[IGSREPORT-29550] Wk 2282 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 20 06:13:15 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2282 (Oct 01, 2023 - Oct 07, 2023)
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 2.2282.
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:
igl2282[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2282 in the SP3 format.
igl22827.sum Combination Report for GPS Week 2282.
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 | -17.1 ns
1 | -13.7 ns
2 | -15.3 ns
3 | -13.6 ns
4 | -15.4 ns
5 | -17.0 ns
6 | -13.5 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 1.2282, 1a.2282).
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 2.2282.0-6)
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 3.2282.0-6).
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 2282 summary. (Oct 01, 2023 - Oct 07, 2023)
Table 1.2282.a GPS week : 2282 MJD: 60218.0-60224.0
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 0 4 -6 -12 44 .09 20 15 | 21331 -844 2699 8643
| 0 0 0 8 10 17 .03 | 2009 1730
esa n/a| 0 1 -2 -16 -15 7 -.12 24 18 | -13005 -907 2691 7105
| 1 0 2 13 6 21 .03 | 7148 1521
gfz n/a| 0 0 4 23 5 5 -.13 23 14 | 0 -789 2713 7886
| 1 0 1 7 15 18 .02 | 0 2241
grg n/a| 1 -2 -7 0 23 -73 .19 23 18 | -14790 -778 2701 7344
| 1 0 1 15 10 24 .04 | 1107 1951
jgx n/a| -1 2 0 16 -8 -25 -.21 32 32 | 25009 -953 2719 8161
| 1 2 1 24 32 51 .07 | 2216 1816
Table 1.2282.b GPS week : 2282 MJD: 60218.0-60224.0
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 | 15 13 14 17 13 17 9 |
R02 | 7 8 8 8 6 7 9 |
R03 | 9 8 7 8 8 5 6 |
R04 | 7 8 8 10 8 8 10 |
R05 | 10 9 10 7 8 5 7 |
R07 | 7 5 7 10 8 7 7 |
R08 | 8 6 5 9 8 7 8 |
R09 | 7 7 7 7 11 10 15 |
R11 | 10 6 9 10 10 11 12 |
R12 | 8 11 7 7 7 11 9 |
R13 | 19 16 17 18 15 20 22 |
R14 | 7 6 7 6 9 9 8 |
R15 | 6 11 9 10 9 10 7 |
R16 | 10 11 9 10 9 9 9 |
R17 | 10 8 7 11 11 7 10 |
R18 | 10 12 10 10 8 8 9 |
R19 | 27 24 29 31 27 32 36 |
R20 | 30 24 28 32 27 38 33 |
R21 | 9 8 9 7 11 8 7 |
R22 | 11 9 9 9 9 8 9 |
R24 | 10 12 13 9 7 9 10 |
R25 | 17 17 12 11 13 14 9 |
R26 | 86 63 82 79 78 84 81 |
Table 1.2282.c GPS week : 2282 MJD: 60218.0-60224.0
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 2282 0 | -38 -20 109 -395 810 -13900 80.6 1905 1905 | -17139 0
brd 2282 1 | 85 5 218 -229 1480 -7923 79.4 1929 1929 | -13715 0
brd 2282 2 | -1 -3 160 1907 859 3360 81.8 1595 1595 | -15256 0
brd 2282 3 | 14 80 135 444 992 4340 81.5 1562 1562 | -13571 0
brd 2282 4 | 15 -4 16 1101 -1642 5455 81.4 1566 1566 | -15420 0
brd 2282 5 | 18 54 99 -290 -1553 5728 80.7 1488 1488 | -17024 0
brd 2282 6 | -56 -7 33 -2713 -2147 603 80.9 1665 1665 | -13539 0
