[IGSREPORT-28277] Wk 2180 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 5 05:47:27 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2180 (Oct 17, 2021 - Oct 23, 2021)
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 2.2180.
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:
igl2180[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2180 in the SP3 format.
igl21807.sum Combination Report for GPS Week 2180.
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 | -0.9 ns
1 | -2.6 ns
2 | -4.7 ns
3 | -1.8 ns
4 | -3.4 ns
5 | -9.6 ns
6 | 2.6 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 1.2180, 1a.2180).
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 2.2180.0-6)
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 3.2180.0-6).
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 2180 summary. (Oct 17, 2021 - Oct 23, 2021)
Table 1.2180.a GPS week : 2180 MJD: 59504.0-59510.0
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 0 2 9 28 .11 20 15 | 13018 -1520 4700 16336
| 0 0 0 10 21 18 .04 | 6182 2720
emx n/a| 0 0 0 -22 -8 -31 -.10 37 33 | -4049 -645 3602 8699
| 1 2 2 23 27 32 .02 | 10589 1447
esx n/a| 0 1 0 -7 -20 20 -.05 27 19 | -1468 -1214 4690 16436
| 0 1 0 19 23 22 .03 | 9067 3061
gfz n/a| 0 0 0 25 3 22 -.00 34 17 | 0 -1878 4805 16519
| 1 1 2 24 26 31 .03 | 0 2990
grg n/a| 0 -3 4 -11 0 -46 .20 27 21 | -4549 -1479 4655 15951
| 1 1 4 7 17 42 .04 | 4435 2719
iac n/a| 0 1 -5 2 19 -13 -.24 27 27 | -2955 -990 4678 16662
| 2 1 1 37 37 65 .06 | 4469 2255
mcc n/a| -1 -3 8 30 13 135 -.69 156 156 | --- --- --- ---
| 8 8 15 73 84 214 .15 | --- ---
Table 1.2180.b GPS week : 2180 MJD: 59504.0-59510.0
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 | 14 13 14 14 15 14 12 |
R02 | 5 7 6 6 8 5 6 |
R03 | 5 6 5 6 5 7 6 |
R04 | 11 8 7 7 7 7 7 |
R05 | 9 9 7 7 8 8 8 |
R07 | 6 8 6 6 8 5 7 |
R08 | 6 6 9 6 10 9 8 |
R09 | 7 7 8 9 8 7 7 |
R11 | 9 8 9 8 11 10 8 |
R12 | 12 13 14 11 10 11 10 |
R13 | 15 18 20 18 16 16 17 |
R14 | 8 8 8 9 9 10 10 |
R15 | 10 8 8 9 9 9 9 |
R16 | 14 17 15 14 16 16 16 |
R17 | 8 8 8 7 8 8 7 |
R18 | 8 8 8 10 9 9 8 |
R19 | 18 18 17 22 21 18 20 |
R20 | 19 23 22 22 22 23 19 |
R21 | 8 7 8 7 10 8 8 |
R22 | 18 26 30 28 25 22 28 |
R24 | 9 10 9 9 8 8 8 |
Table 1.2180.c GPS week : 2180 MJD: 59504.0-59510.0
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 2180 0 | 11 33 35 -26 -29 -1761 83.5 1729 1729 | -861 0
brd 2180 1 | -5 -96 24 -100 -1126 -5596 82.4 1784 1784 | -2575 0
brd 2180 2 | 56 -7 11 -532 -1819 -7092 82.5 1579 1579 | -4701 0
brd 2180 3 | -59 6 37 255 -1352 -9914 81.8 1515 1515 | -1849 0
brd 2180 4 | 7 16 48 816 -2119 -8080 80.8 1489 1489 | -3403 0
