Date: November 9th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 ET - UTC (sec) : 66 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 2837)
---------------------------------------

Vector Time (GMT): 2009/310/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3203973
17                 A    =         6726568
47  meter
 Y    =        5889051
52  meter          E    =           
0005615
 Z    =        -504591
16                 I    =           51
35950
 XDOT =      -4021
960151                 Wp   =          159
71451
 YDOT =      -2699
094210  meter/sec      RA   =          295
09907  deg
 ZDOT =      -5988
015121                 TA   =           25
79945
                                          MA   =           25
77146
                                          Ha   =            186
145  n
mi
                                          Hp   =            182
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10511723
01                 X    =        -3267136
17
 Y    =       19321035
18  feet           Y    =         5852869
69  meter
 Z    =       -1655482
82                 Z    =         -520309
37
 XDOT =     -13195
407321                 XDOT =       -3962
390134
 YDOT =      -8855
295966  feet/sec       YDOT =       -2743
736580  meter/sec
 ZDOT =     -19645
718900                 ZDOT =       -6007
409767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8966042
96                 X    =        -2732849
89
 Y    =      -20079850
82  feet           Y    =        -6120338
53  meter
 Z    =       -1717267
96                 Z    =         -523423
28
 XDOT =      13516
643658                 XDOT =        4119
872987
 YDOT =      -4355
534570  feet/sec       YDOT =       -1327
566937  meter/sec
 ZDOT =     -19722
289092                 ZDOT =       -6011
353715


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   09310
55155124  
00016717  00000-0  10270-3 0  9008
2 25544  51
6424 295
5889 0006201 300
2651  59
7899 15
75929877 28384


Satellite: ISS
Catalog Number: 25544
Epoch time:      09310
55155124   =   yrday
fracday
Element set:     900
Inclination:       51
6424  deg
RA of node:       295
5889  deg
Eccentricity:     
0006201     
Arg of perigee:   300
2651  deg
Mean anomaly:      59
7899  deg
Mean motion:   15
75929877  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2838
Checksum:              336


Coasting Arc #2 (Orbit 2853)
---------------------------------------

Vector Time (GMT): 2009/311/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3342909
67                 A    =         6715131
67  meter
 Y    =        2793986
80  meter          E    =           
0006198
 Z    =        5112568
51                 I    =           51
30920
 XDOT =      -3558
894124                 Wp   =          344
16259
 YDOT =       6700
096711  meter/sec      RA   =          289
91071  deg
 ZDOT =      -1329
032138                 TA   =          118
64056
                                          MA   =          118
57821
                                          Ha   =            186
194  n
mi
                                          Hp   =            182
686

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10967551
42                 X    =         3286582
01
 Y    =        9166623
34  feet           Y    =         2831053
87  meter
 Z    =       16773518
75                 Z    =         5128672
03
 XDOT =     -11676
161824                 XDOT =       -3627
094955
 YDOT =      21981
944591  feet/sec       YDOT =        6659
917824  meter/sec
 ZDOT =      -4360
341660                 ZDOT =       -1346
486730

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13830056
52                 X    =        -4215401
23
 Y    =        3302421
04  feet           Y    =         1006577
93  meter
 Z    =       16837121
21                 Z    =         5131954
55
 XDOT =     -10528
234915                 XDOT =       -3209
006002
 YDOT =     -21418
337455  feet/sec       YDOT =       -6528
309256  meter/sec
 ZDOT =      -4428
945191                 ZDOT =       -1349
942494


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   09311
56612955  
00016717  00000-0  10270-3 0  9011
2 25544  51
6421 290
3640 0006263 303
4865  56
5700 15
75956171 28540


Satellite: ISS
Catalog Number: 25544
Epoch time:      09311
56612955   =   yrday
fracday
Element set:     901
Inclination:       51
6421  deg
RA of node:       290
3640  deg
Eccentricity:     
0006263     
Arg of perigee:   303
4865  deg
Mean anomaly:      56
5700  deg
Mean motion:   15
75956171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2854
Checksum:              305


