[IGSREPORT-29036] Wk 2234 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 18 03:02:59 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2234 (Oct 30, 2022 - Nov 05, 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 2.2234.
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:
igl2234[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2234 in the SP3 format.
igl22347.sum Combination Report for GPS Week 2234.
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 | -1.0 ns
1 | -7.2 ns
2 | -0.0 ns
3 | 0.0 ns
4 | 1.1 ns
5 | 0.1 ns
6 | 0.2 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
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 1.2234, 1a.2234).
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 2.2234.0-6)
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 3.2234.0-6).
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 2234 summary. (Oct 30, 2022 - Nov 05, 2022)
Table 1.2234.a GPS week : 2234 MJD: 59882.0-59888.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 9 -23 5 15 .11 26 19 | 32632 -356 3214 8680
| 1 1 2 9 16 26 .05 | 3278 896
emx n/a| 0 0 -7 14 -11 -36 .05 46 29 | -2251 -363 3202 8548
| 2 1 3 36 18 43 .05 | 12973 608
esx n/a| 0 1 2 -2 -12 11 -.07 32 22 | -4264 -21 3172 8678
| 2 1 1 20 13 34 .07 | 7615 1167
gfz n/a| 0 1 2 7 -27 0 -.03 28 16 | 0 -364 3266 8571
| 3 0 2 21 15 21 .06 | 0 1066
grg n/a| 0 -3 -11 -5 -10 -23 .22 27 22 | -999 -372 3186 7878
| 0 1 9 11 21 62 .05 | 2707 1048
iac n/a| 0 0 0 16 46 5 -.25 27 24 | 1322 -592 3183 9084
| 1 2 6 26 31 86 .07 | 3093 818
Table 1.2234.b GPS week : 2234 MJD: 59882.0-59888.0
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 | 14 15 13 13 16 14 17 |
R02 | 6 6 6 6 7 7 5 |
R03 | 9 6 7 7 7 7 7 |
R04 | 7 6 7 7 7 10 8 |
R05 | 10 11 12 10 8 8 7 |
R07 | 6 7 8 7 6 6 6 |
R08 | 8 6 9 10 8 7 8 |
R09 | 10 12 15 14 12 11 8 |
R11 | 11 10 9 8 8 10 7 |
R12 | 14 10 12 7 8 8 8 |
R13 | 15 17 14 14 12 14 19 |
R14 | 9 8 9 9 9 8 8 |
R15 | 9 9 9 7 8 8 8 |
R17 | 8 9 8 7 7 7 7 |
R18 | 11 10 9 9 10 9 7 |
R19 | 30 26 31 30 33 30 28 |
R20 | 31 29 30 30 32 31 31 |
R21 | 11 8 7 9 7 9 8 |
R22 | 26 14 15 13 16 39 22 |
R24 | 11 11 9 9 10 10 7 |
Table 1.2234.c GPS week : 2234 MJD: 59882.0-59888.0
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 2234 0 | -33 -25 31 -813 1140 2270 80.3 1729 1729 | -968 0
brd 2234 1 | 58 -27 41 -922 219 2147 83.1 1747 1747 | -7219 0
brd 2234 2 | -20 35 24 -2686 -1706 276 82.1 1705 1705 | -28 0
brd 2234 3 | -19 -41 30 -752 -1819 -4751 81.9 1775 1775 | 14 0
brd 2234 4 | 86 -2 94 669 -1184 -12310 79.5 1957 1957 | 1130 0
brd 2234 5 | 104 -18 142 897 -678 -7938 80.8 2147 2147 | 89 0
brd 2234 6 | 14 -63 63 383 -2055 -5643 79.4 2185 2185 | 162 0
