[IGSREPORT-30347] Wk 2354 IGLOS Final Orbits
acc
acc at igs.org
Fri Mar 7 04:56:25 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2354 (Feb 16, 2025 - Feb 22, 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 2.2354.
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:
igl2354[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2354 in the SP3 format.
igl23547.sum Combination Report for GPS Week 2354.
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.
Starting 02-Feb-2025 (GPS week 2352) the IGS Analysis Centers started using
the IGS realization of the updated ITRF2020-u2023, called IGb20. The combined
GLONASS orbits from this date are therefore in IGb20 frame.
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 | 0.5 ns
1 | 1.3 ns
2 | 1.5 ns
3 | 0.3 ns
4 | 4.9 ns
5 | 6.3 ns
6 | 0.5 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
----+--------+---------------
0 | GFZ | R26
1 | GFZ | R26
2 | GFZ | R26
3 | GFZ | R26
4 | GFZ | R26
5 | GFZ | R26
6 | GFZ | 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 1.2354, 1a.2354).
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 2.2354.0-6)
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 3.2354.0-6).
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 2354 summary. (Feb 16, 2025 - Feb 22, 2025)
Table 1.2354.a GPS week : 2354 MJD: 60722.0-60728.0
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 -1 -3 0 42 .13 16 14 | 4293 -1217 3605 11569
| 0 1 0 17 11 26 .04 | 1388 1973
esa n/a| -2 -1 -2 -35 -4 61 -.11 28 24 | 5349 -1941 3597 11121
| 1 1 1 10 13 54 .04 | 1256 3036
gfz n/a| 0 0 2 7 8 -23 .03 19 15 | 0 -1333 3727 10251
| 1 0 2 11 20 8 .03 | 0 2111
grg n/a| 2 0 2 -3 -6 0 .29 19 16 | 2838 -1284 3638 8573
| 0 1 1 14 15 50 .03 | 1925 2092
iac n/a| -1 0 -6 -19 -2 -38 -.22 18 17 | 3422 -816 3626 9839
| 1 1 1 14 17 39 .05 | 2263 1279
jgx n/a| 0 0 5 33 -9 -9 -.18 19 19 | 6815 -1224 3631 8978
| 1 1 1 16 9 42 .03 | 1428 2116
Table 1.2354.b GPS week : 2354 MJD: 60722.0-60728.0
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 | 11 12 14 15 13 13 11 |
R02 | 6 5 7 7 9 8 5 |
R03 | 8 7 6 7 7 7 8 |
R04 | 7 7 7 7 7 7 6 |
R05 | 8 7 8 7 7 8 7 |
R07 | 8 8 7 7 8 7 6 |
R08 | 7 8 7 8 9 9 7 |
R09 | 7 7 7 6 6 6 8 |
R11 | 8 7 9 6 8 9 6 |
R12 | 7 6 8 7 8 6 8 |
R14 | 7 6 6 8 6 5 6 |
R15 | 8 7 7 8 9 8 8 |
R16 | 7 9 9 6 8 9 7 |
R17 | 8 8 6 6 7 7 7 |
R18 | 7 6 8 7 7 6 6 |
R19 | 8 7 8 8 10 9 9 |
R20 | 19 18 19 16 24 21 21 |
R21 | 10 8 9 9 7 8 7 |
R22 | 6 7 8 8 7 7 7 |
R24 | 8 9 7 9 9 8 8 |
R26 | 38 39 44 59 51 46 50 |
Table 1.2354.c GPS week : 2354 MJD: 60722.0-60728.0
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 2354 0 | 7 26 133 59 -237 7602 82.1 1587 1587 | 455 0
brd 2354 1 | -35 38 104 -916 -252 9921 79.6 1689 1689 | 1299 0
brd 2354 2 | 15 57 103 -337 1607 7242 78.8 1596 1596 | 1506 0
