[IGSREPORT-15739] Wk 1454 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Mon Dec 10 03:50:13 PST 2007
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IGS Electronic Report 10 Dec 03:50:17 PST 2007 Message Number 15739
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1454 (Nov 18, 2007 - Nov 24, 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 2.1454.
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:
igl1454[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1454 in the SP3 format.
igl14547.sum Combination Report for GPS Week 1454.
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 | 1545.9 ns
1 | 1547.9 ns
2 | 1523.1 ns
3 | 1553.6 ns
4 | 1418.1 ns
5 | 1503.1 ns
6 | 1500.1 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 | R10 R14 R23 R24
1 | COD | R07
1 | ESX | R10 R14 R23 R24
1 | IAC | R15
2 | COD | R07
2 | ESX | R10 R14 R23 R24
3 | COD | R07
3 | ESX | R10 R14 R23 R24
4 | COD | R07
4 | ESX | R10 R14 R23 R24
5 | ESX | R10 R14 R23 R24
6 | ESX | R10 R14 R23 R24
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 1.1454, 1a.1454).
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 2.1454.0-6)
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 3.1454.0-6).
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 1454 summary. (Nov 18, 2007 - Nov 24, 2007)
Table 1.1454.a GPS week : 1454 MJD: 54422.0-54428.0
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 55| 2 1 7 -42 6 -25 -.05 68 44 | 0 -2498 7561 8755
| 6 4 13 61 81 166 .12 | 0 7297
cod 177| -1 -4 5 58 -17 -106 -.02 52 46 | --- --- --- ---
| 2 4 10 81 80 129 .08 | --- ---
esx 51| -1 3 -9 15 55 161 -.18 183 67 | -163634 1465 8203 16762
| 6 7 5 115 128 214 .13 | 371933 11321
iac n/a| 1 1 -2 -33 -36 69 .27 67 67 | 1518147 -3913 8051 17093
| 3 5 11 61 59 119 .17 | 51956 9250
mcc n/a| -1 -1 9 6 -9 210 .03 280 280 | --- --- --- ---
| 5 4 25 17 25 557 .08 | --- ---
Table 1.1454.b GPS week : 1454 MJD: 54422.0-54428.0
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 | 32 22 24 32 18 16 18 |
R04 | 12 20 25 28 13 27 20 |
R06 | 19 23 25 24 18 33 31 |
R07 | 28 0 --- --- --- 145 180 |
R08 | 27 24 23 39 25 24 24 |
R10E | 27 31 84 213 116 0 0 |
R14E | 25 17 17 26 32 40 88 |
R15E | 91 62 2453 0 0 0 0 |
R19 | 74 68 64 89 72 65 69 |
R20 | --- 0 0 0 84 106 66 |
R21 | 1119 0 0 0 0 0 0 |
R23 | 45 34 43 40 34 21 30 |
R24 | 26 75 32 53 57 61 18 |
Table 1.1454.c GPS week : 1454 MJD: 54422.0-54428.0
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 1454 0 | 135 68 164 -674 4353 -50380 88.2 4688 4688 | 1545940 0
brd 1454 1 | 126 145 -599 324 5083 -45070 86.8 4876 4876 | 1547880 0
brd 1454 2 | -178 -22 -684 -173 4022 -37170 87.7 4770 4770 | 1523089 0
brd 1454 3 | 163 -142 -367 2052 -1991 -40200 82.2 4953 4953 | 1553623 0
brd 1454 4 | -279 -5 -615 -1514 9603 -39000 83.8 4339 4339 | 1418061 0
brd 1454 5 | 32 68 -602 -616 4075 -42010 73.1 5351 5351 | 1503077 0
brd 1454 6 | -115 -118 -232 -318 -3311 -35190 98.3 4424 4424 | 1500139 0
-------------+------------------------------------------------------------+----------------
brd 1454 mean| -16 -1 -419 -131 3119 -41288 85.7 4771 4771 | 1513115 0
brd 1454 sdev| 174 104 303 1114 4408 5132 7.6 340 340 | 47136 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 2.1454.0 GPS week: 1454 Day: 0 MJD: 54422
