Date: November 14th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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 2947)
---------------------------------------

Vector Time (GMT): 2009/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1071666
50                 A    =         6722398
40  meter
 Y    =        6040567
92  meter          E    =           
0002964
 Z    =       -2752970
72                 I    =           51
32411
 XDOT =      -4790
515497                 Wp   =           11
39164
 YDOT =      -3182
770433  meter/sec      RA   =          259
00928  deg
 ZDOT =      -5116
871475                 TA   =          200
23731
                                          MA   =          200
24906
                                          Ha   =            186
725  n
mi
                                          Hp   =            181
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3515966
19                 X    =        -1125759
72
 Y    =       19818136
23  feet           Y    =         6028281
48  meter
 Z    =       -9032056
17                 Z    =        -2758308
39
 XDOT =     -15716
914359                 XDOT =       -4729
711619
 YDOT =     -10442
160212  feet/sec       YDOT =       -3236
000806  meter/sec
 ZDOT =     -16787
636072                 ZDOT =       -5139
996773

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13475939
06                 X    =        -4107466
23
 Y    =      -14937982
41  feet           Y    =        -4553097
04  meter
 Z    =       -9052862
99                 Z    =        -2759312
64
 XDOT =      16758
673619                 XDOT =        5108
043719
 YDOT =      -4885
440079  feet/sec       YDOT =       -1489
082136  meter/sec
 ZDOT =     -16878
981230                 ZDOT =       -5144
713479


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
52615796  
00016717  00000-0  10270-3 0  9008
2 25544  51
6440 259
6680 0006402 327
0337  33
0428 15
76272234 29487


Satellite: ISS
Catalog Number: 25544
Epoch time:      09317
52615796   =   yrday
fracday
Element set:     900
Inclination:       51
6440  deg
RA of node:       259
6680  deg
Eccentricity:     
0006402     
Arg of perigee:   327
0337  deg
Mean anomaly:      33
0428  deg
Mean motion:   15
76272234  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2948
Checksum:              309


Coasting Arc #2 (Orbit 2963)
---------------------------------------

Vector Time (GMT): 2009/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4290355
85                 A    =         6718570
29  meter
 Y    =        3268179
88  meter          E    =           
0010805
 Z    =        4005756
64                 I    =           51
31885
 XDOT =      -1335
435188                 Wp   =           43
04468
 YDOT =       6521
216695  meter/sec      RA   =          253
78473  deg
 ZDOT =      -3876
214989                 TA   =           87
15446
                                          MA   =           87
03080
                                          Ha   =            186
770  n
mi
                                          Hp   =            181
054

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14075970
64                 X    =         4234031
77
 Y    =       10722374
92  feet           Y    =         3315842
14  meter
 Z    =       13142246
18                 Z    =         4026463
10
 XDOT =      -4381
349043                 XDOT =       -1389
426775
 YDOT =      21395
067896  feet/sec       YDOT =        6505
981283  meter/sec
 ZDOT =     -12717
240779                 ZDOT =       -3882
833727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16992192
67                 X    =        -5179220
33
 Y    =        4712813
43  feet           Y    =         1436465
53  meter
 Z    =       13224057
10                 Z    =         4030692
60
 XDOT =     -14137
380534                 XDOT =       -4309
073587
 YDOT =     -15088
389204  feet/sec       YDOT =       -4598
941029  meter/sec
 ZDOT =     -12743
081762                 ZDOT =       -3884
091321


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
54052138  
00016717  00000-0  10270-3 0  9017
2 25544  51
6444 254
4418 0006395 330
5538  29
5265 15
76295311 29644


Satellite: ISS
Catalog Number: 25544
Epoch time:      09318
54052138   =   yrday
fracday
Element set:     901
Inclination:       51
6444  deg
RA of node:       254
4418  deg
Eccentricity:     
0006395     
Arg of perigee:   330
5538  deg
Mean anomaly:      29
5265  deg
Mean motion:   15
76295311  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2964
Checksum:              315


