[IGSREPORT-16442] Wk 1486 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 17 07:19:15 PDT 2008
******************************************************************************
IGS Electronic Report 17 Jul 07:19:18 PDT 2008 Message Number 16442
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1486 (Jun 29, 2008 - Jul 05, 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 2.1486.
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:
igl1486[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1486 in the SP3 format.
igl14867.sum Combination Report for GPS Week 1486.
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 | 824.2 ns
1 | 834.0 ns
2 | 819.5 ns
3 | 817.8 ns
4 | 869.0 ns
5 | 867.6 ns
6 | 866.5 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
----+--------+---------------
4 | BKG | R07
4 | IAC | R11
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 1.1486, 1a.1486).
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 2.1486.0-6)
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 3.1486.0-6).
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 1486 summary. (Jun 29, 2008 - Jul 05, 2008)
Table 1.1486.a GPS week : 1486 MJD: 54646.0-54652.0
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 66| 2 -2 -6 25 20 142 -.13 51 40 | 0 22 2499 2643
| 5 2 3 51 35 151 .05 | 0 282
cod 212| -3 0 -2 -3 -2 0 -.12 32 26 | --- --- --- ---
| 3 2 4 47 29 78 .06 | --- ---
esx 128| 0 1 4 -9 0 0 .49 73 61 | 22919 1621 7511 17243
| 3 6 12 70 43 125 .26 | 32204 2595
iac n/a| 1 0 5 5 -8 -149 .02 134 134 | 843599 -3297 7559 15684
| 2 2 7 44 36 148 .08 | 23969 2616
mcc n/a| 6 -18 28 -70 131 -319 .15 294 294 | --- --- --- ---
| 45 43 10 246 411 1153 1.42 | --- ---
Table 1.1486.b GPS week : 1486 MJD: 54646.0-54652.0
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 | 17 22 38 45 36 39 33 |
R06 | 22 22 26 22 29 27 34 |
R07 | 46 34 46 103 53 36 27 |
R10 | 16 17 20 15 20 17 17 |
R11 | 15 15 62 136 41 36 20 |
R13 | 29 16 27 27 29 20 19 |
R14 | 10 16 16 15 23 19 16 |
R15 | 17 25 25 22 25 19 25 |
R17 | 15 33 22 24 18 23 20 |
R19 | 15 19 20 38 25 27 20 |
R20 | 17 16 23 26 25 13 19 |
R23 | 26 20 25 51 46 25 21 |
R24 | 20 19 22 44 30 13 17 |
Table 1.1486.c GPS week : 1486 MJD: 54646.0-54652.0
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 1486 0 | 88 -153 264 -2219 1328 -11350 108.7 3152 3152 | 824193 0
brd 1486 1 | -177 4 347 -1218 -788 -6640 94.9 >>>>> >>>>> | 834022 0
brd 1486 2 | 80 67 117 2680 1416 -21870 98.0 5248 5248 | 819503 0
brd 1486 3 | 15 -111 307 163 2238 -19280 97.7 5097 5097 | 817815 0
brd 1486 4 | 175 -33 338 -1651 2723 -15380 99.4 2816 2816 | 868958 0
brd 1486 5 | 117 73 615 1521 1161 -15640 93.1 4920 4920 | 867601 0
brd 1486 6 | 5 -106 574 -4370 -3110 -14850 103.6 4125 4125 | 866524 0
-------------+------------------------------------------------------------+----------------
brd 1486 mean| 43 -36 366 -727 709 -15001 99.4 >>>>> >>>>> | 842659 0
brd 1486 sdev| 113 90 174 2382 2012 4988 5.3 >>>>> >>>>> | 23987 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 2.1486.0 GPS week: 1486 Day: 0 MJD: 54646
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 66| 4 0 -12 -70 10 -90 -.16 38 30 | 0 -110 2492 2631
cod 212| -4 -3 0 80 -44 71 -.18 25 23 | --- --- --- ---
