Date: June 7th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14262 18 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 411)
---------------------------------------

Vector Time (GMT): 2009/156/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6398908
92                 A    =         6732330
97  meter
 Y    =        -833465
92  meter          E    =           
0015039
 Z    =       -1914776
79                 I    =           51
68916
 XDOT =       2287
850413                 Wp   =           61
57657
 YDOT =       4720
645955  meter/sec      RA   =            6
13714  deg
 ZDOT =       5631
221707                 TA   =          277
16726
                                          MA   =          277
33822
                                          Ha   =            194
286  n
mi
                                          Hp   =            181
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20993795
66                 X    =         6417055
07
 Y    =       -2734468
24  feet           Y    =         -761807
80  meter
 Z    =       -6282076
09                 Z    =        -1883646
49
 XDOT =       7506
070908                 XDOT =        2207
537452
 YDOT =      15487
683579  feet/sec       YDOT =        4745
780041  meter/sec
 ZDOT =      18475
136833                 ZDOT =        5642
141956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2481326
87                 X    =         -756308
43
 Y    =      -21061261
26  feet           Y    =        -6419472
43  meter
 Z    =       -6160157
76                 Z    =        -1877616
09
 XDOT =      14040
089140                 XDOT =        4279
419170
 YDOT =      -7030
946796  feet/sec       YDOT =       -2143
032583  meter/sec
 ZDOT =      18518
102418                 ZDOT =        5644
317617


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   09156
54808070  
00010596  00000-0  82463-4 0  9003
2 25544  51
6382   6
6355 0008933  80
4486 279
7685 15
73404695  4120


Satellite: ISS
Catalog Number: 25544
Epoch time:      09156
54808070   =   yrday
fracday
Element set:     900
Inclination:       51
6382  deg
RA of node:         6
6355  deg
Eccentricity:     
0008933     
Arg of perigee:    80
4486  deg
Mean anomaly:     279
7685  deg
Mean motion:   15
73404695  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             412
Checksum:              323


Coasting Arc #2 (Orbit 427)
---------------------------------------

Vector Time (GMT): 2009/157/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2547527
41                 A    =         6723457
09  meter
 Y    =       -3900602
53  meter          E    =           
0021200
 Z    =       -4867134
36                 I    =           51
62934
 XDOT =       7111
246898                 Wp   =           77
50494
 YDOT =      -1725
935096  meter/sec      RA   =            1
04296  deg
 ZDOT =      -2343
002693                 TA   =          169
62838
                                          MA   =          169
58457
                                          Ha   =            194
232  n
mi
                                          Hp   =            181
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8358029
56                 X    =        -2480076
92
 Y    =      -12797252
41  feet           Y    =        -3928712
44  meter
 Z    =      -15968288
58                 Z    =        -4879347
28
 XDOT =      23330
862527                 XDOT =        7141
400093
 YDOT =      -5662
516718  feet/sec       YDOT =       -1646
243954  meter/sec
 ZDOT =      -7687
016710                 ZDOT =       -2308
382891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12754629
81                 X    =        -3887611
17
 Y    =        8331305
99  feet           Y    =         2539382
07  meter
 Z    =      -16016283
17                 Z    =        -4881763
11
 XDOT =      -5175
870194                 XDOT =       -1577
605235
 YDOT =     -22415
393300  feet/sec       YDOT =       -6832
211878  meter/sec
 ZDOT =      -7551
459297                 ZDOT =       -2301
684794


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   09157
56428601  
00010596  00000-0  82463-4 0  9015
2 25544  51
6375   1
4207 0009027  84
4022 275
8170 15
73440295  4285


Satellite: ISS
Catalog Number: 25544
Epoch time:      09157
56428601   =   yrday
fracday
Element set:     901
Inclination:       51
6375  deg
RA of node:         1
4207  deg
Eccentricity:     
0009027     
Arg of perigee:    84
4022  deg
Mean anomaly:     275
8170  deg
Mean motion:   15
73440295  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             428
Checksum:              290


