[IGSREPORT-15996] Wk 1466 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Fri Feb 29 08:08:19 PST 2008
******************************************************************************
IGS Electronic Report 29 Feb 08:08:32 PST 2008 Message Number 15996
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1466 (Feb 10, 2008 - Feb 16, 2008)
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 2.1466.
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:
igl1466[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1466 in the SP3 format.
igl14667.sum Combination Report for GPS Week 1466.
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 | 1241.9 ns
1 | 1304.6 ns
2 | 1280.7 ns
3 | 1222.1 ns
4 | 1226.3 ns
5 | 1236.8 ns
6 | 1269.8 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 | ESX | R19
2 | ESX | R08
3 | MCC | R15
4 | ESX | R11
6 | COD | R08
6 | ESX | R15
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 1.1466, 1a.1466).
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 2.1466.0-6)
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 3.1466.0-6).
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 1466 summary. (Feb 10, 2008 - Feb 16, 2008)
Table 1.1466.a GPS week : 1466 MJD: 54506.0-54512.0
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 64| 1 0 14 -24 -11 -16 -.07 40 34 | 0 84 2804 2929
| 2 1 8 36 43 109 .05 | 0 321
cod 176| -3 2 -2 20 14 28 -.10 58 27 | --- --- --- ---
| 2 2 2 44 64 61 .02 | --- ---
esx 112| 3 -2 0 28 14 4 .33 98 57 | -21494 -2009 10933 33504
| 5 5 8 76 50 146 .17 | 27349 7922
iac n/a| 2 -1 -12 -26 13 -51 .03 41 41 | 1249438 -3055 11705 30435
| 2 4 6 36 41 116 .08 | 30031 8674
mcc n/a| -19 -3 -7 -36 -36 674 .49 178 178 | --- --- --- ---
| 25 4 30 59 244 834 .58 | --- ---
Table 1.1466.b GPS week : 1466 MJD: 54506.0-54512.0
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 | 22 16 18 18 26 26 26 |
R04 | 24 18 22 18 14 16 20 |
R06 | 17 17 20 16 20 19 17 |
R07 | --- --- --- 0 0 0 0 |
R08 | 39 19 21 21 20 40 116 |
R09 | 19 16 40 28 27 22 27 |
R10 | 11 17 15 14 24 15 17 |
R11 | 18 15 19 21 22 36 20 |
R13 | 26 23 19 30 29 34 28 |
R14 | 13 16 12 15 18 16 15 |
R15 | 19 24 21 23 42 39 56 |
R17 | 23 29 40 19 28 21 21 |
R19 | 17 23 34 26 34 31 41 |
R20 | 17 20 20 22 20 20 22 |
R23 | 16 17 22 22 20 30 22 |
R24 | --- --- --- --- 0 0 0 |
Table 1.1466.c GPS week : 1466 MJD: 54506.0-54512.0
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 1466 0 | -75 -163 244 -699 -69 -6575 94.8 6729 6729 | 1241896 0
brd 1466 1 | 318 307 -13 127 3768 -10240 93.6 6340 6340 | 1304558 0
brd 1466 2 | 122 134 -49 -1575 1600 -15860 95.3 6128 6128 | 1280671 0
brd 1466 3 | 3 211 -3 -2183 3749 -23410 96.0 5659 5659 | 1222060 0
brd 1466 4 | 8 15 157 -801 -660 -18060 89.0 5619 5619 | 1226345 0
brd 1466 5 | -42 32 239 65 3269 -17950 91.9 6893 6893 | 1236819 0
brd 1466 6 | 88 -202 183 3053 998 -23180 92.3 7032 7032 | 1269825 0
-------------+------------------------------------------------------------+----------------
brd 1466 mean| 60 47 108 -287 1807 -16467 93.3 6342 6342 | 1254596 0
brd 1466 sdev| 133 187 126 1690 1828 6258 2.4 572 572 | 30935 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 2.1466.0 GPS week: 1466 Day: 0 MJD: 54506
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 64| 3 -3 20 -39 25 -99 -.12 37 34 | 0 330 2750 2842
