[IGSREPORT-30193] Wk 2339 IGLOS Final Orbits
acc
acc at igs.org
Thu Nov 28 04:49:53 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2339 (Nov 03, 2024 - Nov 09, 2024)
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 2.2339.
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:
igl2339[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2339 in the SP3 format.
igl23397.sum Combination Report for GPS Week 2339.
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.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 | 7.8 ns
1 | 5.4 ns
2 | 6.1 ns
3 | 5.6 ns
4 | 5.4 ns
5 | 8.4 ns
6 | 6.4 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 | BKG | R26
1 | COD | R26
1 | COF | R26
1 | EMR | R26
1 | ESA | R26
1 | GFZ | R26
1 | GRG | R26
1 | IAC | R26
1 | JGX | R26
1 | MCC | R26
2 | BKG | R26
2 | COD | R26
2 | COF | R26
2 | EMR | R26
2 | ESA | R26
2 | GFZ | R26
2 | GRG | R26
2 | IAC | R26
2 | JGX | R26
2 | MCC | R26
4 | GRG | R26
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 1.2339, 1a.2339).
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 2.2339.0-6)
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 3.2339.0-6).
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 2339 summary. (Nov 03, 2024 - Nov 09, 2024)
Table 1.2339.a GPS week : 2339 MJD: 60617.0-60623.0
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| -2 0 0 8 -11 59 .16 22 19 | 2173 -240 3345 8524
| 0 0 1 6 18 29 .04 | 1630 1024
esa n/a| 0 0 0 -34 19 -11 -.10 24 20 | 9593 -451 3250 7483
| 1 0 1 12 10 20 .03 | 5742 1214
gfz n/a| 1 0 0 24 18 -5 .03 19 15 | 0 -484 3249 7548
| 1 1 2 12 18 39 .05 | 0 1364
grg n/a| 0 -1 3 -14 -17 -20 .29 29 19 | 6372 -377 3259 7071
| 2 1 4 19 9 38 .04 | 1225 1154
iac n/a| 0 0 -5 13 7 -21 -.13 17 16 | 9078 -170 3343 8890
| 2 1 3 22 18 55 .04 | 1718 441
jgx n/a| 0 0 5 -8 -23 25 -.15 24 23 | 3873 -314 3317 7833
| 1 1 2 16 14 32 .03 | 1448 1186
Table 1.2339.b GPS week : 2339 MJD: 60617.0-60623.0
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 | 13 14 14 16 13 15 14 |
R02 | 7 5 7 7 7 6 7 |
R03 | 8 4 6 6 6 8 7 |
R04 | 6 7 5 9 8 9 9 |
R05 | 8 6 10 8 7 9 6 |
R07 | 5 6 6 6 5 7 8 |
R08 | 5 7 8 7 6 7 7 |
R09 | 8 10 7 6 9 7 6 |
R11 | 7 6 7 8 7 7 6 |
R12 | 9 9 15 9 7 7 8 |
R14 | 7 11 14 7 7 7 7 |
R15 | 10 8 15 9 7 9 7 |
R16 | 7 9 13 10 8 8 7 |
R17 | 7 6 6 7 6 7 6 |
R18 | 8 9 9 8 8 6 6 |
R19 | 23 23 26 21 20 22 22 |
R20 | 15 18 21 18 21 19 17 |
R21 | 7 7 6 8 8 7 6 |
R22 | 6 7 5 7 7 6 6 |
R24 | 8 6 8 6 6 7 9 |
R26 | 51 --- --- 179 228 704 1434 |
Table 1.2339.c GPS week : 2339 MJD: 60617.0-60623.0
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 2339 0 | -12 -27 -99 -82 1045 -3108 79.7 2216 2216 | 7773 0
brd 2339 1 | -31 10 -64 -91 125 -11020 80.0 1954 1954 | 5407 0
brd 2339 2 | 44 -43 -99 1158 -66 -9274 80.5 1814 1814 | 6135 0
