Date: March 26th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19568 79 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 1014)
---------------------------------------

Vector Time (GMT): 2010/083/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5142191
25                 A    =         6727512
93  meter
 Y    =       -2608544
33  meter          E    =           
0018156
 Z    =        3451726
33                 I    =           51
36911
 XDOT =        106
612086                 Wp   =           94
39772
 YDOT =       6232
885940  meter/sec      RA   =          304
52030  deg
 ZDOT =       4529
690867                 TA   =          306
71238
                                          MA   =          306
87902
                                          Ha   =            192
467  n
mi
                                          Hp   =            181
966

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16870706
18                 X    =         5154210
60
 Y    =       -8558216
31  feet           Y    =        -2550973
97  meter
 Z    =       11324561
44                 Z    =         3476736
08
 XDOT =        349
777185                 XDOT =          14
902750
 YDOT =      20449
100853  feet/sec       YDOT =        6233
565515  meter/sec
 ZDOT =      14861
190510                 ZDOT =        4529
985818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13050390
51                 X    =         3977759
03
 Y    =      -13612238
54  feet           Y    =        -4149010
31  meter
 Z    =       11423824
01                 Z    =         3481981
56
 XDOT =       5986
328513                 XDOT =        1824
632931
 YDOT =      18271
860287  feet/sec       YDOT =        5569
263015  meter/sec
 ZDOT =      14862
503176                 ZDOT =        4530
090968


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   10083
60645148  
00016717  00000-0  10270-3 0  9003
2 25544  51
6438 304
8250 0005871 100
7471 259
4354 15
73785969 10151


Satellite: ISS
Catalog Number: 25544
Epoch time:      10083
60645148   =   yrday
fracday
Element set:     900
Inclination:       51
6438  deg
RA of node:       304
8250  deg
Eccentricity:     
0005871     
Arg of perigee:   100
7471  deg
Mean anomaly:     259
4354  deg
Mean motion:   15
73785969  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1015
Checksum:              308


Coasting Arc #2 (Orbit 1029)
---------------------------------------

Vector Time (GMT): 2010/084/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -630846
88                 A    =         6725785
35  meter
 Y    =       -5389799
23  meter          E    =           
0013044
 Z    =       -3986960
36                 I    =           51
34636
 XDOT =       5585
234508                 Wp   =          106
36964
 YDOT =      -3546
709879  meter/sec      RA   =          299
31369  deg
 ZDOT =       3917
892154                 TA   =          204
32706
                                          MA   =          204
38869
                                          Ha   =            192
518  n
mi
                                          Hp   =            181
902

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2069707
61                 X    =         -551162
63
 Y    =      -17683068
34  feet           Y    =        -5396408
41  meter
 Z    =      -13080578
60                 Z    =        -3989831
13
 XDOT =      18324
260196                 XDOT =        5605
447200
 YDOT =     -11636
187267  feet/sec       YDOT =       -3484
139243  meter/sec
 ZDOT =      12853
976883                 ZDOT =        3945
074122

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7977202
42                 X    =        -2431451
30
 Y    =      -15907137
55  feet           Y    =        -4848495
52  meter
 Z    =      -13092110
16                 Z    =        -3990475
18
 XDOT =      11946
999779                 XDOT =        3641
445533
 YDOT =     -16640
434673  feet/sec       YDOT =       -5072
004488  meter/sec
 ZDOT =      12961
842406                 ZDOT =        3950
769565


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   10084
55891704  
00016717  00000-0  10270-3 0  9010
2 25544  51
6428 299
9345 0005976 104
8516 255
3310 15
73817647 10303


Satellite: ISS
Catalog Number: 25544
Epoch time:      10084
55891704   =   yrday
fracday
Element set:     901
Inclination:       51
6428  deg
RA of node:       299
9345  deg
Eccentricity:     
0005976     
Arg of perigee:   104
8516  deg
Mean anomaly:     255
3310  deg
Mean motion:   15
73817647  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1030
Checksum:              317


