Date: March 26th 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 3240)
---------------------------------------

Vector Time (GMT): 2009/082/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5760661
71                 A    =         6734022
18  meter
 Y    =        -120564
32  meter          E    =           
0013203
 Z    =       -3502213
40                 I    =           51
79632
 XDOT =       2868
329528                 Wp   =          129
20120
 YDOT =       5502
139835  meter/sec      RA   =           27
38007  deg
 ZDOT =       4531
800009                 TA   =          189
42496
                                          MA   =          189
44976
                                          Ha   =            196
855  n
mi
                                          Hp   =            185
297

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18899808
76                 X    =         5778594
64
 Y    =        -395552
24  feet           Y    =          -56045
25  meter
 Z    =      -11490201
45                 Z    =        -3474184
91
 XDOT =       9410
529946                 XDOT =        2784
576122
 YDOT =      18051
639878  feet/sec       YDOT =        5533
747236  meter/sec
 ZDOT =      14868
110265                 ZDOT =        4545
530300

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13394638
75                 X    =        -4082685
89
 Y    =       13433026
21  feet           Y    =         4094386
39  meter
 Z    =      -11380747
85                 Z    =        -3468851
94
 XDOT =     -18254
805113                 XDOT =       -5564
064599
 YDOT =      -5569
299364  feet/sec       YDOT =       -1697
522446  meter/sec
 ZDOT =      14922
104433                 ZDOT =        4548
257431


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   09082
12924171  
00010596  00000-0  82463-4 0  9006
2 25544  51
6413  27
8951 0009595 147
7249 212
4502 15
71525176 32412


Satellite: ISS
Catalog Number: 25544
Epoch time:      09082
12924171   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:        27
8951  deg
Eccentricity:     
0009595     
Arg of perigee:   147
7249  deg
Mean anomaly:     212
4502  deg
Mean motion:   15
71525176  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3241
Checksum:              298


Coasting Arc #2 (Orbit 3256)
---------------------------------------

Vector Time (GMT): 2009/083/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3742383
73                 A    =         6734123
66  meter
 Y    =       -4440379
03  meter          E    =           
0012639
 Z    =       -3409617
21                 I    =           51
76959
 XDOT =       5964
589693                 Wp   =          130
32540
 YDOT =      -1489
954327  meter/sec      RA   =           22
32421  deg
 ZDOT =      -4625
534023                 TA   =           89
80749
                                          MA   =           89
66266
                                          Ha   =            196
746  n
mi
                                          Hp   =            185
287

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12278161
85                 X    =        -3675889
40
 Y    =      -14568172
67  feet           Y    =        -4481857
09  meter
 Z    =      -11186408
15                 Z    =        -3427635
58
 XDOT =      19568
863821                 XDOT =        6003
277088
 YDOT =      -4888
301598  feet/sec       YDOT =       -1423
038939  meter/sec
 ZDOT =     -15175
636559                 ZDOT =       -4596
464237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18933669
19                 X    =         5770982
37
 Y    =        1707358
07  feet           Y    =          520402
74  meter
 Z    =      -11257075
13                 Z    =        -3431156
50
 XDOT =     -10356
526832                 XDOT =       -3156
669378
 YDOT =      15951
779609  feet/sec       YDOT =        4862
102425  meter/sec
 ZDOT =     -15062
212913                 ZDOT =       -4590
962496


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   09083
14667333  
00010596  00000-0  82463-4 0  9014
2 25544  51
6408  22
6890 0009595 151
4265 208
7425 15
71523800 32572


Satellite: ISS
Catalog Number: 25544
Epoch time:      09083
14667333   =   yrday
fracday
Element set:     901
Inclination:       51
6408  deg
RA of node:        22
6890  deg
Eccentricity:     
0009595     
Arg of perigee:   151
4265  deg
Mean anomaly:     208
7425  deg
Mean motion:   15
71523800  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3257
Checksum:              306


Coasting Arc #3 (Orbit 3272)
---------------------------------------

Vector Time (GMT): 2009/084/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4389992
26                 A    =         6730293
36  meter
 Y    =        2365171
89  meter          E    =           
0013192
 Z    =        4506974
87                 I    =           51
73025
 XDOT =      -5556
333034                 Wp   =          112
32180
 YDOT =      -4313
936008  meter/sec      RA   =           17
16687  deg
 ZDOT =      -3145
870387                 TA   =            9
02171
                                          MA   =            8
99803
                                          Ha   =            196
625  n
mi
                                          Hp   =            185
439