-------------+------------------------------------------------------------+----------------
brd 2234 mean| 27 -20 61 -460 -869 -3707 81.0 1892 1892 | -974 0
brd 2234 sdev| 55 31 43 1238 1180 5516 1.4 204 204 | 2820 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 2.2234.0 GPS week: 2234 Day: 0 MJD: 59882
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 6 -24 -11 17 .20 30 22 | 33616 -2224 3810 9181
emx n/a| -1 0 -7 -15 22 -21 .13 49 33 | 4328 -1067 3787 9152
esx n/a| -3 2 3 5 -6 56 .01 30 22 | 3381 -2181 3789 9180
gfz n/a| -1 2 0 15 -28 10 -.13 30 19 | 0 -2484 3918 9031
grg n/a| 0 -4 0 7 0 12 .21 25 18 | -136 -2401 3819 8818
iac n/a| 2 2 -11 -29 54 -114 -.34 29 29 | 1933 -1475 3792 9731
Table 2.2234.1 GPS week: 2234 Day: 1 MJD: 59883
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 -34 -18 40 .09 29 22 | 25518 -654 3122 7454
emx n/a| 0 1 -11 -27 -9 -79 .08 42 30 | -13207 580 3115 7218
esx n/a| 0 0 1 15 1 23 -.01 28 22 | -8567 -290 3045 9300
gfz n/a| -3 2 0 3 -50 -22 -.01 24 16 | 0 -424 3139 7205
grg n/a| 0 -3 0 -2 3 -82 .14 26 22 | -7122 -558 3058 6799
iac n/a| -1 -3 -2 47 81 76 -.34 28 26 | -5618 232 3057 7820
Table 2.2234.2 GPS week: 2234 Day: 2 MJD: 59884
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 8 -20 1 0 .07 26 21 | 32507 -132 3227 8552
emx n/a| -1 -1 -10 -13 -5 -57 .01 44 32 | -297 104 3266 8328
esx n/a| 0 1 0 -38 -23 11 -.00 27 21 | 3132 690 3192 8085
gfz n/a| 4 2 4 24 -32 18 -.01 30 19 | 0 -193 3313 8278
grg n/a| 0 -6 -15 -1 22 -73 .26 30 23 | -141 -165 3203 7655
iac n/a| 1 0 4 11 42 57 -.27 30 25 | 1983 -633 3188 8973
Table 2.2234.3 GPS week: 2234 Day: 3 MJD: 59885
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 6 -14 17 -8 .16 24 15 | 33014 -1 3491 9093
emx n/a| -1 -1 -10 21 -20 1 .03 48 31 | 10457 -107 3451 9047
esx n/a| 3 0 0 14 9 -51 -.09 32 22 | -18597 -771 3385 11065
gfz n/a| 0 0 0 40 -7 34 -.07 26 18 | 0 -293 3551 9153
grg n/a| 0 -1 -10 -23 -27 97 .24 28 21 | -13 -414 3398 8265
iac n/a| 0 3 6 -1 -18 -60 -.18 27 21 | 2779 -777 3415 9579
Table 2.2234.4 GPS week: 2234 Day: 4 MJD: 59886
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 11 -26 16 -1 .12 27 20 | 33753 557 2967 8907
emx n/a| 0 0 -4 17 -14 7 .07 43 27 | 8948 -292 2939 8888
esx n/a| 1 2 3 -17 -27 -14 -.03 35 22 | -979 1113 2964 7271
gfz n/a| 0 2 4 0 -27 -15 -.05 31 16 | 0 1093 3025 8804
grg n/a| 1 -3 -15 3 -31 -20 .24 25 17 | 425 1122 2989 7859
iac n/a| 2 1 3 32 48 13 -.21 24 22 | 2374 491 2970 9181
Table 2.2234.5 GPS week: 2234 Day: 5 MJD: 59887
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 12 -8 1 0 .08 22 18 | 34699 -79 2808 8083
emx n/a| 2 2 -4 47 -15 -104 -.01 47 27 | -247 -801 2784 7791
esx n/a| -4 3 5 -11 -19 26 -.16 36 19 | -4105 320 2793 6655
gfz n/a| 2 0 4 -24 -8 -15 .06 25 14 | 0 36 2860 8117
