[IGSREPORT-29113] Wk 2240 IGLOS Final Orbits
acc
acc at igs.org
Thu Jan 5 02:00:42 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2240 (Dec 11, 2022 - Dec 17, 2022)
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 2.2240.
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:
igl2240[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2240 in the SP3 format.
igl22407.sum Combination Report for GPS Week 2240.
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. 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.
3. 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).
4. 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
5. 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 | -0.9 ns
1 | -11.5 ns
2 | 0.0 ns
3 | -16.2 ns
4 | 1.9 ns
5 | 1.1 ns
6 | -1.0 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 1.2240, 1a.2240).
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 2.2240.0-6)
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 3.2240.0-6).
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 2240 summary. (Dec 11, 2022 - Dec 17, 2022)
Table 1.2240.a GPS week : 2240 MJD: 59924.0-59930.0
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 0 -10 47 .15 22 17 | 33294 209 3159 8891
| 1 1 1 14 13 20 .02 | 8380 2202
esx n/a| 1 0 2 -15 5 -2 -.20 37 25 | 807 -2 3217 7953
| 2 0 2 13 22 13 .04 | 8265 1758
gfz n/a| 0 2 -3 21 5 -28 -.16 17 14 | 0 452 3149 8890
| 0 1 1 12 19 25 .03 | 0 2222
grg n/a| 1 -4 3 -28 10 -13 .23 31 21 | -4223 400 3206 8200
| 1 0 2 17 21 38 .03 | 7166 1830
iac n/a| 1 0 -5 7 20 37 -.24 27 25 | -1799 -577 3219 9355
| 2 2 3 40 56 120 .07 | 7153 829
Table 1.2240.b GPS week : 2240 MJD: 59924.0-59930.0
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 15 19 22 20 19 20 |
R02 | 10 6 10 9 7 7 10 |
R03 | 9 6 8 8 10 6 6 |
R04 | 11 7 10 10 9 8 9 |
R05 | 9 7 5 7 7 8 8 |
R07 | 9 8 10 5 7 9 12 |
R08 | 9 8 6 7 6 10 7 |
R09 | 26 19 17 18 20 20 18 |
R11 | 14 7 7 7 8 8 8 |
R12 | 13 9 10 6 8 11 5 |
R13 | 17 15 14 18 18 21 17 |
R14 | 8 5 7 7 7 6 7 |
R15 | 13 8 8 8 9 8 9 |
R17 | 8 7 5 6 11 7 6 |
R18 | 13 7 7 6 8 7 9 |
R19 | 31 32 26 26 29 25 28 |
R20 | 34 38 41 41 42 34 31 |
R21 | 13 7 7 7 10 7 8 |
R22 | 139 145 148 148 140 132 134 |
R24 | 10 9 8 6 10 9 9 |
Table 1.2240.c GPS week : 2240 MJD: 59924.0-59930.0
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 2240 0 | 26 -2 -19 -293 1835 1843 82.9 1306 1306 | -923 0
brd 2240 1 | 38 110 -36 1466 698 3554 81.7 1333 1333 | -11479 0
brd 2240 2 | -45 0 -107 -534 -2179 -399 83.6 1395 1395 | 30 0
brd 2240 3 | 56 103 -19 -415 -284 -4855 78.5 1786 1786 | -16221 0
brd 2240 4 | 39 -28 -213 -1631 -1399 -2522 77.4 1684 1684 | 1869 0
brd 2240 5 | 46 -46 -71 396 545 -2346 80.8 1354 1354 | 1111 0
brd 2240 6 | -9 -16 65 -78 605 -4912 81.5 1335 1335 | -1039 0
-------------+------------------------------------------------------------+----------------
brd 2240 mean| 21 17 -57 -155 -25 -1376 80.9 1456 1456 | -3807 0
