[IGSREPORT-27378] Wk 2112 IGLOS Final Orbits
acc
acc at igs.org
Sun Jul 19 02:33:38 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2112 (Jun 28, 2020 - Jul 04, 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 2.2112.
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:
igl2112[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2112 in the SP3 format.
igl21127.sum Combination Report for GPS Week 2112.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -0.7 ns
1 | -1.0 ns
2 | -1.4 ns
3 | -1.3 ns
4 | -0.5 ns
5 | -1.4 ns
6 | -2.0 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2112, 1a.2112).
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 2.2112.0-6)
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 3.2112.0-6).
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 2112 summary. (Jun 28, 2020 - Jul 04, 2020)
Table 1.2112.a GPS week : 2112 MJD: 59028.0-59034.0
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 1 8 -1 7 .09 19 16 | 21785 -621 2938 8100
| 0 1 1 12 22 24 .02 | 407 990
cof n/a| 1 0 3 2 10 15 .10 22 18 | 21786 -631 2938 8101
| 1 0 2 26 27 21 .02 | 405 991
emx n/a| -1 0 -6 18 -5 -33 .02 45 45 | -8490 -466 2949 8121
| 0 2 1 15 27 17 .03 | 8662 716
esx n/a| -1 0 -8 23 4 33 .16 46 32 | -2285 232 2949 10056
| 0 1 1 19 17 21 .06 | 7038 642
gfz n/a| 0 0 5 -18 7 -32 .13 27 18 | 0 -192 2951 7587
| 0 0 2 11 27 33 .06 | 0 1070
grg n/a| 0 0 -3 -21 2 -58 -.37 25 20 | -1002 -335 2927 7167
| 0 0 3 9 17 27 .02 | 444 961
iac n/a| -1 0 2 6 0 79 .03 23 23 | 676 -90 2936 8204
| 1 1 2 18 37 28 .03 | 637 921
mcc n/a| 2 1 -6 9 43 -322 -.21 133 133 | --- --- --- ---
| 6 7 9 105 65 349 .48 | --- ---
Table 1.2112.b GPS week : 2112 MJD: 59028.0-59034.0
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 18 19 22 20 18 25 |
R02 | 9 8 8 9 9 7 9 |
R03 | 6 7 8 7 8 10 9 |
R04 | 13 11 9 12 12 11 12 |
R05 | 9 10 9 9 7 6 11 |
R07 | 8 8 8 7 10 7 10 |
R08 | 6 8 7 8 8 7 12 |
R09 | 7 7 8 8 8 8 7 |
R11 | 6 6 8 7 6 5 6 |
R12 | 9 7 9 9 8 8 8 |
R13 | 18 19 19 21 19 20 21 |
R14 | 7 6 7 6 8 9 7 |
R15 | 7 7 8 9 8 9 7 |
R16 | 12 11 10 14 16 15 13 |
R17 | 9 10 8 10 10 10 13 |
R18 | 6 6 8 9 10 6 8 |
R19 | 28 23 23 23 22 26 24 |
R20 | 31 33 28 27 29 29 36 |
R21 | 10 11 10 10 11 10 12 |
R23 | 9 8 8 8 8 7 8 |
R24 | 12 11 12 14 12 13 18 |
R26 | 17 27 27 29 11 17 0 |
Table 1.2112.c GPS week : 2112 MJD: 59028.0-59034.0
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 2112 0 | -33 7 209 -301 403 425 82.2 1449 1449 | -674 0
brd 2112 1 | -58 -10 192 153 -649 -2244 82.9 1390 1390 | -970 0
