[IGSREPORT-30027] Wk 2325 IGLOS Final Orbits
acc
acc at igs.org
Mon Aug 19 00:30:46 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2325 (Jul 28, 2024 - Aug 03, 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 2.2325.
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:
igl2325[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2325 in the SP3 format.
igl23257.sum Combination Report for GPS Week 2325.
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 | 8.0 ns
1 | 6.1 ns
2 | 7.0 ns
3 | 9.2 ns
4 | 4.8 ns
5 | 5.8 ns
6 | 5.5 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
2 | GFZ | R13
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 1.2325, 1a.2325).
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 2.2325.0-6)
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 3.2325.0-6).
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 2325 summary. (Jul 28, 2024 - Aug 03, 2024)
Table 1.2325.a GPS week : 2325 MJD: 60519.0-60525.0
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| -2 -1 0 -6 -24 66 .19 21 16 | -137 -89 3210 10251
| 1 1 1 15 22 16 .03 | 905 1227
esa n/a| 0 -1 5 -3 10 15 -.17 30 22 | 2250 -258 3136 7445
| 1 0 1 17 14 19 .05 | 4377 1786
gfz n/a| 1 0 0 40 13 1 -.09 30 17 | 0 -313 3162 7974
| 2 0 1 10 29 33 .07 | 0 1473
grg n/a| 2 0 6 -47 14 -48 .39 29 19 | 5592 -66 3233 9275
| 2 0 2 29 24 53 .08 | 1300 1378
iac n/a| -1 1 -7 -4 -9 -17 -.14 18 16 | 7312 -288 3181 9856
| 0 1 2 10 34 45 .08 | 1221 684
jgx n/a| 0 0 -1 15 11 -43 -.12 28 27 | 4552 -474 3129 8078
| 1 0 2 18 11 37 .04 | 624 1673
Table 1.2325.b GPS week : 2325 MJD: 60519.0-60525.0
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 | 18 17 16 17 17 19 20 |
R02 | 7 7 7 8 8 8 7 |
R03 | 8 7 8 8 7 8 8 |
R04 | 8 7 7 8 7 7 7 |
R05 | 7 7 7 8 6 8 9 |
R07 | 9 8 8 7 7 9 9 |
R08 | 8 7 7 10 7 9 9 |
R09 | 5 6 6 5 5 7 7 |
R11 | 7 8 7 7 7 6 7 |
R12 | 6 7 7 6 8 6 7 |
R13 | 15 13 33 --- --- --- --- |
R14 | 5 6 6 6 6 6 5 |
R15 | 6 6 8 6 7 7 8 |
R16 | 6 7 7 8 7 9 8 |
R17 | 9 11 12 10 7 7 7 |
R18 | 7 8 9 14 7 7 6 |
R19 | 20 21 23 26 16 15 19 |
R20 | 26 32 34 29 27 31 28 |
R21 | 8 6 10 12 8 7 7 |
R22 | 7 7 7 7 11 8 7 |
R24 | 12 11 13 8 7 8 8 |
R25 | 12 10 12 13 11 9 10 |
R26 | 35 32 33 37 35 36 36 |
Table 1.2325.c GPS week : 2325 MJD: 60519.0-60525.0
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 2325 0 | 81 -68 136 319 4035 524 79.9 1683 1683 | 8001 0
brd 2325 1 | 46 12 248 844 2356 3426 80.5 1875 1875 | 6074 0
brd 2325 2 | -70 9 144 -611 1088 1273 81.6 1457 1457 | 7042 0
