[IGSREPORT-16304] Wk 1480 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 5 05:57:29 PDT 2008
******************************************************************************
IGS Electronic Report 05 Jun 05:57:36 PDT 2008 Message Number 16304
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1480 (May 18, 2008 - May 24, 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 2.1480.
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:
igl1480[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1480 in the SP3 format.
igl14807.sum Combination Report for GPS Week 1480.
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 | 985.6 ns
1 | 971.5 ns
2 | 903.2 ns
3 | 968.3 ns
4 | 894.9 ns
5 | 940.3 ns
6 | 977.0 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
----+--------+---------------
0 | ESX | R09
4 | ESX | R08
5 | ESX | R08 R19
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 1.1480, 1a.1480).
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 2.1480.0-6)
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 3.1480.0-6).
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 1480 summary. (May 18, 2008 - May 24, 2008)
Table 1.1480.a GPS week : 1480 MJD: 54604.0-54610.0
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 67| 2 0 -6 5 45 11 -.15 48 37 | 0 60 3305 3499
| 3 3 5 25 46 163 .13 | 0 423
cod 206| -2 0 9 -16 38 5 -.11 34 29 | --- --- --- ---
| 5 2 5 27 45 90 .08 | --- ---
esx 118| -2 1 7 -38 -111 -91 .44 83 50 | 15433 573 9662 24577
| 6 4 6 45 93 130 .10 | 35526 4603
iac n/a| 3 0 -6 17 6 22 -.08 48 48 | 947261 -1606 9483 21390
| 3 3 7 33 17 82 .10 | 36675 2487
mcc n/a| 0 13 75 -14 -73 -426 -.38 239 239 | --- --- --- ---
| 22 25 20 209 142 2184 1.55 | --- ---
Table 1.1480.b GPS week : 1480 MJD: 54604.0-54610.0
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 | 19 21 20 25 23 18 23 |
R06 | 15 23 21 27 25 25 33 |
R07 | --- --- --- 0 0 0 0 |
R08 | 22 36 24 24 23 16 32 |
R09 | 8440 0 0 0 0 0 0 |
R10 | 19 24 18 13 18 20 25 |
R11 | 13 27 27 18 19 45 33 |
R13 | 32 39 30 41 24 30 23 |
R14 | 20 14 23 24 23 23 18 |
R15 | 17 22 25 27 36 40 30 |
R17 | 29 28 31 18 24 31 20 |
R19 | 15 19 18 14 28 21 24 |
R20 | 22 16 17 19 26 18 27 |
R23 | 433 65 96 18 25 20 30 |
R24 | 23 19 15 22 16 19 24 |
Table 1.1480.c GPS week : 1480 MJD: 54604.0-54610.0
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 1480 0 | 73 92 204 2874 662 -474 103.9 7035 7035 | 985591 0
brd 1480 1 | 493 7156 8416 ------ -4864 67470 72.9 >>>>> >>>>> | 971535 0
brd 1480 2 | 27 -52 319 -2218 994 326 99.2 6292 6292 | 903166 0
brd 1480 3 | 30 -238 154 -264 690 -6133 103.2 4397 4397 | 968284 0
brd 1480 4 | 199 56 671 -750 1349 -19640 100.5 3835 3835 | 894932 0
brd 1480 5 | 78 185 548 -2922 1374 -13200 104.0 3952 3952 | 940315 0
