[IGSREPORT-29178] Wk 2246 IGLOS Final Orbits
acc
acc at igs.org
Sun Feb 12 23:16:18 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2246 (Jan 22, 2023 - Jan 28, 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 2.2246.
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:
igl2246[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2246 in the SP3 format.
igl22467.sum Combination Report for GPS Week 2246.
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 | 1.7 ns
1 | -0.8 ns
2 | -15.1 ns
3 | 1.4 ns
4 | 0.1 ns
5 | -0.8 ns
6 | 0.2 ns
6. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESA | R22
1 | ESA | R20 R22
2 | ESA | R22
3 | ESA | R20 R22
4 | ESA | R20 R22
5 | ESA | R20 R22
6 | ESA | 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 1.2246, 1a.2246).
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 2.2246.0-6)
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 3.2246.0-6).
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 2246 summary. (Jan 22, 2023 - Jan 28, 2023)
Table 1.2246.a GPS week : 2246 MJD: 59966.0-59972.0
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 -2 -6 53 .05 19 17 | 38198 874 3277 8743
| 0 1 1 17 10 28 .03 | 6911 1921
esa n/a| 0 0 -3 -24 -6 -29 -.22 45 34 | 590 314 3246 8522
| 0 0 1 16 19 22 .05 | 10467 1923
gfz n/a| -1 2 3 35 12 -26 -.06 26 22 | 0 795 3236 8563
| 0 1 2 20 15 20 .05 | 0 1733
grg n/a| 3 -2 -3 -17 -5 -9 .18 24 22 | -2403 774 3236 8057
| 0 1 1 20 14 26 .04 | 6012 1734
iac n/a| 0 1 0 19 58 -79 -.19 26 24 | -23 33 3233 9085
| 1 1 1 39 69 134 .06 | 6171 689
Table 1.2246.b GPS week : 2246 MJD: 59966.0-59972.0
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 | 17 17 20 23 21 24 24 |
R02 | 7 6 7 6 7 8 7 |
R03 | 15 9 8 9 7 9 9 |
R04 | 11 10 11 7 8 7 10 |
R05 | 12 7 8 7 9 9 6 |
R07 | 14 8 8 9 10 12 9 |
R08 | 13 9 8 10 8 10 9 |
R09 | 9 8 9 8 9 7 8 |
R11 | 8 7 8 8 6 6 9 |
R12 | 10 11 9 8 8 10 8 |
R13 | 18 18 18 27 23 16 21 |
R14 | 7 8 7 8 7 5 6 |
R15 | 9 8 9 7 9 9 9 |
R16 | 25 27 20 22 19 19 22 |
R17 | 10 11 9 9 10 8 11 |
R18 | 9 9 12 9 11 8 7 |
R19 | 24 23 29 27 28 23 25 |
R20 | 49 27 40 22 30 33 47 |
R21 | 9 11 9 10 13 11 10 |
R22 | 8 7 6 12 14 15 6 |
R24 | 18 11 12 13 13 12 14 |
Table 1.2246.c GPS week : 2246 MJD: 59966.0-59972.0
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 2246 0 | 1 -3 40 1567 1530 -7891 80.1 1427 1427 | 1709 0
brd 2246 1 | -42 -44 58 1769 420 -1455 79.5 1246 1246 | -829 0
brd 2246 2 | -8 -73 21 125 237 -4270 81.8 1387 1387 | -15069 0
brd 2246 3 | 21 -37 -34 -1248 -733 -12020 79.0 1292 1292 | 1401 0
