[IGSREPORT-30244] Wk 2344 IGLOS Final Orbits
acc
acc at igs.org
Mon Dec 30 11:05:28 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2344 (Dec 08, 2024 - Dec 14, 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 2.2344.
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:
igl2344[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2344 in the SP3 format.
igl23447.sum Combination Report for GPS Week 2344.
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 | -1.0 ns
1 | -6.6 ns
2 | -0.4 ns
3 | 0.6 ns
4 | -2.8 ns
5 | -5.3 ns
6 | -1.8 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2344, 1a.2344).
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 2.2344.0-6)
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 3.2344.0-6).
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 2344 summary. (Dec 08, 2024 - Dec 14, 2024)
Table 1.2344.a GPS week : 2344 MJD: 60652.0-60658.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 1 -3 4 0 51 .15 19 16 | 7315 -571 3197 10607
| 1 0 1 19 9 13 .02 | 2722 2022
esa n/a| 1 0 -1 -4 6 -12 -.15 31 22 | 1300 -717 3170 7398
| 1 1 1 7 9 26 .03 | 3956 2580
gfz n/a| 0 0 0 18 32 -9 -.04 23 18 | 0 -227 3152 7749
| 1 1 1 19 17 16 .05 | 0 2146
grg n/a| 1 0 6 -16 -38 6 .29 28 21 | -4137 -319 3199 10237
| 1 1 1 19 20 35 .03 | 2029 2158
jgx n/a| 0 0 0 -5 -4 -30 -.19 20 20 | 9737 -270 3149 7855
| 1 1 2 19 12 20 .04 | 2777 2217
Table 1.2344.b GPS week : 2344 MJD: 60652.0-60658.0
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 19 17 19 23 19 18 |
R02 | 7 9 8 6 7 5 6 |
R03 | 12 11 11 9 11 7 7 |
R04 | 9 11 8 11 10 10 8 |
R05 | 7 9 7 7 10 9 11 |
R07 | 10 7 7 7 9 8 8 |
R08 | 7 10 8 6 6 8 8 |
R09 | 6 7 6 8 7 7 7 |
R11 | 8 6 7 6 7 8 7 |
R12 | 8 8 8 8 7 6 7 |
R14 | 7 8 8 7 8 8 8 |
R15 | 7 8 7 6 8 7 8 |
R16 | 9 10 10 10 9 9 8 |
R17 | 6 8 6 8 10 9 9 |
R18 | 10 6 8 8 8 9 8 |
R19 | 22 22 24 27 28 26 21 |
R20 | 28 29 27 29 30 23 27 |
R21 | 10 10 11 11 10 11 11 |
R22 | 6 6 6 6 9 7 6 |
R24 | 8 10 9 11 8 12 13 |
R26 | 17 14 8 14 11 14 21 |
Table 1.2344.c GPS week : 2344 MJD: 60652.0-60658.0
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 2344 0 | 41 -46 -226 52 -498 -6095 77.3 1424 1424 | -977 0
brd 2344 1 | -20 -60 -63 -1133 -401 -7555 78.6 1396 1396 | -6642 0
brd 2344 2 | -18 35 -134 -1162 -790 -13100 79.4 1345 1345 | -426 0
brd 2344 3 | 32 -49 -110 -1538 -375 -7812 80.5 1321 1321 | 586 0
brd 2344 4 | -29 34 -24 -2772 -72 -19290 77.4 1460 1460 | -2810 0
brd 2344 5 | -18 -15 -162 -1990 -629 -9483 78.9 1323 1323 | -5283 0
