[IGSREPORT-29158] Wk 2244 IGLOS Final Orbits
acc
acc at igs.org
Sun Jan 29 00:21:42 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2244 (Jan 08, 2023 - Jan 14, 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 2.2244.
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:
igl2244[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2244 in the SP3 format.
igl22447.sum Combination Report for GPS Week 2244.
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 | -2.8 ns
1 | -0.6 ns
2 | -13.4 ns
3 | -11.4 ns
4 | -10.9 ns
5 | 1.0 ns
6 | -0.3 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 1.2244, 1a.2244).
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 2.2244.0-6)
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 3.2244.0-6).
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 2244 summary. (Jan 08, 2023 - Jan 14, 2023)
Table 1.2244.a GPS week : 2244 MJD: 59952.0-59958.0
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 -1 -14 -4 61 .09 19 17 | 30277 -1081 3034 7937
| 0 0 1 12 9 13 .04 | 8090 2543
esa n/a| 1 1 0 -19 23 -33 -.27 40 27 | -2447 -947 3026 7676
| 1 1 1 12 16 23 .04 | 9004 2723
gfz n/a| 0 0 0 12 0 -31 -.11 24 19 | 0 -869 3043 7920
| 0 1 1 14 12 21 .05 | 0 2516
grg n/a| 0 -4 2 9 -20 -15 .21 31 23 | -5220 -857 3012 7227
| 1 2 4 14 14 41 .07 | 6375 2609
iac n/a| 0 1 -2 -9 -19 -16 -.27 26 23 | -3301 -505 3025 8213
| 2 1 4 24 22 96 .06 | 6239 1044
Table 1.2244.b GPS week : 2244 MJD: 59952.0-59958.0
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 | 18 18 23 22 19 16 20 |
R02 | 13 18 8 8 7 8 7 |
R03 | 24 8 7 9 9 7 8 |
R04 | 13 10 9 10 10 10 7 |
R05 | 9 13 10 7 7 9 9 |
R07 | 20 12 11 8 6 8 8 |
R08 | 18 7 9 8 7 9 8 |
R09 | 10 15 13 13 10 9 12 |
R11 | 7 8 8 7 7 8 9 |
R12 | 9 10 9 8 7 7 10 |
R13 | 22 30 18 16 19 24 21 |
R14 | 8 6 10 7 6 5 6 |
R15 | 7 7 8 8 8 11 8 |
R16 | 23 22 20 23 21 22 25 |
R17 | 8 8 8 9 9 10 9 |
R18 | 8 8 9 9 7 7 10 |
R19 | 26 31 28 25 24 32 25 |
R20 | 39 42 41 45 41 41 43 |
R21 | 11 6 12 10 9 9 8 |
R22 | 150 151 151 156 151 149 157 |
R24 | 12 11 12 13 11 13 11 |
Table 1.2244.c GPS week : 2244 MJD: 59952.0-59958.0
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 2244 0 | -5 -29 1 -120 130 -5063 82.2 1550 1550 | -2790 0
brd 2244 1 | -11 -12 22 909 241 -5659 82.2 1446 1446 | -610 0
brd 2244 2 | 32 -5 65 -720 964 -1955 81.9 1533 1533 | -13362 0
brd 2244 3 | 8 11 1 750 708 -377 82.8 1917 1917 | -11350 0
brd 2244 4 | -59 14 48 2386 1292 -319 83.3 1644 1644 | -10946 0
brd 2244 5 | 18 33 -15 -170 1176 1077 81.2 1655 1655 | 980 0
brd 2244 6 | -37 -10 -8 -1692 1353 1676 80.3 1487 1487 | -275 0
-------------+------------------------------------------------------------+----------------
brd 2244 mean| -7 0 16 191 838 -1517 82.0 1604 1604 | -5479 0
brd 2244 sdev| 32 20 30 1307 495 2874 1.0 157 157 | 6140 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 2.2244.0 GPS week: 2244 Day: 0 MJD: 59952
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 -22 -3 46 .16 21 18 | 38699 -6152 3086 8772