brd 2246 4 | -34 19 50 -1709 -2013 -13400 81.4 1163 1163 | 121 0
brd 2246 5 | -71 -36 138 -1199 -1716 -5811 81.5 1372 1372 | -794 0
brd 2246 6 | 43 -5 74 -2733 -278 671 79.5 1272 1272 | 165 0
-------------+------------------------------------------------------------+----------------
brd 2246 mean| -12 -25 50 -489 -364 -6310 80.4 1308 1308 | -1899 0
brd 2246 sdev| 39 30 52 1698 1241 5197 1.1 92 92 | 5888 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 2.2246.0 GPS week: 2246 Day: 0 MJD: 59966
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 -1 28 1 31 .08 22 19 | 38157 2980 3118 9258
esa n/a| 0 0 -5 -26 15 -30 -.15 38 26 | 3934 2036 3120 7647
gfz n/a| -2 3 5 13 7 -29 -.12 27 28 | 0 2892 3090 9063
grg n/a| 3 -3 -2 -36 8 14 .19 34 29 | 101 2770 3117 8615
iac n/a| 0 1 -2 29 72 -175 -.23 28 25 | 3154 393 3094 9628
Table 2.2246.1 GPS week: 2246 Day: 1 MJD: 59967
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 2 -13 1 44 .04 18 16 | 39233 -1076 3385 8070
esa n/a| 0 0 -5 -20 0 -30 -.27 45 31 | 2534 -2086 3368 6729
gfz n/a| -1 0 6 43 11 -48 -.04 24 18 | 0 -1361 3363 7940
grg n/a| 3 -1 -4 -18 -23 19 .12 21 19 | -322 -1099 3347 7531
iac n/a| -1 1 -1 -23 89 -68 -.16 26 23 | 1934 -1045 3355 8527
Table 2.2246.2 GPS week: 2246 Day: 2 MJD: 59968
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 3 6 -5 8 .09 19 16 | 22953 1322 3597 7621
esa n/a| 0 0 -4 -12 -5 14 -.20 42 30 | -15805 1176 3530 6862
gfz n/a| 0 3 0 4 -13 -1 -.12 25 16 | 0 1764 3526 7474
grg n/a| 3 -2 -4 13 7 8 .17 23 21 | -16033 1517 3522 6892
iac n/a| 1 0 0 -28 113 -201 -.22 26 23 | -13886 537 3515 7904
Table 2.2246.3 GPS week: 2246 Day: 3 MJD: 59969
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 5 -2 77 .05 15 12 | 41317 2810 3379 9552
esa n/a| 0 0 -5 -49 -43 -61 -.23 52 53 | 19140 2814 3348 11512
gfz n/a| -1 1 3 42 19 -19 -.03 27 19 | 0 2705 3343 9305
grg n/a| 3 0 -3 -24 -2 -54 .26 25 22 | -252 2819 3316 8643
iac n/a| 2 4 0 58 81 187 -.25 29 28 | 3278 386 3319 9828
Table 2.2246.4 GPS week: 2246 Day: 4 MJD: 59970
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 -4 -23 73 .00 19 18 | 42942 441 3178 8805
esa n/a| 0 0 -2 -15 12 -27 -.28 49 36 | 610 -592 3127 7473
gfz n/a| 0 3 3 41 29 -7 .01 25 25 | 0 99 3119 8587
grg n/a| 2 -1 -4 -23 2 -31 .16 23 21 | 157 267 3148 7967
iac n/a| 1 1 0 64 -92 -120 -.06 29 25 | 2772 -612 3132 9091
Table 2.2246.5 GPS week: 2246 Day: 5 MJD: 59971
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 -25 2 49 .03 18 16 | 41874 -2123 3411 8377