brd 2240 sdev| 36 63 87 944 1372 3226 2.2 194 194 | 7071 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 2.2240.0 GPS week: 2240 Day: 0 MJD: 59924
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 -15 -2 46 .15 23 18 | 34497 -1678 2681 9756
esx n/a| 6 1 -1 -25 9 -3 -.20 35 24 | 1651 -1707 2649 7653
gfz n/a| 0 5 -2 41 37 -69 -.22 29 25 | 0 -2272 2668 9791
grg n/a| 0 -4 3 -34 7 -19 .21 26 19 | -102 -1746 2656 8901
iac n/a| -1 -1 -3 -34 37 76 -.20 30 32 | 1904 -1060 2668 10136
Table 2.2240.1 GPS week: 2240 Day: 1 MJD: 59925
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 6 -7 63 .12 24 20 | 22017 1450 3499 9390
esx n/a| 0 0 0 -39 21 -17 -.17 33 19 | -12028 534 3484 7351
gfz n/a| 0 2 -2 17 -5 9 -.14 13 11 | 0 2587 3486 9598
grg n/a| -1 -5 1 -13 -25 -51 .27 36 23 | -12781 2232 3438 8490
iac n/a| -1 0 0 5 24 157 -.16 29 24 | -10107 414 3488 9741
Table 2.2240.2 GPS week: 2240 Day: 2 MJD: 59926
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 17 5 60 .16 22 18 | 36755 -404 2826 8702
esx n/a| 1 1 0 -17 -2 -9 -.18 39 19 | 12242 -422 2866 8098
gfz n/a| 2 1 -2 5 -9 -30 -.14 13 11 | 0 -369 2829 8662
grg n/a| 0 -4 5 -25 21 7 .22 35 19 | -191 -215 2861 7877
iac n/a| 1 -1 -2 -27 -29 11 -.15 24 20 | 1834 -1062 2883 9089
Table 2.2240.3 GPS week: 2240 Day: 3 MJD: 59927
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 -3 34 .16 25 18 | 21033 -1154 3240 8847
esx n/a| 2 0 4 -15 -21 8 -.14 36 22 | -7957 -125 3354 8109
gfz n/a| 0 1 -5 10 -22 -4 -.12 14 9 | 0 -220 3217 8673
grg n/a| 0 -5 5 -41 43 -57 .19 33 20 | -16405 321 3369 8289
iac n/a| 2 1 -5 80 -43 -82 -.24 23 21 | -13955 290 3370 9272
Table 2.2240.4 GPS week: 2240 Day: 4 MJD: 59928
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 -12 -9 20 .17 22 18 | 36833 3968 3604 9121
esx n/a| 0 0 4 -1 -24 -12 -.20 36 22 | 1886 3053 3729 8840
gfz n/a| 0 1 -6 35 7 -22 -.14 18 13 | 0 3417 3595 9104
grg n/a| 2 -3 8 -57 7 24 .27 36 24 | -27 3068 3701 8547
iac n/a| 5 1 -6 36 -26 -89 -.25 28 24 | 3285 116 3694 9478
Table 2.2240.5 GPS week: 2240 Day: 5 MJD: 59929
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 -15 -27 31 .12 18 12 | 41310 1515 2901 7337
esx n/a| -1 0 4 0 33 -4 -.24 41 30 | 4001 896 2965 6834
gfz n/a| 0 1 -4 19 17 -43 -.17 18 13 | 0 1930 2892 7309
grg n/a| 4 -5 0 -12 17 40 .18 29 25 | 467 847 2982 6588
iac n/a| 0 -4 -8 10 103 -33 -.37 30 30 | 3824 -1058 2975 7850
Table 2.2240.6 GPS week: 2240 Day: 6 MJD: 59930
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 1 -5 -32 78 .16 20 15 | 40619 -2229 3364 9085
esx n/a| 1 0 3 -10 19 20 -.27 40 40 | 5860 -2244 3473 8786
gfz n/a| 0 2 -3 18 10 -35 -.19 16 13 | 0 -1904 3361 9099
grg n/a| 2 -5 2 -11 -1 -41 .23 25 20 | -528 -1705 3440 8710
iac n/a| 3 3 -10 -19 74 224 -.27 26 25 | 619 -1680 3461 9923
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 3.2240.0 GPS week: 2240 Day: 0 MJD: 59924
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 994 42 45 27 20 33 20 | 122 71 105 89 82 96
R02 | 748 7 17 29 10 17 9 | 91 103 79 93 85 91
