[IGSREPORT-16849] Wk 1504 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Nov 20 07:16:30 PST 2008
******************************************************************************
IGS Electronic Report 20 Nov 07:16:33 PST 2008 Message Number 16849
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1504 (Nov 02, 2008 - Nov 08, 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 2.1504.
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:
igl1504[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1504 in the SP3 format.
igl15047.sum Combination Report for GPS Week 1504.
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 | 512.1 ns
1 | 558.3 ns
2 | 553.5 ns
3 | 521.0 ns
4 | 487.9 ns
5 | 489.9 ns
6 | 539.6 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 | R18
2 | BKG | R21
2 | ESX | R04
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 1.1504, 1a.1504).
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 2.1504.0-6)
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 3.1504.0-6).
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 1504 summary. (Nov 02, 2008 - Nov 08, 2008)
Table 1.1504.a GPS week : 1504 MJD: 54772.0-54778.0
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 65| 1 0 -4 -17 23 -75 -.06 36 33 | 0 -158 2618 2748
| 2 2 6 38 35 119 .05 | 0 138
cod 242| -2 0 0 9 4 41 -.11 24 21 | --- --- --- ---
| 2 1 4 41 37 35 .05 | --- ---
esx 125| 3 0 -1 13 6 42 .39 46 36 | 126055 6199 8606 25484
| 2 4 5 38 28 94 .08 | 25345 11228
iac n/a| 1 0 3 -23 -14 -1 -.08 26 26 | 524724 531 7827 14064
| 1 2 6 25 33 42 .06 | 31090 7568
mcc n/a| -34 25 76 -400 429 1127 1.06 502 502 | --- --- --- ---
| 84 66 101 840 601 2816 2.24 | --- ---
Table 1.1504.b GPS week : 1504 MJD: 54772.0-54778.0
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 | 19 16 20 14 11 15 9 |
R06 | 17 22 24 35 20 18 29 |
R07 | 17 17 12 13 12 20 13 |
R09 | 0 0 0 --- --- --- 0 |
R10 | 14 16 16 23 27 20 13 |
R11 | 14 19 12 14 17 17 16 |
R13 | 18 20 11 13 18 16 16 |
R14 | 18 18 12 12 12 13 13 |
R15 | 16 26 17 30 16 13 14 |
R17 | 18 20 17 13 22 14 21 |
R18 | 16 21 14 11 25 11 15 |
R19 | 11 14 16 23 9 11 13 |
R20 | 16 13 16 15 12 10 13 |
R21 | 130 73 129 48 15 15 13 |
R22 | --- --- --- --- 0 0 173 |
R23 | 0 180 54 35 23 20 17 |
R24 | 16 17 15 20 13 11 15 |
Table 1.1504.c GPS week : 1504 MJD: 54772.0-54778.0
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 1504 0 | 87 155 298 1717 717 -6298 92.6 9435 9435 | 512101 0
brd 1504 1 | -179 -46 66 -8569 -1497 -8219 88.8 9750 9750 | 558348 0
brd 1504 2 | -229 -139 -169 33 -2624 -19520 97.1 5947 5947 | 553514 0
brd 1504 3 | -15 20 132 -2496 -1982 -18210 87.0 5943 5943 | 520973 0
brd 1504 4 | -55 -320 3 1877 2230 -19290 93.6 5926 5926 | 487946 0
brd 1504 5 | 27 -114 96 -696 -453 -7169 96.9 5235 5235 | 489876 0
brd 1504 6 | -165 80 -201 -842 82 -7912 96.7 5301 5301 | 539564 0
