[IGSREPORT-26903] Wk 2076 IGLOS Final Orbits
acc
acc at igs.org
Sun Nov 10 18:57:54 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2076 (Oct 20, 2019 - Oct 26, 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 2.2076.
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:
igl2076[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2076 in the SP3 format.
igl20767.sum Combination Report for GPS Week 2076.
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 | 6.2 ns
1 | -7.5 ns
2 | -7.3 ns
3 | -0.7 ns
4 | 8.9 ns
5 | -2.3 ns
6 | -4.8 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
----+--------+---------------
1 | ESX | R11
2 | ESX | 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 1.2076, 1a.2076).
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 2.2076.0-6)
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 3.2076.0-6).
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 2076 summary. (Oct 20, 2019 - Oct 26, 2019)
Table 1.2076.a GPS week : 2076 MJD: 58776.0-58782.0
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 20 1 19 .04 22 18 | -269904 -796 12723 290851
| 0 0 2 19 15 13 .03 | 498774 870
cof n/a| 0 0 -3 20 10 22 .11 25 21 | -269904 -803 12722 290852
| 1 1 2 16 25 19 .04 | 498774 872
emx n/a| 0 0 3 -11 -8 37 .07 24 24 | 0 -575 2768 7721
| 2 1 2 12 31 26 .04 | 0 788
esx n/a| 0 0 5 27 12 -12 .13 27 23 | -4980 -1338 2780 8424
| 1 1 2 14 16 30 .05 | 10242 1289
gfz n/a| 0 -1 -10 3 -17 17 .16 28 23 | -276798 -560 20103 290800
| 1 1 3 18 22 9 .08 | 494061 834
grg n/a| 1 0 0 -40 -11 -70 -.41 28 26 | -284623 -762 18164 290412
| 1 1 5 30 28 20 .05 | 488715 960
iac n/a| 0 0 0 0 18 -19 -.09 34 31 | -283472 -347 12744 290985
| 1 2 4 32 19 81 .05 | 489503 968
mcc n/a| 1 4 16 21 56 432 .18 190 190 | --- --- --- ---
| 9 10 25 225 144 427 .41 | --- ---
Table 1.2076.b GPS week : 2076 MJD: 58776.0-58782.0
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 | 24 25 20 20 20 20 19 |
R02 | 11 11 11 10 8 6 8 |
R03 | 10 10 10 10 10 8 8 |
R05 | 9 11 12 10 12 9 10 |
R07 | 10 10 9 10 9 10 8 |
R08 | 10 13 11 11 10 9 9 |
R09 | 7 7 8 8 8 7 8 |
R11 | 21 8 14 27 8 9 10 |
R12 | 14 10 11 11 11 13 15 |
R13 | 7 7 8 6 10 8 7 |
R14 | 10 8 8 8 10 8 7 |
R15 | 11 12 11 12 13 13 13 |
R16 | 19 18 14 15 15 15 14 |
R17 | 11 10 9 9 10 10 9 |
R18 | 8 7 8 7 6 7 9 |
R19 | 19 21 19 19 20 18 21 |
R20 | 15 12 12 12 17 13 15 |
R21 | 14 13 9 8 9 9 8 |
R22 | 10 10 12 9 9 8 9 |
R23 | 11 9 11 12 11 10 10 |
R24 | 13 11 13 15 15 14 11 |
R26 | 23 19 21 16 15 21 15 |
Table 1.2076.c GPS week : 2076 MJD: 58776.0-58782.0
