[IGSREPORT-29693] Wk 2295 IGLOS Final Orbits
acc
acc at igs.org
Mon Jan 22 10:49:17 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2295 (Dec 31, 2023 - Jan 06, 2024)
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 2.2295.
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:
igl2295[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2295 in the SP3 format.
igl22957.sum Combination Report for GPS Week 2295.
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 | -0.0 ns
1 | -2.0 ns
2 | -15.7 ns
3 | 1.1 ns
4 | -2.1 ns
5 | -2.4 ns
6 | -0.3 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
1 | COD | R25
1 | ESA | R25
1 | GFZ | R25
1 | GRG | R25
1 | IAC | R25
1 | JGX | R25
2 | COD | R25
2 | ESA | R25
2 | GFZ | R25
2 | GRG | R25
2 | IAC | R25
2 | JGX | R25
3 | COD | R25
3 | ESA | R20 R25
3 | GFZ | R25
3 | GRG | R25
3 | IAC | R25
3 | JGX | R25
4 | COD | R25
4 | ESA | R25
4 | GFZ | R25
4 | GRG | R25
4 | IAC | R25
4 | JGX | R25
5 | COD | R25
5 | ESA | R25
5 | GFZ | R25
5 | GRG | R25
5 | IAC | R25
5 | JGX | R25
6 | COD | R25
6 | ESA | R25
6 | GFZ | R25
6 | GRG | R25
6 | IAC | R25
6 | JGX | R25
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 1.2295, 1a.2295).
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 2.2295.0-6)
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 3.2295.0-6).
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 2295 summary. (Dec 31, 2023 - Jan 06, 2024)
Table 1.2295.a GPS week : 2295 MJD: 60309.0-60315.0
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 1 -2 -30 -5 75 .09 21 17 | 41906 -1199 3192 7815
| 0 1 2 19 22 31 .04 | 7834 3768
esa n/a| 0 0 0 -29 12 -4 -.21 39 25 | -4581 -1704 3179 7515
| 0 1 2 8 14 25 .02 | 13141 4389
gfz n/a| 0 0 1 15 -5 -10 .04 22 15 | 0 -1044 3152 7633
| 1 0 1 10 11 8 .04 | 0 3499
grg n/a| 1 -3 -2 18 -1 -39 .29 30 25 | -2744 -1070 3162 7022
| 0 0 1 20 14 33 .05 | 6756 3536
iac n/a| -1 0 -5 0 -4 -54 -.16 22 19 | -737 -808 3195 8155
| 1 1 2 26 29 67 .05 | 6836 1501
jgx n/a| 1 0 2 37 1 -44 -.23 25 24 | 44286 -1022 3164 7938
| 0 1 2 8 20 32 .03 | 8069 3826
Table 1.2295.b GPS week : 2295 MJD: 60309.0-60315.0
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 | 15 15 17 16 19 20 15 |
R02 | 9 8 8 8 7 7 7 |
R03 | 8 8 8 5 7 10 10 |
R04 | 8 7 7 7 6 10 8 |
R05 | 8 7 6 7 8 6 8 |
R07 | 8 7 8 6 6 8 7 |
R08 | 9 7 6 7 7 7 8 |
R09 | 7 8 7 7 7 7 7 |
R11 | 6 7 6 8 8 8 6 |
R12 | 7 9 8 5 7 6 7 |
R13 | 18 20 20 25 16 14 18 |
R14 | 8 6 7 7 7 7 7 |
R15 | 8 10 7 8 9 9 8 |
R16 | 8 12 10 9 9 9 8 |