brd 1480 6 | 19 168 702 -6631 383 -6688 101.8 5583 5583 | 976966 0
-------------+------------------------------------------------------------+----------------
brd 1480 mean| 131 1052 1573 -181987 84 3094 97.9 >>>>> >>>>> | 948684 0
brd 1480 sdev| 171 2695 3025 477131 2212 29234 11.2 >>>>> >>>>> | 36741 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 2.1480.0 GPS week: 1480 Day: 0 MJD: 54604
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 67| 7 -1 -5 4 95 240 -.21 33 32 | 0 28 2818 2922
cod 206| 1 -2 2 2 120 -134 -.07 30 29 | --- --- --- ---
esx 118| -12 3 9 -42 -275 -238 .35 45 37 | 44113 -6226 8563 26224
iac n/a| 8 -5 0 -43 21 105 .01 39 39 | 987902 -3709 7520 20527
mcc n/a| -1 7 76 -53 -264 -3568 -.33 142 142 | --- --- --- ---
Table 2.1480.1 GPS week: 1480 Day: 1 MJD: 54605
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 67| 1 -1 -17 -10 71 124 -.12 59 32 | 0 803 4017 4375
cod 206| -5 -4 16 -65 -14 -88 -.05 44 32 | --- --- --- ---
esx 118| -1 -4 10 42 -95 -111 .32 54 55 | 29769 57 8953 29979
iac n/a| 5 1 0 43 0 -21 -.15 49 49 | 970505 -3904 9324 28670
mcc n/a| 28 66 64 299 -30 2932 -1.46 470 470 | --- --- --- ---
Table 2.1480.2 GPS week: 1480 Day: 2 MJD: 54606
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 67| -1 6 -7 -39 54 -147 -.07 86 37 | 0 143 3048 3152
cod 206| -1 0 1 -13 2 41 .01 27 21 | --- --- --- ---
esx 118| 1 -3 11 -34 -79 -251 .48 130 70 | -32541 4149 10922 18869
iac n/a| 2 2 -1 25 0 102 -.19 47 47 | 904544 -4967 10398 15301
mcc n/a| -35 20 49 89 78 1617 -3.26 267 267 | --- --- --- ---
Table 2.1480.3 GPS week: 1480 Day: 3 MJD: 54607
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 67| 1 -1 0 9 -32 172 -.37 30 31 | 0 317 5001 5247
cod 206| -2 0 10 17 36 12 -.07 41 32 | --- --- --- ---
esx 118| -1 2 0 -54 -79 -136 .54 45 32 | 43812 4047 13510 25764
iac n/a| 1 0 -6 34 -1 -71 -.17 45 45 | 968823 753 12955 24352
mcc n/a| -22 -2 60 -29 -248 -14 -.19 125 125 | --- --- --- ---
Table 2.1480.4 GPS week: 1480 Day: 4 MJD: 54608
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 67| 7 0 -6 33 42 -151 -.17 41 41 | 0 -261 3114 3239
cod 206| -10 2 12 -38 11 0 -.21 31 31 | --- --- --- ---
esx 118| 0 7 4 -108 3 99 .58 67 54 | -34856 1802 7537 22958
iac n/a| 8 -5 -18 57 23 118 .07 47 47 | 893694 181 7888 19352
mcc n/a| 15 -11 70 -332 82 -939 1.27 166 166 | --- --- --- ---
Table 2.1480.5 GPS week: 1480 Day: 5 MJD: 54609
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 67| 1 -3 -4 35 86 -60 -.16 42 44 | 0 -100 2814 3010
cod 206| 5 0 12 -3 59 98 -.16 31 27 | --- --- --- ---
esx 118| -8 2 0 -15 -195 4 .50 176 53 | 12318 -5093 8894 25396
iac n/a| 0 -1 -4 -5 23 -52 -.10 57 57 | 934506 -439 9310 22568
mcc n/a| 4 6 103 120 -115 -2032 .91 442 442 | --- --- --- ---
