Date: March 30th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 23680 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 1091)
---------------------------------------

Vector Time (GMT): 2010/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2740499
66                 A    =         6729835
67  meter
 Y    =       -5705904
49  meter          E    =           
0018398
 Z    =        2267058
37                 I    =           51
32074
 XDOT =       3763
503846                 Wp   =           85
61603
 YDOT =       3975
304830  meter/sec      RA   =          278
99292  deg
 ZDOT =       5419
516090                 TA   =          299
97314
                                          MA   =          300
15564
                                          Ha   =            192
003  n
mi
                                          Hp   =            181
826

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8991140
61                 X    =         2793087
47
 Y    =      -18720159
10  feet           Y    =        -5674964
30  meter
 Z    =        7437855
56                 Z    =         2280500
12
 XDOT =      12347
453564                 XDOT =        3692
444546
 YDOT =      13042
338682  feet/sec       YDOT =        4016
993891  meter/sec
 ZDOT =      17780
564600                 ZDOT =        5437
626109

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6938066
59                 X    =         2114722
70
 Y    =      -19553869
04  feet           Y    =        -5960019
28  meter
 Z    =        7491067
93                 Z    =         2283277
51
 XDOT =      12115
015988                 XDOT =        3692
656873
 YDOT =      11183
339239  feet/sec       YDOT =        3408
681800  meter/sec
 ZDOT =      17852
604160                 ZDOT =        5441
473748


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   10088
55896497  
00016717  00000-0  10270-3 0  9007
2 25544  51
6409 279
3986 0005751 119
8697 240
3039 15
74028235 10920


Satellite: ISS
Catalog Number: 25544
Epoch time:      10088
55896497   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:       279
3986  deg
Eccentricity:     
0005751     
Arg of perigee:   119
8697  deg
Mean anomaly:     240
3039  deg
Mean motion:   15
74028235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1092
Checksum:              341


Coasting Arc #2 (Orbit 1106)
---------------------------------------

Vector Time (GMT): 2010/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3576991
66                 A    =         6722278
55  meter
 Y    =       -3207193
81  meter          E    =           
0017083
 Z    =       -4718306
65                 I    =           51
29162
 XDOT =       2567
862825                 Wp   =          113
37217
 YDOT =      -6747
357784  meter/sec      RA   =          273
79088  deg
 ZDOT =       2640
585914                 TA   =          182
73961
                                          MA   =          182
74898
                                          Ha   =            191
983  n
mi
                                          Hp   =            181
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11735536
95                 X    =        -3517941
60
 Y    =      -10522289
39  feet           Y    =        -3246864
18  meter
 Z    =      -15480008
70                 Z    =        -4735539
99
 XDOT =       8424
746801                 XDOT =        2630
294581
 YDOT =     -22137
000604  feet/sec       YDOT =       -6718
293063  meter/sec
 ZDOT =       8663
339614                 ZDOT =        2653
213008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12839132
89                 X    =        -3913367
70
 Y    =       -9026156
07  feet           Y    =        -2751172
37  meter
 Z    =      -15548544
76                 Z    =        -4739196
44
 XDOT =       4957
027601                 XDOT =        1510
902013
 YDOT =     -22055
592591  feet/sec       YDOT =       -6722
544622  meter/sec
 ZDOT =       8713
282187                 ZDOT =        2655
808411


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   10089
51128724  
00016717  00000-0  10270-3 0  9016
2 25544  51
6405 274
5064 0005838 122
6387 237
5341 15
74057197 11074


Satellite: ISS
Catalog Number: 25544
Epoch time:      10089
51128724   =   yrday
fracday
Element set:     901
Inclination:       51
6405  deg
RA of node:       274
5064  deg
Eccentricity:     
0005838     
Arg of perigee:   122
6387  deg
Mean anomaly:     237
5341  deg
Mean motion:   15
74057197  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1107
Checksum:              304


