[IGSREPORT-16712] Wk 1498 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Tue Oct 14 05:34:54 PDT 2008
******************************************************************************
IGS Electronic Report 14 Oct 05:34:56 PDT 2008 Message Number 16712
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1498 (Sep 21, 2008 - Sep 27, 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 2.1498.
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:
igl1498[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1498 in the SP3 format.
igl14987.sum Combination Report for GPS Week 1498.
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 | 653.5 ns
1 | 612.3 ns
2 | 654.7 ns
3 | 654.4 ns
4 | 546.9 ns
5 | 565.3 ns
6 | 662.7 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
----+--------+---------------
1 | ESX | R23
6 | 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 1.1498, 1a.1498).
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 2.1498.0-6)
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 3.1498.0-6).
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 1498 summary. (Sep 21, 2008 - Sep 27, 2008)
Table 1.1498.a GPS week : 1498 MJD: 54730.0-54736.0
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| 0 1 -3 28 17 -74 -.12 40 36 | 0 -316 2460 2657
| 3 2 10 29 42 242 .09 | 0 364
cod 216| -2 0 0 -17 -36 69 -.19 31 26 | --- --- --- ---
| 3 2 4 27 40 43 .08 | --- ---
esx 133| 2 0 5 -16 45 39 .37 69 42 | 117439 -649 6231 18876
| 3 2 5 40 45 130 .06 | 50472 4208
iac n/a| 0 1 0 -10 -12 -28 -.07 40 40 | 624160 -1353 6112 13524
| 2 1 5 30 52 61 .09 | 47886 3547
mcc n/a| -5 0 56 98 -8 89 -.01 184 184 | --- --- --- ---
| 13 5 8 201 74 252 .42 | --- ---
Table 1.1498.b GPS week : 1498 MJD: 54730.0-54736.0
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 29 32 |
R04 | 16 21 23 21 14 22 13 |
R06 | 23 26 23 29 41 21 27 |
R07 | 13 15 17 17 17 14 14 |
R10 | 21 21 18 13 14 17 21 |
R11 | 15 16 18 20 17 14 12 |
R13 | 18 15 26 15 18 16 16 |
R14 | 15 15 19 14 13 13 10 |
R15 | 25 22 24 13 16 16 12 |
R17 | 21 25 21 18 24 15 16 |
R19 | 33 32 30 31 21 21 15 |
R20 | 26 28 35 28 22 21 18 |
R23 | 42 43 43 38 42 26 31 |
R24 | 18 23 20 28 24 23 21 |
Table 1.1498.c GPS week : 1498 MJD: 54730.0-54736.0
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 1498 0 | 49 18 206 748 -2058 287 99.1 6066 6066 | 653533 0
brd 1498 1 | 76 -5646 -5 -1596 110 -20160 85.8 >>>>> >>>>> | 612321 0
brd 1498 2 | -254 25 0 1417 -4449 -15580 92.8 7224 7224 | 654721 0
brd 1498 3 | 60 -37 259 1575 818 -13570 93.8 6733 6733 | 654402 0
brd 1498 4 | 44 167 91 -532 3270 -4805 93.5 6289 6289 | 546872 0
brd 1498 5 | 84 76 348 -942 -2451 -10910 92.2 5537 5537 | 565341 0
brd 1498 6 | 89 13 118 384 -1140 -17760 92.5 5334 5334 | 662713 0
-------------+------------------------------------------------------------+----------------
brd 1498 mean| 21 -768 145 150 -842 -11785 92.8 >>>>> >>>>> | 621414 0
brd 1498 sdev| 122 2151 132 1208 2508 7287 3.9 >>>>> >>>>> | 47815 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 2.1498.0 GPS week: 1498 Day: 0 MJD: 54730
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 0 2 34 16 -445 -.07 39 36 | 0 60 2111 2248
cod 216| -7 -2 1 -19 -18 68 -.09 29 24 | --- --- --- ---
esx 133| 0 -3 8 -21 34 232 .28 54 39 | 148203 4749 8052 17067
