[IGSREPORT-26812] Wk 2069 IGLOS Final Orbits
acc
acc at igs.org
Sun Sep 22 21:45:52 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2069 (Sep 01, 2019 - Sep 07, 2019)
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 2.2069.
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:
igl2069[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2069 in the SP3 format.
igl20697.sum Combination Report for GPS Week 2069.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://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 | -3.8 ns
1 | -5.2 ns
2 | -3.9 ns
3 | -3.0 ns
4 | -4.2 ns
5 | -2.5 ns
6 | -1.5 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 1.2069, 1a.2069).
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 2.2069.0-6)
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 3.2069.0-6).
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 2069 summary. (Sep 01, 2019 - Sep 07, 2019)
Table 1.2069.a GPS week : 2069 MJD: 58727.0-58733.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -1 14 -2 -15 .09 24 21 | 12836 -1010 2957 7365
| 0 1 2 14 12 42 .04 | 1987 1025
cof n/a| 0 0 -1 17 15 -3 .06 25 23 | 12825 -1004 2962 7368
| 1 1 3 20 21 47 .03 | 1981 1035
emx n/a| 0 0 1 80 -16 81 .01 25 25 | -3696 -835 2943 7389
| 0 1 2 24 14 41 .06 | 8493 831
esx n/a| 0 0 0 6 22 46 .13 21 19 | -8002 -533 2932 9054
| 1 0 1 14 18 38 .04 | 10450 1134
gfz n/a| 0 0 -7 -26 0 25 .14 24 17 | 0 -1059 2927 7282
| 1 1 2 21 11 24 .05 | 0 1185
grg n/a| 1 -1 7 -93 11 -207 -.39 32 26 | -3097 -843 2944 6767
| 0 1 3 15 25 53 .03 | 1174 1050
iac n/a| 0 0 1 4 -29 31 -.09 28 25 | -2872 133 3386 8195
| 2 1 2 36 27 80 .06 | 1141 1027
mcc n/a| 0 2 13 21 -105 216 .07 164 164 | --- --- --- ---
| 8 7 11 187 48 278 .23 | --- ---
Table 1.2069.b GPS week : 2069 MJD: 58727.0-58733.0
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 | 27 19 20 19 16 15 20 |
R02 | 9 8 7 7 7 7 7 |
R03 | 9 9 7 7 7 7 6 |
R05 | 8 7 8 8 8 8 9 |
R07 | 7 8 7 8 7 7 7 |
R08 | 7 9 8 8 7 7 6 |
R09 | 7 6 7 8 7 5 5 |
R11 | 7 7 8 7 7 7 8 |
R12 | 9 8 7 8 8 7 7 |
R13 | 10 9 9 6 9 9 6 |
R14 | 6 8 7 8 7 6 6 |
R15 | 10 8 7 10 9 5 7 |
R16 | 15 14 18 17 17 15 13 |
R17 | 10 10 10 9 9 10 10 |
R18 | 7 8 7 6 8 6 6 |
R19 | 24 22 26 24 22 27 26 |
R20 | 14 14 14 16 17 12 14 |
R21 | 11 11 9 9 11 11 9 |
R22 | 10 11 11 11 11 11 10 |
R23 | 10 8 10 9 9 8 7 |
R24 | 17 16 15 14 10 15 20 |
R26 | 0 22 16 17 25 19 18 |
R27 | --- --- --- --- 0 0 0 |
Table 1.2069.c GPS week : 2069 MJD: 58727.0-58733.0
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 2069 0 | -25 -3 139 -602 475 5381 83.3 1271 1271 | -3754 0
