[IGSREPORT-29521] Wk 2279 IGLOS Final Orbits
acc
acc at igs.org
Fri Sep 29 04:49:16 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2279 (Sep 10, 2023 - Sep 16, 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 2.2279.
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:
igl2279[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2279 in the SP3 format.
igl22797.sum Combination Report for GPS Week 2279.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
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.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
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 | -0.5 ns
1 | 0.2 ns
2 | 0.3 ns
3 | 0.0 ns
4 | -0.8 ns
5 | -0.3 ns
6 | -1.0 ns
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 1.2279, 1a.2279).
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 2.2279.0-6)
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 3.2279.0-6).
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 2279 summary. (Sep 10, 2023 - Sep 16, 2023)
Table 1.2279.a GPS week : 2279 MJD: 60197.0-60203.0
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 1 4 8 -1 42 -.01 18 13 | 125769 -566 28526 406808
| 0 1 1 6 9 30 .04 | 102348 974
esa n/a| -1 0 0 -2 -11 8 -.16 23 17 | 3867 -158 2931 7686
| 1 0 0 13 4 21 .05 | 6881 1258
gfz n/a| 0 0 0 24 14 1 -.05 24 15 | 0 -583 2928 7815
| 0 0 0 8 21 21 .04 | 0 1180
grg n/a| 2 0 -5 -35 2 -77 .24 22 17 | -173 -663 2944 7303
| 0 0 1 12 17 37 .04 | 241 1116
iac n/a| 1 0 -3 -8 19 -57 -.31 32 27 | 32103 -667 9928 146470
| 2 1 2 26 38 116 .10 | 76893 949
jgx n/a| 0 2 2 7 10 56 -.29 31 31 | 46507 -891 2953 7864
| 0 1 1 20 12 59 .03 | 1666 1265
Table 1.2279.b GPS week : 2279 MJD: 60197.0-60203.0
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 19 20 14 16 14 15 |
R02 | 8 8 5 8 8 6 8 |
R03 | 7 9 7 6 8 7 10 |
R04 | 9 8 7 7 6 8 10 |
R05 | 8 7 7 6 5 5 8 |
R07 | 9 8 6 8 9 11 7 |
R08 | 7 10 10 7 5 8 10 |
R09 | 9 7 9 10 10 9 13 |
R11 | 7 7 6 7 7 9 9 |
R12 | 6 7 8 7 9 8 8 |
R13 | 17 17 18 22 16 20 16 |
R14 | 7 5 8 7 6 7 7 |
R15 | 8 11 8 7 9 7 9 |
R16 | 9 13 11 12 11 13 12 |
R17 | 8 7 9 7 8 9 8 |
R18 | 10 11 9 9 8 9 9 |
R19 | 21 18 25 23 26 34 28 |
R20 | 34 26 29 34 33 39 32 |
R21 | 7 7 9 7 9 8 8 |
R22 | 8 9 9 8 7 8 9 |
R24 | 9 9 11 9 8 9 10 |
R25 | --- --- --- --- 0 0 0 |
R26 | --- --- --- --- --- 0 62 |
Table 1.2279.c GPS week : 2279 MJD: 60197.0-60203.0
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 2279 0 | 144 121 130 544 0 -3361 79.4 1606 1606 | -473 0
brd 2279 1 | -64 31 -35 -41 -1788 2735 81.4 1717 1717 | 155 0
brd 2279 2 | 61 42 -57 -1135 562 9452 79.5 1951 1951 | 277 0
brd 2279 3 | -3 9 -27 -2194 1104 6074 81.5 1937 1937 | 19 0
brd 2279 4 | -33 -13 -11 -925 1488 5874 81.8 1837 1837 | -841 0
brd 2279 5 | -17 23 -78 -1250 1261 6456 80.5 1983 1983 | -329 0
brd 2279 6 | -64 -72 32 1197 521 3908 81.2 1922 1922 | -1036 0
