[IGSREPORT-24526] Wk 1899 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Jun 16 17:17:16 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1899 (May 29, 2016 - Jun 04, 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 2.1899.
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:
igl1899[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1899 in the SP3 format.
igl18997.sum Combination Report for GPS Week 1899.
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 | 3.3 ns
1 | 1.2 ns
2 | 2.8 ns
3 | 3.2 ns
4 | 0.4 ns
5 | 2.2 ns
6 | 0.2 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
----+--------+---------------
3 | ESX | R09
3 | GRG | R09
4 | ESX | R09
4 | GRG | 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 1.1899, 1a.1899).
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 2.1899.0-6)
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 3.1899.0-6).
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 1899 summary. (May 29, 2016 - Jun 04, 2016)
Table 1.1899.a GPS week : 1899 MJD: 57537.0-57543.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 16 63 -43 13 .32 40 37 | --- --- --- ---
| 2 1 4 27 25 17 .05 | --- ---
cof n/a| 0 0 17 41 -37 35 .29 43 39 | --- --- --- ---
| 1 1 4 25 34 31 .06 | --- ---
emx n/a| 0 1 4 -16 -42 -12 .23 29 27 | -2392 661 4367 8399
| 2 1 1 35 26 29 .04 | 6497 1136
esx n/a| 0 0 0 -8 0 -16 -.16 16 13 | -155 906 4514 9609
| 0 0 0 9 24 42 .04 | 4539 2469
gfz n/a| -1 -1 -7 34 68 24 .05 25 21 | 0 730 3722 7415
| 1 1 2 14 19 40 .08 | 0 2058
grg n/a| 1 0 0 -42 84 -17 -.23 32 31 | 2249612 11161 431007 433371
| 1 1 2 23 34 51 .07 | 2806371 20337
iac n/a| 0 0 -5 4 -41 40 .07 22 22 | 2294439 7449 431003 433397
| 1 0 1 26 31 97 .03 | 2858900 13635
mcc n/a| 1 -1 26 74 -72 4 .01 156 156 | --- --- --- ---
| 7 8 29 220 131 461 .33 | --- ---
Table 1.1899.b GPS week : 1899 MJD: 57537.0-57543.0
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 11 11 10 12 11 14 |
R02 | 7 8 8 8 8 6 6 |
R03 | 7 8 7 7 7 10 7 |
R04 | 9 10 9 8 8 8 9 |
R05 | 14 11 14 13 13 12 12 |
R06 | 8 9 9 10 9 9 11 |
R07 | 8 10 8 8 9 9 7 |
R08 | 9 11 10 9 9 10 9 |
R09 | 10 11 10 18 13 75 15 |
R10 | 7 9 8 8 8 8 9 |
R12 | 22 22 20 23 24 25 25 |
R13 | 10 10 10 10 10 12 11 |
R14 | 16 18 13 18 21 21 18 |
R15 | 9 8 13 10 11 10 9 |
R16 | 14 13 18 14 16 17 16 |
R17 | 7 8 9 7 13 15 10 |
R18 | 6 7 7 8 11 12 9 |
R19 | 7 8 7 7 8 9 9 |
R20 | 15 12 10 10 11 14 15 |
R21 | 7 10 8 8 8 12 9 |
R22 | 9 10 10 8 8 8 10 |
R23 | 10 10 11 11 12 10 10 |
R24 | 10 11 12 14 13 12 11 |
R26 | 42 48 49 36 42 187 0 |
Table 1.1899.c GPS week : 1899 MJD: 57537.0-57543.0
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 1899 0 | -61 -24 215 1452 188 -3677 82.7 1313 1313 | 3331 0