brd 2069 1 | 22 25 137 -1280 -1025 4968 83.9 1323 1323 | -5243 0
brd 2069 2 | 57 57 121 -361 410 4075 84.8 1315 1315 | -3913 0
brd 2069 3 | -45 -5 19 900 -514 1536 84.4 1259 1259 | -3041 0
brd 2069 4 | -5 -42 34 1355 -216 -1885 83.6 1280 1280 | -4244 0
brd 2069 5 | 15 54 9 296 -122 171 81.8 1052 1052 | -2506 0
brd 2069 6 | -43 -20 68 520 -1157 -218 83.3 1156 1156 | -1540 0
-------------+------------------------------------------------------------+----------------
brd 2069 mean| -3 9 75 118 -307 2004 83.6 1236 1236 | -3463 0
brd 2069 sdev| 37 37 56 916 639 2832 1.0 98 98 | 1215 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 2.2069.0 GPS week: 2069 Day: 0 MJD: 58727
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 0 6 -21 -66 .07 23 20 | 15586 388 3146 6602
cof n/a| 1 1 -2 -15 -19 -95 .06 22 21 | 15564 420 3159 6610
emx n/a| -1 0 -1 117 -34 125 .04 23 23 | -4412 -572 3135 6692
esx n/a| 0 0 1 -3 51 -23 .16 26 24 | 2549 1253 3129 8498
gfz n/a| -1 1 -5 -13 15 -5 .10 28 18 | 0 843 3116 6591
grg n/a| 2 -3 7 -85 -14 -150 -.41 38 23 | -4319 749 3125 6262
iac n/a| 0 0 4 -46 2 107 -.03 29 26 | -2801 409 3126 6782
mcc n/a| -13 15 28 -168 -96 492 .42 204 204 | --- --- --- ---
Table 2.2069.1 GPS week: 2069 Day: 1 MJD: 58728
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 0 3 -41 .01 25 21 | 14681 -2126 2908 7172
cof n/a| -1 0 -1 14 32 -18 .02 26 23 | 14675 -2129 2905 7177
emx n/a| 0 1 1 68 -14 36 .03 21 21 | -1447 -2093 2927 7403
esx n/a| 1 -1 1 13 35 87 .18 21 20 | -7440 -1438 2910 8825
gfz n/a| 1 -1 -10 0 15 4 .24 26 20 | 0 -1426 2901 7313
grg n/a| 0 0 3 -102 -2 -133 -.44 31 25 | -4479 -1973 2925 6860
iac n/a| -1 2 3 -9 -19 -5 -.05 26 24 | -2844 -217 3189 8517
mcc n/a| 4 10 24 -298 -75 -41 -.08 238 238 | --- --- --- ---
Table 2.2069.2 GPS week: 2069 Day: 2 MJD: 58729
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 9 0 -17 .10 27 23 | 12572 -335 2863 8308
cof n/a| 0 1 -1 36 30 -15 .03 30 26 | 12549 -322 2878 8311
emx n/a| 0 2 2 81 -7 86 -.06 25 25 | -18561 -1025 2877 8405
esx n/a| 1 0 0 29 5 25 .19 22 18 | -1567 175 2849 9897
gfz n/a| -1 -2 -6 -49 2 27 .16 22 16 | 0 -1679 2852 8269
grg n/a| 1 -4 7 -83 -25 -191 -.42 33 32 | -3395 -1235 2825 7592
iac n/a| -2 -1 2 -15 -3 49 -.05 29 26 | -4519 -222 3538 9572
mcc n/a| 0 1 9 13 -57 -127 -.07 173 173 | --- --- --- ---
Table 2.2069.3 GPS week: 2069 Day: 3 MJD: 58730
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 3 1 10 10 .16 26 24 | 13528 -64 2653 6929
cof n/a| 0 -3 3 -3 40 33 .07 27 26 | 13515 -50 2659 6932
