[IGSREPORT-29614] Wk 2288 IGLOS Final Orbits
acc
acc at igs.org
Mon Dec 4 00:35:04 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2288 (Nov 12, 2023 - Nov 18, 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 2.2288.
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:
igl2288[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2288 in the SP3 format.
igl22887.sum Combination Report for GPS Week 2288.
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 | -1.2 ns
1 | -0.5 ns
2 | -0.3 ns
3 | -0.2 ns
4 | -1.1 ns
5 | -1.2 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 1.2288, 1a.2288).
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 2.2288.0-6)
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 3.2288.0-6).
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 2288 summary. (Nov 12, 2023 - Nov 18, 2023)
Table 1.2288.a GPS week : 2288 MJD: 60260.0-60266.0
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 0 -6 35 .09 23 17 | 39849 -956 3148 8656
| 1 0 2 9 19 30 .05 | 806 1706
esa n/a| 0 0 0 -43 15 -5 -.17 31 24 | 1833 -1493 3139 7074
| 1 0 2 12 15 14 .04 | 4455 1286
gfz n/a| 0 1 0 23 1 -4 -.09 20 14 | 0 -935 3193 7975
| 1 0 2 6 15 20 .04 | 0 1721
grg n/a| 0 -5 -2 14 4 -28 .20 32 22 | -263 -845 3195 7537
| 1 2 4 22 18 46 .08 | 341 1923
iac n/a| 0 0 -6 5 10 -22 -.18 26 25 | 1425 -781 3143 8587
| 1 0 3 26 26 146 .11 | 837 751
jgx n/a| 0 1 2 29 15 -52 -.24 30 30 | 42616 -640 3180 8135
| 1 1 3 19 22 42 .04 | 866 2085
Table 1.2288.b GPS week : 2288 MJD: 60260.0-60266.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 13 20 22 23 19 20 18 |
R02 | 9 9 9 7 8 10 8 |
R03 | 5 7 7 6 6 7 7 |
R04 | 8 10 13 11 7 10 8 |
R05 | 10 7 7 8 8 6 6 |
R07 | 8 8 6 7 8 11 8 |
R08 | 8 8 8 10 8 9 7 |
R09 | 9 10 7 18 14 9 8 |
R11 | 7 7 6 6 11 12 9 |
R12 | 8 10 8 11 16 7 13 |
R13 | 14 22 21 18 27 21 23 |
R14 | 10 10 8 11 25 12 8 |
R15 | 9 9 10 10 12 18 8 |
R16 | 11 11 10 12 25 10 10 |
R17 | 8 8 9 9 8 7 5 |
R18 | 10 7 11 7 10 11 11 |
R19 | 34 34 26 31 32 29 30 |
R20 | 37 39 43 34 39 35 32 |
R21 | 8 12 9 9 12 8 8 |
R22 | 8 9 8 7 10 8 8 |
R24 | 7 10 9 8 8 7 10 |
R25 | 11 13 17 13 13 20 14 |
R26 | 0 22 16 13 18 16 21 |
Table 1.2288.c GPS week : 2288 MJD: 60260.0-60266.0
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 2288 0 | -17 20 -15 -633 -688 618 81.0 1601 1601 | -1173 0
brd 2288 1 | 126 93 -11 351 1245 592 81.4 1384 1384 | -482 0
brd 2288 2 | -11 -16 55 158 -470 -627 80.3 1337 1337 | -302 0
brd 2288 3 | 9 26 69 -114 279 691 80.3 1576 1576 | -249 0
