[IGSREPORT-16041] Wk 1468 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Fri Mar 14 08:20:34 PDT 2008
******************************************************************************
IGS Electronic Report 14 Mar 08:20:41 PDT 2008 Message Number 16041
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1468 (Feb 24, 2008 - Mar 01, 2008)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
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 2.1468.
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:
igl1468[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1468 in the SP3 format.
igl14687.sum Combination Report for GPS Week 1468.
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 | 1270.3 ns
1 | 1232.5 ns
2 | 1283.8 ns
3 | 1170.9 ns
4 | 1263.3 ns
5 | 1180.2 ns
6 | 1248.7 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 | R19
1 | ESX | R07
2 | ESX | R08 R15
3 | ESX | R19
4 | ESX | R01
5 | COD | R04
5 | ESX | R11
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 1.1468, 1a.1468).
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 2.1468.0-6)
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 3.1468.0-6).
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 1468 summary. (Feb 24, 2008 - Mar 01, 2008)
Table 1.1468.a GPS week : 1468 MJD: 54520.0-54526.0
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 64| -1 0 4 -24 -4 -14 -.05 47 33 | 0 88 2634 2745
| 1 4 4 54 50 80 .07 | 0 80
cod 178| -2 0 4 25 18 98 -.12 45 28 | --- --- --- ---
| 2 2 3 42 45 92 .08 | --- ---
esx 117| 6 2 2 89 -41 -64 .27 212 69 | -19404 -836 8248 25138
| 5 7 6 68 87 70 .12 | 45551 4322
iac n/a| 0 -1 -10 -34 -17 -111 -.00 46 46 | 1231803 -631 7980 19728
| 2 3 4 36 46 102 .06 | 43588 3266
mcc n/a| -4 1 29 -16 -97 -761 -.05 224 224 | --- --- --- ---
| 7 10 25 251 131 1109 .29 | --- ---
Table 1.1468.b GPS week : 1468 MJD: 54520.0-54526.0
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 | 25 26 21 17 23 31 30 |
R04 | 24 44 17 18 34 26 16 |
R06 | 22 27 28 20 14 19 13 |
R07 | 15 25 28 22 19 26 38 |
R08 | 39 35 25 29 23 29 49 |
R09 | 24 19 35 24 38 30 24 |
R10 | 15 26 20 19 25 21 29 |
R11 | 27 21 22 36 35 22 70 |
R13 | 21 29 26 28 16 29 44 |
R14 | 17 21 25 28 31 13 12 |
R15 | 39 38 26 32 29 27 15 |
R17 | 18 37 124 86 18 35 30 |
R19 | 28 25 19 23 22 16 37 |
R20 | 23 17 57 43 27 21 21 |
R23 | 19 19 20 20 22 22 19 |
R24 | 20 48 49 22 14 18 21 |
Table 1.1468.c GPS week : 1468 MJD: 54520.0-54526.0
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 1468 0 | 5 123 320 -2249 -2936 -12070 94.1 5504 5504 | 1270340 0
brd 1468 1 | -66 132 73 -3634 -715 -14250 99.5 5459 5459 | 1232492 0
brd 1468 2 | 102 -175 -180 -2145 2856 -18250 95.7 4888 4888 | 1283847 0
brd 1468 3 | 279 41 -22 -394 5444 -30570 93.7 5525 5525 | 1170920 0
brd 1468 4 | 154 53 -161 -1924 3982 -31490 98.1 6397 6397 | 1263276 0
brd 1468 5 | -338 76 427 -883 -7230 -23130 101.4 6067 6067 | 1180201 0
