[IGSREPORT-23387] Wk 1830 IGLOS Final Orbits [Resubmission]
IGS ACC
igs.acc at noaa.gov
Fri Feb 20 16:00:12 PST 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1830 (Feb 01, 2015 - Feb 07, 2015)
Contact: igs.acc at noaa.gov
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 2.1830.
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:
igl1830[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1830 in the SP3 format.
igl18307.sum Combination Report for GPS Week 1830.
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
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 | 6.7 ns
1 | 7.0 ns
2 | 9.1 ns
3 | 9.4 ns
4 | 4.7 ns
5 | 9.1 ns
6 | 5.7 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | COD | R21
1 | ESX | R23
1 | GRG | R09
2 | ALL | R23
3 | ALL | R23
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 1.1830, 1a.1830).
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 2.1830.0-6)
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 3.1830.0-6).
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 1830 summary. (Feb 01, 2015 - Feb 07, 2015)
Table 1.1830.a GPS week : 1830 MJD: 57054.0-57060.0
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| -1 0 -2 26 47 19 .39 51 35 | --- --- --- ---
| 2 1 1 34 14 42 .04 | --- ---
cof n/a| -2 0 -2 20 27 30 .26 56 38 | --- --- --- ---
| 2 1 2 26 18 43 .06 | --- ---
emx n/a| 0 0 -4 -49 -49 -24 .29 26 27 | 2667 207 3912 7068
| 1 1 1 28 42 25 .07 | 5368 1597
esx n/a| 0 0 5 12 -25 -31 -.12 21 18 | 5683 -231 3955 7037
| 1 1 0 17 21 26 .05 | 3302 3881
gfz n/a| 0 0 -7 44 58 11 .02 23 17 | 0 345 3900 6915
| 1 0 2 25 19 24 .06 | 0 3538
grg n/a| 0 0 -1 -38 -23 25 -.38 38 31 | -933763 48 4093 89661
| 2 1 3 20 45 66 .05 | 48225 3281
iac n/a| 2 1 10 4 47 41 -.08 27 27 | 8503 -434 3905 6974
| 1 1 1 40 36 56 .06 | 1369 2310
mcc n/a| 3 0 22 76 54 107 -.27 133 133 | --- --- --- ---
| 5 3 8 66 140 180 .18 | --- ---
Table 1.1830.b GPS week : 1830 MJD: 57054.0-57060.0
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 | 13 10 11 11 15 13 10 |
R02 | 9 8 7 7 7 10 12 |
R03 | 10 8 8 7 10 12 9 |
R04 | 7 9 8 8 8 9 9 |
R05 | 10 10 10 8 13 11 14 |
R06 | 7 10 9 9 9 8 9 |
R07 | 7 9 10 10 9 11 10 |
R08 | 7 9 12 11 10 9 10 |
R09 | 15 18 18 16 16 15 15 |
R10 | 11 11 11 11 11 11 10 |
R11 | 19 22 20 21 23 24 20 |
R12 | 19 23 19 21 23 20 22 |
R13 | 10 10 10 11 11 13 11 |
R14 | 17 17 17 24 22 18 17 |
R15 | 13 12 12 11 12 13 13 |
R16 | 12 12 12 10 10 11 14 |
R17 | 10 12 10 10 10 11 11 |
R18 | 11 11 10 10 9 8 9 |
R19 | 12 11 12 10 13 10 10 |
R20 | 18 16 16 14 14 13 16 |
R21 | 303 11 14 11 13 11 13 |
R22 | 10 10 10 12 13 11 12 |
R23 | 9 15 --- --- 10 12 10 |
R24 | 9 11 9 10 12 12 11 |
