Date: April 21st 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 3639)
---------------------------------------

Vector Time (GMT): 2009/107/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4071545
43                 A    =         6725180
58  meter
 Y    =        1069829
98  meter          E    =           
0007370
 Z    =       -5250412
24                 I    =           51
29521
 XDOT =      -1794
825500                 Wp   =          112
98075
 YDOT =      -7480
012739  meter/sec      RA   =          257
31447  deg
 ZDOT =       -135
287252                 TA   =          155
74543
                                          MA   =          155
71072
                                          Ha   =            191
802  n
mi
                                          Hp   =            189
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13358088
68                 X    =        -4057700
26
 Y    =        3509940
88  feet           Y    =         1024377
05  meter
 Z    =      -17225761
95                 Z    =        -5270158
19
 XDOT =      -5888
535104                 XDOT =       -1710
392145
 YDOT =     -24540
724209  feet/sec       YDOT =       -7499
611432  meter/sec
 ZDOT =       -443
855815                 ZDOT =        -143
801506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11593320
95                 X    =        -3533644
22
 Y    =        7327543
14  feet           Y    =         2233435
15  meter
 Z    =      -17302806
54                 Z    =        -5273895
43
 XDOT =     -12446
380345                 XDOT =       -3793
656729
 YDOT =     -20796
966079  feet/sec       YDOT =       -6338
915261  meter/sec
 ZDOT =       -477
646309                 ZDOT =        -145
586595


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   09107
49530836  
00010596  00000-0  82463-4 0  9005
2 25544  51
6392 258
0475 0008825 249
0667 110
9551 15
72220749 36400


Satellite: ISS
Catalog Number: 25544
Epoch time:      09107
49530836   =   yrday
fracday
Element set:     900
Inclination:       51
6392  deg
RA of node:       258
0475  deg
Eccentricity:     
0008825     
Arg of perigee:   249
0667  deg
Mean anomaly:     110
9551  deg
Mean motion:   15
72220749  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3640
Checksum:              315


Coasting Arc #2 (Orbit 3655)
---------------------------------------

Vector Time (GMT): 2009/108/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2564617
47                 A    =         6736963
99  meter
 Y    =        6184212
02  meter          E    =           
0010788
 Z    =         683521
79                 I    =           51
34210
 XDOT =      -4232
950221                 Wp   =          169
56130
 YDOT =       2414
841220  meter/sec      RA   =          252
16065  deg
 ZDOT =      -5961
921476                 TA   =            2
96525
                                          MA   =            2
95886
                                          Ha   =            191
555  n
mi
                                          Hp   =            189
835

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8414099
30                 X    =         2491953
53
 Y    =       20289409
50  feet           Y    =         6212484
78  meter
 Z    =        2242525
57                 Z    =          695804
18
 XDOT =     -13887
631958                 XDOT =       -4230
676823
 YDOT =       7922
707414  feet/sec       YDOT =        2367
518585  meter/sec
 ZDOT =     -19560
109829                 ZDOT =       -5982
479649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14391209
42                 X    =         4386440
63
 Y    =       16587066
06  feet           Y    =         5055737
73  meter
 Z    =        2290951
04                 Z    =          698281
88
 XDOT =      -9348
746287                 XDOT =       -2849
497868
 YDOT =      10825
643840  feet/sec       YDOT =        3299
656243  meter/sec
 ZDOT =     -19640
231861                 ZDOT =       -5986
342671


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   09108
51229229  
00010596  00000-0  82463-4 0  9011
2 25544  51
6384 252
8375 0008950 254
3541 105
6633 15
72245658 36566


Satellite: ISS
Catalog Number: 25544
Epoch time:      09108
51229229   =   yrday
fracday
Element set:     901
Inclination:       51
6384  deg
RA of node:       252
8375  deg
Eccentricity:     
0008950     
Arg of perigee:   254
3541  deg
Mean anomaly:     105
6633  deg
Mean motion:   15
72245658  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3656
Checksum:              317


