[IGSREPORT-16217] Wk 1476 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Mon May 12 05:53:04 PDT 2008
******************************************************************************
IGS Electronic Report 12 May 05:53:12 PDT 2008 Message Number 16217
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1476 (Apr 20, 2008 - Apr 26, 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 2.1476.
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:
igl1476[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1476 in the SP3 format.
igl14767.sum Combination Report for GPS Week 1476.
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 | 995.0 ns
1 | 999.7 ns
2 | 1016.0 ns
3 | 1053.2 ns
4 | 1044.2 ns
5 | 1007.0 ns
6 | 1018.8 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
----+--------+---------------
3 | ESX | R19
5 | ESX | R19
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 1.1476, 1a.1476).
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 2.1476.0-6)
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 3.1476.0-6).
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 1476 summary. (Apr 20, 2008 - Apr 26, 2008)
Table 1.1476.a GPS week : 1476 MJD: 54576.0-54582.0
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 66| 1 0 -9 5 30 -7 -.09 41 31 | 0 124 2763 2885
| 1 1 8 40 27 131 .04 | 0 239
cod 177| -3 0 -1 3 5 25 -.05 27 23 | --- --- --- ---
| 1 2 5 24 12 53 .03 | --- ---
esx 116| 1 2 11 -20 -86 -121 .34 77 56 | -22279 2894 9179 30341
| 5 4 9 61 64 103 .08 | 26415 10109
iac n/a| 3 0 5 -18 32 3 .01 37 37 | 1015373 -1782 9308 22921
| 1 2 20 19 30 62 .07 | 24459 8378
mcc n/a| 2 8 14 -43 18 490 .23 351 351 | --- --- --- ---
| 13 11 29 171 189 882 .23 | --- ---
Table 1.1476.b GPS week : 1476 MJD: 54576.0-54582.0
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 | 31 20 18 26 20 17 23 |
R04 | 11 21 21 24 11 16 20 |
R06 | 18 15 49 24 20 29 28 |
R07 | 26 22 25 23 20 28 28 |
R08 | 18 17 18 21 18 27 38 |
R09 | 14 16 19 17 32 21 70 |
R10 | 19 12 15 12 26 14 12 |
R11 | 29 21 30 28 17 15 29 |
R13 | 32 23 17 26 26 17 57 |
R14 | 14 16 15 15 11 14 16 |
R15 | 20 18 19 21 23 20 17 |
R17 | 21 28 18 16 17 17 15 |
R19 | 16 17 23 18 19 25 17 |
R20 | 11 14 24 19 18 24 20 |
R23 | 21 17 18 17 21 30 27 |
R24 | 14 22 18 16 17 26 14 |
Table 1.1476.c GPS week : 1476 MJD: 54576.0-54582.0
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 1476 0 | 98 267 420 -2450 1515 -25490 94.5 6001 6001 | 994984 0
brd 1476 1 | 29 -239 233 -2005 1078 -21230 100.4 >>>>> >>>>> | 999738 0
brd 1476 2 | -99 84 218 -618 482 -19110 97.3 7431 7431 | 1016037 0
brd 1476 3 | 79 -87 274 -3906 5266 -18260 95.4 8419 8419 | 1053221 0
brd 1476 4 | -84 356 406 -1243 5766 -27820 106.9 9868 9868 | 1044150 0
brd 1476 5 | 363 74 559 -1443 -7210 -20140 103.4 9124 9124 | 1007004 0
