Date: March 28th 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 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 3309)
---------------------------------------

Vector Time (GMT): 2009/086/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5840376
81                 A    =         6735270
99  meter
 Y    =        1733096
83  meter          E    =           
0019462
 Z    =        2843637
45                 I    =           51
68009
 XDOT =      -3783
916535                 Wp   =          125
69382
 YDOT =      -4378
033295  meter/sec      RA   =            5
11986  deg
 ZDOT =      -5090
224577                 TA   =           21
68299
                                          MA   =           21
60070
                                          Ha   =            196
224  n
mi
                                          Hp   =            185
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19161341
23                 X    =        -5873136
48
 Y    =        5686013
22  feet           Y    =         1667603
44  meter
 Z    =        9329519
21                 Z    =         2815184
98
 XDOT =     -12414
424327                 XDOT =       -3709
951845
 YDOT =     -14363
626296  feet/sec       YDOT =       -4419
934192  meter/sec
 ZDOT =     -16700
211867                 ZDOT =       -5108
426878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19504839
28                 X    =        -5945075
01
 Y    =        4594282
61  feet           Y    =         1400337
34  meter
 Z    =        9218540
26                 Z    =         2809811
07
 XDOT =     -11153
669957                 XDOT =       -3399
638603
 YDOT =     -13612
745040  feet/sec       YDOT =       -4149
164688  meter/sec
 ZDOT =     -16771
574819                 ZDOT =       -5111
976005


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   09086
51668157  
00010596  00000-0  82463-4 0  9002
2 25544  51
6419   5
4491 0009525 165
4871 194
6566 15
71711249 33106


Satellite: ISS
Catalog Number: 25544
Epoch time:      09086
51668157   =   yrday
fracday
Element set:     900
Inclination:       51
6419  deg
RA of node:         5
4491  deg
Eccentricity:     
0009525     
Arg of perigee:   165
4871  deg
Mean anomaly:     194
6566  deg
Mean motion:   15
71711249  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3310
Checksum:              318


Coasting Arc #2 (Orbit 3325)
---------------------------------------

Vector Time (GMT): 2009/087/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4398300
37                 A    =         6731634
72  meter
 Y    =        3164125
34  meter          E    =           
0016967
 Z    =        3992616
07                 I    =           51
63875
 XDOT =      -5834
113802                 Wp   =          132
83979
 YDOT =       3112
121325  meter/sec      RA   =             
05223  deg
 ZDOT =       3938
697126                 TA   =          276
32165
                                          MA   =          276
51486
                                          Ha   =            195
959  n
mi
                                          Hp   =            185
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14430119
32                 X    =         4343196
09
 Y    =       10380988
65  feet           Y    =         3213001
90  meter
 Z    =       13099134
07                 Z    =         4013849
14
 XDOT =     -19140
793314                 XDOT =       -5887
614137
 YDOT =      10210
371800  feet/sec       YDOT =        3046
582025  meter/sec
 ZDOT =      12922
234666                 ZDOT =        3910
224519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13936523
72                 X    =         4247852
43
 Y    =       10935370
99  feet           Y    =         3333101
08  meter
 Z    =       13182243
75                 Z    =         4017947
89
 XDOT =     -18802
942164                 XDOT =       -5731
136772
 YDOT =       8433
757560  feet/sec       YDOT =        2570
609304  meter/sec
 ZDOT =      12811
270349                 ZDOT =        3904
875202


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   09087
53398445  
00010596  00000-0  82463-4 0  9016
2 25544  51
6419    
2426 0009515 169
4513 190
6850 15
71734596 33262


Satellite: ISS
Catalog Number: 25544
Epoch time:      09087
53398445   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:          
2426  deg
Eccentricity:     
0009515     
Arg of perigee:   169
4513  deg
Mean anomaly:     190
6850  deg
Mean motion:   15
71734596  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3326
Checksum:              318