-------------+------------------------------------------------------------+----------------
brd 2282 mean| 5 14 110 -25 -171 -333 80.9 1672 1672 | -15094 0
brd 2282 sdev| 45 37 70 1454 1532 7618 .8 174 174 | 1564 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 2.2282.0 GPS week: 2282 Day: 0 MJD: 60218
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 4 -4 -2 33 .08 19 15 | 19517 -2079 2750 8104
esa n/a| -2 1 -1 -10 -18 14 -.10 24 17 | -18205 -2364 2747 7032
gfz n/a| 0 2 7 24 11 -1 -.11 27 15 | 0 -2127 2749 7770
grg n/a| 2 -2 -5 11 16 -76 .13 19 15 | -16342 -1746 2733 7399
jgx n/a| -2 6 0 1 -76 -16 -.24 34 33 | 22119 -1697 2822 7940
Table 2.2282.1 GPS week: 2282 Day: 1 MJD: 60219
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 5 2 -19 54 .16 22 18 | 24149 183 2683 8735
esa n/a| 0 1 -1 -12 -5 10 -.12 19 15 | -13326 663 2690 5871
gfz n/a| -1 0 4 16 -12 11 -.14 19 13 | 0 1373 2721 7772
grg n/a| 1 -1 -9 -7 30 -98 .20 21 17 | -14305 1049 2725 7090
jgx n/a| -1 2 0 44 3 -93 -.11 30 30 | 27744 105 2610 8185
Table 2.2282.2 GPS week: 2282 Day: 2 MJD: 60220
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 3 -15 -3 18 .08 16 12 | 22088 -2605 2321 8195
esa n/a| 0 0 -3 3 -22 11 -.15 24 17 | -12273 -2663 2340 5741
gfz n/a| 1 1 5 40 -10 24 -.14 21 14 | 0 -3049 2397 7676
grg n/a| 0 -2 -8 -27 37 -101 .19 25 20 | -13770 -2904 2370 6842
jgx n/a| -2 1 0 2 21 -65 -.25 36 33 | 26012 -3041 2382 7958
Table 2.2282.3 GPS week: 2282 Day: 3 MJD: 60221
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 -1 -31 48 .08 20 17 | 22737 1136 2944 8946
esa n/a| -1 0 0 -36 -15 -34 -.11 24 18 | -21251 309 2907 7836
gfz n/a| 0 1 2 18 6 31 -.13 26 15 | 0 1292 2944 7688
grg n/a| 0 -3 -7 9 28 -73 .23 23 20 | -14354 1094 2951 7167
jgx n/a| -1 1 0 39 0 -51 -.23 31 31 | 26573 914 3007 7868
Table 2.2282.4 GPS week: 2282 Day: 4 MJD: 60222
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 -1 -10 29 .08 18 14 | 21652 -2047 2834 9119
esa n/a| 1 0 -5 -21 -19 7 -.12 25 21 | -907 -2137 2834 8256
gfz n/a| 0 0 4 23 -1 7 -.12 18 15 | 0 -2760 2783 8097
grg n/a| 2 -3 -6 -8 28 -37 .24 23 16 | -13915 -2837 2780 7655
jgx n/a| 1 2 0 43 -15 -9 -.13 32 32 | 25774 -2695 2781 8430
Table 2.2282.5 GPS week: 2282 Day: 5 MJD: 60223
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 -5 -18 58 .07 19 13 | 18125 -2014 2666 8094
esa n/a| 0 2 -4 -29 -9 37 -.05 30 23 | -18200 -1042 2645 7384
gfz n/a| 0 0 3 21 30 -19 -.17 23 14 | 0 -2306 2682 7444
grg n/a| 3 -3 -5 6 5 -77 .18 26 22 | -16403 -1673 2656 6999
jgx n/a| -3 0 0 -4 -10 -6 -.23 34 35 | 21909 -1846 2699 7685
Table 2.2282.6 GPS week: 2282 Day: 6 MJD: 60224
