[IGSREPORT-17022] Wk 1512 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jan 15 10:42:18 PST 2009
******************************************************************************
IGS Electronic Report 15 Jan 10:42:19 PST 2009 Message Number 17022
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1512 (Dec 28, 2008 - Jan 03, 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 2.1512.
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:
igl1512[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1512 in the SP3 format.
igl15127.sum Combination Report for GPS Week 1512.
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 | 278.1 ns
1 | 271.5 ns
2 | 344.3 ns
3 | 334.3 ns
4 | 259.7 ns
5 | 179.9 ns
6 | 344.4 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 1.1512, 1a.1512).
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 2.1512.0-6)
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 3.1512.0-6).
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 1512 summary. (Dec 28, 2008 - Jan 03, 2009)
Table 1.1512.a GPS week : 1512 MJD: 54828.0-54834.0
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 84| 0 -2 15 48 -17 -99 -.17 36 34 | 0 179 2839 2977
| 2 1 3 42 41 130 .06 | 0 549
cod 242| -1 1 -3 25 9 20 -.11 19 17 | --- --- --- ---
| 1 1 1 17 18 26 .05 | --- ---
esx 145| 0 0 -1 -73 42 41 .40 32 28 | 61583 -1998 7671 16035
| 2 1 4 35 26 37 .07 | 64797 5787
iac n/a| 4 -1 -5 25 -78 1 -.12 39 39 | 287630 -981 7180 14232
| 1 3 5 35 22 120 .11 | 58485 4034
mcc n/a| 8 -1 17 -13 -2 1554 .47 234 234 | --- --- --- ---
| 24 11 14 79 215 489 .57 | --- ---
Table 1.1512.b GPS week : 1512 MJD: 54828.0-54834.0
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
------+------------------------------------+------------------------------------------
R04 | 29 18 22 19 28 19 19 |
R06 | 17 22 15 15 18 19 16 |
R07 | 23 24 24 24 20 16 22 |
R10 | 38 11 12 15 17 16 12 |
R11 | 15 16 13 17 14 11 11 |
R13 | 15 14 12 12 16 11 14 |
R14 | 13 11 13 9 10 10 11 |
R15 | 18 12 11 14 14 14 9 |
R17 | 16 18 16 16 17 18 12 |
R18 | 24 13 20 21 20 16 12 |
R19 | 21 17 16 11 14 12 10 |
R20 | 22 20 14 19 15 13 16 |
R21 | 15 17 25 16 12 14 14 |
R22 | 22 10 18 17 22 10 11 |
R23 | 30 24 20 16 28 21 16 |
R24 | 16 17 18 21 28 21 17 |
Table 1.1512.c GPS week : 1512 MJD: 54828.0-54834.0
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 1512 0 | 121 152 214 -983 3116 -29740 91.4 6513 6513 | 278084 0
brd 1512 1 | -8 82 52 -2627 2943 -28240 90.6 8162 8162 | 271525 0
brd 1512 2 | -157 -161 -47 -2103 113 -27160 93.7 5140 5140 | 344341 0
brd 1512 3 | -4 -29 -46 -962 742 -29850 95.4 4909 4909 | 334260 0
brd 1512 4 | 242 -10 -174 358 -2263 -35600 85.4 >>>>> >>>>> | 259707 0
brd 1512 5 | 90 -93 -145 -1404 -1217 -42260 100.6 >>>>> >>>>> | 179936 0
brd 1512 6 | -30 -26 -72 -4242 -3882 -29680 85.6 5349 5349 | 344447 0
