[IGSREPORT-30208] Wk 2341 IGLOS Final Orbits
acc
acc at igs.org
Fri Dec 6 02:44:40 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2341 (Nov 17, 2024 - Nov 23, 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 2.2341.
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:
igl2341[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2341 in the SP3 format.
igl23417.sum Combination Report for GPS Week 2341.
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 | 7.8 ns
2 | 8.7 ns
3 | 6.1 ns
4 | 12.5 ns
5 | 15.0 ns
6 | 9.0 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 1.2341, 1a.2341).
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 2.2341.0-6)
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 3.2341.0-6).
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 2341 summary. (Nov 17, 2024 - Nov 23, 2024)
Table 1.2341.a GPS week : 2341 MJD: 60631.0-60637.0
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 2 -2 -18 71 .19 21 17 | 6334 -653 3049 9324
| 0 0 2 10 15 18 .03 | 3966 2241
esa n/a| 0 0 0 -15 6 16 -.13 27 20 | 14429 -1064 3028 7717
| 1 0 2 8 8 21 .04 | 4028 1906
gfz n/a| 0 1 0 32 20 -3 -.02 19 15 | 0 -631 3031 7304
| 0 1 3 16 19 18 .04 | 0 2210
grg n/a| 0 -1 7 -16 -26 -47 .31 27 19 | 8197 -686 3046 8887
| 1 1 2 20 10 45 .03 | 3302 2115
iac n/a| 0 0 -7 4 9 -38 -.12 15 14 | 11909 -1057 3029 8844
| 1 1 2 24 20 30 .02 | 3441 1084
jgx n/a| 0 -1 4 -21 -10 14 -.15 24 24 | 8923 -720 2999 7441
| 0 1 1 14 13 34 .06 | 3991 2217
Table 1.2341.b GPS week : 2341 MJD: 60631.0-60637.0
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 15 16 15 13 14 14 |
R02 | --- 0 0 0 19 13 14 |
R03 | 8 8 6 6 7 8 8 |
R04 | 8 8 8 7 8 7 10 |
R05 | 5 7 6 6 7 7 8 |
R07 | 7 6 8 8 6 7 9 |
R08 | 7 6 5 7 7 6 7 |
R09 | 6 7 7 7 6 7 6 |
R11 | 8 6 5 7 8 6 7 |
R12 | 7 7 8 7 8 8 8 |
R14 | 7 6 8 6 7 7 6 |
R15 | 8 8 10 7 7 7 8 |
R16 | 8 7 8 8 8 7 7 |
R17 | 6 7 6 8 6 6 6 |
R18 | 7 7 7 8 7 6 6 |
R19 | 20 20 20 21 20 20 19 |
R20 | 18 17 20 18 23 21 25 |
R21 | 6 6 7 5 8 6 7 |
R22 | 9 5 5 7 6 7 6 |
R24 | 7 6 7 9 7 8 8 |
R26 | 36 33 34 33 35 37 30 |
Table 1.2341.c GPS week : 2341 MJD: 60631.0-60637.0
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 2341 0 | 47 71 -46 -1335 1787 -4134 82.9 1673 1673 | 5207 0
brd 2341 1 | -38 69 -16 395 1903 -11330 81.1 1811 1811 | 7785 0
brd 2341 2 | 25 -13 -67 964 135 -5879 79.9 1596 1596 | 8749 0
brd 2341 3 | -12 -21 -162 406 -23 4828 80.9 1674 1674 | 6052 0
brd 2341 4 | -14 48 -114 -1451 -3362 3062 82.0 1680 1680 | 12496 0
brd 2341 5 | -10 45 33 -1900 -1038 -1177 81.4 1494 1494 | 14999 0
brd 2341 6 | 2 52 -17 -2621 1220 -1197 80.0 1245 1245 | 9043 0
-------------+------------------------------------------------------------+----------------
