[IGSREPORT-29715] Wk 2297 IGLOS Final Orbits
acc
acc at igs.org
Mon Feb 5 03:39:34 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2297 (Jan 14, 2024 - Jan 20, 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 2.2297.
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:
igl2297[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2297 in the SP3 format.
igl22977.sum Combination Report for GPS Week 2297.
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 | -18.7 ns
1 | -23.4 ns
2 | -11.4 ns
3 | -9.5 ns
4 | -8.4 ns
5 | -11.1 ns
6 | -2.0 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
----+--------+---------------
0 | COD | R26
0 | ESA | R11 R26
0 | GFZ | R26
0 | GRG | R11 R26
0 | IAC | R26
0 | JGX | R26
1 | COD | R11 R26
1 | ESA | R11 R26
1 | GFZ | R11 R26
1 | GRG | R11 R26
1 | IAC | R11 R26
1 | JGX | R11 R26
2 | COD | R11 R26
2 | ESA | R11 R20 R26
2 | GFZ | R11 R26
2 | GRG | R11 R26
2 | IAC | R11 R26
2 | JGX | R11 R26
3 | COD | R26
3 | ESA | R11 R26
3 | GFZ | R26
3 | GRG | R11 R26
3 | IAC | R26
3 | JGX | R26
4 | COD | R26
4 | ESA | R26
4 | GFZ | R26
4 | GRG | R26
4 | IAC | R26
4 | JGX | R26
5 | COD | R26
5 | ESA | R26
5 | GFZ | R26
5 | GRG | R26
5 | IAC | R26
5 | JGX | R26
6 | COD | R26
6 | ESA | R20 R26
6 | GFZ | R26
6 | GRG | R26
6 | IAC | R26
6 | JGX | R26
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 1.2297, 1a.2297).
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 2.2297.0-6)
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 3.2297.0-6).
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 2297 summary. (Jan 14, 2024 - Jan 20, 2024)
Table 1.2297.a GPS week : 2297 MJD: 60323.0-60329.0
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 0 3 -7 -8 81 .09 23 20 | 14283 -3313 3733 8356
| 1 1 1 25 11 14 .05 | 3192 4185
esa n/a| 0 0 0 -24 -12 -23 -.17 42 27 | -12115 -3656 3749 7926
| 0 1 1 15 15 27 .04 | 7699 4472
gfz n/a| 0 0 2 38 4 -19 .07 25 15 | 0 -3304 3761 7705
| 1 0 2 12 3 37 .05 | 0 4198
grg n/a| 1 -3 -4 -7 4 4 .24 30 23 | -10666 -3309 3817 7410
| 0 1 1 15 21 74 .07 | 6237 4300
iac n/a| -1 1 -3 4 18 -34 -.19 23 20 | -10987 28 3738 8478
| 1 1 2 23 30 28 .10 | 7056 2169
jgx n/a| 0 1 -2 -18 12 -63 -.28 31 28 | 17225 -3277 3758 8016
| 1 1 0 21 18 69 .08 | 3721 4253
Table 1.2297.b GPS week : 2297 MJD: 60323.0-60329.0
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 | 21 17 16 20 18 18 19 |
R02 | 8 8 8 7 7 8 7 |
R03 | 6 6 8 7 7 6 7 |
R04 | 10 8 7 7 7 8 7 |
R05 | 8 7 6 7 8 9 7 |
R07 | 7 7 8 7 7 8 8 |
R08 | 8 11 11 8 10 9 7 |