brd 2288 4 | 19 44 82 7 2255 3948 82.9 1686 1686 | -1071 0
brd 2288 5 | 57 -43 21 1731 661 -615 81.0 1659 1659 | -1160 0
brd 2288 6 | -34 -9 87 2332 -303 1186 84.0 1713 1713 | 971 0
-------------+------------------------------------------------------------+----------------
brd 2288 mean| 21 16 41 547 425 827 81.5 1565 1565 | -495 0
brd 2288 sdev| 55 45 43 1072 1054 1537 1.4 148 148 | 761 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 2.2288.0 GPS week: 2288 Day: 0 MJD: 60260
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 -10 1 -12 .02 23 17 | 40184 -2291 3070 8540
esa n/a| 1 0 0 -55 30 12 -.18 26 17 | 1835 -2703 3036 6983
gfz n/a| 0 1 3 22 2 -17 -.06 19 13 | 0 -2397 3086 7951
grg n/a| 0 -5 -3 44 -11 21 .15 28 18 | -247 -2287 3077 7476
iac n/a| -1 0 -4 25 25 13 -.13 24 22 | 509 -561 3057 8512
jgx n/a| 0 3 3 54 25 -96 -.26 31 27 | 42444 -1693 3048 8083
Table 2.2288.1 GPS week: 2288 Day: 1 MJD: 60261
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| -3 0 1 -1 -11 59 .09 27 20 | 39389 -279 2943 8664
esa n/a| 0 0 1 -57 34 -24 -.15 25 16 | 480 -1765 2929 6104
gfz n/a| 0 0 -3 30 -3 8 -.05 20 14 | 0 -1025 2980 8038
grg n/a| 3 -3 -6 25 3 -52 .27 34 20 | -577 -101 2994 7489
iac n/a| 0 0 -6 -2 11 151 -.04 27 23 | 1411 -377 2953 8657
jgx n/a| 0 3 8 42 11 -105 -.24 30 30 | 42493 25 2966 8279
Table 2.2288.2 GPS week: 2288 Day: 2 MJD: 60262
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| -3 0 1 16 19 13 .05 23 16 | 40251 -978 3734 8809
esa n/a| 1 0 0 -40 20 7 -.22 34 27 | -3662 -1508 3751 8016
gfz n/a| 2 1 2 25 -18 -31 -.07 19 14 | 0 -959 3810 8330
grg n/a| 0 -4 -4 -22 11 43 .27 29 20 | 138 -1123 3764 7899
iac n/a| 1 0 -6 -26 -33 -237 -.09 23 22 | 1729 -1089 3711 8776
jgx n/a| -3 2 1 16 25 -81 -.29 31 31 | 42986 -841 3882 8327
Table 2.2288.3 GPS week: 2288 Day: 3 MJD: 60263
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 0 -2 -1 32 .07 22 16 | 40461 -1255 3157 8655
esa n/a| -1 0 0 -28 17 -1 -.18 35 30 | 5000 -959 3151 7734
gfz n/a| 0 0 0 9 -2 2 -.08 19 14 | 0 -731 3173 7907
grg n/a| 0 -3 1 12 8 -47 .28 31 21 | 44 -1104 3184 7438
iac n/a| 0 0 -6 -29 -13 -209 -.32 25 24 | 2061 -1659 3166 8659
jgx n/a| 0 0 0 50 0 -48 -.26 31 30 | 43318 -262 3072 8140
Table 2.2288.4 GPS week: 2288 Day: 4 MJD: 60264
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 0 -7 -45 21 .18 24 17 | 40447 -2427 2908 9279
esa n/a| 0 1 -3 -27 -10 -4 -.17 34 27 | 8746 -1979 2891 7411
gfz n/a| 0 0 -1 24 26 -11 -.05 21 13 | 0 -2071 2958 8483
