Date: March 6th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 20989 63 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 714)
---------------------------------------

Vector Time (GMT): 2010/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3538470
99                 A    =         6731290
76  meter
 Y    =        5350909
38  meter          E    =           
0019407
 Z    =        2000265
91                 I    =           51
88616
 XDOT =      -5126
245037                 Wp   =           49
53740
 YDOT =       1283
412060  meter/sec      RA   =           42
36518  deg
 ZDOT =       5612
059819                 TA   =          332
69352
                                          MA   =          332
79541
                                          Ha   =            192
405  n
mi
                                          Hp   =            183
133

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11609156
78                 X    =         3468656
32
 Y    =       17555476
98  feet           Y    =         5390088
41  meter
 Z    =        6562552
19                 Z    =         2017285
83
 XDOT =     -16818
389230                 XDOT =       -5167
477560
 YDOT =       4210
669489  feet/sec       YDOT =        1225
857079  meter/sec
 ZDOT =      18412
269746                 ZDOT =        5587
056488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5704649
21                 X    =         1738777
08
 Y    =       20236865
79  feet           Y    =         6168196
69  meter
 Z    =        6630280
91                 Z    =         2020909
62
 XDOT =     -15930
778484                 XDOT =       -4855
701282
 YDOT =      -1533
646841  feet/sec       YDOT =        -467
455557  meter/sec
 ZDOT =      18312
977224                 ZDOT =        5581
795458


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   10064
55953376  
00016717  00000-0  10270-3 0  9001
2 25544  51
6442  42
6164 0007589  13
1385 346
9974 15
73689781  7157


Satellite: ISS
Catalog Number: 25544
Epoch time:      10064
55953376   =   yrday
fracday
Element set:     900
Inclination:       51
6442  deg
RA of node:        42
6164  deg
Eccentricity:     
0007589     
Arg of perigee:    13
1385  deg
Mean anomaly:     346
9974  deg
Mean motion:   15
73689781  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             715
Checksum:              332


Coasting Arc #2 (Orbit 729)
---------------------------------------

Vector Time (GMT): 2010/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4282605
51                 A    =         6722697
56  meter
 Y    =       -1617277
15  meter          E    =           
0014779
 Z    =       -4934025
76                 I    =           51
83384
 XDOT =       4667
925050                 Wp   =           73
87764
 YDOT =       5706
538127  meter/sec      RA   =           37
21201  deg
 ZDOT =       2190
555086                 TA   =          217
31011
                                          MA   =          217
41285
                                          Ha   =            192
673  n
mi
                                          Hp   =            183
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14050543
02                 X    =         4324340
28
 Y    =       -5306027
39  feet           Y    =        -1569153
32  meter
 Z    =      -16187748
55                 Z    =        -4913119
63
 XDOT =      15314
714732                 XDOT =        4593
125373
 YDOT =      18722
237951  feet/sec       YDOT =        5758
319482  meter/sec
 ZDOT =       7186
860519                 ZDOT =        2213
049776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15072975
86                 X    =         4594243
04
 Y    =       -1028474
63  feet           Y    =         -313479
07  meter
 Z    =      -16104736
19                 Z    =        -4908723
59
 XDOT =       9188
862879                 XDOT =        2800
765405
 YDOT =      21215
642113  feet/sec       YDOT =        6466
527716  meter/sec
 ZDOT =       7276
337678                 ZDOT =        2217
827724


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   10065
51208237  
00016717  00000-0  10270-3 0  9018
2 25544  51
6444  37
7273 0007834  16
5794 343
5623 15
73656771  7303


Satellite: ISS
Catalog Number: 25544
Epoch time:      10065
51208237   =   yrday
fracday
Element set:     901
Inclination:       51
6444  deg
RA of node:        37
7273  deg
Eccentricity:     
0007834     
Arg of perigee:    16
5794  deg
Mean anomaly:     343
5623  deg
Mean motion:   15
73656771  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             730
Checksum:              305


