[IGSREPORT-14912] Wk 1417 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Mar 22 23:14:26 PDT 2007
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IGS Electronic Report 22 Mar 23:14:37 PDT 2007 Message Number 14912
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1417 (Mar 04, 2007 - Mar 10, 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 2.1417.
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:
igl1417[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1417 in the SP3 format.
igl14177.sum Combination Report for GPS Week 1417.
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 | 752.9 ns
1 | 757.2 ns
2 | 773.1 ns
3 | 759.0 ns
4 | 749.6 ns
5 | 792.7 ns
6 | 746.3 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
----+--------+---------------
2 | ESX | R23
4 | ESX | R23
6 | ESX | 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 1.1417, 1a.1417).
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 2.1417.0-6)
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 3.1417.0-6).
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 1417 summary. (Mar 04, 2007 - Mar 10, 2007)
Table 1.1417.a GPS week : 1417 MJD: 54163.0-54169.0
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| 0 0 9 123 -47 -4 -.13 53 36 | 0 611 3951 4254
| 2 3 4 45 38 134 .06 | 0 1092
cod 166| 0 0 -1 113 -40 3 -.10 42 34 | --- --- --- ---
| 2 2 6 40 72 29 .08 | --- ---
esx 44| 2 0 21 159 39 -16 -.40 178 68 | -180199 43793 85834 494863
| 2 4 16 135 154 114 .18 | 563947 56858
iac n/a| 0 1 -13 -247 102 -9 .28 39 39 | 857855 30654 87699 466060
| 3 3 8 43 45 85 .07 | 96299 33008
mcc n/a| -5 11 9 -305 57 210 .30 179 179 | --- --- --- ---
| 8 17 20 220 67 727 .50 | --- ---
Table 1.1417.b GPS week : 1417 MJD: 54163.0-54169.0
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 | 21 19 23 27 19 29 30 |
R02 | 12 17 22 17 16 14 19 |
R03 | 82 0 ---- ---- 0 0 22 |
R04 | 13 13 17 17 14 18 28 |
R06 | 25 26 41 33 25 19 53 |
R07 | 20 23 31 25 19 15 24 |
R08 | 19 25 21 21 33 20 25 |
R10 | 15 38 30 19 23 26 27 |
R14 | 28 33 32 19 22 17 21 |
R15 | 0 0 0 0 0 0 0 |
R18 | 37 31 65 29 29 56 43 |
R19 | 20 25 19 12 31 20 20 |
R21 | 62 46 30 33 48 50 32 |
R22 | 17 21 18 26 29 45 32 |
R23 | 69 77 29 72 34 84 19 |
R24 | 68 68 35 78 32 62 41 |
Table 1.1417.c GPS week : 1417 MJD: 54163.0-54169.0
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 1417 0 | -288 -365 -1627 -567 -5219 -389300 80.8 7284 7284 | 752920 0
brd 1417 1 | 54 147 -794 -1707 487 -374000 105.4 5849 5849 | 757218 0
brd 1417 2 | -355 -113 -206 -900 -1743 -362200 83.8 6120 6120 | 773084 0
brd 1417 3 | -9 -190 -1203 2452 -1053 -361400 104.9 5005 5005 | 759035 0
brd 1417 4 | -192 147 -65 3045 -5197 -365300 80.4 5803 5803 | 749623 0
brd 1417 5 | -159 191 -586 6440 -160 -369500 84.9 7615 7615 | 792745 0
brd 1417 6 | -74 -269 373 3714 -432 -377000 88.3 7015 7015 | 746329 0