Table 1.1830.c GPS week : 1830 MJD: 57054.0-57060.0
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 1830 0 | 30 9 57 -463 -2457 -3932 83.8 1570 1570 | 6745 0
brd 1830 1 | -23 35 24 -7 527 -5860 84.8 1882 1882 | 6985 0
brd 1830 2 | 2 6 66 1032 788 -7465 87.1 3455 3455 | 9111 0
brd 1830 3 | -148 -689 -129 58 -1255 -13370 85.2 >>>>> >>>>> | 9371 0
brd 1830 4 | 3 13 44 169 395 -1989 84.9 3305 3305 | 4670 0
brd 1830 5 | -18 -74 75 -64 388 654 86.5 3247 3247 | 9088 0
brd 1830 6 | -13 0 151 -177 -916 1199 86.0 3615 3615 | 5724 0
-------------+------------------------------------------------------------+----------------
brd 1830 mean| -23 -99 41 78 -361 -4394 85.5 30796 30796 | 7384 0
brd 1830 sdev| 57 262 85 466 1207 5081 1.1 73954 73954 | 1849 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 2.1830.0 GPS week: 1830 Day: 0 MJD: 57054
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 44 42 -58 .42 53 39 | --- --- --- ---
cof n/a| -1 0 -2 21 55 -53 .26 57 42 | --- --- --- ---
emx n/a| -1 0 -6 -54 32 -61 .26 27 27 | 739 481 3745 6497
esx n/a| 1 0 5 7 -47 -7 -.11 18 18 | 3221 -112 3748 7282
gfz n/a| 0 -1 -5 4 80 32 .11 21 16 | 0 -387 3728 6181
grg n/a| 0 0 -6 -1 -45 -41 -.39 33 33 | -999999 33 3753 79762
iac n/a| 0 0 10 42 -19 104 -.15 26 26 | 7808 -604 3736 6006
mcc n/a| 2 0 33 192 -94 5 -.29 167 167 | --- --- --- ---
Table 2.1830.1 GPS week: 1830 Day: 1 MJD: 57055
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 -4 56 56 61 .35 52 33 | --- --- --- ---
cof n/a| 0 0 -1 26 20 69 .33 56 34 | --- --- --- ---
emx n/a| -1 0 -4 -12 -48 -39 .36 26 26 | 4877 558 3716 7449
esx n/a| -3 0 6 8 -41 -34 -.12 23 18 | 2731 676 3963 7982
gfz n/a| 1 -1 -4 29 27 -15 .04 21 17 | 0 1367 3689 7219
grg n/a| -3 1 -3 -63 -6 -90 -.39 58 35 | -911034 -89 4311 180447
iac n/a| 2 1 10 12 92 118 -.15 27 27 | 8169 12 3683 7081
mcc n/a| -3 -4 16 99 25 131 -.05 158 158 | --- --- --- ---
Table 2.1830.2 GPS week: 1830 Day: 2 MJD: 57056
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 18 58 8 .41 52 39 | --- --- --- ---
cof n/a| 0 0 -4 35 28 27 .15 57 44 | --- --- --- ---
emx n/a| 1 -1 -5 -20 -81 -22 .39 30 32 | -1804 1796 3703 7513
esx n/a| -1 0 5 7 0 -17 -.13 19 18 | 9926 239 3724 3797
gfz n/a| 0 -1 -10 40 58 -27 -.05 23 17 | 0 2340 3702 7396
grg n/a| 0 -1 0 -24 -62 62 -.28 34 29 | -916798 2018 3731 39132
iac n/a| 2 3 10 -14 44 40 -.02 24 24 | 9343 925 3712 7623
mcc n/a| 1 3 29 -19 -59 -82 -.23 119 119 | --- --- --- ---
Table 2.1830.3 GPS week: 1830 Day: 3 MJD: 57057
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 -1 74 21 5 .36 50 31 | --- --- --- ---
cof n/a| 0 3 0 20 2 32 .26 56 34 | --- --- --- ---
emx n/a| 1 0 -5 -53 -46 14 .19 27 26 | 12734 979 3436 6020
