[IGSREPORT-24299] Wk 1885 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Mar 10 21:14:08 PST 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1885 (Feb 21, 2016 - Feb 27, 2016)
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 2.1885.
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:
igl1885[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1885 in the SP3 format.
igl18857.sum Combination Report for GPS Week 1885.
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 | 3.2 ns
1 | 2.5 ns
2 | 3.7 ns
3 | 6.9 ns
4 | 2.2 ns
5 | 0.9 ns
6 | 1.6 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 | IAC | R09
1 | EMX | R09
1 | IAC | R09
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 1.1885, 1a.1885).
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 2.1885.0-6)
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 3.1885.0-6).
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 1885 summary. (Feb 21, 2016 - Feb 27, 2016)
Table 1.1885.a GPS week : 1885 MJD: 57439.0-57445.0
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 -10 37 -29 11 .26 45 42 | --- --- --- ---
| 1 2 3 40 43 43 .06 | --- ---
cof n/a| 0 0 -13 47 -5 -16 .23 48 45 | --- --- --- ---
| 2 1 3 33 36 50 .10 | --- ---
emx n/a| 0 -1 0 -8 -12 -37 .28 30 30 | 3043 586 3929 7636
| 1 1 2 38 32 27 .03 | 9409 971
esx n/a| 1 0 0 -23 -9 -5 -.05 21 20 | 3776 649 3780 8119
| 0 1 1 28 28 13 .06 | 5253 1819
gfz n/a| 0 0 5 28 69 42 .13 26 22 | 0 401 3653 6676
| 1 1 1 22 32 26 .07 | 0 1512
grg n/a| -4 0 6 -85 73 61 -.44 38 37 | -461567 332 6560 617398
| 1 1 2 30 14 24 .04 | 12295 1705
iac n/a| 0 1 -1 18 -39 -21 -.12 19 19 | 3966 69 3882 7395
| 0 0 1 45 43 29 .03 | 2445 1321
mcc n/a| 0 2 -22 63 -90 538 -.32 158 158 | --- --- --- ---
| 9 2 23 101 140 465 .34 | --- ---
Table 1.1885.b GPS week : 1885 MJD: 57439.0-57445.0
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 15 14 12 16 11 11 |
R02 | 8 10 8 9 9 20 10 |
R03 | 9 9 11 10 13 12 13 |
R04 | 12 9 8 9 10 9 9 |
R05 | 13 13 15 12 14 13 13 |
R06 | 8 10 9 7 9 8 8 |
R07 | 11 13 13 10 11 11 12 |
R08 | 12 11 12 11 12 11 11 |
R09 | 57 14 26 8 9 7 7 |
R10 | 10 8 8 8 10 8 9 |
R11 | 17 18 17 18 17 19 19 |
R13 | 9 8 10 9 9 10 8 |
R14 | 17 21 16 14 13 13 15 |
R15 | 10 10 14 13 10 11 13 |
R17 | 83 71 61 0 0 0 25 |
R18 | 11 9 11 10 9 12 9 |
R19 | 10 9 11 11 11 9 10 |
R20 | 14 16 13 16 14 14 17 |
R21 | 11 12 10 12 12 11 9 |
R22 | 13 14 14 11 11 10 12 |
R23 | 11 10 8 9 8 8 9 |
R24 | 14 19 16 19 17 14 14 |
R26 | 21 25 28 49 65 36 35 |
Table 1.1885.c GPS week : 1885 MJD: 57439.0-57445.0
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 1885 0 | -5 71 63 400 404 3111 84.3 1241 1241 | 3245 0
