[IGSREPORT-27242] Wk 2102 IGLOS Final Orbits
acc
acc at igs.org
Thu May 7 20:22:12 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2102 (Apr 19, 2020 - Apr 25, 2020)
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 2.2102.
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:
igl2102[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2102 in the SP3 format.
igl21027.sum Combination Report for GPS Week 2102.
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 | 0.6 ns
1 | 0.9 ns
2 | -0.8 ns
3 | -1.8 ns
4 | -1.2 ns
5 | -1.3 ns
6 | -1.1 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 1.2102, 1a.2102).
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 2.2102.0-6)
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 3.2102.0-6).
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 2102 summary. (Apr 19, 2020 - Apr 25, 2020)
Table 1.2102.a GPS week : 2102 MJD: 58958.0-58964.0
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 28 -3 39 .08 18 16 | 19776 626 3396 8423
| 0 0 1 11 15 19 .04 | 1219 1032
cof n/a| 0 0 0 23 0 36 .05 21 18 | 19790 627 3401 8436
| 0 1 1 11 24 17 .04 | 1237 1038
emx n/a| 1 0 0 24 6 27 .03 29 29 | -4872 555 3171 8274
| 1 1 2 23 23 13 .03 | 10072 953
esx n/a| 0 1 -1 -18 -28 -49 .17 32 27 | 1820 1517 3165 10133
| 1 1 1 14 11 29 .04 | 6995 1314
gfz n/a| 1 0 -3 -17 8 -69 .14 29 17 | 0 515 3194 7609
| 0 0 2 28 21 22 .06 | 0 1426
grg n/a| 0 0 3 -73 -5 -7 -.38 24 18 | -749 330 3171 7109
| 0 1 1 26 15 44 .03 | 768 1165
iac n/a| -1 0 0 35 19 21 .02 22 22 | 617 401 3362 8465
| 1 1 1 28 43 20 .08 | 1290 1212
Table 1.2102.b GPS week : 2102 MJD: 58958.0-58964.0
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 | 15 17 17 14 17 16 15 |
R02 | 5 6 7 8 7 6 7 |
R03 | 8 8 9 6 8 9 7 |
R04 | 9 10 11 8 8 8 9 |
R05 | 7 8 7 9 7 11 10 |
R07 | 8 7 6 6 7 6 7 |
R08 | 7 8 7 6 7 6 7 |
R09 | 8 8 8 6 7 8 8 |
R11 | 7 6 6 5 6 6 5 |
R12 | 9 9 9 9 9 10 11 |
R13 | 18 19 18 16 17 22 22 |
R14 | 9 6 8 7 7 8 8 |
R15 | 10 9 9 8 8 8 9 |
R16 | 19 15 13 12 16 15 14 |
R17 | 8 7 6 7 8 7 6 |
R18 | 6 7 6 6 6 6 7 |
R19 | 18 17 17 20 21 16 20 |
R20 | 25 28 23 22 25 25 24 |
R21 | 8 8 7 7 7 7 6 |
R22 | 7 8 8 7 8 6 8 |
R23 | 10 10 10 10 11 9 11 |
R24 | 7 8 10 9 9 8 7 |
R26 | 11 14 14 17 14 22 17 |
Table 1.2102.c GPS week : 2102 MJD: 58958.0-58964.0
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 2102 0 | -68 -84 303 -382 634 4495 82.5 1411 1411 | 563 0
brd 2102 1 | 16 9 201 -196 3371 7221 82.7 1495 1495 | 920 0
brd 2102 2 | 63 -60 203 293 1755 6532 80.4 1891 1891 | -781 0
brd 2102 3 | -18 -61 173 244 1829 7784 82.2 1757 1757 | -1774 0
brd 2102 4 | 8 75 290 -1341 -516 6090 82.3 1910 1910 | -1157 0
brd 2102 5 | 27 40 253 -994 -506 5947 81.2 1692 1692 | -1298 0
