[IGSREPORT-16370] Wk 1483 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 26 06:05:11 PDT 2008
******************************************************************************
IGS Electronic Report 26 Jun 06:05:18 PDT 2008 Message Number 16370
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1483 (Jun 08, 2008 - Jun 14, 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 2.1483.
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:
igl1483[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1483 in the SP3 format.
igl14837.sum Combination Report for GPS Week 1483.
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 | 939.4 ns
1 | 871.2 ns
2 | 851.4 ns
3 | 872.2 ns
4 | 932.1 ns
5 | 934.7 ns
6 | 933.5 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
1 | ESX | R13
3 | ESX | R07
4 | ESX | R08 R13
5 | ESX | R19
6 | ESX | R08
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 1.1483, 1a.1483).
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 2.1483.0-6)
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 3.1483.0-6).
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 1483 summary. (Jun 08, 2008 - Jun 14, 2008)
Table 1.1483.a GPS week : 1483 MJD: 54625.0-54631.0
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 67| 3 1 -15 21 -1 29 -.27 37 35 | 0 10 2718 2818
| 2 0 4 41 34 155 .24 | 0 202
cod 200| -2 -1 5 12 22 61 -.07 32 28 | --- --- --- ---
| 5 2 4 36 49 70 .09 | --- ---
esx 118| -2 1 8 -23 4 -48 .51 81 48 | 26977 1502 8313 19996
| 5 5 7 62 49 133 .27 | 36261 7489
iac n/a| 3 1 0 -19 -23 -63 .02 38 38 | 903390 -47 8031 17306
| 4 3 6 48 58 127 .06 | 36222 4959
mcc n/a| 31 47 51 233 -301 -825 .88 680 680 | --- --- --- ---
| 41 52 80 559 323 1665 1.24 | --- ---
Table 1.1483.b GPS week : 1483 MJD: 54625.0-54631.0
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 | 285 426 117 59 38 48 53 |
R04 | 23 25 22 27 21 18 26 |
R06 | 24 18 15 21 17 26 19 |
R07 | 15 20 29 39 26 28 48 |
R08 | 20 21 20 31 24 30 27 |
R09 | --- --- --- 0 0 0 --- |
R10 | 17 22 22 15 13 13 15 |
R11 | 30 27 23 18 21 21 21 |
R13 | 32 26 24 26 24 25 24 |
R14 | 22 24 14 13 14 14 16 |
R15 | 43 22 23 22 22 25 27 |
R17 | 23 22 15 17 22 24 36 |
R19 | 21 24 17 12 19 20 22 |
R20 | 20 23 22 21 18 19 18 |
R23 | 26 29 20 22 17 32 30 |
R24 | 16 25 23 23 23 16 20 |
Table 1.1483.c GPS week : 1483 MJD: 54625.0-54631.0
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 1483 0 | -6 48 260 -1547 -1798 -14870 101.6 5067 5067 | 939407 0
brd 1483 1 | 259 1953 5644 -32189 -8268 77760 <<<< >>>>> >>>>> | 871224 0
brd 1483 2 | 44 70 290 -1324 459 -12770 99.3 3715 3715 | 851397 0
brd 1483 3 | -60 -80 451 577 -2122 -22930 103.3 4768 4768 | 872198 0
brd 1483 4 | -151 34 278 -37 710 -27940 105.9 5146 5146 | 932070 0
brd 1483 5 | -169 -146 323 136 -2000 -21390 95.4 4351 4351 | 934662 0