Coasting Arc #3 (Orbit 745)
---------------------------------------

Vector Time (GMT): 2010/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4567097
43                 A    =         6731432
16  meter
 Y    =       -4588506
69  meter          E    =           
0007407
 Z    =       -1854252
48                 I    =           51
83996
 XDOT =       4645
267125                 Wp   =           75
11438
 YDOT =      -2340
609214  meter/sec      RA   =           32
12739  deg
 ZDOT =      -5666
316637                 TA   =          125
38406
                                          MA   =          125
31484
                                          Ha   =            192
634  n
mi
                                          Hp   =            182
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14983915
45                 X    =        -4506440
98
 Y    =      -15054155
81  feet           Y    =        -4639239
58  meter
 Z    =       -6083505
50                 Z    =        -1876291
71
 XDOT =      15240
377707                 XDOT =        4698
620581
 YDOT =      -7679
164088  feet/sec       YDOT =       -2288
364901  meter/sec
 ZDOT =     -18590
277681                 ZDOT =       -5643
620567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10325048
23                 X    =        -3147074
70
 Y    =      -18532800
64  feet           Y    =        -5648797
63  meter
 Z    =       -6171146
41                 Z    =        -1880965
43
 XDOT =      15501
934850                 XDOT =        4724
989742
 YDOT =      -2494
379960  feet/sec       YDOT =        -760
287012  meter/sec
 ZDOT =     -18500
166592                 ZDOT =       -5638
850777


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   10066
52811156  
00016717  00000-0  10270-3 0  9021
2 25544  51
6450  32
5121 0007904  20
1449 340
0024 15
73719172  7460


Satellite: ISS
Catalog Number: 25544
Epoch time:      10066
52811156   =   yrday
fracday
Element set:     902
Inclination:       51
6450  deg
RA of node:        32
5121  deg
Eccentricity:     
0007904     
Arg of perigee:    20
1449  deg
Mean anomaly:     340
0024  deg
Mean motion:   15
73719172  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             746
Checksum:              265


Coasting Arc #4 (Orbit 761)
---------------------------------------

Vector Time (GMT): 2010/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3800393
49                 A    =         6722260
26  meter
 Y    =        2455152
33  meter          E    =           
0013403
 Z    =        4968011
10                 I    =           51
78297
 XDOT =      -5734
879842                 Wp   =           37
43359
 YDOT =      -4721
422964  meter/sec      RA   =           26
97307  deg
 ZDOT =      -2040
435039                 TA   =           72
34143
                                          MA   =           72
19512
                                          Ha   =            192
759  n
mi
                                          Hp   =            182
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12468482
57                 X    =        -3851698
29
 Y    =        8054961
73  feet           Y    =         2412367
34  meter
 Z    =       16299249
02                 Z    =         4949424
42
 XDOT =     -18815
222578                 XDOT =       -5671
745918
 YDOT =     -15490
232821  feet/sec       YDOT =       -4785
200845  meter/sec
 ZDOT =      -6694
340680                 ZDOT =       -2068
141163

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14195998
04                 X    =        -4326940
20
 Y    =        4606409
83  feet           Y    =         1404033
71  meter
 Z    =       16225461
87                 Z    =         4945520
78
 XDOT =     -13898
394399                 XDOT =       -4236
230613
 YDOT =     -18709
626008  feet/sec       YDOT =       -5702
694007  meter/sec
 ZDOT =      -6804
494008                 ZDOT =       -2074
009774


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   10067
54411960  
00016717  00000-0  10270-3 0  9034
2 25544  51
6451  27
2974 0007852  23
6292 336
5231 15
73742358  7624


Satellite: ISS
Catalog Number: 25544
Epoch time:      10067
54411960   =   yrday
fracday
Element set:     903
Inclination:       51
6451  deg
RA of node:        27
2974  deg
Eccentricity:     
0007852     
Arg of perigee:    23
6292  deg
Mean anomaly:     336
5231  deg
Mean motion:   15
73742358  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             762
Checksum:              302


Coasting Arc #5 (Orbit 777)
---------------------------------------

Vector Time (GMT): 2010/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5398513
51                 A    =         6731460
57  meter
 Y    =        3617972
86  meter          E    =           
0020833
 Z    =        1708704
40                 I    =           51
78739
 XDOT =      -4003
522977                 Wp   =           51
37550
 YDOT =       3252
256878  meter/sec      RA   =           21
88270  deg
 ZDOT =       5728
684481                 TA   =          327
50732
                                          MA   =          327
63539
                                          Ha   =            192
611  n
mi
                                          Hp   =            182
381

