[IGSREPORT-15205] Wk 1429 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Wed Jun 20 06:25:54 PDT 2007
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IGS Electronic Report 20 Jun 06:26:18 PDT 2007 Message Number 15205
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1429 (May 27, 2007 - Jun 02, 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 2.1429.
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:
igl1429[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1429 in the SP3 format.
igl14297.sum Combination Report for GPS Week 1429.
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 | 1024.4 ns
1 | 1058.8 ns
2 | 1067.1 ns
3 | 1008.1 ns
4 | 1069.8 ns
5 | 1078.2 ns
6 | 1079.5 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 | BKG | R07
0 | ESX | R23 R24
1 | BKG | R22
1 | ESX | R23 R24
2 | COD | R22
2 | ESX | R23 R24
3 | ESX | R23 R24
4 | ESX | R23 R24
5 | COD | R10 R22
5 | ESX | R21 R23 R24
6 | BKG | R22
6 | ESX | R21 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 1.1429, 1a.1429).
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 2.1429.0-6)
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 3.1429.0-6).
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 1429 summary. (May 27, 2007 - Jun 02, 2007)
Table 1.1429.a GPS week : 1429 MJD: 54247.0-54253.0
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 60| 0 0 0 93 -60 35 -.07 244 36 | 0 229 4036 4311
| 2 3 6 44 21 212 .04 | 0 349
cod 172| -2 0 -8 128 -59 52 .05 58 39 | --- --- --- ---
| 4 2 9 42 41 164 .11 | --- ---
esx 49| 0 4 14 279 73 -243 -.24 173 69 | 4207557 489557 298833 306132
| 6 5 14 151 130 241 .20 | 5434516 892697
iac n/a| 0 0 -1 -257 74 -32 .18 36 36 | 571044 311369 314435 584076
| 2 2 7 41 69 171 .05 | 869183 801169
mcc n/a| -11 0 -5 -176 -61 832 -.13 171 171 | --- --- --- ---
| 8 5 22 185 298 922 .31 | --- ---
Table 1.1429.b GPS week : 1429 MJD: 54247.0-54253.0
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 | 546 121 60 26 23 31 30 |
R03 | 22 17 19 28 20 22 24 |
R04 | 29 16 15 18 19 20 20 |
R06 | 30 24 23 16 26 26 20 |
R07 | 161 35 24 21 22 16 15 |
R08 | 21 36 24 15 18 20 16 |
R10E | 34 34 24 25 33 104 123 |
R14E | 23 17 33 34 22 19 30 |
R15E | 0 0 0 0 0 0 0 |
R19 | 17 28 22 31 23 16 20 |
R21 | 28 24 20 32 33 26 21 |
R22 | 111 138 183 47 60 144 213 |
R23 | 33 54 32 41 21 26 23 |
R24 | 21 21 21 25 28 26 32 |
Table 1.1429.c GPS week : 1429 MJD: 54247.0-54253.0
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 1429 0 | -166 -340 -1283 4940 -6304 -334200 88.7 7873 7873 | 1024439 0
brd 1429 1 | 103 318 -909 -6172 -297 -320500 94.8 4473 4473 | 1058839 0
brd 1429 2 | 68 118 -632 -4359 6519 -317900 86.3 5152 5152 | 1067071 0
brd 1429 3 | -79 1113 -709 -16490 2148 -324600 86.5 7337 7337 | 1008118 0
