[IGSREPORT-29298] Wk 2258 IGLOS Final Orbits
acc
acc at igs.org
Fri May 5 07:32:30 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2258 (Apr 16, 2023 - Apr 22, 2023)
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 2.2258.
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:
igl2258[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2258 in the SP3 format.
igl22587.sum Combination Report for GPS Week 2258.
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. The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
3. 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).
4. 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
5. 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 | -12.5 ns
1 | -16.1 ns
2 | 1.7 ns
3 | -0.5 ns
4 | -16.7 ns
5 | 1.4 ns
6 | 0.2 ns
6. 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 | ESA | R22
1 | ESA | R22
2 | ESA | R22
3 | ESA | R22
4 | ESA | R22
5 | ESA | R22
6 | ESA | R20 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 1.2258, 1a.2258).
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 2.2258.0-6)
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 3.2258.0-6).
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 2258 summary. (Apr 16, 2023 - Apr 22, 2023)
Table 1.2258.a GPS week : 2258 MJD: 60050.0-60056.0
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 0 -11 -16 35 .06 21 16 | 30243 343 3257 9342
| 1 1 1 11 12 18 .05 | 8711 1928
esa n/a| 0 -1 3 -10 1 -38 -.10 36 22 | -3333 979 3262 8774
| 1 1 2 15 24 30 .04 | 11455 1693
gfz n/a| 1 0 -4 34 -15 -38 -.16 27 17 | 0 342 3236 8566
| 1 1 2 14 22 23 .06 | 0 1940
grg n/a| 0 0 1 -19 33 30 .16 28 21 | -6373 213 3240 8059
| 1 2 5 28 23 58 .08 | 8044 1960
iac n/a| 0 0 -5 -5 -12 -44 -.27 27 24 | -4824 -88 3218 9340
| 1 2 2 16 44 78 .15 | 8268 1229
Table 1.2258.b GPS week : 2258 MJD: 60050.0-60056.0
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 | 16 16 17 18 15 20 17 |
R02 | 8 8 7 9 8 11 7 |
R03 | 6 9 8 9 9 10 7 |
R04 | 6 9 7 11 10 10 6 |
R05 | 11 8 9 8 8 8 6 |
R07 | 9 9 8 7 6 8 7 |
R08 | 7 6 7 11 6 10 8 |
R09 | 8 9 9 14 17 9 7 |
R11 | 6 8 9 8 11 17 9 |
R12 | 10 9 11 11 9 22 10 |
R13 | 23 21 15 16 26 23 20 |
R14 | 8 12 9 13 13 22 9 |
R15 | 9 9 11 7 14 23 10 |
R16 | 21 22 21 23 24 32 20 |
R17 | 11 12 11 8 10 10 10 |
R18 | 8 9 10 9 8 10 8 |
R19 | 23 23 24 28 29 22 25 |
R20 | 36 41 37 41 39 53 28 |
R21 | 10 9 10 11 11 11 12 |
R22 | 13 12 10 9 12 9 17 |
R24 | 13 9 12 12 12 13 11 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2258.c GPS week : 2258 MJD: 60050.0-60056.0
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 2258 0 | -22 -20 150 374 -744 -688 80.8 1348 1348 | -12501 0
