[IGSREPORT-29143] Wk 2243 IGLOS Final Orbits
acc
acc at igs.org
Fri Jan 20 04:45:33 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2243 (Jan 01, 2023 - Jan 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 2.2243.
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:
igl2243[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2243 in the SP3 format.
igl22437.sum Combination Report for GPS Week 2243.
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 | -1.3 ns
1 | 1.9 ns
2 | -1.5 ns
3 | -0.1 ns
4 | -1.1 ns
5 | 0.7 ns
6 | -1.0 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2243, 1a.2243).
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 2.2243.0-6)
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 3.2243.0-6).
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 2243 summary. (Jan 01, 2023 - Jan 07, 2023)
Table 1.2243.a GPS week : 2243 MJD: 59945.0-59951.0
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| -2 1 -1 0 -1 47 .10 19 16 | 41449 -264 3399 8568
| 0 1 1 14 7 9 .03 | 1706 2682
esa n/a| 0 1 1 -1 20 -5 -.22 39 26 | 8559 -483 3367 8715
| 1 1 1 17 9 28 .03 | 7754 2455
gfz n/a| 0 0 0 22 3 -32 -.13 24 16 | 0 -235 3391 8572
| 0 0 1 13 8 15 .03 | 0 2437
grg n/a| 2 -1 4 -30 -18 -5 .19 32 23 | -357 -171 3361 7868
| 1 3 2 20 26 26 .02 | 413 2471
iac n/a| 0 0 -3 6 24 -30 -.24 24 22 | 1725 -319 3364 8916
| 1 1 4 30 33 55 .04 | 854 1391
Table 1.2243.b GPS week : 2243 MJD: 59945.0-59951.0
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 | 21 25 20 20 16 19 43 |
R02 | 7 7 7 6 8 8 9 |
R03 | 9 9 7 7 8 12 10 |
R04 | 12 10 11 8 9 10 12 |
R05 | 13 11 8 9 8 7 12 |
R07 | 13 12 11 10 10 12 10 |
R08 | 7 7 9 8 10 9 14 |
R09 | 13 14 15 15 14 13 8 |
R11 | 8 9 7 9 10 8 7 |
R12 | 6 7 9 8 8 9 12 |
R13 | 21 19 16 22 15 16 22 |
R14 | 7 7 8 8 6 7 7 |
R15 | 8 8 9 6 9 7 8 |
R16 | 23 18 22 24 25 25 25 |
R17 | 9 8 7 7 5 7 8 |
R18 | 10 11 13 8 7 6 6 |
R19 | 29 28 21 29 30 26 26 |
R20 | 41 39 36 40 44 42 44 |
R21 | 11 11 10 11 11 9 9 |
R22 | 136 151 153 146 142 154 150 |
R24 | 11 10 11 13 11 13 12 |
Table 1.2243.c GPS week : 2243 MJD: 59945.0-59951.0
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 2243 0 | -63 -27 -133 -320 2205 -6684 82.6 1312 1312 | -1285 0
brd 2243 1 | -35 -106 -72 -47 614 -12260 79.6 1443 1443 | 1876 0
brd 2243 2 | -33 -56 -8 598 -2594 -19630 82.8 1313 1313 | -1483 0
brd 2243 3 | 27 26 23 444 -3356 -17540 81.2 1411 1411 | -88 0
brd 2243 4 | -27 -23 -21 315 -3262 -10230 79.3 1404 1404 | -1051 0
