[IGSREPORT-16974] Wk 1510 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jan 1 04:42:14 PST 2009
******************************************************************************
IGS Electronic Report 01 Jan 04:42:17 PST 2009 Message Number 16974
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1510 (Dec 14, 2008 - Dec 20, 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 2.1510.
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:
igl1510[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1510 in the SP3 format.
igl15107.sum Combination Report for GPS Week 1510.
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 | 390.0 ns
1 | 336.4 ns
2 | 382.1 ns
3 | 383.9 ns
4 | 370.2 ns
5 | 366.9 ns
6 | 329.8 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 1.1510, 1a.1510).
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 2.1510.0-6)
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 3.1510.0-6).
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 1510 summary. (Dec 14, 2008 - Dec 20, 2008)
Table 1.1510.a GPS week : 1510 MJD: 54814.0-54820.0
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 88| 2 -1 12 14 14 -94 -.12 30 27 | 0 -48 2384 2444
| 1 1 1 20 35 111 .28 | 0 158
cod 247| -3 1 -5 -5 0 23 -.07 18 15 | --- --- --- ---
| 1 1 3 25 17 38 .04 | --- ---
esx 130| 0 0 -5 -6 0 25 .45 32 27 | 90217 -1730 7292 14116
| 3 2 1 34 47 50 .14 | 19951 6290
iac n/a| 4 -1 3 10 -10 21 -.22 32 32 | 366444 -1497 7182 13866
| 1 2 9 34 30 82 .14 | 24195 5324
mcc n/a| 5 5 21 -14 33 1372 -.05 97 97 | --- --- --- ---
| 14 12 8 110 164 424 .48 | --- ---
Table 1.1510.b GPS week : 1510 MJD: 54814.0-54820.0
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 | 18 14 17 20 20 17 20 |
R06 | 13 21 19 17 14 15 16 |
R07 | 19 20 18 15 17 20 19 |
R10 | 16 13 14 11 10 11 11 |
R11 | 11 16 13 15 10 10 13 |
R13 | 10 10 15 12 9 9 14 |
R14 | 12 11 14 9 13 11 13 |
R15 | 12 10 18 14 14 10 13 |
R17 | 15 15 14 14 14 13 15 |
R18 | 14 11 16 16 16 21 11 |
R19 | 15 11 13 13 12 11 10 |
R20 | 17 16 17 17 20 14 15 |
R21 | 13 26 19 12 14 14 13 |
R22 | 13 10 17 15 9 17 15 |
R23 | 21 15 20 15 27 22 23 |
R24 | 23 25 24 20 21 14 20 |
Table 1.1510.c GPS week : 1510 MJD: 54814.0-54820.0
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 1510 0 | -187 -167 4 -957 -1191 -8461 90.0 2545 2545 | 389977 0
brd 1510 1 | 83 -84 -255 -1639 -3540 -12340 85.5 2638 2638 | 336373 0
brd 1510 2 | 74 57 -322 -351 -3684 -13260 91.9 3400 3400 | 382082 0
brd 1510 3 | -64 -25 71 -1079 5053 -19950 91.8 4091 4091 | 383909 0
brd 1510 4 | 83 74 115 -1529 4322 -22260 91.0 5046 5046 | 370237 0
brd 1510 5 | 31 61 354 -284 1872 -27250 93.0 4593 4593 | 366935 0
brd 1510 6 | 233 247 599 1968 2359 -25400 97.1 3434 3434 | 329769 0
