Date: April 10th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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


There are no maneuvers



Coasting Arc #1 (Orbit 1738)
---------------------------------------

Vector Time (GMT): 2008/098/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5850544
02                 A    =         6718781
57  meter
 Y    =         597418
03  meter          E    =           
0012595
 Z    =        3238954
90                 I    =           51
75752
 XDOT =      -3177
663211                 Wp   =           87
18245
 YDOT =      -5150
742554  meter/sec      RA   =           19
89509  deg
 ZDOT =      -4773
333178                 TA   =           54
92069
                                          MA   =           54
80265
                                          Ha   =            185
294  n
mi
                                          Hp   =            179
095

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19194698
24                 X    =        -5872524
15
 Y    =        1960032
92  feet           Y    =          531871
13  meter
 Z    =       10626492
45                 Z    =         3210479
06
 XDOT =     -10425
404237                 XDOT =       -3096
642246
 YDOT =     -16898
761659  feet/sec       YDOT =       -5185
824167  meter/sec
 ZDOT =     -15660
541922                 ZDOT =       -4788
573533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13335505
88                 X    =        -4064662
19
 Y    =       14026779
89  feet           Y    =         4275362
51  meter
 Z    =       10517330
46                 Z    =         3205682
33
 XDOT =     -17826
185991                 XDOT =       -5433
421490
 YDOT =      -5120
214901  feet/sec       YDOT =       -1560
641502  meter/sec
 ZDOT =     -15719
516703                 ZDOT =       -4791
308691


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   08098
60827130  
00020000  00000-0  20000-3 0  9001
2 25544  51
6422  20
2271 0001253 345
4714  14
6414 15
77137005 17391


Satellite: ISS
Catalog Number: 25544
Epoch time:      08098
60827130   =   yrday
fracday
Element set:     900
Inclination:       51
6422  deg
RA of node:        20
2271  deg
Eccentricity:     
0001253     
Arg of perigee:   345
4714  deg
Mean anomaly:      14
6414  deg
Mean motion:   15
77137005  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1739
Checksum:              254


Coasting Arc #2 (Orbit 1754)
---------------------------------------

Vector Time (GMT): 2008/099/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1932389
41                 A    =         6713323
90  meter
 Y    =        4362370
85  meter          E    =           
0006735
 Z    =        4718334
67                 I    =           51
71252
 XDOT =      -7220
196401                 Wp   =          110
34269
 YDOT =        287
088872  meter/sec      RA   =           14
78808  deg
 ZDOT =       2686
220580                 TA   =          313
27396
                                          MA   =          313
33014
                                          Ha   =            185
101  n
mi
                                          Hp   =            178
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6339860
28                 X    =         1860543
89
 Y    =       14312240
32  feet           Y    =         4383578
24  meter
 Z    =       15480100
62                 Z    =         4727547
84
 XDOT =     -23688
308402                 XDOT =       -7235
919438
 YDOT =        941
892625  feet/sec       YDOT =         206
260607  meter/sec
 ZDOT =       8813
059646                 ZDOT =        2651
106099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14179720
86                 X    =         4321978
92
 Y    =        6546817
20  feet           Y    =         1995469
88  meter
 Z    =       15515871
47                 Z    =         4729237
62
 XDOT =     -16642
586915                 XDOT =       -5072
660492
 YDOT =      15436
714093  feet/sec       YDOT =        4705
110455  meter/sec
 ZDOT =       8678
401977                 ZDOT =        2645
176923


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   08099
62205802  
00020000  00000-0  20000-3 0  9011
2 25544  51
6428  14
9962 0001308 345
5024  14
6103 15
77195041 17557


Satellite: ISS
Catalog Number: 25544
Epoch time:      08099
62205802   =   yrday
fracday
Element set:     901
Inclination:       51
6428  deg
RA of node:        14
9962  deg
Eccentricity:     
0001308     
Arg of perigee:   345
5024  deg
Mean anomaly:      14
6103  deg
Mean motion:   15
77195041  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1755
Checksum:              270