Coasting Arc #3 (Orbit 3340)
---------------------------------------

Vector Time (GMT): 2009/088/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4164841
16                 A    =         6731835
60  meter
 Y    =       -3523009
81  meter          E    =           
0013701
 Z    =       -3959858
44                 I    =           51
61032
 XDOT =       6020
054224                 Wp   =          145
80861
 YDOT =       2631
515063  meter/sec      RA   =          354
88140  deg
 ZDOT =       3986
025881                 TA   =          165
64575
                                          MA   =          165
60679
                                          Ha   =            195
834  n
mi
                                          Hp   =            186
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13664177
04                 X    =         4223163
01
 Y    =      -11558431
13  feet           Y    =        -3476110
23  meter
 Z    =      -12991661
56                 Z    =        -3939483
57
 XDOT =      19750
834068                 XDOT =        5970
817133
 YDOT =       8633
579602  feet/sec       YDOT =        2698
559715  meter/sec
 ZDOT =      13077
512732                 ZDOT =        4015
151919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13989733
34                 X    =         4264070
72
 Y    =      -11253852
58  feet           Y    =        -3430174
27  meter
 Z    =      -12912338
98                 Z    =        -3935680
92
 XDOT =      18659
782721                 XDOT =        5687
501773
 YDOT =       8043
816440  feet/sec       YDOT =        2451
755251  meter/sec
 ZDOT =      13191
399465                 ZDOT =        4020
738557


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   09088
48769174  
00010596  00000-0  82463-4 0  9023
2 25544  51
6423 355
3611 0009459 173
1777 186
9515 15
71768462 33410


Satellite: ISS
Catalog Number: 25544
Epoch time:      09088
48769174   =   yrday
fracday
Element set:     902
Inclination:       51
6423  deg
RA of node:       355
3611  deg
Eccentricity:     
0009459     
Arg of perigee:   173
1777  deg
Mean anomaly:     186
9515  deg
Mean motion:   15
71768462  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3341
Checksum:              343


Coasting Arc #4 (Orbit 3356)
---------------------------------------

Vector Time (GMT): 2009/089/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5917787
80                 A    =         6734682
48  meter
 Y    =       -1297540
95  meter          E    =           
0011998
 Z    =       -2931296
60                 I    =           51
59144
 XDOT =       3501
183914                 Wp   =          156
94052
 YDOT =      -4671
647397  meter/sec      RA   =          349
80976  deg
 ZDOT =      -5018
123017                 TA   =           56
82664
                                          MA   =           56
71162
                                          Ha   =            195
589  n
mi
                                          Hp   =            186
104

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19415314
30                 X    =        -5888598
80
 Y    =       -4257024
12  feet           Y    =        -1363553
96  meter
 Z    =       -9617114
84                 Z    =        -2959974
58
 XDOT =      11486
823866                 XDOT =        3577
540228
 YDOT =     -15326
927156  feet/sec       YDOT =       -4632
068295  meter/sec
 ZDOT =     -16463
658193                 ZDOT =       -5000
928518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19338842
95                 X    =        -5894479
33
 Y    =       -4349492
15  feet           Y    =        -1325725
21  meter
 Z    =       -9729165
07                 Z    =        -2965449
51
 XDOT =      11337
688800                 XDOT =        3455
727546
 YDOT =     -13861
408181  feet/sec       YDOT =       -4224
957213  meter/sec
 ZDOT =     -16396
822359                 ZDOT =       -4997
751455


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   09089
50496457  
00010596  00000-0  82463-4 0  9039
2 25544  51
6427 350
1542 0009427 177
7386 182
3821 15
71779468 33576


Satellite: ISS
Catalog Number: 25544
Epoch time:      09089
50496457   =   yrday
fracday
Element set:     903
Inclination:       51
6427  deg
RA of node:       350
1542  deg
Eccentricity:     
0009427     
Arg of perigee:   177
7386  deg
Mean anomaly:     182
3821  deg
Mean motion:   15
71779468  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3357
Checksum:              345


