[IGSREPORT-14888] Wk 1415 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Mar 15 07:08:04 PDT 2007
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IGS Electronic Report 15 Mar 07:08:14 PDT 2007 Message Number 14888
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1415 (Feb 18, 2007 - Feb 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 2.1415.
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:
igl1415[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1415 in the SP3 format.
igl14157.sum Combination Report for GPS Week 1415.
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 | 642.4 ns
1 | 615.7 ns
2 | 673.7 ns
3 | 674.0 ns
4 | 640.6 ns
5 | 700.4 ns
6 | 708.2 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 | R14
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 1.1415, 1a.1415).
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 2.1415.0-6)
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 3.1415.0-6).
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 1415 summary. (Feb 18, 2007 - Feb 24, 2007)
Table 1.1415.a GPS week : 1415 MJD: 54149.0-54155.0
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 53| 0 -1 13 102 -63 -41 -.26 58 50 | 0 1219 4615 5005
| 2 3 6 45 38 408 .13 | 0 1681
cod 171| 1 0 -13 104 -32 79 -.09 46 36 | --- --- --- ---
| 5 2 5 65 66 132 .04 | --- ---
esx 44| -3 2 31 136 -4 -114 -.33 177 69 | -11415 -19137 60484 225638
| 7 5 14 73 104 140 .13 | 756769 72075
iac n/a| 0 -1 -11 -258 54 -49 .25 50 50 | 220934 -303310 337902 432244
| 4 3 8 56 34 181 .10 | 841084 481064
mcc n/a| -10 5 -9 -344 68 1222 -.40 253 253 | --- --- --- ---
| 24 35 71 318 121 439 1.74 | --- ---
Table 1.1415.b GPS week : 1415 MJD: 54149.0-54155.0
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 | 28 23 33 40 27 22 18 |
R02 | 20 16 17 17 31 26 57 |
R03 | 60 90 72 89 0 0 0 |
R04 | 48 25 24 31 27 37 41 |
R06 | 30 48 44 47 37 43 32 |
R07 | 35 21 24 20 21 23 20 |
R08 | 30 36 30 61 22 19 25 |
R10 | 0 45 59 44 32 35 39 |
R14 | 166 203 222 136 473 ---- ---- |
R15 | 0 0 0 0 0 0 0 |
R18 | 52 25 34 27 34 40 39 |
R19 | 20 23 23 22 18 20 18 |
R21 | 0 0 0 0 74 44 30 |
R22 | 0 0 0 1038 119 23 29 |
R23 | 75 59 68 60 64 64 66 |
R24 | 72 72 69 61 71 69 64 |
Table 1.1415.c GPS week : 1415 MJD: 54149.0-54155.0
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 1415 0 | -334 67 -605 -578 -22060 -372400 95.0 6115 6115 | 642362 0
brd 1415 1 | -433 224 -690 -674 -22570 -363400 86.1 6375 6375 | 615654 0
brd 1415 2 | -426 -14 -422 3870 -16600 -362200 92.2 7242 7242 | 673706 0
brd 1415 3 | -70 -214 69 1622 -13740 -356200 92.3 5569 5569 | 673953 0
brd 1415 4 | 329 -466 -590 1426 -12490 -364300 96.9 10310 10310 | 640634 0
brd 1415 5 | -117 -57 -1161 -9736 -19010 -346400 88.3 6928 6928 | 700437 0
brd 1415 6 | 99 43 -493 -3745 -21680 -384000 82.0 7349 7349 | 708164 0
-------------+------------------------------------------------------------+----------------