brd 2112 2 | 2 0 244 -538 -1136 -1103 80.7 1478 1478 | -1422 0
brd 2112 3 | 46 -5 241 289 -360 797 82.1 1395 1395 | -1290 0
brd 2112 4 | -13 36 292 72 -21 1132 80.9 1352 1352 | -466 0
brd 2112 5 | 8 54 292 400 1447 -239 82.2 1382 1382 | -1387 0
brd 2112 6 | 76 51 301 1138 85 -367 82.3 1593 1593 | -2028 0
-------------+------------------------------------------------------------+----------------
brd 2112 mean| 4 19 253 173 -32 -228 81.9 1434 1434 | -1176 0
brd 2112 sdev| 45 27 43 538 826 1167 .8 81 81 | 523 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 2.2112.0 GPS week: 2112 Day: 0 MJD: 59028
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 26 -20 23 .09 19 17 | 22206 859 3496 7348
cof n/a| 0 0 1 -32 -15 31 .11 19 17 | 22204 851 3503 7353
emx n/a| 0 2 -5 18 -3 -10 -.01 49 49 | -8942 436 3511 7293
esx n/a| -1 -3 -8 17 7 15 .09 48 34 | 2567 1154 3509 8538
gfz n/a| 0 0 0 -37 17 -49 .08 27 17 | 0 1560 3509 6700
grg n/a| 0 0 1 -23 37 -79 -.35 25 16 | -1349 1459 3465 6751
iac n/a| 0 -1 1 20 0 83 .01 22 22 | 314 1024 3508 7317
mcc n/a| -1 1 -5 124 -19 -252 .01 118 118 | --- --- --- ---
Table 2.2112.1 GPS week: 2112 Day: 1 MJD: 59029
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 0 7 -29 -5 .11 18 13 | 21647 -79 2623 7831
cof n/a| 4 -1 6 34 -33 28 .12 22 16 | 21654 -94 2629 7832
emx n/a| -2 -3 -9 50 0 -43 .03 47 47 | -18725 -146 2637 7922
esx n/a| -1 1 -9 50 16 48 .10 46 30 | 3292 259 2639 9908
gfz n/a| 0 0 7 -27 -23 -30 .15 25 16 | 0 -249 2645 7135
grg n/a| 0 0 -6 -37 11 -65 -.38 26 23 | -745 -281 2618 6643
iac n/a| 0 1 4 19 23 92 -.01 22 22 | 66 772 2620 7916
mcc n/a| 4 -4 10 110 -30 -7 -.41 113 113 | --- --- --- ---
Table 2.2112.2 GPS week: 2112 Day: 2 MJD: 59030
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 1 15 2 13 .07 19 14 | 21118 -1661 2577 8436
cof n/a| 1 0 0 10 7 19 .08 23 17 | 21119 -1668 2572 8435
emx n/a| -1 0 -8 14 5 -13 .05 43 43 | -3159 -1533 2585 8424
esx n/a| -1 2 -6 29 23 59 .13 45 31 | 5966 -231 2584 10774
gfz n/a| -1 1 6 -7 -11 23 .14 21 16 | 0 -1345 2610 7867
grg n/a| 0 -1 -3 -13 -12 -94 -.39 26 20 | -721 -1503 2556 7186
iac n/a| 0 3 5 21 -13 32 .00 21 21 | 513 -431 2568 8592
mcc n/a| 14 3 -4 -59 73 -252 -.26 132 132 | --- --- --- ---
Table 2.2112.3 GPS week: 2112 Day: 3 MJD: 59031
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 15 32 18 .07 19 15 | 22032 -1196 2543 8526
cof n/a| 0 0 4 0 48 9 .06 23 19 | 22024 -1192 2551 8528
emx n/a| -1 0 -6 11 -7 -26 -.03 42 42 | -14952 -1148 2550 8551