brd 1899 1 | -16 -27 305 692 -1247 -7303 82.2 1310 1310 | 1195 0
brd 1899 2 | -109 -38 325 -608 -344 -2033 84.2 1238 1238 | 2832 0
brd 1899 3 | 80 32 286 -409 1783 2482 85.5 1235 1235 | 3183 0
brd 1899 4 | 2 15 195 -902 253 3816 83.9 1156 1156 | 417 0
brd 1899 5 | 44 21 128 474 484 2971 84.3 1114 1114 | 2209 0
brd 1899 6 | -2 47 231 -758 352 5017 84.5 1333 1333 | 207 0
-------------+------------------------------------------------------------+----------------
brd 1899 mean| -8 3 241 -8 210 181 83.9 1242 1242 | 1910 0
brd 1899 sdev| 63 33 69 888 913 4573 1.1 83 83 | 1305 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 2.1899.0 GPS week: 1899 Day: 0 MJD: 57537
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 19 55 -41 37 .32 41 43 | --- --- --- ---
cof n/a| -2 -2 21 25 -14 17 .22 43 46 | --- --- --- ---
emx n/a| 0 0 2 -15 -31 -19 .26 25 25 | -6933 1570 4519 8939
esx n/a| 0 -1 1 0 21 -33 -.10 16 12 | -4785 3482 4507 9510
gfz n/a| -1 0 -9 50 92 74 .03 25 21 | 0 1300 3784 8622
grg n/a| 0 -1 -2 -45 6 43 -.21 30 29 | 1462 2591 4518 8756
iac n/a| 0 0 -4 -3 -36 31 .06 19 19 | 3091 1471 4511 8961
mcc n/a| -4 0 -7 -54 73 221 -.20 96 96 | --- --- --- ---
Table 2.1899.1 GPS week: 1899 Day: 1 MJD: 57538
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 20 22 2 11 .31 40 36 | --- --- --- ---
cof n/a| 2 0 21 4 10 60 .19 44 39 | --- --- --- ---
emx n/a| 0 2 3 26 -26 -31 .20 28 26 | -6192 -278 3590 7967
esx n/a| 0 0 0 -19 26 16 -.19 13 12 | 2864 -993 3602 8792
gfz n/a| 0 -2 -10 21 78 18 .15 28 27 | 0 -1570 3348 6910
grg n/a| 0 3 0 -18 96 0 -.22 33 33 | 1985 -1217 3608 7949
iac n/a| 1 0 -7 21 -102 3 .05 22 22 | 2671 -712 3626 8051
mcc n/a| 1 -4 1 19 -105 199 -.20 73 73 | --- --- --- ---
Table 2.1899.2 GPS week: 1899 Day: 2 MJD: 57539
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 17 66 -34 28 .28 38 32 | --- --- --- ---
cof n/a| 0 0 21 60 -12 56 .35 39 33 | --- --- --- ---
emx n/a| 3 1 5 19 -15 -60 .25 30 29 | -4808 1109 3866 6990
esx n/a| -1 -1 0 -13 -30 50 -.18 14 13 | -4441 -227 3848 7984
gfz n/a| -2 0 -6 34 50 35 .07 22 18 | 0 2264 3337 5909
grg n/a| 0 0 0 -55 95 -56 -.17 28 28 | 2348 1492 3875 6948
iac n/a| 0 -1 -6 -12 -9 1 .09 20 20 | 4150 -77 3861 7071
mcc n/a| 8 0 6 171 5 -204 -.26 82 82 | --- --- --- ---
Table 2.1899.3 GPS week: 1899 Day: 3 MJD: 57540
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 20 89 -48 -4 .36 38 31 | --- --- --- ---
cof n/a| 0 1 18 25 -38 -26 .34 45 34 | --- --- --- ---
emx n/a| -1 0 5 -42 -72 28 .28 28 26 | -4855 1358 4848 7134
esx n/a| 0 -1 -1 -13 17 -25 -.18 14 12 | -4540 1546 5069 8615
gfz n/a| -2 -3 -10 33 81 35 .15 26 20 | 0 1556 4371 6472
grg n/a| 0 2 0 -77 96 -18 -.29 31 30 | 5045770 55595 999999 999999