brd 2180 5 | 9 26 64 -626 -565 -6881 81.2 1577 1577 | -9565 0
brd 2180 6 | 19 -61 -1 90 -1255 -1493 82.3 1514 1514 | 2577 0
-------------+------------------------------------------------------------+----------------
brd 2180 mean| 5 -11 31 -17 -1180 -5831 82.1 1598 1598 | -2911 0
brd 2180 sdev| 34 48 22 487 710 3158 .9 114 114 | 3725 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 2.2180.0 GPS week: 2180 Day: 0 MJD: 59504
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 -31 11 .16 17 17 | 17972 1558 3874 8657
emx n/a| 0 1 -1 6 -8 20 -.11 32 28 | -1342 316 3870 8972
esx n/a| 0 3 0 -5 6 26 -.02 25 21 | 3610 2445 3884 7502
gfz n/a| -3 -1 -2 27 -15 72 -.01 30 16 | 0 2079 3981 8393
grg n/a| 0 -2 10 -3 21 -28 .15 24 22 | -1880 1574 3872 8317
iac n/a| 3 -1 -4 -13 7 -34 -.17 24 24 | 753 783 3890 9227
mcc n/a| -3 10 -12 -76 19 351 -.73 177 177 | --- --- --- ---
Table 2.2180.1 GPS week: 2180 Day: 1 MJD: 59505
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 6 22 50 .06 21 16 | 16728 36 3352 8253
emx n/a| -2 -2 1 -27 -52 -6 -.07 34 32 | 4394 -1034 3337 8438
esx n/a| 0 3 0 16 -22 39 -.02 28 21 | -8362 887 3334 7829
gfz n/a| 0 -1 1 4 4 16 -.02 38 15 | 0 -642 3358 8107
grg n/a| -1 -3 1 -7 -12 -75 .23 24 19 | -2811 126 3363 7661
iac n/a| 1 0 -4 18 44 -26 -.18 28 28 | -849 -760 3348 8723
mcc n/a| 1 4 -6 -4 169 207 -.78 129 129 | --- --- --- ---
Table 2.2180.2 GPS week: 2180 Day: 2 MJD: 59506
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 12 13 41 .07 18 14 | 17418 -4052 3672 7989
emx n/a| 1 1 2 -19 -22 -35 -.12 40 37 | -23293 -2998 3670 8219
esx n/a| -1 2 1 -25 -33 58 -.05 32 20 | -3244 -3183 3671 6005
gfz n/a| -1 0 0 -13 -2 25 .04 34 19 | 0 -4609 3744 7436
grg n/a| 1 -5 5 -14 0 -79 .21 29 24 | -2995 -3708 3673 7579
iac n/a| -3 0 -6 30 48 -62 -.26 27 27 | -1228 -1920 3677 8574
mcc n/a| -5 -16 8 144 -79 282 -.52 134 134 | --- --- --- ---
Table 2.2180.3 GPS week: 2180 Day: 3 MJD: 59507
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 4 -7 38 .11 21 14 | 15969 -122 3275 8996
emx n/a| 0 2 0 -67 13 -31 -.09 39 33 | -9934 -21 3268 9171
esx n/a| 0 1 -1 1 -26 1 -.10 29 18 | 16140 -373 3261 10657
gfz n/a| 2 -1 -1 34 -37 -9 .01 30 14 | 0 -139 3280 8853
grg n/a| 2 -3 6 -7 16 -17 .17 32 26 | -1724 -449 3238 8397
iac n/a| -3 1 -3 -4 63 -14 -.19 27 27 | -521 1100 3264 9377
mcc n/a| 14 -3 1 21 23 276 -.95 187 187 | --- --- --- ---
Table 2.2180.4 GPS week: 2180 Day: 4 MJD: 59508
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 -7 22 38 .12 22 17 | 14121 -4891 4435 8061
emx n/a| 0 1 0 -17 -27 -49 -.10 35 28 | 7164 -1910 3625 7476
