[IGSREPORT-16286] Wk 1479 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu May 29 09:22:55 PDT 2008
******************************************************************************
IGS Electronic Report 29 May 09:22:58 PDT 2008 Message Number 16286
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1479 (May 11, 2008 - May 17, 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 2.1479.
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:
igl1479[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1479 in the SP3 format.
igl14797.sum Combination Report for GPS Week 1479.
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 | 957.2 ns
1 | 954.2 ns
2 | 1002.8 ns
3 | 947.1 ns
4 | 947.5 ns
5 | 913.1 ns
6 | 988.5 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 | BKG | R07
2 | ESX | R09
3 | ESX | R19
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 1.1479, 1a.1479).
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 2.1479.0-6)
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 3.1479.0-6).
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 1479 summary. (May 11, 2008 - May 17, 2008)
Table 1.1479.a GPS week : 1479 MJD: 54597.0-54603.0
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 68| 2 -1 -5 46 14 5 -.13 37 33 | 0 199 2465 2580
| 1 5 8 53 37 87 .08 | 0 294
cod 218| -5 0 3 -16 9 -4 -.07 32 30 | --- --- --- ---
| 2 2 5 46 59 67 .06 | --- ---
esx 112| 0 4 3 -51 -88 -38 .51 145 54 | 9563 2883 13130 24364
| 4 6 5 52 46 143 .12 | 27398 11256
iac n/a| 4 0 -1 0 21 45 -.05 39 39 | 960446 -1203 13307 20413
| 2 3 7 36 34 69 .06 | 26373 11193
mcc n/a| -33 8 141 -277 449 -856 -.50 1147 1147 | --- --- --- ---
| 99 60 135 442 1035 3975 2.85 | --- ---
Table 1.1479.b GPS week : 1479 MJD: 54597.0-54603.0
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 | 131 --- --- --- --- --- --- |
R04 | 15 22 28 23 27 32 18 |
R06 | 34 16 20 19 21 26 16 |
R07 | 164 --- --- --- --- --- --- |
R08 | 33 36 39 48 23 32 23 |
R09 | 16 23 50 484 0 0 0 |
R10 | 33 29 25 13 16 26 20 |
R11 | 23 21 21 21 21 30 16 |
R13 | 26 38 23 33 27 23 25 |
R14 | 30 14 27 23 17 19 20 |
R15 | 26 21 23 21 23 25 17 |
R17 | 15 22 32 14 21 23 30 |
R19 | 15 10 18 20 21 30 22 |
R20 | 17 18 15 11 15 16 26 |
R23 | 20 32 26 88 --- 0 65 |
R24 | 15 10 21 18 17 21 28 |
Table 1.1479.c GPS week : 1479 MJD: 54597.0-54603.0
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 1479 0 | 57 184 299 -1418 5370 -12810 106.9 5284 5284 | 957240 0
brd 1479 1 | -480 ---- 986 -11200 -5383 -35580 652.6 >>>>> >>>>> | 954221 0
brd 1479 2 | -79 -122 291 2188 -707 -14630 102.9 5863 5863 | 1002801 0
brd 1479 3 | 194 331 26 -4141 3693 -11060 106.6 1918 1918 | 947147 0
brd 1479 4 | -31 -22 499 491 -2294 -18130 102.7 5419 5419 | 947456 0
