Date: December 13th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9149 32 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 3357)
---------------------------------------

Vector Time (GMT): 2009/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4289717
42                 A    =         6714054
98  meter
 Y    =         858649
39  meter          E    =           
0021030
 Z    =       -5111678
08                 I    =           51
89892
 XDOT =      -3238
675563                 Wp   =           72
83175
 YDOT =       6793
097553  meter/sec      RA   =          124
94153  deg
 ZDOT =      -1576
035198                 TA   =          182
06552
                                          MA   =          182
07422
                                          Ha   =            188
973  n
mi
                                          Hp   =            177
672

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14073876
04                 X    =         4304628
87
 Y    =        2817091
16  feet           Y    =          906703
24  meter
 Z    =      -16770597
39                 Z    =        -5090802
16
 XDOT =     -10625
575993                 XDOT =       -3306
740295
 YDOT =      22287
065463  feet/sec       YDOT =        6756
500301  meter/sec
 ZDOT =      -5170
719154                 ZDOT =       -1591
933736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5795899
40                 X    =        -1766590
14
 Y    =       13235596
30  feet           Y    =         4034209
75  meter
 Z    =      -16688003
68                 Z    =        -5086503
52
 XDOT =     -18524
758199                 XDOT =       -5646
346299
 YDOT =     -14713
663980  feet/sec       YDOT =       -4484
724781  meter/sec
 ZDOT =      -5233
351345                 ZDOT =       -1595
125490


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   09343
51858522  
00016717  00000-0  10270-3 0  9002
2 25544  51
6425 125
7530 0007459  62
8494 297
3430 15
76422209 33581


Satellite: ISS
Catalog Number: 25544
Epoch time:      09343
51858522   =   yrday
fracday
Element set:     900
Inclination:       51
6425  deg
RA of node:       125
7530  deg
Eccentricity:     
0007459     
Arg of perigee:    62
8494  deg
Mean anomaly:     297
3430  deg
Mean motion:   15
76422209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3358
Checksum:              317


Coasting Arc #2 (Orbit 3373)
---------------------------------------

Vector Time (GMT): 2009/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2944285
24                 A    =         6725102
37  meter
 Y    =       -6015558
14  meter          E    =           
0017848
 Z    =         553523
22                 I    =           51
95204
 XDOT =       4504
135439                 Wp   =          107
59876
 YDOT =       1635
355551  meter/sec      RA   =          119
78782  deg
 ZDOT =      -6032
746829                 TA   =           66
39755
                                          MA   =           66
21024
                                          Ha   =            188
952  n
mi
                                          Hp   =            177
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9659728
46                 X    =         3008644
48
 Y    =      -19736083
12  feet           Y    =        -5982273
59  meter
 Z    =        1816021
07                 Z    =          567982
67
 XDOT =      14777
347241                 XDOT =        4514
820243
 YDOT =       5365
339733  feet/sec       YDOT =        1685
783618  meter/sec
 ZDOT =     -19792
476473                 ZDOT =       -6010
839367

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17434387
06                 X    =         5314001
18
 Y    =       13366199
09  feet           Y    =         4074017
48  meter
 Z    =        1873001
15                 Z    =          570890
75
 XDOT =      -7233
213016                 XDOT =       -2204
683327
 YDOT =      12264
248439  feet/sec       YDOT =        3738
142924  meter/sec
 ZDOT =     -19705
772426                 ZDOT =       -6006
319435


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   09344
53285675  
00016717  00000-0  10270-3 0  9019
2 25544  51
6419 120
5244 0007384  66
0542 294
1395 15
76439484 33742


Satellite: ISS
Catalog Number: 25544
Epoch time:      09344
53285675   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:       120
5244  deg
Eccentricity:     
0007384     
Arg of perigee:    66
0542  deg
Mean anomaly:     294
1395  deg
Mean motion:   15
76439484  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3374
Checksum:              325


Coasting Arc #3 (Orbit 3389)
---------------------------------------

Vector Time (GMT): 2009/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3615450
91                 A    =         6713139
57  meter
 Y    =       -2025634
73  meter          E    =           
0009915
 Z    =        5273373
09                 I    =           51
92679
 XDOT =       3426
626059                 Wp   =           71
29822
 YDOT =      -6903
242681  meter/sec      RA   =          114
65831  deg
 ZDOT =       -298
828277                 TA   =           21
54370
                                          MA   =           21
50201
                                          Ha   =            189
102  n
mi
                                          Hp   =            177
432

