[IGSREPORT-16147] Wk 1473 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 17 06:25:08 PDT 2008
******************************************************************************
IGS Electronic Report 17 Apr 06:25:11 PDT 2008 Message Number 16147
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1473 (Mar 30, 2008 - Apr 05, 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 2.1473.
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:
igl1473[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1473 in the SP3 format.
igl14737.sum Combination Report for GPS Week 1473.
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 | 1065.3 ns
1 | 1122.5 ns
2 | 1132.6 ns
3 | 1076.4 ns
4 | 1101.7 ns
5 | 1081.0 ns
6 | 1069.6 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 | R11
2 | ESX | R09 R11 R24
3 | ESX | R14
4 | ESX | R08 R11 R15
5 | ESX | R11
6 | ESX | R08 R11
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 1.1473, 1a.1473).
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 2.1473.0-6)
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 3.1473.0-6).
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 1473 summary. (Mar 30, 2008 - Apr 05, 2008)
Table 1.1473.a GPS week : 1473 MJD: 54555.0-54561.0
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 70| 1 0 2 2 1 50 -.08 38 31 | 0 124 2515 2586
| 3 2 8 40 22 110 .05 | 0 210
cod 173| -1 0 -5 -1 13 -18 -.07 26 20 | --- --- --- ---
| 1 3 1 39 25 40 .07 | --- ---
esx 109| -3 0 -8 19 -27 27 .49 102 58 | -29964 289 8539 24316
| 6 5 10 71 60 80 .12 | 29573 6468
iac n/a| 2 0 13 2 -6 -77 -.01 70 70 | 1093174 582 11128 26087
| 1 4 10 33 34 85 .09 | 30394 7601
mcc n/a| -5 3 21 -42 -24 890 .59 294 294 | --- --- --- ---
| 20 19 15 205 165 1834 .44 | --- ---
Table 1.1473.b GPS week : 1473 MJD: 54555.0-54561.0
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 | 20 15 32 19 16 28 24 |
R04 | 14 19 32 15 18 10 13 |
R06 | 18 21 18 25 16 15 14 |
R07 | 9 9 15 12 11 15 104 |
R08 | 26 33 33 31 35 23 24 |
R09 | 23 18 22 23 27 21 20 |
R10 | 13 17 14 10 14 18 22 |
R11 | 17 23 18 23 19 27 26 |
R13 | 29 17 24 30 27 21 34 |
R14 | 12 11 19 26 14 10 19 |
R15 | 24 21 19 18 13 27 28 |
R17 | 27 26 15 15 15 22 21 |
R19 | 20 19 19 15 12 13 22 |
R20 | 21 23 25 23 16 12 22 |
R23 | 30 20 26 26 28 24 40 |
R24 | 21 20 24 --- --- --- --- |
Table 1.1473.c GPS week : 1473 MJD: 54555.0-54561.0
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 1473 0 | 187 145 481 -1491 5250 -34880 93.4 6545 6545 | 1065294 0
brd 1473 1 | -191 -56 2 183 303 -35200 120.8 >>>>> >>>>> | 1122538 0
brd 1473 2 | -413 -80 3 -1962 -3788 -31940 102.2 7704 7704 | 1132608 0
brd 1473 3 | -204 -265 358 -40 -3849 -25880 90.8 6889 6889 | 1076409 0
brd 1473 4 | 1 -1 91 -5003 2670 -30900 86.3 7395 7395 | 1101732 0