Coasting Arc #3 (Orbit 1769)
---------------------------------------

Vector Time (GMT): 2008/100/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6584416
48                 A    =         6722181
28  meter
 Y    =          49224
36  meter          E    =           
0009846
 Z    =       -1329603
17                 I    =           51
71434
 XDOT =       1140
180192                 Wp   =           30
42227
 YDOT =       4879
385429  meter/sec      RA   =            9
59980  deg
 ZDOT =       5854
105686                 TA   =          314
97214
                                          MA   =          315
05192
                                          Ha   =            185
051  n
mi
                                          Hp   =            178
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21602416
28                 X    =         6589835
73
 Y    =         161497
24  feet           Y    =          122885
40  meter
 Z    =       -4362215
13                 Z    =        -1297602
51
 XDOT =       3740
748663                 XDOT =        1057
094856
 YDOT =      16008
482379  feet/sec       YDOT =        4891
670880  meter/sec
 ZDOT =      19206
383484                 ZDOT =        5859
443053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16027230
50                 X    =         4885099
86
 Y    =      -14521508
78  feet           Y    =        -4426155
88  meter
 Z    =       -4239464
19                 Z    =        -1292188
69
 XDOT =      12451
029449                 XDOT =        3795
073776
 YDOT =       8155
472644  feet/sec       YDOT =        2485
788062  meter/sec
 ZDOT =      19227
333595                 ZDOT =        5860
491280


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   08100
57245363  
00020000  00000-0  20000-3 0  9025
2 25544  51
6429  10
0921 0001360 342
7068  17
4051 15
77260254 17704


Satellite: ISS
Catalog Number: 25544
Epoch time:      08100
57245363   =   yrday
fracday
Element set:     902
Inclination:       51
6429  deg
RA of node:        10
0921  deg
Eccentricity:     
0001360     
Arg of perigee:   342
7068  deg
Mean anomaly:      17
4051  deg
Mean motion:   15
77260254  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1770
Checksum:              251


Coasting Arc #4 (Orbit 1785)
---------------------------------------

Vector Time (GMT): 2008/101/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          29543
88                 A    =         6710679
51  meter
 Y    =       -4176472
12  meter          E    =           
0014746
 Z    =       -5265152
28                 I    =           51
64660
 XDOT =       7681
313686                 Wp   =           82
47283
 YDOT =        389
002672  meter/sec      RA   =            4
45668  deg
 ZDOT =       -264
199778                 TA   =          185
01066
                                          MA   =          185
02544
                                          Ha   =            184
922  n
mi
                                          Hp   =            178
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          96928
74                 X    =          101820
99
 Y    =      -13702336
34  feet           Y    =        -4175737
41  meter
 Z    =      -17274121
65                 Z    =        -5264833
35
 XDOT =      25201
160388                 XDOT =        7677
676348
 YDOT =       1276
255487  feet/sec       YDOT =         474
879183  meter/sec
 ZDOT =       -866
797173                 ZDOT =        -226
892507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9306691
77                 X    =        -2836679
65
 Y    =      -10058686
29  feet           Y    =        -3065887
58  meter
 Z    =      -17273303
49                 Z    =        -5264902
90
 XDOT =      18402
268518                 XDOT =        5609
011444
 YDOT =     -15776
669247  feet/sec       YDOT =       -4808
728787  meter/sec
 ZDOT =       -723
652485                 ZDOT =        -220
569277


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   08101
58617774  
00020000  00000-0  20000-3 0  9037
2 25544  51
6425   4
8606 0001434 343
0052  17
1065 15
77317149 17865


Satellite: ISS
Catalog Number: 25544
Epoch time:      08101
58617774   =   yrday
fracday
Element set:     903
Inclination:       51
6425  deg
RA of node:         4
8606  deg
Eccentricity:     
0001434     
Arg of perigee:   343
0052  deg
Mean anomaly:      17
1065  deg
Mean motion:   15
77317149  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1786
Checksum:              274