brd 2102 6 | -20 -3 259 -294 -460 3834 80.5 9914 9914 | -1088 0
-------------+------------------------------------------------------------+----------------
brd 2102 mean| 1 -12 240 -381 872 5986 81.7 2867 2867 | -659 0
brd 2102 sdev| 41 59 48 603 1505 1409 1.0 3112 3112 | 1007 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 2.2102.0 GPS week: 2102 Day: 0 MJD: 58958
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 19 21 39 .02 19 15 | 18642 631 3145 8486
cof n/a| 0 0 0 24 17 61 .04 21 18 | 18632 636 3150 8495
emx n/a| 2 1 0 38 18 35 .04 29 29 | -4122 146 2869 8223
esx n/a| 0 1 -4 -21 -14 13 .18 32 35 | 3384 1442 2877 10002
gfz n/a| 2 0 -1 -3 13 -39 .13 30 16 | 0 414 2886 7658
grg n/a| 1 0 3 -81 -24 -67 -.34 25 20 | 729 -34 2881 7084
iac n/a| -2 0 0 8 -9 6 .04 20 20 | 610 1769 3120 8325
Table 2.2102.1 GPS week: 2102 Day: 1 MJD: 58959
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 35 -17 65 .10 19 16 | 18663 2534 3485 7885
cof n/a| 0 0 0 28 0 49 .09 19 18 | 18643 2566 3478 7884
emx n/a| -2 0 0 28 32 48 .03 30 30 | -4339 2150 3307 7258
esx n/a| 1 0 -2 4 -37 -60 .19 29 31 | -2764 3781 3295 9184
gfz n/a| 1 -1 -1 -9 22 -77 .18 30 18 | 0 3384 3316 6498
grg n/a| 0 0 3 -92 -13 -46 -.37 27 17 | -449 2667 3318 6137
iac n/a| 0 0 0 2 -4 9 -.05 21 21 | 2090 390 3474 7780
Table 2.2102.2 GPS week: 2102 Day: 2 MJD: 58960
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 21 -4 10 .06 18 14 | 21534 1098 3574 8591
cof n/a| 0 -1 -2 38 -18 9 -.01 20 17 | 21536 1078 3574 8598
emx n/a| 0 0 -2 10 3 29 .07 27 27 | -16091 927 3242 8244
esx n/a| -1 2 -1 -21 -37 -78 .08 30 23 | 2970 2438 3256 10297
gfz n/a| 0 0 -3 24 -19 -86 .17 28 18 | 0 1045 3275 7486
grg n/a| 0 0 4 -96 -22 60 -.36 24 20 | -962 564 3237 7220
iac n/a| -1 0 1 53 81 40 -.01 20 20 | 1840 -92 3472 8606
Table 2.2102.3 GPS week: 2102 Day: 3 MJD: 58961
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 47 -15 33 .14 18 15 | 20273 -4 3325 8348
cof n/a| 0 0 1 18 10 24 .03 24 20 | 20256 9 3325 8350
emx n/a| 2 0 -2 -11 -35 31 -.01 28 28 | 12762 -233 3045 8398
esx n/a| 0 0 -1 -4 -28 -48 .18 30 24 | 16036 1320 3025 10669
gfz n/a| 0 0 0 -3 23 -92 .06 27 17 | 0 -756 3061 7595
grg n/a| 1 1 1 -94 1 -11 -.37 20 16 | -1518 -203 3042 7473
iac n/a| 0 -1 0 71 40 49 .15 21 21 | 157 -423 3296 8275
Table 2.2102.4 GPS week: 2102 Day: 4 MJD: 58962
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 37 -19 46 .07 20 18 | 21202 -762 3566 9129
cof n/a| 0 1 0 32 -14 43 .04 21 18 | 21298 -736 3604 9243
emx n/a| 1 0 -1 59 -6 25 .00 30 30 | -15039 -791 3436 9112
esx n/a| 1 1 -1 -26 -44 -52 .20 31 22 | 901 -338 3416 10581
gfz n/a| 0 -2 -5 -28 15 -61 .14 29 17 | 0 -849 3469 8446
grg n/a| 0 0 2 -64 -4 -8 -.38 23 18 | -592 -1058 3426 7562
