Date: October 7th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2332)
---------------------------------------

Vector Time (GMT): 2009/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3829572
25                 A    =         6718744
01  meter
 Y    =        1846411
07  meter          E    =           
0019273
 Z    =       -5218040
87                 I    =           51
94664
 XDOT =      -2082
586099                 Wp   =          122
21199
 YDOT =       7325
432145  meter/sec      RA   =           99
63614  deg
 ZDOT =       1056
473379                 TA   =          157
87917
                                          MA   =          157
79589
                                          Ha   =            191
317  n
mi
                                          Hp   =            181
626

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12564213
41                 X    =         3833989
68
 Y    =        6057779
10  feet           Y    =         1889259
90  meter
 Z    =      -17119556
65                 Z    =        -5199425
74
 XDOT =      -6832
631558                 XDOT =       -2169
477854
 YDOT =      24033
570028  feet/sec       YDOT =        7301
657684  meter/sec
 ZDOT =       3466
120011                 ZDOT =        1046
144290

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13729485
86                 X    =        -4184747
29
 Y    =       -2927162
67  feet           Y    =         -892199
18  meter
 Z    =      -17046064
15                 Z    =        -5195640
35
 XDOT =        827
323133                 XDOT =         252
168091
 YDOT =     -23968
651811  feet/sec       YDOT =       -7305
645072  meter/sec
 ZDOT =       3425
802099                 ZDOT =        1044
184480


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   09278
51413793  
00020000  00000-0  20000-3 0  9008
2 25544  51
6363 100
3830 0008459 166
4947 193
6444 15
74606682 23331


Satellite: ISS
Catalog Number: 25544
Epoch time:      09278
51413793   =   yrday
fracday
Element set:     900
Inclination:       51
6363  deg
RA of node:       100
3830  deg
Eccentricity:     
0008459     
Arg of perigee:   166
4947  deg
Mean anomaly:     193
6444  deg
Mean motion:   15
74606682  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2333
Checksum:              301


Coasting Arc #2 (Orbit 2348)
---------------------------------------

Vector Time (GMT): 2009/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1416284
58                 A    =         6729733
97  meter
 Y    =       -6467925
90  meter          E    =           
0017132
 Z    =       -1151466
60                 I    =           51
98860
 XDOT =       4486
818284                 Wp   =          155
29733
 YDOT =       2029
529674  meter/sec      RA   =           94
53894  deg
 ZDOT =      -5927
994164                 TA   =           37
26264
                                          MA   =           37
14389
                                          Ha   =            191
083  n
mi
                                          Hp   =            181
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4646602
95                 X    =         1494098
55
 Y    =      -21220229
33  feet           Y    =        -6451653
15  meter
 Z    =       -3777777
55                 Z    =        -1144396
74
 XDOT =      14720
532427                 XDOT =        4492
588172
 YDOT =       6658
561923  feet/sec       YDOT =        2079
735869  meter/sec
 ZDOT =     -19448
799751                 ZDOT =       -5906
182697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         798330
64                 X    =          243331
18
 Y    =       21713105
90  feet           Y    =         6618154
68  meter
 Z    =       -3750247
36                 Z    =        -1143075
39
 XDOT =     -14445
641523                 XDOT =       -4403
031536
 YDOT =      -2786
566229  feet/sec       YDOT =        -849
345387  meter/sec
 ZDOT =     -19362
697006                 ZDOT =       -5901
750047


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   09279
52956944  
00020000  00000-0  20000-3 0  9011
2 25544  51
6369  95
1632 0008221 170
2738 189
8586 15
74660228 23493


Satellite: ISS
Catalog Number: 25544
Epoch time:      09279
52956944   =   yrday
fracday
Element set:     901
Inclination:       51
6369  deg
RA of node:        95
1632  deg
Eccentricity:     
0008221     
Arg of perigee:   170
2738  deg
Mean anomaly:     189
8586  deg
Mean motion:   15
74660228  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2349
Checksum:              326


