[IGSREPORT-29051] Wk 2235 IGLOS Final Orbits
acc
acc at igs.org
Sat Nov 26 22:50:07 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2235 (Nov 06, 2022 - Nov 12, 2022)
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 2.2235.
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:
igl2235[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2235 in the SP3 format.
igl22357.sum Combination Report for GPS Week 2235.
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.
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 | -1.6 ns
1 | -1.2 ns
2 | 1.1 ns
3 | -0.7 ns
4 | 0.7 ns
5 | 0.8 ns
6 | -2.1 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
----+--------+---------------
0 | ESX | R22
1 | ESX | R22
2 | ESX | R22
2 | GRG | R11
3 | ESX | R22
4 | ESX | R22
5 | ESX | R22
6 | ESX | R22
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 1.2235, 1a.2235).
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 2.2235.0-6)
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 3.2235.0-6).
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 2235 summary. (Nov 06, 2022 - Nov 12, 2022)
Table 1.2235.a GPS week : 2235 MJD: 59889.0-59895.0
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 8 -6 14 43 .09 25 17 | 32545 -991 2986 8414
| 1 2 1 14 11 28 .04 | 1120 2307
emx n/a| 0 1 -1 31 -9 -15 -.06 46 28 | -486 -750 2978 8319
| 2 1 1 18 11 34 .05 | 5726 1700
esx n/a| 0 2 2 -10 8 -5 -.05 34 23 | -412 -614 2972 7323
| 0 1 1 24 13 35 .04 | 8366 2389
gfz n/a| -1 1 6 -2 4 -8 -.02 26 16 | 0 -1097 3011 8178
| 1 2 2 22 16 28 .08 | 0 2473
grg n/a| 0 -4 -17 7 -15 -40 .19 329 22 | -213 -818 3104 7999
| 1 1 2 12 15 75 .03 | 181 2847
iac n/a| 0 0 -2 -20 -5 20 -.18 31 29 | 2015 -634 2986 8850
| 2 4 2 32 34 112 .06 | 839 1310
Table 1.2235.b GPS week : 2235 MJD: 59889.0-59895.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 13 16 16 14 14 17 14 |
R02 | 6 7 5 8 6 9 8 |
R03 | 8 7 6 5 10 6 7 |
R04 | 8 9 10 7 9 8 6 |
R05 | 8 10 10 10 12 11 9 |
R07 | 6 7 10 9 6 8 6 |
R08 | 8 10 9 9 9 9 8 |
R09 | 12 11 13 15 15 15 12 |
R11 | 10 8 10 7 9 11 9 |
R12 | 9 9 10 8 8 9 9 |
R13 | 16 18 17 15 15 12 13 |
R14 | 8 8 7 12 13 9 7 |
R15 | 7 8 16 8 9 8 8 |
R17 | 8 8 8 9 7 7 7 |
R18 | 9 10 9 9 9 10 8 |
R19 | 32 33 28 30 34 33 30 |
R20 | 27 29 27 26 30 35 34 |
R21 | 8 7 9 8 7 7 7 |
R22 | 11 16 19 15 18 14 12 |
R24 | 8 9 9 11 8 9 8 |
Table 1.2235.c GPS week : 2235 MJD: 59889.0-59895.0
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 2235 0 | 65 21 23 291 -3184 -1976 82.2 2137 2137 | -1553 0
brd 2235 1 | -36 135 106 -2238 -908 -3780 81.5 2024 2024 | -1216 0
brd 2235 2 | -20 11 77 1573 -1462 -15820 81.8 1750 1750 | 1072 0
brd 2235 3 | -10 -32 -37 45 -24 6191 80.3 1323 1323 | -719 0
brd 2235 4 | 5 38 46 160 988 5643 81.7 1368 1368 | 723 0
