[IGSREPORT-27207] Wk 2099 IGLOS Final Orbits
acc
acc at igs.org
Tue Apr 21 20:14:33 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2099 (Mar 29, 2020 - Apr 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 2.2099.
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:
igl2099[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2099 in the SP3 format.
igl20997.sum Combination Report for GPS Week 2099.
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 | -3.0 ns
1 | -0.5 ns
2 | -1.5 ns
3 | -2.3 ns
4 | -1.8 ns
5 | -3.1 ns
6 | -1.1 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 1.2099, 1a.2099).
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 2.2099.0-6)
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 3.2099.0-6).
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 2099 summary. (Mar 29, 2020 - Apr 04, 2020)
Table 1.2099.a GPS week : 2099 MJD: 58937.0-58943.0
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 4 19 -2 53 .12 24 19 | 20185 606 3849 12800
| 1 1 1 25 14 11 .05 | 3578 711
cof n/a| 0 0 7 9 -3 47 .13 26 21 | 20185 595 3850 12804
| 1 0 1 35 19 39 .07 | 3581 711
emx n/a| 1 0 -10 7 46 13 .09 31 30 | -11162 815 2988 8133
| 1 1 1 69 51 32 .07 | 5692 977
esx n/a| 0 0 -7 18 -23 -67 .16 34 28 | 2369 2010 2991 9939
| 1 1 2 20 23 49 .05 | 8606 1011
gfz n/a| 0 -1 2 -8 -17 -93 .02 29 18 | 0 249 3019 7561
| 0 1 2 19 12 31 .05 | 0 1112
grg n/a| 1 0 0 -72 -2 58 -.34 28 21 | -2061 487 3000 7033
| 0 1 1 27 22 29 .04 | 636 979
iac n/a| -2 0 4 34 0 3 -.01 20 20 | -84 296 3890 13336
| 1 1 1 30 24 48 .03 | 2974 1438
Table 1.2099.b GPS week : 2099 MJD: 58937.0-58943.0
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 | 17 18 20 17 18 18 17 |
R02 | 7 7 7 7 6 7 6 |
R03 | 9 9 9 8 11 10 9 |
R04 | 12 13 11 10 11 13 13 |
R05 | 12 10 8 10 10 12 10 |
R07 | 8 9 9 9 8 7 7 |
R08 | 7 7 8 6 10 8 8 |
R09 | 6 7 8 9 9 8 6 |
R11 | 8 7 5 5 6 7 8 |
R12 | 6 7 8 8 8 6 8 |
R13 | 14 13 18 17 13 13 15 |
R14 | 6 8 7 7 7 6 7 |
R15 | 6 7 9 8 8 6 6 |
R16 | 12 16 16 14 14 14 17 |
R17 | 9 11 9 9 9 8 9 |
R18 | 7 9 8 7 8 8 7 |
R19 | 19 19 19 20 18 19 20 |
R20 | 25 25 22 25 23 28 31 |
R21 | 11 8 11 10 8 9 10 |
R22 | 9 10 10 9 9 8 10 |
R23 | 12 10 9 9 10 11 11 |
R24 | 16 17 19 19 17 19 16 |
R26 | 25 33 27 22 20 19 21 |
Table 1.2099.c GPS week : 2099 MJD: 58937.0-58943.0
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 2099 0 | 120 3 339 -562 59 2315 81.6 2015 2015 | -3043 0
brd 2099 1 | 24 129 172 -2375 -381 3988 82.7 1308 1308 | -497 0
brd 2099 2 | 8 73 293 -757 -1440 2242 81.3 1382 1382 | -1473 0
brd 2099 3 | -65 42 270 241 -1968 1740 81.3 1375 1375 | -2298 0
brd 2099 4 | -14 -66 318 -76 -474 1464 83.5 1300 1300 | -1796 0
brd 2099 5 | -55 45 255 -1704 535 325 82.9 1317 1317 | -3053 0
