[IGSREPORT-30275] Wk 2347 IGLOS Final Orbits
acc
acc at igs.org
Mon Jan 20 00:08:39 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2347 (Dec 29, 2024 - Jan 04, 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 2.2347.
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:
igl2347[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2347 in the SP3 format.
igl23477.sum Combination Report for GPS Week 2347.
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 | 11.6 ns
1 | 0.2 ns
2 | 1.5 ns
3 | 5.2 ns
4 | 5.8 ns
5 | 8.9 ns
6 | 3.7 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 1.2347, 1a.2347).
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 2.2347.0-6)
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 3.2347.0-6).
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 2347 summary. (Dec 29, 2024 - Jan 04, 2025)
Table 1.2347.a GPS week : 2347 MJD: 60673.0-60679.0
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 10 -15 53 .17 20 17 | 7252 68 3627 8928
| 1 1 1 14 29 38 .03 | 3102 2330
esa n/a| 0 -1 -1 -12 4 1 -.12 35 24 | 10092 -704 3624 7597
| 1 1 1 9 27 35 .04 | 4756 1804
gfz n/a| 1 0 6 1 3 10 -.03 25 18 | 0 -146 3681 8038
| 1 1 3 20 12 51 .05 | 0 2182
grg n/a| 0 0 2 -36 -34 -54 .31 27 20 | 4793 8 3632 8618
| 0 1 2 30 29 40 .03 | 3650 2031
iac n/a| 0 0 -4 12 37 -27 -.05 19 17 | 6210 -20 3624 8814
| 1 1 1 22 35 63 .03 | 3545 891
jgx n/a| 0 0 -3 3 -6 -14 -.27 25 24 | 9716 -107 3711 8237
| 1 0 2 24 14 20 .04 | 3400 2359
Table 1.2347.b GPS week : 2347 MJD: 60673.0-60679.0
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 | 17 18 13 18 18 16 16 |
R02 | 6 6 8 8 5 6 7 |
R03 | 7 7 7 10 7 7 6 |
R04 | 10 7 9 8 6 7 7 |
R05 | 8 8 9 7 7 6 7 |
R07 | 8 8 9 10 7 6 7 |
R08 | 8 8 9 9 8 8 7 |
R09 | 5 6 7 8 6 7 6 |
R11 | 10 10 10 10 10 14 10 |
R12 | 8 9 7 8 6 6 6 |
R14 | 6 7 7 7 7 7 6 |
R15 | 9 10 8 9 8 8 5 |
R16 | 8 8 9 8 8 7 8 |
R17 | 8 7 7 8 8 7 7 |
R18 | 8 8 7 8 8 7 6 |
R19 | 18 20 19 17 16 21 22 |
R20 | 26 28 28 25 25 25 26 |
R21 | 11 7 8 8 8 8 9 |
R22 | 10 8 8 8 8 7 8 |
R24 | 9 11 9 10 9 8 11 |
R26 | 31 31 30 30 35 34 35 |
Table 1.2347.c GPS week : 2347 MJD: 60673.0-60679.0
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 2347 0 | 7 -75 -1 -1372 -2164 -6242 81.7 1895 1895 | 11612 0
brd 2347 1 | 9 19 33 -1283 -2397 -4291 81.2 1539 1539 | 207 0
brd 2347 2 | -103 154 25 -2559 -2161 -3163 81.1 7162 7162 | 1477 0
brd 2347 3 | -3 42 38 -1290 -1362 -2364 80.7 1649 1649 | 5217 0
brd 2347 4 | -61 -27 -25 -3673 -1273 2669 81.4 1696 1696 | 5795 0
brd 2347 5 | -2 -10 -78 -880 -1650 -1280 77.6 1751 1751 | 8887 0
brd 2347 6 | 134 18 -29 -2630 841 1644 78.9 1455 1455 | 3709 0
-------------+------------------------------------------------------------+----------------