Coasting Arc #3 (Orbit 1122)
---------------------------------------

Vector Time (GMT): 2010/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1758396
10                 A    =         6729364
63  meter
 Y    =        6045772
81  meter          E    =           
0011310
 Z    =       -2370420
50                 I    =           51
31573
 XDOT =      -4375
134803                 Wp   =          129
24614
 YDOT =      -3366
638493  meter/sec      RA   =          268
67241  deg
 ZDOT =      -5365
251561                 TA   =           77
58515
                                          MA   =           77
45860
                                          Ha   =            191
801  n
mi
                                          Hp   =            181
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5769016
08                 X    =        -1814355
15
 Y    =       19835212
65  feet           Y    =         6025796
30  meter
 Z    =       -7776970
15                 Z    =        -2379099
29
 XDOT =     -14354
116808                 XDOT =       -4311
099628
 YDOT =     -11045
401879  feet/sec       YDOT =       -3415
206258  meter/sec
 ZDOT =     -17602
531367                 ZDOT =       -5386
350323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2913699
20                 X    =         -888095
52
 Y    =       20437542
61  feet           Y    =         6229362
99  meter
 Z    =       -7811253
49                 Z    =        -2380870
06
 XDOT =     -14155
607754                 XDOT =       -4314
629244
 YDOT =      -8747
760587  feet/sec       YDOT =       -2666
317427  meter/sec
 ZDOT =     -17686
424276                 ZDOT =       -5390
822119


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   10090
52706773  
00016717  00000-0  10270-3 0  9026
2 25544  51
6408 269
2893 0005731 124
8978 235
2724 15
74120054 11231


Satellite: ISS
Catalog Number: 25544
Epoch time:      10090
52706773   =   yrday
fracday
Element set:     902
Inclination:       51
6408  deg
RA of node:       269
2893  deg
Eccentricity:     
0005731     
Arg of perigee:   124
8978  deg
Mean anomaly:     235
2724  deg
Mean motion:   15
74120054  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1123
Checksum:              301


Coasting Arc #4 (Orbit 1138)
---------------------------------------

Vector Time (GMT): 2010/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4054715
74                 A    =         6722287
97  meter
 Y    =        2650627
85  meter          E    =           
0011422
 Z    =        4650873
71                 I    =           51
29354
 XDOT =      -1426
306652                 Wp   =           90
47032
 YDOT =       7050
794769  meter/sec      RA   =          263
46893  deg
 ZDOT =      -2769
152311                 TA   =           26
96979
                                          MA   =           26
91047
                                          Ha   =            191
655  n
mi
                                          Hp   =            181
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13302873
15                 X    =         4002181
26
 Y    =        8696285
59  feet           Y    =         2695676
62  meter
 Z    =       15258772
03                 Z    =         4670443
95
 XDOT =      -4679
483766                 XDOT =       -1491
591724
 YDOT =      23132
528769  feet/sec       YDOT =        7034
479773  meter/sec
 ZDOT =      -9085
145378                 ZDOT =       -2776
240355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14406848
47                 X    =         4391207
41
 Y    =        6531011
31  feet           Y    =         1990652
25  meter
 Z    =       15336575
55                 Z    =         4674588
23
 XDOT =       -487
746499                 XDOT =        -148
665133
 YDOT =      22520
048580  feet/sec       YDOT =        6864
110807  meter/sec
 ZDOT =      -9113
081731                 ZDOT =       -2777
667312


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   10091
54281939  
00016717  00000-0  10270-3 0  9032
2 25544  51
6405 264
0713 0005762 130
2979 229
8688 15
74125309 11391


Satellite: ISS
Catalog Number: 25544
Epoch time:      10091
54281939   =   yrday
fracday
Element set:     903
Inclination:       51
6405  deg
RA of node:       264
0713  deg
Eccentricity:     
0005762     
Arg of perigee:   130
2979  deg
Mean anomaly:     229
8688  deg
Mean motion:   15
74125309  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1139
Checksum:              317


Coasting Arc #5 (Orbit 1154)
---------------------------------------

Vector Time (GMT): 2010/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         741676
63                 A    =         6728945
66  meter
 Y    =       -6208101
19  meter          E    =           
0017592
 Z    =        2473252
72                 I    =           51
32158
 XDOT =       4889
890905                 Wp   =           91
67357
 YDOT =       2708
522495  meter/sec      RA   =          258
35093  deg
 ZDOT =       5299
316007                 TA   =          296
43811
                                          MA   =          296
61851
                                          Ha   =            191
621  n
mi
                                          Hp   =            181
811

