[IGSREPORT-29704] Wk 2296 IGLOS Final Orbits
acc
acc at igs.org
Sun Jan 28 12:26:26 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2296 (Jan 07, 2024 - Jan 13, 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 2.2296.
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:
igl2296[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2296 in the SP3 format.
igl22967.sum Combination Report for GPS Week 2296.
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).
The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
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 | -1.8 ns
2 | -1.0 ns
3 | -0.4 ns
4 | 0.5 ns
5 | 2.1 ns
6 | -2.7 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 | COD | R25
0 | ESA | R25
0 | GFZ | R25
0 | GRG | R25
0 | IAC | R25
0 | JGX | R25
1 | ESA | R20
4 | ESA | R20
6 | COD | R26
6 | ESA | R26
6 | GFZ | R26
6 | GRG | R26
6 | IAC | R26
6 | JGX | R26
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 1.2296, 1a.2296).
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 2.2296.0-6)
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 3.2296.0-6).
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 2296 summary. (Jan 07, 2024 - Jan 13, 2024)
Table 1.2296.a GPS week : 2296 MJD: 60316.0-60322.0
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 0 -24 -10 88 .09 22 20 | 39478 -319 3635 8794
| 1 1 2 17 19 23 .06 | 2473 2797
esa n/a| 0 0 0 -11 9 1 -.13 40 26 | 1578 -542 3622 8322
| 0 0 2 17 13 13 .03 | 5352 2731
gfz n/a| 0 0 5 32 0 -15 -.02 24 16 | 0 -436 3635 7931
| 1 1 3 19 18 35 .05 | 0 2913
grg n/a| 0 -3 -5 -1 -18 -45 .28 31 23 | -521 -445 3590 7416
| 1 0 2 17 21 37 .06 | 1002 2810
iac n/a| -2 0 -4 4 18 -4 -.16 23 20 | 962 -264 3636 8837
| 1 1 2 31 33 68 .08 | 1066 1299
jgx n/a| 0 0 0 10 17 -41 -.29 32 30 | 43095 -68 3570 8460
| 0 1 2 18 16 68 .09 | 1859 3092
Table 1.2296.b GPS week : 2296 MJD: 60316.0-60322.0
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 | 20 19 14 18 18 16 19 |
R02 | 7 7 9 8 9 10 9 |
R03 | 9 10 8 8 7 10 8 |
R04 | 8 8 7 6 8 9 8 |
R05 | 7 7 9 8 7 6 7 |
R07 | 7 8 8 7 7 10 10 |
R08 | 8 8 7 7 7 8 7 |
R09 | 7 7 8 6 11 9 8 |
R11 | 8 7 5 8 9 6 7 |
R12 | 10 10 9 8 6 7 8 |
R13 | 23 21 23 20 22 20 16 |
R14 | 7 7 7 5 6 10 9 |
R15 | 11 9 8 11 9 11 10 |
R16 | 7 9 10 9 8 9 9 |
R17 | 14 9 9 10 10 10 10 |
R18 | 8 8 10 9 9 7 8 |
R19 | 24 21 19 25 24 26 23 |
R20 | 44 36 37 34 29 45 41 |
R21 | 9 10 8 10 10 14 13 |
R22 | 8 8 9 6 7 7 7 |
R24 | 11 14 10 12 12 13 15 |
R25 | --- 13 14 11 11 14 10 |
Table 1.2296.c GPS week : 2296 MJD: 60316.0-60322.0
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 2296 0 | 76 63 91 2370 2449 4585 79.7 1440 1440 | -1016 0
brd 2296 1 | 54 71 -50 1817 1390 6152 80.4 1426 1426 | -1781 0
brd 2296 2 | -62 52 26 347 -426 4149 81.0 1557 1557 | -1000 0
brd 2296 3 | 0 32 -14 -241 -687 5995 81.8 1325 1325 | -370 0