brd 2347 mean| -2 17 -5 -1955 -1452 -1861 80.4 2449 2449 | 5272 0
brd 2347 sdev| 73 71 42 1013 1098 3167 1.5 2082 2082 | 4000 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 2.2347.0 GPS week: 2347 Day: 0 MJD: 60673
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 2 10 -50 90 .14 21 19 | 13104 819 3571 8817
esa n/a| 0 -2 1 -15 55 40 -.14 34 23 | 19318 14 3624 7270
gfz n/a| 4 0 5 -18 18 102 -.05 27 18 | 0 247 3633 7851
grg n/a| 0 2 4 -18 -20 -76 .32 25 21 | 10681 824 3574 8701
iac n/a| -1 -2 -3 -8 20 -154 -.08 22 20 | 10847 711 3571 8690
jgx n/a| 0 1 -7 10 0 6 -.21 22 22 | 16205 588 3681 8108
Table 2.2347.1 GPS week: 2347 Day: 1 MJD: 60674
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 0 4 -41 54 .14 26 19 | 4176 423 3452 9230
esa n/a| 0 0 0 -3 20 31 -.13 30 18 | 8183 -216 3489 6431
gfz n/a| 0 -1 5 18 -12 -14 -.02 23 16 | 0 952 3510 7899
grg n/a| 0 0 3 16 -58 -91 .26 27 20 | -903 837 3469 8778
iac n/a| -1 0 -7 -20 31 -12 -.06 22 20 | 1405 -148 3459 9055
jgx n/a| 0 0 -3 33 15 -31 -.25 27 27 | 6907 529 3513 8264
Table 2.2347.2 GPS week: 2347 Day: 2 MJD: 60675
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 4 -4 -37 37 .21 21 17 | 5604 -3757 3756 7742
esa n/a| 0 0 -1 -18 2 -22 -.06 35 20 | 5300 -4147 3787 6264
gfz n/a| 1 -1 10 -20 17 55 .02 25 17 | 0 -3687 3819 6605
grg n/a| 0 0 -1 -61 -22 -78 .28 30 20 | 2641 -3368 3751 7246
iac n/a| 2 2 -5 23 70 2 -.08 19 18 | 2049 520 3750 7416
jgx n/a| -3 0 -6 29 -6 -37 -.24 22 22 | 8126 -4134 3845 6864
Table 2.2347.3 GPS week: 2347 Day: 3 MJD: 60676
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 2 2 26 -4 35 .22 18 16 | 5483 -1093 2938 8522
esa n/a| 1 0 -2 -19 -9 3 -.12 34 22 | 6642 -172 2959 7495
gfz n/a| 2 0 11 -13 1 -9 .02 25 16 | 0 -1540 2943 7854
grg n/a| 0 -2 1 -59 -51 -90 .34 33 20 | 5136 -951 2959 8389
iac n/a| 1 0 -4 6 75 19 -.04 21 19 | 6462 -60 2932 8473
jgx n/a| 0 0 -5 6 -21 -29 -.31 28 26 | 6851 -878 2842 7926
Table 2.2347.4 GPS week: 2347 Day: 4 MJD: 60677
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 -10 14 .16 18 16 | 5376 1415 2943 8772
esa n/a| -3 -2 0 -22 -9 -49 -.11 37 26 | 7595 199 2974 7634
gfz n/a| 0 1 4 13 0 -47 -.11 23 18 | 0 853 2975 8096
grg n/a| 1 0 3 -23 -74 13 .35 27 23 | 5004 666 2953 8486
iac n/a| -1 0 -4 26 48 39 -.05 15 14 | 7607 -1086 2947 8913
jgx n/a| 0 1 0 -31 -1 -19 -.27 28 28 | 8071 776 2955 8403
Table 2.2347.5 GPS week: 2347 Day: 5 MJD: 60678
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 34 2 23 .14 19 16 | 9376 3671 5275 10072
esa n/a| -1 -2 0 -4 2 35 -.08 37 33 | 11927 1356 5057 8845
gfz n/a| 1 0 1 1 9 13 -.07 25 21 | 0 3168 5391 9389
grg n/a| 1 0 2 -65 12 -28 .30 25 19 | 7376 3097 5266 9632