brd 1415 mean| -136 -59 -556 -1116 -18307 -364128 90.4 7126 7126 | 664987 0
brd 1415 sdev| 285 223 365 4481 4117 11865 5.2 1541 1541 | 33704 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 2.1415.0 GPS week: 1415 Day: 0 MJD: 54149
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 53| 0 0 11 31 -23 76 -.09 44 35 | 0 -30 3453 3958
cod 171| 6 0 -18 37 41 25 -.13 65 33 | --- --- --- ---
esx 44| -12 12 24 167 -187 -89 -.20 158 77 | 22816 16110 9728 16112
iac n/a| 10 -8 -19 -288 53 -177 .26 96 96 | -999999 -999999 999999 999999
mcc n/a| 8 -9 5 -361 223 842 .46 42 42 | --- --- --- ---
Table 2.1415.1 GPS week: 1415 Day: 1 MJD: 54150
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 53| -4 4 23 117 -92 656 -.13 59 53 | 0 3839 9727 10340
cod 171| 2 -2 -6 50 13 -164 -.10 43 34 | --- --- --- ---
esx 44| 2 2 39 265 72 -66 -.32 160 49 | -999999 -44346 16570 23206
iac n/a| 0 0 -18 -265 1 -284 .17 42 42 | 627791 -50263 16581 23677
mcc n/a| -4 -5 14 -257 -121 606 .05 28 28 | --- --- --- ---
Table 2.1415.2 GPS week: 1415 Day: 2 MJD: 54151
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 53| 1 0 14 107 -103 -696 -.22 69 56 | 0 2973 4450 4882
cod 171| 0 -5 -18 108 -54 248 -.12 38 31 | --- --- --- ---
esx 44| 4 0 38 54 47 67 -.30 153 57 | -443734 -8045 12178 18048
iac n/a| 0 -1 -12 -279 16 233 .28 49 49 | -999999 -999999 999999 999999
mcc n/a| 14 -24 -40 -419 161 1148 .91 189 189 | --- --- --- ---
Table 2.1415.3 GPS week: 1415 Day: 3 MJD: 54152
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 53| 1 -2 16 169 -104 20 -.43 75 63 | 0 -234 3819 4210
cod 171| 8 0 -20 66 -148 26 -.09 43 37 | --- --- --- ---
esx 44| -15 5 31 164 92 -337 -.28 210 77 | -116486 -6973 9388 15398
iac n/a| -4 0 1 -173 96 33 .21 35 35 | 618820 18121 8897 14585
mcc n/a| 2 63 -1 -634 68 1496 .34 262 262 | --- --- --- ---
Table 2.1415.4 GPS week: 1415 Day: 4 MJD: 54153
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 53| 2 -4 15 136 -28 -295 -.41 61 58 | 0 700 3356 3618
cod 171| 1 3 -7 95 -79 146 -.09 45 43 | --- --- --- ---
esx 44| 0 -6 7 98 73 -196 -.33 178 70 | 16155 36980 66119 396755
iac n/a| -1 0 -12 -227 59 108 .09 36 36 | 607165 26258 8158 13694
mcc n/a| -6 -12 -99 -371 -40 1212 -4.02 339 339 | --- --- --- ---
Table 2.1415.5 GPS week: 1415 Day: 5 MJD: 54154
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 53| 2 -5 10 84 -70 -66 -.29 48 44 | 0 -459 3611 3935
cod 171| 0 0 -9 143 17 119 .01 39 34 | --- --- --- ---
esx 44| 0 1 29 58 -55 -201 -.28 181 72 | -49761 40737 57165 544119
iac n/a| -2 2 -17 -349 87 -104 .38 52 52 | 783953 46468 88337 471658
mcc n/a| -35 -21 -68 -660 35 1289 -1.22 416 416 | --- --- --- ---
Table 2.1415.6 GPS week: 1415 Day: 6 MJD: 54155
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 53| 3 0 3 68 -19 17 -.21 52 43 | 0 1744 3892 4098
cod 171| -7 1 -12 227 -21 154 -.09 49 37 | --- --- --- ---