iac n/a| 2 0 -5 15 -57 -5 .10 21 21 | 5274250 36085 999999 999999
mcc n/a| 6 15 22 231 -286 530 .44 167 167 | --- --- --- ---
Table 2.1899.4 GPS week: 1899 Day: 4 MJD: 57541
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 17 35 -35 -3 .36 41 47 | --- --- --- ---
cof n/a| 0 2 18 52 -86 55 .29 41 49 | --- --- --- ---
emx n/a| 0 -1 6 0 -59 15 .24 27 24 | 2813 -606 4037 8971
esx n/a| -1 0 0 5 10 -53 -.11 17 14 | 6577 -2067 4271 10503
gfz n/a| -2 -2 -4 43 60 2 -.06 26 21 | 0 -2793 3839 7674
grg n/a| 0 -1 1 -48 90 49 -.35 33 28 | 5384831 552 999999 999999
iac n/a| 1 -1 -7 -6 -20 86 .08 24 24 | 5461691 330 999999 999999
mcc n/a| 9 0 33 420 -175 439 -.36 168 168 | --- --- --- ---
Table 2.1899.5 GPS week: 1899 Day: 5 MJD: 57542
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 3 12 98 -70 0 .39 43 36 | --- --- --- ---
cof n/a| 1 1 12 39 -66 34 .32 46 39 | --- --- --- ---
emx n/a| 2 2 8 -75 -76 -17 .24 33 30 | 10192 -630 4650 8801
esx n/a| 0 -1 1 -2 -31 -74 -.21 18 15 | 3013 -138 5260 11063
gfz n/a| -2 0 -7 9 77 -50 -.03 26 19 | 0 2478 3696 7299
grg n/a| 1 0 -4 -48 98 -90 -.24 33 33 | 5312569 15453 999999 999999
iac n/a| 0 1 -3 49 -39 233 .10 25 25 | 5314437 14079 999999 999999
mcc n/a| -12 -10 71 -5 66 -648 .25 237 237 | --- --- --- ---
Table 2.1899.6 GPS week: 1899 Day: 6 MJD: 57543
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 9 75 -73 26 .25 38 32 | --- --- --- ---
cof n/a| 0 0 10 80 -52 53 .36 41 34 | --- --- --- ---
emx n/a| -1 2 3 -24 -13 -1 .15 29 26 | -6965 2104 5060 9992
esx n/a| 0 -1 0 -15 -13 4 -.13 18 14 | 222 4742 5047 10802
gfz n/a| 0 0 -5 45 38 54 .01 24 19 | 0 1876 3681 9019
grg n/a| 3 1 4 -7 108 -46 -.12 35 35 | -1680 3662 5051 9950
iac n/a| -1 0 -5 -31 -22 -70 .01 22 22 | 787 972 5031 9705
mcc n/a| 1 -7 57 -260 -82 -505 .37 272 272 | --- --- --- ---
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 3.1899.0 GPS week: 1899 Day: 0 MJD: 57537
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 | 1551 42 42 17 16 18 50 24 --- 12 | 57 58 29 30 26 53 22 --- 25
R02 | 534 20 24 15 10 19 20 11 --- 6 | 54 59 47 42 29 36 28 --- 37
R03 | 698 27 30 16 9 27 12 9 101 7 | 68 69 62 50 47 54 39 25 49
R04 | 1194 24 25 14 7 21 36 13 --- 8 | 66 66 56 44 31 62 38 --- 45
R05 | 635 36 29 29 22 21 54 25 --- 14 | 56 59 60 64 59 44 47 --- 53
R06 | 959 25 30 22 8 18 22 16 --- 8 | 58 60 49 42 31 45 29 --- 39
R07 | 1134 27 34 18 9 24 22 18 109 8 | 67 72 56 47 40 42 33 41 43
R08 | 1227 26 18 32 8 16 17 22 --- 9 | 56 55 54 35 36 29 26 --- 35
XR09 | 1385 24 40 21 14 --- 28 14 --- 9 | 17 29 16 43 --- 41 23 --- 20
R10 | 2837 15 21 14 16 22 13 16 --- 7 | 24 25 21 34 27 28 27 --- 25
R12 | 725 129 139 26 24 58 50 27 --- 22 | 120 130 34 24 38 57 23 --- 25