iac n/a| -2 0 1 6 43 2 .10 22 22 | 1032 1016 3591 9472
Table 2.2102.5 GPS week: 2102 Day: 5 MJD: 58963
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 15 0 58 .10 17 16 | 19100 710 3241 8558
cof n/a| 0 -1 0 3 -36 42 .06 20 18 | 19114 724 3277 8558
emx n/a| 2 -2 0 8 28 6 .04 28 28 | -9324 804 3073 8766
esx n/a| 1 2 0 -36 -19 -64 .18 35 27 | -3311 1411 3069 10224
gfz n/a| 0 -1 -6 -42 -25 -40 .22 31 18 | 0 196 3107 8280
grg n/a| 0 2 6 -23 9 -19 -.42 22 17 | -1500 542 3078 7232
iac n/a| -1 1 -3 62 31 3 -.03 23 23 | 407 -1574 3201 8787
Table 2.2102.6 GPS week: 2102 Day: 6 MJD: 58964
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 23 9 25 .07 17 14 | 19022 180 3439 7969
cof n/a| 0 -1 0 21 34 25 .11 20 17 | 19056 113 3403 7929
emx n/a| 0 0 3 36 4 13 .04 31 31 | 2045 884 3227 7921
esx n/a| 0 0 -1 -26 -20 -54 .17 34 26 | -4474 568 3222 9976
gfz n/a| 1 0 -2 -60 26 -91 .07 28 16 | 0 176 3245 7305
grg n/a| 1 -1 3 -63 15 37 -.40 24 19 | -956 -168 3220 7059
iac n/a| -4 3 -2 40 -50 39 -.05 25 25 | -1813 1722 3386 8011
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 3.2102.0 GPS week: 2102 Day: 0 MJD: 58958
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 730 36 44 26 65 21 16 19 14 | 86 94 68 36 57 60 63 60
R02 | 888 7 9 10 13 15 8 13 5 | 33 36 36 33 43 35 28 33
R03 | 472 10 15 10 30 11 15 20 7 | 62 66 55 51 60 68 65 59
XR04 | 809 11 18 17 34 --- 17 10 9 | 74 78 69 57 --- 74 62 66
R05 | 574 10 15 14 24 14 14 13 6 | 48 57 47 61 60 51 51 50
R07 | 501 13 16 21 12 23 11 17 7 | 62 63 50 62 73 62 62 60
R08 | 903 17 17 12 11 16 10 23 7 | 49 48 41 51 46 43 39 43
R09 | 3587 13 18 15 17 12 22 20 7 | 20 28 32 28 35 28 35 26
R11 | 1809 11 19 18 10 10 10 21 6 | 58 64 53 56 57 55 49 54
R12 | 784 19 23 30 27 17 12 17 9 | 88 93 68 83 93 84 91 84
R13 | 1702 18 20 40 72 45 37 23 17 | 121 121 89 76 131 124 128 112
R14 | 826 9 21 25 21 27 20 16 8 | 79 87 58 66 91 87 73 76
R15 | 698 8 7 20 42 9 20 19 9 | 79 80 70 51 75 82 85 74
R16 | 1246 25 17 50 28 50 60 29 18 | 56 64 46 63 72 74 81 63
R17E | 1806 7 12 28 11 26 18 11 8 | 47 49 43 45 45 45 49 45
R18E | 751 9 10 15 21 13 14 12 6 | 38 41 40 47 46 35 50 41
R19E | 1145 42 31 49 41 44 21 37 17 | 42 47 33 70 71 46 46 43
R20E | 1202 34 35 62 48 85 58 35 24 | 105 112 109 122 132 135 108 111
R21E | 764 13 13 31 20 11 16 15 8 | 37 36 34 42 41 34 41 36
R22E | 2310 15 20 23 16 12 15 10 7 | 120 119 119 109 119 121 118 118
R23E | 1399 17 23 15 28 26 22 18 9 | 86 88 83 80 81 89 78 81
R24E | 1422 8 16 31 11 15 15 10 7 | 48 48 40 44 46 41 50 44
XR26E | 4250 10 32 --- --- --- --- 12 11 | 84 95 --- --- --- --- 82 83
------+----------------------------------------------+------------------------------------------