Coasting Arc #3 (Orbit 2979)
---------------------------------------

Vector Time (GMT): 2009/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1320315
82                 A    =         6718770
28  meter
 Y    =       -5275811
83  meter          E    =           
0008855
 Z    =        3935499
12                 I    =           51
32961
 XDOT =       5069
074607                 Wp   =           65
99305
 YDOT =       4235
497805  meter/sec      RA   =          248
66099  deg
 ZDOT =       3973
898144                 TA   =          342
67255
                                          MA   =          342
70275
                                          Ha   =            186
807  n
mi
                                          Hp   =            180
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4331744
83                 X    =         1360094
18
 Y    =      -17309093
93  feet           Y    =        -5260825
05  meter
 Z    =       12911742
50                 Z    =         3942009
79
 XDOT =      16630
822203                 XDOT =        5002
030676
 YDOT =      13895
990174  feet/sec       YDOT =        4291
808136  meter/sec
 ZDOT =      13037
723571                 ZDOT =        3998
361857

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11486605
56                 X    =         3501117
38
 Y    =       13629685
01  feet           Y    =         4154327
99  meter
 Z    =       12937210
66                 Z    =         3943261
81
 XDOT =     -19984
482828                 XDOT =       -6091
270366
 YDOT =       4364
340848  feet/sec       YDOT =        1330
251090  meter/sec
 ZDOT =      13134
399173                 ZDOT =        4003
364868


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
55486646  
00016717  00000-0  10270-3 0  9025
2 25544  51
6447 249
2152 0006350 334
2337  25
8510 15
76327315 29803


Satellite: ISS
Catalog Number: 25544
Epoch time:      09319
55486646   =   yrday
fracday
Element set:     902
Inclination:       51
6447  deg
RA of node:       249
2152  deg
Eccentricity:     
0006350     
Arg of perigee:   334
2337  deg
Mean anomaly:      25
8510  deg
Mean motion:   15
76327315  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2980
Checksum:              312


Coasting Arc #4 (Orbit 2994)
---------------------------------------

Vector Time (GMT): 2009/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4556544
77                 A    =         6721939
01  meter
 Y    =       -4039463
36  meter          E    =           
0008194
 Z    =       -2837718
43                 I    =           51
35274
 XDOT =       1759
695898                 Wp   =           12
17568
 YDOT =      -5534
624442  meter/sec      RA   =          243
43658  deg
 ZDOT =       5063
473344                 TA   =          315
08314
                                          MA   =          315
14941
                                          Ha   =            186
910  n
mi
                                          Hp   =            180
659

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14949293
85                 X    =        -4497250
57
 Y    =      -13252832
55  feet           Y    =        -4090085
60  meter
 Z    =       -9310099
83                 Z    =        -2859711
08
 XDOT =       5773
280506                 XDOT =        1796
856034
 YDOT =     -18158
216674  feet/sec       YDOT =       -5514
739066  meter/sec
 ZDOT =      16612
445355                 ZDOT =        5072
112096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19405586
74                 X    =         5914822
84
 Y    =       -4573404
53  feet           Y    =        -1393973
70  meter
 Z    =       -9397025
60                 Z    =        -2864213
40
 XDOT =      11264
734454                 XDOT =        3433
491062
 YDOT =      13664
928671  feet/sec       YDOT =        4165
070259  meter/sec
 ZDOT =      16646
301508                 ZDOT =        5073
792700


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
50579931  
00016717  00000-0  10270-3 0  9033
2 25544  51
6448 244
3154 0006457 337
7684  22
3199 15
76340766 29959


Satellite: ISS
Catalog Number: 25544
Epoch time:      09320
50579931   =   yrday
fracday
Element set:     903
Inclination:       51
6448  deg
RA of node:       244
3154  deg
Eccentricity:     
0006457     
Arg of perigee:   337
7684  deg
Mean anomaly:      22
3199  deg
Mean motion:   15
76340766  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2995
Checksum:              336


Coasting Arc #5 (Orbit 3010)
---------------------------------------

Vector Time (GMT): 2009/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1833758
32                 A    =         6715312
30  meter
 Y    =        4337033
77  meter          E    =           
0013534
 Z    =       -4799595
85                 I    =           51
34594
 XDOT =      -5352
697524                 Wp   =           44
08092
 YDOT =      -4963
030539  meter/sec      RA   =          238
30595  deg
 ZDOT =      -2434
167605                 TA   =          201
99352
                                          MA   =          202
05166
                                          Ha   =            187
069  n
mi
                                          Hp   =            180
344