esa n/a| 1 2 -2 -35 -4 -8 -.21 37 27 | -995 -6052 3117 6942
gfz n/a| 0 2 0 14 3 -51 -.08 23 14 | 0 -5853 3104 8781
grg n/a| 1 -6 11 24 -1 35 .09 44 28 | -19 -5937 3110 8061
iac n/a| -3 3 3 -16 -5 29 -.25 30 29 | -284 -1354 3117 9122
Table 2.2244.1 GPS week: 2244 Day: 1 MJD: 59953
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 0 -11 77 .14 21 17 | 34764 -1621 2907 6804
esa n/a| 0 0 1 -3 28 -8 -.26 42 35 | -156 -2165 2890 7081
gfz n/a| 0 1 -2 15 0 -8 -.18 25 28 | 0 -1765 2902 6791
grg n/a| 1 -4 6 -15 -27 -70 .31 35 23 | 148 -1726 2870 6040
iac n/a| -3 2 -3 -40 -43 -32 -.26 25 23 | 479 1084 2891 7074
Table 2.2244.2 GPS week: 2244 Day: 2 MJD: 59954
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 -2 -37 1 60 .10 17 15 | 19720 293 3461 7615
esa n/a| 0 0 2 -20 42 -66 -.29 42 33 | -13674 1408 3439 7396
gfz n/a| 0 -1 1 37 -10 -48 -.16 28 21 | 0 556 3466 7512
grg n/a| -1 0 0 16 -20 15 .23 25 19 | -13877 768 3393 6981
iac n/a| 0 0 -6 -21 -44 -61 -.39 22 21 | -11917 873 3432 7884
Table 2.2244.3 GPS week: 2244 Day: 3 MJD: 59955
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 -10 -20 44 .09 20 18 | 23379 -791 2989 7602
esa n/a| 3 0 0 -37 26 -18 -.26 42 27 | -13677 -949 2976 6947
gfz n/a| 0 0 0 -8 21 -38 -.12 26 12 | 0 -927 3020 7671
grg n/a| 0 -2 0 25 -28 -10 .17 24 21 | -10942 -922 2979 6875
iac n/a| 0 1 -6 -17 2 78 -.31 28 27 | -8207 -1077 2981 7774
Table 2.2244.4 GPS week: 2244 Day: 4 MJD: 59956
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 -5 3 61 .04 19 16 | 22434 -462 3067 7936
esa n/a| 0 1 1 -13 14 -30 -.32 39 23 | -4769 464 3075 7312
gfz n/a| 0 3 -2 2 5 2 -.10 20 12 | 0 66 3073 7955
grg n/a| -1 -5 1 4 -24 -47 .20 26 18 | -11043 -73 3058 7283
iac n/a| 1 1 0 -6 5 101 -.25 26 22 | -9092 -773 3069 8191
Table 2.2244.5 GPS week: 2244 Day: 5 MJD: 59957
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 -10 -5 59 .10 18 17 | 35003 2150 2868 8465
esa n/a| 0 3 0 -10 40 -41 -.29 40 23 | 7649 2088 2837 7189
gfz n/a| 1 0 2 5 0 -22 -.08 25 20 | 0 2155 2876 8436
grg n/a| 0 -6 -3 5 -37 -51 .25 32 25 | -554 2454 2816 7719
iac n/a| 0 0 2 39 -14 -50 -.21 24 22 | 3127 -845 2838 8818
Table 2.2244.6 GPS week: 2244 Day: 6 MJD: 59958
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 0 -15 6 79 .04 20 18 | 37945 -990 2860 8366
esa n/a| 1 0 0 -15 13 -61 -.27 38 22 | 8493 -1423 2850 10871
gfz n/a| 0 0 0 19 -18 -52 -.05 22 26 | 0 -315 2862 8298
grg n/a| 2 -5 0 9 0 23 .21 34 28 | -256 -568 2858 7631
iac n/a| 0 0 -5 -6 -39 -183 -.24 23 19 | 2785 -1446 2847 8629
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 3.2244.0 GPS week: 2244 Day: 0 MJD: 59952
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 951 27 39 22 37 33 17 | 43 52 52 55 49 41
R02E | 910 8 14 19 49 39 13 | 46 43 45 75 61 45
R03E | 1437 21 15 24 94 25 23 | 139 146 141 154 152 138
R04E | 1273 15 19 13 44 38 12 | 179 185 180 168 178 177
R05E | 1484 15 14 9 25 30 9 | 145 153 150 137 154 146
R07E | 827 20 14 16 81 31 20 | 150 149 148 162 144 147
R08E | 1085 13 14 23 69 20 17 | 142 137 141 170 146 143
R09 | 1902 15 12 9 33 16 9 | 40 38 44 41 41 38
