[IGSREPORT-30065] Wk 2328 IGLOS Final Orbits
acc
acc at igs.org
Sun Sep 8 23:45:04 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2328 (Aug 18, 2024 - Aug 24, 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 2.2328.
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:
igl2328[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2328 in the SP3 format.
igl23287.sum Combination Report for GPS Week 2328.
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 | 10.4 ns
1 | 8.3 ns
2 | 8.8 ns
3 | 6.3 ns
4 | 6.4 ns
5 | 5.1 ns
6 | 6.4 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 | R01
1 | IAC | R01
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 1.2328, 1a.2328).
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 2.2328.0-6)
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 3.2328.0-6).
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 2328 summary. (Aug 18, 2024 - Aug 24, 2024)
Table 1.2328.a GPS week : 2328 MJD: 60540.0-60546.0
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 -1 4 -16 -16 45 .11 20 12 | -402 -503 3681 13485
| 1 1 1 10 15 19 .02 | 1505 1935
esa n/a| -1 -1 0 -5 14 10 -.12 22 16 | 6852 202 3303 8104
| 1 1 1 10 14 44 .03 | 7150 2290
gfz n/a| 0 -1 0 48 17 -10 -.04 23 16 | 0 -77 3324 8106
| 0 1 1 11 9 17 .03 | 0 2071
grg n/a| 2 0 1 -23 2 -36 .41 27 16 | 5962 -670 3740 13054
| 1 1 1 16 14 32 .03 | 1960 2198
iac n/a| -1 1 -7 5 10 -52 -.14 24 17 | 7646 -1339 3658 12798
| 1 1 2 13 28 37 .05 | 2359 1080
jgx n/a| 0 1 0 -3 -22 29 -.23 28 28 | 3197 -419 3339 8130
| 1 1 2 11 17 100 .04 | 918 2156
Table 1.2328.b GPS week : 2328 MJD: 60540.0-60546.0
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 | 18 605 155 18 15 11 18 |
R02 | 7 7 7 8 7 7 7 |
R03 | 6 9 9 8 9 8 7 |
R04 | 8 8 8 10 7 6 6 |
R05 | 7 8 6 8 9 8 7 |
R07 | 8 7 9 9 9 10 9 |
R08 | 7 7 6 5 6 8 9 |
R09 | 7 7 7 6 7 6 5 |
R11 | 7 8 8 6 6 7 7 |
R12 | 7 7 6 6 6 9 7 |
R14 | 6 5 6 6 5 6 6 |
R15 | 7 8 6 8 6 5 7 |
R16 | 7 8 7 7 8 9 8 |
R17 | 6 7 8 6 7 7 7 |
R18 | 6 7 8 7 7 7 7 |
R19 | 18 19 22 20 20 26 29 |
R20 | 27 26 30 29 29 29 36 |
R21 | 8 7 6 7 6 8 7 |
R22 | 6 7 6 7 7 7 7 |
R24 | 8 10 12 7 7 6 9 |
R25 | 10 11 11 9 9 10 9 |
R26 | 28 35 28 35 40 30 34 |
Table 1.2328.c GPS week : 2328 MJD: 60540.0-60546.0
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 2328 0 | -28 50 70 -1907 1221 4057 83.0 1492 1492 | 10372 0
brd 2328 1 | -39 75 -5 -1588 497 3538 79.6 1569 1569 | 8301 0
brd 2328 2 | -2 66 47 496 1951 1401 78.7 1803 1803 | 8808 0
brd 2328 3 | -19 1 147 1201 1611 -1511 81.7 1729 1729 | 6313 0
brd 2328 4 | 44 -7 164 211 1221 -612 81.4 1819 1819 | 6402 0
brd 2328 5 | 30 70 123 1 1018 -1933 81.2 1851 1851 | 5131 0
brd 2328 6 | 83 45 219 600 515 2493 82.0 1670 1670 | 6374 0
-------------+------------------------------------------------------------+----------------