Coasting Arc #3 (Orbit 2364)
---------------------------------------

Vector Time (GMT): 2009/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4017728
60                 A    =         6719122
82  meter
 Y    =       -1681579
85  meter          E    =           
0007380
 Z    =        5110937
41                 I    =           51
95325
 XDOT =       1142
775767                 Wp   =          139
12519
 YDOT =      -7460
226605  meter/sec      RA   =           89
39745  deg
 ZDOT =      -1560
395799                 TA   =          325
74909
                                          MA   =          325
79666
                                          Ha   =            191
221  n
mi
                                          Hp   =            181
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13181524
28                 X    =        -4023454
95
 Y    =       -5516994
26  feet           Y    =        -1726540
34  meter
 Z    =       16768167
35                 Z    =         5091404
89
 XDOT =       3749
264329                 XDOT =        1233
692705
 YDOT =     -24475
809071  feet/sec       YDOT =       -7446
939112  meter/sec
 ZDOT =      -5119
408789                 ZDOT =       -1554
623000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14270421
91                 X    =         4349624
60
 Y    =        1767636
73  feet           Y    =          538775
68  meter
 Z    =       16691068
37                 Z    =         5087437
64
 XDOT =       3027
718070                 XDOT =         922
848468
 YDOT =      23555
069123  feet/sec       YDOT =        7179
585069  meter/sec
 ZDOT =      -5097
028052                 ZDOT =       -1553
574150


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   09280
54498765  
00020000  00000-0  20000-3 0  9028
2 25544  51
6365  89
9427 0008440 173
9687 186
1579 15
74619741 23652


Satellite: ISS
Catalog Number: 25544
Epoch time:      09280
54498765   =   yrday
fracday
Element set:     902
Inclination:       51
6365  deg
RA of node:        89
9427  deg
Eccentricity:     
0008440     
Arg of perigee:   173
9687  deg
Mean anomaly:     186
1579  deg
Mean motion:   15
74619741  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2365
Checksum:              342


Coasting Arc #4 (Orbit 2380)
---------------------------------------

Vector Time (GMT): 2009/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -595029
43                 A    =         6729143
94  meter
 Y    =        6511620
49  meter          E    =           
0013028
 Z    =        1583824
37                 I    =           51
98681
 XDOT =      -4729
102866                 Wp   =           98
87089
 YDOT =      -1849
610241  meter/sec      RA   =           84
30726  deg
 ZDOT =       5785
546717                 TA   =          278
51453
                                          MA   =          278
66215
                                          Ha   =            190
886  n
mi
                                          Hp   =            181
925

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1952196
29                 X    =         -675493
39
 Y    =       21363584
27  feet           Y    =         6504516
63  meter
 Z    =        5196274
18                 Z    =         1580738
16
 XDOT =     -15515
429349                 XDOT =       -4736
174544
 YDOT =      -6068
275068  feet/sec       YDOT =       -1902
533363  meter/sec
 ZDOT =      18981
452484                 ZDOT =        5762
555012

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4161095
69                 X    =        -1268301
97
 Y    =      -21048090
12  feet           Y    =        -6415457
87  meter
 Z    =        5184424
13                 Z    =         1580212
48
 XDOT =      15170
606639                 XDOT =        4624
000903
 YDOT =       1688
000532  feet/sec       YDOT =         514
502562  meter/sec
 ZDOT =      18890
704180                 ZDOT =        5757
886634


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   09281
56038728  
00020000  00000-0  20000-3 0  9031
2 25544  51
6372  84
7222 0008459 177
9998 182
1201 15
74686808 23819


Satellite: ISS
Catalog Number: 25544
Epoch time:      09281
56038728   =   yrday
fracday
Element set:     903
Inclination:       51
6372  deg
RA of node:        84
7222  deg
Eccentricity:     
0008459     
Arg of perigee:   177
9998  deg
Mean anomaly:     182
1201  deg
Mean motion:   15
74686808  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2381
Checksum:              322


Coasting Arc #5 (Orbit 2395)
---------------------------------------

Vector Time (GMT): 2009/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4260155
63                 A    =         6719562
95  meter
 Y    =        1557125
78  meter          E    =           
0016969
 Z    =       -4971835
86                 I    =           51
95139
 XDOT =       -251
746946                 Wp   =          134
13698
 YDOT =       7395
307120  meter/sec      RA   =           79
15820  deg
 ZDOT =       2093
259356                 TA   =          156
12477
                                          MA   =          156
04598
                                          Ha   =            190
771  n
mi
                                          Hp   =            182
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13976888
54                 X    =         4266579
71
 Y    =        5108680
40  feet           Y    =         1604801
31  meter
 Z    =      -16311797
44                 Z    =        -4951124
00
 XDOT =       -825
941424                 XDOT =        -344
592718
 YDOT =      24262
818636  feet/sec       YDOT =        7391
972793  meter/sec
 ZDOT =       6867
648805                 ZDOT =        2091
810876