esx n/a| 0 0 -8 -3 15 52 .15 48 32 | -1508 -749 2556 10580
gfz n/a| 0 0 7 -24 16 -57 .12 28 18 | 0 -1197 2549 7890
grg n/a| 0 0 -10 -16 -2 -76 -.35 26 21 | -983 -726 2543 7682
iac n/a| 0 1 3 13 -60 78 .04 23 23 | 1828 -1776 2544 8667
mcc n/a| -5 12 -8 -146 -11 203 -.82 167 167 | --- --- --- ---
Table 2.2112.4 GPS week: 2112 Day: 4 MJD: 59032
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 -14 18 -21 .10 21 19 | 22258 -403 3260 8169
cof n/a| 0 1 1 -25 26 -11 .11 21 19 | 22262 -418 3257 8172
emx n/a| 0 -2 -8 5 -51 -48 -.00 44 45 | 7433 -447 3263 8163
esx n/a| 0 0 -9 27 -26 27 .17 45 29 | -3442 699 3264 10192
gfz n/a| 0 0 6 -9 9 -50 .05 29 21 | 0 592 3231 7738
grg n/a| 0 0 0 -14 -6 -17 -.35 25 21 | -297 -186 3253 7269
iac n/a| -2 1 0 4 17 69 .07 22 22 | 1241 56 3254 8344
mcc n/a| 6 10 -16 -79 131 -782 -.51 145 145 | --- --- --- ---
Table 2.2112.5 GPS week: 2112 Day: 5 MJD: 59033
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 5 -19 -21 .08 21 16 | 21538 1 3166 7960
cof n/a| 0 0 4 -3 16 -13 .10 23 18 | 21541 -6 3165 7959
emx n/a| 0 -1 -4 26 -21 -54 .06 48 48 | -13103 252 3190 7922
esx n/a| -2 -1 -12 1 -8 -1 .23 48 36 | -9837 -94 3188 9764
gfz n/a| 0 0 4 -6 58 -62 .11 29 18 | 0 277 3183 7776
grg n/a| 1 0 -1 -31 0 -35 -.34 22 19 | -1472 32 3160 7083
iac n/a| -3 0 0 -4 -24 126 .08 19 19 | 601 116 3164 8027
mcc n/a| 0 -3 -3 22 50 -575 -.16 128 128 | --- --- --- ---
Table 2.2112.6 GPS week: 2112 Day: 6 MJD: 59034
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 2 3 44 .09 20 14 | 21697 -1869 2901 8433
cof n/a| 1 -1 4 33 22 43 .12 23 17 | 21704 -1890 2894 8429
emx n/a| -1 0 -6 6 39 -35 .06 42 43 | -7987 -682 2910 8578
esx n/a| 0 -1 -7 42 3 35 .22 42 34 | -13033 587 2908 10641
gfz n/a| -1 0 8 -14 -11 3 .24 28 18 | 0 -987 2930 8008
grg n/a| 0 1 -4 -13 -13 -43 -.40 24 19 | -1453 -1143 2897 7560
iac n/a| -2 0 3 -28 54 71 .03 30 30 | 171 -394 2898 8571
mcc n/a| 0 -7 -16 92 113 -588 .70 131 131 | --- --- --- ---
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 3.2112.0 GPS week: 2112 Day: 0 MJD: 59028
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 846 39 27 36 86 33 30 23 --- 18 | 108 103 66 42 82 79 89 --- 80
R02 | 1533 10 14 32 24 27 12 14 118 8 | 78 87 52 60 96 72 88 62 77
R03 | 1332 5 11 15 23 13 8 15 118 5 | 78 77 72 61 81 80 88 48 78
XR04 | 585 24 31 26 22 --- 30 22 --- 12 | 75 77 63 47 --- 46 61 --- 59
R05 | 545 15 26 23 25 21 11 22 --- 8 | 60 69 53 43 55 46 65 --- 53
R07 | 1240 13 10 15 29 17 15 16 159 7 | 79 79 66 51 85 80 67 52 73
