[IGSREPORT-30097] Wk 2331 IGLOS Final Orbits
acc
acc at igs.org
Fri Sep 27 05:22:28 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2331 (Sep 08, 2024 - Sep 14, 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 2.2331.
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:
igl2331[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2331 in the SP3 format.
igl23317.sum Combination Report for GPS Week 2331.
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 | 5.4 ns
2 | 7.4 ns
3 | 6.7 ns
4 | 6.7 ns
5 | 6.1 ns
6 | 6.2 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 1.2331, 1a.2331).
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 2.2331.0-6)
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 3.2331.0-6).
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 2331 summary. (Sep 08, 2024 - Sep 14, 2024)
Table 1.2331.a GPS week : 2331 MJD: 60561.0-60567.0
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| 0 0 4 -8 3 56 .16 20 14 | -2559 -1136 4884 21594
| 0 1 0 14 13 20 .05 | 3584 1963
esa n/a| 0 0 0 -10 -9 2 -.08 20 15 | 8996 -94 3825 12089
| 1 1 1 12 12 30 .06 | 8139 1726
gfz n/a| 0 0 1 38 12 -43 -.00 24 15 | 0 -137 3182 7791
| 1 0 1 20 26 23 .04 | 0 1819
grg n/a| 0 1 0 -18 -10 -47 .30 29 20 | 3134 -510 3979 17425
| 1 0 3 9 21 26 .06 | 1193 1422
iac n/a| 0 0 -4 40 22 -45 -.22 24 22 | 3672 -856 4837 20609
| 1 1 1 20 30 72 .07 | 3214 1585
jgx n/a| 0 0 -4 -57 -30 32 -.14 25 24 | 2949 -198 3194 7964
| 0 1 1 22 20 26 .05 | 1170 1616
Table 1.2331.b GPS week : 2331 MJD: 60561.0-60567.0
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 | 12 13 11 14 14 12 13 |
R02 | 6 5 6 6 5 4 8 |
R03 | 5 5 7 6 7 7 6 |
R04 | 6 6 6 7 7 7 5 |
R05 | 7 7 6 5 5 6 6 |
R07 | 5 5 6 6 8 6 5 |
R08 | 7 6 7 6 7 7 7 |
R09 | 7 6 6 8 7 6 7 |
R11 | 7 7 8 7 7 6 7 |
R12 | 7 7 6 9 8 7 6 |
R14 | 6 5 6 7 6 7 6 |
R15 | 7 7 8 9 8 8 7 |
R16 | 7 8 7 8 9 7 7 |
R17 | 6 17 9 8 7 7 8 |
R18 | 9 8 18 13 8 9 8 |
R19 | 22 17 19 20 22 24 22 |
R20 | 26 26 20 21 24 29 26 |
R21 | 6 7 16 10 7 8 8 |
R22 | 8 6 7 7 9 9 6 |
R24 | 8 12 10 6 7 7 7 |
R25 | 12 11 15 10 18 10 10 |
R26 | 33 35 28 32 35 31 32 |
Table 1.2331.c GPS week : 2331 MJD: 60561.0-60567.0
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 2331 0 | 12 -122 106 152 -587 -6892 79.4 1622 1622 | 5164 0
brd 2331 1 | 44 38 49 92 738 -1904 81.4 1555 1555 | 5415 0
brd 2331 2 | 23 4 84 387 676 -4879 82.7 1696 1696 | 7378 0
brd 2331 3 | 51 43 128 156 2084 -4795 79.8 1583 1583 | 6690 0
brd 2331 4 | 91 59 114 350 988 -4967 78.7 1807 1807 | 6669 0
brd 2331 5 | -85 18 -9 -374 -72 -8303 80.9 2069 2069 | 6062 0
brd 2331 6 | -134 70 78 -334 195 -8125 80.4 1922 1922 | 6205 0
-------------+------------------------------------------------------------+----------------
brd 2331 mean| 0 16 78 61 574 -5694 80.5 1750 1750 | 6226 0