brd 2325 3 | -5 4 45 -1393 -239 -2212 78.3 1413 1413 | 9170 0
brd 2325 4 | 30 2 143 -320 -310 -112 83.5 1569 1569 | 4752 0
brd 2325 5 | 113 58 29 -372 -839 7863 81.9 1565 1565 | 5750 0
brd 2325 6 | -19 16 22 -1281 -1838 7137 80.1 1497 1497 | 5499 0
-------------+------------------------------------------------------------+----------------
brd 2325 mean| 25 5 110 -402 607 2556 80.8 1579 1579 | 6612 0
brd 2325 sdev| 62 37 82 804 2027 3775 1.7 156 156 | 1548 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 2.2325.0 GPS week: 2325 Day: 0 MJD: 60519
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| -4 0 -2 0 -21 40 .22 27 18 | 410 984 3499 13884
esa n/a| -1 0 3 -32 22 17 -.14 32 22 | 2469 998 3449 7050
gfz n/a| -1 0 0 39 -9 -22 -.08 24 14 | 0 823 3510 8901
grg n/a| 4 0 4 -1 -8 45 .34 29 24 | 4968 832 3563 13509
iac n/a| -1 0 -4 -1 18 25 -.09 16 14 | 7510 18 3464 13212
jgx n/a| 3 0 3 0 15 -93 -.12 25 23 | 5133 907 3500 9166
Table 2.2325.1 GPS week: 2325 Day: 1 MJD: 60520
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| -4 -1 0 1 -47 50 .19 21 16 | 1161 -1153 3135 10481
esa n/a| 0 0 4 0 23 47 -.18 35 20 | 4165 -2266 2995 8604
gfz n/a| 0 0 2 36 10 24 -.07 25 14 | 0 -1557 2957 8246
grg n/a| 5 0 4 -33 7 -94 .39 26 21 | 5588 -646 3110 9407
iac n/a| -1 1 -6 0 -8 -5 -.13 18 16 | 7363 -283 3096 10088
jgx n/a| 0 0 0 10 18 -41 -.12 35 34 | 5155 -2266 2761 8018
Table 2.2325.2 GPS week: 2325 Day: 2 MJD: 60521
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 -1 -11 -48 76 .22 21 17 | 84 -1179 3590 9490
esa n/a| 0 -1 6 -7 0 9 -.15 31 18 | 3849 -918 3483 7267
gfz n/a| 0 0 1 43 29 -20 -.06 34 19 | 0 -1818 3499 7814
grg n/a| 4 0 10 -85 27 -49 .27 31 19 | 7522 -1763 3605 8148
iac n/a| -2 1 -10 -7 6 7 -.16 19 15 | 7627 -65 3564 9247
jgx n/a| 0 0 -2 52 -1 -80 -.15 33 33 | 4803 -2146 3533 8045
Table 2.2325.3 GPS week: 2325 Day: 3 MJD: 60522
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 -12 -39 86 .22 25 19 | 375 1973 3270 9054
esa n/a| 0 -1 5 -6 3 36 -.09 30 22 | 8315 3128 3179 7344
gfz n/a| -1 1 0 48 2 -37 -.03 32 17 | 0 2240 3234 7983
grg n/a| 2 0 9 -83 52 -1 .36 34 20 | 7187 2245 3324 8467
iac n/a| 0 3 -6 1 -16 -34 -.24 19 20 | 9715 902 3241 8886
jgx n/a| 0 0 -5 25 15 -39 -.05 24 24 | 4752 2294 3214 8051
Table 2.2325.4 GPS week: 2325 Day: 4 MJD: 60523
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 -35 3 65 .21 19 14 | -1391 -1097 2771 9592
esa n/a| -2 0 6 25 -15 -5 -.16 28 23 | 2000 -1374 2738 7552