brd 2243 5 | -84 15 -37 -1531 -2135 -7057 80.7 1483 1483 | 727 0
brd 2243 6 | -16 -62 -19 -1018 -1361 -6491 81.1 1313 1313 | -975 0
-------------+------------------------------------------------------------+----------------
brd 2243 mean| -33 -33 -38 -222 -1412 -11413 81.0 1382 1382 | -325 0
brd 2243 sdev| 35 46 50 795 2094 5365 1.3 70 70 | 1239 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 2.2243.0 GPS week: 2243 Day: 0 MJD: 59945
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 26 3 48 .09 18 14 | 38894 -1834 3466 8634
esa n/a| 0 2 1 -30 4 10 -.26 41 31 | 10127 -2385 3467 11037
gfz n/a| 0 1 -1 -3 -6 -17 -.11 30 24 | 0 -2203 3446 8687
grg n/a| 2 -4 6 -4 19 -54 .18 27 21 | -360 -2195 3465 7952
iac n/a| 0 1 -9 -12 65 -146 -.28 19 18 | 1142 -2015 3469 9069
Table 2.2243.1 GPS week: 2243 Day: 1 MJD: 59946
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 3 -2 -12 -10 53 .09 18 14 | 40998 4411 3739 8262
esa n/a| 0 0 1 22 16 -37 -.25 38 29 | 6783 3554 3748 6897
gfz n/a| 0 0 -2 26 11 -36 -.16 27 19 | 0 4156 3710 8246
grg n/a| 3 -3 7 -27 -2 10 .17 28 24 | -335 4105 3724 7630
iac n/a| 0 2 -7 -6 -5 -1 -.25 20 20 | 3385 1509 3743 8699
Table 2.2243.2 GPS week: 2243 Day: 2 MJD: 59947
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 2 -2 -1 -8 42 .14 18 17 | 41266 -3675 3530 8440
esa n/a| 2 0 1 -2 17 22 -.22 37 28 | 4752 -2919 3463 7691
gfz n/a| 0 0 0 23 9 -35 -.13 21 14 | 0 -2341 3526 8479
grg n/a| 1 -3 2 -54 -14 4 .21 25 22 | -369 -2475 3474 7723
iac n/a| 0 -1 0 1 64 12 -.20 22 22 | 932 -1414 3460 8736
Table 2.2243.3 GPS week: 2243 Day: 3 MJD: 59948
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 11 3 62 .09 21 17 | 40348 1086 3497 9335
esa n/a| 0 1 0 -14 18 -9 -.22 37 22 | 21986 736 3448 12081
gfz n/a| 0 1 -2 29 -9 -50 -.18 23 18 | 0 724 3505 9384
grg n/a| 1 -4 6 -64 -23 22 .19 31 24 | -786 1343 3442 8489
iac n/a| 0 1 -4 61 34 2 -.18 25 21 | 1657 -64 3453 9551
Table 2.2243.4 GPS week: 2243 Day: 4 MJD: 59949
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 1 -2 -2 -9 41 .10 20 18 | 41617 -947 3156 9043
esa n/a| 0 3 0 -1 33 -47 -.18 40 21 | 14766 -374 3109 8678
gfz n/a| 0 0 0 41 10 -7 -.15 25 13 | 0 -1123 3154 9037
grg n/a| 3 -1 1 -21 -16 -10 .18 28 19 | -937 -479 3122 8434
iac n/a| 2 2 -6 9 -18 -4 -.22 28 24 | 1373 -1675 3113 9356
Table 2.2243.5 GPS week: 2243 Day: 5 MJD: 59950
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 -1 -1 -2 4 51 .08 16 13 | 44204 1114 3232 8269
esa n/a| 0 0 1 7 27 26 -.21 44 27 | 774 1039 3203 7510