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 2076 0 | -66 -26 63 409 177 -4390 82.4 1266 1266 | 6228 0
brd 2076 1 | 59 0 34 107 715 -3710 83.7 1754 1754 | -7511 0
brd 2076 2 | 16 23 30 138 -588 -2883 82.4 1545 1545 | -7319 0
brd 2076 3 | 57 16 5 -539 -815 -415 82.1 1563 1563 | -668 0
brd 2076 4 | 6 100 59 -1680 -98 1424 82.5 1475 1475 | 8853 0
brd 2076 5 | -50 90 -8 -901 267 3607 81.9 1225 1225 | -2292 0
brd 2076 6 | 6 -92 34 1707 -200 2406 81.9 2393 2393 | -4828 0
-------------+------------------------------------------------------------+----------------
brd 2076 mean| 4 15 31 -108 -77 -565 82.4 1603 1603 | -1076 0
brd 2076 sdev| 48 66 26 1076 521 3165 .6 392 392 | 6429 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 2.2076.0 GPS week: 2076 Day: 0 MJD: 58776
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 -8 52 1 2 .10 24 19 | 27045 352 2703 6711
cof n/a| 0 -1 -6 31 12 22 .12 26 21 | 27044 332 2699 6708
emx n/a| -1 1 8 -8 -26 43 .03 25 25 | 0 145 2701 6925
esx n/a| 0 -2 4 2 27 34 .14 29 24 | 7655 12 2807 8918
gfz n/a| 1 0 -10 25 -23 4 .10 31 29 | 16698 972 2698 6670
grg n/a| 0 0 9 -70 -28 -58 -.42 31 27 | 5878 889 2698 6296
iac n/a| -1 0 -7 -21 2 -39 -.06 37 36 | 7005 1570 2707 6944
mcc n/a| 0 9 17 -87 169 565 -.17 150 150 | --- --- --- ---
Table 2.2076.1 GPS week: 2076 Day: 1 MJD: 58777
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 6 10 .02 23 19 | -999999 -1653 72667 999999
cof n/a| -2 -2 -5 26 30 9 .05 26 22 | -999999 -1651 72667 999999
emx n/a| -1 0 5 -8 -1 1 .09 27 27 | 0 592 3031 9154
esx n/a| 0 1 4 21 -19 -21 .07 26 19 | -17114 -549 2990 10727
gfz n/a| 0 -2 -11 -7 -19 21 .12 28 21 | -999999 -1225 72664 999999
grg n/a| 1 0 2 2 -35 -86 -.49 35 29 | -999999 -1568 72672 999999
iac n/a| 0 3 -3 16 25 53 -.17 32 30 | -999999 -1182 72682 999999
mcc n/a| 5 -17 42 -149 -57 597 .27 163 163 | --- --- --- ---
Table 2.2076.2 GPS week: 2076 Day: 2 MJD: 58778
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 18 27 40 .03 24 24 | -999999 -1644 3080 999999
cof n/a| 0 0 -3 0 48 25 .12 26 25 | -999999 -1659 3081 999999
emx n/a| 0 -1 4 -29 -65 4 .08 24 24 | 0 -1242 3087 8035
esx n/a| -1 -1 2 40 16 -7 .10 26 22 | -6264 -3282 3132 3208
gfz n/a| 0 0 -16 -8 -29 32 .14 26 23 | -999999 -894 54740 999999
grg n/a| 0 1 5 -36 29 -62 -.37 24 22 | -999999 -1799 41143 999999
iac n/a| 1 -1 1 22 -10 59 -.14 33 31 | -999999 -871 3103 999999
mcc n/a| 6 14 29 409 38 877 -.00 189 189 | --- --- --- ---
Table 2.2076.3 GPS week: 2076 Day: 3 MJD: 58779
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 -3 -6 20 .06 23 18 | 19594 -532 2792 7640