Coasting Arc #3 (Orbit 2869)
---------------------------------------

Vector Time (GMT): 2009/312/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3004364
68                 A    =         6724931
17  meter
 Y    =       -5730149
29  meter          E    =           
0012270
 Z    =        1805453
85                 I    =           51
33417
 XDOT =       3694
265958                 Wp   =           40
17497
 YDOT =       3720
778863  meter/sec      RA   =          284
76615  deg
 ZDOT =       5649
522677                 TA   =          339
96028
                                          MA   =          340
00842
                                          Ha   =            186
145  n
mi
                                          Hp   =            182
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9856839
49                 X    =         3059446
22
 Y    =      -18799702
39  feet           Y    =        -5696244
83  meter
 Z    =        5923405
03                 Z    =         1820182
76
 XDOT =      12120
295137                 XDOT =        3624
940248
 YDOT =      12207
279735  feet/sec       YDOT =        3761
702408  meter/sec
 ZDOT =      18535
179385                 ZDOT =        5667
301473

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9620824
02                 X    =         2932427
16
 Y    =       18903352
88  feet           Y    =         5761741
96  meter
 Z    =        5981288
90                 Z    =         1823096
86
 XDOT =     -15532
493047                 XDOT =       -4734
303881
 YDOT =       2005
828603  feet/sec       YDOT =         611
376558  meter/sec
 ZDOT =      18605
429510                 ZDOT =        5670
934915


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   09312
58067935  
00016717  00000-0  10270-3 0  9027
2 25544  51
6422 285
1390 0006160 306
1709  53
8885 15
76040732 28708


Satellite: ISS
Catalog Number: 25544
Epoch time:      09312
58067935   =   yrday
fracday
Element set:     902
Inclination:       51
6422  deg
RA of node:       285
1390  deg
Eccentricity:     
0006160     
Arg of perigee:   306
1709  deg
Mean anomaly:      53
8885  deg
Mean motion:   15
76040732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2870
Checksum:              309


Coasting Arc #4 (Orbit 2884)
---------------------------------------

Vector Time (GMT): 2009/313/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3150908
65                 A    =         6716936
70  meter
 Y    =       -3696253
37  meter          E    =           
0005621
 Z    =       -4644264
55                 I    =           51
30065
 XDOT =       3338
310027                 Wp   =           84
53434
 YDOT =      -6351
328045  meter/sec      RA   =          279
55352  deg
 ZDOT =       2793
406721                 TA   =          213
14885
                                          MA   =          213
18408
                                          Ha   =            186
400  n
mi
                                          Hp   =            182
198

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10337626
80                 X    =        -3086781
02
 Y    =      -12126815
50  feet           Y    =        -3731130
00  meter
 Z    =      -15237088
41                 Z    =        -4659416
20
 XDOT =      10952
460718                 XDOT =        3395
513528
 YDOT =     -20837
690435  feet/sec       YDOT =       -6313
677329  meter/sec
 ZDOT =       9164
720212                 ZDOT =        2809
763218

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15797817
28                 X    =         4815174
71
 Y    =       -1589424
38  feet           Y    =         -484456
55  meter
 Z    =      -15296984
83                 Z    =        -4662520
98
 XDOT =      10899
930202                 XDOT =        3322
298725
 YDOT =      19623
830442  feet/sec       YDOT =        5981
343519  meter/sec
 ZDOT =       9228
994397                 ZDOT =        2812
997492


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   09313
53179811  
00016717  00000-0  10270-3 0  9031
2 25544  51
6422 280
2401 0006298 311
3968  48
6655 15
76027563 28854


Satellite: ISS
Catalog Number: 25544
Epoch time:      09313
53179811   =   yrday
fracday
Element set:     903
Inclination:       51
6422  deg
RA of node:       280
2401  deg
Eccentricity:     
0006298     
Arg of perigee:   311
3968  deg
Mean anomaly:      48
6655  deg
Mean motion:   15
76027563  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2885
Checksum:              319