RMS | 1411 19 21 29 32 30 25 20 |T 66 70 58 60 70 66 66 63
WRMS | 1411 15 18 29 35 16 20 20 |NE 65 69 55 55 68 66 65 61
MEDI | 903 13 18 21 21 16 16 17 |MD 62 64 50 56 60 60 62 60
Table 3.2102.1 GPS week: 2102 Day: 1 MJD: 58959
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1018 31 31 38 58 24 39 29 16 | 58 60 52 37 55 37 47 39
R02 | 875 8 15 10 12 15 14 14 5 | 27 28 29 23 30 33 22 25
R03 | 569 18 14 17 29 17 9 14 8 | 41 40 35 31 48 43 46 39
XR04 | 837 18 22 20 26 --- 22 14 10 | 49 50 50 38 --- 47 36 42
R05 | 651 12 11 14 31 15 19 18 8 | 34 31 29 42 37 39 35 32
R07 | 807 11 16 11 15 20 14 12 6 | 46 48 36 42 46 42 48 42
R08 | 972 16 17 21 19 22 12 17 8 | 32 34 30 36 30 26 23 26
R09 | 2765 17 21 18 15 18 11 18 7 | 23 24 27 31 35 29 37 28
R11 | 2333 15 7 11 9 10 13 11 5 | 40 35 40 40 41 47 40 39
R12 | 1050 22 20 20 26 15 11 20 8 | 63 60 57 56 59 59 68 59
R13 | 2151 32 29 42 68 35 45 23 18 | 91 97 94 57 91 98 92 86
R14 | 659 14 10 19 16 9 13 10 6 | 50 44 44 44 48 51 50 47
R15 | 725 14 10 25 25 27 18 13 9 | 53 49 43 36 43 49 45 43
R16 | 1642 19 31 38 29 22 51 29 14 | 41 41 30 38 42 63 62 44
R17E | 1731 5 9 23 16 17 12 20 7 | 33 32 32 33 34 31 37 31
R18E | 615 9 13 19 15 14 18 16 6 | 29 27 33 31 34 23 36 29
R19E | 858 30 28 50 31 49 28 30 16 | 27 36 25 51 54 46 46 32
R20E | 1963 30 31 69 46 97 67 45 27 | 72 75 79 92 101 113 74 77
R21E | 765 11 8 31 18 12 12 16 7 | 25 27 32 28 29 25 29 25
R22E | 2902 8 10 33 18 14 21 13 8 | 86 88 76 88 87 95 86 85
R23E | 957 21 19 15 28 24 17 22 9 | 73 74 66 77 70 68 71 70
R24E | 1559 11 16 33 13 11 17 14 7 | 27 28 24 28 29 28 30 25
XR26E | 3849 13 37 --- --- --- --- 14 13 | 65 62 --- --- --- --- 61 62
------+----------------------------------------------+------------------------------------------
RMS | 1495 19 19 30 29 30 27 21 |T 47 47 43 44 49 49 48 44
WRMS | 1495 16 18 30 31 18 17 21 |NE 46 45 42 39 46 47 46 42
MEDI | 972 15 16 20 19 17 17 16 |MD 41 41 35 38 43 43 46 39
Table 3.2102.2 GPS week: 2102 Day: 2 MJD: 58960
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1095 28 28 31 64 49 29 12 16 | 61 65 60 56 61 62 52 52
R02 | 696 13 15 13 14 16 14 18 6 | 31 31 31 32 27 29 26 26
R03 | 799 8 12 11 16 16 36 18 8 | 54 53 48 49 52 82 47 54
XR04 | 741 19 15 16 33 --- 24 10 10 | 60 58 56 34 --- 63 51 52
R05 | 1020 11 15 18 19 16 14 15 7 | 43 47 44 43 42 35 37 38
R07 | 1047 8 11 15 11 13 11 14 5 | 51 53 47 59 59 61 61 55
R08 | 979 9 10 20 12 20 18 10 6 | 44 48 36 52 55 48 44 44
R09 | 1077 10 14 16 17 20 19 24 8 | 23 30 21 22 31 26 32 22
R11 | 2576 12 16 9 7 11 23 10 6 | 46 50 40 45 47 44 40 42
R12 | 1347 19 29 17 33 20 15 14 9 | 68 74 60 54 74 58 53 60
R13 | 3938 38 31 33 62 43 35 25 18 | 93 94 78 77 98 78 92 84
R14 | 1050 11 13 18 21 17 19 13 7 | 66 68 52 57 66 66 68 62