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14956335
97                 X    =        -4558691
20
 Y    =        -648267
90  feet           Y    =         -197592
06  meter
 Z    =      -16230050
14                 Z    =        -4946919
28
 XDOT =      -6505
174827                 XDOT =       -1982
777287
 YDOT =     -22313
119923  feet/sec       YDOT =       -6801
038953  meter/sec
 ZDOT =       6862
286947                 ZDOT =        2091
625061


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   09282
51231118  
00020000  00000-0  20000-3 0  9046
2 25544  51
6382  79
8286 0008432 180
9292 179
1857 15
74701501 23964


Satellite: ISS
Catalog Number: 25544
Epoch time:      09282
51231118   =   yrday
fracday
Element set:     904
Inclination:       51
6382  deg
RA of node:        79
8286  deg
Eccentricity:     
0008432     
Arg of perigee:   180
9292  deg
Mean anomaly:     179
1857  deg
Mean motion:   15
74701501  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2396
Checksum:              302


Coasting Arc #6 (Orbit 2411)
---------------------------------------

Vector Time (GMT): 2009/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -135614
76                 A    =         6728173
52  meter
 Y    =       -6391017
61  meter          E    =           
0013616
 Z    =       -2075570
98                 I    =           51
97416
 XDOT =       5027
684629                 Wp   =          164
83715
 YDOT =       1700
551748  meter/sec      RA   =           74
07526  deg
 ZDOT =      -5585
780804                 TA   =           38
24412
                                          MA   =           38
14762
                                          Ha   =            190
528  n
mi
                                          Hp   =            182
184

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -444930
33                 X    =          -54056
32
 Y    =      -20967905
54  feet           Y    =        -6392078
10  meter
 Z    =       -6809616
08                 Z    =        -2076031
75
 XDOT =      16495
028310                 XDOT =        5035
430204
 YDOT =       5579
238018  feet/sec       YDOT =        1756
817632  meter/sec
 ZDOT =     -18326
052506                 ZDOT =       -5561
337126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7022249
29                 X    =         2140381
58
 Y    =       19761332
89  feet           Y    =         6023254
26  meter
 Z    =       -6811727
69                 Z    =        -2076214
60
 XDOT =     -16072
952905                 XDOT =       -4899
036045
 YDOT =       -548
410986  feet/sec       YDOT =        -167
155668  meter/sec
 ZDOT =     -18229
578123                 ZDOT =       -5556
375412


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   09283
52767957  
00020000  00000-0  20000-3 0  9054
2 25544  51
6383  74
6082 0008241 185
0419 175
0663 15
74747494 24127


Satellite: ISS
Catalog Number: 25544
Epoch time:      09283
52767957   =   yrday
fracday
Element set:     905
Inclination:       51
6383  deg
RA of node:        74
6082  deg
Eccentricity:     
0008241     
Arg of perigee:   185
0419  deg
Mean anomaly:     175
0663  deg
Mean motion:   15
74747494  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2412
Checksum:              313


Coasting Arc #7 (Orbit 2427)
---------------------------------------

Vector Time (GMT): 2009/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4529424
81                 A    =         6720353
21  meter
 Y    =       -1385399
41  meter          E    =           
0007129
 Z    =        4760862
88                 I    =           51
93805
 XDOT =       -566
257181                 Wp   =          130
32632
 YDOT =      -7217
926360  meter/sec      RA   =           68
91738  deg
 ZDOT =      -2641
072415                 TA   =          345
46490
                                          MA   =          345
48539
                                          Ha   =            190
616  n
mi
                                          Hp   =            182
367