-------------+------------------------------------------------------------+----------------
brd 1512 mean| 36 -12 -31 -1709 -63 -31790 91.8 74410 74410 | 287471 0
brd 1512 sdev| 128 104 131 1464 2600 5332 5.4 >>>>> >>>>> | 59647 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 2.1512.0 GPS week: 1512 Day: 0 MJD: 54828
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 84| 3 -2 12 -28 -62 -69 -.24 44 42 | 0 -147 3102 3173
cod 242| -1 0 -2 30 -1 29 -.12 24 19 | --- --- --- ---
esx 145| 0 0 0 -10 47 97 .30 27 23 | 36670 3077 6329 11058
iac n/a| 3 -2 -1 -19 -95 -187 -.34 75 75 | 277364 -646 6203 10500
mcc n/a| 16 5 4 -47 58 1917 -.22 207 207 | --- --- --- ---
Table 2.1512.1 GPS week: 1512 Day: 1 MJD: 54829
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 84| -1 -4 17 32 13 -53 -.21 33 34 | 0 1340 4472 4944
cod 242| -2 3 -5 24 -24 38 -.11 20 18 | --- --- --- ---
esx 145| 2 0 -8 -69 65 35 .41 33 30 | 67037 -11875 9771 16664
iac n/a| 2 -4 4 22 -51 -3 -.12 34 34 | 276876 -8228 9783 15874
mcc n/a| 32 -17 25 51 -276 2003 .87 488 488 | --- --- --- ---
Table 2.1512.2 GPS week: 1512 Day: 2 MJD: 54830
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 84| 1 -2 16 69 -20 -271 -.21 36 34 | 0 248 2580 2705
cod 242| -3 1 -4 25 14 61 -.12 19 17 | --- --- --- ---
esx 145| 0 -1 -1 -99 23 -11 .41 34 28 | 116190 6486 7858 15805
iac n/a| 4 -4 -1 28 -94 169 -.06 33 33 | 339295 3200 7790 14185
mcc n/a| 33 14 19 -115 -313 1744 1.47 307 307 | --- --- --- ---
Table 2.1512.3 GPS week: 1512 Day: 3 MJD: 54831
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 84| 3 -3 18 77 -26 52 -.11 38 36 | 0 160 2652 2722
cod 242| -2 0 0 3 31 -16 -.05 14 14 | --- --- --- ---
esx 145| -5 0 -5 -116 45 74 .48 46 42 | 128426 -4021 7627 15148
iac n/a| 6 -2 -9 85 -97 -35 -.04 32 32 | 337462 -4092 6887 13931
mcc n/a| -38 5 8 123 287 1670 .34 323 323 | --- --- --- ---
Table 2.1512.4 GPS week: 1512 Day: 4 MJD: 54832
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 84| -2 0 8 22 -7 -31 -.23 39 31 | 0 -43 2397 2463
cod 242| -2 0 -4 26 7 20 -.14 25 22 | --- --- --- ---
esx 145| 2 -1 3 -49 37 30 .45 31 24 | -828 -3186 5387 19568
iac n/a| 7 1 -7 -11 -95 -69 .01 38 38 | 258532 -206 5421 15043
mcc n/a| 1 3 -1 -26 55 1774 -.01 98 98 | --- --- --- ---
Table 2.1512.5 GPS week: 1512 Day: 5 MJD: 54833
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 84| 0 -1 17 80 48 -289 -.10 34 32 | 0 56 2008 2085
cod 242| -1 1 -3 8 14 22 -.19 17 16 | --- --- --- ---
esx 145| -1 -2 0 -72 0 60 .44 26 23 | -36990 -2380 6329 17294
iac n/a| 3 4 -8 50 -46 128 -.18 32 32 | 181371 3044 6420 17534
mcc n/a| 5 -12 30 -8 60 1131 .27 116 116 | --- --- --- ---
Table 2.1512.6 GPS week: 1512 Day: 6 MJD: 54834
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 84| 0 -2 17 88 -67 -28 -.12 29 28 | 0 -358 2662 2748
