Date: February 25th 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 572)
---------------------------------------

Vector Time (GMT): 2010/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3444208
30                 A    =         6726083
88  meter
 Y    =       -3908371
07  meter          E    =           
0011945
 Z    =        4255128
79                 I    =           51
97590
 XDOT =       2637
316512                 Wp   =           34
46692
 YDOT =      -6267
798588  meter/sec      RA   =           88
30870  deg
 ZDOT =      -3607
788297                 TA   =           92
11072
                                          MA   =           91
97393
                                          Ha   =            191
822  n
mi
                                          Hp   =            185
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11299896
00                 X    =        -3420918
41
 Y    =      -12822739
71  feet           Y    =        -3946756
05  meter
 Z    =       13960396
29                 Z    =         4238453
74
 XDOT =       8652
613227                 XDOT =        2724
733736
 YDOT =     -20563
643663  feet/sec       YDOT =       -6237
817754  meter/sec
 ZDOT =     -11836
575776                 ZDOT =       -3594
764201

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4460159
91                 X    =        -1359456
74
 Y    =      -16554922
73  feet           Y    =        -5045940
45  meter
 Z    =       13894044
59                 Z    =         4234904
79
 XDOT =      15777
903159                 XDOT =        4809
104883
 YDOT =     -14181
824666  feet/sec       YDOT =       -4322
620158  meter/sec
 ZDOT =     -11785
028265                 ZDOT =       -3592
076615


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   10055
54121520  
00016717  00000-0  10270-3 0  9008
2 25544  51
6451  88
8859 0007492 337
9458  22
1381 15
73404053  5735


Satellite: ISS
Catalog Number: 25544
Epoch time:      10055
54121520   =   yrday
fracday
Element set:     900
Inclination:       51
6451  deg
RA of node:        88
8859  deg
Eccentricity:     
0007492     
Arg of perigee:   337
9458  deg
Mean anomaly:      22
1381  deg
Mean motion:   15
73404053  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             573
Checksum:              297


Coasting Arc #2 (Orbit 588)
---------------------------------------

Vector Time (GMT): 2010/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1671948
98                 A    =         6730061
82  meter
 Y    =        5780699
72  meter          E    =           
0014068
 Z    =        2993337
32                 I    =           51
98683
 XDOT =      -4398
885928                 Wp   =           51
48350
 YDOT =      -3868
664491  meter/sec      RA   =           83
25051  deg
 ZDOT =       5006
961927                 TA   =          342
93854
                                          MA   =          342
98579
                                          Ha   =            192
071  n
mi
                                          Hp   =            184
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5485396
92                 X    =        -1751006
24
 Y    =       18965550
26  feet           Y    =         5761560
99  meter
 Z    =        9820660
51                 Z    =         2985023
13
 XDOT =     -14432
040447                 XDOT =       -4379
621167
 YDOT =     -12692
468802  feet/sec       YDOT =       -3917
747680  meter/sec
 ZDOT =      16427
040443                 ZDOT =        4985
639542

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13175673
56                 X    =        -4015945
30
 Y    =       14725067
34  feet           Y    =         4488200
53  meter
 Z    =        9787801
95                 Z    =         2983322
03
 XDOT =      -6566
032979                 XDOT =       -2001
326852
 YDOT =     -16753
483292  feet/sec       YDOT =       -5106
461707  meter/sec
 ZDOT =      16342
225366                 ZDOT =        4981
110292


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   10056
55744440  
00016717  00000-0  10270-3 0  9013
2 25544  51
6449  83
6720 0007500 343
4314  16
6603 15
73383520  5892


Satellite: ISS
Catalog Number: 25544
Epoch time:      10056
55744440   =   yrday
fracday
Element set:     901
Inclination:       51
6449  deg
RA of node:        83
6720  deg
Eccentricity:     
0007500     
Arg of perigee:   343
4314  deg
Mean anomaly:      16
6603  deg
Mean motion:   15
73383520  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             589
Checksum:              289


