Date: April 2nd 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 20451 43 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 1123)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1754294
47                 A    =         6729397
52  meter
 Y    =        6049098
48  meter          E    =           
0011326
 Z    =       -2365235
86                 I    =           51
31582
 XDOT =      -4377
241116                 Wp   =          128
69434
 YDOT =      -3358
961477  meter/sec      RA   =          268
67369  deg
 ZDOT =      -5368
217381                 TA   =           78
07314
                                          MA   =           77
94617
                                          Ha   =            191
830  n
mi
                                          Hp   =            181
758

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5755559
27                 X    =        -1810316
19
 Y    =       19846123
64  feet           Y    =         6029167
49  meter
 Z    =       -7759960
15                 Z    =        -2373894
87
 XDOT =     -14361
027282                 XDOT =       -4313
277222
 YDOT =     -11020
214818  feet/sec       YDOT =       -3407
553195  meter/sec
 ZDOT =     -17612
261749                 ZDOT =       -5389
326550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2898957
08                 X    =         -883602
12
 Y    =       20446493
82  feet           Y    =         6232091
31  meter
 Z    =       -7794164
87                 Z    =        -2375661
45
 XDOT =     -14158
244642                 XDOT =       -4315
432967
 YDOT =      -8722
941205  feet/sec       YDOT =       -2658
752479  meter/sec
 ZDOT =     -17696
195751                 ZDOT =       -5393
800465


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
52707935  
00016717  00000-0  10270-3 0  9005
2 25544  51
6409 269
2906 0005744 123
6812 236
4899 15
74112285 11249


Satellite: ISS
Catalog Number: 25544
Epoch time:      10090
52707935   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:       269
2906  deg
Eccentricity:     
0005744     
Arg of perigee:   123
6812  deg
Mean anomaly:     236
4899  deg
Mean motion:   15
74112285  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1124
Checksum:              308


Coasting Arc #2 (Orbit 1139)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4056873
76                 A    =         6722310
40  meter
 Y    =        2639735
55  meter          E    =           
0011484
 Z    =        4655192
06                 I    =           51
29353
 XDOT =      -1418
113690                 Wp   =           90
04998
 YDOT =       7056
219030  meter/sec      RA   =          263
47038  deg
 ZDOT =      -2759
546609                 TA   =           27
28756
                                          MA   =           27
22728
                                          Ha   =            191
696  n
mi
                                          Hp   =            181
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13309953
28                 X    =         4004439
95
 Y    =        8660549
71  feet           Y    =         2684809
02  meter
 Z    =       15272939
84                 Z    =         4674773
03
 XDOT =      -4652
603971                 XDOT =       -1483
506690
 YDOT =      23150
324902  feet/sec       YDOT =        7039
995050  meter/sec
 ZDOT =      -9053
630608                 ZDOT =       -2766
595114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14408189
84                 X    =         4391616
26
 Y    =        6494621
99  feet           Y    =         1979560
78  meter
 Z    =       15350785
64                 Z    =         4678919
46
 XDOT =       -461
258551                 XDOT =        -140
591606
 YDOT =      22533
369644  feet/sec       YDOT =        6868
171067  meter/sec
 ZDOT =      -9081
409768                 ZDOT =       -2768
013697


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
54283822  
00016717  00000-0  10270-3 0  9013
2 25544  51
6406 264
0727 0005780 129
0945 231
0733 15
74111235 11407


Satellite: ISS
Catalog Number: 25544
Epoch time:      10091
54283822   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:       264
0727  deg
Eccentricity:     
0005780     
Arg of perigee:   129
0945  deg
Mean anomaly:     231
0733  deg
Mean motion:   15
74111235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1140
Checksum:              274


Coasting Arc #3 (Orbit 1155)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         729433
20                 A    =         6729032
97  meter
 Y    =       -6214904
17  meter          E    =           
0017687
 Z    =        2459814
17                 I    =           51
32174
 XDOT =       4892
292760                 Wp   =           91
27492
 YDOT =       2688
055013  meter/sec      RA   =          258
35239  deg
 ZDOT =       5307
561018                 TA   =          296
67045
                                          MA   =          296
85145
                                          Ha   =            191
675  n
mi
                                          Hp   =            181
812

