[IGSREPORT-26077] Wk 2012 IGLOS Final Orbits
acc
acc at igs.org
Mon Aug 20 04:36:17 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2012 (Jul 29, 2018 - Aug 04, 2018)
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 2.2012.
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:
igl2012[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2012 in the SP3 format.
igl20127.sum Combination Report for GPS Week 2012.
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 | 6.8 ns
1 | 7.0 ns
2 | 6.2 ns
3 | 4.7 ns
4 | 4.0 ns
5 | 6.3 ns
6 | 5.6 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 1.2012, 1a.2012).
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 2.2012.0-6)
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 3.2012.0-6).
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 2012 summary. (Jul 29, 2018 - Aug 04, 2018)
Table 1.2012.a GPS week : 2012 MJD: 58328.0-58334.0
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 11 11 0 -16 -.01 40 36 | 5116 -967 3685 10071
| 0 1 2 19 23 15 .03 | 712 1413
cof n/a| -1 0 15 16 13 0 .06 42 38 | 5122 -989 3686 10073
| 0 1 3 13 26 28 .05 | 715 1410
emx n/a| -1 0 0 24 -13 26 .06 23 23 | 782 -929 3691 9596
| 1 1 2 16 7 70 .03 | 10001 921
esx n/a| 0 0 0 -9 4 -8 .10 15 12 | -70 -259 3696 11598
| 0 0 1 18 5 21 .02 | 17112 1342
gfz n/a| 0 0 -9 -11 31 20 .08 29 25 | 0 -750 3683 9739
| 0 0 2 20 30 33 .03 | 0 1395
grg n/a| 0 0 9 -32 -16 -113 -.36 51 44 | 6001 -594 3690 9555
| 1 2 5 24 17 82 .08 | 943 1173
iac n/a| 1 0 -3 13 -2 14 -.16 25 24 | 7437 -936 3694 9492
| 1 0 2 41 29 75 .05 | 838 547
mcc n/a| 6 -2 38 13 -46 610 -.81 143 143 | --- --- --- ---
| 3 8 24 89 112 533 .70 | --- ---
Table 1.2012.b GPS week : 2012 MJD: 58328.0-58334.0
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 | 25 21 19 18 21 19 20 |
R02 | 10 12 14 11 9 10 9 |
R03 | 10 12 12 11 10 9 10 |
R04 | 8 8 9 8 10 10 8 |
R05 | 18 17 15 14 16 17 19 |
R07 | 13 11 12 11 14 14 17 |
R08 | 12 10 8 10 11 9 10 |
R09 | 6 6 6 6 7 6 7 |
R10 | 7 7 9 9 7 8 8 |
R11 | 7 7 7 7 9 8 7 |
R13 | 9 9 7 9 9 11 10 |
R14 | 6 7 7 8 6 8 9 |
R15 | 12 11 10 10 11 12 13 |
R16 | 11 13 14 12 12 11 12 |
R17 | 10 11 10 10 11 11 11 |
R18 | 9 10 8 9 7 9 8 |
R19 | 23 20 19 25 19 21 21 |
R20 | 15 16 14 18 18 16 14 |
R21 | 11 13 10 12 9 11 11 |
R22 | 10 11 11 11 9 8 9 |
R23 | 9 11 11 9 9 9 10 |
R24 | 18 16 15 18 17 18 15 |
R26 | 14 15 20 27 19 25 19 |
Table 1.2012.c GPS week : 2012 MJD: 58328.0-58334.0
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 2012 0 | 58 15 110 -35 -1387 726 81.1 2698 2698 | 6843 0
brd 2012 1 | -30 -62 58 76 -729 -1509 82.3 2338 2338 | 6997 0