Coasting Arc #3 (Orbit 603)
---------------------------------------

Vector Time (GMT): 2010/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4167615
54                 A    =         6725240
59  meter
 Y    =        2808840
45  meter          E    =           
0008131
 Z    =       -4472710
96                 I    =           51
96704
 XDOT =      -1151
715616                 Wp   =           60
77989
 YDOT =       6877
925264  meter/sec      RA   =           78
09612  deg
 ZDOT =       3254
436306                 TA   =          241
65177
                                          MA   =          241
73380
                                          Ha   =            192
140  n
mi
                                          Hp   =            184
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13673279
33                 X    =         4157623
82
 Y    =        9215355
82  feet           Y    =         2855389
17  meter
 Z    =      -14674248
57                 Z    =        -4452489
66
 XDOT =      -3778
594542                 XDOT =       -1244
349198
 YDOT =      22565
371601  feet/sec       YDOT =        6864
528275  meter/sec
 ZDOT =      10677
284469                 ZDOT =        3248
616182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8688176
46                 X    =         2648156
19
 Y    =       14097889
98  feet           Y    =         4297036
87  meter
 Z    =      -14593834
64                 Z    =        -4448200
80
 XDOT =     -11839
780937                 XDOT =       -3608
765230
 YDOT =      18297
429334  feet/sec       YDOT =        5577
056461  meter/sec
 ZDOT =      10654
363292                 ZDOT =        3247
449931


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   10057
51013987  
00016717  00000-0  10270-3 0  9026
2 25544  51
6458  78
7845 0007567 345
7932  14
3017 15
73415977  6043


Satellite: ISS
Catalog Number: 25544
Epoch time:      10057
51013987   =   yrday
fracday
Element set:     902
Inclination:       51
6458  deg
RA of node:        78
7845  deg
Eccentricity:     
0007567     
Arg of perigee:   345
7932  deg
Mean anomaly:      14
3017  deg
Mean motion:   15
73415977  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             604
Checksum:              323


Coasting Arc #4 (Orbit 619)
---------------------------------------

Vector Time (GMT): 2010/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         339210
07                 A    =         6730546
62  meter
 Y    =       -6154738
14  meter          E    =           
0005445
 Z    =       -2711776
51                 I    =           51
97665
 XDOT =       5042
082239                 Wp   =           29
87391
 YDOT =       2572
393925  meter/sec      RA   =           73
03373  deg
 ZDOT =      -5207
530252                 TA   =          180
86851
                                          MA   =          180
86946
                                          Ha   =            192
109  n
mi
                                          Hp   =            184
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1112893
93                 X    =          421181
17
 Y    =      -20192710
43  feet           Y    =        -6150486
75  meter
 Z    =       -8896904
56                 Z    =        -2709929
15
 XDOT =      16542
264563                 XDOT =        5038
239038
 YDOT =       8439
612616  feet/sec       YDOT =        2628
755634  meter/sec
 ZDOT =     -17085
073004                 ZDOT =       -5183
046049

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9138868
38                 X    =         2785527
08
 Y    =      -18044182
72  feet           Y    =        -5499866
89  meter
 Z    =       -8889744
26                 Z    =        -2709594
05
 XDOT =      10566
475268                 XDOT =        3220
661662
 YDOT =      13721
141996  feet/sec       YDOT =        4182
204080  meter/sec
 ZDOT =     -16987
728583                 ZDOT =       -5177
859672


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   10058
52633159  
00016717  00000-0  10270-3 0  9038
2 25544  51
6445  73
5699 0007495 349
8804  10
2206 15
73452114  6209


Satellite: ISS
Catalog Number: 25544
Epoch time:      10058
52633159   =   yrday
fracday
Element set:     903
Inclination:       51
6445  deg
RA of node:        73
5699  deg
Eccentricity:     
0007495     
Arg of perigee:   349
8804  deg
Mean anomaly:      10
2206  deg
Mean motion:   15
73452114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             620
Checksum:              301