brd 1479 5 | -4 -30 626 -876 -5506 -14880 101.9 6332 6332 | 913074 0
brd 1479 6 | 160 182 276 -700 -1503 -4790 104.5 4936 4936 | 988476 0
-------------+------------------------------------------------------------+----------------
brd 1479 mean| -26 -5662 429 -2236 -904 -15982 182.6 >>>>> >>>>> | 958630 0
brd 1479 sdev| 223 15212 310 4394 4164 9585 207.3 >>>>> >>>>> | 29425 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 2.1479.0 GPS week: 1479 Day: 0 MJD: 54597
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 68| 5 1 -7 99 89 5 -.20 38 31 | 0 69 2625 2695
cod 218| -8 -3 -6 -47 -13 -22 -.05 31 29 | --- --- --- ---
esx 112| 0 4 4 -123 -133 79 .42 52 46 | -3822 9396 14882 24016
iac n/a| 5 -2 14 67 3 -68 -.03 45 45 | 952077 6268 15566 19136
mcc n/a| 47 35 43 -347 -172 5377 -.26 610 610 | --- --- --- ---
Table 2.1479.1 GPS week: 1479 Day: 1 MJD: 54598
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 68| 2 -2 3 46 17 -131 -.16 32 28 | 0 296 2755 2833
cod 218| -7 1 5 52 -75 118 -.12 45 37 | --- --- --- ---
esx 112| -1 0 0 -102 -71 52 .52 45 40 | 7935 -10193 13016 21273
iac n/a| 7 1 -6 -26 35 61 -.14 44 44 | 959501 -11951 13066 16829
mcc n/a| -17 63 254 -224 -181 520 -3.89 476 476 | --- --- --- ---
Table 2.1479.2 GPS week: 1479 Day: 2 MJD: 54599
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 68| 0 -5 -11 -20 12 75 -.05 49 47 | 0 180 2485 2567
cod 218| -6 4 6 32 -50 -63 -.04 41 33 | --- --- --- ---
esx 112| 3 3 -2 -43 -51 -275 .45 631 65 | 38756 18378 16075 23461
iac n/a| 3 -2 0 -20 21 85 .04 37 37 | 994853 14267 16205 18770
mcc n/a| 15 28 170 -920 -507 -1700 -1.86 397 397 | --- --- --- ---
Table 2.1479.3 GPS week: 1479 Day: 3 MJD: 54600
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 68| 2 -5 -2 -8 12 -15 -.06 28 25 | 0 33 1611 1737
cod 218| -6 2 0 -2 33 -27 -.14 19 25 | --- --- --- ---
esx 112| 2 2 11 -61 -18 88 .76 125 84 | 4925 1691 10421 35021
iac n/a| 7 -4 -3 35 -33 32 -.02 29 29 | 956886 732 10283 34451
mcc n/a| 36 -6 45 359 793 -704 1.64 876 876 | --- --- --- ---
Table 2.1479.4 GPS week: 1479 Day: 4 MJD: 54601
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 68| 3 -6 -14 128 9 100 -.24 42 39 | 0 810 2999 3169
cod 218| -1 -1 7 -70 92 -54 -.16 29 27 | --- --- --- ---
esx 112| -4 8 2 -16 -137 20 .55 38 31 | 5867 -11946 24409 31580
iac n/a| 1 1 -4 -18 49 -21 -.13 38 38 | 957199 -18481 24705 29685
mcc n/a| -67 54 -38 -565 2577 1771 -3.89 1845 1845 | --- --- --- ---
Table 2.1479.5 GPS week: 1479 Day: 5 MJD: 54602
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 68| 3 -3 -15 36 -33 82 -.03 27 25 | 0 92 1984 2155
cod 218| -7 -1 9 -60 61 -43 -.01 32 32 | --- --- --- ---
esx 112| 9 16 8 -46 -75 -36 .51 81 65 | -34698 11917 6137 15857