brd 2012 2 | 18 -70 80 604 518 -279 83.6 1763 1763 | 6211 0
brd 2012 3 | 50 10 139 -316 922 2894 82.2 1672 1672 | 4695 0
brd 2012 4 | 28 -41 179 -502 149 1966 82.4 1576 1576 | 3978 0
brd 2012 5 | 11 9 147 -795 -1151 -471 82.3 1661 1661 | 6316 0
brd 2012 6 | -61 -13 164 19 -38 -1765 82.8 1852 1852 | 5588 0
-------------+------------------------------------------------------------+----------------
brd 2012 mean| 10 -21 125 -135 -245 223 82.4 1937 1937 | 5804 0
brd 2012 sdev| 42 36 44 452 866 1737 .7 419 419 | 1121 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 2.2012.0 GPS week: 2012 Day: 0 MJD: 58328
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| -2 0 11 23 -37 -30 -.04 42 32 | 4235 -2014 3225 10424
cof n/a| -1 1 18 28 -13 -42 .10 44 33 | 4237 -2028 3228 10425
emx n/a| 0 0 1 34 -15 10 .09 24 24 | 8974 -1673 3239 10059
esx n/a| -1 0 -1 -20 5 -25 .08 15 12 | 10186 -251 3233 12092
gfz n/a| 0 0 -11 -22 71 -46 .04 30 27 | 0 -1535 3253 10078
grg n/a| -2 0 5 -44 -25 9 -.36 51 41 | 7714 -1409 3226 9858
iac n/a| 1 -1 -6 29 -4 63 -.25 26 25 | 8277 -1614 3229 9731
mcc n/a| 6 2 18 37 -111 536 -.08 107 107 | --- --- --- ---
Table 2.2012.1 GPS week: 2012 Day: 1 MJD: 58329
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 13 0 20 -16 .02 40 34 | 4066 333 4723 10261
cof n/a| 0 0 13 25 28 25 -.03 41 35 | 4069 317 4727 10265
emx n/a| -1 0 -3 7 -2 28 .02 21 21 | -8275 25 4655 9964
esx n/a| 0 0 -1 31 11 -7 .08 16 15 | -5007 233 4746 11858
gfz n/a| 0 0 -5 -17 59 42 .10 29 21 | 0 328 4656 9865
grg n/a| -1 0 10 -19 -4 -97 -.23 55 48 | 6100 724 4707 10022
iac n/a| 3 0 0 -56 -32 -4 -.10 25 24 | 7682 -436 4750 9744
mcc n/a| 4 2 25 -54 -21 665 -.89 106 106 | --- --- --- ---
Table 2.2012.2 GPS week: 2012 Day: 2 MJD: 58330
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| -2 0 12 -4 28 2 .00 38 37 | 6019 883 3338 10080
cof n/a| -1 0 18 2 22 34 .09 41 39 | 6033 845 3330 10077
emx n/a| 0 0 -3 32 -21 61 .04 20 20 | 14281 317 3349 9461
esx n/a| 0 0 -1 -17 2 -5 .10 15 13 | -9707 1490 3344 11224
gfz n/a| 0 0 -7 -20 -6 14 .06 30 24 | 0 1187 3347 9752
grg n/a| 1 -4 19 -5 -11 -94 -.32 53 50 | 5576 930 3356 9397
iac n/a| 1 0 -2 43 32 -30 -.13 24 23 | 8604 -766 3351 9544
mcc n/a| 2 -16 16 108 57 306 -.31 127 127 | --- --- --- ---
Table 2.2012.3 GPS week: 2012 Day: 3 MJD: 58331
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 15 11 0 -40 -.00 42 41 | 5347 -553 3282 9751
cof n/a| 0 2 20 35 9 -9 .02 44 43 | 5356 -583 3289 9755
emx n/a| -1 0 1 16 -21 90 .11 24 24 | -4234 -275 3287 9258
esx n/a| -1 0 0 -19 11 -2 .09 16 12 | 16845 230 3288 11353
gfz n/a| 0 2 -11 -32 42 15 .10 29 26 | 0 -579 3280 9479