R03 | 1346 8 16 20 15 20 8 | 96 88 93 103 92 95
R04 | 549 22 14 25 14 22 11 | 100 91 88 88 85 92
R05 | 1015 10 14 22 14 19 8 | 89 90 93 84 87 88
R07 | 1748 15 13 15 14 20 8 | 115 104 109 108 112 109
R08 | 1728 11 14 23 14 30 9 | 102 104 109 101 102 103
R09 | 3220 26 34 38 66 48 25 | 80 91 95 65 86 71
R11 | 1437 15 13 40 18 24 13 | 27 35 56 29 42 30
R12 | 1100 12 18 36 18 22 12 | 56 59 74 51 71 56
R13 | 509 27 38 25 29 34 17 | 77 55 70 58 60 63
R14 | 697 11 11 20 6 23 7 | 58 68 66 60 67 61
R15 | 606 17 21 35 9 53 12 | 81 63 94 75 68 77
R17 | 1034 10 18 14 13 13 8 | 46 42 45 42 45 44
R18 | 425 17 23 34 11 25 12 | 28 32 53 34 28 32
R19 | 849 52 66 38 52 29 30 | 35 40 50 44 31 34
R20 | 1765 43 99 38 43 59 34 | 48 62 53 62 38 47
R21 | 1153 10 23 34 19 19 12 | 41 41 56 39 38 41
XR22 | 3795 --- 159 --- 122 122 139 | --- 77 --- 41 35 40
R24 | 702 13 22 19 15 13 10 | 33 35 37 36 29 33
------+------------------------------------+--------------------------------
RMS | 1306 23 35 29 26 30 |T 69 67 75 65 64 65
WRMS | 1306 18 24 25 19 32 |NE 69 67 75 65 64 65
MEDI | 1015 15 18 27 15 23 |MD 77 63 74 60 67 61
Table 3.2240.1 GPS week: 2240 Day: 1 MJD: 59925
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 756 31 33 11 31 22 14 | 76 55 73 65 58 67
R02 | 1288 9 15 7 14 11 6 | 65 71 67 63 61 66
R03 | 1005 8 14 6 14 18 5 | 73 64 65 79 60 69
R04 | 617 14 17 8 13 14 7 | 77 70 77 73 67 74
R05 | 925 17 12 9 11 19 7 | 62 71 65 62 64 64
R07 | 1342 10 24 9 15 13 8 | 89 83 95 102 91 92
R08 | 1779 17 14 10 18 17 8 | 79 85 77 76 82 78
R09 | 3375 28 24 15 63 37 18 | 72 80 74 42 73 63
R11 | 1656 12 9 10 12 11 6 | 16 20 28 22 26 21
R12 | 986 14 19 12 15 20 8 | 47 55 36 50 57 43
R13 | 589 17 25 19 44 43 15 | 61 50 67 51 41 58
R14 | 693 9 12 5 12 22 5 | 36 44 40 43 49 40
R15 | 552 17 16 12 11 23 8 | 52 40 46 48 39 46
R17 | 693 12 10 11 16 11 7 | 33 30 28 38 28 30
R18 | 412 14 14 7 10 22 6 | 32 34 39 37 31 35
R19 | 1141 54 69 18 91 51 32 | 31 55 39 56 22 37
R20 | 1889 57 103 36 82 73 38 | 42 111 84 42 38 69
R21 | 1285 18 15 5 9 17 6 | 41 50 48 52 35 45
XR22 | 1677 --- 144 --- 145 157 145 | --- 123 --- 32 38 67
R24 | 953 14 13 12 22 16 8 | 34 34 37 35 26 33
------+------------------------------------+--------------------------------
RMS | 1333 24 33 13 36 29 |T 53 61 57 53 49 54
WRMS | 1333 20 19 11 23 24 |NE 53 61 57 53 49 54
MEDI | 986 14 15 10 15 19 |MD 52 55 65 50 41 58
Table 3.2240.2 GPS week: 2240 Day: 2 MJD: 59926
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 883 45 25 17 43 20 18 | 92 61 62 60 66 67
R02 | 1321 12 26 10 27 22 10 | 68 84 68 57 57 67
R03 | 665 15 15 11 15 9 7 | 77 65 75 75 70 73
R04 | 692 15 25 13 21 13 10 | 83 59 82 64 72 75
R05 | 583 10 9 3 15 23 5 | 60 65 65 65 71 63
R07 | 1239 11 25 14 21 16 9 | 89 73 99 77 91 89
R08 | 882 9 9 8 17 15 6 | 87 96 92 90 86 91
R09 | 3398 23 17 16 56 33 16 | 81 91 93 53 85 80
R11 | 1501 14 11 11 9 19 6 | 19 24 30 23 25 24
R12 | 663 16 20 16 20 27 10 | 48 46 38 36 51 39
