[IGSREPORT-16746] Wk 1500 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Oct 23 07:05:04 PDT 2008
******************************************************************************
IGS Electronic Report 23 Oct 07:05:08 PDT 2008 Message Number 16746
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1500 (Oct 05, 2008 - Oct 11, 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 2.1500.
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:
igl1500[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1500 in the SP3 format.
igl15007.sum Combination Report for GPS Week 1500.
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 | 623.6 ns
1 | 602.8 ns
2 | 595.5 ns
3 | 589.0 ns
4 | 585.7 ns
5 | 579.6 ns
6 | 524.1 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 1.1500, 1a.1500).
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 2.1500.0-6)
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 3.1500.0-6).
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 1500 summary. (Oct 05, 2008 - Oct 11, 2008)
Table 1.1500.a GPS week : 1500 MJD: 54744.0-54750.0
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 0 -15 7 -6 -.14 37 28 | 0 -210 2418 2514
| 2 2 3 23 18 91 .05 | 0 182
cod 238| -3 1 4 26 -26 -20 -.10 27 21 | --- --- --- ---
| 2 1 6 12 31 60 .03 | --- ---
esx 125| 4 0 4 22 44 62 .41 34 31 | 141329 7207 6796 19466
| 3 3 4 62 37 50 .05 | 24762 5266
iac n/a| 2 0 -7 -28 -25 -26 -.14 28 28 | 587429 -1865 6320 14745
| 2 2 7 30 20 72 .05 | 31025 4107
mcc n/a| -4 0 32 57 -61 530 -.13 337 337 | --- --- --- ---
| 5 11 15 85 97 566 .40 | --- ---
Table 1.1500.b GPS week : 1500 MJD: 54744.0-54750.0
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 | 39 39 39 34 17 20 12 |
R04 | 18 22 15 14 15 16 15 |
R06 | 27 34 29 28 22 21 18 |
R07 | 16 22 16 16 18 13 12 |
R09 | --- --- 0 --- 0 0 0 |
R10 | 20 12 17 14 13 11 14 |
R11 | 13 16 21 15 16 19 13 |
R13 | 16 26 21 20 23 19 22 |
R14 | 9 13 15 11 12 11 15 |
R15 | 13 14 9 18 16 19 24 |
R17 | 15 12 15 21 16 15 12 |
R19 | 10 15 12 14 15 12 12 |
R20 | 13 18 9 14 15 12 11 |
R23 | 22 22 17 16 19 23 19 |
R24 | 17 15 14 55 26 23 17 |
Table 1.1500.c GPS week : 1500 MJD: 54744.0-54750.0
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 1500 0 | -97 137 -345 -1365 451 -8869 95.3 4979 4979 | 623555 0
brd 1500 1 | 279 43 -295 -4684 -205 -15880 95.8 >>>>> >>>>> | 602836 0
brd 1500 2 | 47 2 -228 -1829 179 -10230 93.3 3871 3871 | 595486 0
brd 1500 3 | -84 -32 -468 -624 1119 -22780 91.9 5565 5565 | 589049 0
brd 1500 4 | -221 -66 89 1234 4360 -21660 92.2 4311 4311 | 585720 0
brd 1500 5 | 75 25 -181 958 518 -9801 97.4 4115 4115 | 579585 0
brd 1500 6 | 135 -26 44 3570 -694 -15350 95.3 5600 5600 | 524069 0
-------------+------------------------------------------------------------+----------------
brd 1500 mean| 19 11 -197 -391 818 -14938 94.4 >>>>> >>>>> | 585757 0
brd 1500 sdev| 167 66 202 2634 1663 5673 2.0 >>>>> >>>>> | 30739 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 2.1500.0 GPS week: 1500 Day: 0 MJD: 54744
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 -5 -3 35 111 -.11 32 24 | 0 -353 2469 2523
cod 238| -2 0 10 26 -66 -85 -.07 25 19 | --- --- --- ---
esx 125| 4 7 8 45 35 83 .46 37 32 | 170302 8123 5385 17706
iac n/a| 1 0 -15 -21 6 -28 -.11 25 25 | 627726 -1114 5379 16160
mcc n/a| 0 7 36 6 4 -282 -.53 423 423 | --- --- --- ---