brd 2099 6 | -25 56 236 -798 -458 1868 82.5 1323 1323 | -1121 0
-------------+------------------------------------------------------------+----------------
brd 2099 mean| -1 40 269 -861 -589 1991 82.3 1431 1431 | -1897 0
brd 2099 sdev| 62 60 55 907 854 1101 .9 259 259 | 962 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 2.2099.0 GPS week: 2099 Day: 0 MJD: 58937
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 45 -28 45 .08 24 19 | 21129 385 4142 17351
cof n/a| 0 0 5 51 -34 45 .11 26 21 | 21124 381 4144 17366
emx n/a| 1 1 -9 -144 152 -13 .12 27 27 | -20246 86 2812 8041
esx n/a| -1 2 -10 61 -53 -114 .22 34 24 | -5875 2502 2819 9829
gfz n/a| 0 -2 1 20 -36 -97 .01 31 23 | 0 213 2823 7277
grg n/a| 2 1 0 -25 -39 35 -.41 28 23 | -3231 492 2807 6451
iac n/a| -2 0 5 14 -17 42 .00 17 17 | 2616 928 4333 18808
Table 2.2099.1 GPS week: 2099 Day: 1 MJD: 58938
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 45 -12 51 .04 22 16 | 16054 1326 3682 13416
cof n/a| 0 0 5 2 -17 60 .02 25 19 | 16055 1313 3677 13417
emx n/a| 1 -1 -12 35 50 50 .01 31 31 | -6662 1866 2858 8201
esx n/a| 0 -1 -5 20 -17 27 .18 34 27 | -3549 2834 2856 10280
gfz n/a| 0 0 5 -30 -32 -51 .02 26 18 | 0 959 2892 7266
grg n/a| 3 1 2 -91 22 62 -.33 32 25 | -1346 1635 2876 6980
iac n/a| 0 0 6 4 40 -54 .01 20 20 | -1950 1115 3582 12636
Table 2.2099.2 GPS week: 2099 Day: 2 MJD: 58939
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 4 10 15 33 .10 25 21 | 15247 915 4864 11396
cof n/a| -1 0 8 29 14 -21 .11 28 24 | 15232 933 4867 11402
emx n/a| 2 -1 -11 34 -8 -29 .07 31 30 | -12288 696 3335 8408
esx n/a| 0 0 -3 2 -56 -87 .11 34 28 | -4686 1387 3336 10367
gfz n/a| 0 -3 4 10 -11 -96 -.01 27 18 | 0 605 3377 8022
grg n/a| 1 0 1 -101 -14 108 -.35 28 23 | -1575 471 3352 7197
iac n/a| -2 1 2 52 27 62 -.02 21 21 | -3736 -1927 4698 10635
Table 2.2099.3 GPS week: 2099 Day: 3 MJD: 58940
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 5 -24 -2 59 .14 24 19 | 25824 469 4889 22854
cof n/a| 1 0 7 -60 20 100 .20 28 21 | 25823 474 4887 22855
emx n/a| 3 -1 -10 3 50 24 .09 30 30 | -14759 670 3011 8563
esx n/a| 2 0 -7 18 -5 -64 .08 35 31 | 7773 720 3013 10253
gfz n/a| 1 0 4 -22 -13 -52 .07 32 18 | 0 -1152 3035 8129
grg n/a| 1 0 -2 -73 25 85 -.38 29 22 | -1881 -742 3021 7443
iac n/a| -3 0 2 74 -19 -65 -.03 18 18 | 5004 -445 5204 25576
Table 2.2099.4 GPS week: 2099 Day: 4 MJD: 58941
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 5 19 5 54 .22 23 18 | 20540 921 3053 8025
cof n/a| 0 1 6 12 -13 81 .22 25 19 | 20557 881 3050 8025
emx n/a| 0 1 -8 61 23 15 .17 31 31 | -10851 1474 2960 7762
esx n/a| 0 -1 -12 1 -25 -118 .16 38 31 | 12509 1585 2971 9633
gfz n/a| 0 -1 0 -11 -12 -98 .07 24 16 | 0 337 3014 7221
