Date: May 2nd 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 3797)
---------------------------------------

Vector Time (GMT): 2009/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6142773
21                 A    =         6733374
23  meter
 Y    =         591615
32  meter          E    =           
0005149
 Z    =        2689974
23                 I    =           51
50476
 XDOT =       1749
419137                 Wp   =           82
88093
 YDOT =       5418
073641  meter/sec      RA   =          205
78469  deg
 ZDOT =      -5177
468923                 TA   =           66
41910
                                          MA   =           66
36503
                                          Ha   =            191
582  n
mi
                                          Hp   =            189
102

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20153455
41                 X    =         6122633
46
 Y    =        1940995
14  feet           Y    =          660194
58  meter
 Z    =        8825374
77                 Z    =         2719767
52
 XDOT =       5739
564097                 XDOT =        1713
854996
 YDOT =      17775
832154  feet/sec       YDOT =        5437
438209  meter/sec
 ZDOT =     -16986
446598                 ZDOT =       -5169
056056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17606970
76                 X    =         5366604
69
 Y    =       -9892133
80  feet           Y    =        -3015122
38  meter
 Z    =        8941853
08                 Z    =         2725476
82
 XDOT =      14225
810240                 XDOT =        4336
026961
 YDOT =       9969
297320  feet/sec       YDOT =        3038
641823  meter/sec
 ZDOT =     -16953
164495                 ZDOT =       -5167
324538


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
53727279  
00010596  00000-0  82463-4 0  9000
2 25544  51
6408 206
6130 0008882 291
7304  68
2913 15
72447891 37980


Satellite: ISS
Catalog Number: 25544
Epoch time:      09117
53727279   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       206
6130  deg
Eccentricity:     
0008882     
Arg of perigee:   291
7304  deg
Mean anomaly:      68
2913  deg
Mean motion:   15
72447891  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3798
Checksum:              330


Coasting Arc #2 (Orbit 3813)
---------------------------------------

Vector Time (GMT): 2009/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2502465
26                 A    =         6728634
19  meter
 Y    =       -4565955
78  meter          E    =           
0001690
 Z    =        4260158
68                 I    =           51
51610
 XDOT =       6820
846903                 Wp   =           56
63332
 YDOT =       -433
156829  meter/sec      RA   =          200
69867  deg
 ZDOT =       3542
298759                 TA   =          357
36180
                                          MA   =          357
36269
                                          Ha   =            191
760  n
mi
                                          Hp   =            188
900

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8210187
86                 X    =        -2471917
35
 Y    =      -14980169
89  feet           Y    =        -4593769
39  meter
 Z    =       13976898
55                 Z    =         4248075
32
 XDOT =      22378
106637                 XDOT =        6807
975512
 YDOT =      -1421
118207  feet/sec       YDOT =        -356
954432  meter/sec
 ZDOT =      11621
715089                 ZDOT =        3575
403582

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15490945
63                 X    =        -4721640
23
 Y    =       -7291825
89  feet           Y    =        -2222548
53  meter
 Z    =       13929330
44                 Z    =         4245659
92
 XDOT =      16724
892176                 XDOT =        5097
747135
 YDOT =     -13082
515746  feet/sec       YDOT =       -3987
550799  meter/sec
 ZDOT =      11751
076952                 ZDOT =        3581
728255


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
55409624  
00010596  00000-0  82463-4 0  9015
2 25544  51
6407 201
4024 0009011 295
6797  64
3434 15
72495225 38146


Satellite: ISS
Catalog Number: 25544
Epoch time:      09118
55409624   =   yrday
fracday
Element set:     901
Inclination:       51
6407  deg
RA of node:       201
4024  deg
Eccentricity:     
0009011     
Arg of perigee:   295
6797  deg
Mean anomaly:      64
3434  deg
Mean motion:   15
72495225  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3814
Checksum:              301