brd 2331 sdev| 80 65 47 303 856 2255 1.4 191 191 | 769 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 2.2331.0 GPS week: 2331 Day: 0 MJD: 60561
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 6 8 6 31 .10 19 14 | -1861 58 3534 18195
esa n/a| 0 0 0 -8 -24 24 -.08 21 15 | 2774 311 2978 6348
gfz n/a| 1 1 2 55 -15 -21 -.01 31 15 | 0 308 2972 7583
grg n/a| 2 0 -3 -28 13 -42 .36 21 16 | 1403 230 3586 18221
iac n/a| 0 0 -3 15 35 -68 -.23 19 17 | 3713 435 3483 17192
jgx n/a| -1 0 -3 -37 -50 2 -.19 25 25 | 3129 236 3014 7667
Table 2.2331.1 GPS week: 2331 Day: 1 MJD: 60562
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 2 3 -26 -1 50 .22 17 14 | -2887 -1293 3984 18642
esa n/a| 0 -1 1 3 0 -25 -.17 20 14 | 10656 -121 3204 7684
gfz n/a| 1 0 1 71 22 -83 .05 26 14 | 0 -995 3260 7801
grg n/a| 1 2 -3 -21 -16 -15 .37 32 20 | 2326 -1352 4159 19241
iac n/a| -1 -2 -5 27 63 35 -.18 24 24 | 3021 -774 3963 18020
jgx n/a| 0 -1 -4 -75 -60 17 -.21 24 24 | 1722 -1039 3272 7989
Table 2.2331.2 GPS week: 2331 Day: 2 MJD: 60563
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 4 -13 6 46 .20 20 13 | 148 -30 4164 17594
esa n/a| 0 -2 0 -4 -22 26 -.13 17 13 | 6126 1166 3384 8518
gfz n/a| 3 1 2 43 58 -43 .00 23 17 | 0 619 3435 8062
grg n/a| 0 1 0 -18 10 -61 .31 37 22 | 4735 -300 4175 16439
iac n/a| -2 0 -1 62 -7 -147 -.23 35 37 | 6467 -713 4111 16642
jgx n/a| -1 1 -4 -60 -40 43 -.16 19 19 | 4444 232 3481 8515
Table 2.2331.3 GPS week: 2331 Day: 3 MJD: 60564
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 -26 -15 53 .22 20 15 | -1060 -880 4069 16936
esa n/a| 0 0 -1 -4 -12 -2 -.06 18 14 | 24872 -1144 3414 7781
gfz n/a| -1 0 1 25 1 -29 -.04 19 13 | 0 -1753 3319 7045
grg n/a| 0 0 0 -12 7 -17 .28 28 19 | 4164 -1318 3975 16841
iac n/a| 0 2 -5 62 13 -72 -.34 27 23 | 4456 357 4010 15931
jgx n/a| 0 1 -2 -21 -23 0 -.09 25 25 | 3734 -1458 3338 7243
Table 2.2331.4 GPS week: 2331 Day: 4 MJD: 60565
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 3 3 -8 46 .14 22 14 | -1026 823 4176 16160
esa n/a| 0 -2 0 -9 -19 -45 -.00 19 16 | 5491 2272 3346 7897
gfz n/a| 0 0 2 29 -17 -68 -.04 21 15 | 0 2592 3342 7817
grg n/a| 1 1 3 -29 -20 -92 .23 29 24 | 2867 1270 4189 16313
iac n/a| 0 -1 -5 49 58 63 -.21 22 17 | 5730 44 4128 15214
jgx n/a| -1 2 -3 -63 -5 47 -.09 26 23 | 2473 2181 3314 7979
Table 2.2331.5 GPS week: 2331 Day: 5 MJD: 60566
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 -2 9 79 .12 21 12 | -823 -5192 6571 19765
esa n/a| -2 0 1 -35 4 0 -.04 20 15 | 12497 -3163 3312 8053
gfz n/a| 0 0 1 7 21 -24 .03 24 15 | 0 -2770 2971 7812
grg n/a| 0 1 3 -17 -25 -60 .23 36 17 | 3991 -2844 3678 17328
iac n/a| 0 0 -6 53 -10 -48 -.11 19 15 | 5418 -4174 6524 18579
jgx n/a| -1 2 -7 -87 -17 68 -.12 29 29 | 3859 -2599 2976 7896
Table 2.2331.6 GPS week: 2331 Day: 6 MJD: 60567