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 4 -20 -4 67 .08 21 15 | 21053 1514 2696 9312
esa n/a| -2 1 -2 -7 -20 3 -.15 25 18 | -6874 884 2675 7621
gfz n/a| 0 0 1 23 16 -15 -.12 25 15 | 0 2050 2715 8758
grg n/a| 1 -2 -6 20 14 -46 .19 27 17 | -14446 1569 2693 8262
jgx n/a| -1 1 -3 -9 17 65 -.30 30 30 | 24938 1586 2732 9062
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 3.2282.0 GPS week: 2282 Day: 0 MJD: 60218
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1514 30 30 25 14 62 14 | 75 73 62 60 61 66
R02 | 1158 8 11 13 14 21 7 | 41 51 39 48 44 44
R03 | 746 17 14 19 13 17 9 | 52 64 61 66 56 60
R04 | 1628 13 14 14 8 21 7 | 54 46 47 45 40 47
R05 | 2581 15 14 19 20 13 10 | 47 48 52 53 46 48
R07 | 1589 8 10 13 13 27 6 | 60 63 55 55 49 57
R08 | 911 13 15 16 7 34 7 | 51 55 63 60 49 56
R09 | 2456 11 12 16 11 22 7 | 40 43 39 38 36 38
R11 | 2002 13 7 19 23 --- 9 | 71 75 79 70 --- 72
R12 | 1696 10 14 15 16 28 8 | 77 77 87 86 71 81
R13 | 521 23 35 42 29 60 18 | 101 80 100 90 80 91
R14 | 1394 8 7 17 12 27 7 | 110 112 108 114 107 111
R15 | 1367 9 14 8 9 20 6 | 79 65 73 77 61 73
R16 | 1425 13 21 14 15 24 9 | 71 59 74 61 52 64
R17 | 2951 9 27 15 13 --- 9 | 79 66 80 79 --- 76
R18 | 2072 19 16 13 16 18 9 | 64 77 70 79 68 71
R19 | 2399 51 35 56 44 52 27 | 135 131 165 123 95 136
R20 | 3849 30 66 73 29 60 29 | 58 60 58 46 53 35
R21 | 771 15 20 13 14 22 9 | 73 61 71 67 54 67
R22 | 2246 20 16 13 21 28 10 | 48 51 54 60 52 52
R24 | 1026 18 15 21 12 25 9 | 70 80 85 73 70 75
XR25 |15131 16 17 --- --- --- 16 | 31 37 --- --- --- 32
XR26 |18505 76 --- 98 --- --- 86 | 374 --- 439 --- --- 400
------+------------------------------------+--------------------------------
RMS | 1904 19 24 27 19 34 |T 80 67 89 69 60 80
WRMS | 1904 15 17 15 15 33 |NE 80 67 89 69 60 80
MEDI | 1628 15 15 16 14 25 |MD 70 63 70 66 54 66
Table 3.2282.1 GPS week: 2282 Day: 1 MJD: 60219
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 2902 32 26 15 16 63 13 | 40 41 39 34 31 35
R02 | 2158 10 12 13 19 19 8 | 24 33 23 35 30 26
R03 | 1441 12 11 13 16 22 7 | 25 33 29 36 30 29
R04 | 1052 13 13 14 15 19 8 | 30 38 33 34 37 31
R05 | 1727 17 20 9 11 29 8 | 27 38 28 24 21 27
R07 | 1045 11 8 6 11 19 5 | 38 33 34 34 41 34
R08 | 1464 9 10 13 8 21 6 | 35 32 37 34 36 34
R09 | 2366 12 12 11 14 18 7 | 35 35 37 32 36 33
R11 | 1315 14 7 8 12 20 6 | 62 68 67 66 49 65
R12 | 937 17 21 22 14 23 11 | 62 55 86 77 58 69
R13 | 1865 32 31 26 23 50 16 | 88 91 95 69 91 81
R14 | 819 11 7 9 14 20 6 | 100 111 116 106 108 108
R15 | 1106 8 20 14 30 30 11 | 55 41 43 70 48 50
R16 | 864 15 24 15 19 --- 11 | 52 52 63 61 --- 55
