[IGSREPORT-30316] Wk 2351 IGLOS Final Orbits
acc
acc at igs.org
Fri Feb 14 06:09:22 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2351 (Jan 26, 2025 - Feb 01, 2025)
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 2.2351.
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:
igl2351[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2351 in the SP3 format.
igl23517.sum Combination Report for GPS Week 2351.
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 | 5.2 ns
1 | -1.0 ns
2 | 5.3 ns
3 | 1.9 ns
4 | 4.0 ns
5 | 0.9 ns
6 | 1.8 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
5 | GFZ | R19
5 | GRG | R19
6 | ALL | R19
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 1.2351, 1a.2351).
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 2.2351.0-6)
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 3.2351.0-6).
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 2351 summary. (Jan 26, 2025 - Feb 01, 2025)
Table 1.2351.a GPS week : 2351 MJD: 60701.0-60707.0
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 4 -3 -4 46 .12 18 15 | 5435 429 3352 7903
| 0 1 1 9 12 11 .04 | 2690 2967
esa n/a| -2 0 -1 -34 -3 31 -.10 35 31 | 6436 403 3398 8372
| 1 1 1 12 25 31 .05 | 1937 4193
gfz n/a| 0 0 2 13 14 -29 -.03 22 15 | 0 468 3412 7828
| 0 1 1 19 5 24 .06 | 0 3271
grg n/a| 1 0 -3 17 -32 26 .37 20 16 | 2206 411 3407 7456
| 0 0 1 16 16 43 .05 | 1516 3164
iac n/a| 0 0 -3 1 32 -19 -.17 16 15 | 3899 -331 3356 8332
| 1 1 1 16 19 35 .05 | 2070 1968
jgx n/a| 0 0 1 -17 -12 -36 -.22 24 24 | 6830 505 3396 7969
| 1 1 1 11 18 20 .03 | 2341 3013
Table 1.2351.b GPS week : 2351 MJD: 60701.0-60707.0
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 | 16 16 15 16 15 13 14 |
R02 | 6 7 7 6 6 6 7 |
R03 | 8 7 8 9 8 8 6 |
R04 | 7 7 8 9 7 9 9 |
R05 | 9 8 11 9 8 8 8 |
R06 | 56 51 44 54 37 54 0 |
R07 | 8 8 7 9 9 9 8 |
R08 | 7 10 8 14 10 10 9 |
R09 | 7 7 7 7 7 6 7 |
R11 | 9 10 8 8 10 10 10 |
R12 | 7 7 7 10 9 8 6 |
R14 | 6 6 6 7 6 7 5 |
R15 | 9 10 9 9 9 7 8 |
R16 | 7 8 8 8 7 8 9 |
R17 | 8 7 7 7 7 7 7 |
R18 | 9 7 7 6 7 6 5 |
R19 | 14 18 14 18 19 315 --- |
R20 | 19 21 20 19 25 26 21 |
R21 | 7 6 6 7 7 7 7 |
R22 | 8 7 7 8 6 8 7 |
R24 | 8 8 8 9 6 7 8 |
Table 1.2351.c GPS week : 2351 MJD: 60701.0-60707.0
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 2351 0 | 15 54 173 -958 2922 3783 80.0 1650 1650 | 5206 0
brd 2351 1 | -34 99 123 -989 1071 111 78.6 1478 1478 | -993 0
brd 2351 2 | 39 126 42 -2290 1002 -6452 78.9 1418 1418 | 5316 0
brd 2351 3 | 59 -15 57 -147 -612 -9336 77.7 1354 1354 | 1919 0
brd 2351 4 | -60 12 49 117 -1200 -12340 78.2 1438 1438 | 4015 0
brd 2351 5 | 43 70 -30 -1149 -1239 -1280 77.3 1637 1637 | 865 0
brd 2351 6 | -115 -52 -19 -75 -1400 -5321 79.1 1999 1999 | 1849 0