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17711658
49                 X    =         5349355
05
 Y    =       11869989
70  feet           Y    =         3678067
44  meter
 Z    =        5605985
56                 Z    =         1734810
34
 XDOT =     -13134
917904                 XDOT =       -4067
421112
 YDOT =      10670
134113  feet/sec       YDOT =        3207
130021  meter/sec
 ZDOT =      18794
896592                 ZDOT =        5709
080437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14363471
90                 X    =         4377986
23
 Y    =       15719919
93  feet           Y    =         4791431
59  meter
 Z    =        5709760
82                 Z    =         1740335
10
 XDOT =     -14249
558237                 XDOT =       -4343
265351
 YDOT =       6181
977361  feet/sec       YDOT =        1884
266700  meter/sec
 ZDOT =      18717
081924                 ZDOT =        5704
966570


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   10068
56010487  
00016717  00000-0  10270-3 0  9047
2 25544  51
6453  22
0823 0007780  27
5836 332
5739 15
73791987  7787


Satellite: ISS
Catalog Number: 25544
Epoch time:      10068
56010487   =   yrday
fracday
Element set:     904
Inclination:       51
6453  deg
RA of node:        22
0823  deg
Eccentricity:     
0007780     
Arg of perigee:    27
5836  deg
Mean anomaly:     332
5739  deg
Mean motion:   15
73791987  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             778
Checksum:              328


Coasting Arc #6 (Orbit 792)
---------------------------------------

Vector Time (GMT): 2010/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3169613
89                 A    =         6721901
63  meter
 Y    =       -3179766
31  meter          E    =           
0017002
 Z    =       -5015852
86                 I    =           51
72718
 XDOT =       6554
259502                 Wp   =           77
69374
 YDOT =       3540
168276  meter/sec      RA   =           16
72556  deg
 ZDOT =       1906
458698                 TA   =          210
66644
                                          MA   =          210
76592
                                          Ha   =            192
718  n
mi
                                          Hp   =            182
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10398995
69                 X    =         3229300
60
 Y    =      -10432304
18  feet           Y    =        -3143988
32  meter
 Z    =      -16456210
16                 Z    =        -5000310
08
 XDOT =      21503
476058                 XDOT =        6504
924553
 YDOT =      11614
725316  feet/sec       YDOT =        3613
186143  meter/sec
 ZDOT =       6254
785756                 ZDOT =        1938
178595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12534699
16                 X    =         3820576
30
 Y    =       -7866365
62  feet           Y    =        -2397668
24  meter
 Z    =      -16394527
86                 Z    =        -4997052
09
 XDOT =      17809
331851                 XDOT =        5428
284348
 YDOT =      15141
334494  feet/sec       YDOT =        4615
078754  meter/sec
 ZDOT =       6380
861126                 ZDOT =        1944
886471


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   10069
51257202  
00016717  00000-0  10270-3 0  9052
2 25544  51
6458  17
1928 0007852  30
4003 329
7614 15
73805028  7931


Satellite: ISS
Catalog Number: 25544
Epoch time:      10069
51257202   =   yrday
fracday
Element set:     905
Inclination:       51
6458  deg
RA of node:        17
1928  deg
Eccentricity:     
0007852     
Arg of perigee:    30
4003  deg
Mean anomaly:     329
7614  deg
Mean motion:   15
73805028  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             793
Checksum:              297


Coasting Arc #7 (Orbit 808)
---------------------------------------

Vector Time (GMT): 2010/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6003460
72                 A    =         6731357
67  meter
 Y    =       -2564470
78  meter          E    =           
0009156
 Z    =       -1650071
50                 I    =           51
73126
 XDOT =       3258
306751                 Wp   =           87
23338
 YDOT =      -3952
024647  meter/sec      RA   =           11
62904  deg
 ZDOT =      -5739
490348                 TA   =          110
95381
                                          MA   =          110
85581
                                          Ha   =            192
692  n
mi
                                          Hp   =            182
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19696393
45                 X    =        -5966322
59
 Y    =       -8413618
05  feet           Y    =        -2631397
50  meter
 Z    =       -5413620
41                 Z    =        -1679145
28
 XDOT =      10689
982779                 XDOT =        3330
137615
 YDOT =     -12965
960129  feet/sec       YDOT =       -3915
187070  meter/sec
 ZDOT =     -18830
348911                 ZDOT =       -5723
487121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17542798
03                 X    =        -5347044
84
 Y    =      -12236124
61  feet           Y    =        -3729570
78  meter
 Z    =       -5529164
61                 Z    =        -1685289
37
 XDOT =      12318
991669                 XDOT =        3754
828661
 YDOT =      -9220
357719  feet/sec       YDOT =       -2810
365033  meter/sec
 ZDOT =     -18766
854411                 ZDOT =       -5720
137225