Coasting Arc #5 (Orbit 3372)
---------------------------------------

Vector Time (GMT): 2009/090/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1831931
04                 A    =         6728640
33  meter
 Y    =        4404924
11  meter          E    =           
0008576
 Z    =        4737124
85                 I    =           51
54189
 XDOT =      -7236
903045                 Wp   =          131
03090
 YDOT =       -180
894019  meter/sec      RA   =          344
64180  deg
 ZDOT =      -2632
881954                 TA   =          344
83612
                                          MA   =          344
86180
                                          Ha   =            195
458  n
mi
                                          Hp   =            186
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6010272
44                 X    =        -1904063
73
 Y    =       14451850
75  feet           Y    =         4384035
07  meter
 Z    =       15541748
18                 Z    =         4728050
06
 XDOT =     -23743
120228                 XDOT =       -7221
552245
 YDOT =       -593
484313  feet/sec       YDOT =        -261
735455  meter/sec
 ZDOT =      -8638
064155                 ZDOT =       -2668
001772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5919956
89                 X    =        -1804402
86
 Y    =       14526698
12  feet           Y    =         4427737
59  meter
 Z    =       15506593
89                 Z    =         4726409
82
 XDOT =     -22639
021399                 XDOT =       -6900
373722
 YDOT =        132
613870  feet/sec       YDOT =          40
420708  meter/sec
 ZDOT =      -8775
196978                 ZDOT =       -2674
680039


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   09090
52222167  
00010596  00000-0  82463-4 0  9049
2 25544  51
6422 344
9475 0009313 181
8315 178
2814 15
71831153 33733


Satellite: ISS
Catalog Number: 25544
Epoch time:      09090
52222167   =   yrday
fracday
Element set:     904
Inclination:       51
6422  deg
RA of node:       344
9475  deg
Eccentricity:     
0009313     
Arg of perigee:   181
8315  deg
Mean anomaly:     178
2814  deg
Mean motion:   15
71831153  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3373
Checksum:              302


Coasting Arc #6 (Orbit 3388)
---------------------------------------

Vector Time (GMT): 2009/091/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6453952
48                 A    =         6737161
56  meter
 Y    =       -1013259
94  meter          E    =           
0012193
 Z    =        1643646
22                 I    =           51
54288
 XDOT =       -666
483312                 Wp   =          104
29972
 YDOT =       5098
332427  meter/sec      RA   =          339
55121  deg
 ZDOT =       5721
639468                 TA   =          273
85456
                                          MA   =          273
99395
                                          Ha   =            195
319  n
mi
                                          Hp   =            186
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21174384
77                 X    =         6456818
70
 Y    =       -3324343
62  feet           Y    =         -941072
07  meter
 Z    =        5392540
10                 Z    =         1675006
51
 XDOT =      -2186
625038                 XDOT =        -751
238908
 YDOT =      16726
812426  feet/sec       YDOT =        5090
405474  meter/sec
 ZDOT =      18771
783030                 ZDOT =        5718
195866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21035082
82                 X    =         6411493
24
 Y    =       -3949206
44  feet           Y    =        -1203718
12  meter
 Z    =        5514923
29                 Z    =         1680948
62
 XDOT =      -2086
555286                 XDOT =        -635
982051
 YDOT =      15253
751353  feet/sec       YDOT =        4649
343412  meter/sec
 ZDOT =      18758
657467                 ZDOT =        5717
638796


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   09091
53946473  
00010596  00000-0  82463-4 0  9055
2 25544  51
6426 339
7397 0009285 185
7147 174
3910 15
71820711 33895


Satellite: ISS
Catalog Number: 25544
Epoch time:      09091
53946473   =   yrday
fracday
Element set:     905
Inclination:       51
6426  deg
RA of node:       339
7397  deg
Eccentricity:     
0009285     
Arg of perigee:   185
7147  deg
Mean anomaly:     174
3910  deg
Mean motion:   15
71820711  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3389
Checksum:              340