gfz n/a| 1 0 -2 42 -32 -12 -.02 27 16 | 0 -1371 2767 7332
grg n/a| 0 0 5 -34 -5 -51 .46 30 18 | 4006 -1373 2794 8547
iac n/a| 0 0 -5 -17 31 34 -.19 16 16 | 6099 -1217 2731 9077
jgx n/a| 0 0 0 0 6 -48 -.09 21 21 | 3438 -1389 2790 7423
Table 2.2325.5 GPS week: 2325 Day: 5 MJD: 60524
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 0 0 7 67 .13 17 14 | -1093 -463 2870 9380
esa n/a| 0 -1 6 -9 18 -1 -.24 28 25 | 1100 -780 2761 7644
gfz n/a| 1 1 0 20 51 24 -.24 33 20 | 0 -624 2771 7312
grg n/a| 0 0 6 -49 -7 -94 .45 25 17 | 5182 -241 2879 8498
iac n/a| 0 2 -10 9 -23 -78 .01 19 14 | 6305 -873 2844 8834
jgx n/a| 1 0 0 6 -2 17 -.18 29 29 | 4010 -785 2763 7463
Table 2.2325.6 GPS week: 2325 Day: 6 MJD: 60525
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 1 11 -25 77 .17 20 16 | -506 311 3335 9880
esa n/a| -1 -1 5 3 18 7 -.23 25 21 | -6148 -598 3348 6660
gfz n/a| 6 1 -2 51 41 54 -.13 31 19 | 0 115 3400 8234
grg n/a| 0 0 6 -45 37 -92 .49 26 17 | 4696 483 3362 8354
iac n/a| -2 0 -10 -18 -72 -72 -.19 21 16 | 6569 -504 3329 9650
jgx n/a| 0 0 -3 14 28 -16 -.13 26 26 | 4578 65 3347 8382
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 3.2325.0 GPS week: 2325 Day: 0 MJD: 60519
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1267 47 72 34 23 22 34 17 | 120 56 105 87 83 65 81
R02 | 1087 13 14 16 21 10 23 7 | 76 69 77 71 78 56 71
R03 | 1257 11 19 17 20 11 23 7 | 83 62 85 70 80 60 74
R04 | 2125 12 22 21 14 15 19 8 | 101 92 99 100 104 100 99
R05 | 695 17 15 15 16 11 22 7 | 89 75 78 69 83 70 77
R07 | 1580 22 11 19 31 11 22 8 | 90 70 85 58 76 62 73
R08 | 1049 16 16 11 27 10 23 7 | 81 72 79 64 77 63 72
R09 | 960 11 12 5 8 6 16 4 | 26 33 28 33 32 33 30
R11 | 1364 19 13 16 12 17 15 7 | 43 43 41 45 37 44 39
R12 | 1067 11 11 10 15 15 18 6 | 30 40 37 34 30 40 32
R13 | 704 28 26 19 55 20 52 15 | 20 18 191 19 34 18 19
R14 | 1417 12 11 13 11 10 12 5 | 38 34 39 34 28 35 33
R15 | 1000 15 18 12 14 11 14 6 | 39 40 36 43 40 41 37
R16 | 1105 18 17 8 15 10 18 6 | 46 47 48 41 50 51 46
R17E | 1013 19 14 17 29 21 21 9 | 142 146 143 143 155 137 145
R18E | 1485 12 22 14 23 9 17 7 | 59 61 59 68 64 63 60
R19E | 1572 52 55 60 41 18 39 19 | 78 69 87 74 57 75 63
R20E | 4939 71 90 63 60 32 35 26 | 87 80 92 53 56 56 50
R21E | 1181 17 17 11 21 15 24 7 | 132 134 134 131 130 132 131
R22E | 2162 16 12 11 26 9 13 6 | 52 56 55 68 56 53 54
R24E | 1298 22 20 19 53 22 19 12 | 103 96 93 97 96 91 92
XR25E |12308 15 23 --- --- 13 --- 12 | 34 38 --- --- 44 --- 39