brd 1885 1 | 8 -60 86 457 -1034 -3531 84.1 2045 2045 | 2546 0
brd 1885 2 | 16 28 127 -2219 575 -2058 85.0 2300 2300 | 3655 0
brd 1885 3 | 46 -19 55 -804 1193 -573 84.6 2702 2702 | 6881 0
brd 1885 4 | -6 41 16 -441 -112 -1045 83.7 3208 3208 | 2230 0
brd 1885 5 | -54 -8 -51 12 -1781 -752 83.5 2555 2555 | 861 0
brd 1885 6 | 24 -11 -44 -327 -945 -1486 83.6 1986 1986 | 1629 0
-------------+------------------------------------------------------------+----------------
brd 1885 mean| 4 5 36 -417 -242 -905 84.1 2291 2291 | 3006 0
brd 1885 sdev| 31 43 66 914 1052 2034 .6 623 623 | 1949 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 2.1885.0 GPS week: 1885 Day: 0 MJD: 57439
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 2 -15 17 32 -30 .23 44 39 | --- --- --- ---
cof n/a| -2 0 -16 70 28 -16 .17 48 42 | --- --- --- ---
emx n/a| -1 0 2 -43 -9 -4 .27 22 22 | 5758 357 3961 10251
esx n/a| 2 -2 0 -54 -7 0 -.13 21 20 | 11511 732 3912 8907
gfz n/a| 3 0 4 24 74 63 .06 26 23 | 0 391 3885 8145
grg n/a| -3 0 9 -74 75 67 -.38 36 38 | -482147 694 3972 624403
iac n/a| 0 0 -5 78 -76 -69 -.10 23 23 | 6135 -570 3971 9611
mcc n/a| 1 0 -43 123 -374 511 -.36 400 400 | --- --- --- ---
Table 2.1885.1 GPS week: 1885 Day: 1 MJD: 57440
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 4 -11 2 -53 2 .32 45 41 | --- --- --- ---
cof n/a| 0 2 -15 41 -22 -8 .29 48 44 | --- --- --- ---
emx n/a| 0 -2 0 -28 18 -26 .29 29 31 | -15057 -106 4505 7459
esx n/a| 2 0 -1 14 2 -20 -.10 23 22 | 4887 -2260 4174 7613
gfz n/a| 0 -2 3 51 64 32 .12 26 19 | 0 -1438 3763 5419
grg n/a| -3 1 9 -64 81 81 -.49 35 36 | -458321 -2517 4911 619296
iac n/a| 0 2 0 -38 -57 5 -.14 21 21 | 4398 -1120 4828 8809
mcc n/a| 1 1 -37 -103 1 583 -.82 167 167 | --- --- --- ---
Table 2.1885.2 GPS week: 1885 Day: 2 MJD: 57441
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| -4 -2 -9 84 -39 -4 .19 47 45 | --- --- --- ---
cof n/a| -5 0 -15 65 -59 -1 .10 49 46 | --- --- --- ---
emx n/a| 2 0 -4 -41 -77 -55 .33 47 44 | 2771 -796 4117 6126
esx n/a| 2 0 1 -55 -53 16 -.07 21 20 | 6750 621 3435 7345
gfz n/a| 0 0 5 35 6 49 .26 25 19 | 0 393 3375 5285
grg n/a| -5 2 8 -40 78 13 -.44 36 33 | -441272 -89 8195 611101
iac n/a| 0 1 0 26 26 -20 -.12 19 19 | 4045 232 3424 5173
mcc n/a| 12 5 -47 108 -105 787 .08 116 116 | --- --- --- ---
Table 2.1885.3 GPS week: 1885 Day: 3 MJD: 57442
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 -10 104 -65 60 .21 46 48 | --- --- --- ---
cof n/a| 3 0 -8 78 28 0 .17 49 48 | --- --- --- ---
emx n/a| 0 -4 1 51 -25 -73 .28 30 27 | 2801 77 3864 6945