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2433322
28                 X    =          799026
89
 Y    =      -20367786
06  feet           Y    =        -6199486
58  meter
 Z    =        8114346
19                 Z    =         2476995
32
 XDOT =      16042
949162                 XDOT =        4833
496968
 YDOT =       8886
228658  feet/sec       YDOT =        2762
889023  meter/sec
 ZDOT =      17386
207373                 ZDOT =        5322
934211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1170468
64                 X    =         -356758
84
 Y    =      -20473382
30  feet           Y    =        -6240286
92  meter
 Z    =        8129022
12                 Z    =         2477725
94
 XDOT =      15743
415558                 XDOT =        4798
593062
 YDOT =       6083
329659  feet/sec       YDOT =        1854
198880  meter/sec
 ZDOT =      17480
094521                 ZDOT =        5327
932810


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   10092
55853980  
00016717  00000-0  10270-3 0  9046
2 25544  51
6408 258
8533 0005788 134
1187 226
0453 15
74199228 11555


Satellite: ISS
Catalog Number: 25544
Epoch time:      10092
55853980   =   yrday
fracday
Element set:     904
Inclination:       51
6408  deg
RA of node:       258
8533  deg
Eccentricity:     
0005788     
Arg of perigee:   134
1187  deg
Mean anomaly:     226
0453  deg
Mean motion:   15
74199228  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1155
Checksum:              325


Coasting Arc #6 (Orbit 1169)
---------------------------------------

Vector Time (GMT): 2010/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4468234
98                 A    =         6722289
33  meter
 Y    =       -2089133
01  meter          E    =           
0015943
 Z    =       -4582987
70                 I    =           51
30783
 XDOT =        307
024687                 Wp   =          119
52511
 YDOT =      -7098
567720  meter/sec      RA   =          253
14668  deg
 ZDOT =       2936
439611                 TA   =          179
77325
                                          MA   =          179
77253
                                          Ha   =            191
541  n
mi
                                          Hp   =            181
682

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14659563
59                 X    =        -4422278
40
 Y    =       -6854110
94  feet           Y    =        -2138842
59  meter
 Z    =      -15036048
88                 Z    =        -4604582
82
 XDOT =       1007
298843                 XDOT =         372
114562
 YDOT =     -23289
264173  feet/sec       YDOT =       -7094
770404  meter/sec
 ZDOT =       9633
988225                 ZDOT =        2938
089360

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15606728
52                 X    =        -4756930
85
 Y    =       -3965211
48  feet           Y    =        -1208596
46  meter
 Z    =      -15121889
10                 Z    =        -4609151
80
 XDOT =      -3774
818827                 XDOT =       -1150
564779
 YDOT =     -21908
250820  feet/sec       YDOT =       -6677
634850  meter/sec
 ZDOT =       9640
323255                 ZDOT =        2938
370528


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   10093
51075071  
00016717  00000-0  10270-3 0  9051
2 25544  51
6417 253
9619 0005817 136
8725 223
2895 15
74237173 11704


Satellite: ISS
Catalog Number: 25544
Epoch time:      10093
51075071   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:       253
9619  deg
Eccentricity:     
0005817     
Arg of perigee:   136
8725  deg
Mean anomaly:     223
2895  deg
Mean motion:   15
74237173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1170
Checksum:              309


Coasting Arc #7 (Orbit 1185)
---------------------------------------

Vector Time (GMT): 2010/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         176766
36                 A    =         6728189
92  meter
 Y    =        6167677
24  meter          E    =           
0010476
 Z    =       -2679015
83                 I    =           51
33817
 XDOT =      -5305
264116                 Wp   =          132
73589
 YDOT =      -2086
707148  meter/sec      RA   =          248
03159  deg
 ZDOT =      -5173
903716                 TA   =           77
93080
                                          MA   =           77
81343
                                          Ha   =            191
336  n
mi
                                          Hp   =            181
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         579942
11                 X    =          120799
33
 Y    =       20235161
56  feet           Y    =         6169341
00  meter
 Z    =       -8789422
01                 Z    =        -2678293
09
 XDOT =     -17405
722164                 XDOT =       -5256
401970
 YDOT =      -6846
152059  feet/sec       YDOT =       -2145
760604  meter/sec
 ZDOT =     -16974
749724                 ZDOT =       -5199
558008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4798698
04                 X    =         1462643
16
 Y    =       19667852
96  feet           Y    =         5994761
58  meter
 Z    =       -8786358
31                 Z    =        -2678082
01
 XDOT =     -16912
482407                 XDOT =       -5154
924638
 YDOT =      -3473
351852  feet/sec       YDOT =       -1058
677644  meter/sec
 ZDOT =     -17076
722705                 ZDOT =       -5204
985080