Coasting Arc #5 (Orbit 2900)
---------------------------------------

Vector Time (GMT): 2009/314/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2853038
23                 A    =         6722133
30  meter
 Y    =        5272734
13  meter          E    =           
0003250
 Z    =       -3044489
45                 I    =           51
31557
 XDOT =      -3562
724283                 Wp   =          358
23696
 YDOT =      -4755
767549  meter/sec      RA   =          274
42483  deg
 ZDOT =      -4894
459467                 TA   =          217
21718
                                          MA   =          217
23971
                                          Ha   =            186
553  n
mi
                                          Hp   =            181
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9360361
64                 X    =        -2896997
01
 Y    =       17298996
49  feet           Y    =         5240584
00  meter
 Z    =       -9988482
46                 Z    =        -3058456
47
 XDOT =     -11688
727963                 XDOT =       -3485
502916
 YDOT =     -15602
911905  feet/sec       YDOT =       -4795
176238  meter/sec
 ZDOT =     -16057
937884                 ZDOT =       -4911
579892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9300339
50                 X    =        -2834743
48
 Y    =      -17299592
44  feet           Y    =        -5272915
78  meter
 Z    =      -10043366
85                 Z    =        -3061218
22
 XDOT =      18148
795162                 XDOT =        5531
752765
 YDOT =       -388
714223  feet/sec       YDOT =        -118
480095  meter/sec
 ZDOT =     -16125
647387                 ZDOT =       -4915
097324


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   09314
54629678  
00016717  00000-0  10270-3 0  9045
2 25544  51
6427 275
0143 0006329 315
6262  44
4394 15
76096503 29016


Satellite: ISS
Catalog Number: 25544
Epoch time:      09314
54629678   =   yrday
fracday
Element set:     904
Inclination:       51
6427  deg
RA of node:       275
0143  deg
Eccentricity:     
0006329     
Arg of perigee:   315
6262  deg
Mean anomaly:      44
4394  deg
Mean motion:   15
76096503  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2901
Checksum:              315


Coasting Arc #6 (Orbit 2916)
---------------------------------------

Vector Time (GMT): 2009/315/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3115581
76                 A    =         6719710
36  meter
 Y    =        4574704
75  meter          E    =           
0009632
 Z    =        3809601
85                 I    =           51
30681
 XDOT =      -3227
262622                 Wp   =           47
75474
 YDOT =       5645
894861  meter/sec      RA   =          269
19899  deg
 ZDOT =      -4127
412715                 TA   =           85
65846
                                          MA   =           85
54841
                                          Ha   =            186
604  n
mi
                                          Hp   =            181
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10221724
92                 X    =         3045688
35
 Y    =       15008873
84  feet           Y    =         4609154
25  meter
 Z    =       12498693
72                 Z    =         3824567
82
 XDOT =     -10588
131962                 XDOT =       -3270
105541
 YDOT =      18523
277102  feet/sec       YDOT =        5609
566130  meter/sec
 ZDOT =     -13541
380300                 ZDOT =       -4143
195158

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18111226
41                 X    =        -5520301
81
 Y    =         499795
40  feet           Y    =          152337
64  meter
 Z    =       12557905
14                 Z    =         3827649
49
 XDOT =      -9944
532415                 XDOT =       -3031
093480
 YDOT =     -17491
983892  feet/sec       YDOT =       -5331
556690  meter/sec
 ZDOT =     -13603
405287                 ZDOT =       -4146
317932


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   09315
56076820  
00016717  00000-0  10270-3 0  9054
2 25544  51
6428 269
7887 0006361 319
1174  40
9513 15
76139401 29175


Satellite: ISS
Catalog Number: 25544
Epoch time:      09315
56076820   =   yrday
fracday
Element set:     905
Inclination:       51
6428  deg
RA of node:       269
7887  deg
Eccentricity:     
0006361     
Arg of perigee:   319
1174  deg
Mean anomaly:      40
9513  deg
Mean motion:   15
76139401  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2917
Checksum:              323


Coasting Arc #7 (Orbit 2932)
---------------------------------------

Vector Time (GMT): 2009/316/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2827590
52                 A    =         6718562
82  meter
 Y    =       -4509808
30  meter          E    =           
0006692
 Z    =        4092447
46                 I    =           51
30557
 XDOT =       3614
184235                 Wp   =           69
71111
 YDOT =       5677
221804  meter/sec      RA   =          264
07502  deg
 ZDOT =       3756
394029                 TA   =          341
63511
                                          MA   =          341
65926
                                          Ha   =            186
522  n
mi
                                          Hp   =            181
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9276871
78                 X    =         2857928
98
 Y    =      -14795959
00  feet           Y    =        -4478018
86  meter
 Z    =       13426664
88                 Z    =         4106257
94
 XDOT =      11857
559825                 XDOT =        3532
183617
 YDOT =      18626
055788  feet/sec       YDOT =        5717
179281  meter/sec
 ZDOT =      12324
127393                 ZDOT =        3773
752929

