[IGSREPORT-15221] Wk 1430 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Tue Jun 26 07:16:51 PDT 2007
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IGS Electronic Report 26 Jun 07:16:58 PDT 2007 Message Number 15221
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1430 (Jun 03, 2007 - Jun 09, 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 2.1430.
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:
igl1430[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1430 in the SP3 format.
igl14307.sum Combination Report for GPS Week 1430.
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 | 1061.6 ns
1 | 1086.0 ns
2 | 1086.2 ns
3 | 1104.2 ns
4 | 1071.0 ns
5 | 1085.3 ns
6 | 1133.2 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
----+--------+---------------
0 | COD | R01 R22
0 | ESX | R23 R24
1 | BKG | R01
1 | ESX | R23
2 | BKG | R01
2 | ESX | R23
3 | COD | R01
3 | ESX | R23
4 | ESX | R23 R24
5 | ESX | R23 R24
6 | ESX | 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 1.1430, 1a.1430).
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 2.1430.0-6)
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 3.1430.0-6).
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 1430 summary. (Jun 03, 2007 - Jun 09, 2007)
Table 1.1430.a GPS week : 1430 MJD: 54254.0-54260.0
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 59| 0 0 -4 82 -10 -55 -.07 120 38 | -2317 0 3790 4016
| 4 4 7 99 40 414 .04 | 6130 240
cod 171| 4 0 0 73 -38 148 .03 83 44 | --- --- --- ---
| 5 4 6 112 85 179 .12 | --- ---
esx 44| -1 2 15 122 -77 -242 -.29 201 71 | -99946 -11326 14605 25958
| 4 5 11 168 164 230 .30 | 421002 7955
iac n/a| 0 -1 -3 -212 78 12 .17 49 49 | 1092324 -4414 13276 24462
| 3 5 5 102 54 247 .07 | 24356 6793
mcc n/a| -4 8 10 95 -42 808 .12 184 184 | --- --- --- ---
| 4 16 19 158 200 527 .47 | --- ---
Table 1.1430.b GPS week : 1430 MJD: 54254.0-54260.0
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 | 69 112 214 117 46 23 27 |
R03 | 34 33 20 23 29 22 21 |
R04 | 32 27 21 21 24 29 31 |
R06 | 20 19 26 25 35 25 19 |
R07 | 18 25 25 18 34 19 20 |
R08 | 18 21 21 25 22 33 25 |
R10E | 81 37 41 74 35 21 30 |
R14E | 22 34 22 29 34 27 26 |
R15E | 0 0 0 0 0 0 0 |
R19 | 19 32 27 26 28 18 39 |
R21 | 19 25 37 24 29 24 39 |
R22 | 521 0 0 0 0 133 153 |
R23 | 25 39 46 34 30 26 28 |
R24 | 25 28 22 31 35 24 24 |
Table 1.1430.c GPS week : 1430 MJD: 54254.0-54260.0
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 1430 0 | 78 -214 -1254 -693 -2108 -340400 73.8 4081 4081 | 1061560 0
brd 1430 1 | 76 182 -865 4272 3506 -332900 91.1 5150 5150 | 1085951 0
brd 1430 2 | 280 643 -585 -7524 6971 -322700 84.7 11950 11950 | 1086246 0
brd 1430 3 | 299 630 -792 -7553 6865 -325800 69.2 13400 13400 | 1104163 0