brd 2339 3 | -16 52 17 1970 -438 -8627 80.6 1564 1564 | 5594 0
brd 2339 4 | 109 69 -30 1360 3440 -5511 79.3 1698 1698 | 5375 0
brd 2339 5 | -43 93 40 935 734 -4511 79.6 1513 1513 | 8360 0
brd 2339 6 | -12 -12 7 -217 240 -4486 82.5 1392 1392 | 6352 0
-------------+------------------------------------------------------------+----------------
brd 2339 mean| 5 20 -32 718 725 -6648 80.3 1735 1735 | 6428 0
brd 2339 sdev| 53 52 57 855 1294 2971 1.1 283 283 | 1188 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 2.2339.0 GPS week: 2339 Day: 0 MJD: 60617
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 0 2 -40 86 .09 25 20 | 4075 934 3288 7272
esa n/a| 2 1 -1 -21 30 -50 -.10 24 21 | 6198 426 3297 7031
gfz n/a| 2 0 3 30 -1 -38 .14 20 14 | 0 365 3305 7233
grg n/a| 0 0 0 -13 -21 -29 .36 24 22 | 7396 393 3342 6671
iac n/a| 2 0 -4 3 43 21 -.16 14 14 | 11256 -31 3290 7642
jgx n/a| -2 -1 0 2 -17 36 -.19 24 22 | 4289 1171 3240 7326
Table 2.2339.1 GPS week: 2339 Day: 1 MJD: 60618
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 0 21 -25 61 .21 26 18 | 1108 420 3430 7367
esa n/a| 2 1 0 -50 28 14 -.10 21 17 | 11512 621 3412 7044
gfz n/a| 1 -1 0 19 27 26 .01 19 15 | 0 684 3407 7302
grg n/a| 0 -2 0 -5 -15 -76 .29 26 17 | 4705 676 3398 7132
iac n/a| 0 0 -4 12 7 -50 -.15 17 16 | 7483 -232 3406 7689
jgx n/a| -3 -3 3 -5 -20 29 -.12 27 24 | 2322 651 3438 7416
Table 2.2339.2 GPS week: 2339 Day: 2 MJD: 60619
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 6 -10 63 .18 20 16 | 4147 -249 2875 7800
esa n/a| 0 0 0 -18 9 2 -.09 19 17 | 8623 -581 2872 6463
gfz n/a| 1 0 -1 48 8 10 .03 19 16 | 0 138 2881 7618
grg n/a| -4 0 9 -17 -8 47 .24 45 22 | 5898 62 2894 7174
iac n/a| 1 -3 -10 -16 11 -74 -.11 21 20 | 9670 -210 2878 8237
jgx n/a| 0 0 6 13 -12 -43 -.12 24 24 | 5539 -32 2901 8102
Table 2.2339.3 GPS week: 2339 Day: 3 MJD: 60620
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 -1 7 8 76 .21 24 24 | 1057 -1858 3653 14275
esa n/a| 1 0 -2 -47 12 -3 -.04 28 19 | 20651 -2798 3031 8470
gfz n/a| 0 0 0 25 -5 -2 -.03 16 13 | 0 -3031 3017 7986
grg n/a| 3 -4 -2 11 -13 -10 .28 30 21 | 6705 -2540 3042 7649
iac n/a| -2 0 -1 -1 2 -55 -.17 19 17 | 7143 -866 3673 14354
jgx n/a| 0 1 9 -8 -7 57 -.12 26 24 | 4989 -2270 3089 8521
Table 2.2339.4 GPS week: 2339 Day: 4 MJD: 60621
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 0 7 -1 -3 .18 19 16 | 38 300 3708 7439
esa n/a| 0 0 -1 -34 27 -18 -.14 29 22 | 2251 20 3697 9143
gfz n/a| 3 2 -1 22 43 -27 -.01 21 17 | 0 83 3685 7359
grg n/a| -1 0 4 -9 -34 -50 .33 27 17 | 5063 257 3659 6690
iac n/a| 2 0 -1 14 6 64 -.13 15 12 | 7584 632 3702 7817
jgx n/a| -1 1 8 -36 -36 37 -.15 25 25 | 1934 105 3789 7542
Table 2.2339.5 GPS week: 2339 Day: 5 MJD: 60622
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 2 4 -17 75 .13 20 19 | 3231 188 3171 7954
esa n/a| 0 0 -1 -42 27 -16 -.14 26 26 | 10501 344 3148 7290
