[IGSREPORT-20155] Wk 1652 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 22 05:20:02 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1652 (Sep 04, 2011 - Sep 10, 2011)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths 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 2.1652.
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:
igl1652[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1652 in the SP3 format.
igl16527.sum Combination Report for GPS Week 1652.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
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).
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 | 163.1 ns
1 | 160.4 ns
2 | 161.8 ns
3 | 153.4 ns
4 | 160.4 ns
5 | 158.1 ns
6 | 153.8 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
----+--------+---------------
1 | GRG | R12
3 | ESX | R12
3 | GFZ | R04
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 1.1652, 1a.1652).
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 2.1652.0-6)
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 3.1652.0-6).
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 1652 summary. (Sep 04, 2011 - Sep 10, 2011)
Table 1.1652.a GPS week : 1652 MJD: 55808.0-55814.0
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 252| -1 0 0 27 -25 27 -.02 23 21 | --- --- --- ---
| 1 0 2 13 39 30 .05 | --- ---
esx 142| 0 0 7 21 44 -42 .47 22 20 | 158551 -1060 4899 5060
| 1 1 3 26 31 56 .04 | 4352 5167
gfz 197| 0 0 0 0 0 52 -.20 23 21 | 0 -2221 4908 8989
| 1 1 3 14 56 25 .06 | 0 4924
grg 129| 0 1 -13 -53 -25 78 .02 48 46 | --- --- --- ---
| 2 1 3 56 91 60 .06 | --- ---
iac n/a| 0 0 -3 -34 -10 -54 -.29 23 23 | 1331617 4014 206234 717024
| 1 0 2 29 14 35 .05 | 3271961 17054
mcc n/a| 2 4 23 -4 -3 -217 -.14 127 127 | --- --- --- ---
| 4 6 9 96 77 319 .26 | --- ---
Table 1.1652.b GPS week : 1652 MJD: 55808.0-55814.0
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 | 14 12 17 20 13 11 11 |
R02 | 11 12 11 11 11 11 12 |
R03 | 13 10 10 15 11 8 10 |
R04 | 12 15 11 73 29 30 24 |
R05 | 10 9 10 12 13 12 11 |
R06 | 11 9 11 12 13 13 12 |
R07 | 10 10 11 19 13 14 13 |
R08 | 13 11 10 12 10 8 12 |
R09 | 12 11 11 11 11 19 13 |
R10 | 13 11 10 9 18 13 15 |
R11 | 17 16 21 18 18 16 15 |
R12 | 15 28 33 21 30 12 11 |
R13 | 11 15 9 10 13 11 11 |
R15 | 11 13 11 11 11 12 14 |
R16 | 10 12 10 10 12 17 11 |
R17 | 17 18 22 23 19 17 15 |
R18 | 10 10 10 12 9 13 11 |
R19 | 10 11 14 13 15 11 14 |
R20 | 14 16 16 17 17 16 16 |
R21 | 14 10 12 13 9 11 11 |
R22 | 10 21 9 11 12 13 12 |
R23 | 12 15 13 9 9 11 9 |
R24 | 14 11 11 12 12 12 14 |