iac n/a| 2 0 -2 45 -30 -29 -.01 18 15 | 9537 1141 5260 9982
jgx n/a| 0 0 -2 -23 -4 -5 -.30 23 23 | 12156 3590 5658 9423
Table 2.2347.6 GPS week: 2347 Day: 6 MJD: 60679
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 -1 31 119 .18 21 16 | 7649 -998 3456 9345
esa n/a| 0 0 -2 0 -30 -25 -.16 36 29 | 11682 -1963 3483 9243
gfz n/a| 0 0 5 32 -8 -22 .01 28 18 | 0 -1018 3498 8578
grg n/a| 1 1 -1 -47 -23 -28 .31 20 18 | 3621 -1044 3458 9094
iac n/a| 0 1 -1 12 44 -53 -.05 18 17 | 5564 -1221 3451 9174
jgx n/a| 0 0 0 0 -30 15 -.32 22 22 | 9700 -1226 3489 8677
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 3.2347.0 GPS week: 2347 Day: 0 MJD: 60673
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 2341 37 32 52 39 37 28 17 | 97 121 125 118 85 112 105
XR02E | 1122 10 11 14 11 13 --- 6 | 46 43 46 49 46 --- 45
R03E | 2271 8 13 19 20 16 15 7 | 50 51 57 59 41 50 49
R04E | 977 14 13 21 27 26 20 9 | 80 82 85 84 79 80 80
R05E | 1263 13 12 12 20 21 18 7 | 60 65 58 69 45 71 60
R07E | 536 8 19 18 27 15 14 7 | 68 68 66 73 68 66 66
R08E | 1019 11 20 20 20 16 14 7 | 62 64 55 64 59 58 59
R09 | 666 9 12 16 7 9 12 5 | 14 15 17 14 14 13 12
R11 | 1521 21 9 21 42 14 17 10 | 26 23 29 24 26 21 20
R12 | 2925 24 14 12 20 19 13 8 | 62 51 46 47 57 50 51
R14 | 804 8 14 14 15 12 10 5 | 59 58 64 53 69 61 60
R15 | 896 17 18 18 15 26 16 8 | 66 53 61 57 56 57 57
R16 | 611 21 22 11 13 19 11 7 | 62 50 59 54 49 46 52
R17 | 1063 17 13 19 13 17 20 7 | 74 59 59 70 75 57 65
R18 | 927 14 17 18 25 12 23 8 | 55 62 54 71 59 46 56
R19 | 904 25 76 36 34 34 30 18 | 118 79 135 124 128 104 113
R20 | 5788 51 99 62 45 31 52 26 | 140 70 138 116 125 80 110
R21 | 565 13 28 31 18 25 22 10 | 89 78 104 90 101 73 88
XR22 | 8242 11 8 23 19 26 --- 9 | 41 43 37 43 51 --- 40
R24 | 552 16 24 19 20 19 21 9 | 75 57 82 89 89 64 75
XR26E |19277 31 --- --- 33 58 --- 30 | 40 --- --- 36 28 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1894 21 34 27 25 22 22 |T 65 59 68 66 64 61 61
WRMS | 1894 19 23 18 21 20 22 |NE 67 53 68 65 69 56 61
MEDI | 1019 14 14 19 20 19 17 |MD 62 58 59 64 59 58 59
Table 3.2347.1 GPS week: 2347 Day: 1 MJD: 60674
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1305 37 23 50 38 40 42 17 | 70 70 91 96 59 84 71
XR02E | 834 11 12 7 14 16 --- 6 | 42 40 49 44 47 --- 43
R03E | 1664 12 13 19 17 19 14 7 | 34 32 34 36 40 36 33
R04E | 1455 11 17 12 19 21 16 7 | 61 56 62 65 55 59 58
R05E | 690 10 16 11 17 23 20 7 | 50 53 42 41 37 40 42
R07E | 888 13 14 13 23 20 19 7 | 54 56 54 52 59 54 53
R08E | 1786 12 21 23 17 15 12 7 | 65 70 62 66 67 65 64
R09 | 829 11 13 14 16 10 11 5 | 11 18 22 18 13 11 10
R11 | 638 17 7 20 43 13 12 9 | 15 24 26 61 28 13 21
R12 | 2805 25 8 18 14 19 27 8 | 51 43 42 37 47 43 41