esx n/a| 0 0 0 -40 -44 -5 -.08 26 17 | -9024 -4607 4421 9237
gfz n/a| 1 1 0 17 29 -20 -.01 36 18 | 0 -5196 4609 7895
grg n/a| 2 -3 6 -22 -26 19 .20 27 21 | -1628 -4413 4144 7158
iac n/a| -2 2 -5 60 22 -46 -.25 31 31 | -1153 -3104 4413 8371
mcc n/a| -7 -4 23 69 61 0 -.67 146 146 | --- --- --- ---
Table 2.2180.5 GPS week: 2180 Day: 5 MJD: 59509
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 1 5 29 6 .14 21 15 | 1694 941 4652 17097
emx n/a| 0 -1 4 -27 24 -84 -.13 35 30 | -8134 1288 3545 8907
esx n/a| 0 0 0 0 17 8 -.06 23 16 | -908 1449 4754 18599
gfz n/a| 0 0 5 51 1 32 -.03 38 21 | 0 377 4940 17844
grg n/a| 2 -5 2 -20 14 -103 .25 26 20 | -13597 1229 4660 17185
iac n/a| -3 2 -7 -22 -46 130 -.29 26 26 | -12016 1405 4654 17274
mcc n/a| -9 -5 24 78 -46 96 -.68 146 146 | --- --- --- ---
Table 2.2180.6 GPS week: 2180 Day: 6 MJD: 59510
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 11 14 10 .12 19 16 | 7229 -4115 9644 55302
emx n/a| -1 -2 0 -6 11 -33 -.08 46 42 | 2796 -157 3905 9710
esx n/a| 0 0 0 0 -39 16 -.05 25 20 | -8493 -5119 9509 55227
gfz n/a| -1 1 2 56 42 42 .00 31 18 | 0 -5021 9728 57110
grg n/a| 0 -4 -2 -5 -12 -38 .22 26 19 | -7210 -4718 9636 55362
iac n/a| 0 3 -3 -52 -1 -42 -.32 29 29 | -5677 -4437 9501 55092
mcc n/a| -3 -6 21 -17 -52 -269 -.51 172 172 | --- --- --- ---
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 3.2180.0 GPS week: 2180 Day: 0 MJD: 59504
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 749 36 29 30 20 20 34 --- 13 | 93 91 64 77 71 58 --- 75
R02 | 1071 4 12 9 11 7 18 225 4 | 51 53 57 56 48 53 187 52
R03 | 1162 8 11 15 13 11 15 181 5 | 68 67 71 71 71 70 54 69
XR04 | 876 22 23 15 --- 12 29 --- 10 | 72 64 56 --- 55 57 --- 60
R05 | 762 22 15 18 24 9 24 110 9 | 62 52 52 43 49 42 52 49
R07 | 1455 7 12 14 15 16 14 281 5 | 68 69 71 64 61 68 179 66
R08 | 1118 10 10 15 13 13 17 --- 6 | 57 60 70 69 63 60 --- 62
R09 | 2604 13 16 12 23 13 10 --- 6 | 48 59 55 51 51 52 --- 50
R11 | 5213 20 15 17 25 20 21 --- 9 | 44 29 45 39 40 33 --- 37
R12 | 886 7 47 28 24 28 18 --- 11 | 90 44 69 105 109 100 --- 87
R13 | 1394 24 49 38 23 34 35 --- 15 | 102 53 59 86 107 93 --- 84
R14 | 1305 8 34 20 9 17 14 --- 7 | 67 40 70 67 74 69 --- 64
R15 | 666 8 41 21 18 26 19 78 9 | 87 54 70 90 104 94 28 83
R16 | 1263 18 28 25 36 43 29 --- 13 | 68 59 85 68 76 90 --- 72
R17E | 1180 9 28 14 13 19 20 --- 7 | 100 101 101 101 99 97 --- 99
R18E | 1280 9 22 20 20 21 20 --- 8 | 42 41 50 40 52 49 --- 44
R19E | 991 25 64 33 45 36 41 --- 17 | 119 131 120 120 117 115 --- 116
R20E | 1332 27 50 49 59 39 40 --- 19 | 66 55 66 88 59 56 --- 57
R21E | 717 9 33 12 19 13 18 88 7 | 66 67 70 75 71 74 91 68