Coasting Arc #3 (Orbit 443)
---------------------------------------

Vector Time (GMT): 2009/158/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5978826
84                 A    =         6731573
01  meter
 Y    =        2164565
75  meter          E    =           
0022404
 Z    =        2183115
83                 I    =           51
62778
 XDOT =      -3509
000258                 Wp   =          100
41811
 YDOT =      -4107
836583  meter/sec      RA   =          355
87227  deg
 ZDOT =      -5493
500102                 TA   =           55
11322
                                          MA   =           54
90282
                                          Ha   =            194
075  n
mi
                                          Hp   =            181
378

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19615573
61                 X    =        -6013192
29
 Y    =        7101593
68  feet           Y    =         2097514
45  meter
 Z    =        7162453
51                 Z    =         2153987
37
 XDOT =     -11512
468038                 XDOT =       -3436
118269
 YDOT =     -13477
154143  feet/sec       YDOT =       -4146
667694  meter/sec
 ZDOT =     -18023
294299                 ZDOT =       -5510
370755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7539650
15                 X    =         2298085
37
 Y    =       19493012
67  feet           Y    =         5941470
26  meter
 Z    =        7048420
67                 Z    =         2148358
62
 XDOT =     -11797
455369                 XDOT =       -3595
864396
 YDOT =      11156
550421  feet/sec       YDOT =        3400
516568  meter/sec
 ZDOT =     -18089
542985                 ZDOT =       -5513
692702


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   09158
58046848  
00010596  00000-0  82463-4 0  9028
2 25544  51
6379 356
2053 0008765  86
9896 273
2270 15
73509282  4446


Satellite: ISS
Catalog Number: 25544
Epoch time:      09158
58046848   =   yrday
fracday
Element set:     902
Inclination:       51
6379  deg
RA of node:       356
2053  deg
Eccentricity:     
0008765     
Arg of perigee:    86
9896  deg
Mean anomaly:     273
2270  deg
Mean motion:   15
73509282  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             444
Checksum:              344


Coasting Arc #4 (Orbit 459)
---------------------------------------

Vector Time (GMT): 2009/159/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3545321
82                 A    =         6723848
22  meter
 Y    =        3212439
18  meter          E    =           
0015985
 Z    =        4712783
48                 I    =           51
57146
 XDOT =      -6479
342602                 Wp   =          103
62239
 YDOT =       3204
920525  meter/sec      RA   =          350
77727  deg
 ZDOT =       2678
375446                 TA   =          319
99068
                                          MA   =          320
10833
                                          Ha   =            194
028  n
mi
                                          Hp   =            181
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11631633
25                 X    =         3486242
32
 Y    =       10539498
62  feet           Y    =         3251753
77  meter
 Z    =       15461888
06                 Z    =         4729863
88
 XDOT =     -21257
685701                 XDOT =       -6527
710131
 YDOT =      10514
831119  feet/sec       YDOT =        3132
193761  meter/sec
 ZDOT =       8787
321016                 ZDOT =        2646
781789

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10074887
75                 X    =         3070825
78
 Y    =      -11949685
89  feet           Y    =        -3642264
26  meter
 Z    =       15528926
23                 Z    =         4733216
71
 XDOT =      10478
388556                 XDOT =        3193
812832
 YDOT =      20140
946021  feet/sec       YDOT =        6138
960347  meter/sec
 ZDOT =       8663
664576                 ZDOT =        2640
684963


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   09159
59663394  
00010596  00000-0  82463-4 0  9032
2 25544  51
6371 350
9899 0008891  91
7685 268
4496 15
73493782  4608


Satellite: ISS
Catalog Number: 25544
Epoch time:      09159
59663394   =   yrday
fracday
Element set:     903
Inclination:       51
6371  deg
RA of node:       350
9899  deg
Eccentricity:     
0008891     
Arg of perigee:    91
7685  deg
Mean anomaly:     268
4496  deg
Mean motion:   15
73493782  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             460
Checksum:              370