grg n/a| 0 -1 3 -2 -33 -66 -.40 51 51 | 4921 -654 3273 8926
iac n/a| 0 0 -5 45 -3 -81 -.18 23 23 | 6620 -907 3273 9290
mcc n/a| 8 -11 24 82 36 23 -.33 159 159 | --- --- --- ---
Table 2.2012.4 GPS week: 2012 Day: 4 MJD: 58332
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 10 16 -21 -18 -.05 41 33 | 5621 -3293 3790 9769
cof n/a| 0 0 14 8 -22 -18 .02 46 36 | 5623 -3311 3787 9772
emx n/a| -1 -1 1 19 -4 79 .04 25 25 | 9400 -1868 3816 9296
esx n/a| 0 0 0 -7 -4 3 .10 14 11 | -28726 -1810 3803 10641
gfz n/a| 0 1 -8 -20 -6 15 .08 28 24 | 0 -3192 3811 9442
grg n/a| 2 1 5 -42 -42 -141 -.47 45 39 | 5099 -2437 3795 9311
iac n/a| 1 0 -3 1 37 -50 -.15 24 24 | 6286 -1781 3807 9122
mcc n/a| 5 -3 36 -27 -54 189 -.55 127 127 | --- --- --- ---
Table 2.2012.5 GPS week: 2012 Day: 5 MJD: 58333
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 1 7 45 18 -11 .03 36 34 | 5233 -763 3890 10701
cof n/a| -2 -1 13 11 57 26 .09 41 38 | 5223 -759 3888 10699
emx n/a| -2 1 -1 9 -11 33 .05 24 24 | -11673 -1320 3902 10103
esx n/a| 0 0 1 -19 0 -43 .10 15 12 | 20172 586 3875 12435
gfz n/a| 0 0 -8 23 24 42 .07 31 23 | 0 -445 3848 10354
grg n/a| -2 1 12 -55 0 -145 -.32 50 38 | 6473 -396 3918 10328
iac n/a| 4 1 -3 55 -38 114 -.17 27 26 | 7131 -576 3891 10043
mcc n/a| 13 -2 75 83 30 958 -1.96 173 173 | --- --- --- ---
Table 2.2012.6 GPS week: 2012 Day: 6 MJD: 58334
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 9 -14 -1 1 -.01 39 39 | 5297 -1367 3549 9515
cof n/a| -1 0 11 4 16 -13 .12 38 38 | 5316 -1408 3557 9520
emx n/a| -1 2 -1 53 -19 -119 .05 26 25 | -2993 -1715 3590 9033
esx n/a| 0 0 1 -9 8 24 .14 15 12 | -4254 -2296 3584 11585
gfz n/a| -1 0 -10 12 35 56 .11 29 27 | 0 -1019 3587 9204
grg n/a| 0 -2 11 -62 2 -257 -.43 53 42 | 6125 -916 3555 9045
iac n/a| 0 0 -4 -22 -10 90 -.16 24 22 | 7460 -474 3563 8970
mcc n/a| 2 8 71 -135 -263 1593 -1.53 204 204 | --- --- --- ---
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 3.2012.0 GPS week: 2012 Day: 0 MJD: 58328
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 | 632 100 90 26 38 42 119 33 --- 25 | 88 87 24 48 34 97 39 --- 29
R02 | 1723 33 36 16 11 22 31 26 74 9 | 79 84 53 48 40 80 33 111 50
R03 | 1616 28 29 21 8 30 30 26 111 9 | 75 79 58 50 33 85 35 38 51
R04 | 1868 26 26 13 10 25 10 20 --- 7 | 72 74 55 58 42 57 37 --- 52
R05 |10240 56 55 33 17 34 78 44 --- 17 | 67 77 39 42 40 70 26 --- 35
R07 | 658 46 53 31 13 39 21 24 133 12 | 86 92 57 44 39 63 31 85 46
R08 | 881 29 34 15 12 29 66 25 --- 12 | 75 80 53 49 33 99 40 --- 51
R09 | 4006 12 15 10 9 15 19 19 --- 6 | 34 36 30 33 40 25 36 --- 31
R10 | 2271 10 17 19 11 13 27 7 --- 6 | 63 66 48 65 50 71 58 --- 58
