[IGSREPORT-30164] Wk 2337 IGLOS Final Orbits
acc
acc at igs.org
Thu Nov 7 23:56:30 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2337 (Oct 20, 2024 - Oct 26, 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 2.2337.
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:
igl2337[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2337 in the SP3 format.
igl23377.sum Combination Report for GPS Week 2337.
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 | 4.5 ns
1 | 7.2 ns
2 | 4.1 ns
3 | 8.1 ns
4 | 5.3 ns
5 | 3.4 ns
6 | 8.3 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 1.2337, 1a.2337).
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 2.2337.0-6)
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 3.2337.0-6).
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 2337 summary. (Oct 20, 2024 - Oct 26, 2024)
Table 1.2337.a GPS week : 2337 MJD: 60603.0-60609.0
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| -1 0 3 5 -5 42 .14 21 18 | -2344 -80 4085 16816
| 1 0 1 17 11 25 .02 | 1940 2560
esa n/a| 0 0 0 -41 0 15 -.01 25 19 | 6182 -766 3218 7355
| 0 1 1 17 10 33 .03 | 5206 3001
gfz n/a| 0 0 2 27 6 -3 .01 19 15 | 0 -468 3238 7734
| 1 1 1 11 12 50 .03 | 0 2777
grg n/a| 0 0 0 -7 -3 -50 .25 26 20 | 2683 -232 4122 16841
| 2 1 1 19 20 53 .04 | 1122 2518
iac n/a| 0 0 -9 7 4 -27 -.13 18 16 | 5793 -568 4059 16146
| 1 1 1 24 25 41 .05 | 1662 1606
jgx n/a| 0 0 4 -5 -9 24 -.25 25 24 | 2360 -571 3225 7798
| 1 1 1 17 20 27 .02 | 1437 2692
Table 1.2337.b GPS week : 2337 MJD: 60603.0-60609.0
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 | 14 15 12 15 13 15 13 |
R02 | 7 7 7 6 6 5 6 |
R03 | 8 7 6 7 7 6 7 |
R04 | 7 7 9 6 8 6 7 |
R05 | 7 5 7 8 7 7 7 |
R07 | 7 7 7 6 6 6 7 |
R08 | 6 7 6 6 6 8 6 |
R09 | 7 7 7 7 8 6 6 |
R11 | 6 7 5 8 7 6 7 |
R12 | 7 7 8 8 7 8 6 |
R14 | 7 7 7 7 8 6 9 |
R15 | 10 8 12 8 9 7 7 |
R16 | 9 11 12 9 9 8 9 |
R17 | 7 7 6 8 6 6 7 |
R18 | 8 9 9 8 8 8 8 |
R19 | 24 22 22 25 23 23 23 |
R20 | 17 20 20 18 21 20 14 |
R21 | 6 7 7 9 7 7 7 |
R22 | 6 6 8 9 8 6 7 |
R24 | 6 7 6 8 7 7 10 |
R25 | 10 15 12 182 0 29 10 |
R26 | 30 32 32 31 32 27 37 |
Table 1.2337.c GPS week : 2337 MJD: 60603.0-60609.0
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 2337 0 | -28 91 49 1308 -390 2853 82.8 2247 2247 | 4490 0
brd 2337 1 | 60 -94 3 464 -958 3317 80.6 2495 2495 | 7188 0
brd 2337 2 | 71 21 21 918 -843 1693 81.4 2135 2135 | 4137 0
brd 2337 3 | -6 56 31 -732 899 1678 81.1 1928 1928 | 8136 0
brd 2337 4 | 29 -130 60 1976 854 586 82.4 2223 2223 | 5283 0
brd 2337 5 | -1 -37 58 -773 -246 436 81.7 1996 1996 | 3409 0
brd 2337 6 | 121 112 60 -1816 1632 691 82.9 2276 2276 | 8267 0
-------------+------------------------------------------------------------+----------------
brd 2337 mean| 35 2 40 192 135 1607 81.9 2185 2185 | 5844 0