Coasting Arc #3 (Orbit 3671)
---------------------------------------

Vector Time (GMT): 2009/109/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3147181
31                 A    =         6725752
83  meter
 Y    =       -3051761
47  meter          E    =           
0006768
 Z    =        5106049
81                 I    =           51
31547
 XDOT =       3957
437759                 Wp   =          228
24919
 YDOT =       6445
546460  meter/sec      RA   =          247
03480  deg
 ZDOT =       1409
886592                 TA   =          208
15526
                                          MA   =          208
19187
                                          Ha   =            191
338  n
mi
                                          Hp   =            189
923

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10325398
00                 X    =         3156268
41
 Y    =      -10012340
79  feet           Y    =        -3016516
95  meter
 Z    =       16752131
93                 Z    =         5121360
97
 XDOT =      12983
719682                 XDOT =        3878
219466
 YDOT =      21146
805972  feet/sec       YDOT =        6489
357933  meter/sec
 ZDOT =       4625
612177                 ZDOT =        1428
919304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6313223
46                 X    =         1924270
51
 Y    =      -12845398
96  feet           Y    =        -3915277
60  meter
 Z    =       16811712
33                 Z    =         5124209
92
 XDOT =      18319
113562                 XDOT =        5583
665814
 YDOT =      15169
097380  feet/sec       YDOT =        4623
540882  meter/sec
 ZDOT =       4700
434987                 ZDOT =        1432
692584


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   09109
52926423  
00010596  00000-0  82463-4 0  9024
2 25544  51
6392 247
6281 0008944 258
0865 101
9294 15
72257429 36725


Satellite: ISS
Catalog Number: 25544
Epoch time:      09109
52926423   =   yrday
fracday
Element set:     902
Inclination:       51
6392  deg
RA of node:       247
6281  deg
Eccentricity:     
0008944     
Arg of perigee:   258
0865  deg
Mean anomaly:     101
9294  deg
Mean motion:   15
72257429  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3672
Checksum:              329


Coasting Arc #4 (Orbit 3686)
---------------------------------------

Vector Time (GMT): 2009/110/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4232981
36                 A    =         6735725
35  meter
 Y    =       -4929161
06  meter          E    =           
0006167
 Z    =       -1761718
89                 I    =           51
36307
 XDOT =       2775
783605                 Wp   =          317
63889
 YDOT =      -4410
731874  meter/sec      RA   =          241
86286  deg
 ZDOT =       5664
353409                 TA   =           22
78680
                                          MA   =           22
75944
                                          Ha   =            191
160  n
mi
                                          Hp   =            190
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13887734
12                 X    =        -4168989
90
 Y    =      -16171788
27  feet           Y    =        -4976139
00  meter
 Z    =       -5779917
62                 Z    =        -1782127
19
 XDOT =       9106
901592                 XDOT =        2797
382332
 YDOT =     -14470
905099  feet/sec       YDOT =       -4379
570490  meter/sec
 ZDOT =      18583
836644                 ZDOT =        5677
890828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18626594
15                 X    =        -5677385
90
 Y    =      -10320543
31  feet           Y    =        -3145701
60  meter
 Z    =       -5860010
12                 Z    =        -1786131
08
 XDOT =       2631
036500                 XDOT =         801
939925
 YDOT =     -15343
164381  feet/sec       YDOT =       -4676
596503  meter/sec
 ZDOT =      18636
384695                 ZDOT =        5680
370055


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   09110
48266277  
00010596  00000-0  82463-4 0  9036
2 25544  51
6403 242
7447 0008854 261
5376  98
4783 15
72267239 36873


Satellite: ISS
Catalog Number: 25544
Epoch time:      09110
48266277   =   yrday
fracday
Element set:     903
Inclination:       51
6403  deg
RA of node:       242
7447  deg
Eccentricity:     
0008854     
Arg of perigee:   261
5376  deg
Mean anomaly:      98
4783  deg
Mean motion:   15
72267239  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3687
Checksum:              339


