[IGSREPORT-30108] Wk 2332 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 4 02:17:40 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2332 (Sep 15, 2024 - Sep 21, 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 2.2332.
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:
igl2332[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2332 in the SP3 format.
igl23327.sum Combination Report for GPS Week 2332.
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 | 4.9 ns
1 | 8.4 ns
2 | 8.4 ns
3 | 6.8 ns
4 | 6.5 ns
5 | 6.2 ns
6 | 7.1 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 1.2332, 1a.2332).
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 2.2332.0-6)
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 3.2332.0-6).
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 2332 summary. (Sep 15, 2024 - Sep 21, 2024)
Table 1.2332.a GPS week : 2332 MJD: 60568.0-60574.0
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 3 -6 0 52 .14 19 15 | -1107 -1279 3774 15848
| 0 0 1 11 18 25 .03 | 1353 2005
esa n/a| 0 0 0 -25 -17 -7 -.04 20 16 | 8049 -971 3051 7149
| 1 1 1 15 16 32 .02 | 6434 1821
gfz n/a| 0 0 4 36 11 -13 -.03 23 15 | 0 -603 3077 7220
| 1 1 2 19 20 31 .07 | 0 2087
grg n/a| 1 1 2 -2 -6 -16 .31 22 18 | 4512 -1338 3855 15887
| 0 1 2 22 18 29 .06 | 1351 1919
iac n/a| 0 0 -4 19 14 -32 -.17 19 17 | 6983 -1131 3732 14914
| 1 0 3 12 42 79 .06 | 1459 1362
jgx n/a| 0 0 -5 -44 -21 19 -.16 24 24 | 3236 -794 3081 7339
| 1 0 1 13 14 15 .02 | 1328 1891
Table 1.2332.b GPS week : 2332 MJD: 60568.0-60574.0
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 12 12 14 13 14 12 |
R02 | 6 6 6 7 7 5 6 |
R03 | 7 5 5 9 7 5 7 |
R04 | 6 7 6 7 8 6 7 |
R05 | 5 6 8 7 7 6 6 |
R07 | 8 5 7 7 8 6 6 |
R08 | 6 7 7 8 8 7 6 |
R09 | 6 7 6 7 6 6 7 |
R11 | 7 6 9 7 8 8 9 |
R12 | 7 7 8 6 9 8 6 |
R14 | 7 7 7 5 7 6 6 |
R15 | 8 7 8 7 7 7 6 |
R16 | 8 8 7 8 7 7 7 |
R17 | 9 8 7 8 8 8 8 |
R18 | 10 8 7 7 8 9 7 |
R19 | 22 20 17 21 24 25 25 |
R20 | 23 21 18 28 16 17 19 |
R21 | 8 7 7 9 9 8 7 |
R22 | 7 8 7 6 7 6 6 |
R24 | 8 7 10 8 7 7 7 |
R25 | 8 11 10 17 11 10 11 |
R26 | 33 29 27 27 28 20 28 |
Table 1.2332.c GPS week : 2332 MJD: 60568.0-60574.0
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 2332 0 | 5 26 -2 -1313 223 -5394 80.0 1866 1866 | 4880 0
brd 2332 1 | 15 -1 45 -1255 1105 -1014 81.2 1477 1477 | 8432 0
brd 2332 2 | -20 81 52 -1574 2683 -4334 82.1 1327 1327 | 8365 0
brd 2332 3 | 25 29 192 -573 1465 -5476 79.6 1327 1327 | 6841 0
brd 2332 4 | -16 0 143 -49 1523 -1760 79.5 1387 1387 | 6458 0
brd 2332 5 | 7 26 93 -425 2132 -8424 78.3 1609 1609 | 6245 0
brd 2332 6 | 0 98 108 -1201 1592 -8636 82.0 1480 1480 | 7147 0
-------------+------------------------------------------------------------+----------------