-------------+------------------------------------------------------------+----------------
brd 2351 mean| -7 42 56 -784 77 -4404 78.5 1567 1567 | 2596 0
brd 2351 sdev| 64 63 72 835 1630 5620 .9 220 220 | 2349 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 2.2351.0 GPS week: 2351 Day: 0 MJD: 60701
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 12 -8 43 .15 18 15 | 6980 2369 3453 8175
esa n/a| -3 0 -3 -21 -17 75 -.18 35 28 | 7608 2687 3525 8419
gfz n/a| 0 0 0 10 7 3 -.02 21 16 | 0 2613 3497 8142
grg n/a| 2 -1 -2 50 -4 -49 .42 21 16 | 3632 2607 3510 7787
iac n/a| 0 0 -1 2 21 -27 -.15 16 14 | 6159 1917 3450 8665
jgx n/a| 1 -1 0 -27 -28 -15 -.24 21 21 | 7692 2596 3527 8264
Table 2.2351.1 GPS week: 2351 Day: 1 MJD: 60702
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 0 19 53 .08 19 15 | 1340 -5775 4214 8352
esa n/a| -2 0 -2 -35 -14 1 -.13 35 30 | 4205 -8844 4300 9086
gfz n/a| 0 0 2 18 12 -13 .02 24 15 | 0 -6391 4283 8385
grg n/a| 1 0 -2 19 -26 89 .40 18 17 | 1961 -6288 4299 8083
iac n/a| 1 0 -6 4 27 -68 -.20 18 16 | 1443 -4163 4224 8672
jgx n/a| -1 0 1 -16 -11 -39 -.25 23 23 | 3423 -5844 4275 8445
Table 2.2351.2 GPS week: 2351 Day: 2 MJD: 60703
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 -16 -5 23 .09 18 15 | 4830 2237 3498 7572
esa n/a| -1 0 -1 -44 12 -8 -.06 35 31 | 5355 3077 3524 8840
gfz n/a| 0 0 2 0 21 -18 .07 20 13 | 0 2452 3572 7332
grg n/a| 0 0 -3 16 -45 0 .27 20 18 | 4056 2556 3550 6965
iac n/a| 0 -2 -3 34 55 39 -.23 17 16 | 5901 922 3500 7889
jgx n/a| 0 1 0 -28 -20 -57 -.22 23 23 | 6002 2623 3559 7508
Table 2.2351.3 GPS week: 2351 Day: 3 MJD: 60704
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 -5 -20 52 .15 18 15 | 3001 1010 3744 8515
esa n/a| 0 1 0 -54 27 19 -.10 35 31 | 4076 1368 3817 8739
gfz n/a| 0 0 2 34 10 -38 -.07 22 17 | 0 821 3814 8474
grg n/a| 2 0 -5 -5 -22 16 .41 23 20 | 1332 649 3806 7994
iac n/a| -2 0 -1 -16 63 0 -.12 19 17 | 2881 223 3734 8934
jgx n/a| -1 0 0 -3 -27 -42 -.21 24 24 | 4531 843 3776 8542
Table 2.2351.4 GPS week: 2351 Day: 4 MJD: 60705
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 2 -10 -5 59 .07 17 15 | 6499 2023 2591 7971
esa n/a| -4 -2 1 -20 26 20 -.03 35 29 | 7473 1778 2615 7908
gfz n/a| 1 0 0 -8 22 -29 -.03 23 15 | 0 1649 2668 7906
grg n/a| 1 0 0 17 -39 42 .35 20 14 | 2967 1647 2654 7613
iac n/a| 0 2 -1 0 17 -49 -.18 15 13 | 5946 -1372 2603 8426
jgx n/a| 0 -1 2 -11 0 -11 -.23 29 29 | 8600 1401 2633 8152
Table 2.2351.5 GPS week: 2351 Day: 5 MJD: 60706
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 2 2 -9 50 .13 16 15 | 5886 2054 2923 7054
esa n/a| -4 1 -2 -31 -23 64 -.12 39 32 | 7084 2588 2967 7588
gfz n/a| 0 0 2 -5 16 -75 -.07 26 16 | 0 2852 2998 6895
grg n/a| 3 0 -1 8 -52 39 .35 18 14 | -411 2233 2991 6445
iac n/a| 0 0 -4 -7 16 -23 -.22 15 14 | 1665 409 2935 7520