brd 2337 sdev| 52 92 22 1344 993 1135 .9 188 188 | 1996 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 2.2337.0 GPS week: 2337 Day: 0 MJD: 60603
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 34 -8 75 .14 24 20 | -4341 -3025 4183 16623
esa n/a| 0 0 -2 -58 -3 -7 .01 23 15 | 6690 -3283 3400 7713
gfz n/a| 0 2 0 41 19 30 -.02 16 14 | 0 -3634 3442 8328
grg n/a| -1 0 0 -32 -25 -122 .25 26 18 | 2546 -2692 4216 16539
iac n/a| 1 0 -8 35 7 -44 -.11 18 14 | 4358 -670 4120 15598
jgx n/a| -2 0 5 -37 -14 64 -.25 25 25 | 822 -3622 3450 8507
Table 2.2337.1 GPS week: 2337 Day: 1 MJD: 60604
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 4 -25 38 .12 21 19 | -4034 1445 4325 19307
esa n/a| 1 0 0 -37 -14 39 .04 24 17 | 7943 2913 3327 7518
gfz n/a| 0 0 3 28 16 -10 .04 19 14 | 0 2687 3414 7956
grg n/a| -1 0 0 10 -28 -23 .31 26 17 | 2552 1585 4453 19419
iac n/a| 1 0 -11 3 43 -47 -.19 19 18 | 6804 -1162 4295 18146
jgx n/a| -2 1 2 7 -6 -6 -.24 27 26 | 1224 2517 3403 8077
Table 2.2337.2 GPS week: 2337 Day: 2 MJD: 60605
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 2 -3 0 54 .15 19 17 | -3847 -2183 4443 19687
esa n/a| 0 0 0 -37 15 -22 -.00 28 20 | 1873 -3495 3100 7825
gfz n/a| 1 0 3 37 -2 -98 .03 19 15 | 0 -2506 3163 8206
grg n/a| 4 0 0 -14 -7 -13 .25 34 25 | 1356 -2291 4605 19790
iac n/a| -1 -1 -9 8 13 45 -.09 18 16 | 4401 -2446 4379 18571
jgx n/a| 0 -2 2 -10 13 18 -.22 22 22 | 2273 -2885 3079 8301
Table 2.2337.3 GPS week: 2337 Day: 3 MJD: 60606
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| -3 -1 1 0 -4 54 .19 20 16 | -759 1316 3999 17698
esa n/a| 0 0 -2 -26 11 75 -.02 27 17 | 11854 186 3035 8420
gfz n/a| 0 1 0 20 4 57 .00 19 16 | 0 104 3033 8369
grg n/a| 1 -2 2 -16 24 -104 .26 27 24 | 4269 1126 4001 17716
iac n/a| 0 0 -8 14 -42 -77 -.13 20 19 | 6999 40 3996 17162
jgx n/a| 0 -1 4 -11 15 11 -.25 23 23 | 3472 302 3054 8391
Table 2.2337.4 GPS week: 2337 Day: 4 MJD: 60607
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 1 4 -12 10 44 .14 20 17 | -1096 1888 4744 14098
esa n/a| -1 -1 1 -43 -6 -11 -.01 25 19 | -2093 -1008 4014 7207
gfz n/a| 0 0 1 25 6 24 .03 21 15 | 0 1176 4009 7942
grg n/a| 0 0 1 1 21 -73 .25 26 21 | 1788 2059 4560 12752
iac n/a| 3 -1 -8 0 7 -11 -.13 18 15 | 5746 1776 4730 13935
jgx n/a| 0 0 5 5 -29 28 -.26 26 24 | 2992 1027 4029 7986
Table 2.2337.5 GPS week: 2337 Day: 5 MJD: 60608
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 24 2 36 .14 18 18 | -2992 -3010 3780 16042
esa n/a| 0 -2 3 -68 1 17 -.02 26 22 | 4678 -3904 2800 6371
gfz n/a| 1 1 6 6 14 -9 -.03 22 16 | 0 -3644 2812 6786
grg n/a| -1 0 -2 -24 -1 28 .19 22 19 | 2127 -3615 3850 16361
iac n/a| 0 0 -9 28 2 -55 -.07 16 14 | 3899 -2439 3752 15320
jgx n/a| 0 -1 6 -6 -39 -3 -.29 27 24 | 1056 -3493 2760 6701