brd 2296 4 | -48 -1 -193 149 -1301 -177 81.1 1616 1616 | 459 0
brd 2296 5 | 12 -29 -48 -968 -1529 46 82.1 1581 1581 | 2068 0
brd 2296 6 | -7 -114 -95 -1063 -2149 771 81.0 1624 1624 | -2723 0
-------------+------------------------------------------------------------+----------------
brd 2296 mean| 3 10 -40 344 -322 3074 81.0 1509 1509 | -623 0
brd 2296 sdev| 50 66 90 1313 1658 2783 .8 113 113 | 1555 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 2.2296.0 GPS week: 2296 Day: 0 MJD: 60316
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -1 -39 -16 109 .09 25 24 | 40769 -1057 2773 7685
esa n/a| -1 0 2 15 29 11 -.15 39 20 | -2161 -1438 2758 8388
gfz n/a| 2 2 1 37 -14 32 -.06 27 16 | 0 -1181 2765 7582
grg n/a| 0 -2 -8 -5 9 8 .35 36 23 | -836 -835 2773 6994
iac n/a| -1 1 -7 -42 36 85 -.24 29 23 | 1383 153 2764 7960
jgx n/a| -1 0 2 33 20 -134 -.17 27 27 | 44140 -689 2690 7970
Table 2.2296.1 GPS week: 2296 Day: 1 MJD: 60317
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 -2 -26 -7 97 .00 21 21 | 37523 -3997 3241 7853
esa n/a| 0 0 0 -1 2 17 -.17 46 25 | 4626 -4322 3249 6937
gfz n/a| -1 0 4 23 6 38 .05 22 16 | 0 -4019 3307 7235
grg n/a| 1 -3 -6 16 -40 -67 .21 31 23 | 78 -4216 3281 6806
iac n/a| 0 0 -2 -22 0 0 -.11 21 18 | -480 -1560 3238 8095
jgx n/a| 1 -2 1 15 11 -139 -.21 33 29 | 41415 -3580 3252 7359
Table 2.2296.2 GPS week: 2296 Day: 2 MJD: 60318
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 -1 -25 1 111 .10 24 22 | 35283 1247 3442 7985
esa n/a| 0 0 0 -24 22 1 -.12 37 24 | 1672 1205 3432 8294
gfz n/a| 1 2 4 13 -17 -21 -.04 18 12 | 0 962 3238 6672
grg n/a| 0 -4 -8 21 -31 -20 .28 33 28 | -1970 705 3108 5911
iac n/a| -3 0 -6 12 -22 12 -.18 26 22 | -167 -716 3424 7907
jgx n/a| 0 1 1 20 17 -42 -.24 29 27 | 40199 1479 2754 5982
Table 2.2296.3 GPS week: 2296 Day: 3 MJD: 60319
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 2 -30 98 .11 20 16 | 38581 573 3381 7717
esa n/a| 0 1 0 -32 13 -12 -.13 37 25 | -528 103 3387 7664
gfz n/a| -1 0 3 4 25 -36 -.00 20 17 | 0 1415 3433 6851
grg n/a| 3 -4 -3 11 -44 -93 .35 32 24 | -1430 1425 3415 6526
iac n/a| -1 0 -2 5 6 9 -.17 22 18 | 865 -213 3375 7711
jgx n/a| 0 0 -1 1 6 -13 -.33 31 29 | 42278 334 3265 6366
Table 2.2296.4 GPS week: 2296 Day: 4 MJD: 60320
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 -1 -49 -36 48 .19 18 17 | 41937 238 4563 9746
esa n/a| 0 0 -3 -4 0 15 -.14 48 28 | 12184 -323 4560 8583
gfz n/a| -1 0 6 49 20 -26 -.00 20 14 | 0 83 4638 8374
grg n/a| 0 -3 -5 -10 5 -69 .28 31 26 | 1003 19 4649 8088
iac n/a| -4 1 -3 15 -9 -71 -.01 19 18 | 2713 -24 4566 9531
jgx n/a| 1 0 0 21 38 -6 -.28 33 30 | 44682 700 4771 8611
Table 2.2296.5 GPS week: 2296 Day: 5 MJD: 60321
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 -12 -8 87 .09 22 18 | 40319 4144 4638 10602
esa n/a| 1 0 -2 -5 -6 -7 -.12 36 31 | -2858 3955 4648 9694