R17 | 7 8 8 7 10 9 9 |
R18 | 7 8 8 7 8 7 7 |
R19 | 19 19 27 24 24 23 21 |
R20 | 37 33 29 30 41 35 39 |
R21 | 10 10 12 13 8 11 8 |
R22 | 8 7 8 8 7 6 8 |
R24 | 11 11 10 11 11 12 10 |
R25 | 14 --- --- --- --- --- --- |
R26 | 0 0 --- --- --- --- --- |
Table 1.2295.c GPS week : 2295 MJD: 60309.0-60315.0
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 2295 0 | 74 55 137 -210 -548 3634 80.4 1382 1382 | -3 0
brd 2295 1 | 32 39 26 -1303 -795 1423 81.3 1539 1539 | -1988 0
brd 2295 2 | 27 49 76 -193 -1232 789 82.9 1479 1479 | -15718 0
brd 2295 3 | 52 18 60 -1212 -1353 -191 80.3 1477 1477 | 1098 0
brd 2295 4 | -6 -26 80 -1939 -338 -4379 80.1 1572 1572 | -2123 0
brd 2295 5 | 23 -73 81 -1672 -879 1869 82.7 1407 1407 | -2438 0
brd 2295 6 | 105 10 90 827 242 2972 78.9 1685 1685 | -314 0
-------------+------------------------------------------------------------+----------------
brd 2295 mean| 44 10 79 -814 -700 873 81.0 1505 1505 | -3069 0
brd 2295 sdev| 36 46 33 986 546 2647 1.5 103 103 | 5727 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 2.2295.0 GPS week: 2295 Day: 0 MJD: 60309
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 -8 -16 67 .17 17 15 | 44743 -758 3249 7522
esa n/a| 1 0 1 -17 -3 17 -.19 39 21 | -538 -1691 3247 6660
gfz n/a| 2 0 0 18 -16 1 -.00 19 16 | 0 -435 2950 6575
grg n/a| 1 -2 -2 -17 18 -97 .31 34 24 | -91 -242 2931 6207
iac n/a| 0 0 -1 30 -17 21 -.07 20 19 | 2207 -1089 3247 7653
jgx n/a| 1 0 0 28 30 -6 -.23 22 22 | 47552 42 2972 6874
Table 2.2295.1 GPS week: 2295 Day: 1 MJD: 60310
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 3 -2 -48 12 66 .08 20 16 | 43922 -4550 3037 6482
esa n/a| 0 1 -2 -22 2 -29 -.19 41 28 | 4538 -6151 2920 6007
gfz n/a| 0 0 3 8 -16 -6 .02 18 13 | 0 -3990 3036 6409
grg n/a| 1 -3 -1 25 7 -30 .23 33 31 | 118 -4497 3045 5937
iac n/a| -3 -1 -6 -22 41 -156 -.17 23 21 | 787 -1664 3047 6885
jgx n/a| 2 0 0 35 15 -42 -.27 28 27 | 46388 -4593 3025 6725
Table 2.2295.2 GPS week: 2295 Day: 2 MJD: 60311
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 -26 5 49 .08 15 13 | 24766 4720 3095 7059
esa n/a| 0 1 2 -26 15 -42 -.23 34 24 | -29272 4805 3104 6158
gfz n/a| -1 0 2 -5 7 -6 -.00 19 13 | 0 4066 3093 7026
grg n/a| 2 -4 -3 46 0 -37 .28 28 24 | -18057 4376 3085 6624
iac n/a| -1 0 -6 31 2 -66 -.19 20 17 | -15958 1266 3095 7580
jgx n/a| 2 0 4 48 -10 -49 -.28 28 25 | 26766 5173 3103 7108
Table 2.2295.3 GPS week: 2295 Day: 3 MJD: 60312
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 -1 0 35 .10 19 15 | 48018 1693 2720 7513