R11 | 981 15 18 15 11 25 18 8 117 6 | 63 66 46 52 36 58 46 73 48
R13 | 2471 12 14 22 13 22 39 17 --- 9 | 66 68 42 65 50 86 58 --- 58
R14 | 1075 16 18 13 10 18 21 10 --- 6 | 60 62 41 46 40 48 40 --- 44
R15 | 1901 59 52 23 10 33 21 19 --- 12 | 74 74 38 30 35 34 24 --- 31
R16 | 979 42 64 22 12 31 32 20 --- 10 | 87 97 48 72 55 84 66 --- 64
R17 | 713 36 37 21 9 24 22 27 --- 9 | 59 57 45 37 29 57 29 --- 38
R18 | 1252 24 25 23 14 31 14 19 --- 9 | 35 38 27 39 28 39 32 --- 32
R19 | 1167 90 96 29 25 59 85 51 --- 22 | 111 111 67 53 53 104 44 --- 60
R20 | 838 38 28 27 14 35 72 31 --- 14 | 70 73 37 51 45 72 39 --- 46
R21 | 1020 33 37 13 9 21 43 32 90 10 | 64 65 50 46 37 63 38 63 46
R22 | 1920 30 36 17 11 30 24 28 --- 9 | 56 60 43 44 32 55 30 --- 41
R23 | 661 15 18 27 17 21 16 14 --- 8 | 25 28 34 48 32 28 32 --- 34
R24 | 1099 25 42 49 16 26 101 18 --- 17 | 56 67 54 54 44 76 37 --- 48
XR26 | ---- 16 36 --- --- --- --- 12 --- 14 | 113 118 --- --- --- --- 113 --- 112
------+---------------------------------------------------+-----------------------------------------------
RMS | 2697 42 44 24 15 30 51 26 107 |T 68 72 44 48 39 65 41 74 48
WRMS | 2697 32 33 24 12 27 41 25 107 |NE 68 72 44 48 39 65 41 74 48
MEDI | 1099 29 36 21 11 26 27 20 111 |MD 67 73 45 48 39 63 37 73 46
Table 3.2012.1 GPS week: 2012 Day: 1 MJD: 58329
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 | 1294 83 84 25 21 44 101 42 --- 21 | 55 58 31 42 53 63 36 --- 29
R02 | 1486 40 35 13 11 14 58 32 58 11 | 60 54 34 36 37 69 23 61 35
R03 | 1097 33 31 20 18 31 55 27 106 12 | 55 53 43 40 25 77 25 37 37
R04 | 2725 24 25 10 8 20 19 25 --- 7 | 54 56 38 45 39 53 30 --- 40
R05 | 7596 51 46 20 22 36 95 35 --- 17 | 52 44 21 33 33 33 23 --- 20
R07 | 785 42 42 20 16 27 32 23 137 11 | 64 63 40 36 30 59 27 62 36
R08 | 957 28 28 14 12 34 34 21 --- 9 | 57 56 36 44 33 52 37 --- 39
R09 | 4204 10 13 12 11 12 18 17 --- 6 | 25 28 23 27 30 27 27 --- 24
R10 | 2487 13 10 15 13 16 33 7 --- 7 | 45 43 37 44 33 45 41 --- 39
R11 | 1001 19 15 15 10 19 22 8 133 6 | 41 39 30 34 28 28 32 54 30
R13 | 1543 16 14 20 16 14 42 10 --- 8 | 44 44 32 52 41 60 42 --- 42
R14 | 1150 19 23 10 12 23 21 11 --- 6 | 41 43 31 31 28 42 31 --- 30
R15 | 1277 53 64 19 16 24 27 17 --- 11 | 51 60 30 29 25 21 22 --- 25
R16 | 722 28 38 31 14 32 59 27 --- 13 | 52 49 34 45 45 71 52 --- 40
R17 | 696 38 37 11 11 31 50 20 --- 10 | 27 26 22 24 21 41 17 --- 21
R18 | 1466 26 29 21 21 16 22 20 --- 9 | 21 20 16 29 29 17 21 --- 20
R19 | 1273 84 79 24 23 49 74 47 --- 20 | 48 45 32 41 37 51 35 --- 35
R20 | 838 44 53 41 20 29 77 15 --- 15 | 36 44 30 32 29 37 22 --- 24
