[IGSREPORT-16956] Wk 1509 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 25 06:37:02 PST 2008
******************************************************************************
IGS Electronic Report 25 Dec 06:37:04 PST 2008 Message Number 16956
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1509 (Dec 07, 2008 - Dec 13, 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 2.1509.
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:
igl1509[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1509 in the SP3 format.
igl15097.sum Combination Report for GPS Week 1509.
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 | 404.1 ns
1 | 348.0 ns
2 | 406.0 ns
3 | 394.0 ns
4 | 390.7 ns
5 | 390.8 ns
6 | 392.3 ns
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 1.1509, 1a.1509).
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 2.1509.0-6)
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 3.1509.0-6).
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 1509 summary. (Dec 07, 2008 - Dec 13, 2008)
Table 1.1509.a GPS week : 1509 MJD: 54807.0-54813.0
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 87| 1 0 18 -3 41 -139 -.00 34 33 | 0 -54 2325 2416
| 3 3 4 37 65 178 .57 | 0 72
cod 243| -3 0 -6 10 -5 22 -.08 21 19 | --- --- --- ---
| 1 2 1 26 44 46 .18 | --- ---
esx 137| -1 0 -8 8 -30 -17 .43 48 40 | 111461 1447 6330 14087
| 2 5 5 60 68 78 .28 | 25518 3494
iac n/a| 4 0 -1 -29 -7 69 -.09 30 30 | 390570 7 6114 14908
| 2 4 8 33 64 73 .17 | 19958 2903
mcc n/a| -5 28 -88 -598 -6 733 -.83 316 316 | --- --- --- ---
| 29 118 256 852 797 3195 1.00 | --- ---
Table 1.1509.b GPS week : 1509 MJD: 54807.0-54813.0
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
------+------------------------------------+------------------------------------------
R04 | 15 19 23 23 25 18 21 |
R06 | 42 18 17 19 18 21 25 |
R07 | 17 15 20 13 12 17 14 |
R10 | 18 21 13 12 18 15 14 |
R11 | 15 17 12 27 23 24 16 |
R13 | 17 24 21 15 14 13 15 |
R14 | 17 19 15 14 21 15 11 |
R15 | 15 13 15 17 21 16 13 |
R17 | 12 15 17 19 14 24 19 |
R18 | 13 12 23 13 16 11 14 |
R19 | 10 11 11 12 11 13 12 |
R20 | 19 14 12 15 26 18 19 |
R21 | 19 17 16 17 14 16 14 |
R22 | 13 30 20 16 20 16 16 |
R23 | 22 22 17 30 25 29 26 |
R24 | 13 22 20 18 17 23 17 |
Table 1.1509.c GPS week : 1509 MJD: 54807.0-54813.0
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 1509 0 | 1 183 -203 251 543 -16280 92.9 4611 4611 | 404138 0
brd 1509 1 | 95 -118 -335 3394 -1581 -20110 95.4 4237 4237 | 347967 0
brd 1509 2 | -49 191 -83 -2149 -3036 -17970 92.3 3450 3450 | 406032 0
brd 1509 3 | -265 -44 -8 -3667 867 -23790 89.6 3665 3665 | 394034 0
brd 1509 4 | 19 -25 118 306 -2123 -23490 88.8 3716 3716 | 390720 0
brd 1509 5 | 58 120 -74 1435 -141 -16190 92.8 3465 3465 | 390837 0
brd 1509 6 | -118 127 12 -56 593 -8488 93.1 2328 2328 | 392348 0