Coasting Arc #5 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2009/160/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5272640
90                 A    =         6730909
99  meter
 Y    =       -3379781
31  meter          E    =           
0013262
 Z    =       -2472643
53                 I    =           51
56682
 XDOT =       4535
831536                 Wp   =           77
79576
 YDOT =       3198
973960  meter/sec      RA   =          345
59787  deg
 ZDOT =       5326
330141                 TA   =          254
24797
                                          MA   =          254
39427
                                          Ha   =            194
106  n
mi
                                          Hp   =            181
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17298690
61                 X    =         5322053
97
 Y    =      -11088521
35  feet           Y    =        -3320542
79  meter
 Z    =       -8112347
55                 Z    =        -2446909
65
 XDOT =      14881
337060                 XDOT =        4473
848581
 YDOT =      10495
321392  feet/sec       YDOT =        3249
348660  meter/sec
 ZDOT =      17474
836421                 ZDOT =        5348
215314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12055065
17                 X    =        -3674383
86
 Y    =      -16688290
01  feet           Y    =        -5086590
79  meter
 Z    =       -8011651
86                 Z    =        -2441951
49
 XDOT =       8423
107988                 XDOT =        2567
363315
 YDOT =     -14472
390356  feet/sec       YDOT =       -4411
184581  meter/sec
 ZDOT =      17560
701606                 ZDOT =        5352
501849


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   09160
54926824  
00010596  00000-0  82463-4 0  9040
2 25544  51
6376 346
1003 0008995  96
1254 264
0934 15
73532020  4757


Satellite: ISS
Catalog Number: 25544
Epoch time:      09160
54926824   =   yrday
fracday
Element set:     904
Inclination:       51
6376  deg
RA of node:       346
1003  deg
Eccentricity:     
0008995     
Arg of perigee:    96
1254  deg
Mean anomaly:     264
0934  deg
Mean motion:   15
73532020  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             475
Checksum:              307


Coasting Arc #6 (Orbit 490)
---------------------------------------

Vector Time (GMT): 2009/161/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4308514
39                 A    =         6724075
11  meter
 Y    =       -2360806
68  meter          E    =           
0019115
 Z    =       -4608319
85                 I    =           51
51644
 XDOT =       5552
610698                 Wp   =           83
12574
 YDOT =      -4434
889779  meter/sec      RA   =          340
50247  deg
 ZDOT =      -2927
541217                 TA   =          157
79813
                                          MA   =          157
71525
                                          Ha   =            194
012  n
mi
                                          Hp   =            181
036

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14135545
89                 X    =        -4259408
89
 Y    =       -7745428
74  feet           Y    =        -2408711
57  meter
 Z    =      -15119159
62                 Z    =        -4629131
74
 XDOT =      18217
226699                 XDOT =        5616
011136
 YDOT =     -14550
163318  feet/sec       YDOT =       -4372
442202  meter/sec
 ZDOT =      -9604
794020                 ZDOT =       -2900
413523

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6686243
72                 X    =        -2037967
09
 Y    =       14581645
35  feet           Y    =         4444485
50  meter
 Z    =      -15200791
94                 Z    =        -4633201
38
 XDOT =     -14797
759832                 XDOT =       -4510
357197
 YDOT =     -16659
684070  feet/sec       YDOT =       -5077
871704  meter/sec
 ZDOT =      -9498
676097                 ZDOT =       -2895
196474


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   09161
56539122  
00010596  00000-0  82463-4 0  9055
2 25544  51
6381 340
8854 0009065  99
2720 260
9468 15
73579278  4910


Satellite: ISS
Catalog Number: 25544
Epoch time:      09161
56539122   =   yrday
fracday
Element set:     905
Inclination:       51
6381  deg
RA of node:       340
8854  deg
Eccentricity:     
0009065     
Arg of perigee:    99
2720  deg
Mean anomaly:     260
9468  deg
Mean motion:   15
73579278  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             491
Checksum:              335