Coasting Arc #3 (Orbit 1045)
---------------------------------------

Vector Time (GMT): 2010/085/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4591098
72                 A    =         6727421
50  meter
 Y    =        3542679
33  meter          E    =           
0010818
 Z    =       -3417856
43                 I    =           51
33801
 XDOT =      -1283
385947                 Wp   =           98
23027
 YDOT =      -6056
053053  meter/sec      RA   =          294
21018  deg
 ZDOT =      -4567
150040                 TA   =          122
33122
                                          MA   =          122
22643
                                          Ha   =            192
409  n
mi
                                          Hp   =            181
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15062659
84                 X    =        -4613769
28
 Y    =       11622963
69  feet           Y    =         3491211
91  meter
 Z    =      -11213439
72                 Z    =        -3440215
01
 XDOT =      -4210
583814                 XDOT =       -1193
384621
 YDOT =     -19868
940461  feet/sec       YDOT =       -6069
901773  meter/sec
 ZDOT =     -14984
088058                 ZDOT =       -4573
165551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9781509
75                 X    =        -2981404
17
 Y    =       16257362
17  feet           Y    =         4955243
99  meter
 Z    =      -11302144
89                 Z    =        -3444893
76
 XDOT =      -9839
894221                 XDOT =       -2999
199758
 YDOT =     -16322
657627  feet/sec       YDOT =       -4975
146045  meter/sec
 ZDOT =     -15008
135471                 ZDOT =       -4574
479691


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   10085
57485754  
00016717  00000-0  10270-3 0  9028
2 25544  51
6421 294
7190 0005974 107
7942 252
3873 15
73858407 10467


Satellite: ISS
Catalog Number: 25544
Epoch time:      10085
57485754   =   yrday
fracday
Element set:     902
Inclination:       51
6421  deg
RA of node:       294
7190  deg
Eccentricity:     
0005974     
Arg of perigee:   107
7942  deg
Mean anomaly:     252
3873  deg
Mean motion:   15
73858407  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1046
Checksum:              329


Coasting Arc #4 (Orbit 1061)
---------------------------------------

Vector Time (GMT): 2010/086/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1611376
63                 A    =         6725503
19  meter
 Y    =        5151673
57  meter          E    =           
0015979
 Z    =        3998282
09                 I    =           51
32025
 XDOT =      -4858
580002                 Wp   =           89
76378
 YDOT =       4548
060902  meter/sec      RA   =          289
00134  deg
 ZDOT =      -3888
519782                 TA   =           40
55428
                                          MA   =           40
43534
                                          Ha   =            192
273  n
mi
                                          Hp   =            181
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5286668
75                 X    =         1534227
23
 Y    =       16901816
18  feet           Y    =         5169261
99  meter
 Z    =       13117723
38                 Z    =         4005922
14
 XDOT =     -15940
223103                 XDOT =       -4890
186623
 YDOT =      14921
459653  feet/sec       YDOT =        4493
552251  meter/sec
 ZDOT =     -12757
610833                 ZDOT =       -3912
199721

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11203539
26                 X    =         3414838
77
 Y    =       13685768
77  feet           Y    =         4171422
32  meter
 Z    =       13148207
65                 Z    =         4007573
69
 XDOT =      -8061
703492                 XDOT =       -2457
207224
 YDOT =      18988
518684  feet/sec       YDOT =        5787
700495  meter/sec
 ZDOT =     -12851
530025                 ZDOT =       -3917
146352


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   10086
59077402  
00016717  00000-0  10270-3 0  9039
2 25544  51
6419 289
5022 0005833 112
8303 247
3477 15
73886033 10620


Satellite: ISS
Catalog Number: 25544
Epoch time:      10086
59077402   =   yrday
fracday
Element set:     903
Inclination:       51
6419  deg
RA of node:       289
5022  deg
Eccentricity:     
0005833     
Arg of perigee:   112
8303  deg
Mean anomaly:     247
3477  deg
Mean motion:   15
73886033  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1062
Checksum:              303