-------------+------------------------------------------------------------+----------------
brd 1417 mean| -146 -64 -587 1782 -1902 -371242 89.8 6384 6384 | 761564 0
brd 1417 sdev| 147 225 688 2954 2363 9864 10.8 941 941 | 16225 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 2.1417.0 GPS week: 1417 Day: 0 MJD: 54163
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 -2 3 63 -39 96 -.08 30 24 | 0 241 3381 3653
cod 166| 0 -1 -5 74 49 -15 -.03 44 37 | --- --- --- ---
esx 44| 0 -7 41 318 -127 34 -.26 182 61 | 123151 -6772 28956 281531
iac n/a| 4 0 -20 -259 20 -143 .21 37 37 | 819236 -7091 36007 254142
mcc n/a| 0 -3 3 -392 87 -9 -.50 197 197 | --- --- --- ---
Table 2.1417.1 GPS week: 1417 Day: 1 MJD: 54164
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 8 166 -49 95 -.08 39 32 | 0 -378 4699 5068
cod 166| 1 -3 -10 119 7 -3 -.02 42 35 | --- --- --- ---
esx 44| 2 7 42 3 50 -120 -.44 177 72 | 109002 14055 36728 290171
iac n/a| -1 0 -21 -310 80 -3 .39 50 50 | 802727 21812 46208 244812
mcc n/a| -16 13 9 -74 63 1498 .59 144 144 | --- --- --- ---
Table 2.1417.2 GPS week: 1417 Day: 2 MJD: 54165
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 14 92 -1 -126 -.09 74 34 | 0 -352 3407 3615
cod 166| 2 -3 -2 100 0 8 -.12 35 34 | --- --- --- ---
esx 44| 0 0 21 172 -60 -41 -.55 173 70 | 106637 57938 74400 356142
iac n/a| -5 4 -10 -175 106 92 .18 37 37 | 820024 49329 71126 300349
mcc n/a| -6 4 20 -238 -82 448 .26 121 121 | --- --- --- ---
Table 2.1417.3 GPS week: 1417 Day: 3 MJD: 54166
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 5 14 95 -69 140 -.18 43 34 | 0 480 3574 3878
cod 166| -1 -2 5 69 -69 -14 -.00 43 31 | --- --- --- ---
esx 44| 5 0 19 364 287 -179 -.41 210 70 | 107213 84059 107251 519185
iac n/a| 1 6 -23 -242 95 -33 .31 40 40 | 841979 64680 103492 466582
mcc n/a| -10 41 44 -741 44 -659 -.28 167 167 | --- --- --- ---
Table 2.1417.4 GPS week: 1417 Day: 4 MJD: 54167
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| -4 2 14 102 -69 -132 -.24 63 42 | 0 1276 3267 3523
cod 166| -1 1 8 180 -102 61 -.15 39 37 | --- --- --- ---
esx 44| 4 -1 -1 107 188 169 -.14 160 70 | 292600 147152 198363 999999
iac n/a| 2 -2 -12 -286 150 -52 .27 34 34 | 940049 76199 188004 980249
mcc n/a| 0 9 19 -345 100 -208 .77 172 172 | --- --- --- ---
Table 2.1417.5 GPS week: 1417 Day: 5 MJD: 54168
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 7 166 1 -177 -.08 62 44 | 0 2742 5168 5518
cod 166| -2 2 -5 149 -157 -26 -.22 52 30 | --- --- --- ---
esx 44| 0 2 7 47 -106 40 -.67 154 56 | -999999 20087 143614 999999
iac n/a| 2 -1 -3 -222 158 103 .33 39 39 | 1032863 12550 159386 999999
mcc n/a| -10 -8 -21 -153 125 -287 .70 234 234 | --- --- --- ---
Table 2.1417.6 GPS week: 1417 Day: 6 MJD: 54169
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 -2 6 179 -104 70 -.15 59 44 | 0 273 4167 4528
