[IGSREPORT-28980] Wk 2230 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 21 05:39:37 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2230 (Oct 02, 2022 - Oct 08, 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 2.2230.
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:
igl2230[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2230 in the SP3 format.
igl22307.sum Combination Report for GPS Week 2230.
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.
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 | 0.5 ns
1 | -6.5 ns
2 | -5.6 ns
3 | -6.9 ns
4 | -6.7 ns
5 | -5.2 ns
6 | 0.4 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
----+--------+---------------
6 | ESX | R22
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 1.2230, 1a.2230).
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 2.2230.0-6)
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 3.2230.0-6).
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 2230 summary. (Oct 02, 2022 - Oct 08, 2022)
Table 1.2230.a GPS week : 2230 MJD: 59854.0-59860.0
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 1 -18 9 13 .15 18 14 | 27069 -188 2973 8384
| 0 1 1 10 14 18 .04 | 3994 1347
emx n/a| -1 0 -1 19 1 -32 -.06 37 27 | -3904 -368 2976 8391
| 1 1 2 26 22 37 .06 | 11102 1257
esx n/a| 0 1 0 0 -10 -5 -.07 24 17 | -1290 262 3054 10052
| 1 1 0 15 26 16 .05 | 5215 1036
gfz n/a| 0 0 -1 14 6 20 .02 30 19 | 0 -342 3019 8125
| 1 0 1 13 30 36 .04 | 0 1324
grg n/a| 1 -1 4 5 3 -63 .24 27 21 | -4473 -12 2995 7785
| 1 1 4 18 26 48 .03 | 2992 1305
iac n/a| 0 0 -5 -10 -6 29 -.29 25 23 | -1607 -397 3013 9516
| 1 3 3 20 80 26 .03 | 3074 538
Table 1.2230.b GPS week : 2230 MJD: 59854.0-59860.0
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 | 11 12 12 10 13 11 12 |
R02 | 6 7 7 7 8 6 10 |
R03 | 8 6 6 5 5 5 6 |
R04 | 9 10 7 7 7 8 8 |
R05 | 9 9 8 8 7 7 8 |
R07 | 7 6 6 7 7 7 5 |
R08 | 9 6 7 8 7 7 7 |
R09 | 15 14 14 12 13 12 14 |
R11 | 10 9 8 10 8 10 9 |
R12 | 8 8 9 8 7 8 8 |
R13 | 15 13 17 17 16 14 14 |
R14 | 9 8 7 11 8 8 8 |
R15 | 8 10 6 7 6 7 9 |
R17 | 7 7 8 8 9 8 7 |
R18 | 9 8 7 6 7 8 7 |
R19 | 22 22 21 20 21 21 19 |
R20 | 28 27 30 31 30 28 30 |
R21 | 9 8 7 7 7 8 10 |
R22 | --- --- --- --- --- 0 24 |
R24 | 7 8 9 9 10 7 7 |
R25 | 0 0 0 0 0 --- --- |
Table 1.2230.c GPS week : 2230 MJD: 59854.0-59860.0
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 2230 0 | -71 -27 29 1069 -405 15160 80.9 2086 2086 | 541 0
brd 2230 1 | -2 30 94 -617 779 10360 82.4 2016 2016 | -6516 0
brd 2230 2 | 17 48 0 630 309 -594 83.1 1449 1449 | -5624 0
brd 2230 3 | -25 -80 3 1557 -210 -3682 82.4 1308 1308 | -6860 0
brd 2230 4 | -113 -36 9 -805 -288 -5030 80.3 1424 1424 | -6710 0