brd 1429 4 | -111 -515 -764 2689 6452 -323100 85.6 5318 5318 | 1069848 0
brd 1429 5 | 431 -183 -623 -21 -7223 -329800 99.1 5045 5045 | 1078188 0
brd 1429 6 | 162 71 -572 2452 -1404 -331200 96.6 4875 4875 | 1079490 0
-------------+------------------------------------------------------------+----------------
brd 1429 mean| 58 83 -785 -2423 -15 -325900 91.1 5724 5724 | 1055141 0
brd 1429 sdev| 204 536 246 7366 5518 5984 5.6 1320 1320 | 27839 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 2.1429.0 GPS week: 1429 Day: 0 MJD: 54247
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 60| 3 2 0 123 -85 322 -.03 1486 59 | 0 119 3528 3763
cod 172| -10 3 -9 114 -135 -138 .06 130 42 | --- --- --- ---
esx 49| -2 9 -10 -33 169 -712 -.28 202 101 | 9999999 34454 19474 23906
iac n/a| 1 0 0 -253 99 -137 .25 52 52 | -628277 19844 375507 999999
mcc n/a| 0 0 0 0 0 0 .0 270 270 | --- --- --- ---
Table 2.1429.1 GPS week: 1429 Day: 1 MJD: 54248
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 60| 0 2 7 65 -41 -256 -.05 43 34 | 0 383 3625 3822
cod 172| 0 0 -14 69 -79 167 -.13 55 39 | --- --- --- ---
esx 49| -6 9 19 387 -116 -316 .09 167 59 | 9999999 -23555 16597 24837
iac n/a| -4 -1 -4 -264 161 180 .11 38 38 | -604404 -4630 287219 999999
mcc n/a| -23 2 -47 -449 -705 2732 -.25 208 208 | --- --- --- ---
Table 2.1429.2 GPS week: 1429 Day: 2 MJD: 54249
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 60| 0 1 -11 172 -40 -209 -.11 60 38 | 0 823 3405 3838
cod 172| -5 0 -23 173 -51 -53 .08 58 37 | --- --- --- ---
esx 49| 11 -6 27 219 -26 -109 -.50 171 69 | 9999999 1287495 999999 999999
iac n/a| 2 1 2 -184 46 178 .17 28 28 | 498096 30404 484578 999999
mcc n/a| -20 -8 -21 24 151 194 -.59 92 92 | --- --- --- ---
Table 2.1429.3 GPS week: 1429 Day: 3 MJD: 54250
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 60| 0 0 0 104 -77 240 -.10 39 38 | 0 -279 4318 4602
cod 172| -1 0 -5 93 -62 -101 .06 34 31 | --- --- --- ---
esx 49| 8 4 24 370 146 52 -.04 158 71 | -999999 -35108 19298 36890
iac n/a| 0 -1 3 -236 67 -34 .20 39 39 | 994150 20657 18305 33376
mcc n/a| -5 7 15 -107 -53 403 -.41 98 98 | --- --- --- ---
Table 2.1429.4 GPS week: 1429 Day: 4 MJD: 54251
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 60| -5 -2 6 44 -41 29 -.06 30 30 | 0 256 3550 3681
cod 172| -2 -2 -2 186 0 226 -.07 37 36 | --- --- --- ---
esx 49| -3 0 11 327 251 -255 -.30 159 59 | 53087 -12477 17287 26290
iac n/a| 3 6 -14 -321 -51 -152 .17 33 33 | 1076812 -3256 16286 24697
mcc n/a| -14 5 16 -126 168 673 -.04 159 159 | --- --- --- ---
Table 2.1429.5 GPS week: 1429 Day: 5 MJD: 54252
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 60| 0 0 3 82 -52 58 -.12 23 22 | 0 345 6237 6603
cod 172| 4 -4 6 110 -56 263 .20 44 41 | --- --- --- ---
