[IGSREPORT-15713] Wk 1453 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Nov 29 02:24:18 PST 2007
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IGS Electronic Report 29 Nov 02:24:32 PST 2007 Message Number 15713
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1453 (Nov 11, 2007 - Nov 17, 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 2.1453.
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:
igl1453[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1453 in the SP3 format.
igl14537.sum Combination Report for GPS Week 1453.
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 | 1481.7 ns
1 | 1522.2 ns
2 | 1559.4 ns
3 | 1556.0 ns
4 | 1640.8 ns
5 | 1579.6 ns
6 | 1549.8 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
----+--------+---------------
0 | ESX | R10 R14 R23 R24
1 | ESX | R10 R14 R23 R24
2 | ESX | R10 R14 R19 R23 R24
3 | COD | R19
3 | ESX | R10 R14 R23 R24
4 | ESX | R10 R14 R23 R24
5 | ESX | R10 R14 R23 R24
6 | ESX | R10 R14 R23 R24
6 | IAC | R21
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 1.1453, 1a.1453).
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 2.1453.0-6)
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 3.1453.0-6).
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 1453 summary. (Nov 11, 2007 - Nov 17, 2007)
Table 1.1453.a GPS week : 1453 MJD: 54415.0-54421.0
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 57| 1 0 1 22 -21 -113 -.02 40 41 | 0 691 5522 5967
| 3 2 5 41 44 153 .09 | 0 1759
cod 180| 0 -4 6 -7 17 6 -.02 46 38 | --- --- --- ---
| 3 5 6 85 55 89 .09 | --- ---
esx 54| 2 0 -5 16 84 -51 -.30 215 59 | 141392 -173149 157395 297354
| 8 4 11 80 124 133 .08 | 604497 365056
iac n/a| 0 0 -4 -20 -41 137 .22 43 43 | 1613147 -7534 178207 297242
| 3 2 4 61 34 64 .05 | 669835 17359
mcc n/a| -3 0 41 27 -25 172 .08 476 476 | --- --- --- ---
| 11 5 13 143 229 699 .27 | --- ---
Table 1.1453.b GPS week : 1453 MJD: 54415.0-54421.0
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 | 19 22 22 18 23 17 24 |
R04 | 22 23 19 23 13 16 24 |
R06 | 17 17 14 20 22 27 48 |
R07 | 19 17 14 16 14 13 12 |
R08 | 16 19 21 22 20 19 22 |
R10 | 22 19 17 24 35 23 23 |
R14 | 27 21 17 17 20 24 22 |
R15 | 53 46 62 77 51 41 45 |
R19 | 99 86 76 82 53 81 81 |
R21 | 18 17 15 19 42 46 172 |
R23 | 30 21 22 22 27 28 29 |
R24 | 29 39 20 25 29 27 43 |
Table 1.1453.c GPS week : 1453 MJD: 54415.0-54421.0
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 1453 0 | -33 197 -564 1265 2032 -17470 87.5 5187 5187 | 1481661 0
brd 1453 1 | -232 -24 -226 3309 -4297 -13190 87.9 4312 4312 | 1522225 0
brd 1453 2 | -1 -315 -234 2767 8708 -19780 94.5 4469 4469 | 1559406 0
brd 1453 3 | 344 -159 -121 5597 1160 -23230 98.5 4760 4760 | 1555956 0
brd 1453 4 | 652 -74 259 7723 5158 -35030 101.4 3755 3755 | 1640823 0
brd 1453 5 | 55 -118 -889 1974 4269 -49760 95.4 4086 4086 | 1579585 0
brd 1453 6 | 156 -137 -189 2738 8423 -46640 89.5 4271 4271 | 1549795 0
-------------+------------------------------------------------------------+----------------
brd 1453 mean| 134 -90 -280 3624 3636 -29300 93.5 4405 4405 | 1555635 0
brd 1453 sdev| 288 155 360 2258 4527 14600 5.4 464 464 | 49104 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 2.1453.0 GPS week: 1453 Day: 0 MJD: 54415