Table 2.1500.1 GPS week: 1500 Day: 1 MJD: 54745
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| 3 2 -4 -24 31 -4 -.09 36 28 | 0 -169 2573 2692
cod 238| -1 -1 14 28 -44 -34 -.08 27 21 | --- --- --- ---
esx 125| 8 -4 6 114 64 6 .36 45 38 | 157419 8290 6413 17510
iac n/a| -1 4 -20 -85 -19 91 -.16 30 30 | 607524 -3559 6480 16167
mcc n/a| -1 13 58 53 48 932 -.21 344 344 | --- --- --- ---
Table 2.1500.2 GPS week: 1500 Day: 2 MJD: 54746
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 -1 5 -24 -6 106 -.11 35 28 | 0 -52 2330 2420
cod 238| -2 1 7 41 -37 -67 -.14 26 17 | --- --- --- ---
esx 125| 1 0 -1 -21 75 62 .42 25 24 | 121532 12173 8821 20556
iac n/a| 0 -3 -6 -34 -48 -135 -.24 32 32 | 595438 1216 7488 15192
mcc n/a| 4 0 32 97 55 1047 .35 309 309 | --- --- --- ---
Table 2.1500.3 GPS week: 1500 Day: 3 MJD: 54747
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 -1 -37 3 -133 -.10 55 27 | 0 -374 2506 2651
cod 238| -4 3 0 33 -55 53 -.12 33 21 | --- --- --- ---
esx 125| 2 0 6 88 90 134 .36 39 39 | 150676 4742 6468 16255
iac n/a| 5 -4 -3 -44 -38 -86 -.08 30 30 | 589301 -785 6436 16001
mcc n/a| -7 3 41 -61 -170 1207 -.63 296 296 | --- --- --- ---
Table 2.1500.4 GPS week: 1500 Day: 4 MJD: 54748
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| -3 3 0 -43 -3 -13 -.19 37 29 | 0 -456 2352 2426
cod 238| -2 3 2 34 0 -30 -.13 27 24 | --- --- --- ---
esx 125| 5 -2 0 -33 -7 57 .40 31 29 | 150673 -184 5960 24759
iac n/a| 4 0 -1 0 -28 -15 -.13 27 27 | 587454 -4280 5467 15939
mcc n/a| -9 -5 24 29 -125 579 .17 591 591 | --- --- --- ---
Table 2.1500.5 GPS week: 1500 Day: 5 MJD: 54749
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 3 -2 25 0 -26 -.20 34 29 | 0 10 2175 2251
cod 238| -7 2 -1 14 12 -53 -.05 26 25 | --- --- --- ---
esx 125| 8 -2 5 -50 -1 102 .49 32 29 | 142245 14772 7502 21157
iac n/a| 2 -2 1 1 -7 -27 -.15 25 25 | 576871 4095 6190 12299
mcc n/a| -11 3 23 62 -74 234 .30 235 235 | --- --- --- ---
Table 2.1500.6 GPS week: 1500 Day: 6 MJD: 54750
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 2 -3 -11 -86 -.18 33 32 | 0 -80 2524 2636
cod 238| -1 0 -1 6 6 73 -.10 23 21 | --- --- --- ---
esx 125| 1 -3 8 14 56 -8 .40 27 24 | 96458 2539 7027 18322
iac n/a| 3 1 -8 -12 -46 19 -.11 30 30 | 527690 -8630 6800 11459
mcc n/a| -3 -21 10 213 -167 -5 -.35 165 165 | --- --- --- ---
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 3.1500.0 GPS week: 1500 Day: 0 MJD: 54744
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 34 --- 42 --- 38 | --- 63 --- 85 --- 69
R04 | 3523 17 32 35 37 --- 18 | 34 50 48 45 --- 37
R06 | 6601 64 37 62 21 --- 27 | 153 182 158 162 --- 162
R07 | 4195 32 24 30 27 --- 16 | 24 30 45 27 --- 23
R10 | 1605 41 15 58 21 --- 20 | 47 31 41 48 --- 35
R11 | 5968 23 16 18 29 96 13 | 26 26 32 32 44 21
R13 | 6172 31 27 31 24 --- 16 | 43 34 45 32 --- 32
R14 | 3836 11 10 23 16 --- 9 | 24 21 34 27 --- 21
R15 | 6083 22 21 25 23 83 13 | 47 34 54 42 55 40
R17 | 4226 38 15 27 22 --- 15 | 65 72 86 102 --- 80
R19 | 2399 14 15 20 20 --- 10 | 25 25 31 29 --- 24
R20 | 3310 13 17 36 19 --- 12 | 41 30 70 39 --- 40
R23 | 8863 31 44 42 33 --- 22 | 91 104 101 120 --- 101
R24 | 2738 33 24 45 16 721 17 | 330 318 323 327 459 324
------+------------------------------------+--------------------------------
RMS | 4978 32 25 37 25 423 |T 73 72 82 79 186 72