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14860317
61                 X    =        -4536724
04
 Y    =       -4545273
64  feet           Y    =        -1436090
89  meter
 Z    =       15619628
87                 Z    =         4738840
99
 XDOT =      -1857
799150                 XDOT =        -472
673008
 YDOT =     -23680
860762  feet/sec       YDOT =       -7223
735338  meter/sec
 ZDOT =      -8664
935744                 ZDOT =       -2643
595965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15611510
05                 X    =         4758388
26
 Y    =        -690546
70  feet           Y    =         -210478
64  meter
 Z    =       15532715
71                 Z    =         4734371
75
 XDOT =       9535
848331                 XDOT =        2906
526571
 YDOT =      20590
857602  feet/sec       YDOT =        6276
093397  meter/sec
 ZDOT =      -8675
214855                 ZDOT =       -2644
205488


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   09284
54303347  
00020000  00000-0  20000-3 0  9067
2 25544  51
6383  69
3880 0008352 188
3627 171
7399 15
74719647 24289


Satellite: ISS
Catalog Number: 25544
Epoch time:      09284
54303347   =   yrday
fracday
Element set:     906
Inclination:       51
6383  deg
RA of node:        69
3880  deg
Eccentricity:     
0008352     
Arg of perigee:   188
3627  deg
Mean anomaly:     171
7399  deg
Mean motion:   15
74719647  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2428
Checksum:              328


Coasting Arc #8 (Orbit 2443)
---------------------------------------

Vector Time (GMT): 2009/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         817392
15                 A    =         6727056
12  meter
 Y    =        6174062
80  meter          E    =           
0012539
 Z    =        2540526
58                 I    =           51
95089
 XDOT =      -5366
187901                 Wp   =          112
75067
 YDOT =      -1487
485777  meter/sec      RA   =           63
83968  deg
 ZDOT =       5316
037742                 TA   =          275
91116
                                          MA   =          276
05406
                                          Ha   =            190
192  n
mi
                                          Hp   =            182
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2681732
76                 X    =          735950
44
 Y    =       20256111
54  feet           Y    =         6182748
07  meter
 Z    =        8335060
95                 Z    =         2544299
50
 XDOT =     -17605
603351                 XDOT =       -5374
980298
 YDOT =      -4880
202682  feet/sec       YDOT =       -1547
542660  meter/sec
 ZDOT =      17441
068706                 ZDOT =        5289
947288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9537181
59                 X    =        -2906932
95
 Y    =      -18063527
31  feet           Y    =        -5505763
12  meter
 Z    =        8350217
65                 Z    =         2545146
34
 XDOT =      16979
572246                 XDOT =        5175
373621
 YDOT =       -911
519471  feet/sec       YDOT =        -277
831135  meter/sec
 ZDOT =      17338
101880                 ZDOT =        5284
653453


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   09285
55836654  
00020000  00000-0  20000-3 0  9072
2 25544  51
6395  64
1676 0008377 193
1609 166
9337 15
74812621 24441


Satellite: ISS
Catalog Number: 25544
Epoch time:      09285
55836654   =   yrday
fracday
Element set:     907
Inclination:       51
6395  deg
RA of node:        64
1676  deg
Eccentricity:     
0008377     
Arg of perigee:   193
1609  deg
Mean anomaly:     166
9337  deg
Mean motion:   15
74812621  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2444
Checksum:              325


Coasting Arc #9 (Orbit 2458)
---------------------------------------

Vector Time (GMT): 2009/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4858448
16                 A    =         6721231
39  meter
 Y    =        1204071
58  meter          E    =           
0013086
 Z    =       -4497321
13                 I    =           51
91697
 XDOT =       1258
155583                 Wp   =          149
01144
 YDOT =       6882
965276  meter/sec      RA   =           58
67410  deg
 ZDOT =       3195
090777                 TA   =          152
87440
                                          MA   =          152
80597
                                          Ha   =            190
031  n
mi
                                          Hp   =            182
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15939790
55                 X    =         4866470
28
 Y    =        3950366
08  feet           Y    =         1258446
22  meter
 Z    =      -14754990
59                 Z    =        -4473699
19
 XDOT =       4127
807030                 XDOT =        1165
574265
 YDOT =      22581
907075  feet/sec       YDOT =        6896
517242  meter/sec
 ZDOT =      10482
581290                 ZDOT =        3200
977681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16361591
27                 X    =        -4987013
02
 Y    =        2173212
81  feet           Y    =          662395
26  meter
 Z    =      -14661771
36                 Z    =        -4468907
91
 XDOT =     -11871
698488                 XDOT =       -3618
493699
 YDOT =     -18345
638895  feet/sec       YDOT =       -5591
750735  meter/sec
 ZDOT =      10506
105042                 ZDOT =        3202
260817