brd 2328 mean| 9 43 109 -140 1148 1061 81.1 1704 1704 | 7385 0
brd 2328 sdev| 44 33 76 1162 533 2437 1.5 135 135 | 1825 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 2.2328.0 GPS week: 2328 Day: 0 MJD: 60540
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 0 4 -8 -6 57 .10 16 12 | -318 -360 2938 10190
esa n/a| 0 0 0 -13 19 -41 -.15 27 18 | 11812 -477 2937 7864
gfz n/a| 0 -2 -2 50 21 -33 -.02 25 16 | 0 -841 2985 7454
grg n/a| 0 -1 2 -11 0 -84 .46 23 16 | 9272 -707 2981 9180
iac n/a| 0 3 -9 -14 -42 -30 -.22 21 15 | 10611 -449 2915 9534
jgx n/a| 1 1 0 -10 4 90 -.24 31 31 | 3242 -965 2983 7694
Table 2.2328.1 GPS week: 2328 Day: 1 MJD: 60541
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 3 -22 -5 40 .12 16 12 | -2197 1922 2879 10926
esa n/a| -2 0 0 -1 15 -20 -.15 20 15 | 17104 3609 2895 8509
gfz n/a| -1 -2 -1 63 10 -13 -.01 30 24 | 0 2275 2924 8454
grg n/a| 2 0 3 -7 -7 -43 .40 23 14 | 6212 2539 2943 10477
iac n/a| 0 0 -7 6 12 -55 -.20 21 16 | 8965 -574 2869 10556
jgx n/a| 1 1 2 -11 -11 158 -.26 30 30 | 1613 2081 2927 8589
Table 2.2328.2 GPS week: 2328 Day: 2 MJD: 60542
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 5 -20 -39 54 .09 20 13 | 1880 1508 3908 10176
esa n/a| 0 -2 -2 -24 26 -33 -.10 24 16 | -185 2274 3687 8627
gfz n/a| 0 0 0 36 29 -26 -.01 19 13 | 0 2402 3707 8655
grg n/a| 1 0 2 -7 5 -68 .40 32 15 | 7706 1382 3983 9356
iac n/a| -3 1 -5 5 19 -45 -.07 30 17 | 10402 -743 3887 9999
jgx n/a| -1 1 -2 -17 -19 99 -.15 26 27 | 2904 2252 3703 8105
Table 2.2328.3 GPS week: 2328 Day: 3 MJD: 60543
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 -27 0 60 .11 18 11 | 351 -3045 4009 15214
esa n/a| -1 -1 -2 -7 32 12 -.16 24 18 | 13372 -2828 3485 6911
gfz n/a| 0 0 0 60 9 0 -.08 23 17 | 0 -2580 3460 7584
grg n/a| 3 0 3 -23 -11 -39 .39 26 15 | 5289 -3553 4028 14806
iac n/a| 0 2 -8 29 21 -111 -.10 27 15 | 6659 -3489 3979 14267
jgx n/a| 0 -1 2 -7 -26 40 -.22 26 26 | 3700 -3461 3607 7511
Table 2.2328.4 GPS week: 2328 Day: 4 MJD: 60544
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 -22 -25 65 .10 19 12 | 786 -1995 3687 14830
esa n/a| -2 0 0 5 10 28 -.12 19 18 | 4749 -1094 3315 8215
gfz n/a| 0 0 0 34 25 -15 -.05 22 14 | 0 -1384 3356 7935
grg n/a| 2 0 0 -37 -9 -14 .45 29 18 | 5361 -2267 3755 14432
iac n/a| 0 0 -4 13 50 -73 -.10 21 16 | 6787 -1704 3683 13860
jgx n/a| 0 0 2 17 -40 3 -.27 31 31 | 4601 -1620 3376 8175
Table 2.2328.5 GPS week: 2328 Day: 5 MJD: 60545
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 3 1 -30 12 .14 24 13 | -1545 -2138 3937 15628
esa n/a| 0 -2 2 -2 7 72 -.08 20 15 | -283 -1473 3378 9127
gfz n/a| 0 -2 0 42 18 17 -.05 27 16 | 0 -1862 3412 9215
grg n/a| 4 1 1 -23 30 -14 .39 27 16 | 4164 -2335 3991 15644
iac n/a| -2 2 -7 -3 0 -59 -.14 25 20 | 4821 -1701 3891 14823
jgx n/a| 0 4 0 4 -15 -42 -.25 28 28 | 2819 -1926 3444 9289
