[IGSREPORT-24027] Wk 1868 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sat Nov 14 01:35:40 PST 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1868 (Oct 25, 2015 - Oct 31, 2015)
Contact: igs.acc at noaa.gov
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1868.
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:
igl1868[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1868 in the SP3 format.
igl18687.sum Combination Report for GPS Week 1868.
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 | -1.6 ns
1 | 1.5 ns
2 | 0.1 ns
3 | 1.5 ns
4 | 2.4 ns
5 | 2.6 ns
6 | 2.6 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
----+--------+---------------
6 | COD | R07
6 | EMX | R07
6 | GRG | R07
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 1.1868, 1a.1868).
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 2.1868.0-6)
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 3.1868.0-6).
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 1868 summary. (Oct 25, 2015 - Oct 31, 2015)
Table 1.1868.a GPS week : 1868 MJD: 57320.0-57326.0
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 -5 60 -31 -105 .28 46 49 | --- --- --- ---
| 2 1 4 18 17 36 .05 | --- ---
cof n/a| 0 0 -6 62 -41 -102 .30 47 50 | --- --- --- ---
| 1 1 3 38 25 32 .04 | --- ---
emx n/a| 0 -1 0 -13 -66 -3 .28 31 32 | 1677 -501 3762 7490
| 1 1 1 31 43 40 .05 | 5954 848
esx n/a| 1 0 1 -86 45 -35 -.12 22 21 | -457 135 3758 8083
| 1 1 0 24 42 32 .04 | 5812 2241
gfz n/a| -2 0 1 63 69 70 .04 23 21 | 0 -633 3708 7131
| 1 0 1 14 22 34 .07 | 0 1643
grg n/a| -2 1 -1 34 -20 -70 -.37 41 38 | -582484 -517 4623 686219
| 1 2 4 44 26 38 .10 | 18372 1780
iac n/a| 0 0 0 7 -39 36 -.07 20 20 | 3279 -1055 3762 7344
| 1 0 1 26 42 35 .04 | 1973 1299
mcc n/a| 2 4 51 9 -70 571 -.77 219 219 | --- --- --- ---
| 12 8 21 164 73 681 .44 | --- ---
Table 1.1868.b GPS week : 1868 MJD: 57320.0-57326.0
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 | 11 12 11 15 18 19 17 |
R02 | 8 9 9 12 9 9 10 |
R03 | 9 17 14 8 8 11 10 |
R04 | 10 8 8 8 14 13 9 |
R05 | 12 11 11 11 16 13 14 |
R06 | 8 9 9 9 14 14 10 |
R07 | 14 11 10 10 12 17 155 |
R08 | 10 14 9 10 11 12 10 |
R09 | 17 17 13 16 16 16 14 |
R10 | 11 9 8 9 10 9 9 |
R11 | 21 22 19 24 20 17 17 |
R12 | 16 19 20 21 22 20 17 |
R13 | 12 13 15 16 14 12 12 |
R14 | 18 16 12 13 18 18 19 |
R15 | 11 11 10 11 9 13 11 |
R16 | 10 10 10 11 11 10 10 |
R18 | 8 10 9 8 8 10 8 |
R19 | 8 8 9 9 9 10 9 |
R20 | 12 16 14 11 14 14 11 |
R21 | 10 10 10 9 10 11 9 |
R22 | 8 10 9 9 11 12 10 |
R23 | 9 10 10 10 10 7 12 |
R24 | 12 16 9 14 16 13 11 |
R26 | 0 0 0 0 0 0 0 |
Table 1.1868.c GPS week : 1868 MJD: 57320.0-57326.0
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 1868 0 | -44 -84 -29 269 45 -3161 84.8 2384 2384 | -1576 0
