[IGSREPORT-29261] Wk 2254 IGLOS Final Orbits
acc
acc at igs.org
Tue Apr 11 06:32:18 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2254 (Mar 19, 2023 - Mar 25, 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 2.2254.
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:
igl2254[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2254 in the SP3 format.
igl22547.sum Combination Report for GPS Week 2254.
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 | 0.9 ns
1 | -0.2 ns
2 | 0.2 ns
3 | -17.8 ns
4 | 0.3 ns
5 | -1.1 ns
6 | -11.0 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
2 | GFZ | R20
3 | ESA | R22
4 | ESA | R22
5 | ESA | R22
6 | ESA | 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 1.2254, 1a.2254).
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 2.2254.0-6)
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 3.2254.0-6).
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 2254 summary. (Mar 19, 2023 - Mar 25, 2023)
Table 1.2254.a GPS week : 2254 MJD: 60022.0-60028.0
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 2 -14 -32 44 .04 17 13 | 31360 -15 3219 8938
| 0 1 0 17 7 32 .05 | 7329 1851
esa n/a| 0 0 0 -12 23 -35 -.17 27 22 | -1362 309 3187 9536
| 1 1 0 9 24 24 .04 | 11438 1710
gfz n/a| 0 1 0 6 4 -32 -.08 31 17 | 0 -159 3178 8800
| 1 1 2 12 10 34 .04 | 0 1786
grg n/a| 0 -2 -1 10 17 12 .12 22 17 | -4188 -87 3179 8146
| 1 1 2 29 21 30 .03 | 7008 1870
iac n/a| -1 0 -4 0 -3 -10 -.29 34 27 | -2281 -199 3183 9306
| 2 1 1 16 23 51 .04 | 7288 945
Table 1.2254.b GPS week : 2254 MJD: 60022.0-60028.0
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 21 22 16 16 13 16 |
R02 | 12 7 7 12 6 8 8 |
R03 | 7 8 7 8 9 7 7 |
R04 | 6 10 10 10 9 7 7 |
R05 | 9 8 9 7 8 7 8 |
R07 | 14 7 6 7 6 10 7 |
R08 | 11 11 8 7 9 8 9 |
R09 | 9 10 10 9 11 7 8 |
R11 | 7 8 9 8 8 7 7 |
R12 | 11 10 11 10 9 13 15 |
R13 | 17 18 20 22 20 16 13 |
R14 | 8 6 9 14 6 8 10 |
R15 | 7 11 7 10 10 7 7 |
R16 | 22 24 20 24 22 21 21 |
R17 | 9 8 10 8 8 8 8 |
R18 | 10 10 9 10 9 9 9 |
R19 | 23 20 21 20 22 19 20 |
R20 | 28 22 36 35 33 34 36 |
R21 | 7 8 9 7 10 11 9 |
R22 | 12 9 13 14 13 14 12 |
R24 | 10 12 11 10 13 9 11 |
Table 1.2254.c GPS week : 2254 MJD: 60022.0-60028.0
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 2254 0 | -57 17 50 409 -2211 6255 79.3 1550 1550 | 904 0
brd 2254 1 | 47 -1 162 -771 -2257 6366 80.2 1671 1671 | -249 0
brd 2254 2 | -43 88 188 -1871 -1039 328 80.3 1438 1438 | 187 0
brd 2254 3 | -20 -50 41 -2849 56 2380 82.5 1433 1433 | -17779 0
brd 2254 4 | 35 -41 139 -2513 -1591 6259 79.0 1562 1562 | 269 0