brd 2332 mean| 2 37 90 -913 1531 -5005 80.4 1496 1496 | 6909 0
brd 2332 sdev| 16 38 65 562 773 2948 1.4 191 191 | 1242 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 2.2332.0 GPS week: 2332 Day: 0 MJD: 60568
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 8 1 16 .14 16 14 | -3436 -2568 4169 16800
esa n/a| -1 -1 0 -10 0 -43 -.04 23 16 | 13428 -3437 3401 7079
gfz n/a| 1 -1 1 31 22 -44 .09 30 17 | 0 -3086 3398 7648
grg n/a| 0 1 4 6 -31 10 .33 24 20 | 3070 -2679 4193 16742
iac n/a| 1 0 -5 6 2 44 -.26 17 16 | 4319 -2090 4142 15965
jgx n/a| 1 0 -6 -47 0 -3 -.15 27 26 | 662 -3220 3448 7710
Table 2.2332.1 GPS week: 2332 Day: 1 MJD: 60569
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 4 23 34 .14 15 14 | -857 1122 3572 14547
esa n/a| 0 -2 0 -23 -14 15 -.04 19 15 | 4797 1134 3003 6082
gfz n/a| 0 0 5 11 -2 16 -.09 25 13 | 0 813 3059 6360
grg n/a| 2 0 -1 4 -18 -44 .26 18 16 | 5046 1147 3654 14600
iac n/a| 0 0 -4 22 28 13 -.08 15 14 | 7639 1265 3546 13671
jgx n/a| -2 0 -3 -49 -21 22 -.14 22 22 | 3527 348 2996 6438
Table 2.2332.2 GPS week: 2332 Day: 2 MJD: 60570
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 1 -5 9 60 .14 18 15 | 161 -2868 3600 16579
esa n/a| 1 -2 -3 -7 -15 -8 -.06 19 17 | 1916 -1852 2975 7468
gfz n/a| -1 0 4 13 19 -6 -.08 18 13 | 0 -1780 2918 7624
grg n/a| 0 2 -1 32 9 -3 .35 20 16 | 6459 -2352 3604 16675
iac n/a| 3 0 -4 30 -64 -142 -.21 22 21 | 8922 -2513 3602 15853
jgx n/a| 0 0 -5 -64 -22 31 -.19 26 25 | 3746 -1740 2919 7709
Table 2.2332.3 GPS week: 2332 Day: 3 MJD: 60571
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 -28 15 96 .09 22 15 | -2560 2036 3327 16226
esa n/a| 1 0 0 -15 -13 -45 -.06 21 17 | 19419 1631 2757 8843
gfz n/a| 0 0 2 42 6 -61 -.01 27 12 | 0 3170 2768 7218
grg n/a| 1 0 0 5 -17 -52 .37 23 17 | 2757 1695 3411 16111
iac n/a| 0 0 1 11 -2 61 -.22 23 20 | 6714 -445 3311 15291
jgx n/a| 0 0 -7 -29 -4 13 -.14 25 25 | 2260 2669 2769 7324
Table 2.2332.4 GPS week: 2332 Day: 4 MJD: 60572
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 3 -11 -14 68 .16 22 18 | -216 -1746 3941 16953
esa n/a| 0 0 -2 -37 -17 38 -.05 19 15 | 9069 -522 2648 6343
gfz n/a| 0 0 7 52 -6 20 -.10 23 15 | 0 -285 2679 7131
grg n/a| 2 1 5 -2 23 -43 .37 25 19 | 4150 -2526 4152 17573
iac n/a| 0 0 -5 5 49 -124 -.10 19 17 | 6913 -1507 3827 15799
jgx n/a| 0 0 -6 -44 -34 25 -.15 27 27 | 4455 -512 2692 7324
Table 2.2332.5 GPS week: 2332 Day: 5 MJD: 60573
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 -7 -27 48 .13 18 15 | -592 -2177 3533 14397
esa n/a| 0 0 0 -44 -52 -22 -.03 18 15 | 5574 -1874 3142 6565
gfz n/a| 0 1 5 37 -6 9 .02 17 16 | 0 -2053 3218 6715
grg n/a| 2 1 4 -25 -3 4 .20 22 18 | 4340 -1804 3622 14175
iac n/a| 0 -1 -7 36 64 -18 -.16 14 13 | 6371 -345 3500 13447
jgx n/a| 0 0 -3 -49 -34 5 -.13 20 20 | 4012 -1827 3237 6932