-------------+------------------------------------------------------------+----------------
brd 1504 mean| -75 -51 32 -1282 -503 -12374 93.2 6791 6791 | 523188 0
brd 1504 sdev| 118 157 174 3554 1682 6246 4.1 1939 1939 | 28587 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 2.1504.0 GPS week: 1504 Day: 0 MJD: 54772
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 65| -2 0 5 -21 47 -162 -.09 27 26 | 0 -65 2444 2580
cod 242| -3 -1 3 -52 -19 81 -.03 22 22 | --- --- --- ---
esx 125| 3 3 -4 -1 27 125 .28 66 41 | 103777 199 6917 29512
iac n/a| 2 0 -4 3 -21 4 -.01 24 24 | 515114 -1238 5606 11953
mcc n/a| 7 13 11 -21 -40 583 -.22 180 180 | --- --- --- ---
Table 2.1504.1 GPS week: 1504 Day: 1 MJD: 54773
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 65| -2 2 0 18 -46 -243 -.06 33 31 | 0 -195 3388 3628
cod 242| 1 0 4 78 55 45 -.14 28 25 | --- --- --- ---
esx 125| 5 3 -6 -25 21 176 .44 39 33 | 143855 18619 8649 27179
iac n/a| 3 -2 -2 -27 -71 40 -.18 30 30 | 561611 3469 8199 18688
mcc n/a| -145 128 9 -914 1263 -3605 2.13 563 563 | --- --- --- ---
Table 2.1504.2 GPS week: 1504 Day: 2 MJD: 54774
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 65| 1 0 1 -33 10 84 .02 33 26 | 0 -384 2962 3110
cod 242| -2 2 1 29 54 -17 -.19 20 20 | --- --- --- ---
esx 125| 1 -5 -3 23 -22 -33 .46 52 33 | 153317 -10747 10165 36090
iac n/a| 2 0 4 -7 -15 -7 -.07 28 28 | 562847 -11909 7778 13328
mcc n/a| -17 -15 125 -11 -207 957 2.82 479 479 | --- --- --- ---
Table 2.1504.3 GPS week: 1504 Day: 3 MJD: 54775
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 65| 5 1 -4 -1 59 64 -.05 49 41 | 0 -270 2616 2673
cod 242| -3 0 -5 -11 -28 2 -.10 31 19 | --- --- --- ---
esx 125| 1 -4 -1 -32 -29 -66 .33 50 41 | 124784 6298 6252 23672
iac n/a| 2 3 13 -9 26 25 .01 38 38 | 516951 1706 6241 13619
mcc n/a| -56 -72 167 933 110 4592 4.01 483 483 | --- --- --- ---
Table 2.1504.4 GPS week: 1504 Day: 4 MJD: 54776
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 65| 2 -4 -12 -31 37 -65 -.06 39 37 | 0 33 1985 2074
cod 242| -5 1 -4 -13 -23 72 -.08 24 25 | --- --- --- ---
esx 125| 5 -1 0 46 -16 5 .43 44 36 | 94961 20711 14869 19405
iac n/a| 0 0 8 -23 20 -45 -.09 22 22 | 486009 13355 14889 18622
mcc n/a| 119 43 222 -1175 1002 4510 -1.36 572 572 | --- --- --- ---
Table 2.1504.5 GPS week: 1504 Day: 5 MJD: 54777
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 65| 0 0 -11 -84 37 -64 -.13 34 36 | 0 -84 2428 2583
cod 242| -3 0 -2 23 -21 48 -.11 22 18 | --- --- --- ---
esx 125| 0 6 9 76 23 113 .30 33 28 | 105511 -1327 5905 13914
iac n/a| 2 -2 4 -75 -2 -68 -.09 20 20 | 491234 -2785 5914 10689
mcc n/a| -101 82 67 -1503 898 -50 1.94 774 774 | --- --- --- ---
Table 2.1504.6 GPS week: 1504 Day: 6 MJD: 54778
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 65| 1 -2 -6 30 19 -145 -.03 37 30 | 0 -143 2506 2590