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11861715
59                 X    =        -3618148
72
 Y    =       -6645783
22  feet           Y    =        -2066080
37  meter
 Z    =       17301092
82                 Z    =         5255802
21
 XDOT =      11242
211480                 XDOT =        3505
016330
 YDOT =     -22648
433992  feet/sec       YDOT =       -6864
485796  meter/sec
 ZDOT =       -980
407734                 ZDOT =        -281
991627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8702389
28                 X    =         2652488
25
 Y    =      -10561129
58  feet           Y    =        -3219032
30  meter
 Z    =       17231526
54                 Z    =         5252169
29
 XDOT =      19466
218669                 XDOT =        5933
303450
 YDOT =      14529
672831  feet/sec       YDOT =        4428
644279  meter/sec
 ZDOT =       -914
040498                 ZDOT =        -278
599544


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   09345
54711620  
00016717  00000-0  10270-3 0  9026
2 25544  51
6429 115
2973 0007449  69
4230 290
7743 15
76448794 33907


Satellite: ISS
Catalog Number: 25544
Epoch time:      09345
54711620   =   yrday
fracday
Element set:     902
Inclination:       51
6429  deg
RA of node:       115
2973  deg
Eccentricity:     
0007449     
Arg of perigee:    69
4230  deg
Mean anomaly:     290
7743  deg
Mean motion:   15
76448794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3390
Checksum:              327


Coasting Arc #4 (Orbit 3405)
---------------------------------------

Vector Time (GMT): 2009/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2989256
09                 A    =         6724656
19  meter
 Y    =        5917440
10  meter          E    =           
0021072
 Z    =        1071750
57                 I    =           51
97829
 XDOT =      -3854
413961                 Wp   =           62
49111
 YDOT =      -3038
153402  meter/sec      RA   =          109
53936  deg
 ZDOT =       5945
251645                 TA   =          309
19686
                                          MA   =          309
38380
                                          Ha   =            188
984  n
mi
                                          Hp   =            177
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9807270
65                 X    =        -3060410
24
 Y    =       19414173
56  feet           Y    =         5883614
52  meter
 Z    =        3516242
04                 Z    =         1057056
30
 XDOT =     -12645
715094                 XDOT =       -3849
035800
 YDOT =      -9967
694889  feet/sec       YDOT =       -3081
226298  meter/sec
 ZDOT =      19505
418782                 ZDOT =        5926
539303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17537071
02                 X    =        -5345299
25
 Y    =      -12882078
54  feet           Y    =        -3926457
54  meter
 Z    =        3458300
61                 Z    =         1054090
03
 XDOT =      10987
675771                 XDOT =        3349
043575
 YDOT =      -9671
072960  feet/sec       YDOT =       -2947
743038  meter/sec
 ZDOT =      19431
305128                 ZDOT =        5922
661803


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   09346
56136077  
00016717  00000-0  10270-3 0  9037
2 25544  51
6439 110
0702 0007480  73
6247 286
5740 15
76478820 34062


Satellite: ISS
Catalog Number: 25544
Epoch time:      09346
56136077   =   yrday
fracday
Element set:     903
Inclination:       51
6439  deg
RA of node:       110
0702  deg
Eccentricity:     
0007480     
Arg of perigee:    73
6247  deg
Mean anomaly:     286
5740  deg
Mean motion:   15
76478820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3406
Checksum:              313


Coasting Arc #5 (Orbit 3420)
---------------------------------------

Vector Time (GMT): 2009/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3154565
61                 A    =         6714485
49  meter
 Y    =        3288795
15  meter          E    =           
0019529
 Z    =       -4948378
38                 I    =           51
95348
 XDOT =      -3425
526716                 Wp   =           95
14898
 YDOT =       6535
845474  meter/sec      RA   =          104
38144  deg
 ZDOT =       2165
663449                 TA   =          195
77294
                                          MA   =          195
83386
                                          Ha   =            188
938  n
mi
                                          Hp   =            177
342