brd 1473 5 | -86 144 201 -1434 1361 -24180 90.4 6233 6233 | 1080988 0
brd 1473 6 | 288 -383 211 1366 -5506 -24090 95.5 7961 7961 | 1069634 0
-------------+------------------------------------------------------------+----------------
brd 1473 mean| -59 -70 192 -1197 -508 -29581 97.1 >>>>> >>>>> | 1092743 0
brd 1473 sdev| 241 197 179 2042 3964 4830 11.6 >>>>> >>>>> | 26615 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 2.1473.0 GPS week: 1473 Day: 0 MJD: 54555
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 70| -1 -2 -2 -4 13 184 -.11 35 32 | 0 435 2167 2227
cod 173| -3 0 -6 -41 26 -65 -.13 23 19 | --- --- --- ---
esx 109| 4 6 6 138 -19 -69 .37 88 44 | -71888 7649 6439 20342
iac n/a| 1 0 10 -5 -31 -148 .03 42 42 | 1063583 2655 6141 15467
mcc n/a| 0 -3 24 -283 139 339 .37 568 568 | --- --- --- ---
Table 2.1473.1 GPS week: 1473 Day: 1 MJD: 54556
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 70| 2 0 7 77 34 47 -.13 31 30 | 0 223 2522 2577
cod 173| -1 0 -5 -47 -11 -32 -.10 21 20 | --- --- --- ---
esx 109| 0 2 -10 59 14 -16 .42 62 37 | -3190 7695 7866 30735
iac n/a| 1 -1 3 -8 -10 -12 .06 36 36 | 1135994 14620 26072 80042
mcc n/a| 19 19 31 -251 -34 841 1.32 620 620 | --- --- --- ---
Table 2.1473.2 GPS week: 1473 Day: 2 MJD: 54557
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 70| -2 2 18 -10 -11 186 -.12 34 30 | 0 169 2438 2509
cod 173| 0 -4 -7 -10 -11 -33 -.04 24 22 | --- --- --- ---
esx 109| 0 6 -25 24 48 -80 .59 167 88 | 13327 -4318 6762 20490
iac n/a| 2 6 3 60 7 -94 .02 39 39 | 1133462 -2971 6175 15641
mcc n/a| 1 18 32 -134 -192 294 .32 250 250 | --- --- --- ---
Table 2.1473.3 GPS week: 1473 Day: 3 MJD: 54558
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 70| 0 2 -1 5 -4 -98 -.01 31 28 | 0 154 2254 2320
cod 173| 1 -3 -2 47 35 1 .05 26 23 | --- --- --- ---
esx 109| -1 -2 1 -99 -62 81 .43 65 48 | -36116 -5171 7761 21728
iac n/a| 0 2 11 -31 -4 65 -.19 42 42 | 1077476 -2741 7758 14859
mcc n/a| 0 16 32 133 -1 1458 -.04 114 114 | --- --- --- ---
Table 2.1473.4 GPS week: 1473 Day: 4 MJD: 54559
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 70| 1 -2 0 -50 -12 -37 -.08 27 23 | 0 -39 2252 2338
cod 173| 0 3 -3 55 55 -31 -.15 24 22 | --- --- --- ---
esx 109| -7 -5 -15 -15 -135 74 .68 135 61 | -15751 -8538 8232 29787
iac n/a| 2 1 19 -6 29 -45 -.01 39 39 | 1098368 -7368 8530 24065
mcc n/a| -3 15 0 -39 172 2974 .51 110 110 | --- --- --- ---
Table 2.1473.5 GPS week: 1473 Day: 5 MJD: 54560
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 70| 2 0 1 -24 22 -21 -.08 32 31 | 0 -234 3264 3360
cod 173| -1 3 -5 1 -2 61 -.07 19 15 | --- --- --- ---
esx 109| -8 -7 -5 19 -45 110 .54 82 53 | -46671 3863 15411 27638
iac n/a| 1 1 9 -24 29 -133 -.05 39 39 | 1074165 5310 15863 22662
mcc n/a| -48 -28 -1 -15 26 2790 .84 135 135 | --- --- --- ---