emx n/a| 0 0 2 83 -15 67 -.03 29 29 | 5243 472 2677 6986
esx n/a| 1 1 -1 17 8 47 .11 21 19 | -1073 381 2663 8243
gfz n/a| 0 -2 -7 -31 -13 35 .10 21 14 | 0 420 2649 6947
grg n/a| 3 0 7 -97 26 -289 -.36 28 26 | -3113 435 2663 6220
iac n/a| -5 1 3 50 -54 126 -.12 30 26 | -2449 639 2853 7036
mcc n/a| -4 -2 6 216 -163 396 .36 148 148 | --- --- --- ---
Table 2.2069.4 GPS week: 2069 Day: 4 MJD: 58731
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 -13 19 .10 20 19 | 12728 -2249 2900 6304
cof n/a| 0 0 -1 21 15 35 .07 23 22 | 12712 -2232 2907 6307
emx n/a| 0 0 -2 78 1 94 -.03 23 23 | -10975 -1347 2866 6208
esx n/a| -2 -1 -1 3 35 79 .13 22 20 | -12612 -1325 2867 7795
gfz n/a| 0 0 -6 0 -3 38 .17 26 18 | 0 -2212 2859 6054
grg n/a| 1 -1 14 -116 18 -225 -.37 26 24 | -3206 -1720 2981 5870
iac n/a| 0 1 0 -10 -75 -19 -.09 27 24 | -4106 2003 3606 7846
mcc n/a| 0 -7 9 133 -62 64 -.13 164 164 | --- --- --- ---
Table 2.2069.5 GPS week: 2069 Day: 5 MJD: 58732
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 21 12 44 .07 23 20 | 10626 -1290 3105 7635
cof n/a| -1 0 -7 36 13 41 .11 24 21 | 10625 -1300 3110 7636
emx n/a| -1 0 4 96 -9 26 .02 26 26 | 510 -187 3080 7531
esx n/a| 0 -1 0 -16 6 71 .08 18 17 | -7083 -1763 3079 10170
gfz n/a| 0 0 -9 -46 -5 66 .13 24 17 | 0 -1678 3082 7440
grg n/a| 1 0 10 -68 37 -219 -.35 32 26 | -1909 -1345 3075 6893
iac n/a| 2 0 -1 10 -29 -106 -.15 27 24 | -2254 -406 3505 8120
mcc n/a| 12 -2 -3 123 -97 137 .07 109 109 | --- --- --- ---
Table 2.2069.6 GPS week: 2069 Day: 6 MJD: 58733
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 42 -8 -58 .09 25 23 | 10137 -1400 3125 8607
cof n/a| 0 0 -1 29 -1 -8 .06 27 23 | 10138 -1417 3121 8608
emx n/a| -1 0 1 36 -38 135 .12 28 26 | 3770 -1098 3044 8499
esx n/a| 0 0 1 3 16 38 .09 17 14 | -28791 -1014 3028 9954
gfz n/a| 0 0 -3 -43 -5 12 .10 24 14 | 0 -1684 3031 8360
grg n/a| 2 0 4 -103 38 -242 -.39 34 23 | -1263 -817 3020 7676
iac n/a| 0 1 0 55 -22 66 -.17 27 23 | -1136 -1271 3890 9494
mcc n/a| -3 1 15 128 -182 594 -.11 111 111 | --- --- --- ---
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 3.2069.0 GPS week: 2069 Day: 0 MJD: 58727
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 1252 62 55 30 35 55 116 28 --- 26 | 67 65 71 77 111 156 65 --- 76
R02E | 1524 13 14 28 25 14 13 14 195 8 | 70 67 81 70 69 74 72 104 72
R03E | 1267 11 11 23 13 29 15 14 83 8 | 32 34 41 35 42 28 38 83 33
R05E | 1582 14 13 22 11 15 20 15 --- 7 | 30 34 43 33 32 40 35 --- 33
R07E | 847 18 11 19 11 11 21 12 326 7 | 31 33 31 28 31 33 32 140 28
