[IGSREPORT-16483] Wk 1488 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 31 07:59:40 PDT 2008
******************************************************************************
IGS Electronic Report 31 Jul 07:59:42 PDT 2008 Message Number 16483
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1488 (Jul 13, 2008 - Jul 19, 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 2.1488.
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:
igl1488[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1488 in the SP3 format.
igl14887.sum Combination Report for GPS Week 1488.
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 | 765.0 ns
1 | 754.0 ns
2 | 773.7 ns
3 | 781.1 ns
4 | 746.5 ns
5 | 809.9 ns
6 | 812.2 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
----+--------+---------------
3 | ESX | R19
6 | ESX | R13
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 1.1488, 1a.1488).
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 2.1488.0-6)
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 3.1488.0-6).
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 1488 summary. (Jul 13, 2008 - Jul 19, 2008)
Table 1.1488.a GPS week : 1488 MJD: 54660.0-54666.0
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 66| 1 0 -8 -27 0 114 -.13 40 33 | 0 -91 2717 2828
| 3 2 4 33 45 111 .12 | 0 133
cod 216| -4 -1 -2 -5 -28 15 -.12 33 25 | --- --- --- ---
| 3 2 3 54 33 54 .06 | --- ---
esx 120| 2 1 8 97 -2 9 .43 69 50 | -8607 3296 9342 16639
| 3 2 6 55 66 156 .16 | 29003 10045
iac n/a| 4 1 11 -45 14 -121 -.03 45 45 | 777546 48 8795 15687
| 3 2 7 42 45 105 .06 | 26784 8040
mcc n/a| 1 -3 49 -86 150 -218 .76 317 317 | --- --- --- ---
| 16 12 36 123 200 866 .64 | --- ---
Table 1.1488.b GPS week : 1488 MJD: 54660.0-54666.0
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
------+------------------------------------+------------------------------------------
R04 | 19 28 29 32 26 23 16 |
R06 | 42 67 59 21 24 23 23 |
R07 | 41 37 35 25 25 24 28 |
R10 | 13 15 13 20 15 14 17 |
R11 | 26 13 19 30 20 24 25 |
R13 | 17 22 17 16 16 19 24 |
R14 | 11 19 13 17 13 13 15 |
R15 | 20 25 19 16 18 17 23 |
R17 | 21 25 28 53 31 21 31 |
R19 | 12 22 21 20 17 22 21 |
R20 | 30 17 13 15 18 17 22 |
R23 | 20 26 35 22 25 29 19 |
R24 | 26 32 29 38 16 20 26 |
Table 1.1488.c GPS week : 1488 MJD: 54660.0-54666.0
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 1488 0 | -320 181 551 -3313 -2054 -12240 97.5 5386 5386 | 765033 0
brd 1488 1 | ---- -8352 -1457 89090 -286800 -268300 239.2 >>>>> >>>>> | 754046 0
brd 1488 2 | 193 12 459 3991 -3030 1331 101.0 5339 5339 | 773702 0
brd 1488 3 | -227 -419 396 3043 -2380 -7287 98.1 5384 5384 | 781105 0
brd 1488 4 | -184 10 341 3997 -3694 -13320 96.2 3577 3577 | 746469 0
brd 1488 5 | -95 -89 392 -1090 -3712 -10340 98.9 6829 6829 | 809891 0
brd 1488 6 | 544 -168 583 755 3032 -13890 98.6 4805 4805 | 812175 0
-------------+------------------------------------------------------------+----------------
brd 1488 mean|-7947 -1260 181 13781 -42662 -46292 118.5 >>>>> >>>>> | 777488 0
brd 1488 sdev|20988 3132 727 33319 107679 98035 53.2 >>>>> >>>>> | 25649 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 2.1488.0 GPS week: 1488 Day: 0 MJD: 54660