-------------+------------------------------------------------------------+----------------
brd 1510 mean| 36 23 81 -553 741 -18417 91.5 3678 3678 | 365611 0
brd 1510 sdev| 132 132 323 1227 3581 7147 3.5 947 947 | 23673 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 2.1510.0 GPS week: 1510 Day: 0 MJD: 54814
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 88| 4 -1 10 14 -14 80 -.72 36 30 | 0 -120 2434 2503
cod 247| -1 3 -9 0 -29 -14 -.01 20 17 | --- --- --- ---
esx 130| -5 0 -3 -40 50 -73 .56 30 25 | 111439 -4924 6338 13213
iac n/a| 3 -4 12 56 1 -6 .05 25 25 | 392324 -4911 6215 12995
mcc n/a| -12 -1 24 -42 55 1370 -.14 115 115 | --- --- --- ---
Table 2.1510.1 GPS week: 1510 Day: 1 MJD: 54815
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 88| 4 -3 11 -16 -17 -10 .15 31 26 | 0 -143 1982 2022
cod 247| -1 2 -11 16 10 -12 -.01 16 13 | --- --- --- ---
esx 130| -1 -1 -6 48 -6 64 .20 40 31 | 71147 -524 6228 13799
iac n/a| 4 0 13 -14 -27 -38 -.21 28 28 | 337865 8 5996 13788
mcc n/a| 16 -13 36 -46 -274 1305 .71 105 105 | --- --- --- ---
Table 2.1510.2 GPS week: 1510 Day: 2 MJD: 54816
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 88| 1 -2 14 6 58 -190 -.03 33 30 | 0 1 2578 2661
cod 247| -3 2 -4 -15 -9 88 -.08 19 15 | --- --- --- ---
esx 130| 2 3 -4 22 -83 18 .50 32 30 | 103141 -9991 9011 14928
iac n/a| 6 -2 -1 -28 26 -95 -.40 38 38 | 387432 -6928 9009 14742
mcc n/a| 4 -1 28 -48 9 1871 .12 96 96 | --- --- --- ---
Table 2.1510.3 GPS week: 1510 Day: 3 MJD: 54817
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 88| 3 -2 13 38 70 -66 -.04 24 23 | 0 -161 2462 2529
cod 247| -4 2 0 -49 0 48 -.10 15 14 | --- --- --- ---
esx 130| 4 -1 -3 -21 -19 7 .54 33 26 | 102150 -4094 5582 12206
iac n/a| 2 0 -11 54 22 0 -.30 37 37 | 382887 -4898 5421 12691
mcc n/a| 26 10 11 -61 180 1789 -.49 90 90 | --- --- --- ---
Table 2.1510.4 GPS week: 1510 Day: 4 MJD: 54818
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 88| 1 0 11 -2 -2 -256 -.04 30 29 | 0 160 2466 2519
cod 247| -4 0 -3 15 -10 45 -.07 18 16 | --- --- --- ---
esx 130| 1 0 -5 -17 51 27 .39 33 28 | 90846 9784 11202 17116
iac n/a| 4 0 0 1 -15 132 -.21 29 29 | 366083 8816 11109 15234
mcc n/a| 18 20 12 167 157 1618 -.48 102 102 | --- --- --- ---
Table 2.1510.5 GPS week: 1510 Day: 5 MJD: 54819
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 88| 1 0 12 22 16 -130 -.16 25 23 | 0 -235 2457 2528
cod 247| -3 1 -6 -23 16 0 -.12 17 12 | --- --- --- ---
esx 130| 4 3 -6 9 -13 72 .62 30 26 | 97408 -4245 6519 12680
iac n/a| 3 0 1 22 -21 119 -.20 35 35 | 368289 -3367 6350 12267
mcc n/a| -2 22 18 -167 173 848 -.50 101 101 | --- --- --- ---
Table 2.1510.6 GPS week: 1510 Day: 6 MJD: 54820
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 88| 1 -2 12 37 -10 -87 -.02 30 27 | 0 161 2314 2351