Table 2.2332.6 GPS week: 2332 Day: 6 MJD: 60574
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 -6 -13 40 .17 20 15 | -254 -2752 4278 15436
esa n/a| 0 2 0 -39 -8 15 -.02 22 18 | 2146 -1878 3434 7663
gfz n/a| -1 0 5 64 48 -26 -.01 20 16 | 0 -1002 3500 7850
grg n/a| 2 0 1 -34 -3 15 .31 26 20 | 5763 -2849 4349 15333
iac n/a| 2 0 -6 26 21 -59 -.16 20 18 | 8005 -2286 4201 14375
jgx n/a| -1 0 -4 -25 -31 41 -.19 23 23 | 3993 -1281 3506 7937
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 3.2332.0 GPS week: 2332 Day: 0 MJD: 60568
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 742 21 24 22 29 20 47 12 | 80 64 80 70 81 69 73
R02 | 2805 10 18 11 13 9 16 5 | 45 51 43 43 42 38 43
R03 | 1269 5 15 7 16 17 24 6 | 53 51 50 62 61 46 53
R04 | 990 8 11 10 19 13 12 5 | 53 46 47 45 55 40 48
R05 | 1159 9 11 13 13 14 10 5 | 50 51 50 56 56 45 51
R07 | 1180 13 17 15 12 16 25 7 | 67 59 57 63 69 45 60
R08 | 1590 12 11 23 13 8 15 6 | 62 64 74 71 72 57 65
R09 | 2819 13 13 14 11 12 14 6 | 62 65 63 59 64 60 62
R11 | 2471 12 14 18 18 15 14 6 | 30 34 31 26 27 29 27
R12 | 700 14 10 17 27 14 14 7 | 59 64 70 84 68 56 65
R14 | 818 9 13 17 13 23 17 7 | 87 78 79 86 99 68 84
R15 | 675 10 17 16 19 14 26 7 | 100 84 92 109 99 79 94
R16 | 1800 10 16 16 27 22 17 8 | 90 92 96 79 97 78 88
R17 | 2317 13 20 16 27 13 26 8 | 65 58 61 61 58 46 57
R18 | 1022 14 23 26 21 24 16 9 | 55 68 58 66 62 53 58
R19 | 2493 38 46 63 64 23 59 21 | 76 56 74 50 61 37 56
R20 | 2612 26 58 92 34 30 58 22 | 61 87 91 71 73 91 66
R21 | 1472 14 17 23 14 14 21 7 | 70 55 77 74 65 52 64
R22 | 2983 18 12 11 16 13 21 7 | 37 40 51 49 48 45 42
R24 | 1972 13 18 26 21 12 21 8 | 55 63 67 70 63 54 59
XR25 | 7945 9 14 --- --- 10 --- 8 | 32 40 --- --- 39 --- 36
XR26 |20273 35 --- --- 33 62 --- 32 | 33 --- --- 32 68 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1865 16 23 30 24 17 27 |T 60 60 65 63 64 54 58
WRMS | 1865 14 16 17 20 16 26 |NE 60 60 65 63 64 54 58
MEDI | 1590 13 16 16 19 14 17 |MD 59 59 63 63 63 52 58
Table 3.2332.1 GPS week: 2332 Day: 1 MJD: 60569
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1031 31 23 24 26 22 31 12 | 54 52 42 45 54 42 46
R02 | 2543 8 19 14 12 13 6 5 | 32 42 30 35 29 33 31
R03 | 1423 10 9 13 16 8 7 5 | 34 32 32 28 29 33 28
R04 | 1043 6 14 11 11 19 27 7 | 31 32 37 44 47 24 35
R05 | 1003 11 14 11 19 8 9 5 | 32 39 41 56 43 44 41
R07 | 918 10 8 11 8 12 19 5 | 36 40 34 36 38 32 35
R08 | 738 18 12 11 14 18 22 7 | 40 50 42 50 47 44 44
R09 | 1448 12 16 12 18 12 24 7 | 34 45 38 34 42 40 37
R11 | 2275 15 12 16 17 7 16 6 | 18 25 31 20 20 25 20
R12 | 834 12 14 13 16 13 19 6 | 45 48 54 58 55 41 49
R14 | 1184 14 12 21 10 17 22 7 | 60 58 43 55 59 43 53
R15 | 557 9 19 13 28 9 10 7 | 72 60 63 90 70 65 70
R16 | 1065 14 20 12 17 20 19 8 | 71 76 78 67 83 60 72