brd 2235 5 | 19 66 83 -410 750 5354 80.7 1436 1436 | 802 0
brd 2235 6 | -29 33 74 152 1060 9886 81.4 1581 1581 | -2119 0
-------------+------------------------------------------------------------+----------------
brd 2235 mean| 0 39 53 -60 -396 785 81.4 1659 1659 | -430 0
brd 2235 sdev| 35 52 48 1137 1563 8762 .7 322 322 | 1285 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 2.2235.0 GPS week: 2235 Day: 0 MJD: 59889
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 9 -25 9 4 .08 24 17 | 34184 -2833 2703 7919
emx n/a| 4 3 0 11 -11 -59 .01 44 27 | 8599 -1931 2704 7967
esx n/a| -2 2 3 -4 20 53 -.07 31 23 | 654 -2287 2651 6233
gfz n/a| 0 -2 4 22 22 -18 -.04 30 20 | 0 -3387 2694 7551
grg n/a| -2 -6 -15 15 -26 -86 .17 25 19 | -357 -2738 2670 7335
iac n/a| 0 0 -1 4 8 72 -.24 26 25 | 1203 -584 2665 8286
Table 2.2235.1 GPS week: 2235 Day: 1 MJD: 59890
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 -2 10 10 0 23 .12 25 18 | 31588 -2978 2875 9271
emx n/a| 0 2 -2 14 2 36 -.04 49 30 | 6175 -1874 2871 9223
esx n/a| -1 2 0 9 27 -20 -.08 34 31 | -16799 -1971 2841 9865
gfz n/a| 0 2 5 3 10 -24 -.04 26 15 | 0 -2677 2900 8806
grg n/a| 1 -2 -17 -5 -33 80 .20 29 28 | -80 -2770 2868 8825
iac n/a| 3 0 0 -37 -14 -72 -.11 28 26 | 954 -662 2853 9606
Table 2.2235.2 GPS week: 2235 Day: 2 MJD: 59891
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 9 11 35 63 .10 23 16 | 30970 1937 3672 8136
emx n/a| -1 0 -1 33 -22 -36 -.13 45 31 | -6437 742 3573 7850
esx n/a| 0 0 0 27 -13 -48 -.03 31 23 | 6092 1795 3581 7825
gfz n/a| -1 1 8 0 -18 -28 .01 24 16 | 0 2127 3736 7830
grg n/a| 0 -5 -14 -3 2 29 .13 2134 25 | -333 2403 4377 8320
iac n/a| -3 4 -6 -72 -52 -39 -.20 32 30 | 3123 -11 3605 8506
Table 2.2235.3 GPS week: 2235 Day: 3 MJD: 59892
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 8 -9 15 17 .07 28 20 | 32344 -1567 2775 7245
emx n/a| -2 0 -1 12 -7 -24 -.06 45 32 | -451 -1056 2799 7112
esx n/a| 0 5 4 -19 7 -10 -.11 28 22 | -5666 -2080 2788 5679
gfz n/a| -2 0 10 1 19 -31 .12 25 15 | 0 -1758 2782 7126
grg n/a| 0 -5 -17 -4 -5 -80 .16 24 19 | -92 -1632 2853 6656
iac n/a| 1 0 -4 2 -27 224 -.28 35 34 | 2221 -1645 2810 7832
Table 2.2235.4 GPS week: 2235 Day: 4 MJD: 59893
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 2 8 -17 22 47 .15 27 17 | 32583 953 2665 9340
emx n/a| 0 0 -1 58 -26 -37 -.01 49 27 | -4390 1215 2659 9310
esx n/a| 0 1 3 -17 2 -26 -.02 32 19 | 2573 1115 2675 8738
gfz n/a| -2 0 2 -30 13 -8 -.08 23 15 | 0 948 2647 9106
grg n/a| 1 -5 -18 28 -33 -20 .21 33 23 | -360 1651 2678 8852
iac n/a| 0 6 -3 -13 55 69 -.13 35 33 | 1984 726 2688 9988
Table 2.2235.5 GPS week: 2235 Day: 5 MJD: 59894
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 8 -2 9 79 .03 24 18 | 33727 1203 2943 8973