brd 2258 1 | -103 1 60 221 -957 195 81.4 1384 1384 | -16077 0
brd 2258 2 | 26 -33 180 391 -749 -5340 81.0 1350 1350 | 1695 0
brd 2258 3 | 88 10 163 -192 484 -597 80.4 1483 1483 | -507 0
brd 2258 4 | 20 15 78 -1972 585 4911 81.2 1761 1761 | -16713 0
brd 2258 5 | 0 -22 37 -949 -405 3587 81.5 1752 1752 | 1369 0
brd 2258 6 | -18 17 126 -2048 -948 373 79.7 1553 1553 | 160 0
-------------+------------------------------------------------------------+----------------
brd 2258 mean| -1 -4 114 -596 -390 348 80.9 1518 1518 | -6082 0
brd 2258 sdev| 58 20 55 1070 658 3308 .6 178 178 | 8565 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 2.2258.0 GPS week: 2258 Day: 0 MJD: 60050
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 0 0 -33 25 .00 16 14 | 21913 295 3244 7992
esa n/a| 2 -1 2 -15 -14 -66 -.14 33 22 | -9848 1603 3163 7259
gfz n/a| 1 2 -7 37 -17 -38 -.14 33 21 | 0 867 3122 7683
grg n/a| 0 -2 0 7 51 51 .15 20 18 | -12953 669 3135 7306
iac n/a| 0 -2 -6 -25 5 -109 -.40 27 23 | -10926 -434 3186 8159
Table 2.2258.1 GPS week: 2258 Day: 1 MJD: 60051
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 -2 -19 -14 43 .01 19 15 | 19649 -91 3385 9218
esa n/a| 0 -1 4 -2 -13 14 -.07 36 22 | -20146 334 3344 10857
gfz n/a| 0 1 -3 47 7 -28 -.11 26 16 | 0 -3 3338 7770
grg n/a| 2 -1 0 -9 15 -38 .11 25 21 | -16043 -213 3349 7403
iac n/a| 0 1 -4 -3 -35 79 -.39 26 22 | -14524 -1692 3317 9075
Table 2.2258.2 GPS week: 2258 Day: 2 MJD: 60052
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 0 -30 -13 32 .07 19 15 | 37940 3201 3158 9489
esa n/a| 0 0 3 -27 25 -21 -.06 31 20 | -1665 3917 3189 7943
gfz n/a| 0 0 -2 49 -56 -52 -.17 26 18 | 0 3017 3170 8553
grg n/a| 1 0 0 11 76 48 .01 24 20 | -219 3170 3162 8086
iac n/a| 2 0 -3 1 16 -45 -.29 22 18 | 2945 1106 3110 9431
Table 2.2258.3 GPS week: 2258 Day: 3 MJD: 60053
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 0 -16 -30 11 .07 24 18 | 38767 -1549 3108 9601
esa n/a| -1 -1 4 18 26 -67 -.04 33 20 | 8806 -730 3159 8125
gfz n/a| 3 0 -1 13 -10 -75 -.27 26 18 | 0 -1559 3139 8901
grg n/a| 1 0 -4 -23 32 104 .16 25 19 | 104 -1979 3140 8537
iac n/a| -2 0 0 -4 28 -7 -.25 25 23 | 1652 -1200 3126 9619
Table 2.2258.4 GPS week: 2258 Day: 4 MJD: 60054
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 1 -6 -20 32 .11 24 17 | 21506 -2371 3372 9242
esa n/a| 1 -4 3 -18 28 -21 -.11 32 20 | -13791 -1052 3394 8485
gfz n/a| 0 0 -5 18 -29 -44 -.09 24 13 | 0 -2308 3340 8447
grg n/a| 0 4 7 -14 9 56 .21 37 24 | -15730 -2227 3368 7904
iac n/a| 0 0 -5 21 35 -20 -.02 30 26 | -15132 -689 3330 9176
Table 2.2258.5 GPS week: 2258 Day: 5 MJD: 60055
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 -5 3 71 .13 25 18 | 35824 1971 3401 9538