esx 49| -1 9 0 284 -19 -258 -.32 184 59 | 48421 -14370 19178 31006
iac n/a| -2 0 -6 -274 138 -274 .22 37 37 | 1086295 -11340 19154 30469
mcc n/a| -4 -1 2 -406 73 1208 .07 235 235 | --- --- --- ---
Table 2.1429.6 GPS week: 1429 Day: 6 MJD: 54253
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 60| -1 -6 -5 58 -85 64 -.05 30 29 | 0 -42 3593 3868
cod 172| -1 0 -12 150 -32 2 .14 45 47 | --- --- --- ---
esx 49| -4 2 27 399 106 -107 -.34 170 68 | 351393 2190466 999999 999999
iac n/a| 1 0 8 -264 61 14 .12 27 27 | 1574640 2127906 999999 999999
mcc n/a| -11 -5 -2 -170 -66 614 .31 138 138 | --- --- --- ---
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 3.1429.0 GPS week: 1429 Day: 0 MJD: 54247
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 801 --- 370 --- 545 | --- 663 --- 433 --- 440
R03 |12705 20 64 71 21 --- 22 | 36 34 65 49 --- 35
R04 | 3240 32 69 85 44 --- 29 | 27 27 78 41 --- 27
R06 | 3784 38 81 80 35 --- 30 | 24 63 56 46 --- 28
R07 |16267 4457 359 232 125 290 161 | 9999 170 47 39 60 59
R08 | 3509 26 20 84 27 --- 20 | 37 30 83 40 --- 31
XR10E | 6779 45 58 --- 44 --- 33 | 51 69 --- 56 --- 42
XR14E | 3633 32 50 --- 18 --- 22 | 33 27 --- 36 --- 26
XR15E | ---- --- 16 --- --- 2463 0 | --- 817 --- --- 495 814
R19 | 2544 21 29 72 15 --- 17 | 14 42 47 42 --- 23
R21 | 8200 32 32 81 54 --- 27 | 40 44 58 71 --- 41
XR22 |36187 143 271 --- 75 --- 110 | 180 162 --- 193 --- 161
R23 | 2061 42 73 340 32 --- 33 | 44 30 195 71 --- 42
R24 | 4082 26 41 399 27 248 21 | 42 51 315 42 54 40
------+------------------------------------+--------------------------------
RMS | 7872 1486 130 202 52 270 |T 48 159 104 89 203 129
WRMS | 7872 59 42 101 52 270 |NE 49 119 104 97 57 84
MEDI | 3784 32 58 84 35 290 |MD 37 44 65 46 60 40
Table 3.1429.1 GPS week: 1429 Day: 1 MJD: 54248
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- 179 195 --- 142 --- 120 | 193 289 --- 192 --- 138
R03 | 4658 24 20 55 18 --- 16 | 32 34 58 34 --- 20
R04 | 2407 22 31 34 23 --- 15 | 33 35 40 42 --- 33
R06 | 6210 42 45 46 32 --- 23 | 32 59 46 32 --- 22
R07 | ---- 54 92 44 36 178 34 | 928 166 49 46 112 35
R08 | 2636 33 35 130 42 --- 35 | 35 37 79 48 --- 35
XR10E | 4318 56 48 --- 41 --- 34 | 39 38 --- 62 --- 32
XR14E | 4980 24 21 --- 24 --- 16 | 39 35 --- 35 --- 21
XR15E | ---- --- 14 --- --- 3001 0 | --- 826 --- --- 9999 824
R19 | 3966 70 27 45 39 --- 27 | 60 32 62 50 --- 20
R21 | 7348 27 50 63 31 --- 24 | 42 63 108 50 --- 45
XR22 |44362 444 163 --- 116 --- 138 | 264 114 --- 185 --- 94
R23 | 3503 58 99 273 69 --- 54 | 65 41 81 91 --- 44
R24 | 2241 30 35 383 25 235 21 | 30 40 188 44 63 34
------+------------------------------------+--------------------------------
RMS | 4472 43 55 167 38 208 |T 137 129 79 70 87 99
WRMS | 4472 34 39 59 38 208 |NE 155 82 79 74 87 47
