[IGSREPORT-24266] Wk 1882 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Feb 25 20:49:13 PST 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1882 (Jan 31, 2016 - Feb 06, 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 2.1882.
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:
igl1882[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1882 in the SP3 format.
igl18827.sum Combination Report for GPS Week 1882.
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 | 4.3 ns
1 | -10.4 ns
2 | -15.4 ns
3 | 1.5 ns
4 | -2.2 ns
5 | -12.4 ns
6 | 2.7 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 | GRG | R17
1 | ESX | R17
1 | GRG | R17
2 | ESX | R17
2 | GRG | R17
4 | ESX | R17
4 | GRG | R17
5 | ESX | R17
5 | GRG | R17
6 | ESX | R17
6 | GRG | R17
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 1.1882, 1a.1882).
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 2.1882.0-6)
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 3.1882.0-6).
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 1882 summary. (Jan 31, 2016 - Feb 06, 2016)
Table 1.1882.a GPS week : 1882 MJD: 57418.0-57424.0
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 1 -9 18 -18 -46 .34 37 31 | --- --- --- ---
| 1 1 4 29 30 63 .06 | --- ---
cof n/a| -1 0 -10 10 -20 -32 .33 42 33 | --- --- --- ---
| 2 2 4 35 28 70 .06 | --- ---
emx n/a| 0 0 -4 -14 -14 -49 .26 29 29 | 0 -703 3898 7104
| 1 1 2 29 43 44 .03 | 0 1233
esx n/a| 0 0 5 -29 -32 18 -.11 20 19 | -2766 -2427 3939 7767
| 1 1 1 15 22 13 .04 | 14760 3585
gfz n/a| 0 0 -1 43 51 50 .05 23 18 | -61013 -853 4672 290970
| 0 1 1 18 26 29 .07 | 147109 2762
grg n/a| -3 2 6 -28 -8 -31 -.35 37 33 | -678091 56347 99569 818506
| 2 1 3 28 36 73 .05 | 169336 152002
iac n/a| 1 0 0 5 15 -7 -.09 20 20 | -83250 -233 4157 291060
| 1 0 1 38 56 34 .03 | 135488 1288
mcc n/a| -2 -1 -25 38 87 -99 -.17 168 168 | --- --- --- ---
| 10 5 23 102 72 651 .24 | --- ---
Table 1.1882.b GPS week : 1882 MJD: 57418.0-57424.0
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 | 10 10 8 9 9 11 11 |
R02 | 10 7 8 8 10 8 9 |
R03 | 10 9 8 9 7 8 8 |
R04 | 8 8 9 7 9 8 7 |
R05 | 15 15 12 15 15 15 16 |
R06 | 8 10 6 8 7 9 8 |
R07 | 8 7 7 9 8 9 9 |
R08 | 8 8 9 9 8 9 12 |
R09 | 13 13 17 12 14 14 12 |
R10 | 13 10 10 9 9 10 12 |
R11 | 14 11 12 14 15 17 19 |
R12 | 16 13 14 20 15 19 18 |
R13 | 10 8 8 11 9 10 9 |
R14 | 14 20 15 15 24 15 23 |
R15 | 13 11 12 12 10 14 13 |
R16 | 14 10 10 10 11 10 10 |
R17 | 60 15 18 84 12 11 12 |
R18 | 9 10 9 13 11 9 11 |
R19 | 12 11 9 11 11 11 11 |
R20 | 13 13 14 17 16 12 13 |
R21 | 11 12 11 12 11 11 12 |
R22 | 13 12 12 12 12 12 14 |
R23 | 10 9 9 9 11 10 10 |
R24 | 15 13 14 13 11 14 14 |
R26 | 0 0 0 966 93 89 34 |
Table 1.1882.c GPS week : 1882 MJD: 57418.0-57424.0