cod 176| -1 1 -3 2 -14 28 -.08 21 21 | --- --- --- ---
esx 112| 3 8 -10 35 45 108 .30 60 72 | -24305 2347 7656 24341
iac n/a| 3 -5 -11 28 -5 23 .04 37 37 | 1240795 281 7675 12552
Table 2.1466.1 GPS week: 1466 Day: 1 MJD: 54507
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 64| 0 0 4 -40 24 -175 -.13 24 23 | 0 -141 2361 2417
cod 176| -4 2 -2 70 -19 122 -.12 27 26 | --- --- --- ---
esx 112| -4 1 1 50 30 57 .62 86 51 | 23899 791 8905 21143
iac n/a| 2 -2 0 -19 49 57 -.06 34 34 | 1306343 -8800 12515 21618
Table 2.1466.2 GPS week: 1466 Day: 2 MJD: 54508
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 64| 0 0 3 7 13 59 -.05 24 22 | 0 73 3029 3103
cod 176| -6 6 0 -32 -89 -41 -.11 33 26 | --- --- --- ---
esx 112| 6 -6 6 93 -22 72 .46 120 46 | -3020 -6105 8875 37607
iac n/a| 6 0 -16 -9 72 -99 .03 41 41 | 1271460 -3224 9211 35322
Table 2.1466.3 GPS week: 1466 Day: 3 MJD: 54509
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 64| 1 0 9 4 -12 38 -.09 27 27 | 0 227 3210 3297
cod 176| -5 0 0 -28 39 73 -.11 23 20 | --- --- --- ---
esx 112| 12 -1 -6 -47 -40 -203 .36 70 48 | -56823 573 8039 21134
iac n/a| 3 0 -17 -22 -6 -123 -.05 43 43 | 1220704 -2572 8011 18452
mcc n/a| 0 0 0 0 0 0 .0 432 432 | --- --- --- ---
Table 2.1466.4 GPS week: 1466 Day: 4 MJD: 54510
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 64| -1 0 19 -92 -93 -88 .03 39 39 | 0 247 2553 2670
cod 176| -1 3 -4 34 33 63 -.08 22 22 | --- --- --- ---
esx 112| 3 -8 2 115 104 187 .20 117 76 | -45966 5795 7106 14433
iac n/a| 4 -7 -18 -54 39 -259 .19 51 51 | 1224725 4296 6861 11408
mcc n/a| -53 -4 -49 -124 -367 980 1.15 79 79 | --- --- --- ---
Table 2.1466.5 GPS week: 1466 Day: 5 MJD: 54511
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 64| 4 -1 26 8 -46 142 -.07 55 53 | 0 380 2433 2540
cod 176| -1 0 -4 78 119 0 -.07 36 30 | --- --- --- ---
esx 112| 2 -3 -2 -100 -20 -176 .20 66 51 | -32856 -18088 22131 39955
iac n/a| 3 -1 -10 -17 -44 -21 .02 38 38 | 1236820 -18709 21595 36952
mcc n/a| -23 -8 21 -22 223 1716 .81 68 68 | --- --- --- ---
Table 2.1466.6 GPS week: 1466 Day: 6 MJD: 54512
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 64| 2 2 15 -19 5 5 -.02 74 42 | 0 -528 3293 3639
cod 176| -6 0 -3 15 33 -43 -.11 243 46 | --- --- --- ---
esx 112| 2 -5 15 52 1 -10 .14 165 54 | -11389 622 13819 75921
iac n/a| -2 5 -15 -86 -11 59 .01 42 42 | 1245219 7339 16070 76744
mcc n/a| 0 0 0 0 0 0 .0 133 133 | --- --- --- ---
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 3.1466.0 GPS week: 1466 Day: 0 MJD: 54506
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 7358 64 22 33 27 22 | 50 53 44 35 39
R04 | 8139 23 25 53 63 24 | 47 46 56 71 45
R06 | 3126 39 15 28 37 16 | 32 53 53 59 44
R08 | 8188 50 30 152 28 38 | 63 93 54 31 28
R09 | 9393 37 17 38 45 19 | 93 81 93 85 82
R10 | 1433 24 12 22 19 10 | 21 20 29 22 12
R11 | 4656 30 14 54 32 17 | 20 24 67 36 25
R13 |13584 20 32 79 52 26 | 24 28 68 42 18
R14 | 971 24 19 19 24 12 | 15 26 34 21 19
R15 | 5490 34 16 53 35 18 | 43 33 67 46 27
R17 |10005 44 19 69 39 23 | 40 56 90 61 50
R19 | 1302 44 20 26 29 17 | 39 48 86 73 46
R20 | 1240 32 22 46 26 17 | 24 47 31 49 33
R23 | 2376 18 23 38 34 16 | 60 79 84 67 69
------+-------------------------------+---------------------------
