[IGSREPORT-15844] Wk 1459 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Sat Jan 12 06:19:01 PST 2008
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IGS Electronic Report 12 Jan 06:19:10 PST 2008 Message Number 15844
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1459 (Dec 23, 2007 - Dec 29, 2007)
Contact: Gerd Gendt (gendt at gfz-potsdam.de)
Thomas Nischan ( nisn at gfz-potsdam.de)
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 2.1459.
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:
igl1459[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1459 in the SP3 format.
igl14597.sum Combination Report for GPS Week 1459.
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 | 1443.8 ns
1 | 1438.4 ns
2 | 1449.5 ns
3 | 1424.8 ns
4 | 1427.6 ns
5 | 1416.9 ns
6 | 1396.5 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
----+--------+---------------
0 | ALL | R24
0 | ESX | R19 R20 R23
0 | IAC | R10
1 | ALL | R24
1 | ESX | R19 R20 R23
2 | ALL | R24
2 | ESX | R19 R20 R23
3 | ALL | R24
3 | ESX | R19 R20 R23
4 | ALL | R08
4 | ESX | R19 R20 R23 R24
5 | ALL | R08
5 | ESX | R19 R20 R23 R24
6 | ALL | R24
6 | ESX | R19 R20 R23
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 1.1459, 1a.1459).
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 2.1459.0-6)
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 3.1459.0-6).
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 1459 summary. (Dec 23, 2007 - Dec 29, 2007)
Table 1.1459.a GPS week : 1459 MJD: 54457.0-54463.0
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 56| 2 0 0 -50 10 -15 .14 38 37 | 0 22 2550 2646
| 4 5 7 56 69 193 .19 | 0 80
cod 171| -2 -1 2 57 -58 -2 -.03 37 36 | --- --- --- ---
| 6 5 6 74 39 66 .13 | --- ---
esx 51| -2 0 2 72 114 -21 -.25 266 62 | 1000316 23304 10222 25894
| 8 3 12 109 128 152 .23 | 2355659 29630
iac n/a| 0 -2 -3 -38 -29 97 .16 42 42 | 1429114 4102 8635 22531
| 2 5 6 58 43 81 .21 | 14246 6327
mcc n/a| 0 -36 118 -63 -60 -2194 -.27 267 267 | --- --- --- ---
| 26 70 97 1109 363 1987 2.42 | --- ---
Table 1.1459.b GPS week : 1459 MJD: 54457.0-54463.0
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
------+------------------------------------+------------------------------------------
R01E | 25 26 23 24 20 19 20 |
R04E | 22 25 23 16 19 26 23 |
R06E | 35 31 29 22 12 21 19 |
R07E | 16 18 23 22 25 26 22 |
R08E | 29 23 23 24 --- --- 23 |
R10E | 107 44 23 22 15 19 22 |
R14E | 15 24 21 15 16 14 11 |
R15E | 34 32 38 34 34 26 45 |
R17 | 42 38 41 33 33 27 47 |
R19 | 24 34 23 32 19 31 26 |
R20 | 21 39 34 34 21 24 33 |
R23 | 38 35 46 30 36 40 29 |
R24 | --- --- --- --- 23 32 --- |
Table 1.1459.c GPS week : 1459 MJD: 54457.0-54463.0
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 1459 0 | 293 -549 456 6452 -2891 -38210 90.3 8071 8071 | 1443828 0
brd 1459 1 | -386 143 242 4528 -4262 -28700 104.5 8589 8589 | 1438385 0
brd 1459 2 | -498 -543 490 -9505 -5264 -18750 107.7 10130 10130 | 1449485 0
brd 1459 3 | 285 -262 354 4976 6118 -37320 106.2 8485 8485 | 1424849 0
brd 1459 4 | 913 -93 248 -4472 12220 -49950 110.8 6533 6533 | 1427565 0
brd 1459 5 | -196 1140 107 -10580 9835 -73810 87.3 6583 6583 | 1416940 0
brd 1459 6 | 57 619 -82 -4759 2623 -53220 85.2 5648 5648 | 1396474 0
-------------+------------------------------------------------------------+----------------
