Date: December 2nd 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 1486)
---------------------------------------

Vector Time (GMT): 2008/336/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4863965
47                 A    =         6736022
49  meter
 Y    =        3899566
24  meter          E    =           
0018205
 Z    =        2537216
02                 I    =           51
37387
 XDOT =      -1563
607685                 Wp   =           86
81080
 YDOT =       5396
518026  meter/sec      RA   =          237
69753  deg
 ZDOT =      -5263
164343                 TA   =           64
33907
                                          MA   =           64
15115
                                          Ha   =            195
763  n
mi
                                          Hp   =            185
470

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15957891
96                 X    =         4807672
92
 Y    =       12793852
49  feet           Y    =         3953642
83  meter
 Z    =        8324199
53                 Z    =         2560709
20
 XDOT =      -5129
946474                 XDOT =       -1598
268450
 YDOT =      17705
111633  feet/sec       YDOT =        5378
839763  meter/sec
 ZDOT =     -17267
599552                 ZDOT =       -5270
843904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14131829
04                 X    =        -4307381
49
 Y    =       14734232
26  feet           Y    =         4490993
99  meter
 Z    =        8415645
12                 Z    =         2565088
63
 XDOT =     -16124
703543                 XDOT =       -4914
809640
 YDOT =      -5523
996000  feet/sec       YDOT =       -1683
713981  meter/sec
 ZDOT =     -17296
974948                 ZDOT =       -5272
117964


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08336
57865414  
00020000  00000-0  20000-3 0  9009
2 25544  51
6421 238
4243 0006420  48
2346 311
9364 15
71651545 14873


Satellite: ISS
Catalog Number: 25544
Epoch time:      08336
57865414   =   yrday
fracday
Element set:     900
Inclination:       51
6421  deg
RA of node:       238
4243  deg
Eccentricity:     
0006420     
Arg of perigee:    48
2346  deg
Mean anomaly:     311
9364  deg
Mean motion:   15
71651545  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1487
Checksum:              284


Coasting Arc #2 (Orbit 1502)
---------------------------------------

Vector Time (GMT): 2008/337/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         187144
70                 A    =         6731183
04  meter
 Y    =       -5259297
94  meter          E    =           
0014860
 Z    =        4183285
22                 I    =           51
37459
 XDOT =       6037
095186                 Wp   =           85
17519
 YDOT =       3114
571177  meter/sec      RA   =          232
60746  deg
 ZDOT =       3635
773871                 TA   =          327
62187
                                          MA   =          327
71298
                                          Ha   =            195
774  n
mi
                                          Hp   =            185
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         613991
80                 X    =          225619
31
 Y    =      -17254914
50  feet           Y    =        -5256990
56  meter
 Z    =       13724689
05                 Z    =         4184287
20
 XDOT =      19806
742736                 XDOT =        5984
156773
 YDOT =      10218
409373  feet/sec       YDOT =        3181
785036  meter/sec
 ZDOT =      11928
391965                 ZDOT =        3664
974112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17174988
49                 X    =         5234936
49
 Y    =        1741678
96  feet           Y    =          530863
75  meter
 Z    =       13728163
56                 Z    =         4184344
25
 XDOT =     -11448
172878                 XDOT =       -3489
403093
 YDOT =      17721
683190  feet/sec       YDOT =        5401
569036  meter/sec
 ZDOT =      12041
932775                 ZDOT =        3670
381110


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08337
59598839  
00020000  00000-0  20000-3 0  9017
2 25544  51
6422 233
2176 0006453  50
7882 309
3852 15
71679152 15037


Satellite: ISS
Catalog Number: 25544
Epoch time:      08337
59598839   =   yrday
fracday
Element set:     901
Inclination:       51
6422  deg
RA of node:       233
2176  deg
Eccentricity:     
0006453     
Arg of perigee:    50
7882  deg
Mean anomaly:     309
3852  deg
Mean motion:   15
71679152  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1503
Checksum:              306


