[IGSREPORT-29658] Wk 2292 IGLOS Final Orbits
acc
acc at igs.org
Mon Jan 1 11:39:46 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2292 (Dec 10, 2023 - Dec 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 2.2292.
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:
igl2292[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2292 in the SP3 format.
igl22927.sum Combination Report for GPS Week 2292.
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 | -8.2 ns
1 | -7.1 ns
2 | -11.4 ns
3 | -14.6 ns
4 | -0.9 ns
5 | -12.0 ns
6 | -14.3 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 1.2292, 1a.2292).
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 2.2292.0-6)
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 3.2292.0-6).
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 2292 summary. (Dec 10, 2023 - Dec 16, 2023)
Table 1.2292.a GPS week : 2292 MJD: 60288.0-60294.0
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 -3 -19 -18 51 .14 24 20 | 20873 101 3312 15696
| 1 0 1 8 17 26 .04 | 6423 2133
esa n/a| 0 0 -2 -21 6 6 -.12 35 22 | -12177 -652 3326 16486
| 1 0 1 12 13 33 .03 | 6892 2208
gfz n/a| 1 1 -2 5 7 -13 -.05 22 15 | 0 311 3314 15469
| 1 1 1 10 15 26 .03 | 0 2178
grg n/a| 1 -4 2 4 0 10 .29 35 25 | -12171 151 3321 15218
| 0 0 1 10 15 34 .05 | 6191 2145
iac n/a| -1 -1 -7 -6 22 -70 -.10 24 20 | -9603 -206 3317 15758
| 1 2 2 19 25 30 .03 | 5955 1912
jgx n/a| 0 1 8 28 2 -54 -.18 25 25 | 24701 260 3244 7411
| 0 1 2 20 23 45 .06 | 5329 2419
Table 1.2292.b GPS week : 2292 MJD: 60288.0-60294.0
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 19 17 19 14 16 21 |
R02 | 8 8 8 7 9 7 8 |
R03 | 8 9 7 13 9 10 10 |
R04 | 9 14 12 9 7 8 11 |
R05 | 8 8 9 7 8 7 7 |
R07 | 8 11 9 11 9 11 7 |
R08 | 9 8 10 9 7 7 13 |
R09 | 8 7 8 9 7 8 8 |
R11 | 6 7 8 8 8 6 8 |
R12 | 7 7 8 9 10 8 9 |
R13 | 23 22 16 17 18 19 18 |
R14 | 6 8 8 7 6 7 7 |
R15 | 9 9 9 9 8 9 9 |
R16 | 9 10 10 10 8 8 9 |
R17 | 7 7 8 9 9 10 8 |
R18 | 6 10 7 8 9 10 9 |
R19 | 23 28 24 25 30 22 24 |
R20 | 35 32 30 40 36 37 42 |
R21 | 7 9 8 7 8 9 8 |
R22 | 8 7 8 8 8 10 7 |
R24 | 7 10 12 10 11 8 9 |
R25 | --- --- --- --- --- 0 16 |
R26 | --- --- --- --- --- 0 26 |
Table 1.2292.c GPS week : 2292 MJD: 60288.0-60294.0
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 2292 0 | 22 -1 -153 -98 -180 1792 82.1 1297 1297 | -8158 0
brd 2292 1 | 38 0 -208 265 -1700 -1970 81.1 1230 1230 | -7094 0
brd 2292 2 | -25 -51 -9 -1548 71 -5499 80.9 1315 1315 | -11410 0
brd 2292 3 | -13 -88 -184 -131 1375 -4741 80.3 1556 1556 | -14615 0
brd 2292 4 | 105 23 -67 -237 2432 -5637 81.2 1816 1816 | -950 0
brd 2292 5 | 0 90 -111 -52 1869 964 78.4 2188 2188 | -11987 0
brd 2292 6 | -36 -36 -5 1131 -515 -3236 81.2 1501 1501 | -14261 0
-------------+------------------------------------------------------------+----------------