Coasting Arc #7 (Orbit 506)
---------------------------------------

Vector Time (GMT): 2009/162/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4392789
58                 A    =         6730357
56  meter
 Y    =        4339495
69  meter          E    =           
0022612
 Z    =        2651550
53                 I    =           51
50917
 XDOT =      -5268
986560                 Wp   =          102
46569
 YDOT =      -2133
461101  meter/sec      RA   =          335
31560  deg
 ZDOT =      -5205
073492                 TA   =           47
26164
                                          MA   =           47
07154
                                          Ha   =            193
969  n
mi
                                          Hp   =            181
255

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14412039
31                 X    =        -4453868
77
 Y    =       14237190
59  feet           Y    =         4290030
98  meter
 Z    =        8699312
78                 Z    =         2630062
84
 XDOT =     -17286
701311                 XDOT =       -5219
453035
 YDOT =      -6999
544294  feet/sec       YDOT =       -2192
104120  meter/sec
 ZDOT =     -17077
012770                 ZDOT =       -5230
550185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15495041
44                 X    =         4722888
63
 Y    =       13105837
55  feet           Y    =         3994659
28  meter
 Z    =        8615290
40                 Z    =         2625940
51
 XDOT =      -4450
099565                 XDOT =       -1356
390347
 YDOT =      16623
363749  feet/sec       YDOT =        5066
801271  meter/sec
 ZDOT =     -17176
917237                 ZDOT =       -5235
524374


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   09162
58149284  
00010596  00000-0  82463-4 0  9065
2 25544  51
6375 335
6692 0008887 103
5794 256
6359 15
73586971  5073


Satellite: ISS
Catalog Number: 25544
Epoch time:      09162
58149284   =   yrday
fracday
Element set:     906
Inclination:       51
6375  deg
RA of node:       335
6692  deg
Eccentricity:     
0008887     
Arg of perigee:   103
5794  deg
Mean anomaly:     256
6359  deg
Mean motion:   15
73586971  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             507
Checksum:              358


Coasting Arc #8 (Orbit 522)
---------------------------------------

Vector Time (GMT): 2009/163/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4834056
33                 A    =         6724344
87  meter
 Y    =        1334271
26  meter          E    =           
0017653
 Z    =        4468681
92                 I    =           51
46411
 XDOT =      -4442
779981                 Wp   =          109
85093
 YDOT =       5445
986727  meter/sec      RA   =          330
21804  deg
 ZDOT =       3163
952096                 TA   =          308
41618
                                          MA   =          308
57455
                                          Ha   =            193
684  n
mi
                                          Hp   =            181
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15859764
87                 X    =         4797069
06
 Y    =        4377530
37  feet           Y    =         1388120
99  meter
 Z    =       14661029
91                 Z    =         4492076
03
 XDOT =     -14576
049807                 XDOT =       -4518
717563
 YDOT =      17867
410521  feet/sec       YDOT =        5395
879878  meter/sec
 ZDOT =      10380
420264                 ZDOT =        3142
185575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2645773
60                 X    =          806431
79
 Y    =      -16155404
14  feet           Y    =        -4924167
18  meter
 Z    =       14752745
89                 Z    =         4496636
95
 XDOT =      18167
859066                 XDOT =        5537
563443
 YDOT =      12424
492739  feet/sec       YDOT =        3786
985387  meter/sec
 ZDOT =      10295
352613                 ZDOT =        3138
023477


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   09163
59757269  
00010596  00000-0  82463-4 0  9076
2 25544  51
6383 330
4540 0008829 107
6159 252
5968 15
73655924  5237


Satellite: ISS
Catalog Number: 25544
Epoch time:      09163
59757269   =   yrday
fracday
Element set:     907
Inclination:       51
6383  deg
RA of node:       330
4540  deg
Eccentricity:     
0008829     
Arg of perigee:   107
6159  deg
Mean anomaly:     252
5968  deg
Mean motion:   15
73655924  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             523
Checksum:              343