esx 44| -5 -1 52 145 -76 22 -.60 198 80 | 1491103 -168424 252243 565828
iac n/a| 0 0 0 -225 61 -156 .38 41 41 | 908808 -163760 243347 502097
mcc n/a| -53 51 121 296 148 1963 .68 494 494 | --- --- --- ---
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 3.1415.0 GPS week: 1415 Day: 0 MJD: 54149
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 3629 27 31 --- 63 --- 27 | 59 43 --- 36 --- 43
R02 | 4676 20 26 62 42 --- 19 | 46 53 90 66 --- 49
XR03 |>>>>> --- 46 --- 74 --- 59 | --- 153 --- 99 --- 139
R04 |10475 42 43 66 164 --- 47 | 58 50 51 157 --- 50
R06 | 6650 40 50 63 69 --- 30 | 71 58 70 53 --- 40
R07 | 3057 34 69 99 59 42 34 | 37 52 70 71 105 33
R08 | 6851 38 50 81 58 --- 30 | 33 54 89 78 --- 39
XR10 | ---- --- 12 --- --- --- 0 | --- 284 --- --- --- 285
XR14 |20111 --- 139 --- 199 --- 165 | --- 437 --- 45 --- 312
XR15 | ---- --- 12 --- --- --- 0 | --- 9999 --- --- --- 9999
R18 | 2839 74 128 62 64 --- 52 | 193 189 170 204 --- 176
R19 | 8234 26 30 62 36 --- 20 | 46 30 63 40 --- 35
XR21 |36929 --- 12 --- --- --- 0 | --- 9999 --- --- --- 9999
XR22 | ---- --- 12 --- --- --- 0 | --- 325 --- --- --- 353
R23 | 2547 41 66 285 181 --- 75 | 57 70 79 195 --- 70
R24 | 4694 60 64 329 67 --- 71 | 303 371 427 366 --- 349
------+------------------------------------+--------------------------------
RMS | 6114 44 65 158 96 42 |T 90 154 123 117 105 140
WRMS | 6114 35 33 77 96 42 |NE 90 154 123 117 105 140
MEDI | 6650 38 43 66 64 42 |MD 57 58 79 71 105 50
Table 3.1415.1 GPS week: 1415 Day: 1 MJD: 54150
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2339 36 32 68 34 --- 22 | 59 36 93 45 --- 37
R02 | 3200 34 16 29 28 --- 15 | 56 70 86 70 --- 64
XR03 |>>>>> --- 91 --- 88 --- 90 | --- 147 --- 141 --- 156
R04 | 6928 63 23 62 31 --- 25 | 71 34 75 49 --- 32
R06 |12826 83 49 198 41 --- 47 | 80 68 142 59 --- 44
R07 | 4192 28 36 69 26 28 20 | 62 43 55 34 39 33
R08 | 5564 76 31 36 75 --- 35 | 57 60 87 118 --- 65
XR10 | 7778 57 33 --- --- --- 45 | 154 209 --- --- --- 205
XR14 |18813 --- 204 --- 202 --- 203 | --- 262 --- 152 --- 190
XR15 | ---- --- 10 --- --- --- 0 | --- 467 --- --- --- 466
R18 | 9203 58 41 56 26 --- 25 | 125 141 139 141 --- 136
R19 | 5432 54 38 38 25 --- 22 | 56 34 41 33 --- 27
XR21 | ---- --- 10 --- --- --- 0 | --- 9999 --- --- --- 9999
XR22 | ---- --- 10 --- --- --- 0 | --- 436 --- --- --- 493
R23 | 2509 46 35 296 60 --- 59 | 45 43 52 60 --- 33
R24 | 3030 83 88 334 42 --- 71 | 182 187 179 163 --- 172
------+------------------------------------+--------------------------------
RMS | 6375 59 43 160 42 28 |T 86 149 94 88 39 143
WRMS | 6375 53 34 49 42 28 |NE 86 149 94 88 39 143
MEDI | 5564 57 33 62 34 28 |MD 62 70 86 60 39 65
Table 3.1415.2 GPS week: 1415 Day: 2 MJD: 54151
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4225 81 37 84 36 --- 32 | 131 56 50 48 --- 49
R02 | 3002 36 23 32 26 --- 16 | 70 37 53 40 --- 34
