[IGSREPORT-15974] Wk 1465 IGLOS Final Orbits [Resubmission]
Jim Ray
IGS.ACC at noaa.gov
Fri Feb 22 09:00:11 PST 2008
******************************************************************************
IGS Electronic Report 22 Feb 09:00:19 PST 2008 Message Number 15974
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1465 (Feb 03, 2008 - Feb 09, 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 2.1465.
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:
igl1465[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1465 in the SP3 format.
igl14657.sum Combination Report for GPS Week 1465.
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 | 1239.7 ns
1 | 1275.1 ns
2 | 1229.0 ns
3 | 1265.3 ns
4 | 1248.1 ns
5 | 1294.6 ns
6 | 1248.3 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 | BKG | R07 R08
1 | ESX | R08
3 | ESX | R11
3 | IAC | R10 R24
4 | IAC | R08 R10 R15 R24
5 | ESX | R13
5 | IAC | 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 1.1465, 1a.1465).
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 2.1465.0-6)
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 3.1465.0-6).
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 1465 summary. (Feb 03, 2008 - Feb 09, 2008)
Table 1.1465.a GPS week : 1465 MJD: 54499.0-54505.0
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 65| 0 0 8 -24 50 -14 -.11 55 34 | 0 100 2508 2600
| 4 3 5 17 32 98 .07 | 0 178
cod 170| -3 -1 0 17 -15 36 -.12 36 27 | --- --- --- ---
| 2 3 2 53 56 67 .03 | --- ---
esx 114| 5 -1 0 36 -3 -62 .45 111 52 | -39267 2363 7949 19872
| 2 5 6 41 65 66 .14 | 26101 3419
iac n/a| 0 0 -12 -8 -5 -4 .09 96 96 | 1255972 601 7404 15396
| 2 3 4 44 22 164 .09 | 23345 2354
mcc n/a| -24 -4 -68 -469 -619 -5621 1.73 610 610 | --- --- --- ---
| 71 33 109 817 1846 5037 2.97 | --- ---
Table 1.1465.b GPS week : 1465 MJD: 54499.0-54505.0
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 | 18 18 21 29 37 17 19 |
R04 | 18 20 23 17 13 26 17 |
R06 | 24 18 22 19 19 16 16 |
R07 | 15 --- --- --- --- --- --- |
R08 | 50 66 47 138 86 23 35 |
R09 | 21 23 28 28 27 26 31 |
R10 | 15 22 16 21 22 14 16 |
R11 | 22 21 23 19 31 35 16 |
R13 | --- --- 0 1194 114 49 27 |
R14 | 26 18 16 16 22 15 16 |
R15 | 28 23 23 25 26 22 20 |
R17 | 24 28 33 35 31 19 20 |
R19 | 30 24 21 24 24 36 38 |
R20 | 26 23 17 11 19 23 17 |
R23 | 29 19 26 31 33 21 13 |
R24 | 27 36 26 19 23 58 --- |
Table 1.1465.c GPS week : 1465 MJD: 54499.0-54505.0
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 1465 0 | 51 -125 172 -2673 -2431 -4852 96.6 6903 6903 | 1239724 0
brd 1465 1 | 294 -34 308 834 -1914 -6950 96.4 7281 7281 | 1275143 0
brd 1465 2 | -132 207 226 -2857 -3829 -21810 100.3 5295 5295 | 1229005 0
brd 1465 3 | -452 42 -14 -1549 -7507 -21710 99.6 6786 6786 | 1265321 0