WRMS | 4978 24 19 32 25 423 |NE 73 72 82 79 186 72
MEDI | 4195 31 21 31 22 96 |MD 43 34 48 42 55 37
Table 3.1500.1 GPS week: 1500 Day: 1 MJD: 54745
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 34 --- 43 --- 38 | --- 61 --- 69 --- 57
R04 |>>>>> 29 36 43 43 --- 22 | 37 42 40 36 --- 21
R06 |>>>>> 85 48 64 34 --- 34 | 184 272 289 250 --- 244
R07 |>>>>> 35 42 26 40 --- 22 | 25 30 32 32 --- 10
R10 |>>>>> 21 16 29 18 --- 12 | 37 28 51 25 --- 27
R11 |>>>>> 30 17 38 29 54 16 | 28 35 51 36 21 21
R13 |>>>>> 35 26 85 31 --- 25 | 41 33 111 41 --- 40
R14 |>>>>> 14 12 29 32 --- 13 | 19 17 31 27 --- 19
R15 |>>>>> 22 15 42 15 41 13 | 33 31 45 31 53 28
R17 |>>>>> 20 14 29 22 --- 12 | 42 45 59 64 --- 49
R19 |>>>>> 22 14 42 29 --- 15 | 24 23 42 36 --- 25
R20 |>>>>> 29 31 39 28 --- 18 | 41 31 54 39 --- 26
R23 |>>>>> 40 34 43 33 --- 21 | 59 70 80 88 --- 69
R24 |>>>>> 26 20 36 23 592 15 | 245 254 252 258 319 252
------+------------------------------------+--------------------------------
RMS |>>>>> 36 27 45 30 344 |T 62 69 87 73 131 63
WRMS |>>>>> 28 21 38 30 344 |NE 62 69 87 73 131 63
MEDI |>>>>> 29 20 39 29 54 |MD 37 33 51 36 53 27
Table 3.1500.2 GPS week: 1500 Day: 2 MJD: 54746
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 29 --- 49 --- 38 | --- 58 --- 59 --- 53
R04 | 3787 27 18 32 21 --- 14 | 43 48 55 40 --- 41
R06 | 3060 75 56 25 29 --- 28 | 94 169 163 152 --- 141
R07 | 6206 31 28 21 32 --- 16 | 20 42 32 19 --- 20
XR09 |19870 --- --- 8 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1045 34 17 29 38 --- 17 | 45 32 37 32 --- 29
R11 | 4390 27 28 39 48 62 21 | 24 27 62 53 19 33
R13 | 2739 36 47 11 37 --- 20 | 26 53 32 32 --- 25
R14 | 1977 19 9 20 45 --- 14 | 22 23 26 42 --- 23
R15 | 3410 8 13 12 22 69 8 | 28 21 27 38 30 26
R17 | 3127 31 21 27 24 --- 15 | 37 49 70 64 --- 53
R19 | 3310 24 10 23 22 --- 11 | 12 18 30 38 --- 23
R20 | 3853 18 9 21 10 --- 9 | 27 23 27 22 --- 21
R23 | 2809 39 18 28 34 --- 17 | 68 90 114 99 --- 93
R24 | 6759 34 7 15 33 527 13 | 294 289 289 303 238 292
------+------------------------------------+--------------------------------
RMS | 3871 35 26 25 32 309 |T 56 67 74 70 95 62
WRMS | 3871 28 17 24 32 309 |NE 56 67 74 70 95 62
MEDI | 3310 31 18 21 32 69 |MD 28 42 37 40 30 29
Table 3.1500.3 GPS week: 1500 Day: 3 MJD: 54747
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 35 --- 32 --- 34 | --- 84 --- 46 --- 60
R04 | 5419 23 23 31 22 --- 14 | 38 50 50 62 --- 45
R06 | 5699 74 31 53 36 --- 28 | 207 154 174 147 --- 162
R07 | 3632 36 33 20 23 --- 16 | 28 43 40 33 --- 23
R10 | 9269 21 17 30 24 --- 13 | 41 41 37 43 --- 35
R11 | 5000 24 20 28 31 46 15 | 25 26 42 33 22 21
R13 | 1994 31 40 31 32 --- 19 | 51 60 56 40 --- 43
R14 | 1913 12 15 19 24 --- 11 | 27 26 26 33 --- 21
R15 | 3252 32 31 23 34 106 18 | 34 34 41 53 40 35
R17 |11028 27 37 39 35 --- 20 | 63 58 49 84 --- 57
R19 | 3221 32 16 25 23 --- 14 | 20 42 38 33 --- 25
R20 | 2423 24 14 33 23 --- 14 | 39 24 56 34 --- 32
R23 | 3261 30 27 33 21 --- 16 | 79 80 109 86 --- 85
R24 | 7060 161 76 90 50 499 55 | 387 523 524 469 373 479
------+------------------------------------+--------------------------------
RMS | 5564 55 33 39 30 296 |T 79 88 95 85 145 80
WRMS | 5564 27 21 39 30 296 |NE 79 88 95 85 145 80
MEDI | 3632 30 27 31 24 106 |MD 39 43 49 43 40 35
Table 3.1500.4 GPS week: 1500 Day: 4 MJD: 54748