Coasting Arc #7 (Orbit 3403)
---------------------------------------

Vector Time (GMT): 2009/092/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -639400
13                 A    =         6726645
23  meter
 Y    =       -4262828
67  meter          E    =           
0016931
 Z    =       -5176727
72                 I    =           51
48086
 XDOT =       7196
524212                 Wp   =          131
87468
 YDOT =      -2455
754169  meter/sec      RA   =          334
39757  deg
 ZDOT =       1124
594555                 TA   =          148
95282
                                          MA   =          148
85264
                                          Ha   =            195
104  n
mi
                                          Hp   =            186
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2097769
47                 X    =         -566537
45
 Y    =      -13985658
36  feet           Y    =        -4269571
39  meter
 Z    =      -16984014
82                 Z    =        -5179656
95
 XDOT =      23610
643740                 XDOT =        7217
986949
 YDOT =      -8056
936250  feet/sec       YDOT =       -2375
158442  meter/sec
 ZDOT =       3689
614682                 ZDOT =        1159
607246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2652076
70                 X    =         -808352
98
 Y    =      -13876886
12  feet           Y    =        -4229674
89  meter
 Z    =      -16995721
72                 Z    =        -5180295
98
 XDOT =      22173
943314                 XDOT =        6758
617922
 YDOT =      -8958
994927  feet/sec       YDOT =       -2730
701654  meter/sec
 ZDOT =       3826
171974                 ZDOT =        1166
217218


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   09092
49311455  
00010596  00000-0  82463-4 0  9068
2 25544  51
6429 334
8577 0009292 190
0450 170
0528 15
71867015 34042


Satellite: ISS
Catalog Number: 25544
Epoch time:      09092
49311455   =   yrday
fracday
Element set:     906
Inclination:       51
6429  deg
RA of node:       334
8577  deg
Eccentricity:     
0009292     
Arg of perigee:   190
0450  deg
Mean anomaly:     170
0528  deg
Mean motion:   15
71867015  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3404
Checksum:              310


Coasting Arc #8 (Orbit 3419)
---------------------------------------

Vector Time (GMT): 2009/093/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5898072
30                 A    =         6738301
49  meter
 Y    =        3219553
01  meter          E    =           
0018526
 Z    =        -308120
16                 I    =           51
49384
 XDOT =      -2062
944310                 Wp   =          162
37743
 YDOT =      -4344
594697  meter/sec      RA   =          329
28068  deg
 ZDOT =      -6018
994023                 TA   =           20
97829
                                          MA   =           20
90238
                                          Ha   =            195
025  n
mi
                                          Hp   =            186
920

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19350630
91                 X    =        -5932138
74
 Y    =       10562837
96  feet           Y    =         3153406
85  meter
 Z    =       -1010892
92                 Z    =         -336855
56
 XDOT =      -6768
189995                 XDOT =       -1984
970055
 YDOT =     -14253
919610  feet/sec       YDOT =       -4367
227852  meter/sec
 ZDOT =     -19747
355720                 ZDOT =       -6028
826265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18628889
31                 X    =        -5678085
46
 Y    =       11779047
67  feet           Y    =         3590253
73  meter
 Z    =       -1122891
60                 Z    =         -342257
36
 XDOT =      -6693
426707                 XDOT =       -2040
156460
 YDOT =     -12440
674872  feet/sec       YDOT =       -3791
917701  meter/sec
 ZDOT =     -19786
026288                 ZDOT =       -6030
780813


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   09093
51032821  
00010596  00000-0  82463-4 0  9070
2 25544  51
6430 329
6507 0009467 194
0244 166
0656 15
71834670 34204


Satellite: ISS
Catalog Number: 25544
Epoch time:      09093
51032821   =   yrday
fracday
Element set:     907
Inclination:       51
6430  deg
RA of node:       329
6507  deg
Eccentricity:     
0009467     
Arg of perigee:   194
0244  deg
Mean anomaly:     166
0656  deg
Mean motion:   15
71834670  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3420
Checksum:              304