brd 2292 mean| 13 -9 -105 -95 478 -2618 80.7 1557 1557 | -9782 0
brd 2292 sdev| 48 57 81 792 1465 3027 1.2 341 341 | 4809 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 2.2292.0 GPS week: 2292 Day: 0 MJD: 60288
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 -1 -23 -20 39 .19 23 19 | 19223 2831 3667 6399
esa n/a| 0 0 0 -33 0 -10 -.09 33 25 | -9591 2826 3654 6468
gfz n/a| 0 1 -4 18 6 27 -.07 18 11 | 0 3176 3603 6287
grg n/a| 2 -4 1 4 6 36 .31 35 24 | -10211 2999 3681 6060
iac n/a| -4 0 -6 -7 19 -55 -.09 21 20 | -9964 3215 3653 6696
jgx n/a| 1 2 9 18 -21 -78 -.13 26 26 | 20112 3518 3693 6492
Table 2.2292.1 GPS week: 2292 Day: 1 MJD: 60289
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 -3 -21 -25 57 .08 21 18 | 17515 2587 3708 33846
esa n/a| 1 0 -4 -3 30 -18 -.13 34 24 | -20988 1030 3854 36608
gfz n/a| 0 1 -2 -7 -19 -3 -.10 25 20 | 0 3116 3717 33749
grg n/a| 1 -5 3 -3 9 38 .25 31 26 | -15232 2914 3703 33730
iac n/a| -2 0 -12 16 49 -88 -.12 24 21 | -10776 236 3699 33533
jgx n/a| 0 3 9 35 -2 -75 -.08 30 30 | 25899 3071 2912 7196
Table 2.2292.2 GPS week: 2292 Day: 2 MJD: 60290
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 -3 -23 -31 70 .15 23 20 | 14114 333 3011 38693
esa n/a| 2 0 -4 -32 12 58 -.15 31 21 | -21619 95 3007 38718
gfz n/a| 2 0 -2 4 27 -49 -.01 22 17 | 0 21 2993 38331
grg n/a| 1 -4 5 1 -2 -52 .25 31 24 | -19946 200 3039 38715
iac n/a| -1 0 -8 13 32 -46 -.12 27 25 | -17147 898 3009 38129
jgx n/a| -1 1 4 28 8 -61 -.20 23 23 | 24430 -71 3044 7335
Table 2.2292.3 GPS week: 2292 Day: 3 MJD: 60291
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 -32 -41 71 .14 26 19 | 19183 -1500 3513 8071
esa n/a| -3 0 -2 -11 14 32 -.09 31 22 | -11920 -2673 3486 8611
gfz n/a| 2 5 -4 -7 2 -30 -.05 32 19 | 0 -989 3495 8209
grg n/a| 1 -5 3 23 23 34 .22 32 31 | -14137 -1281 3461 7498
iac n/a| 0 -4 -3 -6 1 -19 -.13 29 22 | -11083 -2231 3478 8388
jgx n/a| 0 0 5 3 45 -84 -.21 24 24 | 20732 -910 3608 8294
Table 2.2292.4 GPS week: 2292 Day: 4 MJD: 60292
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 -5 -6 -5 60 .09 24 22 | 34449 -2233 2673 7076
esa n/a| 0 0 -4 -35 0 9 -.15 39 21 | -2455 -1884 2668 9609
gfz n/a| 1 0 -4 12 18 4 -.06 20 13 | 0 -2147 2671 7012
grg n/a| 1 -3 1 3 -22 0 .37 38 27 | 111 -2233 2666 6601
iac n/a| -1 -2 -7 0 0 -89 -.04 28 20 | 2630 -2197 2675 7492
jgx n/a| 0 0 11 9 10 -100 -.15 24 24 | 35903 -2732 2643 6921
Table 2.2292.5 GPS week: 2292 Day: 5 MJD: 60293
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 2 -3 -11 -20 64 .15 22 20 | 21426 841 3231 7533
esa n/a| 1 1 0 -14 -11 -41 -.12 35 19 | -8693 -455 3236 7542
gfz n/a| 1 0 -2 15 21 -9 -.06 17 12 | 0 782 3246 7303
grg n/a| 3 -4 2 9 -17 -12 .33 40 24 | -12339 335 3230 6922
iac n/a| 0 -2 -9 -41 -7 -101 -.07 20 17 | -9687 -290 3243 8028
jgx n/a| -1 0 7 34 -3 0 -.21 22 22 | 22591 1041 3258 7667