-------------+------------------------------------------------------------+----------------
brd 2279 mean| 3 20 -6 -543 449 4448 80.8 1850 1850 | -318 0
brd 2279 sdev| 75 58 70 1167 1109 4040 1.0 140 140 | 500 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 2.2279.0 GPS week: 2279 Day: 0 MJD: 60197
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 4 6 13 74 .02 20 13 | 43056 -1365 2722 7406
esa n/a| -1 1 1 20 -4 9 -.22 21 17 | 702 851 2721 5462
gfz n/a| 0 1 0 29 2 -18 -.12 22 16 | 0 -376 2733 7353
grg n/a| 3 -1 -4 -49 -4 -79 .26 20 16 | -299 -628 2711 6764
iac n/a| 0 2 -4 8 50 -6 -.12 27 21 | 2713 -877 2714 7993
jgx n/a| 0 0 3 -7 16 11 -.27 29 29 | 45015 -1392 2762 7252
Table 2.2279.1 GPS week: 2279 Day: 1 MJD: 60198
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 3 8 -15 24 -.05 19 14 | 41734 1127 3179 8538
esa n/a| -2 0 0 0 -14 13 -.25 22 18 | 16138 1166 3176 11324
gfz n/a| 0 0 0 19 5 0 -.07 19 12 | 0 1234 3154 8496
grg n/a| 2 0 -3 -47 19 -38 .29 19 17 | -506 975 3175 7931
iac n/a| -1 1 -5 22 -13 -64 -.26 30 23 | 2475 382 3186 9120
jgx n/a| -1 4 3 38 -2 93 -.24 27 27 | 43787 1244 3185 8473
Table 2.2279.2 GPS week: 2279 Day: 2 MJD: 60199
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 3 20 -2 63 -.02 18 13 | 44578 269 3299 9476
esa n/a| 0 0 0 -9 -8 -27 -.13 22 18 | 9085 1215 3295 9111
gfz n/a| 0 1 0 31 38 -2 .01 24 15 | 0 548 3275 9347
grg n/a| 3 0 -5 -48 -6 -39 .22 23 15 | -299 721 3399 8668
iac n/a| 0 -1 -4 7 -37 -100 -.33 34 25 | 3973 -260 3299 9845
jgx n/a| -2 3 3 19 12 63 -.29 31 30 | 46681 561 3326 9577
Table 2.2279.3 GPS week: 2279 Day: 3 MJD: 60200
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 3 12 0 -8 -.05 19 14 | 46301 -767 3087 7480
esa n/a| -1 0 0 9 -8 26 -.11 22 17 | -5317 -278 3078 7464
gfz n/a| 0 0 -1 10 28 5 -.07 24 13 | 0 -909 3074 7429
grg n/a| 2 0 -3 -21 -19 -49 .20 21 16 | 230 -1093 3073 7015
iac n/a| 4 -1 0 -38 51 53 -.40 38 29 | 4437 -2320 3060 7929
jgx n/a| 0 3 5 -3 1 77 -.32 35 34 | 48436 -1554 3119 7285
Table 2.2279.4 GPS week: 2279 Day: 4 MJD: 60201
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 5 1 -7 60 -.04 17 13 | 224351 -883 61851 912325
esa n/a| -3 0 0 -5 -12 39 -.11 28 17 | 3089 -894 2750 7733
gfz n/a| 1 -1 1 25 6 20 -.01 20 12 | 0 -1764 2767 8653
grg n/a| 3 0 -7 -31 17 -132 .18 22 16 | -180 -1642 2762 8314
iac n/a| 0 0 0 -38 34 41 -.28 30 23 | 1817 -1044 2769 9177
jgx n/a| 0 5 0 -23 4 153 -.32 37 37 | 47293 -1863 2750 8801
Table 2.2279.5 GPS week: 2279 Day: 5 MJD: 60202
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 4 7 -7 61 .04 18 12 | 231743 -614 73662 929946
esa n/a| -1 0 -1 -18 -14 -1 -.15 22 17 | 720 -1249 2498 6363
gfz n/a| 1 1 0 36 38 -27 -.08 35 19 | 0 -751 2505 6423
grg n/a| 2 -1 -4 -28 -14 -115 .26 25 21 | 36 -1051 2485 6031
iac n/a| 5 0 -3 -32 59 -289 -.31 28 26 | 2839 -955 2494 7012