Coasting Arc #9 (Orbit 537)
---------------------------------------

Vector Time (GMT): 2009/164/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3339370
45                 A    =         6729647
97  meter
 Y    =       -5106947
27  meter          E    =           
0012517
 Z    =       -2850190
68                 I    =           51
45785
 XDOT =       5715
747734                 Wp   =           93
96932
 YDOT =        922
695352  meter/sec      RA   =          325
02617  deg
 ZDOT =       5061
710375                 TA   =          233
27302
                                          MA   =          233
38805
                                          Ha   =            193
805  n
mi
                                          Hp   =            181
207

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10955939
80                 X    =         3410074
67
 Y    =      -16755076
36  feet           Y    =        -5069208
75  meter
 Z    =       -9351019
29                 Z    =        -2833797
05
 XDOT =      18752
453196                 XDOT =        5680
416409
 YDOT =       3027
215721  feet/sec       YDOT =         986
413922  meter/sec
 ZDOT =      16606
661336                 ZDOT =        5089
391692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18002335
99                 X    =        -5487112
01
 Y    =       -8824646
25  feet           Y    =        -2689752
18  meter
 Z    =       -9286995
20                 Z    =        -2830676
14
 XDOT =         23
433563                 XDOT =           7
142550
 YDOT =     -17575
296867  feet/sec       YDOT =       -5356
950485  meter/sec
 ZDOT =      16715
160092                 ZDOT =        5094
780796


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   09164
55012988  
00010596  00000-0  82463-4 0  9086
2 25544  51
6395 325
5651 0008932 110
5710 249
6412 15
73663613  5380


Satellite: ISS
Catalog Number: 25544
Epoch time:      09164
55012988   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:       325
5651  deg
Eccentricity:     
0008932     
Arg of perigee:   110
5710  deg
Mean anomaly:     249
6412  deg
Mean motion:   15
73663613  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             538
Checksum:              316


Coasting Arc #10 (Orbit 553)
---------------------------------------

Vector Time (GMT): 2009/165/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5093754
37                 A    =         6724557
29  meter
 Y    =        -296263
22  meter          E    =           
0016853
 Z    =       -4394556
48                 I    =           51
41760
 XDOT =       3206
752262                 Wp   =           90
46748
 YDOT =      -6152
125531  meter/sec      RA   =          319
92638  deg
 ZDOT =      -3313
293077                 TA   =          146
13058
                                          MA   =          146
02284
                                          Ha   =            193
645  n
mi
                                          Hp   =            181
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16711792
54                 X    =        -5068714
99
 Y    =        -971992
18  feet           Y    =         -353083
99  meter
 Z    =      -14417836
22                 Z    =        -4419241
13
 XDOT =      10520
840753                 XDOT =        3291
403397
 YDOT =     -20184
138881  feet/sec       YDOT =       -6115
792022  meter/sec
 ZDOT =     -10870
384110                 ZDOT =       -3297
509856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1403829
82                 X    =          427887
33
 Y    =       16596968
82  feet           Y    =         5058756
10  meter
 Z    =      -14514567
43                 Z    =        -4424040
15
 XDOT =     -20274
729340                 XDOT =       -6179
737503
 YDOT =      -7706
146005  feet/sec       YDOT =       -2348
833302  meter/sec
 ZDOT =     -10808
800895                 ZDOT =       -3294
522513


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   09165
56616879  
00010596  00000-0  82463-4 0  9098
2 25544  51
6396 320
3498 0008802 113
9419 246
2667 15
73694783  5547


Satellite: ISS
Catalog Number: 25544
Epoch time:      09165
56616879   =   yrday
fracday
Element set:     909
Inclination:       51
6396  deg
RA of node:       320
3498  deg
Eccentricity:     
0008802     
Arg of perigee:   113
9419  deg
Mean anomaly:     246
2667  deg
Mean motion:   15
73694783  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             554
Checksum:              355


