Date: March 13th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 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


075/02:53:23 433 -2 1 8 0 8 0
N/A 5 0 -0 3 186 3
000/00:11:26 867 -5 9 0 0 178 1

Coasting Arc #1 (Orbit 3470)
---------------------------------------

Vector Time (GMT): 2007/066/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1843279
18                 A    =         6715315
51  meter
 Y    =        5975224
96  meter          E    =           
0016451
 Z    =       -2439780
13                 I    =           51
32593
 XDOT =      -4324
631504                 Wp   =          281
41374
 YDOT =      -3520
510058  meter/sec      RA   =          268
94658  deg
 ZDOT =      -5321
256189                 TA   =          286
33406
                                          MA   =          286
51490
                                          Ha   =            184
352  n
mi
                                          Hp   =            174
673

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6047503
86                 X    =        -1898106
08
 Y    =       19603756
43  feet           Y    =         5954305
64  meter
 Z    =       -8004527
98                 Z    =        -2448868
36
 XDOT =     -14188
423568                 XDOT =       -4259
093724
 YDOT =     -11550
229848  feet/sec       YDOT =       -3568
504487  meter/sec
 ZDOT =     -17458
189596                 ZDOT =       -5342
105626

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15229190
49                 X    =        -4641857
26
 Y    =       13726493
12  feet           Y    =         4183835
10  meter
 Z    =       -8037859
24                 Z    =        -2449939
50
 XDOT =      -5144
972027                 XDOT =       -1568
187474
 YDOT =     -16041
415410  feet/sec       YDOT =       -4889
423417  meter/sec
 ZDOT =     -17536
987871                 ZDOT =       -5345
273903


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   07066
48505197  
00020000  00000-0  20000-3 0  9007
2 25544  51
6332 269
5244 0021287 288
9593  70
9266 15
79017562 34716


Satellite: ISS
Catalog Number: 25544
Epoch time:      07066
48505197   =   yrday
fracday
Element set:     900
Inclination:       51
6332  deg
RA of node:       269
5244  deg
Eccentricity:     
0021287     
Arg of perigee:   288
9593  deg
Mean anomaly:      70
9266  deg
Mean motion:   15
79017562  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3471
Checksum:              315


Coasting Arc #2 (Orbit 3486)
---------------------------------------

Vector Time (GMT): 2007/067/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3414163
78                 A    =         6711886
57  meter
 Y    =        4516915
16  meter          E    =           
0012207
 Z    =        3619412
88                 I    =           51
31756
 XDOT =      -2878
009032                 Wp   =          320
51692
 YDOT =       5661
085672  meter/sec      RA   =          263
69990  deg
 ZDOT =      -4348
794075                 TA   =          175
85609
                                          MA   =          175
84597
                                          Ha   =            184
509  n
mi
                                          Hp   =            174
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11201324
73                 X    =         3345818
86
 Y    =       14819275
47  feet           Y    =         4554712
35  meter
 Z    =       11874714
16                 Z    =         3635832
51
 XDOT =      -9442
286849                 XDOT =       -2919
972638
 YDOT =      18573
115722  feet/sec       YDOT =        5628
667259  meter/sec
 ZDOT =     -14267
697096                 ZDOT =       -4362
877670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2246484
44                 X    =          684728
46
 Y    =       18399743
74  feet           Y    =         5608241
89  meter
 Z    =       11937008
65                 Z    =         3638400
24
 XDOT =     -16045
331708                 XDOT =       -4890
617105
 YDOT =      11251
828827  feet/sec       YDOT =        3429
557426  meter/sec
 ZDOT =     -14319
836055                 ZDOT =       -4364
686030


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   07067
49763098  
00020000  00000-0  20000-3 0  9016
2 25544  51
6336 264
2833 0021427 293
2926  66
5984 15
79114479 34871


Satellite: ISS
Catalog Number: 25544
Epoch time:      07067
49763098   =   yrday
fracday
Element set:     901
Inclination:       51
6336  deg
RA of node:       264
2833  deg
Eccentricity:     
0021427     
Arg of perigee:   293
2926  deg
Mean anomaly:      66
5984  deg
Mean motion:   15
79114479  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3487
Checksum:              329