esx n/a| 0 -1 4 -1 -6 -24 -.03 20 17 | 6036 2572 3443 5956
gfz n/a| -1 -1 -9 77 58 38 .04 23 17 | 0 3122 3419 6127
grg n/a| 0 0 -1 -55 -78 38 -.40 33 27 | -901992 3274 3408 35483
iac n/a| 1 2 10 -30 48 -27 -.05 29 29 | 11013 677 3423 6722
mcc n/a| 9 4 24 91 226 -69 -.52 129 129 | --- --- --- ---
Table 2.1830.4 GPS week: 1830 Day: 4 MJD: 57058
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| -3 0 -2 19 64 66 .43 52 32 | --- --- --- ---
cof n/a| -4 2 -3 15 21 77 .27 52 34 | --- --- --- ---
emx n/a| 0 -2 -3 -96 -40 -5 .30 28 29 | -3863 -3086 4935 8942
esx n/a| 0 0 7 -5 -51 -35 -.17 22 19 | 2072 -7417 4927 9667
gfz n/a| -3 1 -7 33 43 6 .02 24 18 | 0 -6337 4892 8682
grg n/a| 3 0 -4 -46 -2 49 -.39 36 28 | -930696 -6063 4956 166737
iac n/a| 3 0 9 73 57 36 -.03 27 27 | 7324 -5181 4919 8512
mcc n/a| 9 0 27 90 262 151 -.14 95 95 | --- --- --- ---
Table 2.1830.5 GPS week: 1830 Day: 5 MJD: 57059
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| -5 -1 -4 -24 44 16 .35 51 34 | --- --- --- ---
cof n/a| -5 0 -6 56 48 13 .25 57 38 | --- --- --- ---
emx n/a| 0 -2 -3 -67 -58 -40 .28 24 25 | 3272 1103 4014 7357
esx n/a| 0 0 5 37 -27 -10 -.17 22 19 | 10099 4793 4028 8279
gfz n/a| 0 -1 -9 66 59 29 .04 23 19 | 0 3976 4013 7258
grg n/a| -1 2 1 -32 58 85 -.43 40 34 | -999999 3073 4661 77597
iac n/a| 2 1 7 -13 31 -24 -.11 24 24 | 8832 2011 4027 7214
mcc n/a| 7 0 8 28 -42 178 -.12 112 112 | --- --- --- ---
Table 2.1830.6 GPS week: 1830 Day: 6 MJD: 57060
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| -3 -2 -2 -3 42 36 .36 51 36 | --- --- --- ---
cof n/a| -3 -1 -2 -30 18 47 .34 55 37 | --- --- --- ---
emx n/a| -1 0 -4 -40 -103 -15 .26 23 23 | 2718 -376 3841 5702
esx n/a| 1 -2 4 36 -6 -87 -.11 21 19 | 5698 -2372 3855 6298
gfz n/a| -2 -1 -7 61 81 16 -.08 23 19 | 0 -1660 3861 5546
grg n/a| 3 0 1 -41 -24 77 -.38 34 33 | -875826 -1906 3836 48470
iac n/a| 4 0 13 -34 77 45 -.04 32 32 | 7036 -881 3841 5664
mcc n/a| 0 -4 18 54 60 440 -.50 151 151 | --- --- --- ---
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 3.1830.0 GPS week: 1830 Day: 0 MJD: 57054
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 808 42 38 32 21 18 45 23 --- 12 | 80 80 72 55 73 46 59 --- 60
R02 | 725 13 11 15 13 15 29 26 133 8 | 54 55 57 51 60 46 38 70 50
R03 | 1081 28 34 16 20 18 15 36 --- 10 | 48 48 59 74 71 63 45 --- 61
R04 | 709 13 11 9 10 14 24 16 --- 6 | 69 69 74 60 68 53 56 --- 63
R05 | 1846 44 43 22 16 17 23 20 --- 9 | 49 59 60 58 65 49 35 --- 52
R06 | 1753 21 19 15 9 9 18 22 --- 6 | 48 55 62 62 66 71 54 --- 59
R07 | 1214 17 26 12 7 12 23 27 173 7 | 77 85 80 71 81 81 49 77 71
R08 | 952 14 19 14 12 10 28 14 --- 7 | 71 78 76 66 77 53 67 --- 68