R09 | 8 7 6 7 6 7 8 |
R11 | 602 --- --- 11 11 9 8 |
R12 | 9 7 8 7 7 8 7 |
R13 | 18 20 17 21 22 23 16 |
R14 | 7 5 6 8 7 7 7 |
R15 | 7 8 9 17 10 6 9 |
R16 | 8 7 7 9 10 8 9 |
R17 | 9 11 12 11 9 9 9 |
R18 | 7 9 9 11 9 8 8 |
R19 | 21 22 21 20 25 24 24 |
R20 | 44 45 34 44 35 41 40 |
R21 | 10 12 10 14 9 10 12 |
R22 | 7 10 11 7 9 12 8 |
R24 | 13 13 13 12 11 12 10 |
R25 | 11 12 15 0 0 12 15 |
Table 1.2297.c GPS week : 2297 MJD: 60323.0-60329.0
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 2297 0 | 32 64 24 -2216 -761 5616 80.3 1704 1704 | -18745 0
brd 2297 1 | -105 -30 15 -1842 -1978 4611 78.3 1815 1815 | -23445 0
brd 2297 2 | 40 72 36 -1170 -52 -1498 78.9 1958 1958 | -11393 0
brd 2297 3 | -3 -34 179 -44 -47 869 80.8 1909 1909 | -9450 0
brd 2297 4 | 52 -25 259 387 819 -449 79.7 1757 1757 | -8360 0
brd 2297 5 | -17 5 94 -418 1693 -3782 78.7 1501 1501 | -11123 0
brd 2297 6 | -77 72 144 -322 3949 -576 81.2 1426 1426 | -1953 0
-------------+------------------------------------------------------------+----------------
brd 2297 mean| -11 17 107 -803 517 684 79.7 1724 1724 | -12067 0
brd 2297 sdev| 60 50 91 964 1904 3350 1.1 198 198 | 7050 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 2.2297.0 GPS week: 2297 Day: 0 MJD: 60323
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 2 -48 -31 71 .08 28 23 | 20086 -6436 3262 10003
esa n/a| 0 0 -1 -19 -7 -36 -.23 40 25 | -5894 -8215 3281 8260
gfz n/a| 0 2 0 32 2 -22 .09 24 13 | 0 -5915 3239 8463
grg n/a| 1 -3 -3 -3 9 -106 .33 30 26 | -16991 -6085 3313 8564
iac n/a| 0 0 -3 5 26 5 -.13 23 20 | -18783 -1347 3262 10178
jgx n/a| 0 2 -1 -11 33 28 -.42 29 29 | 24378 -6461 3239 8891
Table 2.2297.1 GPS week: 2297 Day: 1 MJD: 60324
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 5 -10 3 66 .12 24 24 | 12583 -5157 3256 8185
esa n/a| 0 0 1 -6 -41 -39 -.15 41 20 | -21980 -5026 3231 6983
gfz n/a| 0 0 0 27 6 -48 .03 26 14 | 0 -4971 3240 7375
grg n/a| 3 -1 -2 -32 26 44 .27 33 24 | -20801 -5172 3255 7139
iac n/a| -1 5 0 11 47 -64 -.08 25 22 | -22028 1403 3259 8400
jgx n/a| 1 1 -3 -8 -11 -3 -.37 28 28 | 14263 -4907 3270 7948
Table 2.2297.2 GPS week: 2297 Day: 2 MJD: 60325
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 1 0 5 -6 106 .18 22 20 | 16511 -6371 3239 8996
esa n/a| -2 1 -1 -9 -17 -25 -.17 46 20 | -6828 -7360 3242 8055
gfz n/a| 1 0 5 26 4 -69 .01 20 16 | 0 -6576 3221 8050
grg n/a| 1 -5 -5 -15 16 23 .25 28 24 | -8055 -6655 3249 7801
iac n/a| 0 2 0 28 -38 -5 -.08 22 20 | -11380 -1423 3239 9040