gfz n/a| 2 0 2 11 29 -60 .04 18 13 | 0 101 3156 7889
grg n/a| 0 0 4 -13 -18 -21 .26 27 18 | 8106 -133 3178 7292
iac n/a| -1 0 -9 32 -15 19 -.06 17 16 | 11087 -305 3165 8452
jgx n/a| 0 0 4 -1 -49 19 -.18 23 22 | 5065 -409 3432 8185
Table 2.2339.6 GPS week: 2339 Day: 6 MJD: 60623
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 0 11 8 59 .15 20 17 | 1556 -1417 3295 7563
esa n/a| -1 0 0 -26 4 -8 -.11 25 20 | 7421 -1191 3294 6942
gfz n/a| 0 1 -3 11 25 52 .02 17 13 | 0 -1730 3293 7450
grg n/a| 1 0 7 -52 -8 -3 .25 24 16 | 6733 -1357 3305 6893
iac n/a| 3 -1 -7 51 -2 -74 -.14 18 17 | 9328 -184 3287 8045
jgx n/a| 0 0 5 -22 -19 44 -.18 23 23 | 2974 -1416 3335 7744
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 3.2339.0 GPS week: 2339 Day: 0 MJD: 60617
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1147 40 27 18 35 15 41 13 | 93 51 76 56 73 53 66
R02 | 3827 11 19 21 13 15 10 7 | 71 87 87 72 70 71 75
R03 | 487 10 19 22 19 8 24 7 | 62 66 69 65 65 50 62
R04 | 533 16 19 8 17 8 13 6 | 71 65 67 69 68 57 65
XR05 | 707 11 18 17 12 19 --- 8 | 63 75 69 65 57 --- 63
R07 | 903 9 11 10 9 7 16 4 | 85 83 83 80 85 72 81
R08 | 1468 9 9 10 11 11 13 5 | 74 79 73 77 75 74 74
R09E | 1687 13 10 16 34 16 10 8 | 37 43 50 46 44 42 41
R11E | 4520 16 12 18 13 11 15 6 | 38 39 48 35 40 36 38
R12E | 2526 16 17 25 19 16 20 8 | 222 225 222 216 216 219 219
R14E | 1345 13 13 15 16 15 21 7 | 279 273 280 279 273 277 277
R15E | 1102 14 18 21 23 26 27 10 | 180 182 189 189 173 178 181
R16E | 1246 19 12 10 18 17 17 7 | 62 64 58 66 69 61 62
R17 | 2087 17 11 12 12 12 26 7 | 36 37 31 36 38 25 33
R18 | 548 16 25 12 12 14 23 7 | 37 47 39 36 40 31 37
R19 | 1691 69 53 46 66 20 53 22 | 62 36 67 58 54 43 49
R20 | 4564 41 54 26 34 14 24 14 | 68 45 54 56 58 50 51
R21 | 801 14 23 16 14 8 20 7 | 35 31 30 38 28 25 29
R22 | 2977 15 13 16 10 10 12 5 | 110 112 114 112 111 112 111
R24 | 1314 27 15 20 14 11 15 7 | 38 49 43 38 35 33 37
XR26 |11852 95 --- --- 43 69 --- 50 | 216 --- --- 44 109 --- 153
------+-----------------------------------------+-------------------------------------
RMS | 2216 25 24 20 24 14 24 |T 92 84 87 82 84 79 85
WRMS | 2216 20 21 14 22 14 22 |NE 74 61 64 60 64 53 65
MEDI | 1345 16 17 16 16 14 20 |MD 68 64 67 65 68 53 63
Table 3.2339.1 GPS week: 2339 Day: 1 MJD: 60618
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 909 44 21 25 24 10 59 14 | 62 37 63 42 41 22 43
R02 | 2047 8 17 8 7 9 13 5 | 54 66 59 59 52 53 57
R03 | 830 12 7 10 8 6 12 4 | 41 37 41 39 36 33 37
R04 | 853 10 13 16 11 11 26 6 | 43 51 44 45 41 30 41
XR05 | 744 10 13 13 9 8 --- 5 | 39 47 44 47 45 --- 43
R07 | 1356 9 13 13 17 12 14 5 | 58 62 58 49 58 46 55
R08 | 1517 11 7 16 10 21 10 6 | 47 50 42 52 60 45 49
R09E | 1059 15 16 23 32 18 21 9 | 27 38 45 51 38 23 33
R11E | 2508 14 10 14 14 13 15 6 | 50 49 55 48 54 41 49