Table 2.2337.6 GPS week: 2337 Day: 6 MJD: 60609
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 3 -6 -9 -6 .12 22 17 | 655 3005 3123 14257
esa n/a| 0 0 1 -19 1 18 -.05 22 21 | 12330 3223 2852 6434
gfz n/a| 3 0 1 30 -15 -17 .03 17 17 | 0 2536 2796 6557
grg n/a| 0 -2 0 22 -9 -45 .25 23 17 | 4147 2201 3170 15316
iac n/a| 1 1 -12 -38 0 0 -.18 18 17 | 8348 925 3147 14296
jgx n/a| -2 0 4 16 -6 58 -.28 22 21 | 4685 2155 2805 6627
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 3.2337.0 GPS week: 2337 Day: 0 MJD: 60603
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 905 34 25 20 33 13 56 14 | 72 53 75 57 60 48 61
R02 | 765 11 20 11 12 14 22 7 | 40 52 47 42 49 29 43
R03 | 1591 13 19 10 22 16 21 7 | 52 52 51 63 58 44 52
R04 | 2412 12 12 10 13 22 18 7 | 47 47 54 43 61 41 49
R05 | 1062 14 19 16 11 14 16 6 | 36 48 42 41 43 32 38
R07 | 1221 17 14 16 18 11 17 7 | 61 63 65 53 58 50 57
R08 | 899 14 8 13 18 15 13 6 | 58 62 59 57 66 61 60
R09E | 1458 15 9 11 17 18 12 6 | 38 45 51 37 45 42 42
R11E | 1514 13 10 12 11 13 13 5 | 36 29 32 34 38 36 33
R12E | 1006 12 13 16 15 16 9 6 | 105 110 110 108 107 108 108
R14E | 1037 10 19 9 23 12 17 6 | 74 83 77 82 76 80 77
R15E | 4099 17 22 20 32 16 24 9 | 45 43 44 49 44 45 42
R16E | 5264 14 24 19 28 9 13 8 | 62 64 66 71 66 64 64
R17 | 796 19 11 15 11 14 12 6 | 61 52 59 57 52 49 54
R18 | 625 13 33 12 9 8 22 8 | 53 72 59 54 52 52 55
R19 | 1033 66 55 28 79 44 54 24 | 83 74 102 92 93 72 81
R20 | 4793 47 48 23 30 34 43 17 | 87 61 64 88 68 74 66
R21 | 558 12 12 12 15 10 12 5 | 80 72 77 76 69 67 73
R22 | 3230 14 12 13 22 9 11 6 | 37 42 50 54 37 39 42
R24 | 981 22 13 13 11 8 8 5 | 60 55 53 55 51 48 52
XR25 |17491 15 12 --- --- 12 --- 9 | 404 193 --- --- 491 --- 475
XR26 |31652 41 --- --- 34 47 --- 30 | 62 --- --- 49 80 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 2247 24 23 16 26 18 25 |T 75 65 61 60 80 54 76
WRMS | 2247 20 15 14 18 14 25 |NE 80 66 61 58 86 50 82
MEDI | 1062 14 14 13 18 14 16 |MD 60 55 59 55 58 48 55
Table 3.2337.1 GPS week: 2337 Day: 1 MJD: 60604
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 932 42 15 14 35 15 65 15 | 42 35 34 28 30 36 31
XR02 | 984 14 15 16 15 10 --- 7 | 31 37 38 24 24 --- 30
R03 | 1024 10 13 15 14 15 27 7 | 37 32 43 40 31 22 33
R04 | 1596 11 13 7 13 26 13 6 | 35 32 34 31 45 35 34
R05 | 780 11 14 8 11 12 11 5 | 24 27 26 24 23 22 21
R07 | 947 12 15 11 16 18 17 6 | 41 45 50 41 53 37 43
R08 | 774 15 15 19 13 11 11 6 | 45 41 35 39 41 42 39
R09E | 1310 16 8 15 14 17 12 6 | 24 28 34 28 27 28 27
R11E | 1978 18 7 19 12 14 9 6 | 33 23 30 25 36 27 27
R12E | 1246 13 16 9 15 19 16 6 | 89 90 91 91 86 91 89
R14E | 1149 10 15 11 13 18 18 6 | 53 56 52 58 49 60 52
R15E | 2892 12 19 11 26 17 20 8 | 58 53 60 57 63 61 56
R16E | 6150 15 29 34 24 21 18 11 | 59 64 63 55 60 62 56
