 |
R16 | 9 11 11 15 16 15 11 |
R17 | 9 9 8 8 10 8 8 |
R18 | 6 7 8 9 7 7 8 |
R19 | 21 25 19 20 22 21 25 |
R20 | 14 11 12 19 14 12 16 |
R21 | 8 9 9 9 9 9 8 |
R22 | --- --- --- --- --- --- 0 |
R23 | 10 9 10 11 9 8 12 |
R24 | 13 16 42 573 --- --- --- |
R26 | 19 23 17 13 14 20 23 |
Table 1.2080.c GPS week : 2080 MJD: 58804.0-58810.0
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 2080 0 | 1 38 138 535 1886 526 81.5 1869 1869 | 1126 0
brd 2080 1 | 11 -26 149 226 2081 -2857 83.6 1483 1483 | 1325 0
brd 2080 2 | -15 35 188 -317 894 -2527 82.8 1528 1528 | -986 0
brd 2080 3 | 20 47 203 -702 -250 -2968 83.3 1577 1577 | 125 0
brd 2080 4 | -2 -11 307 529 -447 -962 83.4 1351 1351 | 727 0
brd 2080 5 | 43 38 176 -679 942 1140 81.9 1216 1216 | 743 0
brd 2080 6 | -4 10 138 490 970 776 85.0 1375 1375 | 492 0
-------------+------------------------------------------------------------+----------------
brd 2080 mean| 7 19 185 11 868 -981 83.1 1485 1485 | 507 0
brd 2080 sdev| 19 28 59 564 957 1812 1.1 208 208 | 767 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 2.2080.0 GPS week: 2080 Day: 0 MJD: 58804
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 6 3 15 .15 18 16 | 23473 1067 3743 16727
cof n/a| 1 0 -1 -15 -24 -21 .01 21 17 | 23444 1065 3712 16710
emx n/a| 0 -3 0 -21 -51 73 -.01 24 24 | 5788 516 2658 7749
esx n/a| 0 1 -1 6 -31 -40 .15 21 19 | -16602 -452 2662 8922
gfz n/a| -1 0 0 40 -36 -46 -.02 31 24 | 0 1309 2638 7749
grg n/a| 5 1 8 -73 29 -63 -.40 42 23 | 441 1068 2638 6694
iac n/a| -1 0 -3 -31 44 39 -.20 25 22 | -333 491 3639 15131
mcc n/a| 0 8 5 315 -136 -622 -1.12 230 230 | --- --- --- ---
Table 2.2080.1 GPS week: 2080 Day: 1 MJD: 58805
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 -3 -3 9 3 2 .16 18 15 | 27104 2449 3624 8205
cof n/a| 2 -3 -1 2 36 20 .14 22 21 | 27086 2456 3629 8220
emx n/a| 0 -2 0 29 -32 12 .04 24 24 | 8479 697 3294 7757
esx n/a| -3 0 1 47 -3 -24 .09 24 20 | 15699 -517 3293 9242
gfz n/a| 0 1 -2 20 -36 -18 .08 29 19 | 0 1880 3301 7813
grg n/a| 2 0 9 -97 -9 37 -.38 24 23 | -203 2663 3321 7135
iac n/a| -3 1 -3 -10 39 17 -.11 22 20 | 2217 1225 3575 8132
mcc n/a| 4 10 8 251 -24 -242 .05 198 198 | --- --- --- ---
Table 2.2080.2 GPS week: 2080 Day: 2 MJD: 58806
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 0 22 38 61 .15 23 19 | 27700 -4113 3543 7225
cof n/a| 0 0 1 43 35 32 .17 26 20 | 27700 -4133 3545 7235
emx n/a| 0 -3 0 24 -3 18 .01 28 28 | -5497 -2824 3131 6787
esx n/a| 0 0 0 9 8 -31 .16 36 33 | -4472 -5544 2849 8276
gfz n/a| -1 0 0 -16 -24 -16 -.12 28 18 | 0 -4011 2825 6631