brd 1483 6 | -85 0 562 243 2558 -24650 93.2 3474 3474 | 933529 0
-------------+------------------------------------------------------------+----------------
brd 1483 mean| -24 268 1115 -4877 -1494 -6684 <<<< >>>>> >>>>> | 904926 0
brd 1483 sdev| 145 746 1999 12070 3457 37615 >>>> >>>>> >>>>> | 38079 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 2.1483.0 GPS week: 1483 Day: 0 MJD: 54625
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 67| 2 2 -15 90 -7 211 -.08 40 42 | 0 -163 2240 2363
cod 200| 2 -3 7 10 25 116 -.16 29 26 | --- --- --- ---
esx 118| 3 4 17 -41 61 -244 .50 73 48 | 56951 4572 7701 16840
iac n/a| -2 6 -11 23 -56 -218 -.01 50 50 | 937942 2136 7564 13817
mcc n/a| 10 2 103 289 -40 -1550 .39 259 259 | --- --- --- ---
Table 2.1483.1 GPS week: 1483 Day: 1 MJD: 54626
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 67| 5 0 -13 -6 10 -88 -.22 38 39 | 0 -90 2823 2908
cod 200| -3 -1 8 -53 39 173 -.15 35 32 | --- --- --- ---
esx 118| -7 1 8 -10 7 -163 .54 80 48 | -262 -3445 7484 19294
iac n/a| 0 3 -1 39 -114 -27 -.10 38 38 | 871756 -3484 7319 15313
mcc n/a| 8 6 75 -95 142 -939 .83 321 321 | --- --- --- ---
Table 2.1483.2 GPS week: 1483 Day: 2 MJD: 54627
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 67| 0 2 -16 -4 -56 -64 -.08 32 31 | 0 397 2641 2731
cod 200| 1 -1 2 61 116 92 -.13 33 30 | --- --- --- ---
esx 118| -10 -3 13 11 63 24 .59 52 47 | -31725 7673 6972 15416
iac n/a| 1 0 4 -43 -71 -89 .05 32 32 | 852585 -31 7243 14261
mcc n/a| 4 18 28 -234 -129 -1309 .05 537 537 | --- --- --- ---
Table 2.1483.3 GPS week: 1483 Day: 3 MJD: 54628
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 67| 3 0 -10 -22 15 75 -.21 36 29 | 0 64 2523 2582
cod 200| -9 0 -2 14 14 16 .06 32 25 | --- --- --- ---
esx 118| 4 1 12 -135 -72 122 .28 72 47 | 2066 -6818 7372 22092
iac n/a| 6 -5 5 -29 -8 -160 .03 35 35 | 872084 -3472 6887 18953
mcc n/a| -11 74 72 151 -401 -3883 -.37 891 891 | --- --- --- ---
Table 2.1483.4 GPS week: 1483 Day: 4 MJD: 54629
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 67| 6 1 -17 27 45 263 -.36 34 32 | 0 -73 2202 2296
cod 200| -11 -4 7 30 -46 7 .05 28 25 | --- --- --- ---
esx 118| 0 0 11 63 -9 -129 .05 128 39 | 53659 12598 9604 17784
iac n/a| 7 2 -1 -96 46 -151 .04 35 35 | 927440 6964 8484 12947
mcc n/a| 44 15 132 -427 -299 433 .05 723 723 | --- --- --- ---
Table 2.1483.5 GPS week: 1483 Day: 5 MJD: 54630
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 67| 6 0 -11 61 -34 -102 -.17 34 31 | 0 114 3599 3697
cod 200| -1 -2 7 -11 0 -32 -.13 25 23 | --- --- --- ---
esx 118| -4 9 -4 3 -37 65 .78 84 58 | 53158 -6890 8511 24856
iac n/a| 9 2 5 -45 19 108 .07 42 42 | 933960 -7024 8414 24387
mcc n/a| 109 70 66 991 -581 933 2.87 934 934 | --- --- --- ---
Table 2.1483.6 GPS week: 1483 Day: 6 MJD: 54631