Table 2.2328.6 GPS week: 2328 Day: 6 MJD: 60546
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 6 -14 -5 25 .14 27 14 | -1774 584 4415 17432
esa n/a| 0 0 0 3 -12 56 -.11 20 12 | 1400 1406 3424 7481
gfz n/a| 0 0 3 49 4 -3 -.07 18 12 | 0 1450 3429 7451
grg n/a| 4 0 0 -49 11 9 .42 30 17 | 3736 249 4503 17488
iac n/a| -2 0 -9 0 9 8 -.12 25 21 | 5281 -715 4382 16551
jgx n/a| 0 2 -2 -1 -46 -140 -.21 26 26 | 3502 705 3337 7551
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 3.2328.0 GPS week: 2328 Day: 0 MJD: 60540
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 627 24 77 13 20 43 32 17 | 34 24 29 22 31 13 23
R02 | 1502 6 15 20 12 13 25 7 | 59 49 69 64 60 44 57
R03 | 1667 8 17 11 10 12 25 6 | 69 54 66 74 76 52 65
R04 | 495 12 16 10 18 24 24 8 | 69 64 70 67 77 61 67
R05 | 744 15 9 10 15 19 22 6 | 60 51 51 53 56 43 51
R07 | 1103 11 22 19 18 12 27 8 | 57 37 58 59 53 39 49
R08 | 1218 9 17 13 16 23 16 7 | 49 50 62 59 69 45 55
R09 | 1375 16 19 19 12 13 18 7 | 57 56 54 54 51 53 53
R11 | 793 14 13 17 14 15 17 6 | 49 44 57 39 41 47 45
R12 | 1739 11 12 19 15 11 22 6 | 72 71 78 76 74 66 72
R14 | 1409 7 14 15 19 8 17 6 | 105 94 107 102 107 104 103
R15 | 933 14 16 11 17 14 26 7 | 79 66 74 80 69 73 73
R16 | 1223 11 20 17 12 16 19 7 | 83 77 79 81 79 88 80
R17E | 1401 9 14 15 15 12 20 6 | 75 72 81 73 77 82 75
R18E | 1067 7 15 16 10 17 19 6 | 73 71 75 74 78 75 74
R19E | 2583 31 37 43 43 37 52 17 | 123 113 119 113 107 92 113
R20E | 2209 38 57 80 62 41 90 27 | 182 193 158 184 170 224 178
R21E | 1575 14 18 20 25 13 20 8 | 63 64 65 67 65 62 63
R22E | 2482 15 14 9 18 9 17 6 | 55 60 56 62 55 53 56
R24E | 1549 9 17 22 23 12 20 7 | 71 71 75 74 73 77 72
XR25E |12670 12 13 --- --- 17 --- 10 | 58 60 --- --- 56 --- 57
XR26 |17487 27 --- --- 29 58 --- 28 | 57 --- --- 59 108 --- 71
------+-----------------------------------------+-------------------------------------
RMS | 1492 16 27 25 23 21 31 |T 72 68 74 73 74 69 70
WRMS | 1492 12 18 16 16 15 31 |NE 64 56 65 63 67 56 61
MEDI | 1401 12 16 16 17 14 20 |MD 63 64 69 67 69 61 65
Table 3.2328.1 GPS week: 2328 Day: 1 MJD: 60541
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01 | 800 >>>> 493 741 --- 2217 --- 605 | 854 3 1 --- 1 --- 9999
R02 | 1853 7 16 22 13 20 23 7 | 39 35 52 42 50 29 39
R03 | 1002 9 22 13 20 24 30 9 | 47 38 51 59 58 38 47
R04 | 887 9 18 29 11 19 18 7 | 51 54 73 46 55 53 52
R05 | 768 12 17 20 16 22 23 8 | 41 48 48 39 37 40 38
R07 | 941 8 13 17 17 13 23 6 | 41 38 41 53 44 43 41
R08 | 767 12 21 11 14 16 20 7 | 41 38 46 44 46 44 39
R09 | 1545 14 15 14 8 19 18 6 | 40 34 36 37 33 34 34
R11 | 806 17 13 20 19 11 21 7 | 38 39 33 26 31 32 31
R12 | 1555 15 13 29 9 10 19 7 | 55 65 79 61 60 64 61
R14 | 1467 6 14 10 11 14 16 5 | 92 86 95 97 95 100 93
R15 | 1257 9 25 11 17 13 18 7 | 57 41 58 60 44 62 51
R16 | 825 12 23 18 10 22 22 8 | 49 59 58 54 38 62 49