Table 1.1652.c GPS week : 1652 MJD: 55808.0-55814.0
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 1652 0 | -137 -11 82 501 -869 -5972 85.9 2426 2426 | 163063 0
brd 1652 1 | 18 69 66 -596 -20 -16970 86.0 1795 1795 | 160421 0
brd 1652 2 | -133 -14 -4 209 -826 -18680 85.3 2076 2076 | 161802 0
brd 1652 3 | 36 44 48 -479 141 -13610 83.3 2208 2208 | 153357 0
brd 1652 4 | -13 43 82 91 -3367 -18410 82.3 2424 2424 | 160351 0
brd 1652 5 | -52 72 71 -2162 -1543 -15100 83.6 2342 2342 | 158130 0
brd 1652 6 | -16 -91 126 -8 -4332 -20490 83.2 2302 2302 | 153775 0
-------------+------------------------------------------------------------+----------------
brd 1652 mean| -42 16 67 -349 -1545 -15604 84.2 2224 2224 | 158699 0
brd 1652 sdev| 69 58 39 886 1694 4831 1.5 226 226 | 3818 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 2.1652.0 GPS week: 1652 Day: 0 MJD: 55808
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 252| 0 0 -1 22 29 47 .07 23 21 | --- --- --- ---
esx 142| -1 -1 8 -6 68 49 .47 19 17 | 162748 -559 4091 4252
gfz 197| -2 1 0 -24 -73 54 -.19 23 19 | 0 -2335 4124 8515
grg 129| 2 3 -12 17 -72 0 .10 51 46 | --- --- --- ---
iac n/a| 0 0 -6 8 -29 -96 -.33 21 21 | 165069 -405 4103 8199
mcc n/a| 6 2 12 -73 11 -529 -.08 103 103 | --- --- --- ---
Table 2.1652.1 GPS week: 1652 Day: 1 MJD: 55809
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 252| -2 0 0 46 -11 23 -.03 23 21 | --- --- --- ---
esx 142| 0 -1 10 -12 37 -34 .45 22 20 | 161728 -3116 5211 5352
gfz 197| 0 0 -3 8 -24 35 -.15 20 19 | 0 -5524 5200 11162
grg 129| 2 1 -17 -68 15 167 -.02 52 53 | --- --- --- ---
iac n/a| 0 0 -1 -8 -1 -52 -.30 22 22 | 162449 -2648 5231 10979
mcc n/a| 2 1 18 81 95 -254 -.10 97 97 | --- --- --- ---
Table 2.1652.2 GPS week: 1652 Day: 2 MJD: 55810
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 252| -3 0 0 28 -53 54 -.01 22 20 | --- --- --- ---
esx 142| 0 0 10 38 19 -126 .45 24 21 | 160180 2119 5453 5641
gfz 197| 0 0 1 1 28 34 -.27 24 20 | 0 1439 5334 10147
grg 129| -2 2 -14 -6 38 68 .02 44 38 | --- --- --- ---
iac n/a| 0 0 -7 -50 0 -31 -.20 22 22 | 5083785 42243 999999 999999
mcc n/a| 2 3 19 50 43 -385 .28 104 104 | --- --- --- ---
Table 2.1652.3 GPS week: 1652 Day: 3 MJD: 55811
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 252| 0 0 1 17 -71 33 -.08 23 22 | --- --- --- ---
esx 142| -1 1 4 30 27 -21 .53 23 19 | 160321 -11541 6074 6291
gfz 197| 0 -1 1 -13 82 19 -.17 28 24 | 0 -10694 6039 9415
grg 129| -2 1 -7 -140 -14 103 .07 51 47 | --- --- --- ---
iac n/a| 2 -1 -7 -66 6 -46 -.35 25 25 | 6910016 -5473 6069 999999