R08E | 1646 14 12 20 7 13 23 16 --- 7 | 38 37 41 38 40 33 43 --- 37
R09 | 2015 13 13 17 14 16 19 11 --- 7 | 34 35 39 38 39 38 44 --- 36
R11 | 537 10 12 12 18 15 15 19 196 6 | 44 44 43 41 41 45 40 51 40
R12 | 820 19 14 15 20 14 19 33 --- 9 | 57 61 53 65 63 62 54 --- 57
R13 | 2436 20 20 21 22 28 27 20 --- 10 | 44 44 40 54 58 62 47 --- 49
R14 | 725 9 6 17 15 14 12 11 --- 6 | 51 48 51 44 45 47 43 --- 45
R15 | 632 20 22 15 36 10 9 26 --- 9 | 64 66 54 51 56 62 59 --- 55
R16 | 982 27 18 27 33 27 57 20 --- 14 | 52 59 58 64 62 84 50 --- 58
R17 | 767 22 21 15 17 19 20 33 --- 9 | 65 65 54 50 67 56 41 --- 55
R18 | 1897 12 16 8 13 20 15 19 --- 6 | 45 46 43 47 45 45 41 --- 43
R19 | 898 39 43 42 56 62 52 71 --- 24 | 83 84 68 48 87 81 53 --- 65
R20 | 752 14 23 31 22 45 22 38 --- 13 | 67 69 44 51 76 63 51 --- 55
R21 | 637 21 20 14 23 32 9 40 137 11 | 70 70 56 55 72 60 47 64 59
R22 | 573 22 24 19 25 17 16 35 --- 10 | 64 64 57 40 55 61 40 --- 51
R23 | 1627 14 19 26 25 18 22 24 --- 9 | 41 43 48 50 50 46 43 --- 43
R24 | 830 15 22 27 40 30 76 29 --- 17 | 47 42 61 62 54 65 48 --- 51
XR26 | 1799 4 45 --- --- --- --- --- --- 0 | 100 113 --- --- --- --- --- --- 100
------+---------------------------------------------------+-----------------------------------------------
RMS | 1271 23 22 23 26 28 38 29 204 |T 54 55 51 49 56 59 46 88 51
WRMS | 1271 20 21 23 24 18 23 26 204 |NE 58 59 51 50 58 58 46 57 53
MEDI | 898 14 18 20 22 18 20 20 195 |MD 51 48 51 50 55 60 44 83 51
Table 3.2069.1 GPS week: 2069 Day: 1 MJD: 58728
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 1119 53 34 31 37 45 44 39 --- 18 | 59 67 71 83 90 81 87 --- 71
R02E | 823 14 19 18 15 19 19 18 100 7 | 49 55 46 51 48 59 45 89 48
R03E | 839 10 11 28 14 23 28 13 99 9 | 36 36 38 38 36 36 40 84 35
R05E | 1627 13 28 20 12 19 14 12 --- 7 | 23 35 33 24 30 22 32 --- 24
R07E | 812 17 20 17 13 18 26 9 484 7 | 31 34 43 36 35 43 39 88 35
R08E | 1618 17 22 19 22 12 25 11 --- 8 | 32 35 43 42 30 44 36 --- 34
R09 | 2443 13 14 15 12 14 9 10 --- 5 | 14 13 18 22 22 21 22 --- 16
R11 | 501 15 18 14 11 12 17 24 131 7 | 19 22 26 26 22 14 27 62 18
R12 | 614 15 16 11 18 13 28 23 --- 8 | 33 41 37 38 40 41 34 --- 34
R13 | 2186 16 20 18 15 21 25 18 --- 8 | 31 33 26 34 32 38 28 --- 29
R14 | 1010 16 18 18 14 22 11 20 --- 7 | 25 27 28 35 43 26 24 --- 27
R15 | 620 20 22 13 24 8 15 13 --- 7 | 32 32 31 24 29 34 38 --- 29
R16 | 945 22 27 18 25 18 64 24 --- 13 | 33 32 40 35 46 49 36 --- 35
R17 | 840 23 22 18 17 23 14 30 --- 9 | 28 30 30 32 43 28 26 --- 28
R18 | 2569 13 17 13 14 18 25 19 --- 7 | 25 30 26 28 33 34 18 --- 24