Table 2.2292.6 GPS week: 2292 Day: 6 MJD: 60294
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 1 -4 -18 12 -2 .16 27 20 | 20207 -2152 3387 8254
esa n/a| 2 0 -2 -16 0 14 -.12 39 25 | -9977 -3507 3383 7852
gfz n/a| 0 1 0 4 -2 -35 -.03 19 11 | 0 -1779 3479 7393
grg n/a| 0 -5 1 -7 1 28 .30 38 23 | -13446 -1873 3469 7002
iac n/a| 0 1 -5 -20 59 -92 -.13 21 18 | -11197 -1073 3463 8046
jgx n/a| 0 2 9 65 -22 19 -.28 25 25 | 23240 -2097 3552 7972
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 3.2292.0 GPS week: 2292 Day: 0 MJD: 60288
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 800 35 27 19 31 17 37 14 | 92 47 77 54 65 41 63
R02 | 937 7 11 16 13 28 23 7 | 72 80 74 72 59 58 70
R03 | 695 14 14 8 22 16 21 7 | 128 113 120 131 122 109 119
R04 | 463 22 11 8 31 10 15 8 | 134 127 127 118 128 93 125
R05 | 1129 12 13 14 20 19 17 7 | 227 228 230 229 225 220 227
R07 | 1198 19 21 10 11 17 19 8 | 121 104 115 115 119 102 111
R08 | 1901 8 11 11 33 20 21 8 | 130 128 131 140 139 124 129
R09 | 832 18 17 13 14 15 16 8 | 40 41 43 38 34 36 38
R11 | 1592 12 6 10 17 16 13 6 | 19 26 23 21 25 22 20
R12M | 1192 14 13 11 12 18 17 6 | 72 72 73 64 66 62 68
R13M | 863 53 18 24 54 21 68 22 | 105 91 109 86 96 35 98
R14 | 1145 7 12 8 18 19 16 6 | 61 67 61 60 65 50 59
R15 | 867 20 9 17 15 26 23 9 | 90 76 69 74 84 68 74
R16 | 850 22 17 7 22 11 24 9 | 101 84 85 80 91 76 84
XR17 | 809 12 13 8 17 28 --- 7 | 39 35 39 42 35 --- 37
R18 | 788 9 18 11 13 17 8 6 | 28 34 29 33 28 23 27
R19 | 1003 35 65 14 80 40 32 22 | 51 39 46 56 52 52 45
R20 | 3005 39 114 58 86 33 43 35 | 74 53 100 87 64 77 76
R21 | 1800 9 18 5 23 16 14 6 | 47 40 45 50 48 45 44
R22 | 1584 13 14 12 27 12 9 7 | 43 48 48 52 46 48 46
R24 | 712 19 13 12 13 19 11 7 | 38 33 42 52 41 35 38
------+-----------------------------------------+-------------------------------------
RMS | 1297 23 33 18 35 21 26 |T 81 74 80 78 79 68 76
WRMS | 1297 19 25 11 24 20 26 |NE 80 73 79 79 78 71 75
MEDI | 937 14 14 11 20 18 17 |MD 72 67 73 64 65 52 68
Table 3.2292.1 GPS week: 2292 Day: 1 MJD: 60289
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 709 43 31 24 35 26 45 18 | 58 38 44 39 51 34 39
R02 | 823 6 17 19 14 23 18 7 | 52 64 61 51 49 46 54
R03 | 1180 11 16 24 15 17 19 8 | 90 80 87 93 79 84 85
XR04 | 448 28 23 13 29 17 --- 14 | 115 111 96 100 104 --- 104
R05 | 859 16 6 10 25 15 14 7 | 186 181 184 183 187 178 182
R07 | 1234 15 17 28 18 20 24 10 | 109 100 107 100 106 91 101
R08 | 1089 16 13 21 8 17 13 7 | 109 115 122 117 114 112 113
R09 | 1232 12 17 15 11 14 14 7 | 36 41 38 33 36 41 36
R11 | 1770 10 8 13 16 25 17 6 | 15 23 28 17 20 21 16
R12M | 1096 7 10 14 15 21 20 6 | 63 62 66 68 60 57 62
R13M | 712 33 23 38 37 22 76 22 | 71 56 93 68 71 26 67
R14 | 1228 15 14 14 14 17 23 8 | 51 51 39 43 52 33 43
R15 | 911 17 13 16 18 25 19 8 | 66 57 64 47 73 53 57