XR26 | 8447 56 --- --- 51 45 --- 35 | 274 --- --- 277 270 --- 272
------+-----------------------------------------+-------------------------------------
RMS | 1683 27 32 24 29 16 25 |T 80 65 80 76 76 64 73
WRMS | 1683 18 22 14 24 14 23 |NE 77 53 73 69 73 52 70
MEDI | 1267 17 17 16 21 13 21 |MD 78 61 79 68 64 60 63
Table 3.2325.1 GPS week: 2325 Day: 1 MJD: 60520
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 557 38 68 35 18 16 38 16 | 80 38 80 56 70 50 62
R02 | 607 6 10 11 22 14 25 6 | 56 56 61 58 66 45 57
R03 | 2728 14 17 10 19 10 22 6 | 65 46 58 62 62 46 57
R04 | 1917 9 15 12 14 13 23 6 | 75 71 79 84 81 69 76
R05 | 645 14 11 20 19 10 16 6 | 58 57 51 52 59 52 54
R07 | 728 17 20 11 20 16 23 8 | 71 56 61 56 70 52 62
R08 | 641 12 10 21 19 9 20 7 | 61 57 63 47 48 48 53
R09 | 794 12 13 13 14 7 16 5 | 20 22 22 30 22 26 20
R11 | 1278 18 30 11 8 16 24 8 | 31 53 38 38 39 34 36
R12 | 741 16 14 15 16 15 19 7 | 16 30 28 18 22 22 17
R13 | 811 22 36 16 38 17 52 13 | 27 26 215 22 29 22 22
R14 | 1629 9 8 15 17 8 18 5 | 23 24 30 22 17 16 20
R15 | 1205 12 15 13 13 9 16 5 | 22 32 36 28 26 27 25
R16 | 863 17 13 17 23 6 16 7 | 27 32 31 22 28 30 25
XR17E | 963 16 24 16 28 20 --- 10 | 146 147 140 136 142 --- 141
R18E | 1381 10 24 14 28 12 16 8 | 42 47 38 59 43 39 42
R19E | 1308 53 52 57 23 32 60 21 | 72 42 71 65 43 64 50
R20E | 6042 37 106 70 70 40 105 31 | 67 73 97 73 68 68 63
R21E | 1371 11 11 18 19 7 17 6 | 118 117 122 120 119 115 118
R22E | 2060 14 17 12 22 11 11 6 | 30 38 37 38 35 35 33
R24E | 1594 22 18 12 29 32 15 10 | 109 105 106 106 111 112 106
XR25E |12426 13 17 --- --- 12 --- 9 | 29 38 --- --- 37 --- 34
XR26 |10870 43 --- --- 37 50 --- 32 | 233 --- --- 232 226 --- 229
------+-----------------------------------------+-------------------------------------
RMS | 1874 21 35 25 26 18 35 |T 64 54 69 64 63 48 60
WRMS | 1874 16 20 14 21 16 34 |NE 57 42 60 55 57 38 54
MEDI | 1278 14 17 15 19 13 19 |MD 58 46 61 56 48 45 53
Table 3.2325.2 GPS week: 2325 Day: 2 MJD: 60521
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 891 38 57 36 14 16 40 16 | 88 29 85 64 74 39 63
R02 | 740 8 9 17 20 17 17 6 | 61 55 47 52 70 56 57
R03 | 2388 17 20 17 25 12 15 8 | 73 49 66 66 65 59 62
R04 | 1884 9 8 22 18 10 25 7 | 105 104 112 95 101 106 103
R05 | 698 11 12 21 22 12 19 7 | 73 72 81 61 72 65 70
R07 | 1170 17 17 15 18 11 25 7 | 85 65 79 71 81 62 74
R08 | 739 9 13 21 20 13 18 7 | 75 66 78 68 79 70 72
R09 | 1236 13 9 18 15 10 19 6 | 22 25 30 24 24 26 22