brd 2254 5 | 43 42 163 -1420 -46 8054 78.5 1924 1924 | -1055 0
brd 2254 6 | 58 52 122 -886 1914 2181 80.1 2041 2041 | -11006 0
-------------+------------------------------------------------------------+----------------
brd 2254 mean| 9 15 124 -1414 -739 4546 80.0 1660 1660 | -4104 0
brd 2254 sdev| 47 50 57 1117 1496 2873 1.3 237 237 | 7319 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 2.2254.0 GPS week: 2254 Day: 0 MJD: 60022
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 3 -18 -45 -21 .08 17 13 | 36919 2030 3250 9511
esa n/a| 0 1 1 -29 41 -5 -.21 25 21 | 4767 2150 3199 7402
gfz n/a| -1 3 2 3 3 25 -.10 33 21 | 0 1692 3197 9245
grg n/a| 2 -1 -2 22 9 47 .14 20 17 | -187 1721 3203 8515
iac n/a| -3 0 -1 -21 0 4 -.26 35 23 | 3207 447 3206 9851
Table 2.2254.1 GPS week: 2254 Day: 1 MJD: 60023
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 1 10 -27 46 .11 17 13 | 35523 422 3256 9325
esa n/a| 0 -1 0 -19 57 -13 -.23 27 23 | 13899 317 3244 12192
gfz n/a| 0 3 0 -12 18 -22 -.11 26 15 | 0 -229 3224 9181
grg n/a| 1 -2 0 13 -12 -7 .11 22 20 | -494 188 3229 8311
iac n/a| -3 -2 -4 8 27 61 -.27 39 24 | 1428 261 3236 9728
Table 2.2254.2 GPS week: 2254 Day: 2 MJD: 60024
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 1 -38 -27 43 .07 18 15 | 35640 36 3170 10088
esa n/a| 0 0 1 -6 34 -39 -.16 26 19 | 7437 1118 3163 12586
gfz n/a| 0 0 0 4 2 -53 -.09 45 16 | 0 304 3181 9912
grg n/a| 2 -2 -4 19 0 2 .12 24 16 | 66 120 3150 9550
iac n/a| 1 1 -4 13 -13 -26 -.25 41 35 | 1490 222 3152 10297
Table 2.2254.3 GPS week: 2254 Day: 3 MJD: 60025
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 -32 -41 37 .05 15 12 | 18961 -2895 4051 8780
esa n/a| 2 -1 0 -3 32 -45 -.15 28 25 | -17782 -1848 3967 7993
gfz n/a| -1 0 0 10 -11 -77 -.01 35 19 | 0 -2837 3957 8731
grg n/a| 0 -2 -1 33 48 29 .09 26 18 | -16577 -2823 3960 7995
iac n/a| 1 0 -5 -20 -9 -79 -.32 39 31 | -15634 -1850 3967 9081
Table 2.2254.4 GPS week: 2254 Day: 4 MJD: 60026
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 2 -18 -25 62 .03 16 13 | 35907 345 3122 9198
esa n/a| 1 0 0 -10 -6 -74 -.17 30 28 | -639 956 3114 11924
gfz n/a| 0 3 -4 -3 17 -55 -.09 30 18 | 0 843 3071 9141
grg n/a| 1 -3 0 43 21 43 .10 22 16 | -298 981 3087 8576
iac n/a| 0 0 -4 -7 1 -50 -.34 29 26 | 2121 527 3085 9660
Table 2.2254.5 GPS week: 2254 Day: 5 MJD: 60027
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 2 -2 -31 63 -.00 19 15 | 33876 -1994 2806 7328
esa n/a| 1 0 1 -3 2 -56 -.14 29 20 | -3047 -2237 2778 7348