brd 1476 6 | -9 52 664 130 -2800 -13450 100.7 8000 8000 | 1018756 0
-------------+------------------------------------------------------------+----------------
brd 1476 mean| 53 72 396 -1647 585 -20785 99.8 >>>>> >>>>> | 1019127 0
brd 1476 sdev| 156 201 169 1310 4510 4747 4.4 >>>>> >>>>> | 22000 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 2.1476.0 GPS week: 1476 Day: 0 MJD: 54576
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 66| 3 0 -8 8 51 106 -.12 28 28 | 0 -208 2546 2616
cod 177| -2 0 1 -10 -13 31 -.03 21 18 | --- --- --- ---
esx 116| -5 9 14 -4 -87 -201 .34 79 69 | -48556 -14622 13111 39259
iac n/a| 5 -2 4 -26 44 -87 .14 34 34 | 992528 -11856 13257 32240
mcc n/a| 5 -5 -46 268 -283 -1292 .33 406 406 | --- --- --- ---
Table 2.1476.1 GPS week: 1476 Day: 1 MJD: 54577
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 66| 1 0 -16 21 16 -58 -.07 24 23 | 0 190 3937 4228
cod 177| -2 1 0 -31 12 17 -.04 23 23 | --- --- --- ---
esx 116| -6 0 18 -20 -191 40 .29 60 53 | -58172 11079 12821 42591
iac n/a| 0 1 15 -2 36 74 .08 37 37 | 985412 12737 13335 35438
mcc n/a| -4 -3 36 40 -112 35 .22 607 607 | --- --- --- ---
Table 2.1476.2 GPS week: 1476 Day: 2 MJD: 54578
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 66| 2 0 -15 -9 58 74 -.04 35 27 | 0 226 2728 2793
cod 177| -4 -3 -7 33 0 -66 -.05 36 25 | --- --- --- ---
esx 116| 0 0 16 -30 -138 -71 .28 63 50 | -38328 -3325 10118 29988
iac n/a| 4 0 16 3 32 -9 -.05 32 32 | 1015659 -9692 9793 21774
mcc n/a| -11 5 21 -191 129 602 .15 431 431 | --- --- --- ---
Table 2.1476.3 GPS week: 1476 Day: 3 MJD: 54579
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 66| 0 2 -5 -33 30 37 -.06 28 27 | 0 180 2469 2586
cod 177| -7 -4 0 31 -8 6 -.01 27 27 | --- --- --- ---
esx 116| 6 -2 -9 -68 -34 -276 .37 101 60 | 656 14462 6716 23699
iac n/a| 3 0 14 -8 12 4 -.06 33 33 | 1049895 4497 7095 16021
mcc n/a| -4 9 24 -57 -23 919 .62 290 290 | --- --- --- ---
Table 2.1476.4 GPS week: 1476 Day: 4 MJD: 54580
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 66| 2 2 -7 -28 -22 111 -.14 35 34 | 0 429 2741 2835
cod 177| -4 -1 -10 2 14 10 -.10 22 19 | --- --- --- ---
esx 116| 3 5 11 79 -12 -171 .33 51 44 | 12403 4307 7766 20675
iac n/a| 3 -3 20 -8 -20 10 -.03 37 37 | 1045314 -1837 7779 16031
mcc n/a| 5 29 15 13 -24 1121 .36 237 237 | --- --- --- ---
Table 2.1476.5 GPS week: 1476 Day: 5 MJD: 54581
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 66| 0 0 5 -3 28 -70 -.14 34 28 | 0 -202 2758 2846
cod 177| -2 0 4 9 21 77 -.04 23 21 | --- --- --- ---
esx 116| 7 -4 16 15 -34 -87 .50 132 68 | -14154 -1369 6876 21868
iac n/a| 2 3 -39 -44 75 83 .00 49 49 | 1007112 -4415 6651 11414
mcc n/a| -1 11 9 -135 290 1275 -.03 285 285 | --- --- --- ---
Table 2.1476.6 GPS week: 1476 Day: 6 MJD: 54582
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 66| 1 -1 -20 86 49 -254 -.05 100 48 | 0 256 2163 2294