mcc n/a| 8 1 21 134 39 -213 -.14 116 116 | --- --- --- ---
Table 2.1652.4 GPS week: 1652 Day: 4 MJD: 55812
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 252| 0 1 3 32 -14 49 -.02 22 20 | --- --- --- ---
esx 142| -2 0 8 22 1 -57 .49 23 22 | 160037 316 4303 4436
gfz 197| 0 0 -3 8 49 75 -.23 22 20 | 0 1250 4390 8572
grg 129| 2 2 -13 -97 -191 125 -.02 46 43 | --- --- --- ---
iac n/a| 2 0 -2 -12 -7 -74 -.26 24 24 | -999999 -5147 419060 999999
mcc n/a| -5 13 35 -31 -1 212 -.14 149 149 | --- --- --- ---
Table 2.1652.5 GPS week: 1652 Day: 5 MJD: 55813
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 252| -3 0 -2 4 -70 -33 -.06 25 22 | --- --- --- ---
esx 142| -2 -2 1 11 78 -15 .49 21 18 | 153613 4401 5019 5145
gfz 197| 0 1 5 16 -12 92 -.25 22 21 | 0 3764 5110 7170
grg 129| 0 -1 -16 -11 -49 77 -.06 47 45 | --- --- --- ---
iac n/a| 0 1 -1 -47 -8 -88 -.33 24 24 | -999999 1960 5022 999999
mcc n/a| 0 13 39 -139 -111 209 -.21 145 145 | --- --- --- ---
Table 2.1652.6 GPS week: 1652 Day: 6 MJD: 55814
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 252| -1 0 0 39 11 15 -.03 24 23 | --- --- --- ---
esx 142| 1 -2 7 63 80 -90 .42 20 20 | 151230 954 4148 4306
gfz 197| 0 0 -2 7 -54 53 -.11 24 22 | 0 -3449 4165 7947
grg 129| 0 2 -12 -69 93 6 .02 49 51 | --- --- --- ---
iac n/a| 0 0 -1 -61 -31 6 -.29 19 19 | -999999 -2432 4159 999999
mcc n/a| 0 -2 18 -49 -103 -563 -.60 176 176 | --- --- --- ---
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 3.1652.0 GPS week: 1652 Day: 0 MJD: 55808
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1105 24 16 25 68 19 --- 13 | 29 62 58 57 50 --- 44
R02 | 1399 12 13 13 58 22 --- 11 | 51 58 45 59 31 --- 44
R03 | 2577 12 15 17 75 19 --- 12 | 31 34 30 68 30 --- 28
XR04 | 3730 22 21 15 --- 21 --- 12 | 221 120 405 --- 205 --- 211
R05 | 635 23 13 17 41 17 89 10 | 67 59 50 37 56 35 54
R06 | 1084 17 22 12 54 16 --- 11 | 48 55 38 44 42 --- 41
R07 | 3160 11 27 16 29 17 --- 10 | 61 74 61 69 54 --- 61
R08 | 1916 14 16 25 55 27 144 12 | 59 65 60 56 61 52 59
R09 | 1125 23 16 21 49 18 --- 11 | 67 82 85 61 75 --- 74
XR10 | 1175 26 20 15 --- 25 --- 13 | 34 46 39 --- 55 --- 40
R11 | 1790 45 25 26 50 26 91 16 | 59 77 86 43 61 32 63
R12 | 1641 22 19 21 80 20 --- 14 | 81 217 86 149 82 --- 86
XR13 | 2457 24 17 13 --- 17 --- 10 | 49 60 65 --- 59 --- 56
R15 | 7086 26 13 16 42 18 75 10 | 44 38 37 55 41 36 36
R16 | 1182 21 15 18 32 15 --- 9 | 86 88 90 88 77 --- 84
R17 | 2181 38 25 31 56 34 --- 17 | 44 82 75 71 103 --- 73
R18 | 1477 19 14 25 26 15 100 9 | 24 19 24 25 25 49 16
R19 | 1725 16 12 20 45 12 --- 9 | 35 25 26 51 34 --- 26