R13 | 2895 43 42 20 10 31 16 16 --- 9 | 51 48 26 26 22 31 21 --- 23
R14 | 1210 34 32 44 28 27 50 25 --- 15 | 31 41 27 55 38 30 29 --- 32
XR15 | 2593 15 16 17 13 --- 26 18 --- 9 | 24 24 28 23 --- 32 17 --- 18
R16 | 1926 36 36 32 31 27 36 25 --- 13 | 30 39 42 49 28 28 25 --- 25
R17 | 922 22 23 17 11 13 18 14 --- 6 | 62 64 45 45 38 48 38 --- 42
R18 | 922 18 16 17 11 19 13 9 --- 6 | 63 61 51 51 50 54 53 --- 51
R19 | 877 31 33 21 10 18 17 6 --- 7 | 55 56 39 38 38 36 38 --- 37
R20 | 762 34 24 51 12 36 38 28 --- 14 | 59 62 66 44 44 39 47 --- 41
R21 | 728 26 26 15 10 19 18 12 73 7 | 62 62 45 45 37 52 39 71 43
R22 | 700 44 45 20 9 24 15 15 --- 9 | 70 71 38 32 29 38 30 --- 33
R23 | 845 33 42 22 17 14 24 21 --- 9 | 45 46 42 69 56 44 54 --- 53
R24 | 750 33 30 23 18 23 21 21 --- 9 | 73 78 58 66 56 58 65 --- 60
XR26 | ---- 69 335 --- --- --- --- 24 --- 41 | 94 370 --- --- --- --- 62 --- 62
------+---------------------------------------------------+-----------------------------------------------
RMS | 1313 41 43 25 16 25 30 19 96 |T 56 71 43 43 38 42 35 45 38
WRMS | 1313 43 46 25 12 21 29 19 96 |NE 51 55 40 40 34 40 28 33 32
MEDI | 922 27 30 20 11 21 22 16 101 |MD 57 59 45 44 38 42 30 41 37
Table 3.1899.1 GPS week: 1899 Day: 1 MJD: 57538
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 | 1551 41 43 25 14 18 45 18 --- 11 | 37 48 40 36 49 58 23 --- 34
R02 | 942 14 19 19 13 8 30 22 --- 8 | 44 50 43 44 38 49 19 --- 37
R03 | 639 29 34 18 6 19 19 22 102 8 | 51 52 41 36 37 48 19 23 33
R04 | 862 39 35 29 10 32 24 14 --- 10 | 49 44 34 23 31 43 20 --- 24
R05 | 706 29 40 17 16 24 44 27 --- 11 | 32 38 39 36 30 41 30 --- 31
R06 | 965 37 31 18 11 18 33 14 --- 9 | 38 41 28 45 45 58 29 --- 37
R07 | 733 33 31 21 6 26 35 24 61 10 | 43 39 37 30 25 55 18 35 28
R08 | 1372 32 34 38 8 29 28 17 --- 10 | 35 37 37 24 32 39 12 --- 20
XR09 | 1553 29 28 25 8 --- 26 26 --- 10 | 21 17 12 30 --- 52 26 --- 19
R10 | 2096 14 19 19 12 35 24 23 --- 9 | 20 28 24 26 26 31 17 --- 19
R12 | 723 121 128 36 16 48 45 38 --- 21 | 90 94 37 32 29 44 24 --- 28
R13 | 2138 41 49 20 10 34 27 13 --- 10 | 44 50 31 30 24 25 21 --- 24
R14 | 1235 38 50 65 20 45 50 32 --- 18 | 30 44 47 43 41 30 25 --- 29
XR15 | 6424 18 23 17 14 --- 16 19 --- 8 | 27 33 26 20 --- 29 17 --- 18
R16 | 2133 28 26 39 23 33 35 19 --- 12 | 29 39 43 38 39 34 20 --- 27
R17 | 1508 23 28 17 10 22 21 16 --- 7 | 53 62 41 47 44 46 34 --- 41
R18 | 1661 20 24 14 9 16 28 11 --- 7 | 60 64 48 55 55 45 57 --- 52
R19 | 969 28 27 18 10 19 29 13 --- 8 | 51 50 34 39 39 44 39 --- 36
R20 | 851 36 37 30 14 41 26 27 --- 12 | 47 47 35 42 48 44 49 --- 37
R21 | 753 27 22 19 14 27 42 16 41 10 | 43 41 31 31 26 53 31 38 29
R22 | 1327 39 50 23 9 20 26 22 --- 9 | 56 65 30 28 30 36 28 --- 28