-------------+------------------------------------------------------------+----------------
brd 1509 mean| -36 62 -82 -69 -696 -18045 92.2 3638 3638 | 389439 0
brd 1509 sdev| 122 123 149 2301 1540 5241 2.3 718 718 | 19341 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 2.1509.0 GPS week: 1509 Day: 0 MJD: 54807
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 87| 1 0 17 1 68 62 -.03 23 25 | 0 25 2156 2273
cod 243| -3 5 -5 -36 37 7 -.16 25 19 | --- --- --- ---
esx 137| -3 -3 -2 54 -99 -10 .60 53 38 | 125131 1433 5702 16062
iac n/a| 6 1 -17 -27 -62 -64 -.23 33 33 | 407866 -2213 5749 16646
mcc n/a| 16 30 15 -243 -43 2136 .27 165 165 | --- --- --- ---
Table 2.1509.1 GPS week: 1509 Day: 1 MJD: 54808
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 87| 0 -2 22 27 -1 -190 -.04 26 22 | 0 -130 2665 2792
cod 243| -3 0 -6 -9 -74 -22 -.07 27 26 | --- --- --- ---
esx 137| -3 10 -13 -58 9 56 .43 56 41 | 55580 2791 5778 9615
iac n/a| 3 -3 -7 -35 17 101 .04 27 27 | 347412 -779 5939 11294
mcc n/a| 2 46 41 -430 274 735 -.92 176 176 | --- --- --- ---
Table 2.1509.2 GPS week: 1509 Day: 2 MJD: 54809
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 87| 5 6 21 32 -42 -83 -.14 32 31 | 0 -34 2459 2539
cod 243| -5 -1 -3 23 22 12 -.17 18 17 | --- --- --- ---
esx 137| -2 0 -14 -77 88 -136 .93 53 46 | 130316 1645 6274 10472
iac n/a| 5 2 0 -12 -57 131 -.17 27 27 | 403918 255 6278 11597
mcc n/a| -1 -33 122 123 -45 4174 -1.75 349 349 | --- --- --- ---
Table 2.1509.3 GPS week: 1509 Day: 3 MJD: 54810
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 87| 0 1 21 -63 -33 -86 .29 32 34 | 0 -113 2165 2285
cod 243| -1 -1 -7 43 46 -28 -.12 18 17 | --- --- --- ---
esx 137| 0 -4 -4 83 0 44 .39 49 43 | 118534 5303 7638 12396
iac n/a| 4 8 1 -96 -83 121 -.21 36 36 | 393237 4775 7666 12695
mcc n/a| 22 -8 78 -147 785 2686 -1.02 554 554 | --- --- --- ---
Table 2.1509.4 GPS week: 1509 Day: 4 MJD: 54811
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 87| 2 -2 22 0 88 44 .72 45 46 | 0 47 1838 1919
cod 243| -2 1 -6 21 -13 23 -.28 24 18 | --- --- --- ---
esx 137| 2 -1 -11 13 -43 -119 .35 37 38 | 121297 -3560 5592 19555
iac n/a| 2 -5 3 6 9 44 -.16 31 31 | 395533 -1992 5685 19718
mcc n/a| -47 270 -561 -2410 -1645 -1407 -2.42 376 376 | --- --- --- ---
Table 2.1509.5 GPS week: 1509 Day: 5 MJD: 54812
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 87| 4 -2 11 -47 102 -424 .30 43 37 | 0 -47 2516 2589
cod 243| -3 0 -7 21 -6 71 -.03 20 19 | --- --- --- ---
esx 137| -5 0 -3 49 -104 18 .06 45 41 | 120793 -2702 8111 17970
iac n/a| 7 -1 4 -36 21 130 -.13 30 30 | 394797 -3018 6314 19128
mcc n/a| -47 -113 -335 -849 647 -5351 -.12 453 453 | --- --- --- ---
Table 2.1509.6 GPS week: 1509 Day: 6 MJD: 54813
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 87| -3 0 13 21 108 -301 -1.11 39 36 | 0 -127 2482 2520