jgx n/a| 0 1 1 15 35 19 -.32 30 30 | 48118 -1257 2509 6614
Table 2.2279.6 GPS week: 2279 Day: 6 MJD: 60203
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 5 2 7 21 .03 17 13 | 248620 -1729 51887 972486
esa n/a| 0 0 0 -15 -17 -3 -.17 24 18 | 2654 -1917 3003 6345
gfz n/a| -1 0 -1 21 -20 34 -.02 24 15 | 0 -2068 2993 7004
grg n/a| 2 -2 -6 -20 24 -86 .26 27 21 | -198 -1923 3006 6401
iac n/a| 0 -1 -4 10 -11 -35 -.44 39 41 | 206469 400 51978 974220
jgx n/a| 0 1 1 12 5 -22 -.28 31 31 | 46225 -1976 3025 7047
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 3.2279.0 GPS week: 2279 Day: 0 MJD: 60197
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 767 28 45 18 22 63 38 17 | 116 72 105 114 135 92 101
R02M | 769 10 19 15 11 16 20 8 | 82 80 90 92 88 74 85
R03M | 1437 10 11 15 12 19 24 7 | 84 79 78 87 93 70 82
R04 | 1120 18 13 9 17 15 27 8 | 93 87 87 90 93 87 88
R05 | 2731 11 16 15 9 11 20 7 | 75 76 71 75 71 64 73
R07M | 899 8 17 18 17 22 29 9 | 80 77 88 75 87 64 78
R08 | 726 10 11 12 11 27 11 6 | 76 81 91 83 88 80 82
R09M | 814 12 10 19 15 16 15 8 | 26 29 28 25 24 27 24
R11M | 1205 12 14 9 9 13 13 6 | 24 26 27 19 25 21 22
R12 | 1234 9 11 8 10 19 24 5 | 68 69 72 75 77 66 70
R13 | 666 24 32 18 37 35 51 16 | 80 55 69 78 86 68 69
R14 | 666 12 10 7 17 22 16 7 | 61 57 56 57 67 50 57
R15 | 678 10 20 10 12 15 20 8 | 76 64 75 81 72 69 73
R16M | 1477 10 20 14 13 18 16 8 | 68 65 77 67 70 66 68
R17E | 1336 9 8 13 17 15 --- 7 | 88 93 98 98 88 --- 93
R18E | 1230 18 13 17 14 26 20 9 | 118 123 123 123 110 115 121
R19E | 2281 43 21 44 29 25 39 21 | 70 69 95 81 69 70 75
R20E | 3726 52 52 70 55 56 74 33 | 121 72 134 96 78 89 96
R21E | 1354 9 12 14 10 14 15 6 | 71 73 75 77 74 77 74
R22E | 2684 14 8 13 16 19 15 7 | 43 49 48 52 43 51 46
R24E | 1500 22 13 11 14 19 21 9 | 72 77 80 86 71 66 77
------+-----------------------------------------+-------------------------------------
RMS | 1605 20 21 22 20 27 29 |T 75 70 79 77 76 68 74
WRMS | 1605 13 17 16 16 21 29 |NE 80 70 78 81 86 72 76
MEDI | 1230 12 13 14 14 19 20 |MD 76 72 78 81 77 68 75
Table 3.2279.1 GPS week: 2279 Day: 1 MJD: 60198
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1416 24 52 16 26 52 33 18 | 85 58 77 86 99 74 75
R02M | 876 13 20 8 15 34 18 8 | 56 58 62 68 71 59 60
R03M | 2082 12 21 16 12 18 21 9 | 58 57 78 75 71 64 66
R04 | 1031 16 11 9 14 19 26 7 | 70 73 78 77 76 76 74
R05 | 2731 13 18 8 7 14 26 7 | 62 57 61 58 51 54 59
R07M | 601 8 9 14 17 14 22 7 | 57 59 60 44 55 53 54
R08 | 998 13 16 23 14 24 28 10 | 53 60 71 52 70 53 58
R09M | 1334 9 9 13 12 25 16 6 | 35 42 41 41 34 40 38
R11M | 2183 12 9 11 12 11 12 6 | 38 38 39 39 41 45 37
R12 | 1117 13 9 13 7 14 23 6 | 63 69 75 66 64 65 68
R13 | 1987 21 29 31 36 27 33 17 | 69 66 79 82 81 53 73
R14 | 831 8 9 7 8 10 12 4 | 55 56 59 60 60 54 57