Coasting Arc #5 (Orbit 635)
---------------------------------------

Vector Time (GMT): 2010/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4586719
70                 A    =         6724401
98  meter
 Y    =       -1670648
34  meter          E    =           
0012997
 Z    =        4624349
49                 I    =           51
94555
 XDOT =       -397
692500                 Wp   =           30
97750
 YDOT =      -7102
511047  meter/sec      RA   =           67
87956  deg
 ZDOT =      -2945
852299                 TA   =           88
16792
                                          MA   =           88
01907
                                          Ha   =            192
257  n
mi
                                          Hp   =            184
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15048292
98                 X    =        -4590161
00
 Y    =       -5481129
72  feet           Y    =        -1721958
56  meter
 Z    =       15171750
29                 Z    =         4602059
58
 XDOT =      -1304
765421                 XDOT =        -303
931347
 YDOT =     -23302
201597  feet/sec       YDOT =       -7106
434317  meter/sec
 ZDOT =      -9664
869747                 ZDOT =       -2947
555818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11873743
57                 X    =        -3619117
04
 Y    =      -10871462
86  feet           Y    =        -3313621
88  meter
 Z    =       15083150
22                 Z    =         4597344
19
 XDOT =       6999
743910                 XDOT =        2133
521944
 YDOT =     -21130
449929  feet/sec       YDOT =       -6440
561138  meter/sec
 ZDOT =      -9671
841994                 ZDOT =       -2947
977440


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   10059
54250400  
00016717  00000-0  10270-3 0  9046
2 25544  51
6437  68
3551 0007597 353
8425   6
2643 15
73504010  6366


Satellite: ISS
Catalog Number: 25544
Epoch time:      10059
54250400   =   yrday
fracday
Element set:     904
Inclination:       51
6437  deg
RA of node:        68
3551  deg
Eccentricity:     
0007597     
Arg of perigee:   353
8425  deg
Mean anomaly:       6
2643  deg
Mean motion:   15
73504010  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             636
Checksum:              286


Coasting Arc #6 (Orbit 651)
---------------------------------------

Vector Time (GMT): 2010/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1033919
48                 A    =         6730922
52  meter
 Y    =        6178678
46  meter          E    =           
0017184
 Z    =        2432201
33                 I    =           51
95531
 XDOT =      -5371
833551                 Wp   =           48
99045
 YDOT =      -1227
865928  meter/sec      RA   =           62
81321  deg
 ZDOT =       5389
304757                 TA   =          338
36894
                                          MA   =          338
44144
                                          Ha   =            192
248  n
mi
                                          Hp   =            184
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3392124
29                 X    =          952936
60
 Y    =       20271254
80  feet           Y    =         6189787
83  meter
 Z    =        7979663
16                 Z    =         2437026
63
 XDOT =     -17624
125824                 XDOT =       -5383
883848
 YDOT =      -4028
431523  feet/sec       YDOT =       -1288
003749  meter/sec
 ZDOT =      17681
446052                 ZDOT =        5363
179770

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4347704
99                 X    =        -1325180
48
 Y    =       20080305
24  feet           Y    =         6120477
04  meter
 Z    =        7999006
52                 Z    =         2438097
19
 XDOT =     -13538
042775                 XDOT =       -4126
395438
 YDOT =      -9950
823136  feet/sec       YDOT =       -3033
010892  meter/sec
 ZDOT =      17577
626171                 ZDOT =        5357
660457


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   10060
55865778  
00016717  00000-0  10270-3 0  9050
2 25544  51
6436  63
1410 0007576 357
2460   2
8660 15
73533932  6520


Satellite: ISS
Catalog Number: 25544
Epoch time:      10060
55865778   =   yrday
fracday
Element set:     905
Inclination:       51
6436  deg
RA of node:        63
1410  deg
Eccentricity:     
0007576     
Arg of perigee:   357
2460  deg
Mean anomaly:       2
8660  deg
Mean motion:   15
73533932  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             652
Checksum:              304


Coasting Arc #7 (Orbit 666)
---------------------------------------

Vector Time (GMT): 2010/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4724093
90                 A    =         6723781
29  meter
 Y    =         475872
10  meter          E    =           
0011647
 Z    =       -4768470
55                 I    =           51
91615
 XDOT =       1955
311380                 Wp   =           69
40769
 YDOT =       6956
411997  meter/sec      RA   =           57
66038  deg
 ZDOT =       2640
497376                 TA   =          226
39613
                                          MA   =          226
49283
                                          Ha   =            192
464  n
mi
                                          Hp   =            183
994