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14402861
76                 X    =        -4438007
68
 Y    =        7759750
28  feet           Y    =         2315812
45  meter
 Z    =       14786662
97                 Z    =         4485531
54
 XDOT =     -18229
439087                 XDOT =       -5492
398940
 YDOT =     -14153
333358  feet/sec       YDOT =       -4375
713028  meter/sec
 ZDOT =     -10321
097069                 ZDOT =       -3172
707129

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4521435
68                 X    =         1378133
59
 Y    =      -15801184
89  feet           Y    =        -4816201
15  meter
 Z    =       14703085
68                 Z    =         4481500
51
 XDOT =      21658
401465                 XDOT =        6601
480766
 YDOT =      -3511
460889  feet/sec       YDOT =       -1070
293279  meter/sec
 ZDOT =     -10426
188108                 ZDOT =       -3177
902135


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   09084
16408888  
00010596  00000-0  82463-4 0  9026
2 25544  51
6417  17
4831 0009385 155
4218 204
7393 15
71594326 32737


Satellite: ISS
Catalog Number: 25544
Epoch time:      09084
16408888   =   yrday
fracday
Element set:     902
Inclination:       51
6417  deg
RA of node:        17
4831  deg
Eccentricity:     
0009385     
Arg of perigee:   155
4218  deg
Mean anomaly:     204
7393  deg
Mean motion:   15
71594326  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3273
Checksum:              323


Coasting Arc #4 (Orbit 3288)
---------------------------------------

Vector Time (GMT): 2009/085/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5742793
71                 A    =         6737250
38  meter
 Y    =        2871910
07  meter          E    =           
0017143
 Z    =        2033491
65                 I    =           51
72460
 XDOT =      -3826
512011                 Wp   =          102
38288
 YDOT =       3676
084984  meter/sec      RA   =           12
09789  deg
 ZDOT =       5571
740688                 TA   =          280
23553
                                          MA   =          280
42880
                                          Ha   =            196
507  n
mi
                                          Hp   =            185
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18841186
70                 X    =         5700374
38
 Y    =        9422277
14  feet           Y    =         2935892
39  meter
 Z    =        6671560
54                 Z    =         2061286
77
 XDOT =     -12554
173266                 XDOT =       -3894
400711
 YDOT =      12060
646272  feet/sec       YDOT =        3632
915724  meter/sec
 ZDOT =      18279
989135                 ZDOT =        5552
986199

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19734104
88                 X    =        -6014955
17
 Y    =        7271321
78  feet           Y    =         2216298
88  meter
 Z    =        6780289
60                 Z    =         2066632
27
 XDOT =        391
060659                 XDOT =         119
195289
 YDOT =     -16045
534099  feet/sec       YDOT =       -4890
678794  meter/sec
 ZDOT =      18207
003577                 ZDOT =        5549
494690


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   09085
18149322  
00010596  00000-0  82463-4 0  9035
2 25544  51
6413  12
2774 0009458 158
1826 201
9740 15
71571241 32891


Satellite: ISS
Catalog Number: 25544
Epoch time:      09085
18149322   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:        12
2774  deg
Eccentricity:     
0009458     
Arg of perigee:   158
1826  deg
Mean anomaly:     201
9740  deg
Mean motion:   15
71571241  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3289
Checksum:              306


Coasting Arc #5 (Orbit 3303)
---------------------------------------

Vector Time (GMT): 2009/086/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2154124
48                 A    =         6727791
07  meter
 Y    =       -3816930
38  meter          E    =           
0020124
 Z    =       -5120992
10                 I    =           51
66332
 XDOT =       7244
925600                 Wp   =          125
03687
 YDOT =       2074
122135  meter/sec      RA   =            6
95347  deg
 ZDOT =       1494
416022                 TA   =          159
36231
                                          MA   =          159
28092
                                          Ha   =            196
375  n
mi
                                          Hp   =            185
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7067337
54                 X    =         2221522
92
 Y    =      -12522737
47  feet           Y    =        -3792465
39  meter
 Z    =      -16801155
18                 Z    =        -5110363
21
 XDOT =      23769
440944                 XDOT =        7213
934318
 YDOT =       6804
862648  feet/sec       YDOT =        2154
965990  meter/sec
 ZDOT =       4902
939706                 ZDOT =        1529
536550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4471596
28                 X    =         1362942
55
 Y    =       13716972
28  feet           Y    =         4180933
15  meter
 Z    =      -16759908
33                 Z    =        -5108420
06
 XDOT =     -19981
296029                 XDOT =       -6090
299030
 YDOT =      12700
897606  feet/sec       YDOT =        3871
233590  meter/sec
 ZDOT =       5040
210653                 ZDOT =        1536
256207