grg n/a| 0 -5 1 -126 -29 59 -.29 146 42 | 1075 -4524 3016 6430
iac n/a| -1 2 -2 -9 39 -32 -.21 23 19 | 1194 -1979 3463 7267
mcc n/a| -3 -8 28 323 310 392 -.06 152 152 | --- --- --- ---
Table 2.2080.3 GPS week: 2080 Day: 3 MJD: 58807
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 43 21 16 .13 20 17 | 25059 235 2913 6273
cof n/a| 0 1 1 51 36 5 .28 25 21 | 25045 261 2913 6290
emx n/a| 0 -1 0 5 -34 88 .01 27 27 | -3127 -524 2720 6352
esx n/a| 0 -2 3 26 -18 -66 .13 25 19 | 5125 -978 2733 8076
gfz n/a| -1 -1 0 21 -5 -36 .12 34 19 | 0 -3 2722 6294
grg n/a| 1 1 6 -104 -31 23 -.33 27 27 | 427 -195 2716 5378
iac n/a| -1 0 -3 -23 22 -1 -.13 20 18 | 1840 -176 2932 6468
mcc n/a| -7 -27 18 -296 91 875 1.30 194 194 | --- --- --- ---
Table 2.2080.4 GPS week: 2080 Day: 4 MJD: 58808
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -3 13 19 17 .17 20 16 | 27648 -860 2907 7671
cof n/a| -1 0 -3 42 18 -24 .08 24 20 | 27638 -867 2904 7667
emx n/a| -1 -2 0 25 -19 67 -.04 25 25 | 12004 -127 2643 7685
esx n/a| 0 1 0 19 -38 -21 .09 22 17 | 7949 -2931 2646 9511
gfz n/a| 0 0 -1 1 -18 -33 .05 24 12 | 0 268 2641 7619
grg n/a| 0 0 3 -121 2 -39 -.38 26 24 | 885 -421 2673 6673
iac n/a| 0 1 3 25 30 15 -.09 23 21 | 2888 239 2816 7781
mcc n/a| -9 -11 37 330 -99 226 -.00 202 202 | --- --- --- ---
Table 2.2080.5 GPS week: 2080 Day: 5 MJD: 58809
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 29 17 67 .21 20 17 | 24533 1199 3306 9215
cof n/a| -3 0 2 34 44 79 .17 23 19 | 24525 1215 3348 9219
emx n/a| -2 -3 -1 1 4 48 -.02 28 28 | -1639 1637 2710 8527
esx n/a| 1 1 0 3 -2 -15 .19 21 17 | 10968 1129 2704 10412
gfz n/a| -1 0 -1 18 -47 -4 .05 26 22 | 0 926 2684 8443
grg n/a| 1 1 -3 -62 22 -14 -.28 24 22 | 286 1071 2712 7450
iac n/a| 0 0 4 16 -5 -45 -.12 23 21 | 1455 502 3461 9091
mcc n/a| 21 -11 13 97 -112 620 -.15 212 212 | --- --- --- ---
Table 2.2080.6 GPS week: 2080 Day: 6 MJD: 58810
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 0 35 15 20 .19 20 17 | 23025 178 3756 16048
cof n/a| 2 0 3 32 17 11 .13 23 20 | 23009 175 3754 16050
emx n/a| 4 -4 -7 17 -6 40 .09 28 28 | -19412 259 2554 6848
esx n/a| 0 0 -1 26 -17 7 .17 21 17 | -6651 -847 2555 8588
gfz n/a| -3 0 0 -8 -7 37 -.09 27 16 | 0 418 2551 6794
grg n/a| 1 1 5 -64 0 -85 -.27 23 19 | 523 -15 2540 5932
iac n/a| -5 0 0 -39 19 19 -.16 26 22 | -163 -520 3598 14114
mcc n/a| 7 0 0 88 119 837 -1.34 226 226 | --- --- --- ---
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 3.2080.0 GPS week: 2080 Day: 0 MJD: 58804