esx n/a| 1 0 0 3 -24 -16 .00 22 22 | 4679 -983 3850 8102
gfz n/a| 0 2 6 42 75 33 .16 24 21 | 0 -875 3819 6458
grg n/a| -5 3 3 -109 61 88 -.45 37 40 | -456345 -368 3873 616546
iac n/a| 0 0 0 -25 -12 7 -.13 16 16 | 7943 -1289 3864 6246
mcc n/a| -2 5 -16 59 -116 1008 .03 89 89 | --- --- --- ---
Table 2.1885.4 GPS week: 1885 Day: 4 MJD: 57443
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 -10 32 -85 85 .28 44 39 | --- --- --- ---
cof n/a| 0 0 -16 48 -42 42 .37 49 43 | --- --- --- ---
emx n/a| 0 -2 0 32 2 -52 .25 28 30 | 13431 1732 4870 7195
esx n/a| 2 0 -2 -1 -32 6 -.02 20 20 | 4682 3197 4883 8271
gfz n/a| 0 1 6 23 66 -3 .08 25 23 | 0 2940 4585 6661
grg n/a| -3 0 3 -130 89 60 -.48 38 39 | -461853 2838 4884 617008
iac n/a| 0 1 -1 -1 -7 -20 -.09 19 19 | 1750 2532 4884 6725
mcc n/a| 9 0 20 159 66 1022 -.08 100 100 | --- --- --- ---
Table 2.1885.5 GPS week: 1885 Day: 5 MJD: 57444
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 -7 17 2 -19 .35 45 38 | --- --- --- ---
cof n/a| 0 0 -14 -23 19 -10 .20 47 41 | --- --- --- ---
emx n/a| 1 -1 0 -33 14 -2 .27 24 26 | -241 1067 2938 6178
esx n/a| 1 0 0 -35 27 -12 -.07 18 18 | -2259 1196 2930 6436
gfz n/a| 0 1 8 -16 111 79 .09 29 29 | 0 -323 2910 5896
grg n/a| -5 -1 5 -104 46 64 -.42 44 33 | -464401 -21 9718 618017
iac n/a| 0 0 -2 75 -94 -52 -.08 19 19 | 2198 -178 2939 6255
mcc n/a| -11 3 -12 146 -44 -210 -.55 98 98 | --- --- --- ---
Table 2.1885.6 GPS week: 1885 Day: 6 MJD: 57445
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 -6 4 4 -13 .22 46 47 | --- --- --- ---
cof n/a| -2 -1 -7 47 11 -121 .29 45 48 | --- --- --- ---
emx n/a| 0 -2 2 2 -11 -49 .27 31 32 | 11843 1776 3248 9302
esx n/a| 0 0 -2 -34 18 -7 .04 19 18 | -3814 2045 3281 10161
gfz n/a| 0 -1 3 36 89 39 .17 24 20 | 0 1720 3234 8871
grg n/a| -1 1 6 -73 80 55 -.44 36 39 | -466634 1791 10370 615420
iac n/a| 1 0 -1 17 -55 0 -.17 17 17 | 1293 878 3270 8952
mcc n/a| -11 1 -23 -48 -64 68 -.54 137 137 | --- --- --- ---
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 3.1885.0 GPS week: 1885 Day: 0 MJD: 57439
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 | 1373 68 85 18 20 24 30 29 --- 13 | 90 106 42 53 27 36 20 --- 36
R02 | 1249 33 42 19 16 13 22 14 --- 8 | 73 79 55 52 46 46 39 --- 47
R03 | 969 43 43 14 8 18 35 17 98 9 | 92 95 60 59 47 45 48 87 53
R04 | 848 47 46 24 16 33 38 12 --- 11 | 86 88 51 57 32 46 43 --- 47
R05 | 1111 49 53 19 26 34 39 26 --- 13 | 78 75 44 54 30 38 43 --- 40
R06 | 1280 16 22 15 10 18 24 25 --- 8 | 57 50 61 67 48 52 64 --- 58
R07 | 1185 40 43 18 13 29 45 20 676 11 | 84 86 64 51 31 42 43 424 46