R19 | 802 58 45 33 43 44 55 59 --- 21 | 56 56 67 44 54 36 53 --- 47
R20 | 1246 31 47 27 16 47 31 30 --- 14 | 41 52 35 30 35 28 32 --- 28
R21 | 1169 23 24 16 22 31 16 37 113 11 | 39 40 38 32 44 31 31 83 33
R22 | 730 29 29 19 22 19 12 40 --- 11 | 33 32 27 23 29 25 21 --- 23
R23 | 1419 14 22 14 18 22 19 14 --- 7 | 30 34 29 28 41 24 24 --- 26
R24 | 1041 24 30 34 25 43 59 26 --- 16 | 27 33 35 33 33 35 32 --- 23
XR26 |15230 20 38 --- --- --- --- 23 --- 21 | 80 110 --- --- --- --- 54 --- 78
------+---------------------------------------------------+-----------------------------------------------
RMS | 1322 25 26 21 21 26 31 26 238 |T 35 39 36 35 38 35 35 81 33
WRMS | 1322 21 23 21 20 20 25 24 238 |NE 34 38 32 30 36 30 31 72 31
MEDI | 1010 17 22 18 17 19 25 20 113 |MD 32 34 35 33 35 34 32 84 29
Table 3.2069.2 GPS week: 2069 Day: 2 MJD: 58729
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 696 56 30 39 36 47 39 42 --- 19 | 65 73 67 85 101 82 75 --- 73
R02E | 781 18 19 18 16 17 14 10 118 7 | 54 54 56 45 54 59 47 40 50
R03E | 1245 15 17 20 10 15 13 17 74 6 | 32 40 34 29 30 31 40 38 29
R05E | 738 15 20 25 14 13 22 21 --- 8 | 40 47 56 38 40 38 34 --- 39
R07E | 1026 14 12 21 13 14 18 13 319 7 | 27 29 38 27 24 27 27 67 26
R08E | 1486 13 29 30 15 13 15 13 --- 8 | 29 42 44 34 33 36 36 --- 32
R09 | 2470 20 20 11 17 13 18 10 --- 7 | 31 32 33 34 36 38 32 --- 32
R11 | 545 20 20 16 12 12 16 25 130 7 | 31 34 28 32 26 33 28 46 26
R12 | 678 15 23 15 18 9 17 23 --- 7 | 33 41 32 32 31 33 30 --- 29
R13 | 1829 21 20 20 13 14 30 20 --- 8 | 29 31 30 36 33 44 41 --- 32
R14 | 895 15 17 14 10 14 19 17 --- 6 | 36 38 33 36 31 34 28 --- 31
R15 | 560 16 16 11 12 11 18 27 --- 7 | 38 38 38 46 36 41 30 --- 36
R16 | 740 28 28 27 25 14 84 44 --- 17 | 37 44 43 54 43 76 25 --- 42
R17 | 800 23 26 19 16 24 16 35 --- 10 | 39 41 33 29 47 34 25 --- 32
R18 | 2940 16 16 14 21 11 19 15 --- 7 | 30 36 25 38 38 29 28 --- 30
R19 | 1830 67 78 50 56 51 55 71 --- 26 | 59 69 53 43 58 41 27 --- 39
R20 | 1114 31 38 34 13 25 52 30 --- 14 | 64 68 47 47 52 42 42 --- 45
R21 | 987 16 20 17 13 18 24 34 108 9 | 45 49 39 44 47 55 35 66 43
R22 | 609 29 41 20 17 16 11 39 --- 10 | 50 57 47 39 41 38 30 --- 39
R23 | 1350 29 26 24 21 15 18 15 --- 9 | 32 37 27 36 35 34 32 --- 29
R24 | 965 20 38 33 30 32 58 23 --- 15 | 42 49 35 33 40 38 48 --- 32
XR26 | 3103 14 35 --- --- --- --- 17 --- 15 | 63 50 --- --- --- --- 40 --- 57
------+---------------------------------------------------+-----------------------------------------------