R22E | 1074 18 24 47 73 37 29 --- 18 | 52 66 67 69 60 64 --- 53
R24E | 2212 11 30 22 19 20 18 --- 8 | 46 40 45 46 49 43 --- 43
------+----------------------------------------------+------------------------------------------
RMS | 1729 17 32 25 30 24 24 177 |T 69 61 67 71 70 68 98 66
WRMS | 1729 17 28 21 16 22 24 177 |NE 69 56 63 68 69 67 100 65
MEDI | 1162 11 28 20 20 20 20 110 |MD 67 59 67 69 63 64 54 64
Table 3.2180.1 GPS week: 2180 Day: 1 MJD: 59505
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 557 32 27 17 18 19 49 --- 13 | 62 56 42 62 50 36 --- 48
R02 | 1281 10 19 14 14 11 27 140 7 | 35 38 41 31 29 38 123 33
R03 | 1262 11 8 7 21 13 13 151 5 | 44 42 45 36 46 41 33 41
XR04 | 1494 17 17 14 --- 18 12 --- 8 | 47 45 38 --- 39 44 --- 42
R05 | 1506 23 11 22 13 12 28 112 9 | 42 35 42 34 33 32 49 33
R07 | 965 12 17 16 15 14 26 191 7 | 48 47 48 53 51 47 78 47
R08 | 598 13 13 13 10 11 16 --- 5 | 40 39 50 37 47 49 --- 43
R09 | 2547 13 13 17 18 20 15 --- 7 | 40 46 45 43 34 45 --- 39
R11 | 5317 18 22 18 14 19 18 --- 8 | 30 23 24 31 35 35 --- 29
R12 | 927 20 61 28 24 24 14 --- 13 | 70 25 45 77 73 63 --- 59
R13 | 1077 25 53 51 47 35 26 --- 17 | 79 48 41 97 71 75 --- 65
R14 | 2034 11 34 22 15 12 16 --- 8 | 57 35 62 59 53 45 --- 51
R15 | 816 11 34 12 15 17 22 84 8 | 68 46 60 54 76 78 28 64
R16 | 1303 27 50 22 36 51 29 --- 16 | 53 56 53 53 36 63 --- 48
R17E | 1191 11 30 19 12 10 18 --- 7 | 71 65 77 68 72 71 --- 70
R18E | 928 12 20 13 21 15 23 --- 7 | 41 40 49 46 48 46 --- 43
R19E | 2263 20 50 30 67 31 38 --- 17 | 92 99 91 108 99 100 --- 93
R20E | 916 41 53 56 74 41 48 --- 23 | 56 50 78 83 59 53 --- 51
R21E | 790 9 27 14 13 10 12 49 6 | 46 38 48 45 47 46 61 44
R22E | 943 41 37 66 104 41 47 --- 26 | 39 64 94 74 49 55 --- 48
R24E | 1874 11 36 19 20 15 32 --- 10 | 41 39 46 51 50 57 --- 44
------+----------------------------------------------+------------------------------------------
RMS | 1784 21 34 28 38 24 28 129 |T 52 46 53 57 52 53 62 49
WRMS | 1784 16 32 21 15 19 28 129 |NE 51 41 45 51 48 49 62 45
MEDI | 1191 13 27 18 18 17 23 112 |MD 47 45 48 53 49 47 49 47
Table 3.2180.2 GPS week: 2180 Day: 2 MJD: 59506
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 557 31 40 25 30 25 32 --- 13 | 76 80 76 70 62 60 --- 69
R02 | 1313 9 15 10 8 13 18 116 5 | 43 43 34 40 35 36 58 37
R03 | 1560 6 8 11 9 12 18 137 5 | 57 52 58 52 58 48 54 54
XR04 | 1445 11 12 15 --- 14 14 --- 6 | 58 55 52 --- 54 50 --- 54
R05 | 2044 14 19 17 17 14 15 114 7 | 47 43 46 41 39 39 51 41
R07 | 506 9 13 17 9 18 18 228 6 | 58 55 54 61 65 50 175 56
R08 | 728 19 24 17 21 12 18 --- 8 | 48 44 66 68 57 59 --- 56