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 67| 2 1 -23 2 20 -91 -.77 45 41 | 0 -178 2999 3154
cod 200| 0 2 6 31 7 55 -.05 43 35 | --- --- --- ---
esx 118| -6 -7 3 -57 17 -12 .82 77 50 | 54995 2830 10552 23694
iac n/a| 1 0 7 15 20 95 .05 37 37 | 927964 4581 10306 21466
mcc n/a| 52 146 -116 959 -797 534 2.31 1099 1099 | --- --- --- ---
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 3.1483.0 GPS week: 1483 Day: 0 MJD: 54625
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 226 --- 358 --- 284 | --- 584 --- 225 --- 386
R04 | 7224 23 24 70 41 --- 22 | 59 73 98 54 --- 65
R06 | 2930 50 27 43 49 --- 24 | 49 53 52 62 --- 46
R07 | 9594 26 18 24 34 --- 14 | 29 45 36 53 --- 34
R08 | 6066 34 22 173 32 --- 20 | 76 60 123 58 --- 62
R10E | 8697 29 17 20 46 --- 17 | 30 25 33 37 --- 25
R11E | 3096 54 41 82 29 181 29 | 41 43 78 42 91 29
R13E | 2300 41 37 100 48 --- 32 | 41 35 74 61 --- 39
R14E | 2850 55 25 40 32 --- 22 | 18 39 57 47 --- 33
R15E | 4591 52 43 55 127 318 43 | 33 19 69 81 365 35
R17 | 2312 35 24 55 49 --- 23 | 44 82 101 43 --- 64
R19 | 3016 27 26 68 24 --- 21 | 20 33 67 33 --- 26
R20 | 2760 28 25 54 34 --- 20 | 29 54 66 60 --- 47
R23 | 4072 58 38 57 30 --- 26 | 33 70 70 52 --- 48
R24 | 3371 29 24 30 26 --- 15 | 110 119 120 102 --- 109
------+------------------------------------+--------------------------------
RMS | 5066 40 29 73 50 259 |T 43 88 74 67 228 69
WRMS | 5066 42 26 48 50 259 |NE 49 117 81 74 --- 88
MEDI | 3096 34 25 55 34 181 |MD 33 53 69 54 91 46
Table 3.1483.1 GPS week: 1483 Day: 1 MJD: 54626
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 415 --- 436 --- 425 | --- 792 --- 397 --- 522
R04 |>>>>> 31 28 72 37 --- 25 | 67 46 98 56 --- 55
R06 |>>>>> 34 30 37 22 --- 17 | 42 50 57 51 --- 43
R07 |48324 39 39 23 30 --- 19 | 32 35 45 44 --- 31
R08 |>>>>> 29 29 63 19 --- 21 | 40 44 119 37 --- 34
R10E |>>>>> 31 29 38 47 --- 21 | 36 36 51 31 --- 26
R11E |>>>>> 28 42 63 50 97 27 | 46 43 78 34 24 35
R13E |>>>>> 29 30 236 47 --- 26 | 31 38 145 41 --- 29
R14E |>>>>> 49 32 50 33 --- 23 | 28 45 65 30 --- 27
R15E |>>>>> 37 27 39 45 443 21 | 22 24 47 49 378 25
R17 |>>>>> 44 38 50 20 --- 22 | 45 62 47 37 --- 37
R19 |>>>>> 45 23 66 24 --- 23 | 24 34 75 39 --- 33
R20 |>>>>> 52 27 16 48 --- 22 | 19 35 46 60 --- 30
R23 |>>>>> 41 55 50 47 --- 28 | 24 49 57 49 --- 24
R24 |>>>>> 34 40 59 38 --- 24 | 80 81 110 70 --- 74
------+------------------------------------+--------------------------------
RMS |>>>>> 38 35 80 38 321 |T 38 94 74 68 201 68
WRMS |>>>>> 39 32 48 38 321 |NE 41 122 72 84 --- 88
MEDI |>>>>> 34 30 50 38 97 |MD 32 44 57 44 24 33
Table 3.1483.2 GPS week: 1483 Day: 2 MJD: 54627
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 110 --- 123 --- 116 | --- 260 --- 353 --- 291
R04 | 3110 36 28 50 39 --- 21 | 54 77 67 58 --- 52