cof n/a| 0 0 -3 -7 19 30 .11 27 20 | 19591 -532 2787 7635
emx n/a| 4 0 3 -23 -16 57 .12 21 21 | 0 -682 2715 7889
esx n/a| -2 -1 6 18 19 10 .09 26 23 | -8793 -1977 2694 9212
gfz n/a| -1 0 -12 -17 19 19 .06 25 20 | 10213 -812 2806 7583
grg n/a| -1 -1 -4 -10 12 -55 -.37 28 28 | -653 -328 2820 6864
iac n/a| -2 -2 2 55 36 -171 -.07 36 33 | 1159 -928 2863 7840
mcc n/a| 4 4 44 63 -154 954 .75 307 307 | --- --- --- ---
Table 2.2076.4 GPS week: 2076 Day: 4 MJD: 58780
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 29 0 24 .05 22 19 | 30195 -379 2634 7179
cof n/a| 0 1 -5 28 -18 -9 .05 26 22 | 30194 -382 2634 7183
emx n/a| -1 2 2 -16 17 62 .11 23 23 | 0 -741 2647 7316
esx n/a| -2 0 9 45 3 -38 .16 28 26 | -9318 141 2648 8863
gfz n/a| 0 -2 -8 32 -51 7 .18 29 19 | 20205 52 2638 7070
grg n/a| 3 -1 -4 -36 -9 -62 -.49 29 29 | 8892 -415 2639 6703
iac n/a| 1 0 6 -36 4 -67 -.04 31 28 | 11137 -118 2648 7367
mcc n/a| -18 3 -26 -265 162 -130 -.42 166 166 | --- --- --- ---
Table 2.2076.5 GPS week: 2076 Day: 5 MJD: 58781
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 26 -23 30 .04 20 16 | 17618 14 2616 6888
cof n/a| 0 -1 -3 26 -22 23 .14 23 18 | 17615 21 2613 6890
emx n/a| 0 -1 2 1 12 32 .01 24 24 | 0 -374 2617 7018
esx n/a| 1 -1 3 35 30 -56 .13 27 25 | 10615 -1300 2608 8571
gfz n/a| 0 0 -8 5 -20 23 .26 27 26 | 8228 -543 2610 6822
grg n/a| 1 2 0 -50 2 -58 -.39 22 22 | -2230 -512 2619 6155
iac n/a| -2 0 2 -11 40 14 -.10 32 28 | -1285 82 2623 6993
mcc n/a| 9 8 -5 -4 251 -23 .23 171 171 | --- --- --- ---
Table 2.2076.6 GPS week: 2076 Day: 6 MJD: 58782
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 20 2 8 -.01 20 15 | 16216 -1733 2570 7547
cof n/a| 0 0 0 36 5 55 .17 24 18 | 16223 -1752 2574 7553
emx n/a| -1 0 1 1 22 64 .03 23 23 | 0 -1728 2579 7710
esx n/a| 0 -1 6 30 12 -8 .21 28 22 | -11645 -2414 2583 9470
gfz n/a| 0 -1 -5 -3 0 14 .27 26 24 | 7065 -1475 2570 7462
grg n/a| 2 1 -8 -82 -52 -111 -.37 25 23 | -4256 -1605 2560 6872
iac n/a| -1 -2 3 -22 31 12 -.06 34 32 | -2328 -985 2582 7757
mcc n/a| 6 6 10 186 -14 188 .59 181 181 | --- --- --- ---
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 3.2076.0 GPS week: 2076 Day: 0 MJD: 58776
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 | 1193 49 46 31 79 24 50 71 --- 24 | 113 112 67 51 94 97 39 --- 71
R02 | 1240 15 22 20 23 30 23 40 141 11 | 79 84 59 50 93 87 44 99 67
R03 | 516 21 25 11 21 19 16 44 125 10 | 80 82 64 48 77 75 40 104 64
R05 | 795 14 21 13 19 31 13 32 --- 9 | 69 72 57 52 76 65 44 --- 58