jgx n/a| 0 0 -2 -18 17 -14 -.24 29 24 | 19058 -6208 3227 8502
Table 2.2297.3 GPS week: 2297 Day: 3 MJD: 60326
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 -15 -1 68 .09 24 23 | 13657 2714 3890 7307
esa n/a| 0 0 -1 -16 -7 10 -.12 36 22 | -22940 2928 3974 7721
gfz n/a| -2 1 3 44 3 -40 .13 28 20 | 0 3070 3967 6664
grg n/a| 0 -2 -2 14 -37 63 .23 35 27 | -11443 3310 4231 6164
iac n/a| -2 0 -5 6 33 -59 -.15 26 21 | -8830 3805 3927 7357
jgx n/a| 0 0 -2 13 23 -76 -.27 33 26 | 16263 3043 4162 7040
Table 2.2297.4 GPS week: 2297 Day: 4 MJD: 60327
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 4 16 -11 85 .09 19 17 | 14711 -3633 4219 7334
esa n/a| 0 -1 -2 -45 9 18 -.17 41 27 | -3807 -4086 4259 6893
gfz n/a| 0 1 1 28 9 41 .03 23 18 | 0 -4623 4242 7063
grg n/a| 2 -4 -3 -5 -11 -98 .27 31 21 | -6217 -4583 4264 6777
iac n/a| -3 0 -5 -7 37 -58 -.27 24 19 | -7023 58 4204 7473
jgx n/a| 0 3 -4 -56 -15 -81 -.22 31 28 | 18150 -4788 3862 7110
Table 2.2297.5 GPS week: 2297 Day: 5 MJD: 60328
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 25 -14 91 .02 21 17 | 10854 -6820 4885 9565
esa n/a| 0 -2 -1 -44 -12 -45 -.16 42 34 | -13279 -6043 4871 9727
gfz n/a| -2 0 1 49 7 3 .14 30 14 | 0 -6527 4970 9539
grg n/a| 0 -4 -4 6 12 32 .11 24 17 | -8002 -6443 4962 9103
iac n/a| -1 1 -4 27 -7 -40 -.27 21 18 | -6625 -2777 4889 9767
jgx n/a| -2 0 -2 -16 17 -143 -.22 32 29 | 13961 -6317 5141 9694
Table 2.2297.6 GPS week: 2297 Day: 6 MJD: 60329
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 1 -23 -1 79 .03 21 15 | 11585 2508 3380 7102
esa n/a| 0 1 0 -28 -10 -49 -.22 47 42 | -10079 2209 3385 7843
gfz n/a| 2 0 5 57 0 -1 .07 25 12 | 0 2414 3453 6781
grg n/a| 1 -2 -5 -19 13 71 .20 24 23 | -3156 2465 3448 6326
iac n/a| -1 0 -7 -39 27 -16 -.34 22 20 | -2240 482 3388 7137
jgx n/a| 0 1 -3 -31 20 -152 -.23 34 33 | 14508 2698 3410 6927
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 3.2297.0 GPS week: 2297 Day: 0 MJD: 60323
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1072 18 50 48 36 38 47 21 | 93 103 109 100 81 101 96
XR02 | 962 15 11 11 16 20 --- 7 | 56 56 57 64 55 --- 55
R03E | 1840 15 10 6 16 16 12 6 | 79 79 83 87 78 73 79
R04E | 1255 10 26 12 22 15 23 9 | 57 73 57 65 55 52 58
R05E | 786 10 9 13 12 17 24 7 | 106 105 101 100 104 98 101
R07E | 3295 14 12 11 18 30 15 7 | 117 117 118 120 113 115 116
R08E | 1716 15 19 10 16 19 17 7 | 42 42 44 51 43 33 41
R09 | 1310 13 12 15 18 21 20 8 | 41 42 43 41 43 38 39
XR11 | 4905 719 >>>> 504 3351 733 --- 602 | 63 9999 9999 9999 57 --- 611