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2393153
53                 X    =          786925
73
 Y    =      -20390105
55  feet           Y    =        -6206425
68  meter
 Z    =        8070256
47                 Z    =         2463497
64
 XDOT =      16050
829264                 XDOT =        4836
087463
 YDOT =       8819
078126  feet/sec       YDOT =        2742
449455  meter/sec
 ZDOT =      17413
257934                 ZDOT =        5331
191349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1213634
33                 X    =         -369915
74
 Y    =      -20488469
64  feet           Y    =        -6244885
55  meter
 Z    =        8084697
33                 Z    =         2464215
75
 XDOT =      15738
314555                 XDOT =        4797
038276
 YDOT =       6019
003585  feet/sec       YDOT =        1834
592293  meter/sec
 ZDOT =      17507
192625                 ZDOT =        5336
192312


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
55856998  
00016717  00000-0  10270-3 0  9026
2 25544  51
6409 258
8548 0005813 132
9345 227
2307 15
74178780 11565


Satellite: ISS
Catalog Number: 25544
Epoch time:      10092
55856998   =   yrday
fracday
Element set:     902
Inclination:       51
6409  deg
RA of node:       258
8548  deg
Eccentricity:     
0005813     
Arg of perigee:   132
9345  deg
Mean anomaly:     227
2307  deg
Mean motion:   15
74178780  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1156
Checksum:              335


Coasting Arc #4 (Orbit 1170)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4469392
85                 A    =         6722321
07  meter
 Y    =       -2062031
00  meter          E    =           
0016076
 Z    =       -4594297
41                 I    =           51
30773
 XDOT =        284
908533                 Wp   =          119
06403
 YDOT =      -7108
826872  meter/sec      RA   =          253
14853  deg
 ZDOT =       2913
444091                 TA   =          179
98308
                                          MA   =          179
98303
                                          Ha   =            191
609  n
mi
                                          Hp   =            181
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14663362
37                 X    =        -4423684
30
 Y    =       -6765193
58  feet           Y    =        -2111754
91  meter
 Z    =      -15073154
23                 Z    =        -4615898
76
 XDOT =        934
739281                 XDOT =         350
226479
 YDOT =     -23322
922807  feet/sec       YDOT =       -7105
275597  meter/sec
 ZDOT =       9558
543607                 ZDOT =        2914
986954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15593372
33                 X    =        -4752859
89
 Y    =       -3877231
00  feet           Y    =        -1181780
01  meter
 Z    =      -15159018
36                 Z    =        -4620468
80
 XDOT =      -3845
594365                 XDOT =       -1172
137162
 YDOT =     -21928
590402  feet/sec       YDOT =       -6683
834355  meter/sec
 ZDOT =       9564
453770                 ZDOT =        2915
245509


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
51079532  
00016717  00000-0  10270-3 0  9035
2 25544  51
6418 253
9635 0005851 135
7183 224
4449 15
74210294 11711


Satellite: ISS
Catalog Number: 25544
Epoch time:      10093
51079532   =   yrday
fracday
Element set:     903
Inclination:       51
6418  deg
RA of node:       253
9635  deg
Eccentricity:     
0005851     
Arg of perigee:   135
7183  deg
Mean anomaly:     224
4449  deg
Mean motion:   15
74210294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1171
Checksum:              300