R15 | 780 15 23 13 19 17 19 10 | 62 54 73 79 54 65 67
R16M | 2082 23 18 25 21 28 28 13 | 51 46 55 52 46 59 47
R17E | 1617 12 14 12 12 22 --- 7 | 40 48 52 56 38 --- 48
R18E | 1198 19 24 14 15 21 23 10 | 85 108 95 96 88 95 95
R19E | 1775 32 28 38 22 49 49 17 | 43 50 54 46 37 37 44
R20E | 3354 48 43 42 42 79 50 25 | 86 90 68 61 73 69 68
R21E | 1403 8 11 10 14 19 19 6 | 37 40 39 37 39 37 37
R22E | 1944 17 11 15 15 17 20 8 | 23 29 32 28 25 29 26
R24E | 1813 13 18 14 18 18 22 9 | 34 39 43 46 34 36 38
------+-----------------------------------------+-------------------------------------
RMS | 1716 19 22 19 19 30 27 |T 55 57 61 59 57 55 56
WRMS | 1716 14 18 12 17 23 27 |NE 64 61 71 70 69 61 66
MEDI | 1416 13 18 14 15 19 22 |MD 56 57 61 58 55 54 58
Table 3.2279.2 GPS week: 2279 Day: 2 MJD: 60199
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1000 33 52 24 16 44 48 20 | 87 40 82 73 90 71 69
R02M | 1127 7 9 9 11 28 19 5 | 61 58 54 61 70 46 58
R03M | 2580 9 10 13 15 21 25 6 | 63 61 58 63 73 61 60
R04 | 976 13 11 12 10 18 13 7 | 67 65 60 74 64 69 66
R05 | 2253 9 13 15 12 18 32 7 | 57 54 64 53 50 47 56
R07M | 536 9 8 9 13 15 25 5 | 60 54 53 59 51 45 56
R08 | 939 19 10 19 14 11 22 9 | 50 64 72 57 60 58 59
R09M | 1399 10 14 15 24 17 25 9 | 35 38 35 30 27 29 32
R11M | 2110 10 9 13 10 22 20 6 | 20 20 24 26 29 24 20
R12 | 1849 16 13 13 13 22 14 8 | 42 58 62 55 57 55 53
R13 | 3233 18 37 21 40 30 52 17 | 66 45 61 53 62 63 55
R14 | 1250 9 18 15 13 12 23 8 | 43 52 33 40 35 31 41
R15 | 566 9 10 16 18 24 19 8 | 61 51 49 66 63 50 56
R16M | 1831 17 16 21 18 13 22 10 | 46 46 37 45 46 51 40
R17E | 1074 8 13 17 18 20 --- 8 | 57 54 63 63 63 --- 57
R18E | 2828 13 9 15 21 25 30 8 | 67 62 67 62 61 62 63
R19E | 1321 25 43 59 44 40 53 25 | 44 59 94 52 46 52 53
R20E | 3994 50 44 57 50 113 66 29 | 95 107 88 69 138 63 83
R21E | 1482 10 16 16 18 20 18 8 | 44 50 45 47 52 45 44
R22E | 2886 16 9 18 14 10 11 8 | 22 28 38 26 23 28 25
R24E | 945 13 18 17 24 28 16 10 | 48 48 51 57 53 47 48
------+-----------------------------------------+-------------------------------------
RMS | 1951 18 22 24 23 34 31 |T 54 53 56 53 57 49 52
WRMS | 1951 13 18 15 15 25 30 |NE 59 53 60 58 60 55 56
MEDI | 1399 13 13 16 16 21 22 |MD 57 54 58 57 57 50 56
Table 3.2279.3 GPS week: 2279 Day: 3 MJD: 60200
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 763 18 32 28 16 16 37 14 | 98 75 110 97 96 100 95
R02M | 1628 13 11 16 15 16 33 8 | 68 73 89 83 80 59 77
R03M | 2105 9 11 8 12 19 26 6 | 75 75 79 75 77 61 75
R04 | 1028 11 8 16 9 17 18 6 | 70 65 60 64 73 59 64
R05 | 1917 9 11 12 11 18 16 6 | 65 66 77 76 61 62 70
R07M | 824 13 15 7 14 24 19 7 | 76 63 68 74 75 61 70
R08 | 1021 8 10 17 8 14 21 6 | 66 68 68 65 74 56 66
R09M | 1076 14 19 18 17 26 20 10 | 43 42 49 39 42 40 41
R11M | 2017 12 14 9 9 25 28 6 | 37 40 37 39 49 31 37
R12 | 1861 12 9 9 17 38 16 7 | 53 56 57 59 74 52 55