brd 1868 1 | 36 12 -21 -699 -1266 -3304 85.5 1528 1528 | 1490 0
brd 1868 2 | 29 76 105 -1419 -1559 -3585 84.4 1327 1327 | 144 0
brd 1868 3 | -13 -78 -7 999 1359 -3831 84.7 1510 1510 | 1514 0
brd 1868 4 | 71 -5 17 190 1843 -1361 85.4 1626 1626 | 2355 0
brd 1868 5 | -1 66 17 1080 2323 -712 84.0 1858 1858 | 2646 0
brd 1868 6 | 29 50 -26 961 3195 -4082 84.2 1960 1960 | 2619 0
-------------+------------------------------------------------------------+----------------
brd 1868 mean| 15 5 8 197 848 -2862 84.7 1741 1741 | 1313 0
brd 1868 sdev| 38 65 47 951 1818 1298 .6 355 355 | 1546 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 2.1868.0 GPS week: 1868 Day: 0 MJD: 57320
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 -2 38 -15 -138 .26 45 50 | --- --- --- ---
cof n/a| -1 2 -8 60 -21 -160 .27 50 56 | --- --- --- ---
emx n/a| 0 0 0 -25 -125 12 .26 27 26 | -6038 -56 3555 7538
esx n/a| 0 -1 0 -113 15 -54 -.12 21 20 | -2920 229 3565 8186
gfz n/a| -1 0 0 42 74 69 .01 21 22 | 0 -331 3497 7109
grg n/a| -2 1 -1 68 14 -113 -.30 41 41 | -592463 140 3571 688134
iac n/a| 0 0 0 22 5 41 -.12 18 18 | -579 -38 3555 7320
mcc n/a| 8 4 51 -37 -77 -411 -1.60 210 210 | --- --- --- ---
Table 2.1868.1 GPS week: 1868 Day: 1 MJD: 57321
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 2 -8 61 -16 -144 .23 48 44 | --- --- --- ---
cof n/a| 0 1 -8 38 -5 -105 .28 47 42 | --- --- --- ---
emx n/a| 1 0 1 -14 -51 27 .30 31 33 | 11344 -384 3909 7277
esx n/a| 0 -1 0 -57 26 -68 -.15 23 20 | -11211 3141 3905 7917
gfz n/a| 0 0 1 63 88 84 -.05 24 21 | 0 -806 3819 6929
grg n/a| -1 3 0 59 -39 -37 -.38 42 39 | -588873 -123 3899 687755
iac n/a| -1 0 0 -19 -41 29 -.01 21 21 | 3202 241 3897 7199
mcc n/a| -3 0 40 -246 -74 -242 -.59 181 181 | --- --- --- ---
Table 2.1868.2 GPS week: 1868 Day: 2 MJD: 57322
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 -9 46 -8 -96 .21 44 45 | --- --- --- ---
cof n/a| 0 0 -11 12 -46 -121 .28 45 46 | --- --- --- ---
emx n/a| 1 0 0 -40 -37 43 .22 29 28 | 6356 -2335 4090 8375
esx n/a| 2 -1 0 -109 77 -35 -.14 21 20 | 3719 -3609 4104 8631
gfz n/a| 0 1 0 84 95 120 .02 22 22 | 0 -4098 4089 8030
grg n/a| -5 2 4 60 -6 -104 -.25 42 39 | -588839 -4455 4126 688949
iac n/a| 1 0 0 37 -95 -3 -.03 16 16 | 3628 -3327 4105 8382
mcc n/a| 5 -5 24 275 36 350 -.63 224 224 | --- --- --- ---
Table 2.1868.3 GPS week: 1868 Day: 3 MJD: 57323
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -5 0 -6 42 -37 -89 .31 44 47 | --- --- --- ---
cof n/a| -2 -2 -4 24 -37 -100 .26 46 46 | --- --- --- ---
emx n/a| 0 -2 -1 -18 -4 -39 .29 30 31 | 605 183 3729 6976
esx n/a| 2 -1 2 -107 113 -17 -.15 24 21 | -1925 1984 3698 7703
gfz n/a| -2 2 2 52 62 64 .04 22 18 | 0 1149 3618 6471