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6016267
45                 X    =        -1858803
25
 Y    =       14229113
42  feet           Y    =         4316388
00  meter
 Z    =      -15746705
53                 Z    =        -4808564
95
 XDOT =     -17561
343583                 XDOT =       -5284
977134
 YDOT =     -16282
908593  feet/sec       YDOT =       -5022
508698  meter/sec
 ZDOT =      -7986
114189                 ZDOT =       -2460
007706

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8463015
25                 X    =        -2579527
05
 Y    =      -12881394
80  feet           Y    =        -3926249
13  meter
 Z    =      -15781917
46                 Z    =        -4810328
44
 XDOT =      22362
439110                 XDOT =        6816
071441
 YDOT =      -4760
564180  feet/sec       YDOT =       -1451
019962  meter/sec
 ZDOT =      -8088
265062                 ZDOT =       -2465
303191


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
52010990  
00016717  00000-0  10270-3 0  9042
2 25544  51
6455 239
0888 0006441 342
5179  17
5756 15
76390967 30111


Satellite: ISS
Catalog Number: 25544
Epoch time:      09321
52010990   =   yrday
fracday
Element set:     904
Inclination:       51
6455  deg
RA of node:       239
0888  deg
Eccentricity:     
0006441     
Arg of perigee:   342
5179  deg
Mean anomaly:      17
5756  deg
Mean motion:   15
76390967  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3011
Checksum:              317


Coasting Arc #6 (Orbit 3026)
---------------------------------------

Vector Time (GMT): 2009/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4763395
05                 A    =         6724547
28  meter
 Y    =        4546438
03  meter          E    =           
0010624
 Z    =        1351982
93                 I    =           51
39388
 XDOT =      -2517
934487                 Wp   =           94
26208
 YDOT =       4378
511435  meter/sec      RA   =          233
10061  deg
 ZDOT =      -5814
259238                 TA   =           70
82389
                                          MA   =           70
70893
                                          Ha   =            187
159  n
mi
                                          Hp   =            180
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15627936
52                 X    =         4705634
10
 Y    =       14916135
28  feet           Y    =         4599382
03  meter
 Z    =        4435639
55                 Z    =         1374984
25
 XDOT =      -8260
939918                 XDOT =       -2538
463298
 YDOT =      14365
194997  feet/sec       YDOT =        4350
240215  meter/sec
 ZDOT =     -19075
653667                 ZDOT =       -5826
541093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21016210
35                 X    =        -6405740
92
 Y    =        4922126
57  feet           Y    =         1500264
18  meter
 Z    =        4526583
93                 Z    =         1379702
78
 XDOT =      -7222
996619                 XDOT =       -2201
569369
 YDOT =     -13139
620990  feet/sec       YDOT =       -4004
956478  meter/sec
 ZDOT =     -19123
939075                 ZDOT =       -5828
976630


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
53440332  
00016717  00000-0  10270-3 0  9052
2 25544  51
6452 233
8622 0006406 345
8000  14
2983 15
76392259 30275


Satellite: ISS
Catalog Number: 25544
Epoch time:      09322
53440332   =   yrday
fracday
Element set:     905
Inclination:       51
6452  deg
RA of node:       233
8622  deg
Eccentricity:     
0006406     
Arg of perigee:   345
8000  deg
Mean anomaly:      14
2983  deg
Mean motion:   15
76392259  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3027
Checksum:              291


Coasting Arc #7 (Orbit 3042)
---------------------------------------

Vector Time (GMT): 2009/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2624438
50                 A    =         6713229
75  meter
 Y    =       -3311523
32  meter          E    =           
0005168
 Z    =        5215035
62                 I    =           51
37507
 XDOT =       5508
549907                 Wp   =           15
37622
 YDOT =       5352
994797  meter/sec      RA   =          227
94747  deg
 ZDOT =        631
751326                 TA   =           68
62861
                                          MA   =           68
57347
                                          Ha   =            187
053  n
mi
                                          Hp   =            180
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8610362
52                 X    =         2635939
24
 Y    =      -10864577
83  feet           Y    =        -3282111
56  meter
 Z    =       17109696
92                 Z    =         5227812
99
 XDOT =      18072
670297                 XDOT =        5445
213375
 YDOT =      17562
318889  feet/sec       YDOT =        5414
240449  meter/sec
 ZDOT =       2072
674953                 ZDOT =         658
359149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4676521
25                 X    =         1425403
68
 Y    =       12983996
37  feet           Y    =         3957522
09  meter
 Z    =       17159985
72                 Z    =         5230363
65
 XDOT =     -23529
899840                 XDOT =       -7171
913471
 YDOT =       5617
168352  feet/sec       YDOT =        1712
112914  meter/sec
 ZDOT =       2177
897258                 ZDOT =         663
823084