R23 | 1418 31 36 32 19 13 25 19 --- 10 | 35 37 31 51 43 43 43 --- 40
R24 | 1044 27 28 30 14 21 37 29 --- 11 | 54 51 51 55 57 64 52 --- 51
XR26 | ---- 71 724 --- --- --- --- 30 --- 47 | 87 713 --- --- --- --- 30 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1309 40 44 28 13 28 33 22 73 |T 44 74 35 36 37 43 28 32 31
WRMS | 1309 36 39 26 12 27 33 22 73 |NE 39 43 34 32 34 42 21 29 27
MEDI | 1235 29 31 21 12 24 28 19 61 |MD 43 44 37 36 38 44 25 35 29
Table 3.1899.2 GPS week: 1899 Day: 2 MJD: 57539
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 | 1140 45 40 30 13 23 26 18 --- 11 | 44 39 28 23 27 37 12 --- 18
R02 | 829 17 22 28 10 16 15 15 --- 7 | 44 50 44 33 24 46 24 --- 32
R03 | 892 16 23 24 7 14 10 21 111 7 | 54 66 64 47 58 44 32 31 47
R04 | 606 32 50 27 8 18 19 22 --- 9 | 57 72 55 33 34 47 23 --- 36
R05 | 787 33 35 31 16 23 52 27 --- 13 | 45 44 49 32 23 39 33 --- 30
R06 | 1572 33 33 18 13 12 24 23 --- 9 | 47 52 34 46 43 41 32 --- 38
R07 | 732 20 21 27 9 15 11 26 80 8 | 50 57 50 47 46 43 31 39 41
R08 | 995 34 38 34 15 18 22 19 --- 10 | 47 53 41 26 27 24 16 --- 23
XR09 | 1502 26 25 19 9 --- 34 11 --- 10 | 19 19 21 87 --- 72 18 --- 16
R10 | 1145 13 22 20 14 23 21 16 --- 8 | 23 33 26 28 20 28 15 --- 19
R12 | 966 113 107 30 15 35 32 33 --- 19 | 98 92 35 32 33 28 24 --- 28
R13 | 1188 41 40 16 15 23 16 20 --- 9 | 48 48 36 39 35 31 22 --- 29
R14 | 2348 27 34 49 19 20 41 13 --- 12 | 37 44 37 44 34 36 32 --- 32
XR15 | 6780 20 21 20 24 --- 44 14 --- 13 | 22 24 25 30 --- 43 17 --- 18
R16 | 1868 20 35 64 25 23 64 21 --- 17 | 31 41 54 40 38 31 29 --- 25
R17 | 942 31 22 21 9 25 21 10 --- 8 | 53 45 35 37 36 41 31 --- 34
R18 | 1348 24 21 18 7 19 12 14 --- 6 | 84 86 74 84 85 73 87 --- 80
R19 | 2007 23 32 16 11 15 12 13 --- 6 | 46 55 34 43 38 37 36 --- 36
R20 | 651 31 29 19 15 29 20 19 --- 9 | 52 51 45 44 41 35 42 --- 38
R21 | 576 28 30 21 11 21 16 15 41 8 | 50 46 37 32 27 40 34 113 31
R22 | 1221 31 27 18 12 25 35 12 --- 9 | 55 53 35 39 37 35 39 --- 35
R23 | 1449 44 32 31 23 18 23 17 --- 11 | 42 55 37 69 62 45 54 --- 52
R24 | 809 21 31 35 17 26 31 26 --- 11 | 58 63 45 55 54 43 55 --- 48
XR26 | ---- 69 365 --- --- --- --- 33 --- 48 | 84 304 --- --- --- --- 47 --- 45
------+---------------------------------------------------+-----------------------------------------------
RMS | 1237 38 39 30 14 22 28 20 82 |T 49 62 40 43 39 40 32 61 34
WRMS | 1237 32 33 29 13 18 28 20 82 |NE 44 48 39 39 34 39 24 35 28
MEDI | 1140 28 31 24 13 21 22 18 80 |MD 47 51 37 39 36 40 31 39 32
Table 3.1899.3 GPS week: 1899 Day: 3 MJD: 57540
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 | 1278 31 46 26 20 25 18 21 --- 10 | 41 64 38 50 51 36 22 --- 35
R02 | 1256 27 26 26 4 20 19 11 --- 7 | 46 41 37 22 22 30 17 --- 24
