[IGSREPORT-16617] Wk 1494 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Sep 11 07:39:52 PDT 2008
******************************************************************************
IGS Electronic Report 11 Sep 07:39:57 PDT 2008 Message Number 16617
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1494 (Aug 24, 2008 - Aug 30, 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 2.1494.
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:
igl1494[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1494 in the SP3 format.
igl14947.sum Combination Report for GPS Week 1494.
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 | 618.8 ns
1 | 638.7 ns
2 | 659.8 ns
3 | 580.5 ns
4 | 651.4 ns
5 | 652.8 ns
6 | 568.6 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 | R13 R17
2 | ESX | R11 R19
4 | ESX | R17
6 | ESX | R17
6 | IAC | R11 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 1.1494, 1a.1494).
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 2.1494.0-6)
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 3.1494.0-6).
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 1494 summary. (Aug 24, 2008 - Aug 30, 2008)
Table 1.1494.a GPS week : 1494 MJD: 54702.0-54708.0
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 63| 1 1 -3 -25 26 34 -.16 43 38 | 0 -320 2840 2985
| 2 2 3 35 51 178 .12 | 0 571
cod 212| -6 0 -4 24 35 -7 -.10 35 28 | --- --- --- ---
| 5 1 6 27 60 83 .10 | --- ---
esx 117| 0 -5 6 4 -99 85 .46 101 53 | -11446 6065 14114 22919
| 7 4 8 62 46 93 .14 | 32903 13659
iac n/a| 3 2 6 -14 -3 -83 -.06 58 58 | 626388 -3084 8719 16093
| 2 3 6 46 39 103 .07 | 34542 8916
mcc n/a| -8 -1 87 115 104 -109 .19 474 474 | --- --- --- ---
| 18 8 31 64 135 1227 .64 | --- ---
Table 1.1494.b GPS week : 1494 MJD: 54702.0-54708.0
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 | 0 0 0 0 0 0 0 |
R04 | 22 33 32 28 19 16 21 |
R06 | 34 25 32 17 25 31 43 |
R07 | 33 39 50 52 17 16 15 |
R09 | --- 0 0 0 0 0 0 |
R10 | 24 21 22 21 24 16 16 |
R11 | 24 16 19 17 33 24 24 |
R13 | 21 22 31 26 28 12 29 |
R14 | 14 13 13 18 15 23 15 |
R15 | 24 15 20 21 11 20 19 |
R17 | 21 29 19 23 16 26 24 |
R19 | 27 23 21 23 15 13 20 |
R20 | 18 22 23 17 14 15 19 |
R23 | 26 25 36 26 23 27 44 |
R24 | 46 19 16 15 12 14 21 |
Table 1.1494.c GPS week : 1494 MJD: 54702.0-54708.0
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 1494 0 | -68 99 404 -2583 -1229 -28190 93.6 4606 4606 | 618814 0
brd 1494 1 |-2409 -1946 802 -5339 -17880 -41370 <<<< >>>>> >>>>> | 638709 0
brd 1494 2 | 15 -33 94 4549 -458 -29450 98.7 5129 5129 | 659822 0
brd 1494 3 | 80 9 487 -505 3577 -26000 102.0 4123 4123 | 580528 0
brd 1494 4 | -16 229 488 2101 -2959 -18220 95.9 3272 3272 | 651427 0
brd 1494 5 | -127 76 202 -1016 -2475 -9462 93.4 4746 4746 | 652775 0