brd 1468 6 | 132 -63 425 5334 1347 -16000 94.8 6492 6492 | 1248700 0
-------------+------------------------------------------------------------+----------------
brd 1468 mean| 38 26 126 -842 392 -20822 96.7 5761 5761 | 1235682 0
brd 1468 sdev| 199 110 264 2915 4393 7786 3.0 578 578 | 44223 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 2.1468.0 GPS week: 1468 Day: 0 MJD: 54520
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 64| 0 0 2 -97 3 40 -.07 30 30 | 0 120 2273 2366
cod 178| -3 -1 4 107 76 2 -.15 39 31 | --- --- --- ---
esx 117| -3 -9 -1 124 -35 -119 .37 75 56 | 24029 -7880 7969 30149
iac n/a| 0 4 -6 -62 -15 -53 -.08 41 41 | 1267078 -7096 7572 23888
mcc n/a| -2 0 27 -163 -26 -66 -.15 234 234 | --- --- --- ---
Table 2.1468.1 GPS week: 1468 Day: 1 MJD: 54521
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 64| -3 -1 5 -5 -33 -140 -.09 45 38 | 0 245 2450 2589
cod 178| 0 1 3 3 8 86 -.07 35 25 | --- --- --- ---
esx 117| 7 2 6 115 -33 -77 .28 159 106 | -18873 -278 8825 30887
iac n/a| -2 -6 -8 -30 -56 49 .02 45 45 | 1225904 1156 9879 25677
mcc n/a| -11 -8 75 523 -145 -3055 .03 345 345 | --- --- --- ---
Table 2.1468.2 GPS week: 1468 Day: 2 MJD: 54522
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 64| 0 -7 13 24 69 5 -.03 78 32 | 0 19 2634 2719
cod 178| -6 -3 0 6 -37 138 -.26 63 36 | --- --- --- ---
esx 117| 2 6 -8 80 -200 -43 .16 454 58 | 28588 -770 7671 27436
iac n/a| 5 -2 -11 -19 76 -83 .01 63 63 | 1278448 -771 7373 20278
mcc n/a| 0 -15 0 -251 109 -733 -.57 106 106 | --- --- --- ---
Table 2.1468.3 GPS week: 1468 Day: 3 MJD: 54523
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 64| -2 1 2 -68 -94 -11 .07 84 45 | 0 4 3138 3225
cod 178| 0 4 9 41 69 250 -.15 47 32 | --- --- --- ---
esx 117| 6 -3 9 182 38 -87 .34 346 53 | -85382 2950 10741 24065
iac n/a| 0 -1 -10 -18 -50 -270 -.08 44 44 | 1168138 3566 10187 18851
mcc n/a| 8 2 18 -65 1 -1055 .40 111 111 | --- --- --- ---
Table 2.1468.4 GPS week: 1468 Day: 4 MJD: 54524
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 64| 0 4 1 -60 14 8 -.10 32 31 | 0 85 2689 2801
cod 178| -1 0 3 29 11 115 .00 28 23 | --- --- --- ---
esx 117| 8 11 4 101 40 -162 .37 117 71 | 11719 -3603 7557 22818
iac n/a| -1 -2 -11 -91 -18 -193 -.03 50 50 | 1258820 459 6817 17265
mcc n/a| -4 13 4 4 -190 -548 .00 88 88 | --- --- --- ---
Table 2.1468.5 GPS week: 1468 Day: 5 MJD: 54525
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 64| 0 -6 5 57 20 -97 -.12 31 26 | 0 97 2579 2741
cod 178| -4 0 1 -28 -36 125 -.10 75 29 | --- --- --- ---
esx 117| 8 9 4 -41 7 52 .33 146 58 | -73524 5443 7419 23369
iac n/a| -1 0 -20 22 -5 -135 .08 40 40 | 1177572 -642 7003 15141
mcc n/a| -14 2 37 -86 -279 -212 -.03 430 430 | --- --- --- ---
Table 2.1468.6 GPS week: 1468 Day: 6 MJD: 54526
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 64| -1 1 0 -20 -12 95 .02 31 30 | 0 46 2681 2780