Coasting Arc #5 (Orbit 1077)
---------------------------------------

Vector Time (GMT): 2010/087/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3856795
82                 A    =         6727335
29  meter
 Y    =       -4351221
80  meter          E    =           
0018000
 Z    =        3371092
64                 I    =           51
31735
 XDOT =       2386
355341                 Wp   =           98
70058
 YDOT =       5699
376756  meter/sec      RA   =          283
89434  deg
 ZDOT =       4602
656309                 TA   =          301
28035
                                          MA   =          301
45651
                                          Ha   =            192
180  n
mi
                                          Hp   =            181
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12653529
61                 X    =         3888789
26
 Y    =      -14275662
06  feet           Y    =        -4307913
53  meter
 Z    =       11060015
23                 Z    =         3389907
05
 XDOT =       7829
249805                 XDOT =        2300
087801
 YDOT =      18698
742638  feet/sec       YDOT =        5725
580589  meter/sec
 ZDOT =      15100
578441                 ZDOT =        4614
038940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5959073
14                 X    =         1816325
49
 Y    =      -18075956
18  feet           Y    =        -5509551
44  meter
 Z    =       11134609
62                 Z    =         3393829
01
 XDOT =      13152
837763                 XDOT =        4008
984950
 YDOT =      13713
222152  feet/sec       YDOT =        4179
790112  meter/sec
 ZDOT =      15145
948265                 ZDOT =        4616
485031


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   10087
60666702  
00016717  00000-0  10270-3 0  9040
2 25544  51
6409 284
2852 0005913 117
4229 242
7536 15
73941556 10783


Satellite: ISS
Catalog Number: 25544
Epoch time:      10087
60666702   =   yrday
fracday
Element set:     904
Inclination:       51
6409  deg
RA of node:       284
2852  deg
Eccentricity:     
0005913     
Arg of perigee:   117
4229  deg
Mean anomaly:     242
7536  deg
Mean motion:   15
73941556  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1078
Checksum:              317


Coasting Arc #6 (Orbit 1092)
---------------------------------------

Vector Time (GMT): 2010/088/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2527380
65                 A    =         6725233
56  meter
 Y    =       -4775300
46  meter          E    =           
0013277
 Z    =       -4019074
66                 I    =           51
30457
 XDOT =       3950
668738                 Wp   =          113
83150
 YDOT =      -5342
784311  meter/sec      RA   =          278
68341  deg
 ZDOT =       3868
517088                 TA   =          196
28622
                                          MA   =          196
32893
                                          Ha   =            192
232  n
mi
                                          Hp   =            181
788

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8291931
28                 X    =        -2454270
61
 Y    =      -15666996
26  feet           Y    =        -4803154
83  meter
 Z    =      -13185940
48                 Z    =        -4031174
53
 XDOT =      12961
511607                 XDOT =        3991
326530
 YDOT =     -17528
819917  feet/sec       YDOT =       -5298
377801  meter/sec
 ZDOT =      12691
985197                 ZDOT =        3887
808810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13904449
25                 X    =        -4238076
13
 Y    =      -10936355
43  feet           Y    =        -3333401
14  meter
 Z    =      -13234135
55                 Z    =        -4033764
51
 XDOT =       3791
300096                 XDOT =        1155
588269
 YDOT =     -20252
399814  feet/sec       YDOT =       -6172
931463  meter/sec
 ZDOT =      12768
440458                 ZDOT =        3891
820652


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
55904627  
00016717  00000-0  10270-3 0  9057
2 25544  51
6411 279
3939 0006061 120
2359 239
9405 15
73958858 10931


Satellite: ISS
Catalog Number: 25544
Epoch time:      10088
55904627   =   yrday
fracday
Element set:     905
Inclination:       51
6411  deg
RA of node:       279
3939  deg
Eccentricity:     
0006061     
Arg of perigee:   120
2359  deg
Mean anomaly:     239
9405  deg
Mean motion:   15
73958858  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1093
Checksum:              332


Coasting Arc #7 (Orbit 1108)
---------------------------------------

Vector Time (GMT): 2010/089/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3045908
06                 A    =         6727027
48  meter
 Y    =        4937345
35  meter          E    =           
0010494
 Z    =       -3411159
36                 I    =           51
30812
 XDOT =      -3342
362863                 Wp   =          106
83312
 YDOT =      -5209
710837  meter/sec      RA   =          273
57559  deg
 ZDOT =      -4570
705251                 TA   =          113
66332
                                          MA   =          113
55315
                                          Ha   =            192
079  n
mi
                                          Hp   =            181
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9993136
69                 X    =        -3084321
08
 Y    =       16198639
60  feet           Y    =         4903069
06  meter
 Z    =      -11191467
71                 Z    =        -3426050
27
 XDOT =     -10965
757423                 XDOT =       -3261
654750
 YDOT =     -17092
227157  feet/sec       YDOT =       -5246
636340  meter/sec
 ZDOT =     -14995
752135                 ZDOT =       -4586
745950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2107887
64                 X    =         -642484
15
 Y    =       18880988
35  feet           Y    =         5754925
25  meter
 Z    =      -11250455
28                 Z    =        -3429138
77
 XDOT =     -15730
026627                 XDOT =       -4794
512116
 YDOT =     -10701
169800  feet/sec       YDOT =       -3261
716555  meter/sec
 ZDOT =     -15059
612288                 ZDOT =       -4590
169825