R17 | 809 11 10 20 11 13 18 6 | 27 24 35 29 23 21 24
R18 | 638 15 30 12 15 20 21 8 | 29 35 29 39 27 26 27
R19 | 1458 42 61 34 73 25 59 22 | 41 47 47 38 34 29 35
R20 | 6237 47 55 38 52 37 31 19 | 43 49 45 51 39 39 35
R21 | 590 9 15 14 19 17 17 7 | 47 56 53 47 49 51 49
R22 | 3584 12 10 8 13 18 15 5 | 27 31 32 37 30 37 30
R24 | 1302 19 12 14 10 13 26 7 | 37 31 40 35 36 25 31
XR25 |14859 20 15 --- --- 25 --- 14 | 345 185 --- --- 387 --- 377
XR26 |45205 35 --- --- 33 58 --- 31 | 40 --- --- 40 52 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 2494 21 24 19 26 19 27 |T 54 48 43 40 56 39 53
WRMS | 2494 19 17 14 17 18 26 |NE 55 47 38 36 57 32 54
MEDI | 1246 14 15 14 15 17 18 |MD 40 37 38 39 36 36 34
Table 3.2337.2 GPS week: 2337 Day: 2 MJD: 60605
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1476 31 20 24 38 10 35 12 | 50 46 49 46 41 57 44
XR02 | 799 13 13 18 14 12 --- 7 | 24 26 28 19 21 --- 19
R03 | 1185 10 10 13 10 9 18 5 | 45 44 42 46 48 32 41
R04 | 849 9 15 27 11 6 30 8 | 44 32 58 40 37 25 38
R05 | 1229 12 20 13 22 14 13 6 | 22 32 33 45 27 28 26
R07 | 945 10 17 18 10 10 21 6 | 37 48 37 41 43 34 38
R08 | 759 9 16 11 13 12 13 5 | 41 38 48 41 36 40 39
R09E | 1385 17 7 15 15 16 15 6 | 24 25 31 24 28 28 24
R11E | 3204 13 12 12 10 10 9 5 | 20 23 23 20 19 20 18
R12E | 780 17 19 11 24 20 15 8 | 86 94 90 95 82 89 87
R14E | 1359 15 15 12 23 13 21 7 | 57 52 59 65 52 55 54
R15E | 1378 16 26 17 66 22 11 12 | 51 45 53 91 56 52 51
R16E | 3992 15 25 21 66 21 15 12 | 64 59 66 100 61 64 63
R17 | 651 14 14 10 17 12 15 6 | 40 34 34 39 34 29 33
R18 | 896 16 21 13 19 16 26 8 | 29 40 41 31 38 25 32
R19 | 2833 33 73 24 64 44 52 21 | 52 54 70 61 65 49 54
R20 | 3211 47 68 42 60 15 23 19 | 62 57 47 70 51 61 51
R21 | 1787 12 12 11 19 13 21 6 | 57 47 49 55 51 43 49
R22 | 4703 14 15 14 15 26 7 7 | 29 33 31 33 25 25 25
R24 | 1403 10 12 14 15 14 10 5 | 42 36 40 45 30 41 36
XR25 |12606 18 18 --- --- 12 --- 11 | 329 149 --- --- 468 --- 442
XR26 |47757 36 --- --- 46 52 --- 32 | 30 --- --- 16 52 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 2135 19 28 19 34 18 22 |T 56 48 46 48 62 41 58
WRMS | 2135 17 20 15 25 16 22 |NE 58 47 43 41 66 37 62
MEDI | 1378 14 16 14 19 13 15 |MD 42 44 42 45 41 40 38
Table 3.2337.3 GPS week: 2337 Day: 3 MJD: 60606
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 844 42 21 21 37 16 47 14 | 57 39 47 48 40 30 41
R02 | 862 14 18 11 10 15 9 6 | 36 44 35 38 40 36 35
R03 | 1520 11 13 11 21 22 7 6 | 48 47 44 45 63 52 48
R04 | 722 12 10 11 12 10 25 6 | 53 47 48 46 50 36 46
R05 | 1039 11 19 17 13 8 29 7 | 46 52 52 41 40 24 41
R07 | 1018 8 15 16 12 9 12 5 | 38 35 43 44 43 32 38
R08 | 851 13 13 16 14 10 9 6 | 41 46 42 39 37 40 39
R09E | 3942 16 12 18 18 19 11 7 | 25 32 35 28 36 32 29