Coasting Arc #3 (Orbit 1517)
---------------------------------------

Vector Time (GMT): 2008/338/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5405846
76                 A    =         6732533
14  meter
 Y    =       -1467037
01  meter          E    =           
0011192
 Z    =       -3742646
61                 I    =           51
39817
 XDOT =      -1208
446047                 Wp   =           78
08284
 YDOT =      -6306
725209  meter/sec      RA   =          227
42038  deg
 ZDOT =       4230
512649                 TA   =          236
60958
                                          MA   =          236
71671
                                          Ha   =            195
673  n
mi
                                          Hp   =            185
265

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17735717
72                 X    =        -5370859
10
 Y    =       -4813113
55  feet           Y    =        -1527292
30  meter
 Z    =      -12279024
33                 Z    =        -3768823
58
 XDOT =      -3964
718003                 XDOT =       -1158
384617
 YDOT =     -20691
355673  feet/sec       YDOT =       -6319
959281  meter/sec
 ZDOT =      13879
634674                 ZDOT =        4224
762922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5739816
16                 X    =         1749495
97
 Y    =      -17385872
01  feet           Y    =        -5299213
79  meter
 Z    =      -12380716
80                 Z    =        -3773642
48
 XDOT =      19608
204991                 XDOT =        5976
580881
 YDOT =      -3364
138218  feet/sec       YDOT =       -1025
389329  meter/sec
 ZDOT =      13856
820991                 ZDOT =        4223
559038


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08338
54972666  
00020000  00000-0  20000-3 0  9028
2 25544  51
6419 228
3364 0006304  52
7936 307
3800 15
71708692 15183


Satellite: ISS
Catalog Number: 25544
Epoch time:      08338
54972666   =   yrday
fracday
Element set:     902
Inclination:       51
6419  deg
RA of node:       228
3364  deg
Eccentricity:     
0006304     
Arg of perigee:    52
7936  deg
Mean anomaly:     307
3800  deg
Mean motion:   15
71708692  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1518
Checksum:              303


Coasting Arc #4 (Orbit 1533)
---------------------------------------

Vector Time (GMT): 2008/339/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2280980
89                 A    =         6734398
57  meter
 Y    =        5494764
04  meter          E    =           
0009908
 Z    =       -3166488
06                 I    =           51
42468
 XDOT =      -5993
787769                 Wp   =           75
94656
 YDOT =       -275
474125  meter/sec      RA   =          222
33647  deg
 ZDOT =      -4805
865778                 TA   =          140
99309
                                          MA   =          140
92158
                                          Ha   =            195
717  n
mi
                                          Hp   =            185
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7483533
12                 X    =         2234750
37
 Y    =       18027441
08  feet           Y    =         5520013
07  meter
 Z    =      -10388740
36                 Z    =        -3155518
79
 XDOT =     -19664
658035                 XDOT =       -5966
915683
 YDOT =       -903
786498  feet/sec       YDOT =        -342
349462  meter/sec
 ZDOT =     -15767
276175                 ZDOT =       -4834
918590

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18284784
74                 X    =        -5573202
39
 Y    =        6895678
33  feet           Y    =         2101802
76  meter
 Z    =      -10345728
28                 Z    =        -3153377
98
 XDOT =       2103
986602                 XDOT =         641
295116
 YDOT =     -18195
686773  feet/sec       YDOT =       -5546
045328  meter/sec
 ZDOT =     -15880
042629                 ZDOT =       -4840
236993


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08339
56703573  
00020000  00000-0  20000-3 0  9031
2 25544  51
6415 223
1294 0006160  56
7785 303
3967 15
71708453 15343


Satellite: ISS
Catalog Number: 25544
Epoch time:      08339
56703573   =   yrday
fracday
Element set:     903
Inclination:       51
6415  deg
RA of node:       223
1294  deg
Eccentricity:     
0006160     
Arg of perigee:    56
7785  deg
Mean anomaly:     303
3967  deg
Mean motion:   15
71708453  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1534
Checksum:              296