gfz n/a| 0 0 11 50 -21 -45 -.09 38 19 | 0 3826 4646 9672
grg n/a| 1 -3 -5 -19 -7 -63 .30 28 17 | 51 3616 4594 9151
iac n/a| -3 -1 -1 5 70 -117 -.18 23 19 | 1420 2189 4665 10612
jgx n/a| 0 2 -1 -22 36 22 -.40 32 30 | 43631 5140 4746 13454
Table 2.2296.6 GPS week: 2296 Day: 6 MJD: 60322
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 3 -21 22 66 .03 25 20 | 41940 -3387 3412 9970
esa n/a| -1 1 -3 -29 1 -13 -.06 39 26 | -1889 -2980 3326 8694
gfz n/a| 1 2 4 51 2 -48 .00 23 15 | 0 -4140 3422 9133
grg n/a| 1 -3 -2 -20 -23 -9 .20 26 19 | -546 -3833 3316 8440
iac n/a| 0 1 -3 58 44 45 -.26 23 21 | 1006 -1678 3420 10043
jgx n/a| 0 0 -3 3 -9 19 -.39 36 36 | 45324 -3863 3512 9479
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 3.2296.0 GPS week: 2296 Day: 0 MJD: 60316
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1636 36 23 61 39 42 20 20 | 89 108 133 105 97 96 101
XR02 | 895 10 12 12 15 16 --- 7 | 50 53 55 61 56 --- 52
R03E | 1236 19 17 18 20 13 14 9 | 78 84 83 78 80 82 79
R04E | 494 13 13 16 13 18 19 7 | 84 84 84 90 85 89 85
R05E | 1828 11 15 12 14 28 15 6 | 95 97 99 102 102 97 97
R07E | 552 12 12 13 14 22 13 6 | 57 60 60 57 60 56 57
R08E | 2949 11 23 11 22 22 14 8 | 118 117 123 131 117 120 120
R09 | 894 19 14 9 8 23 11 6 | 41 44 39 38 34 44 39
R11 | 1072 9 12 18 20 21 15 7 | 44 47 45 50 37 50 46
R12 | 1361 22 13 18 28 24 16 10 | 42 34 37 32 41 33 33
R13 | 1844 53 21 21 48 20 67 23 | 60 40 40 36 38 58 41
R14 | 633 8 17 6 9 14 19 6 | 45 46 40 40 42 33 39
R15 | 878 24 31 9 17 23 18 10 | 58 45 45 46 50 38 44
R16 | 776 16 20 9 13 22 8 6 | 57 41 45 47 49 43 45
XR17 | 1256 12 32 31 15 18 --- 14 | 123 118 143 124 125 --- 127
R18 | 762 13 12 20 10 27 18 8 | 48 58 65 59 67 45 54
R19 | 1225 34 65 19 81 38 25 23 | 83 52 83 99 86 67 71
R20 | 2095 59 136 76 96 72 65 43 | 123 80 157 135 145 105 114
R21 | 569 13 20 18 19 23 20 9 | 64 48 77 72 72 51 62
R22 | 1776 19 10 16 20 18 14 8 | 31 32 38 35 30 27 30
R24 | 1911 18 31 18 20 16 21 10 | 78 54 85 83 78 62 73
------+-----------------------------------------+-------------------------------------
RMS | 1439 25 39 27 36 29 27 |T 67 63 75 72 69 62 67
WRMS | 1439 24 20 16 23 23 27 |NE 60 52 66 63 61 50 58
MEDI | 1225 16 17 18 19 22 18 |MD 58 53 65 61 60 56 57
Table 3.2296.1 GPS week: 2296 Day: 1 MJD: 60317
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1782 20 41 48 25 35 42 18 | 74 95 103 76 82 78 81
XR02 | 475 10 17 8 12 16 --- 7 | 29 33 37 33 36 --- 31
R03E | 1764 15 14 23 22 18 22 9 | 59 55 57 62 57 55 55
R04E | 1131 14 11 18 12 15 24 8 | 53 53 53 54 53 59 53
R05E | 931 13 11 12 17 18 15 7 | 65 68 71 69 66 71 68
R07E | 1118 11 10 15 22 16 18 7 | 54 47 50 55 56 54 49
R08E | 2530 13 16 13 19 15 21 8 | 65 69 65 68 65 56 64
R09 | 689 17 12 12 10 13 14 6 | 36 38 32 37 35 42 35
R11 | 752 8 11 17 9 23 19 6 | 41 48 38 44 44 64 43
R12 | 707 12 18 17 36 16 12 10 | 28 42 40 18 36 33 30