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 57| -1 2 6 70 -51 20 .02 28 25 | 0 -2174 4415 5215
cod 180| -5 -4 4 -67 -63 -90 .02 38 32 | --- --- --- ---
esx 54| 18 4 -14 -33 319 -243 -.28 236 68 | 1427903 -61988 60176 999999
iac n/a| -3 1 -3 81 -49 171 .19 31 31 | 2851887 -7746 489567 999999
mcc n/a| -6 -2 57 -116 -214 -830 -.38 393 393 | --- --- --- ---
Table 2.1453.1 GPS week: 1453 Day: 1 MJD: 54416
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 57| 5 -4 -2 9 -28 64 .01 32 31 | 0 -164 4333 4993
cod 180| 2 -3 5 132 -2 -71 .09 38 38 | --- --- --- ---
esx 54| -2 -2 4 44 52 -162 -.48 237 50 | -4044 -29854 10735 22093
iac n/a| -2 0 -11 -108 -43 123 .29 33 33 | 1518413 3497 10297 21865
mcc n/a| 9 -1 43 -89 -66 -485 .09 562 562 | --- --- --- ---
Table 2.1453.2 GPS week: 1453 Day: 2 MJD: 54417
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 57| 0 -2 0 25 -22 17 -.19 25 24 | 0 1453 4164 4482
cod 180| 1 4 -1 80 69 -69 -.05 31 30 | --- --- --- ---
esx 54| -3 -4 9 -79 117 52 -.25 193 57 | 70674 -41233 8688 16018
iac n/a| 0 -2 -3 -44 -63 72 .23 27 27 | 1561390 -2208 8347 16131
mcc n/a| 11 0 48 -49 -99 -224 .38 279 279 | --- --- --- ---
Table 2.1453.3 GPS week: 1453 Day: 3 MJD: 54418
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 57| 2 -1 6 -47 45 -345 -.07 37 37 | 0 753 2776 2946
cod 180| -5 -8 16 -101 -50 14 -.15 37 31 | --- --- --- ---
esx 54| 0 -3 -21 157 64 155 -.25 207 50 | 3378 -40034 6748 14727
iac n/a| 4 1 -8 6 -33 100 .25 21 21 | 1555991 -1335 6240 14194
mcc n/a| 4 0 50 31 -248 270 .03 290 290 | --- --- --- ---
Table 2.1453.4 GPS week: 1453 Day: 4 MJD: 54419
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 57| 2 1 -4 0 7 -161 -.06 45 48 | 0 2173 5315 5742
cod 180| -1 -2 4 -71 51 42 .02 44 33 | --- --- --- ---
esx 54| -3 0 -6 65 -100 -100 -.34 226 66 | 12680 -37741 7250 14078
iac n/a| 4 1 -2 10 27 218 .25 51 51 | 1643021 -138 6665 13908
mcc n/a| -19 -4 43 -31 -136 756 -.04 450 450 | --- --- --- ---
Table 2.1453.5 GPS week: 1453 Day: 5 MJD: 54420
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 57| 5 0 8 68 -5 -147 .03 52 55 | 0 3112 14988 15421
cod 180| 3 -5 0 -1 61 157 -.14 49 47 | --- --- --- ---
esx 54| 0 0 -14 -40 64 -32 -.27 224 65 | -536754 -999999 999999 999999
iac n/a| -2 2 3 -19 -84 59 .16 70 70 | 544609 1284 718563 999999
mcc n/a| -12 -2 31 252 232 1002 .01 623 623 | --- --- --- ---
Table 2.1453.6 GPS week: 1453 Day: 6 MJD: 54421
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 57| -4 -1 -4 32 -93 -242 .08 63 69 | 0 -310 2668 2975
cod 180| 1 -12 13 -24 53 62 .04 84 57 | --- --- --- ---
esx 54| 8 7 5 -1 71 -27 -.23 182 59 | 15911 -1194 8174 14565
iac n/a| -1 -3 -6 -69 -43 213 .20 71 71 | 1616718 -46097 7772 14599
mcc n/a| -10 11 16 198 354 718 .44 733 733 | --- --- --- ---
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 3.1453.0 GPS week: 1453 Day: 0 MJD: 54415
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1537 37 18 47 28 --- 18 | 40 52 83 56 --- 51
R04 | 2511 22 44 38 41 --- 21 | 41 62 48 40 --- 38
R06 | 2735 22 30 51 18 --- 16 | 33 41 74 44 --- 39
R07 | 3123 19 32 64 18 102 18 | 28 38 36 28 31 24
R08 | 2427 26 33 35 20 --- 16 | 28 42 59 42 --- 34