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
57489261  
00016717  00000-0  10270-3 0  9063
2 25544  51
6414 274
1772 0006004 122
5309 237
6435 15
74012466 11092


Satellite: ISS
Catalog Number: 25544
Epoch time:      10089
57489261   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:       274
1772  deg
Eccentricity:     
0006004     
Arg of perigee:   122
5309  deg
Mean anomaly:     237
6435  deg
Mean motion:   15
74012466  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1109
Checksum:              299


Coasting Arc #8 (Orbit 1124)
---------------------------------------

Vector Time (GMT): 2010/090/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3304816
89                 A    =         6725205
99  meter
 Y    =        4292732
62  meter          E    =           
0015490
 Z    =        3970497
47                 I    =           51
30078
 XDOT =      -2975
269992                 Wp   =           95
33461
 YDOT =       5930
566878  meter/sec      RA   =          268
36356  deg
 ZDOT =      -3923
736498                 TA   =           35
42620
                                          MA   =           35
32340
                                          Ha   =            191
973  n
mi
                                          Hp   =            181
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10842575
11                 X    =         3237281
04
 Y    =       14083768
44  feet           Y    =         4329311
76  meter
 Z    =       13026566
51                 Z    =         3986388
01
 XDOT =      -9761
384488                 XDOT =       -3022
304551
 YDOT =      19457
240413  feet/sec       YDOT =        5897
032334  meter/sec
 ZDOT =     -12873
151241                 ZDOT =       -3938
305216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15866461
90                 X    =         4836097
59
 Y    =        7906821
36  feet           Y    =         2409999
15  meter
 Z    =       13089803
90                 Z    =         3989772
23
 XDOT =        445
200709                 XDOT =         135
697176
 YDOT =      20576
918744  feet/sec       YDOT =        6271
844833  meter/sec
 ZDOT =     -12930
829140                 ZDOT =       -3941
316722


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
59071549  
00016717  00000-0  10270-3 0  9074
2 25544  51
6408 268
9595 0005998 127
7237 232
4475 15
74011493 11251


Satellite: ISS
Catalog Number: 25544
Epoch time:      10090
59071549   =   yrday
fracday
Element set:     907
Inclination:       51
6408  deg
RA of node:       268
9595  deg
Eccentricity:     
0005998     
Arg of perigee:   127
7237  deg
Mean anomaly:     232
4475  deg
Mean motion:   15
74011493  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1125
Checksum:              329


Coasting Arc #9 (Orbit 1140)
---------------------------------------

Vector Time (GMT): 2010/091/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2139910
54                 A    =         6726744
79  meter
 Y    =       -5363327
81  meter          E    =           
0017386
 Z    =        3440002
52                 I    =           51
30967
 XDOT =       4200
314836                 Wp   =          104
23522
 YDOT =       4598
899637  meter/sec      RA   =          263
25520  deg
 ZDOT =       4533
942011                 TA   =          296
73714
                                          MA   =          296
91496
                                          Ha   =            191
861  n
mi
                                          Hp   =            181
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7020703
87                 X    =         2183014
12
 Y    =      -17596219
86  feet           Y    =        -5339156
86  meter
 Z    =       11286097
50                 Z    =         3450503
30
 XDOT =      13780
560487                 XDOT =        4126
551659
 YDOT =      15088
253403  feet/sec       YDOT =        4645
457877  meter/sec
 ZDOT =      14875
137832                 ZDOT =        4554
167901

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1826021
33                 X    =         -556571
30
 Y    =      -18831980
19  feet           Y    =        -5739987
56  meter
 Z    =       11327638
83                 Z    =         3452664
31
 XDOT =      17690
161820                 XDOT =        5391
961323
 YDOT =       7326
569259  feet/sec       YDOT =        2233
138310  meter/sec
 ZDOT =      14955
604475                 ZDOT =        4558
468244