R07 | 629 18 19 14 24 20 25 36 228 10 | 78 80 59 48 71 75 39 78 62
R08 | 667 17 13 14 20 31 17 41 --- 10 | 81 79 56 54 91 78 45 --- 67
R09 | 2223 10 12 11 14 23 22 10 --- 7 | 30 33 29 37 35 44 31 --- 31
XR11 | 1452 22 22 --- 66 38 30 35 220 21 | 58 58 --- 105 55 70 37 40 53
R12 | 1039 21 34 23 41 31 36 40 --- 14 | 82 90 59 48 83 92 40 --- 66
R13 | 3053 12 12 14 11 30 8 12 --- 7 | 57 59 50 57 74 56 53 --- 56
R14 | 721 16 13 17 21 31 15 32 --- 9 | 54 52 40 41 68 55 32 --- 46
R15 | 548 19 19 16 27 32 20 40 --- 11 | 73 74 59 52 89 76 40 --- 64
R16 | 1134 22 29 43 32 15 75 33 --- 18 | 63 67 69 57 66 107 45 --- 64
R17E | 1000 28 20 24 15 19 20 37 --- 10 | 81 77 71 77 80 79 76 --- 75
R18E | 1164 8 11 24 20 17 16 21 --- 8 | 68 66 65 72 70 72 74 --- 68
R19E | 608 47 48 38 33 39 51 38 --- 18 | 81 93 91 115 97 118 107 --- 95
R20E | 1648 21 26 36 23 50 29 40 --- 15 | 71 78 74 67 81 62 62 --- 66
R21E | 1263 26 23 27 19 57 26 34 44 14 | 106 104 100 101 124 101 96 159 101
R22E | 698 26 36 20 10 21 18 37 --- 10 | 89 95 86 90 90 89 87 --- 87
R23E | 696 14 19 28 27 32 24 16 --- 11 | 133 135 134 135 134 134 135 --- 133
R24E | 1375 19 24 33 20 34 36 37 --- 13 | 50 52 55 55 62 50 61 --- 49
XR26E | ---- 18 37 --- --- --- --- 31 --- 23 | 44 57 --- --- --- --- 36 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1266 24 26 25 29 31 31 37 150 |T 74 77 67 67 81 80 57 96 67
WRMS | 1266 19 21 25 24 29 27 36 150 |NE 70 72 55 53 74 75 40 80 59
MEDI | 1039 19 22 20 21 31 23 36 141 |MD 73 77 59 55 80 76 44 99 64
Table 3.2076.1 GPS week: 2076 Day: 1 MJD: 58777
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 | 742 51 48 43 76 32 51 66 --- 25 | 80 78 52 42 68 78 45 --- 51
R02 | 1098 17 23 15 30 24 34 28 128 11 | 55 59 42 33 67 72 40 57 48
R03 | 853 16 18 13 20 19 19 37 99 9 | 55 58 45 36 62 55 27 85 46
R05 | 760 26 27 17 21 22 16 38 --- 10 | 59 58 49 54 60 38 38 --- 48
R07 | 480 17 21 19 17 19 26 36 272 9 | 57 60 39 42 60 65 28 76 47
R08 | 504 17 21 26 19 35 35 39 --- 12 | 60 65 35 41 74 65 42 --- 51
R09 | 2768 12 14 9 7 22 29 14 --- 7 | 23 23 22 28 28 31 23 --- 23
XR11 | 1260 8 18 --- 211 14 12 24 207 8 | 41 50 --- 83 43 45 41 49 44
R12 | 843 21 20 18 22 11 27 31 --- 9 | 61 55 44 49 46 63 47 --- 50
R13 | 2018 8 11 17 9 23 19 18 --- 7 | 46 47 45 37 56 55 40 --- 45
R14 | 648 12 16 19 9 14 30 19 --- 7 | 34 46 37 37 43 58 35 --- 38
R15 | 479 19 23 16 24 31 24 44 --- 11 | 48 50 38 31 50 47 37 --- 39
R16 | 2219 23 29 52 16 24 83 23 --- 17 | 46 50 60 44 57 85 37 --- 48
R17E | 5466 19 14 23 17 15 33 20 --- 9 | 81 78 79 78 85 85 75 --- 79