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 1882 0 | -72 16 54 -2192 1511 -1740 84.2 1159 1159 | 4307 0
brd 1882 1 | -33 -37 24 40 411 -4757 83.4 1214 1214 | -10448 0
brd 1882 2 | -1 -100 62 -270 -1025 -4780 83.6 1268 1268 | -15409 0
brd 1882 3 | -12 66 180 -469 -145 -2070 82.5 1263 1263 | 1461 0
brd 1882 4 | 58 -43 169 188 456 -559 84.1 1910 1910 | -2245 0
brd 1882 5 | 65 -2 143 -210 208 1431 83.9 1535 1535 | -12432 0
brd 1882 6 | -56 6 112 239 803 2054 85.6 1605 1605 | 2673 0
-------------+------------------------------------------------------------+----------------
brd 1882 mean| -7 -13 106 -382 317 -1488 83.9 1422 1422 | -4584 0
brd 1882 sdev| 53 53 60 838 787 2703 .9 272 272 | 8029 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 2.1882.0 GPS week: 1882 Day: 0 MJD: 57418
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 -2 23 -49 49 .32 34 27 | --- --- --- ---
cof n/a| -5 1 -1 -3 -52 84 .32 42 31 | --- --- --- ---
emx n/a| 2 -3 -3 -23 -14 -102 .24 30 30 | 0 1668 4140 5975
esx n/a| 0 1 4 -24 -44 22 -.14 20 17 | 417 4312 4148 6663
gfz n/a| -1 -2 -1 41 10 51 .18 24 26 | -273578 4705 7690 999999
grg n/a| -1 4 5 -72 34 -80 -.36 37 34 | -822425 4511 13826 999999
iac n/a| 2 0 0 40 56 -47 -.14 20 20 | -275211 1769 5278 999999
mcc n/a| 0 -9 -17 72 153 245 .04 114 114 | --- --- --- ---
Table 2.1882.1 GPS week: 1882 Day: 1 MJD: 57419
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 -8 55 -9 -50 .45 32 30 | --- --- --- ---
cof n/a| -4 0 -10 89 -1 -39 .42 45 32 | --- --- --- ---
emx n/a| -1 0 -6 5 -28 -61 .26 25 25 | 0 -278 4316 6343
esx n/a| 0 1 5 -2 -20 30 -.05 19 17 | -21496 -2346 4374 7453
gfz n/a| 0 -1 -3 75 63 20 -.01 28 16 | -278538 -1559 6470 999999
grg n/a| -4 1 9 -3 -23 -18 -.34 34 32 | -828475 -1574 9153 999999
iac n/a| 2 0 0 -49 6 33 -.11 18 18 | -287386 -1788 4856 999999
mcc n/a| 7 1 2 -79 88 164 -.17 122 122 | --- --- --- ---
Table 2.1882.2 GPS week: 1882 Day: 2 MJD: 57420
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 36 16 15 .37 35 31 | --- --- --- ---
cof n/a| 0 -2 -10 -3 4 48 .32 38 31 | --- --- --- ---
emx n/a| -1 -1 -2 -4 -43 14 .30 23 23 | 0 -665 3371 7747
esx n/a| 0 0 5 -35 1 6 -.11 21 21 | -21928 -775 3387 7686
gfz n/a| 0 0 -2 30 47 39 -.02 22 19 | 10366 -364 3348 7445
grg n/a| -2 4 9 0 -24 98 -.40 38 32 | -917239 401002 653824 999999
iac n/a| 1 1 0 12 17 -30 -.08 17 17 | -14135 -737 3391 7616
mcc n/a| 10 0 -34 -83 145 -184 -.20 294 294 | --- --- --- ---
Table 2.1882.3 GPS week: 1882 Day: 3 MJD: 57421
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 -7 19 -65 -26 .37 37 29 | --- --- --- ---
cof n/a| 0 0 -11 -9 -45 -65 .23 42 32 | --- --- --- ---
emx n/a| -1 1 -4 -77 30 -94 .27 32 32 | 0 -1140 3585 7503
esx n/a| 2 -1 1 -46 -25 3 -.14 21 19 | 3980 -3789 3610 7623