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   10094
52641150  
00016717  00000-0  10270-3 0  9061
2 25544  51
6417 248
7440 0005664 139
7317 220
4267 15
74302928 11867


Satellite: ISS
Catalog Number: 25544
Epoch time:      10094
52641150   =   yrday
fracday
Element set:     906
Inclination:       51
6417  deg
RA of node:       248
7440  deg
Eccentricity:     
0005664     
Arg of perigee:   139
7317  deg
Mean anomaly:     220
4267  deg
Mean motion:   15
74302928  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1186
Checksum:              302


Coasting Arc #8 (Orbit 1201)
---------------------------------------

Vector Time (GMT): 2010/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4790278
80                 A    =         6722561
10  meter
 Y    =        1535438
96  meter          E    =           
0011689
 Z    =        4448977
18                 I    =           51
33141
 XDOT =        722
542041                 Wp   =           96
13630
 YDOT =       6983
506349  meter/sec      RA   =          242
82569  deg
 ZDOT =      -3182
215580                 TA   =           25
81352
                                          MA   =           25
75523
                                          Ha   =            191
176  n
mi
                                          Hp   =            181
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15716137
79                 X    =         4751140
95
 Y    =        5037529
40  feet           Y    =         1588787
92  meter
 Z    =       14596381
83                 Z    =         4472153
21
 XDOT =       2370
544753                 XDOT =         659
856107
 YDOT =      22911
766236  feet/sec       YDOT =        6991
235715  meter/sec
 ZDOT =     -10440
339830                 ZDOT =       -3178
857817

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16360413
27                 X    =         4986653
97
 Y    =        1418738
97  feet           Y    =          432431
64  meter
 Z    =       14688502
62                 Z    =         4477055
60
 XDOT =       7592
507486                 XDOT =        2314
196282
 YDOT =      20596
097698  feet/sec       YDOT =        6277
690578  meter/sec
 ZDOT =     -10426
776187                 ZDOT =       -3178
081382


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   10095
54204275  
00016717  00000-0  10270-3 0  9078
2 25544  51
6413 243
5260 0005741 144
1544 216
0005 15
74306443 12020


Satellite: ISS
Catalog Number: 25544
Epoch time:      10095
54204275   =   yrday
fracday
Element set:     907
Inclination:       51
6413  deg
RA of node:       243
5260  deg
Eccentricity:     
0005741     
Arg of perigee:   144
1544  deg
Mean anomaly:     216
0005  deg
Mean motion:   15
74306443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1202
Checksum:              262


Coasting Arc #9 (Orbit 1217)
---------------------------------------

Vector Time (GMT): 2010/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1052217
55                 A    =         6727408
81  meter
 Y    =       -5981153
38  meter          E    =           
0016472
 Z    =        2884064
27                 I    =           51
36452
 XDOT =       5658
883996                 Wp   =          100
14306
 YDOT =       1439
685497  meter/sec      RA   =          237
71428  deg
 ZDOT =       5023
116439                 TA   =          293
16766
                                          MA   =          293
34110
                                          Ha   =            191
052  n
mi
                                          Hp   =            181
885

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3452157
31                 X    =         -999267
20
 Y    =      -19623206
61  feet           Y    =        -5992623
78  meter
 Z    =        9462153
10                 Z    =         2879081
36
 XDOT =      18565
892375                 XDOT =        5617
963335
 YDOT =       4723
377616  feet/sec       YDOT =        1502
737810  meter/sec
 ZDOT =      16480
040812                 ZDOT =        5050
507719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8117397
16                 X    =        -2474182
66
 Y    =      -18206413
65  feet           Y    =        -5549314
88  meter
 Z    =        9442157
30                 Z    =         2877969
55
 XDOT =      17734
886222                 XDOT =        5405
593320
 YDOT =        742
461472  feet/sec       YDOT =         226
302257  meter/sec
 ZDOT =      16588
915443                 ZDOT =        5056
301427


