[Date Prev][Date Next][Thread Prev][Thread Next][Date Index][Thread Index]
[IGSREPORT-16399] Wk 1484 IGLOS Final Orbits
******************************************************************************
IGS Electronic Report 03 Jul 09:01:58 PDT 2008 Message Number 16399
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1484 (Jun 15, 2008 - Jun 21, 2008)
Contact: J. Ray (jim.ray @ noaa.gov),
J. Griffiths (jake.griffiths @ 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 2.1484.
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:
igl1484[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1484 in the SP3 format.
igl14847.sum Combination Report for GPS Week 1484.
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 | 929.6 ns
1 | 918.2 ns
2 | 914.9 ns
3 | 921.4 ns
4 | 924.1 ns
5 | 925.2 ns
6 | 926.3 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 | R08
3 | BKG | R08
4 | BKG | R08
4 | ESX | R08
5 | ESX | R13
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 1.1484, 1a.1484).
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 2.1484.0-6)
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 3.1484.0-6).
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 1484 summary. (Jun 15, 2008 - Jun 21, 2008)
Table 1.1484.a GPS week : 1484 MJD: 54632.0-54638.0
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 64| 3 0 -14 30 -9 221 -.09 54 39 | 0 -7 2461 2568
| 2 4 11 28 51 144 .29 | 0 167
cod 207| -4 0 0 -23 -11 -7 -.09 37 27 | --- --- --- ---
| 2 5 5 42 30 38 .20 | --- ---
esx 120| 0 0 4 -7 66 -117 .47 597 1556 | 49624 -723 8164 17477
| 4 5 7 48 69 80 .34 | 5382 7020
iac n/a| 4 1 10 -8 -34 -80 -.21 54 54 | 922909 -1725 7074 14311
| 2 2 6 48 34 80 .17 | 4836 3571
mcc n/a| -78 18 17 -403 987 3568 -.14 1005 1005 | --- --- --- ---
| 81 113 159 1996 2329 7426 4.90 | --- ---
Table 1.1484.b GPS week : 1484 MJD: 54632.0-54638.0
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 | 30 22 26 22 25 18 16 |
R06 | 26 40 22 28 22 25 29 |
R07 | 39 18 24 34 37 38 55 |
R08 | 54 48 179 120 322 0 --- |
R09 | 0 --- 0 --- --- --- --- |
R10 | 14 15 15 18 13 11 23 |
R11 | 19 18 25 21 17 19 18 |
R13 | 21 29 36 27 20 24 26 |
R14 | 18 29 23 13 15 12 19 |
R15 | 23 24 16 22 20 20 27 |
R17 | 39 35 25 25 31 22 27 |
R19 | 21 17 26 24 13 21 22 |
R20 | 23 16 28 26 21 16 22 |
R23 | 29 36 24 22 32 26 24 |
R24 | 24 22 24 31 26 28 28 |
Table 1.1484.c GPS week : 1484 MJD: 54632.0-54638.0
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 1484 0 | 60 -193 897 50 2305 -27940 97.7 3435 3435 | 929636 0
brd 1484 1 | 218 -114 -4038 -366800 -400 -41520 89.5 >>>>> >>>>> | 918179 0
brd 1484 2 | -66 3 510 339 -4332 -27870 98.4 5211 5211 | 914946 0
brd 1484 3 | 67 98 742 289 622 -24030 100.3 4240 4240 | 921366 0