cod 166| 1 3 -1 100 -10 12 -.15 40 36 | --- --- --- ---
esx 44| 2 0 21 102 47 -16 -.32 191 75 | -999999 -9963 11526 17016
iac n/a| 0 4 -3 -236 105 -29 .26 37 37 | 748110 -2901 9675 16290
mcc n/a| 8 27 -6 -192 65 689 .56 214 214 | --- --- --- ---
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 3.1417.0 GPS week: 1417 Day: 0 MJD: 54163
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |11083 23 35 71 36 --- 20 | 36 41 103 50 --- 37
R02 |10210 13 25 44 13 --- 11 | 36 38 72 29 --- 30
XR03 | ---- --- 53 --- 99 --- 81 | --- 238 --- 51 --- 261
R04 | 5737 19 24 38 16 --- 12 | 49 47 63 42 --- 44
R06 | 6900 34 59 63 23 --- 24 | 41 75 86 52 --- 44
R07 | 6172 14 28 83 35 60 19 | 47 57 70 34 36 40
R08 | 6946 30 36 50 25 --- 18 | 60 79 99 79 --- 69
XR10 | 3298 20 20 --- 22 --- 14 | 79 79 --- 86 --- 77
XR14 | 8486 37 53 --- 27 --- 28 | 36 56 --- 46 --- 39
XR15 | ---- --- 6 --- --- --- 0 | --- 308 --- --- --- 305
R18 | 8504 66 82 42 47 --- 37 | 146 115 111 124 --- 123
R19 | 6003 21 31 76 33 --- 19 | 91 108 109 101 --- 96
XR21 | 9028 --- 69 210 35 --- 62 | --- 108 138 90 --- 87
R22 | 7814 19 34 53 27 130 17 | 49 50 64 68 111 48
R23 | 2110 28 45 413 62 --- 69 | 79 90 136 113 --- 80
R24 | 3968 30 53 402 53 310 67 | 232 276 350 269 298 260
------+------------------------------------+--------------------------------
RMS | 7283 30 44 182 37 197 |T 75 110 116 82 148 102
WRMS | 7283 24 37 61 37 197 |NE 75 110 116 82 148 102
MEDI | 6900 23 35 63 33 130 |MD 49 79 99 68 111 69
Table 3.1417.1 GPS week: 1417 Day: 1 MJD: 54164
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5102 25 41 51 26 --- 19 | 34 49 72 37 --- 35
R02 | 7564 19 28 62 23 --- 16 | 34 46 37 52 --- 33
XR03 | ---- --- 9 --- --- --- 0 | --- 464 --- --- --- 465
R04 | 4609 23 12 33 25 --- 12 | 46 37 46 47 --- 37
R06 | 7642 33 43 90 36 --- 25 | 44 56 105 44 --- 41
R07 | 4170 25 34 80 43 97 23 | 43 45 57 31 69 27
R08 | 4378 37 30 61 56 --- 25 | 84 100 88 122 --- 96
XR10 | 5482 36 60 --- 63 --- 37 | 58 77 --- 42 --- 54
XR14 | 3883 36 51 --- 50 --- 32 | 29 37 --- 45 --- 18
XR15 | ---- --- 9 --- --- --- 0 | --- 9999 --- --- --- 9999
R18 | 4870 60 40 67 54 --- 31 | 165 87 90 80 --- 95
R19 | 7007 35 39 60 48 --- 24 | 82 101 114 98 --- 90
R21 | 8027 74 84 121 64 --- 46 | 77 76 152 122 --- 95
R22 | 6966 25 30 84 29 92 20 | 35 54 69 39 134 36
R23 | 2684 43 42 426 80 --- 77 | 34 41 121 63 --- 29
R24 | 4256 33 44 375 73 210 68 | 142 180 202 172 312 164
------+------------------------------------+--------------------------------
RMS | 5849 39 42 177 50 143 |T 64 96 96 71 171 87
WRMS | 5849 32 35 72 50 143 |NE 64 96 96 71 171 87
MEDI | 4870 33 39 67 48 97 |MD 44 56 88 47 134 41
Table 3.1417.2 GPS week: 1417 Day: 2 MJD: 54165
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3211 24 21 95 28 --- 22 | 37 40 70 37 --- 36