cod 242| 0 1 -2 57 24 -9 -.05 17 13 | --- --- --- ---
esx 145| 0 0 0 -93 81 7 .33 27 25 | 120579 -2088 10400 16709
iac n/a| 3 -2 -12 26 -66 10 -.11 27 27 | 342515 61 7761 12561
mcc n/a| 5 -10 36 -70 109 645 .58 97 97 | --- --- --- ---
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 3.1512.0 GPS week: 1512 Day: 0 MJD: 54828
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |23720 73 21 28 105 --- 29 | 207 201 194 198 --- 196
R06E | 6691 38 14 30 46 --- 17 | 37 33 53 49 --- 38
R07E | 3237 73 31 14 47 --- 23 | 24 41 32 56 --- 31
R10 | 1100 53 42 33 165 --- 38 | 46 29 55 135 --- 36
R11 | 1357 17 11 20 62 128 14 | 29 33 41 57 76 32
R13 | 1096 28 17 27 38 --- 14 | 28 33 51 34 --- 35
R14 | 1475 17 11 16 53 --- 12 | 24 29 36 40 --- 27
R15 | 3821 40 15 22 64 40 18 | 30 28 40 51 41 28
R17 | 1286 32 14 23 56 --- 16 | 40 54 65 31 --- 48
R18 | 1204 44 37 44 41 --- 24 | 49 68 49 28 --- 42
R19 | 774 26 14 17 98 --- 20 | 58 76 65 117 --- 68
R20 | 1212 45 14 16 93 --- 21 | 35 59 65 111 --- 56
R21 | 2523 31 23 15 40 --- 14 | 129 127 138 154 --- 131
R22 | 2447 35 23 21 89 --- 21 | 75 86 92 73 --- 80
R23 | 2879 60 36 57 57 --- 29 | 44 47 83 42 --- 44
R24 | 3745 49 24 12 19 333 15 | 81 132 123 110 530 115
------+------------------------------------+--------------------------------
RMS | 6513 44 24 27 75 207 |T 58 67 73 80 215 62
WRMS | 6513 42 19 23 75 207 |NE 51 61 69 75 215 57
MEDI | 1475 38 17 21 56 128 |MD 40 47 55 56 76 42
Table 3.1512.1 GPS week: 1512 Day: 1 MJD: 54829
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |30545 37 24 30 38 --- 18 | 165 179 200 172 --- 179
R06E | 3878 45 22 41 50 --- 22 | 38 44 78 53 --- 42
R07E | 1687 64 19 39 43 --- 23 | 26 28 31 49 --- 21
R10 | 1749 19 12 26 17 --- 10 | 21 29 49 51 --- 25
R11 | 2167 24 20 46 16 74 16 | 34 33 60 48 46 37
R13 | 895 31 16 29 25 --- 14 | 29 40 49 52 --- 37
R14 | 1648 18 11 15 30 --- 10 | 23 22 30 28 --- 22
R15 | 3549 25 14 19 27 81 12 | 28 24 41 37 38 26
R17 | 2151 28 23 35 36 --- 17 | 31 46 60 30 --- 37
R18 | 639 22 24 21 15 --- 12 | 31 47 32 36 --- 34
R19 | 1314 26 23 32 35 --- 16 | 48 63 64 52 --- 54
R20 | 2216 29 19 50 39 --- 19 | 41 49 86 37 --- 45
R21 | 2251 32 14 38 31 --- 16 | 118 117 146 107 --- 120
R22 | 2997 18 10 14 24 --- 9 | 63 64 57 58 --- 58
R23 | 2548 43 32 32 59 --- 24 | 24 32 38 50 --- 20
R24 | 7682 39 23 27 29 839 17 | 88 107 90 102 349 96
------+------------------------------------+--------------------------------
RMS | 8162 33 20 33 34 488 |T 50 57 69 60 144 53
WRMS | 8162 34 18 30 34 488 |NE 44 51 61 52 144 47
MEDI | 2167 28 19 30 30 81 |MD 31 44 57 50 46 37
Table 3.1512.2 GPS week: 1512 Day: 2 MJD: 54830
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |12733 61 24 37 36 --- 22 | 96 108 111 84 --- 100
R06E | 5371 26 18 23 35 --- 14 | 35 30 51 43 --- 32