Coasting Arc #5 (Orbit 3702)
---------------------------------------

Vector Time (GMT): 2009/111/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1581357
91                 A    =         6727251
76  meter
 Y    =        4505208
90  meter          E    =           
0003621
 Z    =       -4741981
89                 I    =           51
34993
 XDOT =      -5538
761804                 Wp   =           33
39748
 YDOT =      -4672
233689  meter/sec      RA   =          236
75750  deg
 ZDOT =      -2589
833882                 TA   =          211
06442
                                          MA   =          211
08584
                                          Ha   =            190
779  n
mi
                                          Hp   =            190
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5188182
13                 X    =        -1608582
51
 Y    =       14780869
09  feet           Y    =         4487372
81  meter
 Z    =      -15557683
35                 Z    =        -4749730
50
 XDOT =     -18171
790697                 XDOT =       -5473
523403
 YDOT =     -15328
850686  feet/sec       YDOT =       -4733
806698  meter/sec
 ZDOT =      -8496
830321                 ZDOT =       -2616
582735

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         649261
12                 X    =          197894
79
 Y    =       15621707
72  feet           Y    =         4761496
51  meter
 Z    =      -15587608
67                 Z    =        -4751103
12
 XDOT =     -21328
238704                 XDOT =       -6500
847157
 YDOT =      -7703
139575  feet/sec       YDOT =       -2347
916942  meter/sec
 ZDOT =      -8601
679328                 ZDOT =       -2621
791859


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   09111
49960782  
00010596  00000-0  82463-4 0  9041
2 25544  51
6405 237
5360 0008896 266
1939  93
8206 15
72290102 37036


Satellite: ISS
Catalog Number: 25544
Epoch time:      09111
49960782   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       237
5360  deg
Eccentricity:     
0008896     
Arg of perigee:   266
1939  deg
Mean anomaly:      93
8206  deg
Mean motion:   15
72290102  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3703
Checksum:              317


Coasting Arc #6 (Orbit 3718)
---------------------------------------

Vector Time (GMT): 2009/112/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5284995
48                 A    =         6733701
73  meter
 Y    =        3140384
88  meter          E    =           
0005122
 Z    =        2740269
32                 I    =           51
38946
 XDOT =       -717
590955                 Wp   =          119
21122
 YDOT =       5690
793175  meter/sec      RA   =          231
57187  deg
 ZDOT =      -5132
999081                 TA   =           29
38790
                                          MA   =           29
35911
                                          Ha   =            189
712  n
mi
                                          Hp   =            189
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17339224
01                 X    =         5236174
47
 Y    =       10303099
99  feet           Y    =         3199211
93  meter
 Z    =        8990384
92                 Z    =         2765825
44
 XDOT =      -2354
301035                 XDOT =        -756
237523
 YDOT =      18670
581283  feet/sec       YDOT =        5682
552352  meter/sec
 ZDOT =     -16840
548167                 ZDOT =       -5136
579298

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19908556
80                 X    =         6068128
11
 Y    =        2939801
76  feet           Y    =          896051
58  meter
 Z    =        9090462
66                 Z    =         2770773
02
 XDOT =       5241
180044                 XDOT =        1597
511677
 YDOT =      16670
277018  feet/sec       YDOT =        5081
100435  meter/sec
 ZDOT =     -16854
096812                 ZDOT =       -5137
128708


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   09112
51654020  
00010596  00000-0  82463-4 0  9051
2 25544  51
6408 232
3263 0008859 269
7524  90
2623 15
72294819 37192


Satellite: ISS
Catalog Number: 25544
Epoch time:      09112
51654020   =   yrday
fracday
Element set:     905
Inclination:       51
6408  deg
RA of node:       232
3263  deg
Eccentricity:     
0008859     
Arg of perigee:   269
7524  deg
Mean anomaly:      90
2623  deg
Mean motion:   15
72294819  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3719
Checksum:              313