R21 | 1160 42 40 20 15 34 46 29 68 12 | 32 35 24 28 24 37 22 41 23
R22 | 3074 41 41 15 14 34 30 21 --- 10 | 29 32 21 28 32 23 17 --- 20
R23 | 592 15 18 27 28 15 39 11 --- 10 | 19 21 22 30 20 24 15 --- 17
R24 | 1279 30 38 24 14 34 106 29 --- 16 | 36 49 47 36 25 54 19 --- 30
XR26 | ---- 19 30 --- --- --- --- 11 --- 15 | 100 107 --- --- --- --- 108 --- 104
------+---------------------------------------------------+-----------------------------------------------
RMS | 2337 40 41 21 16 29 55 25 106 |T 45 46 30 35 31 44 31 51 33
WRMS | 2337 34 35 21 15 21 48 24 106 |NE 45 46 30 35 31 44 31 51 33
MEDI | 1273 30 35 20 14 27 39 21 106 |MD 45 44 31 34 30 42 27 54 30
Table 3.2012.2 GPS week: 2012 Day: 2 MJD: 58330
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 | 983 65 65 35 25 49 83 32 --- 19 | 54 58 31 49 58 68 41 --- 34
R02 | 1046 45 56 20 16 31 62 33 134 13 | 67 78 36 38 23 83 20 72 34
R03 | 1061 39 36 15 14 28 65 26 87 12 | 63 64 38 33 27 91 31 37 36
R04 | 2263 27 27 12 9 26 33 20 --- 8 | 57 56 41 39 30 68 33 --- 39
R05 | 4133 40 49 19 18 29 85 43 --- 15 | 53 61 38 40 21 31 25 --- 29
R07 | 706 38 35 20 9 39 45 28 123 11 | 69 68 46 43 24 80 24 52 42
R08 | 904 25 27 10 10 19 41 15 --- 7 | 65 67 40 47 38 75 47 --- 47
R09 | 3695 12 13 15 9 17 18 11 --- 5 | 25 26 22 19 30 26 21 --- 20
R10 | 1020 13 17 20 13 20 48 9 --- 8 | 49 50 36 58 47 83 48 --- 49
R11 | 1503 17 23 17 8 24 33 11 178 7 | 50 51 32 38 27 59 41 56 37
R13 | 2200 14 16 16 10 18 34 12 --- 6 | 52 54 37 50 39 56 43 --- 44
R14 | 1062 20 21 12 11 28 21 15 --- 7 | 49 51 39 47 31 47 39 --- 41
R15 | 2432 49 43 13 11 25 25 14 --- 9 | 52 50 22 25 18 29 25 --- 23
R16 | 906 22 39 35 13 41 67 25 --- 13 | 51 79 33 54 55 92 60 --- 47
R17 | 633 36 39 12 9 35 38 20 --- 9 | 36 37 28 29 22 36 18 --- 25
R18 | 1456 24 29 18 13 24 29 11 --- 8 | 28 32 25 22 20 33 23 --- 22
R19 | 658 85 85 19 24 39 70 40 --- 19 | 68 70 50 42 42 64 26 --- 40
R20 | 821 55 69 25 8 29 73 18 --- 13 | 56 69 33 39 40 43 41 --- 36
R21 | 713 31 38 13 5 34 38 30 91 10 | 49 51 39 41 31 52 35 33 38
R22 | 2585 36 41 15 9 30 46 29 --- 10 | 34 38 29 28 26 41 19 --- 26
R23 | 693 18 14 28 25 12 41 12 --- 10 | 25 26 32 34 25 22 20 --- 24
R24 | 834 19 32 31 26 33 80 24 --- 14 | 29 45 26 40 22 32 21 --- 24
XR26 | ---- 23 63 --- --- --- --- 17 --- 20 | 70 94 --- --- --- --- 61 --- 64
------+---------------------------------------------------+-----------------------------------------------
RMS | 1763 38 41 20 15 30 53 24 127 |T 50 55 34 38 31 55 33 50 35
WRMS | 1763 37 39 20 13 24 50 23 127 |NE 50 55 34 38 31 55 33 50 35
MEDI | 1020 27 36 17 11 28 41 20 123 |MD 52 54 33 39 27 52 31 52 36