R14 | 594 6 13 15 15 18 16 6 | 48 41 51 36 55 44 46
R15 | 2210 26 22 18 20 24 14 9 | 43 34 28 38 37 35 32
R16 | 849 19 20 16 18 21 14 8 | 40 40 43 31 37 32 35
R17 | 793 14 12 13 15 16 17 6 | 51 44 50 44 55 42 47
R18 | 1364 14 10 14 19 21 25 8 | 45 50 52 55 52 41 48
R19 | 1270 37 72 29 48 24 43 19 | 90 71 77 93 87 97 80
R20 | 3437 75 83 48 54 33 69 28 | 96 60 65 47 72 48 60
R21 | 425 14 20 10 18 14 15 7 | 57 54 47 55 58 49 52
XR22 | 8304 11 10 20 18 17 --- 8 | 26 27 25 41 37 --- 28
R24 | 756 20 29 20 30 25 26 11 | 46 46 65 77 68 47 56
XR26E |17092 33 --- --- 39 55 --- 31 | 33 --- --- 43 23 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1539 26 30 23 27 22 27 |T 48 46 49 51 49 46 45
WRMS | 1539 19 18 16 20 20 27 |NE 47 42 45 48 49 41 42
MEDI | 1270 14 14 16 18 20 16 |MD 48 44 49 44 52 43 46
Table 3.2347.2 GPS week: 2347 Day: 2 MJD: 60675
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 5579 34 25 37 32 16 24 12 | 48 62 80 80 74 66 64
XR02E | 4489 9 11 17 23 12 --- 7 | 26 31 25 37 29 --- 26
R03E | 2961 12 11 14 23 17 14 7 | 26 23 25 43 27 29 25
R04E | 4208 18 18 27 13 15 20 8 | 76 80 82 81 78 78 77
R05E | 6954 17 21 21 24 17 13 8 | 30 36 38 34 34 30 29
R07E | 5456 9 12 16 22 25 25 9 | 47 47 40 50 45 57 45
R08E |13064 13 18 15 26 25 21 9 | 56 74 68 63 61 55 59
R09 | 5754 12 24 16 12 10 11 6 | 15 27 26 21 19 24 18
R11 | 6470 19 18 23 42 16 8 10 | 15 29 26 57 15 16 16
R12 | 5717 14 14 10 13 17 21 7 | 44 44 39 41 48 37 41
R14 | 4055 10 10 12 20 21 10 6 | 50 53 45 40 63 56 51
R15 | 7322 17 19 17 23 10 14 7 | 55 42 44 65 52 53 50
R16 | 5501 18 24 18 19 19 18 8 | 47 53 50 56 34 35 43
R17 | 6183 16 13 17 15 8 22 7 | 66 59 73 67 58 55 61
R18 | 4822 14 13 20 18 11 20 7 | 53 62 71 67 59 52 58
R19 | 6199 34 72 40 54 27 22 18 | 103 89 97 104 104 91 93
R20 | 6536 46 107 60 77 30 54 27 | 98 82 122 93 111 84 92
R21 | 6859 20 25 11 18 15 21 8 | 73 60 63 64 65 59 63
XR22 |10352 12 13 22 19 13 --- 8 | 38 47 41 41 36 --- 37
R24 |14800 16 21 20 16 20 20 8 | 57 53 75 73 73 59 64
XR26E |15047 37 --- --- 42 47 --- 30 | 37 --- --- 55 19 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 7161 21 35 25 30 19 22 |T 50 52 56 58 52 52 49
WRMS | 7161 17 20 17 20 18 22 |NE 54 53 59 60 56 51 52
MEDI | 6183 16 18 17 22 17 20 |MD 48 53 45 57 52 55 50
Table 3.2347.3 GPS week: 2347 Day: 3 MJD: 60676
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1114 30 33 46 19 39 61 18 | 69 91 90 87 67 107 78
XR02E | 911 10 11 21 18 17 --- 8 | 28 28 36 42 34 --- 29
R03E | 836 10 10 28 48 16 19 10 | 32 29 37 51 38 28 29
R04E | 800 14 11 25 15 15 19 7 | 38 31 39 42 33 34 33
R05E | 2358 10 13 22 23 9 16 7 | 40 43 33 51 37 42 38
R07E | 2074 12 8 21 43 18 20 9 | 64 65 68 66 59 59 59