jgx n/a| 1 -2 3 -5 22 -65 -.24 25 25 | 7406 2369 2981 7020
Table 2.2351.6 GPS week: 2351 Day: 6 MJD: 60707
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 3 -6 -1 44 .18 18 16 | 9515 -911 3044 7686
esa n/a| -2 1 -1 -35 -37 46 -.08 33 32 | 9255 171 3042 8029
gfz n/a| 0 2 5 43 8 -35 -.09 17 15 | 0 -720 3053 7662
grg n/a| 1 -1 -5 15 -37 45 .40 21 15 | 1905 -527 3043 7308
iac n/a| 0 0 -4 -8 23 -7 -.12 14 14 | 3303 -257 3052 8220
jgx n/a| 0 0 1 -29 -22 -21 -.15 21 21 | 10161 -451 3025 7852
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 3.2351.0 GPS week: 2351 Day: 0 MJD: 60701
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 859 39 83 20 30 15 29 15 | 117 48 103 92 81 65 85
R02 | 2059 6 25 8 18 11 12 6 | 56 61 52 63 58 44 55
R03 | 827 12 27 13 16 13 25 7 | 72 65 63 68 68 50 63
R04 | 620 8 20 16 21 12 19 7 | 71 69 77 72 72 58 69
R05 | 802 16 17 16 15 16 29 8 | 105 109 109 111 110 93 105
XR06M | 3495 63 --- --- --- 49 --- 56 | 76 --- --- --- 68 --- 85
R07M | 1602 13 31 18 13 8 25 8 | 80 60 82 77 73 54 72
R08M | 1032 16 20 15 12 11 15 6 | 74 80 75 74 72 61 72
R09M | 789 11 31 11 10 14 16 6 | 22 20 23 26 26 27 21
R11 | 745 13 53 16 18 15 10 9 | 30 58 41 41 40 33 37
R12M | 606 20 22 15 11 8 11 6 | 33 36 29 27 30 18 25
R14M | 3453 9 11 18 9 9 20 6 | 39 35 46 38 41 29 37
R15M | 1003 18 15 12 17 18 34 9 | 52 50 46 46 56 31 45
R16M | 1457 14 29 17 11 9 16 7 | 56 45 63 51 57 42 52
R17E | 2015 12 16 17 26 18 13 8 | 71 67 74 72 68 64 69
R18E | 1346 20 24 10 25 18 12 8 | 35 41 40 42 39 29 34
R19E | 2229 31 41 30 39 24 29 14 | 70 42 174 78 105 34 82
R20E | 2105 24 62 58 39 35 35 18 | 108 111 116 105 112 89 102
R21E | 936 12 29 24 13 10 9 7 | 43 37 41 44 39 39 39
R22E | 2286 19 29 15 15 19 14 8 | 33 40 37 43 40 34 36
R24E | 2482 14 27 11 25 10 15 7 | 84 79 78 84 79 73 79
------+-----------------------------------------+-------------------------------------
RMS | 1650 18 35 21 21 16 21 |T 63 57 68 62 63 48 60
WRMS | 1650 15 28 16 16 14 21 |NE 75 68 74 74 71 57 69
MEDI | 1346 14 27 16 16 14 16 |MD 70 50 63 63 68 42 63
Table 3.2351.1 GPS week: 2351 Day: 1 MJD: 60702
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 673 40 79 29 14 17 24 15 | 91 46 81 67 63 56 67
R02 | 1845 10 29 9 17 13 14 6 | 49 48 42 54 45 41 45
R03 | 945 15 22 11 17 13 18 7 | 52 43 44 47 41 39 43
R04 | 731 11 20 17 16 14 12 6 | 55 52 53 50 53 45 49
R05 | 785 14 28 17 19 20 15 8 | 118 120 114 123 101 105 112
XR06M | 3402 50 --- --- --- 50 --- 50 | 46 --- --- --- 37 --- 54
R07M | 660 15 27 11 18 16 18 7 | 50 49 54 58 56 43 51
R08M | 647 10 24 9 32 17 25 9 | 57 70 57 74 52 51 58
R09M | 1022 18 26 9 15 11 9 6 | 23 28 29 30 27 24 24
R11 | 675 12 45 15 13 22 24 9 | 35 63 45 45 42 33 40
R12M | 596 14 30 14 9 12 10 6 | 30 36 29 30 24 26 25
R14M | 3605 7 20 11 10 16 14 5 | 35 35 32 32 36 26 30