Coasting Arc #5 (Orbit 1186)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         205536
13                 A    =         6728349
96  meter
 Y    =        6179091
69  meter          E    =           
0010600
 Z    =       -2650802
20                 I    =           51
33843
 XDOT =      -5303
745866                 Wp   =          132
59784
 YDOT =      -2042
652122  meter/sec      RA   =          248
03339  deg
 ZDOT =      -5192
944863                 TA   =           77
71101
                                          MA   =           77
59235
                                          Ha   =            191
418  n
mi
                                          Hp   =            181
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         674331
13                 X    =          149302
27
 Y    =       20272610
53  feet           Y    =         6181075
68  meter
 Z    =       -8696857
61                 Z    =        -2649940
34
 XDOT =     -17400
741031                 XDOT =       -5255
283966
 YDOT =      -6701
614572  feet/sec       YDOT =       -2101
690838  meter/sec
 ZDOT =     -17037
220678                 ZDOT =       -5218
592751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4898253
60                 X    =         1492987
70
 Y    =       19685107
73  feet           Y    =         6000020
84  meter
 Z    =       -8693240
93                 Z    =        -2649699
84
 XDOT =     -16876
128835                 XDOT =       -5143
844069
 YDOT =      -3340
299179  feet/sec       YDOT =       -1018
123190  meter/sec
 ZDOT =     -17139
166844                 ZDOT =       -5224
018054


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
52647559  
00016717  00000-0  10270-3 0  9048
2 25544  51
6418 248
7457 0005707 138
5593 221
6004 15
74269825 11878


Satellite: ISS
Catalog Number: 25544
Epoch time:      10094
52647559   =   yrday
fracday
Element set:     904
Inclination:       51
6418  deg
RA of node:       248
7457  deg
Eccentricity:     
0005707     
Arg of perigee:   138
5593  deg
Mean anomaly:     221
6004  deg
Mean motion:   15
74269825  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1187
Checksum:              330


Coasting Arc #6 (Orbit 1202)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4784699
09                 A    =         6722583
42  meter
 Y    =        1483433
74  meter          E    =           
0011668
 Z    =        4472599
48                 I    =           51
33115
 XDOT =        769
311185                 Wp   =           95
83286
 YDOT =       6998
346411  meter/sec      RA   =          242
82814  deg
 ZDOT =      -3138
311701                 TA   =           25
62577
                                          MA   =           25
56799
                                          Ha   =            191
273  n
mi
                                          Hp   =            181
916

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15697831
67                 X    =         4746028
44
 Y    =        4866908
58  feet           Y    =         1536722
91  meter
 Z    =       14673882
80                 Z    =         4495749
53
 XDOT =       2523
986829                 XDOT =         706
242555
 YDOT =      22960
454105  feet/sec       YDOT =        7006
596638  meter/sec
 ZDOT =     -10296
298230                 ZDOT =       -3134
727664

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16304008
26                 X    =         4969461
72
 Y    =        1256623
91  feet           Y    =          383018
97  meter
 Z    =       14765898
75                 Z    =         4500645
94
 XDOT =       7740
298802                 XDOT =        2359
243075
 YDOT =      20613
581754  feet/sec       YDOT =        6283
019719  meter/sec
 ZDOT =     -10281
835194                 ZDOT =       -3133
903367


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
54213063  
00016717  00000-0  10270-3 0  9051
2 25544  51
6414 243
5279 0005792 142
9948 217
1616 15
74266160 12033


Satellite: ISS
Catalog Number: 25544
Epoch time:      10095
54213063   =   yrday
fracday
Element set:     905
Inclination:       51
6414  deg
RA of node:       243
5279  deg
Eccentricity:     
0005792     
Arg of perigee:   142
9948  deg
Mean anomaly:     217
1616  deg
Mean motion:   15
74266160  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1203
Checksum:              298


Coasting Arc #7 (Orbit 1218)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1107783
27                 A    =         6727664
80  meter
 Y    =       -5995082
07  meter          E    =           
0016599
 Z    =        2834360
38                 I    =           51
36500
 XDOT =       5644
855256                 Wp   =           99
33876
 YDOT =       1362
451415  meter/sec      RA   =          237
71663  deg
 ZDOT =       5060
190806                 TA   =          293
32415
                                          MA   =          293
49873
                                          Ha   =            191
161  n
mi
                                          Hp   =            181
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3634459
54                 X    =        -1054431
59
 Y    =      -19668904
42  feet           Y    =        -6007171
59  meter
 Z    =        9299082
60                 Z    =         2829108
51
 XDOT =      18519
866324                 XDOT =        5604
619183
 YDOT =       4469
984956  feet/sec       YDOT =        1425
350678  meter/sec
 ZDOT =      16601
675873                 ZDOT =        5087
515599