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 55| 0 0 0 38 17 -83 -.00 51 42 | 0 -256 1974 2160
cod 177| -1 -13 9 54 -31 -163 -.05 60 57 | --- --- --- ---
esx 51| 6 8 -7 32 44 274 -.23 233 65 | -999999 -1115 6222 14538
iac n/a| 4 0 4 -58 -20 43 .01 63 63 | 1569758 -19498 5701 14672
mcc n/a| -13 -11 67 45 -68 1476 .20 351 351 | --- --- --- ---
Table 2.1454.1 GPS week: 1454 Day: 1 MJD: 54423
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 55| 9 -6 12 33 -35 -154 -.20 74 41 | 0 497 2778 2998
cod 177| 3 -3 6 -77 -64 6 .15 55 48 | --- --- --- ---
esx 51| -14 7 -2 144 -18 548 -.22 271 67 | 16025 4412 6747 12656
iac n/a| 5 -2 -2 56 -114 -2 .33 55 55 | 1558187 -6445 6462 12640
mcc n/a| 0 0 0 0 0 0 .0 237 237 | --- --- --- ---
Table 2.1454.2 GPS week: 1454 Day: 2 MJD: 54424
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 55| 0 8 -10 -129 -72 246 .13 62 41 | 0 -2779 4660 5412
cod 177| -3 -5 16 57 75 -327 -.11 57 53 | --- --- --- ---
esx 51| -3 0 -8 158 83 182 -.31 205 69 | -29851 -2269 5842 14819
iac n/a| 1 6 -4 -101 -70 -20 .33 51 51 | 1524905 -1677 5793 15184
mcc n/a| 0 0 0 0 0 0 .0 368 368 | --- --- --- ---
Table 2.1454.3 GPS week: 1454 Day: 3 MJD: 54425
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 55| 5 4 32 -88 153 111 .02 117 63 | 0 -61 3512 3760
cod 177| 0 -5 -4 156 -129 -179 .03 58 49 | --- --- --- ---
esx 51| -1 0 -12 43 188 -3 -.25 189 90 | 40914 12330 6616 15604
iac n/a| -1 9 -11 -60 -3 281 .19 68 68 | 1549585 6625 6748 16071
mcc n/a| 0 0 0 0 0 0 .0 1008 1008 | --- --- --- ---
Table 2.1454.4 GPS week: 1454 Day: 4 MJD: 54426
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 55| -2 2 1 -41 -16 39 .01 67 44 | 0 -18431 29037 34595
cod 177| 0 0 17 146 35 -108 -.07 44 37 | --- --- --- ---
esx 51| 3 -1 -8 -139 -47 136 .08 200 55 | -112968 17300 8698 18851
iac n/a| -3 4 -18 -90 -25 -55 .42 70 70 | 1415611 6753 8471 17979
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1454.5 GPS week: 1454 Day: 5 MJD: 54427
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 55| -6 4 11 -64 -67 -107 -.19 55 42 | 0 3918 7955 8889
cod 177| -3 -1 0 72 73 -11 -.03 54 43 | --- --- --- ---
esx 51| 0 -4 -19 -12 -107 117 -.08 85 56 | -23188 -17229 15754 24683
iac n/a| 1 -6 0 39 62 69 .10 70 70 | 1506646 -9752 15801 26055
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1454.6 GPS week: 1454 Day: 6 MJD: 54428
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 55| 9 0 4 -49 69 -233 -.13 50 34 | 0 -379 3014 3472
cod 177| -1 0 -11 -1 -79 36 -.06 38 38 | --- --- --- ---
esx 51| -3 15 -6 -116 249 -126 -.24 100 68 | -36372 -3170 7544 16186
iac n/a| 1 -2 16 -16 -86 172 .49 92 92 | 1502340 -3403 7381 17053
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
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 3.1454.0 GPS week: 1454 Day: 0 MJD: 54422
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3557 39 46 79 53 --- 32 | 54 65 71 47 --- 45
R04 | 2951 20 18 23 22 --- 12 | 42 54 54 54 --- 47
R06 | 4328 20 33 48 27 --- 19 | 26 38 57 45 --- 32
R07 | 708 50 70 33 25 57 27 | 4 9999 9 60 21 191
R08 | 3670 38 52 51 41 --- 26 | 31 58 50 54 --- 35
R10 | 2056 29 47 368 36 --- 26 | 56 112 60 20 --- 92
R14 | 4425 34 47 422 22 --- 25 | 55 62 176 53 --- 67
XR15 | 4592 90 96 --- 180 1117 90 | 429 166 --- 29 299 194
R19 | 5244 113 121 100 164 --- 73 | 145 137 155 173 --- 134