brd 2354 3 | 75 4 107 917 1540 5030 80.6 1822 1822 | 309 0
brd 2354 4 | 28 77 92 682 2135 3800 80.9 1934 1934 | 4915 0
brd 2354 5 | -72 34 107 263 954 4429 81.2 1825 1825 | 6339 0
brd 2354 6 | 60 -34 51 649 1293 969 79.3 1959 1959 | 465 0
-------------+------------------------------------------------------------+----------------
brd 2354 mean| 11 29 99 188 1005 5570 80.4 1773 1773 | 2184 0
brd 2354 sdev| 51 36 24 646 925 2936 1.2 151 151 | 2429 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 2.2354.0 GPS week: 2354 Day: 0 MJD: 60722
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 -1 -26 19 50 .05 17 16 | 4638 582 4023 11345
esa n/a| -2 -1 -2 -52 -15 -17 -.08 32 27 | 4895 786 4012 10717
gfz n/a| 1 0 1 5 0 -22 .05 18 14 | 0 319 4141 10429
grg n/a| 2 0 1 -32 -25 57 .29 19 14 | 884 616 4061 9705
iac n/a| 1 0 -6 -8 2 -36 -.15 17 16 | 2022 -554 4021 10834
jgx n/a| -2 0 5 63 3 -55 -.17 17 17 | 6079 1090 4009 9860
Table 2.2354.1 GPS week: 2354 Day: 1 MJD: 60723
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 -3 1 7 .14 16 13 | 5908 -4193 4554 10482
esa n/a| -3 -2 0 -23 -5 121 -.12 26 24 | 6950 -4570 4528 10733
gfz n/a| 3 0 5 26 26 -12 -.00 17 15 | 0 -4547 4657 9287
grg n/a| 2 1 3 -4 22 -25 .31 19 15 | 3271 -4269 4619 8237
iac n/a| 0 1 -7 -25 -28 -5 -.23 15 15 | 2541 -3394 4552 10025
jgx n/a| 0 -3 5 25 -22 -26 -.19 20 20 | 8130 -4265 4626 8620
Table 2.2354.2 GPS week: 2354 Day: 2 MJD: 60724
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 -1 2 0 18 .15 15 13 | 3643 497 3090 10259
esa n/a| -3 0 -3 -37 0 103 -.16 26 22 | 3870 529 3090 10079
gfz n/a| 0 0 2 3 -4 -33 .00 19 17 | 0 375 3281 8892
grg n/a| 3 1 2 -5 -4 -62 .32 20 16 | 1065 579 3084 7201
iac n/a| 0 3 -8 -3 27 32 -.26 19 18 | 1253 70 3105 9859
jgx n/a| 1 -1 7 45 -20 -60 -.20 20 20 | 6103 481 3087 7623
Table 2.2354.3 GPS week: 2354 Day: 3 MJD: 60725
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 16 6 38 .16 16 12 | 2879 -2601 3021 11582
esa n/a| 0 0 -3 -30 -10 81 -.15 26 23 | 5255 -4985 3008 10984
gfz n/a| -1 0 4 6 39 -35 .03 17 15 | 0 -2757 3149 10176
grg n/a| 2 0 4 -5 -12 81 .22 19 18 | 1627 -3182 3025 8577
iac n/a| 0 1 -6 -28 -10 -77 -.17 16 15 | 2145 -1511 3013 9253
jgx n/a| 0 -1 6 24 -3 -18 -.17 21 21 | 5793 -2942 3019 8884
Table 2.2354.4 GPS week: 2354 Day: 4 MJD: 60726
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 0 2 90 .16 19 16 | 4976 -782 3379 11116
esa n/a| 0 0 -3 -39 -22 19 -.10 27 21 | 5464 -418 3394 10750
gfz n/a| 0 0 1 10 -9 -27 .07 25 17 | 0 -354 3506 9379
grg n/a| 1 -1 0 6 -12 -22 .29 18 14 | 5063 -525 3426 7034
iac n/a| -2 -1 -4 -17 4 -47 -.26 19 18 | 5489 358 3433 7881
jgx n/a| 0 0 7 16 -12 47 -.24 19 19 | 7797 -635 3442 7578
Table 2.2354.5 GPS week: 2354 Day: 5 MJD: 60727
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 -1 -25 -11 47 .14 16 14 | 5704 739 3260 13008