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   10096
55763955  
00016717  00000-0  10270-3 0  9086
2 25544  51
6424 238
3081 0005650 148
9162 211
2337 15
74411112 12184


Satellite: ISS
Catalog Number: 25544
Epoch time:      10096
55763955   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:       238
3081  deg
Eccentricity:     
0005650     
Arg of perigee:   148
9162  deg
Mean anomaly:     211
2337  deg
Mean motion:   15
74411112  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1218
Checksum:              294


Coasting Arc #10 (Orbit 1232)
---------------------------------------

Vector Time (GMT): 2010/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5086145
40                 A    =         6722848
48  meter
 Y    =        -985665
80  meter          E    =           
0013505
 Z    =       -4298652
38                 I    =           51
36688
 XDOT =      -1631
777926                 Wp   =          126
29837
 YDOT =      -6670
585305  meter/sec      RA   =          232
50833  deg
 ZDOT =       3459
933289                 TA   =          178
87279
                                          MA   =          178
86975
                                          Ha   =            190
929  n
mi
                                          Hp   =            181
847

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16686828
73                 X    =        -5053863
56
 Y    =       -3233811
67  feet           Y    =        -1042361
76  meter
 Z    =      -14103190
21                 Z    =        -4323282
25
 XDOT =      -5353
602118                 XDOT =       -1573
872587
 YDOT =     -21885
122391  feet/sec       YDOT =       -6688
508924  meter/sec
 ZDOT =      11351
487169                 ZDOT =        3452
147060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16877249
95                 X    =        -5144185
79
 Y    =        1138114
47  feet           Y    =          346897
29  meter
 Z    =      -14201087
80                 Z    =        -4328491
56
 XDOT =     -10775
627415                 XDOT =       -3284
411236
 YDOT =     -18528
254598  feet/sec       YDOT =       -5647
412001  meter/sec
 ZDOT =      11320
320090                 ZDOT =        3450
433563


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   10097
50973555  
00016717  00000-0  10270-3 0  9092
2 25544  51
6426 233
4165 0005483 151
4273 208
7192 15
74420808 12330


Satellite: ISS
Catalog Number: 25544
Epoch time:      10097
50973555   =   yrday
fracday
Element set:     909
Inclination:       51
6426  deg
RA of node:       233
4165  deg
Eccentricity:     
0005483     
Arg of perigee:   151
4273  deg
Mean anomaly:     208
7192  deg
Mean motion:   15
74420808  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1233
Checksum:              306


Coasting Arc #11 (Orbit 1248)
---------------------------------------

Vector Time (GMT): 2010/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1757919
53                 A    =         6726455
70  meter
 Y    =        5660852
83  meter          E    =           
0008903
 Z    =       -3178774
95                 I    =           51
39886
 XDOT =      -5965
135033                 Wp   =          130
76002
 YDOT =       -831
929175  meter/sec      RA   =          227
40010  deg
 ZDOT =      -4794
823175                 TA   =           86
44967
                                          MA   =           86
34785
                                          Ha   =            190
771  n
mi
                                          Hp   =            182
022

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5767452
54                 X    =         1709930
03
 Y    =       18572351
81  feet           Y    =         5680242
45  meter
 Z    =      -10429051
69                 Z    =        -3170351
90
 XDOT =     -19570
652997                 XDOT =       -5932
096671
 YDOT =      -2729
426427  feet/sec       YDOT =        -898
450387  meter/sec
 ZDOT =     -15731
047163                 ZDOT =       -4823
721322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10684084
15                 X    =         3256508
85
 Y    =       16271057
38  feet           Y    =         4959418
29  meter
 Z    =      -10395379
62                 Z    =        -3168511
71
 XDOT =     -18295
482424                 XDOT =       -5576
463043
 YDOT =       1920
063688  feet/sec       YDOT =         585
235412  meter/sec
 ZDOT =     -15845
908189                 ZDOT =       -4829
832816