brd 1484 4 | -108 65 619 -489 603 -22710 104.2 8129 8129 | 924139 0
brd 1484 5 | -430 -392 368 -571 -3255 -16250 103.4 8087 8087 | 925190 0
brd 1484 6 | -47 -301 442 1393 -5846 -9231 101.1 5803 5803 | 926330 0
-------------+------------------------------------------------------------+----------------
brd 1484 mean| -43 -119 -65 -52255 -1471 -24221 99.2 >>>>> >>>>> | 922826 0
brd 1484 sdev| 202 187 1761 138702 3016 10140 4.9 >>>>> >>>>> | 5029 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 2.1484.0 GPS week: 1484 Day: 0 MJD: 54632
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 64| 1 -9 -23 25 50 469 -.64 52 46 | 0 105 2102 2190
cod 207| -6 11 10 -29 -55 -27 -.28 42 37 | --- --- --- ---
esx 120| 0 -3 6 -44 -5 -109 1.11 65 36 | 53753 -854 8600 23219
iac n/a| 0 -4 5 14 1 -225 -.10 43 43 | 928968 -4150 6287 15854
mcc n/a| -137 -74 -278 2424 -2185 -585 -8.35 711 711 | --- --- --- ---
Table 2.1484.1 GPS week: 1484 Day: 1 MJD: 54633
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 64| 8 0 -33 64 -91 299 .17 62 55 | 0 -70 2452 2547
cod 207| -1 -1 1 -70 12 -61 -.13 32 26 | --- --- --- ---
esx 120| -2 2 17 50 59 8 .56 807 48 | 42629 4436 7741 18115
iac n/a| 4 1 7 -29 -36 -56 -.44 45 45 | 916099 -600 6942 14196
mcc n/a| -122 146 265 962 1811 926 -5.87 490 490 | --- --- --- ---
Table 2.1484.2 GPS week: 1484 Day: 2 MJD: 54634
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 64| 5 1 -1 63 35 64 .21 42 39 | 0 288 2905 2997
cod 207| -8 -4 -3 -44 6 40 .16 32 29 | --- --- --- ---
esx 120| -5 -3 -2 -93 126 -233 .19 76 71 | 47610 1970 8775 20468
iac n/a| 6 3 3 60 -65 0 -.39 34 34 | 917800 1830 6828 17629
mcc n/a| -54 56 23 -1266 2401 3108 3.33 544 544 | --- --- --- ---
Table 2.1484.3 GPS week: 1484 Day: 3 MJD: 54635
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 64| 0 3 -6 -14 -49 309 -.19 47 40 | 0 -192 2521 2664
cod 207| -3 2 -3 -32 -5 44 .20 35 29 | --- --- --- ---
esx 120| -1 -8 0 34 -3 -136 .24 58 47 | 53041 -5563 4909 14500
iac n/a| 3 2 4 11 1 -136 -.16 35 35 | 923259 -2971 4826 12811
mcc n/a| -56 163 70 -608 -158 9325 3.42 1312 1312 | --- --- --- ---
Table 2.1484.4 GPS week: 1484 Day: 4 MJD: 54636
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 64| 1 1 -15 40 -16 177 -.22 115 38 | 0 -180 2396 2527
cod 207| -5 -4 -3 -54 28 -1 -.12 71 21 | --- --- --- ---
esx 120| -1 -2 7 -11 105 -189 .69 3048 >>>> | 56741 -10439 10388 15424
iac n/a| 6 0 22 -19 -31 -88 -.22 118 118 | 926251 -6906 8121 12214
mcc n/a| -204 -150 37 -4027 5048 17530 3.59 2225 2225 | --- --- --- ---
Table 2.1484.5 GPS week: 1484 Day: 5 MJD: 54637
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 64| 1 0 -6 19 27 117 -.03 30 27 | 0 -19 2543 2618
cod 207| -6 -1 0 12 -26 -13 -.22 20 19 | --- --- --- ---