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 0 27 89 .12 18 13 | -10406 -1443 7692 43866
esa n/a| -1 0 1 -11 5 39 -.07 21 15 | 557 19 7142 38347
gfz n/a| 0 0 0 34 14 -34 .01 26 14 | 0 1035 2978 8419
grg n/a| 0 0 3 -3 -42 -45 .30 23 23 | 2452 741 4092 17595
iac n/a| 0 0 -4 16 6 -79 -.23 20 17 | -3099 -1172 7646 42689
jgx n/a| 0 0 -6 -54 -13 50 -.15 27 27 | 1284 1058 2968 8462
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 3.2331.0 GPS week: 2331 Day: 0 MJD: 60561
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1375 27 31 29 22 21 30 12 | 88 65 74 80 83 76 76
R02 | 1468 10 15 9 14 15 20 6 | 47 58 51 55 54 42 50
R03 | 803 6 10 9 13 10 12 4 | 53 54 51 61 57 48 53
R04 | 573 10 10 14 8 13 18 5 | 62 66 61 66 72 54 63
R05 | 817 9 9 13 18 19 21 7 | 52 52 57 61 65 43 54
R07 | 1321 12 9 6 10 11 19 5 | 62 58 60 61 59 53 58
R08 | 543 12 11 23 14 11 22 7 | 60 64 70 73 71 57 64
R09 | 1680 10 15 19 13 15 25 7 | 48 55 57 48 48 38 48
R11 | 1153 18 15 13 9 15 11 6 | 29 30 32 22 30 24 26
R12 | 802 12 14 13 16 16 16 6 | 71 63 69 76 75 63 69
R14 | 719 9 11 16 12 15 20 6 | 70 73 70 71 73 58 69
R15 | 1181 12 15 12 9 20 13 6 | 96 80 86 98 100 84 90
R16 | 818 11 16 20 9 17 19 7 | 83 85 96 84 92 70 84
R17E | 2311 12 12 16 21 8 13 6 | 112 113 124 126 109 111 114
R18E | 1612 13 21 16 27 15 18 8 | 65 74 73 73 62 68 68
R19E | 1392 46 38 72 54 40 46 22 | 79 101 123 84 86 89 84
R20E | 2373 43 58 96 35 40 65 25 | 67 83 111 69 58 79 63
R21E | 1850 11 14 14 15 12 12 5 | 70 68 71 76 64 72 69
R22E | 3025 14 12 11 25 19 13 7 | 28 36 31 38 37 30 31
R24E | 3063 20 17 18 18 17 11 7 | 76 88 92 87 84 83 83
XR25E |13595 14 21 --- --- 15 --- 12 | 40 37 --- --- 35 --- 36
XR26 | 8321 38 --- --- 28 65 --- 33 | 37 --- --- 42 93 --- 54
------+-----------------------------------------+-------------------------------------
RMS | 1621 19 21 31 21 19 25 |T 63 66 72 69 68 62 63
WRMS | 1621 14 15 15 16 17 25 |NE 61 61 64 64 69 54 61
MEDI | 1375 12 15 14 15 15 18 |MD 62 65 70 71 65 58 63
Table 3.2331.1 GPS week: 2331 Day: 1 MJD: 60562
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 825 28 28 14 31 14 43 12 | 57 45 51 46 42 40 45
R02 | 1189 11 12 9 11 13 9 5 | 30 38 29 32 33 29 30
R03 | 791 7 10 10 9 13 18 5 | 30 35 33 32 38 27 31
R04 | 630 8 15 8 21 13 15 6 | 38 42 41 44 46 37 39
R05 | 1098 14 7 8 22 19 18 6 | 32 32 36 54 49 26 35
R07 | 1907 10 14 9 11 12 8 5 | 40 32 38 39 39 44 36
R08 | 475 14 12 12 9 17 14 6 | 40 35 43 49 45 49 42
R09 | 833 12 13 16 13 11 9 5 | 38 44 49 37 31 35 38
XR11 | 755 15 7 17 12 9 --- 6 | 20 21 27 18 28 --- 20
R12 | 561 14 12 13 16 16 20 6 | 50 42 47 52 43 39 44
R14 | 597 8 11 11 11 13 11 4 | 47 56 55 51 48 46 50
R15 | 867 14 11 10 16 23 16 7 | 62 58 56 66 70 60 60
R16 | 934 16 20 13 14 24 15 8 | 65 68 66 61 68 52 62