iac n/a| 2 0 -6 15 -55 71 -.06 33 33 | 654101 3859 7745 12678
mcc n/a| 10 -2 59 164 -75 286 .61 226 226 | --- --- --- ---
Table 2.1498.1 GPS week: 1498 Day: 1 MJD: 54731
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 3 -4 19 49 69 -.08 46 42 | 0 -1040 2883 3574
cod 216| 0 0 0 -17 -81 50 -.17 30 26 | --- --- --- ---
esx 133| 6 0 4 -27 83 -16 .36 159 46 | 98403 840 6246 21363
iac n/a| -3 0 0 2 27 -22 -.08 39 39 | 616722 -1379 5844 17960
mcc n/a| -30 8 58 447 48 -114 .36 160 160 | --- --- --- ---
Table 2.1498.2 GPS week: 1498 Day: 2 MJD: 54732
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 5 -19 -5 45 -248 -.02 46 41 | 0 -491 2407 2535
cod 216| -2 0 5 25 -93 114 -.28 37 31 | --- --- --- ---
esx 133| 2 0 5 -17 21 88 .34 49 41 | 151955 -2460 7086 19496
iac n/a| 2 0 -1 21 59 14 .07 41 41 | 658313 -5703 6905 14648
mcc n/a| -6 -1 57 -98 18 574 -.04 169 169 | --- --- --- ---
Table 2.1498.3 GPS week: 1498 Day: 3 MJD: 54733
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 8 36 14 76 -.15 40 35 | 0 -37 2345 2423
cod 216| -5 -4 -1 -12 -58 44 -.15 31 27 | --- --- --- ---
esx 133| 7 2 -3 -25 108 -53 .36 44 77 | 145232 -22 5417 18451
iac n/a| 2 2 9 -10 -75 -90 -.09 46 46 | 655464 1622 5287 10636
mcc n/a| -11 2 64 -117 -94 4 .04 238 238 | --- --- --- ---
Table 2.1498.4 GPS week: 1498 Day: 4 MJD: 54734
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 2 -7 29 -48 289 -.04 47 32 | 0 -266 2478 2638
cod 216| 0 0 -9 -8 9 45 -.31 36 26 | --- --- --- ---
esx 133| -1 0 10 -83 19 -169 .39 33 27 | 39500 -2204 4754 17766
iac n/a| 0 0 7 -48 -47 -86 -.19 48 48 | 547773 -357 4989 12972
mcc n/a| -6 2 39 -26 0 -111 -.61 195 195 | --- --- --- ---
Table 2.1498.5 GPS week: 1498 Day: 5 MJD: 54735
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 8 84 -22 -168 -.17 36 36 | 0 -185 2401 2521
cod 216| 1 -1 -1 -19 -3 140 -.17 23 24 | --- --- --- ---
esx 133| 0 0 0 4 73 93 .46 33 29 | 64940 2763 5165 19298
iac n/a| 0 4 0 -56 -31 -82 -.13 39 39 | 569597 -1762 5103 13875
mcc n/a| 1 5 54 225 -67 -40 -.45 148 148 | --- --- --- ---
Table 2.1498.6 GPS week: 1498 Day: 6 MJD: 54736
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 -2 -9 -1 70 -96 -.27 30 28 | 0 -256 2598 2662
cod 216| 0 4 0 -69 -9 19 -.15 27 21 | --- --- --- ---
esx 133| 3 -1 11 53 -22 100 .43 108 36 | 173844 -8211 6900 18696
iac n/a| 1 0 -3 0 33 0 .02 31 31 | 667151 -5757 6917 11904
mcc n/a| 4 -9 62 93 107 26 .02 151 151 | --- --- --- ---
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 3.1498.0 GPS week: 1498 Day: 0 MJD: 54730
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 59 --- --- --- 61
R04 | 1727 32 20 26 29 --- 15 | 52 35 36 28 --- 31
R06 | 3535 34 42 55 27 --- 23 | 185 214 213 200 --- 201
R07 | 2436 21 22 22 21 --- 12 | 24 40 30 26 --- 25
R10 | 1180 34 18 67 22 --- 21 | 48 26 52 43 --- 33
R11 |12695 28 23 25 29 87 15 | 31 28 40 36 19 27
R13 | 1485 27 22 53 19 --- 17 | 33 32 56 24 --- 25
R14 | 4331 25 26 20 30 --- 15 | 41 32 36 29 --- 28
R15 | 1709 69 23 46 26 80 25 | 72 50 44 43 25 43
R17E |11879 44 36 40 28 --- 21 | 52 32 42 37 --- 27
XR19E | 1627 54 41 --- 42 --- 32 | 76 73 --- 52 --- 54
R20E | 1056 52 41 51 35 --- 25 | 37 27 60 47 --- 31
R23E | 1730 52 39 126 68 --- 42 | 58 66 164 100 --- 66