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 66| 5 0 -9 -57 -75 185 -.29 39 33 | 0 -140 2571 2635
cod 216| -7 0 -4 -19 -17 43 -.07 38 29 | --- --- --- ---
esx 120| 0 0 1 138 131 -76 .56 62 45 | -26049 -729 6962 13329
iac n/a| 4 -1 16 -39 -30 -96 -.10 38 38 | 768180 -4054 6910 13972
mcc n/a| -4 -3 -1 -97 -34 615 .20 844 844 | --- --- --- ---
Table 2.1488.1 GPS week: 1488 Day: 1 MJD: 54661
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 66| 6 -3 -8 -11 3 269 -.27 55 39 | 0 -37 2580 2747
cod 216| -9 -3 4 97 -70 -6 -.20 42 26 | --- --- --- ---
esx 120| -2 1 2 45 -14 -88 .68 62 51 | -38260 7448 8182 16679
iac n/a| 8 7 8 -105 106 -285 -.10 53 53 | 753146 1001 8023 14812
mcc n/a| 5 -2 7 -112 293 -1366 .64 228 228 | --- --- --- ---
Table 2.1488.2 GPS week: 1488 Day: 2 MJD: 54662
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 66| -2 1 -1 1 0 156 -.11 54 35 | 0 3 2399 2517
cod 216| -1 -6 -6 -23 -35 -9 -.17 40 26 | --- --- --- ---
esx 120| 4 0 16 95 4 -222 .41 74 50 | -4259 -7694 6962 13006
iac n/a| 2 0 2 -30 2 -62 .00 39 39 | 777398 -6160 6998 12680
mcc n/a| -1 4 47 -123 45 -571 .98 95 95 | --- --- --- ---
Table 2.1488.3 GPS week: 1488 Day: 3 MJD: 54663
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 66| -4 -3 -11 -73 -18 -61 -.05 34 30 | 0 31 2488 2560
cod 216| 0 -2 -1 9 22 -2 -.04 31 27 | --- --- --- ---
esx 120| 2 2 8 145 -18 5 .27 97 48 | -6035 3342 5353 18212
iac n/a| 8 0 23 -90 33 58 -.08 78 78 | 779288 -26 5530 16772
mcc n/a| -1 -7 50 -165 -46 360 1.35 171 171 | --- --- --- ---
Table 2.1488.4 GPS week: 1488 Day: 4 MJD: 54664
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 66| 0 1 -13 21 21 5 -.09 33 31 | 0 -76 3356 3458
cod 216| -5 1 -5 -52 -20 109 -.12 26 24 | --- --- --- ---
esx 120| 5 5 12 0 9 187 .24 49 43 | -41915 20261 15854 22966
iac n/a| -1 3 12 -44 -14 -165 .07 38 38 | 741571 15643 15043 22338
mcc n/a| -1 -22 58 122 284 956 .93 289 289 | --- --- --- ---
Table 2.1488.5 GPS week: 1488 Day: 5 MJD: 54665
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 66| 1 -1 -11 -27 0 127 -.13 35 32 | 0 -367 3109 3274
cod 216| -6 1 0 17 -6 36 -.12 26 20 | --- --- --- ---
esx 120| 4 -1 14 129 -74 41 .50 59 57 | 31934 -8278 15148 18539
iac n/a| 5 0 5 -31 3 -143 -.00 34 34 | 812577 -8924 12559 15877
mcc n/a| -19 -6 93 23 475 -929 -.30 250 250 | --- --- --- ---
Table 2.1488.6 GPS week: 1488 Day: 6 MJD: 54666
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 66| 1 0 -4 -47 76 117 .04 33 30 | 0 -54 2522 2607
cod 216| -4 -2 -2 -64 -67 -62 -.14 31 25 | --- --- --- ---
esx 120| -1 4 2 130 -58 216 .37 79 59 | 24334 8728 6934 13745
iac n/a| 0 0 8 25 0 -154 -.00 35 35 | 810668 2859 6508 13359
mcc n/a| 34 17 90 -253 38 -597 1.50 341 341 | --- --- --- ---
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 3.1488.0 GPS week: 1488 Day: 0 MJD: 54660
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR04E | 7572 --- 26 30 23 --- 18 | --- 49 58 64 --- 59
R06E |10210 52 44 127 60 --- 41 | 169 172 143 197 --- 164
R07E | 7640 57 74 74 75 --- 40 | 53 69 62 46 --- 33
R10 | 4683 12 32 25 19 --- 13 | 37 42 37 44 --- 35
R11 | 2839 22 33 85 30 52 26 | 30 32 100 38 46 30
R13 | 1992 34 23 36 23 --- 16 | 35 36 47 25 --- 26
R14 | 2284 18 16 12 24 --- 10 | 46 39 56 51 --- 45
R15 | 3023 21 41 45 31 185 20 | 20 40 53 32 40 22