R17 | 2625 12 14 12 13 --- 7 | 52 48 51 44 --- 47
R18 | 2308 28 21 11 23 18 12 | 38 50 57 63 49 51
R19 | 2137 46 33 41 47 --- 24 | 116 107 128 112 --- 112
R20 | 4032 45 35 43 41 53 24 | 48 47 54 66 51 49
R21 | 705 13 14 8 16 23 7 | 44 41 37 42 39 38
R22 | 2497 23 10 13 15 19 9 | 33 42 54 52 41 44
R24 | 1233 18 16 22 22 21 11 | 46 54 59 46 46 49
XR25 |21618 18 15 --- --- --- 16 | 28 40 --- --- --- 32
XR26 |13287 73 --- 54 --- --- 63 | 195 --- 253 --- --- 226
------+------------------------------------+--------------------------------
RMS | 1928 22 19 19 21 30 |T 55 51 64 54 46 57
WRMS | 1928 18 15 13 17 30 |NE 55 51 64 54 46 57
MEDI | 1727 15 14 13 16 21 |MD 44 41 51 46 41 47
Table 3.2282.2 GPS week: 2282 Day: 2 MJD: 60220
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 604 18 19 27 29 58 13 | 53 57 64 40 42 53
R02 | 1509 10 18 13 7 25 7 | 33 47 35 34 28 35
R03 | 1721 8 11 13 15 33 6 | 37 41 45 42 36 39
R04 | 1055 9 21 8 16 29 8 | 44 44 42 45 32 41
R05 | 1428 15 19 21 16 18 10 | 37 46 36 46 32 36
R07 | 715 10 8 12 16 24 6 | 50 45 48 43 41 46
R08 | 1980 5 9 10 12 20 5 | 42 45 45 45 46 44
R09 | 2786 11 11 16 11 20 7 | 27 29 33 26 37 27
R11 | 1279 12 13 11 21 20 8 | 75 74 73 70 49 72
R12 | 1352 9 12 12 16 26 7 | 67 67 70 75 52 68
R13 | 1892 18 43 22 30 81 16 | 77 67 86 91 50 77
R14 | 757 8 11 11 19 17 7 | 104 98 101 101 104 100
R15 | 952 8 22 10 18 27 8 | 58 42 62 65 39 56
R16 | 672 10 21 11 17 30 8 | 53 52 55 53 53 52
R17 | 1398 10 15 9 15 --- 7 | 61 56 58 63 --- 59
R18 | 1779 11 21 16 17 19 9 | 50 71 50 64 54 57
R19 | 1209 43 47 48 62 --- 28 | 81 106 114 102 --- 94
R20 | 2063 35 59 52 49 73 27 | 43 66 61 59 82 45
R21 | 674 10 14 12 21 29 8 | 53 44 53 46 39 48
R22 | 3395 13 11 17 19 22 9 | 52 54 49 52 68 50
R24 | 786 15 23 27 23 22 12 | 51 61 73 51 45 56
XR25 |16125 8 14 --- --- --- 11 | 36 33 --- --- --- 33
XR26 |18827 71 --- 93 --- --- 81 | 241 --- 325 --- --- 271
------+------------------------------------+--------------------------------
RMS | 1594 16 24 21 25 36 |T 61 56 71 57 48 63
WRMS | 1594 12 17 14 20 33 |NE 61 56 71 57 48 63
MEDI | 1398 10 15 13 17 25 |MD 52 52 55 52 45 52
Table 3.2282.3 GPS week: 2282 Day: 3 MJD: 60221
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1374 35 34 23 22 39 17 | 68 54 62 55 67 57
R02 | 1637 13 13 15 11 21 7 | 36 48 43 35 32 39
R03 | 1158 9 16 8 17 28 7 | 37 40 43 52 36 41
R04 | 1371 16 15 15 21 22 10 | 43 37 40 34 35 37
R05 | 693 13 10 10 13 18 7 | 45 39 41 36 33 39
R07 | 639 8 11 19 23 16 9 | 51 56 64 42 45 52
R08 | 1501 9 15 15 21 14 9 | 52 47 52 51 49 49
R09 | 3597 12 6 14 10 16 6 | 22 28 36 30 27 28
R11 | 1592 18 15 16 20 16 10 | 65 65 56 51 53 58
