[IGSREPORT-29912] Wk 2315 IGLOS Final Orbits
acc
acc at igs.org
Fri Jun 7 04:02:29 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2315 (May 19, 2024 - May 25, 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 2.2315.
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:
igl2315[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2315 in the SP3 format.
igl23157.sum Combination Report for GPS Week 2315.
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).
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 | 4.0 ns
1 | -7.4 ns
2 | -15.4 ns
3 | 5.4 ns
4 | 2.3 ns
5 | 3.4 ns
6 | 4.5 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 | ALL | R08
2 | ALL | R08
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 1.2315, 1a.2315).
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 2.2315.0-6)
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 3.2315.0-6).
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 2315 summary. (May 19, 2024 - May 25, 2024)
Table 1.2315.a GPS week : 2315 MJD: 60449.0-60455.0
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 1 -8 -2 19 .17 20 16 | 3348 -34 4012 22448
| 1 0 1 13 8 27 .04 | 10648 2347
esa n/a| -1 -1 0 -9 -1 -1 -.08 38 24 | -1889 644 3006 7058
| 1 1 1 11 19 30 .04 | 5586 1858
gfz n/a| 1 0 6 9 10 -22 -.07 19 15 | 0 -481 3055 6603
| 0 0 2 20 18 23 .04 | 0 2118
grg n/a| 3 0 -2 -19 6 26 .43 30 24 | 3372 -466 4062 22386
| 1 0 1 29 20 41 .05 | 11125 2405
iac n/a| 0 0 -2 9 -12 -4 -.13 19 17 | 5023 -16 4051 23396
| 1 1 2 23 24 25 .06 | 10992 1800
jgx n/a| 0 0 -8 6 30 -20 -.17 29 29 | 1153 -577 3069 6470
| 0 1 1 25 16 37 .02 | 7514 2138
Table 1.2315.b GPS week : 2315 MJD: 60449.0-60455.0
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 | 17 18 15 15 14 16 15 |
R02 | 10 7 7 5 5 6 8 |
R03 | 9 6 6 7 6 6 6 |
R04 | 9 9 7 7 7 7 7 |
R05 | 8 8 6 6 7 6 7 |
R07 | 8 6 6 7 9 9 7 |
R08 | 14 --- --- 20 9 9 9 |
R09 | 10 9 7 8 9 8 8 |
R11 | 8 8 7 9 8 7 8 |
R12 | 6 7 7 6 6 9 9 |
R13 | 18 12 15 14 15 19 17 |
R14 | 7 7 6 6 5 5 6 |
R15 | 8 6 7 7 7 5 7 |
R16 | 8 8 7 7 10 9 8 |
R17 | 6 6 6 6 6 6 8 |
R18 | 8 5 8 9 8 7 6 |
R19 | 18 19 20 18 17 21 21 |
R20 | 27 26 25 27 31 23 25 |
R21 | 8 8 8 9 6 7 6 |
R22 | 6 6 5 7 6 5 7 |
R24 | 8 8 8 7 10 9 7 |
R25 | 9 13 9 8 8 9 10 |
R26 | 32 0 --- 76 39 35 31 |
Table 1.2315.c GPS week : 2315 MJD: 60449.0-60455.0
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 2315 0 | 111 -13 230 -815 342 -1247 81.5 1837 1837 | 3968 0