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
54867714  
00016717  00000-0  10270-3 0  9062
2 25544  51
6450 228
6353 0006451 348
4848  11
6168 15
76460464 30433


Satellite: ISS
Catalog Number: 25544
Epoch time:      09323
54867714   =   yrday
fracday
Element set:     906
Inclination:       51
6450  deg
RA of node:       228
6353  deg
Eccentricity:     
0006451     
Arg of perigee:   348
4848  deg
Mean anomaly:      11
6168  deg
Mean motion:   15
76460464  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3043
Checksum:              319


Coasting Arc #8 (Orbit 3058)
---------------------------------------

Vector Time (GMT): 2009/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4778136
17                 A    =         6725211
01  meter
 Y    =       -4710279
75  meter          E    =           
0017368
 Z    =         266782
66                 I    =           51
43649
 XDOT =       3551
903751                 Wp   =           29
88126
 YDOT =      -3253
406780  meter/sec      RA   =          222
77367  deg
 ZDOT =       6021
028556                 TA   =          333
03129
                                          MA   =          333
12144
                                          Ha   =            187
301  n
mi
                                          Hp   =            179
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15676299
76                 X    =        -4726405
88
 Y    =      -15453673
72  feet           Y    =        -4763422
47  meter
 Z    =         875271
18                 Z    =          243695
24
 XDOT =      11653
227531                 XDOT =        3558
770364
 YDOT =     -10673
906760  feet/sec       YDOT =       -3213
649537  meter/sec
 ZDOT =      19754
030696                 ZDOT =        6038
300337

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21335531
11                 X    =         6503069
88
 Y    =       -5432221
80  feet           Y    =        -1655741
20  meter
 Z    =         783954
00                 Z    =          238949
18
 XDOT =       2774
520735                 XDOT =         845
673920
 YDOT =      13838
489096  feet/sec       YDOT =        4217
971476  meter/sec
 ZDOT =      19822
064682                 ZDOT =        6041
765315


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
56293657  
00016717  00000-0  10270-3 0  9075
2 25544  51
6450 223
4081 0006568 353
0393   7
0679 15
76445455 30596


Satellite: ISS
Catalog Number: 25544
Epoch time:      09324
56293657   =   yrday
fracday
Element set:     907
Inclination:       51
6450  deg
RA of node:       223
4081  deg
Eccentricity:     
0006568     
Arg of perigee:   353
0393  deg
Mean anomaly:       7
0679  deg
Mean motion:   15
76445455  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3059
Checksum:              325


Coasting Arc #9 (Orbit 3073)
---------------------------------------

Vector Time (GMT): 2009/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3613746
64                 A    =         6713499
34  meter
 Y    =        2391180
95  meter          E    =           
0014295
 Z    =       -5138784
33                 I    =           51
42065
 XDOT =      -5348
645356                 Wp   =           73
25877
 YDOT =      -5387
533598  meter/sec      RA   =          217
59137  deg
 ZDOT =       1261
340248                 TA   =          208
80416
                                          MA   =          208
88316
                                          Ha   =            187
315  n
mi
                                          Hp   =            179
562

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11856124
15                 X    =        -3615253
02
 Y    =        7845081
86  feet           Y    =         2350761
98  meter
 Z    =      -16859528
64                 Z    =        -5156343
59
 XDOT =     -17548
049069                 XDOT =       -5294
130937
 YDOT =     -17675
635164  feet/sec       YDOT =       -5447
040619  meter/sec
 ZDOT =       4138
255408                 ZDOT =        1235
488063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -878477
13                 X    =         -267759
83
 Y    =      -14106833
68  feet           Y    =        -4299762
91  meter
 Z    =      -16928739
37                 Z    =        -5159879
76
 XDOT =      23081
210947                 XDOT =        7035
153097
 YDOT =      -6253
452187  feet/sec       YDOT =       -1906
052227  meter/sec
 ZDOT =       4035
981923                 ZDOT =        1230
167290