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10349624
72                 X    =         3141594
01
 Y    =       10790010
33  feet           Y    =         3323999
47  meter
 Z    =      -16234837
19                 Z    =        -4933084
32
 XDOT =     -11238
604712                 XDOT =       -3508
877670
 YDOT =      21443
062579  feet/sec       YDOT =        6497
072896  meter/sec
 ZDOT =       7105
195042                 ZDOT =        2148
820326

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12209556
20                 X    =        -3721472
73
 Y    =        8742408
86  feet           Y    =         2664686
22  meter
 Z    =      -16174239
33                 Z    =        -4929908
15
 XDOT =     -18911
643290                 XDOT =       -5764
268875
 YDOT =     -13423
352476  feet/sec       YDOT =       -4091
437835  meter/sec
 ZDOT =       7038
754201                 ZDOT =        2145
412280


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   09347
51220404  
00016717  00000-0  10270-3 0  9042
2 25544  51
6441 105
1706 0007468  76
6217 283
5779 15
76507517 34212


Satellite: ISS
Catalog Number: 25544
Epoch time:      09347
51220404   =   yrday
fracday
Element set:     904
Inclination:       51
6441  deg
RA of node:       105
1706  deg
Eccentricity:     
0007468     
Arg of perigee:    76
6217  deg
Mean anomaly:     283
5779  deg
Mean motion:   15
76507517  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3421
Checksum:              308


Coasting Arc #6 (Orbit 3436)
---------------------------------------

Vector Time (GMT): 2009/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3001676
73                 A    =         6721951
22  meter
 Y    =       -5389804
06  meter          E    =           
0011501
 Z    =       -2676592
85                 I    =           51
98572
 XDOT =       3413
287476                 Wp   =           97
90730
 YDOT =       4491
314386  meter/sec      RA   =           99
28964  deg
 ZDOT =      -5236
794694                 TA   =          112
43624
                                          MA   =          112
31439
                                          Ha   =            188
953  n
mi
                                          Hp   =            177
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9848020
76                 X    =         3074725
96
 Y    =      -17683084
20  feet           Y    =        -5355828
71  meter
 Z    =       -8781472
60                 Z    =        -2661833
83
 XDOT =      11198
449726                 XDOT =        3388
250890
 YDOT =      14735
283420  feet/sec       YDOT =        4529
344554  meter/sec
 ZDOT =     -17181
084954                 ZDOT =       -5220
272866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16244259
42                 X    =         4951250
27
 Y    =       12116871
64  feet           Y    =         3693222
48  meter
 Z    =       -8723227
51                 Z    =        -2658839
74
 XDOT =     -15196
682308                 XDOT =       -4631
948768
 YDOT =       8100
121127  feet/sec       YDOT =        2468
916919  meter/sec
 ZDOT =     -17115
598131                 ZDOT =       -5216
834310


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   09348
52642407  
00016717  00000-0  10270-3 0  9056
2 25544  51
6448  99
9425 0007464  80
2308 279
9699 15
76511627 34379


Satellite: ISS
Catalog Number: 25544
Epoch time:      09348
52642407   =   yrday
fracday
Element set:     905
Inclination:       51
6448  deg
RA of node:        99
9425  deg
Eccentricity:     
0007464     
Arg of perigee:    80
2308  deg
Mean anomaly:     279
9699  deg
Mean motion:   15
76511627  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3437
Checksum:              349


Coasting Arc #7 (Orbit 3452)
---------------------------------------

Vector Time (GMT): 2009/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2869127
13                 A    =         6717854
57  meter
 Y    =       -4495663
51  meter          E    =           
0018243
 Z    =        4071951
16                 I    =           51
97608
 XDOT =       3442
550317                 Wp   =           79
58925
 YDOT =      -5715
672168  meter/sec      RA   =           94
11182  deg
 ZDOT =      -3867
031927                 TA   =           50
02484
                                          MA   =           49
86478
                                          Ha   =            189
069  n
mi
                                          Hp   =            177
184