brd 1430 4 | 455 -378 -213 9974 6427 -331400 77.5 5554 5554 | 1071021 0
brd 1430 5 | 157 58 -178 -769 -991 -326300 96.7 8684 8684 | 1085283 0
brd 1430 6 | -27 405 -242 -2245 -2264 -314900 98.7 8285 8285 | 1133248 0
-------------+------------------------------------------------------------+----------------
brd 1430 mean| 188 189 -590 -648 2629 -327771 84.5 8157 8157 | 1089638 0
brd 1430 sdev| 165 398 406 6252 4310 8128 11.5 3526 3526 | 23423 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 2.1430.0 GPS week: 1430 Day: 0 MJD: 54254
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 59| -2 -1 0 140 20 -161 -.02 27 27 | 0 150 3746 3980
cod 171| 7 -6 2 -47 -74 392 -.18 55 62 | --- --- --- ---
esx 44| 3 6 23 225 -331 -152 -.02 211 67 | -96799 -8854 18152 27736
iac n/a| -5 2 -6 -252 133 96 .18 35 35 | 1061884 -2694 16509 26330
mcc n/a| -2 3 -17 68 -46 491 -.23 144 144 | --- --- --- ---
Table 2.1430.1 GPS week: 1430 Day: 1 MJD: 54255
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 59| 1 0 0 -67 -35 98 -.04 224 34 | 0 -77 3173 3359
cod 171| 0 4 -10 98 -97 -99 .10 77 46 | --- --- --- ---
esx 44| 2 0 9 347 119 -257 -.31 171 65 | 348267 -3944 14551 26754
iac n/a| 1 -11 2 -315 98 118 .04 56 56 | 1088962 -2097 12424 24154
mcc n/a| -3 42 0 -162 -46 817 .90 114 114 | --- --- --- ---
Table 2.1430.2 GPS week: 1430 Day: 2 MJD: 54256
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 59| 3 9 -5 168 7 -256 -.06 416 53 | 0 55 3446 3689
cod 171| -2 -5 -2 45 114 83 .06 87 41 | --- --- --- ---
esx 44| -2 4 20 -91 -156 170 .02 219 60 | -999999 246 11999 32894
iac n/a| 5 1 -4 -224 147 172 .13 89 89 | 1084540 4578 10933 28689
mcc n/a| -4 0 24 238 -38 1602 .24 97 97 | --- --- --- ---
Table 2.1430.3 GPS week: 1430 Day: 3 MJD: 54257
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 59| 3 2 -18 200 18 -683 -.05 53 35 | 0 294 3554 3971
cod 171| 4 -2 -4 290 4 340 .16 229 47 | --- --- --- ---
esx 44| 0 2 34 -46 -99 -166 -.76 193 71 | 44239 -9722 15406 27304
iac n/a| 2 0 0 -253 86 326 .16 43 43 | 1107481 -5224 13842 26172
mcc n/a| -3 1 15 302 -33 218 -.20 83 83 | --- --- --- ---
Table 2.1430.4 GPS week: 1430 Day: 4 MJD: 54258
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 59| -7 -3 2 67 34 558 -.08 49 50 | -16220 175 4895 5138
cod 171| 13 -2 1 -19 -134 2 .08 57 43 | --- --- --- ---
esx 44| 3 9 8 220 12 -372 -.03 208 70 | -3706 -17908 12304 22408
iac n/a| -2 1 -12 -267 38 -280 .24 47 47 | 1079805 -6923 11655 21628
mcc n/a| -15 -1 21 162 269 446 -.37 210 210 | --- --- --- ---
Table 2.1430.5 GPS week: 1430 Day: 5 MJD: 54259
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 59| 0 0 -11 92 -54 -267 -.15 43 37 | 0 -398 4055 4174
cod 171| 6 0 9 116 -89 231 -.08 36 35 | --- --- --- ---