XR03 |>>>>> --- 62 --- 80 --- 71 | --- 221 --- 71 --- 202
R04 | 5210 61 25 43 40 --- 24 | 73 63 96 73 --- 58
R06 | 6670 116 41 39 81 --- 44 | 95 75 78 56 --- 39
R07 | 5029 42 44 56 29 36 24 | 67 57 74 40 83 40
R08 | 6493 75 26 75 45 --- 30 | 78 44 109 62 --- 28
XR10 | 8591 76 44 --- --- --- 58 | 110 220 --- --- --- 196
XR14 |18449 --- 214 --- 229 --- 221 | --- 354 --- 74 --- 271
XR15 | ---- --- 19 --- --- --- 0 | --- 406 --- --- --- 405
R18 |17836 66 43 88 53 --- 33 | 73 86 160 81 --- 67
R19 | 3424 32 41 50 38 --- 22 | 49 48 54 37 --- 29
XR21 | ---- --- 19 --- --- --- 0 | --- 584 --- --- --- 590
XR22 | ---- --- 19 --- --- --- 0 | --- 346 --- --- --- 452
R23 | 4008 57 44 322 59 --- 68 | 52 64 104 54 --- 41
R24 | 3541 77 50 316 59 265 69 | 200 204 176 193 79 191
------+------------------------------------+--------------------------------
RMS | 7241 69 38 153 49 189 |T 90 179 95 69 81 168
WRMS | 7241 56 31 57 49 189 |NE 90 179 95 69 81 168
MEDI | 5210 66 41 56 45 36 |MD 73 75 78 56 79 58
Table 3.1415.3 GPS week: 1415 Day: 3 MJD: 54152
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7307 120 49 60 39 --- 39 | 165 59 72 49 --- 68
R02 | 3602 31 35 26 23 --- 17 | 114 87 139 97 --- 98
XR03 | ---- --- 65 --- 104 --- 89 | --- 298 --- 100 --- 310
R04 | 1333 31 44 149 31 --- 31 | 61 67 151 52 --- 55
R06 | 3869 134 57 57 57 --- 46 | 94 90 81 50 --- 49
R07 | 7603 41 22 83 18 95 20 | 58 46 92 32 185 33
R08 | 8890 71 47 345 32 --- 61 | 82 63 331 76 --- 69
XR10 |10568 66 69 --- 53 --- 44 | 112 124 --- 58 --- 82
XR14 |16263 --- 155 --- 118 --- 136 | --- 488 --- 66 --- 379
XR15 | ---- --- 17 --- --- --- 0 | --- 353 --- --- --- 351
XR18 |25917 46 37 --- 34 --- 27 | 174 158 --- 155 --- 158
R19 | 2578 30 37 77 29 --- 21 | 31 43 75 27 --- 26
XR21 |17602 --- 15 --- --- --- 0 | --- 358 --- --- --- 365
XR22 |21195 1233 873 --- --- --- 1038 | 350 372 --- --- --- 740
R23 | 6391 55 38 343 41 --- 59 | 52 69 53 73 --- 56
R24 | 3410 80 49 341 28 358 61 | 66 76 152 61 117 54
------+------------------------------------+--------------------------------
RMS | 5568 75 43 210 35 262 |T 113 171 127 68 151 180
WRMS | 5568 63 37 77 35 262 |NE 113 171 127 68 151 180
MEDI | 7307 55 44 83 34 95 |MD 82 87 92 61 117 69
Table 3.1415.4 GPS week: 1415 Day: 4 MJD: 54153
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7887 65 37 68 31 --- 26 | 95 43 50 49 --- 46
R02 | 2574 41 53 117 31 --- 30 | 76 81 126 69 --- 69
XR03 | ---- --- 12 --- --- --- 0 | --- 397 --- --- --- 405
R04 | 2680 71 42 58 25 --- 27 | 68 77 95 94 --- 73
R06 | 7206 98 31 69 57 --- 37 | 77 59 60 40 --- 34
R07 | 8895 40 26 78 24 324 20 | 59 41 73 33 73 34
R08 | 9267 53 29 68 22 --- 22 | 64 49 107 46 --- 44
XR10 | 9576 45 43 --- 45 --- 31 | 87 118 --- 60 --- 101
XR14 |13120 >>>> 353 --- 547 --- 472 | 9 556 --- 56 --- 641
XR15 | ---- --- 12 --- --- --- 0 | --- 556 --- --- --- 554