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   09325
51378681  
00016717  00000-0  10270-3 0  9083
2 25544  51
6452 218
5077 0006549 356
2239   3
8875 15
76492625 30741


Satellite: ISS
Catalog Number: 25544
Epoch time:      09325
51378681   =   yrday
fracday
Element set:     908
Inclination:       51
6452  deg
RA of node:       218
5077  deg
Eccentricity:     
0006549     
Arg of perigee:   356
2239  deg
Mean anomaly:       3
8875  deg
Mean motion:   15
76492625  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3074
Checksum:              338


Coasting Arc #10 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2009/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4460120
18                 A    =         6723552
44  meter
 Y    =        4651159
55  meter          E    =           
0004407
 Z    =       -1924050
22                 I    =           51
47891
 XDOT =      -4767
779883                 Wp   =           78
31627
 YDOT =       2256
904043  meter/sec      RA   =          212
45160  deg
 ZDOT =      -5606
277968                 TA   =          123
13289
                                          MA   =          123
09060
                                          Ha   =            187
417  n
mi
                                          Hp   =            179
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14632940
23                 X    =         4417125
42
 Y    =       15259709
82  feet           Y    =         4700795
01  meter
 Z    =       -6312500
73                 Z    =        -1902486
74
 XDOT =     -15642
322452                 XDOT =       -4765
428001
 YDOT =       7404
540822  feet/sec       YDOT =        2203
601528  meter/sec
 ZDOT =     -18393
300421                 ZDOT =       -5629
434235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20473644
98                 X    =        -6240366
99
 Y    =        5374152
77  feet           Y    =         1638041
76  meter
 Z    =       -6227173
70                 Z    =        -1898042
54
 XDOT =       1496
200321                 XDOT =         456
041858
 YDOT =     -15680
342368  feet/sec       YDOT =       -4779
368354  meter/sec
 ZDOT =     -18484
617912                 ZDOT =       -5634
111540


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   09326
52801169  
00016717  00000-0  10270-3 0  9098
2 25544  51
6452 213
2802 0006441 358
9751   1
1399 15
76480002 30904


Satellite: ISS
Catalog Number: 25544
Epoch time:      09326
52801169   =   yrday
fracday
Element set:     909
Inclination:       51
6452  deg
RA of node:       213
2802  deg
Eccentricity:     
0006441     
Arg of perigee:   358
9751  deg
Mean anomaly:       1
1399  deg
Mean motion:   15
76480002  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3090
Checksum:              296


Coasting Arc #11 (Orbit 3105)
---------------------------------------

Vector Time (GMT): 2009/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4704800
04                 A    =         6715869
59  meter
 Y    =       -1615464
07  meter          E    =           
0013087
 Z    =        4510103
57                 I    =           51
48007
 XDOT =       4761
699816                 Wp   =           39
05829
 YDOT =       5213
854321  meter/sec      RA   =          207
24468  deg
 ZDOT =      -3084
861458                 TA   =           81
79276
                                          MA   =           81
64434
                                          Ha   =            187
354  n
mi
                                          Hp   =            179
262

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15435695
68                 X    =         4700605
23
 Y    =       -5300078
97  feet           Y    =        -1562875
98  meter
 Z    =       14796927
71                 Z    =         4532949
47
 XDOT =      15622
374725                 XDOT =        4718
029567
 YDOT =      17105
821264  feet/sec       YDOT =        5266
858492  meter/sec
 ZDOT =     -10120
936543                 ZDOT =       -3061
834558

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2576095
29                 X    =         -785193
84
 Y    =       16032464
66  feet           Y    =         4886695
23  meter
 Z    =       14887055
38                 Z    =         4537574
48
 XDOT =     -21314
043854                 XDOT =       -6496
520567
 YDOT =       5933
482650  feet/sec       YDOT =        1808
525512  meter/sec
 ZDOT =     -10029
794543                 ZDOT =       -3057
081377


