[IGSREPORT-30459] Wk 2366 IGLOS Final Orbits
acc
acc at igs.org
Thu May 29 07:05:16 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2366 (May 11, 2025 - May 17, 2025)
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 2.2366.
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:
igl2366[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2366 in the SP3 format.
igl23667.sum Combination Report for GPS Week 2366.
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.
Starting 02-Feb-2025 (GPS week 2352) the IGS Analysis Centers started using
the IGS realization of the updated ITRF2020-u2023, called IGb20. The combined
GLONASS orbits from this date are therefore in IGb20 frame.
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 | 5.0 ns
1 | 5.2 ns
2 | 4.6 ns
3 | 6.8 ns
4 | 4.2 ns
5 | 5.4 ns
6 | 3.5 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
----+--------+---------------
0 | ALL | R22
1 | ALL | R22
1 | ESA | R20
2 | ESA | R20
4 | ESA | R20
5 | ESA | R20
6 | ESA | R19
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 1.2366, 1a.2366).
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 2.2366.0-6)
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 3.2366.0-6).
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 2366 summary. (May 11, 2025 - May 17, 2025)
Table 1.2366.a GPS week : 2366 MJD: 60806.0-60812.0
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| -2 1 1 5 -5 16 .14 17 15 | 2472 -22 3248 7433
| 0 0 1 12 16 13 .02 | 975 1689
esa n/a| -3 0 -1 0 2 25 -.06 38 36 | 3387 -1072 3267 7358
| 1 1 1 18 14 44 .03 | 1734 2466
gfz n/a| 1 0 7 18 6 -34 -.10 18 16 | 0 -461 3343 7770
| 0 0 3 12 17 20 .03 | 0 1816
grg n/a| 2 0 0 -32 3 4 .37 22 19 | 4927 -313 3256 7397
| 1 0 2 13 21 33 .05 | 1048 1778
iac n/a| 1 -1 0 10 -10 -48 -.15 18 18 | 6744 -185 3235 8000
| 2 2 2 24 15 32 .05 | 779 1265
jgx n/a| 0 0 -8 -6 -8 9 -.21 21 21 | 3144 -309 3278 7718
| 1 0 2 12 15 21 .04 | 986 1873
Table 1.2366.b GPS week : 2366 MJD: 60806.0-60812.0
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
------+------------------------------------+------------------------------------------
R02 | 8 8 7 7 7 12 12 |
R03 | 5 9 9 7 6 8 5 |
R04 | 8 8 6 8 6 9 6 |
R05 | 7 8 6 5 7 6 7 |
R07 | 10 6 6 5 7 7 7 |
R08 | 11 8 7 7 6 8 5 |
R09 | 7 8 8 8 7 7 9 |
R11 | 8 8 6 8 6 7 8 |
R12 | 7 7 7 6 7 6 5 |
R14 | 8 8 6 5 6 5 5 |
R15 | 6 6 6 7 6 7 8 |
R16 | 9 7 8 7 7 6 7 |
R17 | 6 6 6 6 6 5 5 |
R18 | 6 7 8 7 9 7 8 |
R19 | 21 22 19 19 22 27 193 |
R20 | 23 21 12 22 19 23 25 |
R21 | 7 7 6 8 7 7 6 |
R22 | --- --- 10 7 5 8 8 |
R24 | 8 6 6 7 7 8 9 |
R26 | 24 29 31 27 32 31 30 |
R27 | 36 48 0 --- 0 0 0 |
Table 1.2366.c GPS week : 2366 MJD: 60806.0-60812.0
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 2366 0 | 3 82 179 49 -2360 5815 81.5 2619 2619 | 5006 0