R11 | 1408 18 10 19 10 12 14 6 | 21 20 29 24 24 21 19
R12 | 815 12 16 18 17 13 13 6 | 23 33 34 31 20 20 22
XR13 | 7270 47 --- 1170 43 49 --- 33 | 39 --- 536 22 68 --- 38
R14 | 1000 9 8 11 12 14 21 5 | 33 38 36 41 41 41 37
R15 | 1691 16 16 7 10 22 23 7 | 33 48 42 44 49 38 40
R16 | 1159 17 18 19 16 12 13 7 | 39 47 44 35 38 33 37
R17E | 1158 14 11 18 60 23 24 12 | 144 138 143 147 139 167 139
R18E | 1278 17 18 23 32 13 19 9 | 55 62 63 68 59 57 57
R19E | 1265 39 56 85 30 24 66 22 | 65 58 100 56 54 42 52
R20E | 2366 54 95 100 56 49 100 33 | 67 67 112 65 57 57 50
R21E | 1312 11 14 15 44 17 25 10 | 140 141 137 154 137 143 140
R22E | 2404 14 18 8 28 13 11 7 | 38 36 41 50 38 35 37
R24E | 1541 13 15 15 65 19 21 12 | 60 58 61 89 72 58 61
XR25E |15871 19 14 --- --- 15 --- 11 | 41 36 --- --- 42 --- 37
XR26 |12587 43 --- --- 38 52 --- 32 | 297 --- --- 304 298 --- 299
------+-----------------------------------------+-------------------------------------
RMS | 1456 21 31 34 31 19 33 |T 72 59 93 74 74 59 69
WRMS | 1456 17 18 19 19 15 33 |NE 71 50 92 66 73 48 67
MEDI | 1278 16 15 18 20 14 19 |MD 61 55 66 61 65 56 57
Table 3.2325.3 GPS week: 2325 Day: 3 MJD: 60522
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 985 39 59 49 22 12 26 16 | 103 39 113 89 76 63 77
R02 | 766 12 11 11 17 18 25 7 | 72 68 75 69 84 58 71
R03 | 1980 18 14 18 21 13 15 7 | 81 64 82 60 73 62 70
R04 | 1766 15 11 16 22 20 23 8 | 76 75 77 65 65 68 69
R05 | 1267 23 12 18 24 9 18 7 | 83 73 83 69 73 68 73
R07 | 836 19 16 16 17 11 16 7 | 91 73 86 76 85 74 80
R08 | 1035 10 17 15 18 32 27 10 | 87 81 85 79 103 70 84
R09 | 891 13 8 15 11 10 12 5 | 21 20 25 21 17 28 19
R11 | 1597 17 13 17 14 13 15 6 | 29 22 36 33 25 34 27
R12 | 1629 14 17 14 16 8 8 5 | 22 28 26 30 23 21 22
R14 | 795 8 15 18 12 8 16 6 | 29 41 37 29 29 26 29
R15 | 1583 11 15 15 12 13 11 5 | 37 43 40 45 41 35 38
R16 | 1026 17 25 12 14 16 12 7 | 35 55 39 42 38 44 39
R17E | 1019 19 14 24 32 23 13 9 | 167 163 161 167 147 139 159
R18E | 1082 21 16 14 64 33 21 13 | 54 56 56 62 73 50 52
R19E | 1858 50 65 76 71 27 57 25 | 42 73 73 70 32 48 38
R20E | 1630 63 85 83 73 34 49 28 | 62 80 88 40 39 53 44
R21E | 855 22 11 28 57 16 19 12 | 145 139 151 137 136 137 138
R22E | 2678 16 11 11 22 14 15 6 | 28 32 33 47 33 29 30
R24E | 1232 15 20 22 26 10 14 7 | 65 62 67 69 60 60 60
XR25E |17598 16 20 --- --- 19 --- 13 | 19 29 --- --- 24 --- 19
XR26 |16005 56 --- --- 43 54 --- 37 | 113 --- --- 140 118 --- 118
------+-----------------------------------------+-------------------------------------