R16 | 1346 20 21 14 24 24 19 9 | 79 67 74 68 80 63 70
XR17 | 610 9 14 10 12 20 --- 6 | 24 25 24 31 22 --- 24
R18 | 1085 13 21 18 21 19 22 9 | 23 20 24 31 17 22 19
R19 | 1159 41 79 42 69 32 48 28 | 35 28 42 27 26 37 27
R20 | 1978 29 104 54 77 49 47 32 | 36 33 45 41 35 59 37
R21 | 1458 11 21 22 14 18 13 8 | 24 19 32 26 23 22 22
R22 | 1561 11 12 20 13 21 12 7 | 42 38 57 43 44 44 43
R24 | 1099 12 19 15 31 19 16 9 | 25 31 27 31 16 22 24
------+-----------------------------------------+-------------------------------------
RMS | 1230 21 34 25 31 24 30 |T 62 59 64 59 59 55 58
WRMS | 1230 18 24 20 26 21 30 |NE 61 59 62 59 58 56 57
MEDI | 1099 15 17 18 18 20 19 |MD 52 51 57 43 51 44 43
Table 3.2292.2 GPS week: 2292 Day: 2 MJD: 60290
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 685 37 36 35 28 15 34 17 | 62 26 69 45 53 32 46
R02 | 914 9 19 18 16 13 16 8 | 54 59 38 59 50 40 47
R03 | 1428 15 10 8 12 18 16 6 | 125 121 118 120 113 116 119
XR04 | 1034 16 13 22 31 15 --- 12 | 104 98 114 97 101 --- 102
R05 | 1055 19 12 22 23 20 11 9 | 217 225 225 231 223 224 223
R07 | 738 15 13 22 20 15 17 9 | 113 100 110 100 106 96 103
R08 | 1254 12 13 31 20 12 20 10 | 130 132 137 125 132 126 129
R09 | 1708 11 15 21 14 17 9 7 | 29 35 38 30 26 27 29
R11 | 1857 12 20 15 14 17 13 7 | 13 25 28 27 21 18 17
R12M | 1531 14 17 15 21 19 16 8 | 54 65 59 42 47 53 53
R13M | 1534 24 20 27 51 23 29 15 | 121 112 112 129 128 42 121
R14 | 1608 13 16 7 15 22 20 7 | 49 62 52 56 58 43 51
R15 | 1708 21 18 13 8 24 23 9 | 71 69 64 56 74 51 61
R16 | 1113 25 20 16 16 43 17 9 | 74 72 55 55 92 60 62
XR17 | 659 15 6 16 12 13 --- 8 | 31 28 30 28 29 --- 26
R18 | 784 11 22 10 15 22 13 7 | 26 28 29 28 28 25 25
R19 | 1502 46 58 19 77 37 31 24 | 39 33 57 37 29 30 34
R20 | 1842 48 93 52 56 74 51 30 | 55 50 72 56 50 95 60
R21 | 974 9 19 12 17 19 17 7 | 34 35 35 35 34 33 32
R22 | 973 16 16 17 16 13 12 8 | 29 45 33 45 40 42 37
R24 | 547 14 27 16 43 17 20 12 | 29 28 32 42 30 25 27
------+-----------------------------------------+-------------------------------------
RMS | 1315 23 31 22 31 27 23 |T 69 68 71 68 70 62 66
WRMS | 1315 20 21 17 24 25 23 |NE 67 66 70 66 69 63 64
MEDI | 1113 15 18 17 17 18 17 |MD 54 59 57 55 50 42 51
Table 3.2292.3 GPS week: 2292 Day: 3 MJD: 60291
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 691 48 39 28 34 15 36 19 | 79 42 65 45 51 35 46
R02 | 1035 10 16 14 17 19 13 7 | 56 63 58 49 45 47 53
R03 | 1133 15 24 34 34 19 23 13 | 119 114 144 119 124 102 117
XR04 | 1109 10 19 19 11 26 --- 8 | 84 87 83 84 75 --- 83
R05 | 1444 11 13 14 20 30 14 7 | 110 113 114 111 90 117 112
R07 | 685 21 17 20 32 22 15 10 | 99 94 95 85 100 91 91
R08 | 633 15 15 24 19 26 13 8 | 90 99 113 82 97 90 93
R09 | 1922 17 16 27 13 11 15 9 | 26 25 34 21 21 21 20
R11 | 1827 12 21 19 8 12 13 7 | 16 24 22 17 18 18 15
R12M | 1978 16 21 13 23 22 13 8 | 103 106 99 100 105 95 100