R17E | 1086 7 11 18 14 16 22 6 | 33 32 39 36 39 34 33
R18E | 1660 10 15 17 11 16 19 6 | 37 37 40 42 38 51 38
R19E | 2477 34 30 66 47 39 43 19 | 101 93 95 98 89 72 89
R20E | 2025 44 42 80 60 45 89 26 | 207 192 186 164 162 185 181
R21E | 2503 10 15 15 15 17 18 6 | 40 38 40 39 49 45 39
R22E | 2920 15 8 16 12 12 24 6 | 30 37 44 39 33 42 35
R24E | 790 7 17 30 36 13 19 9 | 45 51 40 65 44 46 45
XR25E |16492 12 18 --- --- 14 --- 10 | 31 34 --- --- 31 --- 29
XR26 |16665 32 --- --- 31 76 --- 34 | 33 --- --- 29 73 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 1568 16 20 30 23 21 30 |T 91 52 57 56 52 56 52
WRMS | 1568 12 15 24 14 16 30 |NE 105 44 51 49 47 50 47
MEDI | 1257 12 17 18 14 16 21 |MD 41 38 46 44 44 45 40
Table 3.2328.2 GPS week: 2328 Day: 2 MJD: 60542
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01 | ---- 122 --- --- 195 --- --- 154 | 535 --- --- 433 --- --- 9999
R02 | 1830 11 15 13 14 26 15 7 | 44 38 43 43 57 43 42
R03 | 1319 9 22 10 20 29 27 9 | 45 44 46 61 64 35 47
R04 | 614 9 13 13 16 22 32 8 | 49 53 54 63 65 48 53
R05 | 756 13 10 17 10 9 17 6 | 47 44 52 46 43 42 45
R07 | 601 15 11 10 16 26 32 8 | 51 46 46 34 59 33 42
XR08 | 1031 9 10 10 18 16 --- 6 | 44 45 50 47 55 --- 47
R09 | 1976 17 16 17 9 14 22 7 | 37 41 40 36 35 33 34
R11 | 1297 19 17 11 19 12 19 7 | 31 27 26 18 25 26 23
R12 | 936 13 13 17 9 11 15 6 | 62 61 50 58 61 60 57
R14 | 1183 7 13 14 14 11 14 5 | 63 74 74 62 67 58 66
R15 | 641 10 20 9 17 13 9 6 | 71 64 70 76 63 72 68
R16 | 958 16 22 11 14 13 11 6 | 58 59 61 62 56 60 58
R17E | 1074 11 16 24 17 12 16 7 | 58 57 70 54 56 61 59
R18E | 2154 19 20 10 15 15 17 7 | 45 48 44 43 45 48 44
R19E | 2765 41 28 40 63 66 49 21 | 78 87 108 89 115 81 85
R20E | 3882 49 75 45 91 85 65 30 | 92 117 104 100 95 86 82
R21E | 2672 10 15 15 16 11 13 6 | 51 51 52 51 47 52 49
R22E | 2277 15 10 9 16 10 12 5 | 41 47 47 46 41 49 43
R24E | 1446 22 18 19 55 16 19 12 | 57 54 54 64 49 56 49
XR25E |19860 16 16 --- --- 12 --- 10 | 40 46 --- --- 41 --- 41
XR26 |16628 25 --- --- 29 59 --- 28 | 36 --- --- 38 70 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1803 20 24 19 32 30 26 |T 74 55 57 72 57 52 51
WRMS | 1803 13 16 13 15 17 27 |NE 83 49 51 76 55 46 48
MEDI | 1319 15 16 13 16 14 17 |MD 49 48 52 54 56 49 47
Table 3.2328.3 GPS week: 2328 Day: 3 MJD: 60543
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01 | ---- 14 --- --- 22 --- --- 17 | 291 --- --- 225 --- --- 9999
R02 | 1354 6 16 21 17 12 25 7 | 45 47 63 57 49 30 47
R03 | 996 11 20 12 11 20 24 7 | 55 41 51 56 60 35 49
R04 | 634 11 18 19 25 34 18 9 | 48 51 49 63 77 55 53
R05 | 966 7 19 14 18 18 28 8 | 50 47 57 64 61 40 51
R07 | 520 13 20 21 9 18 29 8 | 54 45 62 50 54 35 49
XR08 | 1057 7 10 9 12 13 --- 5 | 40 37 42 39 40 --- 38
R09 | 1762 11 18 12 9 8 15 5 | 22 20 21 26 19 23 19
R11 | 1193 11 18 15 9 13 10 6 | 29 30 35 26 23 27 25