R11 | 1216 10 13 14 12 24 7 | 48 51 55 53 53 50
R12 | 1781 11 22 9 18 15 8 | 55 53 53 49 54 52
R13 | 1442 43 36 32 34 26 21 | 71 59 66 48 49 62
R14 | 1449 8 21 11 12 27 7 | 47 58 46 45 63 47
R15 | 1200 12 14 9 13 12 7 | 73 57 68 63 66 66
R16 | 704 29 29 57 26 35 23 | 133 127 137 131 125 132
R17 | 1102 8 18 7 24 26 8 | 68 60 67 70 72 66
R18 | 604 10 21 8 15 21 7 | 46 59 49 52 54 50
R19 | 1317 32 76 13 51 52 25 | 99 46 88 97 101 82
R20 | 3240 41 114 45 71 47 39 | 123 57 117 131 123 104
R21 | 622 11 23 21 18 17 10 | 61 49 73 69 70 63
XR22 | 1295 --- 124 --- 179 178 150 | --- 65 --- 33 31 48
R24 | 3155 12 30 15 27 22 11 | 65 47 68 76 68 63
------+------------------------------------+--------------------------------
RMS | 1549 21 37 23 44 30 |T 88 80 89 89 88 83
WRMS | 1549 18 27 14 28 29 |NE 71 59 71 68 69 65
MEDI | 1273 13 21 14 33 26 |MD 68 58 68 70 68 63
Table 3.2244.1 GPS week: 2244 Day: 1 MJD: 59953
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 455 33 42 21 28 43 18 | 49 57 62 61 54 51
R02E | 852 11 10 38 53 25 18 | 37 43 60 62 32 42
R03E | 669 9 16 12 21 15 8 | 87 85 90 91 80 87
R04E | 2807 18 14 16 18 42 10 | 145 142 140 143 128 141
R05E | 817 18 19 14 37 21 12 | 107 109 120 126 115 113
R07E | 927 17 18 18 32 29 12 | 138 136 141 142 137 138
R08E | 1574 10 13 12 15 10 7 | 94 94 95 92 100 93
R09 | 1686 18 15 21 43 25 14 | 43 45 53 43 44 40
R11 | 1126 8 18 13 15 20 7 | 42 51 52 48 45 47
R12 | 1919 14 15 16 21 17 9 | 40 43 47 34 33 39
R13 | 1567 48 53 42 66 21 29 | 55 30 31 39 34 34
R14 | 1200 6 15 8 13 29 6 | 33 37 31 28 48 31
R15 | 1555 9 15 12 16 13 7 | 51 55 58 47 57 52
R16 | 1258 26 27 56 27 31 22 | 109 106 112 104 107 108
R17 | 726 6 18 13 18 14 7 | 26 28 33 28 27 27
R18 | 753 12 19 9 16 19 8 | 28 32 26 32 31 27
R19 | 2233 36 90 16 70 29 31 | 63 33 49 70 54 51
R20 | 1450 34 132 57 61 32 41 | 52 38 80 81 54 59
R21 | 731 7 12 10 13 20 6 | 32 29 28 35 36 28
XR22 | 942 --- 146 --- 154 147 150 | --- 28 --- 25 24 22
R24 | 2034 16 29 12 23 15 11 | 33 28 23 34 17 26
------+------------------------------------+--------------------------------
RMS | 1446 21 42 25 35 25 |T 63 59 66 65 59 59
WRMS | 1446 17 35 28 23 23 |NE 46 41 47 46 43 42
MEDI | 1200 14 18 14 23 21 |MD 49 43 53 48 48 47
Table 3.2244.2 GPS week: 2244 Day: 2 MJD: 59954
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 423 33 49 45 30 33 22 | 47 52 76 42 46 49
R02E | 713 9 15 14 19 16 8 | 54 53 59 63 54 56
R03E | 713 7 14 13 17 17 7 | 83 80 74 84 72 80
R04E | 3020 10 18 17 17 19 9 | 85 83 93 93 84 87
R05E | 1543 11 16 21 18 23 9 | 83 80 94 87 75 85
R07E | 1336 19 14 14 27 26 11 | 106 101 98 118 94 105
R08E | 1966 13 16 13 21 15 9 | 60 61 61 60 60 59
R09 | 1558 18 15 17 32 20 12 | 44 38 43 25 39 33
R11 | 844 8 16 13 15 26 7 | 56 62 57 65 62 58
R12 | 1975 13 21 12 17 17 9 | 51 46 44 63 45 49
R13 | 667 19 47 22 38 19 17 | 62 40 52 75 52 57
R14 | 712 5 16 16 26 18 9 | 39 44 47 34 49 38
R15 | 1930 13 14 9 18 15 8 | 58 48 56 44 51 52
R16 | 1577 21 18 56 28 24 20 | 98 97 101 102 97 100