esa n/a| 0 0 -2 -3 -12 -31 -.20 48 33 | -4074 -2001 3384 7736
gfz n/a| 0 1 6 68 2 -20 -.08 26 31 | 0 -1179 3372 8266
grg n/a| 2 -3 -5 -38 -26 -18 .17 21 19 | -239 -1585 3370 7785
iac n/a| 0 0 0 -8 91 -161 -.20 24 24 | 956 -279 3380 8778
Table 2.2246.6 GPS week: 2246 Day: 6 MJD: 59972
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 4 -10 -18 90 .07 23 19 | 40912 1765 2876 9524
esa n/a| 0 1 -1 -42 -10 -42 -.24 41 28 | -2209 857 2849 11697
gfz n/a| 0 2 0 34 29 -57 -.05 28 19 | 0 645 2842 9308
grg n/a| 2 -3 -2 6 -5 -6 .17 22 20 | -237 732 2837 8967
iac n/a| 0 0 -2 47 53 -15 -.21 21 20 | 1627 851 2838 9842
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 3.2246.0 GPS week: 2246 Day: 0 MJD: 59966
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1169 27 24 37 19 59 16 | 102 96 126 105 104 106
R02E | 1253 10 12 12 16 22 7 | 39 39 43 47 44 41
R03E | 1396 9 11 35 34 28 14 | 50 43 53 52 53 45
R04E | 2126 14 16 28 10 28 11 | 45 44 57 52 51 48
R05E | 1195 20 19 13 27 23 11 | 72 76 88 99 90 82
R07E | 877 19 29 15 34 22 14 | 54 50 59 68 51 54
R08E | 2507 15 17 19 33 17 12 | 52 50 51 69 55 52
R09 | 754 14 14 12 19 15 8 | 51 58 57 49 51 53
R11 | 879 9 18 9 15 19 7 | 64 66 68 68 60 66
R12 | 1016 17 9 13 23 14 9 | 69 59 59 59 63 61
R13 | 912 30 30 26 40 18 18 | 79 68 76 62 74 69
R14 | 2315 10 14 15 11 23 7 | 66 75 74 69 69 70
R15 | 1081 18 13 11 15 21 8 | 73 68 65 69 71 68
R16 | 2091 26 34 64 29 31 24 | 115 99 108 109 99 108
R17 | 802 15 24 11 15 23 9 | 87 76 87 82 83 83
R18 | 503 18 13 17 14 24 9 | 52 64 68 66 70 61
R19 | 2288 41 57 21 41 33 23 | 98 61 87 92 94 81
R20 | 1023 47 133 57 95 50 49 | 122 71 115 138 121 106
R21 | 551 10 21 16 16 19 9 | 76 57 86 77 73 74
XR22 | 1561 --- 338 6 8 15 7 | --- 115 56 58 50 56
R24 | 1112 23 33 15 49 25 18 | 78 63 82 102 89 78
------+------------------------------------+--------------------------------
RMS | 1427 22 38 27 34 28 |T 72 66 74 75 72 69
WRMS | 1427 19 26 28 29 25 |NE 79 71 77 78 76 73
MEDI | 1112 17 19 15 19 23 |MD 69 64 68 69 70 68
Table 3.2246.1 GPS week: 2246 Day: 1 MJD: 59967
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 712 26 39 35 15 62 17 | 110 113 123 121 127 115
R02E | 736 8 7 9 16 18 6 | 28 28 24 33 31 27
R03E | 1585 13 16 12 17 18 8 | 28 29 25 36 36 26
R04E | 1599 13 18 23 13 23 10 | 43 48 59 52 49 49
R05E | 2143 10 14 12 12 18 6 | 60 54 55 54 59 55
R07E | 807 9 18 13 16 18 8 | 29 34 29 38 34 30
R08E | 1454 14 16 15 15 21 8 | 30 29 35 30 28 28
R09 | 884 8 18 17 10 18 7 | 22 30 38 33 34 28