brd 2344 6 | 20 69 -91 -340 565 -5540 79.8 1376 1376 | -1819 0
-------------+------------------------------------------------------------+----------------
brd 2344 mean| 1 -4 -116 -1268 -314 -9839 78.8 1377 1377 | -2481 0
brd 2344 sdev| 29 51 66 956 447 4863 1.2 52 52 | 2633 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 2.2344.0 GPS week: 2344 Day: 0 MJD: 60652
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 -4 25 4 42 .15 17 14 | 5876 1851 3004 10053
esa n/a| 0 1 -4 -8 10 19 -.14 31 20 | -2515 1898 3052 6360
gfz n/a| 0 0 0 52 56 -12 .04 21 19 | 0 2201 2973 7391
grg n/a| 1 0 8 -2 -60 35 .32 31 23 | -3788 2003 3013 9606
jgx n/a| 1 -2 1 -38 -21 -49 -.25 17 17 | 7941 1897 2923 7695
Table 2.2344.1 GPS week: 2344 Day: 1 MJD: 60653
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 1 -4 0 10 37 .14 20 16 | 2785 -3274 3404 9924
esa n/a| 0 1 -1 -9 4 -7 -.16 29 19 | -302 -3574 3357 7191
gfz n/a| 0 0 1 11 30 -5 -.01 21 22 | 0 -2638 3355 7472
grg n/a| 3 0 7 13 -51 -26 .32 30 20 | -6678 -3053 3418 9489
jgx n/a| 1 -2 0 13 7 -20 -.18 21 21 | 5214 -2655 3360 7638
Table 2.2344.2 GPS week: 2344 Day: 2 MJD: 60654
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 18 7 50 .13 19 16 | 8841 -403 3294 11690
esa n/a| 0 1 -3 -3 -8 1 -.12 29 22 | 5919 748 3236 8901
gfz n/a| 0 -1 -1 36 6 -24 -.09 21 16 | 0 814 3251 8968
grg n/a| 2 1 4 -34 -15 61 .28 29 22 | -2549 579 3313 11337
jgx n/a| 0 1 2 -10 -11 -64 -.20 20 20 | 10853 925 3226 9077
Table 2.2344.3 GPS week: 2344 Day: 3 MJD: 60655
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 -23 -15 58 .16 19 17 | 11690 -1228 3389 10739
esa n/a| 0 0 0 7 16 -14 -.20 35 29 | 6886 -2181 3374 7552
gfz n/a| -1 0 -2 19 22 2 -.07 21 15 | 0 -860 3376 8277
grg n/a| 2 -1 5 -33 -10 -8 .33 29 20 | -655 -1186 3359 10403
jgx n/a| 0 0 1 15 -1 -23 -.15 20 20 | 14299 -1171 3382 7979
Table 2.2344.4 GPS week: 2344 Day: 4 MJD: 60656
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 16 -8 70 .14 18 15 | 6952 1007 3165 10038
esa n/a| 3 0 -2 0 0 -66 -.14 33 25 | 2256 1453 3122 7202
gfz n/a| 2 -2 -1 -2 55 -31 -.06 29 18 | 0 1509 3133 6897
grg n/a| 0 0 7 -30 -29 31 .27 27 28 | -5194 1450 3165 9651
jgx n/a| -1 1 0 -19 -5 -8 -.19 23 23 | 9432 1693 3109 7059
Table 2.2344.5 GPS week: 2344 Day: 5 MJD: 60657
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 -2 -17 1 63 .19 19 18 | 7226 -2988 2823 11287
esa n/a| 2 0 0 -4 6 -13 -.14 27 19 | 285 -4338 2752 7460
gfz n/a| 1 -1 -1 7 29 -12 -.07 25 16 | 0 -3441 2706 7848