grg n/a| -1 3 1 78 -40 -98 -.28 38 36 | -593736 854 9739 687563
iac n/a| -1 1 0 14 -71 61 -.10 20 20 | 2444 -573 3735 6553
mcc n/a| 17 11 28 0 -128 1161 -.26 230 230 | --- --- --- ---
Table 2.1868.4 GPS week: 1868 Day: 4 MJD: 57324
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 -8 71 -44 -98 .30 51 57 | --- --- --- ---
cof n/a| 0 0 -1 100 -32 -64 .31 49 57 | --- --- --- ---
emx n/a| 1 -3 -2 51 -45 -72 .37 33 35 | -576 -605 3861 8218
esx n/a| 2 0 2 -58 73 -53 -.15 27 26 | 2648 -1641 3852 8323
gfz n/a| -3 0 2 58 84 62 .03 23 21 | 0 55 3873 8007
grg n/a| -3 3 0 17 -35 -87 -.42 37 34 | -586769 -428 3845 690048
iac n/a| 1 1 -2 -37 -71 90 -.08 22 22 | 5614 -2363 3862 8419
mcc n/a| -12 10 59 -75 -182 1078 -.51 316 316 | --- --- --- ---
Table 2.1868.5 GPS week: 1868 Day: 5 MJD: 57325
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 1 68 -47 -134 .37 47 51 | --- --- --- ---
cof n/a| -2 -1 -2 88 -60 -91 .37 47 52 | --- --- --- ---
emx n/a| -1 -2 -1 -39 -93 13 .25 34 35 | -3593 -34 3404 7312
esx n/a| 1 0 0 -79 10 27 -.06 21 20 | 6736 831 3390 8615
gfz n/a| -3 0 3 78 48 85 .11 25 25 | 0 -22 3353 6972
grg n/a| -2 -2 -10 -42 -48 -25 -.56 41 37 | -585352 313 3394 688976
iac n/a| 3 2 -2 7 -17 -10 -.07 25 25 | 4440 -707 3393 6842
mcc n/a| -13 14 81 136 -63 1233 -1.05 189 189 | --- --- --- ---
Table 2.1868.6 GPS week: 1868 Day: 6 MJD: 57326
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 3 0 -3 91 -53 -39 .28 44 48 | --- --- --- ---
cof n/a| 2 -2 -10 111 -83 -71 .30 45 48 | --- --- --- ---
emx n/a| -1 -1 1 -8 -106 -8 .25 35 33 | 3645 -276 3787 6740
esx n/a| 1 1 2 -76 2 -43 -.06 19 19 | -247 16 3793 7206
gfz n/a| -3 0 1 63 32 6 .15 25 18 | 0 -382 3710 6402
grg n/a| 0 -1 -3 -2 13 -30 -.39 42 37 | -541358 80 3793 672110
iac n/a| 0 0 0 27 15 48 -.11 16 16 | 4204 -620 3788 6695
mcc n/a| 13 -6 72 13 0 836 -.79 181 181 | --- --- --- ---
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 3.1868.0 GPS week: 1868 Day: 0 MJD: 57320
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 2757 48 54 26 15 21 32 18 --- 11 | 85 86 81 79 92 89 79 --- 81
R02E | 2007 25 19 19 11 18 20 17 292 8 | 131 129 124 123 125 123 126 115 124
R03E | 2461 26 33 22 19 16 25 13 --- 8 | 198 198 194 205 202 200 194 --- 198
R04E | 1061 29 29 29 20 25 26 13 --- 10 | 110 113 112 109 112 106 102 --- 107
R05E | 1387 30 34 30 14 20 48 22 --- 11 | 68 71 72 68 69 74 77 --- 69
R06E | 1704 20 26 20 18 10 28 17 --- 8 | 65 63 62 64 64 62 61 --- 61
R07E | 1689 38 42 28 20 21 43 36 312 13 | 137 126 129 105 130 109 132 130 126
R08E | 1566 45 34 23 15 19 29 14 --- 10 | 214 208 214 205 211 211 208 --- 209
R09 | 1398 26 30 59 24 25 61 24 --- 16 | 37 48 70 50 41 27 28 --- 34