R12E | 2190 13 12 20 19 25 22 8 | 214 212 219 216 215 213 214
R14E | 1480 18 13 20 43 23 15 10 | 230 234 238 248 235 232 235
R15E | 1008 19 17 14 18 18 22 8 | 156 149 159 154 154 151 153
R16E | 747 20 20 30 17 15 15 9 | 91 93 105 91 87 87 91
R17 | 1701 13 11 13 10 12 20 6 | 32 33 30 29 30 22 27
R18 | 946 22 26 10 12 17 22 8 | 30 39 36 31 33 36 33
R19 | 2479 71 50 21 74 24 55 22 | 39 65 50 39 48 37 42
R20 | 5371 47 42 42 36 36 43 18 | 35 38 42 61 25 53 30
R21 | 979 10 20 14 16 11 16 6 | 30 31 34 36 26 30 29
R22 | 2075 16 13 14 25 8 18 7 | 85 92 91 84 83 92 87
R24 | 1386 20 11 10 7 11 18 5 | 33 33 29 37 31 27 30
------+-----------------------------------------+-------------------------------------
RMS | 1954 26 21 19 26 17 27 |T 76 72 74 72 70 67 68
WRMS | 1954 18 17 15 17 16 24 |NE 55 48 47 47 46 40 43
MEDI | 1356 14 13 14 16 12 18 |MD 47 49 45 49 48 41 43
Table 3.2339.2 GPS week: 2339 Day: 2 MJD: 60619
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 700 37 19 21 37 14 52 14 | 73 47 64 56 57 37 54
R02 | 979 11 16 15 16 7 24 7 | 61 58 64 55 57 46 56
R03 | 571 8 16 11 19 12 10 5 | 52 44 57 60 58 52 52
R04 | 1525 10 6 10 15 17 10 5 | 51 46 49 43 53 49 48
XR05 | 861 19 27 19 16 11 --- 10 | 33 55 35 43 43 --- 38
R07 | 1607 12 8 9 22 11 17 5 | 72 66 70 58 69 60 66
R08 | 981 14 20 18 16 13 15 7 | 64 80 59 61 75 65 67
R09E | 1665 17 10 18 18 16 13 7 | 28 42 50 36 40 35 38
R11E | 1837 11 13 12 35 17 13 7 | 43 46 47 33 53 38 42
R12E | 974 16 13 20 97 30 30 15 | 183 187 193 151 195 173 182
R14E | 1616 24 22 13 74 37 26 14 | 252 246 244 258 228 242 243
R15E | 1488 18 18 32 69 32 35 14 | 212 223 222 247 198 208 215
R16E | 1260 22 19 17 73 20 26 12 | 109 103 105 154 100 90 104
R17 | 2710 10 12 8 15 17 19 6 | 25 33 26 29 32 23 26
R18 | 614 18 28 24 15 14 13 9 | 29 28 32 30 34 23 27
XR19 | 1992 72 55 16 81 22 --- 26 | 45 49 43 40 42 --- 38
R20 | 4747 49 47 44 73 43 35 21 | 47 59 56 38 41 42 39
R21 | 853 11 13 12 18 11 13 5 | 27 27 29 27 22 23 24
R22 | 2517 14 11 9 19 12 7 5 | 111 114 109 126 111 114 113
R24 | 868 15 8 16 13 11 30 7 | 26 31 37 31 27 26 27
------+-----------------------------------------+-------------------------------------
RMS | 1814 20 19 19 45 21 24 |T 80 79 79 82 77 74 74
WRMS | 1814 16 17 16 22 20 24 |NE 57 52 52 57 54 46 48
MEDI | 1260 15 16 16 19 14 17 |MD 52 49 56 55 57 46 48
Table 3.2339.3 GPS week: 2339 Day: 3 MJD: 60620
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1021 51 15 24 49 16 54 16 | 76 55 63 35 47 40 49
R02 | 837 9 26 10 12 19 16 7 | 47 58 46 46 42 43 44
R03 | 777 8 12 14 12 9 20 5 | 55 48 56 55 52 41 51
R04 | 1735 17 19 14 12 27 21 8 | 55 39 43 49 62 34 45
XR05 | 763 11 17 18 12 17 --- 8 | 37 49 39 43 45 --- 39
R07 | 883 14 10 13 11 16 13 6 | 60 56 50 51 49 50 51
R08 | 748 17 15 15 12 18 10 7 | 59 68 66 63 51 56 59