R18E | 777 8 15 22 14 13 24 11 --- 7 | 47 43 46 52 45 52 55 --- 48
R19E | 853 48 53 48 33 55 61 41 --- 21 | 64 70 60 78 79 82 87 --- 66
R20E | 1249 19 31 27 19 37 34 32 --- 12 | 56 66 58 63 73 60 65 --- 57
R21E | 2044 13 17 25 22 51 14 26 82 12 | 81 87 74 79 96 79 75 158 79
R22E | 554 24 29 24 18 23 16 29 --- 10 | 87 93 86 90 92 85 81 --- 86
R23E | 1313 16 30 22 22 14 24 13 --- 8 | 92 94 90 96 100 98 96 --- 94
R24E | 994 18 21 37 20 26 29 18 --- 11 | 34 36 40 36 56 55 53 --- 40
XR26E | ---- 13 80 --- --- --- --- 27 --- 19 | 31 73 --- --- --- --- 45 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1754 23 26 27 26 28 35 32 163 |T 56 60 52 53 63 64 50 85 52
WRMS | 1754 19 22 27 19 21 29 30 163 |NE 51 53 42 42 54 58 36 66 44
MEDI | 853 17 21 22 20 23 27 27 128 |MD 55 58 45 44 60 63 42 76 48
Table 3.2076.2 GPS week: 2076 Day: 2 MJD: 58778
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 | 1321 50 46 30 55 35 20 63 --- 19 | 88 85 55 29 83 62 35 --- 55
R02 | 1978 19 19 16 32 17 22 33 109 10 | 64 66 47 41 65 64 35 34 51
R03 | 671 12 13 17 35 20 21 27 179 10 | 64 65 61 42 71 67 45 75 57
R05 | 578 32 39 17 30 14 19 39 --- 11 | 62 68 47 45 54 45 30 --- 44
R07 | 492 15 15 12 21 18 18 29 301 8 | 56 55 50 43 61 61 36 95 50
R08 | 786 11 23 21 16 32 26 37 --- 11 | 66 76 43 53 80 69 35 --- 57
R09 | 2964 11 12 16 14 15 29 18 --- 8 | 25 25 22 24 34 42 23 --- 25
XR11 | 934 11 13 --- 209 19 21 42 164 13 | 45 47 --- 102 46 47 29 82 43
R12 | 1130 16 16 17 23 26 25 39 --- 11 | 57 56 45 41 62 64 39 --- 50
R13 | 3299 12 17 18 19 18 17 16 --- 7 | 49 52 35 43 43 43 42 --- 40
R14 | 567 19 16 18 14 13 16 21 --- 7 | 40 39 28 30 32 37 23 --- 29
R15 | 483 21 24 15 19 31 15 44 --- 11 | 59 61 41 42 65 53 30 --- 47
R16 | 2107 27 29 31 23 22 47 33 --- 14 | 36 47 56 43 38 46 32 --- 38
R17E | 2378 19 21 24 13 20 15 23 --- 8 | 50 54 46 54 58 54 47 --- 49
R18E | 814 11 8 21 15 16 22 16 --- 8 | 24 28 27 33 29 38 35 --- 26
R19E | 703 50 55 41 37 45 23 52 --- 18 | 45 47 44 65 60 55 77 --- 47
R20E | 1115 18 19 29 17 39 19 29 --- 11 | 49 50 47 49 69 49 65 --- 49
R21E | 1126 16 14 22 17 29 13 25 92 9 | 43 45 38 40 51 34 43 86 39
R22E | 623 19 25 30 20 40 17 27 --- 11 | 106 113 106 106 121 113 99 --- 106
R23E | 1978 27 27 26 27 20 23 21 --- 11 | 46 42 47 57 58 44 50 --- 47
R24E | 937 16 38 33 25 23 38 29 --- 12 | 37 43 44 36 41 47 43 --- 37
XR26E | ---- 15 57 --- --- --- --- 27 --- 20 | 24 56 --- --- --- --- 31 --- 19
------+---------------------------------------------------+-----------------------------------------------
RMS | 1545 24 26 24 26 26 24 33 189 |T 51 55 46 48 58 54 42 74 45