gfz n/a| 0 1 -1 22 4 -49 -.11 21 15 | 0 1342 3228 8204
grg n/a| 5 0 4 -20 -23 -22 .18 37 25 | 79 970 3172 7545
iac n/a| 0 0 1 -31 0 -54 -.25 27 27 | 2305 1007 3188 8547
Table 2.2243.6 GPS week: 2243 Day: 6 MJD: 59951
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 -17 7 32 .14 23 21 | 42820 -2007 3174 7998
esa n/a| -1 0 3 10 22 -5 -.17 38 26 | 730 -3034 3137 7115
gfz n/a| 0 0 0 19 6 -32 -.10 24 13 | 0 -2201 3169 7970
grg n/a| 1 4 0 -23 -68 12 .22 49 30 | 204 -2470 3133 7307
iac n/a| 0 -1 1 26 33 -18 -.28 27 24 | 1283 417 3128 8457
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 3.2243.0 GPS week: 2243 Day: 0 MJD: 59945
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1654 32 50 32 31 17 20 | 66 44 73 49 56 52
R02 | 772 6 11 17 15 15 7 | 76 80 79 74 80 77
R03 | 1117 13 24 12 15 12 9 | 70 51 70 61 62 63
R04 | 942 17 21 14 27 13 11 | 81 64 79 59 74 71
R05 | 1355 11 14 26 32 28 12 | 76 71 86 65 71 73
R07 | 1395 7 31 31 15 15 12 | 70 52 86 54 62 65
R08 | 2067 9 15 8 14 18 6 | 60 55 65 63 66 61
R09 | 2237 16 25 21 27 21 12 | 44 40 52 28 34 38
R11 | 1089 10 14 19 12 19 8 | 56 58 50 54 52 54
R12 | 1814 9 11 13 8 19 6 | 72 67 62 62 66 66
R13 | 693 30 39 34 42 18 20 | 77 51 63 42 58 60
R14 | 865 6 13 14 14 10 6 | 58 65 68 56 62 60
R15 | 862 12 14 13 18 14 8 | 82 70 72 68 80 74
R16 | 627 20 22 70 28 24 22 | 129 122 135 125 130 128
R17 | 833 8 19 14 19 13 8 | 48 41 51 54 43 48
R18 | 848 19 14 8 22 19 10 | 36 44 39 45 36 39
R19 | 899 36 74 27 63 39 29 | 73 53 78 72 70 68
R20 | 2196 28 131 75 39 16 40 | 84 43 113 91 82 81
R21 | 715 8 30 16 25 13 11 | 39 31 42 52 45 39
XR22 | 3556 --- 153 --- 120 131 135 | --- 51 --- 47 46 45
R24 | 1212 15 27 12 23 18 11 | 42 32 49 61 49 44
------+------------------------------------+--------------------------------
RMS | 1311 18 40 30 27 19 |T 66 56 70 61 63 62
WRMS | 1311 14 31 24 21 18 |NE 67 57 70 61 63 62
MEDI | 1089 12 22 16 23 18 |MD 70 52 68 59 62 61
Table 3.2243.1 GPS week: 2243 Day: 1 MJD: 59946
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1582 37 49 43 45 28 24 | 59 46 66 46 46 50
R02 | 710 6 16 10 17 14 7 | 57 68 59 53 63 58
R03 | 1339 6 18 21 13 8 8 | 52 53 67 51 57 54
R04 | 833 19 17 8 19 16 9 | 66 53 56 50 57 56
R05 | 1228 15 14 15 26 17 10 | 74 68 66 72 81 69
R07 | 1389 17 24 19 27 13 12 | 60 48 63 50 48 54
R08 | 1847 11 15 13 11 12 7 | 61 56 63 59 61 60
R09 | 1071 15 27 22 33 27 14 | 76 81 81 57 73 71
R11 | 1507 10 10 21 15 16 8 | 72 79 71 75 74 73
R12 | 2603 11 10 6 15 22 6 | 62 56 57 56 60 57