R13 | 2816 48 24 11 43 20 69 20 | 50 26 34 25 19 27 32
R14 | 1072 15 9 12 10 22 18 6 | 37 33 26 26 35 22 27
R15 | 853 20 10 11 8 19 29 8 | 39 30 33 31 21 24 31
R16 | 594 23 21 12 14 17 16 9 | 40 24 25 31 24 28 26
XR17 | 1275 10 22 13 15 20 --- 9 | 84 82 91 88 98 --- 85
R18 | 543 11 9 9 21 13 25 7 | 37 40 35 52 42 32 38
R19 | 1234 35 50 26 61 20 34 21 | 43 40 42 56 35 37 35
R20 | 1803 36 182 39 84 42 86 35 | 61 69 73 112 81 101 88
R21 | 684 11 22 25 11 14 19 9 | 39 34 47 38 43 34 37
R22 | 1626 15 11 13 24 14 13 7 | 25 33 37 31 27 31 29
R24 | 1636 14 30 36 26 22 26 13 | 43 45 70 54 63 52 49
XR25 |14962 13 12 --- --- 15 --- 13 | 22 25 --- --- 23 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1426 21 46 22 31 21 33 |T 46 46 50 50 47 47 45
WRMS | 1426 21 25 16 23 18 29 |NE 40 40 44 45 41 40 39
MEDI | 1118 14 14 13 19 17 21 |MD 41 40 42 52 42 42 37
Table 3.2296.2 GPS week: 2296 Day: 2 MJD: 60318
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1369 27 23 29 18 42 37 14 | 79 85 93 73 83 88 81
XR02 | 1101 14 17 15 17 13 --- 9 | 40 41 35 48 38 --- 37
R03E | 2878 11 17 12 25 19 15 8 | 60 65 57 60 59 56 57
R04E | 1621 12 17 13 17 18 11 7 | 49 53 52 58 45 50 50
R05E | 554 18 21 12 30 17 10 9 | 79 92 87 79 83 84 83
R07E | 1213 9 16 11 22 16 16 7 | 57 52 54 66 66 63 56
R08E | 2271 15 14 12 15 11 13 6 | 50 55 47 51 48 47 48
R09 | 1100 17 13 11 17 15 16 7 | 32 32 33 29 30 37 30
XR11 | 1778 9 12 5 10 24 --- 5 | 40 42 47 43 42 --- 41
R12 | 567 17 11 12 27 15 23 9 | 40 36 32 30 37 22 30
R13 | 3038 50 24 17 52 27 72 22 | 60 36 36 25 45 53 36
R14 | 958 14 10 9 15 11 16 6 | 43 35 36 42 39 34 36
R15 | 1076 25 17 9 12 19 18 8 | 52 40 42 42 38 35 41
R16 | 1016 26 24 9 13 26 24 10 | 49 36 38 44 48 30 36
XR17 | 1579 15 18 11 17 11 --- 8 | 98 94 92 94 95 --- 94
R18 | 569 11 16 13 26 17 29 9 | 38 45 39 58 43 28 38
R19 | 958 25 62 17 56 35 27 19 | 68 39 72 76 64 57 61
R20 | 1992 53 125 49 85 51 61 37 | 86 50 86 113 96 53 66
R21 | 706 11 23 15 15 9 18 8 | 51 34 50 52 43 42 46
R22 | 1412 23 13 12 20 20 13 8 | 31 33 36 40 28 28 31
R24 | 1514 18 26 15 22 42 19 9 | 54 48 57 52 73 45 51
XR25 |17631 13 15 --- --- 23 --- 14 | 24 24 --- --- 23 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1556 24 37 18 33 26 29 |T 53 48 53 55 53 47 48
WRMS | 1556 22 24 12 28 22 27 |NE 50 41 48 52 48 38 43
MEDI | 1213 15 17 12 18 18 18 |MD 50 41 47 52 45 45 41
Table 3.2296.3 GPS week: 2296 Day: 3 MJD: 60319
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1008 25 23 30 51 39 48 17 | 74 70 85 73 58 74 72
XR02 | 2168 11 14 15 15 12 --- 8 | 33 32 32 37 29 --- 30
R03E | 1988 15 15 16 18 23 16 8 | 40 45 46 49 45 39 41
R04E | 863 9 12 11 17 17 13 6 | 40 49 43 45 38 50 43
R05E | 1111 13 9 19 19 19 12 7 | 59 47 48 59 57 52 51
R07E | 753 8 15 13 18 16 15 7 | 46 49 51 49 52 51 47
R08E | 1316 9 20 11 15 22 10 6 | 43 52 44 45 41 44 44