brd 1465 4 | -187 21 -58 -6017 -4209 -19940 88.9 7614 7614 | 1248049 0
brd 1465 5 | 130 -220 187 800 -407 -24160 95.1 8013 8013 | 1294553 0
brd 1465 6 | 399 67 -1 -872 1645 -11230 95.7 8192 8192 | 1248300 0
-------------+------------------------------------------------------------+----------------
brd 1465 mean| 14 -6 117 -1761 -2664 -15807 96.1 7154 7154 | 1257156 0
brd 1465 sdev| 294 138 140 2390 2928 7928 3.7 974 974 | 22533 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 2.1465.0 GPS week: 1465 Day: 0 MJD: 54499
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 65| 8 0 8 -33 55 -20 -.06 105 42 | 0 -214 2507 2580
cod 170| -4 1 4 60 -38 56 -.15 27 26 | --- --- --- ---
esx 114| 8 0 -2 9 77 -171 .49 66 49 | -62953 -265 6507 21363
iac n/a| 2 0 -14 -33 42 20 .02 48 48 | 1237115 1225 6441 17402
mcc n/a| 8 4 -6 168 205 -1224 1.54 207 207 | --- --- --- ---
Table 2.1465.1 GPS week: 1465 Day: 1 MJD: 54500
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 65| -1 -5 2 -6 23 -173 -.18 49 34 | 0 113 2488 2591
cod 170| -7 2 -1 87 6 27 -.13 38 36 | --- --- --- ---
esx 114| 6 0 3 65 -24 0 .51 106 45 | -27575 6460 7018 16711
iac n/a| 1 -3 -9 -19 -8 158 .10 46 46 | 1274295 3002 6775 12773
mcc n/a| 20 -8 21 63 161 -545 1.14 161 161 | --- --- --- ---
Table 2.1465.2 GPS week: 1465 Day: 2 MJD: 54501
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 65| 4 -2 3 -7 27 -106 -.19 36 27 | 0 318 2503 2582
cod 170| -4 1 0 44 76 117 -.14 29 28 | --- --- --- ---
esx 114| 7 -6 6 -37 -1 -39 .44 75 49 | -74632 3331 7657 18502
iac n/a| 0 -2 -20 9 -12 29 .21 47 47 | 1228256 1903 6406 16241
mcc n/a| -121 28 48 -276 -1660 ---- 6.01 1074 1074 | --- --- --- ---
Table 2.1465.3 GPS week: 1465 Day: 3 MJD: 54502
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 65| -2 4 5 -44 74 102 -.16 41 32 | 0 47 2414 2517
cod 170| -2 -2 -1 16 0 109 -.10 62 27 | --- --- --- ---
esx 114| 7 3 -8 37 -23 -105 .63 122 58 | -30193 -278 9208 19537
iac n/a| 4 3 -13 78 -2 -334 .17 199 199 | 1266490 -1427 8826 15284
mcc n/a| -132 27 -193 -1698 -3386 -6939 1.48 704 704 | --- --- --- ---
Table 2.1465.4 GPS week: 1465 Day: 4 MJD: 54503
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 65| -2 4 7 -35 80 11 -.10 75 38 | 0 230 2380 2460
cod 170| -1 -6 0 0 -74 39 -.09 40 27 | --- --- --- ---
esx 114| 0 -9 7 35 -110 -84 .35 110 59 | -50449 7497 8831 19702
iac n/a| -1 5 -6 -62 -18 -62 .11 247 247 | 1244646 3402 7061 13493
mcc n/a| 0 0 0 0 0 0 .0 692 692 | --- --- --- ---
Table 2.1465.5 GPS week: 1465 Day: 5 MJD: 54504
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 65| 1 2 13 -39 88 82 -.01 37 34 | 0 -7 2521 2616
cod 170| -1 -3 -1 -76 -89 -41 -.13 34 27 | --- --- --- ---
esx 114| 3 -6 1 49 80 -64 .21 210 47 | 4288 -313 9676 19587
iac n/a| -3 1 -12 -29 -27 141 .02 50 50 | 1294476 -2422 9819 14321