R20 | 3489 29 23 37 25 25 --- 14 | 42 48 63 52 44 --- 43
R21 | 730 27 27 19 38 30 --- 13 | 43 22 31 42 30 --- 29
XR22 | 1534 19 14 19 --- 18 --- 10 | 33 21 19 --- 25 --- 20
R23 | 1197 18 16 26 51 21 --- 12 | 32 27 28 44 37 --- 28
R24 | 1978 16 25 31 48 24 --- 13 | 24 46 39 48 34 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 2425 23 19 23 51 21 102 |T 54 61 66 58 57 40 54
WRMS | 2425 21 17 19 46 21 102 |NE 54 61 66 58 57 40 54
MEDI | 1641 22 16 19 49 19 91 |MD 44 58 50 55 50 36 44
Table 3.1652.1 GPS week: 1652 Day: 1 MJD: 55809
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 864 13 24 13 60 21 --- 12 | 23 39 33 43 37 --- 30
R02 | 2226 23 22 21 36 19 --- 11 | 35 50 34 40 27 --- 31
R03 | 2655 15 11 20 47 17 --- 10 | 27 28 39 65 28 --- 26
XR04 | 4885 23 26 29 --- 21 --- 14 | 272 167 466 --- 260 --- 262
R05 | 1156 13 18 14 30 16 101 8 | 40 61 40 56 49 33 45
R06 | 1198 15 16 18 27 17 --- 9 | 33 32 16 30 33 --- 24
R07 | 4152 16 15 21 47 11 --- 10 | 39 36 34 35 43 --- 33
R08 | 908 23 16 12 52 17 136 11 | 43 37 33 22 35 28 31
R09 | 822 24 17 14 40 17 --- 10 | 75 79 66 62 70 --- 70
R10 | 1341 17 24 17 38 20 --- 11 | 36 44 33 53 40 --- 35
R11 | 1562 37 26 21 49 32 95 15 | 33 52 51 39 53 35 41
XR12 | ---- 35 --- 50 236 27 --- 28 | 78 --- 62 97 89 --- 75
R13 | 1765 32 15 21 67 21 --- 14 | 61 73 79 72 67 --- 70
R15 | 1491 20 15 28 41 30 81 13 | 37 38 43 52 49 27 37
R16 | 879 21 25 9 49 20 --- 11 | 90 83 85 102 88 --- 86
R17 | 2522 40 36 22 49 39 --- 18 | 37 74 55 67 82 --- 58
R18 | 1976 18 15 20 34 13 52 9 | 25 20 23 42 20 31 17
R19 | 638 19 13 24 48 15 --- 11 | 22 18 40 50 21 --- 20
R20 | 1245 27 26 32 24 40 --- 16 | 24 35 36 50 45 --- 28
R21 | 2017 18 21 21 35 13 --- 10 | 26 18 25 41 26 --- 18
R22 | 537 28 19 20 125 24 --- 20 | 24 26 26 51 20 --- 16
R23 | 1102 21 38 12 69 13 --- 14 | 27 35 22 49 25 --- 21
R24 | 2278 24 21 19 29 22 --- 11 | 20 33 34 49 31 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1794 23 22 20 52 22 97 |T 49 49 59 53 53 30 47
WRMS | 1794 21 20 19 53 22 97 |NE 49 49 59 53 53 30 47
MEDI | 1341 21 19 20 47 20 95 |MD 35 37 36 50 40 31 31
Table 3.1652.2 GPS week: 1652 Day: 2 MJD: 55810
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 996 17 41 26 72 25 --- 17 | 29 71 45 68 26 --- 37
R02 | 1598 22 18 15 35 23 --- 11 | 41 40 37 36 17 --- 29
R03 | 2608 15 17 17 43 18 --- 10 | 28 35 34 45 23 --- 24
XR04 | 4903 20 18 19 --- 17 --- 11 | 202 227 442 --- 189 --- 199
R05 | 883 12 15 21 33 22 93 10 | 53 65 50 49 58 30 54
R06 | 1507 12 21 22 43 12 --- 10 | 43 37 43 46 42 --- 38
XR07 | 2967 10 19 --- 42 11 --- 11 | 41 34 --- 39 35 --- 35