grg n/a| 0 -3 5 27 40 -26 .06 53 29 | -116 -2406 3000 8146
iac n/a| -3 0 -11 7 38 39 -.32 33 39 | 1554 -1090 2891 9089
jgx n/a| -1 -1 -1 21 -21 -21 -.18 30 30 | 43714 -2925 2887 8645
Table 2.2288.5 GPS week: 2288 Day: 5 MJD: 60265
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 -4 -3 69 .08 22 16 | 38218 -1965 3246 7830
esa n/a| 0 0 5 -54 11 -22 -.11 31 30 | -3252 -2618 3247 5700
gfz n/a| 0 2 0 20 -8 30 -.14 19 19 | 0 -2047 3302 7054
grg n/a| 1 -9 -8 20 -11 -92 .20 29 27 | -258 -2005 3318 6567
iac n/a| -1 1 -1 19 34 85 -.17 27 25 | 163 -1308 3249 7727
jgx n/a| 1 1 4 9 16 -16 -.19 32 32 | 41019 -2225 3379 7204
Table 2.2288.6 GPS week: 2288 Day: 6 MJD: 60266
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 0 7 -6 62 .11 21 17 | 39995 2503 2981 8821
esa n/a| 0 0 1 -41 6 -8 -.21 29 22 | 3684 1078 2969 7573
gfz n/a| -1 1 1 29 14 -10 -.15 21 14 | 0 2680 3043 8067
grg n/a| 2 -6 -3 -3 -5 -48 .20 23 17 | -831 3111 3032 7750
iac n/a| 0 0 -5 42 7 2 -.19 22 21 | 2548 611 2975 8695
jgx n/a| -1 1 0 11 49 0 -.25 29 29 | 42341 3439 3029 8269
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 3.2288.0 GPS week: 2288 Day: 0 MJD: 60260
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 689 27 24 13 19 29 42 12 | 88 57 73 61 69 55 69
R02 | 784 8 10 16 20 17 30 8 | 52 57 56 44 48 40 51
R03 | 1511 7 6 10 8 13 28 4 | 62 60 68 64 61 43 63
R04 | 1022 15 11 12 12 15 18 7 | 65 57 68 57 50 47 61
R05 | 639 15 17 15 17 20 14 9 | 46 48 47 39 38 35 44
R07M | 1251 13 11 12 16 19 13 7 | 73 63 76 62 80 61 68
R08M | 1210 13 18 11 13 44 19 8 | 69 80 74 74 98 78 73
R09E | 3992 14 12 19 11 19 18 8 | 40 36 44 42 39 47 39
R11E | 2674 10 10 11 13 12 12 6 | 37 42 40 35 40 37 38
R12E | 1365 12 12 14 15 24 20 8 | 309 318 318 311 308 313 314
R13E | 1537 18 26 29 24 24 49 14 | 67 68 81 66 66 61 69
R14E | 1367 10 14 18 22 14 20 9 | 125 131 129 131 126 134 128
R15E | 1216 19 12 12 18 24 29 9 | 91 96 99 99 92 99 95
R16E | 911 22 21 18 16 25 22 11 | 71 74 85 78 72 76 76
R17 | 1877 11 12 10 19 12 --- 7 | 46 48 46 44 43 --- 45
R18 | 649 9 25 13 17 18 12 9 | 42 51 41 35 41 40 43
R19M | 2123 61 68 25 74 44 77 33 | 72 72 91 90 81 64 76
R20M | 1266 58 70 52 78 49 42 37 | 104 113 124 108 85 107 101
R21M | 1181 13 15 11 16 11 27 8 | 55 43 46 52 47 42 48
R22M | 1544 13 8 11 19 13 14 7 | 41 38 40 51 38 35 40
R24M | 803 12 12 7 16 11 21 7 | 40 41 39 45 40 37 39
XR25 |15506 9 11 --- --- 20 --- 10 | 36 32 --- --- 31 --- 34
XR26 |21613 1 --- --- --- --- --- 0 | 51 --- --- --- --- --- 53