R08 | 799 41 40 20 18 28 38 22 --- 11 | 80 82 61 57 36 31 39 --- 46
XR09 | 3403 69 68 90 74 --- --- 366 --- 57 | 29 33 59 37 --- --- 215 --- 32
R10 | 906 30 31 23 23 15 24 15 --- 9 | 65 63 54 65 47 49 51 --- 52
R11 | 816 88 95 40 14 31 35 35 --- 17 | 70 70 48 52 70 70 57 --- 49
R13 | 1651 28 34 17 20 18 26 11 --- 8 | 54 55 42 39 32 28 27 --- 33
R14 | 2581 31 31 39 21 51 38 42 --- 17 | 69 76 59 70 78 42 77 --- 61
R15 | 2377 25 29 21 21 26 25 21 --- 10 | 47 46 32 45 45 33 35 --- 36
XR17 | 779 126 124 95 --- --- --- 135 --- 83 | 19 34 56 --- --- --- 26 --- 31
R18 | 654 42 42 10 20 24 27 25 --- 10 | 52 55 42 46 40 36 29 --- 34
R19 | 754 36 43 17 20 25 23 19 --- 9 | 59 63 43 48 37 24 34 --- 36
R20 | 611 51 47 28 28 23 52 22 --- 14 | 57 56 52 39 26 22 23 --- 29
R21 | 1025 42 50 19 24 24 36 17 117 11 | 58 62 44 56 41 29 33 117 39
R22 | 578 51 52 22 17 19 46 26 --- 12 | 75 75 52 49 33 33 30 --- 39
R23 | 641 14 16 14 34 18 31 15 --- 10 | 31 32 33 54 36 29 26 --- 33
R24 | 1043 40 49 18 31 31 58 13 --- 13 | 42 43 45 51 27 30 27 --- 31
XR26 | ---- 35 148 --- --- --- --- 13 --- 21 | 42 296 --- --- --- --- 34 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1241 44 48 22 21 26 36 23 400 |T 61 74 49 52 40 38 46 209 40
WRMS | 1241 39 42 22 20 23 38 23 400 |NE 61 74 49 52 40 38 46 209 40
MEDI | 969 41 43 19 20 24 35 21 117 |MD 59 63 51 52 36 36 35 117 39
Table 3.1885.1 GPS week: 1885 Day: 1 MJD: 57440
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 | 1469 69 71 27 24 28 33 29 --- 14 | 67 72 45 43 37 34 18 --- 29
R02 | 1617 31 36 24 22 20 18 20 --- 10 | 55 60 49 54 36 35 27 --- 38
R03 | 1122 45 55 14 12 22 24 13 157 9 | 66 75 41 35 56 33 37 39 40
R04 | 640 44 51 17 9 15 29 10 --- 8 | 63 71 45 39 37 35 33 --- 38
R05 | 808 44 55 18 37 29 39 17 --- 13 | 64 79 58 59 32 39 44 --- 43
R06 | 2265 21 23 23 22 23 15 19 --- 9 | 38 40 48 59 38 41 49 --- 45
R07 | 2462 52 55 39 16 24 24 19 207 12 | 61 61 51 32 31 28 23 330 29
R08 | 607 34 36 27 20 19 36 16 --- 10 | 56 56 56 42 34 39 34 --- 39
XR09 | 3468 23 29 259 8 --- --- 370 --- 14 | 24 25 94 32 --- --- 235 --- 32
R10 | 1244 16 23 17 20 18 25 11 --- 8 | 40 44 33 45 35 40 32 --- 34
R11 | 889 98 92 40 24 34 37 20 --- 17 | 61 63 37 51 64 59 50 --- 43
R13 | 799 28 33 15 13 18 25 14 --- 8 | 39 42 32 30 32 28 21 --- 24
R14 | 2223 42 36 55 38 47 50 48 --- 21 | 56 73 67 76 70 42 65 --- 54
R15 | 7137 20 23 28 20 30 14 11 --- 9 | 32 30 30 36 37 28 25 --- 27
XR17 | 935 112 118 110 --- --- 98 141 --- 70 | 32 43 63 --- --- 15 21 --- 41
R18 | 489 36 42 17 16 19 25 14 --- 8 | 35 42 36 33 31 23 22 --- 26
R19 | 536 40 40 16 15 18 28 11 --- 9 | 38 40 24 34 33 14 22 --- 23