MEDI | 4318 42 35 55 36 235 |MD 39 40 62 48 63 34
Table 3.1429.2 GPS week: 1429 Day: 2 MJD: 54249
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2918 166 128 67 46 --- 60 | 121 132 47 83 --- 88
R03 | 9477 28 36 47 26 --- 19 | 37 28 54 36 --- 24
R04 | 3349 15 29 49 12 --- 14 | 29 23 76 32 --- 26
R06 | 8448 51 44 54 21 --- 23 | 25 32 53 43 --- 24
R07 | 5349 25 58 54 34 53 24 | 510 115 81 34 127 48
R08 | 3058 29 33 81 24 --- 23 | 36 44 56 40 --- 28
XR10E | 2499 42 44 --- 22 --- 24 | 42 36 --- 39 --- 26
XR14E | 4512 57 34 --- 43 --- 32 | 29 29 --- 46 --- 30
XR15E | ---- --- 18 --- --- 1378 0 | --- 759 --- --- 9999 752
R19 | 5412 31 36 71 19 --- 21 | 59 54 43 43 --- 35
R21 | 3041 19 46 59 21 --- 20 | 72 78 64 65 --- 54
XR22 |55314 255 334 --- 130 --- 182 | 150 204 --- 374 --- 260
R23 | 1753 34 64 358 40 --- 32 | 44 36 189 72 --- 48
R24 | 2204 37 36 365 21 119 21 | 37 40 239 64 139 47
------+------------------------------------+--------------------------------
RMS | 5151 60 58 171 28 92 |T 91 115 90 74 133 106
WRMS | 5151 38 37 69 28 92 |NE 101 71 90 80 133 62
MEDI | 3349 34 36 59 24 119 |MD 42 40 56 43 127 35
Table 3.1429.3 GPS week: 1429 Day: 3 MJD: 54250
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7285 38 35 89 33 --- 25 | 60 154 47 58 --- 73
R03 |19050 59 27 45 59 --- 28 | 60 40 65 40 --- 33
R04 | 3662 23 19 75 21 --- 18 | 21 23 72 33 --- 25
R06 | 7387 34 27 24 24 --- 16 | 60 50 60 51 --- 47
R07 | 3338 23 29 68 33 65 20 | 466 87 86 41 82 44
R08 | 2894 25 16 50 23 --- 14 | 50 39 42 39 --- 32
XR10E | 2446 44 36 --- 25 --- 25 | 64 43 --- 76 --- 51
XR14E | 5147 29 41 --- 63 --- 33 | 24 35 --- 44 --- 24
XR15E | ---- --- 9 --- --- 1204 0 | --- 662 --- --- 419 658
R19 | 3245 43 47 112 27 --- 30 | 25 56 99 48 --- 30
R21 | 3765 56 21 124 40 --- 31 | 56 42 92 52 --- 36
XR22 |69262 66 42 --- 87 --- 47 | 197 136 --- 134 --- 124
R23 | 2186 38 59 311 69 --- 41 | 55 54 134 71 --- 35
R24 | 2322 31 37 319 35 123 24 | 37 58 215 33 57 38
------+------------------------------------+--------------------------------
RMS | 7337 39 34 158 39 98 |T 90 105 91 55 186 89
WRMS | 7337 38 31 71 39 98 |NE 98 67 91 54 69 47
MEDI | 3662 38 29 75 33 123 |MD 56 50 72 48 82 36
Table 3.1429.4 GPS week: 1429 Day: 4 MJD: 54251
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5646 32 20 88 29 --- 23 | 64 100 85 70 --- 74
R03 | 9151 35 26 23 40 --- 19 | 31 44 44 54 --- 36
R04 | 3746 23 25 70 20 --- 18 | 29 26 49 36 --- 23
R06 | 8520 32 54 62 35 --- 25 | 28 82 27 38 --- 29
R07 | 3477 28 48 44 36 61 22 | 236 70 37 62 57 41
R08 | 3582 32 32 43 21 --- 17 | 33 52 62 55 --- 37
XR10E | 8307 52 54 --- 33 --- 33 | 46 51 --- 63 --- 33
XR14E | 6994 32 25 --- 34 --- 22 | 28 23 --- 35 --- 18