R13 | 692 23 46 31 37 20 19 | 64 56 67 56 54 59
R14 | 844 7 13 13 15 15 6 | 55 57 57 47 53 53
R15 | 724 13 14 9 16 15 7 | 63 65 60 55 65 60
R16 | 833 22 21 46 27 26 17 | 113 111 120 103 113 112
R17 | 837 6 23 9 17 13 8 | 39 45 39 39 37 39
R18 | 1108 17 16 14 26 17 10 | 47 45 42 50 42 44
R19 | 972 32 76 23 57 44 27 | 55 41 58 49 49 48
R20 | 2397 29 114 74 44 23 38 | 52 54 87 53 47 59
R21 | 866 10 17 21 27 16 11 | 42 44 50 40 38 41
XR22 | 3747 --- 159 --- 142 145 150 | --- 85 --- 50 60 62
R24 | 2702 12 28 17 13 14 10 | 41 39 35 38 37 37
------+------------------------------------+--------------------------------
RMS | 1443 18 38 27 28 20 |T 60 59 63 54 57 57
WRMS | 1443 14 29 19 24 20 |NE 60 60 63 55 58 58
MEDI | 1108 13 18 17 26 16 |MD 59 56 60 51 57 57
Table 3.2243.2 GPS week: 2243 Day: 2 MJD: 59947
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1157 37 45 25 34 28 20 | 51 45 53 39 39 41
R02 | 1137 10 15 9 12 18 6 | 80 85 82 77 72 80
R03 | 1160 10 13 11 12 12 6 | 51 42 48 50 39 47
R04 | 1020 14 15 16 29 12 11 | 50 36 53 34 43 42
R05 | 1323 13 10 12 16 17 7 | 54 52 55 61 55 54
R07 | 1257 16 13 12 29 29 10 | 59 48 56 50 57 52
R08 | 1262 11 20 15 16 16 9 | 55 42 58 53 56 52
R09 | 982 14 28 18 40 21 14 | 57 65 61 29 57 50
R11 | 1391 12 12 12 10 16 6 | 32 31 35 30 27 31
R12 | 2494 13 14 11 21 16 8 | 62 58 59 52 55 57
R13 | 846 23 39 21 27 21 15 | 59 43 55 52 46 51
R14 | 1929 11 12 12 15 14 7 | 50 60 46 66 52 53
R15 | 988 14 13 9 20 16 8 | 65 64 69 53 64 62
R16 | 802 29 23 56 28 27 22 | 132 131 128 127 126 127
R17 | 1226 10 18 9 14 15 7 | 36 38 37 41 35 37
R18 | 798 19 29 13 25 30 12 | 24 40 36 29 30 27
R19 | 1328 25 64 16 40 34 21 | 40 34 37 41 39 33
R20 | 1755 33 120 42 41 44 35 | 67 30 59 53 55 48
R21 | 877 13 18 14 22 13 9 | 26 36 29 36 30 28
XR22 | 2263 --- 170 --- 136 145 152 | --- 87 --- 39 24 43
R24 | 1266 8 37 14 11 20 10 | 39 36 39 44 39 37
------+------------------------------------+--------------------------------
RMS | 1313 18 37 21 25 22 |T 54 52 54 50 49 50
WRMS | 1313 17 28 14 22 22 |NE 54 52 54 50 50 50
MEDI | 1226 13 18 13 22 18 |MD 51 43 53 50 46 48
Table 3.2243.3 GPS week: 2243 Day: 3 MJD: 59948
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1270 28 50 31 28 34 19 | 44 47 55 52 36 39
R02 | 1231 5 14 9 12 14 6 | 67 67 68 63 61 66
R03 | 1006 7 13 13 14 20 6 | 50 44 52 50 42 48
R04 | 1362 14 10 12 20 12 8 | 59 50 50 53 49 51
R05 | 1677 12 11 16 20 12 9 | 49 47 59 54 55 51
R07 | 945 14 17 14 23 18 10 | 61 45 60 50 56 53
R08 | 1329 12 15 13 15 21 8 | 60 54 66 63 71 60