iac n/a| 3 5 0 -19 3 121 -.02 41 41 | 914372 4486 6237 12231
mcc n/a| -241 -115 351 207 477 -4964 1.19 3396 3396 | --- --- --- ---
Table 2.1479.6 GPS week: 1479 Day: 6 MJD: 54603
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 68| 2 8 5 46 -8 -76 -.17 43 39 | 0 -84 2802 2904
cod 218| -4 -3 2 -18 14 60 -.00 30 27 | --- --- --- ---
esx 112| -4 -2 0 34 -130 -196 .38 42 44 | 47980 940 6975 19340
iac n/a| 2 0 -8 -17 69 109 -.04 41 41 | 988239 -3744 7088 11795
mcc n/a| -9 -3 165 -451 163 -6294 3.56 428 428 | --- --- --- ---
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 3.1479.0 GPS week: 1479 Day: 0 MJD: 54597
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 9171 238 193 --- 31 --- 130 | 3 3 --- 1 --- 4
R04 | 2042 25 16 26 35 --- 14 | 36 35 36 38 --- 31
R06 | 5326 78 41 53 56 --- 33 | 130 62 71 82 --- 74
XR07 | ---- 458 77 --- 243 --- 163 | 3 2 --- 1 --- 24
R08 | 3376 47 34 91 51 --- 32 | 24 56 91 43 --- 39
R09 | 9527 21 20 33 34 --- 15 | 24 948 427 37 --- 950
R10E | 5590 44 47 71 68 --- 32 | 71 63 106 85 --- 66
R11 | 5361 44 25 59 30 --- 23 | 107 141 151 114 --- 126
R13 | 9493 36 31 62 55 --- 26 | 113 109 134 111 --- 111
R14E | 2289 40 33 66 67 --- 29 | 53 86 112 69 --- 72
R15E | 8313 38 28 64 51 798 25 | 58 57 99 59 530 54
R17 | 3963 26 22 19 30 --- 14 | 45 65 56 57 --- 50
R19 | 1082 17 22 31 30 --- 14 | 35 42 64 47 --- 38
R20 | 1928 18 26 38 36 --- 17 | 58 61 48 53 --- 50
R23 | 2931 24 42 29 38 --- 20 | 20 9999 42 9999 --- 9999
R24 | 1580 31 23 28 14 330 14 | 159 161 157 158 229 158
------+------------------------------------+--------------------------------
RMS | 5284 38 31 52 45 610 |T 58 126 113 63 379 123
WRMS | 5284 31 29 46 45 610 |NE 51 54 70 53 229 52
MEDI | 3963 36 28 38 36 330 |MD 45 62 91 57 229 54
Table 3.1479.1 GPS week: 1479 Day: 1 MJD: 54598
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |>>>>> 25 53 44 25 --- 21 | 31 41 33 28 --- 19
R06 |>>>>> 22 28 34 26 --- 16 | 71 70 79 81 --- 78
R08 |>>>>> 78 68 33 51 --- 36 | 57 48 65 40 --- 18
R09E |>>>>> 28 34 55 44 --- 23 | 17 9999 487 47 --- 9999
R10E |>>>>> 38 76 45 37 --- 29 | 27 88 61 52 --- 45
R11E |>>>>> 34 36 46 30 --- 21 | 53 80 106 48 --- 61
R13E |>>>>> 28 63 67 95 --- 38 | 58 107 108 85 --- 69
R14E |>>>>> 19 21 30 22 --- 13 | 42 42 51 51 --- 40
R15E |>>>>> 22 43 55 19 543 21 | 44 43 79 47 422 42
R17 |>>>>> 23 35 38 52 --- 22 | 26 31 33 53 --- 19
R19 |>>>>> 13 17 24 15 --- 10 | 27 17 52 20 --- 18
R20 |>>>>> 22 33 43 22 --- 17 | 51 32 69 34 --- 39
R23 |>>>>> 27 53 63 70 --- 31 | 12 9999 64 9999 --- 9999
R24 |>>>>> 16 14 21 17 398 10 | 160 171 163 164 73 164
------+------------------------------------+--------------------------------
RMS |>>>>> 32 45 45 44 476 |T 48 64 103 57 247 51
WRMS |>>>>> 28 37 40 44 476 |NE 54 58 69 60 73 50