grg n/a| 1 -2 -21 -18 -3 -54 .28 28 24 | -90 2 2800 7108
iac n/a| 0 -2 -2 38 52 124 -.20 24 23 | 3224 -1710 2794 8438
Table 2.2234.6 GPS week: 2234 Day: 6 MJD: 59888
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 11 -35 29 63 .06 23 19 | 35320 39 3079 9495
emx n/a| 4 2 -3 73 -39 -4 .01 48 25 | -25743 -958 3076 9415
esx n/a| -2 1 3 10 -17 29 -.16 34 23 | -4116 966 3039 9190
gfz n/a| -3 0 5 -6 -39 -11 -.01 27 15 | 0 -283 3060 9414
grg n/a| 1 -3 -21 0 -33 -42 .19 25 25 | 84 -194 3035 8644
iac n/a| 0 2 4 16 64 -56 -.20 25 23 | 2584 -274 3065 9869
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 3.2234.0 GPS week: 2234 Day: 0 MJD: 59882
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 822 39 34 36 34 21 20 14 | 55 50 38 46 37 41 39
R02 | 484 11 16 10 9 11 16 5 | 24 24 27 25 29 33 24
R03 | 1725 7 17 14 13 17 37 8 | 32 37 32 34 42 37 32
XR04 | 611 5 17 11 --- 14 21 7 | 37 41 39 --- 39 38 36
R05 | 1662 23 24 22 24 19 17 9 | 39 37 62 57 47 51 47
R07 | 657 8 10 10 16 8 18 5 | 33 32 34 29 28 31 29
R08 | 3126 20 21 11 22 11 18 7 | 28 31 37 38 30 36 31
R09E | 3433 20 28 16 23 18 34 10 | 117 124 124 116 115 119 117
R11E | 1810 21 15 17 22 30 25 10 | 39 45 47 43 51 44 43
R12E | 1392 16 46 17 19 23 56 13 | 116 117 109 109 118 123 113
R13E | 1533 42 49 26 25 30 28 14 | 50 53 51 53 49 38 41
R14E | 553 15 37 15 15 18 23 9 | 86 90 92 88 92 85 87
R15E | 582 17 30 16 19 14 26 9 | 107 109 114 109 114 105 109
R17 | 2245 13 28 17 12 11 20 7 | 71 43 62 67 72 62 63
R18 | 1053 26 35 21 18 18 29 10 | 51 43 73 52 61 61 56
R19 | 1227 50 133 49 70 62 32 29 | 91 62 52 114 79 79 69
R20 | 2625 76 98 90 74 25 40 31 | 108 54 44 101 72 84 58
R21 | 569 22 25 17 10 21 38 10 | 77 59 59 71 73 74 67
XR22 | 3223 --- --- 389 --- 21 30 25 | --- --- 195 --- 36 40 37
R24 | 1435 13 50 9 18 33 22 11 | 78 52 72 63 82 77 69
------+-----------------------------------------+-------------------------------------
RMS | 1728 30 49 30 30 25 29 |T 65 58 68 67 63 62 58
WRMS | 1728 22 33 22 19 18 29 |NE 55 43 59 58 51 53 46
MEDI | 1392 20 28 17 19 18 25 |MD 55 50 52 57 51 51 47
Table 3.2234.1 GPS week: 2234 Day: 1 MJD: 59883
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1305 35 29 38 27 29 39 14 | 25 30 42 38 36 39 27
R02 | 628 12 13 15 18 9 13 6 | 20 24 20 29 21 19 18
R03 | 1050 6 10 12 13 13 22 6 | 23 31 29 32 26 24 23
XR04 | 1340 12 13 8 --- 12 16 6 | 29 33 39 --- 44 29 34
R05 | 953 25 20 23 16 31 21 10 | 37 33 57 55 55 43 44
R07 | 470 11 11 9 15 23 15 6 | 26 31 31 36 30 25 26
R08 | 2573 11 16 15 13 13 10 5 | 20 28 30 26 26 21 22
R09E | 3845 21 30 18 25 26 40 12 | 95 96 97 104 95 99 95
R11E | 3182 16 21 14 18 28 27 9 | 25 28 29 28 32 35 23
R12E | 832 13 35 18 12 13 32 9 | 137 132 136 146 143 134 138