esx 120| 7 4 -4 -1 10 -53 .31 68 56 | 50370 -5073 6169 15689
iac n/a| 3 2 15 -1 -17 -63 .04 50 50 | 926954 -2773 6402 14040
mcc n/a| 3 -8 -4 -73 -166 -3278 1.83 1226 1226 | --- --- --- ---
Table 2.1484.6 GPS week: 1484 Day: 6 MJD: 54638
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 64| 3 3 -12 12 -22 113 .05 32 30 | 0 13 2314 2436
cod 207| -2 -4 3 54 -41 -32 -.25 29 27 | --- --- --- ---
esx 120| 4 5 8 10 171 -109 .21 57 53 | 43227 10460 10569 14926
iac n/a| 9 3 12 -96 -90 7 -.21 50 50 | 921034 3494 10116 13435
mcc n/a| 22 -5 11 -237 159 -2045 1.08 528 528 | --- --- --- ---
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 3.1484.0 GPS week: 1484 Day: 0 MJD: 54632
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2282 44 44 71 50 --- 30 | 63 86 90 77 --- 70
R06 | 5527 62 31 52 28 --- 25 | 154 174 193 175 --- 175
R07E | 1233 70 68 94 36 --- 39 | 71 85 64 73 --- 58
R08E | 5647 101 62 153 43 --- 54 | 213 81 9999 120 --- 112
XR09E |27945 --- --- 18 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 3987 33 15 18 27 --- 14 | 54 39 56 65 --- 48
R11E | 1835 33 26 44 28 --- 18 | 36 34 45 28 --- 29
R13E | 4185 26 45 25 37 --- 20 | 73 98 86 63 --- 78
R14E | 1700 35 30 36 24 --- 18 | 60 48 70 53 --- 51
R15E | 3018 34 28 55 37 711 22 | 42 49 56 43 369 40
R17 | 3396 45 62 83 74 --- 39 | 54 56 112 78 --- 47
R19 | 2887 29 31 44 38 --- 20 | 50 36 69 32 --- 33
R20 | 3365 61 29 30 31 --- 22 | 47 45 44 32 --- 23
R23 | 2076 62 36 34 59 --- 28 | 38 51 43 43 --- 29
R24 | 3421 30 44 26 51 --- 23 | 220 225 215 225 --- 218
------+------------------------------------+--------------------------------
RMS | 3434 52 42 65 43 711 |T 83 79 87 79 369 72
WRMS | 3434 46 37 36 43 711 |NE 81 82 96 82 --- 70
MEDI | 3365 35 31 44 37 711 |MD 54 51 69 63 369 48
Table 3.1484.1 GPS week: 1484 Day: 1 MJD: 54633
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |>>>>> 35 26 49 44 --- 22 | 73 74 115 49 --- 66
R06E |>>>>> 126 55 54 38 --- 40 | 75 131 137 112 --- 111
R07E |22583 20 24 47 28 --- 17 | 49 46 70 39 --- 42
R08E |>>>>> 80 44 3014 83 --- 47 | 314 75 9999 108 --- 99
R10E |>>>>> 38 15 24 26 --- 14 | 36 44 48 44 --- 38
R11E |>>>>> 34 24 39 28 --- 17 | 43 41 67 52 --- 40
R13E |>>>>> 73 50 32 45 --- 29 | 75 101 98 95 --- 88
R14E |>>>>> 48 22 88 43 --- 29 | 48 72 126 54 --- 64
R15E |>>>>> 34 31 52 48 490 24 | 37 64 84 48 491 50
R17 |>>>>> 60 25 82 74 --- 34 | 67 39 97 34 --- 41
R19 |>>>>> 45 17 38 24 --- 17 | 34 47 55 56 --- 36
R20 |>>>>> 44 16 31 23 --- 16 | 35 30 37 18 --- 21
R23 |>>>>> 89 31 83 51 --- 35 | 38 56 112 33 --- 37
R24 |>>>>> 58 28 35 31 --- 21 | 198 201 196 212 --- 201
------+------------------------------------+--------------------------------
RMS |>>>>> 62 32 807 45 490 |T 80 72 95 68 491 66