RMS | 1412 25 30 32 34 19 24 |T 66 62 71 68 63 58 61
WRMS | 1412 19 22 17 20 20 24 |NE 62 52 61 60 60 50 58
MEDI | 1232 17 15 16 22 14 16 |MD 62 62 73 65 60 53 52
Table 3.2325.4 GPS week: 2325 Day: 4 MJD: 60523
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1041 47 60 24 24 15 32 16 | 99 45 77 76 70 44 66
R02 | 922 14 12 21 16 17 26 8 | 75 77 86 66 79 56 72
R03 | 845 15 12 12 17 17 16 7 | 77 64 61 64 74 61 67
R04 | 1304 11 11 13 24 11 22 7 | 89 84 82 74 77 89 82
R05 | 925 11 9 10 25 13 10 6 | 71 63 66 64 61 70 65
R07 | 1040 14 16 15 15 14 13 6 | 82 71 78 72 74 70 74
R08 | 1527 16 13 15 15 14 19 7 | 86 76 84 82 85 71 80
R09 | 1759 8 10 17 17 8 7 5 | 24 27 27 25 22 23 22
R11 | 3543 19 18 15 13 12 10 6 | 28 29 26 29 26 23 23
R12 | 1879 9 28 17 18 15 12 7 | 25 25 24 31 35 29 24
R14 | 1263 7 9 21 9 20 7 6 | 30 38 44 32 22 32 30
R15 | 1056 10 13 19 11 22 15 7 | 36 45 33 34 29 41 32
R16 | 559 15 17 13 13 19 17 7 | 38 46 43 34 46 37 38
R17E | 1106 10 23 17 21 10 15 7 | 110 114 113 112 113 99 110
R18E | 1175 12 24 16 19 13 7 6 | 53 56 50 61 59 50 53
R19E | 1831 15 40 50 52 17 35 15 | 54 60 60 52 50 44 46
R20E | 1925 42 78 80 86 30 52 27 | 64 79 108 53 51 59 51
R21E | 1102 16 19 22 23 12 10 7 | 161 163 158 157 156 157 158
R22E | 2526 14 10 21 54 24 12 11 | 68 68 66 98 55 68 66
R24E | 1049 12 20 17 15 12 18 7 | 57 57 60 59 53 50 53
XR25E |17109 16 16 --- --- 14 --- 11 | 50 49 --- --- 59 --- 52
XR26 |>>>>> 46 --- --- 41 56 --- 35 | 259 --- --- 270 255 --- 258
------+-----------------------------------------+-------------------------------------
RMS | 1568 19 28 27 30 16 21 |T 74 63 67 73 70 58 69
WRMS | 1568 14 23 16 18 16 21 |NE 72 53 56 68 68 49 66
MEDI | 1175 14 16 17 18 14 15 |MD 64 60 61 64 59 50 53
Table 3.2325.5 GPS week: 2325 Day: 5 MJD: 60524
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1213 35 74 45 20 27 44 19 | 90 42 107 75 87 44 73
R02 | 1055 9 12 21 16 17 24 7 | 65 58 75 65 66 46 61
R03 | 1340 15 16 12 17 19 19 7 | 74 57 68 64 79 57 67
R04 | 803 17 11 15 15 17 20 7 | 97 96 86 96 97 84 92
R05 | 834 16 13 16 27 12 13 7 | 74 73 57 64 70 63 66
R07 | 1530 12 20 23 23 18 26 9 | 77 61 90 79 82 55 73
R08 | 1584 9 21 22 19 24 23 9 | 73 61 89 72 90 57 73
R09 | 993 18 14 21 9 7 15 6 | 32 35 38 35 34 32 32
R11 | 2529 12 8 20 14 12 16 6 | 32 39 46 30 39 34 34
R12 | 2195 11 20 14 17 9 10 6 | 34 31 39 33 34 33 31
R14 | 1472 7 7 15 20 14 10 5 | 44 46 41 47 39 42 41
R15 | 1197 12 11 17 15 17 22 7 | 47 47 49 51 36 38 42