R08 | 2979 12 15 20 33 23 148 10 | 36 36 43 55 30 31 34
R09 | 1354 23 22 22 28 15 --- 10 | 46 59 59 50 52 --- 50
R10 | 1906 12 17 20 36 17 --- 9 | 27 33 29 39 38 --- 28
R11 | 1276 40 36 38 67 32 119 20 | 28 77 70 64 57 31 48
XR12 | 3482 32 --- --- --- 33 --- 32 | 53 --- --- --- 33 --- 42
R13 | 1057 15 17 21 30 15 --- 9 | 40 40 47 38 42 --- 41
R15 | 2468 17 19 21 31 22 70 10 | 37 31 33 47 34 33 30
R16 | 896 20 13 19 34 16 --- 9 | 53 67 67 47 59 --- 58
R17 | 5486 50 38 33 48 43 --- 21 | 32 82 75 56 95 --- 61
R18 | 1806 17 25 14 27 18 66 10 | 23 21 20 22 22 40 13
R19 | 900 16 19 22 69 13 --- 13 | 31 30 32 55 34 --- 26
R20 | 3024 20 21 44 57 27 --- 16 | 46 35 65 57 56 --- 44
R21 | 1815 21 20 20 41 23 --- 11 | 38 36 31 40 28 --- 29
R22 | 1034 19 19 18 25 13 --- 9 | 32 28 25 43 28 --- 23
R23 | 720 18 27 25 46 14 --- 12 | 30 31 33 31 32 --- 24
R24 | 757 18 25 14 30 23 --- 11 | 22 26 20 30 24 --- 16
------+-----------------------------------------+-------------------------------------
RMS | 2075 22 24 24 44 22 104 |T 43 51 61 45 45 33 42
WRMS | 2075 20 21 20 38 22 104 |NE 43 51 61 45 45 33 42
MEDI | 1598 18 19 21 36 18 93 |MD 37 36 43 46 34 31 35
Table 3.1652.3 GPS week: 1652 Day: 3 MJD: 55811
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 840 22 50 27 62 39 --- 19 | 31 88 68 38 20 --- 46
R02 | 1097 19 11 16 52 19 --- 10 | 35 35 24 49 26 --- 27
R03 | 3117 16 23 21 82 22 --- 15 | 35 44 44 43 37 --- 32
XR04 |24008 67 --- 3255 --- 78 --- 72 | 432 --- 9999 --- 353 --- 394
R05 | 1590 21 15 26 53 15 88 12 | 65 56 64 44 52 67 55
R06 | 1796 12 13 25 57 21 --- 12 | 47 50 55 34 44 --- 44
R07 | 3986 35 10 63 59 22 --- 19 | 52 37 55 77 34 --- 34
R08 | 4203 25 20 30 36 10 139 12 | 45 31 35 43 35 59 31
R09 | 804 21 16 23 31 21 --- 10 | 91 102 95 87 87 --- 92
R10 | 2351 12 6 18 42 19 --- 9 | 41 51 41 47 59 --- 44
R11 | 926 39 32 40 47 29 170 18 | 46 80 88 61 67 54 64
XR12 | 1229 19 297 --- --- 22 --- 20 | 100 152 --- --- 83 --- 93
R13 | 1254 18 14 17 35 21 --- 9 | 68 77 76 52 66 --- 70
R15 | 3046 13 19 18 46 22 63 11 | 47 45 41 61 61 51 45
R16 | 1029 15 15 18 43 16 --- 10 | 98 107 106 109 110 --- 104
R17 | 3917 46 42 41 43 53 --- 23 | 35 83 61 45 104 --- 60
R18 | 1554 23 20 20 40 20 87 11 | 28 22 22 32 23 68 14
R19 | 865 13 22 13 62 29 --- 13 | 36 33 31 38 44 --- 32
R20 | 3452 20 27 21 82 34 --- 17 | 44 45 40 71 45 --- 38
R21 | 810 17 22 24 61 15 --- 13 | 33 32 39 50 30 --- 28
R22 | 629 17 22 20 25 26 --- 11 | 31 29 26 29 30 --- 22
R23 | 709 15 15 20 22 18 --- 8 | 29 35 39 48 37 --- 32