R10 | 1256 30 46 23 23 20 46 13 --- 10 | 27 41 29 34 22 33 16 --- 16
R11 | 1052 111 123 52 21 38 57 19 --- 20 | 107 115 54 28 31 30 11 --- 18
R12 | 599 100 101 24 17 24 41 19 83 16 | 99 98 28 28 29 28 13 14 18
R13 | 1428 65 87 14 13 19 28 21 --- 11 | 71 78 32 19 25 16 13 --- 16
R14 | 1479 49 48 27 47 20 75 28 --- 17 | 48 50 30 42 24 26 28 --- 25
R15 | 8859 33 40 20 21 28 34 13 --- 10 | 33 34 31 25 25 21 15 --- 16
R16 | 889 29 37 22 25 22 26 16 --- 10 | 40 48 27 35 18 13 20 --- 17
R18 | 1292 24 30 23 16 16 29 11 131 8 | 57 62 56 45 29 30 31 42 37
R19 | 1349 26 25 17 12 25 27 8 --- 8 | 66 67 59 48 31 46 41 --- 44
R20 | 556 20 16 26 31 14 57 19 --- 12 | 44 48 60 61 44 32 35 --- 45
R21 | 856 38 37 29 13 14 33 16 114 10 | 68 68 58 41 31 14 31 53 37
R22 | 1046 28 33 17 13 18 22 18 --- 8 | 71 77 62 57 59 48 39 --- 52
R23 | 2069 18 22 18 27 22 29 11 --- 9 | 37 37 40 72 49 47 48 --- 49
R24 | 1822 24 29 20 26 16 64 16 --- 11 | 51 69 60 71 55 37 50 --- 53
XR26 | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 42 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS | 2383 45 50 27 21 21 41 18 209 |T 81 84 73 70 66 61 60 70 62
WRMS | 2383 50 56 26 20 22 41 18 209 |NE 57 62 46 43 34 29 28 36 32
MEDI | 1398 29 34 23 19 20 32 16 131 |MD 68 69 60 57 44 37 39 53 44
Table 3.1868.1 GPS week: 1868 Day: 1 MJD: 57321
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1466 63 43 22 14 21 33 19 --- 12 | 99 95 97 101 110 109 86 --- 96
R02E | 1680 21 21 18 16 15 29 17 292 8 | 90 93 86 87 87 92 90 60 87
R03E | 2395 28 29 25 27 26 96 27 --- 17 | 159 156 157 158 159 116 145 --- 149
R04E | 914 19 22 22 13 19 28 8 --- 7 | 75 76 76 73 80 88 72 --- 75
R05E | 2251 25 29 28 25 17 34 17 --- 10 | 60 59 56 53 56 61 66 --- 56
R06E | 1088 26 31 24 16 16 32 12 --- 8 | 46 52 43 45 43 50 49 --- 44
R07E | 1613 36 36 25 18 20 26 23 212 10 | 102 103 104 101 106 100 83 68 92
R08E | 1253 34 36 29 22 18 38 40 --- 13 | 197 200 199 198 193 204 185 --- 193
R09 | 968 30 33 52 24 30 75 23 --- 17 | 26 32 33 29 33 25 21 --- 19
R10 | 706 16 24 24 23 23 21 13 --- 9 | 21 23 19 29 22 28 24 --- 18
R11 | 1219 110 109 47 35 41 52 33 --- 22 | 77 90 44 64 49 28 14 --- 33
R12 | 1124 112 115 31 18 36 35 23 80 18 | 66 75 27 40 38 20 16 11 22
R13 | 1317 76 61 10 14 19 26 26 --- 13 | 58 47 20 23 22 30 17 --- 16
R14 | 1406 54 44 43 42 15 54 19 --- 16 | 36 37 31 54 38 25 25 --- 27
R15 | 3609 41 39 23 21 27 35 15 --- 11 | 27 30 25 18 31 21 11 --- 12
R16 | 1119 42 34 17 16 31 29 12 --- 10 | 32 31 22 27 38 24 14 --- 19
R18 | 535 28 25 23 10 32 26 10 138 9 | 40 38 39 32 22 25 29 32 25
R19 | 754 25 27 17 17 12 27 10 --- 7 | 45 47 33 41 38 34 34 --- 35
R20 | 593 16 24 69 19 31 36 19 --- 15 | 34 26 61 42 37 44 31 --- 33
R21 | 818 28 42 19 22 16 39 18 94 10 | 45 59 37 50 36 17 26 33 33
