[IGSREPORT-15907] Wk 1462 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Sat Feb 2 10:45:27 PST 2008
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IGS Electronic Report 02 Feb 10:45:30 PST 2008 Message Number 15907
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1462 (Jan 13, 2008 - Jan 19, 2008)
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 2.1462.
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:
igl1462[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1462 in the SP3 format.
igl14627.sum Combination Report for GPS Week 1462.
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 | 1372.8 ns
1 | 1364.9 ns
2 | 1380.1 ns
3 | 1358.3 ns
4 | 1356.0 ns
5 | 1371.2 ns
6 | 1342.4 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 | R08 R19 R20 R23 R24
1 | ESX | R19 R20 R23 R24
2 | ESX | R14 R19 R20 R23 R24
3 | ESX | R14 R19 R20 R23 R24
4 | ESX | R19 R20 R23 R24
5 | ESX | R19 R20 R23 R24
6 | ESX | R10 R14 R19 R20 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 1.1462, 1a.1462).
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 2.1462.0-6)
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 3.1462.0-6).
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 1462 summary. (Jan 13, 2008 - Jan 19, 2008)
Table 1.1462.a GPS week : 1462 MJD: 54478.0-54484.0
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 58| 0 3 -11 -7 24 -53 .08 48 45 | 0 125 2831 2959
| 4 5 7 60 40 222 .20 | 0 227
cod 178| -2 0 3 -29 -48 87 -.02 36 34 | --- --- --- ---
| 4 5 6 74 105 114 .16 | --- ---
esx 51| -2 -3 6 65 106 -97 -.55 299 85 | -152841 3473 8614 16552
| 5 7 18 110 112 221 .16 | 374897 4516
iac n/a| 6 1 6 -85 -107 44 .66 59 59 | 1364251 -137 8094 15652
| 9 8 8 116 123 278 .30 | 12816 1106
mcc n/a| 1 -1 -19 -80 -140 837 1.03 655 655 | --- --- --- ---
| 15 21 30 158 191 1953 .27 | --- ---
Table 1.1462.b GPS week : 1462 MJD: 54478.0-54484.0
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
------+------------------------------------+------------------------------------------
R01E | 13 22 27 25 16 18 22 |
R04E | 27 17 32 24 25 29 21 |
R06E | 18 19 38 26 15 28 19 |
R07E | 36 31 39 33 28 35 28 |
R08E | 39 30 37 25 26 27 24 |
R10 | 22 17 23 20 13 20 29 |
R11 | --- --- 0 0 0 0 0 |
R14 | 15 19 24 16 20 20 19 |
R15 | 42 83 40 34 36 30 44 |
R17 | 41 44 54 36 16 40 28 |
R19 | 38 24 41 48 37 31 26 |
R20 | 19 36 31 49 29 29 29 |
R23 | 28 31 36 27 27 32 27 |
R24 | 20 50 38 27 22 35 30 |
Table 1.1462.c GPS week : 1462 MJD: 54478.0-54484.0
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 1462 0 | 741 1635 594 -54640 48330 -5106 111.0 10630 10630 | 1372840 0
brd 1462 1 | 891 786 43 -14380 7511 21170 98.5 8618 8618 | 1364930 0
brd 1462 2 | 201 385 141 -12360 10450 -16700 98.3 7408 7408 | 1380146 0