Coasting Arc #5 (Orbit 1549)
---------------------------------------

Vector Time (GMT): 2008/340/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4816038
06                 A    =         6729180
09  meter
 Y    =        -948001
36  meter          E    =           
0014425
 Z    =        4595360
41                 I    =           51
43090
 XDOT =       3964
028165                 Wp   =           62
23791
 YDOT =       5924
218602  meter/sec      RA   =          217
15591  deg
 ZDOT =      -2918
653406                 TA   =           56
82044
                                          MA   =           56
68217
                                          Ha   =            195
519  n
mi
                                          Hp   =            185
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15800649
80                 X    =         4803957
16
 Y    =       -3110240
67  feet           Y    =         -894213
51  meter
 Z    =       15076641
76                 Z    =         4618727
56
 XDOT =      13005
341750                 XDOT =        3911
666407
 YDOT =      19436
412735  feet/sec       YDOT =        5968
254100  meter/sec
 ZDOT =      -9575
634534                 ZDOT =       -2899
522711

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2819596
74                 X    =          859413
09
 Y    =       15768437
61  feet           Y    =         4806219
78  meter
 Z    =       15167251
16                 Z    =         4622978
15
 XDOT =     -18524
159256                 XDOT =       -5646
163741
 YDOT =      12493
678643  feet/sec       YDOT =        3808
073251  meter/sec
 ZDOT =      -9500
905211                 ZDOT =       -2895
875908


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08340
58433034  
00020000  00000-0  20000-3 0  9048
2 25544  51
6417 217
9221 0006229  59
1901 300
9873 15
71793277 15504


Satellite: ISS
Catalog Number: 25544
Epoch time:      08340
58433034   =   yrday
fracday
Element set:     904
Inclination:       51
6417  deg
RA of node:       217
9221  deg
Eccentricity:     
0006229     
Arg of perigee:    59
1901  deg
Mean anomaly:     300
9873  deg
Mean motion:   15
71793277  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1550
Checksum:              284


Coasting Arc #6 (Orbit 1565)
---------------------------------------

Vector Time (GMT): 2008/341/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4529102
65                 A    =         6736998
31  meter
 Y    =       -4604618
33  meter          E    =           
0020262
 Z    =        1881885
60                 I    =           51
48028
 XDOT =       4719
752270                 Wp   =           65
85010
 YDOT =      -2327
237176  meter/sec      RA   =          212
06295  deg
 ZDOT =       5625
311906                 TA   =          315
09916
                                          MA   =          315
26288
                                          Ha   =            195
662  n
mi
                                          Hp   =            185
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14859260
67                 X    =        -4486418
43
 Y    =      -15107015
51  feet           Y    =        -4655026
84  meter
 Z    =        6174165
34                 Z    =         1859986
29
 XDOT =      15484
751542                 XDOT =        4718
097898
 YDOT =      -7635
292573  feet/sec       YDOT =       -2274
467790  meter/sec
 ZDOT =      18455
747722                 ZDOT =        5648
236618

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15125592
19                 X    =         4610280
50
 Y    =      -14875582
42  feet           Y    =        -4534077
52  meter
 Z    =        6088790
63                 Z    =         1855863
39
 XDOT =       6531
108333                 XDOT =        1990
681820
 YDOT =      14284
972975  feet/sec       YDOT =        4354
059763  meter/sec
 ZDOT =      18544
532072                 ZDOT =        5652
373375


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08341
60161407  
00020000  00000-0  20000-3 0  9055
2 25544  51
6409 212
7147 0006161  63
4983 296
6811 15
71787724 15668


Satellite: ISS
Catalog Number: 25544
Epoch time:      08341
60161407   =   yrday
fracday
Element set:     905
Inclination:       51
6409  deg
RA of node:       212
7147  deg
Eccentricity:     
0006161     
Arg of perigee:    63
4983  deg
Mean anomaly:     296
6811  deg
Mean motion:   15
71787724  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1566
Checksum:              295