brd 2315 1 | -14 -10 294 2 -710 -6460 81.8 1686 1686 | -7376 0
brd 2315 2 | -6 98 277 431 99 -5885 81.7 1378 1378 | -15400 0
brd 2315 3 | -60 -29 291 -436 1441 1214 81.9 1178 1178 | 5419 0
brd 2315 4 | 90 -3 284 -1655 12 6734 81.4 1358 1358 | 2330 0
brd 2315 5 | -41 55 171 -729 1319 8287 81.9 1539 1539 | 3363 0
brd 2315 6 | 16 35 233 1201 3546 409 80.7 1746 1746 | 4486 0
-------------+------------------------------------------------------------+----------------
brd 2315 mean| 13 18 254 -285 864 436 81.6 1531 1531 | -458 0
brd 2315 sdev| 65 45 45 929 1402 5660 .4 238 238 | 7874 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 2.2315.0 GPS week: 2315 Day: 0 MJD: 60449
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 -1 0 11 11 -1 .19 21 15 | 18922 2614 8163 79328
esa n/a| 0 -1 -1 -16 41 -31 -.12 41 27 | -4290 627 3115 7133
gfz n/a| 1 0 6 -6 1 -59 -.11 21 17 | 0 -1016 3100 6289
grg n/a| 4 0 -3 -40 23 93 .54 28 30 | 19091 1930 8442 80979
iac n/a| -1 0 -3 -2 -45 32 -.24 22 22 | 20440 2683 8282 81205
jgx n/a| 0 1 -8 28 43 23 -.16 30 27 | 5548 -1424 3134 5662
Table 2.2315.1 GPS week: 2315 Day: 1 MJD: 60450
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 -10 0 -4 .22 21 17 | -7920 1501 2758 7080
esa n/a| -4 -2 0 -13 -7 13 -.03 37 21 | -9272 3000 2759 7552
gfz n/a| 1 0 2 -9 -16 -40 -.10 17 14 | 0 1439 2768 6414
grg n/a| 2 0 -2 -29 16 78 .42 33 24 | -8263 1451 2798 5850
iac n/a| 1 0 -1 29 -21 -25 -.09 18 16 | -6273 37 2759 6992
jgx n/a| 0 0 -5 46 14 22 -.14 27 27 | -7659 1848 2786 5484
Table 2.2315.2 GPS week: 2315 Day: 2 MJD: 60451
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 -13 14 .14 19 16 | -12968 -2510 3020 7187
esa n/a| -2 0 1 -5 -9 13 -.11 37 22 | -7972 -1394 3016 6391
gfz n/a| 2 0 7 25 -5 7 -.11 17 14 | 0 -2801 3063 6418
grg n/a| 4 0 -1 4 -12 1 .46 29 24 | -14073 -2910 3018 6201
iac n/a| 0 0 -3 8 16 -12 -.06 17 14 | -12473 -2080 3014 7174
jgx n/a| 0 2 -9 -25 22 -46 -.15 32 32 | -11379 -2989 3241 6795
Table 2.2315.3 GPS week: 2315 Day: 3 MJD: 60452
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 -10 -5 20 .20 20 15 | 4881 1198 3228 7489
esa n/a| -2 -3 2 -25 -6 32 -.05 40 22 | 1820 976 3036 7208
gfz n/a| 2 0 3 -7 11 -21 -.08 17 11 | 0 1431 3259 7131
grg n/a| 3 0 -3 -15 8 -15 .40 30 26 | 4937 565 3094 7165
iac n/a| 0 3 -3 26 8 -13 -.12 19 16 | 6076 1985 3228 7488
jgx n/a| -1 0 -8 -2 23 -16 -.19 30 30 | 5597 657 3080 6997
Table 2.2315.4 GPS week: 2315 Day: 4 MJD: 60453
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 -17 -10 77 .11 20 17 | 6083 -1227 4364 20659