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 | 1209 26 33 42 27 29 48 34 --- 15 | 88 84 98 74 79 47 58 --- 73
R02 | 3301 12 17 13 19 14 87 14 363 13 | 56 59 55 57 52 82 50 148 50
R03 | 495 15 11 17 15 13 95 17 118 14 | 63 61 61 56 61 103 55 56 57
R05 | 1783 20 15 20 21 22 19 18 --- 9 | 57 54 60 42 44 39 41 --- 45
R07 | 762 10 11 16 22 30 92 11 189 15 | 65 67 66 54 54 113 55 166 59
R08 | 1061 7 14 17 12 18 13 17 --- 6 | 60 58 70 61 65 64 56 --- 61
R09 | 4197 12 12 14 15 18 22 21 --- 7 | 148 146 147 149 146 143 149 --- 147
R11 | 509 10 15 17 7 26 14 17 281 6 | 80 81 72 73 82 67 66 54 73
R12 | 1048 22 28 20 24 33 15 32 --- 11 | 70 74 45 51 80 59 38 --- 55
R13 | 2332 13 19 18 14 14 18 15 --- 6 | 53 56 40 64 56 42 53 --- 52
R14 | 2970 15 12 31 16 35 19 19 --- 10 | 99 100 87 94 115 98 84 --- 94
R15 | 583 23 19 21 24 32 29 41 --- 12 | 75 72 51 40 83 78 37 --- 57
R16 | 785 14 26 17 21 19 26 26 --- 9 | 64 76 54 76 67 88 67 --- 67
R17E | 2111 17 18 26 17 25 17 21 --- 9 | 48 51 44 52 54 49 45 --- 46
R18E | 739 5 11 11 12 17 19 11 --- 5 | 37 38 40 44 36 40 38 --- 38
R19E | 2276 38 42 46 34 72 44 50 --- 21 | 64 70 50 59 108 52 56 --- 57
R20E | 1733 20 17 37 19 55 24 28 --- 14 | 33 39 34 39 72 32 46 --- 33
R21E | 1065 11 17 23 11 27 14 17 62 7 | 44 43 40 37 47 43 36 91 38
R23E | 1632 20 21 16 26 25 18 19 --- 9 | 39 39 48 44 41 39 46 --- 39
R24E | 1092 25 28 30 33 30 40 23 --- 13 | 67 544 62 84 9999 246 45 --- 62
XR26E | 3981 15 62 --- --- --- --- 24 --- 19 | 61 69 --- --- --- --- 70 --- 63
------+---------------------------------------------------+-----------------------------------------------
RMS | 1869 18 21 24 21 31 42 25 230 |T 65 89 61 62 70 76 56 103 60
WRMS | 1869 16 17 24 19 24 23 22 230 |NE 75 76 69 68 75 78 62 106 68
MEDI | 1209 15 17 18 19 25 19 19 189 |MD 63 67 54 56 65 59 53 91 57
Table 3.2080.1 GPS week: 2080 Day: 1 MJD: 58805
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
------+---------------------------------------------------+-----------------------------------------------
XR01 | 1639 40 32 46 35 68 --- 28 --- 22 | 60 74 61 62 85 --- 45 --- 58
R02 | 1858 13 20 10 18 11 17 15 305 6 | 37 43 32 46 41 36 41 82 36
R03 | 1173 12 19 12 13 16 8 14 115 5 | 39 46 36 28 33 36 37 52 33
R05 | 1204 17 30 33 20 28 19 18 --- 10 | 41 50 38 34 36 38 24 --- 30
R07 | 811 6 14 14 18 12 14 13 117 6 | 40 42 44 30 35 45 40 108 38
R08 | 1392 15 21 9 21 15 19 7 --- 6 | 38 37 46 47 46 33 41 --- 39
R09 | 3015 10 15 8 21 20 12 17 --- 6 | 137 136 137 135 130 135 129 --- 134
R11 | 611 15 16 15 9 12 12 17 263 6 | 85 83 80 80 71 72 69 43 76