grg n/a| 0 1 7 -2 -53 -29 .23 25 18 | -5641 -3187 2825 10966
jgx n/a| -2 -1 -3 2 -11 -11 -.23 20 20 | 10237 -3631 2750 8048
Table 2.2344.6 GPS week: 2344 Day: 6 MJD: 60658
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 -1 15 -2 35 .13 18 15 | 7835 1033 3303 10520
esa n/a| 0 -1 0 -15 18 -8 -.16 29 21 | -3425 972 3303 7122
gfz n/a| 0 1 1 5 28 17 -.04 22 19 | 0 822 3275 7394
grg n/a| 1 -1 4 -25 -50 -16 .29 25 18 | -4454 1156 3305 10212
jgx n/a| 0 0 -3 0 15 -35 -.16 21 21 | 10189 1050 3299 7491
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 3.2344.0 GPS week: 2344 Day: 0 MJD: 60652
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 981 30 30 23 20 28 13 | 82 57 75 65 55 63
R02 | 1168 10 13 19 17 14 7 | 83 91 90 80 70 81
R03 | 954 15 13 34 21 24 11 | 115 104 129 98 94 107
R04 | 1156 21 12 14 22 16 9 | 102 84 91 72 70 84
R05 | 2490 15 14 12 16 11 6 | 111 106 114 104 100 106
R07 | 866 17 23 22 15 18 9 | 100 98 105 98 90 97
R08 | 756 13 15 14 16 14 7 | 100 105 109 103 95 101
R09 | 1882 12 13 10 12 12 6 | 27 35 30 30 33 29
R11 | 950 13 15 26 12 7 8 | 21 24 38 22 23 22
R12 | 1348 8 23 18 24 7 8 | 60 64 57 50 56 56
R14 | 1548 14 19 16 12 8 7 | 71 76 66 55 64 66
R15 | 950 15 12 12 17 10 6 | 96 86 92 81 82 87
R16 | 1723 17 17 21 15 18 9 | 91 80 72 78 81 80
XR17 | 1464 9 13 9 11 --- 6 | 70 64 66 73 --- 66
R18 | 1703 10 9 31 15 23 10 | 55 64 74 69 47 59
R19 | 1381 21 74 23 66 27 21 | 98 50 99 112 88 88
R20 | 2232 31 86 33 94 27 27 | 109 71 107 136 99 99
R21 | 696 13 32 18 24 16 10 | 83 64 86 91 67 77
R22 | 1672 14 10 10 15 8 6 | 36 35 41 42 38 37
R24 | 890 11 26 13 18 10 7 | 82 67 85 89 75 79
XR26 | 8016 13 --- --- 22 --- 17 | 36 --- --- 40 --- 34
------+------------------------------------+--------------------------------
RMS | 1423 17 31 21 31 17 |T 77 71 81 75 69 72
WRMS | 1423 14 20 19 23 17 |NE 77 71 81 75 69 72
MEDI | 1348 14 15 18 17 14 |MD 83 67 85 78 70 79
Table 3.2344.1 GPS week: 2344 Day: 1 MJD: 60653
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1298 32 40 43 27 38 18 | 66 45 72 48 47 53
R02 | 897 12 9 22 18 23 9 | 70 67 82 62 50 66
R03 | 1231 17 18 27 12 26 10 | 92 85 103 98 75 90
R04 | 1372 24 12 16 18 27 10 | 69 58 61 54 44 56
R05 | 1617 16 21 13 21 16 8 | 78 87 80 66 72 76
R07 | 1061 16 15 10 12 17 7 | 71 62 65 76 59 65
R08 | 866 12 17 25 15 19 9 | 79 75 96 90 69 80
R09 | 2549 14 9 12 17 16 7 | 27 28 32 28 32 27
R11 | 925 12 12 11 11 10 5 | 16 22 26 14 22 18
R12 | 839 14 18 10 26 10 8 | 45 44 37 34 39 38