cod 178| -1 4 5 19 36 -29 -.10 27 23 | --- --- --- ---
esx 117| 15 0 5 67 -111 -12 .04 183 77 | -22390 -1717 7558 17246
iac n/a| 0 0 -5 -42 -55 -96 .05 40 40 | 1246666 -1095 7034 17002
mcc n/a| -9 13 40 -76 -148 339 -.04 251 251 | --- --- --- ---
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 3.1468.0 GPS week: 1468 Day: 0 MJD: 54520
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7466 36 50 41 41 --- 24 | 60 90 86 43 --- 58
R04 | 6873 28 40 62 39 --- 23 | 27 64 61 28 --- 24
R06 | 3338 39 20 42 47 --- 21 | 40 56 63 65 --- 49
R07 | 5863 17 26 22 36 31 15 | 30 37 114 49 62 32
R08 | 5220 48 87 72 58 --- 38 | 36 94 58 59 --- 32
R09 | 7343 20 45 48 51 --- 23 | 22 47 60 40 --- 26
R10 | 1789 29 24 28 21 --- 15 | 20 35 47 29 --- 20
R11 | 8167 31 38 83 43 --- 27 | 35 64 84 62 --- 47
R13 | 6803 24 23 32 57 --- 20 | 28 25 52 53 --- 26
R14 | 2063 31 20 45 22 --- 17 | 17 33 49 23 --- 16
R15 | 3604 25 32 138 67 237 38 | 24 17 268 45 180 18
R17 |10068 14 25 59 29 --- 18 | 677 677 722 704 --- 693
R19 | 1704 33 54 173 22 --- 28 | 48 59 231 58 --- 50
R20 | 2491 39 28 68 27 --- 23 | 307 314 274 324 --- 308
R23 | 2919 20 24 67 21 --- 19 | 81 80 110 95 --- 86
R24 | 1571 28 37 45 32 327 20 | 607 662 678 648 487 645
------+------------------------------------+--------------------------------
RMS | 5503 30 39 75 41 234 |T 128 147 184 145 243 133
WRMS | 5503 30 31 56 41 234 |NE 128 147 184 145 243 133
MEDI | 3604 28 28 48 36 237 |MD 35 59 84 53 180 32
Table 3.1468.1 GPS week: 1468 Day: 1 MJD: 54521
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7242 47 32 57 51 --- 26 | 30 65 82 63 --- 47
R04 | 5139 52 42 196 37 --- 44 | 24 58 152 23 --- 32
R06 | 7110 32 43 49 61 --- 27 | 29 40 51 34 --- 23
R07 | 5440 35 20 490 49 183 25 | 41 41 369 57 31 38
R08 | 7175 53 51 121 39 --- 35 | 25 91 76 57 --- 48
R09 | 7092 26 19 60 36 --- 18 | 17 39 70 53 --- 27
R10 | 1389 41 10 113 20 --- 25 | 32 38 109 36 --- 32
R11 | 4120 29 29 55 40 --- 20 | 20 52 117 43 --- 35
R13 |10513 25 44 51 69 --- 28 | 30 43 64 79 --- 32
R14 | 2292 33 25 57 37 --- 20 | 11 40 73 38 --- 27
R15 | 3271 46 23 177 33 153 38 | 18 30 370 34 106 28
R17 | 6447 48 34 155 46 --- 37 | 708 733 814 807 --- 758
R19 | 1277 29 45 49 50 --- 25 | 34 59 201 68 --- 48
R20 | 1714 31 18 52 24 --- 16 | 353 399 398 404 --- 388
R23 | 4652 29 16 54 39 --- 18 | 62 54 84 72 --- 61
R24 | 1664 103 65 124 61 548 48 | 577 636 679 617 556 620
------+------------------------------------+--------------------------------
RMS | 5458 45 35 159 45 345 |T 125 151 231 155 231 140
WRMS | 5458 38 25 106 45 345 |NE 125 151 231 155 231 140
MEDI | 4652 33 29 57 39 183 |MD 30 52 109 57 106 35
Table 3.1468.2 GPS week: 1468 Day: 2 MJD: 54522
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5793 23 34 46 37 --- 20 | 47 64 101 42 --- 48
R04 | 5635 18 32 35 31 --- 17 | 36 34 95 40 --- 24