esa n/a| -3 -3 -5 -24 19 105 -.05 29 24 | 6996 906 3246 11874
gfz n/a| 0 -1 3 10 19 -15 .01 18 13 | 0 784 3366 11626
grg n/a| 2 0 2 8 -18 -9 .30 20 18 | 5721 633 3299 9646
iac n/a| -3 1 -5 -12 -14 -77 -.22 18 17 | 7565 -242 3296 10304
jgx n/a| 1 1 2 36 -11 14 -.14 21 21 | 8830 589 3290 10060
Table 2.2354.6 GPS week: 2354 Day: 6 MJD: 60728
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 1 -1 13 -15 47 .08 14 13 | 2303 -2765 3913 13193
esa n/a| -5 -3 0 -43 3 17 -.08 28 30 | 4015 -5837 3904 12710
gfz n/a| 0 -1 0 -10 -16 -19 .07 19 15 | 0 -3153 3990 11974
grg n/a| 1 -1 3 7 2 -16 .28 19 14 | 2240 -2842 3953 9615
iac n/a| -2 0 -5 -44 0 -59 -.27 19 17 | 2939 -444 3965 10721
jgx n/a| 2 0 3 25 0 33 -.14 17 17 | 4973 -2890 3947 10221
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 3.2354.0 GPS week: 2354 Day: 0 MJD: 60722
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1053 34 41 12 15 21 20 10 | 111 57 84 91 86 84 86
XR02 | 1666 10 9 10 12 14 --- 5 | 76 67 72 70 64 --- 69
R03 | 711 12 12 10 12 25 26 8 | 74 66 76 80 79 62 72
R04 | 2243 11 28 19 16 12 8 7 | 89 75 94 91 85 81 86
R05 | 2285 13 26 22 13 21 7 7 | 72 65 79 72 60 63 67
R07 | 1457 12 35 14 14 16 18 7 | 83 75 77 84 75 63 75
R08 | 1017 14 35 14 12 15 9 7 | 89 104 87 84 92 90 89
R09 | 812 12 34 13 7 14 9 6 | 31 28 37 29 28 32 29
R11 | 965 13 50 8 15 12 12 8 | 27 36 41 39 40 33 34
R12 | 1091 20 13 16 16 19 8 7 | 66 54 57 50 60 53 55
R14 | 775 13 27 11 14 9 19 7 | 62 62 63 55 55 45 55
R15 | 589 19 25 15 13 15 20 8 | 84 76 89 77 75 67 77
R16 | 1911 21 28 12 8 14 13 7 | 88 75 77 77 74 69 76
R17E | 2116 11 21 10 20 24 11 7 | 119 118 119 112 126 110 117
R18E | 973 9 20 15 15 13 15 6 | 21 24 18 30 24 18 20
R19E | 1518 15 20 16 19 19 13 7 | 191 198 196 198 193 206 196
R20E | 1862 33 72 45 40 29 44 19 | 108 113 128 106 106 106 107
R21E | 1760 12 22 27 40 11 13 10 | 172 169 168 184 171 166 171
R22E | 1884 13 22 11 15 12 10 6 | 36 35 36 38 40 33 35
R24E | 2749 13 20 17 26 15 12 7 | 71 68 73 66 68 68 67
XR26 |76718 59 56 1000 --- 46 --- 37 | 33 98 750 --- 23 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 1586 17 32 18 19 17 17 |T 81 79 115 81 77 76 77
WRMS | 1586 16 27 14 14 16 17 |NE 70 67 120 69 64 61 65
MEDI | 1518 13 26 14 15 15 13 |MD 76 68 77 77 74 67 72
Table 3.2354.1 GPS week: 2354 Day: 1 MJD: 60723
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1053 40 40 11 20 12 33 12 | 59 38 35 39 43 37 39
R02 | 964 8 18 6 13 11 9 4 | 53 53 46 56 49 38 50
R03 | 1531 7 17 14 20 13 16 6 | 48 48 49 61 52 46 50
R04 | 1850 10 20 14 14 14 24 7 | 61 52 69 68 63 47 60
R05 | 1498 9 36 13 15 8 12 7 | 50 51 56 58 44 47 50
R07 | 1511 13 29 12 19 12 25 8 | 55 46 55 61 48 40 50
R08 | 1393 12 30 11 23 12 19 8 | 72 95 72 58 73 72 71
R09 | 618 14 29 13 9 16 12 7 | 21 29 23 22 22 26 20