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15498995
73                 X    =         4741585
56
 Y    =        1561260
16  feet           Y    =          528797
01  meter
 Z    =      -15644588
42                 Z    =        -4745478
78
 XDOT =       6415
063582                 XDOT =        1864
551333
 YDOT =      22822
874007  feet/sec       YDOT =        6977
770268  meter/sec
 ZDOT =       8663
049135                 ZDOT =        2649
774950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14044427
33                 X    =         4280741
45
 Y    =        6946964
98  feet           Y    =         2117434
93  meter
 Z    =      -15553240
41                 Z    =        -4740627
68
 XDOT =      -1567
102972                 XDOT =        -477
652986
 YDOT =      22578
687278  feet/sec       YDOT =        6881
983882  meter/sec
 ZDOT =       8700
092945                 ZDOT =        2651
788330


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   10061
51128538  
00016717  00000-0  10270-3 0  9064
2 25544  51
6436  58
2522 0007695    
9919 359
1258 15
73520918  6679


Satellite: ISS
Catalog Number: 25544
Epoch time:      10061
51128538   =   yrday
fracday
Element set:     906
Inclination:       51
6436  deg
RA of node:        58
2522  deg
Eccentricity:     
0007695     
Arg of perigee:      
9919  deg
Mean anomaly:     359
1258  deg
Mean motion:   15
73520918  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             667
Checksum:              317


Coasting Arc #8 (Orbit 682)
---------------------------------------

Vector Time (GMT): 2010/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2348506
86                 A    =         6731246
03  meter
 Y    =       -5914021
59  meter          E    =           
0005836
 Z    =       -2205361
18                 I    =           51
92461
 XDOT =       5369
103712                 Wp   =           56
11180
 YDOT =        -81
321615  meter/sec      RA   =           52
58738  deg
 ZDOT =      -5506
696877                 TA   =          148
46990
                                          MA   =          148
43492
                                          Ha   =            192
446  n
mi
                                          Hp   =            183
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7705075
00                 X    =        -2271487
52
 Y    =      -19402957
99  feet           Y    =        -5939853
56  meter
 Z    =       -7235436
93                 Z    =        -2216582
50
 XDOT =      17615
169660                 XDOT =        5396
364319
 YDOT =       -266
803200  feet/sec       YDOT =         -21
129194  meter/sec
 ZDOT =     -18066
590804                 ZDOT =       -5480
547789

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -703779
68                 X    =         -214512
05
 Y    =      -20849422
29  feet           Y    =        -6354903
91  meter
 Z    =       -7280164
24                 Z    =        -2218994
06
 XDOT =      15261
947637                 XDOT =        4651
841640
 YDOT =       5748
852013  feet/sec       YDOT =        1752
250094  meter/sec
 ZDOT =     -17962
718148                 ZDOT =       -5475
036492


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   10062
52740241  
00016717  00000-0  10270-3 0  9078
2 25544  51
6434  53
0370 0007728   5
4915 354
6331 15
73573956  6834


Satellite: ISS
Catalog Number: 25544
Epoch time:      10062
52740241   =   yrday
fracday
Element set:     907
Inclination:       51
6434  deg
RA of node:        53
0370  deg
Eccentricity:     
0007728     
Arg of perigee:     5
4915  deg
Mean anomaly:     354
6331  deg
Mean motion:   15
73573956  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             683
Checksum:              296


Coasting Arc #9 (Orbit 698)
---------------------------------------

Vector Time (GMT): 2010/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4609923
73                 A    =         6723156
37  meter
 Y    =         611290
43  meter          E    =           
0013306
 Z    =        4853676
00                 I    =           51
87818
 XDOT =      -3398
535326                 Wp   =           31
71910
 YDOT =      -6481
728877  meter/sec      RA   =           47
43507  deg
 ZDOT =      -2397
487980                 TA   =           81
66677
                                          MA   =           81
51593
                                          Ha   =            192
570  n
mi
                                          Hp   =            183
468

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15124421
70                 X    =        -4639994
79
 Y    =        2005546
03  feet           Y    =          559571
73  meter
 Z    =       15924133
87                 Z    =         4831208
07
 XDOT =     -11150
050283                 XDOT =       -3314
156411
 YDOT =     -21265
514688  feet/sec       YDOT =       -6519
261700  meter/sec
 ZDOT =      -7865
774213                 ZDOT =       -2413
792533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15061160
63                 X    =        -4590641
76
 Y    =       -2960712
51  feet           Y    =         -902425
17  meter
 Z    =       15834898
41                 Z    =         4826477
04
 XDOT =      -3944
075077                 XDOT =       -1202
154084
 YDOT =     -22600
264640  feet/sec       YDOT =       -6888
560662  meter/sec
 ZDOT =      -7930
697064                 ZDOT =       -2417
276465