R11 | 1196 7 21 6 13 21 7 | 39 42 40 43 36 40
R12 | 999 24 14 6 23 33 11 | 34 35 26 34 41 30
R13 | 812 26 41 21 33 20 17 | 45 44 37 29 44 36
R14 | 1171 8 21 9 15 17 7 | 35 49 39 39 35 38
R15 | 989 14 15 12 11 10 7 | 43 37 39 38 36 38
R16 | 2367 30 37 70 32 27 26 | 53 32 34 49 37 41
R17 | 801 12 25 12 23 30 10 | 59 62 64 53 53 57
R18 | 562 16 18 11 13 22 8 | 32 41 41 42 44 37
R19 | 1240 38 64 21 31 31 22 | 73 42 55 61 61 58
R20 | 989 25 161 49 38 24 27 | 66 52 45 82 66 67
R21 | 699 10 30 20 11 20 10 | 44 34 54 52 38 46
XR22 | 1368 --- 337 6 7 17 7 | --- 57 21 30 26 25
R24 | 1329 11 31 9 23 23 11 | 37 35 36 47 45 38
------+------------------------------------+--------------------------------
RMS | 1245 18 45 24 21 26 |T 45 44 43 47 45 43
WRMS | 1245 16 31 18 19 23 |NE 44 42 40 45 42 41
MEDI | 999 13 21 12 15 21 |MD 39 41 39 42 38 38
Table 3.2246.2 GPS week: 2246 Day: 2 MJD: 59968
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 790 21 53 43 18 64 20 | 89 117 110 91 125 97
R02E | 895 10 11 13 9 12 6 | 25 25 26 27 28 23
R03E | 1420 12 12 11 19 15 8 | 36 43 35 41 36 36
R04E | 967 14 15 27 15 17 10 | 38 32 39 41 37 34
R05E | 846 7 10 17 15 18 7 | 41 41 42 48 54 41
R07E | 2126 12 13 14 14 16 7 | 39 37 35 35 35 35
R08E | 1126 12 14 15 12 14 7 | 24 25 24 31 33 23
R09 | 1705 19 12 11 17 23 9 | 34 29 23 18 38 24
R11 | 1133 13 17 15 10 19 8 | 31 36 47 35 34 35
R12 | 1302 11 22 10 17 22 8 | 38 41 47 37 34 39
R13 | 833 25 40 25 36 27 18 | 47 39 43 30 36 38
R14 | 1017 8 11 15 12 15 6 | 41 51 41 45 40 42
R15 | 662 12 7 20 18 25 9 | 47 50 64 43 47 49
R16 | 1517 17 33 54 23 20 19 | 81 84 90 82 76 83
R17 | 968 10 23 12 18 20 9 | 52 43 46 57 56 49
R18 | 737 19 18 13 28 26 12 | 32 42 33 54 46 36
R19 | 3242 44 86 20 45 47 28 | 89 35 76 66 75 69
R20 | 1329 38 133 53 52 30 40 | 97 49 108 98 100 83
R21 | 1677 6 27 15 13 13 9 | 54 44 60 63 58 56
XR22 | 1015 --- 335 6 5 20 5 | --- 75 24 27 28 25
R24 | 822 15 32 17 18 19 11 | 66 47 45 62 59 55
------+------------------------------------+--------------------------------
RMS | 1387 19 42 25 23 26 |T 50 46 50 49 51 46
WRMS | 1387 16 30 16 21 23 |NE 54 47 53 51 51 48
MEDI | 1017 12 18 15 17 20 |MD 41 42 43 43 40 39
Table 3.2246.3 GPS week: 2246 Day: 3 MJD: 59969
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1108 31 46 54 27 63 23 | 142 149 159 153 118 145
R02E | 859 9 9 10 12 26 6 | 29 33 34 37 38 31
R03E | 989 7 15 20 21 19 9 | 35 37 33 41 30 33
R04E | 1369 8 15 15 13 17 7 | 35 30 41 41 40 35
R05E | 1257 10 14 11 14 23 7 | 74 67 70 79 61 71