R09 | 2113 12 8 10 18 19 13 6 | 27 26 34 21 19 26 25
XR11 | 2582 12 17 15 9 29 --- 8 | 24 23 34 26 32 --- 25
R12 | 472 19 13 8 23 16 16 8 | 28 29 31 24 24 25 25
R13 | 1054 34 22 14 52 35 68 20 | 46 44 47 36 35 44 41
R14 | 547 5 13 6 12 15 7 4 | 30 40 31 28 31 31 31
R15 | 910 12 9 29 23 14 29 11 | 43 43 68 32 47 29 44
R16 | 1302 17 18 9 15 15 27 8 | 50 50 46 46 37 31 43
XR17 | 1184 9 17 15 30 15 --- 10 | 110 104 106 127 113 --- 109
R18 | 622 9 28 12 20 17 18 8 | 45 59 44 51 52 37 44
R19 | 1396 25 88 36 59 36 30 24 | 91 42 108 89 92 83 82
R20 | 2626 52 107 43 65 32 68 33 | 107 56 105 101 102 53 81
R21 | 645 8 22 20 17 11 27 9 | 53 40 59 63 57 35 50
R22 | 1619 11 12 10 11 14 16 6 | 27 33 35 42 29 27 31
R24 | 1207 14 33 15 29 15 29 11 | 68 52 68 73 59 45 61
XR25 |17928 10 12 --- --- 20 --- 11 | 14 21 --- --- 25 --- 14
------+-----------------------------------------+-------------------------------------
RMS | 1325 20 37 20 32 22 31 |T 49 45 55 53 48 43 47
WRMS | 1325 16 25 17 24 18 29 |NE 49 43 56 53 48 38 46
MEDI | 1184 12 15 15 18 17 16 |MD 43 44 46 46 41 39 43
Table 3.2296.4 GPS week: 2296 Day: 4 MJD: 60320
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1507 31 26 28 57 34 46 18 | 73 77 71 111 74 62 72
XR02 | 2162 6 14 17 20 18 --- 8 | 42 41 46 36 41 --- 39
R03E | 1210 13 13 11 14 18 18 6 | 45 46 41 48 49 50 43
R04E | 945 14 18 16 15 18 15 8 | 46 47 50 49 40 39 44
R05E | 516 10 13 16 11 18 19 7 | 66 68 72 69 68 59 66
R07E | 781 13 11 12 15 13 17 6 | 47 45 42 48 44 39 43
R08E | 1625 12 17 10 19 19 14 7 | 53 58 56 53 58 51 53
R09 | 2576 23 13 11 25 13 38 11 | 31 40 40 26 30 59 35
R11 | 4597 12 20 17 19 19 17 8 | 41 33 46 42 40 23 36
R12 | 919 9 12 14 11 19 14 6 | 31 31 19 34 29 34 26
R13 | 715 33 18 22 65 15 74 21 | 43 24 44 23 39 35 32
R14 | 573 8 12 6 15 11 16 5 | 35 34 25 26 30 26 28
R15 | 1175 14 20 14 21 12 21 8 | 42 65 46 35 46 52 46
R16 | 477 13 13 16 13 20 24 8 | 52 55 58 53 49 45 52
XR17 | 1142 18 17 10 22 17 --- 9 | 136 120 127 117 134 --- 126
R18 | 738 11 18 12 21 14 25 8 | 37 46 43 36 41 27 37
R19 | 1058 33 76 25 55 37 33 23 | 82 41 85 96 73 69 71
R20 | 2104 23 184 50 57 23 73 29 | 96 41 125 107 92 75 108
R21 | 1130 9 22 25 15 10 22 9 | 52 41 62 53 47 40 50
R22 | 1262 13 13 13 20 14 16 7 | 16 21 28 24 19 19 18
R24 | 1194 23 29 18 19 15 33 12 | 67 54 70 66 57 42 60
XR25 |18774 9 12 --- --- 12 --- 11 | 19 23 --- --- 21 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 1616 18 48 20 31 19 33 |T 52 47 56 54 50 44 50
WRMS | 1616 17 28 14 26 18 30 |NE 51 44 57 51 49 42 48
MEDI | 1142 13 17 16 19 17 21 |MD 45 41 46 48 44 42 43
Table 3.2296.5 GPS week: 2296 Day: 5 MJD: 60321
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1324 30 25 35 30 31 41 16 | 51 65 67 50 74 72 54
XR02 | 1259 17 12 23 17 23 --- 10 | 27 31 44 37 38 --- 30
R03E | 1327 10 11 33 21 16 16 9 | 43 42 54 42 52 46 42