R09 | 2827 14 20 19 15 16 24 --- 8 | 39 37 42 44 45 54 --- 40
R11 | 3304 17 13 9 17 29 21 --- 8 | 43 20 39 37 41 43 --- 38
R12 | 1257 7 59 34 14 24 44 --- 13 | 81 55 64 85 92 119 --- 82
R13 | 1009 17 66 51 45 56 35 --- 19 | 85 53 53 113 111 72 --- 80
R14 | 2753 9 34 17 26 15 11 --- 8 | 58 40 64 78 64 55 --- 59
R15 | 575 7 37 12 14 23 12 93 7 | 77 58 75 77 95 79 37 77
R16 | 1371 18 49 38 34 43 22 --- 14 | 51 59 74 48 51 65 --- 54
R17E | 1622 13 34 17 11 13 18 --- 7 | 99 100 93 90 91 94 --- 94
R18E | 835 11 21 18 22 20 21 --- 8 | 48 40 55 50 61 48 --- 48
R19E | 1753 16 59 37 52 37 26 --- 16 | 88 82 98 104 89 94 --- 89
R20E | 670 38 63 56 57 27 51 --- 21 | 51 47 73 87 57 65 --- 50
R21E | 715 12 31 14 13 10 22 54 7 | 53 53 60 60 60 55 67 55
R22E | 969 35 63 84 101 72 39 --- 29 | 42 51 106 59 48 46 --- 45
R24E | 889 9 45 13 15 16 22 --- 8 | 40 56 44 46 48 41 --- 42
------+----------------------------------------------+------------------------------------------
RMS | 1578 18 40 32 34 29 26 134 |T 59 53 63 65 63 60 73 58
WRMS | 1578 14 37 20 19 24 26 134 |NE 58 49 56 62 62 59 75 56
MEDI | 1257 13 34 17 17 18 21 114 |MD 53 53 60 60 58 55 54 54
Table 3.2180.3 GPS week: 2180 Day: 3 MJD: 59507
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 671 34 32 20 30 37 34 --- 14 | 76 79 69 74 56 63 --- 67
R02 | 1288 9 7 17 16 11 16 166 6 | 39 43 57 43 42 52 54 44
R03 | 1603 12 8 7 15 11 15 154 5 | 52 49 50 54 54 48 43 50
XR04 | 1132 11 10 13 --- 9 21 --- 7 | 55 53 46 --- 50 50 --- 50
R05 | 1861 14 14 14 14 15 22 182 7 | 50 47 54 56 41 44 101 48
R07 | 541 13 12 9 13 14 21 342 6 | 56 50 54 49 43 51 305 50
R08 | 1150 13 17 8 16 13 17 --- 6 | 51 47 55 63 55 64 --- 55
R09 | 3119 12 16 20 18 27 19 --- 8 | 26 35 36 30 29 37 --- 27
R11 | 1867 18 21 16 9 20 26 --- 8 | 29 35 29 25 31 44 --- 27
R12 | 1271 12 37 24 10 28 35 --- 11 | 75 53 72 83 102 98 --- 79
R13 | 2768 29 56 49 34 35 43 --- 18 | 97 50 48 99 97 105 --- 81
R14 | 2372 8 34 19 18 17 19 --- 8 | 59 30 64 66 61 55 --- 56
R15 | 701 12 34 17 12 20 24 80 8 | 73 44 54 70 81 76 52 66
R16 | 741 23 38 30 19 46 28 --- 13 | 57 42 72 58 66 75 --- 59
R17E | 656 10 31 12 11 17 17 --- 7 | 61 61 64 56 65 67 --- 61
R18E | 965 17 31 17 16 22 26 --- 9 | 47 54 48 46 46 51 --- 45
R19E | 1109 30 73 35 60 63 40 --- 22 | 113 117 113 135 105 112 --- 111
R20E | 1030 36 65 45 73 32 32 --- 21 | 43 57 57 75 57 53 --- 47
R21E | 1071 11 26 10 10 10 22 52 6 | 40 30 34 35 40 39 80 35
R22E | 1005 41 77 82 63 76 39 --- 28 | 40 50 118 85 50 68 --- 56
R24E | 1064 12 31 13 19 21 22 --- 8 | 42 44 40 45 52 32 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1514 21 39 29 30 32 27 187 |T 56 50 58 62 58 61 105 54