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9413146
74                 X    =        -2838423
59
 Y    =      -14749552
19  feet           Y    =        -4527576
75  meter
 Z    =       13359419
83                 Z    =         4058086
67
 XDOT =      11294
456420                 XDOT =        3524
993640
 YDOT =     -18752
205274  feet/sec       YDOT =       -5676
713968  meter/sec
 ZDOT =     -12687
112620                 ZDOT =       -3850
108479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15728003
45                 X    =         4793895
45
 Y    =       -7762233
54  feet           Y    =        -2365928
78  meter
 Z    =       13304448
79                 Z    =         4055195
99
 XDOT =      16780
442283                 XDOT =        5114
678808
 YDOT =      12269
531488  feet/sec       YDOT =        3739
753198  meter/sec
 ZDOT =     -12620
296946                 ZDOT =       -3846
666509


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   09349
54063187  
00016717  00000-0  10270-3 0  9062
2 25544  51
6454  94
7159 0007600  83
6133 276
5897 15
76510451 34533


Satellite: ISS
Catalog Number: 25544
Epoch time:      09349
54063187   =   yrday
fracday
Element set:     906
Inclination:       51
6454  deg
RA of node:        94
7159  deg
Eccentricity:     
0007600     
Arg of perigee:    83
6133  deg
Mean anomaly:     276
5897  deg
Mean motion:   15
76510451  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3453
Checksum:              329


Coasting Arc #8 (Orbit 3468)
---------------------------------------

Vector Time (GMT): 2009/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3029201
05                 A    =         6718017
85  meter
 Y    =        4480723
82  meter          E    =           
0018379
 Z    =        3970487
31                 I    =           51
97893
 XDOT =      -3228
561170                 Wp   =           95
30499
 YDOT =      -5746
600579  meter/sec      RA   =           89
03237  deg
 ZDOT =       4004
530972                 TA   =          313
38782
                                          MA   =          313
54073
                                          Ha   =            188
935  n
mi
                                          Hp   =            177
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9938323
65                 X    =        -3098368
17
 Y    =       14700537
48  feet           Y    =         4446462
14  meter
 Z    =       13026533
18                 Z    =         3955604
08
 XDOT =     -10592
392289                 XDOT =       -3183
515120
 YDOT =     -18853
676440  feet/sec       YDOT =       -5782
453034  meter/sec
 ZDOT =      13138
224973                 ZDOT =        3988
955017

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13671717
21                 X    =        -4167139
41
 Y    =      -11379294
39  feet           Y    =        -3468408
93  meter
 Z    =       12967746
66                 Z    =         3952569
18
 XDOT =      18960
610080                 XDOT =        5779
193952
 YDOT =      -7813
220772  feet/sec       YDOT =       -2381
469691  meter/sec
 ZDOT =      13076
452945                 ZDOT =        3985
702858


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   09350
55482391  
00016717  00000-0  10270-3 0  9078
2 25544  51
6461  89
4885 0007494  87
0013 273
2009 15
76579648 34693


Satellite: ISS
Catalog Number: 25544
Epoch time:      09350
55482391   =   yrday
fracday
Element set:     907
Inclination:       51
6461  deg
RA of node:        89
4885  deg
Eccentricity:     
0007494     
Arg of perigee:    87
0013  deg
Mean anomaly:     273
2009  deg
Mean motion:   15
76579648  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3469
Checksum:              345


Coasting Arc #9 (Orbit 3483)
---------------------------------------

Vector Time (GMT): 2009/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2787331
32                 A    =         6721556
18  meter
 Y    =        5440889
93  meter          E    =           
0011780
 Z    =       -2800396
79                 I    =           51
98902
 XDOT =      -3568
788633                 Wp   =           77
57774
 YDOT =       4469
420469  meter/sec      RA   =           83
85378  deg
 ZDOT =       5152
031027                 TA   =          250
51255
                                          MA   =          250
63984
                                          Ha   =            188
900  n
mi
                                          Hp   =            177
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9144787
80                 X    =         2739887
02
 Y    =       17850688
73  feet           Y    =         5471794
68  meter
 Z    =       -9187653
52                 Z    =        -2786970
29
 XDOT =     -11708
624125                 XDOT =       -3643
528907
 YDOT =      14663
452983  feet/sec       YDOT =        4429
093458  meter/sec
 ZDOT =      16902
988933                 ZDOT =        5134
512984