Coasting Arc #7 (Orbit 1580)
---------------------------------------

Vector Time (GMT): 2008/342/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3228139
23                 A    =         6726991
65  meter
 Y    =        2944201
78  meter          E    =           
0019560
 Z    =       -5131869
43                 I    =           51
47152
 XDOT =      -6170
167684                 Wp   =           90
61509
 YDOT =      -4364
421136  meter/sec      RA   =          206
90318  deg
 ZDOT =       1381
689043                 TA   =          192
65054
                                          MA   =          192
69970
                                          Ha   =            195
663  n
mi
                                          Hp   =            184
931

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10591007
98                 X    =        -3235891
70
 Y    =        9659454
66  feet           Y    =         2908059
85  meter
 Z    =      -16836841
95                 Z    =        -5147570
65
 XDOT =     -20243
332298                 XDOT =       -6127
617548
 YDOT =     -14318
966982  feet/sec       YDOT =       -4433
181703  meter/sec
 ZDOT =       4533
100536                 ZDOT =        1351
816885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9825434
98                 X    =        -2994792
58
 Y    =      -10338646
66  feet           Y    =        -3151219
50  meter
 Z    =      -16897543
43                 Z    =        -5150371
24
 XDOT =      13239
914477                 XDOT =        4035
525933
 YDOT =     -19778
377023  feet/sec       YDOT =       -6028
449317  meter/sec
 ZDOT =       4416
792801                 ZDOT =        1346
238446


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08342
55530628  
00020000  00000-0  20000-3 0  9066
2 25544  51
6400 207
8322 0006196  66
9579 293
2236 15
71797454 15818


Satellite: ISS
Catalog Number: 25544
Epoch time:      08342
55530628   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       207
8322  deg
Eccentricity:     
0006196     
Arg of perigee:    66
9579  deg
Mean anomaly:     293
2236  deg
Mean motion:   15
71797454  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1581
Checksum:              306


Coasting Arc #8 (Orbit 1596)
---------------------------------------

Vector Time (GMT): 2008/343/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6065391
80                 A    =         6738367
51  meter
 Y    =        2878964
95  meter          E    =           
0014649
 Z    =        -530620
83                 I    =           51
53642
 XDOT =      -2477
354461                 Wp   =          116
21681
 YDOT =       4138
941868  meter/sec      RA   =          201
79198  deg
 ZDOT =      -5995
544023                 TA   =           69
55813
                                          MA   =           69
40089
                                          Ha   =            195
710  n
mi
                                          Hp   =            185
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19899579
39                 X    =         6035325
66
 Y    =        9445423
06  feet           Y    =         2946623
60  meter
 Z    =       -1740881
99                 Z    =         -501227
30
 XDOT =      -8127
803351                 XDOT =       -2494
326746
 YDOT =      13579
205603  feet/sec       YDOT =        4111
144234  meter/sec
 ZDOT =     -19670
420022                 ZDOT =       -6007
620178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8780298
27                 X    =        -2676234
91
 Y    =       20211399
12  feet           Y    =         6160434
45  meter
 Z    =       -1626546
81                 Z    =         -495771
47
 XDOT =     -12363
361658                 XDOT =       -3768
352633
 YDOT =      -6919
818000  feet/sec       YDOT =       -2109
160526  meter/sec
 ZDOT =     -19716
957307                 ZDOT =       -6009
728587


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08343
57256590  
00020000  00000-0  20000-3 0  9073
2 25544  51
6399 202
6258 0006160  71
1468 289
0362 15
71789360 15979


Satellite: ISS
Catalog Number: 25544
Epoch time:      08343
57256590   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       202
6258  deg
Eccentricity:     
0006160     
Arg of perigee:    71
1468  deg
Mean anomaly:     289
0362  deg
Mean motion:   15
71789360  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1597
Checksum:              314