brd 2366 1 | 2 -12 216 25 -1423 1168 81.5 2803 2803 | 5216 0
brd 2366 2 | 21 54 255 -787 578 1016 81.1 2380 2380 | 4567 0
brd 2366 3 | 60 -3 106 -389 1716 4289 78.8 1849 1849 | 6834 0
brd 2366 4 | -23 62 164 -828 1828 11180 80.5 2183 2183 | 4192 0
brd 2366 5 | 24 49 232 -1400 230 2840 82.4 2043 2043 | 5404 0
brd 2366 6 | 62 15 93 -591 1672 4850 81.5 1975 1975 | 3493 0
-------------+------------------------------------------------------------+----------------
brd 2366 mean| 21 35 178 -560 320 4451 81.0 2264 2264 | 4958 0
brd 2366 sdev| 31 36 61 512 1650 3475 1.2 351 351 | 1054 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 2.2366.0 GPS week: 2366 Day: 0 MJD: 60806
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 1 2 4 5 .12 16 15 | 2342 -1889 3671 6442
esa n/a| -3 1 -1 2 -7 61 -.09 37 29 | 1586 -2312 3731 7378
gfz n/a| 1 0 3 25 15 -47 -.10 18 17 | 0 -2176 3715 6668
grg n/a| 2 0 2 -35 -35 41 .33 22 17 | 5744 -1880 3676 6399
iac n/a| 6 -6 -2 39 -21 -108 -.17 30 32 | 6109 259 3651 6895
jgx n/a| 0 0 -6 -2 -15 28 -.26 23 23 | 3028 -1859 3666 6594
Table 2.2366.1 GPS week: 2366 Day: 1 MJD: 60807
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 2 13 -7 33 .17 18 16 | 817 2227 2884 7152
esa n/a| -4 -2 0 23 30 17 -.03 41 45 | 1487 1656 2925 6339
gfz n/a| 1 0 7 10 29 -27 -.09 21 17 | 0 2107 2917 7141
grg n/a| 2 0 1 -35 4 -41 .32 23 15 | 3975 2392 2875 7080
iac n/a| 3 0 0 -17 -27 -48 -.20 18 18 | 6701 633 2864 7524
jgx n/a| 0 0 -12 0 -7 28 -.22 21 21 | 1409 2288 2891 7280
Table 2.2366.2 GPS week: 2366 Day: 2 MJD: 60808
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 1 11 -5 15 .12 17 16 | 2060 -942 3082 7159
esa n/a| 0 -1 -3 -22 -11 14 -.02 39 41 | 2734 -1222 3057 6692
gfz n/a| 1 0 8 13 13 -62 -.15 17 17 | 0 -2141 3655 7713
grg n/a| 4 0 0 -9 2 52 .41 23 24 | 5109 -1485 3054 7039
iac n/a| 0 2 2 11 6 -13 -.11 14 13 | 6754 -1567 3065 7736
jgx n/a| -2 -2 -11 -17 -11 -28 -.15 16 16 | 3114 -1560 3191 7669
Table 2.2366.3 GPS week: 2366 Day: 3 MJD: 60809
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 -1 -6 9 12 .16 17 14 | 2922 2026 3035 7412
esa n/a| -4 0 -4 -12 12 13 -.07 37 38 | 5245 1342 3030 6694
gfz n/a| 1 0 12 22 -13 -10 -.12 16 15 | 0 1694 3042 7745
grg n/a| 2 1 -1 -50 10 -4 .43 22 22 | 5978 1481 3015 7424
iac n/a| 2 -2 -3 33 -3 -43 -.14 17 16 | 7691 941 3019 8096
jgx n/a| 0 0 -6 3 1 10 -.22 20 20 | 3620 1971 3021 7902
Table 2.2366.4 GPS week: 2366 Day: 4 MJD: 60810
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 -16 14 30 .12 18 15 | 3968 -1818 3504 8399
esa n/a| -4 0 0 23 -5 57 -.08 39 39 | 5101 -2393 3485 8889
gfz n/a| 0 -1 9 6 -18 -55 -.09 17 17 | 0 -1830 3520 8622
grg n/a| 3 1 -2 -25 -3 -10 .40 20 18 | 5128 -2271 3530 8350
iac n/a| 0 0 -2 16 -29 -24 -.12 15 15 | 7818 -2366 3495 8956
jgx n/a| 0 -1 -5 -7 16 0 -.16 21 21 | 4626 -2355 3546 8530