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   09286
51022909  
00020000  00000-0  20000-3 0  9080
2 25544  51
6399  59
2740 0008192 196
9744 163
1146 15
74799033 24592


Satellite: ISS
Catalog Number: 25544
Epoch time:      09286
51022909   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:        59
2740  deg
Eccentricity:     
0008192     
Arg of perigee:   196
9744  deg
Mean anomaly:     163
1146  deg
Mean motion:   15
74799033  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2459
Checksum:              324


Coasting Arc #10 (Orbit 2474)
---------------------------------------

Vector Time (GMT): 2009/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1346321
34                 A    =         6725772
73  meter
 Y    =       -5841198
93  meter          E    =           
0009047
 Z    =       -3040612
75                 I    =           51
91638
 XDOT =       5756
029943                 Wp   =          170
69256
 YDOT =       1251
761749  meter/sec      RA   =           53
59886  deg
 ZDOT =      -4964
131150                 TA   =           44
38816
                                          MA   =           44
31568
                                          Ha   =            189
832  n
mi
                                          Hp   =            182
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4417064
77                 X    =        -1266133
07
 Y    =      -19164038
50  feet           Y    =        -5855806
17  meter
 Z    =       -9975763
62                 Z    =        -3046958
02
 XDOT =      18884
612675                 XDOT =        5765
719837
 YDOT =       4106
829885  feet/sec       YDOT =        1316
182865  meter/sec
 ZDOT =     -16286
519521                 ZDOT =       -4936
144618

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11332294
08                 X    =         3454083
24
 Y    =       16057549
00  feet           Y    =         4894340
94  meter
 Z    =      -10001046
12                 Z    =        -3048318
86
 XDOT =     -17941
341981                 XDOT =       -5468
521036
 YDOT =       2608
819681  feet/sec       YDOT =         795
168239  meter/sec
 ZDOT =     -16176
085721                 ZDOT =       -4930
470928


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   09287
52553124  
00020000  00000-0  20000-3 0  9091
2 25544  51
6401  54
0528 0008153 200
9243 159
1588 15
74827912 24751


Satellite: ISS
Catalog Number: 25544
Epoch time:      09287
52553124   =   yrday
fracday
Element set:     909
Inclination:       51
6401  deg
RA of node:        54
0528  deg
Eccentricity:     
0008153     
Arg of perigee:   200
9243  deg
Mean anomaly:     159
1588  deg
Mean motion:   15
74827912  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2475
Checksum:              294


Coasting Arc #11 (Orbit 2490)
---------------------------------------

Vector Time (GMT): 2009/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5194099
10                 A    =         6722404
64  meter
 Y    =        -947112
13  meter          E    =           
0008315
 Z    =        4152115
19                 I    =           51
88678
 XDOT =      -1816
894119                 Wp   =          124
61407
 YDOT =      -6482
489899  meter/sec      RA   =           48
42616  deg
 ZDOT =      -3750
876328                 TA   =            3
60243
                                          MA   =            3
59644
                                          Ha   =            189
818  n
mi
                                          Hp   =            183
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17041007
54                 X    =        -5203292
83
 Y    =       -3107323
27  feet           Y    =        -1005246
65  meter
 Z    =       13622425
18                 Z    =         4126859
62
 XDOT =      -5960
938712                 XDOT =       -1726
049387
 YDOT =     -21268
011480  feet/sec       YDOT =       -6502
299869  meter/sec
 ZDOT =     -12306
024699                 ZDOT =       -3759
481706

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16947257
66                 X    =         5165524
13
 Y    =       -3942937
90  feet           Y    =        -1201807
47  meter
 Z    =       13522779
39                 Z    =         4121743
16
 XDOT =      13558
926070                 XDOT =        4132
760666
 YDOT =      15948
294463  feet/sec       YDOT =        4861
040152  meter/sec
 ZDOT =     -12340
243551                 ZDOT =       -3761
306234