R12 | 696 11 21 11 14 15 10 6 | 57 77 64 70 53 60 62
R14 | 1049 9 14 11 14 15 9 5 | 67 65 60 62 69 68 64
R15 | 1180 11 20 17 20 15 20 7 | 71 59 71 72 66 62 66
R16 | 887 12 24 12 8 17 8 6 | 66 65 62 71 72 73 66
R17E | 1245 8 13 14 13 11 14 5 | 56 56 51 53 61 57 54
R18E | 1068 9 15 14 14 11 28 7 | 46 49 45 50 49 52 47
R19E | 2060 31 39 54 40 50 51 19 | 69 77 84 86 62 74 69
R20E | 5297 51 58 48 82 78 62 28 | 124 110 98 89 113 72 91
R21E | 1137 13 12 16 20 10 16 6 | 44 44 44 51 47 43 43
XR22E | 1649 14 13 14 15 13 --- 7 | 49 58 56 49 46 --- 49
R24E | 1334 13 13 15 18 12 13 6 | 61 64 56 52 60 61 58
XR25E |17790 11 13 --- --- 15 --- 9 | 39 42 --- --- 38 --- 38
XR26 |15571 33 --- --- 28 79 --- 34 | 42 --- --- 46 109 --- 59
------+-----------------------------------------+-------------------------------------
RMS | 1728 18 24 23 26 27 26 |T 64 54 56 64 58 51 52
WRMS | 1728 11 18 17 15 15 26 |NE 66 48 53 66 57 46 49
MEDI | 1180 11 18 14 15 15 18 |MD 50 49 56 56 60 55 51
Table 3.2328.4 GPS week: 2328 Day: 4 MJD: 60544
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01 | ---- 10 --- --- 21 --- --- 14 | 203 --- --- 160 --- --- 9999
R02 | 902 8 15 9 13 20 19 6 | 49 43 46 52 59 36 47
R03 | 832 7 26 10 24 21 24 8 | 58 47 58 75 68 45 57
R04 | 669 10 15 9 14 14 27 6 | 61 57 67 73 62 39 59
R05 | 700 15 24 9 24 24 15 8 | 47 44 56 70 70 51 54
R07 | 795 13 22 24 23 9 27 9 | 62 54 74 61 54 45 58
R08 | 676 7 16 10 18 13 12 5 | 49 50 55 50 56 47 50
R09 | 2055 11 21 12 19 9 16 6 | 33 30 35 42 32 31 32
R11 | 780 11 16 10 10 14 8 5 | 20 25 28 25 23 24 22
R12 | 761 13 16 12 13 15 9 6 | 54 53 58 59 61 50 54
R14 | 1334 8 11 10 12 13 8 4 | 70 74 69 70 79 71 71
R15 | 1653 10 11 13 11 10 20 5 | 65 79 77 73 67 65 70
R16 | 1138 19 20 21 20 16 12 8 | 72 66 68 59 71 67 66
R17E | 2144 10 12 16 22 12 14 6 | 55 61 57 50 56 59 55
R18E | 2092 13 13 16 21 12 18 7 | 27 34 35 32 30 26 29
R19E | 1963 37 35 53 49 37 56 19 | 59 70 83 71 71 67 64
R20E | 4590 54 31 53 92 58 104 29 | 72 95 106 86 106 96 81
R21E | 1050 10 11 13 20 14 17 6 | 43 43 43 48 43 35 40
R22E | 1282 15 14 14 21 11 10 6 | 28 31 39 42 28 34 30
R24E | 3386 18 12 19 20 14 10 7 | 35 37 35 31 33 33 32
XR25E |13226 13 12 --- --- 11 --- 8 | 31 29 --- --- 27 --- 28
XR26 |14958 40 --- --- 47 76 --- 40 | 28 --- --- 30 99 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1819 19 19 22 29 21 31 |T 55 51 57 59 56 48 49
WRMS | 1819 12 18 14 18 16 31 |NE 62 51 57 64 61 47 53
MEDI | 1282 11 15 13 20 14 16 |MD 49 47 57 59 59 45 54
Table 3.2328.5 GPS week: 2328 Day: 5 MJD: 60545
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01 | ---- 10 --- --- 12 --- --- 11 | 191 --- --- 139 --- --- 9999
R02 | 1053 8 12 14 9 19 28 7 | 44 41 42 44 49 31 40
R03 | 992 6 20 19 13 24 19 8 | 48 44 58 61 63 43 51
R04 | 1023 10 10 13 15 13 20 6 | 61 50 57 62 61 57 57