emx n/a| 0 1 0 40 -6 22 -.13 48 24 | -2563 844 2958 8662
esx n/a| 0 3 4 -45 5 34 -.05 41 22 | 7375 2612 3017 6898
gfz n/a| -3 4 8 22 -8 49 -.12 29 17 | 0 1147 2996 8858
grg n/a| 2 -3 -21 13 -4 -143 .21 31 22 | -356 2107 3032 8532
iac n/a| 2 -7 -1 -45 -20 -105 -.11 34 30 | 3016 675 3028 9332
Table 2.2235.6 GPS week: 2235 Day: 6 MJD: 59895
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 5 -13 10 65 .07 21 15 | 32421 -3656 3271 8020
emx n/a| 2 0 -3 47 2 -12 -.05 46 24 | -4339 -3193 3283 8109
esx n/a| 0 1 3 -25 10 -17 .02 42 25 | 2887 -3488 3252 6025
gfz n/a| -1 1 7 -34 -8 0 -.01 24 16 | 0 -4082 3322 7970
grg n/a| 1 -4 -17 13 -5 -60 .22 30 20 | 83 -4751 3251 7479
iac n/a| 0 1 -2 17 10 -6 -.16 28 24 | 1604 -2941 3254 8401
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 3.2235.0 GPS week: 2235 Day: 0 MJD: 59889
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1040 32 35 32 24 16 31 12 | 85 74 61 69 73 65 69
R02 | 1416 10 12 14 13 8 19 5 | 49 36 49 50 53 57 50
R03 | 1466 9 14 15 19 17 24 7 | 58 63 64 62 71 70 63
XR04 | 1396 11 13 13 --- 13 22 7 | 62 63 58 --- 58 64 60
R05 | 951 16 18 15 20 12 22 7 | 53 56 52 45 47 58 49
R07 | 1081 7 13 9 20 9 22 6 | 62 63 59 58 63 80 63
R08 | 1305 14 12 19 25 8 27 8 | 54 58 70 70 62 75 63
R09E | 3621 23 25 18 29 31 36 12 | 129 125 134 145 128 143 132
R11E | 2880 21 24 16 21 25 24 9 | 45 43 55 53 743 57 50
R12E | 912 15 32 14 17 13 26 8 | 250 243 252 256 254 258 252
R13E | 659 24 50 43 29 32 39 16 | 71 47 65 78 63 65 60
R14E | 4782 14 23 21 10 14 18 7 | 91 80 86 85 86 80 84
R15E | 2375 9 26 13 14 17 16 7 | 56 42 55 59 63 59 56
R17 | 779 10 29 14 15 15 17 7 | 53 36 43 50 47 58 47
R18 | 657 15 26 23 14 15 24 8 | 44 43 58 44 47 55 46
R19 | 1985 48 123 67 79 73 30 31 | 89 65 67 116 72 80 70
R20 | 3768 62 95 77 61 22 36 27 | 90 55 62 82 77 72 57
R21 | 1032 17 27 14 13 14 26 8 | 62 46 52 52 48 68 53
XR22 | 3948 --- --- 366 --- 11 11 11 | --- --- 153 --- 39 44 41
R24 | 1332 9 33 15 19 21 10 8 | 59 41 59 58 57 57 54
------+-----------------------------------------+-------------------------------------
RMS | 2137 24 44 31 30 25 26 |T 76 67 77 79 107 78 70
WRMS | 2137 17 27 23 20 19 25 |NE 63 53 64 63 58 64 56
MEDI | 1332 15 26 15 19 15 24 |MD 62 56 59 59 63 65 57
Table 3.2235.1 GPS week: 2235 Day: 1 MJD: 59890
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 771 37 42 33 37 31 34 16 | 49 48 46 49 55 39 42
R02 | 1122 12 12 14 12 12 23 6 | 32 27 29 39 35 34 31
R03 | 1636 9 10 8 15 13 27 6 | 39 41 48 40 41 65 44
XR04 | 1412 10 13 15 --- 15 30 9 | 42 51 45 --- 42 65 47
R05 | 1001 19 16 25 22 18 29 10 | 37 42 64 50 29 43 40
R07 | 890 9 7 8 9 22 28 7 | 42 42 50 42 38 56 43
R08 | 631 23 21 18 21 18 28 9 | 38 31 41 45 46 61 42
R09E | 3968 24 19 23 23 22 33 11 | 104 115 131 127 112 117 116