R17 | 575 9 20 10 13 17 7 | 43 43 39 45 38 41
R18 | 570 17 17 12 13 13 9 | 25 35 34 37 28 30
R19 | 2168 28 95 23 43 23 27 | 75 38 76 63 57 63
R20 | 2211 31 127 77 43 49 40 | 79 48 113 84 88 80
R21 | 671 12 27 28 12 13 11 | 38 38 54 41 43 40
XR22 | 1143 --- 174 --- 130 126 150 | --- 67 --- 42 30 46
R24 | 1928 12 39 11 19 16 12 | 43 30 37 46 31 38
------+------------------------------------+--------------------------------
RMS | 1532 17 42 28 25 22 |T 61 56 65 62 56 59
WRMS | 1532 15 33 21 19 21 |NE 54 48 57 54 50 51
MEDI | 1336 13 18 14 19 19 |MD 56 48 57 63 52 56
Table 3.2244.3 GPS week: 2244 Day: 3 MJD: 59955
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 464 37 46 41 22 36 21 | 59 68 89 69 62 68
R02E | 1122 8 12 12 17 25 7 | 66 66 73 77 81 70
R03E | 1171 10 13 12 22 29 8 | 48 50 47 48 60 45
R04E | 2459 10 16 15 22 27 9 | 104 101 102 104 104 102
R05E | 2104 13 11 12 12 21 7 | 105 107 114 113 106 109
R07E | 1719 11 14 12 14 35 7 | 85 89 92 90 103 87
R08E | 3341 14 13 12 15 29 8 | 54 56 55 62 64 54
R09 | 1786 12 19 22 32 16 12 | 41 47 49 37 46 38
R11 | 690 9 15 7 13 20 6 | 29 29 31 38 40 30
R12 | 2175 15 15 10 16 24 8 | 42 43 38 28 51 36
R13 | 583 25 42 11 31 20 16 | 57 36 55 44 51 47
R14 | 640 10 12 10 14 20 6 | 39 49 43 49 43 43
R15 | 1844 12 23 9 10 28 7 | 53 50 54 49 55 50
R16 | 978 30 25 59 25 34 22 | 61 62 65 50 58 58
R17 | 678 10 21 10 19 19 8 | 49 42 45 59 43 48
R18 | 490 9 17 16 20 16 9 | 39 47 40 44 45 40
R19 | 1699 32 76 28 34 27 24 | 65 43 70 76 57 61
R20 | 2513 42 139 69 59 61 44 | 114 49 112 94 108 91
R21 | 891 11 26 17 13 17 9 | 48 48 61 59 61 53
XR22 | 944 --- 189 --- 128 124 156 | --- 108 --- 30 32 54
R24 | 4674 18 42 9 16 22 12 | 59 41 54 62 51 53
------+------------------------------------+--------------------------------
RMS | 1917 20 42 26 24 28 |T 60 58 64 61 62 58
WRMS | 1917 18 27 12 21 27 |NE 53 49 55 51 52 50
MEDI | 1171 12 19 12 19 25 |MD 54 49 55 59 57 53
Table 3.2244.4 GPS week: 2244 Day: 4 MJD: 59956
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 584 29 41 34 24 30 18 | 50 50 77 50 49 52
R02E | 1104 12 11 10 12 9 6 | 53 49 47 46 45 48
R03E | 1116 14 14 15 16 18 8 | 61 57 51 64 57 56
R04E | 1528 13 14 14 25 23 9 | 63 65 63 54 60 60
R05E | 1677 9 12 9 14 15 6 | 66 67 61 59 66 62
R07E | 1274 7 13 8 15 26 6 | 64 60 65 62 68 62
R08E | 3594 9 14 7 15 24 6 | 68 64 65 75 67 67
R09 | 2282 9 18 16 25 17 10 | 28 32 39 22 34 26
R11 | 553 8 14 14 8 22 6 | 51 50 64 55 56 55
R12 | 2236 9 15 10 15 18 7 | 50 53 48 50 52 49
R13 | 557 32 34 27 39 33 19 | 49 21 36 29 24 33
R14 | 1096 8 9 9 11 17 5 | 34 32 35 45 31 36
R15 | 2167 12 19 12 11 13 8 | 53 47 62 48 44 52
R16 | 718 27 28 54 21 29 21 | 104 104 109 106 97 107
R17 | 625 9 24 7 19 17 8 | 42 34 44 53 42 43
R18 | 906 12 9 9 14 19 6 | 32 33 40 42 34 35
R19 | 1434 26 61 25 53 26 23 | 49 40 64 64 54 51
R20 | 2210 50 135 30 65 69 40 | 92 67 91 75 90 75
R21 | 896 8 29 12 15 13 9 | 44 32 48 52 40 44
XR22 | 1002 --- 175 --- 129 131 150 | --- 114 --- 35 24 59
R24 | 2308 16 30 15 13 28 10 | 52 38 42 46 56 43