cod 247| -1 0 -5 17 20 11 -.08 18 16 | --- --- --- ---
esx 130| -2 2 -7 -44 25 63 .36 29 26 | 55390 1884 6166 14875
iac n/a| 3 -4 11 -16 -59 40 -.30 33 33 | 330228 801 6176 15345
mcc n/a| -8 2 19 94 -69 807 .40 72 72 | --- --- --- ---
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 3.1510.0 GPS week: 1510 Day: 0 MJD: 54814
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2433 40 26 33 27 --- 18 | 43 54 54 51 --- 46
R06E | 4461 22 21 29 18 --- 13 | 65 75 91 73 --- 73
R07E | 2018 45 19 37 32 --- 18 | 37 43 56 43 --- 38
R10 | 2875 26 14 48 21 --- 16 | 30 37 50 46 --- 36
R11 | 2006 25 14 20 21 112 11 | 27 24 35 28 45 23
R13 | 793 17 14 16 20 --- 9 | 32 31 30 27 --- 27
R14 | 3950 15 18 17 27 --- 11 | 24 30 28 37 --- 27
R15 | 1786 31 14 14 20 118 11 | 25 30 39 44 36 32
R17 | 1033 20 16 32 34 --- 15 | 61 65 90 60 --- 66
R18 | 2151 30 11 36 17 --- 13 | 57 54 80 51 --- 56
R19 | 1855 36 15 38 18 --- 15 | 61 61 66 54 --- 54
R20 | 1347 43 15 27 35 --- 17 | 51 55 60 77 --- 56
R21 | 1537 20 18 29 22 --- 13 | 61 71 85 88 --- 71
R22 | 2624 31 19 21 18 --- 12 | 62 84 78 70 --- 73
R23 | 3310 52 26 35 38 --- 21 | 49 36 54 40 --- 32
R24 | 3289 72 38 19 22 --- 23 | 163 190 188 173 --- 176
------+------------------------------------+--------------------------------
RMS | 2544 36 20 30 25 115 |T 53 58 67 60 40 55
WRMS | 2544 30 17 25 25 115 |NE 54 59 67 61 40 56
MEDI | 2018 30 16 29 21 112 |MD 49 54 56 51 36 46
Table 3.1510.1 GPS week: 1510 Day: 1 MJD: 54815
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR04E | 3520 --- 14 25 21 --- 13 | --- 48 59 49 --- 47
R06E | 6692 38 20 59 34 --- 21 | 47 57 97 68 --- 58
R07E | 1517 31 19 48 44 --- 19 | 42 55 76 63 --- 51
R10 | 2479 23 10 31 30 --- 13 | 25 27 46 50 --- 30
R11 | 2280 22 26 38 18 89 15 | 19 27 39 23 37 21
R13 | 905 15 12 17 22 --- 9 | 22 28 43 26 --- 27
R14 | 3256 22 12 21 21 --- 10 | 25 28 38 31 --- 27
R15 | 2097 25 9 11 24 119 10 | 19 27 24 40 39 24
R17 | 1295 28 17 33 29 --- 14 | 40 59 81 38 --- 50
R18 | 2324 17 13 31 20 --- 11 | 22 38 48 22 --- 28
R19 | 1748 21 11 27 16 --- 10 | 27 37 49 28 --- 32
R20 | 2175 39 12 22 38 --- 16 | 15 34 29 35 --- 24
R21 | 994 20 15 95 36 --- 25 | 40 51 88 44 --- 43
R22 | 2079 16 13 23 18 --- 9 | 47 57 61 37 --- 50
R23 | 1577 36 15 25 31 --- 15 | 29 32 42 27 --- 23
R24 | 2722 71 29 47 25 --- 25 | 85 155 167 134 --- 135
------+------------------------------------+--------------------------------
RMS | 2637 31 16 40 28 105 |T 33 47 61 44 38 41
WRMS | 2637 26 13 31 28 105 |NE 31 46 58 41 38 39
MEDI | 2097 23 13 27 24 89 |MD 27 37 48 37 37 30
Table 3.1510.2 GPS week: 1510 Day: 2 MJD: 54816
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2741 42 22 19 35 --- 17 | 102 81 83 78 --- 79
R06E | 7016 28 26 50 26 --- 19 | 48 66 99 73 --- 66