------+-----------------------------------------+-------------------------------------
RMS | 1601 23 26 19 28 24 31 |T 73 73 80 75 72 72 72
WRMS | 1601 17 17 13 18 22 27 |NE 54 51 57 49 47 43 51
MEDI | 1266 13 12 13 17 19 20 |MD 62 57 68 61 50 47 61
Table 3.2288.1 GPS week: 2288 Day: 1 MJD: 60261
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 839 44 19 19 50 21 65 19 | 54 43 31 33 38 33 35
R02 | 620 9 18 10 23 13 24 8 | 36 48 51 38 47 30 43
R03 | 1716 6 16 13 7 15 31 7 | 44 36 52 46 42 30 44
R04 | 910 7 26 15 11 15 26 9 | 49 43 55 59 43 39 49
R05 | 655 9 13 7 16 21 31 6 | 31 37 34 34 26 29 32
R07M | 990 11 13 11 20 14 19 8 | 47 45 52 41 53 44 45
R08M | 1039 12 8 17 11 37 21 7 | 52 57 51 62 72 47 53
R09E | 2140 22 11 15 17 21 23 9 | 37 35 41 30 35 37 33
R11E | 1676 12 8 12 12 11 14 6 | 29 29 29 25 29 28 26
R12E | 838 20 14 14 23 36 21 10 | 299 289 295 289 292 290 293
R13E | 801 29 31 49 37 42 45 22 | 66 72 104 60 63 56 71
R14E | 887 9 12 18 27 16 21 10 | 118 117 121 132 115 119 120
R15E | 1718 11 14 18 14 17 20 8 | 101 100 93 104 93 99 98
R16E | 1270 19 18 18 17 18 18 10 | 53 51 47 55 43 50 48
R17 | 1410 7 17 11 15 20 --- 7 | 30 34 33 33 25 --- 31
R18 | 447 13 15 6 9 16 21 6 | 35 38 37 38 29 36 38
R19M | 2116 54 60 19 96 37 52 34 | 56 69 65 77 56 70 60
R20M | 2195 79 68 42 80 66 40 38 | 68 94 76 81 57 76 64
R21M | 749 24 20 19 16 13 15 11 | 29 30 34 32 26 20 24
R22M | 2472 17 12 11 22 18 23 9 | 30 31 26 33 21 31 26
R24M | 772 21 14 18 18 32 25 10 | 27 26 24 25 31 24 22
XR25 |15571 12 12 --- --- 33 --- 12 | 19 32 --- --- 24 --- 23
XR26 |37942 24 --- 19 --- 94 --- 22 | 42 --- 53 --- 82 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1383 27 25 20 34 27 30 |T 58 61 63 63 58 59 57
WRMS | 1383 20 16 14 20 23 30 |NE 37 38 43 40 39 32 38
MEDI | 1039 13 14 15 17 20 23 |MD 44 43 51 41 43 37 44
Table 3.2288.2 GPS week: 2288 Day: 2 MJD: 60262
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 633 55 30 14 40 23 46 21 | 85 49 51 45 49 50 55
R02 | 701 12 22 10 20 20 12 9 | 47 56 42 36 54 42 43
R03 | 862 13 11 12 12 16 30 7 | 54 63 64 53 56 42 58
R04 | 967 9 24 30 21 19 36 13 | 53 47 81 50 59 41 60
R05 | 820 10 15 9 14 22 30 7 | 41 38 44 44 39 35 41
R07M | 1699 10 10 10 11 18 16 6 | 56 62 61 57 50 56 58
R08M | 938 13 16 12 12 20 18 7 | 53 68 66 56 48 58 60
R09E | 2057 11 15 11 10 30 22 7 | 53 52 52 45 62 59 49
R11E | 1482 10 9 9 11 23 15 5 | 31 37 37 27 36 35 32
R12E | 694 13 14 10 19 28 22 8 | 189 185 184 186 192 185 185