brd 1459 mean| 66 64 259 -1908 2625 -42851 98.8 7719 7719 | 1428218 0
brd 1459 sdev| 484 625 200 7145 7027 18025 10.8 1542 1542 | 18009 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 2.1459.0 GPS week: 1459 Day: 0 MJD: 54457
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 56| 9 -3 6 -53 33 281 .02 38 35 | 0 -24 2185 2243
cod 171| -14 -1 -4 -39 -97 -35 .19 43 36 | --- --- --- ---
esx 51| -3 1 -1 -56 24 -294 -.18 254 62 | 10631 2512 6943 18073
iac n/a| 1 1 -8 -9 13 118 .07 40 40 | 1443023 324 5928 15143
mcc n/a| 35 -133 177 1879 242 -1268 .87 426 426 | --- --- --- ---
Table 2.1459.1 GPS week: 1459 Day: 1 MJD: 54458
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 56| 3 0 8 47 79 196 .01 47 48 | 0 147 2695 2841
cod 171| -4 -8 13 107 1 -114 -.05 49 45 | --- --- --- ---
esx 51| -9 -2 6 5 -29 -179 .00 277 68 | 16339 11883 10311 15027
iac n/a| 0 2 -11 -21 -52 -63 -.08 32 32 | 1437675 1722 8699 13969
mcc n/a| -2 -23 139 -1161 53 -2039 -3.01 382 382 | --- --- --- ---
Table 2.1459.2 GPS week: 1459 Day: 2 MJD: 54459
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 56| -5 5 4 -38 20 -256 .20 31 33 | 0 -60 2381 2469
cod 171| 5 -9 5 150 -87 65 -.05 46 49 | --- --- --- ---
esx 51| 2 2 -14 -14 211 70 -.01 207 53 | 13624 8395 6713 11902
iac n/a| 0 0 -7 52 -85 177 -.09 42 42 | 1447850 411 5280 11305
mcc n/a| -19 -133 260 -642 -488 -1758 -3.54 325 325 | --- --- --- ---
Table 2.1459.3 GPS week: 1459 Day: 3 MJD: 54460
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 56| 0 -4 -8 -96 5 -156 .49 45 50 | 0 18 2404 2530
cod 171| 1 -1 1 29 -99 49 -.18 28 30 | --- --- --- ---
esx 51| 11 -1 -5 80 287 38 -.48 270 68 | 48249 14316 12548 21045
iac n/a| 2 0 0 -48 -7 119 .19 44 44 | 1424814 5990 9685 18835
mcc n/a| -33 37 186 -1337 -644 1066 1.85 331 331 | --- --- --- ---
Table 2.1459.4 GPS week: 1459 Day: 4 MJD: 54461
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 56| 0 0 -4 -30 64 -98 -.02 25 22 | 0 102 2263 2330
cod 171| -5 0 8 55 -67 15 .09 38 35 | --- --- --- ---
esx 51| -1 -4 6 56 -7 47 -.15 317 51 | -10064 5335 5444 17012
iac n/a| -2 1 -5 -134 0 150 .34 41 41 | 1425540 -1168 5218 15195
mcc n/a| 32 8 37 428 48 -2075 -1.67 171 171 | --- --- --- ---
Table 2.1459.5 GPS week: 1459 Day: 5 MJD: 54462
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 56| 1 7 -9 -132 -134 7 .26 45 41 | 0 -64 2443 2537
cod 171| 0 -1 -1 127 -34 -49 -.11 31 32 | --- --- --- ---
esx 51| -4 6 25 212 232 59 -.61 249 67 | 604341 34512 13782 32484
iac n/a| -1 -6 -4 -81 -85 136 .24 44 44 | 1415042 17342 11520 27206
mcc n/a| -21 20 20 395 314 -4563 2.32 128 128 | --- --- --- ---
Table 2.1459.6 GPS week: 1459 Day: 6 MJD: 54463
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 56| 5 -6 -1 -47 3 -85 .02 36 33 | 0 37 3484 3572
cod 171| -2 8 -4 -26 -27 54 -.09 25 25 | --- --- --- ---
esx 51| -12 4 0 225 81 110 -.29 290 65 | 6319098 86181 15813 65719
iac n/a| 6 -13 9 -26 8 46 .49 51 51 | 1409859 4099 14119 56070
mcc n/a| 8 -30 9 -4 50 -4721 1.31 109 109 | --- --- --- ---
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 3.1459.0 GPS week: 1459 Day: 0 MJD: 54457
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9687 35 59 39 35 --- 24 | 39 59 62 48 --- 38
R04E | 5516 47 42 26 31 --- 22 | 95 62 71 65 --- 69
R06E | 1631 54 50 57 73 --- 34 | 69 72 98 57 --- 59