R12 | 1414 20 9 16 18 11 22 8 | 55 51 59 50 54 46 51
R13 | 551 40 27 18 51 17 38 17 | 66 43 56 49 52 39 49
R14 | 1004 14 12 10 15 14 14 6 | 52 50 47 50 49 52 49
R15 | 1171 15 14 10 15 22 12 6 | 56 45 45 43 46 49 45
R16 | 686 20 15 10 13 20 15 7 | 55 50 47 50 49 44 48
XR17 | 1826 7 27 13 12 13 --- 9 | 82 63 86 92 82 --- 80
R18 | 1693 11 10 12 8 17 24 7 | 65 76 73 80 75 54 68
R19 | 2886 50 53 26 45 30 33 20 | 99 55 81 94 92 71 75
R20 | 2628 78 135 71 81 47 74 44 | 147 76 164 108 137 87 114
R21 | 806 18 20 12 21 20 23 9 | 91 69 92 89 89 68 81
R22 | 2153 14 11 8 16 14 13 6 | 43 47 44 47 39 35 42
R24 | 1217 25 39 13 24 19 23 12 | 105 70 100 105 96 76 91
XR25 | 9186 8 12 --- --- 17 --- 10 | 53 35 --- --- 49 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 1704 28 40 24 30 23 29 |T 73 64 75 74 69 62 92
WRMS | 1704 23 25 13 26 20 29 |NE 70 55 71 68 66 54 96
MEDI | 1310 15 14 12 18 19 22 |MD 63 56 59 65 55 52 58
Table 3.2297.1 GPS week: 2297 Day: 1 MJD: 60324
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1591 19 43 44 23 38 29 16 | 84 92 99 76 74 83 84
XR02 | 741 9 11 14 18 14 --- 7 | 54 49 52 53 56 --- 50
R03E | 963 8 14 13 12 17 7 5 | 61 57 63 65 63 57 60
R04E | 1903 15 18 14 18 23 12 7 | 62 62 54 56 57 57 56
R05E | 2048 10 13 13 19 12 10 6 | 94 96 91 84 93 90 90
R07E | 1256 10 14 14 14 25 12 6 | 81 84 84 82 86 77 81
R08E | 1241 20 16 13 25 17 30 10 | 44 47 45 40 45 40 41
R09 | 798 12 16 12 13 22 15 7 | 37 44 38 39 42 36 37
R12 | 1337 14 8 11 18 33 12 6 | 38 37 43 36 54 34 36
R13 | 1634 43 25 17 42 18 59 20 | 47 40 43 36 43 36 37
R14 | 706 5 10 7 15 15 13 5 | 42 40 43 36 44 47 42
R15 | 1784 15 16 16 9 18 22 8 | 43 39 47 40 32 37 40
R16 | 718 13 20 8 11 29 11 6 | 43 44 46 40 37 44 42
XR17 | 1305 10 28 12 20 14 --- 10 | 54 46 64 77 66 --- 59
R18 | 937 12 14 13 25 23 22 9 | 49 51 54 64 63 45 51
R19 | 3038 42 61 28 55 30 30 22 | 57 52 54 65 68 47 47
R20 | 4313 57 141 80 100 44 65 45 | 91 88 120 55 100 85 75
R21 | 1069 15 23 25 15 19 32 11 | 57 44 64 52 62 38 51
R22 | 2151 16 12 17 34 15 15 10 | 33 39 37 48 34 32 35
R24 | 1042 31 39 18 14 24 24 13 | 72 46 64 62 68 48 58
XR25 |11197 9 15 --- --- 23 --- 12 | 49 33 --- --- 42 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1814 24 41 26 33 25 28 |T 56 53 69 55 58 51 53
WRMS | 1814 24 20 14 24 22 28 |NE 51 46 68 50 54 44 47
MEDI | 1305 14 16 14 18 22 15 |MD 52 46 54 53 57 45 50
Table 3.2297.2 GPS week: 2297 Day: 2 MJD: 60325
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1630 31 34 34 21 43 31 15 | 50 64 60 46 45 61 51