brd 2230 5 | 20 -111 113 1314 -751 -9319 80.7 1518 1518 | -5229 0
brd 2230 6 | 114 -42 131 1966 -1073 -8048 80.9 1483 1483 | 391 0
-------------+------------------------------------------------------------+----------------
brd 2230 mean| -8 -31 54 730 -234 -164 81.5 1612 1612 | -4286 0
brd 2230 sdev| 73 56 56 1068 622 9378 1.1 307 307 | 3299 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 2.2230.0 GPS week: 2230 Day: 0 MJD: 59854
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 -6 16 21 .21 19 13 | 32540 347 2817 8322
emx n/a| 0 -2 -1 45 -17 -24 -.03 34 27 | 12422 302 2820 8239
esx n/a| 0 2 1 22 -51 -1 -.13 24 18 | 7974 1594 2842 10582
gfz n/a| 0 0 0 31 -1 -22 .03 37 24 | 0 282 2867 7970
grg n/a| 4 -3 5 -31 53 -142 .20 28 23 | 28 678 2837 7608
iac n/a| 0 3 0 -35 -11 59 -.30 25 24 | 3186 -251 2837 8865
Table 2.2230.1 GPS week: 2230 Day: 1 MJD: 59855
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 -3 1 -15 22 0 .20 18 15 | 25086 -303 3361 8294
emx n/a| -2 0 -2 22 0 0 .01 40 26 | -12536 -872 3383 8255
esx n/a| 0 1 0 1 -1 -3 -.09 22 17 | -2611 112 3364 11484
gfz n/a| -1 -1 0 8 27 44 .04 29 20 | 0 -1087 3411 8161
grg n/a| 1 -1 0 3 4 -67 .26 28 25 | -6479 -472 3361 7704
iac n/a| 1 1 -1 -21 -77 39 -.31 24 21 | -3436 -345 3394 10467
Table 2.2230.2 GPS week: 2230 Day: 2 MJD: 59856
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 -20 -3 30 .12 20 14 | 26263 -311 2838 8369
emx n/a| -1 -2 -6 31 12 -45 -.00 37 28 | -21862 -750 2839 8355
esx n/a| 0 2 1 -20 0 26 -.01 24 16 | -3708 252 2830 7823
gfz n/a| 1 0 0 4 9 61 .01 30 16 | 0 259 2864 8030
grg n/a| 1 -1 7 0 -10 -87 .23 30 22 | -5959 131 2853 7751
iac n/a| 0 -1 -6 7 -33 1 -.24 26 21 | -2742 189 2912 10092
Table 2.2230.3 GPS week: 2230 Day: 3 MJD: 59857
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 0 -4 15 25 .12 24 16 | 24209 -1373 3009 9042
emx n/a| -2 0 -2 -10 0 -30 -.05 39 28 | 2611 -2064 3009 8958
esx n/a| -1 1 0 11 -41 -4 -.12 26 17 | -3530 -1107 3016 12062
gfz n/a| 0 0 0 -7 -20 28 .09 27 16 | 0 -1405 3066 8863
grg n/a| 0 -1 10 23 -36 -88 .25 25 17 | -6334 -1426 3012 8407
iac n/a| 0 -5 -9 4 67 52 -.30 25 23 | -3561 -287 3063 10689
Table 2.2230.4 GPS week: 2230 Day: 4 MJD: 59858
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 -33 -11 30 .10 16 13 | 24148 -1956 2797 8550
emx n/a| -2 2 -3 54 -32 -88 -.10 36 29 | -4577 -1460 2728 8849
esx n/a| -1 0 0 0 3 -13 -.09 21 15 | -4498 -876 2797 11828
gfz n/a| -2 0 -3 23 -33 -12 -.04 20 12 | 0 -2216 2855 8270
grg n/a| 0 0 8 4 1 -30 .23 27 22 | -6027 -1756 2800 7915
iac n/a| 4 2 -6 -39 121 23 -.25 24 24 | -3933 -1510 2792 9174
Table 2.2230.5 GPS week: 2230 Day: 5 MJD: 59859