Coasting Arc #3 (Orbit 3828)
---------------------------------------

Vector Time (GMT): 2009/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5610346
96                 A    =         6731071
45  meter
 Y    =        1306336
00  meter          E    =           
0004807
 Z    =       -3475879
68                 I    =           51
55201
 XDOT =      -3930
670109                 Wp   =          327
13854
 YDOT =      -4825
598116  meter/sec      RA   =          195
51775  deg
 ZDOT =       4531
863350                 TA   =          351
58644
                                          MA   =          351
59449
                                          Ha   =            191
835  n
mi
                                          Hp   =            188
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18406650
13                 X    =        -5607652
33
 Y    =        4285879
27  feet           Y    =         1243613
21  meter
 Z    =      -11403804
72                 Z    =        -3503128
29
 XDOT =     -12895
899307                 XDOT =       -3898
432461
 YDOT =     -15832
014815  feet/sec       YDOT =       -4869
373325  meter/sec
 ZDOT =      14868
318077                 ZDOT =        4512
845872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12114550
50                 X    =        -3692514
99
 Y    =       14421255
84  feet           Y    =         4395598
78  meter
 Z    =      -11510227
55                 Z    =        -3508317
36
 XDOT =     -18828
236415                 XDOT =       -5738
846459
 YDOT =      -4011
919604  feet/sec       YDOT =       -1222
833095  meter/sec
 ZDOT =      14793
616750                 ZDOT =        4509
094385


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   09119
50735746  
00010596  00000-0  82463-4 0  9029
2 25544  51
6398 196
5188 0009009 299
9999  60
0269 15
72509991 38299


Satellite: ISS
Catalog Number: 25544
Epoch time:      09119
50735746   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       196
5188  deg
Eccentricity:     
0009009     
Arg of perigee:   299
9999  deg
Mean anomaly:      60
0269  deg
Mean motion:   15
72509991  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3829
Checksum:              368


Coasting Arc #4 (Orbit 3844)
---------------------------------------

Vector Time (GMT): 2009/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4274996
64                 A    =         6730777
23  meter
 Y    =        3719896
00  meter          E    =           
0006275
 Z    =       -3635520
97                 I    =           51
57884
 XDOT =      -5844
879701                 Wp   =          341
80206
 YDOT =       2443
512527  meter/sec      RA   =          190
43994  deg
 ZDOT =      -4364
872395                 TA   =          241
76580
                                          MA   =          241
82917
                                          Ha   =            192
174  n
mi
                                          Hp   =            188
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14025579
52                 X    =         4250743
16
 Y    =       12204383
21  feet           Y    =         3767566
18  meter
 Z    =      -11927562
23                 Z    =        -3614811
59
 XDOT =     -19176
114506                 XDOT =       -5850
565243
 YDOT =       8016
773384  feet/sec       YDOT =        2378
120224  meter/sec
 ZDOT =     -14320
447491                 ZDOT =       -4393
280524

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18616837
57                 X    =         5674412
09
 Y    =        1004357
95  feet           Y    =          306128
30  meter
 Z    =      -11846316
51                 Z    =        -3610757
27
 XDOT =     -10099
366365                 XDOT =       -3078
286868
 YDOT =      16679
122782  feet/sec       YDOT =        5083
796624  meter/sec
 ZDOT =     -14431
332942                 ZDOT =       -4398
670281


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   09120
52415573  
00010596  00000-0  82463-4 0  9037
2 25544  51
6391 191
3085 0009004 304
4763  55
5548 15
72506139 38455


Satellite: ISS
Catalog Number: 25544
Epoch time:      09120
52415573   =   yrday
fracday
Element set:     903
Inclination:       51
6391  deg
RA of node:       191
3085  deg
Eccentricity:     
0009004     
Arg of perigee:   304
4763  deg
Mean anomaly:      55
5548  deg
Mean motion:   15
72506139  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3845
Checksum:              302