XR02 | 510 12 10 14 18 21 --- 8 | 27 28 27 36 30 --- 26
R03E | 837 9 17 16 20 22 9 7 | 48 54 50 54 42 46 48
R04E | 2056 12 10 11 17 21 16 6 | 48 49 46 50 44 48 46
R05E | 1833 9 11 13 15 17 10 6 | 78 82 78 84 77 79 79
R07E | 943 15 13 16 17 21 11 7 | 67 79 83 86 63 68 76
R08E | 1045 28 16 17 17 16 22 10 | 42 43 46 43 40 39 41
R09 | 723 17 11 12 9 10 10 6 | 14 21 23 21 16 19 18
R12 | 1182 10 20 11 14 24 20 7 | 40 56 44 42 58 37 42
R13 | 3506 32 31 17 35 17 51 17 | 48 31 46 31 42 46 37
R14 | 868 12 9 12 14 12 10 5 | 36 28 25 38 37 34 30
R15 | 1630 25 12 17 15 13 16 9 | 41 31 28 35 28 20 27
R16 | 849 21 10 16 13 16 9 7 | 41 32 27 39 30 29 31
XR17 | 904 9 32 15 19 14 --- 11 | 60 48 65 67 66 --- 58
R18 | 1190 9 10 12 27 25 21 8 | 49 51 52 73 68 41 52
R19 | 1222 37 60 27 46 22 33 20 | 75 48 69 82 58 54 61
R20 | 5479 26 169 45 75 24 78 33 | 91 76 112 115 91 86 100
R21 | 1402 26 22 8 21 24 18 9 | 66 49 56 47 59 46 51
R22 | 1543 24 19 14 32 27 14 10 | 37 56 44 63 47 37 43
R24 | 662 12 29 27 27 11 32 13 | 62 53 78 70 63 65 63
XR25 | 9545 14 16 --- --- 26 --- 15 | 56 57 --- --- 40 --- 52
------+-----------------------------------------+-------------------------------------
RMS | 1958 22 46 20 28 22 29 |T 50 49 56 56 48 47 49
WRMS | 1958 20 20 16 24 20 24 |NE 48 44 54 54 47 42 46
MEDI | 1190 15 16 15 18 21 16 |MD 48 49 50 47 44 46 48
Table 3.2297.3 GPS week: 2297 Day: 3 MJD: 60326
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1703 25 46 46 28 37 43 19 | 73 76 94 73 68 64 71
XR02 | 780 12 10 11 11 16 --- 6 | 31 35 39 42 31 --- 34
R03E | 1049 14 17 11 15 15 12 7 | 51 49 52 57 52 50 49
R04E | 1555 12 12 15 17 17 16 7 | 47 45 35 49 38 43 41
R05E | 1469 12 11 11 18 18 19 7 | 66 71 69 67 62 69 67
R07E | 1124 9 15 15 14 21 15 7 | 62 58 62 55 57 62 58
R08E | 1065 17 18 10 18 27 20 8 | 69 67 65 70 71 63 65
R09 | 495 17 8 15 16 15 13 7 | 25 16 27 15 26 25 18
XR11 | 2242 9 328 11 3981 25 --- 10 | 24 381 64 9999 31 --- 84
R12 | 540 7 11 17 10 17 23 7 | 34 40 44 37 43 28 36
R13 | 4240 41 27 21 40 24 73 21 | 58 36 55 48 57 42 46
R14 | 1000 7 9 11 21 17 23 7 | 30 27 30 26 31 43 28
R15 | 1019 41 13 16 63 28 16 17 | 41 27 39 61 31 25 26
R16 | 773 19 9 20 17 20 18 8 | 42 39 35 41 43 26 34
XR17 | 638 8 28 17 18 19 --- 10 | 71 57 82 73 75 --- 69
R18 | 705 19 12 19 28 24 27 10 | 53 66 73 82 79 52 63
R19 | 1349 38 56 23 39 30 31 19 | 91 43 70 86 74 64 69
R20 | 5067 52 120 80 98 64 79 43 | 117 59 136 138 129 64 92
R21 | 1467 13 28 40 14 20 31 13 | 66 50 96 74 72 52 67