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 4 -17 26 6 .14 18 14 | 24163 2262 2491 8203
emx n/a| -1 0 2 3 10 -63 -.08 38 26 | -5110 1306 2484 8209
esx n/a| 0 0 0 -20 -8 -24 -.04 25 18 | -6547 389 2936 7103
gfz n/a| 1 0 -2 21 5 -12 .04 31 13 | 0 1771 2547 7888
grg n/a| -1 -2 1 15 6 -2 .21 24 19 | -6311 1928 2490 7876
iac n/a| 0 1 -6 6 -2 44 -.30 24 22 | -3287 -507 2493 8879
Table 2.2230.6 GPS week: 2230 Day: 6 MJD: 59860
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 -28 3 -18 .15 16 12 | 33076 15 3501 7912
emx n/a| 0 0 0 -13 37 23 -.15 36 26 | 1724 961 3572 7877
esx n/a| 1 0 1 -1 24 -17 -.01 27 17 | 3889 1471 3596 9485
gfz n/a| 0 0 -1 19 56 58 .00 36 33 | 0 -2 3529 7697
grg n/a| 1 -3 1 20 8 -23 .27 26 20 | -234 831 3614 7236
iac n/a| -1 3 -7 3 -110 -12 -.33 26 24 | 2524 -69 3601 8451
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 3.2230.0 GPS week: 2230 Day: 0 MJD: 59854
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1152 14 28 31 19 29 24 11 | 83 79 60 74 83 81 74
R02 | 901 9 14 12 14 11 18 5 | 49 44 57 55 56 63 53
R03 | 989 7 12 14 20 16 27 7 | 59 56 58 56 68 75 61
XR04 | 1443 16 10 25 --- 11 16 8 | 67 58 55 --- 54 57 57
R05 | 890 17 23 18 14 15 31 9 | 56 49 48 47 57 57 50
R07 | 1004 11 15 11 18 14 20 6 | 54 51 49 51 57 52 51
R08 | 2530 12 20 22 19 22 21 8 | 52 47 66 63 68 63 58
R09 | 2169 29 24 17 31 55 39 15 | 94 81 89 92 66 93 82
R11 | 1607 16 16 17 28 36 17 10 | 37 32 39 29 39 32 32
R12 | 1519 10 35 12 12 11 23 8 | 74 44 72 75 81 86 72
R13 | 1135 28 47 35 35 37 13 14 | 95 45 64 80 79 71 73
R14 | 1721 12 28 19 27 9 23 8 | 66 44 74 56 73 78 66
R15 | 1075 8 24 16 8 21 23 7 | 83 71 73 87 97 93 83
R17E | 851 10 25 11 18 13 19 7 | 73 74 71 67 74 69 71
R18E | 2718 14 22 18 22 15 28 9 | 54 53 56 55 57 49 52
R19E | 1829 43 58 48 74 48 27 22 | 51 47 65 95 58 52 52
R20E | 5707 36 82 49 112 50 44 27 | 81 65 96 118 93 56 75
R21E | 2286 12 37 11 22 13 21 8 | 72 69 68 73 72 66 69
R24E | 1639 11 26 12 16 18 14 7 | 105 103 108 111 106 103 106
XR25 |11728 --- --- --- --- --- 6 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 2085 19 34 24 37 28 25 |T 68 58 66 71 70 68 65
WRMS | 2085 13 27 18 24 23 24 |NE 66 53 61 63 67 69 62
MEDI | 1519 12 24 17 19 16 21 |MD 67 53 65 67 68 66 66
Table 3.2230.1 GPS week: 2230 Day: 1 MJD: 59855
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 931 19 30 29 29 32 13 11 | 59 63 47 53 71 51 53
R02 | 1185 10 16 12 14 14 20 6 | 36 36 44 38 48 39 38
R03 | 705 9 14 7 14 17 16 5 | 42 39 46 50 55 46 45
XR04 | 746 22 11 17 --- 18 23 10 | 51 45 49 --- 39 40 43
R05 | 774 20 16 18 18 10 27 8 | 47 44 40 34 43 40 39
R07 | 548 8 12 12 10 12 19 5 | 40 40 43 41 32 29 36