Coasting Arc #9 (Orbit 1612)
---------------------------------------

Vector Time (GMT): 2008/344/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         971308
73                 A    =         6726389
62  meter
 Y    =       -4071479
83  meter          E    =           
0008453
 Z    =        5258117
10                 I    =           51
52313
 XDOT =       7424
947175                 Wp   =           82
72398
 YDOT =       2045
446150  meter/sec      RA   =          196
66161  deg
 ZDOT =        213
019798                 TA   =            5
25647
                                          MA   =            5
24760
                                          Ha   =            195
673  n
mi
                                          Hp   =            184
973

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3186708
44                 X    =          991220
88
 Y    =      -13357873
46  feet           Y    =        -4060507
31  meter
 Z    =       17251040
35                 Z    =         5262883
77
 XDOT =      24360
062911                 XDOT =        7400
487981
 YDOT =       6710
781332  feet/sec       YDOT =        2128
339425  meter/sec
 ZDOT =        698
883851                 ZDOT =         249
031888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13496166
64                 X    =         4113631
59
 Y    =        2411226
11  feet           Y    =          734941
72  meter
 Z    =       17269214
28                 Z    =         5263656
51
 XDOT =      -5300
555226                 XDOT =       -1615
609233
 YDOT =      23678
391011  feet/sec       YDOT =        7217
173580  meter/sec
 ZDOT =        838
853783                 ZDOT =         255
682633


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08344
58981278  
00020000  00000-0  20000-3 0  9084
2 25544  51
6391 197
4178 0006185  74
7094 285
4752 15
71800678 16132


Satellite: ISS
Catalog Number: 25544
Epoch time:      08344
58981278   =   yrday
fracday
Element set:     908
Inclination:       51
6391  deg
RA of node:       197
4178  deg
Eccentricity:     
0006185     
Arg of perigee:    74
7094  deg
Mean anomaly:     285
4752  deg
Mean motion:   15
71800678  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1613
Checksum:              328


Coasting Arc #10 (Orbit 1627)
---------------------------------------

Vector Time (GMT): 2008/345/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6643736
60                 A    =         6737975
65  meter
 Y    =        -629771
65  meter          E    =           
0015235
 Z    =        -895869
00                 I    =           51
58964
 XDOT =       -328
639337                 Wp   =           53
71794
 YDOT =      -4877
502769  meter/sec      RA   =          191
52505  deg
 ZDOT =       5944
746661                 TA   =          296
50610
                                          MA   =          296
66225
                                          Ha   =            195
604  n
mi
                                          Hp   =            184
924

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21797036
09                 X    =        -6631848
53
 Y    =       -2066179
96  feet           Y    =         -703999
16  meter
 Z    =       -2939202
75                 Z    =         -928116
28
 XDOT =      -1078
213048                 XDOT =        -302
953085
 YDOT =     -16002
305673  feet/sec       YDOT =       -4881
035006  meter/sec
 ZDOT =      19503
762010                 ZDOT =        5943
211811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         591247
82                 X    =          180212
34
 Y    =      -21869575
43  feet           Y    =        -6665846
59  meter
 Z    =       -3064456
16                 Z    =         -934046
24
 XDOT =      14290
486814                 XDOT =        4355
740381
 YDOT =      -2310
960435  feet/sec       YDOT =        -704
380741  meter/sec
 ZDOT =      19497
411161                 ZDOT =        5942
810922


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08345
54346940  
00020000  00000-0  20000-3 0  9093
2 25544  51
6377 192
5351 0006099  77
9298 282
2547 15
71830115 16282


Satellite: ISS
Catalog Number: 25544
Epoch time:      08345
54346940   =   yrday
fracday
Element set:     909
Inclination:       51
6377  deg
RA of node:       192
5351  deg
Eccentricity:     
0006099     
Arg of perigee:    77
9298  deg
Mean anomaly:     282
2547  deg
Mean motion:   15
71830115  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1628
Checksum:              317