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8304404
97                 X    =        -2531182
63
 Y    =      -18207231
51  feet           Y    =        -5549564
16  meter
 Z    =        9278017
75                 Z    =         2827939
81
 XDOT =      17628
604266                 XDOT =        5373
198580
 YDOT =        521
347639  feet/sec       YDOT =         158
906760  meter/sec
 ZDOT =      16710
283783                 ZDOT =        5093
294497


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
55775549  
00016717  00000-0  10270-3 0  9066
2 25544  51
6424 238
3101 0005708 147
7601 212
3912 15
74364900 12190


Satellite: ISS
Catalog Number: 25544
Epoch time:      10096
55775549   =   yrday
fracday
Element set:     906
Inclination:       51
6424  deg
RA of node:       238
3101  deg
Eccentricity:     
0005708     
Arg of perigee:   147
7601  deg
Mean anomaly:     212
3912  deg
Mean motion:   15
74364900  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1219
Checksum:              300


Coasting Arc #8 (Orbit 1233)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5065196
42                 A    =         6722836
60  meter
 Y    =        -901772
53  meter          E    =           
0013853
 Z    =       -4341934
41                 I    =           51
36638
 XDOT =      -1714
842059                 Wp   =          125
75178
 YDOT =      -6686
000061  meter/sec      RA   =          232
51159  deg
 ZDOT =       3388
697324                 TA   =          178
59437
                                          MA   =          178
59047
                                          Ha   =            191
051  n
mi
                                          Hp   =            181
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16618098
50                 X    =        -5033643
99
 Y    =       -2958571
31  feet           Y    =         -958238
31  meter
 Z    =      -14245191
64                 Z    =        -4366464
30
 XDOT =      -5626
122240                 XDOT =       -1656
412127
 YDOT =     -21935
695739  feet/sec       YDOT =       -6704
849623  meter/sec
 ZDOT =      11117
773373                 ZDOT =        3380
508847

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16739336
63                 X    =        -5102149
81
 Y    =        1386256
60  feet           Y    =          422531
01  meter
 Z    =      -14342689
03                 Z    =        -4371651
61
 XDOT =     -11032
568223                 XDOT =       -3362
726794
 YDOT =     -18517
565154  feet/sec       YDOT =       -5644
153859  meter/sec
 ZDOT =      11085
007487                 ZDOT =        3378
710282


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
50988180  
00016717  00000-0  10270-3 0  9070
2 25544  51
6427 233
4188 0005551 150
2735 209
8745 15
74368125 12342


Satellite: ISS
Catalog Number: 25544
Epoch time:      10097
50988180   =   yrday
fracday
Element set:     907
Inclination:       51
6427  deg
RA of node:       233
4188  deg
Eccentricity:     
0005551     
Arg of perigee:   150
2735  deg
Mean anomaly:     209
8745  deg
Mean motion:   15
74368125  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1234
Checksum:              316


Coasting Arc #9 (Orbit 1249)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1850900
08                 A    =         6726831
70  meter
 Y    =        5673232
54  meter          E    =           
0009134
 Z    =       -3103248
91                 I    =           51
39959
 XDOT =      -5927
935491                 Wp   =          132
18022
 YDOT =       -715
806216  meter/sec      RA   =          227
40322  deg
 ZDOT =      -4859
418058                 TA   =           84
00166
                                          MA   =           83
89758
                                          Ha   =            190
908  n
mi
                                          Hp   =            182
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6072506
82                 X    =         1802398
34
 Y    =       18612967
65  feet           Y    =         5693659
06  meter
 Z    =      -10181262
84                 Z    =        -3094375
40
 XDOT =     -19448
607253                 XDOT =       -5895
884613
 YDOT =      -2348
445592  feet/sec       YDOT =        -781
916966  meter/sec
 ZDOT =     -15942
972632                 ZDOT =       -4888
137895

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10987214
48                 X    =         3348902
97
 Y    =       16227133
74  feet           Y    =         4946030
36  meter
 Z    =      -10145800
39                 Z    =        -3092439
96
 XDOT =     -18075
936897                 XDOT =       -5509
545566
 YDOT =       2230
714593  feet/sec       YDOT =         679
921808  meter/sec
 ZDOT =     -16057
120974                 ZDOT =       -4894
210473