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   10063
54349903  
00016717  00000-0  10270-3 0  9082
2 25544  51
6434  47
8224 0007767   7
9823 352
1462 15
73608816  6990


Satellite: ISS
Catalog Number: 25544
Epoch time:      10063
54349903   =   yrday
fracday
Element set:     908
Inclination:       51
6434  deg
RA of node:        47
8224  deg
Eccentricity:     
0007767     
Arg of perigee:     7
9823  deg
Mean anomaly:     352
1462  deg
Mean motion:   15
73608816  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             699
Checksum:              326


Coasting Arc #10 (Orbit 714)
---------------------------------------

Vector Time (GMT): 2010/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3557165
22                 A    =         6731356
67  meter
 Y    =        5345934
22  meter          E    =           
0019349
 Z    =        1980561
98                 I    =           51
88578
 XDOT =      -5109
659827                 Wp   =           49
05158
 YDOT =       1308
883689  meter/sec      RA   =           42
35748  deg
 ZDOT =       5621
230116                 TA   =          332
94872
                                          MA   =          333
04942
                                          Ha   =            192
397  n
mi
                                          Hp   =            183
191

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11670489
57                 X    =         3487500
51
 Y    =       17539154
26  feet           Y    =         5385323
13  meter
 Z    =        6497906
75                 Z    =         1997673
08
 XDOT =     -16763
975809                 XDOT =       -5151
222957
 YDOT =       4294
237826  feet/sec       YDOT =        1251
512325  meter/sec
 ZDOT =      18442
356024                 ZDOT =        5596
306552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5768405
82                 X    =         1758210
09
 Y    =       20240015
36  feet           Y    =         6169156
68  meter
 Z    =        6565997
54                 Z    =         2001316
05
 XDOT =     -15904
195860                 XDOT =       -4847
598898
 YDOT =      -1442
218954  feet/sec       YDOT =        -439
588337  meter/sec
 ZDOT =      18343
380936                 ZDOT =        5591
062509


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
55957479  
00016717  00000-0  10270-3 0  9098
2 25544  51
6438  42
6083 0007585  12
1418 347
9927 15
73678707  7159


Satellite: ISS
Catalog Number: 25544
Epoch time:      10064
55957479   =   yrday
fracday
Element set:     909
Inclination:       51
6438  deg
RA of node:        42
6083  deg
Eccentricity:     
0007585     
Arg of perigee:    12
1418  deg
Mean anomaly:     347
9927  deg
Mean motion:   15
73678707  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             715
Checksum:              341


Coasting Arc #11 (Orbit 729)
---------------------------------------

Vector Time (GMT): 2010/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4262888
93                 A    =         6722692
68  meter
 Y    =       -1641618
28  meter          E    =           
0014736
 Z    =       -4943017
37                 I    =           51
83322
 XDOT =       4691
945386                 Wp   =           73
62112
 YDOT =       5697
128878  meter/sec      RA   =           37
20467  deg
 ZDOT =       2163
659339                 TA   =          217
29374
                                          MA   =          217
39615
                                          Ha   =            192
668  n
mi
                                          Hp   =            183
156

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13985856
08                 X    =         4304941
03
 Y    =       -5385886
74  feet           Y    =        -1593713
16  meter
 Z    =      -16217248
59                 Z    =        -4922206
26
 XDOT =      15393
521607                 XDOT =        4617
379793
 YDOT =      18691
367709  feet/sec       YDOT =        5749
180150  meter/sec
 ZDOT =       7098
619877                 ZDOT =        2186
271287

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15034065
42                 X    =         4582383
14
 Y    =       -1123477
02  feet           Y    =         -342435
80  meter
 Z    =      -16134614
17                 Z    =        -4917830
40
 XDOT =       9266
780439                 XDOT =        2824
514678
 YDOT =      21211
643592  feet/sec       YDOT =        6465
308967  meter/sec
 ZDOT =       7188
562619                 ZDOT =        2191
073886