esx 128| 0 3 4 -49 87 -75 .62 41 32 | 154 -2156 9655 16845
iac n/a| 1 2 10 -51 -32 47 -.07 49 49 | 827257 -7144 9233 14738
mcc n/a| 0 -23 4 -217 757 -800 -2.66 265 265 | --- --- --- ---
Table 2.1486.1 GPS week: 1486 Day: 1 MJD: 54647
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 66| 0 -1 -8 26 12 360 -.15 40 35 | 0 170 2767 3017
cod 212| 0 1 -3 -1 44 -83 -.12 27 27 | --- --- --- ---
esx 128| -1 0 -3 -41 -18 -232 .21 41 36 | 13683 1799 7741 16508
iac n/a| 4 2 16 33 -58 -58 -.07 45 45 | 833345 -1112 7707 12291
mcc n/a| 0 -88 37 -443 137 -425 -.68 486 486 | --- --- --- ---
Table 2.1486.2 GPS week: 1486 Day: 2 MJD: 54648
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 66| -3 -6 -7 52 69 191 -.12 51 48 | 0 18 3024 3224
cod 212| -10 0 -9 -53 -2 100 -.04 39 32 | --- --- --- ---
esx 128| 5 8 -1 5 26 35 .35 75 45 | -11189 5006 6339 11621
iac n/a| -1 0 9 34 3 -279 .02 54 54 | 820910 -1055 8518 14418
mcc n/a| 27 10 33 -201 317 -828 1.11 83 83 | --- --- --- ---
Table 2.1486.3 GPS week: 1486 Day: 3 MJD: 54649
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 66| -2 -3 -6 23 -11 135 -.05 85 49 | 0 -244 2455 2586
cod 212| 0 4 -1 13 -31 40 -.20 53 37 | --- --- --- ---
esx 128| -1 7 24 87 -13 -7 .18 119 88 | -8688 1621 7920 17771
iac n/a| 0 -2 0 -56 6 -399 .17 152 152 | 817938 -339 7767 16208
mcc n/a| -17 -62 27 322 283 2025 1.48 407 407 | --- --- --- ---
Table 2.1486.4 GPS week: 1486 Day: 4 MJD: 54650
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 66| 12 -3 -3 102 69 61 -.21 56 40 | 0 -140 2252 2368
cod 212| -4 -3 -4 -54 13 15 -.11 25 20 | --- --- --- ---
esx 128| -1 -5 10 51 -9 165 .52 89 80 | 45001 4000 6840 15702
iac n/a| 5 2 5 5 49 -139 .06 562 562 | 872122 -4315 6061 13933
mcc n/a| 96 36 33 -67 193 249 .90 659 659 | --- --- --- ---
Table 2.1486.5 GPS week: 1486 Day: 5 MJD: 54651
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 66| 2 0 -4 23 -18 54 -.13 48 41 | 0 -123 1917 2010
cod 212| -1 -1 0 20 1 -39 -.06 28 22 | --- --- --- ---
esx 128| 7 2 -14 -125 -33 52 .88 81 84 | 53366 2368 6169 16275
iac n/a| -2 0 5 14 12 -75 .01 39 39 | 869103 -5883 5508 14981
mcc n/a| -12 -2 34 46 -264 -1273 .23 71 71 | --- --- --- ---
Table 2.1486.6 GPS week: 1486 Day: 6 MJD: 54652
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 66| 0 -5 -4 23 12 282 -.10 40 37 | 0 589 2586 2665
cod 212| -3 0 3 -29 3 -107 -.15 26 23 | --- --- --- ---
esx 128| -3 -6 10 3 -33 57 .68 65 58 | 68111 -1285 7918 25981
iac n/a| 1 2 -5 59 -36 -137 .01 38 38 | 864519 -3234 8119 23221
mcc n/a| -47 -2 28 68 -507 -1185 .70 87 87 | --- --- --- ---
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 3.1486.0 GPS week: 1486 Day: 0 MJD: 54646
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 3192 24 25 37 34 --- 17 | 59 103 86 79 --- 85
R06E | 1695 32 26 51 39 --- 21 | 43 45 79 63 --- 44
R07E | 1937 94 36 46 129 --- 45 | 313 257 288 112 --- 270
R10 | 1928 32 23 19 34 --- 15 | 34 51 53 67 --- 46
R11 | 3660 26 10 28 35 --- 14 | 52 50 56 214 --- 45
R13 | 3933 24 32 88 37 --- 28 | 32 30 62 36 --- 28
R14 | 4330 15 9 24 18 --- 9 | 32 27 36 27 --- 27
R15 | 4433 33 19 38 26 159 17 | 23 42 63 34 34 33
R17 | 2633 23 21 29 29 --- 14 | 44 58 63 34 --- 45
R19 | 3259 22 23 24 31 --- 14 | 109 96 97 105 --- 99