R14 | 834 10 21 13 21 8 7 | 50 58 43 40 49 47
R15 | 713 18 10 14 18 10 7 | 75 68 58 61 67 65
R16 | 1323 23 17 25 16 12 9 | 63 50 43 59 48 51
R17 | 1370 10 19 8 19 19 7 | 35 38 38 46 46 36
R18 | 2532 9 11 14 11 15 6 | 28 33 36 34 29 31
R19 | 967 44 57 16 62 36 22 | 49 37 42 39 26 33
R20 | 1548 34 84 43 93 32 29 | 55 41 36 80 31 40
R21 | 729 8 27 20 21 20 9 | 38 39 40 46 37 38
R22 | 2180 15 11 7 16 10 6 | 21 26 24 26 23 22
R24 | 824 14 29 16 26 17 10 | 44 36 47 50 36 41
XR26 | 8782 12 --- --- 16 --- 14 | 21 --- --- 27 --- 21
------+------------------------------------+--------------------------------
RMS | 1396 20 29 21 30 21 |T 52 49 53 51 45 47
WRMS | 1396 16 19 22 20 21 |NE 52 49 53 51 45 47
MEDI | 1231 14 17 14 18 17 |MD 50 44 43 48 44 41
Table 3.2344.2 GPS week: 2344 Day: 2 MJD: 60654
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1379 33 37 35 22 39 17 | 67 40 65 45 31 46
R02 | 948 11 15 14 15 18 7 | 69 62 66 72 50 62
R03 | 1009 16 21 27 23 20 11 | 75 60 85 60 58 67
R04 | 1294 18 12 13 19 18 8 | 72 62 68 59 51 62
R05 | 845 16 13 15 12 13 7 | 79 77 71 75 65 72
R07 | 874 16 18 12 13 11 7 | 64 43 50 58 45 51
R08 | 997 15 14 15 26 10 8 | 60 63 75 84 58 66
R09 | 2168 12 12 10 13 11 5 | 16 24 23 18 23 18
R11 | 1500 10 11 12 20 17 7 | 18 24 26 25 22 19
R12 | 1246 9 18 12 23 15 7 | 57 68 63 51 52 57
R14 | 1190 8 19 14 20 12 7 | 51 59 50 39 54 49
R15 | 764 18 11 13 10 13 7 | 82 89 86 80 74 81
R16 | 1170 23 17 17 7 22 9 | 82 86 76 77 74 77
R17 | 1213 10 13 11 17 11 6 | 55 45 50 63 38 52
R18 | 1935 12 24 9 18 15 7 | 45 54 46 54 39 45
R19 | 1167 37 71 30 66 39 24 | 88 56 74 91 77 76
R20 | 2152 35 74 54 79 30 27 | 80 54 81 105 69 75
R21 | 690 11 28 16 27 23 10 | 60 46 60 70 54 57
R22 | 2031 12 12 10 11 9 5 | 26 28 31 34 29 28
R24 | 734 18 23 17 21 11 9 | 62 58 70 64 59 62
XR26 | 9736 7 --- --- 8 --- 8 | 28 --- --- 28 --- 26
------+------------------------------------+--------------------------------
RMS | 1345 19 29 21 29 20 |T 58 54 60 59 51 54
WRMS | 1345 16 22 16 22 20 |NE 58 54 60 59 51 54
MEDI | 1190 15 17 14 19 15 |MD 62 56 65 60 52 57
Table 3.2344.3 GPS week: 2344 Day: 3 MJD: 60655
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1196 33 46 42 26 41 19 | 73 50 86 58 41 58
R02 | 1699 12 13 9 12 13 6 | 73 72 76 68 61 69
R03 | 2044 16 21 16 14 17 8 | 78 57 75 72 58 68
R04 | 1134 28 14 17 20 21 10 | 80 62 52 61 57 61
R05 | 1392 14 13 8 15 15 6 | 104 105 103 104 92 100
R07 | 950 19 13 13 10 13 7 | 72 56 56 59 51 58