R11 | 1046 8 26 17 9 14 16 6 | 16 29 32 19 22 24 19
R12 | 786 10 21 9 15 14 14 6 | 52 51 54 43 51 42 48
R14 | 997 9 28 12 14 9 14 6 | 45 56 47 44 48 37 45
R15 | 841 15 21 12 11 16 20 7 | 62 51 63 55 60 48 56
R16 | 1457 15 28 19 9 15 27 8 | 65 55 69 61 60 51 59
R17E | 2089 13 18 21 23 18 10 8 | 137 142 146 137 132 137 138
R18E | 1180 12 19 13 8 12 9 5 | 20 21 21 24 20 21 18
R19E | 3593 10 18 14 17 16 15 6 | 132 139 125 139 128 143 133
R20E | 2707 26 49 48 35 35 48 18 | 94 91 91 82 86 87 83
R21E | 2221 11 16 14 30 16 14 8 | 123 122 127 122 123 123 123
R22E | 1011 18 20 12 14 13 8 6 | 25 28 22 30 30 28 25
R24E | 2211 16 17 21 27 16 12 8 | 61 53 55 60 51 56 54
XR26 |90110 61 60 1019 --- 43 --- 38 | 35 72 461 --- 19 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1688 16 26 17 19 15 20 |T 61 62 81 61 58 57 59
WRMS | 1688 13 24 15 15 15 20 |NE 49 51 80 49 46 42 47
MEDI | 1457 12 21 13 15 14 14 |MD 55 52 55 58 51 46 50
Table 3.2354.2 GPS week: 2354 Day: 2 MJD: 60724
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 957 35 41 21 35 18 33 14 | 82 55 71 89 74 71 73
R02 | 717 8 23 16 13 18 18 7 | 47 42 50 47 53 28 46
R03 | 1032 8 14 19 13 13 12 6 | 63 59 82 68 61 72 67
R04 | 1050 12 19 14 18 18 12 7 | 79 69 84 85 66 74 76
R05 | 1512 15 20 14 17 10 25 7 | 67 62 55 72 62 45 59
R07 | 687 10 21 8 18 7 20 6 | 63 47 59 70 57 49 58
R08 | 1340 14 21 13 17 10 21 7 | 59 54 52 64 53 46 54
R09 | 679 13 20 12 13 19 13 6 | 25 25 32 23 27 26 24
R11 | 1198 18 29 23 11 19 11 8 | 13 41 39 21 19 27 21
R12 | 853 13 20 13 24 17 16 7 | 48 49 46 31 45 46 41
R14 | 645 9 14 19 10 12 16 6 | 54 57 50 62 56 58 54
R15 | 1709 11 10 9 23 23 14 7 | 68 80 79 70 79 69 71
R16 | 586 13 46 10 11 23 12 9 | 74 48 65 70 76 58 64
R17E | 2687 8 14 11 16 18 17 6 | 111 110 116 111 100 106 108
R18E | 932 8 26 18 15 18 14 7 | 22 28 21 28 26 21 19
R19E | 4435 13 18 14 18 22 15 7 | 137 135 144 136 137 143 138
R20E | 1659 30 51 54 37 40 46 19 | 59 69 95 76 62 45 60
R21E | 652 13 15 17 24 27 16 8 | 121 116 123 126 131 117 122
R22E | 1841 14 28 17 16 15 16 8 | 15 42 22 33 25 23 22
R24E | 1460 12 15 16 18 15 19 7 | 64 69 70 65 56 60 62
XR26 |>>>>> 61 76 1077 --- 48 --- 43 | 25 100 632 --- 20 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1595 15 26 19 20 19 20 |T 61 64 94 67 61 59 61
WRMS | 1595 13 22 17 16 18 20 |NE 54 56 99 59 53 51 54
MEDI | 1050 13 20 16 17 18 16 |MD 63 57 65 68 57 49 59
Table 3.2354.3 GPS week: 2354 Day: 3 MJD: 60725
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1061 31 65 20 39 13 26 15 | 89 38 76 92 72 69 73
R02 | 700 8 29 7 17 15 18 7 | 46 49 45 57 46 32 45
R03 | 1416 10 26 14 20 12 16 7 | 56 45 52 61 52 44 51
R04 | 764 12 19 15 19 11 16 6 | 67 48 60 63 57 65 59
R05 | 1209 10 20 17 16 16 12 6 | 58 49 68 69 48 54 57
R07 | 667 13 15 13 15 10 19 6 | 62 47 63 59 49 42 54