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   10070
52851498  
00016717  00000-0  10270-3 0  9063
2 25544  51
6466  11
9773 0007870  34
1819 325
9849 15
73851463  8096


Satellite: ISS
Catalog Number: 25544
Epoch time:      10070
52851498   =   yrday
fracday
Element set:     906
Inclination:       51
6466  deg
RA of node:        11
9773  deg
Eccentricity:     
0007870     
Arg of perigee:    34
1819  deg
Mean anomaly:     325
9849  deg
Mean motion:   15
73851463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             809
Checksum:              333


Coasting Arc #8 (Orbit 824)
---------------------------------------

Vector Time (GMT): 2010/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2501102
34                 A    =         6721620
07  meter
 Y    =        3705800
68  meter          E    =           
0013357
 Z    =        5013705
68                 I    =           51
66901
 XDOT =      -7122
302589                 Wp   =           44
68828
 YDOT =      -2282
487141  meter/sec      RA   =            6
46894  deg
 ZDOT =      -1853
612591                 TA   =           63
23840
                                          MA   =           63
10179
                                          Ha   =            192
783  n
mi
                                          Hp   =            181
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8205716
34                 X    =        -2566710
53
 Y    =       12158138
71  feet           Y    =         3677465
44  meter
 Z    =       16449165
63                 Z    =         5001395
93
 XDOT =     -23367
134477                 XDOT =       -7087
245745
 YDOT =      -7488
474871  feet/sec       YDOT =       -2361
937100  meter/sec
 ZDOT =      -6081
406140                 ZDOT =       -1888
126648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10423657
55                 X    =        -3177130
82
 Y    =       10397371
12  feet           Y    =         3169118
72  meter
 Z    =       16400341
59                 Z    =         4998824
12
 XDOT =     -20767
432200                 XDOT =       -6329
913334
 YDOT =     -10947
199798  feet/sec       YDOT =       -3336
706498  meter/sec
 ZDOT =      -6218
553301                 ZDOT =       -1895
415046


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   10071
54443566  
00016717  00000-0  10270-3 0  9070
2 25544  51
6468   6
7624 0007845  37
9213 322
2502 15
73883119  8253


Satellite: ISS
Catalog Number: 25544
Epoch time:      10071
54443566   =   yrday
fracday
Element set:     907
Inclination:       51
6468  deg
RA of node:         6
7624  deg
Eccentricity:     
0007845     
Arg of perigee:    37
9213  deg
Mean anomaly:     322
2502  deg
Mean motion:   15
73883119  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             825
Checksum:              307


Coasting Arc #9 (Orbit 840)
---------------------------------------

Vector Time (GMT): 2010/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6376226
59                 A    =         6731298
87  meter
 Y    =        1407205
66  meter          E    =           
0021569
 Z    =        1587126
57                 I    =           51
67202
 XDOT =      -2438
508374                 Wp   =           55
10586
 YDOT =       4499
841223  meter/sec      RA   =            1
36696  deg
 ZDOT =       5764
034911                 TA   =          322
41646
                                          MA   =          322
56702
                                          Ha   =            192
687  n
mi
                                          Hp   =            181
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20919378
57                 X    =         6352307
24
 Y    =        4616816
48  feet           Y    =         1478374
83  meter
 Z    =        5207108
18                 Z    =         1618043
45
 XDOT =      -8000
355558                 XDOT =       -2516
645271
 YDOT =      14763
258607  feet/sec       YDOT =        4472
136049  meter/sec
 ZDOT =      18910
875693                 ZDOT =        5751
998637

