[IGSREPORT-30230] Wk 2343 IGLOS Final Orbits
acc
acc at igs.org
Fri Dec 20 06:03:58 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2343 (Dec 01, 2024 - Dec 07, 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 2.2343.
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:
igl2343[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2343 in the SP3 format.
igl23437.sum Combination Report for GPS Week 2343.
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 | 17.0 ns
1 | 15.7 ns
2 | 15.9 ns
3 | 14.8 ns
4 | 11.1 ns
5 | 11.6 ns
6 | 5.5 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
----+--------+---------------
5 | GFZ | R11
6 | GRG | R11
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 1.2343, 1a.2343).
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 2.2343.0-6)
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 3.2343.0-6).
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 2343 summary. (Dec 01, 2024 - Dec 07, 2024)
Table 1.2343.a GPS week : 2343 MJD: 60645.0-60651.0
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 0 -2 -21 1 83 .18 20 17 | 5930 1752 3336 10223
| 0 0 2 13 17 24 .03 | 2097 1481
esa n/a| 0 0 0 -12 -3 13 -.14 33 25 | 15256 1335 3304 8592
| 1 0 2 13 10 19 .02 | 5989 1600
gfz n/a| 1 0 1 28 20 11 -.05 39 16 | 0 1801 3266 7617
| 0 2 2 7 11 36 .03 | 0 1723
grg n/a| 0 0 5 -5 -42 -36 .32 43 21 | 10570 1926 3312 9857
| 1 1 3 9 27 34 .03 | 4573 1434
iac n/a| 0 0 -5 0 14 -44 -.12 16 15 | 13411 -914 3329 9813
| 1 0 2 16 20 52 .03 | 4288 748
jgx n/a| -1 0 5 -7 -21 -6 -.18 24 24 | 8579 1767 3372 7909
| 0 2 1 22 16 28 .04 | 2141 1392
Table 1.2343.b GPS week : 2343 MJD: 60645.0-60651.0
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 | 14 14 15 18 18 16 12 |
R02 | 8 7 7 6 7 5 8 |
R03 | 7 7 8 7 7 6 9 |
R04 | 8 7 8 9 10 7 10 |
R05 | 6 9 7 8 8 7 7 |
R07 | 7 6 8 10 8 8 8 |
R08 | 6 8 8 5 8 8 9 |
R09 | 6 6 6 6 8 8 6 |
R11 | 7 7 6 6 14 7 23 |
R12 | 7 7 8 8 7 7 7 |
R14 | 6 5 6 5 7 6 6 |
R15 | 8 7 6 6 9 7 10 |
R16 | 10 8 8 7 9 8 8 |
R17 | 7 9 9 7 7 7 6 |
R18 | 7 8 7 7 8 7 9 |
R19 | 17 20 23 20 20 18 22 |
R20 | 23 22 19 18 22 24 23 |
R21 | 7 8 8 9 8 7 7 |
R22 | 6 6 6 6 6 8 6 |
R24 | 8 7 11 9 10 10 8 |
R26 | 28 31 29 32 33 31 30 |
Table 1.2343.c GPS week : 2343 MJD: 60645.0-60651.0
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 2343 0 | -13 65 -77 -572 442 -5935 81.8 1695 1695 | 16980 0
brd 2343 1 | -65 28 -24 -2245 2304 -4314 82.0 1519 1519 | 15657 0
brd 2343 2 | 59 32 -90 -1174 5139 -1212 81.3 1263 1263 | 15922 0
brd 2343 3 | -18 20 -9 95 885 -8901 80.3 1605 1605 | 14757 0
brd 2343 4 | -11 72 -10 1379 1522 -2975 79.0 1500 1500 | 11135 0
brd 2343 5 | -12 14 -86 612 2065 -912 82.4 1485 1485 | 11597 0
brd 2343 6 | -11 -59 -167 1443 183 -2617 80.0 1513 1513 | 5487 0