R08 | 1240 9 11 20 20 18 11 10 --- 6 | 77 81 65 60 84 80 74 --- 74
R09 | 3908 16 10 13 15 14 11 16 --- 6 | 37 36 39 42 45 30 43 --- 37
R11 | 2033 7 10 28 9 16 15 8 70 6 | 58 57 43 55 67 53 60 105 56
R12 | 676 17 14 29 17 20 17 23 --- 9 | 85 84 72 63 76 62 81 --- 74
R13 | 1816 30 25 46 46 42 56 23 --- 18 | 74 77 35 49 90 40 75 --- 59
R14 | 788 11 11 28 11 9 22 9 --- 7 | 67 72 58 69 73 77 77 --- 70
R15 | 730 17 7 25 17 15 8 10 --- 7 | 82 77 70 54 65 62 73 --- 69
R16 | 1292 20 30 38 20 37 20 25 --- 11 | 65 63 56 73 101 78 94 --- 77
R17 | 644 7 12 25 38 24 9 17 --- 8 | 49 48 36 34 62 56 61 --- 50
R18 | 602 7 11 25 13 10 15 9 --- 5 | 39 38 30 38 44 48 42 --- 40
R19 | 580 38 31 139 88 37 53 29 --- 27 | 89 94 42 45 94 93 93 --- 78
R20 | 1649 26 31 115 136 54 47 60 --- 31 | 111 105 50 46 128 134 131 --- 105
R21 | 700 7 8 42 29 28 16 15 106 9 | 54 57 36 45 70 57 64 55 55
R23 | 1622 12 22 10 33 28 17 10 --- 8 | 22 20 24 40 33 20 29 --- 24
R24 | 889 12 16 51 42 20 22 20 --- 11 | 64 67 43 58 72 78 76 --- 65
XR26 | ---- 14 68 --- --- --- --- 19 --- 16 | 41 79 --- --- --- --- 51 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 1448 19 19 49 48 27 25 22 118 |T 67 70 51 51 75 65 71 64 63
WRMS | 1448 17 17 49 34 17 16 22 118 |NE 67 70 51 51 75 65 71 64 63
MEDI | 889 13 14 28 24 20 16 16 118 |MD 67 77 52 49 73 62 73 55 65
Table 3.2112.1 GPS week: 2112 Day: 1 MJD: 59029
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 | 977 46 42 45 71 33 29 18 --- 18 | 80 79 42 38 80 53 51 --- 59
R02 | 1115 8 19 32 22 26 10 13 112 8 | 58 60 39 51 77 53 68 31 60
R03 | 1710 7 11 17 27 15 8 14 131 6 | 57 58 47 43 70 58 74 35 59
XR04 | 831 22 24 28 23 --- 19 15 --- 10 | 56 58 58 42 --- 42 53 --- 49
R05 | 598 14 13 19 20 18 33 21 --- 9 | 41 34 41 43 48 25 50 --- 39
R07 | 881 11 9 18 27 15 19 15 153 7 | 52 51 45 39 55 59 51 25 50
R08 | 494 11 14 21 28 11 20 10 --- 7 | 53 53 42 39 43 58 49 --- 48
R09 | 3703 12 15 16 13 15 14 18 --- 6 | 36 33 31 39 48 26 40 --- 35
R11 | 1479 9 15 22 15 12 16 11 60 6 | 42 48 28 45 45 28 46 74 39
R12 | 873 14 16 26 12 15 15 16 --- 7 | 67 72 60 63 61 65 70 --- 64
R13 | 863 20 33 62 59 56 36 24 --- 18 | 47 63 22 38 82 27 55 --- 43
R14 | 1371 6 9 23 13 15 12 14 --- 6 | 51 51 48 51 52 52 49 --- 50
R15 | 752 16 18 27 19 13 14 11 --- 7 | 55 63 52 45 56 47 57 --- 52
R16 | 1617 16 25 32 18 36 14 20 --- 10 | 45 53 46 50 73 46 61 --- 52
R17 | 896 12 12 33 30 10 19 33 --- 10 | 22 25 22 23 30 27 42 --- 25
R18 | 746 8 14 20 14 16 11 13 --- 6 | 22 22 23 29 29 16 20 --- 20
