[IGSREPORT-17175] Wk 1519 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Mar 5 06:44:25 PST 2009
******************************************************************************
IGS Electronic Report 05 Mar 06:44:27 PST 2009 Message Number 17175
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1519 (Feb 15, 2009 - Feb 21, 2009)
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 centers
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 2.1519.
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:
igl1519[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1519 in the SP3 format.
igl15197.sum Combination Report for GPS Week 1519.
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.
3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151]
BKG, ESA, and CODE will start to refer their GLONASS orbit products
to the following satellite antenna offset (SAO) values:
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.
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 254.6 ns
1 | 138.3 ns
2 | 235.7 ns
3 | 241.5 ns
4 | 245.0 ns
5 | 237.3 ns
6 | 235.9 ns
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 1.1519, 1a.1519).
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 2.1519.0-6)
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 3.1519.0-6).
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 1519 summary. (Feb 15, 2009 - Feb 21, 2009)
Table 1.1519.a GPS week : 1519 MJD: 54877.0-54883.0
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]
--------+----------------------------------------------------+------------------------------
bkg 96| 0 0 0 -1 7 -71 -.09 27 25 | 0 -74 2065 2142
| 0 1 3 32 19 113 .05 | 0 114
cod 236| 0 0 1 20 -14 64 -.14 15 13 | --- --- --- ---
| 0 1 1 12 22 42 .02 | --- ---
esx 130| 0 -1 0 -15 44 41 .38 28 25 | 106049 -1623 5707 11378
| 1 2 4 30 37 72 .07 | 40455 2614
iac n/a| 0 0 -4 -11 -32 -125 -.04 28 28 | 226965 -1207 5701 10842
| 1 1 4 24 20 84 .06 | 40065 1546
mcc n/a| -2 -1 18 -1 -62 -386 .11 98 98 | --- --- --- ---
| 8 5 7 136 158 398 .35 | --- ---
Table 1.1519.b GPS week : 1519 MJD: 54877.0-54883.0
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
------+------------------------------------+------------------------------------------
R02 | 14 12 12 11 11 11 11 |
R03 | 12 8 16 12 9 12 14 |
R04 | 13 18 13 12 12 15 17 |
R06 | 186 101 78 71 63 48 43 |
R07 | 11 16 14 9 12 13 13 |
R08 | 9 14 15 13 11 13 9 |
R10 | 12 16 14 11 12 9 9 |
R11 | 12 13 14 18 8 15 9 |
R13 | 13 15 13 12 17 17 12 |
R14 | 13 8 15 10 9 18 9 |
R15 | 12 14 11 15 11 16 12 |
R17 | 13 19 16 11 12 12 18 |
R18 | 9 12 10 10 9 11 18 |
R19 | 10 11 11 11 11 9 9 |
R20 | 15 14 20 13 15 19 13 |