R09 | 1587 12 22 22 43 20 14 | 62 64 66 41 66 55
R11 | 1029 10 13 20 13 11 8 | 32 33 28 29 35 29
R12 | 1583 15 11 8 20 22 8 | 64 60 55 47 63 56
R13 | 640 35 34 31 51 17 21 | 65 43 47 43 55 46
R14 | 2324 13 9 17 8 22 7 | 55 54 52 57 67 53
R15 | 1343 11 10 11 10 16 6 | 68 75 76 69 64 71
R16 | 956 33 28 60 23 31 23 | 73 72 74 74 67 72
R17 | 734 12 14 7 12 14 6 | 39 35 33 40 39 36
R18 | 882 13 15 5 18 13 7 | 32 36 34 46 38 35
R19 | 1058 32 69 25 72 37 28 | 45 40 60 63 52 47
R20 | 941 50 117 39 65 65 39 | 67 58 95 71 74 65
R21 | 1035 11 22 15 25 24 10 | 35 34 43 45 47 38
XR22 | 1910 --- 149 --- 142 143 145 | --- 101 --- 39 39 59
R24 | 3049 10 38 15 25 23 13 | 47 31 48 55 41 44
------+------------------------------------+--------------------------------
RMS | 1410 21 37 23 31 25 |T 53 51 56 52 53 51
WRMS | 1410 17 22 18 24 21 |NE 54 52 56 52 54 51
MEDI | 1231 12 15 15 20 20 |MD 55 47 55 52 55 51
Table 3.2243.4 GPS week: 2243 Day: 4 MJD: 59949
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1241 24 37 22 30 46 16 | 45 45 45 58 42 40
R02 | 865 9 13 12 21 20 8 | 85 83 93 86 75 86
R03 | 1032 12 19 12 10 29 7 | 39 33 38 38 31 36
R04 | 1627 16 19 12 13 28 8 | 48 36 41 38 31 40
R05 | 1289 11 16 10 16 22 7 | 40 51 46 44 54 43
R07 | 1409 16 25 11 19 13 10 | 53 32 47 45 45 44
R08 | 1698 15 20 20 16 24 10 | 55 45 67 57 69 56
R09 | 1962 14 21 20 35 21 13 | 50 61 57 43 52 48
R11 | 614 11 14 20 22 14 10 | 32 38 39 44 34 35
R12 | 746 9 16 7 21 22 8 | 64 66 56 54 68 59
R13 | 997 30 18 19 32 14 15 | 53 41 42 38 46 39
R14 | 1734 9 12 7 12 19 5 | 49 51 43 38 56 44
R15 | 2012 18 14 17 8 15 9 | 58 51 51 55 60 52
R16 | 1566 30 35 68 25 29 25 | 98 93 114 103 96 100
R17 | 500 5 11 10 10 12 5 | 34 34 34 38 35 34
R18 | 818 11 18 11 9 18 7 | 30 28 27 29 26 27
R19 | 1776 47 79 23 59 29 30 | 41 45 42 43 44 35
R20 | 2291 39 135 61 72 66 44 | 63 79 99 60 69 66
R21 | 858 8 29 20 14 31 10 | 30 35 41 34 43 32
XR22 | 1114 --- 166 --- 120 124 141 | --- 105 --- 30 26 57
R24 | 1234 14 30 21 11 21 11 | 34 32 39 38 39 34
------+------------------------------------+--------------------------------
RMS | 1404 20 40 25 28 28 |T 50 51 53 48 49 47
WRMS | 1404 18 21 13 19 24 |NE 50 51 53 47 49 48
MEDI | 1241 14 19 17 19 22 |MD 48 45 43 43 45 43
Table 3.2243.5 GPS week: 2243 Day: 5 MJD: 59950
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1233 17 47 33 47 32 19 | 62 60 85 80 60 68
R02 | 783 8 15 10 22 25 7 | 71 75 66 64 82 68
R03 | 903 13 29 18 26 41 11 | 93 88 99 86 85 91