R08E | 741 9 25 20 18 27 22 9 | 89 95 79 97 77 75 83
XR09 | 5698 10 20 16 15 17 --- 7 | 19 27 22 23 21 --- 18
R11 | 806 12 13 17 50 20 18 10 | 12 26 25 43 12 12 13
R12 | 616 8 10 18 30 26 10 8 | 27 37 27 21 45 29 29
R14 | 1428 8 10 15 12 23 18 7 | 44 39 34 37 54 31 39
R15 | 2192 22 23 23 17 11 20 9 | 59 37 39 35 48 54 44
R16 | 970 18 24 11 19 14 12 7 | 44 36 38 46 32 33 36
R17 | 1797 10 19 13 19 16 25 7 | 62 52 61 68 66 44 58
R18 | 1085 16 13 16 16 19 19 7 | 43 55 46 57 58 40 47
R19 | 4104 33 62 25 52 15 41 17 | 87 52 71 81 67 63 67
R20 | 1539 34 99 51 68 28 55 25 | 112 68 123 111 96 83 95
R21 | 586 11 25 21 20 11 22 8 | 74 63 82 78 73 56 70
XR22 | 7007 16 15 17 21 12 --- 8 | 46 56 45 44 42 --- 44
R24 | 647 14 30 17 24 24 18 9 | 67 53 79 77 87 62 70
XR26E |15915 32 --- --- 51 49 --- 30 | 43 --- --- 42 26 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 1648 18 34 25 33 21 28 |T 52 49 53 57 51 50 47
WRMS | 1648 16 22 16 20 19 26 |NE 53 46 53 55 53 46 48
MEDI | 1114 12 15 20 20 17 19 |MD 44 43 39 51 48 44 44
Table 3.2347.4 GPS week: 2347 Day: 4 MJD: 60677
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 947 24 47 41 30 26 65 17 | 88 91 104 85 80 96 84
XR02E | 1159 6 12 10 13 8 --- 4 | 35 33 31 38 33 --- 33
R03E | 971 12 16 21 14 9 13 6 | 34 38 35 34 33 31 31
R04E | 1060 9 14 14 17 10 15 5 | 80 83 83 78 79 80 80
R05E | 1369 12 19 15 27 13 5 7 | 46 45 44 55 37 44 42
R07E | 2597 10 20 20 16 15 8 6 | 77 91 84 71 70 81 77
R08E | 664 20 18 22 16 13 17 8 | 64 59 67 63 59 61 61
R09 | 1276 10 27 10 13 11 9 6 | 26 24 21 26 26 24 21
XR11 | 581 15 23 16 34 10 --- 9 | 18 40 18 64 23 --- 25
R12 | 609 10 12 9 24 15 11 6 | 48 52 54 41 48 46 47
R14 | 938 7 9 20 21 15 12 6 | 49 50 66 35 55 43 50
R15 | 1250 18 21 10 15 11 29 8 | 58 44 56 42 59 44 51
R16 | 1202 25 28 17 16 11 7 8 | 57 40 48 35 47 43 44
R17 | 1782 12 20 11 25 15 22 7 | 70 61 64 78 68 57 65
R18 | 1153 12 16 10 28 11 28 8 | 59 65 54 66 60 54 57
R19 | 3940 39 62 16 41 14 43 16 | 110 68 78 85 88 78 85
R20 | 2047 26 106 61 66 24 65 25 | 99 54 117 116 105 57 93
R21 | 776 14 25 13 22 11 25 8 | 80 71 74 86 69 68 73
R22 | 2855 14 24 13 24 16 9 7 | 46 67 54 62 42 16 49
R24 | 922 10 39 18 20 18 20 9 | 69 54 81 80 79 65 72
XR26E |15691 42 --- --- 46 56 --- 35 | 26 --- --- 36 26 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1695 18 37 23 27 15 28 |T 59 56 61 60 56 54 55
WRMS | 1695 16 26 18 23 14 28 |NE 60 53 60 62 59 49 56
MEDI | 1159 12 20 15 22 13 15 |MD 58 54 56 63 59 54 51
Table 3.2347.5 GPS week: 2347 Day: 5 MJD: 60678
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1564 16 61 45 22 29 38 16 | 129 148 138 131 119 159 133
XR02E | 1585 11 10 13 7 10 --- 5 | 30 28 31 31 30 --- 28
R03E | 1128 11 13 17 26 14 11 7 | 31 31 28 43 31 27 29