-------------+------------------------------------------------------------+----------------
brd 2343 mean| -10 25 -66 -65 1791 -3838 81.0 1511 1511 | 13076 0
brd 2343 sdev| 36 43 57 1359 1675 2826 1.2 132 132 | 4007 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 2.2343.0 GPS week: 2343 Day: 0 MJD: 60645
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 1 0 -18 6 72 .21 19 16 | 2706 913 3267 10256
esa n/a| 0 0 1 -21 7 3 -.15 31 20 | 23282 905 3200 9814
gfz n/a| 1 0 1 27 31 -6 -.02 18 15 | 0 1471 3213 7424
grg n/a| 0 0 8 0 -26 -17 .33 29 19 | 14740 1191 3253 9817
iac n/a| 0 0 -10 15 15 -55 -.12 15 14 | 17109 -793 3251 9800
jgx n/a| -1 0 9 12 -46 20 -.11 23 23 | 5089 1470 3198 7494
Table 2.2343.1 GPS week: 2343 Day: 1 MJD: 60646
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 -5 -27 8 100 .12 22 17 | 3691 756 3287 10461
esa n/a| -1 0 0 -31 -14 2 -.15 31 27 | 9086 257 3087 7611
gfz n/a| 0 3 1 41 28 -24 -.07 19 16 | 0 618 3073 7370
grg n/a| 1 0 1 -3 -2 -54 .32 23 15 | 13484 1015 3303 10043
iac n/a| 1 0 -3 -23 11 42 -.09 15 13 | 16357 -1201 3269 10002
jgx n/a| 0 -2 4 -9 -24 -53 -.19 24 24 | 6639 602 3117 7693
Table 2.2343.2 GPS week: 2343 Day: 2 MJD: 60647
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 -2 -28 10 71 .18 21 21 | 6121 1122 2849 9114
esa n/a| -1 0 -2 -14 -14 23 -.12 33 28 | 21246 323 2840 7467
gfz n/a| 1 2 2 16 18 54 -.04 18 15 | 0 705 2831 7102
grg n/a| 0 0 1 -5 -25 -75 .29 26 21 | 14020 937 2834 8704
iac n/a| 0 -1 -4 -8 -20 -63 -.09 17 16 | 16887 -1334 2832 8848
jgx n/a| -1 -2 5 10 -35 21 -.16 24 24 | 8728 866 2877 7498
Table 2.2343.3 GPS week: 2343 Day: 3 MJD: 60648
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 -4 -40 2 131 .17 21 16 | 6401 3569 3097 9757
esa n/a| -1 0 0 -6 3 47 -.09 33 34 | 16480 2648 3107 7039
gfz n/a| 1 0 1 25 22 59 -.03 20 16 | 0 3836 3105 7943
grg n/a| 1 -1 11 6 -30 -39 .29 26 21 | 12194 3674 3117 9512
iac n/a| 0 0 -5 -5 -2 -132 -.11 13 12 | 14679 37 3099 9524
jgx n/a| -1 0 3 17 -11 16 -.16 23 23 | 8558 4043 3120 8174
Table 2.2343.4 GPS week: 2343 Day: 4 MJD: 60649
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 -3 -5 -8 68 .19 22 20 | 7984 -189 3763 10716
esa n/a| 1 0 1 10 -1 10 -.12 30 25 | 10616 -899 3796 8440
gfz n/a| 2 -1 0 26 20 32 -.02 27 20 | 0 -456 3710 8492
grg n/a| 1 0 7 -13 -68 -75 .35 27 19 | 9390 262 3766 10398
iac n/a| -1 0 -5 16 26 -19 -.14 18 17 | 12817 -2217 3759 10277
jgx n/a| 0 2 4 -13 -22 -20 -.23 24 24 | 10363 144 3793 8603
Table 2.2343.5 GPS week: 2343 Day: 5 MJD: 60650
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 -26 -33 80 .22 20 15 | 8476 2474 3517 10946
esa n/a| 2 1 1 -9 7 18 -.17 31 20 | 8348 2634 3506 10081
gfz n/a| 1 0 -3 32 -1 -3 -.08 148 16 | 0 2251 3602 7390