Coasting Arc #3 (Orbit 3502)
---------------------------------------

Vector Time (GMT): 2007/068/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3171234
17                 A    =         6707856
63  meter
 Y    =       -3523773
75  meter          E    =           
0013947
 Z    =        4754050
84                 I    =           51
30676
 XDOT =       3376
247503                 Wp   =          295
86207
 YDOT =       6441
768597  meter/sec      RA   =          258
54681  deg
 ZDOT =       2534
333288                 TA   =          129
26460
                                          MA   =          129
14078
                                          Ha   =            184
730  n
mi
                                          Hp   =            174
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10404311
57                 X    =         3187307
57
 Y    =      -11560937
51  feet           Y    =        -3488221
15  meter
 Z    =       15597279
66                 Z    =         4769495
85
 XDOT =      11076
927503                 XDOT =        3291
652499
 YDOT =      21134
411406  feet/sec       YDOT =        6479
050805  meter/sec
 ZDOT =       8314
741760                 ZDOT =        2550
529271

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14626413
33                 X    =         4458130
78
 Y    =       -5116112
74  feet           Y    =        -1559391
16  meter
 Z    =       15654824
55                 Z    =         4771590
52
 XDOT =       -961
115302                 XDOT =        -292
947944
 YDOT =      22765
876244  feet/sec       YDOT =        6939
039079  meter/sec
 ZDOT =       8376
459717                 ZDOT =        2553
144922


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   07068
51019186  
00020000  00000-0  20000-3 0  9023
2 25544  51
6324 259
0417 0021263 297
3809  62
5193 15
79064484 35038


Satellite: ISS
Catalog Number: 25544
Epoch time:      07068
51019186   =   yrday
fracday
Element set:     902
Inclination:       51
6324  deg
RA of node:       259
0417  deg
Eccentricity:     
0021263     
Arg of perigee:   297
3809  deg
Mean anomaly:      62
5193  deg
Mean motion:   15
79064484  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3503
Checksum:              293


Coasting Arc #4 (Orbit 3517)
---------------------------------------

Vector Time (GMT): 2007/069/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2345117
11                 A    =         6717506
11  meter
 Y    =       -6254809
18  meter          E    =           
0022323
 Z    =        -564420
20                 I    =           51
34608
 XDOT =       4350
312200                 Wp   =          329
93001
 YDOT =      -2179
245072  meter/sec      RA   =          253
32253  deg
 ZDOT =       5992
170167                 TA   =           23
88077
                                          MA   =           23
77737
                                          Ha   =            184
926  n
mi
                                          Hp   =            174
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7693953
77                 X    =        -2272258
80
 Y    =      -20521027
49  feet           Y    =        -6280626
23  meter
 Z    =       -1851772
31                 Z    =         -575635
59
 XDOT =      14272
677820                 XDOT =        4345
248733
 YDOT =      -7149
754173  feet/sec       YDOT =       -2130
625591  meter/sec
 ZDOT =      19659
350941                 ZDOT =        6013
291666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2845665
42                 X    =          867358
82
 Y    =      -21726726
37  feet           Y    =        -6622306
20  meter
 Z    =       -1894757
00                 Z    =         -577521
93
 XDOT =      14277
652653                 XDOT =        4351
828529
 YDOT =        125
541222  feet/sec       YDOT =          38
264965  meter/sec
 ZDOT =      19738
407466                 ZDOT =        6016
266596


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   07069
45944276  
00020000  00000-0  20000-3 0  9035
2 25544  51
6315 254
1281 0021382 300
7675  59
1385 15
79120381 35185


Satellite: ISS
Catalog Number: 25544
Epoch time:      07069
45944276   =   yrday
fracday
Element set:     903
Inclination:       51
6315  deg
RA of node:       254
1281  deg
Eccentricity:     
0021382     
Arg of perigee:   300
7675  deg
Mean anomaly:      59
1385  deg
Mean motion:   15
79120381  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3518
Checksum:              292


Coasting Arc #5 (Orbit 3533)
---------------------------------------

Vector Time (GMT): 2007/070/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4334586
61                 A    =         6705897
54  meter
 Y    =         182744
34  meter          E    =           
0010207
 Z    =       -5108652
96                 I    =           51
31619
 XDOT =      -1837
649650                 Wp   =          340
46586
 YDOT =      -7377
478800  meter/sec      RA   =          248
11923  deg
 ZDOT =       1304
060306                 TA   =          301
99196
                                          MA   =          302
09112
                                          Ha   =            184
976  n
mi
                                          Hp   =            174
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14221084
67                 X    =        -4311491
16
 Y    =         599554
93  feet           Y    =          134401
63  meter
 Z    =      -16760672
43                 Z    =        -5129654
16
 XDOT =      -6029
034285                 XDOT =       -1761
351899
 YDOT =     -24204
326772  feet/sec       YDOT =       -7397
601805  meter/sec
 ZDOT =       4278
413079                 ZDOT =        1295
318491