esa n/a| 1 -1 0 -30 0 14 -.18 48 27 | -10195 2378 2732 7063
gfz n/a| -1 2 0 18 10 -24 .03 22 16 | 0 1860 2740 7432
grg n/a| 1 -2 -3 14 -15 -14 .37 31 25 | 12 1588 2731 6656
iac n/a| -4 1 -7 18 19 -33 -.23 18 16 | 4344 -642 2742 7956
jgx n/a| 0 0 5 44 -16 -14 -.18 28 25 | 51019 966 2660 7389
Table 2.2295.4 GPS week: 2295 Day: 4 MJD: 60313
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 -31 -40 93 .06 20 15 | 46816 -4267 2993 8217
esa n/a| 0 1 0 -36 35 1 -.22 39 26 | 3040 -5311 2999 9226
gfz n/a| 0 0 0 17 -1 -15 .06 31 16 | 0 -4075 2978 8098
grg n/a| 1 -3 0 4 5 -34 .30 29 23 | -110 -3970 2986 7362
iac n/a| -1 1 -2 -12 -45 26 -.15 20 16 | 750 -117 2980 8340
jgx n/a| 1 2 2 30 19 -28 -.21 22 21 | 49095 -3672 2975 8447
Table 2.2295.5 GPS week: 2295 Day: 5 MJD: 60314
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 -52 -26 85 .04 29 22 | 42785 -5529 3858 9344
esa n/a| 0 0 -2 -32 20 -13 -.23 34 25 | -9625 -6182 3853 9117
gfz n/a| 0 0 3 17 -3 -7 .10 23 16 | 0 -5298 3847 9372
grg n/a| 0 -2 -3 27 -3 3 .27 27 20 | -544 -5026 3930 8875
iac n/a| 0 0 -3 -30 -28 -116 -.13 24 21 | 665 -3480 3841 9733
jgx n/a| 0 1 4 31 -10 -80 -.23 23 23 | 44727 -5700 3892 9810
Table 2.2295.6 GPS week: 2295 Day: 6 MJD: 60315
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 0 -45 23 131 .08 28 25 | 42296 296 3398 8571
esa n/a| 0 0 2 -42 20 22 -.20 36 23 | 9980 223 3404 8378
gfz n/a| 0 0 0 28 -15 -15 .05 22 14 | 0 564 3420 8520
grg n/a| 0 -4 -4 25 -22 -63 .27 30 30 | -542 278 3428 7495
iac n/a| 0 -2 -8 -21 -2 -60 -.20 28 22 | 2046 69 3414 8941
jgx n/a| 2 -1 4 45 -20 -91 -.23 24 24 | 44459 625 3522 9219
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 3.2295.0 GPS week: 2295 Day: 0 MJD: 60309
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1493 24 36 34 30 33 24 14 | 79 74 90 72 75 67 74
XR02 | 1343 11 12 14 21 24 --- 8 | 57 60 65 51 60 --- 58
R03E | 1480 15 14 18 17 17 17 8 | 106 109 109 111 111 108 107
R04E | 1798 12 16 15 16 12 19 7 | 114 120 117 115 119 121 116
R05E | 1463 14 12 20 16 17 9 7 | 141 139 138 137 144 138 138
R07E | 954 6 18 19 19 15 15 7 | 137 133 140 141 136 137 137
R08E | 1726 14 24 15 10 9 21 8 | 89 106 93 90 94 83 89
R09 | 1090 20 17 10 10 22 11 7 | 23 21 23 21 26 20 19
R11 | 1201 11 12 15 11 19 10 6 | 16 20 22 21 30 19 16
R12 | 1411 8 23 9 14 15 15 6 | 56 57 56 50 48 45 52
XR13 | 958 30 27 18 44 19 --- 17 | 61 38 46 33 45 --- 45
R14 | 1254 11 16 19 13 34 14 7 | 56 61 67 32 62 49 56