R13E | 619 41 32 37 29 34 38 20 | 78 66 84 64 71 71 67
R14E | 884 13 12 13 18 21 18 8 | 95 94 92 94 93 94 93
R15E | 1387 17 13 15 19 27 18 9 | 80 80 81 75 78 75 78
R16E | 914 14 20 14 21 20 17 10 | 47 47 55 43 44 45 46
R17 | 451 10 21 12 14 14 --- 8 | 32 29 38 33 32 --- 31
XR18 | 680 14 19 12 --- 14 22 10 | 32 36 34 --- 33 30 33
R19M | 1475 34 73 25 49 32 67 26 | 89 75 95 77 96 77 85
R20M | 1744 50 111 43 92 27 55 42 | 82 80 85 91 80 98 75
R21M | 699 15 17 16 15 16 14 9 | 37 32 35 41 33 31 34
R22M | 3362 14 16 11 13 20 17 7 | 22 27 29 28 23 24 23
R24M | 810 10 10 16 18 24 14 8 | 34 31 24 43 33 32 30
XR25 |20279 14 21 --- --- 23 --- 17 | 28 25 --- --- 21 --- 24
XR26 |32602 17 --- 14 --- 118 --- 16 | 44 --- 39 --- 88 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1336 23 34 19 29 23 31 |T 59 58 62 59 59 59 56
WRMS | 1336 16 27 14 20 22 31 |NE 46 42 49 43 47 40 43
MEDI | 914 13 16 12 18 22 18 |MD 53 49 52 45 50 45 49
Table 3.2288.3 GPS week: 2288 Day: 3 MJD: 60263
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1016 52 51 15 37 21 41 23 | 96 57 72 57 67 53 70
R02 | 681 10 14 4 19 25 16 7 | 67 66 67 57 60 54 64
R03 | 1240 10 10 9 10 17 19 5 | 75 73 77 68 71 66 74
R04 | 885 10 24 21 20 13 35 11 | 75 63 82 68 69 52 73
R05 | 1193 8 15 15 12 31 39 7 | 62 63 73 64 51 56 66
R07M | 1292 11 8 10 15 19 16 6 | 69 72 68 73 63 62 70
R08M | 1195 15 17 18 18 17 20 9 | 75 83 83 79 77 72 78
R09E | 2572 13 22 23 58 28 17 18 | 58 57 59 77 62 57 54
R11E | 1617 10 9 11 11 33 19 6 | 49 52 53 50 47 55 50
R12E | 864 18 19 14 22 30 22 10 | 258 259 263 258 270 257 259
R13E | 494 34 36 29 25 32 65 18 | 79 87 86 78 78 74 77
R14E | 1885 13 22 20 19 21 16 11 | 177 170 182 181 174 175 178
R15E | 1850 15 15 14 24 24 22 9 | 122 127 121 133 124 128 124
R16E | 648 18 28 19 13 19 14 11 | 65 75 58 62 59 67 62
R17 | 411 9 14 14 24 27 --- 9 | 58 57 59 58 57 --- 56
XR18 | 1180 8 15 7 --- 18 23 7 | 50 55 55 --- 46 54 53
R19M | 1408 37 76 39 70 36 57 31 | 71 53 86 75 66 67 69
R20M | 2537 44 99 35 62 24 39 34 | 81 63 75 88 70 85 72
R21M | 842 10 26 11 18 21 28 9 | 65 58 70 73 57 65 66
R22M | 3748 13 11 8 17 24 11 7 | 56 60 55 51 48 56 54
R24M | 570 8 14 12 19 17 14 7 | 66 66 65 59 57 58 63
XR25 |22325 9 17 --- --- 19 --- 13 | 53 51 --- --- 42 --- 51
XR26 |16989 12 --- 12 --- 80 --- 12 | 60 --- 51 --- 72 --- 56
------+-----------------------------------------+-------------------------------------
RMS | 1575 22 35 19 31 25 31 |T 82 80 84 85 77 80 79
WRMS | 1575 16 30 14 21 24 30 |NE 66 60 67 62 59 55 62