esx 44| -8 0 12 215 -187 -352 -.58 198 85 | -14800 -18140 14271 23128
iac n/a| -1 -2 -3 -177 50 14 .25 30 30 | 1085189 -1097 13511 23189
mcc n/a| -2 14 35 83 -416 620 -.10 261 261 | --- --- --- ---
Table 2.1430.6 GPS week: 1430 Day: 6 MJD: 54260
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 59| 4 -3 -1 -26 -66 320 -.12 32 29 | 0 -202 3664 3801
cod 171| 0 4 5 33 9 89 .10 41 37 | --- --- --- ---
esx 44| -5 -7 0 -10 101 -567 -.32 210 81 | 23173 -20965 15554 21483
iac n/a| 0 -5 0 0 -4 -361 .23 42 42 | 1138407 -17445 14064 21075
mcc n/a| -3 0 -6 -27 12 1462 .57 379 379 | --- --- --- ---
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 3.1430.0 GPS week: 1430 Day: 0 MJD: 54254
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |21568 59 573 --- 79 --- 68 | 344 547 --- 100 --- 77
R03 | 4869 38 70 106 45 --- 34 | 32 42 60 72 --- 41
R04 | 3270 32 91 82 39 --- 31 | 36 66 52 44 --- 31
R06 | 6933 23 52 46 27 --- 19 | 25 41 43 41 --- 23
R07 | 1896 19 39 58 22 104 18 | 33 53 44 40 33 30
R08 | 4488 26 40 39 28 --- 18 | 42 58 96 73 --- 59
XR10E |14458 103 70 --- 140 --- 80 | 60 69 --- 101 --- 55
XR14E | 5750 26 41 --- 31 --- 22 | 33 31 --- 33 --- 24
XR15E | ---- --- 23 --- --- 1572 0 | --- 878 --- --- 20 873
R19 | 3804 22 37 42 38 --- 19 | 45 47 98 62 --- 49
R21 | 3893 24 39 27 39 --- 18 | 22 23 79 57 --- 26
XR22 | ---- 274 1550 --- 726 --- 520 | 2 215 --- 148 --- 9999
R23 | 3531 25 61 426 31 --- 25 | 98 49 292 77 --- 77
R24 | 1247 27 46 439 37 175 24 | 49 61 248 57 62 49
------+------------------------------------+--------------------------------
RMS | 4080 27 55 211 35 144 |T 63 155 112 69 38 108
WRMS | 4080 27 62 67 35 144 |NE 66 109 112 70 47 46
MEDI | 3893 26 46 58 38 175 |MD 36 53 79 62 33 49
Table 3.1430.1 GPS week: 1430 Day: 1 MJD: 54255
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | ---- 668 180 186 85 --- 111 | 366 153 87 102 --- 57
R03 | 7768 43 53 71 72 --- 33 | 46 52 72 60 --- 31
R04 | 2384 23 56 56 59 --- 27 | 34 57 49 57 --- 27
R06 | 9405 20 37 40 39 --- 19 | 27 43 50 38 --- 27
R07 | 2050 19 54 39 57 114 24 | 38 56 48 59 31 29
R08 | 4315 29 23 52 43 --- 21 | 42 68 98 95 --- 62
XR10E | 6537 43 62 --- 53 --- 36 | 57 41 --- 75 --- 41
XR14E | 6413 37 67 --- 38 --- 33 | 58 64 --- 55 --- 44
XR15E | ---- --- 12 --- --- 1789 0 | --- 931 --- --- 23 927
R19 | 3288 31 36 109 41 --- 32 | 44 50 110 42 --- 45
R21 | 4612 35 57 44 32 --- 24 | 49 28 53 45 --- 28
XR22 | ---- --- 11 --- --- --- 0 | --- 104 --- --- --- 397
R23 | 1652 40 71 448 56 --- 38 | 58 26 191 74 --- 43
XR24 | 1766 20 54 --- 47 105 28 | 27 42 --- 49 45 25
------+------------------------------------+--------------------------------
RMS | 5149 224 77 171 56 114 |T 70 122 84 62 33 127
WRMS | 5149 34 46 65 56 114 |NE 73 61 84 62 38 70