R15 | 1497 21 13 16 12 17 7 7 | 73 57 51 54 54 54 57
R16 | 1280 18 22 17 8 21 12 8 | 73 55 51 62 56 56 60
XR17 | 1851 7 20 9 8 15 --- 6 | 65 55 67 66 64 --- 64
R18 | 1373 5 9 14 13 19 19 6 | 53 60 60 62 62 40 54
R19 | 1826 18 68 19 64 18 26 19 | 97 54 92 112 92 69 85
R20 | 1479 37 130 39 112 28 57 36 | 115 83 119 156 124 100 101
R21 | 876 12 29 19 18 13 20 9 | 68 48 77 75 69 53 65
R22 | 1326 15 11 10 19 12 19 7 | 31 31 36 34 27 33 31
R24 | 811 12 26 16 31 21 24 10 | 74 59 82 87 80 59 72
XR25 |10681 8 21 --- --- 22 --- 13 | 16 24 --- --- 30 --- 6
XR26 | ---- 5 --- --- --- --- --- 0 | 8 --- --- --- --- --- 8
------+-----------------------------------------+-------------------------------------
RMS | 1381 17 39 19 34 20 22 |T 69 66 76 75 73 69 65
WRMS | 1381 15 21 16 24 19 22 |NE 55 48 60 61 58 49 49
MEDI | 1373 12 18 16 16 18 17 |MD 68 57 67 66 62 56 60
Table 3.2295.1 GPS week: 2295 Day: 1 MJD: 60310
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 2350 26 34 31 18 40 39 15 | 63 65 68 64 62 59 59
XR02 | 1305 10 16 15 16 18 --- 8 | 51 54 50 55 50 --- 50
R03E | 1878 12 18 15 13 15 22 8 | 123 119 115 116 121 110 116
R04E | 891 9 14 13 18 16 14 6 | 98 98 100 108 93 102 100
R05E | 710 14 11 16 15 22 13 7 | 105 106 109 108 97 106 106
R07E | 637 11 13 11 16 19 16 6 | 108 101 101 105 99 106 103
XR08E | 1100 13 --- 12 16 25 8 7 | 61 --- 62 70 61 64 62
R09 | 1255 18 14 17 15 22 14 8 | 20 15 26 17 26 17 15
R11 | 875 13 20 11 13 18 16 7 | 21 25 30 21 20 23 21
R12 | 1207 13 18 16 15 19 23 8 | 46 51 53 45 34 41 46
R13 | 728 36 25 16 45 25 63 19 | 46 40 36 27 39 36 34
R14 | 1489 9 16 9 15 21 8 5 | 45 48 46 31 52 45 44
R15 | 1735 26 13 7 10 12 31 10 | 62 46 40 49 48 47 47
XR16 | 1138 23 23 17 13 16 --- 11 | 51 29 28 47 30 --- 37
XR17 | 1077 11 22 6 15 19 --- 7 | 40 40 39 38 43 --- 39
XR18 | 752 14 12 13 11 16 --- 7 | 33 35 45 42 42 --- 39
R19 | 651 22 72 13 55 20 35 19 | 61 40 55 72 53 62 56
R20 | 3608 42 127 36 92 40 40 33 | 62 60 50 89 63 48 49
R21 | 921 7 28 18 24 13 21 9 | 40 33 49 51 38 37 43
R22 | 1443 13 9 8 19 21 15 6 | 27 30 30 32 19 28 28
R24 | 1096 9 32 17 32 23 21 10 | 43 39 51 45 48 35 43
XR26 | ---- 5 --- --- --- --- --- 0 | 7 --- --- --- --- --- 8
------+-----------------------------------------+-------------------------------------
RMS | 1539 20 41 18 33 23 28 |T 53 52 56 58 52 56 52
WRMS | 1539 16 28 13 31 21 27 |NE 39 38 41 44 39 38 37
MEDI | 1100 13 18 15 16 19 21 |MD 46 40 50 49 48 47 44
Table 3.2295.2 GPS week: 2295 Day: 2 MJD: 60311