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19803404
39                 X    =         6036077
66
 Y    =        8091120
97  feet           Y    =         2466173
67  meter
 Z    =        5329944
27                 Z    =         1624567
01
 XDOT =      -9906
767595                 XDOT =       -3019
582763
 YDOT =      11730
872396  feet/sec       YDOT =        3575
569906  meter/sec
 ZDOT =      18863
158165                 ZDOT =        5749
490609


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   10072
56033394  
00016717  00000-0  10270-3 0  9088
2 25544  51
6470   1
5465 0007844  41
4685 318
7072 15
73908512  8419


Satellite: ISS
Catalog Number: 25544
Epoch time:      10072
56033394   =   yrday
fracday
Element set:     908
Inclination:       51
6470  deg
RA of node:         1
5465  deg
Eccentricity:     
0007844     
Arg of perigee:    41
4685  deg
Mean anomaly:     318
7072  deg
Mean motion:   15
73908512  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             841
Checksum:              301


Coasting Arc #10 (Orbit 855)
---------------------------------------

Vector Time (GMT): 2010/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1760400
92                 A    =         6721397
26  meter
 Y    =       -4112364
12  meter          E    =           
0018521
 Z    =       -5031699
63                 I    =           51
60940
 XDOT =       7408
185617                 Wp   =           82
24478
 YDOT =        953
802811  meter/sec      RA   =          356
20219  deg
 ZDOT =       1820
462596                 TA   =          205
29425
                                          MA   =          205
38505
                                          Ha   =            192
712  n
mi
                                          Hp   =            181
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5775593
57                 X    =         1830697
98
 Y    =      -13492008
28  feet           Y    =        -4092285
78  meter
 Z    =      -16508200
87                 Z    =        -5022976
53
 XDOT =      24305
070921                 XDOT =        7388
126090
 YDOT =       3129
274314  feet/sec       YDOT =        1036
533588  meter/sec
 ZDOT =       5972
646311                 ZDOT =        1856
402166

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7862021
14                 X    =         2396344
04
 Y    =      -12438660
86  feet           Y    =        -3791303
83  meter
 Z    =      -16473639
68                 Z    =        -5021165
37
 XDOT =      22601
083459                 XDOT =        6888
810238
 YDOT =       6221
622172  feet/sec       YDOT =        1896
350438  meter/sec
 ZDOT =       6115
417015                 ZDOT =        1863
979106


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   10073
51271731  
00016717  00000-0  10270-3 0  9094
2 25544  51
6477 356
6567 0007826  44
8470 315
3324 15
73946891  8563


Satellite: ISS
Catalog Number: 25544
Epoch time:      10073
51271731   =   yrday
fracday
Element set:     909
Inclination:       51
6477  deg
RA of node:       356
6567  deg
Eccentricity:     
0007826     
Arg of perigee:    44
8470  deg
Mean anomaly:     315
3324  deg
Mean motion:   15
73946891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             856
Checksum:              331


Coasting Arc #11 (Orbit 871)
---------------------------------------

Vector Time (GMT): 2010/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6528655
20                 A    =         6731036
16  meter
 Y    =        -276955
74  meter          E    =           
0010670
 Z    =       -1620948
22                 I    =           51
61294
 XDOT =       1623
169391                 Wp   =           95
48682
 YDOT =      -4857
853679  meter/sec      RA   =          351
09571  deg
 ZDOT =      -5740
896374                 TA   =          102
40133
                                          MA   =          102
28189
                                          Ha   =            192
675  n
mi
                                          Hp   =            181
467

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21419472
45                 X    =        -6517198
82
 Y    =        -908647
44  feet           Y    =         -349899
18  meter
 Z    =       -5318071
59                 Z    =        -1652636
21
 XDOT =       5325
358894                 XDOT =        1705
258072
 YDOT =     -15937
840154  feet/sec       YDOT =       -4839
244125  meter/sec
 ZDOT =     -18834
961858                 ZDOT =       -5732
811145

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21067356
45                 X    =        -6421330
25
 Y    =       -3798869
00  feet           Y    =        -1157895
27  meter
 Z    =       -5443933
52                 Z    =        -1659310
94
 XDOT =       7268
830112                 XDOT =        2215
539418
 YDOT =     -13518
281891  feet/sec       YDOT =       -4120
372320  meter/sec
 ZDOT =     -18802
953338                 ZDOT =       -5731
140177