grg n/a| -1 -1 4 -3 -77 -12 .31 25 21 | 8507 2531 3531 10637
iac n/a| 0 2 -3 -9 42 -54 -.16 18 17 | 10817 -595 3514 10371
jgx n/a| -1 2 5 -27 3 -3 -.20 24 24 | 11377 2407 3488 7955
Table 2.2343.6 GPS week: 2343 Day: 6 MJD: 60651
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 -4 22 59 .15 17 16 | 6134 3621 3578 10315
esa n/a| 1 -1 4 -16 -12 -14 -.14 46 25 | 17734 3478 3595 9693
gfz n/a| 1 -1 3 33 27 -28 -.06 20 15 | 0 4185 3329 7602
grg n/a| 3 0 4 -21 -64 16 .37 143 30 | 1658 3876 3384 9891
iac n/a| 1 0 -7 20 27 -30 -.11 18 15 | 5213 -297 3580 9873
jgx n/a| -1 1 4 -40 -14 -26 -.21 23 23 | 9304 2839 4014 7948
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 3.2343.0 GPS week: 2343 Day: 0 MJD: 60645
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 707 39 41 29 26 15 39 14 | 86 38 69 52 55 43 55
R02 | 1098 13 21 9 29 16 19 8 | 69 76 59 54 67 51 61
R03 | 1493 12 16 12 12 16 25 7 | 88 71 87 80 88 62 80
R04 | 622 21 14 20 13 8 26 8 | 121 116 117 111 113 106 113
R05 | 1541 12 8 18 14 11 14 6 | 226 230 231 234 219 226 227
R07 | 2733 17 16 15 9 13 18 6 | 91 64 70 81 90 72 79
R08 | 1388 7 15 14 10 15 19 6 | 103 94 106 99 114 95 102
R09 | 2929 16 10 15 14 15 7 6 | 29 40 38 30 33 31 31
R11 | 1752 15 18 13 17 16 17 7 | 27 30 58 55 31 31 24
R12 | 1296 10 18 12 21 12 17 6 | 72 72 70 63 75 55 68
R14 | 1317 15 14 14 11 8 18 6 | 78 84 81 78 81 65 77
R15 | 2045 16 12 16 15 18 23 7 | 109 99 90 93 108 86 97
R16 | 2066 24 20 26 21 20 18 10 | 104 93 76 85 97 78 87
R17 | 1304 7 18 13 15 17 19 6 | 36 31 36 40 37 14 33
R18 | 810 11 16 16 16 11 26 7 | 28 34 33 31 28 24 27
R19 | 1082 36 66 19 52 22 36 17 | 62 32 60 61 53 47 50
R20 | 2566 31 90 37 94 14 34 23 | 67 52 50 88 57 37 49
R21 | 1792 9 21 9 18 10 24 7 | 41 34 40 48 43 31 39
R22 | 1477 14 17 14 14 12 12 6 | 22 36 32 27 23 28 25
R24 | 1527 16 24 13 23 18 16 8 | 45 32 42 49 39 31 38
XR26 |14972 34 --- --- 39 43 --- 28 | 52 --- --- 53 73 --- 60
------+-----------------------------------------+-------------------------------------
RMS | 1695 19 31 18 29 15 23 |T 74 67 72 72 72 60 67
WRMS | 1695 16 20 15 19 14 23 |NE 74 67 72 72 72 60 67
MEDI | 1493 15 17 14 16 15 19 |MD 69 52 60 61 67 47 60
Table 3.2343.1 GPS week: 2343 Day: 1 MJD: 60646
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 734 44 45 21 20 17 43 14 | 65 34 46 44 46 35 40
R02 | 1296 23 16 13 14 13 12 7 | 61 48 38 47 34 39 41
R03 | 1697 19 16 15 15 9 19 7 | 71 64 71 66 63 56 64
R04 | 1085 15 8 15 16 11 18 6 | 136 134 139 134 127 134 133
R05 | 1122 13 12 24 17 16 29 8 | 215 217 218 224 202 213 214
R07 | 2599 17 14 15 10 6 13 5 | 69 63 62 70 63 58 63
R08 | 1035 13 15 17 9 20 22 7 | 93 88 84 89 95 90 89
R09 | 2861 13 12 16 13 16 8 6 | 41 47 56 47 36 44 44
R11 | 2239 15 14 26 9 11 19 7 | 32 37 41 51 30 36 30