R21 | 14 10 10 10 11 11 18 |
R22 | 13 13 11 11 12 12 10 |
R23 | 20 16 19 22 16 14 18 |
R24 | 40 15 14 25 --- 0 0 |
Table 1.1519.c GPS week : 1519 MJD: 54877.0-54883.0
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 1519 0 | -80 -37 139 -322 2033 -1101 97.3 >>>>> >>>>> | 254646 0
brd 1519 1 | ---- -341 6188 2734 -612300 -12130 77.3 >>>>> >>>>> | 138276 0
brd 1519 2 | -22 -189 117 -100 4085 -13880 113.2 >>>>> >>>>> | 235704 0
brd 1519 3 | -106 -81 14 5413 1490 -16970 98.8 >>>>> >>>>> | 241521 0
brd 1519 4 | 215 42 -25 1942 -4066 -16190 84.9 >>>>> >>>>> | 244953 0
brd 1519 5 | -95 182 22 -192 -3106 -13270 95.1 >>>>> >>>>> | 237334 0
brd 1519 6 | -21 -54 1020 402 -2582 -16480 99.5 >>>>> >>>>> | 235889 0
-------------+------------------------------------------------------------+----------------
brd 1519 mean| ---- -68 1068 1410 -87777 -12860 95.2 >>>>> >>>>> | 226903 0
brd 1519 sdev|71503 166 2286 2118 231312 5493 11.4 >>>>> >>>>> | 39646 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 2.1519.0 GPS week: 1519 Day: 0 MJD: 54877
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]
--------+----------------------------------------------------+------------------------------
bkg 96| 1 1 0 3 0 -10 -.13 39 29 | 0 -142 2053 2106
cod 236| -1 -1 0 16 -33 42 -.11 19 14 | --- --- --- ---
esx 130| 2 0 -1 3 83 124 .30 23 22 | 138338 931 6032 11020
iac n/a| 0 -1 0 -4 -51 -251 -.13 28 28 | 252342 823 6026 10489
mcc n/a| -7 -5 16 -4 201 -575 .22 106 106 | --- --- --- ---
Table 2.1519.1 GPS week: 1519 Day: 1 MJD: 54878
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]
--------+----------------------------------------------------+------------------------------
bkg 96| 0 1 2 -47 -19 134 -.02 21 21 | 0 37 2106 2294
cod 236| 0 -1 1 37 -15 1 -.14 17 15 | --- --- --- ---
esx 130| -1 0 3 18 94 -18 .38 30 28 | 17230 -2023 7827 12065
iac n/a| 0 0 -8 -19 -36 -208 .03 29 29 | 137074 501 7826 12079
mcc n/a| -10 -8 6 -108 -118 -355 .52 107 107 | --- --- --- ---
Table 2.1519.2 GPS week: 1519 Day: 2 MJD: 54879
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]
--------+----------------------------------------------------+------------------------------
bkg 96| 1 0 2 -16 -2 -132 -.07 32 32 | 0 -52 2505 2593
cod 236| 0 -1 0 -3 1 83 -.13 14 14 | --- --- --- ---
esx 130| 0 -3 1 -38 9 -9 .37 27 25 | 124743 -5807 7010 11343
iac n/a| 2 2 -2 17 -14 -88 -.10 29 29 | 236883 -3640 7001 10898
mcc n/a| -4 -3 18 178 -106 103 -.47 94 94 | --- --- --- ---
Table 2.1519.3 GPS week: 1519 Day: 3 MJD: 54880
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]
--------+----------------------------------------------------+------------------------------