R13E | 1458 41 52 31 29 35 40 16 | 44 46 60 55 47 35 41
R14E | 1592 11 29 14 12 17 22 7 | 97 99 105 108 113 96 102
R15E | 647 13 32 13 16 19 26 8 | 101 98 99 103 107 99 100
R17 | 1978 11 29 12 14 21 26 8 | 44 33 39 43 53 34 40
R18 | 820 14 29 26 24 20 16 9 | 35 34 45 27 49 33 34
R19 | 1678 64 96 44 57 50 25 25 | 52 58 43 63 41 47 41
R20 | 2057 74 94 82 37 52 40 29 | 68 47 34 48 75 39 37
R21 | 488 19 23 12 13 14 26 8 | 48 45 40 43 49 49 43
XR22 | 3079 --- --- 369 --- 12 14 13 | --- --- 101 --- 34 33 32
R24 | 1198 16 50 12 19 10 30 10 | 46 32 38 43 43 57 39
------+-----------------------------------------+-------------------------------------
RMS | 1747 29 42 28 24 26 28 |T 51 50 55 57 55 49 47
WRMS | 1747 22 30 22 16 22 26 |NE 36 35 42 40 41 35 32
MEDI | 1305 14 29 15 16 19 25 |MD 44 33 40 43 44 35 37
Table 3.2234.2 GPS week: 2234 Day: 2 MJD: 59884
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1522 34 36 26 27 18 28 12 | 39 53 36 36 43 25 32
R02 | 974 10 13 14 14 13 19 6 | 15 21 23 24 19 24 15
R03 | 696 8 21 12 12 23 18 7 | 21 24 23 21 36 26 20
XR04 | 1687 9 11 11 --- 11 22 6 | 20 21 24 --- 28 16 18
R05 | 1104 28 26 16 35 17 27 11 | 28 39 37 40 28 36 28
R07 | 668 11 14 21 16 22 22 8 | 24 19 33 24 19 32 20
R08 | 936 13 17 19 22 25 23 9 | 22 27 34 34 20 29 24
R09E | 4435 32 28 24 34 42 31 14 | 102 99 97 99 91 82 92
R11E | 3081 15 20 12 18 30 19 8 | 25 30 24 38 37 31 24
R12E | 576 17 34 24 27 20 37 11 | 78 89 97 99 90 68 85
R13E | 819 15 58 25 34 28 30 14 | 30 40 46 68 46 30 37
R14E | 2111 16 21 21 21 21 20 9 | 65 60 60 61 63 56 58
R15E | 1235 11 31 13 15 19 25 8 | 74 74 72 78 75 77 73
R17 | 1601 12 34 14 17 13 17 8 | 53 35 46 55 54 56 50
R18 | 732 15 35 23 19 10 13 8 | 44 39 55 47 43 44 44
R19 | 1775 38 117 55 84 73 40 30 | 83 41 63 112 68 75 66
R20 | 1411 75 83 70 37 51 76 29 | 65 68 41 53 67 74 36
R21 | 785 16 27 15 11 14 16 7 | 57 39 47 48 53 53 49
XR22 | 3125 --- --- 391 --- 15 13 14 | --- --- 124 --- 35 43 37
R24 | 989 21 39 13 11 18 19 9 | 54 48 50 50 52 60 50
------+-----------------------------------------+-------------------------------------
RMS | 1704 26 44 27 30 30 30 |T 47 45 51 54 48 46 42
WRMS | 1704 21 32 21 19 23 25 |NE 40 36 45 45 40 42 34
MEDI | 1104 15 28 19 19 19 22 |MD 44 39 46 48 43 43 37
Table 3.2234.3 GPS week: 2234 Day: 3 MJD: 59885
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 791 33 38 28 18 33 26 13 | 54 47 40 41 30 30 35
R02 | 637 12 22 15 10 9 11 5 | 21 33 24 23 23 22 19
R03 | 500 7 16 15 16 24 14 7 | 25 29 22 22 36 25 23
XR04 | 981 11 12 14 --- 11 20 7 | 29 28 29 --- 31 23 26
R05 | 1437 18 23 21 31 21 14 10 | 22 23 35 29 29 27 21
R07 | 663 10 11 9 18 11 22 6 | 23 26 24 25 25 27 22