R11E | 2846 14 20 15 14 15 30 8 | 17 19 24 19 942 34 20
R12E | 1292 15 26 21 12 15 32 9 | 263 255 263 258 254 284 262
R13E | 815 29 61 28 44 36 43 18 | 38 31 52 70 43 38 39
R14E | 3551 9 24 25 7 14 20 7 | 52 44 54 46 53 43 47
R15E | 2601 12 28 17 13 14 19 7 | 64 48 59 60 71 72 62
R17 | 1204 9 34 12 15 18 20 8 | 38 29 34 40 32 43 34
R18 | 819 8 21 40 21 15 14 9 | 37 33 42 36 34 43 34
R19 | 1293 48 149 64 59 75 38 32 | 73 45 58 68 56 56 50
R20 | 3858 59 86 98 46 60 32 29 | 58 36 44 47 76 59 41
R21 | 488 18 26 14 12 13 16 7 | 38 26 33 29 30 30 29
XR22 | 2636 --- --- 350 --- 13 17 15 | --- --- 107 --- 34 37 34
R24 | 1586 15 42 14 18 15 10 8 | 35 38 38 38 38 34 33
------+-----------------------------------------+-------------------------------------
RMS | 2023 25 49 34 26 29 28 |T 57 52 63 61 103 62 54
WRMS | 2023 18 30 31 15 28 26 |NE 42 37 48 43 41 47 38
MEDI | 1292 15 24 18 15 15 28 |MD 39 41 46 45 42 43 41
Table 3.2235.2 GPS week: 2235 Day: 2 MJD: 59891
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1050 32 41 45 39 25 27 16 | 57 58 46 50 56 62 49
R02 | 924 7 7 10 14 12 17 5 | 30 25 41 33 37 44 34
R03 | 1116 6 7 16 13 16 18 6 | 40 41 55 46 52 39 44
XR04 | 1040 12 19 21 --- 16 28 9 | 49 54 42 --- 40 54 45
R05 | 1612 14 14 32 15 17 37 10 | 39 41 44 32 30 60 37
R07 | 1062 9 11 13 16 18 49 9 | 46 46 57 55 45 89 54
R08 | 963 21 17 26 12 12 24 8 | 42 48 69 54 51 66 53
R09E | 3169 22 25 25 21 26 47 12 | 115 104 126 115 113 105 112
R11E | 1826 16 17 12 20 9051 30 9 | 26 24 34 37 9999 31 28
R12E | 942 16 32 15 13 13 40 9 | 218 209 216 221 224 202 215
R13E | 860 23 63 19 42 31 49 17 | 49 49 44 60 54 47 42
R14E | 2621 9 15 17 10 16 23 6 | 48 44 55 50 48 51 48
R15E | 1426 19 33 20 14 75 30 16 | 51 46 52 54 81 59 49
R17 | 1474 9 30 16 7 15 24 7 | 34 21 29 30 39 38 30
R18 | 863 15 25 26 17 20 21 9 | 29 30 39 30 32 39 29
R19 | 756 51 119 60 57 56 31 28 | 69 100 67 88 64 76 64
R20 | 3510 51 93 83 31 59 27 26 | 59 43 34 42 74 43 35
R21 | 950 11 28 13 21 22 28 9 | 37 27 33 48 36 53 37
XR22 | 2433 --- 33 349 --- 18 30 19 | --- 28 107 --- 32 36 27
R24 | 2573 12 44 12 10 13 27 9 | 33 32 30 31 39 57 32
------+-----------------------------------------+-------------------------------------
RMS | 1749 23 45 31 24 2133 32 |T 56 53 61 59 60 62 53
WRMS | 1749 16 31 23 16 25 30 |NE 43 42 49 44 44 54 40
MEDI | 1062 15 25 19 15 18 28 |MD 46 43 44 48 48 53 42
Table 3.2235.3 GPS week: 2235 Day: 3 MJD: 59892
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 646 42 29 34 21 22 33 13 | 75 71 46 59 53 54 55
R02 | 600 9 15 14 14 14 38 8 | 39 27 31 30 40 66 36
R03 | 762 10 12 13 10 11 15 5 | 47 51 59 53 62 61 55
XR04 | 826 8 11 20 --- 10 19 7 | 45 53 48 --- 50 61 48
R05 | 1024 18 12 26 17 13 44 10 | 46 46 41 37 40 58 40