R11E | 4699 18 7 14 15 30 16 8 | 28 22 24 25 32 23 22
R12E | 869 16 12 18 15 21 21 8 | 105 105 105 98 115 114 107
R14E | 1238 7 12 17 20 19 17 7 | 40 43 37 47 41 41 39
R15E | 1902 12 14 18 18 21 15 7 | 46 43 57 60 37 43 46
R16E | 845 15 15 17 32 18 12 8 | 54 54 62 58 50 54 52
R17 | 880 10 13 17 16 21 19 7 | 45 34 38 52 48 36 39
R18 | 754 13 19 12 17 13 27 7 | 34 44 38 35 33 35 34
R19 | 816 32 79 39 78 38 56 24 | 48 24 72 70 63 40 48
R20 | 2444 46 64 37 38 26 18 18 | 70 40 53 62 49 59 48
R21 | 1621 16 23 12 24 18 24 8 | 45 33 41 55 44 31 40
R22 | 3444 18 11 10 29 26 12 8 | 30 29 26 39 19 20 23
R24 | 713 15 21 16 16 16 20 7 | 34 40 30 33 42 29 32
XR25 |14061 172 --- --- --- 192 --- 182 | 201 --- --- --- 293 --- 171
XR26 |26472 33 --- --- 31 58 --- 30 | 24 --- --- 24 65 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1928 20 27 19 27 20 23 |T 52 42 46 47 58 40 47
WRMS | 1928 16 17 16 24 19 23 |NE 53 39 43 44 60 35 47
MEDI | 1018 15 14 16 18 19 17 |MD 45 40 42 45 42 36 39
Table 3.2337.4 GPS week: 2337 Day: 4 MJD: 60607
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1241 35 18 8 27 14 56 13 | 56 50 39 48 46 32 43
R02 | 613 9 16 12 11 12 10 5 | 29 37 34 31 30 28 30
R03 | 1128 13 14 17 11 13 17 6 | 45 48 52 44 49 37 45
R04 | 782 22 9 8 12 13 28 7 | 49 36 35 33 43 28 36
R05 | 881 13 16 13 13 10 28 7 | 47 46 44 42 45 25 41
R07 | 853 9 11 10 20 9 11 5 | 45 49 54 59 51 48 50
R08 | 1080 15 8 13 13 12 17 6 | 38 39 45 36 44 45 40
R09E | 4983 17 16 19 18 16 10 7 | 18 32 36 28 24 25 24
R11E | 6184 16 9 13 13 16 22 6 | 24 22 21 24 21 30 19
R12E | 571 14 16 15 14 17 18 7 | 112 104 113 97 108 111 107
R14E | 2633 12 12 20 27 14 14 7 | 54 53 53 62 48 60 52
R15E | 1407 12 15 24 29 17 21 9 | 27 28 31 42 28 28 25
R16E | 1352 13 18 29 19 21 14 9 | 44 48 46 58 41 50 44
R17 | 819 9 10 14 11 15 19 6 | 35 35 28 31 36 20 29
R18 | 872 18 17 14 13 14 28 8 | 31 33 34 31 34 24 29
R19 | 541 21 73 30 73 42 62 23 | 67 61 71 80 72 54 62
R20 | 3127 53 61 59 46 25 22 21 | 58 25 53 45 29 40 37
R21 | 1056 15 16 14 21 9 23 7 | 43 41 40 48 38 38 39
R22 | 2252 13 13 11 26 22 12 7 | 18 28 23 28 31 26 22
R24 | 708 12 17 14 20 10 15 6 | 33 37 37 34 33 28 30
XR25 | ---- --- --- --- --- 5 --- 0 | --- --- --- --- 356 --- 376
XR26 |25899 45 --- --- 29 52 --- 31 | 25 --- --- 24 52 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 2223 20 25 21 26 18 26 |T 42 42 44 44 57 38 55
WRMS | 2223 17 19 15 21 15 24 |NE 41 40 42 40 61 33 58
MEDI | 1080 14 16 14 19 14 18 |MD 43 37 39 42 41 30 37
Table 3.2337.5 GPS week: 2337 Day: 5 MJD: 60608
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1259 33 23 18 22 26 65 14 | 51 53 44 50 47 55 47
R02 | 1281 7 14 11 9 9 11 4 | 35 46 46 45 38 38 40
R03 | 747 6 8 12 21 11 12 5 | 33 30 30 44 26 32 31
R04 | 793 13 9 14 16 9 11 5 | 32 30 25 26 23 25 25