brd 1494 6 | -17 -2 204 -1184 846 -12050 95.2 4657 4657 | 568611 0
-------------+------------------------------------------------------------+----------------
brd 1494 mean| -363 -223 383 -568 -2939 -23534 <<<< >>>>> >>>>> | 624383 0
brd 1494 sdev| 904 764 240 3181 6943 11098 757.2 >>>>> >>>>> | 36659 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 2.1494.0 GPS week: 1494 Day: 0 MJD: 54702
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 63| 2 1 -5 -6 -48 203 -.31 68 48 | 0 -135 2486 2572
cod 212| -7 -1 0 36 47 93 .08 28 26 | --- --- --- ---
esx 117| 14 -4 4 -36 -43 -6 .61 288 64 | -10296 -15248 15780 29391
iac n/a| 1 6 6 8 -27 -223 -.13 38 38 | 625324 -21529 15520 30772
mcc n/a| 5 -10 60 153 -5 -575 .37 527 527 | --- --- --- ---
Table 2.1494.1 GPS week: 1494 Day: 1 MJD: 54703
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 63| 3 0 -4 -88 -7 -18 -.06 38 31 | 0 -1588 4382 4849
cod 212| -7 -1 -14 57 70 53 -.05 39 34 | --- --- --- ---
esx 117| -1 -9 12 125 -141 76 .37 64 51 | -25169 24544 35024 46763
iac n/a| 6 4 10 -57 -10 -20 .03 35 35 | 638767 -730 9011 12118
mcc n/a| -1 -9 74 98 222 -390 -.88 503 503 | --- --- --- ---
Table 2.1494.2 GPS week: 1494 Day: 2 MJD: 54704
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 63| 4 3 -5 20 24 -145 -.06 53 48 | 0 -199 2569 2668
cod 212| -16 -3 -7 -9 128 -73 -.16 57 38 | --- --- --- ---
esx 117| -1 -5 15 -22 -122 108 .22 89 55 | 19336 7030 6014 14642
iac n/a| 8 4 -3 -5 -20 70 .01 30 30 | 659519 1549 6013 12880
mcc n/a| -33 5 88 60 155 -2343 -.21 506 506 | --- --- --- ---
Table 2.1494.3 GPS week: 1494 Day: 3 MJD: 54705
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 63| 0 0 3 -21 64 -115 -.35 47 45 | 0 -87 2618 2684
cod 212| -7 0 3 -8 -9 0 -.11 42 32 | --- --- --- ---
esx 117| 4 -9 -1 57 -114 189 .55 61 46 | -51907 8017 6487 14639
iac n/a| 3 -1 1 21 49 -41 .01 28 28 | 586405 -709 6474 15145
mcc n/a| 17 9 47 66 193 164 .38 277 277 | --- --- --- ---
Table 2.1494.4 GPS week: 1494 Day: 4 MJD: 54706
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 63| -1 5 -4 0 93 270 -.15 36 38 | 0 -273 3099 3187
cod 212| -1 1 0 31 -54 -85 -.09 20 18 | --- --- --- ---
esx 117| 0 -9 -5 -32 -22 -56 .39 79 48 | 24088 -8530 9370 17338
iac n/a| 0 6 8 19 52 -51 -.12 36 36 | 654242 -6561 8341 14441
mcc n/a| -5 1 88 244 -140 -103 .98 366 366 | --- --- --- ---
Table 2.1494.5 GPS week: 1494 Day: 5 MJD: 54707
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 63| 2 0 -6 -38 68 181 -.10 29 27 | 0 -62 2302 2372
cod 212| -1 0 -6 15 0 -113 -.11 32 26 | --- --- --- ---
esx 117| -7 1 16 -29 -133 91 .47 56 53 | 16343 12713 9537 17343
iac n/a| 3 1 7 11 -16 -124 -.10 30 30 | 649026 5764 6516 12720
mcc n/a| -10 3 121 99 223 1101 .80 510 510 | --- --- --- ---