WRMS |>>>>> 55 26 48 45 490 |NE 74 74 99 70 --- 67
MEDI |>>>>> 45 25 47 38 490 |MD 48 56 97 49 491 42
Table 3.1484.2 GPS week: 1484 Day: 2 MJD: 54634
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 6295 37 26 92 42 --- 26 | 71 52 122 58 --- 61
R06E | 3569 43 24 49 40 --- 21 | 126 117 139 142 --- 125
R07E | 2169 35 36 72 36 --- 24 | 85 36 94 63 --- 54
XR08E |18623 --- 168 --- 191 --- 179 | --- 293 --- 234 --- 187
XR09E |33816 --- --- 17 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1546 28 17 32 29 --- 15 | 26 39 63 69 --- 44
R11E | 9075 33 29 92 33 --- 25 | 51 74 90 50 --- 51
R13E | 7177 68 61 89 42 --- 35 | 38 123 161 65 --- 80
R14 | 2623 61 26 43 26 --- 22 | 62 64 61 63 --- 52
R15 | 4556 29 26 39 23 544 16 | 24 49 54 61 330 43
R17 |10701 37 27 88 35 --- 24 | 54 47 126 80 --- 62
R19 | 2939 28 25 104 36 --- 26 | 32 56 114 32 --- 36
R20 | 1588 37 30 101 39 --- 27 | 23 33 104 40 --- 28
R23 | 2385 25 33 88 29 --- 23 | 35 41 101 31 --- 28
R24 | 813 54 37 56 22 --- 23 | 295 301 337 305 --- 304
------+------------------------------------+--------------------------------
RMS | 5211 41 32 76 34 544 |T 70 94 120 92 330 82
WRMS | 5211 39 29 71 34 544 |NE 87 95 156 97 --- 91
MEDI | 3569 37 27 72 35 544 |MD 51 52 104 63 330 52
Table 3.1484.3 GPS week: 1484 Day: 3 MJD: 54635
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 4230 46 25 52 35 --- 22 | 61 82 94 64 --- 67
R06E | 9219 47 33 71 45 --- 28 | 118 118 156 144 --- 130
R07E | 1886 58 64 48 57 --- 33 | 70 74 76 41 --- 44
XR08E |16715 1295 118 --- 121 --- 119 | 678 145 --- 146 --- 110
R10 | 1237 39 24 23 36 --- 18 | 39 54 67 80 --- 57
R11 | 3540 29 22 70 21 --- 21 | 48 51 116 43 --- 55
R13 | 2157 60 32 31 53 --- 26 | 70 81 85 92 --- 74
R14 | 2587 26 26 17 18 --- 13 | 55 70 69 51 --- 58
R15 | 1817 39 28 45 41 1311 22 | 51 60 94 77 305 63
R17 | 8476 47 32 73 26 --- 25 | 48 45 102 72 --- 62
R19 | 2857 24 31 81 23 --- 24 | 54 70 81 40 --- 49
R20 | 1977 28 31 89 25 --- 26 | 37 38 93 24 --- 25
R23 | 3689 51 21 51 30 --- 21 | 56 49 65 56 --- 37
R24 | 994 83 55 48 17 --- 31 | 197 222 230 208 --- 207
------+------------------------------------+--------------------------------
RMS | 4239 47 35 58 35 1311 |T 113 82 102 81 305 74
WRMS | 4239 40 29 47 35 1311 |NE 78 84 114 80 --- 76
MEDI | 2587 46 31 51 30 1311 |MD 55 70 93 64 305 58
Table 3.1484.4 GPS week: 1484 Day: 4 MJD: 54636
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 8135 33 37 56 49 --- 24 | 61 55 61 57 --- 47
R06E |15483 41 19 37 57 --- 22 | 90 83 99 103 --- 87
R07E | 9124 45 41 115 66 --- 37 | 54 68 88 63 --- 61
R08E |10897 407 249 >>>> 417 --- 322 | 490 271 9999 140 --- 362
R10 | 1325 20 16 26 30 --- 13 | 47 32 45 50 --- 39
R11 | 2589 18 28 47 24 --- 17 | 60 74 69 50 --- 60