R10 | 2120 37 25 417 26 --- 21 | 112 127 177 124 --- 121
R14 | 1489 15 49 459 44 --- 27 | 28 39 192 40 --- 34
XR15 |10721 43 87 --- 87 223 53 | 106 124 --- 125 31 108
XR19 | ---- --- 76 129 --- --- 99 | --- 287 326 --- --- 327
R21 | 6502 27 34 46 25 --- 18 | 100 69 56 258 --- 70
R23 | 1755 35 53 278 37 --- 29 | 79 112 129 90 --- 87
R24 |13607 32 46 288 42 547 28 | 462 482 488 458 205 464
------+------------------------------------+--------------------------------
RMS | 5186 28 38 236 31 393 |T 96 122 151 118 89 116
WRMS | 5186 25 32 68 31 393 |NE 96 122 151 118 89 116
MEDI | 2511 27 34 64 28 223 |MD 41 62 83 56 31 51
Table 3.1453.1 GPS week: 1453 Day: 1 MJD: 54416
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3696 44 27 34 38 --- 21 | 44 39 53 40 --- 40
R04 | 1721 39 59 34 26 --- 23 | 35 77 72 34 --- 49
R06 | 2296 26 33 34 21 --- 16 | 47 28 45 46 --- 30
R07 | 1943 23 33 36 27 80 17 | 56 40 44 63 26 46
R08 | 2466 22 44 25 36 --- 18 | 37 44 53 65 --- 45
R10 | 1433 16 32 461 29 --- 18 | 129 144 169 144 --- 138
R14 | 1335 20 37 439 29 --- 20 | 36 43 137 48 --- 38
XR15 | 7431 63 56 --- 73 133 46 | 119 97 --- 83 36 88
XR19 | ---- --- 151 80 125 --- 85 | --- 206 306 258 --- 282
R21 | 1972 23 28 38 24 --- 16 | 57 48 74 242 --- 50
R23 | 1815 24 37 262 27 --- 21 | 55 71 70 65 --- 58
R24 |11963 60 41 283 56 791 38 | 344 340 316 328 247 333
------+------------------------------------+--------------------------------
RMS | 4311 32 38 237 33 562 |T 87 98 121 118 103 99
WRMS | 4311 31 38 50 33 562 |NE 87 98 121 118 103 99
MEDI | 1972 24 37 38 29 133 |MD 55 48 72 65 36 49
Table 3.1453.2 GPS week: 1453 Day: 2 MJD: 54417
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5618 19 32 55 41 --- 21 | 35 35 69 38 --- 32
R04 | 1747 36 34 39 18 --- 18 | 30 65 81 58 --- 51
R06 | 1713 22 29 25 22 --- 14 | 37 50 53 49 --- 41
R07 | 1866 24 18 32 19 37 13 | 32 32 34 35 35 26
R08 | 4376 21 53 56 19 --- 21 | 38 45 60 49 --- 34
XR10 | 1563 17 29 --- 24 --- 16 | 92 102 --- 108 --- 99
R14 | 1222 22 22 439 27 --- 17 | 27 37 168 33 --- 25
XR15 | 2666 86 66 --- 98 168 61 | 68 76 --- 163 36 92
XR19 | ---- --- 94 208 60 --- 75 | --- 205 217 229 --- 257
R21 | 1532 19 30 40 20 --- 15 | 55 52 64 248 --- 45
R23 | 1570 26 27 228 38 --- 22 | 102 89 148 70 --- 82
R24 |10642 29 23 285 30 392 20 | 375 356 433 377 319 369
------+------------------------------------+--------------------------------
RMS | 4469 25 31 193 27 279 |T 81 95 132 121 130 96
WRMS | 4469 24 30 57 27 279 |NE 81 95 132 121 130 96
MEDI | 1747 22 29 55 24 168 |MD 38 52 69 58 36 45
Table 3.1453.3 GPS week: 1453 Day: 3 MJD: 54418
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6171 47 27 28 23 --- 18 | 43 57 38 49 --- 41
R04 | 1221 42 34 68 25 --- 23 | 57 65 45 40 --- 40
R06 | 1534 40 37 56 17 --- 20 | 32 45 82 47 --- 35
R07 | 2716 16 38 47 14 55 16 | 34 45 51 47 27 37
R08 | 4936 45 35 61 24 --- 22 | 40 45 67 49 --- 35
XR10 | 1744 24 47 --- 27 --- 23 | 98 124 --- 114 --- 111
R14 | 4602 27 28 435 18 --- 16 | 24 29 139 39 --- 23
XR15 | 9099 121 93 --- 108 164 76 | 106 122 --- 148 31 111
XR19 | ---- --- 262 143 44 --- 82 | --- 154 208 229 --- 227
R21 | 4919 44 34 36 21 --- 19 | 107 34 42 243 --- 52
R23 | 1548 35 36 274 24 --- 21 | 39 61 157 67 --- 54