brd 2341 mean| 0 35 -55 -791 88 -2261 81.2 1596 1596 | 9190 0
brd 2341 sdev| 28 38 65 1368 1855 5473 1.1 182 182 | 3477 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 2.2341.0 GPS week: 2341 Day: 0 MJD: 60631
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 0 -20 74 .18 19 17 | -29 74 3209 8489
esa n/a| -1 0 0 -8 9 38 -.12 26 21 | 16724 454 3127 7510
gfz n/a| 0 2 -4 24 -7 -13 -.01 18 16 | 0 313 3120 7122
grg n/a| 2 -3 3 15 -11 6 .30 26 20 | 4069 138 3216 8044
iac n/a| 0 0 -4 -33 29 -36 -.13 14 14 | 8662 -2294 3197 8257
jgx n/a| -1 -1 5 -35 -6 -25 -.12 26 26 | 2696 147 3039 7200
Table 2.2341.1 GPS week: 2341 Day: 1 MJD: 60632
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 2 10 4 64 .15 21 17 | 4053 1920 2937 8658
esa n/a| 1 0 3 -22 7 -19 -.08 26 19 | 9324 952 2921 7983
gfz n/a| 0 1 -5 1 3 -7 .03 19 14 | 0 1572 2922 6609
grg n/a| 2 -2 9 -34 -27 -70 .28 26 20 | 6057 1388 2959 8151
iac n/a| 0 0 -5 7 33 9 -.13 12 11 | 10309 60 2916 8086
jgx n/a| -1 0 2 -3 -31 16 -.10 24 24 | 7181 1544 2941 6685
Table 2.2341.2 GPS week: 2341 Day: 2 MJD: 60633
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 -6 -10 57 .20 23 20 | 6426 560 3451 9509
esa n/a| 0 0 0 -1 -10 22 -.13 24 20 | 11321 315 3465 7305
gfz n/a| 0 -1 1 25 26 0 -.03 21 18 | 0 822 3472 7549
grg n/a| 0 0 10 -42 -35 14 .30 25 18 | 6983 698 3426 9138
iac n/a| 2 0 -9 22 5 -82 -.09 15 14 | 11212 523 3430 9037
jgx n/a| -2 -2 1 -17 -24 22 -.19 25 25 | 8922 1284 3401 7656
Table 2.2341.3 GPS week: 2341 Day: 3 MJD: 60634
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 -21 -34 101 .19 21 15 | 4694 -3254 3100 9543
esa n/a| 1 0 1 -17 4 17 -.15 21 16 | 20806 -2859 3115 9629
gfz n/a| 1 1 -1 39 28 -18 -.01 19 15 | 0 -2454 3120 7474
grg n/a| 0 0 7 -29 -31 -26 .38 25 21 | 5813 -2406 3117 9039
iac n/a| 0 -1 -9 44 11 -43 -.13 16 16 | 8653 -1188 3087 8878
jgx n/a| 0 -2 5 -6 -3 -33 -.15 25 25 | 6470 -2791 3112 7504
Table 2.2341.4 GPS week: 2341 Day: 4 MJD: 60635
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 2 3 -41 70 .24 20 18 | 9773 -655 2721 9746
esa n/a| 0 1 2 -13 3 17 -.11 28 18 | 11177 -1517 2691 7257
gfz n/a| 0 3 2 40 8 22 -.10 20 17 | 0 -761 2686 7441
grg n/a| 0 0 9 -7 -13 -98 .32 33 23 | 11325 -687 2737 9282
iac n/a| 2 -2 -11 -7 22 -37 -.11 14 13 | 15497 -618 2704 9201
jgx n/a| 0 0 5 -19 -6 15 -.08 23 23 | 12480 -834 2726 7693
Table 2.2341.5 GPS week: 2341 Day: 5 MJD: 60636
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 -9 88 .19 21 15 | 12095 933 2751 9814
esa n/a| 0 0 -1 -24 17 -3 -.14 32 23 | 16619 -590 2741 6970
gfz n/a| 0 0 -1 45 46 -25 -.05 16 11 | 0 748 2739 7495
grg n/a| 0 -1 6 -17 -40 -76 .30 27 18 | 13011 652 2751 9429
iac n/a| 0 0 -5 -7 -13 -15 -.15 15 15 | 17709 -2004 2740 9259
