[IGSREPORT-28593] Wk 2202 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 8 05:25:56 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2202 (Mar 20, 2022 - Mar 26, 2022)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.2202.
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:
igl2202[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2202 in the SP3 format.
igl22027.sum Combination Report for GPS Week 2202.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -7.0 ns
1 | -7.3 ns
2 | -5.7 ns
3 | -6.6 ns
4 | -7.1 ns
5 | -7.3 ns
6 | -5.9 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 1.2202, 1a.2202).
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 2.2202.0-6)
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 3.2202.0-6).
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 2202 summary. (Mar 20, 2022 - Mar 26, 2022)
Table 1.2202.a GPS week : 2202 MJD: 59658.0-59664.0
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 3 2 -32 23 .13 21 16 | 27501 -143 3510 8995
| 1 1 1 21 8 16 .04 | 759 2081
emx n/a| 0 0 -2 53 54 30 -.09 36 28 | -10569 173 3504 8925
| 2 0 1 14 28 33 .05 | 13147 1360
esx n/a| 0 0 0 -19 -26 -39 -.08 27 20 | -8674 -248 3502 12031
| 1 1 2 11 14 36 .04 | 8268 1761
gfz n/a| 0 1 2 -28 11 -31 -.05 31 14 | 0 -155 3447 8664
| 1 1 2 28 12 23 .06 | 0 1781
grg n/a| 1 -2 -1 -1 5 50 .26 26 18 | -6769 -185 3508 8484
| 1 1 3 10 11 44 .05 | 615 1826
iac n/a| -2 0 -5 6 34 -39 -.29 32 29 | -4773 -420 3506 9629
| 2 2 4 22 36 114 .09 | 573 1140
Table 1.2202.b GPS week : 2202 MJD: 59658.0-59664.0
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 15 14 17 17 15 15 |
R02 | 7 7 7 7 9 11 7 |
R03 | 9 10 8 7 6 7 9 |
R04 | 10 8 8 9 12 9 9 |
R05 | 10 10 10 8 8 9 9 |
R07 | 7 7 8 9 7 7 7 |
R08 | 9 7 8 9 10 8 9 |
R09 | 8 7 8 10 8 9 7 |
R12 | 8 8 8 8 8 9 7 |
R13 | 18 13 14 15 17 14 16 |
R14 | 8 7 6 7 7 7 7 |
R15 | 5 7 7 8 7 6 7 |
R17 | 8 7 7 8 8 9 8 |
R18 | 7 7 7 7 8 8 8 |
R19 | 24 23 19 18 19 22 24 |
R20 | 22 26 24 29 23 20 22 |
R21 | 8 9 8 7 9 9 11 |
R22 | 23 24 28 22 26 25 24 |
R24 | 8 8 9 9 9 10 7 |
Table 1.2202.c GPS week : 2202 MJD: 59658.0-59664.0
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 2202 0 | -50 -45 28 -927 -469 -8977 80.4 1544 1544 | -7014 0
brd 2202 1 | 39 63 182 110 -812 -10390 80.2 1620 1620 | -7262 0
brd 2202 2 | 46 -124 187 692 -931 -8131 81.9 1453 1453 | -5736 0
brd 2202 3 | 83 -57 215 101 -2021 -4243 83.1 1376 1376 | -6647 0
brd 2202 4 | 93 7 71 -1554 -1134 -131 81.7 1420 1420 | -7058 0
brd 2202 5 | -66 35 139 -1824 -878 2173 82.4 1569 1569 | -7318 0
brd 2202 6 | 13 -27 150 -549 2732 5250 81.0 1540 1540 | -5948 0