R15M | 595 17 13 21 13 17 38 9 | 46 49 54 43 49 29 42
R16M | 741 18 16 18 14 13 23 7 | 44 39 45 33 43 27 36
R17E | 1370 10 20 14 19 11 15 6 | 67 60 60 77 59 67 64
R18E | 1541 9 27 20 15 11 12 7 | 42 50 34 46 39 31 37
R19E | 2476 29 55 56 28 27 43 17 | 72 45 210 65 110 41 86
R20E | 1536 37 61 61 30 37 54 20 | 114 118 119 102 119 101 109
R21E | 917 11 24 12 13 10 8 5 | 40 38 38 51 34 37 38
R22E | 2113 17 23 16 12 14 14 7 | 37 37 46 44 40 40 39
R24E | 1757 13 28 18 18 16 15 8 | 74 72 70 76 72 71 71
------+-----------------------------------------+-------------------------------------
RMS | 1477 19 35 24 18 18 23 |T 56 54 62 57 54 46 53
WRMS | 1477 15 30 15 17 16 23 |NE 66 62 63 64 57 53 59
MEDI | 945 14 26 15 15 16 15 |MD 49 48 46 50 45 40 45
Table 3.2351.2 GPS week: 2351 Day: 2 MJD: 60703
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1082 36 70 34 14 26 22 15 | 91 36 87 72 48 56 66
R02 | 2052 9 27 10 20 13 19 7 | 50 59 52 64 45 39 49
R03 | 992 15 31 11 18 9 20 7 | 66 50 69 75 60 51 62
R04 | 1019 11 26 10 16 15 28 7 | 65 53 67 68 70 51 62
R05 | 1263 17 39 16 29 30 19 11 | 105 114 99 87 97 102 97
XR06M | 1221 45 --- --- --- 42 --- 43 | 88 --- --- --- 57 --- 91
R07M | 834 8 25 12 18 10 21 6 | 63 53 66 74 62 46 61
R08M | 629 16 22 18 23 12 13 7 | 48 59 52 67 55 46 52
R09M | 653 11 35 13 18 9 16 7 | 16 43 22 15 13 17 14
R11 | 690 17 32 11 13 20 19 8 | 25 44 32 38 45 44 34
R12M | 672 16 23 11 8 11 19 6 | 32 21 21 25 29 16 23
R14M | 3160 7 19 16 10 13 11 5 | 27 23 35 33 25 27 27
R15M | 640 23 22 23 15 11 25 9 | 44 37 44 42 44 33 39
R16M | 830 15 15 14 13 11 35 8 | 43 48 48 42 39 27 39
R17E | 1191 9 21 9 17 14 18 6 | 41 42 40 46 42 32 38
R18E | 766 7 26 15 14 21 12 7 | 28 40 27 33 33 20 27
R19E | 1987 32 48 25 22 26 41 14 | 54 33 194 60 64 44 56
R20E | 1685 28 70 54 48 26 50 20 | 81 76 79 77 75 72 71
R21E | 874 11 28 11 12 10 10 6 | 35 31 41 39 35 30 34
R22E | 2043 16 22 11 15 16 12 6 | 25 38 35 34 33 26 30
R24E | 1987 10 37 17 22 12 12 8 | 41 57 40 43 44 33 39
------+-----------------------------------------+-------------------------------------
RMS | 1418 18 35 20 20 17 23 |T 50 47 57 51 48 40 48
WRMS | 1418 15 31 13 18 16 23 |NE 67 59 67 67 60 57 61
MEDI | 1019 15 26 13 16 13 19 |MD 44 43 44 43 45 33 39
Table 3.2351.3 GPS week: 2351 Day: 3 MJD: 60704
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1450 35 63 44 18 20 33 15 | 93 26 103 63 55 44 67
R02 | 1694 11 21 8 16 14 10 5 | 47 48 41 53 34 35 41
R03 | 1279 16 26 14 14 13 30 8 | 65 51 66 63 62 39 57
R04 | 1903 6 32 14 15 22 24 8 | 60 51 68 69 79 45 62
R05 | 2025 9 48 21 19 11 19 9 | 126 137 131 132 122 116 125
XR06M | 1316 51 --- --- --- 56 --- 53 | 54 --- --- --- 75 --- 68
R07M | 819 14 28 18 28 17 12 8 | 65 54 52 81 68 63 62
R08M | 990 30 37 16 46 33 17 13 | 60 67 43 55 61 42 45