R15 | 989 10 17 19 30 11 14 24 8 | 62 72 55 56 69 54 74 61
R16 | 1276 22 19 38 30 27 41 21 13 | 41 53 38 53 69 71 57 50
R17E | 2170 9 9 20 13 14 14 13 6 | 50 54 53 59 58 54 59 54
R18E | 774 12 12 13 14 8 13 14 5 | 17 22 20 25 24 18 27 20
R19E | 1339 27 33 47 33 48 41 33 17 | 30 39 31 47 62 41 32 30
R20E | 3053 32 29 62 55 72 31 45 22 | 55 58 61 81 88 56 46 55
R21E | 1029 7 8 27 17 12 15 14 7 | 32 36 35 44 38 39 37 35
R22E | 4216 11 12 28 20 14 22 16 8 | 58 62 57 70 56 63 54 57
R23E | 1857 19 23 21 29 27 16 18 9 | 77 79 70 84 77 67 71 73
R24E | 1456 19 27 27 22 13 27 17 9 | 43 48 37 45 37 39 44 38
XR26E | 4117 12 19 --- --- --- --- 14 13 | 30 42 --- --- --- --- 33 30
------+----------------------------------------------+------------------------------------------
RMS | 1891 18 20 27 30 28 24 20 |T 49 53 46 52 56 52 49 47
WRMS | 1891 14 17 27 23 18 20 20 |NE 53 56 47 49 57 55 52 50
MEDI | 1095 12 15 19 20 16 19 15 |MD 50 53 47 52 58 54 47 52
Table 3.2102.3 GPS week: 2102 Day: 3 MJD: 58961
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 684 28 23 29 50 31 29 20 14 | 65 70 72 59 72 71 55 61
R02 | 610 15 18 22 16 11 20 23 8 | 30 34 36 38 29 34 22 27
R03 | 937 10 12 13 15 19 8 15 6 | 49 50 45 38 41 43 50 44
XR04 | 693 7 13 11 30 --- 13 11 7 | 57 56 50 38 --- 63 57 53
R05 | 694 15 11 24 29 29 9 13 9 | 38 38 41 40 40 44 46 38
R07 | 1133 13 12 11 23 12 10 9 6 | 52 52 45 38 45 54 50 47
R08 | 1127 8 11 17 15 12 12 14 6 | 43 45 37 53 48 41 55 44
R09 | 761 10 11 14 9 16 11 14 5 | 23 24 23 29 34 19 29 24
R11 | 2628 9 17 11 13 10 13 11 5 | 47 50 41 43 49 45 52 45
R12 | 1437 21 33 16 30 14 15 14 8 | 62 66 54 41 46 63 49 51
R13 | 2718 30 32 34 63 41 20 24 16 | 91 88 64 33 79 84 96 76
R14 | 1005 15 18 19 9 17 8 16 6 | 56 57 41 45 45 46 43 45
R15 | 856 12 39 19 32 11 11 16 7 | 64 71 50 41 60 60 69 58
R16 | 906 23 39 34 20 36 28 21 12 | 45 57 47 45 61 64 64 52
R17E | 2824 9 12 23 21 16 15 12 7 | 41 44 50 46 42 47 38 42
R18E | 959 12 28 13 19 12 14 11 6 | 27 24 30 32 38 23 34 28
R19E | 2915 28 21 63 50 58 25 48 20 | 33 37 31 72 82 48 41 41
R20E | 3240 29 51 54 55 61 48 45 21 | 47 75 32 83 81 62 48 49
R21E | 771 12 13 23 15 17 15 12 7 | 38 37 33 34 45 29 32 33
R22E | 3137 10 9 23 10 14 14 13 6 | 37 39 33 33 38 38 33 34
R23E | 771 19 23 16 22 31 25 19 10 | 97 99 87 92 96 109 92 95
R24E | 1264 12 13 33 18 8 16 21 8 | 40 44 28 35 37 35 48 35
XR26E | 4390 15 43 --- --- --- --- 19 17 | 19 47 --- --- --- --- 30 21
------+----------------------------------------------+------------------------------------------
RMS | 1756 18 24 28 30 27 20 21 |T 47 52 44 45 52 51 49 45
WRMS | 1756 15 20 28 24 17 16 21 |NE 51 54 46 41 49 52 52 47
MEDI | 1005 13 18 19 20 16 14 15 |MD 45 50 41 40 45 46 48 44