R04 | 1081 17 18 12 22 21 10 | 49 36 38 45 36 41
R05 | 591 6 15 13 15 14 6 | 40 35 44 42 46 39
R07 | 1243 7 26 24 29 14 12 | 60 49 62 59 59 56
R08 | 2260 11 22 15 18 17 9 | 47 36 53 51 49 46
R09 | 2729 14 10 20 43 25 13 | 54 54 61 28 56 48
R11 | 792 10 18 12 15 27 7 | 24 32 24 34 29 25
R12 | 554 9 23 16 18 25 9 | 74 75 55 67 76 66
R13 | 1284 20 45 15 40 24 16 | 65 56 54 39 49 54
R14 | 1335 6 18 12 10 19 6 | 47 55 34 53 40 44
R15 | 1831 12 14 12 12 19 7 | 60 49 48 56 41 54
R16 | 1355 29 33 60 36 24 24 | 105 98 101 98 108 101
R17 | 623 10 19 10 14 13 7 | 34 25 32 35 38 32
R18 | 759 10 9 10 12 18 6 | 25 21 24 26 24 22
R19 | 1894 26 82 16 69 28 26 | 36 55 32 47 34 32
R20 | 3107 34 142 30 104 54 42 | 42 68 56 60 44 37
R21 | 819 11 26 13 18 12 9 | 24 27 25 28 25 22
XR22 | 995 --- 160 --- 147 148 153 | --- 72 --- 32 26 47
R24 | 982 17 29 15 32 41 12 | 43 37 40 50 47 40
------+------------------------------------+--------------------------------
RMS | 1483 16 44 21 37 27 |T 52 52 51 51 50 49
WRMS | 1483 13 27 15 25 27 |NE 52 52 49 50 49 48
MEDI | 1081 11 23 15 22 24 |MD 47 54 48 50 46 46
Table 3.2243.6 GPS week: 2243 Day: 6 MJD: 59951
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1744 43 31 58 155 36 42 | 70 63 96 155 53 73
R02 | 1011 11 13 11 27 14 8 | 97 103 101 94 102 98
R03 | 1352 14 17 12 26 20 9 | 68 72 71 77 68 70
R04 | 1020 18 19 12 39 35 12 | 76 56 63 70 57 64
R05 | 985 18 13 16 38 15 12 | 69 60 58 67 64 60
R07 | 686 10 16 10 35 17 10 | 103 101 102 94 98 99
R08 | 1955 18 25 16 38 17 13 | 83 91 94 91 79 87
R09 | 2402 12 11 9 24 17 7 | 43 45 40 33 46 38
R11 | 1061 11 13 13 13 24 7 | 35 44 45 42 35 40
R12 | 888 14 17 21 33 14 12 | 82 77 84 71 80 78
R13 | 958 42 43 26 37 15 21 | 80 61 46 45 57 57
R14 | 958 6 11 9 20 14 6 | 62 66 58 59 64 60
R15 | 1665 17 12 13 9 18 8 | 86 74 66 73 71 74
R16 | 636 34 31 59 30 35 24 | 149 134 144 139 138 142
R17 | 986 11 19 8 14 15 7 | 55 43 53 60 57 52
R18 | 530 13 7 9 11 12 6 | 36 43 43 44 43 40
R19 | 1037 34 76 14 50 38 26 | 73 37 62 77 73 60
R20 | 1908 46 125 35 94 53 43 | 99 56 100 98 92 84
R21 | 717 9 18 12 27 22 9 | 43 39 45 50 53 42
XR22 | 1074 --- 123 --- 181 187 149 | --- 56 --- 33 30 47
R24 | 1761 14 31 12 26 46 12 | 59 39 61 66 72 56
------+------------------------------------+--------------------------------
RMS | 1313 23 38 24 49 27 |T 73 64 71 73 68 67
WRMS | 1313 21 26 13 30 24 |NE 73 64 70 69 68 67
MEDI | 1020 14 18 12 30 18 |MD 70 60 62 70 64 60
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