R20 | 586 48 55 50 21 26 48 24 --- 15 | 38 49 52 28 29 24 14 --- 18
R21 | 663 49 43 25 12 23 39 17 126 11 | 35 33 29 20 27 22 23 84 20
R22 | 578 62 70 29 21 21 50 23 --- 14 | 46 54 30 31 25 27 22 --- 20
R23 | 932 14 13 24 28 19 28 10 --- 9 | 21 25 36 39 32 34 23 --- 26
R24 | 1893 20 27 33 41 46 69 30 --- 18 | 42 47 59 49 37 25 29 --- 31
XR26 | ---- 45 225 --- --- --- --- 13 --- 24 | 36 301 --- --- --- --- 61 --- 46
------+---------------------------------------------------+-----------------------------------------------
RMS | 2044 45 48 29 23 26 35 21 167 |T 45 61 46 41 37 31 40 151 33
WRMS | 2044 41 44 31 22 19 36 21 167 |NE 45 61 46 41 37 31 40 151 33
MEDI | 932 42 42 25 20 22 29 17 157 |MD 40 49 45 39 34 33 27 84 32
Table 3.1885.2 GPS week: 1885 Day: 2 MJD: 57441
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 | 1713 69 60 28 21 37 36 16 --- 14 | 67 67 28 46 51 20 20 --- 29
R02 | 1292 35 36 17 15 17 20 14 --- 8 | 61 61 45 49 29 46 33 --- 38
R03 | 1209 52 52 29 18 18 28 17 130 11 | 68 70 46 45 32 27 28 37 33
R04 | 601 44 43 12 11 14 21 9 --- 7 | 66 64 38 42 45 39 37 --- 40
R05 | 881 62 57 49 22 25 49 18 --- 14 | 70 72 57 46 38 45 39 --- 39
R06 | 583 14 18 17 25 22 17 13 --- 8 | 47 53 51 66 38 41 47 --- 48
R07 | 1326 59 64 33 19 35 22 14 125 12 | 71 76 46 46 23 32 27 199 30
R08 | 921 50 56 28 23 14 33 19 --- 11 | 66 71 54 50 32 28 26 --- 35
R09 | 2538 29 26 148 26 20 25 51 --- 26 | 23 34 52 37 31 23 92 --- 32
R10 | 1089 22 20 25 16 13 28 11 --- 8 | 54 52 44 49 45 53 49 --- 47
R11 | 1231 95 93 46 21 35 43 12 --- 17 | 60 63 49 58 71 60 51 --- 50
R13 | 839 37 35 31 18 18 28 11 --- 9 | 48 47 37 32 28 28 24 --- 25
R14 | 1375 37 44 42 27 35 37 35 --- 15 | 55 72 65 68 69 42 74 --- 60
R15 | 9114 22 27 39 21 49 29 15 --- 13 | 43 43 34 44 67 37 34 --- 38
XR17 | 970 83 94 75 --- --- 89 124 --- 61 | 43 50 24 --- --- 20 19 --- 51
R18 | 621 35 38 23 24 24 41 11 --- 11 | 47 47 36 43 26 32 25 --- 28
R19 | 807 39 43 21 25 19 35 16 --- 10 | 52 50 36 51 42 25 32 --- 35
R20 | 641 43 73 58 11 19 45 17 --- 13 | 37 60 34 24 20 17 19 --- 19
R21 | 562 41 51 20 22 19 28 14 90 10 | 48 57 38 44 31 24 26 56 31
R22 | 557 64 61 23 19 31 50 14 --- 13 | 57 51 29 32 31 32 27 --- 24
R23 | 719 21 21 20 19 13 34 9 --- 8 | 23 24 24 35 24 37 25 --- 24
R24 | 1877 30 44 67 30 16 65 14 --- 16 | 41 36 50 51 35 31 37 --- 35
XR26 | ---- 56 416 --- --- --- --- 14 --- 27 | 25 685 --- --- --- --- 46 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 2300 47 49 47 21 25 36 19 116 |T 50 82 41 45 38 33 36 97 36
WRMS | 2300 45 46 44 20 19 33 19 116 |NE 50 82 41 45 38 33 36 97 36