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   10098
52527287  
00016717  00000-0  10270-3 0  9104
2 25544  51
6427 228
1973 0005438 155
2453 204
8972 15
74474089 12491


Satellite: ISS
Catalog Number: 25544
Epoch time:      10098
52527287   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:       228
1973  deg
Eccentricity:     
0005438     
Arg of perigee:   155
2453  deg
Mean anomaly:     204
8972  deg
Mean motion:   15
74474089  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1249
Checksum:              329


Coasting Arc #12 (Orbit 1264)
---------------------------------------

Vector Time (GMT): 2010/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5325061
67                 A    =         6723424
20  meter
 Y    =         445853
14  meter          E    =           
0012499
 Z    =        4068061
92                 I    =           51
41097
 XDOT =       2388
213553                 Wp   =          101
73236
 YDOT =       6263
633289  meter/sec      RA   =          222
19396  deg
 ZDOT =      -3805
309130                 TA   =           27
46735
                                          MA   =           27
40135
                                          Ha   =            190
551  n
mi
                                          Hp   =            182
039

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17470674
76                 X    =         5299918
46
 Y    =        1462772
78  feet           Y    =          505260
84  meter
 Z    =       13346659
85                 Z    =         4093869
85
 XDOT =       7835
346302                 XDOT =        2336
480410
 YDOT =      20549
977983  feet/sec       YDOT =        6290
050208  meter/sec
 ZDOT =     -12484
610005                 ZDOT =       -3793
833313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17069125
52                 X    =         5202669
46
 Y    =       -3641503
61  feet           Y    =        -1109930
30  meter
 Z    =       13449234
75                 Z    =         4099326
75
 XDOT =      13260
775766                 XDOT =        4041
884454
 YDOT =      16129
858764  feet/sec       YDOT =        4916
380951  meter/sec
 ZDOT =     -12438
775744                 ZDOT =       -3791
338847


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   10099
54077936  
00016717  00000-0  10270-3 0  9119
2 25544  51
6433 222
9790 0005434 157
9884 202
1514 15
74500405 12653


Satellite: ISS
Catalog Number: 25544
Epoch time:      10099
54077936   =   yrday
fracday
Element set:     911
Inclination:       51
6433  deg
RA of node:       222
9790  deg
Eccentricity:     
0005434     
Arg of perigee:   157
9884  deg
Mean anomaly:     202
1514  deg
Mean motion:   15
74500405  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1265
Checksum:              306


Coasting Arc #13 (Orbit 1280)
---------------------------------------

Vector Time (GMT): 2010/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2364420
02                 A    =         6725255
52  meter
 Y    =       -5251318
91  meter          E    =           
0014979
 Z    =        3466346
81                 I    =           51
44213
 XDOT =       6232
318418                 Wp   =          111
18785
 YDOT =        192
891827  meter/sec      RA   =          217
09039  deg
 ZDOT =       4522
324892                 TA   =          290
07130
                                          MA   =          290
23246
                                          Ha   =            190
406  n
mi
                                          Hp   =            182
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7757283
53                 X    =        -2322361
97
 Y    =      -17228736
58  feet           Y    =        -5277523
84  meter
 Z    =       11372528
90                 Z    =         3454963
03
 XDOT =      20447
238904                 XDOT =        6207
729652
 YDOT =        632
847201  feet/sec       YDOT =         262
448181  meter/sec
 ZDOT =      14837
023923                 ZDOT =        4552
541714

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12725309
50                 X    =        -3878674
34
 Y    =      -14003669
17  feet           Y    =        -4268318
36  meter
 Z    =       11327090
24                 Z    =         3452497
11
 XDOT =      18553
672012                 XDOT =        5655
159229
 YDOT =      -4705
688307  feet/sec       YDOT =       -1434
293796  meter/sec
 ZDOT =      14957
116882                 ZDOT =        4558
929226


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   10100
55625082  
00016717  00000-0  10270-3 0  9125
2 25544  51
6442 217
7599 0005297 162
6774 197
4571 15
74610677 12810