WRMS | 1545 24 25 24 22 23 22 31 189 |NE 54 57 44 44 56 53 33 71 45
MEDI | 937 16 19 21 21 20 21 29 164 |MD 49 52 45 43 58 49 35 82 47
Table 3.2076.3 GPS week: 2076 Day: 3 MJD: 58779
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 | 1484 48 56 24 55 41 22 76 --- 20 | 99 104 59 29 91 65 23 --- 60
R02 | 2250 17 16 12 22 13 26 40 101 9 | 68 71 51 46 66 75 32 54 56
R03 | 462 11 12 17 29 12 31 32 329 10 | 72 73 62 53 74 86 45 179 64
R05 | 567 21 31 15 35 15 16 31 --- 10 | 62 71 50 44 59 50 33 --- 47
R07 | 670 14 17 10 27 17 35 30 342 10 | 62 61 53 43 68 85 35 144 56
R08 | 1117 13 11 16 18 23 28 50 --- 11 | 65 57 48 49 73 78 31 --- 56
R09 | 3707 15 15 14 16 19 24 21 --- 8 | 16 18 16 17 30 28 26 --- 17
XR11 | 685 35 31 --- 91 24 34 44 145 26 | 48 48 --- 109 41 40 18 131 46
R12 | 1381 20 34 16 25 22 21 40 --- 10 | 76 88 59 56 71 77 47 --- 64
R13 | 1217 12 16 9 14 11 17 13 --- 5 | 41 45 32 41 36 33 30 --- 34
R14 | 883 15 17 19 17 14 22 22 --- 8 | 45 47 31 39 42 49 29 --- 37
R15 | 465 18 21 17 26 26 30 43 --- 11 | 63 67 47 40 69 71 32 --- 54
R16 | 1817 24 19 27 24 37 44 47 --- 15 | 43 34 39 41 46 55 26 --- 38
R17E | 2616 16 21 22 15 17 23 24 --- 8 | 68 71 64 75 75 61 57 --- 66
R18E | 761 15 15 17 13 16 14 12 --- 6 | 21 22 24 25 30 24 22 --- 21
R19E | 1026 52 58 31 36 45 33 56 --- 18 | 47 52 54 73 80 55 87 --- 56
R20E | 1098 15 16 29 25 36 25 25 --- 12 | 46 47 47 58 58 53 47 --- 47
R21E | 603 15 21 20 17 15 17 20 377 7 | 58 60 60 60 61 60 61 343 58
R22E | 576 14 14 21 15 22 21 29 --- 9 | 72 70 79 67 76 66 61 --- 70
R23E | 2491 28 29 25 23 35 27 14 --- 12 | 27 30 28 43 56 35 34 --- 30
R24E | 1140 29 28 31 22 26 51 31 --- 14 | 25 34 31 42 39 55 32 --- 29
XR26E | ---- 10 30 --- --- --- --- 23 --- 16 | 24 32 --- --- --- --- 37 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1562 23 27 21 26 25 28 36 307 |T 52 54 46 50 59 57 38 170 47
WRMS | 1562 18 20 21 23 20 28 33 307 |NE 58 60 45 46 58 60 31 127 48
MEDI | 1098 15 19 17 23 22 25 30 329 |MD 48 52 48 44 61 55 32 144 47
Table 3.2076.4 GPS week: 2076 Day: 4 MJD: 58780
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 | 1166 44 45 25 67 40 17 62 --- 20 | 91 93 65 39 101 72 33 --- 65
R02 | 2002 17 21 14 23 11 20 24 106 8 | 59 62 43 39 50 54 32 54 46
R03 | 561 18 18 13 24 15 32 29 121 10 | 63 64 51 38 44 76 32 97 50
R05 | 906 22 15 24 31 22 23 37 --- 12 | 58 54 51 55 42 60 27 --- 46
R07 | 548 25 28 16 19 14 22 26 157 9 | 61 65 49 40 52 43 26 112 44
R08 | 1661 16 26 15 20 23 16 35 --- 9 | 56 63 49 34 59 52 25 --- 45