R04E | 1914 12 12 16 21 16 11 6 | 59 51 53 59 60 57 55
R05E | 2158 13 13 14 20 11 10 6 | 35 37 36 44 33 36 34
R07E | 2024 11 12 19 21 9 7 6 | 40 38 38 45 40 40 38
R08E | 1046 21 16 23 20 15 14 8 | 87 85 84 86 79 80 82
R09 | 1294 12 14 16 16 13 23 7 | 13 17 19 15 24 22 13
XR11 | 1225 14 15 16 58 20 --- 14 | 18 36 23 70 20 --- 25
R12 | 804 17 15 10 13 11 9 5 | 34 18 26 24 27 25 25
R14 | 826 11 10 10 21 23 12 7 | 32 41 36 27 51 35 36
R15 | 716 14 12 23 13 11 29 8 | 45 39 57 39 46 30 41
R16 | 1764 13 12 18 22 16 10 7 | 42 44 48 36 51 38 42
R17 | 766 14 16 16 13 14 15 6 | 44 32 29 44 47 34 38
R18 | 951 15 16 10 22 13 16 7 | 39 46 41 58 49 37 44
R19 | 3466 46 85 44 41 30 41 21 | 92 36 87 66 59 45 62
R20 | 3666 31 99 54 61 34 53 24 | 79 42 80 86 72 52 66
R21 | 1144 9 24 26 14 8 19 7 | 52 42 60 57 43 42 48
R22 | 1270 17 16 13 11 16 16 7 | 40 36 30 33 33 20 34
R24 | 1208 16 28 14 21 11 18 8 | 55 40 41 57 46 44 46
XR26E |17254 38 --- --- 43 57 --- 33 | 22 --- --- 34 20 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 1751 19 37 25 25 18 23 |T 48 44 49 51 46 45 44
WRMS | 1751 16 33 21 19 15 23 |NE 45 36 44 47 43 35 40
MEDI | 1270 14 15 16 21 14 15 |MD 40 38 38 44 46 37 38
Table 3.2347.6 GPS week: 2347 Day: 6 MJD: 60679
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1016 32 54 40 24 29 33 15 | 85 118 94 101 100 113 97
R02E | 1301 9 11 24 14 14 13 6 | 30 34 35 28 37 9 30
R03E | 912 13 12 12 11 15 17 6 | 29 31 29 32 28 32 28
R04E | 2017 14 12 15 15 14 15 6 | 66 70 70 70 69 74 69
R05E | 2225 11 11 20 15 12 16 6 | 35 35 35 35 35 33 32
R07E | 838 12 13 9 15 21 10 6 | 49 51 45 51 48 51 47
R08E | 954 15 25 15 12 18 12 7 | 86 99 92 91 78 92 88
R09 | 1096 11 12 10 11 17 15 6 | 21 29 20 25 30 29 23
R11 | 1687 20 14 11 33 12 24 9 | 17 25 24 44 26 21 22
R12 | 1374 12 13 19 12 11 9 5 | 46 40 38 38 41 37 38
R14 | 1360 7 8 14 15 16 10 5 | 44 42 48 35 54 41 44
R15 | 983 14 11 11 8 10 10 4 | 51 42 43 43 48 42 44
R16 | 2105 17 14 20 14 18 25 8 | 53 49 50 43 52 34 44
R17 | 865 18 21 11 13 13 18 7 | 78 59 68 69 75 58 67
R18 | 534 10 15 12 13 14 15 6 | 62 69 62 75 69 51 64
R19 | 1921 45 92 51 34 27 34 21 | 136 53 138 118 105 89 105
R20 | 2213 39 100 81 44 28 49 25 | 130 53 159 121 121 86 111
R21 | 941 15 28 27 15 18 22 9 | 88 66 93 86 88 67 81
R22 | 1325 16 15 19 18 17 13 7 | 47 48 49 47 40 17 43
R24 | 1646 31 32 18 19 18 26 11 | 93 67 87 90 92 75 83
XR26E |14834 40 --- --- 38 63 --- 34 | 35 --- --- 41 33 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1455 21 36 28 20 18 22 |T 61 54 63 61 60 52 56
WRMS | 1455 16 29 18 18 17 22 |NE 66 49 67 64 64 49 59
MEDI | 1325 15 14 15 15 17 15 |MD 51 49 49 47 52 42 44
More information about the IGSREPORT
mailing list