R09M | 582 12 26 11 20 11 8 6 | 15 26 17 21 20 18 15
R11 | 754 14 37 14 14 15 13 7 | 29 42 37 41 40 31 33
R12M | 720 10 22 17 24 27 28 9 | 39 45 38 25 55 35 36
R14M | 1731 9 26 12 18 14 9 6 | 33 25 36 41 32 36 32
R15M | 806 21 37 15 20 9 11 8 | 85 84 82 86 85 87 83
R16M | 922 19 19 21 13 14 19 8 | 47 37 55 47 43 35 43
R17E | 1492 9 23 17 19 17 13 7 | 49 44 48 55 54 43 47
R18E | 556 7 25 14 12 12 13 6 | 33 46 31 41 38 30 33
R19E | 2228 36 50 43 38 34 42 17 | 83 43 354 74 145 44 109
R20E | 1384 27 61 39 38 26 65 19 | 133 146 117 134 146 129 133
R21E | 1047 9 34 14 16 13 12 7 | 42 36 48 45 43 33 39
R22E | 1431 19 21 12 21 19 13 8 | 25 34 34 42 36 25 29
R24E | 1467 12 23 22 22 22 14 8 | 50 51 55 48 48 38 45
------+-----------------------------------------+-------------------------------------
RMS | 1353 18 35 22 23 19 24 |T 58 54 72 60 63 48 57
WRMS | 1353 15 31 17 19 17 24 |NE 70 59 74 70 65 51 64
MEDI | 1316 14 26 15 19 17 13 |MD 50 45 48 53 55 38 45
Table 3.2351.4 GPS week: 2351 Day: 4 MJD: 60705
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2052 33 64 33 27 21 30 14 | 82 27 82 82 48 43 61
R02 | 1888 9 16 18 11 8 18 6 | 42 43 54 44 40 31 41
R03 | 2227 13 31 12 18 9 28 8 | 52 35 52 63 46 33 47
R04 | 1674 12 29 9 10 12 26 7 | 53 41 41 52 53 31 46
R05 | 1237 18 38 12 16 8 17 8 | 74 66 64 77 76 63 70
XR06M | 1509 42 --- --- --- 32 --- 37 | 75 --- --- --- 56 --- 80
R07M | 860 21 38 12 18 11 28 9 | 59 52 46 49 46 40 45
R08M | 1043 22 28 18 24 16 26 9 | 55 62 63 64 49 44 53
R09M | 618 10 25 22 13 9 9 6 | 35 46 41 38 38 33 36
R11 | 821 17 53 16 17 10 20 9 | 21 44 27 34 23 20 24
R12M | 920 17 28 22 28 14 19 9 | 33 30 39 21 31 24 27
R14M | 1565 6 15 14 10 9 24 5 | 47 45 53 42 50 40 46
R15M | 984 17 25 13 12 16 39 9 | 393 394 388 394 388 399 392
R16M | 974 17 26 10 12 10 12 6 | 39 27 32 32 31 34 31
R17E | 1390 9 18 20 19 15 15 7 | 58 58 52 62 60 56 56
R18E | 1108 8 20 20 10 15 15 6 | 38 43 27 43 47 29 37
XR19E | 2338 47 44 34 41 26 --- 19 | 85 49 648 162 191 --- 139
R20E | 1338 31 71 69 44 36 87 24 | 94 98 131 104 90 105 98
R21E | 1009 11 25 13 16 12 19 7 | 45 38 39 45 42 40 40
R22E | 1937 15 19 14 15 11 11 6 | 31 41 40 36 38 26 33
R24E | 2085 10 20 12 17 12 16 6 | 49 52 54 46 53 40 47
------+-----------------------------------------+-------------------------------------
RMS | 1437 17 35 23 20 15 29 |T 69 64 98 74 71 59 69
WRMS | 1437 15 29 15 14 13 29 |NE 54 42 53 58 47 36 48
MEDI | 1338 17 26 14 16 12 19 |MD 52 44 52 46 48 40 46
Table 3.2351.5 GPS week: 2351 Day: 5 MJD: 60706
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1819 39 61 17 19 23 23 13 | 79 36 59 63 44 56 57
R02 | 1632 10 19 17 8 10 12 5 | 43 45 42 46 47 35 42
R03 | 2844 14 24 14 11 14 25 7 | 62 47 58 61 65 54 59