R19 | 648 27 33 109 68 30 53 28 --- 22 | 41 49 43 33 40 42 42 --- 37
R20 | 2249 35 48 124 141 47 65 48 --- 33 | 58 77 57 66 66 72 57 --- 53
R21 | 832 10 12 39 34 14 17 29 82 10 | 31 34 32 30 34 21 40 34 28
R23 | 1076 13 15 15 35 15 19 14 --- 8 | 19 26 31 32 29 21 26 --- 22
R24 | 989 10 14 47 32 12 16 27 --- 10 | 40 38 40 53 48 41 54 --- 43
XR26 | ---- 23 56 --- --- --- --- 32 --- 27 | 19 56 --- --- --- --- 29 --- 18
------+---------------------------------------------------+-----------------------------------------------
RMS | 1390 18 22 47 46 25 26 22 113 |T 45 50 40 42 53 41 49 39 42
WRMS | 1390 13 16 47 30 16 23 22 113 |NE 45 50 40 42 53 41 49 39 42
MEDI | 896 12 15 27 27 15 17 16 112 |MD 45 51 42 42 48 42 50 34 43
Table 3.2112.2 GPS week: 2112 Day: 2 MJD: 59030
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 | 1141 43 49 37 100 29 20 12 --- 19 | 83 90 60 49 70 66 64 --- 61
R02 | 1658 7 11 29 28 14 9 16 115 7 | 65 65 49 48 73 65 66 65 62
R03 | 1356 11 10 29 21 18 10 12 148 7 | 68 70 61 64 88 79 81 37 74
XR04 | 751 19 20 18 24 --- 13 12 --- 8 | 60 58 43 43 --- 43 48 --- 48
R05 | 1128 15 19 19 22 13 29 22 --- 9 | 44 51 43 49 52 31 58 --- 45
R07 | 1420 9 11 16 38 18 12 16 149 8 | 57 55 44 38 67 57 49 19 53
R08 | 457 11 12 22 19 18 19 10 --- 7 | 57 56 43 44 51 57 53 --- 50
R09 | 3212 18 16 16 16 16 12 21 --- 7 | 31 30 34 27 33 30 35 --- 28
R11 | 834 14 12 19 14 13 27 10 122 7 | 49 46 37 48 55 26 39 73 41
R12 | 703 11 15 33 12 19 27 17 --- 9 | 43 43 28 39 54 30 54 --- 40
R13 | 1163 26 27 65 54 53 27 22 --- 18 | 60 59 31 37 84 47 66 --- 53
R14 | 2386 7 13 20 13 14 11 25 --- 7 | 50 54 44 54 48 45 69 --- 50
R15 | 971 17 20 27 16 13 17 11 --- 7 | 66 68 55 53 58 55 65 --- 58
R16 | 1588 18 23 32 18 20 21 25 --- 10 | 50 55 55 67 65 63 77 --- 60
R17 | 1407 10 15 25 27 13 21 15 --- 8 | 31 32 25 26 34 36 38 --- 29
R18 | 743 7 14 17 10 15 29 21 --- 8 | 26 35 27 26 28 37 27 --- 24
R19 | 640 37 39 98 65 28 54 23 --- 22 | 66 70 36 40 55 57 55 --- 49
R20 | 2328 29 47 99 122 30 55 47 --- 27 | 77 94 63 48 74 78 73 --- 66
R21 | 926 9 10 33 30 16 13 28 122 9 | 38 39 25 29 39 29 47 42 34
R23 | 715 11 9 16 35 11 19 10 --- 7 | 20 25 33 33 24 13 22 --- 19
R24 | 1589 11 16 53 38 17 16 28 --- 12 | 46 53 32 48 55 51 52 --- 46
XR26 | ---- 23 78 --- --- --- --- 32 --- 27 | 25 88 --- --- --- --- 33 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1478 19 23 43 45 21 26 21 132 |T 50 56 41 43 55 47 53 47 46
WRMS | 1478 14 17 43 31 16 20 21 132 |NE 50 56 41 43 55 47 53 47 46