R07E | 4375 53 24 38 52 --- 23 | 36 32 57 56 --- 30
R10 | 2736 31 5 25 20 --- 11 | 44 25 46 37 --- 29
R11 | 8844 25 12 30 23 109 12 | 43 35 60 31 37 38
R13 | 2369 35 10 14 22 --- 11 | 40 35 34 37 --- 31
R14 | 2307 24 10 26 32 --- 13 | 35 33 46 33 --- 32
R15 | 4699 12 17 20 24 85 11 | 29 28 37 41 35 28
R17 | 4671 19 26 33 26 --- 15 | 34 50 40 39 --- 38
R18 | 2298 30 31 33 42 --- 19 | 56 53 85 58 --- 53
R19 | 1537 38 15 27 31 --- 15 | 38 56 57 40 --- 46
R20 | 3341 22 17 17 36 --- 13 | 52 41 42 36 --- 40
R21 | 2690 37 19 72 42 --- 25 | 98 84 109 65 --- 81
R22 | 5769 24 10 51 33 --- 17 | 106 88 122 80 --- 95
R23 | 1835 48 26 27 37 --- 19 | 47 36 47 35 --- 30
R24 | 3059 52 26 14 24 514 17 | 66 88 70 78 108 74
------+------------------------------------+--------------------------------
RMS | 5140 36 19 34 33 307 |T 53 51 63 49 60 48
WRMS | 5140 34 17 28 33 307 |NE 52 50 61 46 60 47
MEDI | 3059 30 17 27 32 109 |MD 43 36 51 40 37 38
Table 3.1512.3 GPS week: 1512 Day: 3 MJD: 54831
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 8171 48 12 48 39 --- 19 | 191 180 190 196 --- 184
R06E | 5774 29 13 36 33 --- 14 | 35 39 73 49 --- 42
R07E | 5831 61 19 51 53 --- 24 | 33 30 61 56 --- 31
R10 | 7181 26 16 34 36 --- 15 | 30 43 46 32 --- 31
R11 | 8303 27 15 63 24 132 17 | 22 41 78 29 24 33
R13 | 3994 27 8 34 25 --- 12 | 43 37 69 46 --- 42
R14 | 1761 19 9 20 20 --- 9 | 37 43 43 33 --- 38
R15 | 2402 17 11 53 26 76 14 | 17 28 54 31 30 25
R17 | 3384 39 19 30 30 --- 16 | 41 72 82 39 --- 58
R18 | 6602 52 14 66 28 --- 20 | 27 40 84 38 --- 37
R19 | 1945 20 12 25 24 --- 10 | 42 58 75 45 --- 53
R20 | 3418 48 13 37 41 --- 18 | 15 54 50 70 --- 47
R21 | 2461 28 15 56 17 --- 15 | 76 91 86 85 --- 82
R22 | 3926 27 14 56 30 --- 16 | 75 89 101 87 --- 84
R23 | 2753 20 18 47 36 --- 16 | 29 31 41 38 --- 25
R24 | 2562 66 14 48 25 539 20 | 110 154 163 149 146 143
------+------------------------------------+--------------------------------
RMS | 4909 38 14 46 32 323 |T 51 64 81 63 66 59
WRMS | 4909 36 14 42 32 323 |NE 43 60 74 55 66 53
MEDI | 3418 27 14 47 28 132 |MD 35 43 73 45 30 42
Table 3.1512.4 GPS week: 1512 Day: 4 MJD: 54832
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |>>>>> 75 32 48 28 --- 27 | 65 105 122 83 --- 90
R06E |>>>>> 30 28 40 24 --- 18 | 32 32 65 43 --- 38
R07E |>>>>> 44 24 31 41 --- 20 | 30 22 34 40 --- 18
R10 |>>>>> 16 22 25 49 --- 17 | 28 43 31 39 --- 26
R11 |>>>>> 24 15 26 33 126 14 | 36 38 53 25 24 33
R13 |>>>>> 29 32 19 27 --- 16 | 41 49 46 34 --- 35
R14 |>>>>> 13 14 16 25 --- 10 | 29 28 39 26 --- 28
R15 |>>>>> 30 13 13 34 57 13 | 22 27 40 30 39 24
R17 |>>>>> 24 21 27 44 --- 17 | 32 48 56 23 --- 36
R18 |>>>>> 41 28 30 39 --- 19 | 60 52 19 66 --- 39
R19 |>>>>> 22 22 25 25 --- 13 | 28 51 51 52 --- 43
R20 |>>>>> 42 16 23 22 --- 15 | 36 32 45 37 --- 33