cod 242| 0 0 2 16 15 55 -.10 19 17 | --- --- --- ---
esx 125| 4 0 -3 9 42 -25 .46 37 37 | 156181 9643 7487 28616
iac n/a| 0 -2 4 -26 -38 39 -.10 22 22 | 539305 1120 6162 11553
mcc n/a| -44 -3 -69 -108 -15 902 -1.92 460 460 | --- --- --- ---
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 3.1504.0 GPS week: 1504 Day: 0 MJD: 54772
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |18671 30 25 47 28 --- 18 | 46 64 52 48 --- 50
R06 |22129 40 24 31 19 --- 16 | 210 248 243 237 --- 234
R07 | 2057 33 19 39 26 --- 16 | 27 33 42 27 --- 25
XR09 |14756 --- --- 9 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 3578 20 28 17 27 --- 14 | 58 58 51 63 --- 55
R11 | 3465 28 16 29 22 140 13 | 39 44 45 46 378 38
R13 |11912 32 24 43 28 --- 17 | 47 50 66 56 --- 44
R14 | 2091 21 23 44 33 --- 17 | 34 41 51 35 --- 30
R15 | 2997 18 17 43 34 102 16 | 49 46 64 72 325 54
R17 | 6044 24 25 50 23 --- 17 | 52 46 96 61 --- 56
R18 | 9039 20 24 198 22 --- 16 | 56 53 177 65 --- 57
R19 | 2420 17 14 30 14 --- 10 | 27 37 61 49 --- 38
R20 | 2568 30 28 33 15 --- 15 | 60 29 52 43 --- 39
XR21 |13739 --- 120 --- 140 --- 130 | --- 195 --- 216 --- 175
XR23 | 6091 --- 6 --- --- --- 0 | --- 209 --- --- --- 208
R24 | 1989 29 18 43 18 258 15 | 74 69 71 63 150 65
------+------------------------------------+--------------------------------
RMS | 9435 27 22 66 24 180 |T 59 81 82 77 284 77
WRMS | 9435 26 22 41 24 180 |NE 69 98 99 89 150 94
MEDI | 3578 28 24 39 23 140 |MD 49 50 61 56 325 54
Table 3.1504.1 GPS week: 1504 Day: 1 MJD: 54773
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |22455 33 17 36 27 --- 16 | 36 44 74 40 --- 40
R06 |20499 48 26 43 33 --- 21 | 321 325 349 347 --- 333
R07 | 3237 32 25 30 27 --- 16 | 38 36 32 29 --- 24
XR09 |11473 --- --- 13 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 3324 35 12 28 31 --- 15 | 21 40 44 48 --- 35
R11 | 4047 14 24 36 46 811 18 | 15 31 39 32 311 22
R13 |11600 44 32 29 30 --- 20 | 41 38 54 45 --- 35
R14 | 2122 27 33 37 23 --- 17 | 22 31 54 27 --- 26
R15 | 4303 26 45 73 30 496 26 | 29 31 91 57 288 35
R17 | 5888 25 45 38 26 --- 20 | 53 37 79 50 --- 48
R18 | 8258 30 26 54 37 --- 21 | 39 37 105 50 --- 41
R19 | 1309 32 17 25 21 --- 14 | 35 44 53 38 --- 34
R20 | 2322 18 18 30 24 --- 13 | 21 34 57 41 --- 29
XR21 |15031 --- 66 --- 79 --- 72 | --- 194 --- 170 --- 167
XR23 |11550 --- 165 --- 194 --- 179 | --- 266 --- 119 --- 227
R24 | 2425 41 16 29 25 220 16 | 43 45 65 39 358 40
------+------------------------------------+--------------------------------
RMS | 9749 32 28 39 30 563 |T 54 82 84 75 319 75
WRMS | 9749 31 25 33 30 563 |NE 73 106 101 92 358 98
MEDI | 4303 32 26 30 30 496 |MD 36 38 57 45 311 35
Table 3.1504.2 GPS week: 1504 Day: 2 MJD: 54774
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 8679 19 26 165 36 --- 20 | 40 39 92 55 --- 42
R06 |16464 73 24 38 25 --- 24 | 154 210 218 194 --- 196