R17 | 1064 18 25 18 13 12 18 8 | 46 41 34 44 41 31 38
R18 | 839 16 16 14 18 19 15 7 | 44 48 46 51 51 49 46
XR19 | 1363 43 37 47 43 23 --- 19 | 54 45 66 49 45 --- 51
R20 | 1149 23 48 89 26 22 54 21 | 47 66 55 37 40 57 39
R21 | 1470 16 15 11 20 13 19 7 | 43 33 38 53 33 29 37
R22 | 3085 19 11 21 14 12 24 7 | 26 39 40 44 32 37 33
R24 | 1656 9 16 13 17 14 17 6 | 33 37 33 38 36 31 33
XR25 |12650 16 13 --- --- 17 --- 11 | 34 30 --- --- 29 --- 29
XR26 |19571 32 --- --- 30 55 --- 29 | 18 --- --- 26 37 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1477 15 19 25 18 15 22 |T 41 44 43 45 43 40 40
WRMS | 1477 14 15 13 16 14 22 |NE 41 44 43 45 43 40 40
MEDI | 1149 14 15 13 17 13 19 |MD 36 42 40 44 41 40 37
Table 3.2332.2 GPS week: 2332 Day: 2 MJD: 60570
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 721 25 23 15 29 25 48 12 | 68 60 49 48 61 51 53
R02 | 1867 14 15 6 17 18 13 6 | 49 54 46 59 42 48 48
R03 | 1680 7 12 6 10 18 15 5 | 48 54 47 46 43 50 47
R04 | 1180 8 14 8 17 19 17 6 | 46 57 52 48 57 41 49
R05 | 952 8 17 15 12 15 36 8 | 42 47 41 53 48 36 42
R07 | 931 17 11 8 10 14 26 6 | 51 53 52 52 45 54 50
R08 | 1235 17 12 11 9 27 14 7 | 52 57 57 65 63 46 56
R09 | 1959 13 15 12 15 14 15 6 | 47 58 58 43 56 45 50
R11 | 1746 21 25 15 16 27 21 9 | 37 43 35 32 37 29 32
R12 | 793 10 12 16 8 33 23 8 | 50 49 61 54 58 40 52
R14 | 1405 8 12 14 14 26 14 6 | 65 58 61 70 74 53 62
R15 | 866 9 22 9 19 21 25 7 | 85 71 77 93 86 65 80
R16 | 928 10 25 5 15 24 17 7 | 73 79 73 68 85 66 73
R17 | 912 15 21 13 13 18 17 7 | 52 40 42 53 50 45 45
R18 | 668 11 18 10 18 8 19 6 | 41 46 42 54 40 44 43
R19 | 1125 40 28 45 39 19 37 16 | 50 45 60 51 43 51 42
R20 | 772 40 30 40 45 30 52 18 | 70 90 105 108 74 100 85
R21 | 800 13 23 9 16 15 12 6 | 64 63 58 58 57 58 59
R22 | 2635 15 16 10 14 21 13 6 | 62 68 62 65 62 72 63
R24 | 1360 15 21 23 15 31 32 10 | 49 52 58 56 58 44 50
XR25 |16240 13 10 --- --- 19 --- 10 | 36 34 --- --- 30 --- 35
XR26 |17726 29 --- --- 21 63 --- 27 | 32 --- --- 47 54 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 1326 18 19 18 20 22 26 |T 53 56 56 58 55 51 52
WRMS | 1326 15 17 13 16 21 25 |NE 53 56 56 58 55 51 52
MEDI | 1125 13 17 11 15 19 17 |MD 50 54 57 54 56 48 50
Table 3.2332.3 GPS week: 2332 Day: 3 MJD: 60571
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 660 35 38 21 23 28 33 13 | 80 61 77 73 78 72 71
R02 | 854 10 14 19 13 16 19 7 | 53 56 58 59 41 46 51
R03 | 2372 19 15 10 33 22 16 9 | 60 70 66 81 59 63 65
R04 | 1543 13 16 14 9 20 11 6 | 55 61 53 52 50 55 53
R05 | 787 16 20 12 11 5 15 6 | 57 64 50 53 49 52 53
R07 | 1512 7 10 10 16 25 18 6 | 64 67 70 69 68 60 66
R08 | 1516 17 17 7 15 27 10 7 | 63 60 68 56 69 56 61
R09 | 1054 13 12 21 16 19 8 7 | 46 54 59 48 54 39 48
R11 | 1893 12 19 9 16 11 17 6 | 34 45 39 27 28 33 33