WRMS | 1514 14 33 18 14 26 27 187 |NE 56 46 54 59 57 61 111 54
MEDI | 1109 13 31 17 16 20 22 154 |MD 52 49 54 56 54 53 54 50
Table 3.2180.4 GPS week: 2180 Day: 4 MJD: 59508
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 547 45 24 32 29 24 29 --- 14 | 70 55 58 56 41 64 --- 53
R02 | 1735 13 13 12 12 16 35 180 8 | 38 43 44 41 42 57 72 41
R03 | 1697 10 9 11 7 16 16 165 5 | 45 46 56 48 53 46 53 48
XR04 | 1280 10 15 12 --- 16 17 --- 7 | 48 51 49 --- 37 36 --- 44
R05 | 1065 18 15 15 11 12 34 100 8 | 45 39 42 31 32 20 42 34
R07 | 1092 14 10 16 17 22 28 123 8 | 57 53 54 51 42 59 143 50
R08 | 1241 19 16 16 31 18 29 --- 9 | 41 41 38 61 60 66 --- 48
R09 | 3411 15 16 18 18 10 26 --- 7 | 43 46 50 50 47 37 --- 43
XR11 | 1597 17 --- 25 10 23 30 --- 11 | 26 --- 45 36 34 36 --- 30
R12 | 1474 13 32 18 16 30 26 --- 10 | 61 46 64 69 74 57 --- 60
R13 | 2233 24 48 36 27 46 39 --- 16 | 83 53 49 58 103 98 --- 72
R14 | 998 12 32 17 17 11 32 --- 9 | 51 34 58 46 54 67 --- 50
R15 | 467 10 41 13 15 16 26 153 9 | 74 45 63 76 81 84 67 70
R16 | 940 23 33 31 38 40 45 --- 15 | 42 38 62 66 66 87 --- 56
R17E | 746 8 30 9 14 17 22 --- 7 | 94 94 89 92 89 103 --- 92
R18E | 627 8 24 18 18 24 26 --- 8 | 35 37 38 29 34 42 --- 32
R19E | 1146 34 77 28 61 45 40 --- 21 | 94 93 82 89 92 66 --- 77
R20E | 1043 27 67 46 77 33 34 --- 21 | 42 33 60 79 59 45 --- 44
R21E | 1808 13 30 18 13 20 37 141 9 | 44 40 47 46 49 46 108 42
R22E | 1119 41 37 58 94 41 35 --- 24 | 36 41 47 74 57 43 --- 27
R24E | 1808 12 24 13 19 15 20 --- 7 | 30 20 30 36 38 30 --- 27
------+----------------------------------------------+------------------------------------------
RMS | 1488 22 35 26 36 27 31 146 |T 52 47 53 56 56 56 80 49
WRMS | 1488 17 28 17 18 21 31 146 |NE 51 45 52 53 54 58 75 49
MEDI | 1146 14 24 18 17 20 29 141 |MD 45 43 50 51 53 57 67 48
Table 3.2180.5 GPS week: 2180 Day: 5 MJD: 59509
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1038 35 28 32 34 29 24 --- 14 | 52 46 42 36 41 45 --- 40
R02 | 1389 8 11 9 12 8 19 251 5 | 32 29 30 24 30 36 128 29
R03 | 831 10 15 10 12 16 26 139 6 | 39 37 36 35 48 58 23 40
XR04 | 1207 11 15 12 --- 10 20 --- 7 | 45 47 43 --- 55 53 --- 47
R05 | 658 15 22 22 22 15 14 93 8 | 40 41 53 32 34 41 28 38
R07 | 1259 8 10 10 18 12 14 138 5 | 50 50 57 42 52 57 110 51
R08 | 2032 16 13 17 29 16 24 --- 8 | 40 39 53 58 44 48 --- 44
R09 | 2936 11 15 10 17 12 27 --- 7 | 44 48 54 54 57 61 --- 50
XR11 | 4111 19 --- 16 16 21 23 --- 9 | 22 --- 23 26 32 23 --- 20
R12 | 1282 10 43 20 31 12 27 --- 10 | 60 39 59 79 67 65 --- 59
R13 | 1618 39 45 35 35 22 31 --- 15 | 78 42 42 43 60 63 --- 53