MEDI |>>>>> 23 35 43 26 398 |MD 42 43 65 48 73 40
Table 3.1479.2 GPS week: 1479 Day: 2 MJD: 54599
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 5287 52 46 54 45 --- 28 | 64 43 71 46 --- 41
R06 | 7412 35 33 39 29 --- 19 | 60 98 82 84 --- 82
R08 | 5282 82 45 115 30 --- 38 | 61 36 109 36 --- 19
R09E |11129 63 81 2353 64 --- 50 | 20 9999 9999 46 --- 9999
R10E | 7282 55 40 42 33 --- 24 | 51 60 53 27 --- 29
R11E | 3449 53 22 52 24 --- 21 | 99 66 80 58 --- 65
R13E | 7723 35 39 27 48 --- 23 | 87 66 67 73 --- 62
R14E | 2231 34 56 59 37 --- 27 | 55 65 61 63 --- 52
R15E | 3587 48 22 62 30 476 23 | 52 35 82 45 361 41
R17 | 9779 48 32 114 28 --- 32 | 57 64 105 46 --- 45
R19 | 1481 22 27 49 29 --- 18 | 29 54 113 23 --- 31
R20 | 1223 15 9 54 21 --- 15 | 24 33 69 28 --- 27
R23 | 1773 60 36 35 44 --- 25 | 29 9999 43 9999 --- 9999
R24 | 1316 42 30 43 29 298 20 | 84 98 90 80 72 82
------+------------------------------------+--------------------------------
RMS | 5863 49 41 631 37 397 |T 55 59 78 50 216 48
WRMS | 5863 47 33 65 37 397 |NE 51 60 85 49 72 46
MEDI | 3587 48 33 52 30 298 |MD 55 60 80 46 72 41
Table 3.1479.3 GPS week: 1479 Day: 3 MJD: 54600
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR04 | 7875 --- 25 23 44 --- 22 | --- 46 55 33 --- 40
XR06 | 4500 --- 20 41 28 --- 19 | --- 122 136 129 --- 120
XR08 | 5321 --- 18 137 61 --- 48 | --- 29 116 46 --- 33
XR09E |15525 --- 209 --- 756 --- 483 | --- 9999 --- 70 --- 9999
XR10E | 5568 --- 14 27 18 --- 13 | --- 52 37 33 --- 41
XR11E | 1477 --- 17 46 31 --- 20 | --- 76 85 66 --- 69
XR13E | 3484 --- 36 64 48 --- 32 | --- 70 95 71 --- 62
XR14E | 6220 --- 25 44 36 --- 23 | --- 40 54 60 --- 44
R15E | 3172 26 20 67 37 1187 20 | 26 28 85 51 527 31
R17 | 2057 25 15 37 28 --- 14 | 35 41 70 46 --- 40
R19 | 707 27 27 263 31 --- 20 | 36 47 191 38 --- 32
R20 | 928 18 14 32 17 --- 11 | 38 46 62 40 --- 42
XR23 |15256 --- 38 --- 136 --- 87 | --- 9999 --- 9999 --- 9999
R24 | 1653 41 17 43 28 354 17 | 106 120 127 138 85 120
------+------------------------------------+--------------------------------
RMS | 1917 28 19 125 29 876 |T 48 59 92 63 306 56
WRMS | 1917 25 25 84 29 876 |NE 53 64 108 67 85 61
MEDI | 3484 26 20 43 31 354 |MD 36 46 85 51 85 41
Table 3.1479.4 GPS week: 1479 Day: 4 MJD: 54601
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 7470 49 33 49 54 --- 26 | 49 47 68 34 --- 32
R06 | 2975 55 25 21 36 --- 20 | 80 64 83 67 --- 69
R08 | 7112 43 31 58 25 --- 23 | 78 31 63 35 --- 36
XR09E |13069 --- 9 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 2821 28 26 23 30 --- 15 | 56 38 57 26 --- 36
R11E | 3953 39 35 41 31 --- 21 | 74 63 90 71 --- 62
R13E | 7732 63 31 35 54 --- 26 | 82 62 61 79 --- 54