Table 2.1473.6 GPS week: 1473 Day: 6 MJD: 54561
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 70| 7 -2 -5 21 -31 93 -.02 78 44 | 0 166 2714 2775
cod 173| -3 2 -4 -12 4 -26 -.08 47 19 | --- --- --- ---
esx 109| -15 -4 -11 12 10 92 .40 115 76 | -49460 848 7305 19494
iac n/a| 6 -8 34 35 -67 -173 .05 253 253 | 1069176 -5426 7361 9878
mcc n/a| -3 -16 31 291 -284 -2464 .84 263 263 | --- --- --- ---
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 3.1473.0 GPS week: 1473 Day: 0 MJD: 54555
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7461 40 11 63 23 --- 20 | 41 37 67 50 --- 35
R04 | 2065 25 23 25 27 --- 14 | 28 31 58 34 --- 30
R06 | 4473 32 30 29 33 --- 18 | 31 58 32 42 --- 38
R07 | 6035 9 11 28 11 155 8 | 48 38 29 40 61 34
R08 | 5279 51 27 80 26 --- 26 | 74 58 66 34 --- 43
R09 |12065 33 21 70 42 --- 23 | 31 21 79 34 --- 20
R10 | 3125 21 11 29 33 --- 13 | 23 17 37 36 --- 15
R11 | 4755 29 15 274 27 --- 16 | 39 29 183 40 --- 31
R13 | 9484 56 43 70 26 --- 28 | 88 136 136 116 --- 112
R14 | 3455 23 12 25 23 --- 11 | 63 60 93 78 --- 65
R15 | 7286 29 25 75 45 118 24 | 65 68 75 65 61 65
R17E |11964 49 22 48 70 --- 27 | 48 47 94 100 --- 58
XR19E | 2473 27 23 --- 36 --- 20 | 65 54 --- 47 --- 51
R20E | 3507 28 16 62 44 --- 21 | 54 60 89 73 --- 60
R23E | 1822 39 33 38 87 --- 29 | 61 64 70 121 --- 63
R24E | 2558 26 21 56 47 964 20 | 32 22 54 27 9999 27
------+------------------------------------+--------------------------------
RMS | 6544 35 23 87 42 568 |T 49 50 77 58 61 46
WRMS | 6544 32 19 44 42 568 |NE 48 50 77 51 61 44
MEDI | 4473 29 21 56 33 155 |MD 48 47 70 42 61 38
Table 3.1473.1 GPS week: 1473 Day: 1 MJD: 54556
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 13 20 51 23 --- 14 | 27 31 56 40 --- 30
R04 |>>>>> 22 19 52 43 --- 18 | 32 49 95 71 --- 46
R06 |>>>>> 39 25 58 35 --- 21 | 21 51 63 36 --- 33
R07 |>>>>> 18 11 20 14 135 8 | 45 23 38 26 68 20
R08 |>>>>> 58 27 119 35 --- 32 | 45 38 113 29 --- 25
R09 |10080 35 14 54 32 --- 18 | 22 28 83 35 --- 24
R10 |>>>>> 37 21 33 31 --- 17 | 37 16 43 37 --- 20
R11 |>>>>> 39 20 78 31 --- 22 | 41 29 127 24 --- 21
R13 |12014 34 22 44 24 --- 17 | 113 102 101 99 --- 100
R14 |>>>>> 14 12 27 26 --- 10 | 57 71 111 93 --- 72
R15 |>>>>> 18 20 77 38 171 20 | 61 74 59 54 123 62
R17E | 9181 30 10 83 61 --- 25 | 36 42 89 72 --- 43
R19E |>>>>> 25 30 35 41 --- 18 | 34 58 48 39 --- 37
R20E |>>>>> 23 29 86 29 --- 23 | 44 55 73 59 --- 47
R23E |>>>>> 41 24 33 39 --- 19 | 50 47 82 107 --- 52
R24E |>>>>> 24 16 60 50 1052 20 | 22 26 78 25 9999 19
------+------------------------------------+--------------------------------
RMS |>>>>> 31 21 62 36 620 |T 42 46 78 52 95 40
WRMS |>>>>> 30 20 37 36 620 |NE 45 46 80 49 95 41
MEDI |>>>>> 25 20 52 32 171 |MD 37 42 78 39 68 33
Table 3.1473.2 GPS week: 1473 Day: 2 MJD: 54557