R08 | 2456 15 13 13 9 14 12 5 | 36 38 50 45 46 46 42
R09 | 2114 25 18 19 19 60 24 13 | 78 69 77 74 55 75 67
R11 | 1876 19 18 14 15 35 9 8 | 32 35 40 35 55 34 32
R12 | 747 14 36 10 25 9 12 8 | 65 36 52 69 55 62 56
R13 | 1107 31 43 32 19 28 17 12 | 75 32 51 55 64 62 57
R14 | 1918 12 29 21 10 16 15 7 | 53 34 59 47 54 60 51
R15 | 727 12 32 18 14 14 34 9 | 61 52 57 73 70 94 67
R17E | 1210 11 26 13 15 18 15 7 | 70 65 71 65 79 69 68
R18E | 1911 14 17 15 29 19 14 8 | 44 45 42 40 50 41 41
R19E | 1171 18 98 34 60 53 40 22 | 45 62 60 74 53 51 47
R20E | 5860 34 96 55 79 48 54 26 | 69 50 81 96 71 51 59
R21E | 2495 12 32 12 16 13 20 7 | 63 62 63 64 68 64 62
R24E | 1557 12 35 16 17 13 15 8 | 96 95 99 96 95 95 95
XR25 |11745 --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 2016 18 40 22 29 28 24 |T 55 49 56 58 58 55 52
WRMS | 2016 15 26 17 20 25 21 |NE 51 43 50 51 52 52 48
MEDI | 1185 14 26 16 16 17 16 |MD 53 45 51 53 55 51 51
Table 3.2230.2 GPS week: 2230 Day: 2 MJD: 59856
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 693 31 29 24 15 25 24 11 | 67 53 39 49 41 49 48
R02 | 918 10 12 12 14 14 25 6 | 42 40 49 43 36 53 42
R03 | 1461 4 15 7 16 17 17 5 | 47 44 50 48 56 47 47
XR04 | 977 13 9 10 --- 13 17 6 | 52 47 43 --- 42 44 46
R05 | 821 14 16 21 18 16 21 8 | 40 44 52 38 40 40 39
R07 | 541 9 13 12 13 16 15 5 | 43 40 40 40 47 42 41
R08 | 693 9 12 14 14 18 19 6 | 39 38 47 39 45 40 39
R09 | 2537 17 22 15 21 68 28 13 | 73 74 73 75 57 73 65
R11 | 2127 12 17 7 20 37 15 8 | 25 27 30 22 56 23 26
R12 | 624 8 41 19 17 23 17 9 | 64 34 70 66 85 68 64
R13 | 1021 28 54 46 38 41 27 17 | 86 59 51 98 70 86 73
R14 | 1807 9 32 20 10 15 9 7 | 55 36 67 63 62 52 56
R15 | 1141 8 27 11 11 17 13 6 | 71 62 67 74 76 73 70
R17E | 623 11 28 13 15 13 26 8 | 70 68 75 77 67 59 68
R18E | 1017 10 21 14 14 18 12 6 | 36 41 39 39 48 40 37
R19E | 1233 22 83 30 62 47 41 20 | 35 42 46 86 57 56 43
R20E | 2910 58 77 64 85 49 62 29 | 61 54 95 98 70 75 60
R21E | 1740 7 27 12 17 16 14 6 | 49 43 52 50 55 53 49
R24E | 1214 13 35 15 13 25 21 8 | 63 59 61 62 61 63 59
XR25 |18300 --- --- --- --- --- 5 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1449 20 37 24 30 30 26 |T 53 47 55 59 56 54 51
WRMS | 1449 14 28 16 16 22 21 |NE 54 46 52 54 54 53 50
MEDI | 1021 11 27 14 15 18 17 |MD 52 44 51 50 56 53 48
Table 3.2230.3 GPS week: 2230 Day: 3 MJD: 59857
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 580 26 36 19 22 18 18 10 | 75 66 71 68 61 64 66
R02 | 878 11 10 7 11 11 28 6 | 40 39 44 39 42 64 43
R03 | 2209 7 13 9 10 12 14 5 | 54 49 56 51 49 54 52
XR04 | 967 9 15 9 --- 16 22 7 | 49 51 47 --- 40 53 46
R05 | 1004 14 21 13 16 19 25 8 | 40 45 47 36 46 43 40