R24 | 677 19 20 28 36 21 --- 11 | 28 15 29 46 35 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 2207 23 23 27 51 25 116 |T 65 56 51 52 64 59 61
WRMS | 2207 22 19 24 47 25 116 |NE 65 56 51 52 64 59 61
MEDI | 1254 19 20 21 46 21 88 |MD 44 45 41 47 44 59 44
Table 3.1652.4 GPS week: 1652 Day: 4 MJD: 55812
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1177 22 31 15 47 24 --- 13 | 39 43 27 54 27 --- 28
R02 | 736 22 18 22 36 15 --- 10 | 29 39 36 41 31 --- 29
R03 | 4306 10 27 12 43 18 --- 10 | 30 42 36 48 30 --- 30
XR04 | 6113 28 --- --- --- 28 --- 28 | 380 --- --- --- 363 --- 371
R05 | 1710 24 26 14 52 17 80 12 | 63 64 50 36 35 44 47
R06 | 1442 19 16 15 63 18 --- 12 | 51 50 40 43 41 --- 39
R07 | 6420 15 25 25 45 24 --- 12 | 41 57 40 51 32 --- 36
R08 | 2912 14 24 18 23 23 153 10 | 47 64 43 46 33 68 43
R09 | 1237 19 23 17 48 14 --- 11 | 87 76 83 114 93 --- 86
R10 | 2610 14 20 41 46 49 --- 18 | 52 58 60 40 44 --- 47
R11 | 1226 41 39 27 55 26 236 18 | 33 71 59 51 42 64 43
XR12 | 1541 22 --- 55 111 30 --- 29 | 86 --- 123 121 98 --- 83
R13 | 2265 15 22 15 56 28 --- 12 | 60 74 66 52 46 --- 58
R15 | 3610 14 16 23 34 27 118 11 | 53 58 61 58 40 27 50
R16 | 1156 18 14 23 49 18 --- 11 | 114 108 108 111 108 --- 107
R17 | 2031 43 31 32 56 36 --- 19 | 37 68 51 89 83 --- 57
R18 | 2393 19 19 19 13 14 108 9 | 21 19 18 27 21 73 13
R19 | 1291 25 19 27 57 27 --- 14 | 28 30 27 47 36 --- 24
R20 | 2143 25 34 29 49 36 --- 16 | 28 45 47 68 54 --- 38
R21 | 795 16 12 16 35 12 --- 8 | 33 24 29 45 29 --- 25
R22 | 703 23 21 10 45 23 --- 11 | 31 33 35 50 22 --- 25
R23 | 831 16 12 16 38 14 --- 9 | 30 19 28 46 32 --- 22
R24 | 983 24 19 19 46 15 --- 11 | 32 32 28 49 29 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2424 22 23 22 46 24 149 |T 61 51 49 58 59 55 57
WRMS | 2424 20 22 20 43 24 149 |NE 61 51 49 58 59 55 57
MEDI | 1541 19 21 19 46 23 118 |MD 39 50 40 49 36 64 39
Table 3.1652.5 GPS week: 1652 Day: 5 MJD: 55813
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2316 17 16 11 52 22 --- 11 | 27 30 28 59 19 --- 23
R02 | 1102 19 11 19 48 16 --- 10 | 33 27 38 44 40 --- 29
R03 | 2905 16 17 15 25 11 --- 8 | 30 46 30 40 28 --- 31
XR04 | 1507 37 51 --- --- 34 --- 29 | 396 95 --- --- 372 --- 389
R05 | 1398 30 16 21 44 15 64 11 | 54 45 51 27 36 38 39
R06 | 1176 28 21 14 55 20 --- 13 | 46 27 33 36 40 --- 29
R07 | 5938 19 11 29 75 13 --- 14 | 47 34 48 55 37 --- 36
R08 | 1081 9 8 20 27 16 198 7 | 37 44 51 48 39 37 41
R09 | 1165 26 35 30 64 44 --- 19 | 138 156 140 130 140 --- 139
R10 | 1391 24 13 20 62 24 --- 13 | 49 51 55 44 40 --- 43
R11 | 1249 42 28 23 45 27 202 16 | 41 80 77 51 59 46 61