R12 | 1380 12 18 15 14 11 25 7 | 52 58 57 59 49 41 51
R14 | 913 9 23 7 9 8 11 5 | 54 62 47 51 47 49 50
R15 | 1396 21 10 12 9 15 18 6 | 88 73 75 77 70 62 74
R16 | 1471 20 18 15 12 16 24 8 | 85 78 63 70 73 64 70
XR17 | 1220 12 23 15 11 23 --- 9 | 35 29 26 31 34 --- 29
R18 | 690 10 21 15 9 18 31 8 | 35 30 32 33 25 31 28
R19 | 1049 47 73 18 56 31 39 20 | 53 43 48 58 39 50 45
R20 | 2100 30 77 46 68 19 39 21 | 48 48 44 59 35 35 39
R21 | 1147 9 31 19 14 14 23 8 | 36 39 39 36 38 32 35
R22 | 920 16 8 17 9 12 8 5 | 27 40 40 33 30 39 33
R24 | 533 16 28 9 9 11 20 7 | 32 36 30 32 28 35 30
XR26 |16093 37 --- --- 40 48 --- 30 | 53 --- --- 51 67 --- 56
------+-----------------------------------------+-------------------------------------
RMS | 1519 22 31 19 23 15 24 |T 65 63 62 64 58 60 59
WRMS | 1519 17 27 16 15 13 24 |NE 65 63 62 64 58 60 59
MEDI | 1220 16 16 15 13 15 20 |MD 53 48 47 51 46 44 45
Table 3.2343.2 GPS week: 2343 Day: 2 MJD: 60647
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 819 42 51 15 28 26 40 15 | 59 33 32 33 49 21 31
R02 | 1057 11 13 15 19 13 13 6 | 66 61 60 72 51 58 60
R03 | 1781 20 14 14 16 15 20 7 | 95 82 86 83 73 64 79
R04 | 602 23 12 16 16 15 23 8 | 88 82 82 88 81 78 81
R05 | 1300 21 15 12 16 15 16 7 | 151 153 150 152 143 144 148
R07 | 1239 16 22 11 15 17 19 7 | 77 57 71 66 75 61 68
R08 | 949 16 15 12 17 25 18 8 | 76 79 80 76 93 74 79
R09 | 2610 15 9 14 9 17 8 6 | 19 27 32 24 30 22 24
R11 | 1881 16 19 8 12 15 13 6 | 19 30 66 67 24 17 17
R12 | 1415 12 18 21 12 19 22 8 | 58 67 69 49 54 51 56
R14 | 996 7 21 15 10 9 8 5 | 56 65 52 49 54 55 53
R15 | 816 19 12 16 8 10 12 6 | 80 71 65 68 76 67 70
R16 | 926 22 20 10 11 13 21 7 | 86 87 80 77 70 66 76
XR17 | 1594 14 26 16 17 14 --- 8 | 31 32 33 24 23 --- 25
R18 | 829 9 20 14 14 14 21 7 | 25 26 22 27 26 23 22
R19 | 1342 35 82 26 81 30 50 23 | 54 38 56 57 36 67 47
R20 | 1499 30 78 37 39 15 46 18 | 41 28 45 36 36 32 31
R21 | 598 10 28 21 10 17 20 8 | 28 23 36 33 36 20 28
R22 | 665 16 15 14 7 17 8 6 | 13 23 25 22 20 17 16
R24 | 662 21 24 20 34 13 28 10 | 41 33 39 39 31 29 31
XR26 |18400 28 --- --- 37 50 --- 29 | 46 --- --- 43 60 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1263 21 33 18 26 17 24 |T 57 54 59 56 54 50 51
WRMS | 1263 21 28 15 21 16 24 |NE 57 54 59 56 54 50 51
MEDI | 1057 16 19 15 16 15 20 |MD 56 38 56 49 51 55 49
Table 3.2343.3 GPS week: 2343 Day: 3 MJD: 60648
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 899 44 45 31 49 22 51 17 | 66 44 49 28 40 26 35
R02 | 1152 8 18 10 9 11 15 5 | 45 53 40 39 42 32 40
R03 | 1976 17 16 20 19 10 12 7 | 105 93 105 91 97 91 97
R04 | 769 21 11 17 33 13 17 8 | 122 112 124 105 111 106 113
R05 | 777 19 13 17 23 12 22 7 | 99 88 103 88 90 79 90