Coasting Arc #9 (Orbit 3435)
---------------------------------------

Vector Time (GMT): 2009/094/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2849193
85                 A    =         6726115
04  meter
 Y    =        3101754
89  meter          E    =           
0009615
 Z    =        5245124
53                 I    =           51
42876
 XDOT =      -6019
483441                 Wp   =          182
12058
 YDOT =       4777
626226  meter/sec      RA   =          324
14897  deg
 ZDOT =        435
101535                 TA   =          263
67859
                                          MA   =          263
78811
                                          Ha   =            194
659  n
mi
                                          Hp   =            187
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9347748
86                 X    =         2788818
13
 Y    =       10176361
18  feet           Y    =         3133278
87  meter
 Z    =       17208413
82                 Z    =         5258819
01
 XDOT =     -19748
961422                 XDOT =       -6074
573901
 YDOT =      15674
626725  feet/sec       YDOT =        4710
004843  meter/sec
 ZDOT =       1427
498473                 ZDOT =         405
725163

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10043366
70                 X    =         3061218
17
 Y    =        9392511
43  feet           Y    =         2862837
48  meter
 Z    =       17262090
15                 Z    =         5261485
08
 XDOT =     -17734
860222                 XDOT =       -5405
585396
 YDOT =      16493
794658  feet/sec       YDOT =        5027
308612  meter/sec
 ZDOT =       1313
100868                 ZDOT =         400
233145


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   09094
52752433  
00010596  00000-0  82463-4 0  9081
2 25544  51
6430 324
4433 0009253 198
4360 161
6468 15
71909214 34361


Satellite: ISS
Catalog Number: 25544
Epoch time:      09094
52752433   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:       324
4433  deg
Eccentricity:     
0009253     
Arg of perigee:   198
4360  deg
Mean anomaly:     161
6468  deg
Mean motion:   15
71909214  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3436
Checksum:              312


Coasting Arc #10 (Orbit 3450)
---------------------------------------

Vector Time (GMT): 2009/095/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4439824
34                 A    =         6737604
25  meter
 Y    =       -4960580
88  meter          E    =           
0002603
 Z    =       -1042732
75                 I    =           51
44389
 XDOT =       4229
940441                 Wp   =          107
39029
 YDOT =       2549
033006  meter/sec      RA   =          319
00073  deg
 ZDOT =       5895
404302                 TA   =          241
19655
                                          MA   =          241
22269
                                          Ha   =            194
511  n
mi
                                          Hp   =            187
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14566352
81                 X    =         4500029
77
 Y    =      -16274871
64  feet           Y    =        -4910595
61  meter
 Z    =       -3421039
19                 Z    =        -1021017
70
 XDOT =      13877
757353                 XDOT =        4172
483775
 YDOT =       8362
969181  feet/sec       YDOT =        2596
013796  meter/sec
 ZDOT =      19341
877630                 ZDOT =        5915
813452

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12915783
08                 X    =         3936730
68
 Y    =      -17629617
04  feet           Y    =        -5373507
27  meter
 Z    =       -3336576
21                 Z    =        -1016988
43
 XDOT =      13235
373020                 XDOT =        4034
141696
 YDOT =       6027
944510  feet/sec       YDOT =        1837
317487  meter/sec
 ZDOT =      19421
739883                 ZDOT =        5919
746316


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   09095
48113293  
00010596  00000-0  82463-4 0  9093
2 25544  51
6424 319
5608 0009199 202
8733 157
2020 15
71934330 34515


Satellite: ISS
Catalog Number: 25544
Epoch time:      09095
48113293   =   yrday
fracday
Element set:     909
Inclination:       51
6424  deg
RA of node:       319
5608  deg
Eccentricity:     
0009199     
Arg of perigee:   202
8733  deg
Mean anomaly:     157
2020  deg
Mean motion:   15
71934330  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3451
Checksum:              308