R17E | 1605 18 17 22 83 59 17 17 | 157 158 163 189 140 156 156
R18E | 1288 16 19 17 23 11 19 8 | 76 90 73 80 86 84 80
R19E | 3219 34 30 42 49 29 41 16 | 82 85 104 93 92 81 84
R20E | 1791 31 57 87 40 48 63 26 | 56 60 107 44 39 47 45
R21E | 1561 16 16 20 21 11 10 7 | 82 76 83 79 76 75 77
R22E | 2902 13 7 14 18 16 16 6 | 24 30 35 38 29 24 27
R24E | 2463 11 13 19 64 22 13 11 | 148 144 147 167 138 142 145
XR25E |16847 12 13 --- --- 21 --- 11 | 42 54 --- --- 43 --- 46
XR26 | 9318 39 --- --- 21 72 --- 34 | 29 --- --- 42 61 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1554 17 20 26 32 24 24 |T 56 59 64 62 58 57 55
WRMS | 1554 14 14 14 20 24 24 |NE 41 42 43 44 45 40 40
MEDI | 1098 14 13 13 18 16 16 |MD 42 45 49 49 45 46 44
Table 3.2331.2 GPS week: 2331 Day: 2 MJD: 60563
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 709 32 23 18 24 24 23 11 | 65 49 58 58 59 48 54
R02 | 695 11 10 11 19 16 13 5 | 44 48 45 50 38 44 44
R03 | 855 10 8 9 26 23 19 6 | 47 51 48 58 40 42 45
R04 | 725 10 14 13 11 12 10 5 | 52 56 56 47 46 52 51
R05 | 1103 9 15 15 15 6 9 5 | 44 47 50 48 41 41 44
R07 | 1257 6 8 17 12 14 15 5 | 47 45 56 45 48 42 46
R08 | 495 13 13 14 10 28 9 6 | 48 47 54 54 67 54 51
R09 | 1717 14 13 15 20 14 5 6 | 41 47 46 33 47 40 42
XR11 | 979 17 13 12 24 21 --- 8 | 24 31 26 32 25 --- 24
R12 | 643 12 12 12 11 11 19 6 | 69 71 73 67 63 62 67
R14 | 682 8 9 15 14 16 14 5 | 56 56 67 68 61 49 57
R15 | 642 16 15 21 33 19 8 8 | 75 63 83 96 63 70 72
R16 | 892 16 12 9 16 24 17 7 | 69 63 62 72 76 50 62
R17E | 898 15 12 15 40 27 19 9 | 112 120 114 130 89 123 114
R18E | 1266 10 18 22 82 89 16 17 | 106 106 101 129 121 105 103
R19E | 4554 40 33 46 56 52 41 19 | 91 110 107 84 77 103 92
R20E | 2326 43 40 55 30 69 32 20 | 48 71 100 57 56 59 52
R21E | 1295 22 16 23 90 55 16 16 | 121 120 122 164 93 112 117
R22E | 2723 13 11 22 18 20 11 7 | 32 40 45 41 34 31 34
R24E | 2578 17 16 26 38 21 22 10 | 139 140 138 155 121 139 138
XR25E |11756 18 19 --- --- 27 --- 14 | 41 51 --- --- 47 --- 44
XR26 | 8919 28 --- --- 27 63 --- 27 | 31 --- --- 41 53 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 1695 20 17 23 37 35 19 |T 63 68 72 72 62 66 62
WRMS | 1695 13 13 17 22 37 19 |NE 50 51 55 54 51 49 49
MEDI | 979 14 13 15 24 21 16 |MD 48 56 58 58 56 52 51
Table 3.2331.3 GPS week: 2331 Day: 3 MJD: 60564
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 644 31 25 17 34 25 47 13 | 78 63 78 81 80 75 74
R02 | 2061 11 11 7 9 15 19 5 | 51 53 47 50 45 40 47
R03 | 934 9 10 14 19 10 18 6 | 47 57 51 60 52 43 50
R04 | 643 15 9 9 9 16 24 6 | 45 48 40 45 43 34 41
R05 | 1912 12 8 8 13 12 7 4 | 48 46 45 44 43 48 45
R07 | 779 8 16 10 10 12 15 5 | 54 58 54 51 46 47 51
R08 | 665 8 7 10 21 22 11 6 | 62 59 62 59 65 61 60
R09 | 1787 17 6 11 21 31 10 7 | 28 31 37 33 44 28 30