grg n/a| 0 0 -1 -56 -5 40 -.34 22 17 | -2025 640 2974 7208
iac n/a| -4 0 4 65 -24 -6 -.06 24 24 | -942 -559 3039 8266
Table 2.2099.5 GPS week: 2099 Day: 5 MJD: 58942
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 5 3 -7 68 .12 26 20 | 20869 -826 2923 8087
cof n/a| 0 0 6 0 0 42 .08 26 21 | 20879 -846 2922 8088
emx n/a| 2 0 -10 33 44 57 .15 32 30 | -2371 -841 2788 8117
esx n/a| 0 1 -9 15 -13 -57 .16 33 27 | 13679 1414 2790 9796
gfz n/a| 1 0 0 -27 -12 -131 -.07 32 17 | 0 -1155 2823 7749
grg n/a| 0 -1 0 -59 -8 27 -.32 24 18 | -2540 -747 2798 7264
iac n/a| 0 -2 6 30 0 10 .00 19 19 | -1610 406 2926 8356
Table 2.2099.6 GPS week: 2099 Day: 6 MJD: 58943
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 4 33 9 59 .13 24 19 | 21632 1058 3394 8477
cof n/a| -2 0 9 29 4 25 .15 25 20 | 21627 1032 3403 8481
emx n/a| -1 1 -10 27 9 -8 -.01 32 32 | -10963 1756 3158 7845
esx n/a| 0 1 -7 10 3 -58 .18 33 25 | -3266 3630 3152 9419
gfz n/a| 0 -2 1 0 -3 -123 .02 29 14 | 0 1937 3171 7266
grg n/a| 0 2 0 -99 2 50 -.28 32 22 | -1832 1662 3173 6694
iac n/a| 0 -1 7 -2 -3 35 .02 22 22 | 27 2558 3448 9075
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 3.2099.0 GPS week: 2099 Day: 0 MJD: 58937
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1217 37 28 38 68 41 33 20 17 | 100 106 67 73 111 87 81 80
R02 | 1807 12 20 17 14 25 9 7 6 | 60 66 48 56 63 54 58 55
R03 | 1210 11 11 24 38 15 16 17 9 | 80 80 61 47 78 82 82 72
XR04 | 1011 16 24 28 43 --- 21 15 12 | 94 96 84 76 --- 95 87 85
R05 | 1916 23 26 23 35 17 36 26 12 | 66 68 52 65 65 77 62 60
R07 | 945 16 14 21 28 11 22 12 8 | 85 86 69 56 81 84 72 74
R08 | 759 11 15 18 14 24 14 6 6 | 73 76 58 59 81 65 71 67
R09 | 1055 10 18 13 12 21 16 7 6 | 30 41 41 38 38 32 33 33
R11 | 1327 7 8 19 11 19 23 16 7 | 42 42 41 49 48 46 50 44
R12 | 1870 16 20 11 24 14 11 8 6 | 64 69 63 63 77 66 69 66
R13 | 6567 30 29 26 47 32 34 18 13 | 70 71 71 44 79 76 69 67
R14 | 1565 18 24 11 10 18 8 7 5 | 50 56 45 48 50 50 50 47
R15 | 851 10 16 8 19 7 23 10 6 | 70 72 62 58 63 70 65 64
R16 | 1406 15 22 25 29 29 43 14 11 | 50 56 60 54 56 76 61 57
R17 | 1712 15 20 28 14 25 17 13 8 | 89 91 80 84 89 76 84 82
R18 | 949 11 15 27 10 11 11 16 7 | 65 66 64 72 79 74 80 71
R19 | 2580 65 68 39 41 39 43 24 19 | 70 68 49 51 54 59 64 49
R20 | 1531 28 36 56 84 90 44 32 24 | 74 66 41 47 106 59 78 57
R21 | 761 11 10 35 27 37 12 14 10 | 79 77 55 55 91 62 81 70
R22 | 1832 18 17 27 24 13 12 18 8 | 131 135 109 111 128 114 131 122
R23 | 682 30 27 32 32 17 27 23 12 | 61 64 59 82 67 79 84 70
R24 | 1423 35 39 29 27 37 57 19 15 | 92 104 97 102 110 98 104 95
XR26 | 3350 32 49 --- --- --- --- 18 24 | 30 57 --- --- --- --- 54 38
------+----------------------------------------------+------------------------------------------