R12 | 1349 16 26 20 17 25 23 28 --- 9 | 52 61 39 41 54 49 36 --- 43
R13 | 1191 8 10 17 17 10 16 9 --- 6 | 49 52 45 58 58 47 56 --- 51
R14 | 2177 17 28 28 20 17 13 11 --- 8 | 108 115 103 113 102 105 103 --- 105
R15 | 930 23 31 19 26 23 25 36 --- 11 | 58 62 44 31 55 59 34 --- 44
R16 | 578 19 20 17 22 19 36 21 --- 10 | 61 59 72 78 67 85 72 --- 70
R17E | 1923 16 14 24 14 19 15 25 --- 8 | 55 52 55 55 56 59 57 --- 54
R18E | 1356 8 8 17 19 19 13 13 --- 6 | 26 26 25 30 35 28 30 --- 26
R19E | 811 35 34 58 60 79 56 48 --- 25 | 66 71 59 63 104 64 56 --- 57
R20E | 875 22 23 22 19 34 24 24 --- 10 | 39 41 34 44 45 38 38 --- 34
R21E | 885 16 14 24 16 17 23 24 88 9 | 25 28 16 28 34 26 32 62 22
R23E | 1750 14 18 15 27 27 24 16 --- 9 | 38 40 44 56 54 38 41 --- 41
R24E | 1858 30 31 34 39 49 36 21 --- 15 | 56 467 43 58 9999 345 25 --- 58
XR26E | 4605 21 71 --- --- --- --- 25 --- 23 | 69 89 --- --- --- --- 58 --- 61
------+---------------------------------------------------+-----------------------------------------------
RMS | 1483 18 22 24 24 29 24 22 198 |T 56 79 52 55 60 70 50 69 52
WRMS | 1483 15 21 24 20 19 23 20 198 |NE 61 66 59 60 62 61 55 71 58
MEDI | 1349 16 20 17 19 19 19 18 117 |MD 52 52 44 47 54 47 41 62 44
Table 3.2080.2 GPS week: 2080 Day: 2 MJD: 58806
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 | 1038 45 40 63 50 33 57 16 --- 20 | 64 67 71 63 54 30 48 --- 49
R02 | 740 12 17 15 13 15 77 12 200 11 | 42 46 46 53 46 93 51 107 47
R03 | 1712 17 20 13 9 11 62 14 106 9 | 43 41 44 54 53 86 45 39 48
R05 | 741 16 13 27 16 16 17 13 --- 8 | 37 34 42 30 29 43 26 --- 30
R07 | 715 13 17 15 12 9 97 18 80 13 | 52 51 51 49 48 95 59 89 49
R08 | 1184 17 13 16 13 24 17 14 --- 7 | 45 51 48 57 61 56 57 --- 52
R09 | 2679 11 15 13 11 21 14 19 --- 7 | 113 115 115 112 116 120 107 --- 113
R11 | 945 12 12 18 7 23 24 22 172 8 | 72 70 67 64 79 74 47 34 65
R12 | 929 19 20 22 18 27 34 25 --- 10 | 52 51 43 46 60 59 40 --- 46
R13 | 3076 11 12 14 21 16 27 11 --- 7 | 45 47 42 63 49 45 47 --- 49
R14 | 1027 22 23 23 12 8 19 14 --- 7 | 74 73 60 59 61 64 53 --- 60
R15 | 615 29 31 19 17 27 18 27 --- 10 | 65 69 45 37 62 47 35 --- 46
R16 | 702 19 32 18 16 30 53 15 --- 11 | 61 56 69 68 76 105 64 --- 68
R17E | 2370 15 13 26 9 23 19 15 --- 8 | 36 36 35 28 38 27 27 --- 29
R18E | 1230 14 17 22 17 13 18 14 --- 7 | 26 26 38 37 31 29 29 --- 31
R19E | 1752 52 63 44 30 49 45 38 --- 19 | 56 62 50 46 71 48 60 --- 45
R20E | 998 20 23 28 18 31 27 29 --- 11 | 30 38 30 41 57 40 51 --- 37
R21E | 814 20 17 23 15 13 28 17 168 8 | 31 30 25 32 32 30 27 50 26
R23E | 1289 15 15 22 22 29 25 18 --- 9 | 36 42 42 40 34 43 41 --- 35