bkg 96| 0 1 6 -13 19 -115 -.13 23 23 | 0 72 1814 1857
cod 236| 0 1 3 31 -37 21 -.15 13 12 | --- --- --- ---
esx 130| -2 -5 -8 -68 23 101 .49 30 26 | 118230 -4509 5518 10827
iac n/a| 0 1 -8 13 -20 -60 -.06 24 24 | 243545 -1658 5509 10365
mcc n/a| 1 8 27 185 -93 205 -.24 84 84 | --- --- --- ---
Table 2.1519.4 GPS week: 1519 Day: 4 MJD: 54881
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]
--------+----------------------------------------------------+------------------------------
bkg 96| 0 0 -1 -17 16 -179 -.11 21 20 | 0 -237 2103 2184
cod 236| -2 1 3 21 -37 115 -.17 12 12 | --- --- --- ---
esx 130| 0 -3 0 8 12 -10 .43 24 23 | 124651 168 4792 9247
iac n/a| 0 2 -5 -25 -9 -24 .02 29 29 | 245323 -821 4773 8895
mcc n/a| 10 3 14 -1 67 -745 .36 100 100 | --- --- --- ---
Table 2.1519.5 GPS week: 1519 Day: 5 MJD: 54882
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]
--------+----------------------------------------------------+------------------------------
bkg 96| 0 0 -5 33 -2 -174 -.04 22 22 | 0 -177 2110 2152
cod 236| 0 1 0 18 19 105 -.14 16 16 | --- --- --- ---
esx 130| 2 -1 4 -19 75 130 .28 30 27 | 112708 393 4333 12221
iac n/a| -2 0 3 -8 -66 -78 .00 26 26 | 238151 -2200 4350 11852
mcc n/a| -9 -2 25 -112 -304 -797 .25 97 97 | --- --- --- ---
Table 2.1519.6 GPS week: 1519 Day: 6 MJD: 54883
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]
--------+----------------------------------------------------+------------------------------
bkg 96| 1 -4 -1 45 41 -19 -.13 30 29 | 0 -20 1767 1814
cod 236| -1 0 0 18 -1 79 -.13 12 11 | --- --- --- ---
esx 130| -1 3 3 -10 14 -24 .42 29 25 | 106447 -517 4440 12929
iac n/a| 1 -1 -7 -52 -30 -168 -.03 28 28 | 235442 -1455 4423 11317
mcc n/a| 5 -6 18 -145 -85 -543 .09 100 100 | --- --- --- ---
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 3.1519.0 GPS week: 1519 Day: 0 MJD: 54877
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 29 7 33 20 --- 13 | 25 26 38 35 --- 27
R03 |>>>>> 15 19 26 15 --- 11 | 24 29 35 31 --- 26
R04 |>>>>> 24 17 27 14 --- 12 | 25 34 39 34 --- 31
XR06 | ---- --- 138 --- 248 --- 186 | --- 130 --- 197 --- 145
R07 |>>>>> 15 15 23 22 --- 11 | 22 32 33 23 --- 22
R08 |>>>>> 17 9 17 20 --- 9 | 24 29 45 29 --- 29
R10 |>>>>> 26 12 25 19 --- 11 | 20 18 32 27 --- 19
R11 |>>>>> 24 13 21 25 94 11 | 22 30 38 30 31 28
R13 |>>>>> 36 11 24 16 --- 12 | 22 25 39 23 --- 20
R14 |>>>>> 26 16 21 29 --- 13 | 24 19 36 21 --- 18
R15 |>>>>> 28 9 15 33 116 12 | 30 22 25 34 34 17
R17 |>>>>> 16 19 16 32 --- 12 | 39 32 47 62 --- 41
R18 |>>>>> 18 10 15 18 --- 8 | 18 22 32 31 --- 21
R19 |>>>>> 14 11 13 26 --- 9 | 17 19 30 29 --- 19
R20 |>>>>> 23 27 20 34 --- 15 | 21 37 32 24 --- 24