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
13529531  
00010596  00000-0  82463-4 0  9046
2 25544  51
6411   7
3966 0009339 162
0245 198
1249 15
71583628 33045


Satellite: ISS
Catalog Number: 25544
Epoch time:      09086
13529531   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:         7
3966  deg
Eccentricity:     
0009339     
Arg of perigee:   162
0245  deg
Mean anomaly:     198
1249  deg
Mean motion:   15
71583628  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3304
Checksum:              311


Coasting Arc #6 (Orbit 3319)
---------------------------------------

Vector Time (GMT): 2009/087/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6672226
04                 A    =         6738769
82  meter
 Y    =        -658436
52  meter          E    =           
0019746
 Z    =        -559024
24                 I    =           51
67203
 XDOT =        960
695550                 Wp   =          150
78632
 YDOT =      -4722
376328  meter/sec      RA   =            1
85651  deg
 ZDOT =      -6009
800495                 TA   =           35
29378
                                          MA   =           35
16321
                                          Ha   =            196
173  n
mi
                                          Hp   =            185
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21890505
39                 X    =        -6661651
73
 Y    =       -2160224
79  feet           Y    =         -732990
16  meter
 Z    =       -1834069
03                 Z    =         -591412
47
 XDOT =       3151
888286                 XDOT =        1042
625350
 YDOT =     -15493
360657  feet/sec       YDOT =       -4711
175684  meter/sec
 ZDOT =     -19717
193224                 ZDOT =       -6004
933985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16033291
80                 X    =         4886947
34
 Y    =      -15043747
01  feet           Y    =        -4585334
09  meter
 Z    =       -1960570
43                 Z    =         -597581
87
 XDOT =       8412
703519                 XDOT =        2564
192033
 YDOT =      11491
035161  feet/sec       YDOT =        3502
467517  meter/sec
 ZDOT =     -19698
503395                 ZDOT =       -6004
103835


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
15267066  
00010596  00000-0  82463-4 0  9052
2 25544  51
6417   2
1905 0009338 165
1147 195
0292 15
71633359 33200


Satellite: ISS
Catalog Number: 25544
Epoch time:      09087
15267066   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:         2
1905  deg
Eccentricity:     
0009338     
Arg of perigee:   165
1147  deg
Mean anomaly:     195
0292  deg
Mean motion:   15
71633359  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3320
Checksum:              302


Coasting Arc #7 (Orbit 3335)
---------------------------------------

Vector Time (GMT): 2009/088/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         526489
20                 A    =         6726790
17  meter
 Y    =        4149458
07  meter          E    =           
0010465
 Z    =        5264949
62                 I    =           51
60163
 XDOT =      -7669
982335                 Wp   =          156
01415
 YDOT =        638
945446  meter/sec      RA   =          356
73585  deg
 ZDOT =        253
847557                 TA   =          291
51943
                                          MA   =          291
63096
                                          Ha   =            196
042  n
mi
                                          Hp   =            185
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1727326
78                 X    =          454473
67
 Y    =       13613707
58  feet           Y    =         4154943
23  meter
 Z    =       17273456
76                 Z    =         5267332
16
 XDOT =     -25163
984040                 XDOT =       -7677
790237
 YDOT =       2096
277710  feet/sec       YDOT =         553
131591  meter/sec
 ZDOT =        832
833192                 ZDOT =         216
567350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11448733
97                 X    =        -3489574
11
 Y    =       -7544032
62  feet           Y    =        -2299421
14  meter
 Z    =       17283028
16                 Z    =         5267866
98
 XDOT =      14093
665393                 XDOT =        4295
749212
 YDOT =     -19741
861041  feet/sec       YDOT =       -6017
319245  meter/sec
 ZDOT =        687
320427                 ZDOT =         209
495266


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
17003110  
00010596  00000-0  82463-4 0  9064
2 25544  51
6410 356
9847 0009328 169
1986 190
9378 15
71657986 33360


Satellite: ISS
Catalog Number: 25544
Epoch time:      09088
17003110   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:       356
9847  deg
Eccentricity:     
0009328     
Arg of perigee:   169
1986  deg
Mean anomaly:     190
9378  deg
Mean motion:   15
71657986  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3336
Checksum:              344