gfz n/a| 0 1 0 16 -2 -5 -.02 25 13 | 0 -2337 2786 7307
grg n/a| 0 -2 -3 -40 13 9 .13 18 15 | 101 -2497 2781 6673
iac n/a| -1 1 -4 20 -46 48 -.28 26 23 | 944 -1251 2790 7801
Table 2.2254.6 GPS week: 2254 Day: 6 MJD: 60028
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 1 -1 -31 80 -.03 21 14 | 22699 1950 2880 8342
esa n/a| 0 0 0 -17 0 -17 -.12 28 20 | -14175 1709 2850 7307
gfz n/a| 1 0 -1 24 0 -39 -.12 26 15 | 0 1449 2833 8083
grg n/a| 0 0 0 -17 38 -38 .16 21 17 | -11928 1696 2845 7405
iac n/a| -3 0 -3 0 12 -32 -.34 29 25 | -9528 250 2845 8729
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 3.2254.0 GPS week: 2254 Day: 0 MJD: 60022
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 437 27 42 36 16 24 17 | 80 60 55 68 62 64
R02 | 724 16 20 9 27 17 11 | 63 75 64 67 60 65
R03M | 616 7 14 12 15 13 7 | 49 45 49 52 45 48
R04 | 655 6 15 15 8 18 6 | 56 55 49 55 49 53
R05 | 669 14 17 19 15 18 9 | 34 43 45 48 45 40
R07M | 670 18 22 37 21 25 13 | 54 50 57 59 59 51
R08 | 1156 15 21 22 18 20 10 | 53 63 49 62 58 56
R09 | 1241 12 18 14 18 15 9 | 51 60 59 38 52 50
R11 | 1810 10 14 14 9 25 6 | 34 33 42 32 45 33
R12 | 1300 11 24 18 21 18 10 | 82 92 71 74 71 79
R13M | 1086 17 39 43 21 41 17 | 107 79 127 95 116 100
R14M | 732 6 22 9 11 17 7 | 84 101 81 82 79 86
R15M | 1861 11 15 8 12 14 7 | 103 110 105 97 108 103
R16M | 1410 21 26 77 21 29 22 | 129 115 124 122 128 124
R17E | 2164 7 11 20 23 15 9 | 104 102 104 106 100 103
R18E | 1447 11 17 17 23 18 10 | 50 49 49 51 51 49
R19E | 1137 27 40 58 34 49 22 | 69 69 65 58 72 58
R20E | 4108 39 50 73 34 119 27 | 71 102 111 66 118 76
R21E | 1476 10 11 12 13 13 6 | 28 33 34 35 28 30
XR22E | 4270 --- 327 14 9 15 12 | --- 136 30 34 29 30
R24E | 1860 10 16 18 23 21 10 | 120 119 120 123 119 120
------+------------------------------------+--------------------------------
RMS | 1549 17 25 33 20 35 |T 71 75 70 67 71 67
WRMS | 1549 13 21 21 17 23 |NE 56 60 54 55 55 55
MEDI | 1241 11 20 18 18 18 |MD 63 69 59 62 60 58
Table 3.2254.1 GPS week: 2254 Day: 1 MJD: 60023
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 909 29 50 31 33 18 20 | 60 46 48 69 57 53
R02 | 671 12 15 13 7 16 7 | 44 55 42 47 43 45
R03M | 717 7 16 13 15 14 7 | 38 41 35 50 38 39
R04 | 665 9 18 14 25 23 9 | 43 57 47 47 40 45
R05 | 1053 11 14 15 17 20 8 | 27 32 45 45 27 35
R07M | 1692 8 14 13 12 20 6 | 36 28 33 41 38 34
R08 | 1668 12 19 22 23 18 11 | 40 40 42 50 47 42
R09 | 1252 15 19 20 11 25 9 | 38 44 46 35 56 38
R11 | 2345 9 18 18 9 24 8 | 27 20 41 28 45 28
R12 | 1312 13 25 17 15 20 10 | 63 71 55 65 53 62