R04 | 1692 15 30 25 15 12 27 8 | 52 51 71 63 56 43 55
R05 | 798 12 36 8 18 14 20 7 | 114 120 110 114 116 112 114
XR06M | 1568 55 --- --- --- 52 --- 54 | 57 --- --- --- 77 --- 69
R07M | 1329 16 31 20 16 16 24 8 | 59 47 64 60 48 40 53
R08M | 701 21 26 16 19 15 34 9 | 64 62 59 57 60 45 56
R09M | 809 11 32 13 10 7 16 6 | 61 69 62 60 63 64 62
R11 | 678 12 70 16 9 13 15 10 | 16 35 22 20 21 18 17
R12M | 710 19 14 16 20 14 15 7 | 29 24 31 17 17 22 19
R14M | 1933 9 28 15 11 12 19 6 | 74 81 74 76 81 71 75
R15M | 827 11 18 13 10 15 24 6 | 810 813 825 813 809 816 815
R16M | 994 12 39 20 11 13 17 7 | 38 30 46 47 49 38 42
R17E | 2851 11 24 15 15 19 14 7 | 56 53 57 61 45 54 52
R18E | 1551 4 20 17 9 12 12 5 | 34 37 29 37 39 28 33
XR19E |19544 324 --- 2915 849 305 --- 314 | 146 --- 9999 372 653 --- 400
R20E | 2119 24 94 88 49 28 68 25 | 151 166 162 155 154 147 150
R21E | 1117 10 28 14 13 11 17 6 | 31 35 43 41 35 32 35
R22E | 2067 15 38 14 11 17 15 7 | 27 38 35 36 38 34 32
R24E | 1871 12 19 21 20 12 9 7 | 47 45 46 53 48 44 45
------+-----------------------------------------+-------------------------------------
RMS | 1636 16 39 26 18 15 25 |T 97 96 99 112 122 92 108
WRMS | 1636 15 32 16 14 14 25 |NE 61 55 60 61 58 53 57
MEDI | 1568 12 28 16 13 14 17 |MD 57 47 58 60 49 44 55
Table 3.2351.6 GPS week: 2351 Day: 6 MJD: 60707
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1346 42 53 22 31 14 28 14 | 105 43 82 71 70 57 72
R02 | 1027 12 15 10 28 9 12 6 | 55 57 53 47 50 41 48
R03 | 1723 10 17 10 12 14 17 6 | 74 67 67 69 74 58 67
R04 | 1802 12 21 12 13 27 24 8 | 66 57 67 65 87 53 67
R05 | 1833 10 23 23 24 11 19 8 | 88 94 101 76 85 92 88
XR06M |13950 4 --- --- --- --- --- 0 | 124 --- --- --- --- --- 132
R07M | 2507 15 32 11 13 12 22 7 | 71 48 67 66 65 44 61
R08M | 789 22 32 11 19 13 23 8 | 68 68 64 80 77 59 68
R09M | 1100 14 30 11 11 11 12 6 | 124 127 126 127 124 127 125
R11 | 1088 13 60 12 15 16 8 9 | 21 40 28 25 33 23 25
R12M | 1324 12 15 14 17 8 11 5 | 36 29 34 24 30 33 29
R14M | 1914 7 20 9 12 9 10 5 | 94 85 96 90 90 93 91
R15M | 1172 22 31 15 16 10 17 8 | 9999 9999 9999 9999 9999 9999 9999
R16M | 793 22 19 17 18 15 27 9 | 61 46 51 53 46 36 48
R17E | 1277 9 18 12 24 11 12 6 | 67 62 66 74 61 62 64
R18E | 930 7 19 12 12 10 13 5 | 42 46 35 45 43 37 39
R20E | 5975 27 84 43 49 24 55 20 | 119 161 146 114 132 120 126
R21E | 886 12 18 15 13 16 14 6 | 48 48 51 55 51 47 49
R22E | 2476 19 14 18 12 12 9 6 | 37 47 50 45 44 45 43
R24E | 1283 14 16 13 28 16 11 7 | 68 74 69 81 74 67 71
------+-----------------------------------------+-------------------------------------
RMS | 1999 18 33 17 21 14 21 |T 72 66 106 73 74 60 71
WRMS | 1999 16 32 15 15 14 21 |NE 68 59 66 58 66 54 61
MEDI | 1283 12 20 12 16 12 14 |MD 68 57 67 69 70 53 67
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