RMS | 6728 37 21 60 37 |T 40 49 61 49 38
WRMS | 6728 34 21 72 37 |NE 40 49 61 49 38
MEDI | 4656 32 19 38 32 |MD 39 47 56 46 33
Table 3.1466.1 GPS week: 1466 Day: 1 MJD: 54507
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 6045 16 31 24 35 16 | 37 41 37 29 28
R04 | 8578 27 32 36 29 17 | 82 81 62 80 75
R06 | 2639 21 31 41 31 17 | 21 43 54 40 30
R08 | 8080 25 25 64 28 19 | 48 89 112 30 31
R09 | 9292 19 17 45 35 16 | 88 81 68 100 80
R10 | 1442 24 11 41 43 17 | 17 28 36 28 18
R11 | 6012 19 25 46 20 15 | 25 31 65 22 21
R13 | 8066 34 21 80 32 22 | 36 20 68 37 20
R14 | 2026 30 16 40 26 16 | 13 25 43 37 17
R15 | 5670 20 23 95 36 24 | 17 35 85 36 19
R17 |12071 21 30 109 50 28 | 31 31 101 49 27
R19 | 2179 25 35 238 34 22 | 31 49 167 48 31
R20 | 1054 15 40 49 32 19 | 34 49 33 32 29
R23 | 1668 25 18 41 39 17 | 55 42 61 58 47
------+-------------------------------+---------------------------
RMS | 6339 24 27 86 34 |T 38 46 70 44 33
WRMS | 6339 23 26 51 34 |NE 38 46 70 44 33
MEDI | 5670 21 25 45 32 |MD 31 41 62 37 28
Table 3.1466.2 GPS week: 1466 Day: 2 MJD: 54508
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 6881 26 30 30 40 18 | 44 43 43 42 33
R04 | 6905 24 49 45 39 22 | 45 75 81 50 51
R06 | 3278 25 37 47 37 20 | 26 59 60 38 35
R08 | 6957 25 34 306 31 21 | 40 62 198 32 21
R09 | 7579 38 31 183 30 40 | 65 53 218 55 67
R10 | 1749 17 16 31 39 14 | 24 15 40 28 18
R11 | 5935 16 26 62 43 19 | 22 36 67 55 30
R13 |11371 20 25 66 36 19 | 24 37 56 34 20
R14 | 3146 12 18 28 27 11 | 17 20 29 27 9
R15 | 7156 25 20 75 36 20 | 37 38 89 60 34
R17 | 8540 19 42 182 46 40 | 20 48 167 47 31
R19 | 2405 35 34 131 60 34 | 65 42 135 62 53
R20 | 1913 16 32 44 51 19 | 19 32 47 50 24
R23 | 1698 28 44 43 43 22 | 35 67 62 60 44
------+-------------------------------+---------------------------
RMS | 6127 24 33 120 41 |T 34 44 92 45 33
WRMS | 6127 22 26 46 41 |NE 34 44 92 45 33
MEDI | 5935 24 31 47 39 |MD 26 42 62 47 31
Table 3.1466.3 GPS week: 1466 Day: 3 MJD: 54509
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5001 32 20 47 33 --- 17 | 55 53 84 62 --- 51
R04 | 5188 39 26 45 15 --- 18 | 57 40 47 46 --- 33
R06 | 2744 29 24 24 32 --- 15 | 36 61 48 57 --- 43
XR07 | ---- --- 5 --- --- >>>> 0 | --- 272 --- --- 9999 273
R08 | 5167 18 29 79 30 --- 21 | 49 92 45 30 --- 29
R09 | 8021 27 30 104 51 --- 28 | 117 124 192 135 --- 126
R10 | 2575 22 17 38 27 --- 13 | 17 29 42 51 --- 23
R11 | 2729 19 22 64 53 --- 21 | 23 24 97 74 --- 33
R13 |10356 23 34 132 28 --- 30 | 20 50 133 30 --- 28
R14 | 3997 22 24 34 25 --- 14 | 21 40 28 26 --- 22
R15 | 6287 22 24 81 46 432 22 | 51 60 121 54 401 43
R17 | 8329 28 17 50 47 --- 19 | 31 54 63 85 --- 49
R19 | 2022 43 17 84 47 --- 25 | 33 26 139 46 --- 29
R20 | 3201 28 15 52 65 --- 22 | 38 38 76 47 --- 37
R23 | 6109 20 20 57 64 --- 22 | 51 47 69 76 --- 48
------+------------------------------------+--------------------------------
RMS | 5659 27 23 70 43 432 |T 42 67 84 58 401 57
WRMS | 5659 27 20 48 43 432 |NE 42 67 84 58 401 57
MEDI | 5001 23 22 52 33 432 |MD 36 50 69 51 401 37
Table 3.1466.4 GPS week: 1466 Day: 4 MJD: 54510
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2547 33 17 111 42 --- 26 | 77 77 112 94 --- 72
R04 | 4947 27 18 33 24 --- 13 | 33 33 64 35 --- 27
R06 | 5546 43 21 38 41 --- 19 | 28 42 62 52 --- 37