R07E | 1969 10 18 13 20 29 8 | 43 42 37 46 35 39
R08E | 1332 11 18 15 22 23 9 | 38 48 42 56 43 42
R09 | 937 10 18 17 11 24 8 | 31 35 33 33 35 30
R11 | 1024 9 15 13 20 19 8 | 31 35 35 43 39 33
R12 | 1630 11 16 12 19 21 8 | 38 43 46 36 36 39
R13 | 545 26 55 45 62 29 26 | 55 45 58 31 34 46
R14 | 739 4 15 12 21 23 7 | 32 40 37 31 38 33
R15 | 695 8 12 14 14 21 7 | 36 51 46 41 34 40
R16 | 851 22 30 66 22 36 21 | 57 71 72 54 69 62
R17 | 833 9 27 16 12 31 9 | 61 45 67 61 64 58
R18 | 671 12 17 12 21 27 9 | 42 50 41 58 55 45
R19 | 2804 32 84 22 43 33 27 | 99 45 96 99 77 86
R20 | 1769 16 186 45 34 42 22 | 119 48 146 127 125 129
R21 | 1401 8 21 22 15 21 9 | 63 57 80 75 75 67
XR22 | 984 --- 353 10 12 21 11 | --- 112 37 38 29 35
R24 | 778 11 43 14 20 21 13 | 77 59 81 76 77 73
------+------------------------------------+--------------------------------
RMS | 1292 15 52 27 25 29 |T 56 54 61 59 54 55
WRMS | 1292 12 53 19 22 28 |NE 57 52 62 57 56 55
MEDI | 989 10 18 15 20 23 |MD 42 45 46 46 40 42
Table 3.2246.4 GPS week: 2246 Day: 4 MJD: 59970
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1410 35 50 35 24 68 21 | 91 111 114 108 119 101
R02E | 789 11 12 11 11 20 6 | 40 40 37 46 36 39
R03E | 1067 11 13 12 13 21 7 | 52 56 55 56 59 53
R04E | 1588 11 16 14 15 16 8 | 35 38 42 41 38 36
R05E | 1535 13 14 13 18 13 8 | 43 45 52 48 46 45
R07E | 1293 12 19 17 17 27 9 | 48 46 54 54 59 48
R08E | 1199 10 14 13 14 19 7 | 52 47 49 59 57 51
R09 | 1367 14 15 15 16 24 8 | 39 45 49 38 48 41
R11 | 722 7 9 14 8 22 5 | 51 52 50 53 59 51
R12 | 1091 15 15 7 15 26 8 | 62 53 51 63 75 57
R13 | 769 26 43 34 50 43 22 | 71 52 64 48 59 59
R14 | 554 9 17 9 12 25 7 | 59 63 59 56 65 58
R15 | 614 17 13 16 12 25 8 | 61 61 53 64 67 59
R16 | 1182 24 17 54 21 20 19 | 99 112 104 104 113 105
R17 | 761 17 17 10 19 26 9 | 88 90 85 78 83 84
R18 | 719 15 19 19 18 13 10 | 54 72 70 57 61 61
R19 | 1945 42 80 24 43 27 28 | 98 56 91 84 71 81
R20 | 1633 27 179 58 38 46 30 | 110 50 125 104 104 114
R21 | 902 10 27 33 16 17 13 | 73 64 88 70 84 73
XR22 | 1511 --- 350 14 13 16 13 | --- 120 56 55 57 54
R24 | 821 21 37 11 19 17 13 | 86 67 76 85 77 78
------+------------------------------------+--------------------------------
RMS | 1162 19 49 25 23 29 |T 65 63 67 65 68 64
WRMS | 1162 18 36 25 21 25 |NE 73 68 72 68 73 69
MEDI | 1091 14 17 14 16 22 |MD 59 56 56 57 61 58
Table 3.2246.5 GPS week: 2246 Day: 5 MJD: 59971
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 2929 22 62 51 28 25 24 | 79 98 90 70 61 76
R02E | 1441 10 13 15 17 30 8 | 50 54 56 57 46 53