R07 | 748 14 15 13 9 16 25 7 | 48 36 41 39 42 38 39
R08 | 547 10 15 21 15 17 26 8 | 41 37 55 47 39 50 43
R09 | 2304 16 16 25 26 43 26 12 | 69 69 71 73 42 73 61
R11 | 2292 22 20 18 26 19 27 10 | 21 23 26 25 24 29 14
R12 | 1289 15 33 11 15 19 12 7 | 53 31 54 64 71 52 54
R13 | 678 24 55 46 33 40 21 16 | 97 41 52 99 109 85 81
R14 | 1184 11 43 22 28 13 24 10 | 59 31 68 81 65 48 59
R15 | 1235 8 22 11 15 18 18 6 | 65 52 67 65 74 61 64
R17E | 1092 9 32 13 7 14 22 7 | 68 67 67 67 69 67 66
R18E | 918 8 23 13 15 13 13 6 | 27 27 29 25 39 26 26
R19E | 1064 18 85 34 50 49 30 19 | 37 36 45 76 48 41 39
R20E | 1266 80 89 73 73 43 47 31 | 62 92 100 101 75 84 63
R21E | 794 13 27 13 14 13 16 7 | 76 80 72 74 74 78 74
R24E | 1376 14 29 12 21 13 29 8 | 122 118 118 113 131 128 121
XR25 |21432 --- --- --- --- --- 8 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1307 24 39 26 27 25 25 |T 58 52 59 63 60 59 55
WRMS | 1307 16 28 17 16 17 23 |NE 54 43 53 57 54 54 50
MEDI | 1064 14 23 13 15 17 22 |MD 54 45 55 65 49 54 54
Table 3.2230.4 GPS week: 2230 Day: 4 MJD: 59858
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 866 29 36 28 23 26 27 12 | 67 58 58 65 52 53 57
XR02 | 653 12 --- 22 11 14 20 8 | 36 --- 57 43 36 44 41
R03 | 2490 9 9 8 11 11 14 4 | 47 49 52 50 54 61 50
XR04 | 1137 11 18 7 --- 23 13 7 | 52 58 51 --- 40 44 48
R05 | 2103 9 19 19 14 14 24 7 | 47 51 54 50 38 42 45
R07 | 1383 10 15 20 11 10 21 6 | 45 40 32 36 40 50 38
R08 | 961 11 17 9 15 18 19 6 | 43 35 46 59 48 57 47
R09 | 2018 14 36 27 30 51 19 13 | 79 74 84 87 37 90 73
R11 | 1858 15 25 14 15 19 19 7 | 15 25 28 20 28 20 18
R12 | 1091 11 28 10 12 18 14 6 | 51 30 51 45 53 52 47
R13 | 602 30 50 42 31 41 20 15 | 86 41 43 77 88 59 66
R14 | 942 9 32 21 13 13 21 8 | 53 30 61 59 54 43 51
R15 | 1401 6 24 10 11 17 17 6 | 69 60 66 71 75 71 68
R17E | 889 11 31 17 11 13 35 8 | 62 60 65 70 74 68 65
R18E | 820 12 28 11 11 15 19 7 | 30 25 35 34 45 38 32
R19E | 1734 22 91 39 44 63 41 21 | 47 34 46 67 53 47 39
XR20E | 958 44 --- 79 75 49 35 29 | 64 --- 100 96 70 53 68
R21E | 948 11 29 17 14 12 15 7 | 57 56 66 68 62 66 61
R24E | 958 18 37 13 17 18 37 10 | 94 95 93 96 90 82 90
XR25 | 2885 --- --- --- --- --- 6 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1423 16 36 21 20 27 24 |T 54 48 57 60 54 54 52
WRMS | 1423 13 29 15 12 22 24 |NE 53 45 52 55 49 52 49
MEDI | 961 11 28 17 14 18 19 |MD 52 49 54 59 53 53 50
Table 3.2230.5 GPS week: 2230 Day: 5 MJD: 59859
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1669 25 23 28 26 16 20 10 | 56 43 55 43 50 44 47
R02 | 668 8 15 12 8 9 22 5 | 32 30 37 32 28 39 31
R03 | 1980 11 14 13 9 10 10 5 | 39 37 56 53 46 46 45
XR04 | 926 11 19 10 --- 9 27 7 | 45 52 46 --- 43 24 40