MEDI | 921 41 44 28 21 19 33 14 125 |MD 52 57 38 46 32 32 32 56 35
Table 3.1885.3 GPS week: 1885 Day: 3 MJD: 57442
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 | 1150 66 71 20 24 24 35 16 --- 12 | 72 77 28 42 33 27 22 --- 26
R02 | 1394 30 33 15 18 22 36 14 --- 9 | 69 71 45 59 41 48 45 --- 47
R03 | 702 43 44 20 22 23 22 18 117 10 | 81 78 45 59 36 44 40 44 45
R04 | 563 48 46 11 20 20 23 11 --- 9 | 76 72 36 53 29 33 37 --- 39
R05 | 803 52 63 34 24 18 23 19 --- 11 | 63 73 41 38 39 44 32 --- 34
R06 | 771 20 18 13 10 14 24 13 --- 6 | 58 54 43 46 35 43 44 --- 42
R07 | 888 50 52 18 17 30 30 7 73 10 | 80 84 48 54 38 30 41 121 43
R08 | 1006 55 60 23 18 31 32 8 --- 11 | 80 83 53 46 27 37 43 --- 41
R09 | 1893 17 29 24 19 11 15 17 --- 8 | 23 32 60 41 28 25 48 --- 26
R10 | 1122 24 32 18 15 19 28 9 --- 7 | 64 67 43 57 55 36 51 --- 49
R11 | 1283 94 85 53 36 22 35 15 --- 17 | 67 59 59 48 56 52 46 --- 42
R13 | 577 39 37 23 16 21 26 11 --- 9 | 44 42 31 28 28 29 24 --- 22
R14 | 1400 29 33 32 24 31 51 29 --- 14 | 49 54 51 67 58 41 73 --- 57
R15 |11514 32 31 28 21 47 37 14 --- 13 | 50 49 33 38 60 27 26 --- 29
XR17 | ---- 10 157 --- --- --- --- --- --- 0 | 40 131 --- --- --- --- --- --- 45
R18 | 599 31 36 21 17 15 47 11 --- 9 | 43 48 42 35 27 34 22 --- 27
R19 | 639 46 53 23 17 29 34 8 --- 10 | 56 62 35 39 28 32 28 --- 28
R20 | 651 48 34 58 23 16 54 24 --- 16 | 46 39 50 42 37 42 22 --- 29
R21 | 873 53 54 25 23 26 35 16 70 11 | 53 52 35 49 46 35 36 34 37
R22 | 631 52 54 13 28 22 36 13 --- 11 | 61 64 38 50 22 18 23 --- 30
R23 | 808 20 17 14 23 16 35 14 --- 8 | 31 32 31 36 27 30 24 --- 25
R24 | 1327 38 74 64 36 24 77 23 --- 19 | 58 92 46 60 40 35 24 --- 36
XR26 | ---- 109 1355 --- --- --- --- 21 --- 48 | 83 9999 --- --- --- --- 39 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 2701 46 49 30 22 24 37 16 89 |T 58 64 42 47 37 35 35 66 36
WRMS | 2701 48 48 27 22 21 40 16 89 |NE 58 64 42 47 37 35 35 66 36
MEDI | 873 43 46 23 21 22 35 14 73 |MD 58 62 43 46 36 35 36 44 36
Table 3.1885.4 GPS week: 1885 Day: 4 MJD: 57443
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 | 1471 71 77 42 26 46 32 10 --- 16 | 70 77 37 32 34 17 20 --- 17
R02 | 1134 34 39 16 14 19 31 16 --- 8 | 58 64 36 40 33 52 38 --- 35
R03 | 1326 44 44 30 15 23 61 11 75 12 | 73 75 58 51 44 36 43 56 45
R04 | 574 38 46 22 11 24 41 13 --- 10 | 69 77 55 50 37 42 42 --- 45
R05 | 911 42 37 28 28 26 50 21 --- 13 | 56 53 38 50 35 29 29 --- 31
R06 | 823 12 24 20 23 14 22 20 --- 9 | 51 70 34 51 53 52 46 --- 45
R07 | 848 54 54 26 11 22 24 21 82 11 | 71 71 48 40 25 38 22 70 33
R08 | 737 52 52 24 21 28 43 14 --- 12 | 72 77 51 55 26 16 35 --- 39