Coasting Arc #7 (Orbit 3734)
---------------------------------------

Vector Time (GMT): 2009/113/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -378285
60                 A    =         6729242
33  meter
 Y    =       -5254113
65  meter          E    =           
0002342
 Z    =        4187965
99                 I    =           51
39553
 XDOT =       6326
357011                 Wp   =          156
89275
 YDOT =       2445
397173  meter/sec      RA   =          226
47959  deg
 ZDOT =       3636
562291                 TA   =          255
88932
                                          MA   =          255
91535
                                          Ha   =            190
649  n
mi
                                          Hp   =            190
198

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1241094
48                 X    =         -339849
85
 Y    =      -17237905
67  feet           Y    =        -5258128
82  meter
 Z    =       13740045
89                 Z    =         4186221
77
 XDOT =      20755
764471                 XDOT =        6280
875894
 YDOT =       8022
956605  feet/sec       YDOT =        2515
888008  meter/sec
 ZDOT =      11930
978646                 ZDOT =        3667
185732

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8052882
89                 X    =        -2454518
70
 Y    =      -15298205
79  feet           Y    =        -4662893
13  meter
 Z    =       13732827
28                 Z    =         4185765
76
 XDOT =      21056
083629                 XDOT =        6417
894290
 YDOT =       -257
803645  feet/sec       YDOT =         -78
578551  meter/sec
 ZDOT =      12050
803463                 ZDOT =        3673
084895


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   09113
53345718  
00010596  00000-0  82463-4 0  9066
2 25544  51
6420 227
1168 0008928 274
2331  85
7811 15
72361083 37350


Satellite: ISS
Catalog Number: 25544
Epoch time:      09113
53345718   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:       227
1168  deg
Eccentricity:     
0008928     
Arg of perigee:   274
2331  deg
Mean anomaly:      85
7811  deg
Mean motion:   15
72361083  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3735
Checksum:              306


Coasting Arc #8 (Orbit 3749)
---------------------------------------

Vector Time (GMT): 2009/114/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5587722
01                 A    =         6731249
65  meter
 Y    =       -1102395
53  meter          E    =           
0003454
 Z    =       -3584288
85                 I    =           51
42366
 XDOT =      -1623
355731                 Wp   =          279
09835
 YDOT =      -6100
672120  meter/sec      RA   =          221
29025  deg
 ZDOT =       4404
001194                 TA   =           37
95588
                                          MA   =           37
93154
                                          Ha   =            190
988  n
mi
                                          Hp   =            190
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18332421
31                 X    =        -5557567
33
 Y    =       -3616783
24  feet           Y    =        -1164712
13  meter
 Z    =      -11759477
85                 Z    =        -3611361
35
 XDOT =      -5325
970245                 XDOT =       -1576
410656
 YDOT =     -20015
328478  feet/sec       YDOT =       -6118
562900  meter/sec
 ZDOT =      14448
822815                 ZDOT =        4396
228855

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18129409
19                 X    =        -5525843
92
 Y    =        4240581
54  feet           Y    =         1292529
25  meter
 Z    =      -11865331
95                 Z    =        -3616553
18
 XDOT =     -12876
189653                 XDOT =       -3924
662606
 YDOT =     -14678
424935  feet/sec       YDOT =       -4473
983920  meter/sec
 ZDOT =      14417
989394                 ZDOT =        4394
603167


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   09114
48680754  
00010596  00000-0  82463-4 0  9074
2 25544  51
6421 222
2339 0008979 279
1041  80
9105 15
72331450 37500


Satellite: ISS
Catalog Number: 25544
Epoch time:      09114
48680754   =   yrday
fracday
Element set:     907
Inclination:       51
6421  deg
RA of node:       222
2339  deg
Eccentricity:     
0008979     
Arg of perigee:   279
1041  deg
Mean anomaly:      80
9105  deg
Mean motion:   15
72331450  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3750
Checksum:              304