R08 | 763 8 17 14 23 18 23 7 | 66 65 67 64 57 54 61
R09 | 771 15 20 15 9 10 14 6 | 18 26 25 25 24 20 19
R11 | 1416 10 24 9 8 9 13 5 | 10 29 19 16 19 15 14
R12 | 1056 11 23 13 14 15 13 6 | 38 35 35 28 36 31 32
R14 | 658 4 13 20 8 14 31 7 | 48 51 63 53 51 33 49
R15 | 890 18 12 16 6 20 28 8 | 59 46 47 45 55 31 47
R16 | 726 12 20 14 9 14 13 6 | 65 56 67 58 68 53 61
R17E | 4798 12 14 12 14 14 11 6 | 141 143 150 135 140 142 141
R18E | 747 11 20 14 18 13 17 7 | 22 26 28 28 20 19 21
R19E | 4538 18 27 16 18 17 13 8 | 78 67 75 76 72 78 74
R20E | 1771 30 35 41 27 32 49 16 | 56 65 77 64 53 55 55
R21E | 934 20 18 13 30 17 12 8 | 130 126 122 136 118 130 126
R22E | 2364 19 20 11 13 23 11 7 | 18 33 23 27 34 20 22
R24E | 640 15 26 21 22 20 16 9 | 49 60 56 56 48 42 49
XR26 |>>>>> 44 80 1072 --- --- --- 59 | 35 110 687 --- --- --- 57
------+-----------------------------------------+-------------------------------------
RMS | 1821 16 26 17 19 16 21 |T 57 57 90 60 55 51 55
WRMS | 1821 12 23 15 18 15 21 |NE 51 49 98 53 48 41 48
MEDI | 934 12 20 14 16 14 16 |MD 56 49 63 58 51 42 54
Table 3.2354.4 GPS week: 2354 Day: 4 MJD: 60726
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1469 33 60 24 17 18 18 13 | 85 38 59 65 63 90 66
R02 | 871 11 35 15 14 22 16 8 | 50 43 53 56 41 33 47
R03 | 1481 7 19 11 16 8 20 6 | 54 47 52 53 46 43 49
R04 | 488 14 16 18 22 9 11 7 | 69 56 76 50 60 57 60
R05 | 1081 12 19 20 18 17 7 7 | 58 46 48 54 49 48 49
R07 | 1133 17 14 18 11 26 20 8 | 63 48 44 46 69 48 52
R08 | 704 12 18 17 18 18 25 8 | 58 60 69 56 63 52 58
R09 | 1308 17 17 18 10 8 13 6 | 27 37 34 29 24 32 27
R11 | 733 16 14 15 19 17 22 8 | 14 26 24 25 32 24 20
R12 | 1604 14 30 9 11 16 18 7 | 49 43 45 36 49 49 43
R14 | 1370 10 19 18 7 15 10 6 | 58 58 58 53 46 52 53
R15 | 586 29 15 9 9 16 27 8 | 76 67 61 68 58 58 63
R16 | 1204 17 24 15 12 21 19 8 | 76 70 73 61 63 54 64
R17E | 2073 12 19 18 19 11 10 6 | 84 85 94 70 81 76 80
R18E | 831 11 17 21 15 11 14 6 | 28 27 30 25 27 26 24
R19E | 4541 21 19 24 26 17 17 9 | 166 163 163 161 177 174 167
R20E | 1955 39 56 85 41 43 43 23 | 71 86 117 82 67 62 68
R21E | 1190 16 29 14 13 14 11 7 | 152 142 153 150 150 152 150
R22E | 5117 15 21 13 11 22 9 7 | 12 29 24 25 29 15 18
R24E | 970 14 22 13 22 21 18 8 | 54 54 51 57 50 62 52
XR26 |>>>>> 41 62 1033 --- --- --- 50 | 24 74 578 --- --- --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1933 19 27 25 18 19 19 |T 63 61 90 61 62 60 59
WRMS | 1933 16 21 17 14 18 19 |NE 54 50 91 50 51 49 49
MEDI | 1204 15 19 18 15 17 17 |MD 58 54 58 54 50 52 52
Table 3.2354.5 GPS week: 2354 Day: 5 MJD: 60727
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1805 19 65 16 27 21 23 13 | 82 48 89 85 92 65 78
R02 | 969 16 31 13 14 14 14 7 | 51 40 49 43 38 25 42
R03 | 1729 10 21 15 15 13 17 6 | 54 48 58 52 45 44 50