gfz n/a| 0 0 -2 33 88 12 .09 23 17 | 31819 -2585 3528 6821
grg n/a| -3 1 8 -57 -33 0 -.27 36 35 | -537046 -1885 3603 682233
iac n/a| 0 0 0 63 -35 31 -.07 20 20 | 2358 -374 3599 7025
mcc n/a| -3 7 -21 68 -28 -713 -.64 188 188 | --- --- --- ---
Table 2.1882.4 GPS week: 1882 Day: 4 MJD: 57422
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 1 -6 20 -15 -117 .33 41 35 | --- --- --- ---
cof n/a| -3 -3 -10 8 -12 -74 .31 40 35 | --- --- --- ---
emx n/a| 2 0 -8 -1 58 -68 .26 31 30 | 0 -1945 4116 7050
esx n/a| 0 0 4 -42 -44 33 -.13 18 18 | 7467 -4410 4117 7143
gfz n/a| -1 1 0 37 64 83 .05 19 13 | 29918 -1293 3983 7178
grg n/a| 0 1 7 -2 54 -104 -.38 46 35 | -543479 -2193 8641 682504
iac n/a| 1 0 1 -20 -66 -47 -.07 20 20 | -849 480 4064 7013
mcc n/a| -2 -2 -15 53 14 -619 -.21 110 110 | --- --- --- ---
Table 2.1882.5 GPS week: 1882 Day: 5 MJD: 57423
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 -15 15 16 -112 .29 40 32 | --- --- --- ---
cof n/a| 0 0 -15 -9 15 -103 .34 46 36 | --- --- --- ---
emx n/a| 0 0 -2 9 -54 -10 .28 29 31 | 0 -1962 4352 8126
esx n/a| 0 0 6 -17 -27 4 -.12 20 18 | -5558 -7232 4437 9694
gfz n/a| 0 0 1 23 62 91 .01 21 16 | 20853 -4161 4226 8398
grg n/a| -5 0 1 -34 -27 -107 -.36 35 33 | -554502 -4397 4422 682885
iac n/a| 0 1 2 -14 21 14 -.06 24 24 | -10520 -1637 4417 8817
mcc n/a| -6 0 -19 217 156 -665 -.13 126 126 | --- --- --- ---
Table 2.1882.6 GPS week: 1882 Day: 6 MJD: 57424
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 3 -14 -40 -22 -84 .30 42 33 | --- --- --- ---
cof n/a| 1 2 -14 1 -53 -73 .34 44 34 | --- --- --- ---
emx n/a| 2 0 -5 -12 -51 -24 .23 31 30 | 0 -601 3407 6988
esx n/a| 1 0 8 -35 -68 31 -.04 23 20 | 17754 -2749 3502 8110
gfz n/a| 1 -3 0 59 25 52 .08 27 17 | 32064 -720 3459 6952
grg n/a| -6 1 3 -28 -37 -9 -.31 36 33 | -543476 -1029 3520 681927
iac n/a| 0 0 -1 7 106 -4 -.08 20 20 | 2989 654 3496 6956
mcc n/a| -21 -6 -72 17 80 1076 .09 224 224 | --- --- --- ---
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 3.1882.0 GPS week: 1882 Day: 0 MJD: 57418
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 | 1523 22 32 31 20 20 32 16 --- 10 | 65 80 60 68 67 59 51 --- 58
R02 | 1316 12 17 29 12 11 55 11 158 10 | 49 53 62 36 41 26 41 57 39
R03 | 836 11 20 15 29 13 32 18 --- 9 | 63 69 61 77 59 39 52 --- 59
R04 | 1195 8 14 15 10 14 34 18 --- 7 | 66 71 70 70 67 83 56 --- 65
R05 | 515 34 38 37 21 25 65 25 --- 14 | 50 69 64 59 65 48 41 --- 49
R06 | 856 11 14 12 14 10 40 11 --- 7 | 48 51 47 56 49 71 48 --- 49
R07 | 1018 20 23 26 12 13 26 17 140 8 | 70 68 78 60 60 59 62 122 62
R08 | 937 18 23 21 13 13 34 16 --- 8 | 72 73 64 63 64 49 52 --- 58
R09E | 1897 26 23 29 24 27 36 30 --- 12 | 56 56 37 56 45 41 37 --- 41
XR10E |>>>>> 27 81 --- 24 22 36 23 --- 12 | 36 74 --- 39 37 43 36 --- 33