esa n/a| 0 -1 0 -18 -34 -52 -.15 40 26 | 7918 1830 3423 8682
gfz n/a| 2 -1 -9 42 6 -1 -.17 32 17 | 0 2407 3381 8736
grg n/a| -1 -1 10 -72 26 -60 .22 43 25 | 248 1987 3387 8051
iac n/a| 0 3 -8 -24 -64 -169 -.12 30 27 | 1246 1543 3351 9484
Table 2.2258.6 GPS week: 2258 Day: 6 MJD: 60056
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 0 0 -9 30 .04 19 15 | 36104 948 3137 10319
esa n/a| 0 -1 6 -11 -4 -56 -.11 47 24 | 5393 953 3168 10067
gfz n/a| 0 0 -3 35 -8 -26 -.16 23 14 | 0 -23 3165 9874
grg n/a| 0 0 -1 -31 23 53 .23 23 20 | -24 88 3142 9128
iac n/a| -1 0 -7 -1 -74 -36 -.40 32 26 | 966 747 3109 10441
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 3.2258.0 GPS week: 2258 Day: 0 MJD: 60050
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 597 21 30 36 28 30 16 | 91 82 85 96 88 89
R02M | 572 8 16 19 10 12 7 | 33 32 31 34 29 30
R03M | 560 8 12 11 12 15 6 | 29 28 31 33 27 29
R04 | 437 7 10 12 9 26 5 | 29 36 37 32 27 32
R05 | 1257 17 19 26 12 20 10 | 27 38 43 31 28 29
R07 | 1911 6 25 15 16 16 9 | 32 35 33 34 32 31
R08 | 1546 10 10 19 8 25 7 | 35 33 44 36 31 36
R09M | 2753 9 17 20 13 20 8 | 41 45 44 42 42 41
R11E | 1441 8 12 14 7 18 6 | 51 51 56 50 54 51
R12E | 730 12 18 10 22 20 9 | 99 103 96 85 91 95
R13E | 678 27 47 52 37 33 22 | 121 91 133 102 97 109
R14E | 913 11 16 12 15 23 8 | 103 110 104 108 91 105
R15E | 2334 12 17 19 16 31 9 | 98 98 96 96 84 96
R16E | 913 17 35 66 27 20 20 | 127 123 121 119 115 121
R17 | 472 13 16 22 22 19 10 | 67 52 72 52 67 60
R18M | 495 11 16 18 12 13 8 | 60 71 66 62 71 63
R19M | 709 34 32 60 31 37 22 | 67 50 96 61 61 63
R20M | 1718 29 113 70 26 65 36 | 93 49 97 79 52 64
R21M | 862 21 13 12 18 26 10 | 69 48 61 53 65 58
XR22 | 3873 --- 386 17 9 29 13 | --- 198 31 30 37 28
R24 | 2260 11 14 37 24 16 12 | 67 51 72 63 67 61
XR25M |10665 2 --- --- --- 51 0 | 44 --- --- --- 56 45
------+------------------------------------+--------------------------------
RMS | 1348 16 33 33 20 27 |T 65 67 69 61 59 60
WRMS | 1348 14 22 21 18 23 |NE 49 65 52 46 47 45
MEDI | 913 11 17 19 16 20 |MD 67 51 66 53 56 58
Table 3.2258.1 GPS week: 2258 Day: 1 MJD: 60051
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 647 32 32 22 13 28 15 | 67 62 58 71 60 64
R02M | 909 14 16 13 15 13 8 | 17 25 20 16 20 15
R03M | 679 10 16 19 12 17 8 | 14 15 23 9 26 12
R04 | 897 13 17 15 12 16 8 | 15 18 19 14 16 14
R05 | 1060 11 9 15 14 9 7 | 20 17 19 21 13 16
R07 | 1645 9 12 18 21 14 9 | 17 22 23 18 22 16
R08 | 1295 7 12 11 8 21 5 | 19 24 29 19 25 21
R09M | 2496 11 20 18 14 21 9 | 38 36 50 41 42 39
R11E | 2129 10 9 18 15 17 7 | 25 34 41 29 31 29
R12E | 934 10 16 14 19 21 8 | 81 90 80 82 86 82