RMS | 2015 24 26 27 34 31 28 17 |T 70 74 62 63 76 71 72 66
WRMS | 2015 19 21 27 24 23 23 17 |NE 70 74 62 63 76 71 72 66
MEDI | 1406 16 20 25 27 21 21 16 |MD 70 69 60 56 78 74 71 67
Table 3.2099.1 GPS week: 2099 Day: 1 MJD: 58938
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 834 32 45 50 75 32 30 19 18 | 72 89 47 57 87 56 61 61
R02 | 949 9 11 18 14 16 17 16 6 | 47 47 39 48 39 36 53 43
R03 | 1192 9 13 28 36 14 22 15 9 | 53 56 39 36 54 62 58 50
XR04 | 1415 14 21 26 41 --- 23 22 12 | 64 66 54 57 --- 70 70 62
R05 | 1117 16 15 24 29 24 27 12 9 | 49 53 39 43 56 64 55 49
R07 | 787 20 21 19 36 15 17 14 9 | 59 61 44 37 58 57 45 49
R08 | 1240 11 15 17 26 12 22 10 7 | 51 56 43 38 50 58 53 48
R09 | 1206 7 10 21 6 18 23 17 7 | 24 27 29 31 30 21 29 24
R11 | 797 10 11 19 12 12 13 19 6 | 27 29 25 25 39 37 40 32
R12 | 1940 11 19 14 20 22 17 11 7 | 45 53 43 46 66 47 51 49
R13 | 1398 21 35 20 56 32 12 20 12 | 44 44 53 38 57 59 50 48
R14 | 1548 15 13 10 16 13 28 15 7 | 33 33 28 28 33 49 24 29
R15 | 803 14 18 9 25 13 21 12 7 | 45 47 41 34 38 50 51 42
R16 | 1072 25 25 43 29 33 64 13 15 | 50 71 65 57 47 47 48 47
R17 | 1142 21 13 29 31 17 29 17 10 | 60 62 54 62 64 52 59 56
R18 | 776 14 16 28 9 12 18 23 8 | 49 50 43 56 56 54 49 48
R19 | 2008 56 41 38 32 30 66 25 19 | 50 42 35 37 36 48 31 31
R20 | 1369 16 39 64 70 78 49 41 24 | 33 59 51 46 68 32 54 38
R21 | 784 12 12 30 27 14 11 13 8 | 46 46 35 31 46 46 51 43
R22 | 2070 21 25 25 20 12 32 19 9 | 107 111 95 101 101 90 103 99
R23 | 677 19 25 21 30 18 24 17 9 | 42 42 44 51 45 47 47 43
R24 | 2074 37 42 55 26 25 46 35 17 | 64 58 71 67 70 53 74 61
XR26 | 4027 35 73 --- --- --- --- 31 33 | 23 58 --- --- --- --- 38 22
------+----------------------------------------------+------------------------------------------
RMS | 1307 22 25 31 34 26 32 20 |T 49 54 46 46 54 51 51 46
WRMS | 1307 16 19 31 27 18 24 20 |NE 49 54 46 46 54 51 51 46
MEDI | 1192 16 19 24 27 17 23 17 |MD 49 53 43 43 54 50 51 48
Table 3.2099.2 GPS week: 2099 Day: 2 MJD: 58939
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1139 45 51 42 87 21 23 28 19 | 79 90 51 47 57 49 67 52
R02 | 902 11 14 21 14 11 17 17 7 | 49 53 39 52 53 49 54 47
R03 | 737 10 9 25 28 12 12 22 8 | 68 66 43 47 69 58 73 60
XR04 | 1568 18 17 21 31 --- 18 19 10 | 71 70 71 54 --- 59 71 65
R05 | 1335 19 15 23 16 16 17 19 8 | 54 53 36 45 41 36 54 43
R07 | 582 22 23 17 32 13 19 15 9 | 75 75 54 41 65 72 52 59
R08 | 500 16 14 18 23 21 14 13 8 | 59 60 43 47 57 42 39 46
R09 | 972 13 15 18 9 16 24 16 7 | 18 20 23 23 26 25 24 18
R11 | 1543 6 10 7 9 13 9 13 4 | 32 35 33 32 35 35 31 31
R12 | 969 16 11 19 25 17 19 16 8 | 52 46 49 45 46 36 45 42
R13 | 1064 22 38 25 46 42 62 33 18 | 67 90 73 48 79 53 82 67