Table 2.2366.5 GPS week: 2366 Day: 5 MJD: 60811
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 2 13 -24 -5 .15 15 14 | 2992 -258 2902 7659
esa n/a| -1 0 0 1 2 75 -.06 37 26 | 5207 -5203 2933 7770
gfz n/a| 2 -2 8 42 14 -24 -.09 19 17 | 0 -1119 2907 8195
grg n/a| 2 1 -3 -29 13 10 .31 21 20 | 5503 -835 2927 7880
iac n/a| 0 0 0 16 -3 -70 -.10 17 20 | 6438 153 2876 8258
jgx n/a| 1 0 -6 -28 -10 -2 -.22 21 21 | 3550 -1022 2912 8016
Table 2.2366.6 GPS week: 2366 Day: 6 MJD: 60812
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 0 19 -27 24 .16 14 13 | 2208 496 3661 7812
esa n/a| -2 -1 0 -19 -6 -57 -.03 33 37 | 2351 623 3713 7748
gfz n/a| 1 0 2 12 5 -15 -.05 15 12 | 0 233 3650 8310
grg n/a| 1 0 -2 -42 35 -18 .41 25 18 | 3053 405 3717 7609
iac n/a| 1 -1 2 -26 6 -28 -.24 18 16 | 5698 649 3675 8538
jgx n/a| 0 0 -7 5 -33 28 -.26 23 23 | 2662 372 3725 8039
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 3.2366.0 GPS week: 2366 Day: 0 MJD: 60806
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 651 7 28 14 21 20 20 8 | 93 72 98 107 95 75 92
R03 | 1541 5 13 9 15 16 7 4 | 83 73 89 89 86 78 83
R04 | 1034 19 15 11 12 35 12 7 | 74 54 67 65 53 57 62
R05 | 658 14 14 16 10 29 15 7 | 64 57 70 57 44 52 58
R07 | 1600 9 20 16 18 49 24 9 | 88 72 96 83 115 69 86
R08 | 910 14 37 12 12 54 22 10 | 75 81 95 90 119 69 85
R09 | 2570 10 26 17 16 20 10 7 | 39 54 44 38 47 43 41
R11 | 5539 17 21 15 19 30 11 8 | 56 52 60 44 53 50 52
R12 | 800 11 19 13 12 28 20 7 | 56 63 52 59 44 50 52
R14 | 1314 9 14 12 13 40 18 7 | 63 77 76 75 92 57 70
R15 | 1320 7 14 15 14 16 18 6 | 73 77 84 72 77 62 73
R16 | 2241 11 36 22 16 17 23 9 | 75 65 93 75 81 63 76
R17 | 1920 6 10 14 12 21 19 6 | 38 45 49 39 40 34 40
R18 | 736 6 23 13 13 17 14 6 | 23 27 23 27 24 22 21
R19 | 810 43 59 14 64 35 50 20 | --- --- --- --- --- --- 0
R20 | 7822 29 116 49 29 28 46 22 | 38 27 52 39 34 37 35
R21 | 894 8 24 11 13 20 23 7 | 29 32 36 38 36 30 31
R24 | 1575 12 27 11 14 32 22 8 | 35 36 41 37 39 33 34
XR26 | 8461 24 87 20 --- 45 --- 23 | 46 107 53 --- 83 --- 63
XR27 | 9990 20 --- --- --- 60 --- 35 | 154 --- --- --- 24 --- 153
------+-----------------------------------------+-------------------------------------
RMS | 2619 16 37 18 22 30 23 |T 64 59 66 62 63 51 64
WRMS | 2619 15 29 17 17 32 23 |NE 64 59 66 62 63 51 64
MEDI | 1320 11 23 14 14 28 19 |MD 63 61 67 59 53 52 62
Table 3.2366.1 GPS week: 2366 Day: 1 MJD: 60807
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 878 8 32 24 13 15 12 7 | 68 50 83 64 66 56 64
R03 | 1539 7 31 24 14 26 18 9 | 62 44 80 64 79 52 63
R04 | 504 12 24 20 11 12 21 7 | 56 36 66 58 47 39 50
R05 | 463 19 14 14 16 23 9 7 | 45 38 44 38 23 32 35
R07 | 1249 7 15 14 13 13 11 5 | 58 56 56 61 58 53 56
R08 | 1206 10 14 15 16 26 19 7 | 52 56 55 57 64 40 52
R09 | 1718 13 16 17 17 23 12 7 | 25 31 31 20 33 28 24