R13M | 1230 18 46 24 34 34 17 | 72 64 77 77 82 71
R14M | 1587 7 15 10 11 16 6 | 69 72 78 70 77 71
R15M | 2134 16 21 16 20 13 10 | 90 95 78 79 76 84
R16M | 1185 25 34 70 28 26 24 | 99 104 104 86 102 99
R17E | 3387 11 13 10 17 13 7 | 84 87 86 89 79 85
R18E | 1984 12 21 12 22 11 9 | 61 53 58 63 64 58
R19E | 1284 22 44 39 37 74 20 | 63 77 65 64 81 61
R20E | 2755 34 41 45 34 135 22 | 63 89 102 73 92 72
R21E | 1440 12 15 14 16 17 8 | 31 37 36 39 30 34
XR22E | 4726 --- 313 9 9 11 9 | --- 123 27 28 23 26
R24E | 1158 19 23 18 25 17 12 | 100 106 99 116 102 103
------+------------------------------------+--------------------------------
RMS | 1671 17 27 26 22 39 |T 57 63 59 60 59 56
WRMS | 1671 13 23 15 20 24 |NE 42 45 45 48 46 43
MEDI | 1312 12 19 16 17 18 |MD 60 57 48 63 56 53
Table 3.2254.2 GPS week: 2254 Day: 2 MJD: 60024
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 711 40 47 23 32 38 21 | 66 38 46 38 44 45
R02 | 572 6 11 18 7 16 6 | 70 71 71 73 70 70
R03M | 890 8 17 11 12 29 7 | 43 44 42 51 48 44
R04 | 653 20 17 19 13 16 10 | 39 35 22 26 27 28
R05 | 1754 15 12 22 11 19 9 | 30 29 23 27 32 24
R07M | 1759 10 14 11 6 17 6 | 40 32 45 42 44 39
R08 | 738 10 13 14 14 14 7 | 34 36 47 32 28 36
R09 | 1755 12 22 16 19 26 10 | 37 46 43 28 43 36
R11 | 894 14 19 18 12 20 9 | 31 22 43 35 45 30
R12 | 993 15 21 13 22 14 10 | 62 66 58 56 65 59
R13M | 1493 21 35 35 42 35 19 | 71 49 71 78 57 66
R14M | 1234 15 16 18 13 19 9 | 51 56 47 51 52 50
R15M | 2422 11 8 15 14 14 7 | 73 80 78 88 71 78
R16M | 1365 22 32 59 18 25 20 | 107 100 114 118 106 109
R17E | 1991 13 16 23 18 15 10 | 70 73 83 76 78 73
R18E | 1256 14 16 12 17 26 8 | 42 40 45 39 41 39
R19E | 1376 22 39 36 44 59 20 | 52 61 66 75 68 55
R20E | 2148 28 64 172 56 148 35 | 60 101 189 70 92 66
R21E | 1201 11 21 11 17 15 9 | 34 40 36 29 25 31
XR22E | 2924 --- 319 15 11 19 13 | --- 125 22 28 24 23
R24E | 1655 18 18 20 15 18 10 | 86 74 79 73 79 76
------+------------------------------------+--------------------------------
RMS | 1438 18 26 45 24 41 |T 54 58 60 53 54 51
WRMS | 1438 15 19 16 16 35 |NE 46 42 44 39 44 41
MEDI | 1365 14 18 18 15 19 |MD 51 49 47 51 48 45
Table 3.2254.3 GPS week: 2254 Day: 3 MJD: 60025
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 804 25 33 26 24 62 15 | 66 37 46 46 42 50
R02 | 737 16 11 41 10 19 12 | 34 29 43 37 32 30
R03M | 789 5 7 21 18 16 7 | 44 45 29 56 45 43
R04 | 1171 15 15 22 15 24 9 | 40 33 22 33 21 30
R05 | 1611 7 16 17 12 14 7 | 25 35 26 21 20 25
R07M | 1611 7 17 12 10 17 6 | 43 39 44 43 41 41
R08 | 714 4 8 21 15 22 7 | 40 38 49 42 25 40