cod 177| -2 3 -1 -13 11 100 -.10 36 28 | --- --- --- ---
esx 116| 7 5 13 -114 -105 -85 .29 55 48 | -9808 9727 6851 34307
iac n/a| 1 0 6 -40 49 -55 -.01 37 37 | 1011695 -1914 7249 27531
mcc n/a| 30 12 40 -239 151 773 -.02 199 199 | --- --- --- ---
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 3.1476.0 GPS week: 1476 Day: 0 MJD: 54576
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5528 45 17 138 39 --- 30 | 30 50 79 61 --- 39
R04 | 2660 16 16 39 17 --- 11 | 26 31 63 28 --- 24
R06 | 2249 9 17 82 29 --- 17 | 169 183 212 168 --- 175
R07 | 3346 41 14 94 48 294 25 | 51 58 84 72 249 54
R08 | 4961 19 25 64 34 --- 18 | 44 53 50 63 --- 48
R09 |14978 17 18 50 23 --- 13 | 38 48 60 44 --- 40
R10 | 1516 40 17 39 39 --- 19 | 23 37 48 46 --- 32
R11 | 5539 15 13 142 47 --- 28 | 47 44 115 49 --- 46
R13 | 9134 46 30 118 56 --- 31 | 54 31 123 46 --- 40
R14 | 1871 16 22 26 29 --- 13 | 23 23 34 32 --- 20
R15 | 5817 24 23 91 18 97 19 | 36 44 99 56 86 43
R17 | 5395 23 29 70 42 --- 21 | 32 48 92 51 --- 42
R19 | 4328 31 19 45 23 --- 15 | 55 48 83 59 --- 53
R20 | 1864 16 14 38 18 --- 11 | 46 39 58 59 --- 45
R23 | 7492 32 32 62 32 --- 20 | 76 91 105 91 --- 82
R24 | 3486 23 17 39 24 632 13 | 128 147 186 150 578 145
------+------------------------------------+--------------------------------
RMS | 6001 28 21 79 34 406 |T 54 60 93 67 304 58
WRMS | 6001 28 18 69 34 406 |NE 54 60 93 67 304 58
MEDI | 4328 23 17 62 29 294 |MD 44 48 83 56 249 43
Table 3.1476.1 GPS week: 1476 Day: 1 MJD: 54577
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |>>>>> 39 29 36 30 --- 19 | 22 73 82 50 --- 47
R04 |>>>>> 14 17 90 35 --- 21 | 18 28 66 34 --- 19
R06 |>>>>> 20 21 45 27 --- 15 | 174 196 183 164 --- 178
R07 | 4267 25 22 70 49 125 21 | 36 39 77 50 113 33
R08 |>>>>> 22 23 64 17 --- 17 | 43 39 57 29 --- 28
R09 |>>>>> 16 15 50 41 --- 16 | 34 42 81 51 --- 38
R10 |>>>>> 16 10 43 24 --- 12 | 21 30 60 34 --- 26
R11 |>>>>> 30 31 57 37 --- 20 | 33 36 86 50 --- 31
R13 |>>>>> 20 14 96 38 --- 22 | 36 27 125 36 --- 35
R14 |>>>>> 17 18 36 42 --- 15 | 16 31 42 29 --- 21
R15 |>>>>> 15 25 53 41 58 18 | 46 55 51 54 36 45
R17 |>>>>> 26 34 86 66 --- 28 | 25 31 114 51 --- 31
R19 |>>>>> 31 29 29 23 --- 16 | 48 37 75 48 --- 40
R20 |>>>>> 17 19 41 25 --- 13 | 41 39 66 54 --- 43
R23 |>>>>> 21 24 42 39 --- 17 | 53 59 81 62 --- 55
R24 |>>>>> 37 23 73 25 1042 21 | 64 103 146 104 624 92
------+------------------------------------+--------------------------------
RMS |>>>>> 24 23 60 37 607 |T 44 54 87 56 257 47
WRMS |>>>>> 23 23 53 37 607 |NE 44 54 87 56 257 47
MEDI |>>>>> 20 22 50 35 125 |MD 36 39 77 50 113 35
Table 3.1476.2 GPS week: 1476 Day: 2 MJD: 54578
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9748 28 29 42 29 --- 18 | 34 59 83 46 --- 48
R04 | 2711 29 40 54 26 --- 21 | 20 53 48 34 --- 23