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
51213044  
00016717  00000-0  10270-3 0  9100
2 25544  51
6440  37
7193 0007831  15
6075 344
5329 15
73644847  7304


Satellite: ISS
Catalog Number: 25544
Epoch time:      10065
51213044   =   yrday
fracday
Element set:     910
Inclination:       51
6440  deg
RA of node:        37
7193  deg
Eccentricity:     
0007831     
Arg of perigee:    15
6075  deg
Mean anomaly:     344
5329  deg
Mean motion:   15
73644847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             730
Checksum:              288


Coasting Arc #12 (Orbit 745)
---------------------------------------

Vector Time (GMT): 2010/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4590315
25                 A    =         6731513
94  meter
 Y    =       -4576436
86  meter          E    =           
0007309
 Z    =       -1826588
25                 I    =           51
83962
 XDOT =       4615
863638                 Wp   =           75
23840
 YDOT =      -2370
393849  meter/sec      RA   =           32
11971  deg
 ZDOT =      -5677
995956                 TA   =          124
94086
                                          MA   =          124
87218
                                          Ha   =            192
633  n
mi
                                          Hp   =            182
797

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15060089
39                 X    =        -4529926
43
 Y    =      -15014556
62  feet           Y    =        -4627430
88  meter
 Z    =       -5992743
61                 Z    =        -1848740
92
 XDOT =      15143
909572                 XDOT =        4669
609071
 YDOT =      -7776
882706  feet/sec       YDOT =       -2318
476152  meter/sec
 ZDOT =     -18628
595655                 ZDOT =       -5655
441773

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10409600
86                 X    =        -3172846
34
 Y    =      -18515394
56  feet           Y    =        -5643492
26  meter
 Z    =       -6080834
90                 Z    =        -1853438
48
 XDOT =      15436
941148                 XDOT =        4705
179662
 YDOT =      -2608
300456  feet/sec       YDOT =        -795
009979  meter/sec
 ZDOT =     -18539
048804                 ZDOT =       -5650
702075


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
52816774  
00016717  00000-0  10270-3 0  9112
2 25544  51
6447  32
5041 0007903  19
1761 340
9698 15
73706129  7465


Satellite: ISS
Catalog Number: 25544
Epoch time:      10066
52816774   =   yrday
fracday
Element set:     911
Inclination:       51
6447  deg
RA of node:        32
5041  deg
Eccentricity:     
0007903     
Arg of perigee:    19
1761  deg
Mean anomaly:     340
9698  deg
Mean motion:   15
73706129  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             746
Checksum:              311


Coasting Arc #13 (Orbit 761)
---------------------------------------

Vector Time (GMT): 2010/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3768007
94                 A    =         6722251
27  meter
 Y    =        2482093
52  meter          E    =           
0013293
 Z    =        4979380
14                 I    =           51
78233
 XDOT =      -5763
146145                 Wp   =           36
65647
 YDOT =      -4702
494222  meter/sec      RA   =           26
96591  deg
 ZDOT =      -2003
835685                 TA   =           72
75094
                                          MA   =           72
60550
                                          Ha   =            192
761  n
mi
                                          Hp   =            182
668

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12362230
77                 X    =        -3819671
64
 Y    =        8143351
43  feet           Y    =         2439668
67  meter
 Z    =       16336549
00                 Z    =         4960949
90
 XDOT =     -18907
959793                 XDOT =       -5700
399575
 YDOT =     -15428
130650  feet/sec       YDOT =       -4766
590358  meter/sec
 ZDOT =      -6574
264059                 ZDOT =       -2031
680065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14115844
27                 X    =        -4302509
33
 Y    =        4718796
52  feet           Y    =         1438289
18  meter
 Z    =       16263383
88                 Z    =         4957079
41
 XDOT =     -13996
334153                 XDOT =       -4266
082650
 YDOT =     -18679
088067  feet/sec       YDOT =       -5693
386043  meter/sec
 ZDOT =      -6684
966228                 ZDOT =       -2037
577706


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
54418451  
00016717  00000-0  10270-3 0  9126
2 25544  51
6447  27
2894 0007853  22
6650 337
4859 15
73728098  7629