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 823 17 44 39 24 32 48 17 | 47 52 72 56 52 44 48
XR02 | 1403 9 15 20 9 20 --- 8 | 43 45 50 50 36 --- 44
R03E | 1601 10 19 14 16 17 18 7 | 69 79 75 73 69 57 69
R04E | 1327 9 15 15 15 22 13 6 | 58 66 69 58 60 53 60
R05E | 539 11 10 9 16 17 11 6 | 65 59 59 66 70 64 62
R07E | 1165 10 16 17 17 10 17 7 | 58 57 64 60 57 54 57
R08E | 2443 8 19 8 17 15 12 6 | 49 48 48 50 49 41 46
XR09 | 749 11 10 10 15 12 --- 7 | 20 22 24 18 20 --- 18
R11 | 1100 9 14 15 8 17 10 5 | 13 16 33 15 25 23 18
R12 | 1219 8 11 20 14 26 25 8 | 43 44 53 40 43 36 43
R13 | 542 34 18 20 45 22 69 20 | 37 31 28 26 27 25 27
R14 | 1274 8 20 11 13 10 14 6 | 36 50 40 25 38 42 38
R15 | 1344 11 12 14 10 13 20 7 | 54 53 56 52 46 42 52
R16 | 1576 19 20 15 18 13 29 10 | 64 54 41 62 58 50 52
XR17 | 1216 8 22 8 19 26 --- 8 | 47 38 49 57 60 --- 47
R18 | 670 5 22 11 21 16 22 8 | 36 45 37 37 40 27 34
XR19 | 739 30 84 19 55 31 --- 26 | 82 47 76 81 79 --- 73
R20 | 3051 28 111 39 75 31 44 29 | 85 52 102 111 97 63 81
R21 | 1011 7 34 15 32 20 29 11 | 50 31 51 70 59 38 48
R22 | 2093 12 14 12 27 12 14 8 | 20 23 30 29 18 23 20
R24 | 686 12 33 14 24 27 14 9 | 52 41 54 54 59 46 49
------+-----------------------------------------+-------------------------------------
RMS | 1478 15 34 19 28 20 28 |T 48 44 52 51 49 42 46
WRMS | 1478 13 24 13 23 17 25 |NE 44 38 48 48 45 37 42
MEDI | 1216 10 19 15 17 17 18 |MD 47 45 51 54 49 42 48
Table 3.2295.3 GPS week: 2295 Day: 3 MJD: 60312
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 556 25 40 30 29 34 34 15 | 43 50 54 47 48 36 40
XR02 | 810 12 11 12 16 14 --- 7 | 47 50 44 54 44 --- 45
R03E | 1111 9 14 10 7 16 11 5 | 121 118 117 121 118 114 118
R04E | 1020 12 15 12 15 20 15 7 | 48 42 39 48 37 38 40
R05E | 590 10 15 13 16 17 14 6 | 37 35 41 42 42 26 34
R07E | 847 12 12 12 13 13 12 6 | 42 39 46 46 36 39 40
R08E | 2944 9 20 13 20 12 10 7 | 46 48 43 54 53 46 45
R09 | 1328 15 11 14 18 14 15 7 | 13 21 27 21 18 25 17
R11 | 1704 13 25 15 17 17 10 8 | 16 23 28 17 22 15 15
R12 | 819 8 10 8 19 14 8 5 | 29 30 31 17 23 27 26
R13 | 827 45 25 23 74 24 73 25 | 50 27 35 34 26 24 26
R14 | 708 7 14 16 18 10 15 7 | 36 45 43 19 37 25 34
R15 | 991 12 17 15 16 10 20 8 | 45 58 47 36 43 43 44
R16 | 1500 15 16 18 14 19 23 8 | 52 60 64 43 67 38 50
XR17 | 1195 11 15 9 13 25 --- 7 | 57 46 53 54 60 --- 53
R18 | 728 7 16 12 21 14 10 6 | 42 50 42 47 42 41 42
R19 | 839 33 86 23 67 29 28 24 | 93 40 91 106 83 95 83
R20 | 3332 33 169 58 48 19 64 29 | 108 37 141 114 115 86 114