R13 |19031 30 28 43 37 --- 19 | 40 43 77 59 --- 40
R14 | 2509 30 15 35 25 --- 14 | 38 48 32 51 --- 41
R15 | 1762 36 18 39 49 2225 20 | 45 54 68 68 9999 53
R17 | 3793 61 27 102 27 --- 31 | 41 50 129 41 --- 44
R19 | 1249 20 12 32 29 --- 13 | 28 36 60 32 --- 27
R20 | 1312 41 10 57 36 --- 20 | 28 45 89 28 --- 35
R23 | 4039 28 36 105 51 --- 31 | 29 38 94 36 --- 26
R24 | 1758 69 28 33 40 --- 25 | 275 326 327 335 --- 313
------+------------------------------------+--------------------------------
RMS | 8128 115 71 3048 118 2225 |T 94 87 95 79 --- 88
WRMS | 8128 38 21 >>>> 118 2225 |NE 80 99 139 94 --- 89
MEDI | 2589 33 27 43 37 2225 |MD 45 50 77 51 --- 44
Table 3.1484.5 GPS week: 1484 Day: 5 MJD: 54637
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |12754 38 18 32 37 --- 17 | 34 48 70 62 --- 46
R06E |12048 44 16 57 65 --- 24 | 74 74 95 95 --- 75
XR07E | ---- 47 50 --- 70 --- 38 | 40 67 --- 55 --- 42
XR08E | ---- --- --- --- 10 --- 0 | --- --- --- 196 --- 496
R10 | 1069 17 17 17 24 --- 10 | 21 36 38 25 --- 25
R11 | 7851 25 21 36 58 386 19 | 44 55 71 52 342 47
R13 |19122 29 14 166 61 --- 23 | 24 35 167 48 --- 31
R14 | 1276 14 15 33 21 --- 11 | 33 42 60 48 --- 41
R15 | 3488 16 21 55 51 258 19 | 55 61 102 70 9999 63
R17 | 3996 30 27 54 54 --- 22 | 22 45 84 77 --- 34
R19 | 1528 31 16 50 58 --- 20 | 19 42 65 50 --- 32
R20 | 1049 29 13 49 25 --- 16 | 25 15 68 24 --- 22
R23 | 2939 18 23 83 59 --- 25 | 31 34 76 36 --- 30
R24 | 2594 49 34 56 62 2071 27 | 140 177 192 178 987 165
------+------------------------------------+--------------------------------
RMS | 8087 30 20 68 50 1225 |T 43 56 90 72 664 82
WRMS | 8087 27 19 56 50 1225 |NE 47 62 97 73 987 56
MEDI | 2939 29 18 50 54 386 |MD 33 45 71 52 342 41
Table 3.1484.6 GPS week: 1484 Day: 6 MJD: 54638
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 6841 22 17 40 37 --- 16 | 52 42 64 48 --- 45
R06E | 7912 41 24 55 80 --- 28 | 120 116 136 147 --- 123
XR07E | ---- 64 83 --- 88 --- 55 | 36 92 --- 70 --- 52
R10 | 1003 27 46 35 44 --- 22 | 41 64 74 57 --- 51
R11 | 7769 18 17 47 41 112 17 | 50 53 69 55 39 51
R13 |12520 30 26 56 70 --- 25 | 44 35 84 70 --- 48
R14 | 1442 32 15 54 25 --- 18 | 42 53 69 60 --- 50
R15 | 6995 28 21 90 45 71 27 | 52 54 85 71 502 57
R17 | 3752 20 40 85 37 --- 27 | 60 53 118 67 --- 58
R19 | 1129 33 30 35 55 --- 21 | 23 36 40 50 --- 20
R20 | 2628 31 25 51 49 --- 21 | 36 34 73 51 --- 31
R23 | 934 28 35 55 50 --- 23 | 22 34 55 47 --- 24
R24 | 1568 57 37 53 44 906 28 | 140 164 181 175 84 157
------+------------------------------------+--------------------------------
RMS | 5803 32 29 57 50 528 |T 55 63 87 74 208 59
WRMS | 5803 30 27 53 50 528 |NE 56 64 93 78 84 58
MEDI | 2628 30 26 53 45 112 |MD 44 53 73 60 84 51