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7809733
19                 X    =         2380406
68
 Y    =       15573310
83  feet           Y    =         4746745
14  meter
 Z    =       13480954
72                 Z    =         4108995
00
 XDOT =     -20903
730888                 XDOT =       -6371
457175
 YDOT =       -252
479140  feet/sec       YDOT =         -76
955642  meter/sec
 ZDOT =      12392
826277                 ZDOT =        3777
333449


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   09316
57521141  
00016717  00000-0  10270-3 0  9068
2 25544  51
6432 264
5627 0006272 321
8911  38
1809 15
76196044 29336


Satellite: ISS
Catalog Number: 25544
Epoch time:      09316
57521141   =   yrday
fracday
Element set:     906
Inclination:       51
6432  deg
RA of node:       264
5627  deg
Eccentricity:     
0006272     
Arg of perigee:   321
8911  deg
Mean anomaly:      38
1809  deg
Mean motion:   15
76196044  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2933
Checksum:              308


Coasting Arc #8 (Orbit 2947)
---------------------------------------

Vector Time (GMT): 2009/317/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3212476
67                 A    =         6722777
20  meter
 Y    =       -5263836
13  meter          E    =           
0008083
 Z    =       -2665945
40                 I    =           51
32403
 XDOT =       3312
782445                 Wp   =            3
55943
 YDOT =      -4641
689465  meter/sec      RA   =          258
85062  deg
 ZDOT =       5181
765728                 TA   =          325
89043
                                          MA   =          325
94235
                                          Ha   =            186
732  n
mi
                                          Hp   =            181
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10539621
62                 X    =        -3140425
73
 Y    =      -17269803
56  feet           Y    =        -5299357
06  meter
 Z    =       -8746540
02                 Z    =        -2681377
06
 XDOT =      10868
708808                 XDOT =        3339
267616
 YDOT =     -15228
639976  feet/sec       YDOT =       -4604
495917  meter/sec
 ZDOT =      17000
543726                 ZDOT =        5197
923990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20203613
53                 X    =         6158061
40
 Y    =        -267330
64  feet           Y    =          -81482
38  meter
 Z    =       -8807623
75                 Z    =        -2684563
72
 XDOT =       7632
052356                 XDOT =        2326
249558
 YDOT =      15536
418312  feet/sec       YDOT =        4735
500302  meter/sec
 ZDOT =      17064
088277                 ZDOT =        5201
134107


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   09317
52622860  
00016717  00000-0  10270-3 0  9075
2 25544  51
6430 259
6629 0006406 326
2728  33
8028 15
76199133 29488


Satellite: ISS
Catalog Number: 25544
Epoch time:      09317
52622860   =   yrday
fracday
Element set:     907
Inclination:       51
6430  deg
RA of node:       259
6629  deg
Eccentricity:     
0006406     
Arg of perigee:   326
2728  deg
Mean anomaly:      33
8028  deg
Mean motion:   15
76199133  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2948
Checksum:              327


Coasting Arc #9 (Orbit 2963)
---------------------------------------

Vector Time (GMT): 2009/318/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3023086
68                 A    =         6715378
89  meter
 Y    =        3529183
21  meter          E    =           
0012557
 Z    =       -4858574
02                 I    =           51
30764
 XDOT =      -3740
675125                 Wp   =           43
94484
 YDOT =      -6331
763055  meter/sec      RA   =          253
71602  deg
 ZDOT =      -2266
356098                 TA   =          203
85810
                                          MA   =          203
91635
                                          Ha   =            186
830  n
mi
                                          Hp   =            181
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9918263
39                 X    =        -3038723
12
 Y    =       11578685
07  feet           Y    =         3495289
96  meter
 Z    =      -15940203
47                 Z    =        -4873298
53
 XDOT =     -12272
556184                 XDOT =       -3658
584333
 YDOT =     -20773
500836  feet/sec       YDOT =       -6373
134440  meter/sec
 ZDOT =      -7435
551504                 ZDOT =       -2284
329622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5232469
56                 X    =        -1594856
72
 Y    =      -14255130
63  feet           Y    =        -4344963
81  meter
 Z    =      -15998140
41                 Z    =        -4876233
20
 XDOT =      23062
961309                 XDOT =        7029
590607
 YDOT =        -21
024407  feet/sec       YDOT =          -6
408239  meter/sec
 ZDOT =      -7506
707596                 ZDOT =       -2288
044475