R13 | 1144 31 25 17 26 26 14 | 76 59 66 53 52 62
R14 | 511 13 19 8 13 15 7 | 48 65 53 54 50 53
R15 | 555 17 15 9 16 21 8 | 63 50 59 49 57 56
R17 | 1048 7 10 8 12 17 5 | 36 33 34 31 42 32
R18 | 702 10 17 8 12 12 6 | 26 30 27 29 25 26
R19 | 814 33 82 9 64 51 26 | 35 51 49 29 38 37
R20 | 1641 51 127 30 96 41 41 | 39 70 42 48 31 36
R21 | 1620 11 16 6 18 12 6 | 32 25 28 27 30 26
XR22 | 2123 --- 152 --- 143 143 148 | --- 92 --- 60 64 66
R24 | 2681 14 22 6 11 12 7 | 36 25 33 30 23 30
------+------------------------------------+--------------------------------
RMS | 1395 22 39 13 35 24 |T 57 58 57 50 54 54
WRMS | 1395 18 19 11 19 20 |NE 57 58 57 50 54 54
MEDI | 883 14 19 10 18 19 |MD 60 59 59 53 52 56
Table 3.2240.3 GPS week: 2240 Day: 3 MJD: 59927
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1124 54 44 17 38 15 22 | 110 57 83 61 72 79
R02 | 1096 13 22 8 19 15 8 | 74 79 68 62 77 70
R03 | 914 8 17 13 15 28 7 | 91 84 103 84 90 93
R04 | 684 16 19 13 23 21 10 | 91 68 85 70 80 80
R05 | 863 15 7 9 14 11 6 | 72 68 74 78 71 72
R07 | 1388 7 9 6 14 15 5 | 86 78 89 76 79 84
R08 | 681 7 8 10 21 19 7 | 84 84 91 70 77 84
R09 | 3136 22 19 21 59 24 18 | 81 88 92 40 76 76
R11 | 1102 14 11 10 8 17 6 | 35 44 45 39 36 40
R12 | 513 8 12 9 15 19 6 | 50 45 52 47 51 48
R13 | 1348 36 30 23 37 23 17 | 71 48 58 46 58 52
R14 | 814 9 15 7 20 11 7 | 57 68 62 70 57 62
R15 | 517 13 17 8 14 14 7 | 69 60 66 68 71 65
R17 | 822 9 17 7 10 13 6 | 55 65 57 56 53 57
R18 | 527 9 13 7 14 14 6 | 35 38 36 38 34 36
R19 | 746 30 67 21 70 41 26 | 39 45 46 42 33 39
R20 | 4173 65 120 33 76 50 41 | 57 75 55 33 32 45
R21 | 1885 5 14 9 22 22 7 | 40 36 39 36 44 37
XR22 | 4412 --- 147 --- 148 147 147 | --- 45 --- 39 38 36
R24 | 4141 11 13 8 13 23 6 | 37 37 38 38 27 37
------+------------------------------------+--------------------------------
RMS | 1786 25 36 14 33 23 |T 64 60 65 54 57 59
WRMS | 1786 18 22 9 20 21 |NE 64 60 65 54 57 59
MEDI | 914 13 17 9 19 19 |MD 69 60 62 47 57 57
Table 3.2240.4 GPS week: 2240 Day: 4 MJD: 59928
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 747 41 48 12 33 21 19 | 96 46 73 56 61 69
R02 | 855 7 14 7 18 27 6 | 77 83 87 76 79 81
R03 | 898 12 21 20 15 30 10 | 83 68 99 75 67 84
R04 | 1046 14 18 10 22 17 9 | 86 66 86 70 72 79
R05 | 1174 14 7 11 14 19 7 | 69 60 55 58 62 60
R07 | 717 10 15 7 16 24 6 | 88 75 85 91 73 85
R08 | 781 13 12 8 10 19 6 | 79 89 87 90 85 85
R09 | 2281 22 21 23 66 29 19 | 72 86 85 50 72 70
R11 | 636 15 9 10 19 38 7 | 28 36 44 42 38 36
R12 | 1063 14 14 11 11 27 7 | 56 68 72 58 56 63
R13 | 923 40 25 19 39 27 18 | 66 49 52 49 55 51
R14 | 604 8 12 12 18 19 7 | 54 54 45 50 54 49
R15 | 704 16 18 8 19 29 8 | 73 55 66 56 77 63
R17 | 1058 18 9 17 29 21 11 | 72 73 76 65 60 71
R18 | 624 6 17 14 14 15 7 | 34 37 40 34 33 35
R19 | 1301 30 76 21 77 27 28 | 53 48 56 46 47 49
R20 | 4667 54 108 54 80 62 41 | 42 57 44 41 48 37
R21 | 2235 8 26 6 29 15 10 | 39 37 37 46 32 37