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 15 --- 18 --- 17 | --- 62 --- 55 --- 56
R04 | 5023 38 23 20 18 --- 14 | 24 40 44 46 --- 33
R06 | 8399 66 37 26 11 --- 22 | 56 133 136 122 --- 113
R07 | 1635 24 32 40 25 --- 18 | 24 26 57 34 --- 21
XR09 | 7659 --- --- 8 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1789 24 14 22 27 --- 13 | 24 34 44 40 --- 32
R11 | 7928 31 24 23 32 50 16 | 31 29 42 35 23 28
R13 | 2404 28 35 44 45 --- 22 | 26 31 49 53 --- 30
R14 | 2267 16 15 31 15 --- 11 | 25 24 48 30 --- 28
R15 | 3062 30 19 33 27 100 16 | 34 26 49 33 38 27
R17 | 5320 27 18 22 36 --- 15 | 58 65 70 84 --- 68
R19 | 2442 24 32 30 14 --- 15 | 16 29 15 25 --- 15
R20 | 2314 27 15 33 24 --- 14 | 37 19 34 31 --- 23
R23 | 1260 35 29 38 32 --- 19 | 64 79 78 83 --- 72
R24 | 3945 70 42 36 27 1018 25 | 326 363 366 369 743 355
------+------------------------------------+--------------------------------
RMS | 4311 37 27 31 27 591 |T 57 68 79 74 268 64
WRMS | 4311 29 24 29 27 591 |NE 57 68 79 74 268 64
MEDI | 2442 28 23 30 25 100 |MD 31 31 49 40 38 30
Table 3.1500.5 GPS week: 1500 Day: 5 MJD: 54749
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 19 --- 20 --- 19 | --- 45 --- 68 --- 55
R04 | 4419 37 27 27 16 --- 15 | 31 29 50 32 --- 27
R06 |10142 40 31 47 22 --- 20 | 217 228 256 237 --- 234
R07 | 1240 19 21 20 25 --- 12 | 24 27 25 15 --- 13
XR09 | 7134 --- --- 11 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1977 27 10 21 19 --- 11 | 21 30 32 28 --- 24
R11 | 5566 27 24 43 35 70 19 | 17 36 56 22 24 23
R13 | 5334 27 28 33 38 --- 18 | 39 39 58 39 --- 38
R14 | 1515 20 16 22 16 --- 10 | 29 32 29 34 --- 23
R15 | 1808 37 43 18 23 87 18 | 34 21 35 32 49 28
R17 | 3634 27 24 31 20 --- 14 | 68 73 72 76 --- 70
R19 | 1015 24 17 26 15 --- 12 | 26 23 25 17 --- 15
R20 | 2151 22 19 21 19 --- 11 | 28 25 42 41 --- 28
R23 | 554 41 30 52 34 --- 22 | 45 65 105 90 --- 75
R24 | 2838 65 30 35 28 391 23 | 500 485 487 481 823 486
------+------------------------------------+--------------------------------
RMS | 4114 34 26 32 25 235 |T 83 82 97 86 298 81
WRMS | 4114 29 25 29 25 235 |NE 83 82 97 86 298 81
MEDI | 2151 27 24 26 20 87 |MD 31 32 50 34 49 28
Table 3.1500.6 GPS week: 1500 Day: 6 MJD: 54750
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 12 --- 12 --- 12 | --- 70 --- 79 --- 73
R04 | 4770 26 27 22 26 --- 14 | 35 51 44 43 --- 42
R06 |14522 36 29 28 34 --- 18 | 132 166 150 152 --- 149
R07 | 1586 24 18 20 22 --- 12 | 24 24 30 31 --- 19
XR09 |14208 --- --- 8 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2426 32 23 18 22 --- 13 | 37 39 32 46 --- 35
R11 | 1904 21 14 25 26 74 12 | 27 31 36 30 28 24
R13 | 8910 41 16 32 55 --- 21 | 42 46 75 40 --- 47
R14 | 4163 26 18 34 26 --- 15 | 38 32 58 31 --- 36
R15 | 2052 54 43 42 19 125 24 | 40 35 66 43 47 38
R17 | 3502 23 20 20 17 --- 11 | 74 76 77 83 --- 76
R19 | 1208 25 14 25 20 --- 12 | 20 26 44 33 --- 25
R20 | 1357 23 14 14 22 --- 10 | 32 24 31 32 --- 25
R23 | 1244 35 30 27 39 --- 18 | 62 90 91 106 --- 86
R24 | 6623 39 13 27 36 247 17 | 537 569 568 545 649 555
------+------------------------------------+--------------------------------
RMS | 5599 33 23 27 30 165 |T 84 91 100 92 241 87
WRMS | 5599 32 21 24 30 165 |NE 84 91 100 92 241 87
MEDI | 2426 26 18 25 22 125 |MD 38 39 58 43 47 38
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