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   09288
54081707  
00020000  00000-0  20000-3 0  9109
2 25544  51
6409  48
8326 0008076 204
1342 155
9445 15
74831586 24912


Satellite: ISS
Catalog Number: 25544
Epoch time:      09288
54081707   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:        48
8326  deg
Eccentricity:     
0008076     
Arg of perigee:   204
1342  deg
Mean anomaly:     155
9445  deg
Mean motion:   15
74831586  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2491
Checksum:              303


Coasting Arc #12 (Orbit 2506)
---------------------------------------

Vector Time (GMT): 2009/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1776397
92                 A    =         6724193
75  meter
 Y    =        5457881
06  meter          E    =           
0011286
 Z    =        3503008
61                 I    =           51
87415
 XDOT =      -6154
874178                 Wp   =          131
72805
 YDOT =       -917
285428  meter/sec      RA   =           43
35174  deg
 ZDOT =       4533
678309                 TA   =          269
74274
                                          MA   =          269
87206
                                          Ha   =            189
350  n
mi
                                          Hp   =            183
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5828077
17                 X    =         1698217
57
 Y    =       17906433
93  feet           Y    =         5477308
96  meter
 Z    =       11492810
41                 Z    =         3511448
17
 XDOT =     -20193
156752                 XDOT =       -6166
183749
 YDOT =      -3009
466627  feet/sec       YDOT =        -986
175710  meter/sec
 ZDOT =      14874
272666                 ZDOT =        4503
749899

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12636236
23                 X    =        -3851524
80
 Y    =      -13934164
66  feet           Y    =        -4247133
39  meter
 Z    =       11526323
79                 Z    =         3513223
49
 XDOT =      18698
356159                 XDOT =        5699
258957
 YDOT =      -4705
208891  feet/sec       YDOT =       -1434
147670  meter/sec
 ZDOT =      14756
204827                 ZDOT =        4497
691231


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   09289
55608222  
00020000  00000-0  20000-3 0  9119
2 25544  51
6420  43
6117 0008042 209
0429 151
0288 15
74921540 25079


Satellite: ISS
Catalog Number: 25544
Epoch time:      09289
55608222   =   yrday
fracday
Element set:     911
Inclination:       51
6420  deg
RA of node:        43
6117  deg
Eccentricity:     
0008042     
Arg of perigee:   209
0429  deg
Mean anomaly:     151
0288  deg
Mean motion:   15
74921540  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2507
Checksum:              270


Coasting Arc #13 (Orbit 2521)
---------------------------------------

Vector Time (GMT): 2009/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5557908
35                 A    =         6723648
25  meter
 Y    =         634438
60  meter          E    =           
0007888
 Z    =       -3738063
04                 I    =           51
84960
 XDOT =       2197
565170                 Wp   =          169
90035
 YDOT =       6004
685624  meter/sec      RA   =           38
17413  deg
 ZDOT =       4280
323452                 TA   =          145
14755
                                          MA   =          145
09587
                                          Ha   =            189
163  n
mi
                                          Hp   =            183
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18234607
44                 X    =         5568560
18
 Y    =        2081491
47  feet           Y    =          696649
70  meter
 Z    =      -12263986
36                 Z    =        -3711036
18
 XDOT =       7209
859482                 XDOT =        2109
462812
 YDOT =      19700
412153  feet/sec       YDOT =        6028
767795  meter/sec
 ZDOT =      14043
055945                 ZDOT =        4290
785068

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17433760
32                 X    =        -5313810
14
 Y    =        5958273
49  feet           Y    =         1816081
76  meter
 Z    =      -12157378
62                 Z    =        -3705569
00
 XDOT =     -14443
021679                 XDOT =       -4402
233008
 YDOT =     -13479
331173  feet/sec       YDOT =       -4108
500142  meter/sec
 ZDOT =      14084
556492                 ZDOT =        4292
972819


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   09290
50788107  
00020000  00000-0  20000-3 0  9128
2 25544  51
6423  38
7181 0007881 213
8082 146
2580 15
74899501 25225