R11E | 2103 39 58 39 26 30 45 23 --- 14 | 58 77 47 56 61 57 48 --- 47
R12E | 985 52 47 42 25 35 38 30 71 16 | 69 73 54 61 70 64 56 73 54
R13E | 752 40 37 22 15 18 33 17 --- 10 | 55 53 43 39 39 40 45 --- 37
R14E | 1135 48 45 38 20 34 30 27 --- 14 | 92 101 90 95 88 86 81 --- 85
R15E | 1823 30 39 31 17 48 25 16 --- 13 | 35 44 33 27 48 32 26 --- 24
R16E | 1599 37 93 26 28 27 28 35 --- 13 | 55 111 30 52 44 32 32 --- 34
XR17E | 2496 96 95 --- 133 77 257 94 --- 60 | 40 42 --- 144 76 109 40 --- 67
R18 | 625 33 34 8 16 19 32 15 59 9 | 70 68 40 53 28 30 37 39 40
R19 | 778 50 54 21 15 24 37 12 --- 11 | 81 89 48 53 35 30 39 --- 43
R20 | 973 37 58 43 11 26 42 14 --- 12 | 67 77 44 44 39 33 37 --- 37
R21 | 505 47 55 23 17 21 28 14 109 11 | 77 81 41 51 32 43 39 57 42
R22 | 536 58 59 23 17 26 38 14 --- 12 | 87 89 48 55 33 35 37 --- 44
R23 | 845 24 27 30 26 11 18 14 --- 9 | 40 40 41 73 49 47 57 --- 52
R24 | 729 28 25 56 33 21 39 19 --- 14 | 72 75 67 92 71 45 58 --- 66
XR26 | ---- --- --- --- --- --- --- --- --- 0 | 35 712 --- --- --- --- 9999 --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1159 34 42 30 20 24 37 20 114 |T 60 95 53 61 52 50 46 69 49
WRMS | 1159 27 31 30 17 26 34 20 114 |NE 63 110 55 60 50 46 47 68 50
MEDI | 973 30 37 26 17 21 34 17 109 |MD 63 73 48 56 49 43 41 57 47
Table 3.1882.1 GPS week: 1882 Day: 1 MJD: 57419
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 | 1880 30 26 25 20 18 34 11 --- 9 | 56 54 52 46 50 44 43 --- 44
R02 | 960 15 19 22 17 14 20 8 174 7 | 38 41 41 31 26 37 39 81 32
R03 | 581 14 21 18 19 13 45 10 --- 9 | 42 53 43 40 45 36 35 --- 36
R04 | 1084 12 17 12 17 11 17 21 --- 7 | 49 49 51 59 52 38 35 --- 46
R05 | 812 33 30 25 31 33 49 30 --- 14 | 33 44 37 67 72 58 33 --- 46
R06 | 1102 11 14 16 17 18 51 16 --- 10 | 39 42 39 37 36 49 37 --- 35
R07 | 795 12 17 20 11 8 26 10 160 6 | 54 63 63 53 53 46 55 257 54
R08 | 618 24 26 18 14 9 20 18 --- 7 | 55 59 51 48 42 38 34 --- 42
R09E | 1308 30 69 25 25 30 27 29 --- 12 | 51 92 32 52 46 46 38 --- 36
XR10E |66725 28 69 --- 16 16 22 15 --- 9 | 42 82 --- 42 40 36 30 --- 33
R11E | 1037 35 39 25 13 28 31 15 --- 10 | 56 65 40 51 62 54 43 --- 46
R12E | 886 50 23 37 15 25 34 21 65 13 | 62 59 64 51 62 58 57 76 51
R13E | 1625 27 60 18 14 21 29 8 --- 8 | 44 72 33 34 38 45 29 --- 31
R14E | 2081 31 117 41 25 81 37 34 --- 20 | 65 133 68 69 106 74 57 --- 66
R15E | 2487 20 17 21 14 38 32 19 --- 10 | 33 41 31 36 61 32 28 --- 30
R16E | 1555 25 52 34 19 16 25 16 --- 10 | 44 72 34 34 38 33 26 --- 30
XR17E | 3972 30 34 --- 252 21 251 15 --- 15 | 36 34 --- 118 56 99 35 --- 52
R18 | 966 34 37 23 18 15 33 14 70 9 | 46 45 36 38 32 22 27 43 30
R19 | 639 44 53 15 20 19 37 16 --- 10 | 57 64 39 45 31 28 23 --- 34
R20 | 1110 47 38 24 22 31 44 14 --- 13 | 52 44 39 37 40 36 31 --- 32