R09 | 3763 15 17 11 21 19 25 12 --- 8 | 17 19 13 21 31 24 24 --- 17
R11 | 562 10 21 17 13 13 20 30 266 8 | 39 46 20 79 31 49 19 108 34
R12 | 1099 24 34 14 24 18 23 41 --- 11 | 65 74 54 49 54 60 31 --- 51
R13 | 1178 15 16 11 35 14 30 16 --- 9 | 47 48 43 55 36 28 37 --- 38
R14 | 1629 13 25 23 19 30 18 19 --- 9 | 42 53 41 50 59 35 39 --- 41
R15 | 575 14 15 20 29 32 35 39 --- 12 | 55 57 42 40 70 70 36 --- 50
R16 | 870 18 24 32 43 32 37 36 --- 15 | 42 53 46 39 61 47 32 --- 40
R17E | 1513 15 17 29 16 23 22 20 --- 9 | 49 52 51 45 58 52 49 --- 48
R18E | 694 11 14 17 9 15 19 8 --- 6 | 29 32 31 31 26 35 29 --- 28
R19E | 752 42 50 39 39 58 27 55 --- 19 | 43 53 36 36 59 37 54 --- 31
R20E | 1377 21 18 33 22 53 51 34 --- 16 | 79 77 72 74 91 102 87 --- 78
R21E | 582 12 13 24 15 22 26 17 130 9 | 47 47 51 49 54 49 41 157 46
R22E | 1144 14 15 23 14 23 20 17 --- 8 | 76 79 67 81 91 79 71 --- 76
R23E | 2044 24 24 25 25 24 26 24 --- 11 | 51 52 60 61 61 51 50 --- 52
R24E | 2059 24 39 23 23 41 60 17 --- 15 | 33 53 42 38 40 53 35 --- 32
XR26E | ---- 11 45 --- --- --- --- 18 --- 14 | 25 55 --- --- --- --- 27 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1475 22 26 23 28 29 29 31 166 |T 51 56 46 47 55 53 38 105 44
WRMS | 1475 19 22 23 26 19 29 28 166 |NE 53 57 43 44 53 51 30 92 43
MEDI | 1144 16 21 23 23 23 23 24 130 |MD 49 53 49 40 54 52 32 108 45
Table 3.2076.5 GPS week: 2076 Day: 5 MJD: 58781
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 | 574 48 51 30 58 42 19 62 --- 20 | 85 89 60 36 80 56 30 --- 58
R02 | 937 14 19 12 19 10 9 18 160 6 | 55 58 47 41 52 45 40 39 47
R03 | 534 17 15 14 28 19 10 20 78 8 | 57 55 47 37 58 45 38 69 47
R05 | 1240 13 16 18 21 16 15 34 --- 8 | 44 47 43 43 38 43 33 --- 39
R07 | 454 21 24 15 28 14 18 38 181 10 | 58 58 45 29 48 54 20 74 43
R08 | 2128 9 12 15 14 28 14 34 --- 8 | 55 59 50 54 73 57 42 --- 55
R09 | 2482 10 13 15 18 18 14 7 --- 6 | 37 36 42 45 41 36 41 --- 39
R11 | 613 7 9 15 17 24 24 35 271 9 | 31 29 18 40 42 46 29 85 31
R12 | 858 17 12 18 37 39 22 45 --- 13 | 43 38 38 29 57 46 25 --- 38
R13 | 1465 10 18 11 22 9 29 11 --- 7 | 45 43 43 51 40 35 39 --- 40
R14 | 1194 16 12 22 18 11 11 18 --- 7 | 40 37 31 40 37 27 27 --- 32
R15 | 717 14 14 17 23 19 34 52 --- 12 | 47 45 35 35 49 56 23 --- 41
R16 | 955 14 21 35 48 24 46 20 --- 15 | 38 51 30 33 51 54 43 --- 38
R17E | 957 11 20 26 14 38 12 22 --- 9 | 68 69 68 71 89 74 64 --- 71
R18E | 780 12 14 21 13 16 14 19 --- 7 | 39 43 42 47 46 45 46 --- 42
R19E | 603 38 56 40 45 51 20 45 --- 18 | 51 62 45 55 72 54 69 --- 50
R20E | 1147 25 29 38 16 38 25 30 --- 13 | 91 98 79 80 85 89 85 --- 81