R14 | 509 14 37 14 14 17 34 --- 10 | 41 27 46 43 56 65 --- 44
R15 | 613 10 38 14 10 23 17 101 8 | 56 37 49 54 73 62 21 55
R16 | 1108 17 41 31 37 54 21 --- 15 | 53 40 58 69 92 66 --- 60
R17E | 1407 9 24 14 21 18 24 --- 8 | 74 70 73 75 71 66 --- 70
R18E | 1039 16 31 17 18 15 24 --- 9 | 36 29 36 34 44 34 --- 33
R19E | 2260 23 67 29 63 35 36 --- 18 | 177 198 172 168 178 169 --- 175
R20E | 1078 29 65 41 100 42 30 --- 23 | 49 41 51 100 63 41 --- 46
R21E | 1322 11 30 19 14 19 19 85 8 | 52 42 39 46 57 58 63 47
R22E | 2076 46 34 38 73 53 42 --- 21 | 88 54 80 79 66 71 --- 67
R24E | 2688 7 26 12 26 13 20 --- 7 | 27 25 26 39 37 30 --- 27
------+----------------------------------------------+------------------------------------------
RMS | 1576 21 35 23 38 26 26 146 |T 55 49 53 56 59 57 62 52
WRMS | 1576 15 30 16 21 20 26 146 |NE 46 40 46 45 52 53 62 45
MEDI | 1282 14 28 17 21 17 24 101 |MD 49 41 49 43 56 58 28 47
Table 3.2180.6 GPS week: 2180 Day: 6 MJD: 59510
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1330 25 32 22 29 22 30 --- 11 | 89 90 72 67 74 69 --- 76
R02 | 3091 13 10 10 14 11 19 321 6 | 49 49 55 51 54 58 175 51
R03 | 601 12 12 9 9 19 20 142 6 | 57 55 59 53 69 68 65 59
XR04 | 1013 11 10 19 --- 13 17 --- 7 | 61 60 49 --- 57 65 --- 57
R05 | 770 18 22 10 19 12 20 99 7 | 55 50 51 40 54 46 36 48
R07 | 536 12 14 14 18 12 22 166 6 | 78 76 73 65 75 78 120 73
R08 | 820 18 15 14 8 11 28 --- 7 | 63 66 77 78 73 79 --- 71
R09 | 2331 15 15 9 15 17 26 --- 7 | 59 65 62 68 64 69 --- 62
XR11 | 8617 15 --- 11 16 17 18 --- 7 | 35 --- 35 39 39 38 --- 34
R12 | 560 11 43 15 14 11 34 --- 9 | 81 46 68 82 85 97 --- 76
R13 | 827 37 77 38 25 28 29 --- 17 | 107 59 57 90 92 98 --- 83
R14 | 956 13 44 19 13 14 36 --- 10 | 65 40 72 69 74 82 --- 66
R15 | 565 10 42 13 13 17 27 111 8 | 81 49 70 84 94 95 40 80
R16 | 1829 20 40 34 44 48 25 --- 16 | 69 50 77 71 101 83 --- 74
R17E | 1170 10 29 10 16 11 24 --- 7 | 110 108 111 112 108 114 --- 110
R18E | 947 14 30 18 18 10 14 --- 7 | 51 49 59 58 53 48 --- 51
R19E | 1433 25 92 39 51 33 36 --- 19 | 175 202 178 179 178 167 --- 175
R20E | 1007 32 55 42 56 29 37 --- 18 | 54 42 50 81 56 48 --- 46
R21E | 688 11 35 14 14 15 15 72 7 | 67 59 63 68 72 73 103 66
R22E | 1404 29 103 54 81 72 49 --- 28 | 71 90 90 72 76 73 --- 66
R24E | 3396 12 24 14 15 18 25 --- 7 | 37 30 32 39 41 33 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 1514 19 46 25 31 26 28 172 |T 72 66 69 73 75 75 89 69
WRMS | 1514 16 42 20 18 19 28 172 |NE 67 58 62 65 71 73 87 65
MEDI | 1007 14 30 14 16 17 25 111 |MD 65 55 63 68 73 73 65 66
More information about the IGSREPORT
mailing list