R13E | 866 27 44 41 38 48 21 | 84 59 94 63 74 74
R14E | 575 8 24 16 29 16 11 | 85 88 81 94 76 85
R15E | 1626 12 15 13 18 23 8 | 66 64 63 74 59 66
R16E | 1161 23 40 57 28 35 22 | 104 110 100 100 98 102
R17 | 702 19 13 10 33 21 12 | 39 37 27 32 41 30
R18M | 511 9 22 11 19 13 9 | 30 40 28 34 27 30
R19M | 641 31 32 41 53 29 23 | 53 55 57 62 52 53
R20M | 1518 42 128 55 46 60 40 | 48 77 69 61 29 44
R21M | 749 13 19 15 15 15 9 | 44 33 42 38 37 39
XR22 | 3078 --- 391 11 12 27 11 | --- 147 33 37 40 34
R24 | 3084 12 21 14 16 22 9 | 40 40 42 41 48 39
XR25M |12502 3 --- --- --- 32 0 | 28 --- --- --- 44 28
------+------------------------------------+--------------------------------
RMS | 1383 19 36 26 25 26 |T 44 52 47 45 43 42
WRMS | 1383 15 22 16 21 22 |NE 31 45 31 31 33 29
MEDI | 934 12 19 15 16 21 |MD 39 40 42 38 40 34
Table 3.2258.2 GPS week: 2258 Day: 2 MJD: 60052
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 661 31 28 33 19 19 16 | 88 83 88 82 79 84
R02M | 1125 8 13 10 16 14 7 | 21 23 23 19 21 19
R03M | 792 15 12 12 16 13 8 | 20 26 23 24 16 20
R04 | 571 5 13 16 13 17 7 | 21 26 34 24 31 22
R05 | 523 10 18 13 16 25 8 | 19 31 26 24 24 19
R07 | 1203 12 10 19 12 17 8 | 21 26 32 27 25 23
R08 | 1183 8 17 7 10 16 6 | 24 26 21 25 22 22
R09M | 2290 11 21 17 11 14 9 | 45 58 57 44 46 48
R11E | 2386 11 10 17 18 16 8 | 21 25 27 32 28 22
R12E | 848 9 20 13 28 9 10 | 74 84 70 65 70 71
R13E | 1378 15 28 28 32 18 15 | 78 67 81 68 75 72
R14E | 1004 8 22 9 22 23 9 | 74 78 79 75 66 75
R15E | 707 12 14 21 24 11 10 | 78 70 86 78 81 77
R16E | 938 22 30 60 23 23 21 | 119 111 123 120 120 117
R17 | 1093 13 19 15 25 13 10 | 51 37 49 42 46 43
R18M | 559 11 21 13 25 13 10 | 42 45 39 42 35 40
R19M | 807 38 33 46 46 43 23 | 58 41 65 46 44 47
R20M | 2146 47 106 45 48 53 37 | 58 67 66 48 38 45
R21M | 588 13 28 13 15 16 10 | 52 41 47 50 49 46
XR22 | 3658 --- 405 9 10 25 9 | --- 171 25 32 30 28
R24 | 2761 16 16 29 18 14 11 | 46 43 68 53 47 50
XR25M |15300 3 --- --- --- 28 0 | 37 --- --- --- 48 37
------+------------------------------------+--------------------------------
RMS | 1350 19 31 26 24 22 |T 49 56 53 48 47 46
WRMS | 1350 15 20 18 20 18 |NE 38 55 42 38 38 36
MEDI | 1004 12 20 16 18 16 |MD 46 43 49 44 44 43
Table 3.2258.3 GPS week: 2258 Day: 3 MJD: 60053
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 644 29 42 22 28 26 18 | 56 63 63 44 50 53
R02M | 816 18 14 15 14 12 9 | 29 30 37 34 25 29
R03M | 906 9 22 8 18 20 9 | 26 27 25 23 25 23
R04 | 486 19 12 22 16 16 10 | 26 33 36 33 30 30
R05 | 734 17 12 14 11 25 8 | 27 36 36 27 36 28
R07 | 663 9 11 13 12 31 6 | 26 25 25 24 30 22
R08 | 2029 15 23 18 18 25 10 | 27 38 31 32 33 27