R02 | 5237 22 27 79 31 --- 21 | 34 53 63 24 --- 30
R04 | 7295 24 30 42 26 --- 17 | 37 41 61 41 --- 35
R06 |13149 24 37 177 48 --- 40 | 44 57 114 48 --- 43
R07 | 3361 71 42 82 38 81 31 | 57 53 46 45 68 37
R08 | 3463 35 21 71 33 --- 21 | 58 95 105 118 --- 89
XR10 | 8336 25 40 --- 51 --- 29 | 58 70 --- 63 --- 61
XR14 | 2416 41 43 --- 49 --- 31 | 52 40 --- 70 --- 43
XR15 | ---- --- 7 --- --- --- 0 | --- 9999 --- --- --- 9999
R18 | 5344 211 70 96 54 --- 64 | 208 85 135 86 --- 76
R19 | 7397 42 22 44 30 --- 18 | 73 65 85 56 --- 64
R21 | 3091 68 28 103 28 --- 30 | 91 67 89 63 --- 56
R22 | 4944 24 22 65 24 151 18 | 37 55 76 49 125 43
R23 | 2739 32 37 494 49 --- 29 | 62 63 170 74 --- 71
XR24 | 7032 72 28 --- 51 362 35 | 203 206 --- 219 255 207
------+------------------------------------+--------------------------------
RMS | 6119 74 35 173 37 121 |T 75 70 92 70 149 63
WRMS | 6119 34 34 70 37 121 |NE 75 70 92 70 149 63
MEDI | 4944 32 28 82 33 151 |MD 57 57 85 56 125 43
Table 3.1417.3 GPS week: 1417 Day: 3 MJD: 54166
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3331 17 37 154 24 --- 27 | 45 58 85 31 --- 35
R02 | 2971 17 25 63 28 --- 16 | 42 40 52 45 --- 38
R04 | 5995 35 27 43 19 --- 16 | 61 45 61 33 --- 35
R06 | 6305 44 69 103 36 --- 32 | 48 62 83 53 --- 32
R07 | 3847 25 48 68 44 97 25 | 51 63 66 36 54 39
R08 | 4234 44 19 48 37 --- 20 | 71 70 95 81 --- 71
XR10 | 6098 33 23 --- 23 --- 19 | 50 54 --- 40 --- 38
XR14 | 2491 24 21 --- 32 --- 19 | 28 54 --- 53 --- 38
XR15 | ---- --- 6 --- --- --- 0 | --- 566 --- --- --- 565
XR18 | 6618 --- 38 55 39 --- 28 | --- 104 108 78 --- 91
R19 | 7002 21 15 29 24 --- 12 | 57 45 66 39 --- 43
R21 | 5013 81 40 75 36 --- 32 | 79 58 95 62 --- 52
R22 | 4452 29 25 147 21 104 25 | 29 49 150 46 84 40
R23 | 2717 32 38 453 66 --- 71 | 62 64 122 74 --- 46
R24 | 6769 70 78 454 65 252 77 | 85 159 345 94 224 102
------+------------------------------------+--------------------------------
RMS | 5005 43 43 210 40 167 |T 54 99 110 54 120 84
WRMS | 5005 34 31 70 40 167 |NE 54 99 110 54 120 84
MEDI | 4452 32 27 68 32 104 |MD 51 58 85 46 84 40
Table 3.1417.4 GPS week: 1417 Day: 4 MJD: 54167
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5596 29 20 61 27 --- 18 | 37 49 62 52 --- 36
R02 | 2876 22 28 30 27 --- 15 | 28 41 65 36 --- 31
XR03 | ---- --- 14 --- --- --- 0 | --- 142 --- --- --- 136
R04 | 5902 18 20 43 21 --- 14 | 36 43 48 30 --- 30
R06 | 8577 63 33 48 39 --- 25 | 51 55 56 68 --- 39
R07 | 6562 25 21 66 25 58 18 | 52 43 61 36 34 36
R08 | 6788 74 33 122 22 --- 33 | 65 60 126 63 --- 61
XR10 | 1443 48 16 --- 33 --- 22 | 41 49 --- 61 --- 48
XR14 | 2340 38 29 --- 30 --- 22 | 30 29 --- 48 --- 24
XR15 | ---- --- 13 --- --- --- 0 | --- 258 --- --- --- 257
XR18 | 8978 --- 40 62 30 --- 28 | --- 128 115 102 --- 109
R19 | 5834 55 61 33 52 --- 31 | 127 166 143 101 --- 126