esa n/a| -1 -1 1 9 -2 -33 -.05 40 30 | -292 903 3167 7494
gfz n/a| 1 0 11 12 28 -12 .00 20 17 | 0 -817 3183 7435
grg n/a| 3 0 0 23 36 9 .43 32 23 | 7067 -2286 4444 21219
iac n/a| 0 0 -6 -22 -44 -28 -.15 17 14 | 8582 -1396 4407 22237
jgx n/a| -1 0 -10 -19 60 -26 -.19 32 32 | 3170 -558 3162 7168
Table 2.2315.5 GPS week: 2315 Day: 5 MJD: 60454
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 0 0 21 .16 21 16 | 5665 1653 3169 17743
esa n/a| 0 0 0 -13 -15 -35 -.13 39 27 | 393 2484 2775 7072
gfz n/a| 3 0 6 44 33 -32 -.08 21 17 | 0 1802 2789 6090
grg n/a| 0 0 0 -16 -13 18 .40 28 23 | 5564 1675 3192 17691
iac n/a| 0 1 -1 -13 0 29 -.08 17 15 | 8554 76 3230 19379
jgx n/a| 0 -1 -6 14 25 -81 -.14 28 28 | 4683 1804 2805 6379
Table 2.2315.6 GPS week: 2315 Day: 6 MJD: 60455
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 1 -1 1 12 .14 19 16 | 8777 -3468 3386 17652
esa n/a| 0 -1 0 -2 -12 29 -.10 35 22 | 6384 -2088 3174 6559
gfz n/a| 1 -1 6 5 18 -2 -.04 18 16 | 0 -3411 3228 6450
grg n/a| 2 -1 -4 -65 -12 0 .38 29 19 | 9284 -3688 3448 17600
iac n/a| -2 0 1 37 -4 -15 -.14 23 20 | 10258 -1423 3443 19298
jgx n/a| 0 0 -7 5 19 -14 -.19 26 26 | 8115 -3377 3278 6809
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 3.2315.0 GPS week: 2315 Day: 0 MJD: 60449
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1446 46 63 16 33 28 40 17 | 126 58 97 91 96 73 92
R02 | 970 9 22 28 19 21 25 9 | 104 90 121 97 105 88 102
R03 | 1173 8 21 26 19 19 20 8 | 93 83 112 92 100 83 95
R04 | 1078 22 14 14 8 28 18 8 | 92 82 72 78 74 62 75
R05 | 1916 16 17 11 15 26 13 7 | 105 98 91 98 106 89 97
R07 | 1878 10 20 14 29 19 13 8 | 91 78 94 105 90 90 91
XR08 | 1175 22 23 11 25 43 --- 13 | 83 81 116 9999 103 --- 89
XR09 | 3479 16 22 11 18 27 --- 9 | 43 45 48 48 57 --- 44
XR11 | 3475 15 15 9 21 15 --- 7 | 38 44 43 50 43 --- 41
R12 | 938 7 22 10 15 18 13 6 | 49 59 53 53 49 44 48
R13 | 2164 33 47 43 39 23 54 18 | 87 47 94 60 71 55 67
R14 | 2386 13 13 10 15 25 11 7 | 50 50 55 55 58 40 50
R15 | 1370 8 16 14 16 28 12 7 | 55 51 52 55 65 46 52
R16 | 1105 11 25 17 13 18 16 7 | 62 62 72 60 55 47 58
XR17 | 722 10 16 8 9 16 --- 6 | 37 39 35 41 38 --- 36
R18 | 807 12 15 17 23 15 20 7 | 33 35 30 38 35 32 31
R19 | 668 35 48 26 62 14 42 17 | 35 36 36 37 32 37 29
R20 | 4477 34 123 41 53 30 70 26 | 50 80 58 45 32 57 42
R21 | 871 12 19 8 19 19 25 7 | 37 41 39 41 35 42 37
R22 | 2597 16 11 10 16 16 12 6 | 54 59 63 54 58 58 57