-------------+------------------------------------------------------------+----------------
brd 2202 mean| 22 -21 139 -564 -502 -3492 81.5 1503 1503 | -6711 0
brd 2202 sdev| 61 63 66 928 1505 6049 1.1 88 88 | 635 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 2.2202.0 GPS week: 2202 Day: 0 MJD: 59658
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 4 -8 -16 -5 .06 21 15 | 26688 -250 3650 9223
emx n/a| 2 0 -4 37 31 31 -.10 40 30 | -17756 968 3596 9039
esx n/a| 1 0 2 -35 -22 -93 -.11 31 21 | -4621 -685 3625 11650
gfz n/a| 1 2 5 -9 16 -50 -.03 28 15 | 0 -183 3631 9078
grg n/a| 1 -2 -7 13 14 68 .28 23 17 | -6787 -464 3645 8619
iac n/a| -3 -1 -5 -27 53 -1 -.34 34 33 | -5117 -337 3654 9736
Table 2.2202.1 GPS week: 2202 Day: 1 MJD: 59659
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 -10 -37 29 .15 23 16 | 28015 -2180 3838 9156
emx n/a| 1 1 -4 54 63 7 -.01 40 30 | 4474 -929 3851 9196
esx n/a| 0 1 -1 -26 -25 -66 -.10 27 19 | -9058 -2253 3838 12250
gfz n/a| -1 3 2 9 -8 -10 -.08 27 14 | 0 -2456 3827 8773
grg n/a| 3 -3 -1 -6 2 97 .30 25 18 | -6319 -2063 3830 8768
iac n/a| -6 2 -3 28 66 -73 -.30 36 34 | -4884 -1940 3813 9827
Table 2.2202.2 GPS week: 2202 Day: 2 MJD: 59660
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 4 -23 -38 5 .15 20 16 | 27382 2244 3149 8700
emx n/a| -1 0 -1 42 55 36 -.13 36 30 | -22789 1523 3143 8735
esx n/a| 2 -2 -3 -13 -18 -21 -.06 26 21 | -2128 1929 3141 12230
gfz n/a| -1 0 0 -27 15 -8 -.02 32 13 | 0 2281 3124 8391
grg n/a| 3 -2 0 5 -15 54 .17 25 17 | -6937 1996 3157 8371
iac n/a| -2 -1 0 37 71 -32 -.18 33 30 | -4131 851 3136 9395
Table 2.2202.3 GPS week: 2202 Day: 3 MJD: 59661
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 -13 -33 32 .11 22 18 | 28610 -2015 2909 8587
emx n/a| 0 0 0 50 73 -13 -.16 34 26 | -22567 -1265 2909 8560
esx n/a| 0 0 -1 -1 -4 -21 -.12 24 19 | -2655 -1827 2886 11762
gfz n/a| 0 0 4 -14 4 -54 -.03 33 12 | 0 -827 2826 8376
grg n/a| 0 -1 2 -5 22 -30 .27 30 19 | -6020 -1728 2892 8139
iac n/a| -1 -3 -12 -3 -18 97 -.18 31 28 | -4484 -1335 2896 9264
Table 2.2202.4 GPS week: 2202 Day: 4 MJD: 59662
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 18 -32 36 .16 24 16 | 26531 1664 3628 8605
emx n/a| 2 0 -1 66 92 87 -.05 32 27 | -9614 1225 3613 8345
esx n/a| 0 0 0 -20 -50 19 -.12 25 21 | -1893 1804 3626 11339
gfz n/a| -1 0 0 -41 25 -29 -.04 32 14 | 0 641 3289 8104
grg n/a| 0 -4 0 -3 5 89 .30 29 19 | -7945 1594 3625 7983
iac n/a| -3 1 -8 -5 -1 -271 -.29 29 25 | -5524 1164 3640 9173
Table 2.2202.5 GPS week: 2202 Day: 5 MJD: 59663
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 2 24 -23 26 .14 21 15 | 28039 -2398 3759 9582