XR07 | ---- --- 6 --- --- 88 0 | --- 161 --- --- 9999 161
R08 | 8228 29 24 67 30 --- 19 | 54 144 66 28 --- 31
R09 | 7323 32 26 76 70 --- 26 | 65 86 97 68 --- 70
R10 | 2367 32 23 66 60 --- 23 | 19 37 85 46 --- 35
R11 | 2535 32 24 294 39 --- 21 | 27 56 223 44 --- 43
R13 | 9948 64 33 52 62 --- 29 | 31 68 92 69 --- 44
R14 | 4667 23 17 64 36 --- 17 | 14 34 57 26 --- 17
R15 | 4672 63 19 164 81 79 41 | 71 48 213 39 31 47
R17 | 5672 26 12 128 48 --- 28 | 61 55 93 81 --- 56
R19 | 807 37 24 151 51 --- 34 | 37 31 118 44 --- 24
R20 | 1770 37 20 47 46 --- 20 | 26 39 46 40 --- 28
R23 | 8268 39 17 39 49 --- 19 | 30 47 64 83 --- 44
XR24 | ---- --- 5 --- --- --- 0 | --- 60 --- --- --- 58
------+------------------------------------+--------------------------------
RMS | 5619 39 22 117 51 79 |T 40 63 99 53 31 49
WRMS | 5619 39 22 76 51 79 |NE 40 63 99 53 31 49
MEDI | 4672 32 19 66 46 79 |MD 31 48 85 44 31 43
Table 3.1466.5 GPS week: 1466 Day: 5 MJD: 54511
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2317 59 28 47 48 --- 26 | 57 61 66 80 --- 55
R04 | 4577 37 17 37 20 --- 15 | 36 52 70 48 --- 49
R06 | 4514 42 27 37 27 --- 19 | 37 53 36 44 --- 37
XR07 | ---- --- 9 --- --- 224 0 | --- 198 --- --- 9999 198
R08 | 7660 78 63 111 25 --- 40 | 68 195 106 25 --- 36
R09 |14499 45 32 46 34 --- 22 | 84 98 117 102 --- 93
R10 | 2010 27 13 34 30 --- 15 | 17 41 47 28 --- 25
R11 | 9047 42 27 128 35 --- 35 | 32 62 182 36 --- 61
R13 |11996 53 47 101 40 --- 34 | 44 42 74 56 --- 25
R14 | 3543 30 21 40 23 --- 16 | 17 28 46 22 --- 16
R15 | 3428 68 71 70 60 68 39 | 60 50 157 73 15 47
R17 | 8263 29 28 50 37 --- 20 | 27 46 70 42 --- 37
R19 | 1133 82 30 52 53 --- 31 | 52 62 128 81 --- 69
R20 | 2290 40 27 37 33 --- 19 | 19 21 57 28 --- 23
R23 | 4535 90 26 35 46 --- 29 | 33 72 73 88 --- 63
XR24 | ---- --- 9 --- --- --- 0 | --- 53 --- --- --- 53
------+------------------------------------+--------------------------------
RMS | 6892 55 36 66 38 68 |T 41 70 87 53 15 55
WRMS | 6892 53 30 51 38 68 |NE 41 70 87 53 15 55
MEDI | 4514 42 27 46 34 68 |MD 36 53 70 44 15 47
Table 3.1466.6 GPS week: 1466 Day: 6 MJD: 54512
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3255 59 31 42 44 --- 25 | 43 64 66 40 --- 42
R04 | 2898 46 15 33 35 --- 19 | 32 44 59 52 --- 39
R06 | 2215 40 27 33 18 --- 17 | 44 77 58 63 --- 58
XR07 | ---- --- 5 --- --- 214 0 | --- 177 --- --- 9999 178
R08 | 3231 195 898 207 97 --- 116 | 162 508 176 37 --- 62
R09 |15845 41 54 57 36 --- 27 | 60 66 77 64 --- 57
R10 | 1471 22 26 38 31 --- 17 | 19 30 38 23 --- 19
R11 |12176 22 32 54 31 --- 20 | 21 38 55 38 --- 23
R13 | 9639 39 22 85 42 --- 28 | 24 27 118 32 --- 32
R14 | 2837 27 25 32 22 --- 15 | 18 28 35 24 --- 15
R15 | 4085 124 54 556 51 133 56 | 152 23 210 67 27 53
R17 | 9732 27 39 60 19 --- 21 | 48 45 89 55 --- 52
R19 | 1390 93 89 35 38 --- 40 | 64 73 86 80 --- 69
R20 | 2300 39 29 57 30 --- 22 | 20 50 46 37 --- 30
R23 | 6075 34 20 65 32 --- 22 | 79 77 90 76 --- 73
XR24 | ---- --- 5 --- --- --- 0 | --- 30 --- --- --- 32
------+------------------------------------+--------------------------------
RMS | 7032 74 243 165 42 133 |T 56 84 85 49 27 52
WRMS | 7032 42 46 54 42 133 |NE 56 84 85 49 27 52
MEDI | 3231 39 27 54 32 133 |MD 43 45 66 40 27 42
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