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18520192
52                 X    =        -5644954
68
 Y    =        7762247
94  feet           Y    =         2365933
17  meter
 Z    =       -9134395
74                 Z    =        -2784163
82
 XDOT =     -13121
150073                 XDOT =       -3999
326542
 YDOT =     -11576
402942  feet/sec       YDOT =       -3528
487617  meter/sec
 ZDOT =      16833
764789                 ZDOT =        5130
931508


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   09351
50562024  
00016717  00000-0  10270-3 0  9087
2 25544  51
6463  84
5889 0007415  88
7669 271
4345 15
76545306 34847


Satellite: ISS
Catalog Number: 25544
Epoch time:      09351
50562024   =   yrday
fracday
Element set:     908
Inclination:       51
6463  deg
RA of node:        84
5889  deg
Eccentricity:     
0007415     
Arg of perigee:    88
7669  deg
Mean anomaly:     271
4345  deg
Mean motion:   15
76545306  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3484
Checksum:              338


Coasting Arc #10 (Orbit 3499)
---------------------------------------

Vector Time (GMT): 2009/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3268762
75                 A    =         6714497
06  meter
 Y    =       -3241949
84  meter          E    =           
0019517
 Z    =       -4905210
20                 I    =           51
96068
 XDOT =       3145
762529                 Wp   =           80
72591
 YDOT =       6632
513689  meter/sec      RA   =           78
76426  deg
 ZDOT =      -2291
883737                 TA   =          167
06423
                                          MA   =          167
01409
                                          Ha   =            188
849  n
mi
                                          Hp   =            177
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10724287
23                 X    =         3328600
43
 Y    =      -10636318
36  feet           Y    =        -3205061
30  meter
 Z    =      -16093209
32                 Z    =        -4889185
72
 XDOT =      10320
743204                 XDOT =        3082
496329
 YDOT =      21760
215516  feet/sec       YDOT =        6667
338064  meter/sec
 ZDOT =      -7519
303598                 ZDOT =       -2276
754336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9949049
59                 X    =         3032470
31
 Y    =       11453950
64  feet           Y    =         3491164
15  meter
 Z    =      -16029860
21                 Z    =        -4885901
39
 XDOT =     -21522
762604                 XDOT =       -6560
138042
 YDOT =       8276
931909  feet/sec       YDOT =        2522
808846  meter/sec
 ZDOT =      -7459
280546                 ZDOT =       -2273
588711


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   09352
51978974  
00016717  00000-0  10270-3 0  9095
2 25544  51
6460  79
3616 0007424  93
3059 266
8955 15
76569893 35000


Satellite: ISS
Catalog Number: 25544
Epoch time:      09352
51978974   =   yrday
fracday
Element set:     909
Inclination:       51
6460  deg
RA of node:        79
3616  deg
Eccentricity:     
0007424     
Arg of perigee:    93
3059  deg
Mean anomaly:     266
8955  deg
Mean motion:   15
76569893  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3500
Checksum:              359


Coasting Arc #11 (Orbit 3515)
---------------------------------------

Vector Time (GMT): 2009/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2711791
80                 A    =         6724235
39  meter
 Y    =       -6035844
24  meter          E    =           
0020955
 Z    =        1148486
07                 I    =           51
98610
 XDOT =       3968
195896                 Wp   =          113
28328
 YDOT =      -2925
044694  meter/sec      RA   =           73
60397  deg
 ZDOT =      -5926
352717                 TA   =           54
18068
                                          MA   =           53
98615
                                          Ha   =            188
876  n
mi
                                          Hp   =            177
049

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8896954
74                 X    =        -2649675
50
 Y    =      -19802638
57  feet           Y    =        -6065821
94  meter
 Z    =        3767998
92                 Z    =         1135462
31
 XDOT =      13019
015407                 XDOT =        4029
398351
 YDOT =      -9596
603328  feet/sec       YDOT =       -2880
326985  meter/sec
 ZDOT =     -19443
414425                 ZDOT =       -5906
927039

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20179937
78                 X    =         6150845
04
 Y    =       -8028522
15  feet           Y    =        -2447093
55  meter
 Z    =        3716323
03                 Z    =         1132735
26
 XDOT =       8417
527593                 XDOT =        2565
662410
 YDOT =      12075
318769  feet/sec       YDOT =        3680
557161  meter/sec
 ZDOT =     -19366
590669                 ZDOT =       -5902
936836