jgx n/a| 0 -1 4 -43 9 56 -.16 24 24 | 14757 144 2647 7677
Table 2.2341.6 GPS week: 2341 Day: 6 MJD: 60637
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 0 -6 -20 45 .17 19 18 | 7330 -4154 3179 9509
esa n/a| 2 0 -2 -23 13 40 -.20 35 25 | 15033 -4207 3138 7368
gfz n/a| 0 2 3 51 38 21 .01 18 14 | 0 -4657 3161 7438
grg n/a| 1 -2 4 -2 -27 -81 .29 30 15 | 10122 -4587 3122 9126
iac n/a| 0 0 -8 5 -19 -63 -.13 17 16 | 11323 -1882 3132 9194
jgx n/a| 0 0 3 -24 -8 52 -.27 24 24 | 9960 -4537 3131 7675
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 3.2341.0 GPS week: 2341 Day: 0 MJD: 60631
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 595 49 25 17 16 10 45 13 | 98 44 48 61 65 27 57
R03 | 904 11 16 24 11 14 24 7 | 83 77 95 79 74 61 78
R04 | 1114 25 7 12 21 10 21 7 | 102 94 88 84 97 84 91
R05 | 1470 15 13 9 14 6 11 5 | 91 95 87 83 90 22 88
R07 | 1256 11 18 14 18 12 18 6 | 76 63 85 85 77 63 75
R08 | 1119 15 12 13 21 14 21 7 | 67 71 68 77 73 57 68
R09 | 2922 16 13 12 12 13 8 6 | 30 40 33 28 34 29 31
R11 | 1305 16 16 15 15 15 22 7 | 29 44 35 30 34 26 30
R12 | 562 14 17 13 13 13 27 7 | 70 68 67 60 65 51 63
R14 | 767 14 17 11 20 15 14 6 | 61 73 66 62 72 52 64
R15 | 903 17 8 13 25 14 23 7 | 96 82 83 73 91 71 83
R16 | 829 16 13 17 16 12 25 7 | 100 78 91 82 94 74 87
R17 | 1004 11 14 10 8 19 14 6 | 26 22 29 25 29 20 23
R18 | 857 10 25 11 18 14 16 7 | 26 24 28 33 27 25 25
R19 | 1392 23 62 14 78 18 55 19 | 32 34 29 37 30 42 29
R20 | 5000 19 62 48 40 20 36 17 | 27 24 47 24 22 29 20
R21 | 1098 10 18 15 10 13 14 6 | 26 21 22 28 25 23 21
XR22 | 894 17 10 9 23 23 --- 9 | 32 32 37 39 36 --- 33
R24 | 664 17 22 12 17 12 17 7 | 26 30 24 25 24 19 22
XR26 |14959 43 --- --- 51 54 --- 35 | 44 --- --- 34 97 --- 61
------+-----------------------------------------+-------------------------------------
RMS | 1673 19 26 18 26 14 26 |T 57 53 55 52 57 43 52
WRMS | 1673 17 21 16 20 14 26 |NE 57 53 55 52 57 43 52
MEDI | 1004 16 16 13 17 14 21 |MD 44 44 48 39 65 29 57
Table 3.2341.1 GPS week: 2341 Day: 1 MJD: 60632
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 926 55 30 24 38 16 39 15 | 75 39 46 44 54 39 47
XR02 | ---- 4 --- --- --- --- --- 0 | 62 --- --- --- --- --- 63
R03 | 1758 11 12 13 35 12 13 7 | 57 55 64 69 54 52 56
R04 | 1135 18 11 17 11 16 24 7 | 79 78 73 78 83 65 76
XR05 | 1720 9 16 17 14 12 --- 7 | 74 75 63 67 75 --- 70
R07 | 938 11 11 19 15 7 15 5 | 54 48 63 50 51 47 52
R08 | 757 13 11 10 23 7 15 5 | 50 53 55 64 51 48 52
R09 | 2937 13 12 14 24 13 13 6 | 27 33 32 25 30 29 27
R11 | 1466 15 14 12 11 10 16 5 | 26 39 39 31 31 23 30
R12 | 755 12 13 15 14 11 24 6 | 52 47 54 50 44 37 46
R14 | 1579 9 14 10 21 9 22 6 | 41 49 51 49 51 33 46