R22 | 1395 34 38 30 11 12 29 23 --- 10 | 51 53 50 36 42 24 21 --- 34
R23 | 1491 25 27 22 26 20 24 13 --- 9 | 30 32 31 50 58 34 29 --- 38
R24 | 1875 32 44 37 39 23 60 26 --- 15 | 61 69 63 68 43 26 46 --- 47
XR26 | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 47 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1528 48 47 31 23 24 42 21 181 |T 64 66 58 61 60 53 49 40 52
WRMS | 1528 44 42 33 20 21 39 21 181 |NE 43 45 35 40 36 27 25 25 28
MEDI | 1253 30 34 24 19 20 33 18 138 |MD 51 53 43 50 42 30 29 33 34
Table 3.1868.2 GPS week: 1868 Day: 2 MJD: 57322
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 2057 56 57 26 14 23 30 17 --- 11 | 93 90 95 85 96 89 80 --- 85
R02E | 671 27 25 27 16 16 30 13 211 9 | 123 125 119 130 131 120 116 105 122
R03E | 1547 17 17 20 19 19 95 16 --- 14 | 76 75 72 84 84 80 74 --- 76
R04E | 933 20 13 20 14 20 24 12 --- 7 | 100 104 103 103 110 102 96 --- 101
R05E | 3151 19 21 28 24 20 36 23 --- 11 | 44 47 49 54 52 49 51 --- 45
R06E | 1019 30 31 23 23 15 29 12 --- 9 | 66 67 63 74 71 62 63 --- 65
R07E | 1802 34 35 16 18 26 31 14 418 9 | 115 121 118 68 127 113 115 162 115
R08E | 933 36 38 21 13 20 19 13 --- 8 | 99 102 90 100 108 104 104 --- 100
R09 | 732 31 26 39 16 28 52 21 --- 13 | 31 31 36 35 39 18 25 --- 26
R10 | 961 23 29 13 23 14 34 10 --- 8 | 22 31 27 41 31 21 17 --- 22
R11 | 1163 99 105 35 33 27 70 22 --- 19 | 81 90 37 53 40 30 16 --- 27
R12 | 1321 93 94 54 38 37 37 31 81 20 | 79 87 60 77 57 28 20 13 43
R13 | 861 76 80 39 14 32 36 19 --- 15 | 62 63 44 29 30 28 18 --- 19
R14 | 1055 48 42 36 24 13 43 15 --- 12 | 38 43 36 46 30 37 31 --- 31
R15 | 1092 37 42 15 20 28 27 15 --- 10 | 34 34 30 23 38 12 13 --- 19
R16 | 1756 35 38 21 19 14 49 8 --- 9 | 31 36 27 37 25 35 21 --- 22
R18 | 497 26 29 18 17 28 17 9 139 8 | 47 51 37 44 35 22 26 41 31
R19 | 629 35 38 21 16 30 16 9 --- 9 | 53 54 42 35 23 30 33 --- 30
R20 | 750 15 21 50 15 22 71 18 --- 14 | 43 59 54 44 53 43 37 --- 41
R21 | 1059 32 23 21 12 18 45 14 74 9 | 64 58 55 53 40 21 37 53 42
R22 | 1175 31 32 23 17 14 34 17 --- 9 | 57 58 48 53 42 22 33 --- 40
R23 | 1301 29 29 20 29 11 29 12 --- 9 | 31 36 42 65 52 36 39 --- 45
R24 | 1177 17 16 27 20 15 20 15 --- 8 | 48 52 55 41 42 42 35 --- 38
XR26 | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 36 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1327 44 45 29 21 22 42 16 224 |T 62 65 58 59 58 49 47 74 51
WRMS | 1327 45 46 28 20 22 39 16 224 |NE 48 52 42 45 38 28 27 35 32
MEDI | 1059 31 31 23 18 20 34 14 139 |MD 57 58 49 53 42 36 35 53 40
Table 3.1868.3 GPS week: 1868 Day: 3 MJD: 57323
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1651 51 72 21 36 27 27 33 --- 14 | 98 105 87 103 110 90 78 --- 90