Coasting Arc #11 (Orbit 1643)
---------------------------------------

Vector Time (GMT): 2008/346/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1520630
85                 A    =         6727304
52  meter
 Y    =        4199989
58  meter          E    =           
0019494
 Z    =       -5047781
58                 I    =           51
58176
 XDOT =      -7453
790333                 Wp   =           78
71740
 YDOT =        573
500015  meter/sec      RA   =          186
42525  deg
 ZDOT =      -1770
284133                 TA   =          174
19014
                                          MA   =          174
16750
                                          Ha   =            195
645  n
mi
                                          Hp   =            184
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4988946
37                 X    =         1498074
57
 Y    =       13779493
39  feet           Y    =         4216868
90  meter
 Z    =      -16560963
18                 Z    =        -5040448
27
 XDOT =     -24454
692693                 XDOT =       -7451
049421
 YDOT =       1881
561728  feet/sec       YDOT =         490
163049  meter/sec
 ZDOT =      -5808
018810                 ZDOT =       -1806
488642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13299439
27                 X    =        -4053669
09
 Y    =        6232361
61  feet           Y    =         1899623
82  meter
 Z    =      -16532153
80                 Z    =        -5039000
48
 XDOT =      -3487
681787                 XDOT =       -1063
045409
 YDOT =     -23204
130256  feet/sec       YDOT =       -7072
618902  meter/sec
 ZDOT =      -5948
560765                 ZDOT =       -1813
121321


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08346
56069219  
00020000  00000-0  20000-3 0  9109
2 25544  51
6366 187
3271 0006209  82
4987 277
6880 15
71860301 16448


Satellite: ISS
Catalog Number: 25544
Epoch time:      08346
56069219   =   yrday
fracday
Element set:     910
Inclination:       51
6366  deg
RA of node:       187
3271  deg
Eccentricity:     
0006209     
Arg of perigee:    82
4987  deg
Mean anomaly:     277
6880  deg
Mean motion:   15
71860301  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1644
Checksum:              309


Coasting Arc #12 (Orbit 1659)
---------------------------------------

Vector Time (GMT): 2008/347/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6163355
60                 A    =         6735982
81  meter
 Y    =       -1589534
70  meter          E    =           
0019637
 Z    =        2180483
77                 I    =           51
64136
 XDOT =       3096
971244                 Wp   =          101
77684
 YDOT =       4418
645097  meter/sec      RA   =          181
26926  deg
 ZDOT =      -5495
166182                 TA   =           53
81104
                                          MA   =           53
62959
                                          Ha   =            195
443  n
mi
                                          Hp   =            184
771

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20220982
93                 X    =         6170079
42
 Y    =       -5215008
84  feet           Y    =        -1520575
31  meter
 Z    =        7153818
16                 Z    =         2210441
79
 XDOT =      10160
666812                 XDOT =        3074
025937
 YDOT =      14496
867117  feet/sec       YDOT =        4453
149979  meter/sec
 ZDOT =     -18028
760440                 ZDOT =       -5480
175778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7241805
10                 X    =         2207302
20
 Y    =       19543907
02  feet           Y    =         5956982
86  meter
 Z    =        7270043
99                 Z    =         2215909
41
 XDOT =     -11951
478286                 XDOT =       -3642
810582
 YDOT =      11158
325652  feet/sec       YDOT =        3401
057659  meter/sec
 ZDOT =     -17970
193376                 ZDOT =       -5477
314941


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08347
57790032  
00020000  00000-0  20000-3 0  9116
2 25544  51
6368 182
1188 0005996  84
4206 275
7640 15
71919122 16605


Satellite: ISS
Catalog Number: 25544
Epoch time:      08347
57790032   =   yrday
fracday
Element set:     911
Inclination:       51
6368  deg
RA of node:       182
1188  deg
Eccentricity:     
0005996     
Arg of perigee:    84
4206  deg
Mean anomaly:     275
7640  deg
Mean motion:   15
71919122  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1660
Checksum:              303

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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