R09 | 2139 19 48 19 17 13 28 20 --- 8 | 13 34 29 32 30 31 44 --- 21
R10 | 1356 27 20 26 20 19 28 12 --- 9 | 56 56 41 49 38 37 43 --- 40
R11 | 645 95 97 38 21 27 44 26 --- 17 | 64 68 40 48 56 60 43 --- 40
R13 | 1003 27 42 20 14 24 24 19 --- 9 | 35 49 28 32 31 23 23 --- 21
R14 | 1329 24 35 37 25 23 39 29 --- 13 | 37 46 49 61 45 36 60 --- 47
R15 |13805 36 45 31 16 22 21 11 --- 9 | 47 60 33 34 38 33 26 --- 26
XR17 | ---- 10 23 --- --- --- --- --- --- 0 | 38 63 --- --- --- --- --- --- 41
R18 | 556 25 28 16 13 26 18 18 --- 8 | 38 41 39 40 39 30 37 --- 34
R19 | 893 38 44 20 20 24 47 18 --- 11 | 50 53 41 44 35 32 19 --- 30
R20 | 655 51 74 36 22 26 50 25 --- 14 | 48 70 43 30 29 37 14 --- 19
R21 | 1158 46 43 24 24 18 39 26 134 12 | 74 71 66 74 67 50 54 27 61
R22 | 668 50 51 25 21 21 28 19 --- 11 | 53 52 28 45 36 24 33 --- 33
R23 | 1074 15 16 13 20 17 25 12 --- 7 | 22 31 26 30 22 17 18 --- 20
R24 | 1779 40 39 40 31 35 61 28 --- 16 | 57 55 56 48 21 26 20 --- 28
XR26 | ---- 126 2882 --- --- --- --- 33 --- 65 | 92 9999 --- --- --- --- 51 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 3208 44 49 28 20 25 38 19 100 |T 54 59 41 44 36 34 34 51 33
WRMS | 3208 39 43 30 20 23 39 19 100 |NE 54 59 41 44 36 34 34 51 33
MEDI | 1003 38 44 25 20 23 32 19 82 |MD 56 60 40 45 35 33 35 56 33
Table 3.1885.5 GPS week: 1885 Day: 5 MJD: 57444
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 | 1460 54 75 20 14 34 31 13 --- 11 | 40 62 30 32 39 24 24 --- 24
R02 | 590 38 38 16 20 41 130 12 --- 19 | 48 50 28 35 27 121 33 --- 34
R03 | 1146 53 59 28 19 31 42 12 137 12 | 62 72 37 35 41 30 31 56 32
R04 | 541 44 39 16 8 24 35 11 --- 9 | 61 59 44 45 35 41 38 --- 39
R05 | 1022 33 38 14 26 33 58 20 --- 12 | 37 51 41 43 40 48 29 --- 34
R06 | 1023 16 17 21 21 13 23 14 --- 8 | 44 53 43 59 40 48 38 --- 45
R07 | 997 58 60 22 12 19 24 22 78 10 | 63 67 39 32 26 30 17 92 26
R08 | 689 60 59 16 17 21 30 16 --- 10 | 61 63 37 34 25 27 21 --- 27
R09 | 2348 18 19 16 15 11 15 14 --- 6 | 19 21 39 35 34 30 45 --- 26
R10 | 689 37 44 15 18 18 23 11 --- 8 | 56 71 42 47 36 30 37 --- 39
R11 | 1353 110 114 43 20 40 45 22 --- 18 | 76 86 34 56 68 49 46 --- 40
R13 | 1017 27 19 16 24 19 21 20 --- 9 | 39 36 28 35 32 29 22 --- 25
R14 | 884 24 29 29 23 19 42 30 --- 12 | 47 70 59 60 52 47 60 --- 53
R15 |10552 36 38 19 18 39 36 15 --- 11 | 54 53 37 39 43 18 28 --- 29
XR17 | ---- 6 34 --- --- --- --- --- --- 0 | 37 44 --- --- --- --- --- --- 42
R18 | 710 26 30 28 16 26 36 30 --- 11 | 65 65 78 65 66 48 44 --- 57
R19 | 929 22 27 12 14 26 32 20 --- 9 | 44 47 40 39 33 30 45 --- 37