R11 | 5624 16 26 14 9 24 9 7 | 44 40 43 31 43 35 38
R12 | 605 7 26 17 16 15 13 6 | 40 52 41 49 37 33 39
R14 | 1642 16 17 18 16 20 12 7 | 41 59 46 63 57 41 48
R15 | 1012 9 15 16 11 8 16 5 | 57 54 63 57 50 43 53
R16 | 1428 9 28 15 10 13 15 6 | 55 46 64 63 65 48 56
R17 | 2190 10 21 14 10 8 14 5 | 34 39 44 41 36 45 38
R18 | 1199 9 23 16 12 13 15 6 | 20 19 20 22 17 11 13
R19 | 972 48 56 25 74 14 46 21 | --- --- --- --- --- --- 0
R20 | 9079 42 139 52 33 20 50 20 | 33 19 51 30 24 38 30
R21 | 1236 11 24 24 7 12 12 6 | 22 25 25 24 16 20 19
R24 | 1712 12 26 14 9 12 12 6 | 25 20 29 28 23 22 22
XR26 | 4672 42 68 32 --- 58 --- 28 | 39 77 47 --- 64 --- 48
XR27 | 8685 40 --- --- --- 56 --- 47 | 136 --- --- --- 29 --- 139
------+-----------------------------------------+-------------------------------------
RMS | 2802 18 41 21 23 18 21 |T 49 42 50 47 45 37 48
WRMS | 2802 16 45 17 15 18 21 |NE 49 42 50 47 45 37 48
MEDI | 1249 11 24 17 13 15 13 |MD 44 40 47 49 43 39 48
Table 3.2366.2 GPS week: 2366 Day: 2 MJD: 60808
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 724 12 20 19 10 12 16 6 | 86 68 93 84 81 63 79
R03 | 1322 12 36 23 17 16 18 9 | 78 75 98 98 90 68 84
R04 | 597 16 13 14 11 16 10 6 | 71 58 76 73 63 58 65
R05 | 1067 18 17 9 10 18 7 6 | 54 45 43 55 37 36 43
R07 | 908 10 26 14 13 11 9 6 | 64 51 52 70 57 60 58
R08 | 1249 15 18 18 15 15 14 7 | 59 66 78 65 72 52 65
R09 | 1842 14 26 16 22 10 15 7 | 38 55 42 54 47 42 44
R11 | 5660 13 19 17 15 10 10 6 | 48 46 49 40 42 34 43
R12 | 703 7 22 14 15 13 15 6 | 44 50 48 49 52 36 44
R14 | 2564 15 16 17 16 8 12 6 | 59 71 77 77 67 55 65
R15 | 796 9 14 11 11 12 14 5 | 72 71 71 68 75 57 68
R16 | 882 10 25 22 18 15 12 7 | 64 51 81 63 76 51 64
XR17 | 1222 9 16 14 12 12 --- 6 | 29 33 24 25 26 --- 25
R18 | 1084 16 26 22 20 12 10 7 | 24 31 36 40 31 21 27
R19 | 914 40 56 22 68 21 38 18 | --- --- --- --- --- --- 0
R20 | 6314 28 127 24 29 11 25 12 | 46 26 45 43 33 33 36
R21 | 941 11 14 13 15 8 15 5 | 26 22 21 31 24 21 22
XR22 | 2064 17 19 27 24 10 --- 10 | 50 84 73 72 54 --- 59
R24 | 1847 10 15 11 18 13 11 5 | 30 26 30 31 31 27 26
XR26 | 8283 40 75 47 --- 56 --- 31 | 36 76 40 --- 77 --- 53
XR27 | 8392 2 --- --- --- --- --- 0 | 469 --- --- --- --- --- 468
------+-----------------------------------------+-------------------------------------
RMS | 2379 17 39 17 23 14 16 |T 72 52 56 57 54 44 71
WRMS | 2379 16 41 17 24 13 16 |NE 72 52 56 57 54 44 71
MEDI | 1222 13 19 17 15 12 14 |MD 50 51 49 55 54 42 53
Table 3.2366.3 GPS week: 2366 Day: 3 MJD: 60809
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 750 11 17 11 13 20 17 6 | 96 85 100 93 103 89 95
R03 | 1071 10 24 14 19 14 10 6 | 80 67 85 69 80 68 75
R04 | 824 21 22 18 13 19 11 7 | 67 47 71 51 41 49 54
R05 | 1086 15 20 9 11 9 9 5 | 61 56 56 51 53 46 53