Coasting Arc #5 (Orbit 1801)
---------------------------------------

Vector Time (GMT): 2008/102/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6629237
21                 A    =         6722398
44  meter
 Y    =        -627184
84  meter          E    =           
0008837
 Z    =        -894692
34                 I    =           51
65682
 XDOT =       1245
566643                 Wp   =          138
52587
 YDOT =      -4726
316930  meter/sec      RA   =          359
30386  deg
 ZDOT =      -5955
718732                 TA   =           51
24953
                                          MA   =           51
17059
                                          Ha   =            184
890  n
mi
                                          Hp   =            178
845

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21749465
92                 X    =        -6617384
97
 Y    =       -2057693
03  feet           Y    =         -701250
45  meter
 Z    =       -2935342
31                 Z    =         -926868
46
 XDOT =       4086
504735                 XDOT =        1327
256332
 YDOT =     -15506
289141  feet/sec       YDOT =       -4711
931315  meter/sec
 ZDOT =     -19539
759621                 ZDOT =       -5949
469516

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16924341
88                 X    =        -5158539
41
 Y    =       13787668
25  feet           Y    =         4202481
28  meter
 Z    =       -3058832
91                 Z    =         -932332
27
 XDOT =      -6888
148686                 XDOT =       -2099
507719
 YDOT =     -12757
091333  feet/sec       YDOT =       -3888
361438  meter/sec
 ZDOT =     -19516
244396                 ZDOT =       -5948
551292


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   08102
59987102  
00020000  00000-0  20000-3 0  9045
2 25544  51
6424 359
6294 0001279 339
5756  20
5358 15
77308526 18027


Satellite: ISS
Catalog Number: 25544
Epoch time:      08102
59987102   =   yrday
fracday
Element set:     904
Inclination:       51
6424  deg
RA of node:       359
6294  deg
Eccentricity:     
0001279     
Arg of perigee:   339
5756  deg
Mean anomaly:      20
5358  deg
Mean motion:   15
77308526  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1802
Checksum:              304


Coasting Arc #6 (Orbit 1817)
---------------------------------------

Vector Time (GMT): 2008/103/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2117516
31                 A    =         6712104
10  meter
 Y    =        4100486
34  meter          E    =           
0007222
 Z    =        4871173
91                 I    =           51
59379
 XDOT =      -7289
872902                 Wp   =           45
77392
 YDOT =      -1058
349038  meter/sec      RA   =          354
11370  deg
 ZDOT =      -2271
007131                 TA   =           66
34775
                                          MA   =           66
27196
                                          Ha   =            184
788  n
mi
                                          Hp   =            178
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6947232
00                 X    =        -2186874
43
 Y    =       13453039
17  feet           Y    =         4076419
14  meter
 Z    =       15981541
71                 Z    =         4860718
68
 XDOT =     -23916
905845                 XDOT =       -7266
464369
 YDOT =      -3472
273747  feet/sec       YDOT =       -1139
737622  meter/sec
 ZDOT =      -7450
810797                 ZDOT =       -2306
364396

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4678310
61                 X    =         1425949
07
 Y    =       14444009
36  feet           Y    =         4402534
05  meter
 Z    =       15941830
95                 Z    =         4859070
07
 XDOT =     -18140
930483                 XDOT =       -5529
355611
 YDOT =      14274
474414  feet/sec       YDOT =        4350
859802  meter/sec
 ZDOT =      -7586
551342                 ZDOT =       -2312
380849


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   08103
61352940  
00020000  00000-0  20000-3 0  9056
2 25544  51
6424 354
3972 0001527 341
6108  18
5002 15
77432637 18184


Satellite: ISS
Catalog Number: 25544
Epoch time:      08103
61352940   =   yrday
fracday
Element set:     905
Inclination:       51
6424  deg
RA of node:       354
3972  deg
Eccentricity:     
0001527     
Arg of perigee:   341
6108  deg
Mean anomaly:      18
5002  deg
Mean motion:   15
77432637  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1818
Checksum:              272