MEDI | 1195 12 17 14 19 24 20 |MD 67 63 70 68 63 62 66
Table 3.2288.4 GPS week: 2288 Day: 4 MJD: 60264
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 879 45 23 27 19 27 35 18 | 66 42 32 49 48 43 44
R02 | 759 10 20 7 16 35 11 7 | 41 56 42 40 46 49 43
R03 | 1529 12 8 8 10 32 17 5 | 56 52 54 53 54 47 53
R04 | 1307 14 8 4 20 16 16 6 | 57 49 50 41 52 47 50
R05 | 1423 17 13 13 11 19 25 8 | 52 60 66 53 76 45 58
R07M | 1676 9 21 8 18 29 17 8 | 47 38 54 60 57 42 47
R08M | 1583 16 14 9 13 23 16 7 | 47 57 59 56 67 50 54
R09E | 2647 17 12 17 56 19 14 14 | 46 53 56 84 57 56 52
R11E | 1976 11 20 13 40 23 22 11 | 47 53 47 55 55 38 45
R12E | 776 18 17 12 65 65 28 15 | 156 150 149 139 166 156 148
R13E | 1078 44 27 37 91 48 87 27 | 106 98 110 133 104 84 102
R14E | 2600 26 31 19 105 58 21 25 | 126 129 129 193 102 134 132
R15E | 2045 16 13 14 44 23 19 11 | 81 79 78 93 80 76 78
R16E | 959 26 15 28 107 42 23 25 | 73 69 67 135 67 68 69
R17 | 580 12 8 16 20 15 --- 8 | 35 34 33 37 35 --- 32
XR18 | 1076 10 20 10 --- 22 22 9 | 32 39 32 --- 42 33 33
R19M | 2436 35 77 29 83 28 48 31 | 67 51 72 70 57 67 59
R20M | 1500 43 108 43 60 28 17 38 | 77 52 114 92 74 72 77
R21M | 764 17 9 22 38 30 20 12 | 44 37 32 58 51 34 36
R22M | 3186 15 14 19 25 24 10 10 | 32 33 32 39 37 30 30
R24M | 521 10 12 13 18 14 22 7 | 47 43 44 49 42 37 45
XR25 |13856 11 14 --- --- 27 --- 13 | 29 26 --- --- 42 --- 26
XR26 |19529 19 --- 16 --- 93 --- 17 | 46 --- 58 --- 63 --- 52
------+-----------------------------------------+-------------------------------------
RMS | 1685 24 34 21 53 33 30 |T 61 59 64 76 64 60 59
WRMS | 1685 17 27 13 29 39 30 |NE 46 44 45 45 50 44 43
MEDI | 1500 16 14 14 25 27 20 |MD 47 52 54 56 57 47 52
Table 3.2288.5 GPS week: 2288 Day: 5 MJD: 60265
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1171 47 37 22 20 21 48 19 | 67 47 47 51 43 44 51
R02 | 689 14 20 18 18 18 18 10 | 43 52 45 43 40 46 43
R03 | 1759 11 10 9 14 24 19 6 | 51 50 47 47 43 48 48
R04 | 1013 14 11 14 24 16 17 9 | 52 47 47 47 48 44 47
R05 | 1334 9 10 7 16 26 16 6 | 52 47 45 56 58 48 49
R07M | 1005 8 18 25 21 16 19 11 | 63 57 84 62 61 57 67
R08M | 1477 18 13 15 11 14 18 8 | 55 57 66 70 60 56 61
R09E | 2474 16 12 15 14 31 13 8 | 41 46 51 49 52 45 46
R11E | 2468 16 13 13 36 15 21 12 | 35 40 38 58 37 40 37
R12E | 694 10 10 9 19 61 34 7 | 343 342 344 334 331 335 341
R13E | 724 29 36 38 44 36 69 21 | 67 68 93 67 60 69 67
R14E | 2253 17 17 14 32 29 16 11 | 236 235 252 248 235 235 242