R15 | 986 22 14 16 25 11 24 8 | 69 49 63 47 58 49 55
R16 | 2147 14 16 11 22 11 21 7 | 69 57 63 56 70 53 62
R17 | 932 9 11 19 19 10 19 6 | 20 22 29 24 23 18 20
R18 | 464 13 22 11 19 11 14 6 | 21 25 21 26 21 16 19
R19 | 1192 27 70 29 62 22 57 19 | 46 30 45 29 30 29 30
R20 | 4796 34 61 50 33 15 26 17 | 30 27 40 28 29 29 26
R21 | 740 10 14 14 13 11 19 6 | 22 22 27 28 17 20 20
R22 | 2561 13 10 8 15 9 11 5 | 22 27 33 32 26 31 27
R24 | 555 19 12 15 13 11 15 6 | 29 27 24 26 24 19 21
XR26 |15653 46 --- --- 54 43 --- 33 | 34 --- --- 25 53 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1811 21 26 19 26 12 24 |T 45 42 46 42 43 35 42
WRMS | 1811 17 19 14 20 11 24 |NE 45 42 46 42 43 35 42
MEDI | 1135 13 14 15 19 11 19 |MD 46 39 46 32 44 31 46
Table 3.2341.2 GPS week: 2341 Day: 2 MJD: 60633
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1115 48 28 16 32 22 54 15 | 70 31 45 28 61 20 42
XR02 | ---- 4 --- --- --- --- --- 0 | 75 --- --- --- --- --- 74
R03 | 1855 8 12 10 22 9 14 6 | 54 54 52 50 54 44 51
R04 | 1975 18 11 18 19 14 25 8 | 70 53 67 52 61 48 58
XR05 | 1425 13 9 15 13 9 --- 6 | 76 80 86 75 77 --- 78
R07 | 1072 11 18 7 21 23 13 7 | 64 50 56 48 74 53 58
R08 | 1228 12 11 10 12 10 15 5 | 62 61 53 57 59 50 56
R09 | 1134 14 21 17 11 10 10 6 | 22 36 25 18 26 24 22
R11 | 2703 12 11 13 12 11 10 5 | 29 35 41 33 39 29 33
R12 | 742 17 14 20 19 19 16 8 | 58 57 47 45 64 45 51
R14 | 1250 20 13 10 10 13 29 7 | 52 60 55 62 64 47 56
R15 | 777 8 21 26 11 13 36 9 | 70 70 87 65 72 49 69
R16 | 1516 17 17 15 25 15 22 8 | 68 68 68 52 65 54 61
R17 | 943 10 12 9 22 8 16 6 | 21 19 21 28 16 18 17
R18 | 620 16 17 13 18 11 16 6 | 19 16 22 23 17 19 16
R19 | 1858 54 60 19 61 26 34 19 | 30 30 30 27 18 25 20
R20 | 2822 39 49 62 44 22 41 19 | 40 26 47 47 25 57 32
R21 | 852 11 20 15 14 15 17 7 | 27 23 22 23 21 15 19
R22 | 2479 13 8 14 9 9 13 5 | 24 26 32 27 29 23 26
R24 | 1191 10 22 13 24 10 12 7 | 21 25 19 24 18 19 17
XR26 |18581 37 --- --- 47 54 --- 34 | 29 --- --- 24 70 --- 43
------+-----------------------------------------+-------------------------------------
RMS | 1596 23 24 21 25 15 25 |T 46 43 46 40 46 35 42
WRMS | 1596 20 20 18 18 14 25 |NE 46 43 46 40 46 35 42
MEDI | 1228 13 17 15 19 13 16 |MD 52 36 47 33 54 29 43
Table 3.2341.3 GPS week: 2341 Day: 3 MJD: 60634
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 545 51 30 20 23 17 51 15 | 79 30 50 46 63 18 47
XR02 | 9048 7 --- --- --- --- --- 0 | 51 --- --- --- --- --- 51
R03 | 2532 6 14 15 19 7 12 5 | 63 53 69 79 62 70 64
R04 | 2386 16 10 21 15 14 13 7 | 58 49 51 46 44 45 47
R05 | 1200 9 15 16 11 12 16 6 | 50 42 61 49 56 21 49
R07 | 1061 13 8 13 18 24 23 7 | 70 62 64 55 85 47 65
R08 | 904 10 12 13 10 20 21 6 | 68 63 70 69 84 54 68