Satellite: ISS
Catalog Number: 25544
Epoch time:      09290
50788107   =   yrday
fracday
Element set:     912
Inclination:       51
6423  deg
RA of node:        38
7181  deg
Eccentricity:     
0007881     
Arg of perigee:   213
8082  deg
Mean anomaly:     146
2580  deg
Mean motion:   15
74899501  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2522
Checksum:              295


Coasting Arc #14 (Orbit 2537)
---------------------------------------

Vector Time (GMT): 2009/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2018962
34                 A    =         6722644
88  meter
 Y    =       -5037950
22  meter          E    =           
0004543
 Z    =       -3965555
51                 I    =           51
82294
 XDOT =       6558
566196                 Wp   =          154
39465
 YDOT =        518
039321  meter/sec      RA   =           33
09757  deg
 ZDOT =      -4002
966391                 TA   =           74
23706
                                          MA   =           74
18696
                                          Ha   =            188
965  n
mi
                                          Hp   =            183
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6623892
19                 X    =        -1943212
52
 Y    =      -16528708
08  feet           Y    =        -5060104
12  meter
 Z    =      -13010352
73                 Z    =        -3975179
66
 XDOT =      21517
605629                 XDOT =        6571
732205
 YDOT =       1699
604071  feet/sec       YDOT =         591
454481  meter/sec
 ZDOT =     -13133
091834                 ZDOT =       -3971
071975

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13202001
92                 X    =         4023970
19
 Y    =       11907441
51  feet           Y    =         3629388
17  meter
 Z    =      -13048501
78                 Z    =        -3977183
34
 XDOT =     -19237
558766                 XDOT =       -5863
607912
 YDOT =       7095
741994  feet/sec       YDOT =        2162
782160  meter/sec
 ZDOT =     -13007
298135                 ZDOT =       -3964
624472


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   09291
52311522  
00020000  00000-0  20000-3 0  9135
2 25544  51
6429  33
4978 0007887 217
2326 142
8291 15
74928773 25384


Satellite: ISS
Catalog Number: 25544
Epoch time:      09291
52311522   =   yrday
fracday
Element set:     913
Inclination:       51
6429  deg
RA of node:        33
4978  deg
Eccentricity:     
0007887     
Arg of perigee:   217
2326  deg
Mean anomaly:     142
8291  deg
Mean motion:   15
74928773  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2538
Checksum:              311


Coasting Arc #15 (Orbit 2553)
---------------------------------------

Vector Time (GMT): 2009/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745632
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5882859
19                 A    =         6725008
32  meter
 Y    =        -235763
18  meter          E    =           
0010276
 Z    =        3235981
66                 I    =           51
80498
 XDOT =      -2412
110647                 Wp   =          129
25635
 YDOT =      -5538
613570  meter/sec      RA   =           27
91733  deg
 ZDOT =      -4784
947288                 TA   =           12
94563
                                          MA   =           12
91927
                                          Ha   =            188
876  n
mi
                                          Hp   =            183
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19300719
14                 X    =        -5895505
92
 Y    =        -773501
24  feet           Y    =         -301619
39  meter
 Z    =       10616737
72                 Z    =         3207371
13
 XDOT =      -7913
748843                 XDOT =       -2326
752505
 YDOT =     -18171
304363  feet/sec       YDOT =       -5565
110091  meter/sec
 ZDOT =     -15698
645959                 ZDOT =       -4796
458179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17556646
38                 X    =         5351265
82
 Y    =       -8201419
58  feet           Y    =        -2499792
69  meter
 Z    =       10503907
27                 Z    =         3201590
94
 XDOT =      14692
840158                 XDOT =        4478
377680
 YDOT =      11272
774259  feet/sec       YDOT =        3435
941594  meter/sec
 ZDOT =     -15744
244453                 ZDOT =       -4798
845709


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   09292
53833261  
00020000  00000-0  20000-3 0  9147
2 25544  51
6428  28
2779 0007684 220
5403 139
5189 15
74950670 25540


Satellite: ISS
Catalog Number: 25544
Epoch time:      09292
53833261   =   yrday
fracday
Element set:     914
Inclination:       51
6428  deg
RA of node:        28
2779  deg
Eccentricity:     
0007684     
Arg of perigee:   220
5403  deg
Mean anomaly:     139
5189  deg
Mean motion:   15
74950670  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2554
Checksum:              309

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/[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