R24E | 9407 22 26 30 38 372 17 | 70 87 99 118 63 91
------+------------------------------------+--------------------------------
RMS | 6066 39 29 54 33 225 |T 59 57 72 60 35 53
WRMS | 6066 36 24 39 33 225 |NE 60 57 63 53 22 52
MEDI | 1730 34 23 40 29 87 |MD 52 35 44 43 25 31
Table 3.1498.1 GPS week: 1498 Day: 1 MJD: 54731
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 70 --- --- --- 71
R04 |>>>>> 48 21 56 17 --- 21 | 44 39 40 29 --- 25
R06 |>>>>> 59 42 29 45 --- 26 | 220 221 226 202 --- 216
R07 |>>>>> 38 17 17 28 --- 14 | 17 38 44 49 --- 34
R10 |>>>>> 42 43 20 32 --- 21 | 53 31 29 46 --- 27
R11 |>>>>> 26 21 35 26 112 15 | 22 26 37 23 17 18
R13 |>>>>> 29 16 31 28 --- 15 | 32 25 46 20 --- 22
R14 |>>>>> 31 18 31 23 --- 14 | 34 31 43 38 --- 30
XR15 |>>>>> --- 22 46 22 68 21 | --- 54 56 39 23 41
R17E |>>>>> 38 38 58 39 --- 25 | 34 32 46 31 --- 20
XR19E |>>>>> 49 43 --- 45 --- 32 | 72 78 --- 54 --- 60
R20E |>>>>> 65 27 68 33 --- 28 | 40 35 52 43 --- 31
R23E |>>>>> 70 42 510 72 --- 43 | 79 60 468 94 --- 61
R24E |>>>>> 26 26 50 50 197 23 | 68 61 97 83 82 69
------+------------------------------------+--------------------------------
RMS |>>>>> 46 30 159 39 160 |T 59 57 98 57 40 51
WRMS |>>>>> 42 26 46 39 160 |NE 60 59 65 55 20 53
MEDI |>>>>> 38 22 35 32 112 |MD 40 38 46 43 23 31
Table 3.1498.2 GPS week: 1498 Day: 2 MJD: 54732
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 10 --- --- --- 0 | --- 101 --- --- --- 100
R04 | 991 50 39 41 26 --- 22 | 63 45 34 30 --- 33
R06 |12576 38 48 26 41 --- 23 | 140 138 128 139 --- 133
R07 | 1999 41 30 25 14 --- 16 | 40 33 35 25 --- 20
R10 | 1277 35 29 32 25 --- 17 | 54 26 42 38 --- 30
R11 | 6817 26 23 46 24 131 17 | 47 28 40 31 33 22
R13 |12583 32 32 65 41 --- 25 | 40 34 65 34 --- 23
R14 | 1719 31 36 40 21 --- 19 | 43 47 30 25 --- 22
R15 | 5536 58 35 42 27 40 23 | 54 35 62 53 40 39
R17E | 6197 45 27 29 39 --- 20 | 22 36 37 40 --- 29
XR19E | 1266 44 43 --- 40 --- 30 | 48 64 --- 55 --- 47
R20E | 1826 78 28 93 33 --- 35 | 63 40 92 52 --- 48
R23E | 7390 54 68 71 91 --- 42 | 55 98 140 95 --- 63
R24E |11256 34 22 22 52 258 20 | 58 66 69 96 211 69
------+------------------------------------+--------------------------------
RMS | 7224 46 37 49 41 169 |T 55 56 64 54 94 48
WRMS | 7224 41 31 41 41 169 |NE 60 54 54 46 36 46
MEDI | 5536 41 30 40 33 131 |MD 54 40 42 40 40 33
Table 3.1498.3 GPS week: 1498 Day: 3 MJD: 54733
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 64 --- --- --- 62
R04 | 1430 39 23 55 19 --- 21 | 44 41 61 36 --- 31
R06 |10902 49 25 80 26 --- 28 | 288 283 316 274 --- 286
R07 | 2085 30 30 23 32 --- 17 | 38 43 31 25 --- 22
R10 | 1324 17 14 28 28 --- 13 | 29 35 30 28 --- 26
R11 |13230 25 40 20 43 129 19 | 26 55 26 31 35 26
R13 | 6457 27 19 25 31 --- 14 | 23 31 29 26 --- 22
R14 | 1673 24 19 28 21 --- 13 | 48 28 53 51 --- 41
R15 | 7919 26 17 19 24 58 12 | 33 28 49 36 40 30
R17E | 8737 35 18 26 43 --- 18 | 19 19 33 39 --- 19
R19E | 893 40 40 84 41 --- 31 | 61 62 153 80 --- 62
R20E | 1596 55 36 48 58 --- 28 | 30 49 57 76 --- 40
R23E | 2077 58 60 45 94 --- 38 | 55 113 106 110 --- 80
R24E | 9797 60 22 17 74 388 27 | 62 44 48 87 254 52
------+------------------------------------+--------------------------------
RMS | 6732 40 31 44 46 238 |T 58 63 76 69 109 57