Coasting Arc #11 (Orbit 3466)
---------------------------------------

Vector Time (GMT): 2009/096/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4350595
82                 A    =         6727096
61  meter
 Y    =       -1224564
15  meter          E    =           
0009870
 Z    =       -4988609
66                 I    =           51
38623
 XDOT =       3957
796895                 Wp   =          119
61265
 YDOT =      -6313
885838  meter/sec      RA   =          313
88989  deg
 ZDOT =      -1909
365348                 TA   =          131
90797
                                          MA   =          131
82376
                                          Ha   =            194
206  n
mi
                                          Hp   =            187
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14273608
34                 X    =        -4312345
54
 Y    =       -4017598
93  feet           Y    =        -1273001
60  meter
 Z    =      -16366829
60                 Z    =        -5009651
75
 XDOT =      12984
897950                 XDOT =        4037
380983
 YDOT =     -20714
848551  feet/sec       YDOT =       -6269
182625  meter/sec
 ZDOT =      -6264
322008                 ZDOT =       -1889
944624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14547589
01                 X    =        -4434105
13
 Y    =       -2354930
62  feet           Y    =         -717782
85  meter
 Z    =      -16449074
84                 Z    =        -5013678
01
 XDOT =      10372
061008                 XDOT =        3161
404195
 YDOT =     -21018
125974  feet/sec       YDOT =       -6406
324797  meter/sec
 ZDOT =      -6188
916383                 ZDOT =       -1886
381714


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   09096
49830028  
00010596  00000-0  82463-4 0  9109
2 25544  51
6413 314
3527 0009167 207
5903 152
4773 15
71957595 34679


Satellite: ISS
Catalog Number: 25544
Epoch time:      09096
49830028   =   yrday
fracday
Element set:     910
Inclination:       51
6413  deg
RA of node:       314
3527  deg
Eccentricity:     
0009167     
Arg of perigee:   207
5903  deg
Mean anomaly:     152
4773  deg
Mean motion:   15
71957595  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3467
Checksum:              328


Coasting Arc #12 (Orbit 3482)
---------------------------------------

Vector Time (GMT): 2009/097/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 669292
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2372538
28                 A    =         6735687
12  meter
 Y    =        5866932
23  meter          E    =           
0014803
 Z    =        2277603
55                 I    =           51
39589
 XDOT =      -5468
755076                 Wp   =          144
27107
 YDOT =       -103
140355  meter/sec      RA   =          308
71700  deg
 ZDOT =      -5425
152777                 TA   =           10
05014
                                          MA   =           10
02057
                                          Ha   =            194
053  n
mi
                                          Hp   =            187
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7783918
23                 X    =        -2449031
16
 Y    =       19248465
32  feet           Y    =         5839973
63  meter
 Z    =        7472452
58                 Z    =         2265891
42
 XDOT =     -17942
109828                 XDOT =       -5440
840850
 YDOT =       -338
386993  feet/sec       YDOT =        -164
139575  meter/sec
 ZDOT =     -17799
057668                 ZDOT =       -5451
652200

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5208520
45                 X    =        -1587557
03
 Y    =       20115653
41  feet           Y    =         6131251
16  meter
 Z    =        7427122
62                 Z    =         2263786
97
 XDOT =     -16259
674168                 XDOT =       -4955
948687
 YDOT =       2407
047478  feet/sec       YDOT =         733
668071  meter/sec
 ZDOT =     -17902
532916                 ZDOT =       -5456
692033


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   09097
51545297  
00010596  00000-0  82463-4 0  9115
2 25544  51
6415 309
1454 0009088 211
4683 148
5937 15
71987523 34833


Satellite: ISS
Catalog Number: 25544
Epoch time:      09097
51545297   =   yrday
fracday
Element set:     911
Inclination:       51
6415  deg
RA of node:       309
1454  deg
Eccentricity:     
0009088     
Arg of perigee:   211
4683  deg
Mean anomaly:     148
5937  deg
Mean motion:   15
71987523  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3483
Checksum:              338

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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