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[IGSREPORT-15860] Wk 1460 IGLOS Final Orbits
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IGS Electronic Report 17 Jan 00:05:04 PST 2008 Message Number 15860
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1460 (Dec 30, 2007 - Jan 05, 2008)
Contact: Gerd Gendt (gendt @ gfz-potsdam.de)
Thomas Nischan ( nisn @ 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 2.1460.
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:
igl1460[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1460 in the SP3 format.
igl14607.sum Combination Report for GPS Week 1460.
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 | 1430.4 ns
1 | 1415.6 ns
2 | 1424.6 ns
3 | 1426.3 ns
4 | 1420.4 ns
5 | 1366.7 ns
6 | 1386.3 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
----+--------+---------------
0 | ESX | R08 R19 R20 R23 R24
1 | ESX | R19 R20 R23 R24
2 | ESX | R19 R20 R23 R24
3 | ESX | R19 R20 R23 R24
4 | ESX | R19 R20 R23 R24
5 | ESX | R19 R20 R23 R24
5 | IAC | R23
6 | ESX | R08 R19 R20 R23 R24
6 | IAC | R23
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 1.1460, 1a.1460).
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 2.1460.0-6)
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 3.1460.0-6).
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 1460 summary. (Dec 30, 2007 - Jan 05, 2008)
Table 1.1460.a GPS week : 1460 MJD: 54464.0-54470.0
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 57| -1 4 -2 -35 15 103 .04 51 47 | 0 102 2844 2971
| 4 6 11 76 86 259 .19 | 0 292
cod 172| -1 -5 2 50 -69 -4 -.26 34 32 | --- --- --- ---
| 5 3 8 38 32 111 .16 | --- ---
esx 48| 1 2 6 94 68 9 -.46 282 67 | 4583935 66235 9737 15807
| 8 4 12 114 120 171 .25 | 3159775 40808
iac n/a| 0 1 -4 -66 -26 -62 .64 40 40 | 1413532 -4450 12422 19811
| 3 5 8 60 48 74 .19 | 28603 10767
mcc n/a| 0 -5 54 45 6 -750 .10 955 955 | --- --- --- ---
| 9 14 27 191 116 1561 .61 | --- ---
Table 1.1460.b GPS week : 1460 MJD: 54464.0-54470.0
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 | 18 28 22 28 21 19 17 |
R04E | 17 22 21 21 24 22 26 |
R06E | 22 20 23 22 22 20 30 |
R07E | 25 23 27 30 32 26 30 |
R08E | 29 31 27 17 14 19 29 |
R10 | 19 16 19 18 16 15 18 |
R14 | 14 17 24 13 24 22 21 |
R15 | 40 28 50 26 29 19 32 |
R17 | 41 40 34 24 36 23 28 |
R19 | 32 20 18 21 27 30 41 |
R20 | 16 27 46 23 25 26 26 |
R23 | 31 48 38 36 44 213 134 |
R24 | 40 42 27 19 31 27 33 |
Table 1.1460.c GPS week : 1460 MJD: 54464.0-54470.0
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 1460 0 | -717 -221 -453 2751 -3715 -39400 106.5 5345 5345 | 1430440 0
brd 1460 1 | -964 486 -369 -6740 3568 -47990 102.6 8209 8209 | 1415608 0