Coasting Arc #11 (Orbit 569)
---------------------------------------

Vector Time (GMT): 2009/166/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2239146
29                 A    =         6729246
56  meter
 Y    =        5605144
81  meter          E    =           
0021825
 Z    =        2949759
57                 I    =           51
41119
 XDOT =      -5877
452335                 Wp   =          105
27604
 YDOT =        286
162236  meter/sec      RA   =          314
72859  deg
 ZDOT =      -4980
438503                 TA   =           40
54788
                                          MA   =           40
38550
                                          Ha   =            193
631  n
mi
                                          Hp   =            181
268

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7346280
50                 X    =        -2315986
99
 Y    =       18389582
72  feet           Y    =         5579675
38  meter
 Z    =        9677688
87                 Z    =         2938695
80
 XDOT =     -19282
980102                 XDOT =       -5856
021296
 YDOT =        938
852479  feet/sec       YDOT =         220
557555  meter/sec
 ZDOT =     -16340
021336                 ZDOT =       -5008
939150

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19334133
89                 X    =         5893044
01
 Y    =        4378172
91  feet           Y    =         1334467
10  meter
 Z    =        9634579
41                 Z    =         2936619
80
 XDOT =       4302
607021                 XDOT =        1311
434620
 YDOT =      17383
384331  feet/sec       YDOT =        5298
455544  meter/sec
 ZDOT =     -16451
678137                 ZDOT =       -5014
471496


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   09166
58218684  
00010596  00000-0  82463-4 0  9105
2 25544  51
6394 315
1337 0008811 117
9272 242
2784 15
73711698  5709


Satellite: ISS
Catalog Number: 25544
Epoch time:      09166
58218684   =   yrday
fracday
Element set:     910
Inclination:       51
6394  deg
RA of node:       315
1337  deg
Eccentricity:     
0008811     
Arg of perigee:   117
9272  deg
Mean anomaly:     242
2784  deg
Mean motion:   15
73711698  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             570
Checksum:              324


Coasting Arc #12 (Orbit 585)
---------------------------------------

Vector Time (GMT): 2009/167/13:03:56
106
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5107675
88                 A    =         6724633
27  meter
 Y    =        -791643
73  meter          E    =           
0018194
 Z    =        4292146
17                 I    =           51
37753
 XDOT =      -1895
520435                 Wp   =          114
59085
 YDOT =       6620
722096  meter/sec      RA   =          309
62649  deg
 ZDOT =       3457
867662                 TA   =          300
26568
                                          MA   =          300
44563
                                          Ha   =            193
307  n
mi
                                          Hp   =            181
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16757466
81                 X    =         5095297
96
 Y    =       -2597256
34  feet           Y    =         -734596
44  meter
 Z    =       14081844
39                 Z    =         4316929
26
 XDOT =      -6218
899064                 XDOT =       -1986
211396
 YDOT =      21721
529185  feet/sec       YDOT =        6599
017781  meter/sec
 ZDOT =      11344
710176                 ZDOT =        3448
439672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5495656
94                 X    =        -1675076
23
 Y    =      -15956596
82  feet           Y    =        -4863570
71  meter
 Z    =       14178912
11                 Z    =         4321732
41
 XDOT =      21325
806838                 XDOT =        6500
105924
 YDOT =       2758
205055  feet/sec       YDOT =         840
700901  meter/sec
 ZDOT =      11308
057503                 ZDOT =        3446
695927


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   09167
59818107  
00010596  00000-0  82463-4 0  9114
2 25544  51
6403 309
9183 0008654 121
6787 238
5221 15
73792634  5868


Satellite: ISS
Catalog Number: 25544
Epoch time:      09167
59818107   =   yrday
fracday
Element set:     911
Inclination:       51
6403  deg
RA of node:       309
9183  deg
Eccentricity:     
0008654     
Arg of perigee:   121
6787  deg
Mean anomaly:     238
5221  deg
Mean motion:   15
73792634  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             586
Checksum:              332

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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