brd 1462 3 | 841 -873 -466 301 13690 -6810 104.7 6834 6834 | 1358341 0
brd 1462 4 | 166 303 535 -7580 924 -21670 94.2 8765 8765 | 1355987 0
brd 1462 5 |-1440 742 -122 -7879 -21110 -45200 97.1 7488 7488 | 1371203 0
brd 1462 6 |-3134 -163 670 -11220 -33540 -43040 91.0 7673 7673 | 1342433 0
-------------+------------------------------------------------------------+----------------
brd 1462 mean| -247 402 199 -15393 3750 -16765 99.3 8202 8202 | 1363697 0
brd 1462 sdev| 1504 789 421 17943 26336 23083 6.7 1269 1269 | 12598 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 2.1462.0 GPS week: 1462 Day: 0 MJD: 54478
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 58| 2 -5 -13 18 71 -110 -.15 52 51 | 0 464 3752 3967
cod 178| -1 2 -1 -71 -23 53 -.01 24 22 | --- --- --- ---
esx 51| 3 1 29 55 104 143 -.49 278 90 | -53609 3811 13214 23260
iac n/a| -2 -2 15 75 -145 -290 .74 67 67 | 1371235 1451 11547 20839
mcc n/a| -4 0 -11 -144 -166 -1366 1.34 781 781 | --- --- --- ---
Table 2.1462.1 GPS week: 1462 Day: 1 MJD: 54479
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 58| 3 11 -2 49 59 2 -.11 34 28 | 0 133 3200 3361
cod 178| -5 -7 6 3 -9 -15 .07 51 51 | --- --- --- ---
esx 51| -13 0 -20 -37 -75 224 -.31 329 87 | -53764 1793 6807 12422
iac n/a| 21 -1 -4 -210 21 -228 1.23 57 57 | 1365881 200 8332 15024
mcc n/a| -2 -14 -42 46 -271 -659 .84 641 641 | --- --- --- ---
Table 2.1462.2 GPS week: 1462 Day: 2 MJD: 54480
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 58| -7 7 -3 -21 58 -238 .00 54 50 | 0 46 2484 2569
cod 178| 5 0 13 64 -278 128 -.30 48 40 | --- --- --- ---
esx 51| -5 -3 -10 183 285 -143 -.65 320 113 | 26297 1656 6747 15440
iac n/a| -2 11 5 -257 -59 164 .70 59 59 | 1380533 26 6466 14675
mcc n/a| -7 -27 40 95 -53 -1237 1.07 559 559 | --- --- --- ---
Table 2.1462.3 GPS week: 1462 Day: 3 MJD: 54481
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 58| -2 -2 -21 -68 -1 -365 .27 58 53 | 0 -145 2625 2731
cod 178| -6 8 1 -143 -44 71 .15 33 27 | --- --- --- ---
esx 51| 1 0 18 152 144 -86 -.70 307 67 | 12726 106 10130 16477
iac n/a| 6 -9 3 -7 -179 535 .25 66 66 | 1357473 -906 9405 15523
mcc n/a| 12 19 -6 -132 -224 1231 .98 376 376 | --- --- --- ---
Table 2.1462.4 GPS week: 1462 Day: 4 MJD: 54482
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 58| 4 1 -18 -83 -37 -101 .40 58 59 | 0 399 2697 2854
cod 178| 0 3 2 -7 -24 84 .13 19 22 | --- --- --- ---
esx 51| -3 -14 3 63 150 -118 -.55 261 53 | -10648 13411 6754 18728
iac n/a| 7 7 1 -51 -335 161 .44 72 72 | 1357667 199 5657 14600
mcc n/a| -15 31 -36 94 -361 1772 1.02 404 404 | --- --- --- ---
Table 2.1462.5 GPS week: 1462 Day: 5 MJD: 54483
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 58| -1 6 -10 -26 -5 276 .15 46 40 | 0 38 2305 2407