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12859696
73                 X    =        -3919635
56
 Y    =       -5880177
13  feet           Y    =        -1792277
99  meter
 Z    =      -16839553
80                 Z    =        -5132696
00
 XDOT =       5168
114339                 XDOT =        1575
241251
 YDOT =     -23376
076141  feet/sec       YDOT =       -7125
028008  meter/sec
 ZDOT =       4244
565057                 ZDOT =        1293
743429


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   07070
47195676  
00020000  00000-0  20000-3 0  9042
2 25544  51
6306 248
8869 0021213 304
6477  55
2689 15
79185018 35343


Satellite: ISS
Catalog Number: 25544
Epoch time:      07070
47195676   =   yrday
fracday
Element set:     904
Inclination:       51
6306  deg
RA of node:       248
8869  deg
Eccentricity:     
0021213     
Arg of perigee:   304
6477  deg
Mean anomaly:      55
2689  deg
Mean motion:   15
79185018  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3534
Checksum:              317


Coasting Arc #6 (Orbit 3549)
---------------------------------------

Vector Time (GMT): 2007/071/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         661494
25                 A    =         6714099
28  meter
 Y    =        6099529
13  meter          E    =           
0016543
 Z    =       -2731560
80                 I    =           51
35605
 XDOT =      -5482
657216                 Wp   =          310
78368
 YDOT =      -1717
109192  meter/sec      RA   =          242
95727  deg
 ZDOT =      -5131
076627                 TA   =          260
59917
                                          MA   =          260
78624
                                          Ha   =            185
349  n
mi
                                          Hp   =            174
104

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2170256
72                 X    =          606508
58
 Y    =       20011578
52  feet           Y    =         6106618
87  meter
 Z    =       -8961813
64                 Z    =        -2728480
89
 XDOT =     -17987
720526                 XDOT =       -5438
123162
 YDOT =      -5633
560341  feet/sec       YDOT =       -1778
170361  meter/sec
 ZDOT =     -16834
240903                 ZDOT =       -5157
602944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6782966
69                 X    =        -2067448
25
 Y    =       18957500
88  feet           Y    =         5778246
27  meter
 Z    =       -8949408
69                 Z    =        -2727779
77
 XDOT =     -12226
886975                 XDOT =       -3726
755150
 YDOT =     -12416
946043  feet/sec       YDOT =       -3784
685154  meter/sec
 ZDOT =     -16934
149166                 ZDOT =       -5161
528666


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   07071
48444698  
00020000  00000-0  20000-3 0  9056
2 25544  51
6305 243
6470 0021305 308
8692  51
0572 15
79225333 35508


Satellite: ISS
Catalog Number: 25544
Epoch time:      07071
48444698   =   yrday
fracday
Element set:     905
Inclination:       51
6305  deg
RA of node:       243
6470  deg
Eccentricity:     
0021305     
Arg of perigee:   308
8692  deg
Mean anomaly:      51
0572  deg
Mean motion:   15
79225333  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3550
Checksum:              286


Coasting Arc #7 (Orbit 3565)
---------------------------------------

Vector Time (GMT): 2007/072/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5025086
60                 A    =         6712353
06  meter
 Y    =        2978914
77  meter          E    =           
0014607
 Z    =        3323820
33                 I    =           51
36475
 XDOT =       -537
777851                 Wp   =          347
51765
 YDOT =       6108
043615  meter/sec      RA   =          237
71098  deg
 ZDOT =      -4650
929682                 TA   =          153
20337
                                          MA   =          153
12784
                                          Ha   =            185
552  n
mi
                                          Hp   =            173
833

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16486504
59                 X    =         4975256
17
 Y    =        9773342
42  feet           Y    =         3034829
50  meter
 Z    =       10904922
36                 Z    =         3348110
82
 XDOT =      -1764
363027                 XDOT =        -583
445826
 YDOT =      20039
513172  feet/sec       YDOT =        6101
774511  meter/sec
 ZDOT =     -15258
955650                 ZDOT =       -4653
653136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10747412
81                 X    =         3275811
42
 Y    =       15805316
05  feet           Y    =         4817460
33  meter
 Z    =       10996612
65                 Z    =         3351767
54
 XDOT =      -8848
400081                 XDOT =       -2696
992345
 YDOT =      16663
044418  feet/sec       YDOT =        5078
895939  meter/sec
 ZDOT =     -15268
352358                 ZDOT =       -4653
793799