R14 | 2834 9 20 17 17 14 14 18 6 | 41 48 32 37 46 37 47 39
R15 | 1961 20 21 7 27 17 22 16 8 | 49 50 44 41 43 44 49 44
R16 | 1097 38 39 39 34 25 52 16 15 | 38 39 44 50 42 56 48 42
R17 | 799 15 17 30 26 12 15 19 9 | 43 48 30 38 46 43 47 39
R18 | 546 12 14 22 13 9 26 12 7 | 38 40 33 36 36 51 40 37
R19 | 1907 60 58 43 39 38 34 33 19 | 64 65 36 26 54 22 34 25
R20 | 1648 30 43 60 56 74 34 30 22 | 32 34 39 35 73 25 41 29
R21 | 997 16 18 29 27 22 24 22 10 | 60 64 37 39 64 39 66 51
R22 | 2157 18 16 32 19 23 18 15 9 | 82 82 66 68 91 72 79 76
R23 | 1138 18 19 23 35 16 14 12 9 | 65 68 69 80 72 62 66 67
R24 | 1527 40 45 58 24 45 50 28 19 | 60 63 30 54 86 45 69 56
XR26 | 3755 29 45 --- --- --- --- 24 27 | 24 51 --- --- --- --- 32 24
------+----------------------------------------------+------------------------------------------
RMS | 1381 25 28 31 34 27 28 21 |T 53 56 44 44 56 45 52 46
WRMS | 1381 21 24 30 28 18 23 21 |NE 53 56 44 44 56 45 52 46
MEDI | 1138 18 18 23 26 17 19 18 |MD 54 53 39 45 54 44 49 44
Table 3.2099.3 GPS week: 2099 Day: 3 MJD: 58940
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 850 47 34 34 76 26 24 17 17 | 93 82 53 37 56 51 61 56
R02 | 881 8 11 25 20 15 22 8 7 | 52 57 33 34 59 60 48 47
R03 | 538 12 13 23 26 13 12 15 7 | 68 69 47 47 73 68 68 63
XR04 | 781 21 21 19 20 --- 14 19 9 | 63 64 42 46 --- 45 57 51
R05 | 2047 15 19 32 25 29 11 21 10 | 52 54 31 43 67 45 60 49
R07 | 546 15 16 21 30 24 17 9 8 | 74 77 55 44 90 71 64 66
R08 | 784 11 15 16 17 11 10 13 6 | 60 63 46 44 62 49 53 52
R09 | 1358 15 21 14 30 17 24 15 8 | 14 19 13 30 27 21 30 18
R11 | 1524 6 9 13 10 12 15 8 5 | 33 34 31 34 35 38 36 33
R12 | 878 13 20 26 22 17 21 12 8 | 48 62 40 45 61 62 60 52
R13 | 973 21 26 26 45 29 68 25 16 | 69 74 53 49 67 101 80 70
R14 | 2696 10 10 16 13 16 19 16 7 | 41 42 38 43 41 38 46 39
R15 | 2867 10 12 11 28 18 21 13 7 | 47 48 48 41 55 38 53 46
R16 | 1651 34 29 30 38 48 27 12 14 | 40 45 26 32 64 46 39 36
R17 | 912 17 16 29 21 8 16 20 8 | 56 55 39 39 53 39 54 47
R18 | 494 12 13 24 17 7 18 16 7 | 64 60 54 66 63 57 69 62
R19 | 889 53 72 48 60 43 31 28 19 | 75 98 40 42 76 40 49 47
R20 | 744 39 58 54 65 89 65 30 25 | 50 75 35 39 86 29 44 33
R21 | 1076 21 25 28 26 16 25 20 10 | 60 64 39 34 54 35 65 49
R22 | 1889 18 21 28 20 27 20 11 9 | 73 75 54 49 80 52 58 60
R23 | 717 18 21 18 35 21 15 9 8 | 63 66 67 79 64 65 73 67
R24 | 1009 35 30 62 23 59 37 26 18 | 73 84 45 65 115 59 78 70
XR26 | 5318 26 61 --- --- --- --- 17 21 | 30 46 --- --- --- --- 39 33
------+----------------------------------------------+------------------------------------------
RMS | 1374 24 28 30 35 32 29 18 |T 56 61 42 44 64 50 55 49
WRMS | 1374 19 21 30 31 18 22 18 |NE 56 61 42 44 64 50 55 49