R05 | 1762 14 15 20 14 11 15 6 | 37 42 48 47 37 35 38
R07 | 1183 11 12 8 8 7 29 6 | 42 40 50 49 49 65 47
R08 | 1115 14 20 9 23 11 19 7 | 38 41 42 50 38 49 41
R09 | 2670 16 26 21 21 46 22 12 | 78 86 83 84 47 80 73
R11 | 2283 20 12 23 18 34 18 10 | 29 30 31 31 38 28 23
R12 | 1516 12 31 14 10 11 26 7 | 47 40 49 44 50 62 47
R13 | 1282 24 44 33 26 36 33 14 | 61 38 40 48 68 60 51
R14 | 1010 11 25 19 13 13 25 7 | 49 35 48 44 52 37 43
R15 | 2109 9 26 18 17 15 12 7 | 74 69 65 81 87 75 74
R17E | 936 10 31 10 15 17 22 7 | 64 67 66 67 65 66 64
R18E | 1724 12 24 18 15 15 26 8 | 39 40 44 38 41 48 39
R19E | 745 28 84 31 63 44 37 21 | 45 58 62 97 48 50 50
R20E | 906 36 97 68 93 45 40 28 | 58 57 80 75 65 36 49
R21E | 846 10 32 20 9 18 20 8 | 72 76 72 71 78 77 72
XR22E | 2226 --- --- 2 --- --- --- 0 | --- --- 106 --- --- --- 146
R24E | 921 14 29 14 15 13 14 7 | 171 173 175 173 165 176 172
------+-----------------------------------------+-------------------------------------
RMS | 1517 18 38 25 31 24 24 |T 56 55 62 62 57 57 59
WRMS | 1517 14 26 18 13 19 22 |NE 48 44 50 50 48 49 46
MEDI | 1183 12 25 18 15 15 22 |MD 47 42 50 49 49 49 47
Table 3.2230.6 GPS week: 2230 Day: 6 MJD: 59860
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 2513 21 26 43 22 19 20 11 | 78 76 60 68 70 76 69
R02 | 819 11 20 14 21 9 43 9 | 48 43 51 51 50 83 52
R03 | 914 5 12 13 6 22 21 6 | 55 50 55 56 65 58 55
XR04 | 1052 8 23 8 --- 16 21 7 | 62 64 61 --- 58 57 59
R05 | 1141 13 14 23 17 14 24 8 | 60 56 70 61 58 72 60
R07 | 1279 5 10 8 17 13 12 4 | 63 60 64 65 67 64 63
R08 | 1167 12 15 12 26 12 15 6 | 58 61 67 79 58 65 62
R09 | 3102 24 20 22 23 57 25 14 | 86 83 83 82 61 80 74
R11 | 1589 15 17 19 20 29 22 9 | 32 33 35 30 43 35 29
R12 | 1648 13 29 17 21 12 17 8 | 73 47 67 70 67 71 65
R13 | 1168 25 49 29 27 29 33 14 | 93 48 59 75 90 80 74
R14 | 732 10 26 16 8 13 25 7 | 64 37 70 64 71 53 61
R15 | 1374 10 26 19 21 22 31 9 | 88 74 76 97 101 86 86
R17E | 1242 6 23 14 22 17 19 7 | 81 80 77 80 82 76 78
R18E | 1417 10 20 19 23 13 13 7 | 47 46 52 50 52 47 47
R19E | 1251 20 79 32 55 37 36 18 | 58 74 68 105 65 63 65
R20E | 933 29 84 71 120 50 43 29 | 78 64 79 126 91 56 69
R21E | 1267 12 39 26 18 16 22 9 | 83 75 74 76 85 82 78
XR22E | 2600 --- 51 348 --- 23 27 24 | --- 11 94 --- 17 14 99
R24E | 1095 12 26 12 15 13 22 7 | 159 154 158 159 160 163 158
------+-----------------------------------------+-------------------------------------
RMS | 1482 16 36 27 36 26 26 |T 71 61 71 77 70 69 70
WRMS | 1482 12 26 17 33 20 24 |NE 66 56 62 66 66 67 62
MEDI | 1242 12 23 19 21 16 22 |MD 64 60 67 70 65 65 65
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