cod 243| -1 0 -7 8 -48 95 .29 18 14 | --- --- --- ---
esx 137| 0 2 -7 -8 -61 21 .24 41 32 | 108580 5224 5216 12539
iac n/a| 1 0 7 -1 100 21 .24 28 28 | 391228 3024 5173 13284
mcc n/a| 13 3 20 -234 -17 2159 .12 141 141 | --- --- --- ---
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 3.1509.0 GPS week: 1509 Day: 0 MJD: 54807
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2312 24 15 32 34 --- 14 | 65 66 58 55 --- 58
R06 |15558 27 61 151 26 --- 41 | 114 114 211 124 --- 122
R07 | 1338 21 22 47 30 --- 16 | 43 39 57 54 --- 41
R10E | 4773 20 26 45 37 --- 18 | 39 49 72 53 --- 45
R11E | 4120 16 15 41 35 107 15 | 57 58 82 74 82 63
R13E | 1706 18 13 45 41 --- 16 | 44 49 70 59 --- 47
R14E | 1034 20 18 48 34 --- 16 | 46 53 73 54 --- 50
R15E | 1595 19 24 43 22 208 15 | 46 52 66 41 187 46
R17 | 672 15 19 23 25 --- 11 | 51 61 64 48 --- 51
R18 | 3754 13 20 29 27 --- 12 | 40 60 60 52 --- 49
R19 | 569 12 11 31 19 --- 10 | 57 69 77 60 --- 63
R20 | 537 35 24 23 45 --- 19 | 36 62 62 73 --- 53
R21 | 2897 27 23 57 28 --- 19 | 44 70 83 69 --- 61
R22 | 3828 15 13 31 33 --- 13 | 80 87 113 63 --- 80
R23 | 1320 44 26 33 47 --- 22 | 38 39 51 41 --- 24
R24 | 2163 23 21 25 21 --- 13 | 174 191 187 184 --- 183
------+------------------------------------+--------------------------------
RMS | 4610 23 25 53 33 165 |T 60 69 86 69 134 64
WRMS | 4610 25 19 38 33 165 |NE 65 79 87 73 --- 70
MEDI | 1706 20 20 33 30 107 |MD 46 60 70 55 82 51
Table 3.1509.1 GPS week: 1509 Day: 1 MJD: 54808
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 3527 33 20 60 23 --- 19 | 58 84 114 73 --- 74
R06 |12447 31 29 44 26 --- 18 | 89 108 140 114 --- 104
R07 | 2227 25 24 30 25 --- 14 | 51 52 56 58 --- 50
R10E | 3331 18 35 63 35 --- 21 | 27 31 51 46 --- 27
R11E | 3500 15 31 46 27 118 16 | 31 48 45 36 69 33
R13E | 2046 33 25 71 45 --- 24 | 26 36 87 50 --- 33
R14E | 3581 18 24 42 43 --- 18 | 18 24 56 50 --- 25
R15E | 3199 20 24 26 21 218 13 | 24 35 29 26 409 22
R17 | 712 17 21 40 26 --- 14 | 36 43 52 33 --- 36
R18 | 2929 16 19 36 15 --- 11 | 24 37 25 28 --- 24
R19 | 937 13 17 23 24 --- 11 | 31 44 51 29 --- 33
R20 | 632 22 26 24 22 --- 13 | 25 51 58 52 --- 39
R21 | 2443 16 25 62 20 --- 17 | 32 43 74 27 --- 35
R22 | 3002 25 36 122 22 --- 30 | 19 45 127 23 --- 30
R23 | 2368 32 29 75 14 --- 21 | 23 50 94 40 --- 37
R24 | 5769 51 39 37 17 --- 22 | 123 155 132 130 --- 133
------+------------------------------------+--------------------------------
RMS | 4236 26 27 56 27 176 |T 39 55 74 50 239 45
WRMS | 4236 22 26 41 27 176 |NE 39 58 76 45 --- 45
MEDI | 2929 20 25 42 23 118 |MD 27 44 56 40 69 33
Table 3.1509.2 GPS week: 1509 Day: 2 MJD: 54809
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1730 62 27 28 37 --- 23 | 45 86 65 72 --- 65
R06 |10058 27 22 46 30 --- 16 | 84 106 124 108 --- 101