R04E | 872 12 20 21 22 21 13 8 | 43 40 46 50 43 42 41
R05E | 813 10 14 15 8 14 14 6 | 95 87 87 91 93 92 90
R07E | 1490 16 19 18 27 15 12 9 | 43 44 51 60 51 46 46
R08E | 1545 10 15 19 14 35 18 7 | 54 58 56 55 67 55 54
R09 | 1632 15 11 20 11 12 27 8 | 41 52 56 43 40 47 45
R11 | 4246 10 10 14 11 18 17 6 | 42 44 53 39 37 54 45
R12 | 1710 13 14 15 10 21 14 6 | 25 22 20 23 26 22 18
R13 | 659 19 29 21 53 20 60 19 | 37 37 46 50 40 31 37
R14 | 593 11 12 22 15 19 32 9 | 33 30 40 26 36 25 28
R15 | 1137 20 16 19 15 18 34 11 | 37 30 32 26 28 30 28
R16 | 626 16 11 19 18 18 23 8 | 41 46 46 32 40 44 39
XR17 | 1865 18 21 12 15 24 --- 10 | 109 111 106 120 114 --- 110
R18 | 1007 8 14 13 16 19 21 7 | 37 47 44 46 41 40 41
R19 | 1232 43 72 38 53 22 46 25 | 70 36 74 68 56 42 54
R20 | 1899 61 116 132 65 54 68 44 | 75 43 98 59 71 56 46
R21 | 764 9 34 43 22 12 25 13 | 41 32 68 50 42 35 41
R22 | 1701 12 8 18 13 20 19 7 | 22 21 33 31 24 22 22
R24 | 1491 21 33 26 16 19 32 13 | 54 40 55 52 34 35 46
XR25 |15017 13 16 --- --- 23 --- 14 | 21 27 --- --- 29 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 1581 22 36 38 28 23 32 |T 47 44 56 50 48 44 44
WRMS | 1581 18 31 19 17 19 30 |NE 44 40 54 46 43 37 40
MEDI | 1324 13 15 20 16 19 23 |MD 41 40 53 50 40 42 41
Table 3.2296.6 GPS week: 2296 Day: 6 MJD: 60322
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 934 29 42 45 27 39 47 19 | 66 69 72 68 62 70 63
XR02 | 929 14 11 13 22 14 --- 9 | 62 61 62 66 60 --- 60
R03E | 1445 9 15 12 19 19 22 7 | 90 95 88 91 90 92 89
R04E | 932 9 18 12 23 21 14 8 | 85 87 80 90 84 83 84
R05E | 934 11 11 11 11 22 22 6 | 123 128 127 123 129 129 125
R07E | 1640 10 18 24 23 20 20 10 | 49 50 57 61 53 53 51
R08E | 1814 8 14 8 20 23 21 7 | 105 101 104 112 102 102 104
R09 | 1406 14 22 15 11 15 20 8 | 41 57 45 43 42 52 44
R11 | 3475 11 11 17 8 12 18 6 | 51 56 64 51 52 48 55
R12 | 1593 16 10 8 23 23 15 7 | 49 44 46 38 46 44 43
R13 | 632 33 24 15 31 14 53 16 | 68 47 52 54 53 38 51
R14 | 716 10 14 21 15 20 25 8 | 51 49 62 43 45 52 50
R15 | 947 24 10 7 10 17 35 9 | 57 44 44 42 48 36 44
R16 | 992 23 16 13 14 18 25 9 | 58 50 48 46 45 41 47
XR17 | 1359 8 26 15 14 20 --- 9 | 164 152 166 162 164 --- 161
R18 | 1387 10 14 14 13 14 29 8 | 57 69 65 65 62 49 60
R19 | 1934 39 60 20 54 40 56 23 | 100 45 97 111 98 76 85
R20 | 2946 72 133 59 61 39 79 41 | 129 51 146 119 125 74 102
R21 | 715 9 31 28 16 11 36 12 | 76 54 94 82 75 52 73
R22 | 1912 14 11 13 15 15 14 7 | 27 30 33 35 30 27 28
R24 | 1223 28 42 20 18 24 43 15 | 100 59 94 93 74 58 82
XR25 | 9953 8 12 --- --- 29 --- 10 | 38 41 --- --- 43 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1623 25 39 23 26 23 36 |T 74 65 78 75 71 61 69
WRMS | 1623 20 26 15 19 21 36 |NE 70 56 74 70 66 49 63
MEDI | 1359 11 15 15 18 20 25 |MD 62 54 65 66 60 52 60
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