R09E | 987 75 69 38 17 19 39 32 --- 14 | 60 61 41 35 33 58 49 --- 33
R10E | 1208 51 56 15 17 17 26 29 --- 10 | 47 57 28 30 33 24 20 --- 23
R11E | 1914 107 115 34 18 36 56 36 --- 18 | 116 125 43 55 77 84 46 --- 54
R12E | 2110 91 101 42 17 32 66 29 271 18 | 121 122 118 122 110 134 121 79 114
R13E | 1386 45 55 25 13 13 25 27 --- 10 | 53 63 28 24 26 38 27 --- 23
R14E | 2473 66 55 47 29 30 38 33 --- 17 | 45 67 55 60 55 57 48 --- 48
R15E | 1912 53 58 30 17 26 28 39 --- 13 | 93 93 82 77 94 93 77 --- 81
R16E | 3798 69 52 21 17 13 37 23 --- 11 | 101 101 86 80 87 94 85 --- 84
R17 | 680 52 48 23 13 23 23 18 75 10 | 79 81 47 51 38 30 37 44 41
R18 | 1295 42 45 28 20 20 28 24 111 11 | 75 76 46 54 31 35 34 47 41
R19 | 1231 45 46 28 18 25 29 21 --- 11 | 67 68 65 57 49 51 51 --- 50
R20 | 1536 75 87 42 34 31 38 38 --- 17 | 77 87 52 60 39 27 32 --- 38
XR21 | 7917 691 689 --- --- 158 --- 423 --- 303 | 77 97 --- --- 753 --- 1 --- 755
R22 | 685 56 60 20 15 18 29 11 --- 10 | 90 95 44 50 33 25 39 --- 40
R23 | 959 37 46 19 16 20 19 10 --- 8 | 77 84 47 426 54 47 60 --- 43
R24 | 942 42 73 14 20 18 18 20 --- 9 | 67 89 40 52 30 34 38 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1570 53 57 27 18 21 33 26 167 |T 72 78 59 75 87 56 48 63 82
WRMS | 1570 39 42 27 18 16 33 26 167 |NE 69 75 58 83 99 47 43 59 95
MEDI | 1214 45 48 22 17 18 28 24 133 |MD 71 78 57 58 60 51 46 70 50
Table 3.1830.1 GPS week: 1830 Day: 1 MJD: 57055
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 1063 25 30 15 20 19 35 23 --- 10 | 52 59 48 69 70 44 45 --- 55
R02 | 1273 15 25 19 13 16 25 18 214 8 | 40 47 41 34 42 30 27 128 34
R03 | 749 14 13 17 16 14 26 23 --- 8 | 34 34 37 33 27 35 22 --- 29
R04 | 661 14 21 31 15 10 22 13 --- 8 | 42 45 54 25 26 31 29 --- 31
R05 | 2104 25 21 18 17 13 24 35 --- 10 | 26 32 36 39 38 50 21 --- 31
R06 | 1960 13 13 12 24 15 23 32 --- 9 | 31 34 36 44 40 26 25 --- 32
R07 | 924 16 17 22 19 11 21 27 219 9 | 51 49 51 59 43 47 38 142 46
R08 | 1092 12 9 17 15 15 16 29 --- 8 | 46 40 51 45 52 58 38 --- 45
R09E | 827 80 101 31 26 20 223 39 --- 18 | 70 93 43 41 50 177 51 --- 38
R10E | 938 56 52 19 21 14 21 16 --- 10 | 49 45 25 25 23 22 22 --- 17
R11E | 1684 109 118 50 20 36 60 35 --- 21 | 117 126 59 64 74 77 62 --- 59
R12E | 1493 89 88 41 52 32 72 40 161 23 | 118 123 68 85 87 96 45 101 71
R13E | 1316 47 49 19 12 16 32 18 --- 10 | 56 56 25 26 32 40 26 --- 24
R14E | 3709 49 54 29 37 31 50 41 --- 17 | 48 66 39 43 57 64 46 --- 38
R15E | 1784 48 48 34 16 24 29 20 --- 12 | 68 73 57 52 56 39 42 --- 47
R16E | 4938 52 66 30 26 16 21 17 --- 11 | 88 100 81 86 88 91 83 --- 83
R17 | 642 62 68 25 18 22 23 18 28 12 | 58 66 32 33 23 18 23 43 23