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   10074
52857132  
00016717  00000-0  10270-3 0  9103
2 25544  51
6482 351
4409 0007760  48
8461 311
3370 15
73977590  8723


Satellite: ISS
Catalog Number: 25544
Epoch time:      10074
52857132   =   yrday
fracday
Element set:     910
Inclination:       51
6482  deg
RA of node:       351
4409  deg
Eccentricity:     
0007760     
Arg of perigee:    48
8461  deg
Mean anomaly:     311
3370  deg
Mean motion:   15
73977590  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             872
Checksum:              310


Coasting Arc #12 (Orbit 887)
---------------------------------------

Vector Time (GMT): 2010/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1059537
20                 A    =         6721169
27  meter
 Y    =        4357839
64  meter          E    =           
0013451
 Z    =        4999156
04                 I    =           51
55010
 XDOT =      -7468
846185                 Wp   =           52
75244
 YDOT =        341
987132  meter/sec      RA   =          345
92603  deg
 ZDOT =      -1869
637793                 TA   =           55
35597
                                          MA   =           55
22924
                                          Ha   =            192
651  n
mi
                                          Hp   =            181
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3476171
92                 X    =        -1132473
44
 Y    =       14297374
15  feet           Y    =         4345584
05  meter
 Z    =       16401430
57                 Z    =         4993831
16
 XDOT =     -24504
088532                 XDOT =       -7463
032937
 YDOT =       1122
005026  feet/sec       YDOT =         258
498336  meter/sec
 ZDOT =      -6133
982260                 ZDOT =       -1905
907133

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5241094
62                 X    =        -1597485
64
 Y    =       13773880
72  feet           Y    =         4198278
84  meter
 Z    =       16380376
69                 Z    =         4992738
82
 XDOT =     -23423
801388                 XDOT =       -7139
574663
 YDOT =      -1402
218914  feet/sec       YDOT =        -427
396325  meter/sec
 ZDOT =      -6278
017866                 ZDOT =       -1913
539845


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   10075
54440146  
00016717  00000-0  10270-3 0  9110
2 25544  51
6477 346
2253 0007750  51
6906 308
4956 15
74048386  8888


Satellite: ISS
Catalog Number: 25544
Epoch time:      10075
54440146   =   yrday
fracday
Element set:     911
Inclination:       51
6477  deg
RA of node:       346
2253  deg
Eccentricity:     
0007750     
Arg of perigee:    51
6906  deg
Mean anomaly:     308
4956  deg
Mean motion:   15
74048386  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             888
Checksum:              322


Coasting Arc #13 (Orbit 903)
---------------------------------------

Vector Time (GMT): 2010/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6457965
49                 A    =         6730834
89  meter
 Y    =        -864372
81  meter          E    =           
0021871
 Z    =        1644813
85                 I    =           51
55410
 XDOT =       -789
999054                 Wp   =           60
67492
 YDOT =       5092
747711  meter/sec      RA   =          340
81532  deg
 ZDOT =       5731
628990                 TA   =          317
53633
                                          MA   =          317
70532
                                          Ha   =            192
649  n
mi
                                          Hp   =            181
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21187550
82                 X    =         6459160
89
 Y    =       -2835868
79  feet           Y    =         -792149
13  meter
 Z    =        5396370
89                 Z    =         1676189
58
 XDOT =      -2591
860414                 XDOT =        -874
731523
 YDOT =      16708
489864  feet/sec       YDOT =        5083
440342  meter/sec
 ZDOT =      18804
557054                 ZDOT =        5727
584804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21333922
73                 X    =         6502579
65
 Y    =        -676827
62  feet           Y    =         -206297
06  meter
 Z    =        5520953
33                 Z    =         1682786
58
 XDOT =      -4431
460005                 XDOT =       -1350
709009
 YDOT =      14793
256607  feet/sec       YDOT =        4508
984614  meter/sec
 ZDOT =      18788
605676                 ZDOT =        5726
767010


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   10076
56021078  
00016717  00000-0  10270-3 0  9123
2 25544  51
6481 341
0090 0007814  55
6910 304
4992 15
74041996  9040