R05 | 1009 14 17 18 13 21 17 7 | 41 40 46 54 59 37 44
R07 | 939 19 16 14 28 12 31 9 | 54 33 37 67 38 37 43
R08 | 998 10 15 21 11 22 22 7 | 45 40 56 51 59 43 47
R09 | 1504 13 10 11 14 12 18 5 | 44 45 34 44 34 43 40
R11 | 738 14 19 16 8 14 22 7 | 23 28 28 25 22 27 21
R12 | 707 17 25 18 12 20 15 8 | 49 43 54 56 55 47 48
R14 | 1362 8 9 15 11 18 12 5 | 48 50 43 52 58 47 48
R15 | 1967 10 9 15 10 10 13 5 | 61 63 64 55 66 56 60
R16 | 1866 18 25 20 19 11 14 8 | 54 75 69 47 53 49 57
R17E | 2201 7 10 21 22 13 18 7 | 46 49 51 42 45 49 45
R18E | 1906 13 14 17 19 14 20 7 | 24 32 30 31 29 32 26
R19E | 1582 47 41 67 56 68 69 25 | 71 84 117 107 114 97 83
R20E | 5256 77 41 70 85 46 59 29 | 92 93 114 143 100 91 90
R21E | 952 13 13 21 15 20 16 7 | 47 46 53 54 42 47 46
R22E | 1494 15 12 14 14 18 19 7 | 38 49 52 50 49 36 44
R24E | 2190 12 12 14 14 13 14 6 | 37 41 45 43 43 44 40
XR25E |14767 14 13 --- --- 15 --- 10 | 33 42 --- --- 39 --- 37
XR26 |11262 32 --- --- 25 61 --- 29 | 36 --- --- 42 70 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1851 24 20 27 27 25 28 |T 53 49 55 60 54 48 48
WRMS | 1851 13 15 16 16 20 28 |NE 57 46 49 57 52 43 46
MEDI | 1494 13 13 17 14 18 19 |MD 46 44 52 52 53 44 46
Table 3.2328.6 GPS week: 2328 Day: 6 MJD: 60546
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01 | ---- 15 --- --- 20 --- --- 17 | 234 --- --- 147 --- --- 9999
R02 | 851 11 9 17 16 11 25 6 | 67 58 71 61 68 55 63
R03 | 1100 11 10 11 11 19 31 7 | 69 61 66 77 81 58 67
R04 | 1505 10 12 8 20 12 10 5 | 78 76 74 79 81 78 76
R05 | 871 12 9 8 15 21 22 6 | 70 72 75 85 88 62 74
R07 | 1539 21 15 16 20 19 27 8 | 78 54 62 76 72 57 64
R08 | 1119 10 17 10 24 33 28 9 | 70 60 72 81 93 55 70
R09 | 1143 10 8 11 9 10 17 5 | 60 57 55 60 50 60 56
R11 | 989 15 9 7 16 13 25 6 | 39 40 38 33 36 45 37
R12 | 775 18 15 12 14 19 15 7 | 71 66 79 78 76 70 72
R14 | 959 10 6 14 12 18 17 5 | 63 64 71 61 60 61 63
R15 | 1480 9 10 8 21 18 26 6 | 81 73 78 85 82 74 77
R16 | 1652 13 14 15 16 17 27 7 | 75 76 78 69 80 65 74
R17E | 2403 11 12 12 24 13 14 6 | 64 67 64 61 61 65 62
R18E | 3440 10 16 18 16 15 15 7 | 59 54 54 53 56 58 54
XR19E | 1453 36 31 70 82 67 --- 29 | 137 153 174 120 120 --- 140
R20E | 2518 103 69 55 106 79 69 36 | 211 120 135 118 180 99 130
R21E | 1609 11 16 15 21 13 17 7 | 69 60 70 59 66 73 65
R22E | 1489 16 11 11 18 16 15 6 | 43 50 50 54 44 39 46
R24E | 2031 22 13 19 26 19 16 8 | 58 58 50 53 48 53 51
XR25E |14018 15 11 --- --- 9 --- 8 | 35 39 --- --- 35 --- 35
XR26 | 9664 36 --- --- 29 68 --- 33 | 48 --- --- 58 117 --- 71
------+-----------------------------------------+-------------------------------------
RMS | 1670 27 20 18 30 25 26 |T 80 67 74 74 75 62 68
WRMS | 1670 14 12 12 17 21 26 |NE 78 63 68 75 75 61 66
MEDI | 1489 12 12 12 20 18 17 |MD 69 60 71 69 72 60 65
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