R17 | 5284 31 35 40 41 --- 21 | 41 48 77 38 --- 39
R19 | 985 26 17 18 22 --- 12 | 51 43 56 48 --- 45
R20 | 1593 69 19 80 27 --- 30 | 44 40 85 49 --- 43
R23 | 4665 23 41 49 24 --- 20 | 33 56 55 44 --- 38
R24 | 9162 56 43 45 32 1450 25 | 331 284 254 291 907 294
------+------------------------------------+--------------------------------
RMS | 5386 39 38 62 38 844 |T 74 73 83 74 331 67
WRMS | 5386 33 29 45 38 844 |NE 66 66 82 66 331 61
MEDI | 4665 26 33 45 27 185 |MD 41 43 58 46 46 39
Table 3.1488.1 GPS week: 1488 Day: 1 MJD: 54661
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR04E |>>>>> --- 34 46 42 --- 28 | --- 51 84 63 --- 55
R06E |>>>>> 156 96 112 84 --- 67 | 82 236 261 201 --- 176
R07E |40878 54 63 53 82 --- 36 | 30 70 67 87 --- 40
R10 |>>>>> 28 17 24 35 --- 15 | 38 56 50 65 --- 47
R11 |>>>>> 18 26 24 18 118 13 | 26 34 37 35 62 26
R13 |>>>>> 25 31 63 34 --- 22 | 26 39 77 21 --- 21
R14 |>>>>> 25 16 49 44 --- 19 | 46 40 78 40 --- 44
R15 |>>>>> 21 24 57 66 86 24 | 17 31 57 49 31 23
R17 |>>>>> 18 33 73 48 --- 25 | 37 35 118 27 --- 38
R19 |>>>>> 38 32 46 37 --- 21 | 41 43 57 57 --- 40
R20 |>>>>> 23 19 39 35 --- 16 | 38 45 49 33 --- 29
R23 |>>>>> 29 27 70 55 --- 26 | 49 42 47 76 --- 38
R24 |>>>>> 57 42 74 52 367 32 | 258 264 298 245 767 250
------+------------------------------------+--------------------------------
RMS |>>>>> 55 42 62 53 228 |T 57 75 98 76 286 63
WRMS |>>>>> 39 26 51 53 228 |NE 57 62 86 64 286 55
MEDI |>>>>> 25 31 53 44 118 |MD 38 43 67 57 62 40
Table 3.1488.2 GPS week: 1488 Day: 2 MJD: 54662
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 5945 68 33 53 45 --- 29 | 42 75 88 73 --- 72
R06E |12483 139 86 96 77 --- 59 | 188 256 279 265 --- 228
R07E | 3391 46 56 105 41 --- 34 | 40 82 100 52 --- 45
R10 | 1382 18 10 38 24 --- 12 | 27 33 42 38 --- 30
R11 | 6428 9 20 65 33 102 18 | 21 21 67 46 16 19
XR13 | 7932 28 18 --- 25 --- 17 | 35 29 --- 26 --- 26
R14 | 2946 23 15 30 21 --- 12 | 42 31 69 32 --- 37
R15 | 4038 15 21 69 25 87 18 | 19 33 59 32 22 22
R17 | 5846 45 22 90 38 --- 27 | 45 32 93 17 --- 29
R19 | 1213 42 29 36 38 --- 21 | 79 60 64 72 --- 66
R20 | 2196 17 19 46 13 --- 13 | 38 25 49 21 --- 23
R23 | 1482 26 58 118 41 --- 34 | 38 35 113 59 --- 35
XR24 | 6643 37 45 --- 41 137 29 | 267 272 --- 249 341 261
------+------------------------------------+--------------------------------
RMS | 5339 54 40 74 39 95 |T 67 75 93 75 126 68
WRMS | 5339 35 26 50 39 95 |NE 61 57 69 59 126 54
MEDI | 4038 28 22 65 38 102 |MD 40 33 69 46 22 35
Table 3.1488.3 GPS week: 1488 Day: 3 MJD: 54663
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2949 62 52 48 54 --- 31 | 25 87 70 69 --- 50
R06E | 9443 27 25 39 60 --- 20 | 124 121 158 170 --- 134
R07E | 1865 34 31 45 72 --- 24 | 37 70 84 79 --- 52
R10 | 1516 35 17 48 39 --- 19 | 57 48 57 51 --- 47
R11 |12489 27 26 88 74 121 30 | 38 37 107 63 28 31
R13 | 4399 16 23 33 40 --- 15 | 27 24 48 46 --- 24
R14 | 3505 27 19 35 41 --- 16 | 39 48 58 43 --- 40
R15 | 6295 12 26 36 37 124 15 | 18 25 48 60 28 24
R17 | 3962 49 55 128 160 --- 52 | 55 62 132 208 --- 71
R19 | 2144 15 20 286 56 --- 19 | 31 34 276 57 --- 26
R20 | 2364 14 17 33 43 --- 14 | 41 38 56 47 --- 37
R23 | 963 21 26 31 84 --- 22 | 30 41 91 58 --- 37
R24 | 4376 52 33 58 137 240 38 | 124 150 216 190 184 135