brd 1460 2 | -574 249 553 -8641 3611 -30420 92.7 7159 7159 | 1424633 0
brd 1460 3 | -667 -242 555 -9859 -5134 -13440 88.2 7230 7230 | 1426299 0
brd 1460 4 | -147 -225 671 2609 -5662 6932 101.3 7190 7190 | 1420432 0
brd 1460 5 | 151 215 -395 5859 463 -38180 86.6 5704 5704 | 1366688 0
brd 1460 6 | 78 95 291 741 -3135 -26120 110.7 5557 5557 | 1386289 0
-------------+------------------------------------------------------------+----------------
brd 1460 mean| -406 51 121 -1897 -1429 -26945 98.4 6627 6627 | 1410055 0
brd 1460 sdev| 431 287 507 6342 3952 18560 9.3 1088 1088 | 24069 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 2.1460.0 GPS week: 1460 Day: 0 MJD: 54464
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 57| 5 0 4 12 61 -184 .07 38 32 | 0 627 3207 3482
cod 172| -9 -4 8 9 -80 65 .00 35 34 | --- --- --- ---
esx 48| 8 1 -4 122 31 262 -.28 289 78 | 6243486 88873 8593 17272
iac n/a| 0 2 -7 -146 -60 -151 .48 51 51 | 1450229 -27706 37330 48642
mcc n/a| 2 11 17 -101 -189 -4263 .55 96 96 | --- --- --- ---
Table 2.1460.1 GPS week: 1460 Day: 1 MJD: 54465
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 57| -5 3 6 -141 -69 -83 .27 64 54 | 0 24 2662 2770
cod 172| -2 -10 10 113 -23 -1 -.30 36 36 | --- --- --- ---
esx 48| 5 1 -5 8 237 -119 -.51 244 59 | 6400231 101659 9929 16285
iac n/a| 3 1 -13 -44 -100 44 .42 45 45 | 1416738 -12 8362 13733
mcc n/a| 3 -10 25 75 -90 204 -.38 1708 1708 | --- --- --- ---
Table 2.1460.2 GPS week: 1460 Day: 2 MJD: 54466
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 57| -6 10 -17 -97 137 345 .33 53 53 | 0 -4 2578 2684
cod 172| 6 -5 11 22 -78 -94 -.14 26 23 | --- --- --- ---
esx 48| -8 0 2 47 -64 -5 -.31 279 69 | 6438190 91260 9191 16870
iac n/a| -4 7 -11 -70 28 -89 .63 50 50 | 1425470 380 8490 17554
mcc n/a| -14 9 51 108 39 -168 -.12 500 500 | --- --- --- ---
Table 2.1460.3 GPS week: 1460 Day: 3 MJD: 54467
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 57| 3 -8 5 59 -60 66 -.04 38 36 | 0 -227 3343 3462
cod 172| 0 -2 0 36 -33 190 -.33 35 33 | --- --- --- ---
esx 48| -9 10 -2 -68 150 -126 -.96 259 69 | 6503885 78704 11712 15563
iac n/a| -1 2 -5 38 -66 -134 .60 30 30 | 1427990 -5103 9264 15736
mcc n/a| -10 5 96 68 177 -446 -.40 723 723 | --- --- --- ---
Table 2.1460.4 GPS week: 1460 Day: 4 MJD: 54468
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 57| -1 7 2 -95 -87 539 -.12 59 53 | 0 3 2371 2442
cod 172| -1 -9 0 89 -117 -28 -.53 38 37 | --- --- --- ---
esx 48| -1 0 21 132 181 -129 -.55 318 62 | 6579811 88315 8663 16723
iac n/a| 3 4 -9 -32 8 -86 .56 27 27 | 1421952 -3480 7444 15264
mcc n/a| -4 -10 77 -302 41 -189 -.32 1188 1188 | --- --- --- ---