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   07072
49691277  
00020000  00000-0  20000-3 0  9066
2 25544  51
6304 238
4050 0021399 312
3070  47
6282 15
79259080 35668


Satellite: ISS
Catalog Number: 25544
Epoch time:      07072
49691277   =   yrday
fracday
Element set:     906
Inclination:       51
6304  deg
RA of node:       238
4050  deg
Eccentricity:     
0021399     
Arg of perigee:   312
3070  deg
Mean anomaly:      47
6282  deg
Mean motion:   15
79259080  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3566
Checksum:              296


Coasting Arc #8 (Orbit 3581)
---------------------------------------

Vector Time (GMT): 2007/073/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1738782
45                 A    =         6706580
14  meter
 Y    =       -4208818
43  meter          E    =           
0015344
 Z    =        4927856
11                 I    =           51
36088
 XDOT =       5708
499680                 Wp   =          321
83517
 YDOT =       4749
435285  meter/sec      RA   =          232
55692  deg
 ZDOT =       2057
496423                 TA   =          108
25923
                                          MA   =          108
09220
                                          Ha   =            185
750  n
mi
                                          Hp   =            173
800

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5704666
83                 X    =         1761778
61
 Y    =      -13808459
43  feet           Y    =        -4189245
75  meter
 Z    =       16167506
92                 Z    =         4936358
89
 XDOT =      18728
673492                 XDOT =        5644
971774
 YDOT =      15582
136762  feet/sec       YDOT =        4812
915748  meter/sec
 ZDOT =       6750
316347                 ZDOT =        2085
073458

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10754014
13                 X    =         3277823
51
 Y    =      -10322426
58  feet           Y    =        -3146275
62  meter
 Z    =       16198880
98                 Z    =         4937418
92
 XDOT =       9966
673705                 XDOT =        3037
842145
 YDOT =      21061
668228  feet/sec       YDOT =        6419
596476  meter/sec
 ZDOT =       6854
615429                 ZDOT =        2089
286783


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   07073
50935723  
00020000  00000-0  20000-3 0  9077
2 25544  51
6296 233
1627 0021268 316
7163  43
2331 15
79261337 35829


Satellite: ISS
Catalog Number: 25544
Epoch time:      07073
50935723   =   yrday
fracday
Element set:     907
Inclination:       51
6296  deg
RA of node:       233
1627  deg
Eccentricity:     
0021268     
Arg of perigee:   316
7163  deg
Mean anomaly:      43
2331  deg
Mean motion:   15
79261337  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3582
Checksum:              288


Coasting Arc #9 (Orbit 3596)
---------------------------------------

Vector Time (GMT): 2007/074/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4574833
87                 A    =         6717090
31  meter
 Y    =       -4895036
77  meter          E    =           
0025414
 Z    =         -59763
14                 I    =           51
41598
 XDOT =       3479
719175                 Wp   =          348
86502
 YDOT =      -3330
668921  meter/sec      RA   =          227
34434  deg
 ZDOT =       6036
291642                 TA   =           10
48120
                                          MA   =           10
42832
                                          Ha   =            185
869  n
mi
                                          Hp   =            173
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15009297
46                 X    =        -4519466
54
 Y    =      -16059831
92  feet           Y    =        -4945885
55  meter
 Z    =        -196073
31                 Z    =          -81852
59
 XDOT =      11416
401493                 XDOT =        3487
381947
 YDOT =     -10927
391474  feet/sec       YDOT =       -3291
713709  meter/sec
 ZDOT =      19804
106438                 ZDOT =        6053
214502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7517910
99                 X    =        -2291459
27
 Y    =      -20655226
75  feet           Y    =        -6295713
11  meter
 Z    =        -279782
90                 Z    =          -85277
83
 XDOT =      13176
731183                 XDOT =        4016
267665
 YDOT =      -5077
497214  feet/sec       YDOT =       -1547
621151  meter/sec
 ZDOT =      19867
248189                 ZDOT =        6055
537248


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   07074
45849919  
00020000  00000-0  20000-3 0  9084
2 25544  51
6301 228
2486 0021143 320
2327  39
7288 15
79318936 35973