R20 | 1586 31 17 38 34 --- 17 | 34 50 61 52 --- 42
R23 | 2322 42 36 40 61 --- 25 | 27 31 51 77 --- 34
R24 | 3987 39 34 27 31 339 19 | 206 207 208 219 231 208
------+------------------------------------+--------------------------------
RMS | 3152 38 25 41 49 265 |T 77 80 92 86 132 77
WRMS | 3152 30 23 32 49 265 |NE 44 50 62 50 34 45
MEDI | 3192 31 23 37 34 159 |MD 43 50 63 67 34 45
Table 3.1486.1 GPS week: 1486 Day: 1 MJD: 54647
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |>>>>> 61 24 36 28 --- 22 | 67 61 80 58 --- 61
R06E |>>>>> 39 25 25 57 --- 21 | 38 38 53 64 --- 38
R07E | 3650 64 23 47 96 --- 34 | 234 193 274 162 --- 220
R10 |>>>>> 21 25 31 39 --- 16 | 24 33 34 40 --- 28
R11 |>>>>> 29 14 22 36 --- 14 | 55 53 66 250 --- 54
R13 |>>>>> 17 21 30 39 --- 15 | 19 27 57 30 --- 16
R14 |>>>>> 37 13 23 37 --- 16 | 27 30 33 36 --- 24
R15 |>>>>> 52 36 42 45 147 25 | 23 49 71 28 40 35
R17 |>>>>> 34 46 87 44 --- 32 | 30 39 91 21 --- 33
R19 |>>>>> 26 26 52 22 --- 19 | 84 70 110 92 --- 82
R20 |>>>>> 22 24 38 19 --- 15 | 19 47 50 49 --- 36
R23 |>>>>> 41 30 27 40 --- 20 | 36 35 38 39 --- 23
R24 |>>>>> 37 31 33 32 671 19 | 186 182 144 168 335 171
------+------------------------------------+--------------------------------
RMS |>>>>> 40 27 41 45 486 |T 64 65 84 79 187 63
WRMS |>>>>> 35 27 36 45 486 |NE 32 42 63 42 40 36
MEDI |>>>>> 37 25 33 39 147 |MD 36 47 66 49 40 36
Table 3.1486.2 GPS week: 1486 Day: 2 MJD: 54648
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR04E | 5515 76 47 --- 29 --- 37 | 91 84 --- 75 --- 73
R06E | 3326 59 32 49 39 --- 25 | 43 59 86 61 --- 49
R07E |13397 67 53 61 120 --- 45 | 271 245 290 168 --- 259
R10 | 1827 44 28 32 31 --- 19 | 32 64 48 47 --- 42
R11 | 2065 42 65 209 56 --- 61 | 41 53 237 213 --- 53
R13 | 4391 39 42 65 37 --- 26 | 34 36 68 36 --- 28
XR14 | 3118 26 17 --- 24 --- 15 | 28 41 --- 54 --- 37
R15 | 3395 50 44 34 39 83 24 | 37 50 38 40 44 32
R17 | 6445 45 40 29 32 --- 21 | 46 49 48 31 --- 34
R19 | 1543 29 37 34 35 --- 19 | 88 82 75 63 --- 70
R20 | 2387 56 20 34 44 --- 22 | 41 33 43 47 --- 24
R23 | 3671 56 21 37 56 --- 25 | 27 31 42 48 --- 16
R24 | 3306 58 22 34 35 --- 22 | 270 284 301 289 --- 285
------+------------------------------------+--------------------------------
RMS | 5248 51 39 75 54 83 |T 80 85 116 90 44 77
WRMS | 5248 48 32 45 54 83 |NE 43 50 53 45 44 38
MEDI | 3326 50 37 34 37 83 |MD 41 53 68 54 44 42
Table 3.1486.3 GPS week: 1486 Day: 3 MJD: 54649
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 8755 101 44 118 41 --- 44 | 56 52 102 47 --- 39
R06E | 3044 26 22 35 69 --- 21 | 28 46 52 50 --- 32
R07E |12352 227 118 275 94 --- 103 | 667 449 540 411 --- 485
R10 | 3045 18 22 33 33 --- 14 | 34 40 45 54 --- 36
R11 | 1861 67 106 204 495 --- 136 | 59 63 165 774 --- 103
R13 | 2169 60 23 69 42 --- 27 | 32 45 88 49 --- 38
R14 | 2854 15 21 38 28 --- 14 | 23 38 43 35 --- 28
R15 | 2905 25 21 78 33 211 22 | 30 58 108 39 55 49
R17 | 5755 38 32 49 55 --- 24 | 53 42 103 72 --- 54
R19 | 1771 48 53 123 38 --- 38 | 55 76 172 63 --- 69
R20 | 1194 31 21 87 44 --- 25 | 25 38 87 67 --- 33
R23M | 3676 80 32 66 168 --- 50 | 29 31 71 203 --- 56
R24 | 3732 109 48 95 41 535 43 | 225 256 300 228 267 241
------+------------------------------------+--------------------------------