mcc n/a| 40 -17 -133 -1598 2268 -8845 -2.90 683 683 | --- --- --- ---
Table 2.1465.6 GPS week: 1465 Day: 6 MJD: 54505
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 65| -1 1 16 -2 4 0 -.04 40 34 | 0 215 2748 2857
cod 170| -2 -3 2 -7 9 -55 -.08 20 18 | --- --- --- ---
esx 114| 8 5 -8 91 -19 25 .54 88 58 | -33356 115 6749 23703
iac n/a| 0 -1 -13 0 -8 17 -.03 34 34 | 1246526 -1476 6505 18258
mcc n/a| 15 -69 -214 55 -1928 -8926 4.83 752 752 | --- --- --- ---
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 3.1465.0 GPS week: 1465 Day: 0 MJD: 54499
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |14563 31 16 39 40 --- 17 | 27 40 58 46 --- 36
R04 | 4728 19 24 53 26 --- 17 | 125 119 129 117 --- 121
R06 | 3204 54 35 24 46 --- 24 | 65 49 44 56 --- 44
XR07 | 4208 4935 10 --- 20 --- 14 | 2 71 --- 1 --- 71
R08 | 7684 365 28 117 75 --- 49 | 231 128 160 121 --- 113
R09 | 9418 29 29 63 18 --- 20 | 28 52 75 45 --- 42
R10 | 2190 30 16 26 34 --- 15 | 39 34 36 56 --- 32
R11 | 6443 36 14 71 34 --- 22 | 28 57 111 47 --- 50
R14 | 2258 44 21 71 51 --- 26 | 23 27 70 39 --- 20
R15 | 8178 42 24 91 41 207 28 | 47 23 92 60 281 27
R17 | 6253 33 18 86 30 --- 24 | 33 57 89 60 --- 52
R19 | 1987 81 36 35 46 --- 30 | 55 59 41 63 --- 45
R20 | 1172 47 45 43 41 --- 25 | 36 35 52 51 --- 36
R23 | 2925 29 26 79 69 --- 29 | 50 39 74 58 --- 39
R24 |10165 34 25 49 75 --- 26 | 144 155 159 126 --- 141
------+------------------------------------+--------------------------------
RMS | 6902 105 27 66 48 207 |T 62 63 85 63 281 57
WRMS | 6902 42 26 49 48 207 |NE 62 63 85 63 281 57
MEDI | 4728 36 24 53 41 207 |MD 39 52 74 56 281 44
Table 3.1465.1 GPS week: 1465 Day: 1 MJD: 54500
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |11107 28 30 34 27 --- 17 | 31 40 55 40 --- 32
R04 | 5377 30 37 29 41 --- 20 | 124 119 116 121 --- 118
R06 | 2834 23 32 25 39 --- 17 | 34 41 33 63 --- 35
R08 | 8090 124 66 363 75 --- 65 | 117 129 333 155 --- 108
R09 |12713 33 24 62 34 --- 23 | 21 39 81 51 --- 37
R10 | 1280 48 17 33 47 --- 21 | 18 45 55 48 --- 32
R11 | 3851 28 30 41 43 --- 20 | 17 47 58 36 --- 27
R14 | 1650 31 26 28 40 --- 18 | 39 37 34 37 --- 23
R15 |14067 34 21 61 36 161 22 | 51 55 63 56 509 41
R17 | 7929 31 32 69 58 --- 28 | 37 63 92 74 --- 52
R19 | 1087 35 31 48 50 --- 23 | 47 45 61 47 --- 35
R20 | 2209 22 46 27 52 --- 22 | 32 23 30 44 --- 24
R23 | 1934 32 19 27 48 --- 18 | 49 40 52 42 --- 39
R24 | 8062 75 69 49 37 --- 35 | 140 146 166 159 --- 144
------+------------------------------------+--------------------------------
RMS | 7281 49 38 106 46 161 |T 54 62 87 69 509 53
WRMS | 7281 34 36 45 46 161 |NE 54 62 87 69 509 53
MEDI | 3851 31 30 34 41 161 |MD 37 45 58 48 509 35
Table 3.1465.2 GPS week: 1465 Day: 2 MJD: 54501