R08 | 2053 13 16 21 27 34 15 10 | 25 26 36 38 29 32 26
R09E | 4052 34 34 26 38 28 28 14 | 99 104 94 96 89 95 92
R11E | 3259 16 22 15 16 19 19 7 | 29 34 39 40 46 31 32
R12E | 690 10 25 13 17 15 19 7 | 133 127 132 132 128 132 130
R13E | 1389 22 49 29 26 35 36 14 | 35 33 52 44 44 38 32
R14E | 1427 12 27 20 16 21 19 8 | 101 104 100 104 110 111 104
R15E | 1036 10 32 12 10 16 14 6 | 84 81 78 80 80 83 80
R17 | 1891 8 33 10 9 15 15 6 | 54 32 52 50 62 60 52
R18 | 625 10 26 27 16 20 22 9 | 45 30 63 45 50 58 47
R19 | 2906 46 123 72 64 70 44 30 | 77 40 59 111 106 90 75
R20 | 1416 61 112 88 46 38 63 30 | 88 79 45 71 56 74 53
R21 | 1111 13 40 18 13 12 19 8 | 59 35 43 54 59 70 53
XR22 | 3137 --- --- 380 --- 13 12 12 | --- --- 137 --- 31 22 23
R24 | 702 18 41 15 19 12 21 9 | 59 40 49 38 58 63 51
------+-----------------------------------------+-------------------------------------
RMS | 1775 24 48 32 26 28 27 |T 55 50 57 57 56 55 49
WRMS | 1775 15 31 22 18 21 21 |NE 44 36 47 45 44 44 37
MEDI | 1111 13 27 18 17 19 19 |MD 54 34 45 44 46 38 35
Table 3.2234.4 GPS week: 2234 Day: 4 MJD: 59886
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1393 48 37 37 34 27 17 15 | 47 43 43 37 28 34 33
R02 | 656 14 11 13 10 17 21 7 | 22 24 29 27 21 29 22
R03 | 617 11 12 10 15 14 22 6 | 30 32 36 47 38 39 36
XR04 | 713 12 14 17 --- 11 12 6 | 32 37 26 --- 40 31 31
R05 | 972 17 16 13 16 18 25 8 | 37 40 44 47 43 49 40
R07 | 792 10 11 11 15 9 14 5 | 27 29 30 23 28 23 24
R08 | 2465 13 24 25 8 12 22 8 | 25 25 28 21 38 43 27
R09E | 2827 25 19 24 22 30 30 11 | 87 96 95 93 89 91 88
R11E | 3382 18 14 15 12 25 17 8 | 27 31 39 30 42 28 30
R12E | 899 17 28 17 14 14 13 7 | 75 73 68 67 78 70 70
R13E | 845 26 36 24 35 20 20 12 | 43 36 41 50 35 27 32
R14E | 3064 15 22 29 19 18 19 9 | 61 62 78 68 62 65 64
R15E | 1576 13 33 16 14 15 17 8 | 70 67 65 68 72 68 67
R17 | 1773 17 24 14 16 15 10 7 | 45 32 35 31 45 41 37
R18 | 689 18 34 25 21 11 27 10 | 35 28 51 31 47 61 41
R19 | 3307 58 120 66 83 70 38 32 | 68 50 51 93 41 57 45
R20 | 3059 53 94 104 74 42 55 31 | 95 59 57 113 84 61 67
R21 | 1052 16 26 16 12 6 11 6 | 47 32 41 42 39 37 38
XR22 | 2861 --- --- 367 --- 16 16 16 | --- --- 141 --- 40 35 32
R24 | 799 24 39 13 17 11 22 9 | 62 49 45 46 45 46 46
------+-----------------------------------------+-------------------------------------
RMS | 1956 27 43 35 31 25 24 |T 49 44 52 51 47 46 43
WRMS | 1956 20 27 22 16 17 22 |NE 44 36 46 46 41 41 37
MEDI | 1052 17 24 17 16 15 19 |MD 45 37 43 46 41 41 37
Table 3.2234.5 GPS week: 2234 Day: 5 MJD: 59887
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1082 32 40 31 29 32 18 13 | 26 32 45 29 24 21 24
R02 | 655 11 15 18 10 11 23 6 | 16 21 29 17 22 29 17
R03 | 857 15 13 14 9 15 25 7 | 20 20 22 26 25 30 21