R06 | 1913 37 51 41 55 --- 27 | 33 51 50 44 --- 32
R07 | 5069 36 47 62 49 43 28 | 30 32 157 28 37 29
R08 | 7932 18 33 627 43 --- 24 | 23 54 582 26 --- 21
R09 | 5321 37 26 124 30 --- 34 | 22 52 122 44 --- 40
R10 | 1446 33 42 41 22 --- 20 | 15 39 52 33 --- 24
R11 | 2364 26 26 73 17 --- 21 | 31 48 131 51 --- 48
R13 | 8451 31 40 48 54 --- 25 | 39 29 48 51 --- 23
R14 | 4213 56 47 32 30 --- 24 | 19 59 32 18 --- 25
R15 | 3875 20 44 1667 36 144 25 | 16 52 9999 45 93 32
R17 | 6770 211 187 281 195 --- 124 | 9999 9999 9999 9999 --- 9999
R19 | 3575 16 28 43 37 --- 18 | 24 41 222 39 --- 26
R20 | 1210 150 79 95 59 --- 56 | 325 469 471 398 --- 410
R23 | 4402 33 29 36 37 --- 19 | 51 57 88 87 --- 63
R24 | 2247 132 58 82 61 --- 49 | 317 395 400 385 --- 371
------+------------------------------------+--------------------------------
RMS | 4888 78 63 454 63 106 |T 68 98 182 88 65 81
WRMS | 4888 32 36 58 63 106 |NE 68 98 182 88 65 81
MEDI | 4213 33 40 48 37 43 |MD 31 52 101 44 37 32
Table 3.1468.3 GPS week: 1468 Day: 3 MJD: 54523
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4557 14 31 37 30 --- 17 | 41 52 49 29 --- 39
R04 | 4944 50 19 33 23 --- 18 | 28 70 57 36 --- 31
R06 | 1589 34 28 51 29 --- 20 | 25 42 63 53 --- 38
R07 | 6428 25 34 38 47 62 22 | 35 38 120 49 54 34
R08 | 8517 63 37 69 40 --- 29 | 26 46 104 64 --- 48
XR09 | 5285 37 30 --- 35 --- 24 | 14 43 --- 51 --- 26
R10 | 1507 28 30 36 37 --- 19 | 23 44 61 37 --- 26
R11 | 4162 68 43 79 63 --- 35 | 15 40 162 114 --- 63
R13 | 8304 34 43 77 35 --- 28 | 18 17 108 46 --- 35
R14 | 3421 49 42 62 46 --- 28 | 33 32 83 52 --- 26
R15 | 3681 50 28 97 44 145 32 | 23 26 310 55 75 42
R17 |10985 272 127 105 68 --- 86 | 574 805 725 652 --- 691
R19 | 4373 41 21 1320 35 --- 22 | 35 66 9999 93 --- 66
R20 | 2491 86 64 81 70 --- 42 | 436 428 473 484 --- 452
R23 | 5295 41 29 40 32 --- 20 | 65 65 80 99 --- 72
R24 | 2909 52 26 49 31 --- 22 | 261 278 280 273 --- 273
------+------------------------------------+--------------------------------
RMS | 5525 84 47 346 44 111 |T 103 130 191 136 64 122
WRMS | 5525 45 32 53 44 111 |NE 103 130 191 136 64 122
MEDI | 4373 41 30 62 35 62 |MD 28 44 104 53 54 39
Table 3.1468.4 GPS week: 1468 Day: 4 MJD: 54524
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3920 20 22 337 54 --- 22 | 41 51 303 52 --- 43
R04 | 5154 42 69 60 58 --- 34 | 26 90 71 51 --- 60
R06 | 2184 30 18 24 26 --- 14 | 28 51 47 52 --- 39
R07 | 3901 22 21 46 47 95 18 | 34 41 72 48 64 39
R08 | 6370 31 25 70 44 --- 22 | 15 32 89 50 --- 16
R09 | 6647 35 24 178 32 --- 38 | 24 29 166 35 --- 28
R10 | 2218 35 22 95 37 --- 25 | 25 20 79 18 --- 13
R11 | 7587 36 27 108 88 --- 34 | 29 32 99 97 --- 39
R13 |13565 22 19 38 39 --- 16 | 31 20 62 33 --- 22
R14 | 2369 33 12 98 81 --- 30 | 25 20 98 75 --- 17
R15 | 7180 28 25 120 41 80 28 | 38 15 213 43 103 24
R17 |11955 27 18 60 33 --- 18 | 755 770 771 786 --- 773