R09E | 2044 19 14 12 14 13 12 6 | 26 35 34 26 29 32 28
R11E | 2124 19 12 19 14 25 12 8 | 41 44 38 43 51 38 39
R12E | 1105 14 13 18 23 20 24 8 | 167 169 169 169 151 157 162
R14E | 1081 18 18 9 23 13 17 7 | 130 135 127 131 132 128 129
R15E | 1635 17 16 16 33 17 21 9 | 119 119 122 121 118 118 118
R16E | 1323 18 20 15 37 15 29 9 | 86 88 84 111 81 78 85
XR17 | 2127 13 9 12 14 18 --- 7 | 30 24 24 31 28 --- 25
R18 | 495 11 31 13 16 11 13 7 | 26 29 24 31 25 26 24
R19 | 870 46 69 21 75 18 46 20 | 37 43 53 43 42 39 39
R20 | 4140 36 59 22 48 44 34 18 | 56 55 48 62 58 48 44
R21 | 737 20 15 9 18 11 29 7 | 42 38 35 35 32 33 33
XR22 | 2362 16 22 8 8 15 --- 7 | 42 63 43 46 36 --- 44
R24 | 828 18 17 8 13 13 15 6 | 30 37 30 38 27 26 29
XR26 | 9978 208 --- --- --- 152 --- 178 | 263 --- --- --- 187 --- 156
------+-----------------------------------------+-------------------------------------
RMS | 1564 24 28 16 30 19 26 |T 70 62 59 61 64 58 61
WRMS | 1564 24 19 13 21 17 24 |NE 61 47 44 44 52 39 48
MEDI | 1081 17 16 14 14 17 20 |MD 55 49 46 46 49 41 44
Table 3.2339.4 GPS week: 2339 Day: 4 MJD: 60621
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 898 47 32 21 26 20 23 13 | 62 33 47 36 46 41 41
R02 | 1530 10 29 11 16 11 15 7 | 55 63 61 52 54 58 55
R03 | 776 10 7 16 13 8 21 5 | 47 47 57 53 50 35 48
R04 | 763 19 17 23 17 9 22 8 | 57 48 68 41 49 36 49
R05 | 931 12 15 20 8 14 22 7 | 33 36 51 37 40 9 35
R07 | 999 9 15 11 12 7 12 4 | 49 53 39 41 49 41 45
R08 | 719 12 21 15 14 9 11 6 | 45 54 46 42 47 47 45
R09E | 2185 18 18 18 16 19 21 8 | 28 39 46 25 38 43 35
R11E | 2199 14 12 23 16 9 19 7 | 28 36 47 30 32 27 32
R12E | 2236 17 15 10 21 15 18 7 | 170 169 168 160 165 163 166
R14E | 2084 9 21 12 18 13 19 6 | 204 192 202 201 192 196 197
R15E | 1199 13 12 19 14 14 22 7 | 169 169 169 181 166 168 169
R16E | 1257 14 19 18 16 19 19 8 | 77 77 83 80 60 65 71
XR17 | 1360 11 14 11 11 10 --- 5 | 35 36 36 35 37 --- 34
R18 | 692 13 25 19 12 7 32 8 | 35 37 43 33 34 30 33
R19 | 1154 15 67 25 62 33 65 20 | 42 45 56 52 60 38 44
R20 | 3923 39 73 49 75 13 30 21 | 51 53 49 68 52 59 47
R21 | 578 20 15 14 19 14 20 7 | 47 40 37 40 34 34 36
R22 | 2575 19 15 16 13 13 12 6 | 114 118 112 122 112 110 114
R24 | 1385 14 9 21 14 11 11 6 | 34 30 29 37 29 31 28
XR26 |11054 266 --- --- 683 194 --- 227 | 578 --- --- 682 296 --- 306
------+-----------------------------------------+-------------------------------------
RMS | 1698 19 29 21 27 15 25 |T 93 68 72 97 78 64 77
WRMS | 1698 16 22 17 17 12 25 |NE 85 49 52 91 65 43 64
MEDI | 1257 14 15 18 16 13 20 |MD 49 47 49 42 49 41 45
Table 3.2339.5 GPS week: 2339 Day: 5 MJD: 60622
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 826 47 30 19 29 18 44 14 | 68 39 49 47 51 42 47
R02 | 1340 11 12 10 9 15 15 5 | 55 55 55 50 54 51 52
R03 | 809 20 11 17 9 18 23 7 | 51 58 64 56 67 50 56