XR21 | ---- --- 741 --- 1376 --- 1118 | --- 229 --- 1 --- 590
R23 | 2073 64 58 287 65 --- 44 | 40 99 191 108 --- 81
R24 |10490 27 48 353 33 493 25 | 216 217 295 255 227 242
------+------------------------------------+--------------------------------
RMS | 4687 51 60 233 63 351 |T 99 112 111 74 182 145
WRMS | 4687 42 57 65 63 351 |NE 99 112 111 74 182 145
MEDI | 3670 38 48 79 36 493 |MD 54 99 60 53 227 81
Table 3.1454.1 GPS week: 1454 Day: 1 MJD: 54423
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3092 39 22 31 51 --- 22 | 72 40 53 46 --- 44
R04 | 2263 48 14 45 25 --- 20 | 34 44 53 49 --- 33
R06 | 3588 24 44 61 28 --- 23 | 29 39 70 37 --- 24
XR07 | 1296 --- 294 --- 8 --- 0 | --- 9999 --- 59 --- 175
R08 | 3906 29 39 70 21 --- 23 | 34 37 50 47 --- 28
R10 | 2401 37 39 479 52 --- 31 | 64 153 66 26 --- 122
R14 | 5738 24 24 447 21 --- 16 | 50 57 184 65 --- 63
XR15 | 5378 68 55 --- 728 663 61 | 674 204 --- 13 234 489
R19 | 3362 124 113 120 113 --- 67 | 134 90 112 86 --- 86
XR20 | ---- --- 8 --- --- --- 0 | --- 864 --- --- --- 867
XR21 | ---- --- 8 --- --- --- 0 | --- 358 --- --- --- 306
R23 | 2386 47 45 306 50 --- 33 | 31 49 60 47 --- 32
R24 |10746 158 82 335 64 237 75 | 240 234 270 207 199 211
------+------------------------------------+--------------------------------
RMS | 4876 74 55 271 55 237 |T 136 180 102 62 216 190
WRMS | 4876 41 48 67 55 237 |NE 136 180 102 62 216 190
MEDI | 3362 39 39 120 50 237 |MD 50 57 66 47 199 86
Table 3.1454.2 GPS week: 1454 Day: 2 MJD: 54424
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4093 30 34 64 35 --- 24 | 46 28 93 67 --- 55
R04 | 747 42 23 58 45 --- 25 | 45 50 63 51 --- 44
R06 | 2069 44 61 35 29 --- 25 | 51 46 60 48 --- 36
R08 | 3964 42 40 48 24 --- 22 | 29 58 33 31 --- 25
XR10E | 2206 133 122 --- 101 --- 83 | 81 234 --- 25 --- 179
R14E | 6152 26 22 400 25 --- 17 | 41 41 145 34 --- 39
XR15E | 3570 2619 2297 --- --- 1690 2452 | 362 85 --- --- 470 9999
R19 | 1326 139 106 93 100 --- 63 | 187 71 110 90 --- 81
XR20 | ---- --- 21 --- --- --- 0 | --- 343 --- --- --- 352
XR21 | ---- --- 21 --- --- --- 0 | --- 426 --- --- --- 425
R23 | 2208 47 64 289 65 --- 42 | 44 84 90 35 --- 50
R24 |10008 46 55 271 34 368 32 | 197 200 207 186 478 184
------+------------------------------------+--------------------------------
RMS | 4769 62 57 205 51 368 |T 108 138 100 63 474 133
WRMS | 4769 41 53 69 51 368 |NE 85 145 93 72 478 139
MEDI | 2208 44 40 64 35 368 |MD 46 71 90 48 470 55
Table 3.1454.3 GPS week: 1454 Day: 3 MJD: 54425
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4079 32 50 85 33 --- 31 | 49 45 112 54 --- 44
R04 | 1481 53 27 60 51 --- 27 | 39 44 100 64 --- 59
R06 | 3164 66 47 17 31 --- 24 | 31 61 46 61 --- 46
R08 | 4378 64 76 86 29 --- 38 | 47 75 102 67 --- 40
XR10E | 3081 300 153 --- --- --- 212 | 197 170 --- --- --- 154
R14E | 6005 31 40 310 36 --- 26 | 57 84 139 81 --- 76
XR15E | 8600 --- 16 --- --- 1456 0 | --- 285 --- --- 134 840
R19 | 1577 272 102 99 150 --- 88 | 225 64 128 175 --- 74
XR20 | ---- --- 16 --- --- --- 0 | --- 475 --- --- --- 480
XR21 | ---- --- 16 --- --- --- 0 | --- 305 --- --- --- 275
R23 | 2322 67 49 298 58 --- 40 | 44 52 178 57 --- 47
R24 |10211 132 33 269 63 1008 52 | 184 63 128 68 419 69
------+------------------------------------+--------------------------------