emx n/a| 0 2 0 46 61 10 -.07 37 26 | 10292 -1576 3769 9400
esx n/a| 0 -2 1 -10 -30 -53 -.02 29 20 | -18837 -1563 3752 12778
gfz n/a| -1 2 0 -39 23 -62 .02 31 16 | 0 -2103 3772 8999
grg n/a| 3 -1 -1 -17 5 55 .21 24 17 | -6487 -2059 3750 9194
iac n/a| -4 0 -8 19 11 17 -.45 28 25 | -5249 -1119 3749 10237
Table 2.2202.6 GPS week: 2202 Day: 6 MJD: 59664
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 30 -41 35 .18 20 14 | 27245 1928 3642 9118
emx n/a| -3 0 -2 79 4 51 -.09 33 25 | -16025 1268 3649 9201
esx n/a| 0 0 1 -26 -33 -39 -.04 29 21 | -21530 858 3647 12211
gfz n/a| 0 1 0 -79 5 -8 -.17 36 16 | 0 1556 3661 8927
grg n/a| 0 0 -5 6 3 16 .29 25 19 | -6894 1427 3658 8317
iac n/a| 1 0 0 -2 59 -15 -.26 30 25 | -4027 -230 3656 9772
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 3.2202.0 GPS week: 2202 Day: 0 MJD: 59658
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1052 44 44 49 22 20 37 16 | 110 75 74 93 87 81 85
R02 | 1331 9 13 16 16 14 27 7 | 68 60 76 71 63 66 66
R03 | 1496 10 26 17 10 13 42 8 | 92 78 92 95 97 103 92
XR04 | 882 14 23 21 --- 14 35 10 | 113 97 113 --- 109 108 108
R05 | 1776 19 16 30 17 25 13 9 | 80 71 98 90 77 80 81
R07 | 806 8 23 11 19 9 22 6 | 79 68 77 87 85 78 79
R08 | 1669 17 15 19 18 11 33 8 | 81 69 88 82 82 68 79
R09 | 1845 10 11 22 23 15 28 8 | 51 50 46 43 53 64 49
R12 | 1727 11 23 15 17 14 24 7 | 96 85 93 97 89 92 92
R13 | 544 20 50 46 30 53 33 17 | 107 78 73 94 106 104 93
R14 | 625 8 18 18 18 12 30 7 | 59 54 64 51 55 71 57
R15 | 1005 6 15 9 12 7 17 4 | 71 62 75 68 70 77 70
R17E | 2467 7 30 16 12 15 25 7 | 79 83 81 82 85 84 81
R18E | 1133 7 19 14 16 13 27 7 | 44 39 47 42 47 49 43
R19E | 996 29 105 57 53 30 51 24 | 114 115 126 126 122 115 114
R20E | 2819 35 59 58 51 43 59 22 | 133 139 139 152 121 122 130
R21E | 1066 9 31 17 14 11 26 8 | 58 52 54 54 58 58 55
R22E | 2246 47 57 42 66 34 54 22 | 35 35 68 62 65 70 46
R24E | 772 9 30 14 14 16 29 8 | 55 50 62 59 61 61 57
------+-----------------------------------------+-------------------------------------
RMS | 1543 21 40 31 28 23 34 |T 80 71 81 80 80 81 77
WRMS | 1543 15 30 21 15 17 33 |NE 83 70 80 79 81 82 79
MEDI | 1133 10 23 18 17 14 29 |MD 79 69 76 82 82 78 79
Table 3.2202.1 GPS week: 2202 Day: 1 MJD: 59659
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 818 40 37 39 17 20 34 14 | 75 54 49 65 56 67 57
R02 | 1375 4 19 9 10 14 35 7 | 42 39 52 49 43 60 45
R03 | 1700 7 23 15 18 23 42 9 | 59 58 66 75 80 52 65
XR04 | 456 8 22 13 --- 14 26 8 | 81 75 83 --- 87 83 81
R05 | 856 21 25 24 18 13 25 9 | 58 63 87 81 65 63 69
R07 | 615 13 21 10 7 10 26 6 | 53 48 50 44 46 47 47
R08 | 628 12 18 12 15 15 28 7 | 60 47 56 52 54 52 53