R19 | 2536 29 26 62 51 --- 22 | 44 54 204 70 --- 49
R20 | 4448 43 30 92 42 --- 27 | 308 339 389 346 --- 339
R23 | 4040 42 32 39 37 --- 21 | 66 90 88 85 --- 78
R24 | 4331 18 19 27 36 --- 14 | 336 358 355 341 --- 343
------+------------------------------------+--------------------------------
RMS | 6396 32 28 117 50 88 |T 114 125 194 136 83 120
WRMS | 6396 31 23 71 50 88 |NE 114 125 194 136 83 120
MEDI | 4331 30 22 62 41 80 |MD 31 41 98 52 64 39
Table 3.1468.5 GPS week: 1468 Day: 5 MJD: 54525
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4910 32 24 127 39 --- 30 | 38 38 172 43 --- 34
R04 | 5231 31 269 45 37 --- 25 | 37 216 22 37 --- 28
R06 | 3669 33 34 27 33 --- 19 | 39 46 60 66 --- 45
R07 | 1831 23 40 88 40 72 25 | 39 56 91 48 67 44
R08 | 3919 23 44 111 35 --- 29 | 26 53 185 55 --- 39
R09 |13558 14 36 94 68 --- 29 | 16 32 110 39 --- 22
R10 | 3477 18 31 46 50 --- 20 | 13 27 55 25 --- 14
R11 | 8415 23 20 481 46 --- 21 | 23 35 456 48 --- 31
XR13 |15815 --- 30 79 25 --- 29 | --- 53 87 40 --- 33
R14 | 1618 25 20 26 21 --- 13 | 23 23 30 20 --- 18
R15 | 9052 21 24 117 36 122 27 | 21 37 126 28 83 25
R17 | 6331 68 31 123 32 --- 35 | 641 633 622 621 --- 630
R19 | 2059 33 21 29 25 --- 15 | 28 49 106 64 --- 43
R20 | 3737 34 27 40 45 --- 20 | 324 331 313 324 --- 325
R23 | 2524 30 25 57 47 --- 21 | 37 53 82 71 --- 47
R24 | 7242 21 25 66 25 731 18 | 290 290 308 309 453 295
------+------------------------------------+--------------------------------
RMS | 6066 31 75 146 40 430 |T 106 123 176 114 201 104
WRMS | 6066 26 29 58 40 430 |NE 106 123 176 114 201 104
MEDI | 3919 25 27 66 36 122 |MD 37 49 106 48 83 34
Table 3.1468.6 GPS week: 1468 Day: 6 MJD: 54526
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5580 18 16 182 32 --- 29 | 35 37 130 33 --- 33
R04 | 4221 18 29 32 30 --- 15 | 27 81 32 39 --- 32
R06 | 3592 26 13 35 22 --- 12 | 65 59 68 59 --- 59
R07 | 1903 17 55 193 44 62 37 | 35 49 165 37 50 39
R08 | 5032 45 28 308 18 --- 49 | 40 31 216 39 --- 31
R09 |14353 25 27 97 46 --- 23 | 17 31 103 37 --- 23
R10 | 3242 33 28 96 65 --- 28 | 18 26 85 28 --- 16
R11 | 7217 41 31 452 40 --- 70 | 27 41 399 55 --- 45
R13 |11137 38 18 268 41 --- 43 | 23 25 237 32 --- 24
R14 | 1714 25 11 44 15 --- 11 | 21 14 37 28 --- 12
R15 | 7735 25 19 51 25 83 14 | 21 23 143 36 84 18
R17 | 6653 51 23 97 63 --- 30 | 692 685 724 703 --- 695
R19 | 1322 27 35 220 32 --- 37 | 36 51 146 61 --- 48
R20 | 1358 29 31 37 46 --- 20 | 287 282 292 279 --- 284
R23 | 2729 22 23 91 28 --- 19 | 63 75 109 78 --- 69
R24 | 8525 31 20 58 47 423 20 | 387 396 395 396 447 392
------+------------------------------------+--------------------------------
RMS | 6491 31 27 183 40 251 |T 112 119 205 121 193 113
WRMS | 6491 30 23 77 40 251 |NE 112 119 205 121 193 113
MEDI | 4221 26 23 96 32 83 |MD 35 41 143 39 84 33
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