R21 | 593 52 54 20 14 26 36 21 95 12 | 61 62 37 40 32 35 30 61 34
R22 | 512 56 62 23 12 28 32 14 --- 12 | 56 59 34 32 29 32 29 --- 30
R23 | 534 22 25 21 22 15 25 11 --- 8 | 35 39 33 50 35 50 41 --- 38
R24 | 964 26 29 42 21 19 43 20 --- 12 | 72 70 66 75 65 56 51 --- 60
XR26 | ---- --- --- --- --- --- --- --- --- 0 | 83 9999 --- --- --- --- 9999 --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1214 32 45 25 19 28 34 18 122 |T 50 59 43 49 47 45 36 103 40
WRMS | 1214 30 32 25 17 16 32 18 122 |NE 51 52 44 46 42 40 36 110 39
MEDI | 966 28 30 22 17 19 32 15 95 |MD 51 59 39 45 42 38 35 76 36
Table 3.1882.2 GPS week: 1882 Day: 2 MJD: 57420
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 | 954 20 20 20 22 11 17 15 --- 8 | 55 52 34 64 52 49 45 --- 48
R02 | 501 16 18 23 14 14 22 12 115 7 | 45 47 48 30 36 30 35 88 35
R03 | 1187 11 12 21 14 8 25 17 --- 7 | 51 50 60 48 53 38 42 --- 47
R04 | 1188 18 22 19 16 14 40 11 --- 8 | 51 51 50 42 47 27 41 --- 41
R05 | 1064 25 25 19 30 24 39 21 --- 11 | 35 33 28 42 48 42 19 --- 30
R06 | 1824 9 13 12 8 14 14 16 --- 5 | 38 43 43 40 48 39 38 --- 40
R07 | 1540 17 16 15 17 11 26 13 602 7 | 53 52 52 41 57 50 53 327 50
R08 | 622 27 25 22 16 13 25 16 --- 8 | 52 51 46 45 35 29 30 --- 37
R09E | 1034 32 52 21 27 20 102 18 --- 16 | 48 70 35 36 32 90 35 --- 33
XR10E | 5386 35 61 --- 16 15 27 13 --- 9 | 45 68 --- 35 34 39 34 --- 32
R11E | 1510 42 22 22 15 32 39 21 --- 12 | 54 53 55 58 64 48 45 --- 49
R12E | 899 63 33 35 26 24 34 16 119 14 | 73 61 56 62 67 54 52 77 54
R13E | 1084 28 30 17 10 21 27 12 --- 8 | 46 50 47 38 41 47 32 --- 36
R14E | 2206 40 75 40 22 32 44 28 --- 15 | 56 93 61 57 61 65 47 --- 49
R15E | 2557 34 55 27 17 37 26 22 --- 12 | 31 53 36 31 56 29 24 --- 26
R16E | 524 35 42 27 20 15 37 12 --- 10 | 37 53 28 35 26 37 26 --- 25
XR17E | 4963 20 31 --- 210 28 261 23 --- 17 | 33 37 --- 161 45 85 34 --- 47
R18 | 1381 38 43 9 15 22 36 10 146 9 | 52 54 32 36 24 31 35 55 31
R19 | 1092 39 40 20 14 19 27 13 --- 9 | 63 65 54 45 34 27 34 --- 39
R20 | 1095 50 48 21 33 28 48 19 --- 14 | 52 58 34 42 33 28 26 --- 27
R21 | 647 51 43 17 13 27 28 17 143 11 | 69 60 43 39 31 32 30 82 34
R22 | 641 60 55 22 14 20 35 16 --- 11 | 70 66 41 38 31 24 28 --- 33
R23 | 1098 22 21 24 15 15 31 12 --- 8 | 35 38 44 46 43 47 45 --- 41
R24 | 907 30 41 32 44 25 30 22 --- 14 | 59 74 64 72 46 49 43 --- 49
XR26 | ---- >>>> >>>> --- --- --- --- 2 --- 0 | 50 445 --- --- --- --- 9999 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1268 35 38 23 21 22 38 17 294 |T 50 71 45 49 43 43 36 125 38
WRMS | 1268 31 31 23 21 19 32 17 294 |NE 51 77 44 44 41 36 36 138 38
MEDI | 1092 32 33 21 16 20 30 16 143 |MD 51 53 44 42 43 39 35 82 37
Table 3.1882.3 GPS week: 1882 Day: 3 MJD: 57421