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5094 31 24 51 47 --- 21 | 46 69 91 77 --- 59
R04 | 3431 43 21 42 56 --- 23 | 95 76 94 79 --- 80
R06 | 2711 34 37 46 35 --- 21 | 49 43 52 49 --- 36
R08 | 6459 74 40 170 42 --- 47 | 136 151 142 170 --- 128
R09 |10362 31 21 100 52 --- 28 | 55 86 160 58 --- 78
R10 | 2198 21 20 39 36 --- 16 | 30 31 35 102 --- 26
R11 | 4757 19 27 60 56 --- 22 | 31 35 89 52 --- 39
XR13 |17331 --- 9 --- --- --- 0 | --- 122 --- --- --- 235
R14 | 1481 32 25 27 20 --- 15 | 10 50 69 30 --- 33
R15 | 8546 18 29 38 70 1073 23 | 35 45 65 86 635 48
R17 | 6110 32 30 103 71 --- 32 | 30 53 77 89 --- 40
R19 | 1413 35 27 61 22 --- 20 | 80 52 100 55 --- 57
R20 | 3092 26 23 28 43 --- 17 | 22 38 47 36 --- 28
R23 | 2621 21 37 86 38 --- 25 | 40 40 91 57 --- 35
R24 | 6315 47 36 66 39 --- 26 | 96 101 133 111 --- 100
------+------------------------------------+--------------------------------
RMS | 5295 36 29 75 47 1073 |T 53 66 88 75 635 68
WRMS | 5295 27 28 49 47 1073 |NE 53 66 88 75 635 68
MEDI | 4757 31 27 51 42 1073 |MD 40 52 89 58 635 48
Table 3.1465.3 GPS week: 1465 Day: 3 MJD: 54502
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4949 42 32 57 85 --- 29 | 43 69 72 120 --- 54
R04 | 5725 26 22 28 45 --- 16 | 117 130 118 122 --- 122
R06 | 2457 25 34 37 41 --- 19 | 54 54 46 62 --- 46
R08 | 6816 105 212 240 464 --- 138 | 205 243 197 534 --- 187
R09 |14722 26 33 99 36 --- 28 | 28 37 79 32 --- 31
R10 | 3525 21 22 50 502 --- 20 | 29 39 70 410 --- 37
R11 | 8183 21 27 318 38 --- 19 | 34 47 275 40 --- 37
XR13 | ---- --- 758 --- 1875 --- 1193 | --- 164 --- 699 --- 350
R14 | 3186 23 19 47 20 --- 16 | 28 47 50 48 --- 36
R15 | 7920 39 23 72 45 704 25 | 43 38 69 58 353 25
R17 |11691 40 14 113 80 --- 34 | 30 47 125 81 --- 48
R19 | 1435 25 21 81 40 --- 23 | 56 46 61 50 --- 38
R20 | 3865 18 14 17 25 --- 10 | 23 41 41 34 --- 28
R23 | 2534 52 48 63 55 --- 30 | 45 56 91 59 --- 37
R24 | 2400 25 20 34 242 --- 18 | 69 41 56 240 --- 53
------+------------------------------------+--------------------------------
RMS | 6786 41 62 122 199 704 |T 57 73 96 172 353 75
WRMS | 6786 32 27 58 199 704 |NE 57 73 96 172 353 75
MEDI | 3865 25 23 57 45 704 |MD 43 47 70 62 353 38
Table 3.1465.4 GPS week: 1465 Day: 4 MJD: 54503
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4335 54 24 35 132 --- 36 | 49 46 75 162 --- 60
R04 | 2966 15 12 32 36 --- 12 | 84 87 104 76 --- 84
R06 | 2064 27 22 38 54 --- 19 | 30 53 48 48 --- 43
R08 | 7922 133 97 159 769 --- 86 | 143 177 126 582 --- 132
R09 |13184 25 21 101 42 --- 26 | 58 52 82 48 --- 47
R10 | 2589 20 21 59 255 --- 22 | 14 34 51 240 --- 22
R11 | 9747 25 40 97 58 --- 30 | 28 52 90 31 --- 27
R13 |18753 227 75 327 208 --- 113 | 105 160 432 767 --- 277
R14 | 2710 21 18 79 41 --- 22 | 14 17 60 38 --- 16