R03 | 1216 20 11 26 7 23 13 12 112 7 | 59 49 56 37 32 43 35 27 40
R04 | 950 25 18 14 13 15 29 15 --- 8 | 65 61 49 44 38 65 33 --- 44
R05 | 604 36 48 33 12 26 44 29 --- 12 | 58 68 70 55 56 46 40 --- 50
R06 | 1986 33 29 21 13 27 33 12 --- 9 | 52 47 30 22 24 51 23 --- 27
R07 | 630 19 20 21 9 16 25 16 150 7 | 60 55 47 46 37 50 32 54 42
R08 | 679 22 26 13 8 16 38 19 --- 8 | 56 56 46 47 49 36 36 --- 42
XR09 | 1727 23 29 31 287 --- 384 21 --- 18 | 20 34 36 137 --- 311 25 --- 25
R10 | 1109 14 29 14 15 21 24 11 --- 7 | 24 33 29 30 21 31 20 --- 22
R12 | 582 117 135 33 18 57 49 38 --- 22 | 102 121 43 30 37 50 26 --- 26
R13 | 752 36 38 23 6 26 26 19 --- 9 | 46 48 37 27 31 34 26 --- 26
R14 | 2858 45 47 67 17 27 43 40 --- 17 | 47 61 53 38 41 39 31 --- 33
XR15 | 3994 22 34 28 15 --- 22 13 --- 9 | 29 40 24 26 --- 28 20 --- 20
R16 | 793 40 74 43 27 34 33 20 --- 14 | 42 76 47 41 33 30 32 --- 26
R17 | 1196 27 28 21 8 18 21 11 --- 7 | 67 68 54 43 43 54 39 --- 45
R18 | 570 20 21 22 11 20 22 15 --- 7 | 63 61 47 49 53 55 47 --- 48
R19 | 1786 22 19 19 10 20 23 8 --- 7 | 51 51 46 38 39 43 35 --- 38
R20 | 671 30 41 19 13 29 27 20 --- 9 | 61 77 50 50 58 55 47 --- 48
R21 | 1341 27 30 20 12 22 23 14 220 8 | 70 71 49 57 45 69 45 136 52
R22 | 832 27 22 21 10 20 20 11 --- 7 | 56 48 38 35 34 39 37 --- 35
R23 | 1179 30 34 30 18 18 21 25 --- 10 | 56 55 60 69 62 59 53 --- 57
R24 | 1024 22 46 23 20 25 57 29 --- 13 | 60 91 53 59 64 57 66 --- 55
XR26 | ---- 54 1247 --- --- --- --- 23 --- 36 | 77 9999 --- --- --- --- 77 --- 57
------+---------------------------------------------------+-----------------------------------------------
RMS | 1235 38 45 28 14 26 31 21 167 |T 54 59 45 45 41 57 36 72 38
WRMS | 1235 31 33 26 12 20 30 21 167 |NE 49 56 42 43 36 58 27 40 32
MEDI | 1109 27 29 23 13 22 25 16 150 |MD 56 56 47 43 39 46 33 54 38
Table 3.1899.4 GPS week: 1899 Day: 4 MJD: 57541
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 | 635 31 19 27 15 41 24 21 --- 11 | 35 27 27 43 75 33 25 --- 34
R02 | 1258 19 18 22 12 21 15 15 --- 7 | 35 37 38 31 30 39 21 --- 27
R03 | 704 19 26 21 8 22 11 13 136 7 | 48 52 49 30 24 37 29 23 32
R04 | 1065 25 31 18 5 12 32 14 --- 8 | 49 54 42 32 35 33 27 --- 31
R05 | 519 32 23 30 18 16 54 21 --- 12 | 58 67 58 60 54 38 45 --- 50
R06 | 1840 26 28 18 10 18 24 23 --- 8 | 46 46 35 33 38 45 25 --- 32
R07 | 1239 32 32 22 10 26 13 13 239 8 | 49 51 36 25 27 32 31 27 28
R08 | 641 20 23 23 15 15 30 12 --- 8 | 46 49 41 39 33 29 31 --- 33
XR09 | 1657 18 31 --- 291 --- 138 7 --- 12 | 16 24 --- 96 --- 190 23 --- 38
R10 | 1215 19 18 11 22 13 23 9 --- 7 | 17 24 21 37 21 26 20 --- 23
R12 | 727 129 132 32 20 55 44 43 --- 24 | 101 103 37 49 59 47 35 --- 36