Table 2.1460.5 GPS week: 1460 Day: 5 MJD: 54469
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 57| 1 6 1 -13 66 125 -.13 58 59 | 0 -75 2979 3075
cod 172| 0 -5 -2 60 -63 -11 -.30 25 25 | --- --- --- ---
esx 48| 5 -2 10 129 -11 -57 -.32 283 54 | -54853 11704 11984 15475
iac n/a| -4 2 2 -103 11 -38 .87 34 34 | 1363168 5300 9051 13803
mcc n/a| 7 -13 55 225 39 -96 .08 2404 2404 | --- --- --- ---
Table 2.1460.6 GPS week: 1460 Day: 6 MJD: 54470
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 57| -6 12 -18 28 59 -82 -.11 45 41 | 0 368 2768 2886
cod 172| -6 0 -12 20 -91 -153 -.21 45 37 | --- --- --- ---
esx 48| 10 5 24 292 -45 241 -.28 303 79 | -23202 3133 8088 12466
iac n/a| -1 -10 11 -109 -7 20 .92 43 43 | 1389177 -533 7016 13947
mcc n/a| 10 -27 58 244 28 -294 1.25 68 68 | --- --- --- ---
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 3.1460.0 GPS week: 1460 Day: 0 MJD: 54464
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 5393 21 25 34 42 --- 17 | 51 46 38 52 --- 41
R04E | 3843 23 24 20 46 --- 16 | 44 42 37 60 --- 46
R06E | 3603 31 42 36 38 --- 21 | 40 53 27 48 --- 36
R07E | 2236 33 37 51 48 96 24 | 34 23 41 49 100 27
R08E |12038 44 21 118 51 --- 28 | 29 33 58 51 --- 35
XR10 | 3683 19 29 --- 33 --- 19 | 24 23 --- 32 --- 24
XR14 | 2505 17 19 --- 25 --- 14 | 22 29 --- 39 --- 28
XR15 | 5126 42 35 --- 89 292 39 | 40 45 --- 83 74 51
XR17 | 9144 43 56 --- 77 --- 41 | 55 90 --- 92 --- 78
R19 | 1942 26 43 486 65 --- 31 | 71 80 490 141 --- 117
XR20 | 6599 19 22 --- 28 --- 16 | 69 89 --- 95 --- 86
R23 | 3566 37 35 472 62 --- 31 | 427 383 116 256 --- 412
R24 | 2305 67 45 438 48 --- 39 | 241 246 403 246 --- 251
------+------------------------------------+--------------------------------
RMS | 5345 38 35 289 51 96 |T 88 90 151 95 87 94
WRMS | 5345 32 34 78 51 96 |NE 118 123 336 123 74 130
MEDI | 3683 31 35 51 48 96 |MD 44 46 41 60 74 46
Table 3.1460.1 GPS week: 1460 Day: 1 MJD: 54465
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9315 33 32 87 42 --- 28 | 52 56 71 49 --- 39
R04E | 7476 30 41 46 35 --- 22 | 60 67 91 73 --- 67
R06E | 6476 37 36 33 31 --- 20 | 37 46 31 47 --- 28
R07E | 6983 46 20 58 39 128 23 | 30 22 60 40 109 29
R08E |11880 85 32 46 45 --- 31 | 36 43 68 44 --- 36
XR10 | 9480 23 20 --- 23 --- 15 | 24 25 --- 26 --- 22
XR14 | 4976 18 24 --- 28 --- 17 | 22 34 --- 30 --- 28
XR15 | 6752 36 35 --- 44 278 27 | 24 46 --- 59 70 35
XR17 |10648 51 36 --- 76 --- 39 | 47 48 --- 154 --- 95
XR19 | 5165 33 18 --- 34 --- 20 | 39 61 --- 81 --- 61
XR20 | 9220 30 40 --- 40 --- 26 | 65 72 --- 92 --- 73
R23 | 8541 88 37 497 77 --- 48 | 346 305 94 269 --- 347
R24 | 4925 91 50 394 32 2411 42 | 223 247 270 226 9999 235