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
60651215  
00016717  00000-0  10270-3 0  9082
2 25544  51
6418 263
7424 0005976 131
9794 228
1880 15
74087501 11410


Satellite: ISS
Catalog Number: 25544
Epoch time:      10091
60651215   =   yrday
fracday
Element set:     908
Inclination:       51
6418  deg
RA of node:       263
7424  deg
Eccentricity:     
0005976     
Arg of perigee:   131
9794  deg
Mean anomaly:     228
1880  deg
Mean motion:   15
74087501  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1141
Checksum:              306


Coasting Arc #10 (Orbit 1155)
---------------------------------------

Vector Time (GMT): 2010/092/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4003447
52                 A    =         6725109
02  meter
 Y    =       -3727501
50  meter          E    =           
0012492
 Z    =       -3926317
49                 I    =           51
31033
 XDOT =       1937
026545                 Wp   =          120
02848
 YDOT =      -6280
650204  meter/sec      RA   =          258
04403  deg
 ZDOT =       3990
866436                 TA   =          191
63477
                                          MA   =          191
66367
                                          Ha   =            191
825  n
mi
                                          Hp   =            181
827

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13134670
33                 X    =        -3942394
89
 Y    =      -12229335
62  feet           Y    =        -3771929
19  meter
 Z    =      -12881619
05                 Z    =        -3945617
97
 XDOT =       6355
073965                 XDOT =        1987
726875
 YDOT =     -20605
807757  feet/sec       YDOT =       -6258
705613  meter/sec
 ZDOT =      13093
393819                 ZDOT =        4000
399937

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17278763
23                 X    =        -5266567
03
 Y    =       -4640778
67  feet           Y    =        -1414509
34  meter
 Z    =      -12958388
73                 Z    =        -3949716
88
 XDOT =      -4501
704370                 XDOT =       -1372
119492
 YDOT =     -19874
470269  feet/sec       YDOT =       -6057
738538  meter/sec
 ZDOT =      13131
067383                 ZDOT =        4002
349338


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
55880050  
00016717  00000-0  10270-3 0  9099
2 25544  51
6429 258
8519 0005964 134
4228 225
7424 15
74104320 11561


Satellite: ISS
Catalog Number: 25544
Epoch time:      10092
55880050   =   yrday
fracday
Element set:     909
Inclination:       51
6429  deg
RA of node:       258
8519  deg
Eccentricity:     
0005964     
Arg of perigee:   134
4228  deg
Mean anomaly:     225
7424  deg
Mean motion:   15
74104320  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1156
Checksum:              304


Coasting Arc #11 (Orbit 1171)
---------------------------------------

Vector Time (GMT): 2010/093/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1265101
52                 A    =         6726240
74  meter
 Y    =        5572070
91  meter          E    =           
0009919
 Z    =       -3553251
78                 I    =           51
32200
 XDOT =      -4914
823297                 Wp   =          111
80602
 YDOT =      -3931
128815  meter/sec      RA   =          252
93627  deg
 ZDOT =      -4428
286682                 TA   =          110
76057
                                          MA   =          110
65427
                                          Ha   =            191
650  n
mi
                                          Hp   =            181
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4150595
54                 X    =        -1310054
26
 Y    =       18281072
55  feet           Y    =         5557672
40  meter
 Z    =      -11657650
21                 Z    =        -3559506
95
 XDOT =     -16124
748349                 XDOT =       -4848
987514
 YDOT =     -12897
404249  feet/sec       YDOT =       -3985
721251  meter/sec
 ZDOT =     -14528
499614                 ZDOT =       -4452
003026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5315829
85                 X    =         1620264
94
 Y    =       17960821
37  feet           Y    =         5474458
35  meter
 Z    =      -11682324
87                 Z    =        -3560772
62
 XDOT =     -18975
756905                 XDOT =       -5783
810705
 YDOT =      -3866
169105  feet/sec       YDOT =       -1178
408343  meter/sec
 ZDOT =     -14622
822257                 ZDOT =       -4457
036224


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
57454944  
00016717  00000-0  10270-3 0  9103
2 25544  51
6429 253
6347 0005852 138
1020 222
0592 15
74147930 11728


Satellite: ISS
Catalog Number: 25544
Epoch time:      10093
57454944   =   yrday
fracday
Element set:     910
Inclination:       51
6429  deg
RA of node:       253
6347  deg
Eccentricity:     
0005852     
Arg of perigee:   138
1020  deg
Mean anomaly:     222
0592  deg
Mean motion:   15
74147930  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1172
Checksum:              295