Table 2.1480.6 GPS week: 1480 Day: 6 MJD: 54610
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 67| 1 -1 -4 5 0 -98 .04 42 40 | 0 -509 2325 2550
cod 206| -1 0 9 -11 52 109 -.20 35 31 | --- --- --- ---
esx 118| 8 0 17 -56 -58 -4 .34 61 51 | 45419 5281 9258 22854
iac n/a| -1 0 -14 9 -21 -24 -.02 52 52 | 970855 842 8988 18963
mcc n/a| 9 8 104 -198 -14 -980 .39 59 59 | --- --- --- ---
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 3.1480.0 GPS week: 1480 Day: 0 MJD: 54604
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |11559 29 25 43 35 --- 19 | 43 37 28 53 --- 31
R06 | 6130 21 27 35 22 --- 15 | 100 123 143 121 --- 119
R08 | 8791 24 42 53 28 --- 21 | 49 45 76 30 --- 36
XR09E |20132 8672 8213 >>>> --- --- 8440 | 5 9999 7 --- --- 9999
R10E | 1106 28 30 32 37 --- 18 | 24 53 36 36 --- 29
R11E | 2074 19 19 20 30 --- 12 | 28 33 44 48 --- 34
R13E |17419 66 25 73 52 --- 32 | 44 55 103 86 --- 55
R14E | 1704 16 21 60 30 --- 19 | 28 28 74 45 --- 28
R15E | 2570 21 28 31 35 142 16 | 42 35 70 48 98 32
R17 | 3963 61 30 49 56 --- 29 | 46 69 93 99 --- 65
R19 | 2017 17 23 33 32 --- 15 | 40 42 73 43 --- 37
R20 | 1932 22 44 47 37 --- 22 | 31 48 69 65 --- 43
XR23 |>>>>> 824 481 --- 424 --- 433 | 464 468 --- 425 --- 426
R24 | 1826 30 32 34 60 --- 23 | 236 236 220 254 --- 234
------+------------------------------------+--------------------------------
RMS | 7034 33 30 45 39 142 |T 84 97 79 104 98 89
WRMS | 7034 32 29 37 39 142 |NE 126 133 100 136 --- 123
MEDI | 2570 24 28 43 35 142 |MD 42 48 73 53 98 37
Table 3.1480.1 GPS week: 1480 Day: 1 MJD: 54605
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |>>>>> 26 35 37 44 --- 21 | 28 42 39 45 --- 22
R06 |>>>>> 48 22 51 32 --- 22 | 129 138 165 129 --- 135
R08 |>>>>> 41 67 88 39 --- 36 | 74 62 115 49 --- 65
XR09E |80298 --- 11 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E |>>>>> 40 29 49 44 --- 23 | 29 46 56 46 --- 35
R11E |>>>>> 32 34 48 65 --- 26 | 23 48 59 58 --- 33
R13E |>>>>> 32 49 93 79 --- 38 | 25 35 90 82 --- 29
R14E |>>>>> 13 17 26 32 --- 13 | 30 31 48 38 --- 29
R15E |>>>>> 30 36 37 44 266 21 | 23 22 52 47 78 25
R17 |>>>>> 48 36 34 65 --- 27 | 21 54 46 75 --- 41
R19 |>>>>> 28 22 52 21 --- 18 | 27 44 101 42 --- 43
R20 |>>>>> 21 26 38 17 --- 15 | 36 53 58 63 --- 43
R23 |>>>>> 177 102 56 74 --- 64 | 455 327 474 298 --- 313
R24 |>>>>> 45 17 43 21 609 19 | 204 230 228 221 321 218
------+------------------------------------+--------------------------------
RMS |>>>>> 59 44 54 49 470 |T 84 87 117 91 199 79
WRMS |>>>>> 32 32 55 49 470 |NE 121 118 153 115 321 110
MEDI |>>>>> 32 29 48 44 266 |MD 29 48 59 58 78 41
Table 3.1480.2 GPS week: 1480 Day: 2 MJD: 54606
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |11610 31 23 68 38 --- 20 | 38 53 68 40 --- 41