------+------------------------------------+--------------------------------
RMS | 8209 64 36 244 45 1707 |T 77 82 97 91 89 84
WRMS | 8209 54 36 59 45 1707 |NE 98 104 182 117 70 112
MEDI | 7476 36 35 58 39 278 |MD 39 48 71 59 70 39
Table 3.1460.2 GPS week: 1460 Day: 2 MJD: 54466
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |12771 51 24 31 52 --- 22 | 53 57 58 57 --- 44
R04E | 3292 48 20 50 38 --- 21 | 39 51 62 63 --- 43
R06E | 8356 56 34 41 30 --- 22 | 43 48 42 30 --- 30
R07E | 2120 51 23 48 74 87 27 | 28 25 43 54 42 22
R08E |11926 66 17 73 36 --- 27 | 42 36 40 49 --- 36
XR10 | 1612 32 19 --- 34 --- 18 | 25 38 --- 28 --- 24
XR14 | 2077 41 27 --- 40 --- 24 | 23 52 --- 41 --- 34
XR15 | 7401 75 39 --- 109 289 50 | 34 35 --- 52 40 26
XR17 |10413 56 39 --- 59 --- 34 | 36 71 --- 52 --- 51
R19 | 2005 39 15 485 27 --- 18 | 26 50 375 38 --- 54
XR20 | 2374 48 54 --- 91 --- 45 | 52 83 --- 112 --- 73
R23 | 3008 50 37 455 79 --- 37 | 354 352 102 202 --- 358
R24 | 2547 59 27 412 33 702 26 | 259 231 337 245 578 244
------+------------------------------------+--------------------------------
RMS | 7159 53 26 279 50 500 |T 78 86 132 78 220 79
WRMS | 7159 53 23 69 50 500 |NE 101 114 271 96 309 108
MEDI | 3008 51 27 50 40 289 |MD 39 51 58 52 42 43
Table 3.1460.3 GPS week: 1460 Day: 3 MJD: 54467
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |13245 40 47 87 29 --- 28 | 41 72 76 63 --- 53
R04E | 3874 35 25 69 24 --- 21 | 36 70 65 78 --- 61
R06E | 5832 35 42 50 29 --- 22 | 53 47 46 45 --- 34
R07E | 2833 60 44 61 43 84 29 | 52 30 57 66 60 47
R08E |11348 28 29 32 27 --- 16 | 34 37 46 34 --- 24
XR10 | 2569 27 21 --- 26 --- 17 | 30 29 --- 33 --- 24
XR14 | 2181 18 15 --- 21 --- 13 | 24 26 --- 30 --- 24
XR15 | 7051 32 35 --- 39 295 25 | 55 46 --- 53 49 42
XR17 |10163 33 33 --- 35 --- 24 | 57 52 --- 40 --- 39
R19 | 1785 31 26 455 30 --- 20 | 43 34 363 49 --- 50
XR20 | 2159 42 20 --- 31 --- 22 | 86 95 --- 95 --- 89
XR23 | 5022 32 60 --- 53 --- 36 | 328 315 --- 170 --- 307
R24 | 1199 30 26 492 22 1018 18 | 118 142 368 135 9999 143
------+------------------------------------+--------------------------------
RMS | 7230 38 35 258 30 723 |T 73 76 145 68 54 72
WRMS | 7230 36 33 69 30 723 |NE 92 92 365 75 49 89
MEDI | 3874 32 29 69 29 295 |MD 52 47 65 53 49 47
Table 3.1460.4 GPS week: 1460 Day: 4 MJD: 54468
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |11768 39 32 57 25 --- 20 | 47 43 68 51 --- 41
R04E | 5608 80 23 57 19 --- 24 | 67 46 74 52 --- 48
R06E | 5715 58 43 45 19 --- 22 | 29 61 26 42 --- 34
R07E | 6335 89 54 62 32 104 31 | 71 33 63 64 50 39
R08E |11430 32 20 33 17 --- 13 | 44 38 66 39 --- 36
XR10 | 3903 31 23 --- 20 --- 16 | 28 32 --- 28 --- 22