MEDI | 1141 11 15 27 24 16 19 17 122 |MD 50 55 43 44 55 47 53 42 48
Table 3.2112.3 GPS week: 2112 Day: 3 MJD: 59031
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 | 773 41 32 62 96 38 30 36 --- 22 | 89 87 47 52 70 73 89 --- 68
R02 | 2916 16 14 22 37 15 11 22 130 9 | 66 65 43 42 66 52 72 127 59
R03 | 647 8 11 18 19 16 15 14 164 6 | 65 67 51 50 70 70 56 62 62
XR04 | 563 28 32 22 17 --- 17 23 --- 11 | 63 64 48 39 --- 30 32 --- 43
R05 | 1300 9 12 22 32 23 18 18 --- 8 | 49 57 34 38 69 41 59 --- 49
R07 | 976 12 16 13 26 21 13 9 151 7 | 61 67 46 46 75 48 60 15 57
R08 | 1033 7 9 24 26 18 23 7 --- 7 | 56 56 41 45 64 63 59 --- 56
R09 | 3315 12 17 14 17 27 20 13 --- 8 | 23 31 19 30 27 29 24 --- 21
R11 | 826 9 13 18 11 25 13 6 210 6 | 53 57 45 48 68 39 50 139 50
R12 | 534 15 15 27 13 20 22 23 --- 9 | 60 59 44 49 66 34 58 --- 51
R13 | 737 28 32 56 53 68 46 29 --- 20 | 68 72 38 35 99 46 78 --- 58
R14 | 1734 7 13 22 12 16 10 10 --- 5 | 53 54 35 45 55 42 52 --- 47
R15 | 753 19 20 27 20 14 22 10 --- 8 | 61 62 46 44 58 36 56 --- 51
R16 | 824 30 35 33 33 33 30 33 --- 14 | 55 51 51 72 91 78 99 --- 72
R17 | 1289 10 15 34 42 15 22 20 --- 10 | 41 44 28 27 50 50 48 --- 41
R18 | 639 15 20 30 22 11 22 21 --- 9 | 30 30 24 38 41 52 49 --- 38
R19 | 1118 35 40 93 72 35 55 22 --- 23 | 79 92 47 47 76 82 73 --- 67
R20 | 1138 22 43 87 126 51 26 50 --- 26 | 97 109 67 48 114 105 113 --- 92
R21 | 660 9 12 32 46 20 12 16 168 9 | 46 48 36 31 50 45 49 63 42
R23 | 1025 8 13 23 30 16 15 16 --- 7 | 19 22 25 30 18 14 25 --- 16
R24 | 1674 23 31 54 41 15 33 25 --- 14 | 46 53 26 31 44 56 44 --- 40
XR26 | ---- 25 35 --- --- --- --- 32 --- 28 | 29 51 --- --- --- --- 40 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1394 19 23 42 48 28 26 23 167 |T 54 59 40 42 63 51 58 81 50
WRMS | 1394 15 19 42 32 18 21 23 167 |NE 54 59 40 42 63 51 58 81 50
MEDI | 976 15 16 27 30 20 22 20 164 |MD 55 57 43 44 66 48 56 63 50
Table 3.2112.4 GPS week: 2112 Day: 4 MJD: 59032
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 | 876 42 39 69 74 37 30 27 --- 20 | 76 77 57 61 66 54 56 --- 57
R02 | 3177 12 16 31 29 13 18 18 125 8 | 55 60 42 37 51 64 55 96 52
R03 | 616 10 11 15 17 18 21 23 105 8 | 65 66 59 60 76 76 54 65 64
XR04 | 583 29 34 19 25 --- 12 29 --- 12 | 58 60 44 27 --- 39 36 --- 41
R05 | 1119 8 10 20 20 19 16 17 --- 7 | 44 43 34 37 58 38 51 --- 43
R07 | 736 12 10 19 37 20 10 28 166 9 | 61 62 46 41 76 57 79 16 61
R08 | 636 9 10 25 21 9 20 18 --- 7 | 60 60 49 49 62 74 72 --- 62
R09 | 2928 13 12 16 17 35 8 14 --- 8 | 30 24 29 29 38 24 26 --- 25