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6698 20 10 164 48 --- 32 | 38 43 136 50 --- 37
R04 | 3322 32 11 163 35 --- 31 | 27 31 109 37 --- 28
R06 | 4343 34 18 37 42 --- 18 | 27 58 62 75 --- 47
R07 | 1785 21 8 60 32 138 15 | 37 40 53 55 53 30
R08 | 7382 77 39 87 33 --- 32 | 72 42 121 29 --- 40
R09 |12978 30 29 354 32 --- 21 | 19 38 315 29 --- 19
R10 | 4003 20 12 56 19 --- 13 | 21 25 68 30 --- 23
R11 |14185 21 23 264 33 --- 18 | 32 46 252 51 --- 34
R13 |14195 30 37 66 45 --- 23 | 52 80 84 59 --- 59
R14 | 5045 33 18 73 28 --- 19 | 36 64 69 64 --- 54
R15 | 5800 23 26 50 45 89 19 | 45 58 98 47 84 46
R17E | 7295 18 16 52 34 --- 15 | 30 38 59 48 --- 30
R19E | 2216 30 16 77 30 --- 19 | 50 54 89 59 --- 51
R20E | 1542 39 37 68 46 --- 25 | 39 66 103 70 --- 56
R23E | 5983 39 18 85 56 --- 25 | 55 44 91 68 --- 52
R24E | 8632 32 25 384 48 401 24 | 23 38 144 30 9999 29
------+------------------------------------+--------------------------------
RMS | 7704 34 24 167 39 250 |T 37 47 115 50 68 39
WRMS | 7704 30 22 88 39 250 |NE 36 47 124 47 68 37
MEDI | 5800 30 18 73 34 138 |MD 36 43 91 50 53 37
Table 3.1473.3 GPS week: 1473 Day: 3 MJD: 54558
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7240 28 20 62 25 --- 19 | 28 35 126 47 --- 39
R04 | 4620 27 10 29 33 --- 14 | 52 48 35 71 --- 49
R06 | 3903 30 26 67 54 --- 24 | 39 74 73 94 --- 60
R07 | 3374 14 14 28 25 104 11 | 48 41 40 30 67 28
R08 | 6789 50 42 80 52 --- 31 | 56 55 90 32 --- 39
R09 |12387 28 33 70 35 --- 23 | 22 41 72 39 --- 29
R10 | 2944 13 16 26 17 --- 10 | 17 27 34 22 --- 16
R11 | 7534 24 34 64 42 --- 23 | 34 34 82 66 --- 42
R13 |13366 40 34 72 69 --- 30 | 97 111 125 100 --- 97
R14 | 4109 32 14 145 56 --- 25 | 56 65 154 101 --- 69
R15 | 5520 32 28 36 24 122 17 | 87 124 108 112 63 109
R17 | 8797 31 20 26 28 --- 15 | 53 41 48 39 --- 39
R19E | 2181 25 16 28 36 --- 15 | 34 51 51 71 --- 46
R20E | 1653 37 33 48 44 --- 23 | 72 89 70 84 --- 73
R23E | 5966 32 30 76 47 --- 25 | 55 62 95 84 --- 53
------+------------------------------------+--------------------------------
RMS | 6889 31 26 65 42 113 |T 50 59 80 66 65 52
WRMS | 6889 28 23 48 42 113 |NE 48 59 85 64 65 52
MEDI | 5520 30 26 62 36 104 |MD 52 51 73 71 63 46
Table 3.1473.4 GPS week: 1473 Day: 4 MJD: 54559
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5249 10 20 52 33 --- 16 | 43 47 54 64 --- 44
R04 | 6137 19 22 55 34 --- 17 | 25 32 69 53 --- 30
R06 | 4932 23 24 32 37 --- 16 | 30 44 37 28 --- 25
R07 | 2968 8 13 32 22 67 10 | 26 45 56 47 91 28
R08 | 6471 54 49 191 41 --- 35 | 59 63 85 64 --- 59
R09 |14512 43 26 67 62 --- 27 | 12 47 85 63 --- 25
R10 | 3498 21 15 44 24 --- 14 | 43 35 42 27 --- 28
R11 | 6012 19 18 436 46 --- 19 | 25 37 402 46 --- 28
R13 |13604 25 33 67 69 --- 26 | 62 60 116 102 --- 68