R07 | 2829 19 17 20 27 --- 12 | 36 27 32 35 --- 25
XR09 |15900 --- --- 8 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2219 31 20 31 27 --- 15 | 61 47 64 58 --- 52
R11 | 1961 20 11 24 27 509 12 | 29 28 41 35 190 30
R13 | 4738 17 14 21 19 --- 10 | 51 45 44 45 --- 42
R14 | 1700 15 15 19 32 --- 12 | 40 36 46 48 --- 39
R15 | 5531 30 28 24 35 485 17 | 60 66 54 79 209 60
R17 | 4913 26 22 45 18 --- 17 | 46 39 82 34 --- 46
R18 | 2302 39 17 15 24 --- 14 | 73 46 67 55 --- 55
R19 | 1495 34 23 20 31 --- 15 | 48 42 46 57 --- 42
R20 | 1889 41 14 23 31 --- 16 | 54 35 31 23 --- 29
XR21 |12684 318 109 --- 151 --- 128 | 124 302 --- 170 --- 237
XR23 |13375 --- 46 --- 63 --- 54 | --- 133 --- 101 --- 108
R24 | 2330 27 26 23 26 441 15 | 60 51 71 59 216 54
------+------------------------------------+--------------------------------
RMS | 5947 33 20 52 28 479 |T 62 76 68 69 205 70
WRMS | 5947 26 20 33 28 479 |NE 70 92 79 78 216 83
MEDI | 2829 27 22 23 27 485 |MD 51 45 54 55 209 46
Table 3.1504.3 GPS week: 1504 Day: 3 MJD: 54775
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 3700 31 16 29 21 --- 13 | 24 38 74 61 --- 43
R06 |15606 64 33 93 55 --- 34 | 452 478 515 510 --- 486
R07 | 2060 23 17 34 11 --- 12 | 20 33 40 27 --- 24
R10 | 3985 34 29 60 34 --- 22 | 61 86 74 78 --- 71
R11 | 2221 27 14 31 25 344 13 | 44 45 48 45 132 40
R13 | 3161 22 18 24 25 --- 12 | 52 44 56 50 --- 47
R14 | 1789 29 14 24 18 --- 12 | 27 50 56 37 --- 39
R15 | 7809 55 20 91 44 617 30 | 44 77 143 97 290 81
R17 | 5124 20 18 27 23 --- 12 | 45 56 61 49 --- 48
R18 | 3203 21 9 29 15 --- 10 | 29 24 49 34 --- 28
R19 | 1329 31 39 49 40 --- 23 | 56 43 87 60 --- 49
R20 | 4004 23 10 44 22 --- 14 | 27 26 50 23 --- 22
R21 | 9087 115 75 36 86 --- 47 | 98 143 40 113 --- 107
R23 | 5425 88 49 57 52 --- 35 | 30 93 64 58 --- 100
R24 | 2627 42 24 41 31 448 19 | 117 136 144 118 287 125
------+------------------------------------+--------------------------------
RMS | 5942 49 31 50 38 483 |T 75 91 100 90 236 87
WRMS | 5942 41 19 41 38 483 |NE 89 107 112 105 287 103
MEDI | 3700 31 18 36 25 448 |MD 44 50 61 58 287 48
Table 3.1504.4 GPS week: 1504 Day: 4 MJD: 54776
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 7049 23 14 26 13 --- 10 | 28 32 41 33 --- 28
R06 |16597 43 34 39 24 --- 19 | 195 250 213 215 --- 221
R07 | 1754 30 14 27 12 --- 11 | 33 35 45 29 --- 31
R10E | 4265 63 30 75 31 --- 27 | 59 98 131 78 --- 83
R11 | 2715 19 30 39 25 529 16 | 28 48 55 37 233 34
R13 | 7186 35 25 41 29 --- 18 | 60 62 76 54 --- 57
R14E | 2067 28 18 25 15 --- 11 | 28 43 54 35 --- 36
R15E | 4127 31 18 39 27 733 16 | 59 88 102 75 424 77
R17 | 4143 60 24 57 20 --- 22 | 31 49 93 36 --- 42
R18 | 3920 27 40 81 15 --- 24 | 48 34 100 61 --- 50
R19 | 2638 24 8 18 13 --- 9 | 37 25 27 22 --- 23
R20 | 2815 33 15 25 15 --- 12 | 24 30 49 31 --- 29
R21 | 6217 39 19 24 21 --- 14 | 70 177 42 122 --- 148