R09 | 1470 13 18 14 16 19 13 7 | 17 29 25 28 33 21 22
R11 | 2303 13 16 9 19 15 18 6 | 38 59 47 52 47 37 46
R12 | 572 13 11 18 14 14 17 6 | 69 70 62 65 71 56 65
R14 | 812 13 11 10 11 16 18 6 | 55 65 58 65 66 51 60
R15 | 718 12 13 18 12 8 24 6 | 67 59 75 67 65 51 64
R16 | 896 21 20 12 14 10 20 7 | 65 67 67 57 61 50 60
R17 | 1243 8 15 11 21 13 30 7 | 19 22 25 24 19 16 17
R18 | 637 14 25 15 11 11 24 7 | 26 21 23 23 20 23 20
R19 | 1849 45 55 30 74 26 45 21 | 42 41 32 29 23 33 27
R20 | 1828 40 40 38 49 25 47 17 | 29 31 53 37 22 59 33
R21 | 1053 8 11 9 16 9 13 5 | 20 20 21 25 18 15 17
R22 | 4127 13 10 22 14 18 10 7 | 17 27 30 25 32 24 22
R24 | 884 14 11 31 16 19 13 8 | 22 18 35 24 19 17 18
XR26 |10714 41 --- --- 36 54 --- 32 | 31 --- --- 32 65 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1673 21 21 19 25 16 25 |T 45 43 48 44 47 37 43
WRMS | 1673 15 16 15 21 16 25 |NE 45 43 48 44 47 37 43
MEDI | 1200 13 14 15 16 15 18 |MD 50 42 51 46 47 37 47
Table 3.2341.4 GPS week: 2341 Day: 4 MJD: 60635
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 987 43 22 20 36 11 31 12 | 73 43 43 41 56 35 48
XR02 | 6394 17 --- 19 --- --- --- 18 | 66 --- 24 --- --- --- 57
R03 | 1346 7 19 16 14 14 15 6 | 68 57 69 72 77 61 68
R04 | 2237 22 11 28 11 10 14 8 | 71 60 52 60 67 60 60
XR05 | 2152 13 21 11 13 10 --- 6 | 62 74 63 60 61 --- 62
R07 | 792 12 15 11 16 12 10 5 | 66 51 61 61 73 58 63
R08 | 1077 11 12 17 21 14 14 6 | 70 62 59 60 77 61 65
R09 | 1397 15 17 15 22 9 8 6 | 20 33 32 18 30 24 25
R11 | 2004 14 22 24 11 12 10 7 | 20 37 25 25 29 28 24
R12 | 785 10 15 17 23 14 24 7 | 58 60 65 51 68 45 58
R14 | 871 10 19 15 17 11 21 7 | 57 63 49 42 57 38 51
R15 | 1041 12 18 12 11 13 27 7 | 69 58 66 71 67 53 64
R16 | 565 13 19 17 27 12 24 8 | 71 62 66 85 65 54 65
R17 | 639 6 9 15 17 7 22 6 | 24 19 27 22 23 22 21
R18 | 658 12 18 13 24 14 16 7 | 23 18 20 23 22 22 19
R19 | 1945 42 66 22 80 16 44 19 | 30 44 31 33 32 30 30
R20 | 1188 35 77 49 74 34 48 22 | 31 72 67 26 27 42 34
R21 | 1568 13 19 15 34 11 14 7 | 24 20 24 36 18 16 17
R22 | 4798 17 11 12 13 13 13 6 | 38 38 43 41 41 30 39
R24 | 959 14 10 15 25 14 21 7 | 26 21 23 26 27 21 21
XR26 | 8816 45 --- --- 54 49 --- 34 | 32 --- --- 33 65 --- 43
------+-----------------------------------------+-------------------------------------
RMS | 1679 20 28 20 33 14 23 |T 47 46 45 44 49 38 44
WRMS | 1679 18 18 17 23 13 23 |NE 47 46 45 44 49 38 44
MEDI | 1188 13 18 15 21 12 16 |MD 57 51 43 41 56 35 48
Table 3.2341.5 GPS week: 2341 Day: 5 MJD: 60636
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1328 52 19 17 30 17 37 13 | 60 48 44 35 31 35 36
XR02 | 6449 14 --- 18 --- 21 --- 13 | 53 --- 26 --- 22 --- 63