R07 | 872 10 10 20 19 11 42 8 | 55 51 46 40 55 75 50
R08 | 873 8 16 24 13 20 30 8 | 50 49 64 56 48 74 53
R09E | 3366 30 24 26 28 36 47 14 | 97 95 119 113 101 94 100
R11E | 1091 14 16 11 12 20 20 7 | 25 25 34 30 9999 43 30
R12E | 1551 10 31 15 11 12 33 8 | 188 175 183 189 181 199 185
R13E | 1445 24 68 22 28 22 45 15 | 52 44 56 71 47 62 50
R14E | 1125 42 23 21 15 20 24 11 | 63 42 53 47 58 55 49
R15E | 1453 15 29 15 13 14 25 8 | 53 43 53 62 62 64 54
R17 | 1390 7 35 15 11 14 35 8 | 40 27 38 39 48 58 39
R18 | 535 20 34 26 14 11 21 9 | 32 35 51 38 35 45 36
R19 | 767 35 115 62 77 65 32 30 | 63 40 58 103 76 53 58
R20 | 1118 79 94 63 27 28 53 26 | 83 58 40 56 62 56 41
R21 | 957 7 32 14 12 11 38 8 | 43 24 35 42 42 61 39
XR22 | 1822 --- 29 359 --- 11 25 14 | --- 33 127 --- 37 52 41
R24 | 1474 21 39 21 22 14 31 10 | 40 36 38 29 34 49 31
------+-----------------------------------------+-------------------------------------
RMS | 1322 28 45 28 25 24 35 |T 59 51 61 60 59 67 54
WRMS | 1322 20 32 22 15 19 34 |NE 50 42 51 48 48 58 44
MEDI | 1024 15 29 21 14 14 32 |MD 50 43 48 47 50 58 48
Table 3.2235.4 GPS week: 2235 Day: 4 MJD: 59893
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 868 39 23 34 17 34 21 13 | 72 57 48 63 45 62 55
R02 | 602 10 9 8 12 18 20 6 | 40 33 47 51 43 40 42
R03 | 501 12 12 7 20 16 48 9 | 39 44 44 36 57 83 46
XR04 | 704 8 5 22 --- 14 34 9 | 40 40 38 --- 42 67 42
R05 | 770 18 15 22 28 19 51 12 | 35 38 49 44 40 71 40
R07 | 723 8 14 17 14 9 18 6 | 48 47 36 47 47 47 43
R08 | 1087 16 19 20 13 21 27 8 | 42 42 53 54 44 67 48
R09E | 3233 45 35 23 28 32 39 15 | 103 118 115 119 107 119 109
R11E | 906 20 18 7 14 34 25 9 | 34 39 38 36 833 46 35
R12E | 1839 11 33 13 11 16 31 8 | 247 245 244 241 248 254 245
R13E | 1111 25 51 40 23 22 38 14 | 38 38 46 42 46 47 36
R14E | 827 41 30 29 17 17 30 12 | 69 57 64 58 57 74 57
R15E | 1413 14 33 12 14 16 34 9 | 54 47 56 51 52 72 53
R17 | 2398 9 27 11 10 23 17 7 | 41 31 41 39 49 49 39
R18 | 492 13 24 25 20 14 29 9 | 33 31 44 34 42 45 35
R19 | 1634 36 133 73 59 104 31 34 | 67 78 62 90 79 68 63
R20 | 928 59 117 80 37 44 72 30 | 69 80 66 65 44 70 48
R21 | 742 11 26 12 10 12 29 7 | 44 35 41 42 42 51 40
XR22 | 2079 --- --- 356 --- 14 22 17 | --- --- 111 --- 46 38 40
R24 | 1174 18 22 17 13 14 28 8 | 45 33 39 32 42 48 37
------+-----------------------------------------+-------------------------------------
RMS | 1368 27 49 32 23 33 35 |T 61 59 64 63 100 70 57
WRMS | 1368 17 27 19 15 23 33 |NE 47 45 51 49 47 57 44
MEDI | 906 16 24 20 14 17 29 |MD 44 42 47 47 46 62 42
Table 3.2235.5 GPS week: 2235 Day: 5 MJD: 59894
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 923 43 35 45 34 39 21 17 | 50 44 46 50 27 47 39
XR02 | 724 16 --- 12 15 20 26 9 | 28 --- 22 17 18 33 20