R21 |>>>>> 17 25 27 17 --- 13 | 22 34 30 31 --- 24
R22 |>>>>> 24 15 21 31 --- 13 | 26 25 26 39 --- 25
R23 |>>>>> 44 22 21 52 --- 20 | 68 93 101 99 --- 90
R24 |>>>>> 130 48 33 52 --- 39 | 63 9999 51 49 --- 9999
------+------------------------------------+--------------------------------
RMS |>>>>> 39 19 23 28 106 |T 28 36 39 44 32 34
WRMS |>>>>> 29 14 22 28 106 |NE 28 36 39 44 32 34
MEDI |>>>>> 24 15 21 25 94 |MD 24 29 35 31 31 24
Table 3.1519.1 GPS week: 1519 Day: 1 MJD: 54878
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 13 16 29 26 --- 12 | 22 27 36 20 --- 21
R03 |>>>>> 12 13 16 17 --- 8 | 18 25 24 22 --- 18
R04 |>>>>> 18 25 50 31 --- 18 | 24 29 61 26 --- 28
XR06 | ---- --- 71 --- 140 --- 100 | --- 167 --- 222 --- 183
R07 |>>>>> 31 26 25 21 --- 15 | 26 33 39 24 --- 22
R08 |>>>>> 22 19 29 24 --- 13 | 26 27 39 25 --- 20
R10 |>>>>> 20 16 51 24 --- 16 | 17 17 55 13 --- 15
R11 |>>>>> 27 11 30 24 118 13 | 20 24 49 23 16 20
R13 |>>>>> 22 18 36 30 --- 15 | 10 31 30 31 --- 16
R14 |>>>>> 14 6 22 12 --- 7 | 10 17 40 17 --- 16
R15 |>>>>> 16 12 42 21 94 13 | 12 18 48 23 23 14
R17 |>>>>> 24 24 19 59 --- 19 | 26 28 34 53 --- 27
R18 |>>>>> 27 6 24 24 --- 12 | 24 19 32 29 --- 17
R19 |>>>>> 21 8 20 24 --- 10 | 19 13 20 18 --- 9
R20 |>>>>> 19 21 20 38 --- 14 | 19 29 27 30 --- 21
R21 |>>>>> 14 11 26 16 --- 9 | 27 27 43 27 --- 26
R22 |>>>>> 24 10 23 30 --- 12 | 31 27 37 24 --- 24
R23 |>>>>> 24 25 28 35 --- 16 | 53 66 78 68 --- 61
R24 |>>>>> 23 15 31 39 --- 15 | 59 9999 29 46 --- 9999
------+------------------------------------+--------------------------------
RMS |>>>>> 21 17 30 29 107 |T 24 34 40 39 19 31
WRMS |>>>>> 21 15 28 29 107 |NE 24 34 40 39 19 31
MEDI |>>>>> 21 16 26 24 94 |MD 22 27 37 25 16 20
Table 3.1519.2 GPS week: 1519 Day: 2 MJD: 54879
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 30 11 27 19 --- 12 | 30 18 33 23 --- 16
R03 |>>>>> 24 23 37 27 --- 16 | 26 30 37 27 --- 19
R04 |>>>>> 31 16 19 24 --- 12 | 27 19 40 25 --- 19
XR06 | ---- --- 51 --- 117 --- 77 | --- 199 --- 130 --- 155
R07 |>>>>> 45 13 26 12 --- 14 | 35 21 36 24 --- 19
R08 |>>>>> 40 9 33 29 --- 15 | 26 29 42 37 --- 25
R10 |>>>>> 35 14 23 31 --- 14 | 23 35 41 19 --- 26
R11 |>>>>> 24 16 31 30 102 14 | 14 16 45 26 19 18
R13 |>>>>> 37 6 22 23 --- 12 | 21 31 54 37 --- 32
R14 |>>>>> 24 10 44 22 --- 14 | 18 19 37 22 --- 17
R15 |>>>>> 18 12 20 29 86 11 | 24 25 33 18 24 18
R17 |>>>>> 33 14 21 44 --- 15 | 37 25 35 42 --- 28
R18 |>>>>> 23 6 19 21 --- 9 | 36 20 20 17 --- 17
R19 |>>>>> 27 8 22 20 --- 10 | 24 18 22 29 --- 16
R20 |>>>>> 49 19 23 53 --- 20 | 32 14 20 32 --- 15
R21 |>>>>> 27 7 18 22 --- 10 | 31 18 17 28 --- 17
R22 |>>>>> 28 9 14 26 --- 10 | 28 21 30 41 --- 21