Table 3.2102.4 GPS week: 2102 Day: 4 MJD: 58962
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 996 30 30 35 70 30 27 13 16 | 60 59 58 37 36 52 44 42
R02 | 1313 13 14 16 12 15 14 16 6 | 26 27 25 29 22 21 26 22
R03 | 790 8 9 16 11 29 9 26 8 | 48 44 43 44 44 37 57 44
XR04 | 587 14 15 12 23 --- 16 16 8 | 58 59 51 49 --- 46 58 51
R05 | 571 13 17 14 23 21 12 12 7 | 40 37 40 50 48 41 44 42
R07 | 919 10 11 16 25 11 11 14 6 | 54 50 46 40 52 49 46 47
R08 | 495 11 13 13 8 17 15 20 6 | 38 41 39 34 35 26 51 35
R09 | 1124 15 19 13 11 18 23 14 7 | 20 21 15 18 29 24 19 15
R11 | 1638 10 10 12 10 17 10 16 5 | 47 51 39 47 56 51 37 45
R12 | 1684 23 19 16 29 17 18 15 9 | 65 70 60 54 58 52 64 57
R13 | 4091 22 37 38 67 35 27 37 17 | 90 111 81 77 119 97 117 95
R14 | 886 16 13 16 18 15 14 11 6 | 59 59 50 48 55 49 51 51
R15 | 1113 16 22 17 25 17 10 12 7 | 59 68 51 43 57 49 52 51
R16 | 1055 28 26 51 22 29 49 19 15 | 39 44 48 49 40 57 53 42
R17E | 2019 12 9 28 14 18 15 15 7 | 65 65 71 67 70 73 74 69
R18E | 696 9 12 17 17 12 13 15 6 | 24 27 28 26 23 18 33 22
R19E | 4032 40 32 54 42 68 21 51 21 | 24 30 29 55 94 35 40 30
R20E | 3007 45 35 62 60 66 53 44 24 | 58 77 76 85 76 102 55 67
R21E | 878 12 11 25 10 18 13 13 7 | 23 25 27 27 35 30 31 26
R22E | 3632 14 23 24 17 18 12 15 7 | 66 69 70 77 73 73 66 69
R23E | 914 14 18 23 18 36 35 16 11 | 84 89 78 83 87 83 78 80
R24E | 712 14 11 37 15 14 13 17 8 | 38 35 28 34 39 34 38 33
XR26E | 4256 15 57 --- --- --- --- 13 14 | 39 69 --- --- --- --- 39 36
------+----------------------------------------------+------------------------------------------
RMS | 1910 20 21 30 31 29 23 22 |T 48 53 47 48 54 49 51 46
WRMS | 1910 18 18 30 22 17 18 22 |NE 50 52 46 44 50 46 51 45
MEDI | 1055 14 17 17 18 18 14 15 |MD 48 51 46 47 52 49 51 44
Table 3.2102.5 GPS week: 2102 Day: 5 MJD: 58963
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1159 27 29 32 71 34 22 11 15 | 64 66 62 50 57 62 48 53
R02 | 2171 7 9 14 12 16 16 15 6 | 33 33 32 26 20 39 30 28
R03 | 1123 17 12 18 11 14 14 29 8 | 42 51 44 56 57 58 72 53
XR04 | 711 12 27 16 16 --- 21 16 8 | 55 64 51 53 --- 47 52 50
R05 | 597 13 14 20 18 28 29 28 10 | 36 44 43 48 56 34 47 39
R07 | 922 10 11 15 23 15 8 10 6 | 52 55 54 53 63 55 46 52
R08 | 706 9 12 13 15 20 12 15 6 | 43 41 41 35 43 37 32 38
R09 | 1444 12 23 11 13 18 26 14 7 | 23 31 18 26 28 26 25 20
R11 | 1129 8 15 14 15 19 11 17 6 | 45 49 37 36 55 34 41 41
R12 | 1058 17 34 38 31 19 18 11 10 | 60 76 42 58 73 69 59 58
R13 | 3767 24 28 42 84 40 35 60 21 | 78 86 53 65 82 73 105 73
R14 | 1137 12 23 24 26 22 14 9 8 | 58 60 52 62 71 66 58 59
R15 | 1679 8 12 18 35 21 11 14 8 | 62 63 54 44 68 49 56 55
R16 | 1395 31 23 34 36 39 38 20 14 | 42 34 30 32 35 29 35 30