R06 | 4607 24 14 44 22 --- 14 | 48 48 79 54 --- 51
R07 | 2098 37 60 74 28 --- 29 | 31 77 79 32 --- 35
R08 | 4311 44 30 42 19 --- 20 | 45 55 74 60 --- 49
R10E | 2790 27 42 49 33 --- 21 | 21 47 51 28 --- 22
R11E | 3966 18 34 72 34 116 23 | 31 37 95 49 26 35
R13E | 3148 39 39 46 42 --- 23 | 29 40 88 43 --- 26
R14E | 1730 19 26 32 18 --- 13 | 16 31 40 28 --- 18
R15E | 4895 32 34 45 49 750 23 | 28 36 50 51 330 30
R17 | 7325 18 26 33 26 --- 14 | 20 45 47 36 --- 30
R19 | 2499 23 23 48 26 --- 17 | 27 39 86 35 --- 32
R20 | 2489 17 15 74 39 --- 21 | 39 42 58 65 --- 38
R23 | 1814 36 21 41 39 --- 20 | 61 46 43 43 --- 34
R24 | 3084 47 37 50 20 --- 22 | 83 74 62 74 --- 67
------+------------------------------------+--------------------------------
RMS | 3714 32 33 52 32 537 |T 38 63 65 67 178 54
WRMS | 3714 31 30 47 32 537 |NE 45 76 66 81 --- 67
MEDI | 3084 27 30 46 33 116 |MD 31 46 62 49 26 35
Table 3.1483.3 GPS week: 1483 Day: 3 MJD: 54628
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 53 --- 66 --- 59 | --- 253 --- 182 --- 229
R04 | 2898 52 22 87 33 --- 27 | 121 80 85 115 --- 96
R06 | 6020 39 18 69 26 --- 21 | 60 69 106 67 --- 66
R07 | 3172 47 62 175 50 --- 38 | 32 84 146 41 --- 45
R08 | 6651 70 36 81 26 --- 30 | 57 79 119 45 --- 52
XR09E |12633 --- --- 14 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 5637 18 27 21 33 --- 15 | 20 25 26 28 --- 12
R11E | 2200 21 29 38 34 258 17 | 27 41 48 41 35 28
R13E |11968 19 39 47 62 --- 25 | 35 29 67 53 --- 31
R14E | 1469 22 24 26 20 --- 13 | 19 38 26 31 --- 19
R15E | 2033 19 35 37 53 1234 22 | 28 26 54 52 9999 27
R17 | 2807 31 31 34 21 --- 17 | 36 66 62 43 --- 43
R19 | 1922 18 12 35 19 --- 11 | 46 42 67 48 --- 42
R20 | 2587 23 17 77 33 --- 21 | 54 67 130 39 --- 59
R23 | 3153 25 32 69 28 --- 21 | 39 51 86 21 --- 26
R24 | 2217 49 30 55 25 --- 22 | 108 123 117 123 --- 114
------+------------------------------------+--------------------------------
RMS | 4767 36 32 72 35 891 |T 48 71 81 61 35 59
WRMS | 4767 29 25 47 35 891 |NE 61 91 102 72 --- 77
MEDI | 2898 23 30 47 33 258 |MD 36 66 67 45 35 43
Table 3.1483.4 GPS week: 1483 Day: 4 MJD: 54629
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 35 --- 41 --- 38 | --- 158 --- 172 --- 155
R04 | 4744 32 38 30 40 --- 20 | 43 66 71 47 --- 51
R06 | 4562 37 21 36 27 --- 17 | 52 82 105 58 --- 69
R07 | 5181 27 48 59 38 --- 25 | 42 65 69 39 --- 33
R08 | 7574 40 34 227 25 --- 23 | 64 62 214 73 --- 65
XR09E |18189 --- --- 11 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 6389 20 17 25 25 --- 12 | 24 25 42 20 --- 22
R11E | 5056 31 24 50 37 166 20 | 29 30 66 50 50 29
R13E | 9090 31 29 396 40 --- 23 | 55 33 381 37 --- 33
R14E | 1795 22 18 24 34 --- 14 | 27 26 32 38 --- 22
R15E | 2328 20 26 51 50 1009 21 | 27 46 44 45 638 27
R17 | 2965 39 23 51 38 --- 21 | 31 67 88 53 --- 51