Satellite: ISS
Catalog Number: 25544
Epoch time:      07074
45849919   =   yrday
fracday
Element set:     908
Inclination:       51
6301  deg
RA of node:       228
2486  deg
Eccentricity:     
0021143     
Arg of perigee:   320
2327  deg
Mean anomaly:      39
7288  deg
Mean motion:   15
79318936  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3597
Checksum:              319


Coasting Arc #10 (Orbit 3607)
---------------------------------------

Vector Time (GMT): 2007/075/02:59:06
867
Vector Time (MET): N/A
Weight (LBS)     : 478751
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4347879
52                 A    =         6721183
94  meter
 Y    =        5065135
71  meter          E    =           
0005393
 Z    =        -796345
13                 I    =           51
43092
 XDOT =      -4132
972612                 Wp   =          302
34104
 YDOT =       2607
229919  meter/sec      RA   =          223
89872  deg
 ZDOT =      -5949
824406                 TA   =          246
37327
                                          MA   =          246
42990
                                          Ha   =            186
253  n
mi
                                          Hp   =            178
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14264696
59                 X    =         4294785
72
 Y    =       16617899
31  feet           Y    =         5113459
23  meter
 Z    =       -2612680
87                 Z    =         -775352
79
 XDOT =     -13559
621430                 XDOT =       -4132
917291
 YDOT =       8553
903934  feet/sec       YDOT =        2561
012716  meter/sec
 ZDOT =     -19520
421280                 ZDOT =       -5969
901964

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21434750
99                 X    =        -6533312
10
 Y    =       -4538424
24  feet           Y    =        -1383311
71  meter
 Z    =       -2533061
92                 Z    =         -772077
27
 XDOT =       5165
688857                 XDOT =        1574
501964
 YDOT =     -13399
638005  feet/sec       YDOT =       -4084
209664  meter/sec
 ZDOT =     -19595
522738                 ZDOT =       -5972
715331


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   07075
15456134  
00020000  00000-0  20000-3 0  9096
2 25544  51
6325 224
6503 0015688 314
4882  45
4999 15
77777549 36080


Satellite: ISS
Catalog Number: 25544
Epoch time:      07075
15456134   =   yrday
fracday
Element set:     909
Inclination:       51
6325  deg
RA of node:       224
6503  deg
Eccentricity:     
0015688     
Arg of perigee:   314
4882  deg
Mean anomaly:      45
4999  deg
Mean motion:   15
77777549  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3608
Checksum:              328


Coasting Arc #11 (Orbit 3623)
---------------------------------------

Vector Time (GMT): 2007/076/02:59:06
867
Vector Time (MET): N/A
Weight (LBS)     : 478751
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4449586
04                 A    =         6710993
53  meter
 Y    =       -1382528
69  meter          E    =           
0016092
 Z    =        4839401
01                 I    =           51
41858
 XDOT =       4378
349261                 Wp   =          343
11207
 YDOT =       5888
413029  meter/sec      RA   =          218
69202  deg
 ZDOT =      -2330
221697                 TA   =          129
73816
                                          MA   =          129
59626
                                          Ha   =            186
413  n
mi
                                          Hp   =            177
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14598379
38                 X    =         4441206
49
 Y    =       -4535855
28  feet           Y    =        -1332817
40  meter
 Z    =       15877299
90                 Z    =         4860996
43
 XDOT =      14364
662930                 XDOT =        4323
498350
 YDOT =      19318
940383  feet/sec       YDOT =        5937
067308  meter/sec
 ZDOT =      -7645
084307                 ZDOT =       -2309
085794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8562467
98                 X    =        -2609840
24
 Y    =       12561556
12  feet           Y    =         3828762
31  meter
 Z    =       15958282
05                 Z    =         4864084
37
 XDOT =     -22370
292575                 XDOT =       -6818
465177
 YDOT =      -5583
239479  feet/sec       YDOT =       -1701
771393  meter/sec
 ZDOT =      -7564
796280                 ZDOT =       -2305
749906


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   07076
16794410  
00020000  00000-0  20000-3 0  9102
2 25544  51
6324 219
4158 0015788 318
6530  41
3439 15
77827964 36243


Satellite: ISS
Catalog Number: 25544
Epoch time:      07076
16794410   =   yrday
fracday
Element set:     910
Inclination:       51
6324  deg
RA of node:       219
4158  deg
Eccentricity:     
0015788     
Arg of perigee:   318
6530  deg
Mean anomaly:      41
3439  deg
Mean motion:   15
77827964  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3624
Checksum:              307