Coasting Arc #9 (Orbit 3765)
---------------------------------------

Vector Time (GMT): 2009/115/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2439249
20                 A    =         6731628
62  meter
 Y    =        5220972
27  meter          E    =           
0004260
 Z    =       -3478521
34                 I    =           51
44835
 XDOT =      -6230
739441                 Wp   =          302
10680
 YDOT =       -101
582142  meter/sec      RA   =          216
20475  deg
 ZDOT =      -4515
396814                 TA   =          279
25431
                                          MA   =          279
30249
                                          Ha   =            191
252  n
mi
                                          Hp   =            189
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8002786
10                 X    =         2397584
56
 Y    =       17129174
12  feet           Y    =         5248016
48  meter
 Z    =      -11412471
59                 Z    =        -3466772
29
 XDOT =     -20442
058535                 XDOT =       -6207
204933
 YDOT =       -333
274744  feet/sec       YDOT =        -171
126235  meter/sec
 ZDOT =     -14814
294008                 ZDOT =       -4545
609314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14626000
74                 X    =         4458005
02
 Y    =       12024475
11  feet           Y    =         3665060
01  meter
 Z    =      -11366169
09                 Z    =        -3464408
34
 XDOT =     -17661
465675                 XDOT =       -5383
214738
 YDOT =       7348
228359  feet/sec       YDOT =        2239
740004  meter/sec
 ZDOT =     -14932
347580                 ZDOT =       -4551
379542


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   09115
50370101  
00010596  00000-0  82463-4 0  9081
2 25544  51
6424 217
0248 0008889 282
6663  77
3505 15
72363988 37665


Satellite: ISS
Catalog Number: 25544
Epoch time:      09115
50370101   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:       217
0248  deg
Eccentricity:     
0008889     
Arg of perigee:   282
6663  deg
Mean anomaly:      77
3505  deg
Mean motion:   15
72363988  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3766
Checksum:              326


Coasting Arc #10 (Orbit 3781)
---------------------------------------

Vector Time (GMT): 2009/116/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5128337
20                 A    =         6728784
28  meter
 Y    =        -883263
30  meter          E    =           
0005777
 Z    =        4268449
52                 I    =           51
46367
 XDOT =       3903
422865                 Wp   =            9
57377
 YDOT =       5619
234915  meter/sec      RA   =          211
01899  deg
 ZDOT =      -3520
708381                 TA   =          116
25502
                                          MA   =          116
19564
                                          Ha   =            191
441  n
mi
                                          Hp   =            189
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16825253
27                 X    =         5117097
01
 Y    =       -2897845
46  feet           Y    =         -825978
30  meter
 Z    =       14004099
48                 Z    =         4293336
22
 XDOT =      12806
505462                 XDOT =        3857
400884
 YDOT =      18435
810089  feet/sec       YDOT =        5662
628117  meter/sec
 ZDOT =     -11550
880515                 ZDOT =       -3501
856625

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13720176
13                 X    =         4181909
68
 Y    =      -10025574
17  feet           Y    =        -3055795
01  meter
 Z    =       14101279
65                 Z    =         4298070
04
 XDOT =      18985
010115                 XDOT =        5786
631083
 YDOT =       9810
044015  feet/sec       YDOT =        2990
101416  meter/sec
 ZDOT =     -11476
793119                 ZDOT =       -3498
126543


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   09116
52058200  
00010596  00000-0  82463-4 0  9098
2 25544  51
6423 211
8160 0008769 287
7135  72
3069 15
72377811 37824


Satellite: ISS
Catalog Number: 25544
Epoch time:      09116
52058200   =   yrday
fracday
Element set:     909
Inclination:       51
6423  deg
RA of node:       211
8160  deg
Eccentricity:     
0008769     
Arg of perigee:   287
7135  deg
Mean anomaly:      72
3069  deg
Mean motion:   15
72377811  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3782
Checksum:              312