R03 | 594 9 11 8 14 13 20 5 | 30 31 35 35 32 38 31
XR04 | 678 9 15 25 --- 13 18 8 | 33 31 33 --- 31 36 30
R05 | 988 14 13 26 31 13 34 10 | 29 34 45 36 37 45 33
R07 | 734 12 13 18 21 14 19 7 | 41 38 32 30 42 35 35
R08 | 1190 12 18 19 15 14 37 9 | 37 32 41 29 49 66 39
R09E | 3182 31 32 29 26 37 40 14 | 117 118 129 118 116 110 114
R11E | 995 17 21 10 22 35 27 10 | 23 24 29 24 416 42 27
R12E | 1784 17 26 21 15 17 28 9 | 223 222 222 222 222 214 220
R13E | 986 23 32 26 33 24 24 12 | 38 39 49 66 52 31 40
R14E | 1140 9 21 19 14 16 39 9 | 44 40 44 39 48 50 41
R15E | 1475 10 30 14 15 15 16 7 | 61 50 60 54 57 65 56
R17 | 2099 12 20 13 13 15 19 6 | 30 22 23 23 32 30 24
R18 | 657 14 22 37 15 14 22 9 | 25 23 36 29 29 36 26
R19 | 1938 53 134 84 52 74 44 33 | 56 55 54 44 43 60 38
R20 | 1146 38 111 119 71 60 77 35 | 64 53 64 98 80 96 61
R21 | 918 10 27 11 14 13 23 7 | 33 28 33 27 33 33 29
XR22 | 901 --- 17 355 --- 22 18 13 | --- 33 109 --- 27 29 23
R24 | 1185 19 22 9 19 16 27 8 | 39 29 30 39 33 25 28
------+-----------------------------------------+-------------------------------------
RMS | 1436 24 48 41 29 31 34 |T 52 49 56 54 71 56 47
WRMS | 1436 18 24 22 17 22 30 |NE 38 34 43 38 36 43 32
MEDI | 988 14 22 19 15 16 24 |MD 38 34 41 36 37 38 33
Table 3.2235.6 GPS week: 2235 Day: 6 MJD: 59895
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 838 23 33 38 31 30 32 13 | 85 70 49 55 55 79 62
XR02 | 962 12 --- 20 8 17 16 7 | 46 --- 49 43 42 56 45
R03 | 739 12 13 13 13 16 20 6 | 52 58 54 52 62 55 54
XR04 | 668 9 12 13 --- 9 18 6 | 54 55 52 --- 53 57 52
R05 | 1382 15 14 20 22 18 24 8 | 46 46 52 49 53 63 48
R07 | 770 7 16 11 15 10 22 6 | 58 61 53 50 61 67 56
R08 | 593 10 15 11 14 10 35 7 | 55 56 65 59 62 72 59
R09E | 2970 24 25 26 19 35 25 11 | 146 153 154 149 152 141 147
R11E | 1692 12 15 14 17 37 21 9 | 28 34 34 33 417 44 31
R12E | 2984 19 16 29 14 11 27 9 | 306 299 299 304 304 302 302
R13E | 1254 24 27 32 28 30 39 13 | 43 48 40 58 59 66 46
R14E | 1608 10 19 18 15 17 20 7 | 54 54 55 49 59 52 52
R15E | 1930 11 32 15 19 11 18 8 | 62 50 57 66 59 65 59
R17 | 1991 10 24 15 18 9 20 7 | 48 27 41 45 45 47 41
R18 | 867 13 15 32 11 12 16 7 | 32 27 51 32 37 45 35
R19 | 734 44 127 66 47 71 44 29 | 86 64 43 94 71 89 64
R20 | 973 46 108 135 53 61 48 34 | 111 63 72 108 104 85 74
R21 | 1308 9 31 10 13 16 15 7 | 54 38 46 50 53 55 48
XR22 | 1062 --- --- 345 --- 13 10 12 | --- --- 152 --- 28 22 23
R24 | 1407 15 29 15 14 15 16 7 | 56 35 49 47 48 42 46
------+-----------------------------------------+-------------------------------------
RMS | 1580 21 46 42 24 30 28 |T 74 68 73 74 91 75 67
WRMS | 1580 15 24 25 16 20 24 |NE 60 50 59 57 55 59 50
MEDI | 1062 12 19 18 15 16 20 |MD 54 54 52 50 59 57 52
More information about the IGSREPORT
mailing list