XR15E | ---- --- 17 --- --- 1317 0 | --- 943 --- --- 253 944
R19 | 2803 25 43 66 36 --- 23 | 31 34 55 49 --- 23
R21 | 5949 32 36 137 38 --- 33 | 69 109 62 62 --- 65
XR22 |80691 79 54 --- 106 --- 59 | 170 312 --- 147 --- 120
R23 | 3012 30 30 273 28 --- 21 | 56 47 134 67 --- 52
R24 | 1799 29 45 369 42 216 27 | 30 37 207 45 116 25
------+------------------------------------+--------------------------------
RMS | 5317 30 37 159 33 159 |T 65 137 76 60 142 108
WRMS | 5317 30 36 59 33 159 |NE 70 83 76 62 86 47
MEDI | 5646 32 32 66 35 216 |MD 33 51 55 55 116 36
Table 3.1429.5 GPS week: 1429 Day: 5 MJD: 54252
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9224 33 48 113 33 --- 31 | 28 115 88 53 --- 44
R03 | 5245 23 36 65 35 --- 21 | 26 39 63 38 --- 19
R04 | 2993 28 34 36 38 --- 19 | 28 36 60 34 --- 29
R06 | 8146 22 78 39 34 --- 25 | 18 80 38 43 --- 20
R07 | 2122 21 32 37 28 55 16 | 466 64 75 35 44 30
R08 | 2608 13 39 53 39 --- 20 | 28 32 47 44 --- 26
XR10E |16474 85 316 --- 126 --- 103 | 58 201 --- 192 --- 96
XR14E | 7200 18 34 --- 29 --- 18 | 27 35 --- 25 --- 19
XR15E | ---- --- 17 --- --- 2984 0 | --- 9999 --- --- 261 9999
R19 | 4157 15 22 57 19 --- 15 | 32 37 49 44 --- 31
R21 | 4136 29 26 251 49 --- 25 | 53 53 211 65 --- 48
XR22 | ---- 118 773 --- 174 --- 143 | 236 555 --- 199 --- 84
R23 | 4286 19 48 330 44 --- 25 | 29 33 149 36 --- 17
R24 | 1585 18 46 372 45 328 25 | 19 20 176 32 225 13
------+------------------------------------+--------------------------------
RMS | 5044 23 44 184 37 235 |T 80 100 95 64 176 36
WRMS | 5044 22 41 59 37 235 |NE 87 96 95 56 134 32
MEDI | 4157 22 36 57 38 328 |MD 28 39 63 43 225 29
Table 3.1429.6 GPS week: 1429 Day: 6 MJD: 54253
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8169 42 73 60 41 --- 29 | 70 103 78 87 --- 74
R03 | 5668 26 48 88 20 --- 23 | 34 27 63 55 --- 37
R04 | 2571 21 46 64 21 --- 19 | 27 34 41 42 --- 25
R06 | 7630 34 45 34 27 --- 19 | 37 62 46 41 --- 31
R07 | 1522 20 29 50 15 51 14 | 423 46 51 39 78 30
R08 | 2968 14 32 62 15 --- 16 | 31 39 78 56 --- 39
XR10E |16478 134 240 --- 164 --- 123 | 73 232 --- 201 --- 89
XR14E | 6627 44 29 --- 45 --- 30 | 20 16 --- 28 --- 18
XR15E | ---- --- 11 --- --- 2580 0 | --- 672 --- --- 470 675
R19 | 4635 40 29 66 15 --- 20 | 45 50 77 64 --- 49
R21 | 3899 26 46 202 20 --- 20 | 27 50 118 45 --- 31
XR22 | ---- 1011 317 --- 142 --- 213 | 504 221 --- 339 --- 265
R23 | 4695 37 23 352 30 --- 22 | 26 49 215 61 --- 38
R24 | 2028 31 60 314 44 189 31 | 47 61 275 36 230 35
------+------------------------------------+--------------------------------
RMS | 4875 30 45 170 27 138 |T 104 118 104 84 259 102
WRMS | 4875 29 47 68 27 138 |NE 115 67 104 78 154 59
MEDI | 4635 34 45 64 27 189 |MD 37 50 77 55 230 37
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