R21E | 841 11 12 26 16 23 16 26 92 9 | 88 88 93 94 97 79 86 159 88
R22E | 951 10 11 21 13 25 13 17 --- 7 | 60 62 57 60 67 52 55 --- 57
R23E | 1816 16 20 31 20 17 22 21 --- 9 | 83 85 83 87 87 90 81 --- 84
R24E | 1823 24 22 31 28 42 37 28 --- 14 | 32 36 39 45 51 37 32 --- 33
XR26E | ---- 14 46 --- --- --- --- 30 --- 20 | 35 48 --- --- --- --- 36 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1224 20 23 24 27 27 22 32 171 |T 53 56 49 50 60 53 44 85 49
WRMS | 1224 16 18 24 25 26 22 28 171 |NE 48 49 40 39 51 46 33 66 42
MEDI | 951 14 16 21 20 23 18 26 160 |MD 47 51 45 45 52 52 39 74 42
Table 3.2076.6 GPS week: 2076 Day: 6 MJD: 58782
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 | 988 50 57 24 59 15 16 64 --- 18 | 114 118 74 48 91 85 35 --- 74
R02 | 995 10 14 16 23 18 15 27 179 8 | 71 75 61 51 76 71 46 65 62
R03 | 663 14 16 12 25 14 10 26 142 7 | 77 81 69 52 76 73 50 100 67
R05 | 791 14 14 17 28 21 29 27 --- 10 | 73 70 66 55 58 75 50 --- 61
R07 | 470 18 16 12 27 11 17 22 203 8 | 78 77 61 48 67 79 45 70 63
R08 | 1945 7 12 14 18 30 21 32 --- 9 | 72 78 65 64 99 89 52 --- 73
R09 | 2159 13 17 15 18 21 18 13 --- 7 | 42 42 44 49 49 45 50 --- 45
R11 | 749 8 13 12 12 39 15 32 256 9 | 52 55 14 64 66 55 28 86 47
R12 | 9712 27 26 16 48 25 27 51 --- 14 | 82 84 59 56 84 87 40 --- 67
R13 | 725 6 10 9 16 23 18 17 --- 6 | 58 57 52 63 60 48 54 --- 54
R14 | 770 11 18 13 7 16 12 27 --- 6 | 54 54 40 46 56 55 32 --- 47
R15 | 901 15 19 16 22 14 36 58 --- 12 | 77 77 63 54 78 89 34 --- 66
R16 | 1474 17 32 32 34 31 45 22 --- 14 | 59 58 49 50 67 75 50 --- 55
R17E | 1119 10 15 22 17 27 17 26 --- 9 | 93 96 93 90 101 97 84 --- 92
R18E | 1369 10 8 26 14 25 21 17 --- 8 | 70 70 67 75 76 74 76 --- 71
R19E | 989 44 38 43 46 59 44 54 --- 21 | 64 73 56 94 94 81 67 --- 67
R20E | 1081 25 17 38 32 30 35 33 --- 14 | 111 107 105 100 117 110 114 --- 107
R21E | 1130 14 18 24 12 21 11 24 71 8 | 118 117 118 116 121 111 116 158 115
R22E | 963 9 14 25 18 25 12 30 --- 9 | 100 98 93 92 102 97 92 --- 95
R23E | 1173 17 34 21 19 26 28 18 --- 9 | 133 142 131 135 140 134 132 --- 133
R24E | 832 20 31 28 22 21 32 27 --- 11 | 45 59 49 60 55 57 46 --- 48
XR26E | ---- 10 57 --- --- --- --- 22 --- 15 | 36 63 --- --- --- --- 48 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 2393 20 24 22 28 26 25 34 181 |T 76 79 68 69 82 80 60 95 70
WRMS | 2393 15 18 22 22 24 23 32 181 |NE 69 71 55 53 71 71 43 80 60
MEDI | 989 14 17 17 22 23 18 27 179 |MD 72 75 63 60 76 79 50 86 66
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