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   09318
54061949  
00016717  00000-0  10270-3 0  9084
2 25544  51
6440 254
4362 0006334 330
6659  29
4149 15
76269028 29642


Satellite: ISS
Catalog Number: 25544
Epoch time:      09318
54061949   =   yrday
fracday
Element set:     908
Inclination:       51
6440  deg
RA of node:       254
4362  deg
Eccentricity:     
0006334     
Arg of perigee:   330
6659  deg
Mean anomaly:      29
4149  deg
Mean motion:   15
76269028  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2964
Checksum:              330


Coasting Arc #10 (Orbit 2979)
---------------------------------------

Vector Time (GMT): 2009/319/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3311806
53                 A    =         6724973
93  meter
 Y    =        5718491
96  meter          E    =           
0009300
 Z    =        1233880
53                 I    =           51
35042
 XDOT =      -3684
081532                 Wp   =           99
90513
 YDOT =       3402
532700  meter/sec      RA   =          248
51065  deg
 ZDOT =      -5845
175417                 TA   =           66
50210
                                          MA   =           66
40439
                                          Ha   =            186
914  n
mi
                                          Hp   =            180
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10865507
00                 X    =         3241621
05
 Y    =       18761456
57  feet           Y    =         5755134
05  meter
 Z    =        4048164
46                 Z    =         1249799
59
 XDOT =     -12086
881668                 XDOT =       -3693
459705
 YDOT =      11163
165026  feet/sec       YDOT =        3361
282972  meter/sec
 ZDOT =     -19177
084700                 ZDOT =       -5863
095884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21661573
58                 X    =        -6602447
63
 Y    =         559860
25  feet           Y    =          170645
40  meter
 Z    =        4111194
09                 Z    =         1253091
96
 XDOT =      -4043
887103                 XDOT =       -1232
576789
 YDOT =     -14273
270760  feet/sec       YDOT =       -4350
492928  meter/sec
 ZDOT =     -19247
637921                 ZDOT =       -5866
680038


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   09319
55498327  
00016717  00000-0  10270-3 0  9091
2 25544  51
6445 249
2099 0006299 334
1504  25
9345 15
76293016 29805


Satellite: ISS
Catalog Number: 25544
Epoch time:      09319
55498327   =   yrday
fracday
Element set:     909
Inclination:       51
6445  deg
RA of node:       249
2099  deg
Eccentricity:     
0006299     
Arg of perigee:   334
1504  deg
Mean anomaly:      25
9345  deg
Mean motion:   15
76293016  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2980
Checksum:              340


Coasting Arc #11 (Orbit 2995)
---------------------------------------

Vector Time (GMT): 2009/320/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3472982
34                 A    =         6713422
01  meter
 Y    =       -2397038
58  meter          E    =           
0004707
 Z    =        5220979
70                 I    =           51
32430
 XDOT =       3819
670820                 Wp   =             
39294
 YDOT =       6671
691487  meter/sec      RA   =          243
35289  deg
 ZDOT =        526
892177                 TA   =           84
60929
                                          MA   =           84
55559
                                          Ha   =            186
762  n
mi
                                          Hp   =            180
714

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11394299
00                 X    =         3474164
94
 Y    =       -7864299
82  feet           Y    =        -2358195
40  meter
 Z    =       17129198
49                 Z    =         5237854
69
 XDOT =      12531
728413                 XDOT =        3742
223284
 YDOT =      21888
751599  feet/sec       YDOT =        6713
972230  meter/sec
 ZDOT =       1728
648876                 ZDOT =         545
261068

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1747054
18                 X    =          532502
11
 Y    =       13650761
50  feet           Y    =         4160752
11  meter
 Z    =       17195674
30                 Z    =         5241241
53
 XDOT =     -24202
874931                 XDOT =       -7377
036279
 YDOT =        847
470801  feet/sec       YDOT =         258
309100  meter/sec
 ZDOT =       1801
385426                 ZDOT =         549
062278