R02E | 1341 23 27 24 17 16 42 32 83 11 | 128 134 126 127 130 133 110 138 122
R03E | 1464 24 22 20 14 13 28 17 --- 8 | 124 124 124 112 117 87 113 --- 113
R04E | 1596 31 26 11 15 16 23 14 --- 8 | 111 110 106 105 111 106 101 --- 105
R05E | 2004 22 15 33 21 17 35 21 --- 11 | 75 76 81 68 80 76 75 --- 72
R06E | 1772 25 25 17 22 14 24 16 --- 8 | 94 94 102 96 96 88 87 --- 93
R07E | 1380 35 44 20 13 30 23 13 460 10 | 117 112 111 80 121 112 115 268 113
R08E | 1323 34 42 14 17 28 31 13 --- 10 | 138 141 132 132 142 133 129 --- 132
R09 | 782 31 34 48 27 20 66 27 --- 16 | 26 32 39 40 20 27 21 --- 20
R10 | 853 17 18 21 20 19 32 10 --- 8 | 24 26 32 32 26 29 18 --- 20
R11 | 2353 112 100 73 32 35 62 25 --- 24 | 86 80 84 66 47 28 28 --- 40
R12 | 851 95 98 38 42 36 56 32 80 20 | 90 99 55 81 70 28 25 31 45
R13 | 646 64 74 36 20 19 42 34 --- 15 | 64 72 55 49 42 36 20 --- 33
R14 | 789 45 42 24 38 24 37 17 --- 13 | 45 48 44 50 34 34 25 --- 32
R15 | 3318 34 30 22 24 29 17 15 --- 10 | 37 38 27 34 41 17 16 --- 20
R16 | 1898 36 38 22 30 17 35 18 --- 11 | 36 40 35 51 35 18 25 --- 28
R18 | 535 41 37 19 12 14 16 13 174 8 | 57 54 43 30 29 28 18 90 28
R19 | 876 35 31 21 13 22 29 11 --- 9 | 62 58 51 40 31 28 30 --- 35
R20 | 842 28 34 21 15 9 60 19 --- 11 | 49 47 47 45 35 18 43 --- 35
R21 | 835 29 32 18 16 17 25 16 105 8 | 64 66 50 53 47 47 40 111 45
R22 | 842 26 18 25 13 24 19 12 --- 9 | 64 58 59 50 35 50 40 --- 45
R23 | 2267 26 31 20 32 16 28 10 --- 9 | 34 31 40 73 49 31 46 --- 47
R24 | 922 18 23 41 31 16 51 21 --- 13 | 52 60 59 70 54 42 36 --- 48
XR26 | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 80 --- 80
------+---------------------------------------------------+-----------------------------------------------
RMS | 1510 44 46 30 24 22 38 20 230 |T 72 74 69 69 65 55 54 127 60
WRMS | 1510 47 46 31 21 18 36 20 230 |NE 52 53 48 50 39 30 31 77 37
MEDI | 1323 31 32 21 20 19 31 16 105 |MD 64 66 55 66 47 36 40 111 45
Table 3.1868.4 GPS week: 1868 Day: 4 MJD: 57324
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 910 46 41 30 40 37 34 50 --- 18 | 77 88 84 93 100 69 72 --- 75
R02E | 2141 30 20 19 17 17 30 11 192 8 | 158 153 165 161 163 167 155 166 160
R03E | 3064 16 24 17 17 19 26 16 --- 8 | 70 76 68 68 76 66 69 --- 67
R04E | 992 50 32 32 21 20 33 36 --- 14 | 125 134 138 126 126 133 113 --- 123
R05E | 1174 48 31 44 34 29 40 27 --- 16 | 119 141 135 146 134 133 138 --- 133
R06E | 1042 28 32 48 25 20 30 26 --- 13 | 108 113 92 107 109 110 84 --- 96
R07E | 872 43 45 20 18 26 22 31 607 12 | 162 155 153 68 165 159 149 416 157
R08E | 2569 38 36 23 21 25 29 11 --- 10 | 85 85 92 83 94 91 84 --- 86
R09 | 1102 45 33 48 36 12 60 19 --- 16 | 36 34 31 42 29 27 21 --- 24