R18 | 1917 48 44 24 18 19 28 24 69 11 | 51 50 27 32 28 23 25 56 24
R19 | 1614 45 59 19 13 21 35 28 --- 11 | 78 82 81 79 79 81 51 --- 72
R20 | 1812 61 54 34 25 29 40 31 --- 15 | 63 62 34 49 44 36 30 --- 33
XR21 |18711 41 41 --- 12 20 26 20 --- 11 | 54 55 --- 41 90 27 42 --- 92
R22 | 726 60 57 13 15 19 23 15 --- 10 | 67 64 32 35 24 29 29 --- 29
XR23 | 1098 38 43 28 818 19 --- 23 --- 15 | 74 85 48 697 53 --- 57 --- 40
R24 | 1903 51 47 19 21 24 28 16 --- 11 | 57 51 31 39 29 22 23 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1881 52 56 26 23 21 58 27 158 |T 59 64 45 73 48 50 37 94 42
WRMS | 1881 33 34 26 18 17 35 27 158 |NE 51 53 42 84 44 37 32 92 40
MEDI | 1316 47 47 22 18 19 26 23 161 |MD 54 56 41 41 43 39 30 101 34
Table 3.1830.2 GPS week: 1830 Day: 2 MJD: 57056
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 744 25 33 25 26 17 22 32 --- 11 | 62 72 59 72 66 51 38 --- 56
R02 | 1060 16 19 10 11 14 15 23 121 6 | 47 54 50 52 57 51 35 106 47
R03 | 1563 31 27 21 15 15 22 12 --- 8 | 43 54 51 46 52 34 43 --- 44
R04 | 1179 11 16 20 8 14 21 26 --- 8 | 49 51 62 53 52 63 30 --- 49
R05 | 1507 20 17 20 19 22 32 24 --- 10 | 39 43 45 53 55 33 35 --- 41
R06 | 2172 18 15 21 12 15 20 28 --- 8 | 41 41 48 39 49 31 27 --- 36
R07 | 2354 12 18 25 12 21 31 23 164 9 | 54 63 67 51 71 34 43 153 52
XR08 | 1309 20 22 30 17 8 --- 35 --- 12 | 51 51 67 54 49 --- 27 --- 48
R09E | 634 81 84 40 33 26 57 27 --- 18 | 64 66 25 48 37 62 34 --- 27
R10E | 858 61 64 31 17 12 17 13 --- 10 | 53 58 27 25 16 14 23 --- 15
R11E | 895 101 111 48 18 33 58 33 --- 20 | 112 124 37 64 80 78 60 --- 58
R12E | 2658 91 101 47 18 34 57 32 83 19 | 114 121 90 70 100 103 94 89 84
R13E | 1674 50 55 27 13 18 22 17 --- 10 | 60 65 29 28 32 36 29 --- 26
R14E | 2640 45 55 28 34 38 51 35 --- 16 | 62 77 63 60 56 77 50 --- 50
R15E | 1557 58 58 25 16 32 27 12 --- 11 | 68 68 34 33 46 39 41 --- 33
R16E | 4422 50 39 35 21 16 27 22 --- 12 | 67 59 62 51 56 59 47 --- 50
R17 | 962 61 68 16 11 19 27 12 49 10 | 73 80 38 40 26 28 33 40 33
R18 | 1418 46 61 20 17 22 20 18 140 10 | 69 82 40 48 29 35 31 49 37
R19 | 1635 46 48 33 14 20 33 28 --- 12 | 66 65 66 56 54 38 37 --- 48
R20 | 840 51 61 42 25 33 40 33 --- 15 | 59 69 40 47 40 32 33 --- 31
R21 |13961 50 56 47 26 26 31 19 --- 14 | 51 56 56 28 44 27 34 --- 50
R22 | 1099 50 60 15 17 19 27 18 --- 10 | 74 84 41 54 32 31 41 --- 41
R24 | 1151 36 54 18 15 25 25 12 --- 9 | 52 67 40 40 24 27 37 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 3454 52 57 30 19 23 34 24 119 |T 61 67 49 67 48 44 39 87 42
WRMS | 3454 39 44 32 18 17 29 24 119 |NE 55 61 51 76 46 36 36 87 42
MEDI | 1418 46 55 25 17 20 27 23 121 |MD 59 65 48 51 49 35 35 89 44