R24E | 2408 35 38 52 138 70 626 54 --- 41 | 46 578 54 42 9999 366 50 --- 70
XR26E | 4464 18 111 --- --- --- --- 16 --- 17 | 35 121 --- --- --- --- 40 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1527 23 26 28 36 28 146 23 152 |T 50 81 50 51 55 75 47 63 49
WRMS | 1527 19 20 28 33 18 42 19 152 |NE 58 59 57 58 61 70 52 67 55
MEDI | 1038 17 17 22 16 23 27 16 168 |MD 45 51 45 46 54 48 47 50 47
Table 3.2080.3 GPS week: 2080 Day: 3 MJD: 58807
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 | 991 43 43 56 55 19 36 25 --- 18 | 78 80 86 60 59 40 48 --- 58
R02 | 688 9 11 19 13 23 21 14 207 7 | 43 39 52 44 36 41 49 243 42
R03 | 1818 6 15 7 17 20 18 12 148 6 | 49 56 52 50 55 60 47 105 50
R05 | 888 19 21 26 24 27 23 12 --- 9 | 42 42 49 38 43 36 38 --- 36
R07 | 660 14 18 16 17 23 16 11 246 7 | 59 62 54 52 51 64 49 200 53
R08 | 836 9 14 15 13 11 15 13 --- 5 | 51 54 44 52 52 44 53 --- 49
R09 | 2929 13 15 14 21 22 26 12 --- 8 | 60 60 59 55 65 79 63 --- 62
R11 | 1035 9 16 16 18 15 16 17 144 6 | 80 83 79 88 89 83 74 34 81
R12 | 569 21 25 27 20 36 24 30 --- 12 | 61 63 33 41 70 47 29 --- 43
R13 | 3504 13 11 13 18 12 19 11 --- 6 | 65 70 62 75 72 60 72 --- 67
R14 | 1014 14 20 17 15 17 15 15 --- 7 | 121 126 116 124 119 123 109 --- 117
R15 | 676 29 34 19 16 13 24 26 --- 10 | 66 71 47 42 48 49 32 --- 44
R16 | 1182 21 46 34 26 47 57 17 --- 15 | 92 100 84 99 99 124 100 --- 94
R17E | 1861 11 15 21 12 17 20 19 --- 7 | 37 37 34 39 46 34 38 --- 35
R18E | 1319 11 16 23 27 18 28 16 --- 9 | 35 42 39 48 37 29 28 --- 32
R19E | 1777 34 36 48 51 63 36 37 --- 20 | 92 99 91 116 122 91 85 --- 94
R20E | 1406 25 38 37 19 93 35 27 --- 19 | 30 55 29 34 109 41 39 --- 33
R21E | 1018 18 13 27 22 16 24 14 206 9 | 30 30 22 36 30 31 25 119 26
R23E | 2014 23 24 19 20 33 23 20 --- 10 | 27 28 39 45 40 38 42 --- 34
XR24E | 8189 453 3484 --- --- 9201 725 --- --- 573 | 53 9999 --- --- 9999 320 126 --- 137
XR26E | 5794 12 61 --- --- --- --- 13 --- 13 | 19 60 --- --- --- --- 28 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS | 1577 20 25 27 25 34 27 20 194 |T 56 62 56 59 65 71 55 140 57
WRMS | 1577 17 21 27 19 19 27 18 194 |NE 66 69 62 63 66 65 58 145 61
MEDI | 1182 14 20 19 19 20 23 15 206 |MD 53 60 52 50 55 47 48 119 49
Table 3.2080.4 GPS week: 2080 Day: 4 MJD: 58808
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 | 584 29 38 53 36 18 29 22 --- 14 | 70 81 80 53 59 62 46 --- 59
R02 | 893 12 22 19 14 7 16 15 358 6 | 41 47 46 37 39 32 40 244 37
R03 | 919 9 9 12 13 7 16 12 110 5 | 44 45 42 46 40 44 38 45 41