XR22 | 4014 --- 131 --- 149 152 140 | --- 74 --- 60 51 70
R24 | 3123 9 21 14 24 20 9 | 43 43 50 47 30 44
------+------------------------------------+--------------------------------
RMS | 1684 22 36 18 36 28 |T 63 60 65 58 57 60
WRMS | 1684 18 22 13 24 24 |NE 63 60 65 58 57 60
MEDI | 923 14 18 12 19 24 |MD 69 57 66 56 56 63
Table 3.2240.5 GPS week: 2240 Day: 5 MJD: 59929
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 948 41 37 19 32 23 19 | 89 55 58 57 70 66
R02 | 866 7 17 10 16 24 7 | 79 90 77 83 76 80
R03 | 1455 8 18 7 12 36 6 | 73 62 72 73 85 71
R04 | 657 12 14 8 23 27 8 | 73 70 65 60 74 67
R05 | 1533 8 19 8 22 25 8 | 66 72 71 55 63 65
R07 | 682 9 30 13 9 43 8 | 78 66 84 78 66 78
R08 | 930 14 14 13 27 27 10 | 71 74 73 98 74 76
R09 | 1991 23 42 26 50 34 19 | 83 84 89 51 74 74
R11 | 695 11 12 14 15 30 7 | 23 31 36 27 40 27
R12 | 1358 19 16 22 14 50 11 | 52 46 75 57 58 58
R13 | 774 35 37 32 44 36 21 | 68 58 70 42 61 59
R14 | 829 6 10 11 13 20 5 | 52 49 59 57 54 54
R15 | 752 11 16 11 16 20 7 | 69 58 59 63 74 63
R17 | 707 7 17 8 20 25 7 | 78 74 77 85 96 78
R18 | 637 9 21 10 12 17 7 | 32 24 31 37 24 31
R19 | 1313 27 78 24 55 35 25 | 34 51 46 41 28 41
R20 | 2802 15 128 38 59 23 34 | 29 33 67 40 20 42
R21 | 1231 6 21 10 11 24 6 | 30 29 31 31 28 30
XR22 | 3324 --- 154 --- 113 122 132 | --- 51 --- 38 46 41
R24 | 2611 8 33 14 11 21 9 | 32 29 38 35 24 31
------+------------------------------------+--------------------------------
RMS | 1354 18 41 18 29 30 |T 58 55 62 55 56 56
WRMS | 1354 12 30 13 25 30 |NE 58 55 62 55 56 56
MEDI | 930 11 19 13 16 25 |MD 68 55 67 55 61 59
Table 3.2240.6 GPS week: 2240 Day: 6 MJD: 59930
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1096 42 49 21 26 34 19 | 138 102 115 106 104 115
R02 | 795 6 34 13 18 22 10 | 115 131 113 111 110 116
R03 | 2061 11 15 6 10 30 6 | 114 106 115 110 125 112
R04 | 888 8 22 14 16 22 8 | 121 110 117 117 116 117
R05 | 1041 13 13 7 18 21 7 | 116 112 112 102 114 111
R07 | 1075 10 29 24 21 30 12 | 127 116 143 120 114 129
R08 | 858 12 11 7 19 31 7 | 121 121 125 133 116 125
R09 | 924 28 24 20 48 39 18 | 113 106 117 86 98 104
R11 | 1525 11 19 14 15 22 8 | 64 74 72 71 70 69
R12 | 1215 9 12 5 11 23 5 | 85 83 92 88 88 87
R13 | 558 19 37 27 33 33 16 | 101 87 108 84 92 95
R14 | 823 9 20 6 15 22 7 | 89 92 91 79 86 87
R15 | 1130 19 23 6 14 21 9 | 104 84 93 88 99 93
R17 | 668 7 18 7 12 19 6 | 109 103 102 107 105 105
R18 | 761 14 24 11 18 15 9 | 48 49 47 60 40 49
R19 | 1350 50 83 20 50 32 28 | 56 56 54 55 45 54
R20 | 2107 25 114 34 43 24 30 | 48 52 61 57 52 52
R21 | 626 14 19 11 12 13 7 | 51 47 47 51 43 49
XR22 | 2742 --- 166 --- 107 112 133 | --- 79 --- 55 54 61
R24 | 3066 15 20 12 16 27 9 | 50 50 52 52 40 50
------+------------------------------------+--------------------------------
RMS | 1335 20 40 16 25 26 |T 93 88 93 86 85 89
WRMS | 1335 15 40 13 20 25 |NE 93 88 93 86 85 89
MEDI | 1041 13 22 12 18 23 |MD 104 87 102 86 92 93
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