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   09320
56931781  
00016717  00000-0  10270-3 0  9102
2 25544  51
6443 243
9835 0006345 336
5187  23
5687 15
76377235 29963


Satellite: ISS
Catalog Number: 25544
Epoch time:      09320
56931781   =   yrday
fracday
Element set:     910
Inclination:       51
6443  deg
RA of node:       243
9835  deg
Eccentricity:     
0006345     
Arg of perigee:   336
5187  deg
Mean anomaly:      23
5687  deg
Mean motion:   15
76377235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2996
Checksum:              339


Coasting Arc #12 (Orbit 3011)
---------------------------------------

Vector Time (GMT): 2009/321/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3307452
13                 A    =         6725409
95  meter
 Y    =       -5834788
80  meter          E    =           
0016453
 Z    =         333392
99                 I    =           51
37935
 XDOT =       4341
607805                 Wp   =           27
56530
 YDOT =      -2111
642013  meter/sec      RA   =          238
17739  deg
 ZDOT =       6011
477356                 TA   =          336
07797
                                          MA   =          336
15433
                                          Ha   =            187
025  n
mi
                                          Hp   =            180
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10851220
90                 X    =        -3243580
29
 Y    =      -19143007
88  feet           Y    =        -5871417
58  meter
 Z    =        1093809
04                 Z    =          317479
56
 XDOT =      14244
120095                 XDOT =        4335
694361
 YDOT =      -6927
959360  feet/sec       YDOT =       -2063
125193  meter/sec
 ZDOT =      19722
694736                 ZDOT =        6032
554945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21977703
78                 X    =         6698804
11
 Y    =       -1148118
82  feet           Y    =         -349946
62  meter
 Z    =        1030787
82                 Z    =          314184
13
 XDOT =       -207
532533                 XDOT =         -63
255916
 YDOT =      14132
430161  feet/sec       YDOT =        4307
564713  meter/sec
 ZDOT =      19805
769883                 ZDOT =        6036
798660


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   09321
58362876  
00016717  00000-0  10270-3 0  9119
2 25544  51
6445 238
7566 0006399 341
6214  18
4718 15
76368835 30129


Satellite: ISS
Catalog Number: 25544
Epoch time:      09321
58362876   =   yrday
fracday
Element set:     911
Inclination:       51
6445  deg
RA of node:       238
7566  deg
Eccentricity:     
0006399     
Arg of perigee:   341
6214  deg
Mean anomaly:      18
4718  deg
Mean motion:   15
76368835  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3012
Checksum:              332


Coasting Arc #13 (Orbit 3026)
---------------------------------------

Vector Time (GMT): 2009/322/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4151013
27                 A    =         6713728
48  meter
 Y    =        1299126
39  meter          E    =           
0012889
 Z    =       -5124172
78                 I    =           51
35797
 XDOT =      -3684
752913                 Wp   =           73
55170
 YDOT =      -6628
882829  meter/sec      RA   =          232
99025  deg
 ZDOT =       1310
663824                 TA   =          209
00555
                                          MA   =          209
07722
                                          Ha   =            187
015  n
mi
                                          Hp   =            180
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13618809
94                 X    =        -4140338
89
 Y    =        4262225
68  feet           Y    =         1252767
51  meter
 Z    =      -16811590
48                 Z    =        -5144312
85
 XDOT =     -12089
084360                 XDOT =       -3616
720853
 YDOT =     -21748
303246  feet/sec       YDOT =       -6669
707655  meter/sec
 ZDOT =       4300
078162                 ZDOT =        1292
927423

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1994735
43                 X    =          607995
36
 Y    =      -14035063
03  feet           Y    =        -4277887
21  meter
 Z    =      -16891008
34                 Z    =        -5148379
34
 XDOT =      23823
675744                 XDOT =        7261
456367
 YDOT =      -1679
769774  feet/sec       YDOT =        -511
993827  meter/sec
 ZDOT =       4229
823974                 ZDOT =        1289
250347


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   09322
53451801  
00016717  00000-0  10270-3 0  9123
2 25544  51
6449 233
8566 0006356 344
8982  15
1991 15
76429128 30275