R21 |>>>>> 19 19 19 27 --- 12 | 93 83 79 62 --- 76
R22 |>>>>> 41 33 46 32 --- 22 | 121 100 109 87 --- 98
R23 |>>>>> 48 41 33 70 --- 27 | 49 30 54 42 --- 23
R24 |>>>>> 69 26 46 51 --- 27 | 101 133 140 73 --- 111
------+------------------------------------+--------------------------------
RMS |>>>>> 39 25 31 38 98 |T 50 54 61 47 31 46
WRMS |>>>>> 31 22 24 38 98 |NE 52 54 58 45 31 46
MEDI |>>>>> 30 22 26 32 57 |MD 36 43 51 40 24 35
Table 3.1512.5 GPS week: 1512 Day: 5 MJD: 54833
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | ---- 49 22 20 39 --- 18 | 162 132 134 141 --- 138
R06E |>>>>> 36 19 47 23 --- 18 | 44 49 99 55 --- 58
R07E |>>>>> 32 14 31 34 --- 15 | 19 23 24 40 --- 18
R10 | 4952 27 19 32 33 --- 15 | 28 31 47 34 --- 25
R11 | 3478 26 12 18 21 137 10 | 34 31 36 24 44 27
R13 | 4151 30 10 15 18 --- 10 | 37 31 24 22 --- 24
R14 | 1777 23 11 17 16 --- 9 | 37 32 51 35 --- 35
R15 |>>>>> 33 12 22 34 91 14 | 20 28 35 27 26 23
R17 | 2042 45 21 25 35 --- 17 | 43 30 26 24 --- 21
R18 |>>>>> 19 20 25 41 --- 15 | 18 32 44 21 --- 26
R19 |>>>>> 29 14 17 25 --- 12 | 31 61 50 56 --- 50
R20 |>>>>> 34 17 16 19 --- 12 | 17 26 38 33 --- 20
R21 |>>>>> 29 18 27 24 --- 14 | 47 67 66 69 --- 61
R22 | 1185 24 12 14 19 --- 9 | 95 110 115 104 --- 106
R23 | 4175 56 22 25 48 --- 21 | 54 33 51 29 --- 32
R24 | 2125 31 22 39 51 --- 20 | 130 166 188 159 --- 161
------+------------------------------------+--------------------------------
RMS |>>>>> 34 17 26 32 116 |T 51 55 64 54 35 51
WRMS |>>>>> 32 16 23 32 116 |NE 45 52 59 49 35 47
MEDI | 4952 30 17 22 25 91 |MD 37 32 47 34 26 27
Table 3.1512.6 GPS week: 1512 Day: 6 MJD: 54834
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |17051 31 26 23 46 --- 18 | 111 117 114 107 --- 111
R06E | 6526 34 21 34 23 --- 16 | 56 51 77 50 --- 55
R07E | 5379 40 25 38 49 --- 21 | 29 25 23 38 --- 23
R10 | 3058 23 19 17 23 --- 12 | 25 31 30 37 --- 26
R11 | 5159 23 20 12 21 111 11 | 32 34 34 29 39 29
R13 | 2989 29 8 37 19 --- 13 | 33 26 40 25 --- 24
R14 | 1538 20 7 30 19 --- 11 | 29 27 35 30 --- 26
R15 | 2060 21 7 16 18 80 9 | 22 25 38 40 23 26
R17 | 1713 24 14 17 26 --- 11 | 45 51 50 35 --- 43
R18 | 957 18 19 12 29 --- 12 | 39 54 35 32 --- 38
R19 | 1571 23 7 17 20 --- 9 | 51 62 63 67 --- 59
R20 | 1675 34 19 34 27 --- 16 | 35 47 60 61 --- 47
R21 | 1162 34 15 28 17 --- 13 | 95 110 116 111 --- 106
R22 | 773 32 14 17 14 --- 11 | 122 136 139 127 --- 131
R23 | 1563 42 15 30 21 --- 15 | 36 33 34 32 --- 26
R24 | 5521 26 18 44 29 --- 17 | 98 115 128 112 --- 111
------+------------------------------------+--------------------------------
RMS | 5349 29 17 27 27 97 |T 53 59 63 58 31 55
WRMS | 5349 28 13 25 27 97 |NE 50 57 61 56 31 53
MEDI | 1713 26 15 23 21 80 |MD 36 47 40 38 23 38
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