Satellite: ISS
Catalog Number: 25544
Epoch time:      10076
56021078   =   yrday
fracday
Element set:     912
Inclination:       51
6481  deg
RA of node:       341
0090  deg
Eccentricity:     
0007814     
Arg of perigee:    55
6910  deg
Mean anomaly:     304
4992  deg
Mean motion:   15
74041996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             904
Checksum:              297


Coasting Arc #14 (Orbit 918)
---------------------------------------

Vector Time (GMT): 2010/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         336948
01                 A    =         6721127
74  meter
 Y    =       -4509452
93  meter          E    =           
0019180
 Z    =       -4988641
75                 I    =           51
49402
 XDOT =       7265
349012                 Wp   =           87
60263
 YDOT =      -1595
314098  meter/sec      RA   =          335
63974  deg
 ZDOT =       1939
998257                 TA   =          201
17143
                                          MA   =          201
25091
                                          Ha   =            192
598  n
mi
                                          Hp   =            181
105

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1105472
46                 X    =          411582
43
 Y    =      -14794793
06  feet           Y    =        -4505268
15  meter
 Z    =      -16366934
87                 Z    =        -4986823
13
 XDOT =      23836
446891                 XDOT =        7273
223943
 YDOT =      -5233
970137  feet/sec       YDOT =       -1514
024429  meter/sec
 ZDOT =       6364
823679                 ZDOT =        1975
312653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2443669
49                 X    =          744830
46
 Y    =      -14641368
43  feet           Y    =        -4462689
10  meter
 Z    =      -16359808
62                 Z    =        -4986469
67
 XDOT =      23087
214121                 XDOT =        7036
982864
 YDOT =      -3388
811693  feet/sec       YDOT =       -1032
909804  meter/sec
 ZDOT =       6505
025678                 ZDOT =        1982
731827


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   10077
51250883  
00016717  00000-0  10270-3 0  9138
2 25544  51
6484 336
1187 0007699  58
9131 301
2787 15
74095011  9197


Satellite: ISS
Catalog Number: 25544
Epoch time:      10077
51250883   =   yrday
fracday
Element set:     913
Inclination:       51
6484  deg
RA of node:       336
1187  deg
Eccentricity:     
0007699     
Arg of perigee:    58
9131  deg
Mean anomaly:     301
2787  deg
Mean motion:   15
74095011  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             919
Checksum:              319


Coasting Arc #15 (Orbit 934)
---------------------------------------

Vector Time (GMT): 2010/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6212427
15                 A    =         6730469
65  meter
 Y    =        1892948
05  meter          E    =           
0011521
 Z    =       -1770970
43                 I    =           51
49874
 XDOT =         24
083950                 Wp   =          101
52850
 YDOT =      -5197
629223  meter/sec      RA   =          330
52576  deg
 ZDOT =      -5673
470392                 TA   =           98
11521
                                          MA   =           97
98449
                                          Ha   =            192
552  n
mi
                                          Hp   =            181
065

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20381978
83                 X    =        -6224529
62
 Y    =        6210459
49  feet           Y    =         1823409
20  meter
 Z    =       -5810270
44                 Z    =        -1801180
04
 XDOT =         79
015583                 XDOT =         109
763768
 YDOT =     -17052
589315  feet/sec       YDOT =       -5196
881271  meter/sec
 ZDOT =     -18613
748006                 ZDOT =       -5673
144881

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20718207
58                 X    =        -6314909
67
 Y    =        4831440
04  feet           Y    =         1472622
92  meter
 Z    =       -5930191
62                 Z    =        -1807522
40
 XDOT =       1684
286129                 XDOT =         513
370412
 YDOT =     -15491
174275  feet/sec       YDOT =       -4721
709919  meter/sec
 ZDOT =     -18612
563857                 ZDOT =       -5673
109464


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   10078
52827227  
00016717  00000-0  10270-3 0  9143
2 25544  51
6484 330
9019 0007531  63
1550 297
0382 15
74098218  9354


Satellite: ISS
Catalog Number: 25544
Epoch time:      10078
52827227   =   yrday
fracday
Element set:     914
Inclination:       51
6484  deg
RA of node:       330
9019  deg
Eccentricity:     
0007531     
Arg of perigee:    63
1550  deg
Mean anomaly:     297
0382  deg
Mean motion:   15
74098218  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             935
Checksum:              311

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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