Table 3.1830.3 GPS week: 1830 Day: 3 MJD: 57057
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 884 28 25 24 10 19 42 25 --- 11 | 65 63 71 63 77 35 44 --- 59
R02 |>>>>> 10 13 11 9 13 18 26 104 6 | 47 47 51 54 58 65 41 64 51
R03 | ---- 25 28 14 11 9 29 14 --- 7 | 48 45 52 54 57 36 58 --- 50
R04 |>>>>> 14 17 16 12 18 23 21 --- 7 | 56 57 58 43 47 45 58 --- 47
R05 | 1481 16 15 19 19 10 21 17 --- 7 | 44 50 56 53 50 37 35 --- 45
R06 |>>>>> 14 16 31 12 11 16 27 --- 9 | 41 43 60 38 41 38 31 --- 38
R07 | ---- 10 17 18 16 13 13 41 115 9 | 69 67 76 72 76 68 36 82 66
R08 |>>>>> 18 24 26 20 11 26 36 --- 10 | 60 65 66 58 59 42 24 --- 50
R09E | 959 70 66 41 27 27 37 22 --- 16 | 62 64 38 43 46 55 55 --- 35
R10E |>>>>> 53 60 31 19 15 21 18 --- 11 | 48 51 27 25 21 21 25 --- 16
R11E | ---- 105 111 40 28 34 64 34 --- 21 | 111 114 47 63 79 91 50 --- 54
R12E | ---- 93 111 55 16 29 59 44 194 20 | 124 135 94 107 115 120 95 54 101
R13E |>>>>> 52 68 22 14 23 19 20 --- 10 | 64 77 32 39 44 43 30 --- 34
R14E | ---- 60 75 29 47 56 73 59 --- 23 | 59 113 48 102 123 51 48 --- 69
R15E | ---- 59 73 17 21 18 28 19 --- 11 | 78 90 47 50 57 42 36 --- 44
R16E | ---- 46 52 23 14 14 25 23 --- 10 | 83 83 75 73 86 88 81 --- 77
R17 | ---- 48 55 18 20 15 24 15 42 10 | 81 87 50 52 41 32 45 32 45
R18 | ---- 44 42 13 13 27 14 25 142 9 | 75 77 52 52 29 47 51 41 46
R19 | 1988 47 59 23 12 21 19 21 --- 10 | 81 92 65 64 51 56 45 --- 57
R20 | ---- 47 53 33 18 25 35 36 --- 13 | 79 82 60 53 41 34 36 --- 44
R21 | ---- 49 52 24 15 17 27 30 --- 11 | 65 67 30 38 30 23 27 --- 38
R22 | ---- 56 60 18 20 19 29 26 --- 11 | 82 84 43 45 27 22 36 --- 36
R24 | ---- 36 24 21 20 21 18 19 --- 9 | 72 61 51 56 37 45 49 --- 47
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 50 56 27 20 23 33 29 129 |T 69 74 54 81 57 49 45 54 49
WRMS |>>>>> 31 34 26 17 17 27 29 129 |NE 64 66 56 90 49 41 42 54 47
MEDI |>>>>> 47 52 23 16 18 25 25 115 |MD 65 67 52 53 50 43 44 54 47
Table 3.1830.4 GPS week: 1830 Day: 4 MJD: 57058
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 962 40 30 44 24 32 43 16 --- 15 | 62 65 67 60 65 32 40 --- 50
R02 | 1132 11 16 17 11 12 15 23 96 7 | 38 34 48 40 45 55 29 27 40
R03 | 571 23 25 13 23 14 11 37 --- 10 | 40 49 42 54 49 47 37 --- 43
R04 | 1739 13 21 10 14 15 31 16 --- 7 | 49 53 48 49 47 54 52 --- 47
R05 | 1033 22 27 22 30 24 30 33 --- 12 | 46 69 54 75 67 44 28 --- 52
R06 | 1180 17 22 20 19 16 27 22 --- 9 | 36 38 49 54 49 33 44 --- 43
R07 | 923 18 17 31 13 11 19 22 91 9 | 57 57 64 46 56 58 41 44 51
R08 | 1171 20 18 26 15 17 21 29 --- 10 | 60 61 65 56 62 50 33 --- 53
R09E | 641 65 63 40 26 17 33 40 --- 16 | 60 58 41 59 47 53 49 --- 42
R10E | 1398 50 56 20 20 16 28 19 --- 10 | 44 53 33 38 25 31 23 --- 24