cod 178| -8 -7 6 -89 55 -25 -.01 40 42 | --- --- --- ---
esx 51| 2 -14 23 154 23 -322 -.74 280 82 | -999999 1413 8579 15929
iac n/a| 17 10 0 -33 1 27 .60 48 48 | 1374508 -2106 7543 15708
mcc n/a| -6 5 -47 -280 -134 2513 1.39 720 720 | --- --- --- ---
Table 2.1462.6 GPS week: 1462 Day: 6 MJD: 54484
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 58| 5 2 -13 81 26 164 -.00 34 31 | 0 -58 2756 2825
cod 178| 0 -2 -6 36 -16 314 -.16 35 32 | --- --- --- ---
esx 51| 0 5 4 -116 115 -377 -.39 318 102 | 9106 2125 8067 13609
iac n/a| -2 -4 21 -111 -58 -62 .64 42 42 | 1342466 177 7714 13199
mcc n/a| 31 -21 -31 -240 231 3607 .61 1103 1103 | --- --- --- ---
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 3.1462.0 GPS week: 1462 Day: 0 MJD: 54478
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |12048 20 10 33 39 --- 12 | 59 62 78 70 --- 60
R04E |16821 41 23 77 77 --- 27 | 30 49 50 58 --- 39
R06E | 8342 31 18 48 48 --- 18 | 47 34 43 44 --- 34
R07E | 7073 76 19 75 116 70 36 | 50 24 62 87 32 17
R08E |16903 80 37 158 60 --- 38 | 78 57 47 53 --- 46
XR10 | 6278 23 17 --- 67 --- 21 | 41 37 --- 26 --- 33
XR14 | 5734 23 12 --- 37 --- 14 | 20 28 --- 26 --- 25
XR15 | 6407 77 25 --- 106 146 41 | 100 51 --- 67 34 49
XR17 |10711 80 22 --- 99 --- 40 | 70 70 --- 94 --- 68
R19 | 4400 80 40 442 38 --- 37 | 47 77 425 79 --- 58
R20 | 4356 39 16 366 31 --- 18 | 55 68 385 63 --- 60
R23 |10375 29 19 389 90 --- 28 | 70 51 339 59 --- 53
R24 | 6162 27 14 418 59 1103 20 | 208 220 478 207 768 216
------+------------------------------------+--------------------------------
RMS |10632 52 24 278 67 781 |T 67 63 211 71 278 58
WRMS |10632 51 22 90 67 781 |NE 76 75 406 77 401 70
MEDI | 7073 39 19 158 60 146 |MD 55 51 78 63 34 49
Table 3.1462.1 GPS week: 1462 Day: 1 MJD: 54479
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 4074 26 34 54 51 --- 22 | 57 75 49 74 --- 54
R04E |14718 16 26 45 45 --- 17 | 42 42 61 34 --- 31
R06E |12882 19 34 45 41 --- 18 | 34 38 60 44 --- 34
R07E | 6479 20 55 70 87 93 30 | 36 22 86 83 37 26
XR08E | 3815 30 51 --- 54 --- 29 | 62 67 --- 52 --- 46
XR10 | 2578 17 22 --- 39 --- 17 | 33 31 --- 35 --- 29
XR14 | 2704 19 17 --- 47 --- 18 | 14 26 --- 31 --- 20
XR15 | 3175 87 133 --- 160 87 82 | 166 126 --- 64 34 93
XR17 |11674 32 40 --- 126 --- 44 | 78 71 --- 148 --- 85
R19 | 2001 24 42 479 39 --- 23 | 55 52 318 47 --- 43
R20 | 2043 45 58 485 54 --- 36 | 45 43 274 34 --- 24
R23 |10760 34 39 343 69 --- 31 | 41 36 177 43 --- 28
R24 | 5390 62 91 523 57 901 50 | 202 191 409 179 707 193
------+------------------------------------+--------------------------------
RMS | 8618 34 51 329 57 641 |T 66 63 179 66 259 54
WRMS | 8618 28 51 87 57 641 |NE 79 72 294 72 370 64