R05 | 1243 11 23 21 13 18 29 9 --- 7 | 34 50 44 42 46 26 33 --- 35
R07 | 1094 17 21 13 16 12 11 17 107 6 | 51 55 47 36 39 39 43 58 41
R08 | 722 9 8 11 18 13 29 30 --- 8 | 56 57 44 57 49 62 35 --- 49
R09 | 3643 10 13 11 11 16 19 16 --- 6 | 117 119 124 127 125 120 124 --- 122
R11 | 712 11 15 16 10 14 12 12 148 5 | 44 42 38 47 54 43 35 55 43
R12 | 820 16 31 22 24 27 16 29 --- 10 | 55 68 38 54 67 52 42 --- 49
R13 | 1272 8 9 17 18 14 20 16 --- 7 | 52 50 43 62 59 42 55 --- 51
R14 | 498 13 11 23 17 15 17 20 --- 8 | 55 54 42 69 67 48 52 --- 55
R15 | 710 31 24 19 11 12 15 26 --- 9 | 57 51 41 37 34 33 29 --- 36
R16 | 790 25 35 36 44 40 35 25 --- 15 | 63 81 50 64 80 75 65 --- 61
R17E | 1433 22 26 18 22 27 23 15 --- 9 | 36 40 40 45 39 47 28 --- 35
R18E | 1646 8 12 15 17 13 23 19 --- 7 | 26 32 33 32 31 37 25 --- 26
R19E | 1470 43 47 44 45 63 53 46 --- 22 | 97 101 84 88 106 98 75 --- 85
R20E | 1611 28 25 29 24 28 46 30 --- 14 | 33 33 35 51 49 55 43 --- 34
R21E | 777 21 17 27 13 14 19 19 173 8 | 29 31 22 28 31 29 28 138 25
R23E | 1356 16 17 18 16 26 19 21 --- 8 | 27 33 35 37 28 35 35 --- 29
XR26E | 6251 12 44 --- --- --- --- 16 --- 14 | 31 50 --- --- --- --- 35 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1350 20 24 25 22 24 26 23 202 |T 50 56 48 53 54 51 45 108 47
WRMS | 1350 16 20 25 17 12 24 21 202 |NE 56 61 52 56 58 52 49 100 52
MEDI | 919 13 21 19 17 15 19 19 148 |MD 44 50 42 47 49 44 38 58 41
Table 3.2080.5 GPS week: 2080 Day: 5 MJD: 58809
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 | 842 38 41 66 39 30 39 17 --- 18 | 58 65 65 34 51 38 43 --- 43
R02 | 644 8 9 10 13 12 12 21 347 6 | 35 37 34 45 44 44 22 132 35
R03 | 678 8 11 10 8 9 25 18 131 6 | 36 38 37 40 36 56 29 27 37
R05 | 1082 20 17 24 19 51 14 18 --- 11 | 36 35 39 28 49 33 40 --- 30
R07 | 934 13 10 9 8 18 9 10 221 5 | 42 41 37 43 51 38 36 93 39
R08 | 687 17 18 15 20 16 19 21 --- 8 | 46 54 46 61 58 53 35 --- 48
R09 | 3702 12 14 15 14 19 12 13 --- 6 | 68 68 63 71 65 58 62 --- 64
R11 | 635 11 16 17 10 21 15 14 138 6 | 56 61 49 61 69 50 53 52 55
R12 | 887 20 11 22 15 22 17 27 --- 9 | 59 48 44 46 60 48 33 --- 47
R13 | 1611 13 20 11 15 18 14 12 --- 6 | 53 57 53 57 46 50 53 --- 51
R14 | 663 20 24 28 22 23 18 24 --- 10 | 78 83 71 80 82 77 78 --- 76
R15 | 665 22 24 22 14 29 15 37 --- 10 | 44 48 28 37 53 34 27 --- 34
R16 | 688 27 26 33 31 29 47 20 --- 14 | 65 56 60 77 64 91 76 --- 70
R17E | 1106 16 14 21 12 17 17 18 --- 7 | 45 48 46 48 46 43 42 --- 43
R18E | 1072 10 11 19 14 19 16 12 --- 6 | 25 26 26 32 29 26 26 --- 24