R07E | 4414 29 36 28 14 426 16 | 47 47 58 59 150 45
R08E |17477 32 45 83 34 --- 29 | 77 91 57 75 --- 74
XR10E | 4159 95 119 --- 324 --- 107 | 117 105 --- 129 --- 96
XR14E | 3107 20 17 --- 23 --- 14 | 56 57 --- 60 --- 55
XR15E | 5096 53 39 --- 50 1208 34 | 45 37 --- 58 274 35
XR17 | 7227 75 18 --- 64 --- 41 | 82 100 --- 134 --- 105
R19 | 1667 35 29 477 37 --- 24 | 78 75 469 55 --- 80
R20 | 1146 29 29 460 28 --- 20 | 62 76 442 84 --- 90
XR23 | 2593 45 59 --- 57 --- 38 | 141 108 --- 93 --- 102
------+------------------------------------+--------------------------------
RMS | 8070 38 43 254 40 426 |T 85 86 179 90 212 84
WRMS | 8070 35 36 62 40 426 |NE 114 119 363 124 --- 124
MEDI | 4159 35 39 57 35 426 |MD 77 75 71 65 150 74
Table 3.1459.1 GPS week: 1459 Day: 1 MJD: 54458
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |12141 51 50 47 30 --- 25 | 53 73 68 40 --- 51
R04E | 5305 40 57 38 35 --- 24 | 77 99 94 81 --- 82
R06E | 1855 29 67 92 31 --- 31 | 48 67 82 50 --- 36
R07E | 3744 30 26 45 26 382 17 | 63 34 58 69 93 50
R08E |17902 37 35 70 23 --- 23 | 103 90 74 82 --- 89
XR10 | 1883 73 48 --- 61 --- 44 | 89 115 --- 144 --- 115
XR14 | 4813 34 43 --- 24 --- 23 | 39 47 --- 44 --- 42
XR15 |14622 45 38 --- 48 1230 32 | 33 36 --- 73 179 36
XR17 | 7035 76 31 --- 42 --- 38 | 95 48 --- 45 --- 53
R19 | 1206 65 36 481 35 --- 33 | 83 32 306 19 --- 48
R20 | 1202 65 58 534 42 --- 38 | 90 43 311 62 --- 49
XR23 | 7116 54 56 --- 41 --- 35 | 58 60 --- 56 --- 41
------+------------------------------------+--------------------------------
RMS | 8589 47 49 277 32 382 |T 80 76 152 78 136 71
WRMS | 8589 48 45 68 32 382 |NE 87 78 282 87 179 78
MEDI | 4813 45 43 70 35 382 |MD 77 60 82 62 93 50
Table 3.1459.2 GPS week: 1459 Day: 2 MJD: 54459
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |16488 41 22 52 35 --- 22 | 37 36 52 35 --- 31
R04E | 8301 29 48 50 34 --- 23 | 51 54 105 60 --- 49
R06E | 1949 18 66 34 73 --- 29 | 67 57 62 51 --- 49
R07E | 2259 21 58 53 27 325 23 | 64 44 95 71 109 61
R08E |16204 40 25 50 36 --- 22 | 52 76 101 103 --- 70
XR10 | 2776 31 29 --- 34 --- 22 | 76 69 --- 98 --- 78
XR14 | 1911 25 36 --- 26 --- 20 | 53 41 --- 40 --- 42
XR15 |12157 45 48 --- 68 1190 37 | 47 57 --- 59 199 37
XR17 | 7992 60 61 --- 49 --- 40 | 111 41 --- 54 --- 60
R19 | 1980 27 41 496 29 --- 23 | 66 56 379 41 --- 73
XR20 | 1313 37 56 --- 53 --- 33 | 70 80 --- 55 --- 58
XR23 | 7763 54 86 --- 55 --- 46 | 89 97 --- 91 --- 69
------+------------------------------------+--------------------------------
RMS |10134 31 46 207 42 325 |T 70 69 132 67 154 62
WRMS |10134 33 49 53 42 325 |NE 80 79 379 69 199 69
MEDI | 2776 31 48 50 35 325 |MD 66 57 95 59 109 60
Table 3.1459.3 GPS week: 1459 Day: 3 MJD: 54460
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |15483 43 25 71 35 --- 23 | 58 49 77 40 --- 45
R04E | 9109 25 12 46 34 --- 15 | 69 63 50 70 --- 61
R06E | 2207 29 25 59 51 --- 22 | 59 42 59 53 --- 42
R07E | 2389 38 38 53 25 331 22 | 73 32 88 69 229 48
R08E |12860 41 16 43 73 --- 24 | 96 130 67 161 --- 125
XR10 | 2528 37 18 --- 43 --- 22 | 69 62 --- 55 --- 58
XR14 | 5058 21 18 --- 25 --- 14 | 23 27 --- 32 --- 24
XR15 |11379 46 27 --- 76 1073 33 | 54 50 --- 72 435 48
XR17 | 9438 56 32 --- 58 --- 33 | 54 76 --- 76 --- 62
R19 | 1639 60 36 502 30 --- 31 | 48 61 423 48 --- 63