R07E | 2818 26 19 29 54 --- 18 | 37 30 38 64 --- 32
R10 | 1367 23 14 27 34 --- 13 | 26 39 62 49 --- 39
R11 | 2976 23 16 30 24 101 13 | 19 32 49 26 53 25
R13 | 1108 15 12 33 40 --- 14 | 26 30 44 27 --- 26
R14 | 1253 16 13 21 44 --- 13 | 28 24 39 48 --- 29
R15 | 2348 29 16 30 55 91 18 | 18 30 54 39 43 30
R17 | 1889 19 15 28 37 --- 14 | 60 58 67 34 --- 52
R18 | 682 19 19 28 43 --- 15 | 26 49 55 36 --- 36
R19 | 839 38 9 26 17 --- 13 | 22 44 64 60 --- 44
R20 | 1582 36 13 33 36 --- 16 | 20 35 43 52 --- 30
R21 | 2941 39 8 19 59 --- 18 | 26 56 53 102 --- 54
R22 | 866 40 14 39 21 --- 16 | 37 66 96 71 --- 65
R23 | 1753 35 28 48 21 --- 19 | 32 44 60 39 --- 31
R24 | 9027 60 34 32 35 --- 23 | 183 208 195 188 --- 193
------+------------------------------------+--------------------------------
RMS | 3399 33 19 32 38 96 |T 44 55 68 61 48 51
WRMS | 3399 30 15 30 38 96 |NE 40 55 67 59 48 50
MEDI | 1753 28 15 29 35 91 |MD 26 44 55 49 43 36
Table 3.1510.3 GPS week: 1510 Day: 3 MJD: 54817
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2358 34 23 48 40 --- 20 | 103 116 122 109 --- 112
R06E | 8402 25 10 50 37 --- 17 | 42 53 95 62 --- 57
R07E | 3582 23 16 32 38 --- 14 | 73 69 83 79 --- 70
R10 | 1276 14 17 20 25 --- 10 | 29 39 39 40 --- 32
R11 | 2721 18 12 41 32 62 14 | 23 34 55 30 36 29
R13 | 1994 18 12 33 22 --- 12 | 22 31 46 27 --- 26
R14 | 2868 19 8 16 24 --- 9 | 26 39 40 41 --- 33
R15 | 2026 28 5 13 49 111 14 | 22 32 33 42 87 28
R17 | 2404 23 21 30 24 --- 13 | 57 46 75 61 --- 54
R18 | 1333 10 26 46 17 --- 15 | 39 58 47 49 --- 43
R19 | 1730 31 15 16 28 --- 13 | 28 62 56 70 --- 52
R20 | 2031 26 10 14 65 --- 17 | 29 40 42 99 --- 44
R21 | 3071 20 8 19 36 --- 11 | 33 42 67 80 --- 48
R22 | 1711 24 15 32 34 --- 14 | 42 66 57 83 --- 57
R23 | 3422 25 14 35 39 --- 15 | 22 34 57 23 --- 29
R24 |10706 34 18 42 49 --- 19 | 78 74 112 131 --- 88
------+------------------------------------+--------------------------------
RMS | 4090 24 15 33 37 90 |T 41 52 64 64 61 50
WRMS | 4090 23 14 26 37 90 |NE 34 45 55 59 61 43
MEDI | 2358 23 14 32 34 62 |MD 29 42 56 61 36 44
Table 3.1510.4 GPS week: 1510 Day: 4 MJD: 54818
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 4950 45 26 39 30 --- 19 | 41 51 77 58 --- 50
R06E | 9990 21 19 34 22 --- 13 | 45 54 76 64 --- 54
R07E | 1136 37 16 35 34 --- 17 | 38 45 57 62 --- 44
R10 | 1667 18 13 18 19 --- 9 | 38 36 39 32 --- 34
R11 | 2182 13 11 27 18 102 10 | 32 27 36 26 30 26
R13 | 2506 15 12 16 21 --- 9 | 36 36 39 30 --- 32
R14 | 3549 25 7 35 18 --- 12 | 42 31 40 31 --- 31
R15 | 3970 23 15 30 27 102 13 | 36 33 37 40 41 32
R17 | 1912 23 26 27 18 --- 14 | 56 47 53 46 --- 45
R18 | 933 22 19 41 26 --- 15 | 44 43 80 50 --- 49
R19 | 2261 24 13 23 20 --- 11 | 42 59 66 51 --- 53
R20 | 4226 46 15 13 54 --- 20 | 41 47 55 89 --- 53