R06 | 5061 48 14 86 20 --- 20 | 101 105 167 130 --- 114
R08 | 4361 41 22 88 42 --- 24 | 40 41 89 40 --- 33
XR09E |21558 --- 2 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 1828 27 25 44 37 --- 18 | 18 21 52 37 --- 20
XR11E | 3230 50 27 --- 44 --- 26 | 23 54 --- 59 --- 35
R13E | 3000 43 39 56 71 --- 30 | 44 33 64 83 --- 35
R14E | 2179 25 30 32 60 --- 23 | 27 33 37 55 --- 28
R15E | 5356 25 35 73 52 185 25 | 47 19 69 42 47 24
R17 | 2353 42 20 121 62 --- 31 | 42 62 144 53 --- 51
R19 | 1149 35 21 58 27 --- 17 | 46 62 148 65 --- 66
R20 | 1490 39 18 37 36 --- 17 | 55 51 67 43 --- 45
R23 |14448 272 45 388 60 --- 96 | 306 414 511 385 --- 409
R24 | 5651 34 17 48 24 329 15 | 199 187 170 189 50 187
------+------------------------------------+--------------------------------
RMS | 6291 86 27 130 47 267 |T 75 87 132 93 48 83
WRMS | 6291 37 21 70 47 267 |NE 103 121 170 118 50 118
MEDI | 3230 39 22 58 42 185 |MD 44 53 69 55 47 41
Table 3.1480.3 GPS week: 1480 Day: 3 MJD: 54607
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 4769 27 54 35 55 --- 25 | 48 67 80 61 --- 49
R06 | 3590 32 44 60 49 --- 26 | 100 141 130 98 --- 115
XR07 | ---- --- 7 --- --- --- 0 | --- 292 --- --- --- 292
R08 | 4640 29 48 47 41 --- 23 | 78 62 115 47 --- 55
XR09E |20016 --- 7 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 1413 16 15 35 22 --- 13 | 34 41 56 56 --- 41
R11E | 5256 22 33 31 35 --- 17 | 26 43 66 45 --- 33
R13E | 3483 55 88 72 65 --- 40 | 42 125 84 59 --- 51
R14E | 2823 29 29 37 66 --- 23 | 36 49 67 88 --- 53
R15E | 4647 33 34 59 59 119 27 | 30 23 74 65 38 28
R17 | 4910 26 33 37 30 --- 18 | 43 60 96 55 --- 55
R19 | 994 19 28 21 27 --- 13 | 26 43 92 43 --- 28
R20 | 3625 32 17 41 37 --- 19 | 33 28 62 30 --- 28
R23 | 8219 23 33 38 27 --- 17 | 349 309 180 285 --- 305
R24 | 4120 33 31 47 41 131 22 | 99 105 117 94 82 96
------+------------------------------------+--------------------------------
RMS | 4396 30 41 45 45 125 |T 72 99 93 78 60 87
WRMS | 4396 31 32 32 45 125 |NE 97 123 109 89 82 113
MEDI | 4120 29 33 38 41 119 |MD 42 60 84 59 38 51
Table 3.1480.4 GPS week: 1480 Day: 4 MJD: 54608
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 4457 24 42 38 50 --- 23 | 37 75 50 61 --- 44
R06 | 4584 41 34 56 44 --- 25 | 104 121 132 110 --- 110
XR07 | ---- --- 10 --- --- --- 0 | --- 192 --- --- --- 194
R08 | 4786 30 32 166 36 --- 23 | 28 57 169 29 --- 36
XR09E |79106 --- 10 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 1587 23 26 29 44 --- 17 | 36 44 42 35 --- 30
R11E | 4317 34 29 37 30 --- 18 | 20 34 66 39 --- 23
R13E | 4046 44 27 62 35 --- 24 | 35 49 69 77 --- 40
R14E | 3132 45 23 40 52 --- 23 | 29 27 56 61 --- 29
R15E | 3268 56 25 83 84 103 36 | 44 33 62 53 39 31
R17 | 4588 43 22 52 53 --- 24 | 56 29 51 40 --- 23