------+------------------------------------+--------------------------------
RMS | 1643 19 39 20 26 26 |T 55 52 57 53 51 53
WRMS | 1643 16 23 12 18 22 |NE 52 49 55 51 48 50
MEDI | 1116 12 18 12 15 22 |MD 51 50 51 52 52 52
Table 3.2244.5 GPS week: 2244 Day: 5 MJD: 59957
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1439 25 27 33 15 53 15 | 67 67 87 64 57 68
R02E | 735 10 11 13 19 14 7 | 58 59 61 55 67 57
R03E | 626 11 17 11 12 15 7 | 93 87 97 94 93 92
R04E | 1475 14 18 14 24 10 10 | 137 130 129 139 135 133
R05E | 1478 12 14 12 22 12 8 | 119 109 116 115 114 115
R07E | 1327 6 17 11 22 16 8 | 103 106 100 103 104 101
R08E | 1575 13 19 18 15 13 9 | 88 89 94 90 92 89
R09 | 2725 12 15 15 17 18 8 | 26 33 37 19 40 27
R11 | 463 12 14 20 7 18 8 | 39 44 47 36 43 40
R12 | 1455 8 14 9 19 26 7 | 50 55 48 48 57 49
R13 | 1759 36 38 37 54 29 23 | 49 40 50 33 47 40
R14 | 1318 5 11 6 11 15 4 | 36 28 32 42 30 34
R15 | 1918 14 26 18 18 19 10 | 51 30 39 65 46 45
R16 | 984 23 35 60 24 27 22 | 102 86 98 103 97 96
R17 | 584 14 22 19 11 10 9 | 38 32 44 35 29 36
R18 | 555 10 10 10 16 14 6 | 30 29 28 32 31 28
R19 | 1326 32 79 28 86 32 32 | 30 57 54 45 41 36
R20 | 3537 38 133 49 66 51 40 | 46 67 74 53 58 48
R21 | 623 6 24 18 10 14 8 | 30 26 34 31 27 29
XR22 | 1088 --- 164 --- 135 141 149 | --- 86 --- 50 43 57
R24 | 2932 10 35 18 26 21 12 | 33 28 44 48 42 36
------+------------------------------------+--------------------------------
RMS | 1654 18 40 25 32 24 |T 61 61 65 61 61 59
WRMS | 1654 17 23 20 25 22 |NE 43 45 48 45 45 42
MEDI | 1327 12 19 18 19 18 |MD 49 57 50 50 47 48
Table 3.2244.6 GPS week: 2244 Day: 6 MJD: 59958
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 986 21 44 42 29 24 20 | 61 63 86 61 65 64
R02E | 1239 9 16 10 13 12 6 | 56 54 62 64 58 58
R03E | 835 15 15 10 15 14 8 | 119 122 124 124 128 122
R04E | 793 12 14 12 10 13 7 | 156 154 158 151 161 155
R05E | 1127 12 13 14 23 15 9 | 131 133 129 137 137 131
R07E | 1103 8 13 14 17 19 7 | 124 124 122 120 124 122
R08E | 712 9 23 9 15 21 8 | 118 124 119 114 125 118
R09 | 2082 15 21 18 31 19 11 | 32 47 50 25 36 35
R11 | 473 16 15 15 10 18 8 | 49 53 57 54 57 52
R12 | 1077 13 11 13 30 21 10 | 63 55 57 54 64 57
R13 | 3434 24 38 31 58 21 21 | 64 38 69 35 49 52
R14 | 691 11 10 10 9 13 6 | 50 52 47 50 49 49
R15 | 1156 15 19 5 12 13 7 | 69 51 64 64 64 63
R16 | 1324 31 34 60 28 32 24 | 127 116 127 127 125 124
R17 | 828 9 24 11 22 21 9 | 62 47 60 63 58 58
R18 | 664 20 10 10 25 13 10 | 40 48 46 60 51 46
R19 | 1178 28 70 15 63 37 25 | 77 51 83 91 89 73
R20 | 2225 52 124 39 94 52 43 | 129 71 134 115 135 108
R21 | 1073 7 23 12 13 14 8 | 56 47 63 63 56 57
XR22 | 903 --- 157 --- 155 154 156 | --- 98 --- 50 44 68
R24 | 2766 11 31 8 29 25 11 | 65 43 61 77 72 61
------+------------------------------------+--------------------------------
RMS | 1486 20 38 22 34 23 |T 82 75 85 80 83 79
WRMS | 1486 18 22 26 28 19 |NE 67 58 70 66 67 64
MEDI | 1077 13 21 12 23 19 |MD 64 54 64 64 64 63
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