R22 | 1708 15 12 10 24 9 10 7 | 35 40 40 37 31 34 35
R24 | 591 20 28 20 25 18 28 12 | 75 54 77 67 76 58 65
XR25 |11390 4 --- --- --- 37 --- 0 | 69 --- --- --- 61 --- 67
------+-----------------------------------------+-------------------------------------
RMS | 1908 24 36 28 35 26 33 |T 55 63 61 59 56 48 53
WRMS | 1908 23 22 20 27 21 26 |NE 53 64 60 59 55 42 52
MEDI | 1065 14 15 16 18 20 20 |MD 53 49 62 57 57 50 58
Table 3.2297.4 GPS week: 2297 Day: 4 MJD: 60327
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1403 16 57 38 29 39 40 18 | 71 64 86 67 59 71 68
XR02 | 822 10 14 12 11 17 --- 6 | 51 53 60 52 46 --- 52
R03E | 3099 12 15 13 18 13 12 7 | 65 63 72 63 64 62 64
R04E | 1567 11 16 11 20 21 13 7 | 44 51 48 47 40 45 44
R05E | 1086 10 14 19 22 24 15 8 | 98 98 86 91 94 89 91
R07E | 2383 13 15 12 15 14 13 6 | 89 89 90 82 86 83 86
R08E | 1483 18 23 18 17 14 18 9 | 53 43 53 53 48 45 48
R09 | 562 10 10 10 16 16 15 6 | 40 38 43 39 40 33 38
XR11 | 1156 14 11 20 30 15 --- 11 | 49 283 61 441 61 --- 72
R12 | 624 12 16 11 13 17 16 6 | 48 42 46 46 47 44 44
R13 | 3809 34 22 17 63 30 72 22 | 57 47 49 42 45 55 50
R14 | 1353 12 11 12 15 13 13 6 | 42 55 57 44 47 52 48
R15 | 887 10 9 29 20 15 24 10 | 49 55 67 43 54 51 51
R16 | 674 13 21 15 17 11 30 9 | 46 49 52 51 47 37 44
XR17 | 487 10 17 11 21 13 --- 8 | 67 56 55 66 58 --- 59
R18 | 886 7 22 17 25 26 19 8 | 57 64 57 67 67 49 55
R19 | 861 21 90 39 66 36 31 24 | 92 52 111 96 89 85 85
R20 | 2906 52 119 54 57 52 68 34 | 107 57 103 104 110 60 80
R21 | 613 13 25 14 14 11 23 8 | 68 55 70 69 66 57 64
R22 | 1910 13 17 13 30 12 15 8 | 35 38 42 54 37 37 35
R24 | 413 12 33 16 24 18 27 11 | 73 59 75 77 64 56 68
XR25 | 9935 5 --- --- --- 44 --- 0 | 50 --- --- --- 40 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1757 19 41 23 31 24 31 |T 61 67 65 80 59 56 58
WRMS | 1757 17 27 18 21 19 28 |NE 58 66 63 86 57 51 55
MEDI | 1086 12 17 15 20 16 18 |MD 53 55 60 63 54 52 52
Table 3.2297.5 GPS week: 2297 Day: 5 MJD: 60328
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1233 31 49 45 24 42 30 18 | 82 87 99 87 90 75 82
XR02 | 1035 10 12 13 17 11 --- 7 | 31 29 32 38 25 --- 30
R03E | 2571 9 15 12 13 12 13 6 | 59 55 61 64 60 53 58
R04E | 1280 14 20 12 18 12 19 8 | 49 50 39 45 40 45 43
R05E | 803 10 11 18 23 17 19 8 | 72 73 66 75 69 74 70
R07E | 2063 9 21 11 16 12 17 7 | 83 93 84 89 84 80 85
R08E | 2019 12 21 10 19 12 21 8 | 42 44 43 52 42 36 42
R09 | 1401 10 10 10 18 25 17 6 | 22 21 28 18 20 27 19
R11 | 1202 17 14 14 26 16 18 9 | 30 397 43 204 32 16 24