R14 | 2563 28 9 23 36 --- 14 | 55 40 57 49 --- 43
R15 | 6039 15 16 115 23 141 12 | 47 60 142 60 44 55
R17 |13208 16 22 41 25 --- 14 | 43 44 47 65 --- 42
R19 | 2327 7 17 31 29 --- 11 | 32 32 52 52 --- 36
R20 | 2148 28 14 47 24 --- 15 | 50 54 79 58 --- 52
R23 | 2877 36 29 93 45 --- 27 | 70 67 100 141 --- 72
------+------------------------------------+--------------------------------
RMS | 7394 27 24 135 39 110 |T 41 47 94 61 67 42
WRMS | 7394 23 22 61 39 110 |NE 38 46 104 54 67 39
MEDI | 5249 21 20 52 34 67 |MD 43 45 69 58 44 42
Table 3.1473.5 GPS week: 1473 Day: 5 MJD: 54560
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5407 39 20 107 49 --- 27 | 41 58 129 84 --- 60
R04 | 4176 10 13 30 21 --- 10 | 32 42 31 47 --- 35
R06 | 3683 12 13 65 18 --- 14 | 36 48 69 58 --- 44
R07 | 3905 19 11 62 22 93 15 | 56 49 45 75 180 32
R08 | 6924 45 32 58 33 --- 22 | 69 40 85 55 --- 49
R09 |13213 21 20 55 58 --- 21 | 31 17 75 61 --- 27
R10 | 3033 40 14 49 29 --- 17 | 39 29 49 19 --- 25
R11 | 5996 43 19 223 56 --- 27 | 25 36 146 61 --- 29
R13 | 9797 22 27 70 37 --- 20 | 100 84 139 117 --- 98
R14 | 1989 15 11 28 17 --- 9 | 33 43 64 63 --- 43
R15 | 4428 58 22 68 52 167 26 | 91 80 132 107 68 82
R17 |10251 42 17 34 58 --- 21 | 28 50 68 72 --- 43
R19 | 2811 17 12 39 29 --- 12 | 26 23 30 28 --- 21
R20 | 1065 18 12 39 25 --- 12 | 75 72 77 73 --- 71
R23 | 2407 33 27 83 45 --- 24 | 52 39 94 254 --- 46
------+------------------------------------+--------------------------------
RMS | 6232 32 19 82 39 135 |T 48 47 82 78 124 47
WRMS | 6232 31 15 53 39 135 |NE 50 47 87 67 124 47
MEDI | 4176 22 17 58 33 93 |MD 39 43 75 63 68 43
Table 3.1473.6 GPS week: 1473 Day: 6 MJD: 54561
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3517 49 24 36 60 --- 23 | 53 50 67 83 --- 53
R04 | 5415 28 12 23 32 --- 13 | 35 41 43 36 --- 37
R06 | 1551 37 12 22 29 --- 14 | 30 43 40 42 --- 36
R07 | 2371 251 163 127 182 361 104 | 151 134 38 135 244 66
R08 | 9020 50 23 127 31 --- 23 | 43 41 68 38 --- 36
R09 |11435 29 19 46 48 --- 20 | 21 29 60 47 --- 25
R10 | 2492 44 14 56 42 --- 22 | 25 30 38 41 --- 23
R11 | 6863 42 26 364 46 --- 25 | 29 39 117 50 --- 35
R13 |10845 43 35 96 58 --- 33 | 73 91 101 100 --- 76
R14 | 1748 33 11 44 49 --- 19 | 43 44 68 52 --- 44
R15 |10901 76 20 60 40 87 27 | 85 87 113 67 80 79
R17 |19339 37 18 48 50 --- 21 | 34 35 59 67 --- 38
R19 | 3690 30 11 63 44 --- 21 | 35 37 73 42 --- 38
R20 | 2457 41 20 58 38 --- 22 | 78 64 81 56 --- 64
R23 | 1543 73 46 57 950 --- 40 | 114 73 93 745 --- 80
------+------------------------------------+--------------------------------
RMS | 7961 78 47 115 253 262 |T 56 55 70 106 162 48
WRMS | 7961 44 19 76 253 262 |NE 53 57 68 62 162 46
MEDI | 3690 42 20 57 46 87 |MD 43 43 68 52 80 38
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