R15E | 2600 15 18 27 54 18 22 17 | 92 94 98 130 101 89 98
R16E | 1696 18 14 14 19 48 23 9 | 81 86 86 101 58 84 85
R17 | 766 5 15 9 16 16 --- 6 | 42 47 41 46 40 --- 42
R18 | 670 15 30 12 14 17 28 10 | 44 47 43 37 37 43 43
R19M | 2909 53 65 26 52 16 66 28 | 113 99 119 99 91 95 108
R20M | 2196 39 98 38 63 30 49 35 | 62 50 69 85 71 59 63
R21M | 1170 10 18 16 11 16 15 8 | 48 45 62 52 49 45 51
R22M | 1728 12 13 12 16 19 13 7 | 33 36 40 46 32 37 37
R24M | 481 11 10 10 17 29 23 7 | 53 53 55 59 52 46 54
XR25 |12017 17 22 --- --- 21 --- 19 | 47 31 --- --- 36 --- 38
XR26 |22638 17 --- 14 --- 69 --- 16 | 60 --- 54 --- 67 --- 57
------+-----------------------------------------+-------------------------------------
RMS | 1659 22 31 19 29 27 32 |T 77 76 83 85 74 78 77
WRMS | 1659 16 30 19 27 25 32 |NE 50 46 46 46 45 45 46
MEDI | 1477 15 15 14 19 21 19 |MD 53 50 54 58 52 48 51
Table 3.2288.6 GPS week: 2288 Day: 6 MJD: 60266
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1088 38 34 31 20 21 47 18 | 89 60 66 68 72 59 70
R02 | 870 5 19 15 11 13 9 7 | 52 67 54 55 56 52 55
R03 | 741 12 11 11 15 23 19 7 | 65 71 70 73 61 59 69
R04 | 757 12 9 15 19 13 20 8 | 66 61 72 59 62 52 65
R05 | 988 11 9 9 10 12 28 5 | 60 61 64 60 60 51 61
R07M | 861 9 13 15 18 16 11 8 | 72 67 78 67 74 64 71
R08M | 1868 9 10 14 11 15 19 6 | 75 79 84 80 78 78 79
R09E | 3358 11 17 12 12 25 16 7 | 47 54 53 49 59 51 49
R11E | 2641 12 17 18 14 14 15 9 | 32 39 33 37 34 33 32
R12E | 1376 16 14 24 27 25 26 12 | 295 305 300 290 289 293 297
R13E | 774 22 40 49 39 26 64 22 | 65 80 92 70 72 76 72
R14E | 1330 11 16 15 11 32 31 7 | 206 199 204 212 209 210 205
R15E | 3492 9 18 12 11 28 36 7 | 86 83 86 90 89 86 85
R16E | 1729 19 18 15 13 13 25 9 | 71 61 65 72 56 63 66
R17 | 728 6 10 6 10 16 --- 4 | 47 46 47 52 43 --- 47
R18 | 626 20 28 9 13 16 23 10 | 39 54 42 36 42 43 44
R19M | 2890 55 64 20 58 28 34 29 | 132 119 128 133 142 131 127
R20M | 1313 47 84 43 42 37 46 31 | 95 57 89 90 86 89 81
R21M | 1420 8 21 11 12 13 13 7 | 66 61 65 70 64 60 65
R22M | 1499 12 10 13 16 28 15 7 | 37 38 39 41 37 38 37
R24M | 611 12 16 12 24 20 23 9 | 92 91 88 95 87 91 91
XR25 |11898 12 15 --- --- 21 --- 13 | 38 29 --- --- 28 --- 34
XR26 |19259 20 --- 20 --- 80 --- 20 | 59 --- 53 --- 80 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 1713 21 29 21 23 22 29 |T 82 81 85 85 81 83 80
WRMS | 1713 17 22 14 17 21 29 |NE 57 56 58 57 56 52 55
MEDI | 1330 12 16 15 14 21 23 |MD 66 61 66 70 64 60 66
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