R12 | 1344 25 20 19 47 20 --- 12 | 135 94 112 104 134 --- 130
R13 | 2051 24 16 22 38 15 --- 10 | 68 77 77 72 57 --- 70
R15 | 3837 23 21 22 29 29 102 12 | 45 48 51 57 47 28 45
R16 | 946 26 23 26 43 49 --- 17 | 192 190 187 171 169 --- 181
R17 | 2490 44 24 27 53 29 --- 17 | 35 68 71 52 74 --- 58
R18 | 3340 27 16 27 48 15 106 12 | 22 31 37 55 24 53 22
R19 | 1718 20 22 21 37 16 --- 11 | 31 39 27 32 38 --- 29
R20 | 3939 28 33 22 47 32 --- 15 | 42 49 52 55 36 --- 37
R21 | 787 18 21 20 37 16 --- 10 | 36 30 38 50 36 --- 31
R22 | 659 28 14 31 38 21 --- 12 | 30 26 43 42 24 --- 26
R23 | 1348 15 22 21 39 14 --- 10 | 36 32 26 35 31 --- 27
R24 | 817 18 22 20 46 22 --- 12 | 33 35 33 39 27 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2342 25 21 22 47 24 145 |T 69 58 59 59 67 40 67
WRMS | 2342 22 18 21 45 24 145 |NE 69 58 59 59 67 40 67
MEDI | 1391 24 21 21 45 20 106 |MD 41 45 48 50 39 38 37
Table 3.1652.6 GPS week: 1652 Day: 6 MJD: 55814
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2453 15 19 19 49 14 --- 10 | 39 52 51 46 35 --- 40
R02 | 1560 24 22 21 47 14 --- 11 | 49 55 39 39 37 --- 40
R03 | 1246 16 18 15 46 12 --- 9 | 32 33 30 45 27 --- 27
XR04 | 1414 41 49 --- 63 27 --- 24 | 322 158 --- 3 308 --- 321
R05 | 1114 19 21 14 49 19 116 11 | 73 72 60 36 54 31 60
R06 | 1092 20 20 23 53 17 --- 12 | 66 54 69 31 72 --- 60
R07 | 2770 21 21 28 57 12 --- 12 | 67 67 59 46 54 --- 57
R08 | 1243 25 11 17 67 9 305 11 | 61 56 54 59 46 65 51
R09 | 1039 19 19 33 37 26 --- 13 | 136 140 147 135 109 --- 130
R10 | 1507 23 19 22 73 26 --- 14 | 45 48 48 43 51 --- 44
R11 | 1177 30 21 23 63 25 134 15 | 38 53 44 51 52 57 41
R12 | 1282 25 20 21 37 14 --- 10 | 172 137 152 117 161 --- 167
R13 | 2442 17 28 13 38 18 --- 11 | 49 47 50 68 43 --- 46
R15 | 3190 21 17 35 36 29 117 13 | 49 55 69 59 47 34 50
R16 | 1182 20 14 19 43 24 --- 11 | 183 178 182 201 155 --- 174
R17 | 2853 44 23 17 40 25 --- 15 | 54 92 79 90 105 --- 82
R18 | 3903 25 19 18 48 12 128 11 | 40 23 24 49 26 55 22
R19 | 1330 26 28 29 32 24 --- 13 | 32 48 46 36 28 --- 31
R20 | 6430 28 24 28 73 24 --- 16 | 40 34 39 35 37 --- 30
R21 | 1020 22 16 26 38 12 --- 10 | 32 26 33 33 32 --- 25
R22 | 1322 31 25 17 34 13 --- 11 | 33 25 20 33 27 --- 21
R23 | 1014 15 16 22 32 10 --- 8 | 32 28 35 36 30 --- 27
R24 | 803 24 10 43 51 15 --- 14 | 32 28 34 39 29 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 2301 24 20 24 49 19 176 |T 72 65 62 57 68 48 68
WRMS | 2301 23 20 22 51 19 176 |NE 72 65 62 57 68 48 68
MEDI | 1322 23 20 21 47 17 128 |MD 49 53 48 45 46 55 44
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