Coasting Arc #5 (Orbit 3860)
---------------------------------------

Vector Time (GMT): 2009/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4482070
04                 A    =         6728780
36  meter
 Y    =       -2867747
53  meter          E    =           
0008914
 Z    =        4121948
96                 I    =           51
60323
 XDOT =       5717
865396                 Wp   =           19
09552
 YDOT =       3518
218958  meter/sec      RA   =          185
26098  deg
 ZDOT =      -3759
140122                 TA   =          109
51584
                                          MA   =          109
41954
                                          Ha   =            192
288  n
mi
                                          Hp   =            187
914

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14704954
21                 X    =         4493780
87
 Y    =       -9408620
51  feet           Y    =        -2817561
16  meter
 Z    =       13523454
58                 Z    =         4143751
15
 XDOT =      18759
400906                 XDOT =        5696
360344
 YDOT =      11542
713118  feet/sec       YDOT =        3582
039430  meter/sec
 ZDOT =     -12333
136882                 ZDOT =       -3731
414763

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5507405
56                 X    =         1678657
21
 Y    =      -16496033
88  feet           Y    =        -5027991
13  meter
 Z    =       13608489
72                 Z    =         4147867
67
 XDOT =      20705
675890                 XDOT =        6311
090011
 YDOT =      -3200
187242  feet/sec       YDOT =        -975
417071  meter/sec
 ZDOT =     -12224
460421                 ZDOT =       -3726
015536


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   09121
54093834  
00010596  00000-0  82463-4 0  9043
2 25544  51
6399 186
0978 0009202 309
0424  50
9919 15
72572576 38617


Satellite: ISS
Catalog Number: 25544
Epoch time:      09121
54093834   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:       186
0978  deg
Eccentricity:     
0009202     
Arg of perigee:   309
0424  deg
Mean anomaly:      50
9919  deg
Mean motion:   15
72572576  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3861
Checksum:              330


Coasting Arc #6 (Orbit 3876)
---------------------------------------

Vector Time (GMT): 2009/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5598110
74                 A    =         6732681
76  meter
 Y    =       -2324114
74  meter          E    =           
0010619
 Z    =        2914275
73                 I    =           51
64510
 XDOT =       4269
691095                 Wp   =           39
79343
 YDOT =      -3969
675614  meter/sec      RA   =          180
18432  deg
 ZDOT =       5033
922905                 TA   =          353
74981
                                          MA   =          353
76305
                                          Ha   =            192
598  n
mi
                                          Hp   =            187
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18366505
06                 X    =        -5585863
07
 Y    =       -7625048
36  feet           Y    =        -2386647
69  meter
 Z    =        9561272
07                 Z    =         2887109
77
 XDOT =      14008
172884                 XDOT =        4289
309439
 YDOT =     -13023
870125  feet/sec       YDOT =       -3921
819895  meter/sec
 ZDOT =      16515
495096                 ZDOT =        5054
712613

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19036647
84                 X    =        -5802370
26
 Y    =        5924477
83  feet           Y    =         1805780
84  meter
 Z    =        9454860
95                 Z    =         2881841
62
 XDOT =       2793
219665                 XDOT =         851
373354
 YDOT =     -17521
949785  feet/sec       YDOT =       -5340
690294  meter/sec
 ZDOT =      16596
494257                 ZDOT =        5058
611449


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   09122
55771013  
00010596  00000-0  82463-4 0  9058
2 25544  51
6395 180
8872 0009028 313
8661  46
1755 15
72556031 38770


Satellite: ISS
Catalog Number: 25544
Epoch time:      09122
55771013   =   yrday
fracday
Element set:     905
Inclination:       51
6395  deg
RA of node:       180
8872  deg
Eccentricity:     
0009028     
Arg of perigee:   313
8661  deg
Mean anomaly:      46
1755  deg
Mean motion:   15
72556031  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3877
Checksum:              318