R10 | 1562 23 19 21 22 27 31 12 --- 10 | 26 28 31 27 28 25 15 --- 15
R11 | 2336 110 110 49 22 36 27 23 --- 19 | 73 74 36 39 44 26 24 --- 20
R12 | 983 124 125 48 42 28 46 25 79 22 | 82 86 33 68 54 42 27 16 33
R13 | 866 69 50 32 18 28 33 10 --- 13 | 57 49 39 29 24 18 20 --- 20
R14 | 840 48 50 54 36 26 60 21 --- 17 | 48 60 52 44 38 40 24 --- 26
R15 | 3973 28 34 21 26 18 20 11 --- 9 | 29 36 26 31 26 16 15 --- 18
R16 | 1493 47 44 26 28 16 22 15 --- 11 | 40 44 23 46 35 15 29 --- 26
R18 | 575 24 32 13 10 16 18 22 138 7 | 50 55 42 42 54 30 24 62 37
R19 | 582 34 42 25 16 11 27 17 --- 9 | 56 61 47 33 33 40 21 --- 31
R20 | 992 21 31 22 31 18 66 17 --- 13 | 46 49 48 47 31 21 33 --- 31
R21 | 851 46 52 21 14 23 30 11 264 10 | 57 61 42 31 33 28 34 120 31
R22 | 799 38 42 38 17 22 20 13 --- 11 | 56 58 49 36 32 35 37 --- 35
R23 | 1214 29 22 25 26 22 21 14 --- 10 | 29 34 31 58 43 56 50 --- 42
R24 | 1047 31 30 32 48 18 62 14 --- 15 | 39 47 41 83 59 42 52 --- 52
XR26 | ---- --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 55 --- 55
------+---------------------------------------------------+-----------------------------------------------
RMS | 1625 51 49 33 27 23 37 22 316 |T 70 74 65 65 66 60 56 156 58
WRMS | 1625 57 57 35 26 21 34 22 316 |NE 48 51 38 43 37 30 30 66 31
MEDI | 1042 38 34 26 22 22 30 16 192 |MD 57 61 47 47 44 40 34 120 35
Table 3.1868.5 GPS week: 1868 Day: 5 MJD: 57325
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 | 1821 65 60 49 38 29 66 29 --- 19 | 61 61 72 85 92 93 76 --- 73
R02E | 2414 29 40 17 15 20 33 15 232 9 | 113 112 121 112 122 130 116 120 116
R03E | 3634 16 18 28 17 18 46 18 --- 10 | 111 115 107 110 114 96 109 --- 108
R04 | 983 48 43 46 18 26 34 15 --- 13 | 111 122 133 128 136 131 120 --- 124
R05 | 628 40 42 33 20 24 34 24 --- 12 | 87 95 112 103 111 92 103 --- 101
R06 | 2880 22 20 39 22 20 21 44 --- 13 | 113 119 131 118 130 113 83 --- 111
R07 | 708 61 51 27 20 24 42 51 --- 16 | 208 206 213 109 209 214 186 --- 194
R08 | 3120 46 29 30 18 20 28 30 --- 12 | 143 140 142 133 134 140 126 --- 132
R09 | 1366 44 52 63 20 21 38 26 --- 15 | 35 45 37 28 25 26 25 --- 18
R10 | 1816 11 19 17 24 19 16 16 --- 8 | 23 27 17 29 24 22 12 --- 17
R11 | 1783 77 77 34 25 33 43 33 --- 17 | 65 64 50 52 38 17 11 --- 33
R12 | 1006 109 107 38 22 41 51 26 80 20 | 68 68 25 47 57 39 19 13 29
R13 | 783 60 67 21 18 25 34 12 --- 11 | 47 53 24 30 23 22 16 --- 19
R14 | 961 41 36 53 34 28 67 31 --- 18 | 40 43 53 48 41 30 19 --- 31
R15 | 4059 27 24 28 17 47 32 14 --- 12 | 24 25 25 27 39 18 15 --- 17
R16 | 877 35 30 18 23 29 21 13 --- 10 | 33 35 25 29 29 14 18 --- 17
R18 | 1335 37 30 28 11 17 28 16 125 9 | 39 37 43 29 23 17 17 38 22
R19 | 741 31 32 24 10 14 36 27 --- 10 | 42 44 40 34 39 18 13 --- 27