MEDI | 4074 26 40 70 54 93 |MD 45 43 86 47 37 34
Table 3.1462.2 GPS week: 1462 Day: 2 MJD: 54480
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 6899 35 50 58 35 --- 26 | 38 27 87 51 --- 37
R04E | 3954 40 63 59 58 --- 32 | 34 46 50 45 --- 29
R06E |11699 83 50 62 58 --- 37 | 47 26 57 66 --- 24
R07E | 7732 67 38 90 71 81 39 | 36 31 85 78 69 35
R08E | 6083 51 74 46 80 --- 37 | 102 106 110 101 --- 87
XR10 | 1833 32 22 --- 41 --- 23 | 30 21 --- 55 --- 26
XR11 | ---- --- 21 --- --- --- 0 | --- 209 --- --- --- 213
R14 | 2357 36 35 489 31 --- 24 | 16 40 76 24 --- 25
XR15 | 2957 51 49 --- 70 134 40 | 72 62 --- 95 65 42
XR17 | 5219 89 60 --- 77 --- 54 | 41 76 --- 93 --- 52
R19 | 1055 51 39 482 79 --- 41 | 23 42 359 92 --- 38
R20 | 2720 48 27 490 51 --- 30 | 46 37 362 68 --- 46
R23 |14614 60 35 362 53 --- 35 | 59 46 222 25 --- 25
R24 | 4925 52 55 401 52 787 37 | 99 143 323 120 587 123
------+------------------------------------+--------------------------------
RMS | 7408 54 48 320 59 559 |T 49 65 173 70 240 57
WRMS | 7408 50 40 113 59 559 |NE 48 75 268 71 326 65
MEDI | 4925 51 39 90 58 134 |MD 41 42 87 68 69 37
Table 3.1462.3 GPS week: 1462 Day: 3 MJD: 54481
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |10749 46 32 49 55 --- 25 | 72 78 70 91 --- 69
R04E | 3413 50 26 39 60 --- 24 | 32 36 49 45 --- 25
R06E | 6424 43 27 41 77 --- 25 | 30 27 54 56 --- 26
R07E | 2760 64 23 43 110 102 33 | 25 42 37 97 52 19
R08E | 8698 47 31 47 56 --- 24 | 151 105 125 121 --- 121
XR10 | 2516 36 19 --- 37 --- 20 | 53 25 --- 31 --- 25
XR11 | ---- --- 12 --- --- --- 0 | --- 193 --- --- --- 196
R14 | 3095 27 18 504 23 --- 15 | 22 17 85 23 --- 15
XR15 | 6080 62 30 --- 61 88 33 | 90 42 --- 91 65 54
XR17 | 5774 52 42 --- 66 --- 35 | 56 76 --- 54 --- 59
R19 | 1390 54 60 410 98 --- 47 | 67 65 316 126 --- 56
R20 | 2918 109 42 493 45 --- 48 | 90 48 363 44 --- 35
R23 |13414 49 26 363 42 --- 26 | 86 61 280 64 --- 59
R24 | 3910 55 22 370 42 522 27 | 178 201 330 192 446 195
------+------------------------------------+--------------------------------
RMS | 6834 58 33 307 66 376 |T 73 72 170 79 187 68
WRMS | 6834 53 27 67 66 376 |NE 80 80 274 78 255 77
MEDI | 3910 50 26 49 56 102 |MD 67 48 85 64 65 54
Table 3.1462.4 GPS week: 1462 Day: 4 MJD: 54482
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9402 41 15 22 48 --- 15 | 42 58 73 49 --- 54
R04E | 3806 32 21 45 105 --- 25 | 34 26 67 57 --- 30
R06E |15906 32 17 23 48 --- 15 | 41 17 44 48 --- 26
R07E | 3572 74 16 37 101 165 28 | 43 36 64 61 37 33
R08E | 7552 79 13 52 55 --- 26 | 56 67 65 129 --- 63
XR10 | 2244 21 10 --- 36 --- 12 | 30 19 --- 21 --- 19
XR11 | ---- --- 5 --- --- --- 0 | --- 98 --- --- --- 100
XR14 | 2999 40 18 --- 41 --- 19 | 29 24 --- 44 --- 23