R13 | 808 36 33 16 9 32 27 20 --- 10 | 42 43 35 39 31 46 20 --- 30
R14 | 1738 59 60 61 30 38 60 45 --- 21 | 33 41 39 53 62 24 30 --- 35
XR15 |12369 22 26 21 20 --- 34 19 --- 11 | 31 34 25 32 --- 43 20 --- 23
R16 | 1048 37 31 48 34 21 50 19 --- 16 | 44 37 35 37 28 31 23 --- 22
R17 | 1036 40 35 24 15 20 32 38 --- 12 | 93 108 96 92 89 90 70 --- 83
R18 | 1039 26 22 20 16 21 28 30 --- 10 | 91 92 79 91 80 94 69 --- 81
R19 | 1301 20 21 16 12 25 26 9 --- 8 | 53 50 36 37 34 53 38 --- 37
R20 | 1281 32 38 25 14 26 32 22 --- 10 | 55 70 45 56 53 68 49 --- 49
R21 | 1436 33 31 20 9 15 22 14 97 8 | 110 117 107 96 92 105 87 115 96
R22 | 695 26 22 14 11 22 27 15 --- 8 | 77 79 62 65 53 70 60 --- 61
R23 | 1755 39 39 23 19 18 30 29 --- 11 | 70 76 65 84 67 82 59 --- 70
R24 | 961 15 31 37 21 27 41 31 --- 13 | 52 60 40 70 63 71 46 --- 53
XR26E | ---- 60 202 --- --- --- --- 29 --- 42 | 103 404 --- --- --- --- 103 --- 90
------+---------------------------------------------------+-----------------------------------------------
RMS | 1155 41 41 27 17 26 33 24 168 |T 56 72 47 53 49 57 41 55 45
WRMS | 1155 47 49 24 14 21 28 24 168 |NE 43 45 37 42 39 46 27 25 31
MEDI | 1065 26 31 22 15 21 30 19 136 |MD 49 51 39 43 53 45 31 27 35
Table 3.1899.5 GPS week: 1899 Day: 5 MJD: 57542
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 | 912 27 27 40 14 26 25 22 --- 11 | 30 31 37 36 23 44 26 --- 26
R02 | 757 13 16 14 8 12 12 13 --- 5 | 28 26 30 23 26 31 24 --- 24
R03 | 662 21 25 23 12 12 40 15 153 9 | 44 48 49 45 35 39 33 16 36
R04 | 1021 24 21 21 10 16 18 19 --- 7 | 41 37 43 32 28 32 23 --- 29
R05 | 548 27 14 34 13 20 47 24 --- 12 | 46 46 48 52 47 62 49 --- 48
R06 | 1801 17 32 20 11 12 36 23 --- 9 | 44 55 41 38 37 63 33 --- 38
R07 | 744 37 36 27 11 16 13 16 351 8 | 47 48 39 28 32 36 28 23 30
R08 | 865 34 27 29 13 29 14 11 --- 9 | 39 34 32 22 25 26 34 --- 22
XR09 | 1933 102 104 --- 159 --- 105 107 --- 74 | 17 28 --- 140 --- 40 34 --- 84
R10 | 890 14 25 19 11 26 20 9 --- 7 | 21 23 20 24 22 36 21 --- 19
R12 | 645 133 140 33 35 50 39 33 --- 24 | 88 103 34 62 58 36 24 --- 35
R13 | 706 47 54 23 25 31 21 19 --- 12 | 42 50 30 41 30 26 24 --- 23
R14 | 787 65 47 69 35 48 30 41 --- 21 | 38 59 48 72 84 38 34 --- 45
XR15 |11001 19 25 24 17 --- 30 13 --- 10 | 22 30 26 24 --- 28 22 --- 18
R16 | 1765 35 66 62 23 22 66 14 --- 17 | 28 59 53 16 27 18 24 --- 17
R17E | 882 40 40 32 14 24 34 53 --- 15 | 110 112 98 91 85 105 64 --- 84
R18E | 1449 29 30 21 12 31 28 37 --- 11 | 60 65 47 46 44 59 59 --- 45
R19E | 1215 25 27 29 15 15 27 12 --- 9 | 65 69 56 72 68 58 61 --- 62
R20E | 566 35 37 34 18 25 42 31 --- 13 | 69 70 71 81 84 91 72 --- 74
R21E | 1682 41 53 26 12 24 33 31 148 12 | 135 142 136 135 138 160 124 105 135