Coasting Arc #7 (Orbit 1833)
---------------------------------------

Vector Time (GMT): 2008/104/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5878866
69                 A    =         6718441
54  meter
 Y    =        1264871
36  meter          E    =           
0013076
 Z    =        2981397
99                 I    =           51
58555
 XDOT =      -3542
746993                 Wp   =           76
53537
 YDOT =       4707
191673  meter/sec      RA   =          348
99090  deg
 ZDOT =       4973
542880                 TA   =          317
99971
                                          MA   =          318
09990
                                          Ha   =            184
675  n
mi
                                          Hp   =            178
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19287620
39                 X    =         5849802
76
 Y    =        4149840
43  feet           Y    =         1330449
70  meter
 Z    =        9781489
48                 Z    =         3009886
78
 XDOT =     -11623
185672                 XDOT =       -3619
280681
 YDOT =      15443
542235  feet/sec       YDOT =        4667
146714  meter/sec
 ZDOT =      16317
397901                 ZDOT =        4956
146425

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16239037
72                 X    =         4949658
70
 Y    =      -11107415
69  feet           Y    =        -3385540
30  meter
 Z    =        9890904
05                 Z    =         3014747
55
 XDOT =       2344
023072                 XDOT =         714
458232
 YDOT =      17942
053206  feet/sec       YDOT =        5468
737817  meter/sec
 ZDOT =      16251
119456                 ZDOT =        4953
341210


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   08104
62715916  
00020000  00000-0  20000-3 0  9065
2 25544  51
6414 349
1646 0001581 344
2290  15
8826 15
77440206 18347


Satellite: ISS
Catalog Number: 25544
Epoch time:      08104
62715916   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:       349
1646  deg
Eccentricity:     
0001581     
Arg of perigee:   344
2290  deg
Mean anomaly:      15
8826  deg
Mean motion:   15
77440206  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1834
Checksum:              284


Coasting Arc #8 (Orbit 1848)
---------------------------------------

Vector Time (GMT): 2008/105/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3946906
09                 A    =         6716748
28  meter
 Y    =       -4100792
60  meter          E    =           
0004920
 Z    =       -3569906
75                 I    =           51
55096
 XDOT =       5998
298479                 Wp   =           80
16877
 YDOT =       1919
664427  meter/sec      RA   =          343
77258  deg
 ZDOT =       4432
596287                 TA   =          237
10705
                                          MA   =          237
15440
                                          Ha   =            184
679  n
mi
                                          Hp   =            178
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12949166
97                 X    =         4009810
32
 Y    =      -13454043
97  feet           Y    =        -4056304
40  meter
 Z    =      -11712292
49                 Z    =        -3550579
91
 XDOT =      19679
456952                 XDOT =        5954
854051
 YDOT =       6298
111638  feet/sec       YDOT =        1986
498009  meter/sec
 ZDOT =      14542
638737                 ZDOT =        4461
630296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1137345
10                 X    =         -346662
79
 Y    =      -18684768
15  feet           Y    =        -5695117
33  meter
 Z    =      -11638552
54                 Z    =        -3547430
81
 XDOT =      16514
070639                 XDOT =        5033
488731
 YDOT =     -10120
856533  feet/sec       YDOT =       -3084
837071  meter/sec
 ZDOT =      14654
210240                 ZDOT =        4466
603281


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   08105
57740672  
00020000  00000-0  20000-3 0  9078
2 25544  51
6407 344
2589 0001521 343
5938  16
5178 15
77496390 18495


Satellite: ISS
Catalog Number: 25544
Epoch time:      08105
57740672   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:       344
2589  deg
Eccentricity:     
0001521     
Arg of perigee:   343
5938  deg
Mean anomaly:      16
5178  deg
Mean motion:   15
77496390  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1849
Checksum:              315