Table 2.1494.6 GPS week: 1494 Day: 6 MJD: 54708
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 63| 0 3 -3 -42 -12 -132 -.08 31 28 | 0 102 2426 2566
cod 212| -2 1 -3 52 66 73 -.24 25 18 | --- --- --- ---
esx 117| -2 -4 2 -28 -117 196 .61 72 55 | -52517 13932 16590 20318
iac n/a| 4 -2 14 -98 -52 -195 -.13 212 212 | 571434 627 9164 14576
mcc n/a| -29 -7 134 83 84 1381 -.11 631 631 | --- --- --- ---
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 3.1494.0 GPS week: 1494 Day: 0 MJD: 54702
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 8 --- --- --- 0 | --- 722 --- --- --- 721
R04 | 1392 36 31 49 39 --- 21 | 51 48 52 32 --- 35
R06 | 5533 107 35 55 49 --- 33 | 181 207 218 210 --- 199
R07 | 3019 68 27 103 40 --- 32 | 42 50 126 33 --- 38
R10 | 5463 67 31 56 25 --- 24 | 37 49 54 33 --- 24
R11 | 3436 25 22 83 32 35 24 | 19 31 64 58 143 30
R13 | 3309 39 21 1004 32 --- 20 | 58 44 838 33 --- 35
R14 | 3248 33 18 21 25 --- 13 | 15 32 37 43 --- 26
R15 | 4115 21 23 78 37 102 23 | 34 25 58 31 26 27
R17 | 1330 35 17 157 37 --- 20 | 33 44 102 58 --- 43
R19 | 3373 80 32 42 36 --- 26 | 282 327 360 294 --- 313
R20 | 593 37 18 43 33 --- 18 | 79 84 108 93 --- 86
R23 | 3977 65 19 60 46 --- 25 | 36 49 94 97 --- 54
R24 |11167 145 49 88 50 907 45 | 122 91 78 103 661 88
------+------------------------------------+--------------------------------
RMS | 4606 68 28 288 38 527 |T 76 128 168 86 276 122
WRMS | 4606 48 26 64 38 527 |NE 76 128 168 86 276 122
MEDI | 3373 39 22 60 37 102 |MD 42 49 94 58 143 38
Table 3.1494.1 GPS week: 1494 Day: 1 MJD: 54703
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 11 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 |>>>>> 81 26 68 41 --- 32 | 105 43 58 36 --- 40
R06 |>>>>> 52 28 54 36 --- 24 | 302 320 324 341 --- 319
R07 |30289 54 78 83 60 --- 39 | 37 122 82 35 --- 35
XR09 |>>>>> --- --- 15 --- --- 0 | --- --- 9999 --- --- 9999
XR10 |>>>>> --- 18 47 26 --- 20 | --- 29 73 25 --- 30
R11 |>>>>> 16 29 46 20 35 15 | 14 26 73 31 111 12
R13 |>>>>> 32 24 80 22 --- 22 | 34 49 242 28 --- 37
R14 |>>>>> 14 15 43 22 --- 13 | 15 34 39 25 --- 18
R15 |>>>>> 11 20 40 30 106 14 | 32 29 52 37 30 33
R17 |>>>>> 34 56 87 26 --- 28 | 24 67 80 59 --- 48
R19 |>>>>> 29 47 42 37 --- 22 | 262 234 297 264 --- 249
R20 |>>>>> 24 36 67 31 --- 22 | 106 98 137 100 --- 100
R23 |>>>>> 27 34 66 47 --- 24 | 37 72 60 99 --- 53
R24 |>>>>> 23 32 62 21 864 19 | 103 75 54 65 589 64
------+------------------------------------+--------------------------------
RMS |>>>>> 38 39 64 35 503 |T 89 92 120 88 243 79
WRMS |>>>>> 31 34 51 35 503 |NE 89 92 120 88 243 79
MEDI |>>>>> 27 28 54 30 106 |MD 37 67 73 37 111 40
Table 3.1494.2 GPS week: 1494 Day: 2 MJD: 54704
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 14 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 1601 87 44 55 32 --- 31 | 83 53 61 23 --- 26