Table 3.2012.3 GPS week: 2012 Day: 3 MJD: 58331
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 | 659 78 70 31 27 26 71 25 --- 17 | 65 66 32 51 42 50 30 --- 31
R02 | 825 41 41 19 10 31 39 26 224 11 | 70 70 46 43 32 65 24 123 41
R03 | 1169 40 44 16 7 35 37 28 80 11 | 73 80 51 46 26 67 24 41 43
R04 | 1390 32 26 11 7 18 24 19 --- 7 | 67 68 46 44 37 55 29 --- 43
R05 | 1604 41 49 19 23 29 74 23 --- 14 | 57 73 27 57 35 32 24 --- 37
R07 | 897 43 46 24 5 30 19 29 143 10 | 75 78 55 43 25 45 23 51 41
R08 | 1349 32 39 12 7 40 45 15 --- 10 | 73 76 47 41 29 76 37 --- 44
R09 | 3172 10 16 14 10 13 12 16 --- 5 | 23 27 20 21 27 16 23 --- 19
R10 | 1019 15 19 23 14 22 37 13 --- 8 | 54 54 48 62 51 76 54 --- 55
R11 | 1435 16 17 13 7 24 38 9 201 7 | 62 65 48 54 44 75 42 57 51
R13 | 2864 16 15 12 16 13 43 24 --- 9 | 56 57 45 47 45 76 48 --- 48
R14 | 806 26 32 12 14 24 23 15 --- 8 | 55 61 42 44 28 33 33 --- 38
R15 | 3822 41 43 20 9 33 22 17 --- 10 | 59 62 39 34 23 26 23 --- 31
R16 | 858 23 24 25 17 16 68 27 --- 12 | 74 73 46 63 50 93 52 --- 56
R17 | 603 41 45 12 8 31 28 27 --- 10 | 43 47 34 32 25 44 22 --- 29
R18 | 1290 16 21 11 15 29 36 18 --- 8 | 30 32 25 38 22 50 21 --- 28
R19 | 735 105 112 33 42 47 94 37 --- 24 | 83 83 48 55 30 77 19 --- 39
R20 | 1351 60 60 53 8 25 82 27 --- 18 | 76 74 47 46 49 57 37 --- 45
R21 | 1062 39 36 23 9 36 39 30 91 11 | 50 50 42 34 27 52 32 53 35
R22 | 2174 37 35 14 6 39 44 28 --- 11 | 51 49 34 35 19 57 25 --- 32
R23 | 692 17 21 24 19 14 18 17 --- 8 | 23 28 30 38 32 29 24 --- 28
R24 | 1946 27 39 48 23 32 99 24 --- 18 | 45 51 50 48 41 41 26 --- 38
XR26 | ---- 35 100 --- --- --- --- 19 --- 26 | 64 106 --- --- --- --- 40 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1672 42 44 24 16 29 51 23 159 |T 57 62 41 44 33 54 30 65 39
WRMS | 1672 41 43 24 12 26 51 23 159 |NE 57 62 41 44 33 54 30 65 39
MEDI | 1169 35 39 19 10 29 38 24 143 |MD 59 65 45 44 30 52 26 53 39
Table 3.2012.4 GPS week: 2012 Day: 4 MJD: 58332
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 | 628 83 104 32 29 49 80 25 --- 20 | 65 88 32 51 45 60 35 --- 33
R02 | 599 31 40 15 9 24 41 16 136 9 | 58 66 39 45 33 65 35 43 41
R03 | 1529 41 45 20 8 31 33 18 73 10 | 66 70 47 40 31 61 34 37 41
R04 | 1024 34 36 18 8 30 16 30 --- 9 | 60 63 44 42 29 47 28 --- 38
R05 | 1300 54 58 43 15 32 58 27 --- 15 | 57 63 35 32 41 38 30 --- 26
XR07 |29656 48 35 --- 11 34 36 26 137 13 | 77 66 --- 48 27 70 26 47 43
R08 | 1949 34 33 11 5 35 47 22 --- 10 | 68 69 42 43 33 74 34 --- 43
R09 | 2122 14 18 22 14 14 18 14 --- 7 | 22 20 24 32 34 28 25 --- 25
R10 | 1930 15 11 16 13 20 24 12 --- 7 | 49 50 44 58 41 56 50 --- 50