Coasting Arc #12 (Orbit 3639)
---------------------------------------

Vector Time (GMT): 2007/077/02:59:06
867
Vector Time (MET): N/A
Weight (LBS)     : 478751
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3084210
85                 A    =         6716964
64  meter
 Y    =       -5056365
51  meter          E    =           
0013956
 Z    =        3149930
13                 I    =           51
46270
 XDOT =       5981
223805                 Wp   =           14
47796
 YDOT =       -646
562053  meter/sec      RA   =          213
55581  deg
 ZDOT =       4827
281346                 TA   =           22
41352
                                          MA   =           22
35261
                                          Ha   =            186
706  n
mi
                                          Hp   =            177
557

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10118802
00                 X    =        -3042742
18
 Y    =      -16589125
68  feet           Y    =        -5090622
69  meter
 Z    =       10334416
43                 Z    =         3135048
51
 XDOT =      19623
437679                 XDOT =        5964
559514
 YDOT =      -2121
266579  feet/sec       YDOT =        -579
769336  meter/sec
 ZDOT =      15837
537225                 ZDOT =        4856
297273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18387107
94                 X    =         5604390
50
 Y    =        6377425
38  feet           Y    =         1943839
26  meter
 Z    =       10277748
54                 Z    =         3132657
75
 XDOT =     -13297
086142                 XDOT =       -4052
951856
 YDOT =      12684
836386  feet/sec       YDOT =        3866
338131  meter/sec
 ZDOT =      15946
521989                 ZDOT =        4860
499902


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   07077
18130489  
00020000  00000-0  20000-3 0  9116
2 25544  51
6331 214
1803 0015823 322
8409  37
1660 15
77845894 36401


Satellite: ISS
Catalog Number: 25544
Epoch time:      07077
18130489   =   yrday
fracday
Element set:     911
Inclination:       51
6331  deg
RA of node:       214
1803  deg
Eccentricity:     
0015823     
Arg of perigee:   322
8409  deg
Mean anomaly:      37
1660  deg
Mean motion:   15
77845894  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3640
Checksum:              289


Coasting Arc #13 (Orbit 3654)
---------------------------------------

Vector Time (GMT): 2007/078/02:59:06
867
Vector Time (MET): N/A
Weight (LBS)     : 478751
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5833297
68                 A    =         6716213
61  meter
 Y    =        -154152
51  meter          E    =           
0013947
 Z    =       -3307641
09                 I    =           51
48656
 XDOT =      -2505
893148                 Wp   =          343
77105
 YDOT =      -5589
466193  meter/sec      RA   =          208
32765  deg
 ZDOT =       4688
302464                 TA   =          337
16291
                                          MA   =          337
22488
                                          Ha   =            186
724  n
mi
                                          Hp   =            177
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19138115
75                 X    =        -5815072
60
 Y    =        -505749
70  feet           Y    =         -219282
18  meter
 Z    =      -10851840
86                 Z    =        -3335934
72
 XDOT =      -8221
434211                 XDOT =       -2465
979423
 YDOT =     -18338
143677  feet/sec       YDOT =       -5617
264788  meter/sec
 ZDOT =      15381
569763                 ZDOT =        4676
226531

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14870282
75                 X    =         4532462
18
 Y    =      -11961506
09  feet           Y    =        -3645867
06  meter
 Z    =      -10958228
44                 Z    =        -3340068
03
 XDOT =      17328
893208                 XDOT =        5281
846650
 YDOT =       7518
966047  feet/sec       YDOT =        2291
780851  meter/sec
 ZDOT =      15335
367547                 ZDOT =        4674
220028


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   07078
13130871  
00020000  00000-0  20000-3 0  9128
2 25544  51
6340 209
2727 0015888 326
4186  33
5971 15
77899403 36550


Satellite: ISS
Catalog Number: 25544
Epoch time:      07078
13130871   =   yrday
fracday
Element set:     912
Inclination:       51
6340  deg
RA of node:       209
2727  deg
Eccentricity:     
0015888     
Arg of perigee:   326
4186  deg
Mean anomaly:      33
5971  deg
Mean motion:   15
77899403  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3655
Checksum:              310

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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:

http://www aus-city com/cgi-bin/dada/mail cgi/list/[list]

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

<mailto:list
admin@aus-city
com>

The following physical address is associated with this mailing list:

http://www aus-city com

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