R07 | 1139 10 11 14 13 8 9 5 | 66 57 63 58 67 62 62
R08 | 1931 14 24 8 13 16 16 6 | 63 60 73 80 76 73 71
R09 | 2128 12 21 14 13 24 12 7 | 17 31 29 19 28 23 20
XR11 | 5078 17 17 17 13 17 --- 8 | 47 49 52 45 50 --- 46
R12 | 590 8 23 8 14 12 18 6 | 39 50 46 48 48 30 41
R14 | 2298 10 22 9 13 10 10 5 | 56 64 64 58 48 50 55
R15 | 1131 11 17 20 9 12 15 6 | 66 64 89 79 77 66 73
R16 | 1240 10 22 22 11 12 14 7 | 69 56 84 72 60 59 67
R17 | 708 13 21 9 20 12 9 6 | 27 28 31 33 31 27 28
R18 | 952 11 21 17 22 10 10 6 | 18 20 25 27 16 17 17
R19 | 974 41 74 30 64 15 26 18 | --- --- --- --- --- --- 0
R20 | 5690 29 106 26 37 32 59 21 | 36 31 49 47 36 38 36
R21 | 946 14 22 10 13 24 14 7 | 28 26 32 37 34 24 27
XR22 | 1410 15 11 18 7 7 --- 6 | 25 26 41 38 30 --- 32
R24 | 946 12 23 16 10 18 14 7 | 38 35 35 31 30 28 30
XR26 | 7803 33 80 35 --- 52 --- 27 | 41 93 39 --- 73 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 1848 17 37 16 22 17 20 |T 49 49 56 52 51 46 49
WRMS | 1848 14 38 15 22 16 20 |NE 49 49 56 52 51 46 49
MEDI | 1086 12 22 14 13 14 14 |MD 47 50 52 48 48 46 53
Table 3.2366.4 GPS week: 2366 Day: 4 MJD: 60810
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 886 15 18 8 14 17 16 6 | 87 80 79 73 78 65 76
R03 | 854 10 25 10 11 16 11 6 | 80 69 77 79 82 71 76
R04 | 1341 20 13 10 10 18 7 6 | 71 58 60 58 56 57 59
R05 | 1431 13 17 18 11 10 17 6 | 65 49 71 57 54 49 57
R07 | 1542 8 22 13 10 22 16 7 | 62 52 71 60 69 52 61
R08 | 2388 15 19 17 11 8 14 6 | 58 66 78 70 63 61 65
R09 | 2391 11 18 11 16 20 8 6 | 31 42 37 33 38 29 32
R11 | 5570 14 16 13 9 13 10 5 | 53 41 57 50 46 61 49
R12 | 768 10 25 19 9 13 19 7 | 38 48 54 45 49 34 42
R14 | 2092 9 22 14 12 11 12 6 | 53 54 50 57 43 51 50
R15 | 1290 11 18 13 13 6 11 5 | 62 66 66 60 54 50 58
R16 | 843 10 19 16 9 19 15 6 | 62 52 70 66 55 61 60
R17 | 809 11 17 14 17 13 10 6 | 27 28 25 29 28 23 24
R18 | 811 16 29 25 20 12 20 9 | 23 24 29 30 23 22 20
R19 | 952 51 84 32 59 22 33 21 | --- --- --- --- --- --- 0
R20 | 5302 31 123 26 39 15 59 18 | 30 25 28 22 26 24 22
R21 | 838 12 20 19 9 12 22 7 | 26 23 31 29 26 27 25
R22 | 1095 15 10 10 11 10 13 5 | 51 44 51 58 53 17 52
R24 | 881 12 24 19 14 17 11 7 | 38 34 35 38 32 37 34
XR26 | 8667 35 63 59 --- 65 --- 32 | 30 74 30 --- 81 --- 44
XR27 | ---- 2 --- --- --- --- --- 0 | 233 --- --- --- --- --- 233
------+-----------------------------------------+-------------------------------------
RMS | 2183 18 39 17 20 15 21 |T 59 48 52 50 50 43 56
WRMS | 2183 15 39 17 18 15 21 |NE 59 48 52 50 50 43 56
MEDI | 1095 12 19 14 11 13 14 |MD 53 49 54 57 53 49 50
Table 3.2366.5 GPS week: 2366 Day: 5 MJD: 60811
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 819 22 26 23 22 43 16 12 | 131 124 130 119 134 124 124
R03 | 1217 14 13 13 12 27 20 8 | 67 64 65 67 84 53 65
R04 | 1731 18 20 16 28 15 10 8 | 70 65 62 42 64 52 57