R19E | 661 46 49 50 46 47 50 42 --- 21 | 104 111 105 107 110 102 103 --- 99
R20E | 650 15 36 35 19 27 24 36 --- 11 | 35 47 27 34 39 32 37 --- 28
R21E | 647 13 16 30 10 29 17 20 136 9 | 29 31 31 24 37 29 22 54 26
R23E | 1218 13 20 25 16 20 11 20 --- 8 | 28 30 30 33 33 41 37 --- 30
XR26E | 6053 18 65 --- --- --- --- 22 --- 20 | 53 80 --- --- --- --- 63 --- 54
------+---------------------------------------------------+-----------------------------------------------
RMS | 1216 20 23 28 21 26 24 23 212 |T 49 53 46 50 53 49 45 71 46
WRMS | 1216 17 19 28 17 22 22 21 212 |NE 52 53 48 52 56 51 45 76 48
MEDI | 688 15 17 22 15 21 17 20 138 |MD 45 48 44 45 51 44 37 54 43
Table 3.2080.6 GPS week: 2080 Day: 6 MJD: 58810
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 | 579 30 34 53 31 22 35 19 --- 14 | 87 90 101 52 72 46 60 --- 67
R02 | 809 10 23 11 10 12 12 10 296 4 | 53 56 53 46 48 47 47 161 48
R03 | 1679 8 9 12 14 14 11 14 148 5 | 57 59 55 62 55 64 61 36 58
R05 | 456 26 22 28 26 39 11 22 --- 12 | 50 51 59 47 55 49 37 --- 43
R07 | 1070 9 8 12 16 14 12 8 337 5 | 57 60 58 62 58 52 52 152 55
R08 | 1766 8 18 13 13 12 14 13 --- 5 | 61 63 64 68 64 66 55 --- 62
R09 | 3698 12 16 11 12 20 12 19 --- 6 | 106 106 103 107 106 104 100 --- 104
R11 | 638 15 22 20 10 15 8 16 132 6 | 70 73 60 67 70 66 60 53 65
R12 | 781 22 27 25 19 25 21 29 --- 10 | 76 80 47 56 77 67 45 --- 60
R13 | 1979 12 15 19 19 13 11 16 --- 7 | 61 60 49 65 56 51 58 --- 56
R14 | 1263 9 8 20 23 13 14 20 --- 7 | 67 62 63 60 63 58 71 --- 61
R15 | 786 20 24 26 21 33 18 36 --- 11 | 71 72 45 40 73 56 29 --- 51
R16 | 819 18 18 24 22 32 31 23 --- 11 | 66 67 54 77 80 75 73 --- 67
R17E | 1388 16 17 23 14 14 15 20 --- 7 | 51 52 50 50 50 47 44 --- 47
R18E | 584 14 17 21 10 18 23 20 --- 8 | 28 29 37 34 34 26 31 --- 29
R19E | 980 47 54 53 52 66 40 72 --- 24 | 96 99 106 101 101 82 96 --- 88
R20E | 593 15 21 56 20 46 33 36 --- 15 | 40 40 36 46 70 42 44 --- 40
R21E | 663 15 17 23 11 17 15 23 120 7 | 36 40 36 34 37 37 29 81 33
XR22E | ---- 3 32 --- --- --- --- --- --- 0 | 17 23 --- --- --- --- --- --- 16
R23E | 1447 25 28 15 18 22 47 16 --- 12 | 32 32 29 40 41 54 37 --- 33
XR26E | 5328 18 28 --- --- --- --- 28 --- 22 | 77 92 --- --- --- --- 69 --- 73
------+---------------------------------------------------+-----------------------------------------------
RMS | 1374 20 23 28 21 27 23 26 226 |T 59 62 58 58 63 57 54 96 55
WRMS | 1374 17 20 28 17 16 19 22 226 |NE 67 69 62 62 67 61 57 100 61
MEDI | 819 15 21 21 18 18 15 20 148 |MD 61 60 54 56 63 54 52 81 56
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