RMS | 4953 117 58 189 68 1008 |T 97 143 116 78 276 183
WRMS | 4953 63 49 90 68 1008 |NE 88 131 113 78 419 126
MEDI | 3164 66 40 86 36 1008 |MD 49 64 112 64 134 69
Table 3.1454.4 GPS week: 1454 Day: 4 MJD: 54426
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5705 26 32 36 27 --- 18 | 45 64 51 64 --- 50
R04 | 2526 21 15 27 26 --- 13 | 38 40 70 33 --- 35
R06 | 6017 23 32 36 29 --- 18 | 22 79 38 44 --- 35
R08 | 3965 53 21 54 42 --- 24 | 39 40 58 44 --- 27
XR10E | 3902 151 88 --- --- --- 116 | 179 171 --- --- --- 140
R14E | 5458 50 48 396 34 --- 32 | 40 63 163 54 --- 48
XR15E | 8439 --- 15 --- --- 1548 0 | --- 105 --- --- 162 294
R19 | 2401 142 88 112 166 --- 72 | 129 97 144 214 --- 114
XR20 | 4520 102 70 --- --- --- 83 | 53 303 --- --- --- 286
XR21 |21490 --- 15 --- --- --- 0 | --- 210 --- --- --- 245
R23 | 2320 69 34 324 44 --- 34 | 72 81 188 49 --- 65
XR24 | 9192 --- 43 302 74 952 57 | --- 66 188 65 282 52
------+------------------------------------+--------------------------------
RMS | 4339 67 44 200 70 0 |T 68 109 112 70 222 115
WRMS | 4339 44 37 55 70 0 |NE 56 108 105 73 282 101
MEDI | 4520 53 32 54 34 952 |MD 45 79 70 49 162 52
Table 3.1454.5 GPS week: 1454 Day: 5 MJD: 54427
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5784 17 16 50 29 --- 16 | 32 45 41 34 --- 32
R04 | 1007 53 16 89 25 --- 27 | 25 44 99 50 --- 42
R06 | 8808 23 67 67 60 --- 32 | 26 63 58 70 --- 38
XR07 | ---- --- 132 --- 158 327 144 | --- 728 --- 50 36 243
R08 | 5051 55 21 52 39 --- 24 | 29 31 52 41 --- 24
XR10E | 4451 --- 6 --- --- --- 0 | --- 180 --- --- --- 170
XR14E | 4399 49 53 --- 64 --- 39 | 61 117 --- 106 --- 114
XR15E |14380 --- 6 --- --- 1384 0 | --- 246 --- --- 124 335
R19 | 2362 92 96 137 133 --- 65 | 114 110 173 168 --- 125
XR20 | 8896 127 113 --- 200 --- 105 | 30 273 --- 51 --- 320
XR21 |17893 --- 6 --- --- --- 0 | --- 239 --- --- --- 238
XR23 | 2056 --- 17 272 24 --- 21 | --- 94 177 88 --- 87
XR24 |10528 --- 54 376 67 1174 60 | --- 95 219 101 131 88
------+------------------------------------+--------------------------------
RMS | 5350 55 54 85 70 0 |T 45 174 117 75 97 142
WRMS | 5350 42 43 56 70 0 |NE 42 172 117 72 83 123
MEDI | 5051 53 21 89 60 1174 |MD 30 110 99 51 124 114
Table 3.1454.6 GPS week: 1454 Day: 6 MJD: 54428
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2819 32 18 45 36 --- 17 | 52 42 61 33 --- 41
R04 | 2409 30 17 48 49 --- 19 | 34 46 77 43 --- 42
R06 | 7678 30 19 78 95 --- 31 | 28 53 71 82 --- 34
XR07 | ---- --- 65 --- 313 809 180 | --- 665 --- 52 30 498
R08 | 3891 33 26 68 49 --- 23 | 36 47 65 42 --- 31
XR10E | 4130 --- 8 --- --- --- 0 | --- 243 --- --- --- 253
XR14E | 3148 --- 35 --- 150 --- 87 | --- 106 --- 159 --- 105
XR15E | 9013 --- 8 --- --- 1450 0 | --- 286 --- --- 117 317
R19 | 3160 92 74 186 164 --- 69 | 121 98 216 196 --- 121
XR20 | 7543 56 52 --- 175 --- 65 | 31 308 --- 49 --- 322
XR21 |12250 --- 8 --- --- --- 0 | --- 168 --- --- --- 201
XR23 | 1711 --- 17 274 47 --- 29 | --- 95 207 51 --- 79
XR24 | 8291 --- 14 332 24 1487 18 | --- 92 262 91 279 86
------+------------------------------------+--------------------------------
RMS | 4423 50 38 100 92 0 |T 50 173 137 79 142 163
WRMS | 4423 34 38 68 92 0 |NE 50 161 137 71 154 145
MEDI | 3891 32 18 78 49 1450 |MD 34 98 77 51 117 105
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