R20 | 1605 66 35 492 38 --- 33 | 57 103 471 98 --- 103
XR23 | 6876 43 38 --- 50 --- 30 | 62 64 --- 61 --- 52
------+------------------------------------+--------------------------------
RMS | 8485 45 28 270 44 331 |T 67 71 176 76 332 69
WRMS | 8485 50 30 68 44 331 |NE 64 76 355 75 435 72
MEDI | 5058 41 25 59 38 331 |MD 59 62 77 69 229 58
Table 3.1459.4 GPS week: 1459 Day: 4 MJD: 54461
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |11789 27 27 39 50 --- 20 | 35 27 32 51 --- 29
R04E | 9625 17 40 40 42 --- 19 | 83 85 120 100 --- 87
R06E | 2378 15 17 16 32 --- 11 | 35 30 26 33 --- 26
R07E | 2023 15 34 68 58 171 24 | 49 34 52 75 138 44
XR10 | 8657 18 22 --- 24 --- 15 | 36 30 --- 39 --- 32
XR14 | 5884 17 25 --- 29 --- 16 | 29 31 --- 28 --- 26
XR15 | 9819 34 45 --- 73 272 34 | 51 53 --- 56 362 43
XR17 | 6316 39 63 --- 27 --- 32 | 60 93 --- 61 --- 64
R19 | 2303 23 27 494 32 --- 18 | 65 50 380 43 --- 62
R20 | 1864 26 38 524 20 --- 20 | 48 64 416 54 --- 68
R23 | 6970 43 66 422 40 --- 36 | 85 50 99 46 --- 51
XR24 | 4715 28 43 --- 23 --- 23 | 145 142 --- 112 --- 131
------+------------------------------------+--------------------------------
RMS | 6533 25 38 317 41 171 |T 62 61 161 60 250 58
WRMS | 6533 22 35 51 41 171 |NE 64 64 298 54 362 59
MEDI | 5884 23 34 68 32 171 |MD 51 50 99 54 138 51
Table 3.1459.5 GPS week: 1459 Day: 5 MJD: 54462
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9988 38 31 33 29 --- 19 | 26 36 55 55 --- 36
R04E | 8959 35 25 68 53 --- 25 | 50 63 114 46 --- 48
R06E | 3596 34 28 51 39 --- 21 | 37 48 71 40 --- 30
R07E | 3012 40 23 66 55 128 26 | 38 29 59 60 117 32
XR10 | 4116 27 23 --- 30 --- 18 | 50 39 --- 48 --- 44
XR14 | 6859 23 15 --- 23 --- 14 | 24 29 --- 27 --- 21
XR15 | 8551 37 26 --- 49 330 25 | 32 48 --- 78 147 46
XR17 | 7565 40 20 --- 54 --- 26 | 85 87 --- 66 --- 74
XR19 | 4101 56 22 --- 53 --- 31 | 30 53 --- 88 --- 46
R20 | 4643 40 25 452 39 --- 24 | 82 91 276 103 --- 97
R23 | 6032 73 47 394 41 --- 39 | 102 49 75 59 --- 72
XR24 | 3818 37 41 --- 60 --- 32 | 105 90 --- 128 --- 99
------+------------------------------------+--------------------------------
RMS | 6582 45 31 249 44 128 |T 61 62 112 73 132 60
WRMS | 6582 41 32 67 44 128 |NE 63 60 175 74 147 62
MEDI | 4643 37 25 66 41 128 |MD 50 49 75 60 117 46
Table 3.1459.6 GPS week: 1459 Day: 6 MJD: 54463
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 6973 28 22 62 28 --- 19 | 33 29 33 35 --- 28
R04E | 8204 32 33 50 50 --- 23 | 37 66 75 60 --- 46
R06E | 3840 25 24 31 51 --- 18 | 49 42 58 55 --- 41
R07E | 1987 37 23 47 50 109 21 | 48 29 42 68 96 44
R08E | 8350 24 23 74 47 --- 23 | 103 143 172 109 --- 119
XR10 | 2790 24 15 --- 53 --- 21 | 48 43 --- 44 --- 38
XR14 | 5657 13 13 --- 20 --- 10 | 24 25 --- 33 --- 25
XR15 | 4755 45 46 --- 103 282 44 | 43 67 --- 111 121 69
XR17 |10929 56 65 --- 82 --- 47 | 51 108 --- 50 --- 62
R19 | 2430 42 20 466 51 --- 26 | 57 87 473 113 --- 108
R20 | 5798 56 24 527 58 --- 32 | 88 107 508 122 --- 118
R23 | 3356 35 27 406 63 --- 28 | 87 49 107 90 --- 82
------+------------------------------------+--------------------------------
RMS | 5647 36 25 290 51 109 |T 64 73 183 83 108 73
WRMS | 5647 33 25 65 51 109 |NE 70 80 362 94 121 84
MEDI | 4755 32 23 62 51 109 |MD 49 66 75 68 96 62
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