R20 | 748 44 20 27 25 28 44 33 --- 14 | 48 25 41 44 38 31 21 --- 30
R21 | 984 40 50 29 15 35 29 17 62 11 | 52 60 58 42 38 38 43 62 42
R22 | 573 41 45 25 15 25 18 18 --- 10 | 47 47 41 35 31 34 30 --- 33
R23 | 940 15 20 18 20 27 23 9 --- 8 | 21 23 32 31 28 26 20 --- 23
R24 | 2086 39 43 39 16 43 50 15 --- 14 | 52 53 57 35 23 19 30 --- 33
XR26 | ---- 75 690 --- --- --- --- 15 --- 36 | 56 684 --- --- --- --- 34 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 2555 45 47 24 18 29 44 19 98 |T 49 80 42 41 37 38 33 70 34
WRMS | 2555 38 41 26 18 29 33 19 98 |NE 49 80 42 41 37 38 33 70 34
MEDI | 984 38 38 20 18 26 32 15 78 |MD 48 53 40 39 36 30 31 62 33
Table 3.1885.6 GPS week: 1885 Day: 6 MJD: 57445
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 | 1030 52 15 24 17 23 24 16 --- 10 | 80 74 35 48 32 22 25 --- 32
R02 | 708 40 39 19 19 27 26 15 --- 10 | 70 73 50 55 29 60 39 --- 42
R03 | 666 61 62 39 15 32 27 17 166 13 | 91 89 56 52 35 31 38 48 43
R04 | 506 43 47 22 16 18 26 13 --- 9 | 88 90 53 60 41 37 48 --- 51
R05 | 785 30 23 28 19 16 67 15 --- 12 | 69 70 40 57 42 37 42 --- 43
R06 | 818 18 31 26 23 15 17 10 --- 8 | 58 55 55 76 50 57 61 --- 61
R07 | 964 53 50 28 15 29 37 12 152 11 | 87 88 65 52 31 32 32 125 42
R08 | 714 59 62 24 20 11 19 22 --- 11 | 91 96 57 58 38 36 35 --- 45
R09 | 1905 19 25 16 15 14 15 14 --- 6 | 21 20 31 30 30 18 62 --- 20
R10 | 591 33 23 27 13 14 35 9 --- 8 | 60 57 35 54 44 45 45 --- 44
R11 | 1201 121 117 45 20 34 32 26 --- 19 | 83 82 38 57 78 65 62 --- 49
R13 | 528 28 30 16 16 18 20 10 --- 7 | 45 47 28 32 27 22 21 --- 23
R14 | 827 32 31 45 30 25 38 31 --- 14 | 59 68 84 88 70 48 77 --- 72
R15 | 8068 33 43 20 17 52 33 14 --- 12 | 51 62 34 39 53 26 31 --- 31
XR17 | 3086 37 45 --- --- 16 --- --- --- 24 | 40 58 --- --- 7 --- --- --- 52
R18 | 502 28 21 23 19 19 29 16 --- 9 | 53 57 62 53 53 48 43 --- 49
R19 | 1524 27 25 15 16 9 54 12 --- 9 | 58 56 41 48 38 21 32 --- 36
R20 | 680 31 44 63 23 20 75 24 --- 17 | 51 56 43 40 42 28 27 --- 32
R21 | 878 36 30 24 19 22 19 11 76 9 | 71 71 59 71 57 56 53 48 58
R22 | 733 44 41 31 22 29 31 16 --- 11 | 69 70 63 49 24 29 30 --- 39
R23 | 1039 13 18 21 26 17 21 11 --- 8 | 24 24 23 36 20 34 16 --- 20
R24 | 945 42 53 52 12 26 47 17 --- 13 | 53 59 48 42 30 31 22 --- 30
XR26 | ---- 73 258 --- --- --- --- 16 --- 35 | 76 511 --- --- --- --- 30 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1985 46 45 31 19 24 36 17 137 |T 62 84 47 52 39 37 39 73 41
WRMS | 1985 47 48 32 18 20 39 17 137 |NE 62 84 47 52 39 37 39 73 41
MEDI | 818 36 39 24 19 19 29 15 152 |MD 60 68 48 52 38 34 35 48 42
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