MEDI | 912 17 21 25 25 18 20 16 |MD 60 63 40 43 63 46 57 49
Table 3.2099.4 GPS week: 2099 Day: 4 MJD: 58941
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 665 43 48 38 89 19 24 26 18 | 90 97 61 39 61 70 54 61
R02 | 1621 16 16 20 16 8 9 14 6 | 59 61 47 48 50 50 50 50
R03 | 748 12 9 27 49 11 18 30 11 | 72 72 54 38 72 83 89 70
XR04 | 821 16 21 24 35 --- 12 24 11 | 79 77 69 59 --- 71 80 71
R05 | 1856 18 15 23 30 19 14 29 9 | 55 59 39 52 55 39 67 48
R07 | 470 11 12 20 31 21 11 12 8 | 76 73 61 48 83 69 78 71
R08 | 1205 12 20 30 24 28 13 24 10 | 60 57 49 51 88 60 81 66
R09 | 1901 18 17 15 18 24 21 21 9 | 21 25 25 31 41 23 33 24
R11 | 848 7 11 21 11 12 12 14 6 | 32 34 33 45 37 38 40 35
R12 | 718 17 14 16 27 10 19 20 8 | 58 59 54 46 53 40 56 50
R13 | 1155 17 31 26 41 27 34 25 12 | 71 80 59 57 81 65 69 69
R14 | 1126 10 18 18 26 14 12 20 7 | 50 55 40 43 48 54 53 47
R15 | 2241 6 11 13 30 13 17 22 7 | 57 59 53 50 59 70 67 60
R16 | 2133 17 34 34 43 37 29 16 13 | 52 63 84 68 86 60 66 67
R17 | 546 12 17 28 27 22 10 17 8 | 50 53 38 35 57 45 47 45
R18 | 684 13 11 27 10 10 15 23 7 | 61 63 58 60 69 66 75 64
R19 | 497 51 48 53 59 25 17 40 18 | 67 65 44 42 44 47 37 40
R20 | 647 43 40 58 67 62 46 34 23 | 63 60 49 33 72 35 58 39
R21 | 697 18 14 26 19 9 13 14 7 | 62 60 47 45 53 49 62 53
R22 | 2554 23 24 26 23 12 13 15 8 | 67 66 56 65 61 55 61 59
R23 | 650 20 21 31 27 16 20 24 10 | 72 74 69 83 78 70 92 76
R24 | 922 22 30 53 26 39 40 34 16 | 69 63 45 63 73 56 82 60
XR26 | 4829 19 45 --- --- --- --- 21 20 | 39 51 --- --- --- --- 48 42
------+----------------------------------------------+------------------------------------------
RMS | 1300 23 25 31 38 24 22 24 |T 60 62 51 50 62 55 62 55
WRMS | 1300 18 19 31 31 16 17 24 |NE 60 62 51 50 62 55 62 55
MEDI | 848 17 18 26 27 19 15 22 |MD 61 61 49 48 61 55 62 59
Table 3.2099.5 GPS week: 2099 Day: 5 MJD: 58942
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 700 41 41 34 82 24 26 14 17 | 92 93 54 41 73 81 69 66
R02 | 1460 17 20 24 11 14 11 13 6 | 52 55 38 40 46 50 37 43
R03 | 1503 20 22 18 40 23 13 17 10 | 64 65 47 43 69 48 56 53
XR04 | 1831 20 27 22 48 --- 17 18 13 | 72 77 69 68 --- 73 72 69
R05 | 1402 21 18 32 33 19 19 30 11 | 49 51 36 49 52 34 57 43
R07 | 673 12 13 20 29 12 10 13 7 | 65 68 60 53 68 62 67 62
R08 | 609 8 8 25 25 14 14 17 8 | 63 68 51 50 73 70 75 65
R09 | 2144 22 26 17 12 20 15 15 7 | 39 41 28 30 39 37 30 32
R11 | 640 9 12 17 13 16 20 12 6 | 32 36 32 32 26 43 33 31
R12 | 821 14 20 14 19 9 13 13 6 | 35 42 38 38 38 39 38 36
R13 | 2593 13 17 32 44 36 33 11 13 | 48 45 55 29 45 63 43 44
R14 | 759 15 15 12 10 16 13 15 6 | 40 40 33 38 34 34 46 37
R15 | 873 9 12 14 23 11 6 8 5 | 44 48 41 37 50 45 46 43