R14E | 8309 37 20 25 34 --- 17 | 27 35 52 58 --- 34
R15E | 6050 35 34 24 59 2519 23 | 17 42 51 48 534 30
R17 | 6336 36 27 45 33 --- 20 | 39 38 61 34 --- 33
R19 | 992 34 26 54 28 --- 21 | 36 49 115 47 --- 40
R20 | 2464 29 24 24 29 --- 15 | 52 41 37 34 --- 31
R24 | 977 37 26 29 24 680 17 | 51 65 55 61 91 54
------+------------------------------------+--------------------------------
RMS | 5419 42 29 38 38 1845 |T 53 47 66 49 312 42
WRMS | 5419 39 27 31 38 1845 |NE 55 47 68 44 91 42
MEDI | 6050 37 26 29 31 680 |MD 51 42 61 47 91 36
Table 3.1479.5 GPS week: 1479 Day: 5 MJD: 54602
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR04 | 8955 --- 41 50 49 --- 32 | --- 54 40 24 --- 30
XR06 | 4548 --- 31 50 38 --- 26 | --- 90 112 98 --- 97
XR08 | 8696 --- 22 81 47 --- 31 | --- 28 77 39 --- 24
XR09E |14162 --- 9 --- --- --- 0 | --- 9999 --- --- --- 9999
XR10E | 2491 --- 23 48 44 --- 25 | --- 28 62 33 --- 26
XR11E | 3418 --- 28 58 49 --- 29 | --- 44 82 59 --- 48
XR13E | 2367 --- 24 44 37 --- 23 | --- 42 70 56 --- 44
XR14E | 3261 --- 20 29 31 --- 18 | --- 43 42 59 --- 45
R15E | 1575 29 46 55 48 4752 24 | 21 46 48 49 9999 21
R17 |13653 25 27 106 20 --- 23 | 40 63 95 36 --- 43
R19 | 1229 29 29 113 61 --- 29 | 60 58 69 64 --- 50
R20 | 2964 17 36 35 21 --- 15 | 20 43 33 31 --- 25
XR23 |80582 --- 9 --- --- --- 0 | --- 9999 --- --- --- 9999
R24 | 1132 31 17 69 40 689 20 | 62 64 77 73 310 54
------+------------------------------------+--------------------------------
RMS | 6332 27 32 81 41 3395 |T 40 50 67 51 310 42
WRMS | 6332 25 32 65 41 3395 |NE 45 57 71 52 310 46
MEDI | 3261 29 24 50 40 689 |MD 40 44 69 49 310 43
Table 3.1479.6 GPS week: 1479 Day: 6 MJD: 54603
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 9891 39 21 38 26 --- 17 | 34 51 59 39 --- 42
R06 | 5641 32 17 31 32 --- 16 | 94 96 95 99 --- 92
R08 | 7022 51 32 40 33 --- 22 | 70 42 44 38 --- 33
XR09E |11039 --- 4 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 1295 43 34 32 29 --- 20 | 45 35 50 41 --- 34
R11E | 3452 24 22 25 38 --- 16 | 65 75 90 74 --- 75
R13E | 2508 30 47 45 47 --- 25 | 73 95 88 99 --- 83
R14E | 2808 29 37 33 37 --- 20 | 42 59 53 54 --- 49
R15E | 2650 24 19 38 36 233 17 | 30 20 48 50 9999 23
R17 | 8320 37 33 58 73 --- 29 | 60 89 101 49 --- 70
R19 | 1212 49 22 45 35 --- 21 | 36 40 79 68 --- 49
R20 | 2210 54 28 60 40 --- 26 | 57 31 35 23 --- 21
XR23 |>>>>> --- 51 --- 80 --- 64 | --- 9999 --- 9999 --- 9999
R24 | 1738 77 30 41 43 559 28 | 114 128 134 128 208 123
------+------------------------------------+--------------------------------
RMS | 4936 43 30 42 41 428 |T 60 63 73 63 208 57
WRMS | 4936 39 27 44 41 428 |NE 66 68 78 63 208 61
MEDI | 2808 37 28 38 37 233 |MD 57 51 59 50 208 49
More information about the IGSREPORT
mailing list