R22E | 680 23 44 21 11 15 26 10 --- 7 | 76 83 64 65 63 69 75 --- 66
R23E | 1928 31 18 26 25 11 21 11 --- 9 | 70 75 75 88 72 68 71 --- 73
R24E | 1089 18 26 32 20 26 38 25 --- 12 | 69 73 67 71 56 73 74 --- 64
XR26E | ---- 260 700 --- --- --- --- 134 --- 187 | 290 647 --- --- --- --- 79 --- 104
------+---------------------------------------------------+-----------------------------------------------
RMS | 1114 43 46 33 18 26 33 25 237 |T 63 83 52 56 51 53 46 48 50
WRMS | 1114 36 39 30 15 19 33 25 237 |NE 38 45 37 43 36 37 28 19 32
MEDI | 890 29 30 26 14 24 30 19 153 |MD 44 55 47 46 44 40 34 23 38
Table 3.1899.6 GPS week: 1899 Day: 6 MJD: 57543
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 | 1144 44 61 32 24 31 47 18 --- 14 | 47 62 31 36 38 47 17 --- 25
R02 | 847 15 16 10 9 12 22 12 --- 6 | 45 49 43 38 35 42 27 --- 35
R03 | 1085 19 23 15 9 13 17 22 149 7 | 67 67 58 59 63 54 39 24 54
R04 | 1018 15 18 11 9 19 30 29 --- 9 | 61 63 58 48 40 70 30 --- 47
R05 | 637 33 32 38 16 14 34 24 --- 11 | 59 60 53 63 50 54 55 --- 54
R06 | 666 21 19 26 10 14 31 33 --- 10 | 62 59 49 45 45 68 28 --- 45
R07 | 944 13 20 20 11 13 14 16 414 6 | 65 72 62 57 62 59 47 33 56
R08 | 925 22 25 25 13 14 15 23 --- 8 | 57 58 53 39 42 46 28 --- 39
R09 | 2440 28 22 49 19 31 33 36 --- 15 | 20 29 47 133 7 63 26 --- 40
R10 | 869 14 19 16 18 19 37 10 --- 9 | 29 36 24 33 29 32 28 --- 25
R12 | 1153 111 114 51 33 43 57 33 --- 24 | 107 120 43 60 60 72 34 --- 42
R13 | 878 49 58 21 13 28 25 16 --- 11 | 54 62 32 37 35 34 30 --- 30
R14 | 860 61 66 48 37 36 24 22 --- 17 | 35 47 29 74 70 31 38 --- 43
XR15 | 8999 20 26 14 16 --- 23 14 --- 8 | 30 32 29 26 --- 15 25 --- 23
R16 | 1079 35 32 39 22 30 62 17 --- 15 | 39 42 27 25 29 38 33 --- 20
R17E | 836 40 32 25 16 23 18 19 --- 10 | 86 86 59 64 58 70 58 --- 61
R18E | 1926 25 26 17 11 25 26 17 --- 9 | 64 66 52 52 52 49 57 --- 52
R19E | 1174 33 38 18 10 19 19 16 --- 8 | 76 79 54 55 52 58 57 --- 55
R20E | 639 22 21 24 18 26 69 36 --- 15 | 74 84 76 79 73 91 82 --- 76
R21E | 1601 29 31 24 13 22 19 15 171 9 | 71 75 53 69 72 76 70 67 66
R22E | 781 33 42 20 11 31 27 18 --- 10 | 61 66 53 48 50 52 53 --- 48
R23E | 3340 22 22 24 19 15 36 15 --- 10 | 55 54 58 64 57 55 57 --- 56
R24E | 1000 20 35 26 23 24 33 18 --- 10 | 69 85 47 64 60 73 63 --- 59
XR26E | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 146 --- 167
------+---------------------------------------------------+-----------------------------------------------
RMS | 1333 38 41 29 18 24 35 22 272 |T 57 63 47 55 49 54 47 41 50
WRMS | 1333 32 34 26 14 19 35 22 272 |NE 51 57 42 51 43 48 32 28 38
MEDI | 1000 25 26 24 16 22 27 18 171 |MD 61 62 52 55 50 54 38 33 47
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