R09 | 2487 11 22 15 16 19 9 | 24 43 38 26 24 29
R11 | 1143 10 12 18 13 15 7 | 30 28 28 32 35 28
R12 | 1060 10 22 15 24 30 10 | 57 67 58 47 39 55
R13M | 1034 19 50 31 50 36 21 | 125 94 118 140 103 119
R14M | 1001 12 29 32 27 11 14 | 63 70 40 42 53 53
R15M | 2295 13 18 26 8 18 9 | 74 81 64 71 63 72
R16M | 2121 20 33 84 21 21 24 | 87 79 127 94 87 92
R17E | 2115 8 13 12 20 16 8 | 34 34 34 31 34 30
R18E | 884 10 17 13 25 16 9 | 56 60 56 63 57 57
R19E | 1206 19 44 52 27 45 20 | 66 89 70 69 66 67
R20E | 1401 32 69 82 68 136 34 | 38 96 106 63 71 50
R21E | 968 8 12 12 17 14 7 | 25 26 26 31 26 24
XR22E | 2518 --- 307 15 13 22 14 | --- 110 30 25 20 23
R24E | 1451 11 17 24 19 21 10 | 33 34 39 31 35 30
------+------------------------------------+--------------------------------
RMS | 1433 15 28 35 26 39 |T 50 55 52 49 44 47
WRMS | 1433 12 25 19 18 31 |NE 39 38 38 35 29 35
MEDI | 1171 11 17 21 18 19 |MD 40 43 43 42 39 41
Table 3.2254.4 GPS week: 2254 Day: 4 MJD: 60026
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1118 16 41 29 27 28 16 | 59 41 60 68 48 56
R02 | 830 10 12 10 10 18 6 | 69 70 69 71 68 69
R03M | 1041 13 16 19 14 16 8 | 54 42 50 59 42 50
R04 | 1048 16 10 18 13 14 8 | 36 37 35 39 31 34
R05 | 1314 13 19 16 9 17 8 | 24 39 32 29 28 28
R07M | 1547 7 11 10 10 12 5 | 42 34 35 45 40 39
R08 | 1238 11 14 25 13 17 9 | 39 29 26 41 34 33
R09 | 2688 12 21 21 22 17 10 | 39 55 58 29 40 42
R11 | 1260 11 13 16 12 13 7 | 28 28 40 34 34 30
R12 | 1407 7 22 14 17 14 8 | 73 84 69 74 72 74
R13M | 1115 15 56 40 26 18 20 | 201 191 216 198 206 200
R14M | 913 7 11 9 11 17 5 | 80 81 81 75 71 79
R15M | 2192 16 16 21 16 22 10 | 92 92 76 88 90 87
R16M | 2748 20 31 66 28 12 21 | 107 94 107 100 99 102
R17E | 1507 10 15 11 19 16 8 | 60 54 61 69 57 60
R18E | 587 10 18 15 18 15 9 | 39 34 40 45 34 37
R19E | 915 22 46 54 30 53 21 | 64 52 81 48 62 54
R20E | 1751 40 78 65 50 92 33 | 55 106 111 66 78 66
R21E | 1085 10 16 19 23 20 9 | 28 34 38 29 27 28
XR22E | 2126 --- 299 14 11 15 12 | --- 115 21 25 20 22
R24E | 2470 16 17 27 29 17 13 | 82 69 66 85 80 74
------+------------------------------------+--------------------------------
RMS | 1562 16 30 30 22 29 |T 63 65 65 62 60 60
WRMS | 1562 13 27 18 16 26 |NE 45 47 48 48 44 45
MEDI | 1260 12 17 19 17 17 |MD 55 54 60 59 48 54
Table 3.2254.5 GPS week: 2254 Day: 5 MJD: 60027
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1439 29 21 23 15 19 13 | 52 33 34 39 49 38
R02 | 828 16 15 12 14 20 8 | 69 81 82 77 70 75
R03M | 1233 9 20 8 8 16 6 | 71 63 70 65 69 67