R23 |>>>>> 29 27 47 26 --- 19 | 85 68 113 80 --- 79
R24 |>>>>> 37 16 16 30 --- 13 | 58 9999 24 46 --- 9999
------+------------------------------------+--------------------------------
RMS |>>>>> 32 14 27 29 94 |T 31 34 37 37 21 30
WRMS |>>>>> 32 14 25 29 94 |NE 31 34 37 37 21 30
MEDI |>>>>> 29 13 22 26 86 |MD 27 21 35 28 19 19
Table 3.1519.3 GPS week: 1519 Day: 3 MJD: 54880
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 14 16 20 21 --- 10 | 19 22 42 38 --- 23
R03 |>>>>> 16 12 29 24 --- 11 | 28 30 33 29 --- 24
R04 |>>>>> 25 14 26 21 --- 12 | 32 18 38 16 --- 17
XR06 | ---- --- 50 --- 98 --- 70 | --- 349 --- 294 --- 326
R07 |>>>>> 15 12 16 16 --- 8 | 26 21 34 30 --- 23
R08 |>>>>> 29 9 32 19 --- 12 | 31 24 47 22 --- 22
R10 |>>>>> 22 11 23 24 --- 11 | 13 20 41 39 --- 20
R11 |>>>>> 16 23 48 33 79 17 | 19 16 66 35 27 21
R13 |>>>>> 25 10 22 25 --- 11 | 15 28 24 27 --- 20
R14 |>>>>> 24 12 22 13 --- 10 | 16 28 17 24 --- 17
R15 |>>>>> 28 11 39 30 88 15 | 22 19 55 18 51 20
R17 |>>>>> 25 11 27 18 --- 11 | 33 36 41 43 --- 32
R18 |>>>>> 20 12 23 17 --- 10 | 22 26 21 22 --- 15
R19 |>>>>> 28 7 20 23 --- 11 | 18 22 22 29 --- 17
R20 |>>>>> 30 11 18 33 --- 13 | 25 35 22 26 --- 24
R21 |>>>>> 18 12 24 17 --- 10 | 23 29 39 25 --- 24
R22 |>>>>> 20 7 16 29 --- 10 | 24 22 33 27 --- 22
R23 |>>>>> 33 23 62 37 --- 21 | 77 67 106 94 --- 76
XR24 |>>>>> 50 28 --- 28 --- 25 | 36 9999 --- 55 --- 9999
------+------------------------------------+--------------------------------
RMS |>>>>> 23 13 30 24 84 |T 26 45 40 47 39 41
WRMS |>>>>> 23 12 26 24 84 |NE 26 45 40 47 39 41
MEDI |>>>>> 24 12 23 24 79 |MD 23 24 38 29 27 22
Table 3.1519.4 GPS week: 1519 Day: 4 MJD: 54881
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 21 9 23 31 --- 11 | 21 18 28 39 --- 18
R03 |>>>>> 15 11 19 16 --- 8 | 21 27 48 33 --- 28
R04 |>>>>> 23 11 27 21 --- 11 | 29 30 39 24 --- 24
XR06 | ---- --- 39 --- 104 --- 63 | --- 153 --- 139 --- 138
R07 |>>>>> 20 11 22 31 --- 11 | 33 29 38 21 --- 26
R08 |>>>>> 19 13 22 23 --- 10 | 25 27 38 19 --- 23
R10 |>>>>> 16 14 21 37 --- 12 | 21 24 34 38 --- 21
R11 |>>>>> 17 8 12 21 54 8 | 22 16 25 27 26 18
R13 |>>>>> 18 20 42 38 --- 16 | 18 29 45 28 --- 19
R14 |>>>>> 17 8 18 25 --- 9 | 15 22 36 22 --- 18
R15 |>>>>> 23 8 12 31 130 10 | 14 19 25 22 33 14
R17 |>>>>> 20 11 31 20 --- 11 | 39 38 59 53 --- 42
R18 |>>>>> 22 10 15 17 --- 9 | 27 25 29 26 --- 21
R19 |>>>>> 22 8 18 31 --- 10 | 22 20 27 30 --- 17
R20 |>>>>> 27 19 29 34 --- 15 | 29 21 32 25 --- 20
R21 |>>>>> 24 11 17 28 --- 11 | 25 20 32 29 --- 20
R22 |>>>>> 17 8 24 36 --- 11 | 23 20 30 33 --- 21
R23 |>>>>> 25 18 33 43 --- 16 | 70 62 93 85 --- 70
------+------------------------------------+--------------------------------