R06 | 3961 98 83 111 45 --- 48 | 189 222 239 190 --- 193
R07 | 7301 28 27 83 40 63 24 | 33 30 87 41 99 23
R08 |11633 22 14 62 28 --- 17 | 24 33 71 36 --- 29
R09 |12543 17 31 65 23 --- 19 | 28 35 71 31 --- 27
R10 | 3602 15 23 34 29 --- 14 | 46 36 68 54 --- 44
R11 | 7221 49 22 109 26 --- 29 | 34 38 148 45 --- 49
R13 | 9970 21 18 42 34 --- 16 | 42 30 48 38 --- 27
R14 | 4906 25 23 35 24 --- 15 | 27 17 51 41 --- 23
R15 | 6183 18 33 55 32 66 19 | 26 30 52 56 51 35
R17 |11511 23 24 56 30 --- 18 | 54 44 102 83 --- 60
R19 | 3027 22 50 50 34 --- 22 | 42 59 115 74 --- 57
R20 | 3363 23 47 41 49 --- 24 | 36 61 57 22 --- 29
R23 | 5508 30 27 41 27 --- 17 | 55 73 54 79 --- 62
R24 | 3048 24 27 59 20 742 18 | 135 134 167 152 256 142
------+------------------------------------+--------------------------------
RMS | 7431 35 36 63 32 431 |T 51 59 91 63 135 54
WRMS | 7431 27 25 50 32 431 |NE 51 59 91 63 135 54
MEDI | 5508 23 27 54 29 66 |MD 34 38 71 45 99 35
Table 3.1476.3 GPS week: 1476 Day: 3 MJD: 54579
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |10884 18 25 113 35 --- 26 | 29 33 87 43 --- 29
R04 | 9525 41 38 58 35 --- 23 | 17 55 55 44 --- 27
R06 | 5158 43 40 36 40 --- 23 | 224 210 219 199 --- 210
R07 |10852 31 39 74 21 75 22 | 29 43 87 41 85 31
R08 |15231 18 16 90 30 --- 21 | 42 33 88 43 --- 33
R09 | 5305 26 17 59 25 --- 17 | 29 37 66 41 --- 28
R10 | 3574 14 16 38 20 --- 11 | 45 39 41 55 --- 39
R11 | 9977 33 29 114 36 --- 28 | 40 67 103 55 --- 54
R13 |10057 36 39 73 44 --- 25 | 49 55 72 63 --- 35
R14 | 4497 19 19 55 21 --- 15 | 29 19 58 26 --- 19
R15 | 8907 36 18 55 43 59 21 | 52 72 69 78 67 65
R17 |11620 14 21 49 31 --- 15 | 46 52 40 67 --- 44
R19 | 1847 16 25 304 34 --- 18 | 36 44 258 57 --- 41
R20 | 1878 27 27 61 24 --- 18 | 28 50 74 47 --- 41
R23 | 4872 26 24 26 39 --- 17 | 42 49 52 76 --- 46
R24 | 6450 19 20 54 28 493 16 | 84 90 109 71 275 81
------+------------------------------------+--------------------------------
RMS | 8419 28 27 101 33 290 |T 51 59 92 62 142 51
WRMS | 8419 27 27 60 33 290 |NE 51 59 92 62 142 51
MEDI | 6450 26 24 58 31 75 |MD 40 49 72 55 85 39
Table 3.1476.4 GPS week: 1476 Day: 4 MJD: 54580
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8365 20 30 45 43 --- 20 | 51 41 68 48 --- 38
R04 | 8712 23 12 28 15 --- 11 | 19 31 28 29 --- 23
R06 | 6733 48 20 46 26 --- 19 | 195 183 176 202 --- 188
R07 |13351 31 31 41 38 86 20 | 24 34 66 41 74 33
R08 |22378 37 15 40 37 --- 18 | 32 25 50 44 --- 24
R09 | 7730 55 24 108 29 --- 32 | 31 32 97 45 --- 29
R10 | 3858 39 20 85 32 --- 25 | 30 39 92 48 --- 39
R11 |10053 28 11 50 29 --- 16 | 44 58 90 51 --- 55
R13 |16148 43 34 59 47 --- 25 | 39 47 57 35 --- 30
R14 | 8296 21 10 27 23 --- 11 | 27 20 27 24 --- 17
R15 | 7147 32 25 33 63 65 22 | 33 53 65 75 140 47
R17 | 4468 28 16 43 31 --- 16 | 50 54 98 94 --- 66