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   09353
53394702  
00016717  00000-0  10270-3 0  9101
2 25544  51
6454  74
1343 0007604  96
4141 263
7890 15
76599522 35162


Satellite: ISS
Catalog Number: 25544
Epoch time:      09353
53394702   =   yrday
fracday
Element set:     910
Inclination:       51
6454  deg
RA of node:        74
1343  deg
Eccentricity:     
0007604     
Arg of perigee:    96
4141  deg
Mean anomaly:     263
7890  deg
Mean motion:   15
76599522  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3516
Checksum:              317


Coasting Arc #12 (Orbit 3531)
---------------------------------------

Vector Time (GMT): 2009/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3706798
12                 A    =         6712546
53  meter
 Y    =        1853461
01  meter          E    =           
0009922
 Z    =        5272175
99                 I    =           51
93806
 XDOT =      -3064
339431                 Wp   =          100
75879
 YDOT =      -7070
894541  meter/sec      RA   =           68
48495  deg
 ZDOT =        328
980138                 TA   =          346
12233
                                          MA   =          346
14959
                                          Ha   =            188
828  n
mi
                                          Hp   =            177
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12161411
14                 X    =        -3752859
48
 Y    =        6080908
84  feet           Y    =         1811751
24  meter
 Z    =       17297165
33                 Z    =         5254056
80
 XDOT =     -10053
607057                 XDOT =       -2986
641816
 YDOT =     -23198
472904  feet/sec       YDOT =       -7104
727402  meter/sec
 ZDOT =       1079
331163                 ZDOT =         314
281549

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5744006
89                 X    =        -1750773
30
 Y    =      -12424102
79  feet           Y    =        -3786866
53  meter
 Z    =       17225485
67                 Z    =         5250328
03
 XDOT =      22558
678595                 XDOT =        6875
885236
 YDOT =      -9003
266834  feet/sec       YDOT =       -2744
195731  meter/sec
 ZDOT =       1021
005297                 ZDOT =         311
202414


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   09354
54808962  
00016717  00000-0  10270-3 0  9112
2 25544  51
6458  68
9062 0007421  99
8222 260
3789 15
76659140 35320


Satellite: ISS
Catalog Number: 25544
Epoch time:      09354
54808962   =   yrday
fracday
Element set:     911
Inclination:       51
6458  deg
RA of node:        68
9062  deg
Eccentricity:     
0007421     
Arg of perigee:    99
8222  deg
Mean anomaly:     260
3789  deg
Mean motion:   15
76659140  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3532
Checksum:              336


Coasting Arc #13 (Orbit 3547)
---------------------------------------

Vector Time (GMT): 2009/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2580906
35                 A    =         6724579
11  meter
 Y    =        6174921
01  meter          E    =           
0019051
 Z    =         591084
66                 I    =           51
96545
 XDOT =      -4608
075445                 Wp   =           68
88470
 YDOT =       1334
626098  meter/sec      RA   =           63
35511  deg
 ZDOT =       6030
291043                 TA   =          297
52844
                                          MA   =          297
72191
                                          Ha   =            188
811  n
mi
                                          Hp   =            177
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8467540
53                 X    =         2508794
12
 Y    =       20258927
18  feet           Y    =         6203378
96  meter
 Z    =        1939254
12                 Z    =          603448
10
 XDOT =     -15118
357758                 XDOT =       -4651
950903
 YDOT =       4378
694548  feet/sec       YDOT =        1282
849949  meter/sec
 ZDOT =      19784
419434                 ZDOT =        6007
798682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20343555
65                 X    =        -6200715
76
 Y    =        8250479
93  feet           Y    =         2514746
28  meter
 Z    =        1988316
94                 Z    =          606039
00
 XDOT =      -3623
079255                 XDOT =       -1104
314557
 YDOT =     -13794
067894  feet/sec       YDOT =       -4204
431894  meter/sec
 ZDOT =      19695
416245                 ZDOT =        6003
162871


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   09355
56222372  
00016717  00000-0  10270-3 0  9121
2 25544  51
6452  63
6787 0007557 101
7145 258
4868 15
76618955 35489