RMS |>>>>> 21 12 24 29 100 |T 26 33 38 38 29 31
WRMS |>>>>> 20 12 23 29 100 |NE 26 33 38 38 29 31
MEDI |>>>>> 20 11 22 31 54 |MD 23 24 34 28 26 21
Table 3.1519.5 GPS week: 1519 Day: 5 MJD: 54882
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 24 9 19 22 --- 10 | 20 17 32 28 --- 20
R03 |>>>>> 24 7 23 27 --- 12 | 20 27 33 38 --- 25
R04 |>>>>> 26 10 36 28 --- 14 | 37 34 52 26 --- 34
XR06 | ---- --- 38 --- 61 --- 48 | --- 178 --- 221 --- 192
R07 |>>>>> 22 19 24 22 --- 12 | 21 33 31 25 --- 22
R08 |>>>>> 19 19 24 24 --- 12 | 20 26 28 39 --- 20
R10 |>>>>> 12 12 18 16 --- 8 | 10 10 21 19 --- 10
R11 |>>>>> 15 23 25 36 24 14 | 7 23 38 26 16 13
R13 |>>>>> 27 17 48 26 --- 17 | 14 24 65 16 --- 23
R14 |>>>>> 30 12 56 13 --- 17 | 24 18 56 12 --- 13
R15 |>>>>> 27 19 32 35 135 16 | 9 31 51 40 30 28
R17 |>>>>> 15 17 19 33 --- 12 | 49 42 50 60 --- 44
R18 |>>>>> 11 11 31 18 --- 10 | 26 23 36 23 --- 20
R19 |>>>>> 17 13 13 16 --- 8 | 20 21 25 23 --- 16
R20 |>>>>> 33 31 35 30 --- 18 | 20 48 44 37 --- 33
R21 |>>>>> 15 11 28 23 --- 11 | 26 31 38 39 --- 26
R22 |>>>>> 14 14 21 30 --- 11 | 25 25 32 39 --- 26
R23 |>>>>> 26 15 22 33 --- 14 | 55 60 73 77 --- 62
XR24 | ---- --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS |>>>>> 22 16 30 26 97 |T 23 37 41 43 23 34
WRMS |>>>>> 22 16 27 26 97 |NE 23 37 41 43 23 34
MEDI |>>>>> 22 14 24 26 24 |MD 20 26 38 28 16 23
Table 3.1519.6 GPS week: 1519 Day: 6 MJD: 54883
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 31 12 15 18 --- 10 | 36 23 33 35 --- 27
R03 |>>>>> 36 12 17 34 --- 13 | 33 27 37 36 --- 29
R04 |>>>>> 37 12 45 28 --- 16 | 28 23 47 27 --- 24
XR06 | ---- --- 26 --- 68 --- 42 | --- 109 --- 132 --- 109
R07 |>>>>> 36 8 26 28 --- 13 | 50 36 48 29 --- 37
R08 |>>>>> 17 7 26 16 --- 9 | 32 27 31 24 --- 25
R10 |>>>>> 21 9 19 15 --- 8 | 20 22 29 25 --- 20
R11 |>>>>> 16 9 15 22 38 8 | 22 22 19 20 17 18
R13 |>>>>> 23 9 34 19 --- 11 | 22 27 37 23 --- 19
R14 |>>>>> 22 9 16 15 --- 8 | 21 19 17 14 --- 13
R15 |>>>>> 24 11 19 33 137 12 | 20 32 36 28 20 27
R17 |>>>>> 44 19 35 34 --- 17 | 48 47 59 61 --- 46
R18 |>>>>> 33 12 50 40 --- 18 | 31 32 21 48 --- 27
R19 |>>>>> 20 10 17 18 --- 8 | 28 27 23 29 --- 24
R20 |>>>>> 26 11 24 33 --- 12 | 21 27 28 32 --- 20
R21 |>>>>> 46 16 41 28 --- 17 | 40 36 43 36 --- 29
R22 |>>>>> 18 11 21 25 --- 10 | 26 23 28 29 --- 22
R23 |>>>>> 40 14 40 42 --- 18 | 84 83 99 99 --- 87
XR24 | ---- --- 5 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS |>>>>> 30 12 29 28 100 |T 33 35 37 40 18 33
WRMS |>>>>> 29 11 25 28 100 |NE 33 35 37 40 18 33
MEDI |>>>>> 26 11 24 28 38 |MD 28 27 33 29 17 25
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