R04 | 590 8 27 13 19 13 14 7 | 66 67 68 71 55 56 63
R05 | 474 9 37 17 21 10 10 8 | 59 53 72 65 57 54 59
R07 | 1231 9 19 15 11 20 14 6 | 51 54 58 58 66 52 55
R08 | 650 9 26 14 19 28 21 9 | 46 47 34 35 59 30 39
R09 | 1106 13 20 12 13 17 9 6 | 35 42 39 42 38 29 36
R11 | 846 21 27 11 26 17 18 9 | 17 37 23 43 33 31 25
R12 | 1551 12 18 13 15 9 12 6 | 46 52 51 38 44 34 43
R14 | 1857 9 12 10 14 12 10 5 | 42 40 35 35 32 45 37
R15 | 1418 24 15 15 7 10 22 7 | 64 60 66 66 61 56 61
R16 | 1075 18 15 15 14 15 32 8 | 61 51 55 60 60 44 54
R17E | 1180 13 18 14 17 16 15 7 | 127 135 124 125 125 122 125
R18E | 740 10 22 11 12 10 9 5 | 22 28 18 23 20 20 19
R19E | 3374 20 22 12 25 20 20 9 | 145 147 142 148 140 156 145
R20E | 1952 30 55 52 45 41 60 21 | 63 78 75 71 59 57 59
R21E | 1914 16 29 13 19 20 11 8 | 147 144 139 141 140 140 142
R22E | 4895 15 24 13 17 13 13 7 | 17 27 27 30 27 22 21
R24E | 1067 17 21 22 17 21 12 8 | 55 57 65 55 57 55 55
XR26 |>>>>> 32 66 1022 --- --- --- 46 | 24 67 497 --- --- --- 32
------+-----------------------------------------+-------------------------------------
RMS | 1824 16 29 18 20 18 21 |T 60 62 84 64 62 56 59
WRMS | 1824 14 24 13 18 17 21 |NE 49 50 85 53 52 43 48
MEDI | 1231 15 22 14 17 15 14 |MD 54 52 58 55 57 45 54
Table 3.2354.6 GPS week: 2354 Day: 6 MJD: 60728
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1766 16 55 24 24 20 15 11 | 101 57 102 102 102 90 94
R02 | 806 7 21 11 10 12 9 5 | 64 62 64 60 64 39 61
R03 | 1969 16 18 14 24 17 19 8 | 74 66 67 80 64 58 67
R04 | 625 11 23 11 14 11 11 6 | 86 81 89 83 75 76 81
R05 | 1074 8 33 9 15 12 12 6 | 76 78 71 78 65 67 71
R07 | 1153 9 16 14 16 13 7 5 | 73 70 67 78 63 67 69
R08 | 670 13 20 16 8 16 17 7 | 66 65 59 61 66 51 60
R09 | 1055 10 32 18 14 14 16 7 | 40 41 47 36 40 42 40
R11 | 1358 13 24 10 9 17 11 6 | 26 38 32 35 35 31 30
R12 | 1380 15 24 22 23 12 15 8 | 63 64 66 48 65 46 56
R14 | 1764 12 16 10 15 16 10 6 | 64 65 59 52 53 53 56
R15 | 2237 22 14 20 7 22 10 7 | 86 85 85 83 77 76 80
R16 | 1092 15 17 15 10 17 13 6 | 83 79 87 83 84 73 80
R17E | 808 14 13 14 14 21 15 7 | 123 119 120 121 118 124 121
R18E | 583 9 21 15 12 12 9 5 | 24 36 26 27 28 20 24
R19E | 1925 15 31 18 22 22 14 9 | 199 198 195 198 191 208 197
R20E | 3221 27 59 50 41 43 55 20 | 76 104 88 78 74 70 74
R21E | 3862 12 29 13 21 16 10 7 | 184 176 180 183 185 182 182
R22E | 4574 13 22 20 15 19 9 7 | 32 43 39 39 37 35 34
R24E | 836 12 20 20 26 17 13 8 | 67 60 69 76 64 69 66
XR26 |>>>>> 32 78 1021 --- --- --- 50 | 36 115 745 --- --- --- 58
------+-----------------------------------------+-------------------------------------
RMS | 1959 14 28 19 19 19 17 |T 78 81 112 80 77 73 76
WRMS | 1959 13 30 15 14 17 17 |NE 67 69 117 67 65 59 64
MEDI | 1358 13 22 15 15 16 12 |MD 73 66 69 78 65 67 67
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