R07 | 1863 17 21 8 16 22 35 9 | 100 87 94 95 106 88 95
R08 | 751 8 9 17 11 8 10 4 | 105 103 102 108 106 108 105
R09 | 2229 14 18 13 14 7 11 5 | 20 35 26 22 21 26 22
R11 | 2049 13 15 12 18 12 10 6 | 17 24 92 57 23 18 17
R12 | 1866 12 21 21 18 14 18 7 | 48 56 46 38 40 35 41
R14 | 1165 10 14 11 14 6 15 5 | 56 61 61 59 57 48 56
R15 | 962 9 17 18 15 11 14 6 | 69 69 86 60 77 64 71
R16 | 2515 20 18 19 11 12 14 7 | 69 68 50 51 61 50 57
XR17 | 1518 13 19 12 18 11 --- 7 | 34 36 30 41 28 --- 30
R18 | 705 18 18 17 24 5 18 7 | 25 32 35 29 24 20 24
R19 | 1666 41 89 36 55 12 35 19 | 70 45 77 60 54 49 56
R20 | 3297 31 73 39 45 25 30 17 | 59 38 50 53 49 49 46
R21 | 484 17 30 22 21 10 25 9 | 30 27 40 40 36 27 32
R22 | 1257 15 14 12 17 10 13 6 | 15 21 24 25 18 25 19
R24 | 631 17 30 17 23 9 21 8 | 43 32 43 46 33 34 35
XR26 |19801 46 --- --- 45 45 --- 32 | 39 --- --- 43 64 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1604 21 33 20 26 13 23 |T 58 56 63 56 56 51 53
WRMS | 1604 16 34 16 21 12 23 |NE 58 56 63 56 56 51 53
MEDI | 1257 17 18 17 18 11 17 |MD 56 45 50 51 49 48 46
Table 3.2343.4 GPS week: 2343 Day: 4 MJD: 60649
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 827 55 31 29 46 15 45 17 | 63 20 43 30 30 21 28
R02 | 1413 12 16 13 17 16 12 6 | 57 57 45 64 44 45 50
R03 | 1171 14 17 16 12 14 22 7 | 85 75 79 79 89 64 78
R04 | 1425 20 17 16 30 28 19 10 | 120 120 115 102 114 108 111
R05 | 1022 19 12 10 26 16 20 8 | 199 188 190 196 191 188 192
R07 | 2637 20 13 15 16 15 23 8 | 81 63 75 67 73 59 69
R08 | 569 16 12 17 11 18 22 7 | 73 61 68 64 67 61 64
R09 | 1410 12 16 23 19 13 15 7 | 27 33 39 26 36 31 30
R11 | 1454 16 30 60 21 14 26 14 | 24 42 110 66 32 23 29
R12 | 2093 13 11 14 16 14 18 6 | 59 51 50 46 50 45 49
R14 | 946 11 16 13 13 16 17 6 | 51 57 58 58 45 52 52
R15 | 920 13 25 21 16 18 27 9 | 79 75 89 65 84 66 75
R16 | 2913 14 19 16 26 21 26 9 | 84 92 95 67 95 71 83
R17 | 878 9 13 12 18 11 22 6 | 29 29 28 36 26 17 26
R18 | 1168 15 24 15 19 11 17 7 | 27 37 37 31 28 26 28
R19 | 707 41 65 39 60 23 42 20 | 47 48 62 49 45 44 43
R20 | 2664 36 74 68 51 35 25 22 | 59 46 50 63 55 64 52
R21 | 706 9 28 10 23 13 13 7 | 35 33 35 44 38 35 35
R22 | 1041 15 19 17 13 11 9 6 | 16 24 27 26 27 23 20
R24 | 744 12 36 24 18 19 23 10 | 34 31 45 43 32 33 33
XR26 |13855 38 --- --- 39 56 --- 33 | 32 --- --- 41 73 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1500 22 30 27 27 18 24 |T 61 59 67 60 60 53 56
WRMS | 1500 20 25 20 19 17 24 |NE 61 59 67 60 60 53 56
MEDI | 1168 15 17 16 19 16 22 |MD 57 48 50 58 45 45 49
Table 3.2343.5 GPS week: 2343 Day: 5 MJD: 60650
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 895 48 38 28 32 14 49 16 | 57 47 57 33 30 34 38
R02 | 982 6 17 13 12 10 12 5 | 45 50 50 45 44 40 44