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 | 1024 25 24 15 16 13 31 21 --- 9 | 59 55 51 51 52 34 38 --- 44
R02 | 753 17 25 27 13 9 26 18 82 8 | 54 57 57 56 54 31 37 50 46
R03 | 984 15 20 30 9 22 24 20 --- 9 | 56 64 67 52 48 50 51 --- 51
R04 | 687 14 17 20 11 11 28 12 --- 7 | 56 57 58 52 54 49 52 --- 51
R05 | 800 29 18 36 19 27 69 21 --- 14 | 43 49 44 59 58 41 39 --- 44
R06 | 1232 13 16 22 15 9 20 24 --- 8 | 50 50 63 58 48 60 36 --- 49
R07 | 711 20 23 19 10 13 31 23 346 8 | 61 65 57 54 49 79 42 101 52
R08 | 747 32 31 26 15 10 17 17 --- 8 | 60 58 57 42 40 35 34 --- 40
R09E | 1505 32 38 30 28 29 29 19 --- 12 | 40 55 47 59 38 53 36 --- 38
XR10E | 7929 28 37 --- 14 14 21 16 --- 9 | 40 44 --- 41 42 35 33 --- 35
R11E | 2217 53 54 44 20 26 42 16 --- 14 | 64 68 43 57 51 53 49 --- 46
R12E | 1592 62 47 49 35 41 44 41 133 19 | 80 80 79 94 86 65 83 71 73
R13E | 777 28 42 45 17 17 25 13 --- 10 | 47 60 54 46 48 49 42 --- 42
R14E | 1802 41 60 34 26 42 35 27 --- 15 | 47 81 61 71 86 52 57 --- 59
R15E | 3005 43 54 26 17 41 17 12 --- 12 | 39 67 31 31 43 29 30 --- 26
R16E | 1018 42 42 27 21 14 22 16 --- 10 | 45 50 39 48 31 41 33 --- 35
XR17E | 5825 143 144 --- 145 --- 149 143 --- 83 | 28 40 --- 162 --- 117 37 --- 123
R18 | 1063 45 43 43 13 23 42 8 128 12 | 65 62 52 41 30 29 38 36 37
R19 | 1245 40 46 28 14 19 46 12 --- 11 | 71 74 58 55 40 38 45 --- 46
R20 | 786 45 84 43 40 25 50 28 --- 16 | 78 113 66 74 57 51 44 --- 54
R21 | 570 36 53 24 29 17 37 20 125 11 | 68 87 49 70 46 47 44 58 51
R22 | 523 52 55 18 18 23 39 19 --- 12 | 74 76 50 54 40 48 39 --- 45
R23 | 982 26 32 23 20 10 28 14 --- 8 | 41 45 50 62 49 50 53 --- 51
R24 | 524 40 22 50 11 22 44 14 --- 13 | 76 61 82 46 47 43 47 --- 49
XR26 | ---- 1499 1561 --- --- --- --- 622 --- 965 | 53 310 --- --- --- --- 9999 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1262 37 42 32 21 23 36 20 188 |T 55 73 55 59 49 49 43 63 49
WRMS | 1262 29 32 32 19 17 35 20 188 |NE 60 80 57 55 47 45 42 61 47
MEDI | 984 36 42 27 17 19 31 19 128 |MD 56 61 54 54 48 48 39 58 46
Table 3.1882.4 GPS week: 1882 Day: 4 MJD: 57422
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 | 2117 23 32 28 18 10 34 15 --- 9 | 55 69 65 60 53 41 46 --- 52
R02 | 556 32 34 33 10 11 37 21 59 10 | 51 55 52 33 36 25 33 52 33
R03 | 711 21 21 13 14 11 20 12 --- 6 | 60 65 61 61 52 43 51 --- 54
R04 | 728 18 17 34 8 17 20 17 --- 8 | 58 64 70 58 53 56 41 --- 53
R05 | 667 49 52 31 24 15 71 25 --- 14 | 49 58 29 57 52 47 44 --- 43
R06 | 2090 10 14 15 12 7 38 13 --- 7 | 45 49 45 51 43 45 48 --- 45
R07 | 1221 15 20 24 11 8 34 17 135 7 | 61 66 71 60 58 41 58 107 58
R08 | 886 16 18 24 17 14 14 17 --- 7 | 56 65 62 59 67 61 52 --- 58
R09E | 3657 46 55 47 25 26 26 28 --- 14 | 45 68 54 59 54 49 41 --- 46
R10E | 6224 33 28 25 19 11 24 20 --- 9 | 47 50 29 47 44 41 40 --- 41