Satellite: ISS
Catalog Number: 25544
Epoch time:      10100
55625082   =   yrday
fracday
Element set:     912
Inclination:       51
6442  deg
RA of node:       217
7599  deg
Eccentricity:     
0005297     
Arg of perigee:   162
6774  deg
Mean anomaly:     197
4571  deg
Mean motion:   15
74610677  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1281
Checksum:              319


Coasting Arc #14 (Orbit 1295)
---------------------------------------

Vector Time (GMT): 2010/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5553668
34                 A    =         6724045
02  meter
 Y    =         110344
80  meter          E    =           
0009860
 Z    =       -3800861
74                 I    =           51
46342
 XDOT =      -2963
309118                 Wp   =          132
27337
 YDOT =      -5748
794395  meter/sec      RA   =          211
88591  deg
 ZDOT =       4163
328148                 TA   =          181
51191
                                          MA   =          181
51489
                                          Ha   =            190
223  n
mi
                                          Hp   =            182
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18220696
65                 X    =        -5536025
52
 Y    =         362023
63  feet           Y    =           48338
72  meter
 Z    =      -12470018
83                 Z    =        -3827798
69
 XDOT =      -9722
142776                 XDOT =       -2919
029586
 YDOT =     -18860
874000  feet/sec       YDOT =       -5781
683964  meter/sec
 ZDOT =      13659
213084                 ZDOT =        4149
040373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17059782
83                 X    =        -5199821
81
 Y    =        6197363
13  feet           Y    =         1888956
28  meter
 Z    =      -12577071
10                 Z    =        -3833491
27
 XDOT =     -14911
458541                 XDOT =       -4545
012563
 YDOT =     -13445
204835  feet/sec       YDOT =       -4098
098434  meter/sec
 ZDOT =      13602
208209                 ZDOT =        4145
953062


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   10101
50822989  
00016717  00000-0  10270-3 0  9137
2 25544  51
6444 212
8678 0005055 166
3098 193
8203 15
74614011 12962


Satellite: ISS
Catalog Number: 25544
Epoch time:      10101
50822989   =   yrday
fracday
Element set:     913
Inclination:       51
6444  deg
RA of node:       212
8678  deg
Eccentricity:     
0005055     
Arg of perigee:   166
3098  deg
Mean anomaly:     193
8203  deg
Mean motion:   15
74614011  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1296
Checksum:              303


Coasting Arc #15 (Orbit 1311)
---------------------------------------

Vector Time (GMT): 2010/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2763840
41                 A    =         6723998
32  meter
 Y    =        4798188
47  meter          E    =           
0007744
 Z    =       -3817653
25                 I    =           51
49023
 XDOT =      -6468
854131                 Wp   =          116
63776
 YDOT =        432
747989  meter/sec      RA   =          206
78613  deg
 ZDOT =      -4149
196177                 TA   =          109
86324
                                          MA   =          109
77976
                                          Ha   =            190
104  n
mi
                                          Hp   =            182
246

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9067717
88                 X    =         2728526
40
 Y    =       15742088
15  feet           Y    =         4828897
62  meter
 Z    =      -12525109
08                 Z    =        -3804312
57
 XDOT =     -21223
274708                 XDOT =       -6453
056213
 YDOT =       1419
776867  feet/sec       YDOT =         360
497411  meter/sec
 ZDOT =     -13612
848350                 ZDOT =       -4180
583767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13934930
75                 X    =         4247366
89
 Y    =       11712582
90  feet           Y    =         3569995
27  meter
 Z    =      -12471900
87                 Z    =        -3801435
38
 XDOT =     -18556
662469                 XDOT =       -5656
070721
 YDOT =       7484
090821  feet/sec       YDOT =        2281
150882  meter/sec
 ZDOT =     -13737
582568                 ZDOT =       -4187
215167


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   10102
52364249  
00016717  00000-0  10270-3 0  9141
2 25544  51
6449 207
6485 0005083 169
8128 190
3140 15
74663860 13125


Satellite: ISS
Catalog Number: 25544
Epoch time:      10102
52364249   =   yrday
fracday
Element set:     914
Inclination:       51
6449  deg
RA of node:       207
6485  deg
Eccentricity:     
0005083     
Arg of perigee:   169
8128  deg
Mean anomaly:     190
3140  deg
Mean motion:   15
74663860  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1312
Checksum:              300

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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