RMS | 1314 27 30 25 22 22 33 29 173 |T 41 45 39 39 41 42 35 51 37
WRMS | 1314 23 26 25 18 16 32 26 173 |NE 41 44 36 38 39 40 32 56 35
MEDI | 965 18 20 20 16 14 18 21 118 |MD 37 41 38 36 38 38 32 46 32
Table 3.2069.3 GPS week: 2069 Day: 3 MJD: 58730
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 725 47 34 45 42 47 28 38 --- 19 | 43 45 46 77 72 51 53 --- 48
R02E | 1603 9 12 16 14 14 18 26 195 7 | 77 79 80 86 79 80 61 47 77
R03E | 1193 11 13 24 9 16 19 17 73 7 | 38 36 43 44 48 44 42 42 41
R05E | 832 17 16 28 10 14 17 17 --- 7 | 33 35 38 33 41 35 34 --- 33
R07E | 1058 11 9 25 12 18 18 26 189 8 | 25 26 28 29 29 31 33 113 25
R08E | 1260 12 14 27 13 16 15 18 --- 7 | 38 40 42 34 38 35 39 --- 34
R09 | 1837 17 15 18 18 21 13 18 --- 8 | 19 23 19 30 25 22 23 --- 18
R11 | 540 18 21 16 10 5 17 22 135 6 | 33 34 31 31 27 31 25 33 27
R12 | 755 22 14 10 17 10 18 19 --- 7 | 42 35 30 31 33 40 23 --- 31
R13 | 1801 14 20 15 12 10 20 12 --- 6 | 29 28 31 36 34 37 26 --- 30
R14 | 986 16 17 21 18 16 17 10 --- 7 | 34 33 34 25 28 35 28 --- 26
R15 | 507 18 22 27 13 22 27 28 --- 10 | 38 40 43 29 31 47 27 --- 31
R16 | 700 32 37 40 20 27 62 46 --- 17 | 32 40 41 49 37 61 23 --- 36
R17 | 592 28 28 22 16 15 15 27 --- 9 | 47 47 36 28 40 39 22 --- 33
R18 | 2543 13 17 18 11 9 11 14 --- 5 | 31 33 36 39 36 31 23 --- 32
R19 | 2057 61 68 46 55 47 40 70 --- 24 | 62 69 69 31 63 45 22 --- 40
R20 | 700 28 28 61 19 16 50 36 --- 16 | 53 54 59 46 52 64 33 --- 43
R21 | 728 25 26 19 11 10 17 31 107 8 | 54 54 38 44 49 39 30 57 42
R22 | 742 20 20 18 19 15 25 43 --- 10 | 52 52 41 43 50 57 26 --- 44
R23 | 822 27 34 28 19 7 17 16 --- 9 | 21 25 40 39 34 33 32 --- 30
R24 | 1682 27 43 39 20 31 48 14 --- 14 | 33 48 46 47 51 34 26 --- 34
XR26 | 4446 15 32 --- --- --- --- 18 --- 16 | 39 47 --- --- --- --- 25 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1258 26 27 29 21 21 28 30 148 |T 39 41 41 40 42 42 30 58 36
WRMS | 1258 24 26 29 19 14 26 26 148 |NE 38 41 39 36 39 41 25 45 33
MEDI | 832 18 20 24 16 16 18 19 135 |MD 38 40 40 36 38 39 26 47 33
Table 3.2069.4 GPS week: 2069 Day: 4 MJD: 58731
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 1238 26 24 43 35 41 31 32 --- 15 | 61 60 60 77 78 68 70 --- 62
R02E | 2963 13 11 17 12 14 16 18 175 6 | 69 75 76 77 75 82 71 50 73
R03E | 1063 13 11 18 13 19 17 12 64 7 | 35 36 38 42 38 35 40 52 36
R05E | 836 13 15 22 20 11 22 18 --- 8 | 43 43 40 49 41 47 46 --- 41
R07E | 739 18 12 17 13 15 14 13 259 6 | 32 30 28 27 31 29 29 181 26
R08E | 670 15 11 19 12 12 16 14 --- 6 | 34 30 35 31 26 32 33 --- 29