R15 | 4461 48 17 53 309 692 26 | 25 50 79 268 700 41
R17 |10287 40 34 74 82 --- 30 | 24 68 87 72 --- 44
R19 | 1199 28 22 46 75 --- 23 | 28 35 51 55 --- 20
R20 | 2316 24 28 41 42 --- 18 | 28 42 60 65 --- 36
R23 | 2193 61 41 57 77 --- 32 | 63 67 43 80 --- 49
R24 | 1759 36 29 36 272 --- 23 | 49 49 74 266 --- 49
------+------------------------------------+--------------------------------
RMS | 7614 75 40 110 247 692 |T 49 65 97 186 700 63
WRMS | 7614 38 27 59 247 692 |NE 49 65 97 186 700 63
MEDI | 2966 28 24 57 77 692 |MD 30 52 75 76 700 44
Table 3.1465.5 GPS week: 1465 Day: 5 MJD: 54504
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6058 24 13 50 29 --- 16 | 49 64 93 83 --- 64
R04 | 2237 33 20 51 73 --- 25 | 58 49 43 72 --- 46
R06 | 2279 17 26 29 37 --- 15 | 31 48 38 52 --- 35
R08 | 9617 23 27 45 64 --- 22 | 169 157 121 311 --- 148
R09 |11169 39 38 68 40 --- 26 | 33 61 89 38 --- 40
R10 | 1600 19 17 27 37 --- 14 | 24 17 43 60 --- 21
R11 | 9415 51 42 101 46 --- 34 | 13 57 136 22 --- 33
R13 |14676 81 62 760 58 --- 48 | 79 207 611 338 --- 193
R14 | 1800 24 12 36 36 --- 15 | 18 23 53 52 --- 27
R15 |12853 28 30 42 55 683 22 | 22 22 69 68 321 33
R17 |12258 32 24 45 35 --- 19 | 29 40 60 42 --- 32
R19 | 1031 40 56 79 80 --- 35 | 34 50 87 84 --- 29
R20 | 1225 38 30 59 29 --- 22 | 25 25 61 20 --- 19
R23 | 2624 21 40 37 46 --- 21 | 39 47 58 66 --- 44
XR24 |13403 56 60 --- 341 --- 58 | 61 88 --- 341 --- 67
------+------------------------------------+--------------------------------
RMS | 8013 37 34 210 50 683 |T 45 63 111 109 321 55
WRMS | 8013 34 27 47 50 683 |NE 45 63 111 109 321 55
MEDI | 6058 32 30 45 46 683 |MD 33 49 61 66 321 35
Table 3.1465.6 GPS week: 1465 Day: 6 MJD: 54505
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8039 26 14 76 31 --- 18 | 36 49 76 37 --- 41
R04 | 4124 35 17 36 37 --- 17 | 44 55 42 59 --- 48
R06 | 3370 29 16 46 29 --- 15 | 37 54 55 58 --- 48
R08 | 9875 87 13 139 28 --- 34 | 150 165 183 193 --- 153
R09 |11923 32 27 130 51 --- 30 | 27 48 139 39 --- 42
R10 | 1997 21 20 68 12 --- 15 | 34 38 56 41 --- 34
R11 | 8246 41 15 31 25 --- 15 | 15 35 47 25 --- 24
R13 |13954 34 27 103 46 --- 26 | 159 193 162 326 --- 143
R14 | 1220 24 23 47 27 --- 16 | 17 32 66 23 --- 25
R15 |15473 34 17 58 45 752 20 | 30 33 60 60 312 32
R17 | 9373 44 20 54 37 --- 20 | 29 35 64 65 --- 33
R19 | 1170 41 34 188 21 --- 37 | 68 60 104 85 --- 65
R20 | 1079 44 13 37 32 --- 17 | 21 27 26 48 --- 23
R23 | 2985 20 15 32 28 --- 12 | 74 73 75 83 --- 74
------+------------------------------------+--------------------------------
RMS | 8192 40 20 88 34 752 |T 52 64 82 81 312 56
WRMS | 8192 34 18 58 34 752 |NE 52 64 82 81 312 56
MEDI | 4124 34 17 54 29 752 |MD 34 48 64 58 312 41
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