R04 | 881 19 16 13 11 24 27 8 | 61 46 50 46 65 40 51
XR05 | 765 15 13 26 11 16 --- 9 | 51 53 71 49 50 --- 54
R07 | 1017 13 15 13 18 16 11 6 | 52 48 47 42 50 52 47
R08 | 1020 13 13 19 6 21 9 7 | 47 51 42 46 55 45 46
R09E | 1531 15 12 13 17 14 13 6 | 28 40 44 26 38 35 34
R11E | 1130 14 15 11 11 18 12 6 | 29 38 34 33 37 29 31
R12E | 2646 13 10 11 19 8 23 6 | 146 144 144 141 145 140 143
R14E | 834 14 18 19 16 13 13 7 | 166 161 160 167 160 164 162
R15E | 798 17 12 21 25 19 24 9 | 142 139 144 151 148 144 144
R16E | 936 11 19 19 13 13 22 7 | 56 59 64 64 54 53 57
R17 | 1091 17 9 13 13 15 20 6 | 37 34 32 37 35 36 33
R18 | 634 8 19 11 12 13 18 6 | 39 41 35 38 40 32 36
R19 | 2038 33 65 34 74 27 51 21 | 48 39 55 45 45 52 45
R20 | 3402 31 67 39 61 21 20 18 | 40 48 71 61 37 54 48
R21 | 724 13 24 11 17 12 18 7 | 44 48 43 41 33 36 39
R22 | 2210 14 14 10 10 20 7 6 | 96 95 99 93 88 96 94
R24 | 1388 11 15 17 23 9 16 7 | 37 42 40 35 35 34 34
XR26 |12307 728 --- --- --- 680 --- 704 | 9999 --- --- --- 500 --- 405
------+-----------------------------------------+-------------------------------------
RMS | 1513 20 26 18 27 17 23 |T 64 63 67 63 85 62 78
WRMS | 1513 19 26 13 18 16 22 |NE 51 49 53 49 80 47 72
MEDI | 1020 14 15 13 13 16 18 |MD 51 48 50 46 51 50 48
Table 3.2339.6 GPS week: 2339 Day: 6 MJD: 60623
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 846 50 23 20 26 19 38 13 | 75 55 56 50 61 45 53
R02 | 1854 12 17 21 10 18 12 7 | 61 66 65 60 57 52 59
R03 | 1255 12 15 12 12 18 20 6 | 59 56 60 55 63 40 55
R04 | 786 17 9 4 18 24 37 9 | 70 54 56 53 71 50 58
XR05 | 854 13 9 11 10 12 --- 5 | 53 52 54 54 51 --- 52
R07 | 1156 8 16 15 14 16 29 7 | 66 61 69 61 71 53 63
R08 | 802 9 9 16 16 19 14 6 | 61 64 52 57 64 59 58
R09E | 1956 17 12 10 13 14 11 5 | 37 49 51 36 54 47 45
R11E | 1091 14 13 15 11 9 15 6 | 34 42 41 31 39 30 35
R12E | 2130 17 16 14 17 23 20 8 | 180 181 180 167 181 164 175
R14E | 937 13 17 11 23 9 16 6 | 187 182 187 191 185 186 186
R15E | 1213 11 9 12 18 20 22 7 | 166 161 164 173 163 162 164
R16E | 747 17 16 10 14 13 24 7 | 96 95 91 97 88 78 90
R17 | 777 12 9 10 13 18 21 6 | 47 48 42 45 45 39 44
R18 | 696 7 21 11 10 11 11 5 | 47 53 47 44 42 40 44
R19 | 1900 38 70 19 76 29 41 21 | 75 55 69 87 72 62 68
R20 | 2483 31 60 43 34 25 22 17 | 72 56 80 72 71 65 66
R21 | 670 10 14 14 12 12 16 6 | 56 48 50 54 51 46 50
R22 | 1719 15 8 10 12 18 14 6 | 126 125 128 122 114 121 122
R24 | 1320 17 20 23 19 16 21 8 | 44 49 45 46 42 34 41
XR26 |14461 1472 --- --- --- 1395 --- 1433 | 9999 --- --- --- 227 --- 9999
------+-----------------------------------------+-------------------------------------
RMS | 1392 20 25 17 24 18 23 |T 80 77 79 77 86 72 76
WRMS | 1392 17 20 13 16 17 23 |NE 65 60 62 61 73 54 59
MEDI | 1156 14 15 12 14 18 20 |MD 61 55 56 55 64 52 58
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