R06 | 6165 87 60 38 34 --- 31 | 133 217 185 163 --- 165
R07 | 1126 53 146 89 45 --- 50 | 40 138 95 28 --- 50
XR09 |31857 --- --- 14 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1918 42 39 56 20 --- 22 | 30 37 67 19 --- 20
R11 | 1510 19 40 167 18 190 18 | 26 26 129 31 101 19
R13 | 9514 67 78 37 34 --- 31 | 36 96 147 60 --- 40
R14 | 5585 25 13 29 22 --- 13 | 15 24 46 38 --- 25
R15 | 3404 31 32 57 18 187 20 | 29 40 51 27 46 16
R17 | 9208 40 23 44 27 --- 19 | 36 43 54 36 --- 29
R19 | 5846 41 23 200 26 --- 21 | 98 90 158 95 --- 91
R20 | 2383 47 40 44 33 --- 23 | 55 75 77 42 --- 50
R23 | 2335 62 51 91 43 --- 35 | 24 70 103 88 --- 62
R24 | 5542 29 22 39 20 835 15 | 114 100 137 86 672 101
------+------------------------------------+--------------------------------
RMS | 5128 53 57 89 30 506 |T 55 77 100 56 273 53
WRMS | 5128 48 38 55 30 506 |NE 55 77 100 56 273 53
MEDI | 3404 42 39 44 27 190 |MD 36 70 95 38 101 40
Table 3.1494.3 GPS week: 1494 Day: 3 MJD: 54705
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 5 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 2508 79 33 54 24 --- 27 | 84 59 61 45 --- 49
R06 | 4927 25 35 31 22 --- 16 | 304 301 278 302 --- 294
R07 | 1038 41 104 158 35 --- 51 | 43 77 150 34 --- 39
XR09 |28782 --- --- 16 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2405 52 26 47 24 --- 21 | 31 42 69 34 --- 29
R11 | 1504 34 26 41 22 385 17 | 21 40 81 68 291 39
R13 | 3247 60 47 43 31 --- 26 | 41 52 109 45 --- 34
R14 | 5003 14 23 41 34 --- 17 | 30 31 50 48 --- 35
R15 | 8995 54 25 36 30 66 21 | 62 36 79 30 41 39
R17 | 5485 39 35 66 24 --- 23 | 38 40 85 39 --- 31
R19 | 3936 55 33 46 24 --- 22 | 133 89 80 105 --- 106
R20 | 2785 41 17 37 22 --- 16 | 70 56 60 59 --- 57
R23 | 1247 51 42 46 41 --- 25 | 27 82 68 96 --- 60
R24 | 3140 25 16 40 20 279 14 | 66 60 70 55 640 58
------+------------------------------------+--------------------------------
RMS | 4122 47 42 61 28 277 |T 73 74 95 73 324 66
WRMS | 4122 45 32 46 28 277 |NE 73 74 95 73 324 66
MEDI | 3140 41 26 41 24 279 |MD 43 56 79 48 291 39
Table 3.1494.4 GPS week: 1494 Day: 4 MJD: 54706
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 508 --- --- --- 508
R04 | 2743 31 23 60 31 --- 19 | 24 40 79 20 --- 33
R06 | 4915 46 17 75 54 --- 25 | 129 88 114 93 --- 96
R07 | 1895 36 26 38 25 --- 17 | 45 44 67 61 --- 39
XR09 |27875 --- --- 9 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1745 53 13 76 38 --- 23 | 32 27 52 47 --- 24
R11 | 1995 46 37 120 47 319 33 | 8 48 127 69 139 39
R13 | 3841 52 15 109 31 --- 28 | 42 42 170 33 --- 37
R14 | 4540 17 14 39 40 --- 15 | 23 18 55 45 --- 22
R15 | 3019 24 14 22 20 70 11 | 27 28 44 31 28 26