R13M | 931 30 19 32 48 26 34 17 | 187 186 183 188 188 112 186
R14 | 1169 11 13 17 11 16 12 6 | 53 58 39 51 53 44 48
R15 | 1595 19 12 14 19 21 20 8 | 61 55 51 65 47 50 54
R16 | 566 21 20 17 11 19 24 10 | 70 72 75 58 69 48 63
XR17 | 1194 10 17 17 19 22 --- 9 | 31 28 34 41 32 --- 31
R18 | 718 11 21 16 13 26 13 7 | 25 26 28 30 28 24 24
R19 | 1995 50 60 26 64 48 41 24 | 43 48 49 51 41 34 41
R20 | 4068 63 94 105 79 82 62 40 | 47 65 117 63 46 95 64
R21 | 1054 8 19 18 14 16 8 7 | 37 32 44 38 43 40 36
R22 | 845 15 15 18 18 14 8 7 | 18 26 31 38 30 23 24
R24 | 1125 19 18 15 28 21 16 9 | 41 31 34 44 39 31 35
------+-----------------------------------------+-------------------------------------
RMS | 1555 26 31 32 32 29 24 |T 66 66 72 65 70 58 63
WRMS | 1555 19 22 19 31 22 24 |NE 58 58 64 57 62 53 55
MEDI | 1125 15 19 18 19 21 15 |MD 56 58 58 51 47 47 53
Table 3.2292.4 GPS week: 2292 Day: 4 MJD: 60292
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 473 34 26 21 37 16 23 14 | 66 49 60 40 55 43 49
R02 | 1017 13 16 13 25 17 17 8 | 48 55 53 41 46 42 46
R03 | 1377 14 15 10 26 19 22 8 | 164 165 163 173 161 156 162
XR04 | 1147 8 14 9 16 39 --- 6 | 106 107 111 116 108 --- 108
R05 | 2552 15 15 10 24 19 12 7 | 212 220 223 217 219 209 215
R07 | 994 19 18 14 13 23 19 8 | 129 111 116 119 111 114 117
R08 | 896 10 10 12 15 18 16 6 | 153 155 145 153 159 154 151
R09 | 1605 13 19 10 18 24 10 6 | 25 33 30 27 28 24 25
R11 | 1433 11 25 16 13 12 8 7 | 18 36 21 21 21 18 18
R12M | 2035 19 18 14 33 20 19 10 | 197 194 192 186 195 196 192
R13M | 723 33 10 28 57 49 40 17 | 299 304 305 286 292 288 290
R14 | 618 10 13 8 18 11 11 6 | 58 65 61 49 59 54 57
R15 | 1648 17 16 10 11 22 18 7 | 76 61 71 69 57 54 66
R16 | 965 19 20 5 12 20 16 7 | 84 79 73 79 78 67 75
XR17 | 620 8 18 11 26 10 --- 9 | 29 24 35 37 27 --- 28
R18 | 609 14 24 9 14 15 25 9 | 28 26 25 29 30 25 24
R19 | 2752 59 76 40 80 26 57 30 | 26 66 48 49 34 33 34
R20 | 5007 51 132 49 101 81 31 36 | 54 120 89 49 36 76 72
R21 | 1546 10 26 18 14 20 12 8 | 28 25 27 29 30 26 24
R22 | 1158 13 16 15 26 11 9 8 | 42 48 52 48 50 48 47
R24 | 1049 15 22 18 25 16 26 10 | 26 22 32 30 25 23 23
------+-----------------------------------------+-------------------------------------
RMS | 1815 24 39 20 38 28 24 |T 88 93 92 87 91 86 86
WRMS | 1815 22 21 13 27 20 24 |NE 72 77 75 72 75 68 70
MEDI | 1147 14 18 13 24 19 18 |MD 58 65 61 49 55 54 57
Table 3.2292.5 GPS week: 2292 Day: 5 MJD: 60293
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 555 44 27 14 29 22 34 15 | 65 42 41 41 51 44 42
R02 | 957 11 18 6 14 13 16 6 | 49 53 42 53 56 36 44
R03 | 1100 14 13 18 18 13 26 9 | 86 81 96 85 88 79 85
R04 | 1020 19 10 9 15 23 17 7 | 68 59 62 58 50 54 60
R05 | 2787 12 9 9 26 17 11 6 | 165 171 171 182 164 173 171
R07 | 874 14 26 23 15 22 24 10 | 75 55 82 69 66 68 70