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   09327
54221787  
00016717  00000-0  10270-3 0  9105
2 25544  51
6451 208
0525 0006697   2
5819 357
5379 15
76575966 31065


Satellite: ISS
Catalog Number: 25544
Epoch time:      09327
54221787   =   yrday
fracday
Element set:     910
Inclination:       51
6451  deg
RA of node:       208
0525  deg
Eccentricity:     
0006697     
Arg of perigee:     2
5819  deg
Mean anomaly:     357
5379  deg
Mean motion:   15
76575966  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3106
Checksum:              334


Coasting Arc #12 (Orbit 3121)
---------------------------------------

Vector Time (GMT): 2009/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3742240
89                 A    =         6720020
50  meter
 Y    =       -4425051
47  meter          E    =           
0015004
 Z    =        3383654
15                 I    =           51
52067
 XDOT =       5986
795389                 Wp   =           63
70933
 YDOT =      -1526
322146  meter/sec      RA   =          202
12821  deg
 ZDOT =       4615
990638                 TA   =          336
38787
                                          MA   =          336
45667
                                          Ha   =            187
660  n
mi
                                          Hp   =            179
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12277693
20                 X    =        -3708918
46
 Y    =      -14517885
40  feet           Y    =        -4466713
28  meter
 Z    =       11101227
54                 Z    =         3365554
80
 XDOT =      19641
717157                 XDOT =        5980
994082
 YDOT =      -5007
618588  feet/sec       YDOT =       -1459
406951  meter/sec
 ZDOT =      15144
326239                 ZDOT =        4645
060714

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18553279
32                 X    =         5655039
54
 Y    =       -4344251
11  feet           Y    =        -1324127
74  meter
 Z    =       11029565
19                 Z    =         3361811
47
 XDOT =      -4797
923908                 XDOT =       -1462
407207
 YDOT =      18327
139668  feet/sec       YDOT =        5586
112171  meter/sec
 ZDOT =      15259
040898                 ZDOT =        4650
955666


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   09328
55641060  
00016717  00000-0  10270-3 0  9118
2 25544  51
6450 202
8243 0006734   7
0654 353
0605 15
76540337 31227


Satellite: ISS
Catalog Number: 25544
Epoch time:      09328
55641060   =   yrday
fracday
Element set:     911
Inclination:       51
6450  deg
RA of node:       202
8243  deg
Eccentricity:     
0006734     
Arg of perigee:     7
0654  deg
Mean anomaly:     353
0605  deg
Mean motion:   15
76540337  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3122
Checksum:              279


Coasting Arc #13 (Orbit 3136)
---------------------------------------

Vector Time (GMT): 2009/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5679365
89                 A    =         6719644
49  meter
 Y    =        1107522
91  meter          E    =           
0008767
 Z    =       -3415284
55                 I    =           51
54826
 XDOT =      -3717
301176                 Wp   =           44
03471
 YDOT =      -4941
811384  meter/sec      RA   =          196
91400  deg
 ZDOT =       4592
268772                 TA   =          275
49481
                                          MA   =          275
59481
                                          Ha   =            187
505  n
mi
                                          Hp   =            178
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18633090
18                 X    =        -5674737
19
 Y    =        3633605
34  feet           Y    =         1044038
91  meter
 Z    =      -11205001
82                 Z    =        -3442864
07
 XDOT =     -12195
870000                 XDOT =       -3684
073468
 YDOT =     -16213
291942  feet/sec       YDOT =       -4983
194849  meter/sec
 ZDOT =      15066
498597                 ZDOT =        4574
290332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4939420
47                 X    =         1505535
36
 Y    =      -18263240
19  feet           Y    =        -5566635
61  meter
 Z    =      -11313858
16                 Z    =        -3448463
97
 XDOT =      18639
198579                 XDOT =        5681
227727
 YDOT =      -4221
680048  feet/sec       YDOT =       -1286
768079  meter/sec
 ZDOT =      14995
282451                 ZDOT =        4570
562091


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   09329
50719856  
00016717  00000-0  10270-3 0  9124
2 25544  51
6448 197
9232 0006694   8
7149 351
4130 15
76582075 31374