R21 | 2778 17 15 36 28 --- 13 | 32 44 33 47 --- 34
R22 | 2877 15 14 15 18 --- 9 | 39 50 50 43 --- 44
R23 | 3879 52 28 60 49 --- 26 | 32 29 60 33 --- 23
R24 |13452 46 24 47 33 --- 21 | 125 142 173 150 --- 142
------+------------------------------------+--------------------------------
RMS | 5045 30 18 33 29 102 |T 44 48 60 53 35 46
WRMS | 5045 29 16 28 29 102 |NE 45 48 58 51 35 46
MEDI | 2778 23 15 30 22 102 |MD 39 44 53 46 30 44
Table 3.1510.5 GPS week: 1510 Day: 5 MJD: 54819
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 4052 36 24 24 36 --- 17 | 80 81 80 84 --- 78
R06E |11239 25 15 37 30 --- 15 | 31 42 67 44 --- 40
R07E | 1952 38 26 30 45 --- 19 | 61 60 65 76 --- 60
R10 | 1869 15 9 22 33 --- 11 | 30 31 47 43 --- 33
R11 | 1697 15 7 25 20 110 9 | 27 22 37 24 24 22
R13 | 1443 16 9 13 24 --- 8 | 20 25 25 25 --- 20
R14 | 1511 15 14 26 23 --- 11 | 25 32 33 34 --- 25
R15 | 4909 15 11 21 26 92 10 | 22 21 22 26 39 19
R17 | 1659 14 19 21 37 --- 13 | 23 35 38 30 --- 28
R18 | 1060 22 34 52 35 --- 21 | 37 32 64 16 --- 26
R19 | 1864 22 6 26 25 --- 11 | 29 35 52 46 --- 37
R20 | 3576 31 12 24 28 --- 13 | 35 56 69 62 --- 51
R21 | 3808 28 15 31 27 --- 14 | 24 47 46 51 --- 37
R22 | 4832 26 10 47 30 --- 16 | 25 38 75 22 --- 37
R23 | 2057 32 22 22 74 --- 22 | 23 31 29 54 --- 20
R24 | 9690 25 14 26 35 --- 13 | 175 180 165 211 --- 179
------+------------------------------------+--------------------------------
RMS | 4593 25 17 30 35 101 |T 41 48 57 53 31 44
WRMS | 4593 23 12 26 35 101 |NE 38 45 54 49 31 41
MEDI | 1952 22 14 25 30 92 |MD 27 35 47 43 24 33
Table 3.1510.6 GPS week: 1510 Day: 6 MJD: 54820
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2419 41 19 39 38 --- 19 | 72 120 127 85 --- 104
R06E | 8377 32 18 29 33 --- 15 | 53 68 85 67 --- 66
R07E | 2749 41 27 26 35 --- 18 | 47 55 55 68 --- 52
R10 | 1711 20 11 26 23 --- 11 | 40 36 50 42 --- 38
R11 | 1189 17 9 28 36 88 13 | 37 29 32 30 29 29
R13 | 984 26 15 27 29 --- 13 | 34 29 45 42 --- 33
R14 | 1699 18 12 20 38 --- 12 | 39 33 42 50 --- 36
R15 | 2180 23 15 29 27 51 13 | 37 39 39 40 44 36
R17 | 1843 33 21 29 23 --- 15 | 42 61 63 51 --- 53
R18 | 1735 24 19 18 15 --- 11 | 42 50 56 46 --- 46
R19 | 1923 21 9 21 17 --- 9 | 45 66 75 58 --- 60
R20 | 3744 18 16 17 47 --- 14 | 46 70 58 86 --- 63
R21 | 3985 30 13 19 30 --- 13 | 44 69 77 94 --- 68
R22 | 3526 27 21 34 18 --- 15 | 58 85 82 83 --- 75
R23 | 2798 44 27 35 58 --- 23 | 43 50 60 56 --- 45
R24 | 5643 43 20 44 36 --- 20 | 218 217 217 233 --- 217
------+------------------------------------+--------------------------------
RMS | 3434 30 18 29 33 72 |T 56 67 72 70 36 63
WRMS | 3434 27 16 26 33 72 |NE 55 64 68 70 36 61
MEDI | 2180 26 16 27 30 51 |MD 43 55 58 56 29 52
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