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
52545567  
00016717  00000-0  10270-3 0  9082
2 25544  51
6428 228
1998 0005513 154
0476 206
0965 15
74414774 12508


Satellite: ISS
Catalog Number: 25544
Epoch time:      10098
52545567   =   yrday
fracday
Element set:     908
Inclination:       51
6428  deg
RA of node:       228
1998  deg
Eccentricity:     
0005513     
Arg of perigee:   154
0476  deg
Mean anomaly:     206
0965  deg
Mean motion:   15
74414774  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1250
Checksum:              324


Coasting Arc #10 (Orbit 1265)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5278110
95                 A    =         6723357
19  meter
 Y    =         326066
41  meter          E    =           
0012278
 Z    =        4140014
19                 I    =           51
41015
 XDOT =       2521
376845                 Wp   =          101
12373
 YDOT =       6273
456031  meter/sec      RA   =          222
19813  deg
 ZDOT =      -3701
684695                 TA   =           26
81575
                                          MA   =           26
75233
                                          Ha   =            190
701  n
mi
                                          Hp   =            182
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17316636
97                 X    =         5253961
18
 Y    =        1069771
67  feet           Y    =          384954
63  meter
 Z    =       13582723
71                 Z    =         4165596
45
 XDOT =       8272
233745                 XDOT =        2469
020579
 YDOT =      20582
204827  feet/sec       YDOT =        6301
358584  meter/sec
 ZDOT =     -12144
634826                 ZDOT =       -3689
563488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16806447
95                 X    =         5122605
34
 Y    =       -3972566
54  feet           Y    =        -1210838
28  meter
 Z    =       13684397
43                 Z    =         4171004
34
 XDOT =      13662
183454                 XDOT =        4164
233517
 YDOT =      16053
795881  feet/sec       YDOT =        4893
196984  meter/sec
 ZDOT =     -12096
235485                 ZDOT =       -3686
932576


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
54100317  
00016717  00000-0  10270-3 0  9096
2 25544  51
6433 222
9818 0005516 156
7821 203
3592 15
74433054 12668


Satellite: ISS
Catalog Number: 25544
Epoch time:      10099
54100317   =   yrday
fracday
Element set:     909
Inclination:       51
6433  deg
RA of node:       222
9818  deg
Eccentricity:     
0005516     
Arg of perigee:   156
7821  deg
Mean anomaly:     203
3592  deg
Mean motion:   15
74433054  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1266
Checksum:              298


Coasting Arc #11 (Orbit 1281)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2506878
67                 A    =         6725780
20  meter
 Y    =       -5254205
30  meter          E    =           
0015202
 Z    =        3361106
45                 I    =           51
44322
 XDOT =       6158
705794                 Wp   =          109
41103
 YDOT =         34
627822  meter/sec      RA   =          217
09461  deg
 ZDOT =       4625
649531                 TA   =          290
33559
                                          MA   =          290
49887
                                          Ha   =            190
571  n
mi
                                          Hp   =            182
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8224667
55                 X    =        -2464266
52
 Y    =      -17238206
35  feet           Y    =        -5282000
19  meter
 Z    =       11027252
14                 Z    =         3349031
95
 XDOT =      20205
727671                 XDOT =        6135
390304
 YDOT =        113
608339  feet/sec       YDOT =         103
368123  meter/sec
 ZDOT =      15176
015523                 ZDOT =        4655
511849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13171187
48                 X    =        -4014577
94
 Y    =      -13870150
78  feet           Y    =        -4227621
96  meter
 Z    =       10979068
37                 Z    =         3346420
04
 XDOT =      18172
563308                 XDOT =        5538
997296
 YDOT =      -5092
857666  feet/sec       YDOT =       -1552
303016  meter/sec
 ZDOT =      15294
693659                 ZDOT =        4661
822627


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
55651999  
00016717  00000-0  10270-3 0  9109
2 25544  51
6443 217
7631 0005388 161
4580 198
6781 15
74536899 12821