R24 | 1244 13 24 10 14 17 25 7 | 43 40 39 46 39 33 38
XR25 |13419 10 16 --- --- 11 --- 8 | 28 33 --- --- 22 --- 25
XR26 | 7500 31 --- --- 34 62 --- 31 | 277 --- --- 200 168 --- 272
------+-----------------------------------------+-------------------------------------
RMS | 1836 21 41 21 28 22 30 |T 72 58 67 68 66 57 68
WRMS | 1836 15 27 17 30 22 27 |NE 72 58 67 68 66 57 68
MEDI | 1370 13 20 14 19 19 20 |MD 54 51 58 55 58 55 52
Table 3.2315.1 GPS week: 2315 Day: 1 MJD: 60450
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1092 45 71 22 29 27 47 18 | 86 33 64 76 77 51 64
R02 | 763 14 16 12 17 19 15 7 | 77 66 59 59 77 57 66
R03 | 1003 8 14 11 19 14 11 5 | 77 82 79 70 77 84 78
R04 | 1228 26 14 8 39 16 12 9 | 64 53 49 56 47 43 50
R05 | 1468 15 11 15 15 23 13 7 | 75 75 72 88 75 68 73
R07 | 843 5 15 17 15 13 14 6 | 58 56 65 65 50 54 57
XR09 | 1735 17 12 20 21 15 --- 8 | 26 30 44 41 27 --- 32
XR11 | 4885 15 15 15 22 14 --- 8 | 18 27 32 48 34 --- 28
R12 | 856 6 14 14 14 16 20 6 | 47 47 53 57 49 41 48
R13 | 1627 32 29 24 26 11 34 11 | 63 45 53 51 50 53 47
R14 | 1106 15 15 14 19 13 16 6 | 44 46 38 39 43 31 38
R15 | 2038 7 12 12 17 13 15 5 | 55 57 58 48 53 61 54
R16 | 1319 13 26 16 23 16 17 8 | 47 48 52 60 41 39 45
XR17 | 1013 9 16 10 14 13 --- 6 | 22 18 20 27 23 --- 19
R18 | 920 10 17 10 9 12 11 5 | 21 21 18 25 21 20 18
R19 | 1128 31 35 29 81 30 51 19 | 39 32 32 40 20 52 27
R20 | 4425 41 115 28 73 31 55 25 | 32 59 55 31 27 34 33
R21 | 995 10 16 16 25 14 22 7 | 25 25 24 33 19 19 21
R22 | 2663 14 15 10 13 12 10 5 | 48 56 58 41 58 53 52
R24 | 943 9 20 16 14 16 30 8 | 25 20 23 29 23 22 20
XR25 |19803 18 16 --- --- 18 --- 12 | 20 24 --- --- 21 --- 14
XR26 |13980 4 --- --- --- --- --- 0 | 414 --- --- --- --- --- 413
------+-----------------------------------------+-------------------------------------
RMS | 1686 21 37 17 33 18 27 |T 62 43 56 49 43 46 58
WRMS | 1686 17 21 14 24 16 27 |NE 62 43 56 49 43 46 58
MEDI | 1128 14 16 15 19 15 16 |MD 47 46 53 48 43 51 47
Table 3.2315.2 GPS week: 2315 Day: 2 MJD: 60451
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 797 42 62 20 17 16 43 15 | 102 56 81 80 82 70 79
R02 | 1440 11 26 19 13 13 11 7 | 86 67 87 84 73 70 78
R03 | 666 12 20 8 16 13 12 6 | 84 82 82 83 83 79 81
R04 | 796 17 13 9 15 18 10 6 | 78 77 75 66 59 65 69
R05 | 1737 12 8 16 17 9 14 6 | 81 77 91 69 74 70 78
R07 | 1371 8 12 16 10 9 17 5 | 75 70 83 76 67 66 72
R09 | 1850 21 13 12 22 12 15 7 | 35 43 50 50 39 28 41