R20 | 1072 14 24 39 26 12 65 23 --- 14 | 31 49 51 49 40 27 21 --- 33
R21 | 1442 45 48 24 15 22 41 15 259 11 | 45 50 29 30 20 20 16 54 19
R22 | 1184 46 46 27 18 25 30 17 --- 11 | 52 53 37 32 28 22 20 --- 25
R23 | 1006 23 25 19 17 12 18 10 --- 7 | 22 25 22 32 26 35 36 --- 27
R24 | 1003 27 45 34 24 23 53 19 --- 13 | 37 35 35 44 34 44 36 --- 33
XR26 | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 33 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1857 47 47 34 21 25 41 25 189 |T 67 70 67 62 66 60 51 56 56
WRMS | 1857 51 52 35 20 25 37 25 189 |NE 40 43 34 36 32 24 20 35 25
MEDI | 1184 40 40 28 20 23 34 18 125 |MD 47 53 43 47 39 30 21 38 31
Table 3.1868.6 GPS week: 1868 Day: 6 MJD: 57326
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 | 647 65 58 40 19 24 87 12 --- 16 | 66 65 71 65 73 106 69 --- 66
R02 | 3500 42 36 16 13 27 39 12 164 10 | 149 149 149 148 151 136 142 111 144
R03 | 1818 22 24 26 21 18 49 12 --- 10 | 98 94 98 85 86 78 85 --- 85
R04 | 1499 35 33 25 18 17 26 10 --- 8 | 102 104 114 97 112 102 103 --- 103
R05 | 751 41 52 33 18 26 67 20 --- 13 | 68 71 70 66 76 73 70 --- 66
R06 | 3441 36 31 28 17 14 34 16 --- 9 | 110 113 121 109 108 125 105 --- 109
XR07 |13599 239 353 252 --- 209 255 114 --- 154 | 583 625 562 --- 560 503 430 --- 468
R08 | 1771 44 44 23 15 23 23 13 --- 9 | 117 121 119 118 124 107 109 --- 114
R09 | 1117 27 18 49 31 24 26 24 --- 13 | 46 44 39 41 32 22 23 --- 26
R10 | 1016 25 18 18 19 17 34 14 --- 8 | 34 32 22 31 22 20 13 --- 16
R11 | 1010 87 90 41 20 35 39 23 --- 16 | 91 92 53 42 35 22 16 --- 27
R12 | 1068 89 83 40 25 35 47 22 87 17 | 85 83 41 55 42 37 20 15 31
R13 | 640 68 66 22 12 29 30 10 --- 11 | 65 63 31 27 29 18 14 --- 18
R14 | 842 39 43 85 21 25 67 22 --- 18 | 34 40 41 27 23 27 23 --- 19
R15 | 5972 29 31 18 10 49 23 12 --- 11 | 30 33 27 21 28 19 25 --- 18
R16 | 1111 22 26 27 22 21 29 14 --- 9 | 38 44 38 37 19 20 15 --- 22
R18 | 1100 36 50 28 12 20 17 9 157 8 | 58 65 51 39 29 36 31 35 35
R19 | 1223 40 35 30 10 15 27 12 --- 9 | 66 66 54 43 36 40 32 --- 39
R20 | 850 14 35 34 17 19 52 14 --- 10 | 47 57 55 54 47 30 41 --- 43
R21 | 1529 33 25 22 13 11 36 14 269 8 | 65 64 50 44 33 23 29 64 36
R22 | 875 40 48 22 15 25 34 14 --- 10 | 72 74 52 51 35 33 37 --- 42
R23 | 748 24 35 23 36 21 32 17 --- 11 | 34 37 38 74 49 40 48 --- 48
R24 | 1083 17 29 49 17 14 36 16 --- 11 | 62 74 55 73 53 55 56 --- 58
XR26 | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 25 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1960 44 45 35 19 25 42 16 181 |T 92 96 84 61 78 72 65 56 69
WRMS | 1960 48 48 33 19 18 37 16 181 |NE 55 57 43 43 34 29 28 38 31
MEDI | 1100 36 35 28 17 23 34 14 157 |MD 66 66 53 51 42 37 32 35 39
More information about the IGSREPORT
mailing list