Coasting Arc #12 (Orbit 1187)
---------------------------------------

Vector Time (GMT): 2010/094/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4571511
23                 A    =         6725286
07  meter
 Y    =        3111698
45  meter          E    =           
0015166
 Z    =        3812080
38                 I    =           51
32906
 XDOT =       -932
479446                 Wp   =          101
21703
 YDOT =       6442
098701  meter/sec      RA   =          247
72516  deg
 ZDOT =      -4129
318566                 TA   =           32
15244
                                          MA   =           32
06004
                                          Ha   =            191
497  n
mi
                                          Hp   =            182
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14998396
43                 X    =         4517857
49
 Y    =       10208984
40  feet           Y    =         3162519
84  meter
 Z    =       12506825
40                 Z    =         3834158
45
 XDOT =      -3059
315767                 XDOT =        -984
387344
 YDOT =      21135
494425  feet/sec       YDOT =        6431
380896  meter/sec
 ZDOT =     -13547
633089                 ZDOT =       -4133
974689

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18031100
71                 X    =         5495879
49
 Y    =        1360429
72  feet           Y    =          414658
98  meter
 Z    =       12594624
97                 Z    =         3838841
69
 XDOT =       8107
083507                 XDOT =        2471
039053
 YDOT =      18470
155373  feet/sec       YDOT =        5629
703358  meter/sec
 ZDOT =     -13565
927321                 ZDOT =       -4134
894647


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
59027394  
00016717  00000-0  10270-3 0  9112
2 25544  51
6429 248
4175 0005885 141
9771 218
1809 15
74164253 11881


Satellite: ISS
Catalog Number: 25544
Epoch time:      10094
59027394   =   yrday
fracday
Element set:     911
Inclination:       51
6429  deg
RA of node:       248
4175  deg
Eccentricity:     
0005885     
Arg of perigee:   141
9771  deg
Mean anomaly:     218
1809  deg
Mean motion:   15
74164253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1188
Checksum:              327


Coasting Arc #13 (Orbit 1203)
---------------------------------------

Vector Time (GMT): 2010/095/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         378946
25                 A    =         6725621
50  meter
 Y    =       -5627262
65  meter          E    =           
0016142
 Z    =        3656187
61                 I    =           51
34451
 XDOT =       5532
724953                 Wp   =          111
42962
 YDOT =       3186
528867  meter/sec      RA   =          242
61903  deg
 ZDOT =       4309
895382                 TA   =          292
72269
                                          MA   =          292
89323
                                          Ha   =            191
348  n
mi
                                          Hp   =            182
022

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1243261
98                 X    =          424082
10
 Y    =      -18462147
81  feet           Y    =        -5622772
64  meter
 Z    =       11995366
19                 Z    =         3658138
22
 XDOT =      18151
984754                 XDOT =        5475
744780
 YDOT =      10454
491034  feet/sec       YDOT =        3248
080541  meter/sec
 ZDOT =      14140
076711                 ZDOT =        4336
634840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8516422
14                 X    =        -2595805
47
 Y    =      -16422104
91  feet           Y    =        -5005457
58  meter
 Z    =       12002934
48                 Z    =         3658494
43
 XDOT =      19674
527277                 XDOT =        5996
795914
 YDOT =        260
100924  feet/sec       YDOT =          79
278762  meter/sec
 ZDOT =      14246
407527                 ZDOT =        4342
305014


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
60597010  
00016717  00000-0  10270-3 0  9123
2 25544  51
6439 243
2005 0005752 146
4731 213
6798 15
74257987 12049


Satellite: ISS
Catalog Number: 25544
Epoch time:      10095
60597010   =   yrday
fracday
Element set:     912
Inclination:       51
6439  deg
RA of node:       243
2005  deg
Eccentricity:     
0005752     
Arg of perigee:   146
4731  deg
Mean anomaly:     213
6798  deg
Mean motion:   15
74257987  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1204
Checksum:              306