R18 |26844 58 65 101 41 --- 34 | 123 89 134 77 --- 82
R19 | 2788 48 32 31 16 --- 18 | 36 40 46 34 --- 31
XR21 | 7982 159 107 --- 43 --- 73 | 28 307 --- 55 --- 274
XR22 | 5559 96 77 404 --- 197 119 | 390 213 333 --- 12 206
R23 | 5987 54 41 358 36 --- 64 | 69 61 70 49 --- 47
R24 | 2492 61 68 375 57 353 71 | 81 96 164 97 83 78
------+------------------------------------+--------------------------------
RMS |10312 61 45 178 36 339 |T 90 173 114 58 56 169
WRMS |10312 58 43 70 36 339 |NE 90 173 114 58 56 169
MEDI | 7206 58 41 78 36 324 |MD 69 81 95 55 73 73
Table 3.1415.5 GPS week: 1415 Day: 5 MJD: 54154
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9483 37 22 38 50 --- 21 | 47 50 46 43 --- 31
R02 | 3765 43 38 57 51 --- 26 | 55 73 83 42 --- 50
XR03 | ---- --- 12 --- --- --- 0 | --- 519 --- --- --- 516
R04 | 4622 86 49 60 52 --- 37 | 95 84 81 83 --- 72
R06 | 8207 70 61 98 84 --- 42 | 58 63 124 55 --- 41
R07 | 5199 25 20 118 25 506 23 | 30 45 106 36 130 32
R08 |10773 26 25 78 26 --- 19 | 61 59 103 76 --- 61
XR10 |13691 38 45 --- 63 --- 34 | 91 66 --- 59 --- 73
XR15 | ---- --- 12 --- --- --- 0 | --- 564 --- --- --- 563
R18 |14044 57 55 173 35 --- 40 | 157 185 225 168 --- 174
R19 | 2424 42 33 39 23 --- 20 | 52 47 40 37 --- 32
R21 | 3438 51 31 195 75 --- 43 | 49 207 59 35 --- 205
R22 | 3811 28 30 69 49 182 23 | 266 113 118 17 13 123
R23 | 2172 33 40 362 52 --- 64 | 56 82 136 61 --- 56
R24 | 2419 36 42 390 62 478 69 | 81 98 150 87 43 80
------+------------------------------------+--------------------------------
RMS | 6928 48 39 181 52 416 |T 84 150 105 61 62 140
WRMS | 6928 44 34 72 52 416 |NE 84 150 105 61 62 140
MEDI | 4622 38 33 78 51 478 |MD 58 82 103 55 43 72
Table 3.1415.6 GPS week: 1415 Day: 6 MJD: 54155
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8991 29 29 36 33 --- 18 | 59 42 39 42 --- 36
R02 | 4946 40 43 349 30 --- 57 | 49 59 117 48 --- 41
XR03 | ---- --- 18 --- --- --- 0 | --- 557 --- --- --- 562
R04 | 4437 98 30 66 69 --- 41 | 77 65 76 106 --- 74
R06 |15062 35 64 104 44 --- 31 | 94 101 86 39 --- 60
R07 | 4438 13 22 111 16 --- 19 | 45 45 75 29 --- 31
R08 |10601 47 26 113 22 --- 25 | 40 59 80 52 --- 42
XR10 | 5561 39 51 --- 66 --- 38 | 79 90 --- 53 --- 72
XR15 | ---- --- 18 --- --- --- 0 | --- 245 --- --- --- 244
R18 | 6424 86 50 45 62 --- 38 | 200 188 168 209 --- 194
R19 | 5614 11 37 64 26 --- 18 | 34 37 48 31 --- 25
R21 | 3537 29 61 99 42 --- 29 | 52 226 65 34 --- 245
R22 | 7573 22 25 172 22 284 29 | 222 167 151 14 9 168
R23 | 3150 50 56 385 58 --- 66 | 40 84 120 83 --- 51
R24 | 3393 74 93 337 31 638 64 | 243 167 253 219 42 207
------+------------------------------------+--------------------------------
RMS | 7348 52 49 198 41 494 |T 94 142 106 73 25 136
WRMS | 7348 43 37 80 41 494 |NE 94 142 106 73 25 136
MEDI | 5561 39 37 104 33 284 |MD 59 90 80 48 9 72
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