XR04 | 986 15 18 16 --- 20 28 10 | 25 26 32 --- 27 22 23
R05 | 894 21 10 21 17 18 12 8 | 17 29 37 32 36 26 26
R07 | 1187 9 13 14 11 13 19 6 | 18 21 29 22 27 27 20
R08 | 2706 9 18 11 12 13 22 6 | 22 22 30 29 36 32 25
R09E | 2205 20 23 26 19 28 25 10 | 107 110 99 110 91 102 101
R11E | 3015 14 20 23 18 29 22 9 | 36 44 51 40 65 38 42
R12E | 929 10 31 16 19 15 19 8 | 124 110 120 122 118 125 120
R13E | 556 21 41 22 39 32 32 14 | 34 38 41 52 42 32 30
R14E | 4761 14 23 18 11 16 21 7 | 101 101 98 106 102 90 99
R15E | 1446 12 35 17 13 13 17 8 | 51 51 58 55 52 57 52
R17 | 1612 9 29 18 10 13 19 7 | 41 28 36 42 43 48 39
R18 | 581 20 30 17 12 15 26 9 | 32 28 37 34 41 45 34
R19 | 3326 46 129 68 52 75 28 29 | 59 66 30 64 41 47 40
R20 | 3863 45 106 112 60 44 42 31 | 73 61 59 100 70 68 64
R21 | 740 15 27 13 14 23 28 9 | 43 33 40 41 51 45 40
XR22 | 2506 --- 98 366 --- 30 33 38 | --- 17 116 --- 35 37 37
R24 | 1321 23 34 13 22 12 22 9 | 52 37 42 32 37 47 37
------+-----------------------------------------+-------------------------------------
RMS | 2147 22 47 36 25 28 24 |T 47 44 52 52 49 48 44
WRMS | 2147 18 27 19 14 24 23 |NE 34 31 41 39 36 37 31
MEDI | 1187 15 27 18 14 16 22 |MD 36 32 40 40 41 38 37
Table 3.2234.6 GPS week: 2234 Day: 6 MJD: 59888
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 720 39 37 35 35 45 36 17 | 63 54 30 35 34 47 38
R02 | 1294 9 11 11 12 9 16 5 | 30 29 25 32 31 39 29
R03 | 1301 12 12 10 14 16 27 7 | 38 42 43 46 49 52 43
XR04 | 1285 16 17 10 --- 21 14 8 | 39 46 39 --- 41 37 39
R05 | 843 13 11 17 19 10 16 6 | 34 36 45 43 48 39 38
R07 | 1035 6 21 13 13 12 17 6 | 36 39 46 38 47 41 40
R08 | 2403 10 10 24 18 18 25 8 | 30 33 44 42 37 48 36
R09E | 3211 13 24 20 17 18 21 8 | 123 119 125 125 126 128 123
R11E | 2771 11 15 12 13 16 24 7 | 50 52 51 52 54 61 51
R12E | 1004 12 28 15 13 16 25 8 | 129 127 129 125 125 125 126
R13E | 593 26 64 37 62 28 30 18 | 53 68 63 92 63 61 57
R14E | 5073 15 26 22 17 12 18 8 | 98 95 86 91 93 90 91
R15E | 2272 10 27 16 18 14 19 7 | 66 69 61 66 63 70 64
R17 | 1069 11 31 16 10 11 20 7 | 76 49 61 70 74 80 70
R18 | 653 13 24 22 8 13 18 7 | 54 44 71 55 62 71 59
R19 | 2370 31 119 64 58 69 35 27 | 97 69 41 118 80 96 77
R20 | 3638 65 119 100 41 33 47 30 | 124 53 56 107 81 96 79
R21 | 1035 6 33 19 12 11 23 7 | 76 55 61 74 73 84 70
XR22 | 3253 --- --- 357 --- 22 21 21 | --- --- 158 --- 37 41 40
R24 | 1640 14 33 12 13 13 15 7 | 81 56 73 66 70 77 70
------+-----------------------------------------+-------------------------------------
RMS | 2184 22 48 34 27 25 25 |T 68 59 65 70 64 69 62
WRMS | 2184 19 25 23 15 25 23 |NE 59 46 56 60 54 60 52
MEDI | 1294 13 26 17 14 16 21 |MD 63 53 56 66 62 61 57
More information about the IGSREPORT
mailing list