R16 | 686 16 20 42 17 13 13 9 | 49 56 59 52 52 39 47
R17E | 1043 11 16 19 19 16 14 7 | 122 119 121 122 121 102 119
R18E | 1358 9 23 21 19 11 8 7 | 54 63 52 58 55 50 53
R19E | 2640 25 25 32 50 30 30 14 | 71 74 76 100 69 75 71
R20E | 2290 38 71 109 61 38 94 30 | 69 77 123 72 61 69 65
R21E | 1063 10 19 14 21 8 11 6 | 116 122 112 110 117 111 114
R22E | 2225 12 13 23 28 10 15 7 | 62 59 62 58 64 59 59
R24E | 932 14 21 16 20 16 17 7 | 77 77 75 84 83 76 77
XR25E |17239 8 17 --- --- 10 --- 8 | 41 48 --- --- 45 --- 43
XR26 |15497 42 --- --- 41 62 --- 35 | 209 --- --- 185 205 --- 202
------+-----------------------------------------+-------------------------------------
RMS | 1564 17 28 33 25 18 29 |T 73 63 73 73 73 58 69
WRMS | 1564 14 25 20 17 14 29 |NE 71 54 64 67 72 48 66
MEDI | 1340 12 17 20 19 16 16 |MD 69 59 68 65 66 55 65
Table 3.2325.6 GPS week: 2325 Day: 6 MJD: 60525
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 599 40 71 30 23 42 41 20 | 140 51 132 111 130 82 107
R02 | 985 12 9 17 20 14 14 6 | 87 86 96 73 94 73 85
R03 | 820 16 13 11 15 14 26 7 | 99 76 88 84 96 72 86
R04 | 761 12 15 17 10 15 23 7 | 120 113 109 111 115 107 112
R05 | 1218 17 11 11 19 22 27 8 | 99 84 91 77 91 74 86
R07 | 1119 23 14 18 27 16 21 9 | 109 88 103 85 92 79 92
R08 | 995 8 17 27 21 16 25 8 | 101 94 117 101 109 80 99
R09 | 985 18 11 17 11 17 14 6 | 26 29 26 24 22 26 23
R11 | 1984 7 16 21 15 16 18 7 | 36 47 27 42 40 39 37
R12 | 1321 12 17 21 16 13 15 7 | 31 49 51 42 34 34 37
R14 | 762 7 10 11 14 13 11 5 | 42 44 41 41 34 40 39
R15 | 1151 17 22 18 14 12 15 7 | 46 49 48 50 42 40 43
R16 | 1941 15 23 22 15 19 16 8 | 47 57 54 46 48 50 47
R17E | 1031 9 23 13 21 12 12 7 | 114 106 111 124 119 104 114
R18E | 877 8 17 16 16 13 11 6 | 43 39 42 50 40 42 40
R19E | 2323 35 31 56 53 44 26 18 | 97 104 115 92 77 71 87
R20E | 2975 41 41 101 71 33 81 28 | 85 56 111 85 58 74 65
R21E | 784 15 16 21 18 10 18 7 | 119 123 124 130 121 121 122
R22E | 2885 15 10 19 28 13 9 7 | 43 47 53 57 50 47 46
R24E | 1070 13 23 20 21 12 11 7 | 59 67 69 75 66 68 65
XR25E |12586 15 12 --- --- 12 --- 9 | 32 33 --- --- 39 --- 33
XR26 |14073 40 --- --- 39 66 --- 36 | 260 --- --- 253 257 --- 255
------+-----------------------------------------+-------------------------------------
RMS | 1496 20 25 31 26 21 26 |T 83 68 80 83 80 66 78
WRMS | 1496 16 21 19 17 16 26 |NE 88 66 75 81 86 61 82
MEDI | 1070 15 16 18 19 14 16 |MD 85 57 88 77 66 71 65
More information about the IGSREPORT
mailing list