R11E | 1427 65 53 36 17 25 50 27 --- 14 | 69 69 43 52 65 59 37 --- 46
R12E | 1972 50 49 39 23 29 37 37 104 15 | 70 75 67 77 85 68 60 45 67
R13E | 1171 39 35 26 14 15 24 17 --- 9 | 52 48 50 41 50 38 34 --- 40
R14E | 1191 56 46 63 22 29 133 30 --- 23 | 50 43 45 58 66 125 44 --- 52
R15E | 2154 31 32 24 18 28 23 17 --- 10 | 41 49 35 37 46 29 37 --- 33
R16E | 698 52 55 24 17 19 19 20 --- 10 | 48 64 43 42 40 35 38 --- 37
XR17E | 4731 21 20 --- 309 --- 295 6 --- 12 | 31 32 --- 173 --- 130 39 --- 43
R18 | 918 41 41 26 18 23 31 12 119 10 | 57 56 40 44 32 27 35 51 36
R19 | 1373 52 50 18 14 19 40 14 --- 10 | 65 63 37 39 31 34 35 --- 34
R20 | 599 58 59 36 22 24 72 17 --- 15 | 74 75 43 49 39 47 40 --- 40
R21 | 493 40 43 17 18 18 38 22 118 10 | 75 76 44 65 52 44 55 50 54
R22 | 480 52 48 24 20 23 31 19 --- 11 | 76 72 60 63 43 38 44 --- 50
R23 | 947 36 37 25 23 14 33 19 --- 10 | 40 39 38 51 35 30 44 --- 38
R24 | 755 31 36 31 16 18 41 14 --- 10 | 52 55 37 52 53 28 39 --- 41
XR26 | ---- 153 184 --- --- --- --- 54 --- 92 | 103 211 --- --- --- --- 9999 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1910 41 40 31 18 19 46 20 110 |T 57 65 48 57 49 49 43 61 45
WRMS | 1910 35 35 30 18 13 35 20 110 |NE 61 71 50 53 46 40 44 65 45
MEDI | 947 39 37 26 18 18 34 17 118 |MD 55 64 45 52 52 41 41 51 43
Table 3.1882.5 GPS week: 1882 Day: 5 MJD: 57423
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 | 2139 31 34 32 22 11 29 25 --- 11 | 46 50 41 46 34 35 29 --- 32
R02 | 530 21 26 21 15 13 30 16 113 8 | 39 43 32 38 35 22 27 114 29
R03 | 857 20 20 18 16 12 23 15 --- 7 | 47 49 44 49 36 31 40 --- 40
R04 | 595 20 25 17 9 10 24 21 --- 7 | 48 52 47 38 38 48 39 --- 39
R05 | 670 41 55 24 28 17 62 34 --- 15 | 45 57 31 54 51 48 28 --- 38
R06 | 2058 15 16 29 16 10 22 26 --- 9 | 31 34 30 33 36 30 31 --- 29
R07 | 889 13 17 27 15 10 39 15 69 9 | 41 45 45 39 39 45 41 121 39
R08 | 1147 14 14 16 20 12 29 21 --- 8 | 41 40 44 46 40 28 31 --- 37
R09E | 2124 46 52 42 23 26 31 27 --- 14 | 40 60 33 40 28 42 36 --- 27
R10E | 1363 46 61 21 16 16 23 17 --- 10 | 38 55 21 37 35 34 35 --- 31
R11E | 2407 69 67 46 13 26 43 39 --- 17 | 75 75 33 49 55 54 36 --- 41
R12E | 3041 63 51 50 26 24 51 52 175 19 | 91 94 90 75 78 77 79 49 75
R13E | 1531 34 46 22 18 18 29 15 --- 9 | 51 61 35 38 39 33 33 --- 33
R14E | 1397 43 52 34 27 30 36 37 --- 15 | 67 83 59 84 91 89 54 --- 70
R15E | 2759 35 46 41 21 39 22 15 --- 13 | 39 39 37 32 39 31 28 --- 28
R16E | 1374 34 33 31 18 16 21 21 --- 10 | 42 50 40 42 37 31 31 --- 33
XR17E | 4633 22 29 --- 318 11 276 14 --- 10 | 21 26 --- 160 38 119 33 --- 28
R18 | 688 42 44 19 13 17 28 9 92 9 | 53 54 34 38 27 28 34 62 32
R19 | 1443 52 62 15 15 26 33 11 --- 11 | 57 64 35 36 27 25 28 --- 28
R20 | 785 47 56 22 22 16 42 23 --- 12 | 61 68 51 54 46 24 36 --- 41