R08 | 935 9 12 15 8 17 21 7 | 80 80 85 85 81 79 81
R09 | 694 13 17 10 19 13 19 7 | 20 31 28 23 20 32 23
R11 | 1580 11 15 12 12 15 10 6 | 30 38 42 32 41 39 35
R12M | 1622 9 16 12 30 17 15 8 | 315 315 314 312 303 315 314
R13M | 2028 33 25 27 67 24 39 19 | 451 462 455 447 424 527 439
R14 | 655 10 21 11 14 14 11 6 | 53 62 49 47 45 47 50
R15 | 2629 25 13 17 11 19 11 8 | 67 56 43 52 52 49 51
R16 | 1063 19 19 10 12 20 17 7 | 65 51 57 60 61 50 55
XR17 | 854 14 16 21 12 12 --- 10 | 22 20 34 22 18 --- 21
R18 | 624 19 15 16 14 9 27 9 | 25 18 24 23 22 19 18
R19 | 4203 35 68 17 73 21 27 21 | 31 45 42 28 32 26 30
R20 | 6456 50 118 41 125 43 34 36 | 32 57 69 45 37 46 32
R21 | 1547 12 20 12 16 14 25 8 | 27 27 25 27 23 19 22
R22 | 1209 11 12 14 45 12 12 9 | 36 58 37 83 42 36 44
R24 | 1025 13 20 7 24 18 12 7 | 27 26 21 27 22 24 22
XR25 |17847 5 --- --- --- --- --- 0 | 322 --- --- --- --- --- 322
XR26 |13254 5 --- --- --- >>>> --- 0 | 14 --- --- --- 576 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 2187 22 35 17 40 20 22 |T 92 86 86 85 103 88 89
WRMS | 2187 20 19 12 24 17 22 |NE 64 54 55 54 77 51 61
MEDI | 1100 13 17 14 16 17 17 |MD 53 55 43 52 50 46 44
Table 3.2292.6 GPS week: 2292 Day: 6 MJD: 60294
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 759 48 44 38 36 22 45 21 | 83 29 73 39 47 27 47
R02 | 803 14 25 5 18 15 18 8 | 55 62 47 46 53 40 48
R03 | 1469 9 14 23 16 12 25 9 | 110 103 119 108 112 97 107
R04 | 1468 28 10 13 19 14 28 10 | 87 70 78 71 72 44 73
R05 | 2730 14 8 11 18 21 17 7 | 206 207 208 216 203 208 208
R07 | 949 15 18 7 13 17 16 7 | 82 74 80 74 82 67 75
R08 | 951 13 28 32 14 24 23 12 | 87 90 108 93 106 87 93
R09 | 1184 15 16 12 13 13 20 7 | 24 32 31 26 21 29 26
R11 | 1369 11 17 13 13 17 21 7 | 40 44 45 44 36 40 41
R12M | 1067 9 26 10 18 14 21 8 | 404 400 402 398 399 400 401
XR13M | 1998 31 36 16 42 19 --- 17 | 961 955 964 949 947 --- 954
R14 | 601 13 16 13 13 13 14 7 | 78 85 69 71 78 69 73
R15 | 2107 26 12 13 13 15 16 8 | 101 86 72 78 82 77 81
R16 | 1613 25 19 14 19 15 15 9 | 98 80 77 83 90 72 81
XR17 | 533 13 16 10 18 27 --- 8 | 30 31 32 35 31 --- 29
R18 | 946 13 17 11 16 22 29 9 | 22 23 21 23 22 21 19
R19 | 1791 41 71 14 74 33 42 24 | 38 35 35 45 33 24 30
R20 | 2806 77 131 47 127 46 35 42 | 89 72 82 64 46 60 56
R21 | 1090 12 16 10 24 12 16 7 | 34 27 30 36 33 30 29
R22 | 1603 12 17 8 21 19 16 7 | 45 55 46 67 53 49 49
R24 | 654 17 20 8 25 24 20 9 | 44 28 34 41 38 29 33
XR25 |14718 14 17 --- --- --- --- 15 | 183 13 --- --- --- --- 183
XR26 |17624 31 --- 20 --- --- --- 25 | 13 --- 21 --- --- --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1500 27 39 19 38 21 25 |T 126 118 121 124 123 77 120
WRMS | 1500 20 25 11 23 18 25 |NE 73 62 65 66 65 59 66
MEDI | 1369 14 17 13 18 17 20 |MD 82 62 69 67 53 49 56
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