WRMS | 6732 35 27 77 46 238 |NE 66 67 74 63 37 60
MEDI | 2085 35 22 28 32 129 |MD 38 43 49 39 40 31
Table 3.1498.4 GPS week: 1498 Day: 4 MJD: 54734
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 7 --- --- --- 0 | --- 45 --- --- --- 48
R04 | 1167 29 22 21 27 --- 14 | 32 26 59 24 --- 24
R06 | 3365 112 52 56 50 --- 41 | 174 203 234 187 --- 191
R07 | 1130 34 33 26 23 --- 17 | 24 35 29 31 --- 16
R10 | 1777 23 21 23 31 --- 14 | 44 34 31 32 --- 25
R11 |11619 16 34 32 26 128 16 | 24 36 39 18 25 16
R13 | 8776 27 21 39 33 --- 18 | 40 31 56 26 --- 27
R14 | 2510 19 12 23 30 --- 12 | 39 29 35 31 --- 25
R15 |10362 21 22 29 35 37 15 | 28 35 39 27 33 24
R17E |10749 50 43 24 46 --- 24 | 28 36 25 41 --- 18
R19E | 682 16 27 35 59 --- 21 | 46 29 169 41 --- 29
R20E | 2430 49 28 32 45 --- 22 | 68 49 58 76 --- 52
R23E | 1502 70 81 42 92 --- 41 | 46 129 98 113 --- 86
R24E | 6869 38 19 26 73 310 23 | 52 59 81 111 116 71
------+------------------------------------+--------------------------------
RMS | 6289 47 36 33 48 195 |T 49 55 73 58 58 46
WRMS | 6289 32 26 27 48 195 |NE 50 52 65 47 29 44
MEDI | 2510 29 22 29 35 128 |MD 40 35 56 32 33 25
Table 3.1498.5 GPS week: 1498 Day: 5 MJD: 54735
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 20 --- 40 --- 29 | --- 45 --- 21 --- 40
R04 | 1070 44 32 26 49 --- 21 | 78 46 112 21 --- 41
R06 | 2473 31 38 36 37 --- 21 | 176 215 201 195 --- 197
R07 | 1557 31 25 14 21 --- 14 | 18 28 32 19 --- 16
R10 | 1148 45 13 36 22 --- 17 | 31 16 43 25 --- 20
R11 |10651 37 17 24 15 148 14 | 25 32 40 32 30 24
R13 |10832 27 20 39 19 --- 15 | 35 39 46 27 --- 29
R14 | 1658 20 13 32 21 --- 12 | 20 20 24 31 --- 16
R15 | 7402 22 20 34 34 35 16 | 29 31 39 19 34 25
R17E | 9302 31 17 26 33 --- 15 | 26 16 29 34 --- 14
R19E | 1423 41 14 25 60 --- 20 | 34 35 148 26 --- 29
R20E | 1590 50 24 33 41 --- 21 | 40 34 50 57 --- 36
R23E | 1827 36 32 48 66 --- 26 | 84 77 102 95 --- 82
R24E | 2176 40 23 45 51 206 22 | 101 77 76 94 118 81
------+------------------------------------+--------------------------------
RMS | 5536 36 23 33 39 148 |T 53 50 72 49 60 46
WRMS | 5536 36 24 29 39 148 |NE 51 52 67 43 32 45
MEDI | 1827 36 20 33 34 148 |MD 34 34 46 27 34 29
Table 3.1498.6 GPS week: 1498 Day: 6 MJD: 54736
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 27 --- 37 --- 32 | --- 69 --- 11 --- 64
R04 | 1146 21 18 366 13 --- 12 | 23 37 94 25 --- 24
R06 | 4881 50 49 42 42 --- 26 | 122 144 151 131 --- 134
R07 | 1208 29 23 16 27 --- 14 | 22 32 27 35 --- 19
R10 | 1720 41 14 60 19 --- 20 | 39 33 29 43 --- 32
R11 | 5185 20 15 26 23 147 12 | 23 46 42 27 33 29
R13 |13972 38 21 31 16 --- 15 | 32 39 26 30 --- 25
R14 | 2084 21 12 23 13 --- 10 | 22 23 32 25 --- 21
R15 | 4869 20 21 18 23 37 12 | 35 52 41 44 39 42
R17E | 8614 29 23 30 30 --- 16 | 24 30 28 47 --- 24
R19E | 954 25 18 17 38 --- 15 | 64 51 141 53 --- 53
R20E | 1292 25 27 35 39 --- 18 | 43 50 55 75 --- 49
R23E | 2868 27 49 85 47 --- 31 | 90 109 134 124 --- 95
R24E | 2245 33 26 38 46 214 21 | 123 103 132 124 135 115
------+------------------------------------+--------------------------------
RMS | 5333 30 27 108 31 151 |T 50 58 71 56 69 51
WRMS | 5333 28 21 36 31 151 |NE 39 52 55 41 36 43
MEDI | 2245 27 21 31 27 147 |MD 35 46 42 43 39 32
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