XR15 | 2648 79 14 --- 96 100 36 | 82 58 --- 60 38 50
XR17 | 8084 36 13 --- 31 --- 16 | 69 42 --- 35 --- 33
R19 | 1423 66 19 436 108 --- 36 | 22 56 328 120 --- 44
R20 | 2235 68 26 403 41 --- 28 | 47 66 265 39 --- 58
R23 |15752 66 24 388 36 --- 27 | 41 67 277 62 --- 54
R24 | 3257 41 20 324 53 548 22 | 176 179 311 148 254 176
------+------------------------------------+--------------------------------
RMS | 8765 58 19 261 72 404 |T 54 58 166 67 109 54
WRMS | 8765 59 22 53 72 404 |NE 62 67 295 66 146 61
MEDI | 3572 41 16 52 48 165 |MD 42 56 73 57 38 44
Table 3.1462.5 GPS week: 1462 Day: 5 MJD: 54483
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8299 29 34 27 34 --- 18 | 49 84 74 80 --- 63
R04E | 4366 28 41 88 39 --- 28 | 36 45 50 48 --- 31
R06E | 8048 33 43 63 59 --- 28 | 38 34 59 35 --- 24
R07E | 8446 75 20 62 75 224 35 | 52 38 40 32 21 26
R08E | 8620 33 34 59 61 --- 26 | 67 74 103 108 --- 78
XR10 | 3058 27 26 --- 33 --- 20 | 42 26 --- 30 --- 21
XR11 | ---- --- 9 --- --- --- 0 | --- 148 --- --- --- 149
XR14 | 2875 17 29 --- 36 --- 19 | 18 22 --- 39 --- 15
XR15 | 3656 45 33 --- 50 93 30 | 42 39 --- 48 21 28
XR17 | 9962 63 61 --- 31 --- 40 | 27 103 --- 39 --- 54
R19 | 3003 42 43 394 44 --- 30 | 35 51 224 55 --- 36
R20 | 2936 47 34 445 40 --- 29 | 50 61 244 35 --- 40
R23 |13025 45 52 453 33 --- 32 | 74 52 249 57 --- 47
R24 | 4353 61 46 361 26 993 34 | 153 162 256 159 180 152
------+------------------------------------+--------------------------------
RMS | 7487 46 40 280 48 719 |T 52 67 144 58 74 54
WRMS | 7487 40 42 82 48 719 |NE 55 73 243 57 100 60
MEDI | 4366 42 34 88 39 224 |MD 42 51 103 48 21 36
Table 3.1462.6 GPS week: 1462 Day: 6 MJD: 54484
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |12013 26 40 53 31 --- 21 | 59 63 97 82 --- 68
R04E | 5407 22 30 42 51 --- 21 | 26 34 47 34 --- 27
R06E | 5689 24 31 43 37 --- 19 | 33 45 55 43 --- 37
R07E | 4986 46 37 66 43 271 27 | 43 26 64 77 31 40
R08E |11656 36 39 59 35 --- 24 | 71 64 77 82 --- 68
R10 | 3354 34 38 503 49 --- 28 | 30 35 6 48 --- 26
XR11 | ---- --- 18 --- --- --- 0 | --- 118 --- --- --- 118
R14 | 3362 28 23 466 29 --- 19 | 21 27 54 28 --- 20
XR15 |14459 52 46 --- 83 163 43 | 24 47 --- 57 40 33
XR17 | 9811 43 31 --- 39 --- 27 | 60 103 --- 86 --- 80
R19 | 4262 35 22 379 47 --- 25 | 41 72 373 94 --- 61
R20 | 3145 40 24 394 53 --- 29 | 77 55 358 65 --- 60
R23 |13630 24 46 392 42 --- 27 | 72 56 322 87 --- 59
R24 | 6676 48 41 422 32 1535 29 | 84 133 387 109 386 106
------+------------------------------------+--------------------------------
RMS | 7673 34 35 318 42 1102 |T 49 62 167 68 152 57
WRMS | 7673 31 32 102 42 1102 |NE 51 71 250 71 213 62
MEDI | 5689 35 31 379 42 271 |MD 43 55 77 77 40 59
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