R09 | 1621 16 13 10 15 20 22 7 | 32 40 32 41 32 34 33
R12 | 1459 10 27 16 14 18 25 8 | 74 65 80 82 68 56 72
R13 | 1042 24 46 24 20 39 20 13 | 77 57 55 67 67 71 65
R14 | 779 12 17 16 17 8 15 6 | 45 43 50 42 44 45 43
R15 | 1744 8 13 15 11 17 22 6 | 52 51 69 56 54 72 57
R17E | 2164 7 27 14 13 11 21 6 | 32 32 28 34 37 33 30
R18E | 1401 8 22 14 13 20 23 7 | 31 36 31 27 32 29 28
R19E | 734 42 94 46 36 35 59 22 | 106 129 124 115 107 116 111
R20E | 4207 33 75 61 70 54 58 26 | 65 87 80 73 82 50 63
R21E | 954 12 33 13 16 17 31 8 | 74 69 71 67 76 94 73
R22E | 1773 50 63 46 60 40 71 24 | 46 55 63 86 66 70 53
R24E | 1344 15 26 16 12 14 24 7 | 27 25 32 30 27 30 25
------+-----------------------------------------+-------------------------------------
RMS | 1619 23 40 27 27 25 36 |T 57 56 60 60 59 59 56
WRMS | 1619 16 30 19 14 18 34 |NE 59 53 60 59 58 58 57
MEDI | 1344 12 25 15 15 17 26 |MD 58 54 56 56 56 56 57
Table 3.2202.2 GPS week: 2202 Day: 2 MJD: 59660
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 838 34 36 38 15 18 40 13 | 82 64 53 68 79 55 65
R02 | 1522 11 22 19 12 13 13 6 | 51 36 59 58 45 56 50
R03 | 1523 15 22 26 8 11 12 7 | 69 53 43 59 66 66 59
XR04 | 666 13 16 15 --- 14 24 8 | 79 68 66 --- 81 56 71
R05 | 756 14 23 27 15 14 36 9 | 67 51 74 68 65 82 65
R07 | 535 16 20 16 12 12 33 8 | 58 43 53 53 51 48 50
R08 | 827 14 19 14 18 14 30 8 | 59 54 58 58 56 55 55
R09 | 2087 12 15 18 16 24 18 8 | 42 47 45 40 39 45 39
R12 | 1515 10 24 15 12 14 26 7 | 75 72 83 65 76 85 74
R13 | 1581 14 49 36 25 36 31 14 | 74 64 52 81 87 79 71
R14 | 721 12 21 14 7 11 13 6 | 53 43 48 49 45 47 47
R15 | 1132 19 14 9 14 11 28 7 | 62 44 52 43 49 56 51
R17E | 1426 11 24 14 10 15 22 7 | 31 44 41 42 43 26 35
R18E | 1596 7 22 19 14 15 17 7 | 29 35 33 31 42 27 30
R19E | 802 30 78 34 42 34 44 19 | 112 119 112 98 119 109 107
R20E | 2571 33 56 40 82 54 47 24 | 49 36 53 79 63 55 45
R21E | 1088 8 30 13 17 22 12 8 | 42 41 44 38 54 42 41
R22E | 1542 42 60 55 84 54 76 27 | 39 65 72 70 75 118 55
R24E | 2180 15 29 16 13 15 29 8 | 30 31 34 32 31 31 28
------+-----------------------------------------+-------------------------------------
RMS | 1453 20 36 26 32 25 33 |T 58 53 56 57 61 59 54
WRMS | 1453 16 30 21 13 17 30 |NE 64 53 57 58 61 60 58
MEDI | 1426 14 23 18 14 15 28 |MD 58 47 53 58 56 55 51
Table 3.2202.3 GPS week: 2202 Day: 3 MJD: 59661
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 863 47 39 25 21 50 25 16 | 85 70 52 65 46 39 55
R02 | 1936 13 20 12 15 15 14 6 | 51 36 52 55 47 42 47
R03 | 1029 11 20 13 14 15 20 7 | 69 50 63 73 58 62 63
XR04 | 752 22 16 15 --- 18 18 9 | 67 49 50 --- 61 64 57