R21 | 972 10 23 36 18 16 26 12 | 57 53 87 73 67 49 63
R22 | 2119 13 16 11 30 15 10 8 | 16 28 28 48 32 23 24
R24 | 1253 14 34 14 22 16 22 10 | 67 53 65 65 58 46 59
------+-----------------------------------------+-------------------------------------
RMS | 1476 19 48 22 31 18 28 |T 49 45 55 52 50 44 48
WRMS | 1476 15 27 16 25 16 24 |NE 47 41 55 49 48 41 46
MEDI | 991 12 16 14 18 16 15 |MD 45 42 44 47 42 38 42
Table 3.2295.4 GPS week: 2295 Day: 4 MJD: 60313
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 811 30 34 53 36 23 29 18 | 53 46 87 49 50 43 51
XR02 | 977 9 13 12 12 10 --- 6 | 40 48 41 43 38 --- 41
R03E | 968 9 10 17 11 16 15 6 | 64 65 70 67 56 68 66
R04E | 1789 8 15 10 15 15 12 6 | 57 63 60 56 57 57 57
R05E | 1058 14 13 16 17 12 14 7 | 71 69 65 67 64 70 68
R07E | 628 12 13 13 14 12 9 6 | 65 62 72 67 63 63 65
R08E | 3249 9 16 12 19 21 9 6 | 45 42 45 50 45 41 44
R09 | 1235 15 8 17 14 15 9 6 | 15 21 28 23 18 20 18
R11 | 2141 14 14 23 19 18 8 8 | 19 25 36 25 26 19 22
R12 | 1147 19 17 10 14 13 10 7 | 44 48 44 50 37 46 45
R13 | 659 24 26 18 45 17 37 15 | 50 37 45 45 32 25 37
R14 | 648 6 8 20 15 19 17 7 | 42 42 55 29 46 39 41
R15 | 602 18 18 15 12 13 20 8 | 54 54 53 46 50 37 47
R16 | 1102 17 25 11 15 13 17 8 | 58 74 55 45 57 47 54
XR17 | 1859 13 23 13 20 14 --- 10 | 52 50 49 52 45 --- 50
R18 | 1119 10 16 13 21 13 14 7 | 43 54 51 50 44 37 45
R19 | 794 40 82 26 66 32 25 24 | 91 42 80 99 72 71 75
R20 | 2253 47 128 108 62 45 63 41 | 104 38 140 112 102 74 86
R21 | 968 10 25 13 22 17 11 8 | 56 45 56 69 62 55 55
R22 | 3293 11 14 11 22 13 12 7 | 25 32 35 26 24 30 28
R24 | 1218 17 27 15 32 24 15 10 | 50 45 44 64 53 42 46
------+-----------------------------------------+-------------------------------------
RMS | 1572 20 39 31 29 20 22 |T 50 46 57 54 49 46 49
WRMS | 1572 15 26 16 23 16 21 |NE 47 42 54 51 46 41 46
MEDI | 1102 14 16 15 19 15 14 |MD 50 45 53 50 46 43 47
Table 3.2295.5 GPS week: 2295 Day: 5 MJD: 60314
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 773 49 25 51 36 34 30 20 | 70 57 75 61 62 60 59
XR02 | 838 7 15 12 13 10 --- 7 | 60 63 56 61 60 --- 59
R03E | 515 29 16 13 23 16 15 9 | 88 84 87 87 85 81 83
R04E | 1037 8 15 24 27 17 14 9 | 88 90 94 86 94 87 87
R05E | 1871 13 11 9 10 14 15 6 | 108 112 110 107 112 106 108
R07E | 713 11 14 18 16 22 15 7 | 112 115 117 115 114 114 114
R08E | 2947 12 14 16 19 22 9 7 | 73 66 76 70 77 67 70
R09 | 906 13 12 16 12 10 9 6 | 16 25 26 18 18 19 17
R11 | 1667 15 15 19 12 23 13 7 | 20 24 27 20 27 24 19