R12 | 1081 11 10 9 16 20 6 | 85 91 90 87 74 87
R13 | 1194 25 35 26 33 45 17 | 95 81 94 111 74 92
R14 | 670 7 13 9 11 25 6 | 95 86 97 100 79 94
R15 | 1059 15 16 16 20 20 9 | 62 53 61 57 48 57
R16 | 681 12 23 11 22 20 10 | 46 50 52 54 37 48
R17 | 463 13 24 18 19 --- 11 | 69 54 71 59 --- 62
R18 | 1102 17 19 14 16 29 9 | 58 69 63 75 56 65
R19 | 1486 45 46 70 51 55 31 | 46 47 94 50 59 51
R20 | 1906 46 57 72 44 76 32 | 61 64 86 43 77 50
R21 | 1342 13 11 12 14 22 7 | 61 52 51 54 44 53
R22 | 3276 14 17 16 14 17 9 | 29 31 31 36 40 28
R24 | 598 14 16 12 18 14 8 | 58 56 58 52 49 54
XR25 | 7395 9 12 --- --- --- 10 | 35 33 --- --- --- 32
XR26 |13380 76 --- 81 --- --- 78 | 325 --- 376 --- --- 344
------+------------------------------------+--------------------------------
RMS | 1561 20 24 26 23 31 |T 67 53 75 55 50 65
WRMS | 1561 17 18 15 20 31 |NE 67 53 75 55 50 65
MEDI | 1342 13 15 15 19 20 |MD 58 52 58 52 48 52
Table 3.2282.4 GPS week: 2282 Day: 4 MJD: 60222
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1676 25 19 21 18 57 12 | 58 52 40 54 57 49
R02 | 961 7 15 11 10 17 6 | 32 40 27 32 25 31
R03 | 609 10 13 11 17 35 7 | 37 51 37 44 34 40
R04 | 730 8 10 15 20 35 8 | 39 48 51 33 26 42
R05 | 708 15 15 11 11 11 7 | 35 38 34 31 33 32
R07 | 634 11 6 16 15 23 7 | 38 40 45 35 31 38
R08 | 2240 13 19 12 12 15 8 | 41 51 45 43 48 43
R09 | 3620 14 19 22 23 12 11 | 30 34 46 50 41 37
R11 | 2142 16 18 12 24 7 10 | 89 92 93 92 53 90
R12 | 1046 8 13 11 14 17 6 | 70 70 73 64 56 69
R13 | 557 26 34 17 25 51 15 | 93 89 87 86 86 86
R14 | 1168 13 12 15 19 35 8 | 118 121 120 109 138 116
R15 | 834 13 24 13 9 21 9 | 61 42 64 53 42 55
R16 | 1299 10 21 11 17 16 8 | 49 53 46 51 46 47
R17 | 650 12 26 17 16 --- 10 | 62 53 69 65 --- 61
R18 | 1584 11 18 11 16 31 8 | 55 58 61 57 48 56
R19 | 1562 45 54 34 55 50 27 | 99 95 108 92 58 94
R20 | 1160 39 63 35 49 53 26 | 65 46 54 53 41 46
R21 | 1266 11 24 24 13 38 11 | 57 53 81 70 40 65
R22 | 3081 15 18 11 18 26 9 | 50 56 48 49 68 49
R24 | 528 8 14 10 13 17 6 | 54 52 42 57 50 50
XR25 |10500 9 15 --- --- --- 12 | 26 36 --- --- --- 29
XR26 |15292 78 --- 78 --- --- 78 | 270 --- 294 --- --- 274
------+------------------------------------+--------------------------------
RMS | 1566 18 25 18 23 32 |T 66 57 71 58 51 65
WRMS | 1566 14 21 15 16 32 |NE 66 57 71 58 51 65
MEDI | 1168 13 18 13 17 23 |MD 55 52 51 53 46 49
Table 3.2282.5 GPS week: 2282 Day: 5 MJD: 60223
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 854 26 22 30 34 57 16 | 44 42 27 34 42 32
R02 | 807 9 14 11 12 9 6 | 22 26 22 24 20 20
R03 | 848 7 13 7 10 20 5 | 28 37 27 30 33 29
R04 | 549 18 7 11 13 13 7 | 37 31 30 27 33 31