Satellite: ISS
Catalog Number: 25544
Epoch time:      10100
55651999   =   yrday
fracday
Element set:     910
Inclination:       51
6443  deg
RA of node:       217
7631  deg
Eccentricity:     
0005388     
Arg of perigee:   161
4580  deg
Mean anomaly:     198
6781  deg
Mean motion:   15
74536899  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1282
Checksum:              334


Coasting Arc #12 (Orbit 1296)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5470589
97                 A    =         6723890
27  meter
 Y    =         266466
10  meter          E    =           
0010569
 Z    =       -3912538
99                 I    =           51
46219
 XDOT =      -3158
854027                 Wp   =          132
12297
 YDOT =      -5742
095923  meter/sec      RA   =          211
89110  deg
 ZDOT =       4025
673654                 TA   =          179
87856
                                          MA   =          179
87830
                                          Ha   =            190
399  n
mi
                                          Hp   =            182
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17948129
83                 X    =        -5454156
59
 Y    =         874232
62  feet           Y    =          205382
28  meter
 Z    =      -12836414
01                 Z    =        -3939075
30
 XDOT =     -10363
694315                 XDOT =       -3113
966162
 YDOT =     -18838
897385  feet/sec       YDOT =       -5777
168801  meter/sec
 ZDOT =      13207
590729                 ZDOT =        4010
437396

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16634497
92                 X    =        -5070194
97
 Y    =        6593534
97  feet           Y    =         2009709
46  meter
 Z    =      -12941868
00                 Z    =        -3944681
37
 XDOT =     -15480
197192                 XDOT =       -4718
364104
 YDOT =     -13249
295654  feet/sec       YDOT =       -4038
385315  meter/sec
 ZDOT =      13146
816529                 ZDOT =        4007
149678


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
50854564  
00016717  00000-0  10270-3 0  9119
2 25544  51
6445 212
8713 0005163 165
0557 195
0760 15
74537004 12978


Satellite: ISS
Catalog Number: 25544
Epoch time:      10101
50854564   =   yrday
fracday
Element set:     911
Inclination:       51
6445  deg
RA of node:       212
8713  deg
Eccentricity:     
0005163     
Arg of perigee:   165
0557  deg
Mean anomaly:     195
0760  deg
Mean motion:   15
74537004  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1297
Checksum:              291


Coasting Arc #13 (Orbit 1312)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2967364
92                 A    =         6724682
05  meter
 Y    =        4781648
95  meter          E    =           
0007753
 Z    =       -3683429
54                 I    =           51
49174
 XDOT =      -6349
462196                 Wp   =          121
41314
 YDOT =        631
704870  meter/sec      RA   =          206
79182  deg
 ZDOT =      -4305
687456                 TA   =          103
00255
                                          MA   =          102
91598
                                          Ha   =            190
296  n
mi
                                          Hp   =            182
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9735449
23                 X    =         2931568
70
 Y    =       15687824
65  feet           Y    =         4814631
35  meter
 Z    =      -12084742
58                 Z    =        -3669101
30
 XDOT =     -20831
568883                 XDOT =       -6335
137710
 YDOT =       2072
522541  feet/sec       YDOT =         560
781153  meter/sec
 ZDOT =     -14126
271182                 ZDOT =       -4336
498631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14542318
27                 X    =         4432498
61
 Y    =       11436144
29  feet           Y    =         3485736
78  meter
 Z    =      -12027609
92                 Z    =        -3666015
50
 XDOT =     -17984
258660                 XDOT =       -5481
602040
 YDOT =       7920
148991  feet/sec       YDOT =        2414
061413  meter/sec
 ZDOT =     -14248
706726                 ZDOT =       -4343
005810


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
52401223  
00016717  00000-0  10270-3 0  9123
2 25544  51
6450 207
6524 0005187 168
5356 191
5927 15
74578038 13134


Satellite: ISS
Catalog Number: 25544
Epoch time:      10102
52401223   =   yrday
fracday
Element set:     912
Inclination:       51
6450  deg
RA of node:       207
6524  deg
Eccentricity:     
0005187     
Arg of perigee:   168
5356  deg
Mean anomaly:     191
5927  deg
Mean motion:   15
74578038  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1313
Checksum:              291