Satellite: ISS
Catalog Number: 25544
Epoch time:      09322
53451801   =   yrday
fracday
Element set:     912
Inclination:       51
6449  deg
RA of node:       233
8566  deg
Eccentricity:     
0006356     
Arg of perigee:   344
8982  deg
Mean anomaly:      15
1991  deg
Mean motion:   15
76429128  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3027
Checksum:              322


Coasting Arc #14 (Orbit 3042)
---------------------------------------

Vector Time (GMT): 2009/323/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3039476
91                 A    =         6723600
69  meter
 Y    =        5673666
39  meter          E    =           
0003123
 Z    =       -1947808
37                 I    =           51
41039
 XDOT =      -5219
902539                 Wp   =           77
07011
 YDOT =        879
858038  meter/sec      RA   =          227
84700  deg
 ZDOT =      -5589
384258                 TA   =          124
68033
                                          MA   =          124
65090
                                          Ha   =            187
106  n
mi
                                          Hp   =            180
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9972037
11                 X    =         2985269
38
 Y    =       18614391
03  feet           Y    =         5707352
73  meter
 Z    =       -6390447
40                 Z    =        -1933173
34
 XDOT =     -17125
664499                 XDOT =       -5202
200526
 YDOT =       2886
673354  feet/sec       YDOT =         821
585587  meter/sec
 ZDOT =     -18337
874862                 ZDOT =       -5614
699981

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21091375
99                 X    =        -6428651
40
 Y    =        1352292
99  feet           Y    =          412178
90  meter
 Z    =       -6332460
65                 Z    =        -1930134
01
 XDOT =       4558
421794                 XDOT =        1389
406963
 YDOT =     -15137
082077  feet/sec       YDOT =       -4613
782617  meter/sec
 ZDOT =     -18437
743836                 ZDOT =       -5619
824321


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   09323
54877483  
00016717  00000-0  10270-3 0  9134
2 25544  51
6449 228
6295 0006282 347
6229  12
4780 15
76444361 30439


Satellite: ISS
Catalog Number: 25544
Epoch time:      09323
54877483   =   yrday
fracday
Element set:     913
Inclination:       51
6449  deg
RA of node:       228
6295  deg
Eccentricity:     
0006282     
Arg of perigee:   347
6229  deg
Mean anomaly:      12
4780  deg
Mean motion:   15
76444361  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3043
Checksum:              327


Coasting Arc #15 (Orbit 3058)
---------------------------------------

Vector Time (GMT): 2009/324/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 716700
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4978280
65                 A    =         6716032
80  meter
 Y    =        -295482
76  meter          E    =           
0012139
 Z    =        4497285
10                 I    =           51
40642
 XDOT =       3185
296698                 Wp   =           35
64702
 YDOT =       6294
080615  meter/sec      RA   =          222
63521  deg
 ZDOT =      -3098
516140                 TA   =           85
38900
                                          MA   =           85
25036
                                          Ha   =            187
052  n
mi
                                          Hp   =            179
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16332941
77                 X    =         4959367
43
 Y    =        -969431
61  feet           Y    =         -239918
91  meter
 Z    =       14754872
38                 Z    =         4521424
03
 XDOT =      10450
448485                 XDOT =        3129
730734
 YDOT =      20649
870784  feet/sec       YDOT =        6329
390119  meter/sec
 ZDOT =     -10165
735366                 ZDOT =       -3083
176018

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5619806
31                 X    =        -1712916
96
 Y    =       15274239
14  feet           Y    =         4655588
09  meter
 Z    =       14850132
63                 Z    =         4526320
43
 XDOT =     -22016
619959                 XDOT =       -6710
665764
 YDOT =       1767
957512  feet/sec       YDOT =         538
873450  meter/sec
 ZDOT =     -10104
929579                 ZDOT =       -3079
982536


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   09324
56300389  
00016717  00000-0  10270-3 0  9144
2 25544  51
6443 223
4023 0006462 351
7319   8
3738 15
76534950 30599


Satellite: ISS
Catalog Number: 25544
Epoch time:      09324
56300389   =   yrday
fracday
Element set:     914
Inclination:       51
6443  deg
RA of node:       223
4023  deg
Eccentricity:     
0006462     
Arg of perigee:   351
7319  deg
Mean anomaly:       8
3738  deg
Mean motion:   15
76534950  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3059
Checksum:              307

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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