Coasting Arc #9 (Orbit 1864)
---------------------------------------

Vector Time (GMT): 2008/106/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4425651
98                 A    =         6712938
11  meter
 Y    =       -2169941
64  meter          E    =           
0010772
 Z    =       -4567889
18                 I    =           51
50985
 XDOT =       5361
081136                 Wp   =           61
46224
 YDOT =      -4645
913751  meter/sec      RA   =          338
65115  deg
 ZDOT =      -2987
391312                 TA   =          178
81374
                                          MA   =          178
81119
                                          Ha   =            184
613  n
mi
                                          Hp   =            178
355

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14519855
58                 X    =        -4378868
52
 Y    =       -7119231
11  feet           Y    =        -2219170
42  meter
 Z    =      -14986513
05                 Z    =        -4589275
20
 XDOT =      17588
848873                 XDOT =        5427
146185
 YDOT =     -15242
499182  feet/sec       YDOT =       -4585
593806  meter/sec
 ZDOT =      -9801
152598                 ZDOT =       -2961
186605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14894450
17                 X    =        -4539828
41
 Y    =        6098587
66  feet           Y    =         1858849
52  meter
 Z    =      -15068769
48                 Z    =        -4592960
94
 XDOT =        712
161522                 XDOT =         217
066832
 YDOT =     -22228
711322  feet/sec       YDOT =       -6775
311211  meter/sec
 ZDOT =      -9701
086035                 ZDOT =       -2956
891024


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   08106
59097408  
00020000  00000-0  20000-3 0  9084
2 25544  51
6396 339
0265 0001539 345
8344  14
2778 15
77535840 18653


Satellite: ISS
Catalog Number: 25544
Epoch time:      08106
59097408   =   yrday
fracday
Element set:     908
Inclination:       51
6396  deg
RA of node:       339
0265  deg
Eccentricity:     
0001539     
Arg of perigee:   345
8344  deg
Mean anomaly:      14
2778  deg
Mean motion:   15
77535840  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1865
Checksum:              319


Coasting Arc #10 (Orbit 1880)
---------------------------------------

Vector Time (GMT): 2008/107/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5225352
05                 A    =         6720948
57  meter
 Y    =        3943232
90  meter          E    =           
0013036
 Z    =        1497833
13                 I    =           51
51131
 XDOT =      -4026
321490                 Wp   =          112
49454
 YDOT =      -3126
272000  meter/sec      RA   =          333
44262  deg
 ZDOT =      -5781
001001                 TA   =           50
94925
                                          MA   =           50
83332
                                          Ha   =            184
523  n
mi
                                          Hp   =            178
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17143543
48                 X    =        -5276333
75
 Y    =       12937115
82  feet           Y    =         3884515
05  meter
 Z    =        4914150
69                 Z    =         1472324
31
 XDOT =     -13209
716176                 XDOT =       -3962
980693
 YDOT =     -10256
797901  feet/sec       YDOT =       -3170
942771  meter/sec
 ZDOT =     -18966
538716                 ZDOT =       -5800
406874

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1312327
80                 X    =         -399997
51
 Y    =       21459175
77  feet           Y    =         6540756
77  meter
 Z    =        4816689
42                 Z    =         1468126
94
 XDOT =     -14743
081193                 XDOT =       -4493
691147
 YDOT =       3398
628723  feet/sec       YDOT =        1035
902035  meter/sec
 ZDOT =     -19041
292971                 ZDOT =       -5803
786098


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   08107
60450911  
00020000  00000-0  20000-3 0  9090
2 25544  51
6402 333
7939 0001708 348
3406  11
7719 15
77623716 18810


Satellite: ISS
Catalog Number: 25544
Epoch time:      08107
60450911   =   yrday
fracday
Element set:     909
Inclination:       51
6402  deg
RA of node:       333
7939  deg
Eccentricity:     
0001708     
Arg of perigee:   348
3406  deg
Mean anomaly:      11
7719  deg
Mean motion:   15
77623716  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1881
Checksum:              292