R09M | 2960 13 13 25 37 18 14 | 45 54 53 63 40 47
R11E | 2567 11 10 17 17 15 8 | 34 36 44 32 33 35
R12E | 684 12 17 19 24 13 10 | 103 104 91 107 95 100
R13E | 1502 22 29 30 30 25 16 | 93 92 84 113 88 91
R14E | 720 15 21 17 32 26 13 | 119 124 118 133 115 121
R15E | 668 8 11 8 18 15 7 | 64 63 58 73 61 63
R16E | 807 30 21 64 27 31 23 | 117 104 100 106 95 106
R17 | 950 14 14 10 16 14 8 | 59 48 53 52 54 52
R18M | 587 15 18 16 14 49 9 | 58 67 57 62 94 59
R19M | 733 53 31 51 54 29 28 | 48 49 84 53 44 52
R20M | 1943 59 117 39 43 41 40 | 87 62 63 65 42 53
R21M | 586 9 27 19 12 11 10 | 60 53 67 71 53 62
XR22 | 2942 --- 388 8 9 28 9 | --- 152 40 40 40 40
R24 | 3337 27 12 22 15 21 11 | 54 37 34 39 39 37
XR25M |17327 2 --- --- --- 40 0 | 33 --- --- --- 50 32
------+------------------------------------+--------------------------------
RMS | 1482 24 33 26 25 25 |T 56 61 57 58 53 52
WRMS | 1482 18 20 18 19 23 |NE 39 54 39 36 39 36
MEDI | 807 15 18 18 18 25 |MD 54 53 53 52 42 47
Table 3.2258.4 GPS week: 2258 Day: 4 MJD: 60054
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 829 29 28 20 25 24 15 | 87 77 84 81 74 81
R02M | 664 10 15 9 24 17 8 | 31 37 37 28 31 31
R03M | 2238 10 17 11 22 19 8 | 34 43 36 30 33 35
R04 | 915 12 20 12 26 27 10 | 32 31 31 38 35 30
R05 | 1013 16 16 11 12 32 8 | 26 38 34 28 32 29
R07 | 1273 6 13 8 14 28 6 | 32 31 27 28 34 29
R08 | 2565 6 12 8 13 26 5 | 37 31 38 36 41 35
R09M | 2241 19 15 21 56 16 16 | 54 52 59 85 52 56
R11E | 2380 17 15 13 30 23 10 | 45 51 46 64 47 48
R12E | 666 12 13 10 24 25 8 | 129 132 127 133 136 130
R13E | 1073 48 24 32 71 25 25 | 89 69 66 102 68 70
R14E | 1130 22 13 13 38 22 12 | 143 158 163 173 149 157
R15E | 671 11 15 16 49 23 13 | 104 107 106 122 108 105
R16E | 826 24 35 53 50 40 24 | 159 161 167 186 157 164
R17 | 916 14 13 15 27 19 10 | 53 41 52 44 51 47
R18M | 595 9 14 11 22 41 8 | 58 55 63 51 79 57
R19M | 1820 37 54 47 65 35 28 | 71 50 88 54 75 65
R20M | 3180 53 104 48 47 64 38 | 115 102 126 103 102 108
R21M | 954 13 24 15 20 28 10 | 64 47 62 53 72 57
XR22 | 2707 --- 379 8 15 31 11 | --- 136 30 41 38 33
R24 | 3946 27 19 10 19 24 11 | 67 53 57 54 52 57
XR25M |13901 3 --- --- --- 41 0 | 61 --- --- --- 77 61
------+------------------------------------+--------------------------------
RMS | 1760 24 32 23 37 30 |T 71 71 71 73 70 67
WRMS | 1760 17 20 13 24 26 |NE 47 54 44 43 44 42
MEDI | 1073 14 16 13 25 25 |MD 61 52 59 54 52 57
Table 3.2258.5 GPS week: 2258 Day: 5 MJD: 60055
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 670 35 29 40 34 11 20 | 145 146 131 134 130 139
R02M | 765 13 20 19 21 13 10 | 25 30 41 31 23 29
R03M | 2739 11 21 9 23 16 9 | 18 30 28 23 24 22
R04 | 1395 21 18 13 14 15 10 | 14 23 23 21 17 16