Coasting Arc #8 (Orbit 3350)
---------------------------------------

Vector Time (GMT): 2009/089/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6439610
65                 A    =         6738453
47  meter
 Y    =       -1733624
12  meter          E    =           
0007553
 Z    =        -977974
19                 I    =           51
61161
 XDOT =       2088
011523                 Wp   =           99
59719
 YDOT =       4435
616129  meter/sec      RA   =          351
60434  deg
 ZDOT =       5923
492829                 TA   =          249
73507
                                          MA   =          249
81628
                                          Ha   =            195
940  n
mi
                                          Hp   =            186
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21127331
54                 X    =         6463268
59
 Y    =       -5687743
16  feet           Y    =        -1661480
39  meter
 Z    =       -3208576
73                 Z    =         -946632
69
 XDOT =       6850
431507                 XDOT =        2009
480954
 YDOT =      14552
546356  feet/sec       YDOT =        4458
526587  meter/sec
 ZDOT =      19434
031590                 ZDOT =        5933
445611

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8961704
14                 X    =        -2731527
42
 Y    =       19979289
46  feet           Y    =         6089687
43  meter
 Z    =       -3086320
82                 Z    =         -940710
59
 XDOT =     -14078
275286                 XDOT =       -4291
058307
 YDOT =      -3326
457999  feet/sec       YDOT =       -1013
904398  meter/sec
 ZDOT =      19473
173455                 ZDOT =        5935
423269


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
12379471  
00010596  00000-0  82463-4 0  9077
2 25544  51
6412 352
1035 0009207 172
5019 187
6283 15
71658745 33519


Satellite: ISS
Catalog Number: 25544
Epoch time:      09089
12379471   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:       352
1035  deg
Eccentricity:     
0009207     
Arg of perigee:   172
5019  deg
Mean anomaly:     187
6283  deg
Mean motion:   15
71658745  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3351
Checksum:              316


Coasting Arc #9 (Orbit 3366)
---------------------------------------

Vector Time (GMT): 2009/090/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3014304
30                 A    =         6727897
85  meter
 Y    =       -3359153
08  meter          E    =           
0014671
 Z    =       -4999250
94                 I    =           51
54786
 XDOT =       6727
318869                 Wp   =          113
93725
 YDOT =      -3186
564697  meter/sec      RA   =          346
50653  deg
 ZDOT =      -1925
376197                 TA   =          137
47128
                                          MA   =          137
35755
                                          Ha   =            195
784  n
mi
                                          Hp   =            186
191

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9889449
81                 X    =        -2952232
00
 Y    =      -11020843
43  feet           Y    =        -3392513
75  meter
 Z    =      -16401741
91                 Z    =        -5013743
75
 XDOT =      22071
256133                 XDOT =        6771
804783
 YDOT =     -10454
608585  feet/sec       YDOT =       -3111
087176  meter/sec
 ZDOT =      -6316
851040                 ZDOT =       -1892
586538

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14718336
23                 X    =         4486148
88
 Y    =        -874310
11  feet           Y    =         -266489
72  meter
 Z    =      -16458538
99                 Z    =        -5016562
68
 XDOT =      -5531
024182                 XDOT =       -1685
856171
 YDOT =      22762
549676  feet/sec       YDOT =        6938
025141  meter/sec
 ZDOT =      -6189
029660                 ZDOT =       -1886
416240


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
14112815  
00010596  00000-0  82463-4 0  9089
2 25544  51
6417 346
8965 0009275 176
5066 183
6162 15
71677607 33674


Satellite: ISS
Catalog Number: 25544
Epoch time:      09090
14112815   =   yrday
fracday
Element set:     908
Inclination:       51
6417  deg
RA of node:       346
8965  deg
Eccentricity:     
0009275     
Arg of perigee:   176
5066  deg
Mean anomaly:     183
6162  deg
Mean motion:   15
71677607  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3367
Checksum:              333


Coasting Arc #10 (Orbit 3382)
---------------------------------------

Vector Time (GMT): 2009/091/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5089069
95                 A    =         6736301
27  meter
 Y    =        3702756
06  meter          E    =           
0018810
 Z    =        2368040
07                 I    =           51
54668
 XDOT =      -4655
958208                 Wp   =          134
07616
 YDOT =      -2944
430724  meter/sec      RA   =          341
34588  deg
 ZDOT =      -5388
418561                 TA   =           19
19997
                                          MA   =           19
12918
                                          Ha   =            195
656  n
mi
                                          Hp   =            186
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16696423
72                 X    =        -5141600
10
 Y    =       12148149
79  feet           Y    =         3645553
38  meter
 Z    =        7769160
33                 Z    =         2343189
72
 XDOT =     -15275
453439                 XDOT =       -4596
511001
 YDOT =      -9660
205787  feet/sec       YDOT =       -2996
163932  meter/sec
 ZDOT =     -17678
538585                 ZDOT =       -5410
892904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         460581
88                 X    =          140385
36
 Y    =      -20679231
96  feet           Y    =        -6303029
90  meter
 Z    =        7672365
38                 Z    =         2338536
97
 XDOT =      15365
036269                 XDOT =        4683
263055
 YDOT =      -6266
114558  feet/sec       YDOT =       -1909
911717  meter/sec
 ZDOT =     -17766
473745                 ZDOT =       -5415
221197