Coasting Arc #7 (Orbit 3891)
---------------------------------------

Vector Time (GMT): 2009/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2882685
96                 A    =         6726817
90  meter
 Y    =        3932634
37  meter          E    =           
0005226
 Z    =       -4636177
02                 I    =           51
65550
 XDOT =      -6932
571450                 Wp   =           52
97133
 YDOT =      -1686
382235  meter/sec      RA   =          175
01526  deg
 ZDOT =       2885
381868                 TA   =          245
55812
                                          MA   =          245
61264
                                          Ha   =            192
667  n
mi
                                          Hp   =            187
354

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9457631
10                 X    =        -2903925
30
 Y    =       12902343
72  feet           Y    =         3900279
78  meter
 Z    =      -15210554
52                 Z    =        -4650232
70
 XDOT =     -22744
656988                 XDOT =       -6927
215507
 YDOT =      -5532
750115  feet/sec       YDOT =       -1763
876380  meter/sec
 ZDOT =       9466
475946                 ZDOT =        2851
716310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1326246
92                 X    =          404240
06
 Y    =       15890002
44  feet           Y    =         4843272
74  meter
 Z    =      -15265225
84                 Z    =        -4652840
83
 XDOT =     -19723
096698                 XDOT =       -6011
599873
 YDOT =      10597
138088  feet/sec       YDOT =        3230
007689  meter/sec
 ZDOT =       9334
684750                 ZDOT =        2845
211912


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   09123
51092052  
00010596  00000-0  82463-4 0  9065
2 25544  51
6395 176
0024 0009101 318
3091  41
7377 15
72580292 38929


Satellite: ISS
Catalog Number: 25544
Epoch time:      09123
51092052   =   yrday
fracday
Element set:     906
Inclination:       51
6395  deg
RA of node:       176
0024  deg
Eccentricity:     
0009101     
Arg of perigee:   318
3091  deg
Mean anomaly:      41
7377  deg
Mean motion:   15
72580292  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3892
Checksum:              294


Coasting Arc #8 (Orbit 3907)
---------------------------------------

Vector Time (GMT): 2009/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6364428
70                 A    =         6734225
42  meter
 Y    =         576152
20  meter          E    =           
0002660
 Z    =       -2127626
35                 I    =           51
71061
 XDOT =      -2287
102949                 Wp   =          331
89869
 YDOT =       4837
110210  meter/sec      RA   =          169
93415  deg
 ZDOT =      -5526
513144                 TA   =          231
83361
                                          MA   =          231
85757
                                          Ha   =            192
849  n
mi
                                          Hp   =            187
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20880671
58                 X    =         6367848
75
 Y    =        1890263
14  feet           Y    =          647342
09  meter
 Z    =       -6980401
41                 Z    =        -2096699
39
 XDOT =      -7503
618598                 XDOT =       -2314
175325
 YDOT =      15869
784154  feet/sec       YDOT =        4811
383132  meter/sec
 ZDOT =     -18131
604803                 ZDOT =       -5537
689729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16868143
48                 X    =         5141410
13
 Y    =      -12518624
11  feet           Y    =        -3815676
63  meter
 Z    =       -6859397
19                 Z    =        -2090744
26
 XDOT =       4132
745137                 XDOT =        1259
660718
 YDOT =      15536
658867  feet/sec       YDOT =        4735
573623  meter/sec
 ZDOT =     -18174
950803                 ZDOT =       -5539
725005


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   09124
52766529  
00010596  00000-0  82463-4 0  9075
2 25544  51
6401 170
7918 0009087 322
8368  37
2164 15
72613486 39084


Satellite: ISS
Catalog Number: 25544
Epoch time:      09124
52766529   =   yrday
fracday
Element set:     907
Inclination:       51
6401  deg
RA of node:       170
7918  deg
Eccentricity:     
0009087     
Arg of perigee:   322
8368  deg
Mean anomaly:      37
2164  deg
Mean motion:   15
72613486  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3908
Checksum:              329