R24 | 9081 32 55 327 20 407 25 | 190 223 296 208 173 207
------+------------------------------------+--------------------------------
RMS | 4760 37 37 207 21 290 |T 70 83 112 106 77 81
WRMS | 4760 37 31 50 21 290 |NE 70 83 112 106 77 81
MEDI | 4602 40 36 61 23 164 |MD 43 57 67 49 31 41
Table 3.1453.4 GPS week: 1453 Day: 4 MJD: 54419
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5359 34 32 54 38 --- 23 | 23 37 55 32 --- 22
R04 | 1945 16 16 34 19 --- 12 | 36 38 44 35 --- 35
R06 | 1702 24 38 55 28 --- 21 | 51 55 94 49 --- 54
R07 | 3084 21 23 26 22 86 13 | 29 22 29 34 18 22
R08 | 3528 29 28 43 36 --- 19 | 26 38 43 44 --- 27
R10 | 2274 36 52 374 57 --- 34 | 52 90 171 57 --- 59
R14 | 6854 28 27 455 28 --- 20 | 38 24 153 24 --- 22
XR15 | 8498 64 39 --- 102 88 51 | 57 64 --- 81 28 56
R19 | 3507 107 46 93 107 --- 52 | 39 194 221 154 --- 209
R21 | 2732 51 97 58 69 --- 41 | 75 110 51 300 --- 54
R23 | 1755 28 25 282 54 --- 26 | 73 65 131 90 --- 66
R24 | 4768 50 36 336 31 630 28 | 367 360 422 357 92 360
------+------------------------------------+--------------------------------
RMS | 3755 45 44 226 51 450 |T 72 91 128 104 46 82
WRMS | 3755 48 33 66 51 450 |NE 72 91 128 104 46 82
MEDI | 3084 29 32 58 36 88 |MD 39 55 94 49 28 54
Table 3.1453.5 GPS week: 1453 Day: 5 MJD: 54420
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4428 33 27 30 25 --- 17 | 35 37 43 26 --- 30
R04 | 3219 32 25 30 23 --- 16 | 27 44 33 29 --- 23
R06 | 2780 62 33 56 25 --- 27 | 56 28 55 34 --- 27
R07 | 2018 20 23 31 16 98 13 | 21 44 49 33 18 33
R08 | 4852 23 40 27 35 --- 18 | 29 36 34 46 --- 29
R10 | 2724 19 30 366 42 --- 22 | 73 69 110 103 --- 79
R14 | 5837 31 28 499 41 --- 24 | 26 38 228 30 --- 22
XR15 | 8007 58 46 --- 69 105 41 | 74 102 --- 90 28 70
R19 | 3460 126 113 103 197 --- 80 | 29 189 168 180 --- 181
R21 | 6351 44 77 116 66 --- 45 | 224 152 136 661 --- 167
R23 | 1807 42 34 251 43 --- 28 | 27 52 105 79 --- 45
R24 | 4615 42 18 275 48 875 27 | 457 463 525 466 96 461
------+------------------------------------+--------------------------------
RMS | 4086 52 49 224 70 623 |T 89 104 135 148 47 97
WRMS | 4086 55 47 65 70 623 |NE 89 104 135 148 47 97
MEDI | 3460 33 30 103 41 105 |MD 29 44 105 46 28 33
Table 3.1453.6 GPS week: 1453 Day: 6 MJD: 54421
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5740 29 44 38 54 --- 24 | 35 64 58 26 --- 38
R04 | 3692 40 32 51 34 --- 24 | 37 39 50 35 --- 37
R06 | 3361 74 152 53 38 --- 47 | 49 121 79 49 --- 49
R07 | 828 26 22 17 18 66 12 | 30 39 35 31 22 28
R08 | 3032 35 66 22 25 --- 22 | 29 68 47 40 --- 36
R10 | 2401 20 41 365 35 --- 23 | 62 56 139 88 --- 63
XR14 | 2444 28 22 --- 38 --- 22 | 30 32 --- 33 --- 24
XR15 | 7366 62 35 --- 79 122 45 | 80 107 --- 128 33 99
R19 | 5690 146 148 79 186 --- 81 | 34 254 253 191 --- 272
XR21 | 9008 146 201 --- 1966 --- 172 | 209 150 --- 9999 --- 170
R23 | 1576 14 58 276 43 --- 29 | 81 89 176 73 --- 77
R24 | 7468 67 73 271 37 1034 42 | 542 562 616 539 149 544
------+------------------------------------+--------------------------------
RMS | 4271 63 84 181 71 733 |T 101 131 161 112 68 119
WRMS | 4271 69 57 59 71 733 |NE 101 131 161 112 68 119
MEDI | 3361 35 44 53 38 122 |MD 37 68 79 49 33 49
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