MEDI | 4315 31 54 56 47 114 |MD 44 52 72 57 31 41
Table 3.1430.2 GPS week: 1430 Day: 2 MJD: 54256
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | ---- 1245 226 471 238 --- 213 | 605 313 184 357 --- 176
R03 |30188 35 41 20 28 --- 19 | 36 41 66 71 --- 43
R04 | 3857 29 41 49 30 --- 21 | 31 47 59 46 --- 29
R06 |11250 32 58 39 45 --- 26 | 42 79 54 40 --- 34
R07 | 2294 42 41 41 48 97 25 | 52 58 44 31 60 32
R08 | 6395 30 24 60 32 --- 20 | 36 40 95 69 --- 47
XR10E | 9385 61 65 --- 40 --- 40 | 51 44 --- 54 --- 37
XR14E | 7956 33 30 --- 30 --- 22 | 46 37 --- 44 --- 31
XR15E | ---- --- 9 --- --- 1111 0 | --- 966 --- --- 54 961
R19 | 4598 21 39 92 31 --- 26 | 42 42 98 44 --- 37
R21 | 3998 29 14 134 63 --- 36 | 40 33 92 60 --- 29
XR22 | ---- --- 9 --- --- --- 0 | --- 172 --- --- --- 289
R23 | 2700 50 81 416 59 --- 45 | 38 49 249 60 --- 18
XR24 | 2136 23 36 --- 34 160 22 | 57 54 --- 45 98 49
------+------------------------------------+--------------------------------
RMS |11954 416 87 219 89 97 |T 89 141 104 76 70 129
WRMS |11954 53 41 60 89 97 |NE 97 84 104 82 79 71
MEDI | 4598 32 39 60 34 160 |MD 42 47 92 46 60 37
Table 3.1430.3 GPS week: 1430 Day: 3 MJD: 54257
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | ---- 115 678 317 99 --- 117 | 451 446 182 114 --- 63
R03 |31480 27 44 70 26 --- 23 | 61 27 67 38 --- 34
R04 | 6641 34 39 54 28 --- 21 | 71 30 76 31 --- 32
R06 |16350 45 47 50 34 --- 24 | 54 72 45 38 --- 36
R07 | 2672 30 34 43 25 83 18 | 32 51 53 39 62 32
R08 | 8783 49 35 70 27 --- 24 | 56 58 59 94 --- 60
XR10E |13195 142 123 --- 43 --- 74 | 94 89 --- 62 --- 48
XR14E | 8651 41 43 --- 37 --- 28 | 83 40 --- 47 --- 45
XR15E | ---- --- 25 --- --- 1499 0 | --- 817 --- --- 84 820
R19 | 4374 30 40 94 20 --- 25 | 64 44 92 41 --- 39
R21 | 3504 44 36 62 29 --- 23 | 62 39 97 65 --- 49
XR22 | ---- --- 25 --- --- --- 0 | --- 134 --- --- --- 168
R23 | 4285 43 60 454 42 --- 34 | 46 36 283 63 --- 30
XR24 | 2699 53 40 --- 39 181 31 | 61 73 --- 49 69 52
------+------------------------------------+--------------------------------
RMS |13400 53 229 193 43 83 |T 94 139 106 56 71 107
WRMS |13400 35 47 71 43 83 |NE 95 91 106 57 65 54
MEDI | 6641 43 40 70 29 181 |MD 61 51 76 47 69 45
Table 3.1430.4 GPS week: 1430 Day: 4 MJD: 54258
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8073 69 78 96 73 --- 45 | 126 113 82 103 --- 71
R03 | 8002 52 47 65 34 --- 29 | 41 47 71 57 --- 33
R04 | 5669 27 36 52 46 --- 23 | 81 59 66 32 --- 43
R06 | 8374 62 90 34 39 --- 35 | 50 80 38 44 --- 35
R07 | 2607 45 75 62 47 63 33 | 41 108 60 65 39 43
R08 | 5472 46 22 41 38 --- 22 | 67 48 89 72 --- 57
XR10E | 7344 57 48 --- 41 --- 34 | 66 56 --- 49 --- 35
XR14E |11551 37 48 --- 54 --- 33 | 72 84 --- 56 --- 50