R17 | 3299 19 16 171 31 --- 15 | 36 25 139 35 --- 22
R19 | 2522 29 18 46 19 --- 15 | 82 88 80 96 --- 90
R20 | 3366 27 14 35 29 --- 14 | 40 33 60 36 --- 30
R23 | 1407 37 20 56 57 --- 23 | 21 58 80 129 --- 49
R24 | 4675 25 13 25 22 543 11 | 122 116 103 106 431 110
------+------------------------------------+--------------------------------
RMS | 3272 36 20 79 36 366 |T 48 83 90 61 199 80
WRMS | 3272 37 18 48 36 366 |NE 48 83 90 61 199 80
MEDI | 3019 31 15 46 31 319 |MD 36 42 80 47 139 37
Table 3.1494.5 GPS week: 1494 Day: 5 MJD: 54707
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 7 --- --- --- 0 | --- 365 --- --- --- 365
R04 | 1146 27 31 34 22 --- 16 | 51 40 47 38 --- 35
R06 | 4963 55 70 39 39 --- 31 | 235 225 241 230 --- 225
R07 | 3552 26 12 41 29 --- 15 | 30 37 73 30 --- 34
XR09 |18516 --- --- 15 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1388 18 27 38 26 --- 15 | 21 43 40 37 --- 30
R11 | 5442 41 38 54 35 370 23 | 10 52 67 51 92 29
R13 | 2001 13 14 36 22 --- 12 | 32 38 81 25 --- 23
R14 | 3842 20 24 86 32 --- 23 | 15 22 89 30 --- 24
R15 | 3930 20 31 66 29 71 20 | 32 29 81 44 19 33
R17 |10843 29 26 92 34 --- 25 | 25 29 106 32 --- 26
R19 | 1520 15 24 27 22 --- 12 | 97 106 99 107 --- 104
R20 | 3495 17 20 51 22 --- 15 | 27 41 65 52 --- 39
R23 | 2271 40 36 79 38 --- 26 | 38 66 101 132 --- 58
R24 | 7153 23 12 37 25 799 13 | 63 60 56 53 297 53
------+------------------------------------+--------------------------------
RMS | 4745 29 32 56 30 510 |T 52 82 88 66 136 77
WRMS | 4745 27 26 53 30 510 |NE 52 82 88 66 136 77
MEDI | 3552 23 24 39 29 370 |MD 32 41 81 44 92 34
Table 3.1494.6 GPS week: 1494 Day: 6 MJD: 54708
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 7 --- --- --- 0 | --- 335 --- --- --- 333
R04 | 838 31 27 56 33 --- 20 | 59 43 61 21 --- 32
R06 | 7594 47 42 74 145 --- 43 | 308 306 335 310 --- 302
R07 | 4565 24 19 29 33 --- 14 | 27 40 53 39 --- 31
XR09 |48340 --- --- 16 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2234 23 19 26 44 --- 15 | 13 40 43 35 --- 26
R11 | 5162 26 18 64 183 519 24 | 15 26 62 145 181 24
R13 | 2161 42 28 75 71 --- 29 | 32 48 118 36 --- 31
R14 | 1962 16 11 50 26 --- 14 | 24 20 50 37 --- 21
R15 | 4239 22 20 54 43 99 19 | 24 21 62 36 25 20
R17 |10153 31 21 139 57 --- 24 | 25 27 116 53 --- 20
R19 | 784 38 11 66 20 --- 20 | 137 140 148 138 --- 140
R20 | 1511 23 22 46 50 --- 19 | 56 44 57 71 --- 49
R23 | 1894 29 43 120 714 --- 44 | 51 56 105 599 --- 60
R24 | 5919 34 25 49 45 957 20 | 86 84 85 67 434 75
------+------------------------------------+--------------------------------
RMS | 4657 31 25 72 212 631 |T 65 87 99 122 213 83
WRMS | 4657 28 18 55 212 631 |NE 65 87 99 122 213 83
MEDI | 2234 29 20 54 45 519 |MD 32 43 62 53 181 31
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