XR14 | 2965 29 36 --- 31 --- 23 | 42 36 --- 37 --- 30
XR15 | 5181 53 44 --- 34 228 29 | 45 45 --- 47 90 32
XR17 | 7352 61 61 --- 38 --- 36 | 54 116 --- 56 --- 77
R19 | 1706 47 38 467 33 --- 26 | 79 68 335 58 --- 71
R20 | 5186 58 37 516 23 --- 25 | 49 94 132 84 --- 94
XR23 | 4740 62 77 --- 47 --- 43 | 495 436 --- 422 --- 466
R24 | 3216 40 47 558 41 1676 30 | 305 288 364 311 9999 300
------+------------------------------------+--------------------------------
RMS | 7190 59 38 318 27 1187 |T 104 102 141 99 70 99
WRMS | 7190 53 37 62 27 1187 |NE 137 139 277 130 90 136
MEDI | 5186 53 38 57 31 228 |MD 49 46 68 52 50 41
Table 3.1460.5 GPS week: 1460 Day: 5 MJD: 54469
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9745 39 20 53 25 --- 19 | 70 47 71 49 --- 47
R04E | 5134 57 26 41 36 --- 21 | 79 71 42 91 --- 77
R06E | 2748 56 20 46 25 --- 20 | 30 34 32 46 --- 29
R07E | 3823 73 31 34 49 63 25 | 47 26 42 65 49 36
R08E | 7308 59 20 37 21 --- 18 | 36 35 34 41 --- 29
XR10 | 2357 34 11 --- 25 --- 15 | 21 25 --- 23 --- 20
XR14 | 1827 45 27 --- 29 --- 22 | 35 29 --- 34 --- 24
XR15 |14640 25 20 --- 33 299 18 | 59 60 --- 47 114 52
XR17 | 6706 60 24 --- 24 --- 23 | 60 86 --- 73 --- 74
XR19 | 2542 68 34 --- 38 --- 30 | 34 72 --- 43 --- 43
R20 | 4550 72 18 518 30 --- 25 | 81 83 123 97 --- 89
XR23 |13281 366 122 --- 580 --- 212 | 621 694 --- 438 --- 581
R24 | 3179 41 35 535 41 3398 27 | 124 149 464 126 9999 137
------+------------------------------------+--------------------------------
RMS | 5703 58 25 283 34 2403 |T 99 108 115 90 81 95
WRMS | 5703 59 25 54 34 2403 |NE 129 149 293 110 114 127
MEDI | 4550 57 24 46 30 299 |MD 59 60 42 49 49 47
Table 3.1460.6 GPS week: 1460 Day: 6 MJD: 54470
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8293 37 19 32 27 --- 17 | 52 54 54 52 --- 48
XR04E | 6889 38 27 --- 44 --- 26 | 54 56 --- 68 --- 54
R06E | 2481 37 63 69 35 --- 30 | 28 57 49 42 --- 36
R07E | 1574 40 45 47 69 68 29 | 51 42 58 86 45 49
R08E |10057 45 32 179 43 --- 28 | 55 30 49 40 --- 33
XR10 | 1827 22 19 --- 34 --- 18 | 21 24 --- 24 --- 20
XR14 | 2276 28 24 --- 33 --- 20 | 28 26 --- 33 --- 24
XR15 |18082 37 44 --- 54 237 32 | 43 39 --- 44 58 34
XR17 | 7537 37 38 --- 43 --- 28 | 97 126 --- 102 --- 109
R19 | 1233 65 65 516 35 --- 41 | 41 106 471 76 --- 94
R20 | 2274 41 25 495 41 --- 26 | 80 95 123 100 --- 104
XR23 |16221 128 139 --- 497 --- 133 | 604 682 --- 855 --- 604
XR24 | 2563 39 56 --- 44 2564 33 | 218 195 --- 204 833 200
------+------------------------------------+--------------------------------
RMS | 5556 45 45 303 43 68 |T 105 117 134 132 312 108
WRMS | 5556 41 37 79 43 68 |NE 141 161 297 179 445 148
MEDI | 2563 38 38 69 43 237 |MD 52 56 54 68 58 49