R05 | 660 18 16 19 10 16 30 8 | 49 43 37 46 51 33 40
R07 | 540 18 24 9 8 20 32 8 | 61 41 56 55 67 50 53
R08 | 844 17 18 18 14 14 30 8 | 52 41 57 56 53 35 48
R09 | 2615 13 12 15 16 37 33 10 | 21 26 29 30 28 45 23
R12 | 1510 21 15 12 10 21 22 7 | 68 49 48 45 41 63 51
R13 | 894 26 37 34 24 42 39 15 | 76 38 39 60 60 76 56
R14 | 711 8 23 15 6 15 16 6 | 46 30 51 40 35 54 42
R15 | 1151 19 17 8 10 13 28 7 | 54 36 46 40 43 38 42
R17E | 1227 11 29 13 12 16 20 7 | 27 38 35 27 34 26 28
R18E | 903 11 22 13 11 18 16 6 | 24 34 29 24 36 28 26
R19E | 1291 26 72 27 47 23 46 18 | 64 53 75 86 75 47 64
R20E | 1782 31 71 52 107 64 40 29 | 40 39 68 104 47 40 45
R21E | 1281 13 26 10 10 17 19 7 | 43 56 46 51 53 36 45
R22E | 938 35 44 48 59 53 56 22 | 32 44 67 50 72 50 38
R24E | 2376 8 30 19 18 16 30 9 | 30 26 28 30 33 37 27
------+-----------------------------------------+-------------------------------------
RMS | 1376 22 34 24 33 30 31 |T 50 42 48 52 49 45 44
WRMS | 1376 18 26 19 12 19 28 |NE 58 42 48 51 49 50 48
MEDI | 1029 18 23 15 14 18 28 |MD 51 41 50 50 47 42 45
Table 3.2202.4 GPS week: 2202 Day: 4 MJD: 59662
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 703 47 32 32 28 48 33 17 | 77 73 68 62 45 41 55
R02 | 1695 11 17 26 14 25 18 8 | 43 41 58 47 36 29 41
R03 | 823 9 20 9 12 14 19 6 | 70 50 63 60 66 66 63
XR04 | 525 15 15 16 --- 20 47 12 | 79 65 74 --- 73 54 67
R05 | 598 12 24 14 13 24 15 7 | 71 58 64 68 87 49 66
R07 | 913 10 20 12 8 19 24 7 | 62 49 61 56 61 52 55
R08 | 1265 16 20 32 15 15 28 10 | 53 46 77 59 57 37 54
R09 | 1518 15 18 14 18 15 20 7 | 36 37 38 38 28 40 34
R12 | 1402 16 20 8 19 23 20 8 | 73 70 72 61 69 74 68
R13 | 610 38 47 25 24 49 43 17 | 75 43 46 65 61 73 55
R14 | 599 14 17 14 13 21 16 7 | 47 38 48 38 40 47 41
R15 | 1199 16 21 12 11 12 19 6 | 64 50 57 58 56 43 54
R17E | 1927 6 24 12 13 23 23 7 | 38 41 40 47 51 38 40
R18E | 1266 9 14 15 17 22 23 7 | 28 26 30 32 32 35 28
R19E | 2363 31 69 35 44 28 48 19 | 119 131 134 127 116 96 118
R20E | 1166 30 52 48 79 56 33 23 | 51 48 81 71 52 60 50
R21E | 1883 13 30 15 14 16 32 9 | 127 133 133 133 142 107 129
R22E | 792 54 46 47 84 41 53 25 | 35 63 88 98 64 66 60
R24E | 2562 13 30 18 14 15 25 8 | 29 34 29 28 35 37 26
------+-----------------------------------------+-------------------------------------
RMS | 1419 24 32 25 32 29 29 |T 61 57 66 63 61 54 58
WRMS | 1419 16 27 21 14 19 25 |NE 62 51 60 55 56 50 54
MEDI | 1199 15 21 15 14 22 24 |MD 62 49 63 59 57 49 55
Table 3.2202.5 GPS week: 2202 Day: 5 MJD: 59663
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 647 35 27 52 26 27 21 15 | 68 49 74 64 57 58 58
R02 | 2082 20 16 37 16 25 28 11 | 39 40 61 43 32 37 37