R09 | 1591 8 10 17 15 11 19 14 --- 6 | 32 34 37 35 43 43 37 --- 35
R11 | 486 16 20 15 9 7 22 16 137 6 | 35 34 30 30 30 28 35 41 30
R12 | 503 9 28 24 11 19 24 20 --- 8 | 37 49 37 42 47 53 39 --- 39
R13 | 1319 17 16 19 16 23 25 19 --- 9 | 32 32 31 42 43 49 34 --- 36
R14 | 1211 12 16 14 21 11 17 13 --- 6 | 37 41 34 37 37 43 34 --- 35
R15 | 578 16 17 15 23 9 20 26 --- 8 | 46 47 41 39 44 51 38 --- 42
R16 | 739 27 31 35 23 39 65 31 --- 17 | 32 38 41 37 44 46 38 --- 35
R17 | 820 21 23 19 21 12 18 30 --- 9 | 43 45 41 35 43 43 34 --- 38
R18 | 2008 14 16 18 14 25 13 11 --- 7 | 35 36 34 37 32 32 35 --- 31
R19 | 2022 46 47 38 43 68 24 69 --- 22 | 54 62 64 50 83 49 40 --- 51
R20 | 891 21 23 31 47 41 47 35 --- 17 | 52 57 56 44 70 51 34 --- 47
R21 | 563 20 24 17 22 27 14 35 115 10 | 47 46 40 39 52 39 38 66 40
R22 | 1383 24 24 20 16 20 15 41 --- 10 | 50 48 47 38 44 33 30 --- 38
R23 | 967 25 28 20 19 17 18 16 --- 8 | 30 27 47 44 44 36 37 --- 37
R24 | 1187 19 30 28 15 19 26 16 --- 9 | 49 59 50 53 65 33 44 --- 47
XR26 | 2893 21 65 --- --- --- --- 30 --- 25 | 70 116 --- --- --- --- 39 --- 65
XR27 | 3496 --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1280 20 23 23 22 26 26 27 164 |T 43 47 43 43 48 43 39 78 41
WRMS | 1280 19 22 23 20 18 24 24 164 |NE 42 48 42 40 48 41 36 53 40
MEDI | 1063 17 20 19 16 19 19 18 137 |MD 37 43 40 39 44 43 37 52 38
Table 3.2069.5 GPS week: 2069 Day: 5 MJD: 58732
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 577 37 20 36 19 40 33 29 --- 14 | 53 60 68 62 73 54 67 --- 58
R02E | 1903 16 9 23 9 19 16 11 120 7 | 65 70 65 72 65 78 57 27 66
R03E | 1492 14 16 21 7 16 18 12 106 6 | 44 46 42 46 52 46 39 43 44
R05E | 547 20 20 20 18 13 22 18 --- 8 | 24 23 32 26 31 39 36 --- 26
R07E | 545 14 11 28 7 14 13 16 129 7 | 29 27 35 28 27 26 26 188 25
R08E | 762 14 11 23 8 12 16 14 --- 6 | 38 39 42 32 37 30 36 --- 33
R09 | 1286 8 12 15 10 11 13 14 --- 5 | 23 25 30 33 25 33 34 --- 27
R11 | 482 14 12 10 7 14 24 21 79 6 | 23 26 24 28 23 34 25 46 24
R12 | 595 15 13 18 12 10 18 12 --- 6 | 32 34 32 32 34 35 34 --- 31
R13 | 1529 18 17 22 14 24 26 22 --- 9 | 21 26 24 32 36 31 21 --- 26
R14 | 827 12 13 15 11 9 22 17 --- 6 | 25 24 25 26 27 33 26 --- 24
R15 | 572 16 14 11 8 9 12 14 --- 5 | 39 38 36 41 40 40 33 --- 37
R16 | 757 22 27 22 12 35 70 30 --- 14 | 31 33 29 31 29 33 31 --- 26
R17 | 921 28 28 18 20 10 19 36 --- 10 | 30 30 30 23 24 30 23 --- 24
R18 | 1154 10 11 11 13 15 17 17 --- 6 | 24 25 28 30 31 25 26 --- 26
R19 | 1620 62 60 69 48 57 65 63 --- 26 | 46 51 72 35 59 45 31 --- 37