R11 | 1499 15 11 16 11 20 10 6 | 26 28 29 25 30 32 25
R12 | 1357 13 12 20 22 23 31 9 | 54 63 72 60 55 37 56
R14 | 606 11 11 19 13 19 13 6 | 52 51 71 67 56 47 56
R15 | 493 11 27 9 33 24 8 9 | 71 63 74 90 77 68 71
R16 | 771 16 19 19 20 21 8 8 | 76 63 66 80 81 71 70
R17E | 1091 15 16 7 30 16 20 7 | 81 81 78 100 76 73 79
R18E | 916 14 26 14 46 52 14 12 | 143 149 140 170 106 149 142
R19E | 3807 43 28 46 64 30 45 19 | 74 84 85 80 71 75 74
R20E | 2453 47 36 44 38 56 63 21 | 66 87 83 68 55 77 61
R21E | 848 11 13 10 37 44 17 10 | 111 103 106 121 98 103 105
R22E | 2126 16 10 12 23 13 10 6 | 31 40 39 44 34 34 35
R24E | 1781 10 9 10 26 15 14 6 | 94 91 96 107 92 82 92
XR25E |10088 16 8 --- --- 16 --- 10 | 57 48 --- --- 54 --- 52
XR26 | 8198 34 --- --- 24 69 --- 32 | 33 --- --- 36 79 --- 43
------+-----------------------------------------+-------------------------------------
RMS | 1583 20 18 19 28 27 25 |T 62 65 67 70 62 61 61
WRMS | 1583 15 14 13 19 23 25 |NE 51 52 55 55 56 48 51
MEDI | 1091 14 11 11 22 20 14 |MD 54 59 66 60 55 48 56
Table 3.2331.4 GPS week: 2331 Day: 4 MJD: 60565
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1427 31 37 18 36 19 36 13 | 71 50 62 68 64 77 62
R02 | 2462 5 9 11 11 12 13 4 | 52 52 55 56 53 50 52
R03 | 1308 9 8 18 18 17 13 6 | 55 62 44 66 54 53 54
R04 | 1013 12 14 9 7 10 28 6 | 60 62 58 57 50 44 55
R05 | 827 10 10 11 12 10 11 5 | 58 52 52 54 52 49 52
R07 | 583 17 16 18 10 14 29 8 | 46 45 37 37 37 34 37
R08 | 1166 14 7 13 13 21 15 6 | 55 59 65 61 58 54 58
R09 | 804 19 9 13 14 16 11 6 | 34 42 47 36 48 35 39
R11 | 1601 12 15 23 14 18 8 7 | 30 36 33 29 37 26 30
R12 | 2019 13 15 19 14 13 23 7 | 72 73 86 86 72 60 73
R14 | 775 11 12 18 14 9 10 5 | 43 44 32 50 31 34 37
R15 | 689 14 20 11 25 13 17 7 | 70 59 57 87 63 53 63
R16 | 678 12 25 16 16 27 17 9 | 64 73 75 68 76 59 68
R17E | 2221 10 16 14 17 11 26 7 | 94 90 96 98 82 82 89
R18E | 1372 15 18 14 28 10 15 7 | 84 93 79 103 86 83 86
R19E | 2677 50 23 48 81 32 62 22 | 73 70 75 90 76 71 70
R20E | 4418 59 42 46 53 66 52 24 | 77 97 100 85 57 84 72
R21E | 1013 13 16 16 23 12 18 7 | 81 80 76 94 72 76 77
R22E | 2003 19 14 16 39 18 13 9 | 49 57 60 63 58 51 53
R24E | 2167 9 19 14 22 10 18 7 | 85 77 81 99 76 74 80
XR25E |12816 21 17 --- --- 32 --- 17 | 47 45 --- --- 44 --- 41
XR26 |13126 44 --- --- 35 61 --- 35 | 24 --- --- 27 66 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1806 22 19 21 29 22 26 |T 60 62 63 67 59 57 58
WRMS | 1806 14 16 15 24 17 23 |NE 52 54 54 55 54 48 51
MEDI | 1372 13 16 16 17 14 17 |MD 58 59 60 66 58 53 55
Table 3.2331.5 GPS week: 2331 Day: 5 MJD: 60566
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2073 22 20 25 29 14 52 12 | 65 60 73 66 66 58 64
R02 | 1660 8 5 8 8 8 9 3 | 43 44 49 46 52 47 46
R03 | 910 13 17 13 10 17 15 6 | 42 35 38 35 49 30 38