Satellite: ISS
Catalog Number: 25544
Epoch time:      09355
56222372   =   yrday
fracday
Element set:     912
Inclination:       51
6452  deg
RA of node:        63
6787  deg
Eccentricity:     
0007557     
Arg of perigee:   101
7145  deg
Mean anomaly:     258
4868  deg
Mean motion:   15
76618955  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3548
Checksum:              344


Coasting Arc #14 (Orbit 3562)
---------------------------------------

Vector Time (GMT): 2009/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4381954
60                 A    =         6713531
83  meter
 Y    =        -489909
37  meter          E    =           
0021037
 Z    =       -5081295
38                 I    =           51
91309
 XDOT =       2753
536762                 Wp   =          103
46662
 YDOT =       6974
298031  meter/sec      RA   =           58
20054  deg
 ZDOT =       1703
220220                 TA   =          182
87300
                                          MA   =          182
88510
                                          Ha   =            188
716  n
mi
                                          Hp   =            177
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14376491
47                 X    =         4411791
11
 Y    =       -1607314
22  feet           Y    =         -440740
51  meter
 Z    =      -16670916
60                 Z    =        -5059935
48
 XDOT =       9033
913262                 XDOT =        2667
070378
 YDOT =      22881
555220  feet/sec       YDOT =        7004
606100  meter/sec
 ZDOT =       5587
992847                 ZDOT =        1716
387437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1710113
97                 X    =          521242
74
 Y    =       14462157
91  feet           Y    =         4408065
73  meter
 Z    =      -16586377
69                 Z    =        -5055527
92
 XDOT =     -21762
824757                 XDOT =       -6633
308986
 YDOT =       9038
028417  feet/sec       YDOT =        2754
791061  meter/sec
 ZDOT =       5640
250104                 ZDOT =        1719
148232


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   09356
51296028  
00016717  00000-0  10270-3 0  9137
2 25544  51
6445  58
7773 0007512 105
0410 255
1587 15
76653148 35636


Satellite: ISS
Catalog Number: 25544
Epoch time:      09356
51296028   =   yrday
fracday
Element set:     913
Inclination:       51
6445  deg
RA of node:        58
7773  deg
Eccentricity:     
0007512     
Arg of perigee:   105
0410  deg
Mean anomaly:     255
1587  deg
Mean motion:   15
76653148  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3563
Checksum:              317


Coasting Arc #15 (Orbit 3578)
---------------------------------------

Vector Time (GMT): 2009/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2144394
79                 A    =         6722107
92  meter
 Y    =       -5921348
31  meter          E    =           
0012982
 Z    =       -2349513
92                 I    =           51
92580
 XDOT =       5452
712504                 Wp   =          119
08351
 YDOT =        170
670321  meter/sec      RA   =           53
09915  deg
 ZDOT =      -5435
373206                 TA   =           87
27749
                                          MA   =           87
12891
                                          Ha   =            188
690  n
mi
                                          Hp   =            176
967

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7035415
98                 X    =        -2066608
35
 Y    =      -19426995
77  feet           Y    =        -5944893
09  meter
 Z    =       -7708378
99                 Z    =        -2359742
90
 XDOT =      17889
476719                 XDOT =        5476
802833
 YDOT =        559
941997  feet/sec       YDOT =         231
780886  meter/sec
 ZDOT =     -17832
589258                 ZDOT =       -5408
825404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19251763
01                 X    =         5867937
36
 Y    =       -7459709
54  feet           Y    =        -2273719
47  meter
 Z    =       -7748980
83                 Z    =        -2361889
36
 XDOT =       -666
483705                 XDOT =        -203
144233
 YDOT =      16598
050345  feet/sec       YDOT =        5059
085745  meter/sec
 ZDOT =     -17727
502370                 ZDOT =       -5403
342723


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   09357
52706912  
00016717  00000-0  10270-3 0  9148
2 25544  51
6447  53
5487 0007646 108
4635 251
7361 15
76684640 35797


Satellite: ISS
Catalog Number: 25544
Epoch time:      09357
52706912   =   yrday
fracday
Element set:     914
Inclination:       51
6447  deg
RA of node:        53
5487  deg
Eccentricity:     
0007646     
Arg of perigee:   108
4635  deg
Mean anomaly:     251
7361  deg
Mean motion:   15
76684640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3579
Checksum:              339

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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