XR11 | 4590 13 18 13 11 12 --- 6 | 30 35 35 33 41 --- 33
R12 | 709 11 13 10 12 18 25 7 | 55 57 62 59 67 59 59
R13 | 1297 25 41 31 39 17 51 14 | 61 39 73 58 56 33 53
R14 | 949 10 22 9 14 10 12 5 | 48 53 39 46 36 36 40
R15 | 2205 17 16 20 14 8 18 7 | 55 50 32 49 39 34 40
R16 | 977 10 30 11 15 13 19 7 | 57 50 57 60 60 49 55
XR17 | 770 9 13 12 16 13 --- 6 | 33 34 34 38 34 --- 32
R18 | 1189 14 23 10 23 15 15 7 | 34 40 39 36 33 32 33
R19 | 1222 35 43 25 80 31 50 19 | 53 46 41 44 33 51 38
R20 | 2110 27 111 21 63 36 83 25 | 37 44 30 45 40 38 32
R21 | 787 10 14 23 12 11 30 8 | 34 32 35 33 35 39 32
R22 | 2108 12 12 8 14 8 13 5 | 32 37 37 38 36 32 34
R24 | 854 10 19 15 18 13 29 7 | 37 32 37 39 38 31 34
XR25 |16667 15 11 --- --- 11 --- 9 | 29 34 --- --- 28 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 1378 19 37 17 29 17 32 |T 54 53 56 54 50 49 50
WRMS | 1378 16 22 14 24 14 32 |NE 54 53 56 54 50 49 50
MEDI | 1222 12 18 13 15 13 17 |MD 53 46 50 49 40 39 40
Table 3.2315.3 GPS week: 2315 Day: 3 MJD: 60452
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1079 38 53 15 38 13 46 15 | 92 50 71 59 73 62 69
R02 | 1332 6 10 9 17 9 17 5 | 67 62 68 79 60 70 66
R03 | 635 13 17 15 20 17 16 7 | 83 73 68 85 83 68 76
R04 | 561 15 20 7 23 10 14 6 | 71 71 58 57 63 52 61
R05 | 835 9 11 14 16 10 16 5 | 59 67 69 56 62 54 61
R07 | 827 13 12 11 12 18 25 7 | 69 62 64 65 74 48 64
XR08 | 1447 9 83 24 --- 15 --- 19 | 66 82 83 --- 63 --- 65
R09 | 2428 23 14 13 20 13 15 7 | 18 29 34 41 32 27 28
XR11 | 2777 15 18 18 16 16 --- 8 | 25 34 45 44 27 --- 32
R12 | 900 8 16 13 18 13 15 6 | 47 56 40 58 48 41 46
R13 | 1316 21 48 36 18 13 43 13 | 78 49 85 67 68 59 66
R14 | 1490 10 18 13 15 5 15 5 | 51 53 47 44 43 37 45
R15 | 846 8 18 17 17 10 16 6 | 55 55 65 50 54 44 54
R16 | 1152 7 20 14 17 14 22 7 | 61 53 65 55 68 47 59
XR17 | 957 7 14 14 9 12 --- 5 | 26 27 27 24 22 --- 23
R18 | 906 13 14 9 17 30 20 8 | 26 27 32 31 39 22 26
R19 | 1235 34 55 22 64 35 34 17 | 35 51 47 61 33 39 37
R20 | 1618 33 125 30 75 43 70 27 | 44 35 30 30 29 50 26
R21 | 560 13 23 19 14 12 32 8 | 23 20 24 24 22 26 20
XR22 | 1931 12 12 12 --- 9 19 6 | 37 39 42 --- 36 31 37
R24 | 756 22 19 11 9 11 19 7 | 25 25 28 29 25 25 23
XR25 |11313 12 15 --- --- 8 --- 8 | 18 20 --- --- 17 --- 14
XR26 |>>>>> 74 --- --- --- 76 --- 75 | 166 --- --- --- 226 --- 153
------+-----------------------------------------+-------------------------------------
RMS | 1178 20 40 17 30 19 30 |T 54 47 52 50 55 44 50