Coasting Arc #14 (Orbit 1328)
---------------------------------------

Vector Time (GMT): 2010/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5604851
72                 A    =         6724677
94  meter
 Y    =        -859592
65  meter          E    =           
0013407
 Z    =        3600263
77                 I    =           51
51979
 XDOT =       3625
332759                 Wp   =          107
88834
 YDOT =       5191
791129  meter/sec      RA   =          201
59107  deg
 ZDOT =      -4394
989798                 TA   =           28
89851
                                          MA   =           28
82434
                                          Ha   =            190
044  n
mi
                                          Hp   =            182
288

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18388621
14                 X    =         5596557
63
 Y    =       -2820185
86  feet           Y    =         -796961
98  meter
 Z    =       11811889
03                 Z    =         3627472
39
 XDOT =      11894
136350                 XDOT =        3588
358102
 YDOT =      17033
435462  feet/sec       YDOT =        5232
124709  meter/sec
 ZDOT =     -14419
257866                 ZDOT =       -4377
467902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16124441
14                 X    =         4914729
66
 Y    =       -9139555
75  feet           Y    =        -2785736
59  meter
 Z    =       11920003
21                 Z    =         3633216
98
 XDOT =      16578
989297                 XDOT =        5053
275938
 YDOT =      10495
176441  feet/sec       YDOT =        3198
929779  meter/sec
 ZDOT =     -14349
412877                 ZDOT =       -4373
701045


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   10103
53945229  
00016717  00000-0  10270-3 0  9135
2 25544  51
6449 202
4341 0005081 170
2820 189
8442 15
74613232 13296


Satellite: ISS
Catalog Number: 25544
Epoch time:      10103
53945229   =   yrday
fracday
Element set:     913
Inclination:       51
6449  deg
RA of node:       202
4341  deg
Eccentricity:     
0005081     
Arg of perigee:   170
2820  deg
Mean anomaly:     189
8442  deg
Mean motion:   15
74613232  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1329
Checksum:              285


Coasting Arc #15 (Orbit 1344)
---------------------------------------

Vector Time (GMT): 2010/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3313673
26                 A    =         6723366
31  meter
 Y    =       -4280441
73  meter          E    =           
0013264
 Z    =        3983344
20                 I    =           51
54456
 XDOT =       6483
607655                 Wp   =          122
78075
 YDOT =      -1340
554870  meter/sec      RA   =          196
49475  deg
 ZDOT =       3936
527614                 TA   =          286
40682
                                          MA   =          286
55258
                                          Ha   =            189
943  n
mi
                                          Hp   =            182
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10871631
42                 X    =        -3284912
98
 Y    =      -14043443
99  feet           Y    =        -4317336
17  meter
 Z    =       13068714
58                 Z    =         3967316
22
 XDOT =      21271
678659                 XDOT =        6478
992859
 YDOT =      -4398
145900  feet/sec       YDOT =       -1268
076899  meter/sec
 ZDOT =      12915
116845                 ZDOT =        3968
014335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15377389
45                 X    =        -4687028
31
 Y    =       -8978418
65  feet           Y    =        -2736622
00  meter
 Z    =       13004840
70                 Z    =         3963875
45
 XDOT =      17395
833853                 XDOT =        5302
250158
 YDOT =     -10826
817389  feet/sec       YDOT =       -3300
013940  meter/sec
 ZDOT =      13040
225414                 ZDOT =        3974
660706


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   10104
55486289  
00016717  00000-0  10270-3 0  9145
2 25544  51
6451 197
2146 0004985 175
4712 184
6497 15
74693389 13454


Satellite: ISS
Catalog Number: 25544
Epoch time:      10104
55486289   =   yrday
fracday
Element set:     914
Inclination:       51
6451  deg
RA of node:       197
2146  deg
Eccentricity:     
0004985     
Arg of perigee:   175
4712  deg
Mean anomaly:     184
6497  deg
Mean motion:   15
74693389  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1345
Checksum:              343

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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