RMS | 5096 85 53 119 152 406 |T 101 94 144 160 161 97
WRMS | 5096 49 37 88 152 406 |NE 36 48 92 54 55 43
MEDI | 3044 48 32 78 42 211 |MD 34 46 102 63 55 49
Table 3.1486.4 GPS week: 1486 Day: 4 MJD: 54650
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 3273 77 43 99 55 --- 35 | 79 84 86 56 --- 62
R06E | 3713 78 13 65 64 --- 29 | 48 53 67 67 --- 43
XR07E | 8113 373 26 105 --- --- 52 | 423 520 529 --- --- 505
R10 | 3107 40 17 57 42 --- 20 | 32 46 84 77 --- 51
R11M | 3052 42 28 125 1938 --- 41 | 92 61 150 9999 --- 69
R13 | 1882 24 27 122 26 --- 28 | 24 33 127 28 --- 28
R14 | 1093 34 11 94 24 --- 22 | 34 46 104 45 --- 39
R15 | 3383 38 22 67 59 107 24 | 33 33 66 49 35 17
R17 | 3144 39 14 32 44 --- 17 | 39 34 41 29 --- 26
R19 | 2905 63 10 80 35 --- 24 | 110 102 98 88 --- 92
R20 | 1385 36 22 85 49 --- 25 | 19 31 107 58 --- 33
R23M | 2524 53 34 134 117 --- 45 | 64 64 98 105 --- 47
R24M | 2977 99 34 40 29 926 29 | 217 302 292 255 157 271
------+------------------------------------+--------------------------------
RMS | 2815 56 25 89 562 659 |T 93 108 142 77 96 98
WRMS | 2815 40 20 80 562 659 |NE 41 46 89 53 35 40
MEDI | 3052 42 22 85 44 107 |MD 48 53 98 58 35 47
Table 3.1486.5 GPS week: 1486 Day: 5 MJD: 54651
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 6005 112 39 100 27 --- 39 | 84 65 81 45 --- 44
R06E | 6761 62 21 76 42 --- 26 | 32 54 88 62 --- 45
R07E | 8850 59 59 99 46 --- 35 | 347 379 409 165 --- 394
R10 | 1291 22 22 60 26 --- 17 | 31 29 86 49 --- 36
R11 | 5722 49 38 77 85 --- 35 | 68 55 78 318 --- 66
R13 | 2842 28 20 60 41 --- 19 | 23 40 86 24 --- 32
R14 | 1760 15 21 84 21 --- 19 | 40 44 89 44 --- 39
R15 | 3729 19 18 70 34 71 18 | 36 32 69 42 41 28
R17 | 7741 60 23 50 33 --- 22 | 30 42 72 31 --- 32
R19 | 3380 31 18 122 33 --- 27 | 129 107 96 128 --- 112
R20 | 1205 29 11 40 16 --- 12 | 51 27 41 21 --- 24
R23 | 2916 18 24 118 21 --- 24 | 58 47 92 46 --- 39
R24 | 3716 26 11 33 25 --- 12 | 128 136 133 121 --- 128
------+------------------------------------+--------------------------------
RMS | 4920 48 28 81 39 71 |T 81 81 109 84 41 78
WRMS | 4920 41 22 84 39 71 |NE 48 45 77 48 41 43
MEDI | 3716 29 21 76 33 71 |MD 51 47 86 46 41 39
Table 3.1486.6 GPS week: 1486 Day: 6 MJD: 54652
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 5058 80 35 77 46 --- 33 | 68 71 77 45 --- 55
R06E | 8072 52 43 103 53 --- 33 | 75 92 77 79 --- 75
R07E | 6049 34 34 78 53 --- 27 | 374 379 340 142 --- 376
R10 | 3184 21 12 58 30 --- 16 | 46 65 92 70 --- 62
R11 | 3451 31 25 66 26 --- 19 | 87 73 94 255 --- 79
R13 | 4459 27 15 45 48 --- 19 | 39 36 49 55 --- 39
R14 | 1306 16 26 35 32 --- 15 | 44 54 40 48 --- 44
R15 | 3696 53 18 74 38 87 24 | 25 42 50 36 45 29
R17 | 3448 39 27 58 24 --- 20 | 41 38 52 28 --- 29
R19 | 2017 41 15 66 20 --- 19 | 131 133 136 131 --- 129
R20 | 1389 32 22 55 33 --- 19 | 48 38 64 61 --- 45
R23 | 4051 24 20 67 39 --- 20 | 69 54 82 77 --- 59
R24 | 1488 25 22 34 39 --- 17 | 108 126 121 125 --- 119
------+------------------------------------+--------------------------------
RMS | 4124 40 26 65 38 87 |T 88 92 98 88 45 87
WRMS | 4124 37 23 58 38 87 |NE 53 58 69 61 45 53
MEDI | 3451 32 22 66 38 87 |MD 68 65 77 70 45 59
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