R12 | 1080 8 10 9 11 15 21 5 | 57 62 52 58 56 43 54
R14 | 1238 9 11 15 13 9 13 5 | 70 71 60 75 69 59 67
R15 | 1360 14 14 16 17 11 15 6 | 74 76 87 91 74 65 77
R16 | 972 14 19 13 9 23 27 8 | 74 73 70 70 81 53 69
R17 | 826 9 19 17 20 10 23 7 | 60 51 67 72 56 47 57
R18 | 938 12 15 15 15 15 13 6 | 46 54 51 59 49 47 50
R19 | 770 43 36 56 45 39 52 20 | 57 60 83 59 66 50 54
R20 | 958 60 41 89 57 53 58 27 | 52 92 112 82 51 106 69
R21 | 584 10 20 15 20 21 24 8 | 71 65 76 66 75 52 66
R22 | 2490 13 12 14 14 17 13 6 | 64 71 75 77 61 67 68
R24 | 1005 19 16 12 12 25 24 8 | 55 62 64 59 68 49 57
XR25 |14616 12 --- --- --- 21 --- 17 | 45 --- --- --- 47 --- 46
XR26 |17481 33 --- --- 21 55 --- 27 | 35 --- --- 39 57 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1326 22 21 27 23 23 25 |T 57 63 66 63 59 55 57
WRMS | 1326 15 17 12 17 20 25 |NE 57 63 66 63 59 55 57
MEDI | 1054 13 16 14 16 20 17 |MD 57 62 66 59 57 52 57
Table 3.2332.4 GPS week: 2332 Day: 4 MJD: 60572
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 834 29 29 14 32 19 45 12 | 57 58 62 54 65 64 58
R02 | 1842 10 16 13 13 10 26 6 | 39 56 52 41 48 34 45
R03 | 1704 11 11 8 32 9 18 7 | 44 49 48 64 46 43 48
R04 | 926 22 10 19 12 17 14 7 | 51 46 47 43 37 45 42
R05 | 1167 15 16 16 15 18 14 7 | 55 58 54 46 45 51 50
R07 | 1657 10 10 12 8 28 28 8 | 53 58 57 54 73 46 57
R08 | 917 12 9 24 24 14 19 7 | 47 48 61 48 54 47 50
R09 | 852 14 10 14 17 9 15 6 | 59 59 59 54 56 51 56
XR11 | 2174 12 16 24 --- 13 12 8 | 31 43 32 --- 40 33 35
R12 | 1390 14 17 20 23 17 30 9 | 58 71 80 65 74 44 65
R14 | 1315 12 11 19 11 16 15 6 | 62 54 72 66 51 47 57
R15 | 998 15 18 15 14 13 16 7 | 72 63 78 76 61 61 67
R16 | 1067 11 16 13 21 11 15 6 | 73 75 79 91 74 64 75
R17 | 1046 10 20 24 16 13 27 8 | 59 66 69 67 55 44 59
R18 | 895 23 16 11 23 11 18 8 | 53 67 61 70 56 49 59
R19 | 760 52 50 63 68 34 57 24 | 76 64 91 50 77 68 65
R20 | 2814 48 20 36 17 43 42 16 | 51 33 43 38 60 49 33
R21 | 1301 14 18 26 18 11 27 8 | 50 43 64 52 50 33 46
R22 | 2158 15 14 14 22 12 17 7 | 68 72 77 75 65 76 70
R24 | 685 12 14 16 15 19 20 7 | 55 55 56 63 54 45 53
XR25 |11172 18 11 --- --- 16 --- 11 | 37 34 --- --- 29 --- 31
XR26 |11860 33 --- --- 29 49 --- 28 | 30 --- --- 34 51 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1387 22 19 23 24 19 27 |T 53 55 62 57 55 49 52
WRMS | 1387 18 15 15 19 17 27 |NE 53 55 62 57 55 49 52
MEDI | 1167 14 16 16 17 14 18 |MD 53 58 61 54 54 47 53
Table 3.2332.5 GPS week: 2332 Day: 5 MJD: 60573
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 617 36 26 21 40 10 49 14 | 48 36 37 36 31 39 33
R02 | 2253 7 11 9 8 15 12 5 | 30 32 31 29 37 30 30
R03 | 726 8 7 9 10 12 18 5 | 32 34 39 33 40 28 33
R04 | 646 15 8 9 10 10 19 5 | 38 31 31 31 29 23 29
R05 | 740 15 14 15 11 13 6 6 | 36 29 23 29 28 25 26