------+------------------------------------+--------------------------------
RMS | 5384 34 31 97 78 171 |T 49 60 107 87 80 54
WRMS | 5384 30 27 48 78 171 |NE 46 50 108 82 80 47
MEDI | 3505 27 26 45 56 124 |MD 38 48 84 60 28 40
Table 3.1488.4 GPS week: 1488 Day: 4 MJD: 54664
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2228 40 36 41 60 --- 26 | 28 48 50 55 --- 30
R06E | 5100 34 30 58 44 --- 23 | 105 102 150 128 --- 113
R07E | 1971 52 28 37 50 --- 24 | 82 62 63 51 --- 49
R10 | 1376 25 14 40 23 --- 14 | 32 50 82 47 --- 46
R11 | 1494 34 25 55 22 91 19 | 29 30 53 35 91 25
R13 | 7401 25 14 44 24 --- 15 | 18 44 65 21 --- 27
R14 | 2673 19 19 32 19 --- 12 | 25 35 58 36 --- 33
R15 | 6168 29 25 40 31 144 17 | 22 34 43 57 41 31
R17 | 1821 29 34 95 49 --- 30 | 35 40 107 57 --- 42
R19 | 2272 36 20 28 35 --- 17 | 57 69 105 60 --- 63
R20 | 1405 29 34 31 23 --- 17 | 41 52 42 34 --- 36
R23 | 3705 37 32 62 46 --- 25 | 26 51 61 40 --- 34
R24 | 1777 23 18 38 35 471 16 | 257 276 252 295 447 281
------+------------------------------------+--------------------------------
RMS | 3576 33 26 49 38 289 |T 58 68 87 70 193 62
WRMS | 3576 31 24 43 38 289 |NE 54 68 86 68 193 61
MEDI | 2228 29 25 40 35 144 |MD 32 50 63 51 91 36
Table 3.1488.5 GPS week: 1488 Day: 5 MJD: 54665
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |13373 32 42 50 34 --- 22 | 28 59 68 37 --- 38
R06E | 7357 35 32 47 46 --- 22 | 76 90 130 127 --- 98
R07E |10072 36 40 62 34 --- 24 | 61 71 60 45 --- 51
R10 | 5488 33 11 31 24 --- 14 | 52 73 84 78 --- 69
R11 | 2530 34 25 93 19 216 24 | 26 35 82 21 110 26
R13 | 9534 16 16 62 40 --- 19 | 21 34 110 31 --- 29
R14 | 5279 20 12 44 19 --- 13 | 29 24 45 22 --- 19
R15 | 5170 21 20 46 32 122 16 | 25 31 63 25 28 21
R17 | 3733 33 25 48 45 --- 21 | 21 22 73 46 --- 19
R19 | 4220 34 16 72 40 --- 22 | 37 50 99 55 --- 51
R20 | 3675 39 18 49 16 --- 16 | 51 52 52 47 --- 45
R23 | 3494 50 29 88 44 --- 28 | 35 33 75 26 --- 18
R24 | 5682 52 22 45 19 356 19 | 254 205 210 221 301 222
------+------------------------------------+--------------------------------
RMS | 6829 35 26 59 34 250 |T 55 59 88 60 146 54
WRMS | 6829 32 20 57 34 250 |NE 55 55 89 57 146 51
MEDI | 5279 34 22 49 34 216 |MD 35 50 75 45 110 38
Table 3.1488.6 GPS week: 1488 Day: 6 MJD: 54666
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 3565 21 26 38 26 --- 15 | 38 57 82 67 --- 56
R06E | 4858 38 26 59 39 --- 22 | 86 102 119 101 --- 95
R07E | 5469 43 51 55 43 --- 27 | 72 70 54 64 --- 60
R10 | 2328 16 20 34 42 --- 16 | 52 46 51 71 --- 50
R11 | 8131 28 27 86 33 165 24 | 44 43 91 55 53 45
R13 | 2147 40 18 186 40 --- 24 | 26 31 126 32 --- 23
R14 | 2775 14 23 38 29 --- 14 | 20 25 48 30 --- 23
R15 | 6399 34 30 71 33 177 23 | 15 46 63 32 29 31
R17 | 9729 26 32 112 44 --- 30 | 28 40 127 47 --- 34
R19 | 2375 24 25 63 36 --- 20 | 55 61 71 69 --- 56
R20 | 1790 44 30 54 27 --- 22 | 60 74 55 62 --- 57
R23 | 1462 31 24 40 35 --- 18 | 27 50 50 40 --- 32
R24 | 1865 51 53 44 23 538 26 | 320 328 285 326 281 321
------+------------------------------------+--------------------------------
RMS | 4805 33 31 79 35 341 |T 64 74 94 76 121 67
WRMS | 4805 30 25 59 35 341 |NE 64 74 96 76 121 67
MEDI | 2775 31 26 55 35 177 |MD 44 50 71 62 53 50
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