R05 | 885 6 10 10 10 16 5 | 30 27 36 26 33 29
R07 | 515 7 15 14 9 11 6 | 30 34 28 34 28 29
R08 | 1041 11 11 13 11 20 7 | 23 37 29 30 34 28
R09 | 4148 11 23 14 19 23 9 | 52 59 62 55 50 55
R11 | 2335 17 22 20 17 15 11 | 25 23 29 27 29 22
R12 | 1222 13 18 16 25 25 10 | 83 75 84 95 65 83
R13 | 687 25 48 27 35 52 19 | 77 54 75 85 60 70
R14 | 1556 10 20 15 16 31 9 | 51 66 47 57 55 53
R15 | 554 10 20 14 20 21 9 | 47 36 44 60 39 46
R16 | 720 15 24 9 10 17 9 | 47 41 36 43 38 40
R17 | 715 9 16 10 11 --- 6 | 50 48 48 56 --- 50
R18 | 1408 10 18 12 16 29 8 | 49 47 51 50 45 47
R19 | 895 35 58 69 57 79 32 | 82 74 92 75 46 74
R20 | 888 57 88 47 69 64 37 | 65 75 44 45 36 37
R21 | 1252 9 18 13 10 28 7 | 54 45 57 58 39 53
R22 | 2840 13 11 13 16 19 8 | 45 36 47 57 41 45
R24 | 596 10 21 12 19 14 9 | 50 51 40 44 40 44
XR25 |14381 11 17 --- --- --- 14 | 23 32 --- --- --- 25
XR26 |19535 77 --- 89 --- --- 83 | 201 --- 246 --- --- 215
------+------------------------------------+--------------------------------
RMS | 1488 19 30 23 26 34 |T 52 45 54 48 40 50
WRMS | 1488 13 23 14 22 35 |NE 52 45 54 48 40 50
MEDI | 888 11 18 13 16 20 |MD 47 41 44 45 39 44
Table 3.2282.6 GPS week: 2282 Day: 6 MJD: 60224
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1114 16 10 19 12 25 8 | 74 70 64 62 67 66
R02 | 935 12 9 18 18 19 8 | 44 53 54 44 44 47
R03 | 1422 9 13 8 8 14 5 | 53 53 55 57 46 54
R04 | 776 22 13 10 15 18 9 | 55 46 49 43 40 47
R05 | 1410 10 10 10 17 10 7 | 53 53 53 45 50 50
R07 | 649 10 13 10 12 12 6 | 61 55 56 58 52 57
R08 | 1132 12 13 12 16 32 7 | 57 58 58 62 53 58
R09 | 3697 19 21 19 38 19 14 | 68 75 71 71 62 68
R11 | 2727 18 20 21 19 18 11 | 40 47 53 45 31 43
R12 | 1712 11 11 20 18 29 9 | 61 61 58 78 52 63
R13 | 807 26 51 40 27 54 21 | 101 45 104 85 48 82
R14 | 2383 10 9 12 21 28 8 | 67 67 71 83 51 71
R15 | 794 7 14 9 16 24 7 | 65 50 61 71 42 61
R16 | 789 10 17 15 19 26 9 | 63 51 63 56 43 57
R17 | 1290 12 19 21 16 --- 10 | 93 83 97 88 --- 90
R18 | 1165 13 17 13 16 15 8 | 80 92 84 91 79 86
R19 | 2096 39 48 74 81 62 35 | 96 97 124 94 59 94
R20 | 2356 63 67 45 47 50 33 | 91 67 66 47 41 53
R21 | 1159 6 17 8 14 33 7 | 91 80 90 88 69 87
R22 | 1827 14 15 16 14 14 8 | 57 53 54 57 52 54
R24 | 715 12 22 11 20 20 9 | 80 95 85 79 79 84
XR25 |12943 8 10 --- --- --- 9 | 33 38 --- --- --- 35
XR26 |14451 75 --- 87 --- --- 81 | 374 --- 482 --- --- 422
------+------------------------------------+--------------------------------
RMS | 1665 21 25 25 27 30 |T 80 63 88 66 53 79
WRMS | 1665 15 18 15 17 30 |NE 80 63 88 66 53 79
MEDI | 1290 12 14 15 17 20 |MD 65 55 63 62 51 61
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