R08 | 960 12 13 12 15 8 6 | 74 69 80 84 72 75
R09 | 2255 12 11 18 20 11 7 | 28 32 37 32 26 28
R11 | 1277 11 12 13 16 9 6 | 36 43 41 38 40 38
R12 | 1784 16 13 12 14 18 7 | 42 46 41 39 43 41
R14 | 810 9 20 14 17 7 6 | 53 60 46 42 46 48
R15 | 825 10 14 9 12 9 5 | 61 58 65 56 55 59
R16 | 920 22 16 14 15 24 9 | 67 68 69 49 46 58
R17 | 1368 10 16 13 24 12 7 | 63 56 59 69 45 59
R18 | 703 12 16 9 25 12 7 | 47 60 51 66 47 51
R19 | 1520 30 94 19 84 33 26 | 101 50 95 125 89 92
R20 | 1494 29 97 54 68 44 29 | 86 46 101 107 68 81
R21 | 1053 8 24 26 17 23 10 | 69 58 79 78 61 68
R22 | 725 13 15 13 8 11 6 | 31 32 42 37 30 33
R24 | 859 24 26 17 27 17 11 | 71 68 75 73 57 66
XR26 | 8892 12 --- --- 15 --- 13 | 47 --- --- 43 --- 43
------+------------------------------------+--------------------------------
RMS | 1321 19 35 21 29 20 |T 64 57 66 64 54 59
WRMS | 1321 17 29 15 20 20 |NE 64 57 66 64 54 59
MEDI | 1196 13 15 13 16 13 |MD 69 57 65 61 51 59
Table 3.2344.4 GPS week: 2344 Day: 4 MJD: 60656
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1213 39 44 59 34 51 23 | 66 46 90 44 35 52
R02 | 2697 7 19 13 16 12 6 | 66 81 74 70 61 68
R03 | 1877 12 16 33 22 19 10 | 78 64 90 70 62 71
R04 | 1155 25 19 11 22 19 10 | 71 53 54 54 46 54
R05 | 1595 25 15 12 18 20 9 | 114 92 95 99 95 99
R07 | 857 15 15 20 16 18 8 | 59 44 56 51 42 49
R08 | 738 12 12 10 11 12 6 | 55 58 55 56 57 55
R09 | 1146 13 15 12 19 7 7 | 25 31 29 28 25 24
R11 | 1285 14 11 9 7 18 6 | 22 28 30 28 34 26
R12 | 1850 11 13 10 13 19 7 | 50 49 40 54 38 45
R14 | 913 7 19 15 12 20 7 | 52 63 62 46 38 51
R15 | 972 14 20 15 12 18 8 | 80 89 91 76 74 81
R16 | 785 19 17 14 19 18 9 | 80 84 77 65 71 75
R17 | 1049 16 12 21 17 28 10 | 50 54 49 51 35 46
R18 | 827 11 15 19 16 13 7 | 36 44 48 40 34 38
R19 | 2213 25 90 47 67 40 27 | 84 32 97 92 61 72
R20 | 1943 30 85 81 66 37 30 | 74 38 98 83 59 66
R21 | 1844 11 27 26 17 16 9 | 52 42 61 57 46 51
R22 | 1418 12 9 19 16 23 8 | 25 33 39 35 26 28
R24 | 727 11 24 15 16 14 8 | 56 53 59 63 59 57
XR26 |14288 9 --- --- 13 --- 11 | 54 --- --- 60 --- 56
------+------------------------------------+--------------------------------
RMS | 1459 18 33 29 27 23 |T 59 53 64 58 49 55
WRMS | 1459 15 25 18 28 23 |NE 59 53 64 58 49 55
MEDI | 1213 13 16 15 16 18 |MD 56 49 59 56 46 54
Table 3.2344.5 GPS week: 2344 Day: 5 MJD: 60657
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 768 42 27 43 38 33 18 | 50 27 50 39 27 32
R02 | 2383 7 15 9 10 9 5 | 45 56 50 54 46 49
R03 | 1054 12 13 12 14 12 6 | 56 57 62 60 52 56