R05 | 1052 8 12 15 17 26 7 | 15 24 29 16 24 18
R07 | 2118 5 10 18 17 22 7 | 15 16 25 22 12 14
R08 | 2590 17 18 13 23 23 10 | 19 23 23 23 18 17
R09M | 2029 14 11 18 19 15 9 | 46 47 46 46 40 45
R11E | 1564 21 14 21 58 25 17 | 41 44 44 67 42 40
R12E | 822 25 21 25 71 59 21 | 195 197 198 228 184 200
R13E | 1475 31 37 45 45 38 22 | 148 149 165 141 135 148
R14E | 1124 29 29 25 64 36 21 | 140 151 156 153 150 145
R15E | 791 21 16 24 84 25 23 | 74 75 87 68 69 66
R16E | 878 35 27 67 86 31 32 | 221 202 222 215 197 212
R17 | 638 14 18 16 21 17 10 | 45 36 45 40 33 40
R18M | 679 10 21 20 19 31 10 | 42 46 33 39 52 38
R19M | 1389 33 43 40 35 32 22 | 57 52 58 72 66 54
R20M | 2659 59 145 77 49 62 52 | 283 264 311 260 290 276
R21M | 908 10 21 23 16 32 10 | 66 66 76 66 80 67
XR22 | 2937 --- 366 8 10 25 9 | --- 84 34 33 32 34
R24 | 3975 19 32 17 12 18 12 | 66 43 64 61 61 58
XR25M |14966 4 --- --- --- 38 0 | 242 --- --- --- 232 241
------+------------------------------------+--------------------------------
RMS | 1751 25 40 32 43 30 |T 91 83 87 83 86 87
WRMS | 1751 18 26 17 25 27 |NE 45 49 46 43 40 42
MEDI | 1389 19 21 20 23 25 |MD 57 47 46 61 52 45
Table 3.2258.6 GPS week: 2258 Day: 6 MJD: 60056
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1707 24 30 25 37 13 16 | 143 138 134 140 136 139
R02M | 667 11 16 10 10 19 7 | 32 46 35 37 41 36
R03M | 1686 15 15 8 10 31 7 | 26 36 28 27 34 27
R04 | 1781 11 12 9 11 24 6 | 27 29 28 30 31 27
R05 | 698 9 11 8 8 24 5 | 23 32 28 30 40 26
R07 | 2484 8 12 13 12 35 6 | 28 33 31 27 40 28
R08 | 866 10 7 16 20 24 8 | 27 29 33 24 26 27
R09M | 1558 11 9 13 15 14 7 | 61 63 66 68 62 63
R11E | 877 12 12 16 18 18 8 | 32 27 33 36 30 29
R12E | 677 14 16 15 23 24 10 | 126 117 128 133 108 125
R13E | 1412 32 35 39 29 28 20 | 149 154 153 142 141 146
R14E | 956 15 14 19 13 23 9 | 112 122 124 117 108 118
R15E | 810 15 18 16 22 32 10 | 114 117 118 99 112 111
R16E | 1060 26 32 48 22 26 19 | 253 260 252 239 247 250
R17 | 686 10 22 20 13 25 10 | 72 55 75 66 64 66
R18M | 542 8 16 8 19 16 7 | 71 76 71 65 76 70
R19M | 1358 41 43 30 54 40 24 | 85 57 99 67 63 73
R20M | 3201 33 187 45 37 90 27 | 434 452 441 451 447 443
R21M | 902 14 24 19 25 20 12 | 93 77 97 89 94 88
XR22 | 3913 --- 371 15 18 24 17 | --- 192 50 51 53 47
R24 | 3073 15 30 9 14 30 10 | 88 64 83 81 91 78
XR25M |16347 2 --- --- --- 40 0 | 327 --- --- --- 329 327
------+------------------------------------+--------------------------------
RMS | 1553 19 47 23 23 32 |T 110 103 100 96 107 106
WRMS | 1553 15 24 14 20 26 |NE 58 71 57 56 60 54
MEDI | 1060 14 16 16 18 24 |MD 85 64 75 67 64 70
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