R11 | 1517 22 22 15 8 21 42 15 176 8 | 57 56 49 49 39 73 40 87 48
R13 | 2552 13 19 18 8 21 49 13 --- 8 | 55 57 43 49 37 74 48 --- 48
R14 | 785 25 23 11 8 17 13 10 --- 6 | 53 55 41 38 36 35 39 --- 39
R15 | 2730 48 37 21 9 35 20 22 --- 11 | 56 50 39 32 40 30 26 --- 32
R16 | 613 20 39 26 19 19 32 37 --- 11 | 69 88 42 65 63 67 63 --- 58
R17 | 637 39 41 17 10 22 46 25 --- 10 | 45 48 40 31 31 50 25 --- 32
R18 | 558 19 20 12 13 25 18 15 --- 7 | 28 30 26 33 24 27 27 --- 27
R19 | 1399 81 85 29 13 56 59 43 --- 19 | 74 77 55 51 41 64 31 --- 46
R20 | 2366 61 76 45 15 29 78 27 --- 17 | 66 78 48 35 38 56 37 --- 39
R21 | 1507 34 39 14 10 20 31 22 96 9 | 42 47 32 39 42 38 32 33 35
R22 | 1076 32 39 14 7 24 26 29 --- 9 | 41 44 31 35 26 38 24 --- 30
R23 | 798 20 18 29 22 14 14 11 --- 9 | 23 25 23 36 26 26 24 --- 25
R24 | 2158 25 28 49 20 18 87 33 --- 17 | 35 42 42 39 33 41 26 --- 28
XR26 | ---- 24 122 --- --- --- --- 15 --- 19 | 70 131 --- --- --- --- 68 --- 70
------+---------------------------------------------------+-----------------------------------------------
RMS | 1575 41 46 25 14 28 45 24 127 |T 53 60 38 41 35 50 35 49 39
WRMS | 1575 33 36 25 11 24 39 24 127 |NE 53 60 38 41 35 50 35 49 39
MEDI | 1399 32 37 18 10 24 33 22 136 |MD 57 57 41 39 34 50 32 43 39
Table 3.2012.5 GPS week: 2012 Day: 5 MJD: 58333
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 | 689 79 91 28 21 39 77 36 --- 19 | 54 65 25 32 33 47 36 --- 24
R02 | 1031 32 34 14 6 32 43 16 150 9 | 48 49 30 32 23 57 24 71 31
R03 | 1573 36 38 16 6 19 28 23 105 8 | 54 58 28 33 30 48 25 35 33
R04 | 642 31 36 20 6 33 28 30 --- 10 | 50 56 41 36 34 50 25 --- 35
R05 | 1224 49 63 52 20 25 62 26 --- 16 | 47 53 45 37 30 29 25 --- 29
XR07 |12878 48 54 --- 15 32 43 18 99 14 | 54 63 --- 31 39 53 26 54 31
R08 | 1682 22 23 14 15 16 27 31 --- 9 | 55 57 34 59 46 52 30 --- 46
R09 | 2044 10 13 13 7 16 19 21 --- 6 | 20 20 17 29 30 18 28 --- 21
R10 | 2841 11 13 20 12 14 33 17 --- 7 | 40 44 37 52 42 64 45 --- 44
R11 | 1052 25 21 23 8 22 22 13 263 8 | 49 46 32 38 29 45 30 52 35
R13 | 3204 11 19 16 8 25 78 13 --- 11 | 41 49 29 37 27 90 32 --- 36
R14 | 703 20 21 14 13 31 14 20 --- 8 | 41 42 30 40 21 36 38 --- 34
R15 | 3546 46 45 19 15 31 25 33 --- 12 | 45 45 29 26 20 35 27 --- 25
R16 | 1115 26 33 25 19 23 32 32 --- 11 | 57 65 51 59 41 54 48 --- 49
R17 | 767 34 38 16 8 34 45 23 --- 10 | 27 29 24 22 16 34 20 --- 21
R18 | 601 21 31 18 15 31 25 16 --- 8 | 19 25 17 22 22 24 19 --- 17
R19 | 970 68 78 23 14 55 99 54 --- 20 | 56 60 49 49 40 87 34 --- 47
R20 | 1997 37 49 33 27 43 62 35 --- 16 | 42 48 58 42 35 29 26 --- 35