R07 | 1188 54 17 36 31 --- 19 | 56 61 73 70 --- 60
R10E | 2347 17 13 35 27 --- 12 | 40 48 68 50 --- 45
R11E | 4413 16 12 34 25 209 11 | 43 41 81 56 129 44
R13E | 1156 26 15 86 27 --- 21 | 35 51 85 46 --- 44
R14E | 2851 31 16 35 25 --- 14 | 41 60 76 47 --- 51
R15E | 2137 29 18 34 26 447 14 | 48 42 59 39 266 39
R17 | 1458 32 16 57 25 --- 17 | 65 55 78 40 --- 51
R18 | 2558 21 18 97 24 --- 22 | 37 44 118 57 --- 52
R19 | 935 20 12 19 23 --- 10 | 32 46 53 41 --- 41
R20 | 1891 23 16 28 21 --- 12 | 30 43 60 46 --- 39
R21 | 1119 33 15 49 20 --- 15 | 44 61 86 56 --- 56
R22 | 1014 29 17 77 25 --- 19 | 45 68 99 73 --- 60
R23 | 3178 24 17 66 17 --- 17 | 11 25 95 30 --- 22
R24 | 4511 32 27 53 35 --- 20 | 217 224 246 221 --- 224
------+------------------------------------+--------------------------------
RMS | 3450 32 18 53 27 349 |T 54 66 91 65 197 62
WRMS | 3450 31 17 46 27 349 |NE 60 70 104 70 --- 68
MEDI | 1891 27 16 36 25 209 |MD 43 51 78 50 129 51
Table 3.1509.3 GPS week: 1509 Day: 3 MJD: 54810
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 3219 49 13 71 34 --- 23 | 49 80 126 52 --- 69
R06 | 9732 39 25 47 20 --- 18 | 84 96 101 96 --- 91
R07E | 1500 17 18 26 28 --- 12 | 51 60 71 62 --- 56
R10E | 2940 23 15 17 25 --- 11 | 54 62 62 64 --- 60
R11E | 1608 20 14 101 52 572 27 | 73 76 145 69 204 78
R13E | 1844 22 20 39 25 --- 14 | 47 58 68 51 --- 51
R14E | 4141 32 13 30 25 --- 13 | 45 76 83 80 --- 69
R15E | 5351 27 15 54 31 534 17 | 35 61 85 47 355 53
R17 | 2303 30 13 47 44 --- 18 | 39 43 66 58 --- 43
R18 | 3314 15 10 37 28 --- 12 | 47 56 86 60 --- 57
R19 | 1357 18 18 27 24 --- 12 | 43 55 52 58 --- 50
R20 | 1449 24 24 25 32 --- 15 | 47 72 58 65 --- 59
R21 | 1810 36 14 37 38 --- 17 | 59 60 61 89 --- 64
R22 | 1218 23 9 37 44 --- 16 | 49 54 60 87 --- 58
R23 | 2943 59 23 76 65 --- 30 | 33 28 88 49 --- 22
R24 | 3674 41 26 29 29 --- 18 | 254 286 279 267 --- 274
------+------------------------------------+--------------------------------
RMS | 3665 32 18 49 36 553 |T 63 76 93 78 279 72
WRMS | 3665 34 17 43 36 553 |NE 71 81 93 91 --- 78
MEDI | 2303 24 15 37 29 534 |MD 47 60 71 62 204 58
Table 3.1509.4 GPS week: 1509 Day: 4 MJD: 54811
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 4856 58 38 45 40 --- 25 | 54 82 91 60 --- 61
R06E | 7909 48 24 27 30 --- 18 | 117 134 122 132 --- 127
R07E | 4154 25 17 18 25 --- 12 | 67 79 96 80 --- 80
R10E | 2204 44 18 31 32 --- 17 | 34 64 75 34 --- 48
R11E | 1253 73 23 38 25 --- 22 | 41 100 118 90 --- 89
R13E | 2862 35 17 28 21 --- 14 | 33 52 69 52 --- 48
R14E | 3438 50 28 55 14 --- 21 | 36 68 110 66 --- 66
R15E | 6464 48 30 45 23 376 20 | 33 65 76 57 389 52
R17 | 1661 41 14 25 23 --- 14 | 50 46 50 42 --- 38
R18 | 2882 21 16 49 17 --- 15 | 50 45 92 36 --- 48
R19 | 1528 25 10 18 21 --- 10 | 45 48 59 37 --- 44
R20 | 2400 40 43 28 58 --- 26 | 46 42 94 108 --- 69