R05 | 2236 14 12 18 11 10 14 6 | 55 49 56 50 49 38 48
R07 | 1146 10 20 17 12 16 13 6 | 53 37 61 56 54 43 50
R08 | 1846 13 24 21 20 14 16 8 | 51 49 72 74 62 49 58
R09 | 3148 14 18 19 14 10 11 6 | 30 40 42 33 33 34 32
R11 | 6133 18 12 17 13 16 10 6 | 34 31 34 34 31 26 31
R12 | 617 9 20 15 12 10 13 6 | 40 52 46 37 34 38 39
R14 | 1288 10 15 13 10 10 12 5 | 53 63 58 50 48 45 51
R15 | 951 10 24 16 15 13 12 6 | 62 73 67 62 61 62 63
R16 | 750 16 14 9 15 11 8 5 | 60 57 57 50 49 55 53
R17 | 701 8 17 13 11 12 9 5 | 23 26 26 33 20 20 22
R18 | 1014 12 15 18 11 12 19 6 | 21 15 29 25 24 19 19
XR19 | 7559 25 --- --- --- 28 --- 27 | --- --- --- --- --- --- 0
R20 | 1935 27 139 33 63 15 65 23 | 24 25 43 31 21 35 24
R21 | 1228 9 21 21 16 9 17 7 | 18 22 19 24 18 13 16
R22 | 1183 15 15 26 7 15 21 7 | 43 51 61 50 38 16 47
R24 | 1016 21 25 26 7 16 14 8 | 40 35 48 42 30 35 35
XR26 | 5988 41 59 52 --- 61 --- 30 | 53 81 49 --- 77 --- 62
XR27 | ---- 3 --- --- --- --- --- 0 | 382 --- --- --- --- --- 382
------+-----------------------------------------+-------------------------------------
RMS | 2043 15 37 19 21 17 21 |T 65 50 53 48 49 42 63
WRMS | 2043 14 26 17 20 20 21 |NE 65 50 53 48 49 42 63
MEDI | 1217 14 20 18 12 14 13 |MD 51 49 56 42 48 38 48
Table 3.2366.6 GPS week: 2366 Day: 6 MJD: 60812
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1485 20 20 14 27 43 19 11 | 185 183 189 197 174 183 183
R03 | 1676 11 11 10 12 10 8 4 | 92 87 89 94 99 79 89
R04 | 2103 16 11 9 16 10 11 5 | 86 77 81 74 76 69 76
R05 | 2804 10 18 14 19 15 17 6 | 76 75 73 66 78 57 70
R07 | 1545 7 31 14 15 17 15 7 | 82 69 79 80 84 66 76
R08 | 1545 5 19 8 13 15 10 5 | 77 78 84 87 88 71 80
R09 | 2538 15 29 21 15 20 15 8 | 35 43 43 40 46 41 37
R11 | 5024 12 26 18 19 20 16 8 | 32 34 42 43 21 30 31
R12 | 592 10 15 12 10 14 7 5 | 54 60 53 52 51 49 52
R14 | 768 5 19 9 8 14 8 4 | 64 75 64 66 67 60 64
R15 | 772 8 31 10 14 9 26 7 | 80 91 85 75 78 64 78
R16 | 1028 10 26 15 22 14 13 7 | 79 77 89 73 76 68 77
R17 | 726 14 14 7 10 7 17 5 | 33 31 35 37 31 28 32
R18 | 1003 15 19 16 19 13 20 7 | 25 28 28 31 27 20 23
XR19 | 1401 183 276 203 --- --- --- 193 | --- --- --- --- --- --- 0
R20 | 2097 20 103 34 84 28 73 25 | 33 28 40 40 29 41 31
R21 | 1835 8 29 11 10 13 10 6 | 35 33 38 38 36 33 35
XR22 | 2258 15 29 13 13 15 --- 8 | 54 57 61 65 53 --- 57
R24 | 800 29 15 16 14 8 22 9 | 55 44 50 48 45 46 46
XR26 | 5191 43 72 30 --- 67 --- 29 | 61 100 54 --- 96 --- 68
XR27 | ---- 4 --- --- --- --- --- 0 | 405 --- --- --- --- --- 405
------+-----------------------------------------+-------------------------------------
RMS | 1975 14 33 15 25 18 23 |T 82 66 67 67 66 59 80
WRMS | 1975 13 37 12 18 16 23 |NE 82 66 67 67 66 59 80
MEDI | 1545 12 20 14 14 14 15 |MD 61 69 61 65 67 57 64
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