R11E | 1321 99 98 46 35 33 79 34 --- 23 | 106 105 41 64 69 87 45 --- 50
R12E | 2833 98 88 54 25 34 63 46 125 22 | 103 95 66 61 78 112 51 28 62
R13E |10892 52 56 18 16 17 32 17 --- 10 | 53 61 28 22 35 33 23 --- 22
R14E | 2077 87 78 26 38 56 64 44 --- 22 | 80 98 55 82 111 62 64 --- 66
R15E | 4902 62 67 17 15 20 30 22 --- 11 | 66 69 26 30 33 46 33 --- 28
R16E | 5464 43 53 17 18 14 28 17 --- 9 | 54 69 48 45 48 49 48 --- 43
R17 | 873 47 45 21 18 22 17 20 38 10 | 71 71 52 49 35 38 38 27 42
R18 | 1647 39 47 16 17 17 28 13 103 9 | 68 74 49 49 36 27 46 29 42
R19 | 2209 53 51 29 14 23 26 36 --- 13 | 107 107 92 90 77 73 61 --- 79
R20 | 870 56 54 29 23 33 24 24 --- 13 | 78 76 51 53 34 43 35 --- 41
R21 | 7019 54 55 24 17 27 33 21 --- 12 | 68 69 44 44 37 28 35 --- 42
R22 | 1653 64 58 19 17 21 36 20 --- 12 | 75 70 35 39 28 22 29 --- 29
R23 | 714 20 24 25 26 11 34 12 --- 10 | 41 39 68 424 48 47 61 --- 66
R24 | 1134 31 51 31 29 22 25 17 --- 11 | 64 83 50 62 39 39 42 --- 45
------+---------------------------------------------------+-----------------------------------------------
RMS | 3305 52 52 28 22 24 36 27 95 |T 63 67 50 68 50 48 41 31 45
WRMS | 3305 32 34 29 19 18 28 27 95 |NE 60 63 54 77 48 43 40 31 47
MEDI | 1180 43 51 22 18 17 28 22 96 |MD 60 69 49 53 47 46 40 28 43
Table 3.1830.5 GPS week: 1830 Day: 5 MJD: 57059
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 663 47 52 28 19 26 29 30 --- 12 | 57 71 51 42 59 36 38 --- 42
R02 | 1840 11 13 25 12 18 37 24 124 10 | 25 28 33 25 30 18 27 35 22
R03 | 613 29 29 24 24 20 34 33 --- 12 | 27 26 42 56 52 58 46 --- 44
R04 | 1247 14 14 25 23 13 21 16 --- 9 | 46 47 49 36 46 36 30 --- 38
R05 | 990 35 33 26 20 27 29 21 --- 11 | 52 61 36 50 55 30 33 --- 39
R06 | 1429 19 15 15 11 15 24 20 --- 7 | 37 38 42 39 54 47 35 --- 40
R07 | 998 16 20 25 13 15 30 33 145 10 | 44 52 61 50 61 35 32 44 48
R08 | 839 19 23 19 14 13 40 20 --- 9 | 45 52 42 44 49 26 40 --- 39
R09E | 801 66 68 18 25 18 57 29 --- 14 | 75 81 48 37 43 83 43 --- 38
R10E | 2608 46 47 26 17 16 25 21 --- 10 | 46 47 21 26 22 27 25 --- 19
R11E | 852 103 112 40 43 42 85 34 --- 23 | 118 132 38 73 84 81 56 --- 54
R12E | 2419 84 94 40 37 31 73 26 144 20 | 88 105 28 74 73 74 54 45 48
R13E | 743 60 48 20 16 24 46 18 --- 12 | 61 53 22 25 26 43 23 --- 20
R14E | 1123 62 76 18 34 39 61 38 --- 17 | 63 83 36 57 70 61 52 --- 42
R15E | 2815 71 77 20 14 24 25 26 --- 12 | 82 88 46 49 55 51 42 --- 46
R16E | 6951 49 56 18 21 14 31 21 --- 10 | 95 102 86 89 86 76 84 --- 83
R17 | 629 44 52 25 19 21 29 25 31 11 | 63 73 50 49 40 32 35 26 41
R18 | 1392 38 41 7 16 19 13 12 68 7 | 54 55 37 40 29 31 33 34 34