Satellite: ISS
Catalog Number: 25544
Epoch time:      10067
54418451   =   yrday
fracday
Element set:     912
Inclination:       51
6447  deg
RA of node:        27
2894  deg
Eccentricity:     
0007853     
Arg of perigee:    22
6650  deg
Mean anomaly:     337
4859  deg
Mean motion:   15
73728098  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             762
Checksum:              329


Coasting Arc #14 (Orbit 777)
---------------------------------------

Vector Time (GMT): 2010/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5424342
93                 A    =         6731558
21  meter
 Y    =        3596481
97  meter          E    =           
0020803
 Z    =        1672210
81                 I    =           51
78710
 XDOT =      -3957
742820                 Wp   =           50
71933
 YDOT =       3283
067031  meter/sec      RA   =           21
87504  deg
 ZDOT =       5742
849920                 TA   =          327
74529
                                          MA   =          327
87234
                                          Ha   =            192
617  n
mi
                                          Hp   =            182
438

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17796400
71                 X    =         5375600
15
 Y    =       11799481
53  feet           Y    =         3656867
71  meter
 Z    =        5486255
93                 Z    =         1698443
23
 XDOT =     -12984
720539                 XDOT =       -4022
057694
 YDOT =      10771
217292  feet/sec       YDOT =        3238
449785  meter/sec
 ZDOT =      18841
371130                 ZDOT =        5723
467259

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14463187
42                 X    =         4408379
52
 Y    =       15671655
77  feet           Y    =         4776720
68  meter
 Z    =        5590533
23                 Z    =         1703994
53
 XDOT =     -14131
367788                 XDOT =       -4307
240902
 YDOT =       6308
426513  feet/sec       YDOT =        1922
808401  meter/sec
 ZDOT =      18764
436499                 ZDOT =        5719
400245


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
56017913  
00016717  00000-0  10270-3 0  9138
2 25544  51
6450  22
0743 0007784  26
6021 333
5540 15
73776870  7780


Satellite: ISS
Catalog Number: 25544
Epoch time:      10068
56017913   =   yrday
fracday
Element set:     913
Inclination:       51
6450  deg
RA of node:        22
0743  deg
Eccentricity:     
0007784     
Arg of perigee:    26
6021  deg
Mean anomaly:     333
5540  deg
Mean motion:   15
73776870  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             778
Checksum:              302


Coasting Arc #15 (Orbit 792)
---------------------------------------

Vector Time (GMT): 2010/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 800608
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3121637
06                 A    =         6721887
08  meter
 Y    =       -3205715
30  meter          E    =           
0017024
 Z    =       -5029413
77                 I    =           51
72652
 XDOT =       6584
448094                 Wp   =           77
30218
 YDOT =       3509
231286  meter/sec      RA   =           16
71861  deg
 ZDOT =       1858
976291                 TA   =          210
58393
                                          MA   =          210
68329
                                          Ha   =            192
725  n
mi
                                          Hp   =            182
389

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10241591
42                 X    =         3181683
39
 Y    =      -10517438
64  feet           Y    =        -3170471
80  meter
 Z    =      -16500701
35                 Z    =        -5014103
19
 XDOT =      21602
519994                 XDOT =        6535
687500
 YDOT =      11513
226005  feet/sec       YDOT =        3582
589949  meter/sec
 ZDOT =       6099
003579                 ZDOT =        1890
844237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12400154
88                 X    =         3779567
21
 Y    =       -7984004
23  feet           Y    =        -2433524
49  meter
 Z    =      -16439941
93                 Z    =        -5010894
30
 XDOT =      17920
603884                 XDOT =        5462
200064
 YDOT =      15074
136505  feet/sec       YDOT =        4594
596807  meter/sec
 ZDOT =       6225
666468                 ZDOT =        1897
583139


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
51265564  
00016717  00000-0  10270-3 0  9142
2 25544  51
6454  17
1849 0007858  29
4274 330
7331 15
73789114  7938


Satellite: ISS
Catalog Number: 25544
Epoch time:      10069
51265564   =   yrday
fracday
Element set:     914
Inclination:       51
6454  deg
RA of node:        17
1849  deg
Eccentricity:     
0007858     
Arg of perigee:    29
4274  deg
Mean anomaly:     330
7331  deg
Mean motion:   15
73789114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             793
Checksum:              324

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