XR22 | ---- --- --- --- --- --- 0 | 9 198 --- --- --- 0
R23 | 2491 58 26 55 28 --- 22 | 32 42 72 56 --- 47
R24 | 2756 32 13 24 22 406 13 | 112 117 119 103 580 110
------+------------------------------------+--------------------------------
RMS | 5925 39 24 44 22 572 |T 53 83 81 65 412 67
WRMS | 5925 37 25 36 22 572 |NE 56 89 80 70 580 72
MEDI | 3920 32 19 39 21 529 |MD 33 48 72 54 424 47
Table 3.1504.5 GPS week: 1504 Day: 5 MJD: 54777
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 4212 34 22 36 17 --- 15 | 35 39 52 30 --- 27
R06 |15961 40 33 31 24 --- 18 | 408 433 437 421 --- 424
R07 | 1573 61 17 37 26 --- 20 | 36 33 41 23 --- 24
R10E | 2740 28 26 54 27 --- 19 | 57 61 89 61 --- 62
R11E | 2988 48 21 22 26 939 17 | 35 42 53 40 362 36
R13E | 2265 38 25 31 18 --- 16 | 63 50 74 54 --- 54
R14E | 2090 23 11 37 16 --- 12 | 42 37 58 40 --- 38
R15E | 3332 24 22 29 18 624 13 | 69 57 70 67 200 62
R17 | 3643 23 29 25 15 --- 13 | 30 51 36 30 --- 31
R18 | 1950 21 9 29 16 --- 10 | 61 50 49 41 --- 44
R19 | 2791 22 15 21 16 --- 10 | 30 23 28 36 --- 28
R20 | 1520 22 17 16 17 --- 10 | 17 22 26 23 --- 15
R21 | 3614 45 15 25 18 --- 14 | 32 143 38 124 --- 134
XR22 |>>>>> --- 4 --- --- --- 0 | --- 160 --- --- --- 120
R23 | 6081 28 32 53 23 --- 19 | 28 50 70 55 --- 48
R24 | 4669 24 13 22 20 726 11 | 66 80 88 75 462 75
------+------------------------------------+--------------------------------
RMS | 5234 34 22 33 20 774 |T 67 83 80 74 341 76
WRMS | 5234 36 18 28 20 774 |NE 74 98 86 85 462 88
MEDI | 2988 28 17 29 18 726 |MD 36 50 53 41 362 44
Table 3.1504.6 GPS week: 1504 Day: 6 MJD: 54778
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 4085 25 12 20 11 --- 9 | 31 31 41 38 --- 31
R06 |10338 91 33 54 26 --- 28 | 321 357 397 362 --- 356
R07 | 1965 34 12 22 22 --- 12 | 33 30 43 27 --- 28
XR09E |18200 --- --- 8 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 1883 28 14 22 25 --- 12 | 47 62 60 61 --- 55
R11E | 5159 35 22 36 24 427 16 | 45 33 64 47 231 37
R13E | 2904 35 17 48 16 --- 16 | 66 55 59 52 --- 53
R14E | 1687 28 15 21 26 --- 12 | 37 43 43 37 --- 37
R15E | 6296 30 15 26 26 448 13 | 61 58 55 60 212 55
R17 |10220 31 23 64 29 --- 20 | 41 49 75 36 --- 39
R18 | 1446 19 27 32 22 --- 15 | 75 55 84 63 --- 63
R19 | 2544 26 9 43 17 --- 13 | 46 36 46 42 --- 36
R20 | 1045 25 17 25 24 --- 13 | 25 23 40 37 --- 24
R21 | 3578 23 16 38 15 --- 12 | 37 179 51 167 --- 173
XR22 |16921 --- 158 --- 189 --- 172 | --- 105 --- 6 --- 59
R23 | 6737 41 27 34 16 --- 16 | 32 59 30 55 --- 64
R24 | 6374 32 13 43 18 502 14 | 73 78 87 76 174 74
------+------------------------------------+--------------------------------
RMS | 5300 37 19 37 22 460 |T 64 78 78 72 205 74
WRMS | 5300 30 17 37 22 460 |NE 71 91 89 82 174 86
MEDI | 4085 30 16 32 22 448 |MD 45 55 55 47 212 53
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