R16 | 1011 24 26 39 18 37 39 24 14 | 30 53 33 47 53 41 57 41
R17 | 728 18 17 28 20 16 10 9 7 | 42 41 29 32 34 42 34 34
R18 | 721 12 15 28 10 16 21 17 8 | 74 72 66 70 76 86 72 74
R19 | 471 62 54 53 26 26 38 31 18 | 39 40 41 37 41 33 41 31
R20 | 845 52 59 60 65 104 60 28 28 | 50 61 37 38 73 37 45 32
R21 | 484 20 23 27 22 18 16 19 9 | 47 48 35 31 42 37 44 37
R22 | 3091 20 24 26 20 14 11 9 7 | 72 75 62 58 72 70 64 66
R23 | 605 24 16 26 22 20 20 28 10 | 125 123 125 129 125 114 130 124
R24 | 1358 35 24 64 35 54 28 32 18 | 48 58 32 64 94 71 81 61
XR26 | 3692 22 46 --- --- --- --- 15 18 | 40 56 --- --- --- --- 47 43
------+----------------------------------------------+------------------------------------------
RMS | 1317 26 26 32 33 32 24 19 |T 54 58 47 47 58 55 55 50
WRMS | 1317 20 21 30 27 17 18 19 |NE 54 58 47 47 58 55 55 50
MEDI | 845 20 20 26 22 18 16 15 |MD 48 55 38 40 52 45 47 43
Table 3.2099.6 GPS week: 2099 Day: 6 MJD: 58943
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1177 40 51 30 78 18 18 21 17 | 107 116 72 41 75 75 84 74
R02 | 955 10 12 19 10 13 12 13 6 | 64 68 46 55 66 62 57 58
R03 | 1411 17 20 15 26 13 24 19 8 | 81 85 61 59 79 85 69 71
XR04 | 2336 20 14 25 43 --- 21 15 12 | 97 95 84 82 --- 97 95 89
R05 | 721 19 21 23 32 16 19 27 10 | 64 66 42 56 61 48 74 57
R07 | 1054 14 14 18 21 17 13 13 7 | 84 85 69 65 91 82 86 80
R08 | 875 9 11 20 23 14 19 20 8 | 79 80 60 60 73 82 83 72
R09 | 2180 14 15 14 11 12 11 9 5 | 31 31 30 30 32 37 30 29
R11 | 1208 8 9 18 17 11 21 21 7 | 40 38 35 37 41 42 47 39
R12 | 918 17 17 16 22 19 20 16 8 | 60 63 66 55 70 62 59 60
R13 | 1981 20 18 32 36 32 59 15 15 | 70 76 76 49 75 78 80 70
R14 | 1590 12 12 14 20 11 17 12 6 | 57 56 42 44 48 46 51 48
R15 | 550 13 10 10 22 13 11 12 6 | 71 68 62 51 60 66 66 63
R16 | 602 24 31 47 35 13 66 23 16 | 50 51 50 56 67 84 74 62
R17 | 1213 15 14 28 23 14 19 19 9 | 65 64 41 42 62 46 60 53
R18 | 1132 10 11 22 12 14 16 17 7 | 82 84 73 83 83 85 92 83
R19 | 764 56 54 49 25 38 51 43 20 | 68 68 34 30 32 39 56 28
R20 | 600 44 38 80 74 99 73 33 31 | 74 74 30 49 114 40 64 50
R21 | 546 15 15 29 23 24 19 20 9 | 63 64 40 39 63 42 55 51
R22 | 3127 24 27 32 23 14 11 17 9 | 93 95 67 67 86 76 77 78
R23 | 609 21 32 30 33 20 16 25 11 | 131 129 124 142 127 118 134 128
R24 | 1306 35 30 46 23 42 25 31 15 | 76 80 47 89 119 86 96 83
XR26 | 3066 23 38 --- --- --- --- 19 21 | 47 39 --- --- --- --- 68 56
------+----------------------------------------------+------------------------------------------
RMS | 1322 24 25 32 33 29 32 22 |T 71 72 56 58 72 67 72 64
WRMS | 1322 19 20 32 25 14 22 22 |NE 71 72 56 58 72 67 72 64
MEDI | 1132 17 17 23 23 14 19 19 |MD 70 68 50 55 70 66 69 62
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