R19 | 1787 44 57 20 13 27 24 15 --- 10 | 75 85 60 56 44 44 60 --- 53
R20 | 5342 57 75 27 18 32 38 16 --- 13 | 64 80 44 43 34 32 33 --- 34
R21 |11476 56 67 18 13 25 23 19 --- 10 | 57 65 30 35 32 26 23 --- 41
R22 | 921 62 73 19 13 22 30 18 --- 11 | 69 77 34 34 20 16 26 --- 26
R23 | 656 25 26 27 35 13 27 19 --- 11 | 49 53 56 165 58 47 61 --- 55
R24 | 1826 41 42 28 19 18 42 27 --- 12 | 63 65 54 56 37 41 30 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 3246 51 57 24 22 23 40 24 112 |T 60 67 43 52 48 43 40 36 41
WRMS | 3246 34 38 25 19 19 34 24 112 |NE 51 58 45 51 43 34 36 34 39
MEDI | 1123 44 48 24 18 20 30 21 124 |MD 57 65 42 44 46 36 35 35 41
Table 3.1830.6 GPS week: 1830 Day: 6 MJD: 57060
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 1026 36 51 21 17 17 18 30 --- 10 | 89 103 79 61 79 52 45 --- 65
R02 | 2200 15 24 32 11 16 40 36 176 12 | 50 54 62 49 60 42 35 52 48
R03 | 638 32 29 13 19 12 8 34 --- 9 | 45 50 65 65 63 61 41 --- 58
R04 | 1488 13 16 17 17 14 26 30 --- 9 | 64 66 79 71 71 57 50 --- 65
R05 | 1450 34 32 18 21 28 22 61 --- 14 | 53 56 59 64 69 50 23 --- 51
R06 | 1086 23 23 14 21 14 16 30 --- 8 | 52 52 58 65 65 46 43 --- 55
R07 | 1160 14 13 29 15 12 33 27 175 10 | 76 73 88 73 77 58 51 67 71
R08 | 1042 13 18 9 21 20 25 36 --- 9 | 76 81 81 76 89 57 46 --- 71
R09E | 1729 76 94 18 24 20 31 39 --- 14 | 67 87 41 44 33 60 48 --- 36
R10E | 2523 45 53 15 17 15 25 20 --- 9 | 49 54 25 29 20 32 31 --- 23
R11E | 892 98 109 31 30 36 63 34 --- 20 | 105 112 51 73 77 80 47 --- 58
R12E | 2514 85 78 36 35 45 70 40 222 21 | 90 89 44 72 88 87 45 45 57
R13E | 2555 52 71 18 15 15 23 30 --- 10 | 54 71 35 38 38 38 26 --- 31
R14E | 816 64 69 38 33 25 35 45 --- 17 | 51 65 47 54 52 39 42 --- 39
R15E | 937 62 69 25 22 26 28 22 --- 13 | 68 77 51 44 52 43 40 --- 42
R16E | 5650 64 77 24 22 31 34 31 --- 14 | 90 105 89 68 74 94 77 --- 76
R17 | 802 45 46 16 18 19 38 24 37 11 | 75 79 52 54 32 33 41 33 41
R18 | 1037 40 31 18 14 20 23 13 49 9 | 72 67 51 50 31 28 39 40 41
R19 | 547 41 46 19 11 17 26 24 --- 9 | 107 109 94 79 66 64 74 --- 78
R20 | 693 60 57 39 22 33 48 26 --- 16 | 83 87 57 47 27 28 41 --- 38
R21 |15449 61 58 19 21 22 28 33 --- 12 | 84 82 37 46 36 28 37 --- 47
R22 | 552 58 55 23 19 26 21 21 --- 11 | 89 89 52 53 34 29 39 --- 43
R23 | 616 29 31 23 26 14 22 15 --- 9 | 67 67 59 185 72 54 75 --- 66
R24 | 994 40 39 16 22 21 32 16 --- 10 | 73 75 49 58 28 34 34 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 3614 51 55 23 21 23 34 32 151 |T 72 77 58 63 55 49 44 47 51
WRMS | 3614 36 37 23 19 19 33 32 151 |NE 72 74 63 68 56 45 44 48 54
MEDI | 1037 41 46 19 21 20 26 30 175 |MD 72 75 52 58 60 46 41 45 48
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