R04 | 671 12 13 9 14 13 7 | 31 33 29 39 35 31
R05 | 784 13 13 11 12 25 7 | 21 28 27 21 27 21
R07M | 788 19 21 13 11 16 9 | 34 45 31 29 29 31
R08 | 778 11 14 10 16 14 7 | 32 30 27 42 29 32
R09 | 2362 9 13 15 9 20 6 | 43 50 46 47 41 45
R11 | 842 9 14 11 10 14 6 | 27 35 32 28 34 28
R12 | 1722 15 35 12 26 14 13 | 51 64 50 46 50 48
R13M | 1969 28 30 23 25 39 15 | 280 278 275 274 294 276
R14M | 772 5 18 10 17 16 8 | 74 81 77 77 78 76
R15M | 2221 13 14 12 10 22 7 | 96 100 95 92 109 95
R16M | 3256 22 32 55 23 26 20 | 96 101 109 98 98 98
R17E | 1273 12 16 11 17 20 8 | 75 75 73 70 78 72
R18E | 758 14 17 12 16 16 8 | 40 45 44 47 43 42
R19E | 903 25 41 39 25 40 18 | 83 99 89 96 96 87
R20E | 5076 48 87 67 30 66 34 | 57 118 99 68 99 70
R21E | 1604 12 20 18 22 13 10 | 30 34 35 28 32 27
XR22E | 2971 --- 317 14 13 21 14 | --- 156 23 28 21 22
R24E | 2617 18 15 14 14 19 9 | 78 86 80 90 82 82
------+------------------------------------+--------------------------------
RMS | 1924 19 29 25 18 26 |T 67 77 67 66 69 64
WRMS | 1924 14 20 13 15 23 |NE 40 44 40 42 41 39
MEDI | 1273 13 18 12 15 19 |MD 52 64 50 47 50 48
Table 3.2254.6 GPS week: 2254 Day: 6 MJD: 60028
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1862 37 24 19 23 34 16 | 73 42 48 45 60 50
R02 | 952 16 15 14 11 26 8 | 77 84 86 80 80 81
R03M | 929 9 16 10 10 20 6 | 86 90 86 86 89 86
R04 | 793 11 12 16 8 12 7 | 48 47 39 50 48 45
R05 | 1147 12 16 15 10 16 7 | 31 31 26 33 33 27
R07M | 662 12 13 12 8 19 6 | 49 42 41 44 40 43
R08 | 1051 10 18 9 20 20 9 | 43 46 48 55 39 47
R09 | 2133 13 16 15 12 17 8 | 53 62 57 51 58 54
R11 | 1048 8 10 16 10 16 6 | 37 37 50 39 51 40
R12 | 1923 20 33 18 32 18 15 | 75 89 67 65 76 70
R13M | 2969 18 26 22 24 36 13 | 377 367 379 371 379 373
R14M | 871 10 27 8 21 14 10 | 90 105 85 80 86 88
R15M | 1828 9 13 11 15 22 7 | 110 112 110 109 108 110
R16M | 3209 21 36 58 23 29 21 | 129 128 145 131 128 132
R17E | 2219 15 15 14 12 22 8 | 115 120 123 120 116 119
R18E | 1100 14 19 14 15 28 9 | 51 42 49 41 53 44
R19E | 1481 22 42 50 22 46 20 | 102 115 96 105 107 101
R20E | 5192 59 78 62 50 73 35 | 119 155 124 89 130 111
R21E | 1326 12 20 19 11 20 9 | 39 42 44 45 36 41
XR22E | 2626 --- 329 12 11 19 12 | --- 145 31 28 28 27
R24E | 2240 14 16 23 23 27 11 | 132 128 130 135 126 131
------+------------------------------------+--------------------------------
RMS | 2041 21 28 26 21 29 |T 91 96 88 85 89 86
WRMS | 2041 14 20 15 17 25 |NE 54 54 52 52 55 51
MEDI | 1481 13 18 15 15 20 |MD 75 89 67 65 76 70
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