Satellite: ISS
Catalog Number: 25544
Epoch time:      09329
50719856   =   yrday
fracday
Element set:     912
Inclination:       51
6448  deg
RA of node:       197
9232  deg
Eccentricity:     
0006694     
Arg of perigee:     8
7149  deg
Mean anomaly:     351
4130  deg
Mean motion:   15
76582075  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3137
Checksum:              332


Coasting Arc #14 (Orbit 3152)
---------------------------------------

Vector Time (GMT): 2009/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2633062
44                 A    =         6715918
79  meter
 Y    =        4220139
53  meter          E    =           
0014680
 Z    =       -4526659
62                 I    =           51
56410
 XDOT =      -6971
673321                 Wp   =           47
36753
 YDOT =       1041
285969  meter/sec      RA   =          191
80165  deg
 ZDOT =      -3081
044713                 TA   =          191
86473
                                          MA   =          191
89936
                                          Ha   =            187
621  n
mi
                                          Hp   =            178
929

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8638656
28                 X    =         2607666
53
 Y    =       13845602
12  feet           Y    =         4249442
15  meter
 Z    =      -14851245
48                 Z    =        -4513929
49
 XDOT =     -22872
943966                 XDOT =       -6967
831556
 YDOT =       3416
292548  feet/sec       YDOT =         963
346197  meter/sec
 ZDOT =     -10108
414414                 ZDOT =       -3114
904396

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16243365
14                 X    =        -4950977
70
 Y    =        1994119
29  feet           Y    =          607807
56  meter
 Z    =      -14800782
06                 Z    =        -4511278
37
 XDOT =       6775
838679                 XDOT =        2065
275629
 YDOT =     -20909
855135  feet/sec       YDOT =       -6373
323845  meter/sec
 ZDOT =     -10242
082938                 ZDOT =       -3121
786879


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   09330
52135766  
00016717  00000-0  10270-3 0  9131
2 25544  51
6441 192
6951 0006679  11
9890 348
1432 15
76605589 31531


Satellite: ISS
Catalog Number: 25544
Epoch time:      09330
52135766   =   yrday
fracday
Element set:     913
Inclination:       51
6441  deg
RA of node:       192
6951  deg
Eccentricity:     
0006679     
Arg of perigee:    11
9890  deg
Mean anomaly:     348
1432  deg
Mean motion:   15
76605589  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3153
Checksum:              326


Coasting Arc #15 (Orbit 3168)
---------------------------------------

Vector Time (GMT): 2009/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6406488
93                 A    =         6723052
69  meter
 Y    =        -758666
80  meter          E    =           
0015011
 Z    =        1881487
67                 I    =           51
61881
 XDOT =       2229
998266                 Wp   =           86
47866
 YDOT =       4752
949528  meter/sec      RA   =          186
60238  deg
 ZDOT =      -5637
262300                 TA   =           72
59501
                                          MA   =           72
43093
                                          Ha   =            187
672  n
mi
                                          Hp   =            178
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21018664
46                 X    =         6405356
18
 Y    =       -2489064
31  feet           Y    =         -687032
07  meter
 Z    =        6172859
80                 Z    =         1912608
34
 XDOT =       7316
267276                 XDOT =        2204
069656
 YDOT =      15593
666431  feet/sec       YDOT =        4777
741933  meter/sec
 ZDOT =     -18494
955054                 ZDOT =       -5626
491509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6343144
80                 X    =        -1933390
53
 Y    =       20154705
23  feet           Y    =         6143154
16  meter
 Z    =        6295733
96                 Z    =         1918939
71
 XDOT =     -15796
834247                 XDOT =       -4814
875078
 YDOT =        831
881140  feet/sec       YDOT =         253
557371  meter/sec
 ZDOT =     -18452
203183                 ZDOT =       -5624
231530


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   09331
53550112  
00016717  00000-0  10270-3 0  9140
2 25544  51
6444 187
4672 0006767  16
6790 343
4596 15
76646408 31696


Satellite: ISS
Catalog Number: 25544
Epoch time:      09331
53550112   =   yrday
fracday
Element set:     914
Inclination:       51
6444  deg
RA of node:       187
4672  deg
Eccentricity:     
0006767     
Arg of perigee:    16
6790  deg
Mean anomaly:     343
4596  deg
Mean motion:   15
76646408  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3169
Checksum:              330

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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