R12 | 817 11 11 18 8 14 26 8 | 28 21 31 28 24 23 24
R13 | 2664 37 31 19 52 25 76 23 | 39 39 37 24 24 22 27
R14 | 754 7 10 18 14 16 13 6 | 36 41 49 40 37 46 40
R15 | 937 7 8 14 17 13 13 6 | 33 44 46 32 47 50 39
R16 | 715 12 14 18 11 15 24 8 | 36 46 52 37 40 30 38
XR17 | 507 15 17 13 17 14 --- 9 | 43 34 32 37 29 --- 35
R18 | 831 10 19 9 21 21 17 7 | 34 39 34 40 47 40 35
R19 | 1016 35 82 41 38 41 45 24 | 79 33 90 78 62 54 66
R20 | 1601 48 139 98 39 31 67 40 | 82 39 117 59 72 81 63
R21 | 585 12 19 22 14 12 29 10 | 49 41 55 50 41 32 45
R22 | 2176 21 23 17 31 11 20 11 | 19 33 21 42 19 21 22
R24 | 1249 21 29 17 18 21 28 11 | 50 44 51 50 39 40 46
XR25 |11134 8 16 --- --- 16 --- 12 | 38 32 --- --- 37 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1501 21 42 30 24 21 32 |T 47 60 52 56 44 44 44
WRMS | 1501 17 34 14 17 18 29 |NE 40 58 47 51 37 37 36
MEDI | 1202 12 17 17 18 15 20 |MD 39 41 46 45 40 40 39
Table 3.2297.6 GPS week: 2297 Day: 6 MJD: 60329
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1471 24 56 43 15 33 36 18 | 82 94 108 87 79 75 85
XR02 | 687 8 14 11 10 16 --- 6 | 40 36 41 48 35 --- 39
R03E | 2161 8 11 13 17 18 21 7 | 75 71 77 86 74 69 75
R04E | 1298 12 16 13 11 14 19 7 | 41 39 44 47 38 36 40
R05E | 1102 9 11 14 22 12 11 7 | 78 75 78 79 78 72 75
R07E | 1362 12 18 16 17 26 11 7 | 103 113 105 112 100 106 106
R08E | 2371 10 20 11 17 23 15 7 | 45 58 43 52 45 46 46
R09 | 1205 17 16 12 9 19 22 7 | 25 26 24 25 30 26 22
R11 | 1796 11 11 11 23 13 20 7 | 38 378 52 357 42 11 58
R12 | 737 12 9 7 20 16 18 6 | 40 38 41 31 44 36 36
R13 | 1530 17 26 11 47 19 46 15 | 55 42 49 49 51 36 45
R14 | 982 9 14 14 14 19 20 7 | 45 47 52 41 50 49 45
R15 | 536 19 12 6 14 23 33 9 | 49 41 42 41 50 37 40
R16 | 759 20 9 19 14 15 19 8 | 50 43 46 41 48 46 43
XR17 | 729 11 16 12 20 19 --- 8 | 75 61 77 75 70 --- 71
R18 | 806 6 21 11 18 23 21 8 | 57 69 63 72 69 51 61
R19 | 1063 53 64 32 41 40 48 24 | 112 46 104 103 97 78 88
R20 | 1513 46 175 77 52 34 96 39 | 144 39 159 124 132 71 119
R21 | 542 13 28 25 15 16 33 11 | 86 56 93 83 77 54 76
R22 | 2114 17 13 15 14 14 16 7 | 34 34 26 34 27 31 29
R24 | 1790 12 24 14 20 24 25 9 | 94 67 95 92 84 67 84
XR25 |11632 11 18 --- --- 26 --- 15 | 45 29 --- --- 37 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 1426 21 47 25 24 22 34 |T 64 68 67 79 61 52 60
WRMS | 1426 15 42 12 23 20 33 |NE 61 65 64 81 58 45 56
MEDI | 1205 12 16 13 17 19 21 |MD 50 46 52 72 50 49 46
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