R13 | 3211 21 44 32 49 34 51 21 | 69 51 61 83 58 82 64
R14 | 1161 11 14 12 10 20 31 7 | 50 68 60 61 63 46 58
R15 | 477 8 11 10 16 19 27 6 | 65 67 69 73 79 57 68
R16M | 1570 25 20 14 18 42 20 11 | 60 62 53 49 67 58 53
R17E | 1218 10 15 9 13 22 --- 7 | 49 54 53 56 54 --- 52
R18E | 3577 13 13 17 15 30 16 8 | 79 87 82 89 80 85 83
R19E | 1123 35 49 39 34 55 75 23 | 63 87 85 70 82 77 69
R20E | 2485 55 48 80 42 127 83 33 | 88 96 111 87 140 93 80
R21E | 1591 7 14 14 14 15 22 7 | 60 61 67 59 60 55 61
R22E | 3821 12 9 8 19 24 17 7 | 32 41 40 44 43 34 38
R24E | 1649 12 16 12 17 24 16 8 | 48 47 47 58 59 43 48
------+-----------------------------------------+-------------------------------------
RMS | 1936 19 22 24 21 38 35 |T 62 64 67 66 70 60 63
WRMS | 1936 14 17 13 16 29 34 |NE 67 64 70 72 72 64 67
MEDI | 1591 12 14 14 15 24 21 |MD 65 65 67 65 73 58 64
Table 3.2279.4 GPS week: 2279 Day: 4 MJD: 60201
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 604 21 42 22 22 29 41 15 | 88 62 87 93 97 72 83
R02M | 1146 12 15 15 10 14 16 8 | 63 73 60 70 59 65 65
R03M | 1681 12 14 13 13 12 39 7 | 67 80 84 79 67 49 77
R04 | 932 8 11 8 10 29 31 5 | 74 73 67 78 76 67 73
R05 | 1049 5 9 10 8 9 21 5 | 59 57 63 62 53 61 60
R07M | 1132 13 19 16 15 21 24 9 | 63 50 60 69 56 42 59
R08 | 855 6 13 5 9 34 22 5 | 60 56 63 68 82 52 61
R09M | 2233 17 16 11 23 17 12 10 | 26 38 35 40 30 24 31
R11M | 1667 10 9 11 17 17 18 7 | 26 32 30 33 29 32 28
R12 | 1635 14 9 14 20 23 15 8 | 60 65 72 72 57 58 66
R13 | 2584 28 33 17 32 21 43 16 | 83 59 74 65 55 64 70
R14 | 1853 6 10 10 12 22 11 5 | 52 56 47 55 60 49 51
R15 | 622 14 14 9 21 13 24 8 | 69 66 79 89 68 62 75
R16M | 947 15 17 15 25 21 35 10 | 61 65 69 52 64 45 60
R17E | 1830 9 14 17 14 18 --- 8 | 54 53 51 55 57 --- 51
R18E | 3922 14 12 7 17 19 20 7 | 45 51 47 57 43 46 48
R19E | 1448 32 47 47 53 55 68 26 | 60 72 77 45 52 46 53
R20E | 1257 39 90 52 40 90 105 32 | 72 92 85 77 80 79 70
R21E | 1488 10 14 16 20 18 26 9 | 57 52 64 51 60 52 55
R22E | 3497 14 9 11 13 19 15 7 | 26 24 29 33 24 24 26
R24E | 1912 12 9 9 19 16 17 7 | 37 35 35 47 40 32 36
XR25 |11119 4 --- --- --- --- --- 0 | 16 --- --- --- --- --- 16
------+-----------------------------------------+-------------------------------------
RMS | 1836 17 27 20 22 30 37 |T 55 57 60 61 57 51 55
WRMS | 1836 13 17 12 16 23 37 |NE 68 61 69 72 68 60 67
MEDI | 1488 12 14 13 17 19 22 |MD 60 57 63 62 57 49 59
Table 3.2279.5 GPS week: 2279 Day: 5 MJD: 60202
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1028 23 33 15 18 31 39 14 | 72 56 70 70 71 67 65
R02M | 1133 7 12 8 12 32 16 5 | 51 59 43 43 65 41 49
R03M | 691 8 13 9 17 26 24 7 | 52 63 50 44 54 43 52
R04 | 720 10 9 16 20 16 28 8 | 68 73 78 68 74 66 70
R05 | 1385 5 8 9 11 13 22 4 | 53 54 54 60 56 41 54
R07M | 1671 11 13 23 25 24 22 10 | 54 46 43 66 54 43 50