R12 | 1692 18 10 8 13 15 12 6 | 48 39 49 37 42 43 42
R13 | 690 31 19 14 39 16 32 14 | 38 33 39 36 33 26 32
XR14 | 543 14 8 12 --- 14 9 6 | 38 40 54 --- 45 46 45
R15 | 508 29 16 10 17 12 15 9 | 51 44 41 29 44 43 39
R16 | 539 19 14 16 12 14 21 8 | 60 62 57 57 60 49 55
XR17 | 1613 15 22 11 10 16 --- 8 | 44 38 42 41 39 --- 39
R18 | 1238 12 17 13 13 10 14 7 | 37 42 42 35 34 36 37
R19 | 1054 51 62 32 47 38 42 23 | 48 31 54 47 51 39 39
R20 | 1521 74 108 48 64 60 51 34 | 69 54 62 49 60 60 46
R21 | 682 17 28 18 23 22 21 10 | 49 42 51 52 55 44 45
R22 | 2347 16 12 12 14 13 9 6 | 40 46 47 55 49 43 45
R24 | 1596 19 33 21 24 18 25 12 | 47 33 44 44 41 31 38
------+-----------------------------------------+-------------------------------------
RMS | 1406 29 34 23 27 24 23 |T 56 53 59 55 55 53 53
WRMS | 1406 22 25 16 20 21 23 |NE 43 40 46 41 42 38 39
MEDI | 1037 16 15 16 16 16 15 |MD 48 42 54 49 49 44 45
Table 3.2295.6 GPS week: 2295 Day: 6 MJD: 60315
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1042 27 35 35 21 29 30 15 | 67 82 98 70 74 67 73
XR02 | 667 11 12 11 9 12 --- 6 | 53 54 57 56 57 --- 54
R03E | 928 27 19 19 20 16 16 10 | 90 87 86 79 86 78 82
R04E | 632 8 18 16 21 24 13 7 | 103 109 105 102 111 103 103
R05E | 2452 10 13 22 15 12 15 8 | 129 127 127 126 129 127 126
R07E | 638 10 14 10 18 17 14 6 | 126 125 126 131 127 129 127
R08E | 3271 9 19 16 24 15 12 8 | 69 57 66 77 70 70 67
R09 | 562 14 13 13 13 15 11 6 | 29 30 31 28 28 25 27
XR11 | 1101 9 12 9 11 20 --- 5 | 18 22 29 28 24 --- 23
R12 | 1223 21 7 9 14 15 15 7 | 54 46 50 44 46 43 46
R13 | 1402 50 24 12 40 27 40 17 | 48 37 37 29 34 37 32
XR14 | 651 12 9 9 --- 12 12 6 | 43 45 51 --- 52 41 44
R15 | 768 15 21 16 12 27 11 7 | 64 51 60 48 53 53 54
R16 | 1231 24 15 7 16 31 13 8 | 76 58 59 57 71 53 60
XR17 | 1674 13 20 10 20 17 --- 9 | 71 57 67 68 65 --- 66
R18 | 1246 11 16 9 18 21 15 7 | 55 67 62 61 59 48 58
R19 | 956 36 52 22 57 41 43 21 | 102 50 92 111 98 71 86
R20 | 3736 79 120 62 80 70 54 39 | 138 79 133 139 136 93 110
R21 | 602 13 18 15 15 26 20 8 | 75 57 83 84 85 61 72
R22 | 1907 12 9 17 18 16 17 7 | 43 43 48 49 46 40 43
R24 | 1573 14 32 17 18 20 19 10 | 74 53 77 79 75 59 68
------+-----------------------------------------+-------------------------------------
RMS | 1685 28 36 22 30 28 24 |T 70 62 73 73 71 66 67
WRMS | 1685 25 23 14 30 22 24 |NE 60 48 62 62 60 52 56
MEDI | 1101 13 18 15 18 20 15 |MD 67 54 66 68 65 59 66
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