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
15844714  
00010596  00000-0  82463-4 0  9092
2 25544  51
6405 341
6898 0009151 179
6931 180
4238 15
71720414 33839


Satellite: ISS
Catalog Number: 25544
Epoch time:      09091
15844714   =   yrday
fracday
Element set:     909
Inclination:       51
6405  deg
RA of node:       341
6898  deg
Eccentricity:     
0009151     
Arg of perigee:   179
6931  deg
Mean anomaly:     180
4238  deg
Mean motion:   15
71720414  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3383
Checksum:              321


Coasting Arc #11 (Orbit 3398)
---------------------------------------

Vector Time (GMT): 2009/092/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4908597
50                 A    =         6730471
02  meter
 Y    =        1595205
38  meter          E    =           
0014911
 Z    =        4319645
99                 I    =           51
49927
 XDOT =      -4682
300843                 Wp   =          144
80322
 YDOT =       5047
202253  meter/sec      RA   =          336
26398  deg
 ZDOT =       3438
933118                 TA   =          270
29162
                                          MA   =          270
46249
                                          Ha   =            195
422  n
mi
                                          Hp   =            186
548

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16104322
51                 X    =         4869410
82
 Y    =        5233613
45  feet           Y    =         1649877
04  meter
 Z    =       14172066
89                 Z    =         4343396
73
 XDOT =     -15361
879407                 XDOT =       -4755
097180
 YDOT =      16559
062511  feet/sec       YDOT =        4994
434983  meter/sec
 ZDOT =      11282
588969                 ZDOT =        3416
009772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13695954
02                 X    =        -4174526
79
 Y    =        9824496
53  feet           Y    =         2994506
54  meter
 Z    =       14264904
65                 Z    =         4347942
94
 XDOT =      -3512
879784                 XDOT =       -1070
725758
 YDOT =     -21234
304190  feet/sec       YDOT =       -6472
215917  meter/sec
 ZDOT =      11193
400117                 ZDOT =        3411
748356


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
17575277  
00010596  00000-0  82463-4 0  9102
2 25544  51
6400 336
4826 0009090 183
4285 176
6816 15
71722742 33996


Satellite: ISS
Catalog Number: 25544
Epoch time:      09092
17575277   =   yrday
fracday
Element set:     910
Inclination:       51
6400  deg
RA of node:       336
4826  deg
Eccentricity:     
0009090     
Arg of perigee:   183
4285  deg
Mean anomaly:     176
6816  deg
Mean motion:   15
71722742  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3399
Checksum:              328


Coasting Arc #12 (Orbit 3413)
---------------------------------------

Vector Time (GMT): 2009/093/02:55:38
824
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2965540
67                 A    =         6733109
08  meter
 Y    =       -4885830
37  meter          E    =           
0010395
 Z    =       -3571832
51                 I    =           51
48266
 XDOT =       6261
288151                 Wp   =          156
63601
 YDOT =        563
273008  meter/sec      RA   =          331
08557  deg
 ZDOT =       4423
011668                 TA   =          160
72749
                                          MA   =          160
68815
                                          Ha   =            195
273  n
mi
                                          Hp   =            186
825

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9729464
12                 X    =         3037305
63
 Y    =      -16029627
21  feet           Y    =        -4852266
73  meter
 Z    =      -11718610
60                 Z    =        -3557251
67
 XDOT =      20542
283959                 XDOT =        6233
038142
 YDOT =       1848
008558  feet/sec       YDOT =         633
132456  meter/sec
 ZDOT =      14511
193138                 ZDOT =        4453
360171

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7429787
10                 X    =         2264599
11
 Y    =       17254957
75  feet           Y    =         5259311
12  meter
 Z    =      -11661987
46                 Z    =        -3554573
78
 XDOT =     -12064
108122                 XDOT =       -3677
140156
 YDOT =      15093
459485  feet/sec       YDOT =        4600
486451  meter/sec
 ZDOT =      14629
731563                 ZDOT =        4459
142181


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
12946297  
00010596  00000-0  82463-4 0  9113
2 25544  51
6410 331
6017 0009015 187
7143 172
3881 15
71753192 34149


Satellite: ISS
Catalog Number: 25544
Epoch time:      09093
12946297   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:       331
6017  deg
Eccentricity:     
0009015     
Arg of perigee:   187
7143  deg
Mean anomaly:     172
3881  deg
Mean motion:   15
71753192  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3414
Checksum:              302

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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