R03E | 720 10 16 16 16 21 8 | 50 46 50 56 49 49
R04E | 1594 9 14 12 12 17 7 | 52 52 52 62 48 53
R05E | 853 10 12 21 15 23 8 | 104 108 110 116 99 109
R07E | 996 18 21 23 18 35 11 | 56 71 74 64 48 63
R08E | 1873 10 20 16 20 33 9 | 30 40 34 42 39 33
R09 | 1338 12 6 15 10 23 6 | 53 62 63 58 53 57
R11 | 817 7 11 11 10 14 5 | 46 53 54 50 39 50
R12 | 847 21 15 13 14 22 9 | 25 20 23 25 24 20
R13 | 1066 20 31 25 33 27 16 | 39 36 42 36 27 37
R14 | 1225 6 11 7 8 11 4 | 26 31 26 29 27 27
R15 | 869 20 14 17 9 18 9 | 29 28 26 29 23 24
R16 | 1009 23 27 54 12 31 18 | 67 54 61 68 72 62
R17 | 884 11 22 13 10 23 8 | 49 44 54 49 45 48
R18 | 869 12 15 10 14 18 7 | 46 48 45 48 43 46
R19 | 943 31 57 25 41 30 22 | 53 44 65 61 45 54
R20 | 1118 37 183 58 45 33 33 | 89 57 71 59 68 77
R21 | 956 9 32 16 12 13 10 | 53 46 59 57 57 53
XR22 | 2262 --- 355 16 13 26 14 | --- 107 42 38 39 36
R24 | 2548 20 31 16 15 22 12 | 57 44 43 48 49 47
------+------------------------------------+--------------------------------
RMS | 1371 18 48 26 21 24 |T 52 54 54 53 47 51
WRMS | 1371 16 33 31 19 24 |NE 48 48 48 46 43 45
MEDI | 1009 12 20 16 14 23 |MD 50 48 54 56 46 50
Table 3.2246.6 GPS week: 2246 Day: 6 MJD: 59972
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1250 24 53 55 28 31 23 | 74 72 105 70 83 75
R02E | 1830 13 11 12 12 14 7 | 34 39 36 46 42 37
R03E | 754 18 13 11 16 22 8 | 36 37 31 47 35 36
R04E | 804 13 19 21 13 24 9 | 47 41 43 47 45 42
R05E | 1011 9 11 9 9 21 5 | 76 76 76 82 73 77
R07E | 577 15 16 10 16 20 8 | 54 47 57 60 40 53
R08E | 1551 13 21 15 13 24 9 | 42 44 39 50 48 42
R09 | 629 17 11 9 16 25 8 | 43 46 43 46 46 43
R11 | 466 15 13 19 12 13 8 | 48 59 63 54 47 54
R12 | 824 14 9 14 15 12 8 | 44 40 45 39 45 41
R13 | 2120 32 32 34 41 21 20 | 61 45 55 44 47 50
R14 | 1452 8 13 14 9 26 6 | 44 49 44 44 50 44
R15 | 918 19 12 15 12 13 8 | 54 43 47 41 42 45
R16 | 523 25 33 58 24 22 21 | 96 78 95 93 89 90
R17 | 1101 20 12 27 12 16 11 | 93 74 83 84 81 83
R18 | 981 11 11 12 11 19 6 | 55 70 60 68 66 62
R19 | 2443 32 68 32 39 28 24 | 110 60 104 101 83 94
R20 | 1477 60 141 67 55 30 47 | 143 79 137 122 124 124
R21 | 809 16 27 10 13 18 9 | 76 59 86 79 77 75
XR22 | 2456 --- 333 6 6 19 6 | --- 138 42 42 39 41
R24 | 1573 18 44 13 17 18 14 | 95 56 85 95 84 84
------+------------------------------------+--------------------------------
RMS | 1272 23 41 28 22 21 |T 66 59 65 64 61 61
WRMS | 1272 19 28 19 20 20 |NE 74 64 70 68 65 66
MEDI | 1011 16 16 14 13 21 |MD 54 56 57 54 48 53
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