R21 | 441 45 56 19 18 26 38 11 152 11 | 57 68 43 46 38 33 38 45 38
R22 | 755 54 57 21 16 22 41 19 --- 12 | 68 71 50 50 39 32 36 --- 41
R23 | 950 27 30 25 21 14 24 23 --- 9 | 34 36 39 51 40 40 38 --- 38
R24 | 1186 49 59 30 31 29 44 13 --- 14 | 66 74 53 51 30 28 40 --- 37
XR26 | ---- 131 189 --- --- --- --- 60 --- 89 | 71 241 --- --- --- --- 9999 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1535 40 46 29 20 20 35 24 126 |T 50 63 42 51 41 41 36 78 37
WRMS | 1535 32 36 31 18 16 33 24 126 |NE 50 65 41 44 37 33 34 85 35
MEDI | 1186 41 46 24 18 16 30 21 113 |MD 47 55 40 46 38 33 35 62 37
Table 3.1882.6 GPS week: 1882 Day: 6 MJD: 57424
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 | 1863 32 43 23 23 22 24 24 --- 10 | 68 79 59 63 63 45 49 --- 54
R02 | 697 22 23 30 11 13 11 23 271 8 | 62 65 64 46 50 38 44 128 47
R03 | 989 19 25 21 13 13 22 22 --- 8 | 72 78 83 71 67 50 60 --- 66
R04 | 606 24 18 14 12 18 22 8 --- 7 | 73 72 71 68 57 67 61 --- 63
R05 | 767 44 55 30 37 32 57 24 --- 16 | 62 70 44 62 48 47 43 --- 46
R06 | 2399 15 17 27 12 18 24 12 --- 8 | 58 57 61 55 52 52 43 --- 50
R07 | 839 22 21 32 16 11 21 18 103 9 | 69 71 72 63 55 59 54 145 59
R08 | 1675 21 16 28 18 20 53 17 --- 11 | 66 68 70 60 60 51 48 --- 55
R09E | 2742 39 45 27 26 25 26 24 --- 12 | 60 68 61 74 60 62 55 --- 58
R10E | 1136 49 59 31 24 23 16 16 --- 11 | 52 77 24 51 46 57 52 --- 48
R11E | 1255 74 94 48 27 45 46 24 --- 18 | 83 98 54 62 78 80 47 --- 56
R12E | 2434 69 70 55 17 31 40 31 217 17 | 103 100 87 83 90 84 74 100 80
R13E | 2485 38 30 21 15 13 26 14 --- 9 | 64 62 48 49 47 50 51 --- 48
R14E | 2375 61 56 45 47 57 59 44 --- 22 | 96 93 76 91 95 97 84 --- 80
R15E | 2420 27 29 32 20 41 28 17 --- 12 | 48 50 46 47 60 46 49 --- 45
R16E | 1355 32 34 28 20 14 25 20 --- 10 | 52 57 44 53 39 50 46 --- 44
XR17E | 3736 25 34 --- 351 14 305 13 --- 11 | 42 40 --- 193 42 139 57 --- 54
R18 | 753 39 40 18 19 22 44 12 231 11 | 81 79 65 65 50 39 56 101 56
R19 | 1662 50 47 17 12 21 37 14 --- 10 | 84 83 60 62 49 45 53 --- 54
R20 | 660 53 49 31 15 26 42 18 --- 13 | 84 82 58 59 47 43 48 --- 51
R21 | 527 41 34 23 22 35 39 11 256 12 | 80 78 54 59 44 50 55 97 52
R22 | 1247 54 59 34 20 26 41 16 --- 13 | 92 96 69 70 49 51 56 --- 59
R23 | 1220 27 29 26 26 19 21 14 --- 9 | 53 52 54 75 51 57 64 --- 58
R24 | 1094 37 29 25 34 27 53 13 --- 14 | 73 66 59 69 52 47 57 --- 57
XR26 | ---- 56 136 --- --- --- --- 19 --- 33 | 70 176 --- --- --- --- 9999 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1605 42 44 31 23 27 36 20 224 |T 69 76 60 68 56 58 54 114 55
WRMS | 1605 33 34 30 20 17 33 20 224 |NE 71 79 62 63 52 49 52 117 55
MEDI | 1247 38 34 28 20 22 28 17 231 |MD 69 72 60 62 51 50 53 101 54
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