R11 | 1121 13 15 16 21 8 14 13 166 6 | 48 50 38 53 38 30 37 135 39
R12 | 551 14 24 25 16 16 18 15 --- 7 | 59 69 46 43 63 46 55 --- 52
R13 | 1495 39 40 52 53 63 27 24 --- 19 | 72 68 44 50 93 61 66 --- 61
R14 | 703 9 13 28 11 11 18 26 --- 8 | 50 55 42 45 51 37 65 --- 48
R15 | 758 7 10 25 21 19 13 16 --- 7 | 58 61 49 44 61 57 64 --- 56
R16 | 903 39 30 45 28 38 19 40 --- 16 | 42 53 49 60 101 80 102 --- 71
R17 | 1032 10 11 38 36 14 13 23 --- 9 | 35 37 23 31 39 34 47 --- 35
R18 | 655 14 17 38 23 14 23 16 --- 9 | 21 23 24 25 38 35 40 --- 28
R19 | 825 29 32 69 80 47 49 28 --- 21 | 60 60 45 40 63 45 58 --- 48
R20 | 1253 32 31 111 117 53 62 27 --- 29 | 67 76 44 46 96 93 81 --- 69
R21 | 681 6 8 36 45 28 11 16 153 10 | 48 49 40 41 59 43 49 67 46
R23 | 1750 12 21 24 32 12 9 12 --- 7 | 19 23 24 30 18 13 21 --- 17
R24 | 1247 14 9 53 39 11 25 20 --- 12 | 58 59 33 50 53 66 54 --- 53
XR26 | ---- 9 70 --- --- --- --- 12 --- 10 | 32 62 --- --- --- --- 30 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1351 21 21 44 45 29 25 22 145 |T 50 54 41 42 60 50 54 75 48
WRMS | 1351 19 19 45 29 21 21 22 145 |NE 50 54 41 42 60 50 54 75 48
MEDI | 876 12 15 28 28 18 18 18 153 |MD 55 60 44 43 59 46 54 67 48
Table 3.2112.5 GPS week: 2112 Day: 5 MJD: 59033
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 | 794 46 53 51 82 23 25 16 --- 18 | 72 78 38 49 54 47 49 --- 49
R02 | 1458 10 12 19 33 10 9 11 115 6 | 50 49 40 34 50 42 40 61 43
R03 | 913 11 11 18 30 15 30 20 83 9 | 56 56 51 41 58 72 42 64 52
XR04 | 554 25 26 21 33 --- 15 20 --- 11 | 56 57 50 41 --- 50 56 --- 50
R05 | 596 9 10 20 16 11 10 13 --- 5 | 41 41 27 35 33 29 38 --- 34
R07 | 1685 10 15 21 37 15 8 11 148 7 | 54 53 49 35 62 51 54 22 52
R08 | 867 9 11 19 29 10 9 17 --- 6 | 51 53 46 33 47 51 56 --- 48
R09 | 2808 15 18 19 17 23 14 16 --- 7 | 26 29 32 36 29 28 35 --- 27
R11 | 726 11 15 16 11 10 8 11 170 5 | 48 51 39 42 46 37 37 108 40
R12 | 1235 15 12 22 25 16 18 14 --- 8 | 50 49 39 38 50 31 45 --- 41
R13 | 2021 32 45 61 62 67 23 20 --- 19 | 59 66 45 51 92 52 60 --- 55
R14 | 658 10 13 33 10 21 20 26 --- 9 | 45 46 37 44 63 35 59 --- 46
R15 | 801 10 11 27 32 27 9 13 --- 8 | 50 50 48 42 68 55 53 --- 52
R16 | 910 32 31 51 26 40 27 28 --- 15 | 48 57 42 52 88 77 82 --- 66
R17 | 1124 10 12 38 33 14 7 31 --- 10 | 28 30 19 30 32 23 42 --- 28
R18 | 694 9 14 22 22 10 14 11 --- 6 | 21 25 20 24 26 22 22 --- 20
R19 | 603 46 41 98 95 54 41 31 --- 25 | 48 49 62 45 63 31 48 --- 40
R20 | 2028 28 31 120 113 60 55 29 --- 28 | 57 57 60 42 75 46 49 --- 52