Coasting Arc #14 (Orbit 1218)
---------------------------------------

Vector Time (GMT): 2010/096/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5069056
51                 A    =         6725456
31  meter
 Y    =       -2448786
88  meter          E    =           
0010523
 Z    =       -3692369
71                 I    =           51
35898
 XDOT =        -26
669862                 Wp   =          125
16823
 YDOT =      -6391
000260  meter/sec      RA   =          237
40963  deg
 ZDOT =       4277
760957                 TA   =          190
23044
                                          MA   =          190
25188
                                          Ha   =            191
255  n
mi
                                          Hp   =            182
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16630762
83                 X    =        -5023360
23
 Y    =       -8034077
68  feet           Y    =        -2505216
66  meter
 Z    =      -12114073
86                 Z    =        -3716884
00
 XDOT =        -87
499546                 XDOT =          24
016956
 YDOT =     -20967
848623  feet/sec       YDOT =       -6391
015000  meter/sec
 ZDOT =      14034
648809                 ZDOT =        4277
754653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18299483
12                 X    =        -5577682
46
 Y    =        1971388
60  feet           Y    =          600879
25  meter
 Z    =      -12211552
17                 Z    =        -3722081
10
 XDOT =     -11121
158214                 XDOT =       -3389
729024
 YDOT =     -16350
792224  feet/sec       YDOT =       -4983
721470  meter/sec
 ZDOT =      14034
411250                 ZDOT =        4277
688549


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
55816468  
00016717  00000-0  10270-3 0  9130
2 25544  51
6439 238
3097 0005547 148
9609 211
1883 15
74247307 12197


Satellite: ISS
Catalog Number: 25544
Epoch time:      10096
55816468   =   yrday
fracday
Element set:     913
Inclination:       51
6439  deg
RA of node:       238
3097  deg
Eccentricity:     
0005547     
Arg of perigee:   148
9609  deg
Mean anomaly:     211
1883  deg
Mean motion:   15
74247307  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1219
Checksum:              331


Coasting Arc #15 (Orbit 1234)
---------------------------------------

Vector Time (GMT): 2010/097/13:12:20
814
Vector Time (MET): N/A
Weight (LBS)     : 782570
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         389762
92                 A    =         6724957
44  meter
 Y    =        5514434
48  meter          E    =           
0009277
 Z    =       -3834137
73                 I    =           51
37510
 XDOT =      -6032
290305                 Wp   =          111
04584
 YDOT =      -2427
657220  meter/sec      RA   =          232
30443  deg
 ZDOT =      -4116
071086                 TA   =          115
79700
                                          MA   =          115
70125
                                          Ha   =            191
119  n
mi
                                          Hp   =            182
192

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1278749
73                 X    =          346695
98
 Y    =       18091976
65  feet           Y    =         5518552
10  meter
 Z    =      -12579192
04                 Z    =        -3832349
09
 XDOT =     -19790
978692                 XDOT =       -5984
700478
 YDOT =      -7964
754660  feet/sec       YDOT =       -2494
847943  meter/sec
 ZDOT =     -13504
170230                 ZDOT =       -4145
260067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10992145
36                 X    =         3350405
91
 Y    =       14432986
08  feet           Y    =         4399174
16  meter
 Z    =      -12571895
06                 Z    =        -3831913
61
 XDOT =     -19815
611534                 XDOT =       -6039
798396
 YDOT =       3259
868008  feet/sec       YDOT =         993
607769  meter/sec
 ZDOT =     -13620
232962                 ZDOT =       -4151
447007


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
57381271  
00016717  00000-0  10270-3 0  9143
2 25544  51
6441 233
0918 0005579 153
0786 207
0668 15
74292617 12359


Satellite: ISS
Catalog Number: 25544
Epoch time:      10097
57381271   =   yrday
fracday
Element set:     914
Inclination:       51
6441  deg
RA of node:       233
0918  deg
Eccentricity:     
0005579     
Arg of perigee:   153
0786  deg
Mean anomaly:     207
0668  deg
Mean motion:   15
74292617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1235
Checksum:              316

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

The following information is a reminder of your current mailing list subscription:

You are subscribed to the following list: [list_name]

using the following email: example@example.com

You may automatically unsubscribe from this list at any time by visiting the following URL:

http://www aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/

If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism

You may also change your subscription by visiting this list's main screen:

<[program_url]/list/[list]>

If you're still having trouble, please contact the list owner at:

<mailto:[list_owner_email]>

The following physical address is associated with this mailing list:

[physical_address]

Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list