XR15E | ---- --- 11 --- --- 1740 0 | --- 9999 --- --- 44 9999
R19 | 3449 37 38 78 31 --- 27 | 79 34 84 44 --- 51
R21 | 3148 49 46 30 62 --- 28 | 68 64 61 61 --- 32
XR22 | ---- --- 12 --- --- --- 0 | --- 468 --- --- --- 480
R23 | 3557 32 47 390 45 --- 29 | 74 32 223 39 --- 30
R24 | 2397 54 56 503 36 290 35 | 64 79 451 37 70 50
------+------------------------------------+--------------------------------
RMS | 5553 49 57 208 47 210 |T 69 97 122 54 51 77
WRMS | 5553 50 43 70 47 210 |NE 69 102 122 55 54 84
MEDI | 5472 46 47 62 41 290 |MD 67 64 71 49 44 43
Table 3.1430.5 GPS week: 1430 Day: 5 MJD: 54259
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8466 46 32 72 30 --- 23 | 139 98 57 45 --- 31
R03 |23569 39 26 77 30 --- 22 | 36 36 64 53 --- 35
R04 | 5477 53 36 119 19 --- 29 | 59 54 82 39 --- 32
R06 | 6465 38 56 45 31 --- 25 | 33 45 44 35 --- 21
R07 | 1835 39 32 42 28 34 19 | 27 53 34 72 29 42
R08 | 4971 76 42 86 44 --- 32 | 84 100 131 106 --- 97
XR10E | 4727 33 26 --- 30 --- 21 | 41 33 --- 59 --- 36
XR14E | 7472 41 40 --- 36 --- 27 | 36 29 --- 60 --- 32
XR15E | ---- --- 17 --- --- 1352 0 | --- 9999 --- --- 38 9999
R19 | 2536 25 23 65 23 --- 17 | 36 45 47 41 --- 29
R21 | 3185 16 29 113 16 --- 23 | 34 29 96 33 --- 28
XR22 | ---- --- 149 --- 116 --- 132 | --- 283 --- 178 --- 252
R23 | 2174 30 39 385 38 --- 26 | 45 27 208 32 --- 19
R24 | 2382 41 37 438 26 367 24 | 29 44 253 38 51 30
------+------------------------------------+--------------------------------
RMS | 8683 43 36 198 30 261 |T 49 67 101 60 39 52
WRMS | 8683 37 35 85 30 261 |NE 52 74 101 61 40 56
MEDI | 4727 39 32 77 30 367 |MD 36 45 64 45 38 32
Table 3.1430.6 GPS week: 1430 Day: 6 MJD: 54260
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9554 20 54 80 43 --- 26 | 104 94 64 52 --- 37
R03 |17838 24 31 61 40 --- 20 | 43 26 60 36 --- 28
R04 | 3946 56 43 65 54 --- 31 | 74 57 50 24 --- 39
R06 | 8228 22 41 56 24 --- 19 | 31 58 44 31 --- 31
R07 | 2856 23 33 45 40 47 19 | 25 42 55 44 36 27
R08 | 6263 45 39 54 36 --- 24 | 74 58 73 72 --- 58
XR10E | 4842 39 23 --- 57 --- 30 | 49 38 --- 45 --- 31
XR14E | 5816 37 35 --- 36 --- 25 | 39 44 --- 42 --- 35
XR15E | ---- --- 6 --- --- 2442 0 | --- 9999 --- --- 41 9999
R19 | 2125 19 25 184 57 --- 39 | 56 42 171 49 --- 50
R21 |11469 38 51 177 31 --- 39 | 36 43 158 35 --- 34
XR22 | ---- --- 156 --- 149 --- 152 | --- 136 --- 100 --- 259
R23 | 2664 21 42 405 50 --- 27 | 33 41 314 49 --- 29
R24 | 1750 28 37 436 34 534 23 | 45 74 368 35 79 48
------+------------------------------------+--------------------------------
RMS | 8284 32 41 210 42 379 |T 50 57 135 47 52 54
WRMS | 8284 29 37 81 42 379 |NE 52 61 135 47 57 58
MEDI | 4842 24 37 65 40 534 |MD 43 44 64 44 41 35
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