Coasting Arc #9 (Orbit 3923)
---------------------------------------

Vector Time (GMT): 2009/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1084787
22                 A    =         6725200
47  meter
 Y    =       -4378891
36  meter          E    =           
0010867
 Z    =        4991096
49                 I    =           51
70867
 XDOT =       7428
952918                 Wp   =          358
65571
 YDOT =       -412
591371  meter/sec      RA   =          164
77969  deg
 ZDOT =      -1966
054502                 TA   =          110
39829
                                          MA   =          110
28153
                                          Ha   =            192
944  n
mi
                                          Hp   =            186
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3559013
20                 X    =         1109425
93
 Y    =      -14366441
48  feet           Y    =        -4366622
91  meter
 Z    =       16374988
49                 Z    =         4996426
28
 XDOT =      24373
205111                 XDOT =        7442
565308
 YDOT =      -1353
646230  feet/sec       YDOT =        -329
440360  meter/sec
 ZDOT =      -6450
310045                 ZDOT =       -1929
931107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7203300
59                 X    =        -2195566
02
 Y    =      -12903539
30  feet           Y    =        -3932998
78  meter
 Z    =       16395505
43                 Z    =         4997350
05
 XDOT =      16071
492950                 XDOT =        4898
591051
 YDOT =     -17032
203813  feet/sec       YDOT =       -5191
415722  meter/sec
 ZDOT =      -6309
048033                 ZDOT =       -1922
997841


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   09125
54439567  
00010596  00000-0  82463-4 0  9088
2 25544  51
6392 165
5812 0009146 326
5251  33
5332 15
72643583 39241


Satellite: ISS
Catalog Number: 25544
Epoch time:      09125
54439567   =   yrday
fracday
Element set:     908
Inclination:       51
6392  deg
RA of node:       165
5812  deg
Eccentricity:     
0009146     
Arg of perigee:   326
5251  deg
Mean anomaly:      33
5332  deg
Mean motion:   15
72643583  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3924
Checksum:              319


Coasting Arc #10 (Orbit 3939)
---------------------------------------

Vector Time (GMT): 2009/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6467750
21                 A    =         6735468
81  meter
 Y    =        1305599
20  meter          E    =           
0017126
 Z    =        1295580
23                 I    =           51
77080
 XDOT =        170
654183                 Wp   =           26
62509
 YDOT =      -4991
866977  meter/sec      RA   =          159
68941  deg
 ZDOT =       5867
689618                 TA   =          347
57303
                                          MA   =          347
61521
                                          Ha   =            193
328  n
mi
                                          Hp   =            186
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21219652
91                 X    =        -6488162
74
 Y    =        4283461
94  feet           Y    =         1233158
88  meter
 Z    =        4250591
31                 Z    =         1264109
79
 XDOT =        559
889052                 XDOT =         197
956715
 YDOT =     -16377
516329  feet/sec       YDOT =       -4989
806084  meter/sec
 ZDOT =      19250
950189                 ZDOT =        5868
584889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12394698
00                 X    =        -3777903
95
 Y    =       17777056
23  feet           Y    =         5418446
74  meter
 Z    =        4127587
16                 Z    =         1258088
57
 XDOT =      -9697
369880                 XDOT =       -2955
758339
 YDOT =     -11243
372582  feet/sec       YDOT =       -3426
979963  meter/sec
 ZDOT =      19254
081127                 ZDOT =        5868
643928


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   09126
56111601  
00010596  00000-0  82463-4 0  9098
2 25544  51
6390 160
3700 0009238 332
1946  27
8721 15
72605293 39406


Satellite: ISS
Catalog Number: 25544
Epoch time:      09126
56111601   =   yrday
fracday
Element set:     909
Inclination:       51
6390  deg
RA of node:       160
3700  deg
Eccentricity:     
0009238     
Arg of perigee:   332
1946  deg
Mean anomaly:      27
8721  deg
Mean motion:   15
72605293  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3940
Checksum:              294