R21 | 6684 145 47 132 31 --- 47 | 118 82 94 105 --- 91
R22 | 3661 48 43 89 38 237 29 | 46 73 114 39 57 46
R23 | 2734 34 58 449 42 --- 33 | 61 99 76 68 --- 72
XR24 | 9218 75 37 --- 33 370 32 | 221 206 --- 203 171 208
------+------------------------------------+--------------------------------
RMS | 5803 63 39 160 34 172 |T 70 95 87 72 87 84
WRMS | 5803 42 37 70 34 172 |NE 70 95 87 72 87 84
MEDI | 5834 48 29 62 30 237 |MD 51 60 76 61 57 48
Table 3.1417.5 GPS week: 1417 Day: 5 MJD: 54168
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8289 43 75 23 34 --- 29 | 39 116 76 32 --- 49
R02 | 4175 29 25 28 18 --- 14 | 35 36 40 50 --- 35
XR03 | ---- --- 14 --- --- --- 0 | --- 65 --- --- --- 62
R04 | 6631 31 19 53 28 --- 17 | 54 43 44 35 --- 37
R06 | 6553 20 41 51 21 --- 18 | 37 50 93 47 --- 34
R07 | 8341 25 29 41 19 65 15 | 51 34 41 34 59 32
R08 | 9236 33 26 54 33 --- 20 | 36 33 60 42 --- 21
XR10 | 6761 50 37 --- 24 --- 26 | 39 49 --- 23 --- 23
XR14 | 2093 16 28 --- 24 --- 17 | 27 28 --- 28 --- 21
XR15 | ---- --- 14 --- --- --- 0 | --- 294 --- --- --- 295
R18 |14014 143 60 146 59 --- 56 | 129 161 216 149 --- 139
R19 | 3752 38 35 51 26 --- 20 | 56 108 108 69 --- 76
R21 | 8168 74 29 231 34 --- 50 | 41 44 115 53 --- 44
R22 | 5082 73 107 69 52 325 44 | 58 118 48 49 108 43
R23 | 2634 59 56 412 69 --- 84 | 61 71 162 97 --- 65
XR24 | 8805 120 96 --- 48 292 62 | 153 225 --- 128 267 153
------+------------------------------------+--------------------------------
RMS | 7615 62 52 154 39 234 |T 58 92 91 59 144 70
WRMS | 7615 44 30 56 39 234 |NE 58 92 91 59 144 70
MEDI | 6631 38 29 53 28 292 |MD 41 50 76 47 108 43
Table 3.1417.6 GPS week: 1417 Day: 6 MJD: 54169
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8675 54 43 108 25 --- 29 | 31 58 55 38 --- 30
R02 | 6063 41 34 41 20 --- 19 | 53 57 38 31 --- 37
XR03 | ---- --- 22 --- 21 --- 21 | --- 72 --- 15 --- 72
R04 | 5715 63 36 50 48 --- 28 | 62 40 63 38 --- 33
R06 | 5485 24 30 255 61 --- 52 | 50 64 186 46 --- 48
R07 | 6776 26 40 90 23 95 23 | 52 36 93 42 42 36
R08 |10215 52 37 62 30 --- 24 | 47 47 42 39 --- 29
XR10 | 8033 29 34 --- 45 --- 26 | 55 62 --- 66 --- 59
XR14 | 5206 26 35 --- 26 --- 21 | 43 59 --- 19 --- 33
XR15 | ---- --- 7 --- --- --- 0 | --- 222 --- --- --- 224
R18 |10572 113 52 97 45 --- 42 | 164 161 184 159 --- 154
R19 | 2467 46 29 53 19 --- 20 | 82 98 102 72 --- 82
R21 | 5969 17 22 151 37 --- 31 | 47 79 164 88 --- 78
R22 | 4235 69 47 76 42 127 31 | 56 52 62 45 123 30
XR23 | 3603 21 30 --- 27 --- 19 | 80 87 --- 98 --- 86
R24 | 6690 78 58 516 37 336 40 | 255 301 361 271 294 275
------+------------------------------------+--------------------------------
RMS | 7014 59 40 191 37 214 |T 76 93 122 71 153 81
WRMS | 7014 44 36 75 37 214 |NE 76 93 122 71 153 81
MEDI | 5969 41 34 90 30 127 |MD 53 62 93 45 123 48
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