R04 | 998 22 14 22 18 19 9 | 65 54 66 51 45 54
R05 | 680 21 15 16 21 12 9 | 75 67 71 56 56 63
R07 | 1159 19 14 12 12 17 7 | 54 42 48 46 39 44
R08 | 604 17 10 16 18 13 7 | 53 45 43 38 42 42
R09 | 1202 16 13 16 12 13 7 | 32 40 40 29 33 32
R11 | 939 11 17 20 12 17 8 | 27 40 26 32 44 32
R12 | 2194 13 9 12 12 11 6 | 43 44 52 41 43 43
R14 | 899 9 15 8 18 23 8 | 42 47 41 48 35 42
R15 | 880 17 16 12 9 12 6 | 70 60 72 61 57 63
R16 | 855 16 18 16 19 15 8 | 74 71 80 61 69 70
R17 | 1339 17 9 12 15 26 8 | 38 34 35 40 21 32
R18 | 832 17 18 20 16 17 9 | 30 31 32 32 22 25
R19 | 2308 24 66 46 73 39 25 | 37 37 57 49 31 36
R20 | 1665 38 70 56 36 28 23 | 48 36 49 42 41 36
R21 | 1589 7 28 33 18 19 11 | 42 38 58 49 35 42
R22 | 1212 12 14 13 15 10 6 | 19 21 29 29 19 21
R24 | 632 11 34 28 25 21 12 | 41 33 53 48 33 39
XR26 |17351 13 --- --- 14 --- 13 | 44 --- --- 56 --- 47
------+------------------------------------+--------------------------------
RMS | 1323 19 27 25 25 20 |T 46 44 50 45 39 42
WRMS | 1323 18 19 16 18 20 |NE 46 44 50 45 39 42
MEDI | 1054 16 15 16 16 17 |MD 44 40 50 48 39 42
Table 3.2344.6 GPS week: 2344 Day: 6 MJD: 60658
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1019 39 31 32 35 35 17 | 66 45 69 46 37 46
R02 | 1111 9 20 13 10 9 6 | 61 68 61 63 53 59
R03 | 696 13 13 13 14 15 7 | 81 69 84 76 66 74
R04 | 1151 17 14 10 14 17 7 | 78 72 71 64 54 67
R05 | 678 16 12 26 26 21 10 | 92 81 95 73 70 81
R07 | 1550 15 18 16 16 18 8 | 74 51 70 59 54 61
R08 | 712 12 15 19 17 16 8 | 67 64 72 64 57 64
R09 | 1122 13 12 13 16 11 6 | 34 38 39 33 33 33
R11 | 966 12 12 10 18 11 6 | 24 35 28 40 31 29
R12 | 2145 19 11 9 12 14 7 | 67 67 59 56 55 60
R14 | 857 12 9 11 19 23 8 | 62 60 62 62 51 58
R15 | 1416 12 16 18 8 19 7 | 90 81 92 85 78 85
R16 | 541 18 20 11 9 17 8 | 99 83 87 81 89 88
R17 | 860 14 15 19 10 27 9 | 71 61 69 67 36 63
R18 | 847 10 17 13 11 22 7 | 53 66 59 61 44 55
R19 | 3024 22 65 42 49 24 20 | 91 55 104 110 81 86
R20 | 2729 33 82 43 67 34 26 | 88 58 95 113 73 81
R21 | 818 10 29 23 20 21 10 | 74 56 88 89 63 74
R22 | 1154 9 16 9 16 7 6 | 27 30 33 38 26 29
R24 | 724 14 37 30 15 25 12 | 79 54 86 86 61 73
XR26 |18285 19 --- --- 23 --- 21 | 47 --- --- 75 --- 57
------+------------------------------------+--------------------------------
RMS | 1376 18 29 22 25 21 |T 67 59 71 68 55 63
WRMS | 1376 15 21 19 18 21 |NE 67 59 71 68 55 63
MEDI | 1019 14 16 13 16 18 |MD 71 60 70 64 54 63
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