R03 | 523 7 26 9 13 10 17 6 | 115 106 117 117 117 106 113
R04 | 1408 12 16 11 15 12 22 6 | 79 77 83 77 78 72 77
R05 | 2216 18 13 14 20 10 16 7 | 118 122 118 115 119 116 117
R07 | 2541 16 20 13 19 13 21 7 | 85 82 82 72 79 75 79
R08 | 684 13 13 12 15 26 18 8 | 81 80 78 86 100 72 83
R09 | 688 12 25 12 20 14 19 7 | 19 38 31 23 30 23 24
R11 | 2461 11 15 658 13 12 13 6 | 21 48 596 203 30 27 23
R12 | 2400 10 15 13 22 15 12 6 | 59 63 52 52 66 59 57
R14 | 1393 14 8 9 11 13 18 5 | 51 51 60 60 57 51 55
R15 | 1048 14 14 15 13 19 20 7 | 76 67 82 72 67 65 71
R16 | 2250 19 25 13 17 10 21 7 | 78 69 73 78 73 62 71
R17 | 824 11 10 15 12 13 25 6 | 27 25 31 28 19 18 22
R18 | 1309 13 26 10 12 12 21 7 | 23 31 21 28 24 22 22
R19 | 670 39 72 16 56 33 22 18 | 36 43 37 41 34 40 34
R20 | 1195 42 76 56 61 43 45 23 | 29 54 50 52 32 58 35
R21 | 789 6 22 12 25 8 20 7 | 31 29 34 36 27 23 29
R22 | 1573 15 17 20 19 19 13 8 | 19 22 31 24 27 21 20
R24 | 698 10 30 22 11 11 35 9 | 33 26 38 29 26 20 27
XR26 |15544 37 --- --- 40 49 --- 30 | 24 --- --- 44 48 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1485 20 31 148 25 18 24 |T 52 56 86 62 53 50 51
WRMS | 1485 15 20 16 21 17 24 |NE 52 56 86 62 53 50 51
MEDI | 1195 13 17 13 17 13 20 |MD 45 50 52 52 44 40 38
Table 3.2343.6 GPS week: 2343 Day: 6 MJD: 60651
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1109 31 33 27 32 15 19 11 | 79 49 71 43 56 46 54
R02 | 1036 11 11 28 21 11 20 8 | 70 73 81 65 70 60 68
R03 | 944 12 15 26 23 12 22 8 | 120 105 125 111 114 106 114
R04 | 1164 22 23 15 19 18 28 9 | 114 99 104 91 104 85 99
R05 | 2327 11 13 11 18 16 21 6 | 163 165 163 160 163 156 161
R07 | 1725 16 25 16 16 14 20 8 | 87 80 88 73 83 71 80
R08 | 998 12 19 19 16 26 18 8 | 80 74 81 77 89 66 77
R09 | 660 12 19 16 12 11 7 6 | 18 32 27 23 22 24 21
R11 | 2633 18 121 13 608 18 33 22 | 25 48 117 226 28 25 23
R12 | 1951 8 25 11 16 13 16 6 | 73 83 65 64 76 60 69
R14 | 1423 13 14 9 13 18 12 6 | 64 73 68 63 77 65 67
R15 | 1625 15 19 19 43 17 8 9 | 96 75 80 106 87 81 86
R16 | 1053 18 25 13 16 18 21 8 | 94 77 82 88 81 78 83
XR17 | 1368 9 12 13 12 10 --- 5 | 44 40 48 44 40 --- 41
R18 | 1455 20 12 21 21 19 24 9 | 31 46 51 52 40 30 39
R19 | 983 31 86 31 77 39 38 21 | 68 59 75 75 66 59 62
R20 | 2634 23 101 41 81 25 44 23 | 73 75 87 79 69 64 68
R21 | 861 11 31 13 14 10 12 6 | 54 40 55 59 52 45 50
R22 | 1147 11 13 12 9 10 17 5 | 22 24 30 31 22 24 23
R24 | 718 11 28 13 14 15 21 7 | 52 37 51 56 46 38 46
XR26 |12673 30 --- --- 39 52 --- 29 | 41 --- --- 49 63 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1513 17 46 20 143 18 23 |T 69 67 77 77 68 62 65
WRMS | 1513 16 25 15 30 15 23 |NE 69 67 77 77 68 62 65
MEDI | 1164 13 19 15 18 16 20 |MD 70 73 75 65 69 60 67
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