R03 | 662 7 20 12 16 22 30 8 | 60 48 66 51 76 38 59
R04 | 1439 20 16 15 10 12 14 6 | 66 54 63 61 53 54 58
XR05 | 1821 8 20 13 18 13 --- 7 | 64 72 64 69 60 --- 63
R07 | 676 10 18 12 13 15 20 6 | 58 49 58 62 60 51 56
R08 | 681 12 12 11 13 9 24 6 | 51 60 60 57 55 55 55
R09 | 2226 13 16 17 11 14 14 6 | 22 28 31 23 21 31 24
R11 | 1088 12 20 12 10 10 19 6 | 35 41 35 38 32 42 35
R12 | 1252 12 18 26 17 13 16 8 | 63 67 49 59 56 58 56
R14 | 1387 16 16 7 13 17 17 6 | 50 63 55 57 64 45 55
R15 | 993 13 12 9 19 18 17 6 | 71 60 63 60 73 56 64
R16 | 604 16 18 10 14 10 25 7 | 71 61 66 77 69 56 66
R17 | 1182 6 9 12 8 11 23 5 | 26 23 26 32 20 19 22
R18 | 900 10 23 9 15 10 15 6 | 25 28 25 23 24 22 23
R19 | 2109 41 75 20 71 13 38 19 | 24 40 45 32 28 24 28
R20 | 2108 27 88 32 64 23 39 20 | 25 56 35 40 32 52 30
R21 | 1094 14 19 7 16 8 14 5 | 23 25 25 32 21 20 22
R22 | 3355 16 14 13 9 18 10 6 | 19 27 31 27 26 21 24
R24 | 642 10 20 18 16 17 26 8 | 28 26 27 31 24 20 23
XR26 |10480 37 --- --- 55 58 --- 36 | 25 --- --- 36 63 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1493 21 32 16 26 15 24 |T 43 46 44 45 43 38 42
WRMS | 1493 15 23 11 18 15 24 |NE 43 46 44 45 43 38 42
MEDI | 1252 13 18 12 15 14 19 |MD 50 48 44 38 32 38 39
Table 3.2341.6 GPS week: 2341 Day: 6 MJD: 60637
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 917 37 42 28 11 29 31 13 | 101 54 76 59 63 49 66
XR02 | 5692 18 --- 16 --- 23 --- 13 | 74 --- 28 --- 24 --- 75
R03 | 862 10 21 15 11 21 24 7 | 89 72 93 84 99 71 86
R04 | 838 17 21 22 16 10 36 9 | 94 76 86 81 82 65 81
XR05 | 990 12 15 16 14 19 --- 8 | 103 110 111 110 97 --- 104
R07 | 772 12 19 15 12 23 36 9 | 86 87 87 91 96 69 85
R08 | 626 8 12 13 16 15 27 7 | 75 79 77 86 88 67 78
R09 | 2124 13 16 9 13 11 15 5 | 26 32 26 26 23 20 23
R11 | 906 13 22 15 11 13 12 6 | 30 37 33 27 34 36 30
R12 | 1129 14 25 9 25 13 19 7 | 73 75 65 56 66 58 64
R14 | 888 8 21 13 20 13 9 6 | 61 75 59 67 66 54 62
R15 | 1215 9 12 15 18 21 23 7 | 89 81 90 76 91 66 83
R16 | 949 11 18 15 13 18 17 7 | 84 73 79 91 89 70 81
R17 | 690 12 15 11 11 12 13 5 | 26 27 32 32 28 20 26
R18 | 878 9 22 10 7 12 18 5 | 23 23 22 24 22 18 20
R19 | 1487 39 71 16 61 22 38 18 | 25 26 23 27 17 19 17
R20 | 1951 44 99 41 94 25 30 25 | 63 50 39 49 28 41 34
R21 | 823 7 22 10 18 14 25 7 | 24 25 24 31 23 20 22
R22 | 2559 10 11 16 15 11 10 5 | 23 29 36 31 28 18 27
R24 | 590 12 27 16 19 14 23 8 | 37 26 39 34 29 26 29
XR26 | 8910 35 --- --- 32 54 --- 30 | 26 --- --- 31 69 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1245 19 35 18 30 17 24 |T 58 55 56 55 55 43 53
WRMS | 1245 18 25 14 15 16 24 |NE 58 55 56 55 55 43 53
MEDI | 917 12 21 15 15 15 23 |MD 63 54 39 49 63 41 62
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