R05 | 1500 12 18 12 17 13 25 7 | 40 41 40 32 42 30 36
R07 | 1526 7 11 18 9 10 14 5 | 41 39 47 40 42 38 40
XR08 | 1123 20 7 14 13 19 --- 8 | 38 40 40 51 56 --- 44
R09E | 3498 13 10 18 13 11 11 5 | 21 22 30 23 23 23 22
R11E | 3290 17 10 14 9 13 14 6 | 21 22 21 17 20 19 17
R12E | 843 14 19 23 16 21 16 8 | 129 147 139 135 124 138 134
R14E | 2447 10 13 13 18 14 12 6 | 50 50 52 54 44 51 48
R15E | 772 14 15 14 24 12 17 7 | 36 41 42 49 35 34 37
R16E | 1214 14 10 24 28 11 18 8 | 48 49 51 72 48 51 50
R17 | 1109 8 16 14 15 10 14 5 | 29 32 37 29 33 34 29
R18 | 740 17 24 14 19 13 9 7 | 32 41 33 32 29 36 31
R19 | 995 36 79 25 54 36 62 22 | 60 37 57 61 63 52 53
R20 | 4787 40 57 60 30 19 48 19 | 45 37 75 45 43 27 41
R21 | 438 11 19 19 10 12 22 7 | 41 36 50 40 41 31 39
R22 | 2920 14 8 17 12 10 16 6 | 23 30 41 26 30 27 28
R24 | 640 12 13 20 25 13 11 7 | 33 34 27 43 27 30 30
XR25 | 7297 31 --- --- --- 26 --- 28 | 619 --- --- --- 513 --- 528
XR26 |22940 32 --- --- 30 46 --- 26 | 22 --- --- 23 32 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 1995 18 26 22 22 16 27 |T 67 42 46 44 62 40 62
WRMS | 1995 18 22 16 19 14 24 |NE 73 37 42 39 67 35 66
MEDI | 1214 14 13 14 17 13 14 |MD 36 37 41 43 38 34 37
Table 3.2337.6 GPS week: 2337 Day: 6 MJD: 60609
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 917 33 31 11 25 23 41 12 | 78 62 70 65 75 54 66
R02 | 1987 11 14 11 9 18 16 6 | 45 59 54 46 53 38 49
R03 | 549 14 19 7 14 11 21 6 | 58 68 65 68 67 59 63
R04 | 807 9 12 12 18 20 22 7 | 60 56 58 50 61 44 54
R05 | 3144 16 13 12 18 20 15 7 | 56 58 53 50 62 41 52
R07 | 784 12 11 10 9 11 29 6 | 66 62 68 65 67 54 63
R08 | 1090 14 13 8 10 13 16 5 | 61 64 66 65 66 55 63
R09E | 1912 13 11 12 12 15 14 5 | 26 31 35 26 32 29 29
R11E | 3906 16 10 20 12 13 11 6 | 27 27 33 27 23 32 26
R12E | 1048 11 12 12 15 11 13 5 | 121 124 123 123 123 126 122
R14E | 2379 17 13 18 25 22 16 8 | 71 78 72 85 69 77 73
R15E | 1515 12 15 11 22 21 12 7 | 54 62 55 66 44 59 55
R16E | 1066 18 18 20 28 18 14 9 | 71 72 70 78 66 72 69
R17 | 989 11 15 16 11 11 23 6 | 40 38 47 44 42 31 39
R18 | 908 19 30 11 12 14 14 8 | 34 52 38 37 40 32 37
R19 | 1970 57 58 32 73 18 51 22 | 74 43 83 77 73 47 62
R20 | 6097 41 35 32 21 24 23 13 | 63 34 51 55 49 48 45
R21 | 638 13 15 10 13 20 19 6 | 51 50 50 53 55 39 48
R22 | 3673 17 14 17 10 11 18 6 | 27 31 39 36 41 30 32
R24 | 553 14 21 29 15 27 13 9 | 45 45 41 45 36 37 38
XR25 | 7294 16 12 --- --- 13 --- 9 | 531 450 --- --- 555 --- 553
XR26 |24212 35 --- --- 45 69 --- 37 | 26 --- --- 34 72 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 2276 22 22 17 23 18 22 |T 76 74 58 56 80 50 76
WRMS | 2276 17 21 17 17 17 21 |NE 82 78 55 52 88 43 81
MEDI | 1090 14 14 12 15 18 16 |MD 56 58 54 53 61 44 52
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