R07 | 1369 11 10 13 10 15 14 5 | 34 36 34 29 36 32 32
R08 | 481 15 16 11 21 19 10 7 | 35 38 49 52 47 43 43
R09 | 1321 15 11 13 13 5 15 5 | 50 50 56 46 53 48 50
R11 | 1779 14 16 26 19 12 12 7 | 28 31 33 21 30 24 25
R12 | 1834 13 19 21 19 12 14 7 | 51 49 70 64 59 47 55
R14 | 652 9 11 10 14 9 20 5 | 54 47 53 56 48 36 48
R15 | 504 10 21 13 23 9 11 6 | 60 53 67 78 57 61 61
R16 | 849 14 23 15 18 8 16 7 | 58 54 67 69 59 58 59
R17 | 1048 12 24 10 18 18 19 7 | 41 34 32 52 46 32 38
R18 | 721 22 11 21 31 9 19 8 | 34 42 48 60 35 36 39
XR19 | 891 69 60 43 53 19 --- 25 | 63 42 59 35 38 --- 39
R20 | 4527 45 29 34 44 34 37 16 | 71 46 57 49 40 45 44
R21 | 2192 8 25 22 21 10 18 8 | 49 44 59 58 46 40 47
R22 | 1743 13 13 12 20 12 12 6 | 45 52 46 59 50 50 48
R24 | 678 10 17 16 22 17 10 7 | 42 40 34 52 48 43 41
XR25 |14717 17 15 --- --- 10 --- 10 | 22 29 --- --- 20 --- 18
XR26 |12909 23 --- --- 29 31 --- 20 | 51 --- --- 63 50 --- 54
------+-----------------------------------------+-------------------------------------
RMS | 1608 18 18 17 22 14 20 |T 44 40 46 47 42 38 40
WRMS | 1608 15 15 16 18 13 20 |NE 44 40 46 47 42 38 40
MEDI | 891 14 16 13 19 12 15 |MD 42 40 46 52 40 39 39
Table 3.2332.6 GPS week: 2332 Day: 6 MJD: 60574
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 797 29 12 28 33 12 38 12 | 86 62 67 66 77 69 70
R02 | 2252 10 11 12 16 16 17 6 | 47 51 47 45 55 38 46
R03 | 851 13 16 13 17 21 15 7 | 58 55 52 63 67 49 56
R04 | 992 17 10 17 11 12 17 6 | 58 52 53 47 57 43 51
R05 | 1310 13 17 12 17 8 10 6 | 59 56 51 52 52 48 52
R07 | 918 11 15 12 16 19 9 6 | 60 55 56 53 60 52 55
R08 | 825 15 9 14 13 12 13 5 | 58 65 69 68 71 58 64
R09 | 1666 13 18 15 22 16 14 7 | 69 76 74 60 71 64 68
R11 | 1689 15 15 29 19 23 14 9 | 31 34 33 21 37 28 28
R12 | 2129 6 14 14 14 16 13 6 | 65 61 63 74 75 54 65
R14 | 1859 8 14 14 14 12 14 6 | 70 69 70 70 65 54 65
R15 | 968 12 16 11 21 7 10 6 | 82 66 72 93 75 70 75
R16 | 820 14 23 17 14 12 15 7 | 79 69 82 72 75 58 72
R17 | 695 9 23 20 16 19 20 8 | 70 64 77 77 75 55 69
R18 | 796 13 14 12 17 11 19 6 | 54 65 51 72 63 58 59
R19 | 1166 39 58 40 78 56 63 25 | 69 39 77 51 89 50 54
R20 | 2022 58 40 39 41 26 38 18 | 80 62 54 56 55 55 49
R21 | 1646 8 16 10 18 14 21 6 | 69 61 74 79 69 54 66
R22 | 2850 15 11 12 15 12 10 5 | 48 57 56 60 51 51 52
R24 | 710 10 22 11 21 18 10 7 | 67 73 72 73 74 65 69
XR25 |16869 17 15 --- --- 15 --- 11 | 20 35 --- --- 30 --- 26
XR26 | 9301 33 --- --- 29 49 --- 27 | 43 --- --- 65 72 --- 55
------+-----------------------------------------+-------------------------------------
RMS | 1480 20 22 20 26 20 23 |T 61 58 62 62 64 53 57
WRMS | 1480 15 17 16 19 18 23 |NE 61 58 62 62 64 53 57
MEDI | 1166 13 15 14 17 15 14 |MD 60 61 63 65 67 54 56
More information about the IGSREPORT
mailing list