WRMS | 1178 15 22 11 26 16 30 |NE 54 47 52 50 55 44 50
MEDI | 1152 13 18 14 17 13 19 |MD 51 50 47 55 48 44 46
Table 3.2315.4 GPS week: 2315 Day: 4 MJD: 60453
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2130 23 53 29 33 14 40 14 | 71 49 82 50 59 42 59
R02 | 1558 8 15 15 10 8 11 5 | 63 65 69 66 63 66 64
R03 | 1041 10 17 9 19 7 19 6 | 58 49 62 72 56 47 57
R04 | 824 14 10 23 19 11 16 7 | 57 57 75 49 47 45 54
R05 | 678 12 17 10 13 21 14 7 | 70 68 80 81 90 68 76
R07 | 1023 14 25 25 15 21 17 9 | 63 57 89 61 86 64 72
XR08 | 1181 13 17 21 --- 11 --- 9 | 64 78 75 --- 68 --- 66
R09 | 1230 19 30 23 16 14 20 9 | 21 39 35 23 24 24 23
XR11 | 1610 13 13 17 21 13 --- 7 | 32 34 32 29 32 --- 28
R12 | 883 7 15 10 15 13 14 5 | 57 69 63 66 58 55 60
R13 | 913 19 51 25 44 18 50 15 | 81 57 79 73 75 60 70
R14 | 2624 6 15 10 8 14 14 5 | 57 49 60 53 58 44 54
R15 | 922 9 14 22 13 8 20 6 | 52 52 73 57 48 38 53
R16 | 849 17 26 31 25 15 18 9 | 61 51 69 56 40 44 51
XR17 | 791 8 12 14 14 12 --- 6 | 24 26 23 26 19 --- 20
R18 | 712 20 14 9 12 16 30 8 | 21 20 24 26 27 22 20
R19 | 1295 34 59 23 62 23 33 17 | 32 24 26 31 25 31 19
R20 | 809 46 125 26 92 35 92 30 | 59 54 39 28 27 48 31
R21 | 1812 9 17 11 10 15 20 6 | 18 18 19 21 18 17 16
R22 | 2122 13 8 11 20 9 18 6 | 17 22 29 28 24 27 21
R24 | 844 28 16 28 14 17 18 9 | 27 26 44 28 23 16 21
XR25 |17953 11 12 --- --- 11 --- 8 | 19 18 --- --- 17 --- 15
XR26 |14749 56 --- --- 32 63 --- 39 | 230 --- --- 66 158 --- 224
------+-----------------------------------------+-------------------------------------
RMS | 1357 20 40 20 32 17 32 |T 54 44 54 47 49 42 51
WRMS | 1357 17 30 17 23 14 32 |NE 54 44 54 47 49 42 51
MEDI | 1041 13 16 21 16 14 18 |MD 57 49 62 50 47 44 53
Table 3.2315.5 GPS week: 2315 Day: 5 MJD: 60454
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1502 31 67 24 33 20 42 15 | 68 42 61 57 60 32 52
R02 | 1758 10 17 8 15 13 10 5 | 51 53 59 65 58 56 56
R03 | 1724 8 9 18 11 9 14 5 | 51 52 56 58 46 43 49
R04 | 881 19 17 19 11 13 15 7 | 47 45 29 42 33 46 38
R05 | 1010 15 7 16 12 6 12 5 | 66 61 52 57 60 66 60
R07 | 1097 7 26 18 11 20 29 8 | 63 49 76 58 77 46 63
R08 | 1684 11 28 18 20 16 23 8 | 61 54 78 547 70 17 65
R09 | 1218 25 28 17 14 12 11 8 | 29 34 34 28 23 20 24
XR11 | 1881 13 17 16 9 13 --- 6 | 25 30 33 32 21 --- 24
R12 | 794 9 18 31 12 20 15 8 | 59 57 36 59 65 61 55
R13 | 1473 22 54 37 55 21 60 18 | 64 36 82 58 73 55 60
R14 | 2436 6 16 13 12 8 14 5 | 40 47 45 40 41 34 40
R15 | 1270 10 17 13 12 8 12 5 | 49 42 51 47 40 41 44