Coasting Arc #11 (Orbit 3954)
---------------------------------------

Vector Time (GMT): 2009/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         764360
81                 A    =         6724262
70  meter
 Y    =        4186620
40  meter          E    =           
0012313
 Z    =       -5214230
65                 I    =           51
76150
 XDOT =      -7188
547101                 Wp   =           58
88821
 YDOT =       2547
960335  meter/sec      RA   =          154
55279  deg
 ZDOT =        999
996972                 TA   =          220
59315
                                          MA   =          220
68502
                                          Ha   =            193
335  n
mi
                                          Hp   =            186
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2507745
45                 X    =          742818
83
 Y    =       13735631
24  feet           Y    =         4195047
70  meter
 Z    =      -17107055
95                 Z    =        -5210569
47
 XDOT =     -23584
472117                 XDOT =       -7221
362454
 YDOT =       8359
449918  feet/sec       YDOT =        2467
390284  meter/sec
 ZDOT =       3280
829960                 ZDOT =         964
994679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11514338
11                 X    =         3509570
26
 Y    =        7929478
20  feet           Y    =         2416904
96  meter
 Z    =      -17092428
42                 Z    =        -5209772
18
 XDOT =     -10318
699944                 XDOT =       -3145
139743
 YDOT =      21704
612463  feet/sec       YDOT =        6615
565879  meter/sec
 ZDOT =       3144
089475                 ZDOT =         958
318472


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   09127
51427509  
00010596  00000-0  82463-4 0  9103
2 25544  51
6395 155
4848 0009191 334
5969  25
4739 15
72645585 39555


Satellite: ISS
Catalog Number: 25544
Epoch time:      09127
51427509   =   yrday
fracday
Element set:     910
Inclination:       51
6395  deg
RA of node:       155
4848  deg
Eccentricity:     
0009191     
Arg of perigee:   334
5969  deg
Mean anomaly:      25
4739  deg
Mean motion:   15
72645585  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3955
Checksum:              348


Coasting Arc #12 (Orbit 3970)
---------------------------------------

Vector Time (GMT): 2009/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5965006
65                 A    =         6735841
63  meter
 Y    =       -3094607
79  meter          E    =           
0004280
 Z    =        -466638
11                 I    =           51
82577
 XDOT =       1826
249962                 Wp   =           88
98594
 YDOT =       4421
399175  meter/sec      RA   =          149
45045  deg
 ZDOT =      -6023
850638                 TA   =           96
06949
                                          MA   =           96
02071
                                          Ha   =            193
417  n
mi
                                          Hp   =            186
072

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19570231
79                 X    =         6001434
63
 Y    =      -10152912
70  feet           Y    =        -3027699
90  meter
 Z    =       -1530964
92                 Z    =         -437571
18
 XDOT =       5991
633733                 XDOT =        1805
936816
 YDOT =      14505
902805  feet/sec       YDOT =        4441
708180  meter/sec
 ZDOT =     -19763
289494                 ZDOT =       -6015
027577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6412933
14                 X    =         1954662
02
 Y    =      -21101766
13  feet           Y    =        -6431818
32  meter
 Z    =       -1417468
46                 Z    =         -432044
39
 XDOT =      13105
905833                 XDOT =        3994
680098
 YDOT =       5296
919824  feet/sec       YDOT =        1614
501162  meter/sec
 ZDOT =     -19728
456200                 ZDOT =       -6013
233450


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   09128
53096670  
00010596  00000-0  82463-4 0  9118
2 25544  51
6383 150
2733 0009144 339
2835  20
7955 15
72682015 39715


Satellite: ISS
Catalog Number: 25544
Epoch time:      09128
53096670   =   yrday
fracday
Element set:     911
Inclination:       51
6383  deg
RA of node:       150
2733  deg
Eccentricity:     
0009144     
Arg of perigee:   339
2835  deg
Mean anomaly:      20
7955  deg
Mean motion:   15
72682015  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3971
Checksum:              313

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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