R21 | 1938 38 37 23 13 37 33 16 128 11 | 45 43 45 37 35 36 39 42 38
R22 | 710 34 36 12 9 16 16 23 --- 8 | 28 33 24 27 31 21 21 --- 24
R23 | 620 15 20 21 22 17 30 16 --- 9 | 18 20 21 25 26 20 15 --- 19
R24 | 835 20 20 39 17 44 107 30 --- 17 | 32 37 53 27 25 30 20 --- 24
XR26 | ---- 28 48 --- --- --- --- 21 --- 24 | 51 82 --- --- --- --- 52 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1661 36 41 24 15 31 50 27 173 |T 42 47 34 36 30 43 29 50 32
WRMS | 1661 34 38 24 12 23 38 26 173 |NE 42 47 34 36 30 43 29 50 32
MEDI | 1052 31 36 20 13 31 32 23 128 |MD 45 48 30 33 30 36 27 52 33
Table 3.2012.6 GPS week: 2012 Day: 6 MJD: 58334
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 | 721 79 69 42 14 36 91 30 --- 19 | 71 74 41 35 46 77 40 --- 29
R02 | 649 32 37 16 9 29 29 22 169 9 | 69 72 48 43 39 72 37 84 44
R03 | 2180 32 32 18 5 33 38 21 144 9 | 72 76 51 48 29 81 35 30 47
R04 | 837 29 27 14 7 20 27 15 --- 7 | 71 73 55 51 42 63 39 --- 50
R05 | 1110 40 40 51 29 20 101 22 --- 18 | 51 64 32 40 33 72 25 --- 29
R07 | 2013 51 48 42 16 28 38 52 102 16 | 85 80 55 45 33 77 29 74 46
R08 | 1871 32 32 17 11 31 41 21 --- 10 | 82 87 63 58 41 88 44 --- 57
R09 | 1792 12 14 16 7 19 26 15 --- 6 | 27 29 27 37 41 28 34 --- 31
R10 | 2440 17 14 21 17 19 21 8 --- 7 | 65 66 57 74 53 80 62 --- 64
R11 | 1085 21 24 13 8 16 25 19 342 7 | 75 77 62 66 48 80 55 75 62
R13 | 2769 14 16 22 10 28 59 13 --- 10 | 71 70 53 67 49 109 57 --- 62
R14 | 913 22 21 23 8 28 32 12 --- 8 | 69 71 58 56 48 68 56 --- 55
R15 | 5601 55 57 24 20 33 28 23 --- 13 | 73 76 41 33 25 50 30 --- 34
R16 | 1187 30 36 18 18 19 53 32 --- 11 | 80 85 54 65 53 94 69 --- 63
R17 | 1220 35 32 17 5 36 49 24 --- 11 | 61 62 53 42 31 65 32 --- 43
R18 | 1041 26 24 16 11 24 32 15 --- 8 | 42 44 35 40 25 45 29 --- 34
R19 | 1175 85 78 25 23 49 87 42 --- 20 | 113 108 73 58 47 115 46 --- 63
R20 | 809 24 32 32 14 32 83 13 --- 13 | 71 76 49 52 43 76 40 --- 48
R21 | 1510 33 32 22 11 38 39 22 175 11 | 73 74 65 63 57 69 54 55 61
R22 | 759 31 32 16 14 28 33 13 --- 9 | 57 56 45 45 36 53 39 --- 43
R23 | 639 21 22 26 22 13 23 17 --- 9 | 31 35 32 46 43 35 32 --- 35
R24 | 867 28 41 41 13 32 81 30 --- 15 | 57 71 70 46 37 62 35 --- 46
XR26 | ---- 24 94 --- --- --- --- 15 --- 19 | 78 114 --- --- --- --- 72 --- 71
------+---------------------------------------------------+-----------------------------------------------
RMS | 1851 39 38 26 15 29 53 24 204 |T 67 71 50 50 40 70 43 63 48
WRMS | 1851 39 38 25 12 27 42 22 204 |NE 67 71 50 50 40 70 43 63 48
MEDI | 1110 30 32 21 11 28 38 21 169 |MD 71 73 53 46 41 72 39 74 47
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