R04 | 945 8 13 18 15 13 30 7 | 43 49 52 35 43 29 42
R05 | 675 11 14 9 10 14 18 5 | 44 43 40 40 40 31 39
R07 | 748 12 13 10 10 14 16 5 | 39 38 38 33 31 36 35
R08 | 2108 12 6 11 10 19 32 7 | 37 42 43 43 49 38 41
R09 | 3078 14 13 15 12 6 13 5 | 36 43 44 38 41 38 39
R11 | 2134 11 12 16 11 11 16 5 | 24 29 28 26 28 24 25
R12 | 1613 9 10 16 24 13 19 6 | 67 63 52 78 65 48 61
R14 | 894 8 18 11 14 17 17 6 | 45 54 39 50 29 37 41
R15 | 1045 11 19 11 20 18 31 8 | 57 42 56 63 59 40 52
R16 | 1631 18 21 10 17 11 12 7 | 56 53 53 58 56 52 53
R17E | 2645 13 15 13 18 10 20 6 | 59 56 62 80 57 53 59
R18E | 1381 13 22 17 23 13 27 8 | 53 60 48 69 53 53 54
R19E | 2999 46 37 49 99 29 65 23 | 106 110 113 132 105 104 106
R20E | 4569 64 49 72 98 52 51 28 | 129 118 120 160 100 112 111
R21E | 651 13 19 21 19 9 18 7 | 62 56 60 75 61 46 59
R22E | 2103 12 11 20 38 17 18 8 | 35 39 39 63 37 40 36
R24E | 2556 8 17 17 22 12 15 6 | 65 61 68 77 69 62 66
XR25E |13126 10 16 --- --- 15 --- 10 | 51 58 --- --- 46 --- 50
XR26 |13586 38 --- --- 40 50 --- 31 | 24 --- --- 24 48 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 2068 21 20 24 36 19 29 |T 53 54 55 61 53 48 52
WRMS | 2068 12 15 15 17 15 29 |NE 44 45 46 45 46 39 43
MEDI | 1660 12 16 15 18 14 18 |MD 45 53 49 58 49 40 46
Table 3.2331.6 GPS week: 2331 Day: 6 MJD: 60567
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1251 31 12 18 33 15 47 12 | 102 88 92 91 96 84 92
R02 | 1754 12 26 15 13 13 15 7 | 59 75 66 62 65 59 63
R03 | 1169 8 16 11 12 12 20 6 | 61 63 67 68 66 63 63
R04 | 831 6 9 9 8 16 11 4 | 57 58 55 57 64 47 56
R05 | 1424 9 11 12 8 13 21 5 | 56 54 52 51 56 43 52
R07 | 1644 5 13 10 16 13 10 5 | 65 59 68 69 59 57 62
R08 | 2153 12 7 16 13 20 19 6 | 63 64 65 67 75 61 65
R09 | 3117 10 18 18 12 16 8 6 | 46 56 52 45 53 48 49
R11 | 1540 12 15 12 17 22 12 7 | 31 35 36 24 36 29 30
R12 | 1003 8 8 12 14 14 24 6 | 76 74 77 86 79 58 75
R14 | 804 10 14 11 14 11 13 5 | 68 68 65 63 56 51 62
R15 | 935 10 15 11 17 19 19 7 | 77 65 73 84 84 63 74
R16 | 1139 18 13 12 20 17 12 7 | 68 59 57 55 65 51 58
R17E | 2382 18 20 16 21 16 16 8 | 93 88 90 105 90 81 90
R18E | 793 18 20 18 14 14 15 7 | 90 103 95 107 95 93 96
R19E | 3647 21 45 46 70 29 72 21 | 88 90 103 96 88 84 87
R20E | 2672 52 52 86 34 54 49 25 | 69 112 85 88 109 95 81
R21E | 833 16 16 16 12 18 25 7 | 88 79 92 90 80 74 83
R22E | 3077 13 11 17 13 11 9 5 | 32 33 38 43 36 32 33
R24E | 2227 13 17 17 19 11 15 7 | 94 98 100 106 95 91 96
XR25E |10826 14 14 --- --- 13 --- 10 | 49 47 --- --- 49 --- 47
XR26 |17282 29 --- --- 36 65 --- 32 | 23 --- --- 29 84 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1921 18 21 26 23 20 27 |T 66 69 71 70 71 63 66
WRMS | 1921 13 15 14 23 17 27 |NE 60 62 63 60 67 54 60
MEDI | 1540 12 15 15 14 15 15 |MD 65 65 67 68 66 59 63
More information about the IGSREPORT
mailing list