R19 | 2088 35 44 74 32 --- 27 | 31 45 75 68 --- 52
R20 | 4208 63 31 37 45 --- 25 | 41 59 72 63 --- 46
R23 | 2471 45 41 38 43 --- 24 | 295 312 171 261 --- 282
R24 | 4486 29 21 30 32 211 16 | 189 182 174 200 153 185
------+------------------------------------+--------------------------------
RMS | 3835 41 31 67 47 166 |T 72 89 91 84 96 80
WRMS | 3835 41 31 54 47 166 |NE 97 119 111 104 153 108
MEDI | 4208 41 27 40 44 103 |MD 37 49 69 61 39 40
Table 3.1480.5 GPS week: 1480 Day: 5 MJD: 54609
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 3219 18 28 44 33 --- 18 | 29 40 51 37 --- 30
R06 | 9504 51 38 44 42 --- 25 | 34 84 115 56 --- 62
XR07 | ---- --- 10 --- --- --- 0 | --- 133 --- --- --- 134
R08 | 3811 26 20 258 24 --- 16 | 46 26 215 32 --- 29
XR09E |59481 --- 10 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 1375 20 28 25 57 --- 19 | 32 47 44 55 --- 39
R11E | 3958 72 34 120 78 --- 45 | 19 43 155 70 --- 55
R13E | 2057 39 50 48 70 --- 29 | 28 27 65 76 --- 31
R14E | 2626 47 24 33 52 --- 22 | 31 19 36 57 --- 25
R15E | 3828 66 30 72 108 88 39 | 46 47 65 65 42 35
R17 | 4193 38 39 76 58 --- 31 | 46 47 99 41 --- 36
R19 | 2277 23 26 550 38 --- 20 | 24 48 462 39 --- 30
R20 | 2470 25 29 33 38 --- 18 | 45 43 37 63 --- 35
R23 | 3230 31 27 35 46 --- 19 | 343 308 186 276 --- 306
R24 | 2268 47 19 20 38 619 18 | 160 184 179 195 164 177
------+------------------------------------+--------------------------------
RMS | 3952 42 31 176 57 442 |T 67 78 131 81 103 73
WRMS | 3952 44 27 53 57 442 |NE 90 101 168 92 164 93
MEDI | 3219 38 28 44 46 88 |MD 34 47 99 57 42 35
Table 3.1480.6 GPS week: 1480 Day: 6 MJD: 54610
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 3297 34 40 43 41 --- 22 | 36 31 43 43 --- 29
R06 |15010 42 45 86 60 --- 32 | 74 75 94 65 --- 65
XR07 | ---- --- 9 --- --- --- 0 | --- 143 --- --- --- 143
R08 | 3717 29 18 96 69 --- 31 | 56 40 80 40 --- 45
XR09E |>>>>> --- 9 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 4625 29 28 54 62 --- 24 | 28 36 27 55 --- 25
R11E | 4714 38 49 74 71 --- 32 | 33 36 59 63 --- 27
R13E | 1392 24 38 53 45 --- 23 | 31 38 76 43 --- 34
R14E | 3651 37 20 32 35 --- 18 | 28 18 42 40 --- 21
R15E | 2322 68 35 43 56 59 29 | 42 46 33 73 32 34
R17 | 8269 26 31 44 39 --- 20 | 52 80 86 45 --- 62
R19 | 2825 41 30 41 57 --- 24 | 30 51 133 44 --- 36
R20 | 975 37 31 66 55 --- 26 | 41 43 87 87 --- 52
R23 | 2761 60 42 68 34 --- 29 | 311 319 241 327 --- 317
R24 | 2449 50 26 55 31 --- 23 | 197 219 224 227 --- 213
------+------------------------------------+--------------------------------
RMS | 5583 42 35 61 52 59 |T 73 83 94 88 32 78
WRMS | 5583 40 31 51 52 59 |NE 99 111 123 109 --- 106
MEDI | 3297 37 31 54 55 59 |MD 41 43 80 55 32 36
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