R21 | 3173 25 13 32 27 --- 14 | 51 44 42 56 --- 45
R22 | 1929 42 14 59 25 --- 20 | 47 51 86 43 --- 49
R23 | 2628 59 28 24 56 --- 24 | 56 26 40 42 --- 23
R24 | 3078 46 25 30 22 --- 17 | 278 311 301 288 --- 296
------+------------------------------------+--------------------------------
RMS | 3716 45 24 37 31 376 |T 64 78 95 76 389 73
WRMS | 3716 46 18 38 31 376 |NE 77 76 95 81 --- 76
MEDI | 2862 42 18 30 25 376 |MD 47 52 86 56 389 49
Table 3.1509.5 GPS week: 1509 Day: 5 MJD: 54812
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 6078 47 15 51 21 --- 18 | 51 66 103 56 --- 62
R06E | 4375 63 25 40 17 --- 20 | 74 121 128 105 --- 108
R07E | 2802 43 27 22 27 --- 17 | 68 73 63 65 --- 64
R10 | 2088 39 10 25 30 --- 14 | 60 63 54 71 --- 62
R11 | 1550 63 24 54 34 --- 23 | 60 111 144 70 --- 92
R13E | 2315 28 15 30 22 --- 12 | 40 55 83 55 --- 54
R14 | 1834 45 10 29 25 --- 15 | 59 91 88 98 --- 83
R15 | 6217 39 16 26 34 453 16 | 43 67 63 67 331 58
R17 | 1613 50 23 52 50 --- 24 | 45 36 44 39 --- 33
R18 | 905 15 10 40 14 --- 11 | 49 45 44 45 --- 42
R19 | 1135 23 18 26 25 --- 13 | 41 29 55 46 --- 36
R20 | 3424 30 24 21 41 --- 17 | 39 49 52 62 --- 49
R21 | 2847 21 13 48 30 --- 15 | 44 43 73 60 --- 49
R22 | 3755 37 20 34 25 --- 15 | 50 52 45 51 --- 44
R23 | 4555 36 30 96 42 --- 28 | 35 37 95 33 --- 22
R24 | 3820 67 21 61 21 --- 23 | 246 283 310 277 --- 278
------+------------------------------------+--------------------------------
RMS | 3465 43 20 45 30 453 |T 62 76 90 75 331 71
WRMS | 3465 37 19 41 30 453 |NE 68 71 89 76 --- 69
MEDI | 2802 39 18 34 25 453 |MD 49 55 63 60 331 54
Table 3.1509.6 GPS week: 1509 Day: 6 MJD: 54813
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2184 40 30 45 38 --- 21 | 72 79 82 66 --- 71
R06E | 1268 41 28 68 39 --- 24 | 126 144 167 146 --- 142
R07E | 1862 39 13 23 22 --- 13 | 94 98 114 106 --- 101
R10 | 3288 40 10 29 22 --- 13 | 48 54 72 52 --- 55
R11 | 1166 51 17 17 28 161 16 | 88 114 121 108 248 107
R13 | 1411 47 16 18 25 --- 15 | 50 73 82 71 --- 69
R14 | 2763 27 13 24 19 --- 11 | 48 61 73 62 --- 58
R15 | 1727 25 14 30 25 118 13 | 33 41 41 40 344 34
R17 | 900 34 16 49 35 --- 18 | 70 69 104 55 --- 67
R18 | 2126 35 12 38 15 --- 13 | 74 67 71 63 --- 64
R19 | 1446 32 11 17 24 --- 11 | 74 61 67 69 --- 61
R20 | 1222 35 20 54 28 --- 18 | 57 62 93 59 --- 58
R21 | 3080 32 13 36 20 --- 13 | 61 60 88 67 --- 62
R22 | 3172 37 19 30 30 --- 16 | 65 75 83 76 --- 72
R23 | 2157 54 31 72 34 --- 26 | 67 51 77 31 --- 31
R24 | 4352 40 13 44 26 --- 16 | 254 270 281 256 --- 264
------+------------------------------------+--------------------------------
RMS | 2328 39 18 41 28 141 |T 80 86 101 82 296 82
WRMS | 2328 36 14 32 28 141 |NE 90 89 108 84 --- 84
MEDI | 1862 37 14 30 25 118 |MD 67 67 82 66 248 64
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