R08 | 1167 11 9 19 18 16 24 8 | 53 54 64 70 61 48 58
R09M | 2900 13 8 23 19 26 19 9 | 35 34 42 26 48 31 32
R11M | 1434 15 13 16 12 14 10 8 | 30 34 38 36 34 34 32
R12 | 1713 11 17 9 19 22 16 8 | 51 49 49 53 60 52 49
R13 | 1518 22 39 31 42 28 44 19 | 51 27 57 44 52 38 41
R14 | 1541 7 10 15 13 25 9 6 | 39 37 40 43 54 34 39
R15 | 714 9 13 10 15 24 9 7 | 62 57 57 66 72 61 60
R16M | 734 17 16 19 34 27 18 12 | 46 52 58 28 54 49 43
R17E | 948 7 12 13 26 17 --- 9 | 58 57 63 71 48 --- 60
R18E | 3909 15 15 16 11 21 25 8 | 63 66 57 67 54 54 63
R19E | 3891 41 28 102 57 61 55 34 | 50 49 119 56 37 42 39
R20E | 1887 42 69 105 50 52 77 38 | 46 81 111 64 60 66 51
R21E | 1480 10 15 11 16 25 12 7 | 53 53 56 56 43 46 53
R22E | 3755 16 9 12 16 24 12 8 | 32 26 25 38 23 32 28
R24E | 1684 17 14 16 16 17 16 9 | 40 43 44 51 37 41 42
XR25E |23632 4 --- --- --- --- --- 0 | 20 --- --- --- --- --- 20
XR26 |37936 4 --- --- --- --- --- 0 | 30 --- --- --- --- --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1982 18 22 35 25 28 30 |T 48 50 58 53 52 46 47
WRMS | 1982 12 17 19 21 26 30 |NE 53 50 58 59 62 50 52
MEDI | 1518 11 13 16 18 24 19 |MD 51 53 56 56 54 43 49
Table 3.2279.6 GPS week: 2279 Day: 6 MJD: 60203
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1285 19 42 15 23 39 57 15 | 103 62 97 107 116 79 92
R02M | 587 10 12 17 13 38 26 7 | 70 73 83 72 82 61 74
R03M | 883 9 12 22 19 30 17 9 | 74 76 67 83 85 59 73
R04 | 672 11 12 15 27 16 21 9 | 94 95 95 88 93 91 92
R05 | 1422 12 14 17 13 28 30 8 | 81 84 94 89 90 67 86
R07M | 1045 8 18 9 13 40 15 7 | 78 65 75 82 97 68 75
R08 | 2723 16 13 18 20 20 18 9 | 71 72 92 94 85 72 80
R09M | 2509 15 12 17 41 24 19 13 | 40 39 41 36 33 36 34
R11M | 1386 15 15 10 17 35 18 8 | 54 53 52 56 61 53 52
R12 | 1740 10 17 9 16 38 11 7 | 70 70 76 78 86 67 72
R13 | 782 22 30 24 38 41 62 16 | 76 54 64 78 68 63 65
R14 | 992 9 10 13 13 38 12 6 | 52 51 46 53 72 51 50
R15 | 587 10 15 15 23 66 7 9 | 80 65 71 89 113 75 75
R16M | 1236 21 23 12 21 48 14 11 | 82 73 72 62 96 76 71
R17 | 981 12 15 15 16 20 --- 8 | 68 71 77 80 67 --- 72
R18E | 2568 13 17 13 19 27 11 8 | 71 72 69 82 70 70 72
R19E | 2769 37 42 53 61 59 65 27 | 64 60 95 71 68 40 61
R20E | 3188 34 68 67 51 75 57 32 | 84 107 113 92 86 84 88
R21E | 1199 11 16 10 16 21 10 7 | 58 62 64 65 64 53 60
R22E | 4493 17 8 11 21 29 10 8 | 31 36 36 35 34 32 33
R24E | 1446 14 11 24 20 23 22 10 | 59 58 66 75 57 57 62
XR25 |17461 3 --- --- --- 28 --- 0 | 16 --- --- --- 12 --- 16
XR26 |50660 56 --- 69 --- --- --- 62 | 31 --- 29 --- --- --- 42
------+-----------------------------------------+-------------------------------------
RMS | 1922 17 24 24 27 39 31 |T 65 66 71 74 74 62 65
WRMS | 1922 13 18 15 21 41 31 |NE 73 69 73 84 90 70 72
MEDI | 1386 13 15 15 20 30 18 |MD 70 65 71 78 72 63 72
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