R19 | 2315 41 31 32 27 --- 19 | 39 48 42 50 --- 31
R20 | 3276 42 12 29 33 --- 17 | 30 55 67 72 --- 52
R23 | 3152 30 20 34 33 --- 17 | 37 26 48 36 --- 23
R24 | 7118 50 29 48 27 --- 22 | 81 126 148 102 --- 109
------+------------------------------------+--------------------------------
RMS | 5145 34 28 128 35 723 |T 41 61 101 59 344 51
WRMS | 5145 32 25 39 35 723 |NE 46 75 94 70 --- 63
MEDI | 4744 31 26 36 34 166 |MD 37 55 67 50 50 33
Table 3.1483.5 GPS week: 1483 Day: 5 MJD: 54630
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 35 --- 64 --- 47 | --- 88 --- 108 --- 72
R04 | 5460 38 23 37 30 --- 18 | 107 100 80 80 --- 88
R06 | 2252 52 23 87 30 --- 26 | 57 59 94 53 --- 53
R07 | 3811 42 44 79 38 --- 27 | 44 51 86 44 --- 34
R08 | 6885 43 27 111 39 --- 29 | 64 72 149 57 --- 69
XR09E |14682 --- --- 13 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 5265 17 15 38 28 --- 13 | 25 34 51 22 --- 22
R11E | 3815 39 21 36 49 328 20 | 38 35 58 61 34 32
R13E | 3122 23 24 92 42 --- 24 | 55 43 86 61 --- 44
R14E | 2662 16 18 42 29 --- 14 | 20 24 43 30 --- 19
R15E | 4081 23 19 93 50 1279 25 | 24 25 84 48 344 23
R17 | 3603 38 27 66 51 --- 24 | 52 50 73 56 --- 45
R19 | 1924 34 14 181 37 --- 19 | 29 24 159 43 --- 21
R20 | 3013 27 16 42 49 --- 18 | 24 35 26 60 --- 29
R23 | 3095 31 40 91 71 --- 31 | 38 43 106 74 --- 37
R24 | 7557 28 13 55 22 --- 15 | 236 237 225 263 --- 241
------+------------------------------------+--------------------------------
RMS | 4351 34 25 84 42 934 |T 58 61 94 70 189 55
WRMS | 4351 31 23 58 42 934 |NE 72 75 110 83 --- 68
MEDI | 3811 31 23 66 39 328 |MD 38 43 84 57 34 37
Table 3.1483.6 GPS week: 1483 Day: 6 MJD: 54631
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 36 --- 64 --- 53 | --- 141 --- 152 --- 143
R04 | 2512 43 46 53 38 --- 25 | 93 111 126 97 --- 103
R06 | 2920 44 18 34 33 --- 19 | 82 70 92 51 --- 66
R07 | 2280 96 86 105 44 --- 48 | 57 94 76 84 --- 52
R08 | 5507 36 40 204 36 --- 26 | 119 92 152 121 --- 106
R10E | 5963 38 13 29 19 --- 14 | 32 26 47 21 --- 25
R11E | 1814 41 36 33 32 804 20 | 33 34 58 41 40 35
R13E | 3699 29 43 49 39 --- 23 | 52 41 69 57 --- 43
R14E | 2076 31 20 33 25 --- 15 | 50 28 34 31 --- 30
R15E | 3546 23 35 87 30 1329 27 | 41 31 76 41 266 33
R17 | 3457 33 70 76 61 --- 36 | 49 88 108 46 --- 59
R19 | 1710 51 38 36 21 --- 21 | 50 51 79 36 --- 34
R20 | 2214 42 24 35 22 --- 17 | 40 54 62 56 --- 44
R23 | 2570 46 36 61 61 --- 30 | 68 27 54 69 --- 35
R24 | 4774 41 35 30 30 --- 19 | 207 224 217 207 --- 211
------+------------------------------------+--------------------------------
RMS | 3474 45 43 77 37 1099 |T 69 74 89 74 153 67
WRMS | 3474 41 35 50 37 1099 |NE 85 95 107 91 --- 85
MEDI | 2570 41 36 36 33 804 |MD 50 54 76 56 40 44
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