R19 | 6103 32 16 31 50 --- 18 | 60 62 76 76 --- 63
R20 | 4454 27 11 54 30 --- 17 | 28 34 46 41 --- 23
R23 | 5264 40 29 31 44 --- 20 | 71 81 76 113 --- 78
R24 | 5168 33 25 26 32 397 16 | 121 141 154 135 277 135
------+------------------------------------+--------------------------------
RMS | 9868 35 22 51 37 237 |T 53 58 79 68 163 55
WRMS | 9868 34 19 44 37 237 |NE 53 58 79 68 163 55
MEDI | 7147 32 20 41 32 86 |MD 33 41 68 48 140 38
Table 3.1476.5 GPS week: 1476 Day: 5 MJD: 54581
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6564 17 18 51 35 --- 16 | 33 21 63 38 --- 24
R04 | 8719 15 10 52 31 --- 15 | 17 23 48 45 --- 23
R06 | 6441 42 33 87 49 --- 29 | 225 254 279 243 --- 247
R07 |13316 58 39 56 39 88 27 | 75 46 63 60 80 47
R08 |20300 29 25 90 48 --- 27 | 40 28 122 43 --- 39
R09 | 8661 48 15 34 47 --- 20 | 76 33 65 55 --- 28
R10 | 6590 18 12 33 39 --- 14 | 22 31 54 58 --- 31
R11 | 4747 25 17 35 33 --- 15 | 36 42 59 54 --- 36
R13 |10148 29 9 41 40 --- 16 | 66 33 57 53 --- 27
R14 | 7287 21 21 31 29 --- 14 | 21 24 32 44 --- 16
R15 |10234 30 30 23 51 410 19 | 44 73 72 86 119 65
R17 | 6674 33 20 29 38 --- 16 | 31 41 43 69 --- 38
R19 | 4395 23 22 489 62 --- 24 | 59 47 409 108 --- 60
R20 | 6637 28 32 50 60 --- 23 | 30 41 45 59 --- 26
R23 | 5013 41 26 67 83 --- 29 | 37 49 115 105 --- 59
R24 | 6860 49 21 46 68 261 25 | 125 159 170 157 289 149
------+------------------------------------+--------------------------------
RMS | 9124 34 23 132 49 285 |T 58 59 106 79 162 57
WRMS | 9124 28 21 68 49 285 |NE 58 59 106 79 162 57
MEDI | 6674 29 21 46 40 261 |MD 37 41 63 58 119 36
Table 3.1476.6 GPS week: 1476 Day: 6 MJD: 54582
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4778 40 30 68 15 --- 22 | 30 28 57 49 --- 34
R04 |19309 26 32 53 21 --- 19 | 26 50 44 39 --- 32
R06 |13003 85 37 25 49 --- 28 | 211 202 205 221 --- 206
R07 | 3306 47 48 60 39 103 27 | 59 49 90 48 95 44
R08 | 5704 52 40 112 48 --- 37 | 38 39 109 51 --- 42
R09 |10422 290 63 43 65 --- 70 | 165 61 56 28 --- 46
R10 | 3504 32 16 20 20 --- 12 | 63 44 53 52 --- 49
R11 | 4615 53 29 76 43 --- 28 | 45 43 93 50 --- 44
R13 |10826 224 57 83 32 --- 57 | 208 57 63 52 --- 65
R14 | 3165 25 15 49 21 --- 16 | 24 27 58 29 --- 28
R15 | 7990 37 12 46 20 310 16 | 36 44 66 57 67 43
R17 | 6656 29 20 33 21 --- 14 | 54 63 79 47 --- 56
R19 | 2727 23 31 33 25 --- 16 | 59 60 194 100 --- 72
R20 | 1393 27 31 18 48 --- 20 | 33 38 56 50 --- 40
R23 | 3822 52 42 27 57 --- 27 | 56 62 87 94 --- 70
R24 | 3806 27 16 34 18 108 13 | 138 137 156 150 124 141
------+------------------------------------+--------------------------------
RMS | 8001 100 36 55 37 199 |T 77 62 91 69 95 63
WRMS | 8001 48 28 48 37 199 |NE 77 62 91 69 95 63
MEDI | 4615 37 31 43 25 108 |MD 54 49 66 50 95 44
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