Coasting Arc #11 (Orbit 3797)
---------------------------------------

Vector Time (GMT): 2009/117/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4302954
41                 A    =         6733675
03  meter
 Y    =       -4439521
91  meter          E    =           
0008087
 Z    =        2654312
02                 I    =           51
50616
 XDOT =       5301
137310                 Wp   =           40
09032
 YDOT =      -2024
707829  meter/sec      RA   =          205
93154  deg
 ZDOT =       5204
616208                 TA   =          350
17730
                                          MA   =          350
19310
                                          Ha   =            191
665  n
mi
                                          Hp   =            189
234

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14117304
48                 X    =        -4265885
54
 Y    =      -14565360
59  feet           Y    =        -4487432
99  meter
 Z    =        8708372
76                 Z    =         2633497
57
 XDOT =      17392
182774                 XDOT =        5298
100364
 YDOT =      -6642
742222  feet/sec       YDOT =       -1965
444794  meter/sec
 ZDOT =      17075
512495                 ZDOT =        5230
362104

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19272461
27                 X    =        -5874246
20
 Y    =       -6437087
51  feet           Y    =        -1962024
27  meter
 Z    =        8626697
63                 Z    =         2629417
44
 XDOT =      11845
214696                 XDOT =        3610
421439
 YDOT =     -12433
821617  feet/sec       YDOT =       -3789
828829  meter/sec
 ZDOT =      17175
977858                 ZDOT =        5235
238051


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   09117
53744834  
00010596  00000-0  82463-4 0  9107
2 25544  51
6421 206
6061 0008849 291
8648  68
1573 15
72420359 37984


Satellite: ISS
Catalog Number: 25544
Epoch time:      09117
53744834   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:       206
6061  deg
Eccentricity:     
0008849     
Arg of perigee:   291
8648  deg
Mean anomaly:      68
1573  deg
Mean motion:   15
72420359  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3798
Checksum:              331


Coasting Arc #12 (Orbit 3812)
---------------------------------------

Vector Time (GMT): 2009/118/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3983429
95                 A    =         6726545
87  meter
 Y    =        2556703
08  meter          E    =           
0003305
 Z    =       -4782053
62                 I    =           51
50933
 XDOT =      -5822
371033                 Wp   =           85
37621
 YDOT =      -4353
373406  meter/sec      RA   =          200
75792  deg
 ZDOT =       2524
255601                 TA   =          209
39028
                                          MA   =          209
40887
                                          Ha   =            191
716  n
mi
                                          Hp   =            188
834

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13068995
91                 X    =        -3988492
71
 Y    =        8388133
47  feet           Y    =         2512130
17  meter
 Z    =      -15689152
29                 Z    =        -4801417
45
 XDOT =     -19102
267169                 XDOT =       -5785
520690
 YDOT =     -14282
721147  feet/sec       YDOT =       -4418
276742  meter/sec
 ZDOT =       8281
678482                 ZDOT =        2496
059248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7447999
75                 X    =        -2270150
32
 Y    =       13539280
16  feet           Y    =         4126772
59  meter
 Z    =      -15764648
09                 Z    =        -4805064
74
 XDOT =     -22645
524210                 XDOT =       -6902
355779
 YDOT =      -2949
864214  feet/sec       YDOT =        -899
118613  meter/sec
 ZDOT =       8171
146903                 ZDOT =        2490
565576


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   09118
49075048  
00010596  00000-0  82463-4 0  9118
2 25544  51
6415 201
7233 0008853 296
1814  63
8438 15
72457549 38133


Satellite: ISS
Catalog Number: 25544
Epoch time:      09118
49075048   =   yrday
fracday
Element set:     911
Inclination:       51
6415  deg
RA of node:       201
7233  deg
Eccentricity:     
0008853     
Arg of perigee:   296
1814  deg
Mean anomaly:      63
8438  deg
Mean motion:   15
72457549  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3813
Checksum:              321

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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