R03 | 533 13 16 12 15 14 20 6 | 57 52 61 56 48 45 52
XR04 | 590 13 20 16 --- 12 25 8 | 81 66 75 --- 69 86 75
R05 | 562 14 20 30 17 11 30 9 | 58 51 75 67 56 69 60
R07 | 1372 10 17 19 12 15 21 7 | 54 46 47 55 63 62 54
R08 | 1855 12 26 16 20 14 24 8 | 44 46 54 51 53 55 48
R09 | 1074 14 18 17 23 17 25 8 | 46 46 44 44 48 56 45
R12 | 1435 14 26 16 14 22 27 9 | 63 60 72 69 60 72 64
R13 | 1140 29 52 26 36 14 32 14 | 70 56 61 61 50 67 58
R14 | 624 12 21 15 12 10 22 6 | 43 27 38 33 35 34 34
R15 | 1843 10 19 9 12 12 13 5 | 49 45 51 45 45 54 47
R17E | 1303 11 25 13 17 24 21 8 | 41 46 44 42 53 39 42
R18E | 1569 14 20 16 19 18 21 8 | 31 29 33 40 26 32 29
R19E | 2870 33 83 45 48 44 38 21 | 118 116 122 136 141 120 121
R20E | 1414 24 67 38 65 39 33 20 | 77 76 82 83 102 77 78
R21E | 805 14 22 16 17 15 34 9 | 87 89 86 82 87 80 84
R22E | 2246 39 58 58 77 49 49 24 | 30 37 85 118 58 54 47
R24E | 2289 21 33 20 15 13 24 9 | 45 44 50 39 45 45 40
------+-----------------------------------------+-------------------------------------
RMS | 1569 21 37 29 31 24 28 |T 57 53 63 62 59 60 56
WRMS | 1569 15 26 20 16 17 25 |NE 56 48 59 53 51 57 52
MEDI | 1372 14 22 17 17 15 25 |MD 54 46 61 55 53 56 52
Table 3.2202.6 GPS week: 2202 Day: 6 MJD: 59664
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 590 29 27 51 28 31 25 15 | 99 71 64 85 82 89 79
R02 | 875 7 17 25 11 10 22 7 | 53 40 69 46 53 58 52
R03 | 727 16 19 24 15 16 25 8 | 80 62 85 76 65 67 72
XR04 | 630 16 16 13 --- 21 14 8 | 104 92 94 --- 86 98 95
R05 | 649 16 18 25 14 18 24 8 | 75 65 94 87 80 70 77
R07 | 1360 7 22 17 14 14 22 7 | 72 59 66 77 79 81 71
R08 | 1483 9 20 23 24 23 20 8 | 63 55 70 73 66 75 65
R09 | 902 16 17 9 17 15 15 6 | 51 58 51 55 47 52 50
R12 | 1433 16 22 15 9 15 16 7 | 93 81 99 96 90 100 92
R13 | 918 20 46 45 28 27 49 16 | 95 74 88 111 90 114 92
R14 | 1604 14 28 11 14 12 13 7 | 61 37 61 51 56 58 53
R15 | 1516 12 19 14 12 12 23 6 | 75 60 72 62 68 59 66
R17E | 723 8 30 14 24 16 17 8 | 56 57 54 58 55 51 54
R18E | 1306 9 15 22 21 22 16 8 | 35 30 39 31 39 35 32
R19E | 2448 34 80 46 78 39 49 24 | 146 141 146 179 151 144 145
R20E | 2271 32 51 32 77 55 44 22 | 104 108 119 130 115 101 107
R21E | 1261 16 20 19 16 23 47 11 | 80 73 81 82 84 68 76
R22E | 3170 40 46 59 78 43 51 23 | 48 54 97 117 84 60 60
R24E | 1719 9 27 12 15 12 20 7 | 51 61 54 55 58 64 55
------+-----------------------------------------+-------------------------------------
RMS | 1540 20 33 29 36 25 30 |T 75 67 79 81 76 76 73
WRMS | 1540 14 25 21 16 19 25 |NE 76 62 76 74 71 76 72
MEDI | 1306 16 22 22 16 18 22 |MD 75 61 72 76 79 68 71
More information about the IGSREPORT
mailing list