R20 | 762 20 29 31 27 25 35 28 --- 12 | 28 39 46 30 34 35 28 --- 28
R21 | 802 21 26 21 15 18 33 38 106 10 | 34 37 30 37 42 44 35 63 34
R22 | 1121 24 26 19 23 24 21 37 --- 11 | 31 32 32 24 39 31 27 --- 28
R23 | 897 24 19 18 20 14 15 14 --- 8 | 24 34 32 32 34 28 22 --- 27
R24 | 1274 20 38 39 11 36 59 37 --- 15 | 44 60 39 31 59 36 49 --- 38
XR26 | 3618 14 66 --- --- --- --- 23 --- 18 | 47 58 --- --- --- --- 30 --- 45
XR27 | 2430 --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1052 23 24 26 18 24 32 27 109 |T 34 38 37 34 39 37 33 73 33
WRMS | 1052 20 21 26 17 17 26 24 109 |NE 31 35 33 31 35 34 29 54 30
MEDI | 897 16 17 21 12 15 21 18 106 |MD 31 34 32 32 34 34 31 46 28
Table 3.2069.6 GPS week: 2069 Day: 6 MJD: 58733
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 1101 34 26 59 27 66 28 41 --- 19 | 46 49 75 58 78 54 61 --- 52
R02E | 1796 9 15 21 8 14 11 26 117 6 | 42 46 37 45 46 45 49 59 42
R03E | 1101 14 17 16 9 14 12 14 96 6 | 56 56 64 61 65 56 62 60 60
R05E | 610 18 18 23 17 16 20 21 --- 8 | 39 41 42 57 46 29 42 --- 43
R07E | 844 15 19 26 9 18 14 15 137 7 | 44 46 44 45 46 46 42 171 42
R08E | 1281 13 17 22 7 11 15 16 --- 6 | 54 55 60 51 55 46 54 --- 52
R09 | 1477 7 7 14 8 10 14 17 --- 5 | 27 28 30 27 33 35 32 --- 27
R11 | 534 14 16 17 9 12 17 33 107 7 | 33 34 29 33 33 40 22 35 30
R12 | 618 11 13 15 16 12 13 18 --- 6 | 47 47 40 53 49 57 39 --- 46
R13 | 2389 11 12 13 9 13 24 14 --- 6 | 32 34 32 45 43 48 36 --- 38
R14 | 724 9 9 13 10 15 18 13 --- 5 | 38 37 40 40 44 44 33 --- 38
R15 | 551 23 18 12 16 12 11 14 --- 7 | 52 51 44 42 50 52 40 --- 46
R16 | 776 33 32 37 17 21 50 18 --- 13 | 36 38 43 46 43 67 34 --- 40
R17 | 1119 27 28 15 19 19 15 36 --- 10 | 59 62 48 36 54 50 26 --- 44
R18 | 857 9 9 15 9 11 21 11 --- 5 | 39 40 42 44 36 41 32 --- 38
R19 | 768 74 72 54 49 40 75 56 --- 25 | 89 94 51 39 88 84 26 --- 55
R20 | 669 19 20 45 18 31 48 33 --- 14 | 57 66 33 52 67 53 36 --- 47
R21 | 1052 31 26 17 13 8 18 21 95 8 | 64 64 45 52 65 50 40 93 51
R22 | 1250 28 26 17 13 12 20 36 --- 9 | 61 61 45 42 54 51 28 --- 46
R23 | 1015 13 24 24 10 15 15 15 --- 6 | 36 37 47 51 53 42 39 --- 43
R24 | 1717 29 56 43 9 47 91 37 --- 19 | 67 89 45 51 60 53 43 --- 49
XR26 | 3038 15 56 --- --- --- --- 19 --- 17 | 62 77 --- --- --- --- 34 --- 61
XR27 | 2067 --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1155 25 27 28 17 24 34 27 111 |T 49 52 44 46 52 49 38 83 45
WRMS | 1155 23 23 26 14 14 23 23 111 |NE 49 53 40 43 51 51 33 64 43
MEDI | 1052 15 18 17 10 14 18 18 107 |MD 46 47 44 45 50 50 36 60 44
More information about the IGSREPORT
mailing list