Coasting Arc #11 (Orbit 1896)
---------------------------------------

Vector Time (GMT): 2008/108/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2531087
01                 A    =         6709879
51  meter
 Y    =        3342088
45  meter          E    =           
0002392
 Z    =        5236986
19                 I    =           51
44696
 XDOT =      -6397
165374                 Wp   =           68
74480
 YDOT =       4287
340829  meter/sec      RA   =          328
28445  deg
 ZDOT =        356
484749                 TA   =           17
86954
                                          MA   =           17
86113
                                          Ha   =            184
507  n
mi
                                          Hp   =            178
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8304091
24                 X    =         2468086
65
 Y    =       10964857
13  feet           Y    =         3370040
54  meter
 Z    =       17181713
22                 Z    =         5249129
08
 XDOT =     -20988
075373                 XDOT =       -6446
363385
 YDOT =      14066
078836  feet/sec       YDOT =        4215
529006  meter/sec
 ZDOT =       1169
569385                 ZDOT =         325
287402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13680512
27                 X    =         4169820
14
 Y    =         644433
07  feet           Y    =          196423
20  meter
 Z    =       17228626
83                 Z    =         5251285
46
 XDOT =      -2457
304583                 XDOT =        -748
986437
 YDOT =      24148
913633  feet/sec       YDOT =        7360
588875  meter/sec
 ZDOT =       1050
326585                 ZDOT =         320
139543


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   08108
61801535  
00020000  00000-0  20000-3 0  9106
2 25544  51
6389 328
5602 0001520 352
6961   7
4181 15
77602751 18977


Satellite: ISS
Catalog Number: 25544
Epoch time:      08108
61801535   =   yrday
fracday
Element set:     910
Inclination:       51
6389  deg
RA of node:       328
5602  deg
Eccentricity:     
0001520     
Arg of perigee:   352
6961  deg
Mean anomaly:       7
4181  deg
Mean motion:   15
77602751  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1897
Checksum:              285


Coasting Arc #12 (Orbit 1912)
---------------------------------------

Vector Time (GMT): 2008/109/13:40:43
799
Vector Time (MET): N/A
Weight (LBS)     : 628879
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5722813
96                 A    =         6721354
89  meter
 Y    =       -3391508
54  meter          E    =           
0014472
 Z    =         906989
57                 I    =           51
46112
 XDOT =       1768
834533                 Wp   =           49
35212
 YDOT =       4586
907689  meter/sec      RA   =          323
11298  deg
 ZDOT =       5938
685955                 TA   =          320
59341
                                          MA   =          320
69860
                                          Ha   =            184
450  n
mi
                                          Hp   =            178
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18775636
35                 X    =         5755906
96
 Y    =      -11126996
53  feet           Y    =        -3327327
69  meter
 Z    =        2975687
57                 Z    =          934871
84
 XDOT =       5803
262904                 XDOT =        1688
562169
 YDOT =      15048
909741  feet/sec       YDOT =        4606
239252  meter/sec
 ZDOT =      19483
877806                 ZDOT =        5947
083855

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2978143
05                 X    =          907738
00
 Y    =      -21606003
40  feet           Y    =        -6585509
84  meter
 Z    =        3082299
42                 Z    =          939484
86
 XDOT =      13743
489028                 XDOT =        4189
015456
 YDOT =       4702
267339  feet/sec       YDOT =        1433
251085  meter/sec
 ZDOT =      19516
549201                 ZDOT =        5948
644197


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   08109
63148754  
00020000  00000-0  20000-3 0  9117
2 25544  51
6379 323
3261 0001523 352
8081   7
3061 15
77678814 19136


Satellite: ISS
Catalog Number: 25544
Epoch time:      08109
63148754   =   yrday
fracday
Element set:     911
Inclination:       51
6379  deg
RA of node:       323
3261  deg
Eccentricity:     
0001523     
Arg of perigee:   352
8081  deg
Mean anomaly:       7
3061  deg
Mean motion:   15
77678814  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1913
Checksum:              285

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:

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