R17E | 1439 12 9 23 11 18 14 13 7 | 51 54 50 55 58 58 54 53
R18E | 1865 9 9 12 11 16 12 14 5 | 15 15 18 18 19 19 27 15
R19E | 2746 24 22 44 47 46 28 35 16 | 22 27 25 57 52 34 32 23
R20E | 2199 26 35 60 70 92 52 39 25 | 74 87 69 112 118 70 74 75
R21E | 1078 10 12 24 11 16 11 16 6 | 17 21 18 25 27 23 25 19
R22E | 1975 11 13 23 9 11 11 10 6 | 109 108 103 107 111 111 108 108
R23E | 1721 16 17 17 23 26 18 16 8 | 121 124 124 119 121 114 118 118
R24E | 607 12 17 29 10 15 12 19 7 | 32 35 28 35 34 33 36 31
XR26E | 5328 20 50 --- --- --- --- 23 21 | 50 49 --- --- --- --- 44 46
------+----------------------------------------------+------------------------------------------
RMS | 1691 17 20 28 35 31 22 23 |T 51 55 47 53 59 51 53 49
WRMS | 1691 16 18 28 27 18 17 23 |NE 49 53 43 46 54 48 50 46
MEDI | 1395 12 17 20 16 19 14 16 |MD 50 51 43 50 57 47 47 50
Table 3.2102.6 GPS week: 2102 Day: 6 MJD: 58964
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 540 27 33 41 64 29 19 15 15 | 77 81 78 52 72 68 64 65
R02 | 1032 10 12 14 27 15 16 9 7 | 39 40 33 29 32 39 29 31
R03 | 1792 7 15 17 13 13 16 23 6 | 59 57 57 58 52 65 66 58
XR04 | 568 13 15 18 27 --- 17 16 9 | 67 65 67 55 --- 55 60 60
R05 | 678 17 17 21 22 34 18 21 10 | 45 51 55 62 68 44 53 51
R07 | 1035 8 9 13 13 16 22 15 6 | 70 73 71 65 77 64 64 68
R08 | 743 9 11 14 12 18 18 17 6 | 54 58 54 48 57 42 43 48
R09 | 1316 17 18 20 15 26 15 17 8 | 27 30 24 34 43 27 34 26
R11 | 1087 9 8 16 12 10 12 13 5 | 57 60 48 50 61 49 53 53
R12 | 750 21 22 42 26 21 12 9 10 | 82 85 63 64 87 76 76 74
R13 |45052 18 39 59 87 25 52 47 21 | 117 125 79 65 124 140 147 113
R14 | 1596 18 18 26 20 20 11 13 8 | 78 78 57 70 83 75 76 73
R15 | 1756 11 12 18 31 10 20 25 8 | 80 79 70 60 75 72 84 73
R16 | 905 21 21 31 35 36 44 22 14 | 51 65 39 61 68 67 64 56
R17E | 1938 8 7 18 9 14 17 16 6 | 52 53 53 51 59 44 57 51
R18E | 1303 7 10 14 15 14 21 16 6 | 37 38 39 37 33 31 47 36
R19E | 1370 23 27 66 55 44 30 45 19 | 42 49 47 75 60 51 47 43
R20E | 1500 40 41 44 59 76 34 60 23 | 113 117 109 134 145 125 117 116
R21E | 849 8 9 23 13 9 17 12 6 | 34 34 35 39 40 41 39 36
R22E | 2349 9 11 23 16 21 21 13 7 | 109 109 110 108 110 108 108 108
R23E | 1200 18 21 18 25 29 31 17 10 | 118 118 120 130 116 129 117 119
R24E | 542 11 20 28 9 16 18 13 7 | 43 47 38 39 46 39 47 41
XR26E | 5365 15 51 --- --- --- --- 20 17 | 74 87 --- --- --- --- 78 75
------+----------------------------------------------+------------------------------------------
RMS | 9913 17 20 31 34 28 24 24 |T 66 69 61 63 71 65 68 64
WRMS | 9913 14 17 31 26 16 19 24 |NE 64 67 56 55 69 63 65 60
MEDI | 1200 13 17 20 20 20 18 16 |MD 59 65 55 58 68 55 64 58
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