R21 | 1262 8 10 38 43 10 19 16 104 9 | 39 42 38 38 40 40 33 48 37
R23 | 2389 14 10 28 20 10 14 12 --- 7 | 19 21 27 29 25 22 16 --- 17
R24 | 1099 10 13 63 50 13 22 19 --- 13 | 52 53 42 42 43 44 49 --- 44
XR26 | ---- 17 66 --- --- --- --- 16 --- 17 | 35 88 --- --- --- --- 31 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1382 21 23 48 48 29 22 19 128 |T 45 50 40 39 52 42 45 60 41
WRMS | 1382 16 18 48 36 18 19 19 128 |NE 45 50 40 39 52 42 45 60 41
MEDI | 913 11 13 27 32 15 15 16 115 |MD 48 50 40 41 50 42 45 61 43
Table 3.2112.6 GPS week: 2112 Day: 6 MJD: 59034
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 | 637 42 45 53 83 41 32 41 --- 24 | 107 107 52 49 94 70 87 --- 73
R02 | 2439 8 12 21 28 20 16 29 114 9 | 66 70 50 44 73 67 77 33 61
R03 | 596 12 15 22 32 17 12 14 83 9 | 71 75 62 52 80 77 73 50 69
XR04 | 515 17 12 29 29 --- 10 14 --- 12 | 70 69 61 41 --- 60 68 --- 59
R05 | 618 14 11 27 33 28 14 34 --- 11 | 56 53 38 36 59 50 65 --- 47
R07 | 1922 6 8 27 26 24 14 18 148 9 | 74 76 60 50 92 80 71 55 74
R08 | 622 7 10 35 28 29 19 14 --- 11 | 75 77 55 54 91 86 78 --- 73
R09 | 2576 8 11 15 17 14 13 18 --- 6 | 31 31 37 40 36 34 36 --- 32
R11 | 1037 10 10 19 10 10 11 24 171 6 | 67 66 48 67 65 50 66 125 59
R12 | 859 14 16 21 13 12 13 17 --- 7 | 63 67 44 47 61 45 58 --- 53
R13 | 3926 29 25 36 44 54 48 34 --- 21 | 82 74 44 43 90 50 78 --- 60
R14 | 531 12 12 20 14 14 9 26 --- 6 | 56 57 41 54 57 44 69 --- 52
R15 | 805 13 11 19 16 9 15 25 --- 7 | 67 65 52 54 63 53 64 --- 58
R16 | 1009 12 20 37 25 35 18 30 --- 12 | 65 64 49 84 104 88 102 --- 79
R17 | 813 8 11 38 38 29 21 20 --- 13 | 53 54 35 38 66 61 60 --- 51
R18 | 995 12 16 23 12 18 10 26 --- 7 | 38 38 31 41 47 46 45 --- 38
R19 | 621 42 54 75 56 41 24 55 --- 23 | 88 90 47 52 92 76 93 --- 73
R20 | 913 40 36 109 111 33 67 53 --- 35 | 112 118 89 49 122 128 122 --- 98
R21 | 1731 9 13 38 29 19 23 28 120 11 | 63 64 43 43 67 65 71 36 58
R23 | 1551 9 19 20 33 10 7 14 --- 8 | 29 29 25 47 32 26 31 --- 28
R24 | 2336 17 27 61 39 44 12 27 --- 17 | 78 83 54 60 90 74 75 --- 70
XR26 | ---- 3 119 --- --- --- --- 30 --- 0 | 54 116 --- --- --- --- 42 --- 52
------+---------------------------------------------------+-----------------------------------------------
RMS | 1592 20 23 42 42 28 24 30 131 |T 66 70 48 49 74 63 69 59 59
WRMS | 1592 14 17 43 34 18 19 30 131 |NE 66 70 48 49 74 63 69 59 59
MEDI | 913 12 13 27 29 20 14 26 120 |MD 66 67 48 49 67 61 69 50 59
More information about the IGSREPORT
mailing list