R16 | 861 15 25 28 21 9 17 8 | 52 59 71 49 49 48 52
XR17 | 781 7 11 7 16 11 --- 5 | 21 24 22 27 19 --- 19
R18 | 720 15 24 17 9 12 18 7 | 20 22 33 26 29 21 22
R19 | 1736 46 64 32 66 34 38 20 | 39 34 32 51 27 34 27
R20 | 1263 43 107 20 55 18 64 23 | 46 26 42 34 27 36 26
R21 | 2326 9 13 11 13 20 17 6 | 24 22 27 30 26 22 22
R22 | 2663 15 11 12 13 9 8 5 | 16 20 27 26 22 21 19
R24 | 790 15 18 24 21 22 22 9 | 24 24 24 26 33 19 18
XR25 |21404 13 14 --- --- 10 --- 8 | 18 21 --- --- 21 --- 18
XR26 |16650 39 --- --- 44 58 --- 34 | 160 --- --- 65 130 --- 152
------+-----------------------------------------+-------------------------------------
RMS | 1539 21 39 21 28 17 28 |T 47 38 46 67 45 37 43
WRMS | 1539 16 27 17 23 15 28 |NE 47 38 46 67 45 37 43
MEDI | 1473 15 17 18 13 13 17 |MD 47 36 42 47 40 36 40
Table 3.2315.6 GPS week: 2315 Day: 6 MJD: 60455
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 863 36 48 22 39 17 39 15 | 98 51 82 61 76 49 70
R02 | 1506 11 24 14 13 24 17 7 | 83 68 87 83 79 67 78
R03 | 875 10 9 14 14 18 11 6 | 75 72 76 79 73 63 72
R04 | 1138 10 15 9 13 27 11 6 | 69 68 61 61 53 55 60
R05 | 2183 17 12 10 20 19 11 6 | 84 76 82 86 78 79 80
R07 | 1874 8 22 9 24 21 12 7 | 84 65 87 90 91 71 82
R08 | 1731 13 12 24 14 17 25 8 | 80 82 102 401 89 18 83
R09 | 2393 20 25 15 14 13 12 7 | 33 38 37 31 31 19 30
R11 | 2231 12 12 13 31 22 11 7 | 37 35 37 36 43 13 34
R12 | 797 11 20 15 20 29 20 8 | 85 94 89 85 106 82 88
R13 | 1378 35 42 24 40 34 55 17 | 99 54 90 77 94 63 80
R14 | 1570 5 16 15 17 12 14 6 | 64 65 68 57 66 51 62
R15 | 2075 12 21 17 11 21 11 7 | 67 63 57 59 62 50 58
R16 | 945 13 28 15 21 18 9 7 | 73 66 82 66 72 67 70
XR17 | 821 11 14 21 16 17 --- 8 | 23 23 29 30 22 --- 21
R18 | 771 12 21 10 12 17 12 6 | 20 20 21 25 29 16 17
R19 | 1251 29 54 23 78 32 59 20 | 45 50 42 46 24 51 36
R20 | 2138 35 110 41 57 36 50 24 | 52 45 41 36 28 44 34
R21 | 1914 9 11 10 17 15 16 5 | 27 24 31 32 33 26 27
R22 | 3583 13 13 12 12 25 7 6 | 21 23 29 33 27 25 23
R24 | 663 13 17 10 11 10 22 6 | 22 28 25 26 23 16 20
XR25 |18196 12 19 --- --- 9 --- 9 | 22 23 --- --- 20 --- 18
XR26 |19695 41 --- --- 25 59 --- 31 | 205 --- --- 71 139 --- 200
------+-----------------------------------------+-------------------------------------
RMS | 1745 19 35 18 29 23 26 |T 63 51 59 71 59 46 58
WRMS | 1745 16 22 16 19 20 26 |NE 63 51 59 71 59 46 58
MEDI | 1570 12 19 15 17 19 12 |MD 67 51 61 59 62 50 60
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