Date: January 19th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 411)
---------------------------------------

Vector Time (GMT): 2008/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3939176
05                 A    =         6713634
42  meter
 Y    =       -2489358
23  meter          E    =           
0006872
 Z    =       -4839298
37                 I    =           51
94813
 XDOT =       1504
195628                 Wp   =           51
47524
 YDOT =       7143
869459  meter/sec      RA   =           93
32984  deg
 ZDOT =      -2448
564448                 TA   =          194
69771
                                          MA   =          194
71770
                                          Ha   =            183
447  n
mi
                                          Hp   =            181
543

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12923805
95                 X    =         3990227
87
 Y    =       -8167185
79  feet           Y    =        -2445022
45  meter
 Z    =      -15876963
14                 Z    =        -4820038
15
 XDOT =       4935
025026                 XDOT =        1436
094556
 YDOT =      23437
891926  feet/sec       YDOT =        7160
309570  meter/sec
 ZDOT =      -8033
347927                 ZDOT =       -2441
422226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12539780
00                 X    =         3822124
94
 Y    =        8877264
13  feet           Y    =         2705790
11  meter
 Z    =      -15803599
00                 Z    =        -4816936
98
 XDOT =     -19078
724761                 XDOT =       -5815
195307
 YDOT =      12687
845522  feet/sec       YDOT =        3867
255315  meter/sec
 ZDOT =      -8005
297530                 ZDOT =       -2440
014687


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   08014
52004876  
00020000  00000-0  20000-3 0  9004
2 25544  51
6382  93
9655 0006063 276
4356  83
6118 15
76964852  4129


Satellite: ISS
Catalog Number: 25544
Epoch time:      08014
52004876   =   yrday
fracday
Element set:     900
Inclination:       51
6382  deg
RA of node:        93
9655  deg
Eccentricity:     
0006063     
Arg of perigee:   276
4356  deg
Mean anomaly:      83
6118  deg
Mean motion:   15
76964852  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             412
Checksum:              295


Coasting Arc #2 (Orbit 427)
---------------------------------------

Vector Time (GMT): 2008/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1122775
89                 A    =         6722953
21  meter
 Y    =       -6519698
75  meter          E    =           
0008591
 Z    =        1168156
87                 I    =           51
98072
 XDOT =       4571
603353                 Wp   =          136
04153
 YDOT =      -1851
564677  meter/sec      RA   =           88
16383  deg
 ZDOT =      -5920
209457                 TA   =           31
20712
                                          MA   =           31
15615
                                          Ha   =            183
589  n
mi
                                          Hp   =            181
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3683647
93                 X    =        -1055462
83
 Y    =      -21390087
77  feet           Y    =        -6531877
97  meter
 Z    =        3832535
65                 Z    =         1162865
58
 XDOT =      14998
698665                 XDOT =        4620
727203
 YDOT =      -6074
687259  feet/sec       YDOT =       -1800
167404  meter/sec
 ZDOT =     -19423
259374                 ZDOT =       -5897
881520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18122353
15                 X    =         5523693
24
 Y    =      -11951787
09  feet           Y    =        -3642904
70  meter
 Z    =        3811633
26                 Z    =         1161785
82
 XDOT =      10739
223656                 XDOT =        3273
315370
 YDOT =      10095
765157  feet/sec       YDOT =        3077
189220  meter/sec
 ZDOT =     -19338
096977                 ZDOT =       -5894
251959


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   08015
53394185  
00020000  00000-0  20000-3 0  9012
2 25544  51
6382  88
7352 0005902 282
3625  77
6879 15
77040339  4281


Satellite: ISS
Catalog Number: 25544
Epoch time:      08015
53394185   =   yrday
fracday
Element set:     901
Inclination:       51
6382  deg
RA of node:        88
7352  deg
Eccentricity:     
0005902     
Arg of perigee:   282
3625  deg
Mean anomaly:      77
6879  deg
Mean motion:   15
77040339  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             428
Checksum:              305


Coasting Arc #3 (Orbit 443)
---------------------------------------

Vector Time (GMT): 2008/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4084709
41                 A    =         6711262
66  meter
 Y    =         682043
47  meter          E    =           
0003647
 Z    =        5284056
78                 I    =           51
94013
 XDOT =      -1061
732214                 Wp   =          291
46382
 YDOT =      -7628
782367  meter/sec      RA   =           83
03983  deg
 ZDOT =        165
341236                 TA   =          156
98243
                                          MA   =          156
96608
                                          Ha   =            183
761  n
mi
                                          Hp   =            181
188

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13401277
58                 X    =        -4117701
44
 Y    =        2237675
42  feet           Y    =          636181
03  meter
 Z    =       17336144
29                 Z    =         5264133
24
 XDOT =      -3483
373407                 XDOT =        -977
150287
 YDOT =     -25028
813540  feet/sec       YDOT =       -7640
182352  meter/sec
 ZDOT =        542
458122                 ZDOT =         160
388195

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7646725
57                 X    =        -2330721
95
 Y    =      -11347319
23  feet           Y    =        -3458662
90  meter
 Z    =       17260048
24                 Z    =         5260862
70
 XDOT =      20487
047667                 XDOT =        6244
452129
 YDOT =     -13017
670122  feet/sec       YDOT =       -3967
785853  meter/sec
 ZDOT =        522
744669                 ZDOT =         159
332575


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   08016
54779989  
00020000  00000-0  20000-3 0  9024
2 25544  51
6387  83
5043 0006013 286
2537  73
7966 15
77108449  4444


Satellite: ISS
Catalog Number: 25544
Epoch time:      08016
54779989   =   yrday
fracday
Element set:     902
Inclination:       51
6387  deg
RA of node:        83
5043  deg
Eccentricity:     
0006013     
Arg of perigee:   286
2537  deg
Mean anomaly:      73
7966  deg
Mean motion:   15
77108449  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             444
Checksum:              320


Coasting Arc #4 (Orbit 459)
---------------------------------------

Vector Time (GMT): 2008/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         697727
15                 A    =         6723019
90  meter
 Y    =        6618306
80  meter          E    =           
0011740
 Z    =         900121
92                 I    =           51
97454
 XDOT =      -4850
493440                 Wp   =           29
34955
 YDOT =       -305
468095  meter/sec      RA   =           77
91037  deg
 ZDOT =       5983
283441                 TA   =          340
44710
                                          MA   =          340
49209
                                          Ha   =            184
038  n
mi
                                          Hp   =            181
055

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2289131
06                 X    =          619295
76
 Y    =       21713604
97  feet           Y    =         6625670
55  meter
 Z    =        2953155
91                 Z    =          903321
68
 XDOT =     -15913
692387                 XDOT =       -4875
782743
 YDOT =      -1002
191912  feet/sec       YDOT =        -359
851116  meter/sec
 ZDOT =      19630
195016                 ZDOT =        5959
658372

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18610374
71                 X    =        -5672442
21
 Y    =       11414831
22  feet           Y    =         3479240
56  meter
 Z    =        2966053
46                 Z    =          904053
09
 XDOT =      -5174
474858                 XDOT =       -1577
179937
 YDOT =     -13532
730527  feet/sec       YDOT =       -4124
776265  meter/sec
 ZDOT =      19539
842872                 ZDOT =        5955
744108


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   08017
56162822  
00020000  00000-0  20000-3 0  9030
2 25544  51
6383  78
2735 0005848 293
5796  66
4755 15
77101416  4602


Satellite: ISS
Catalog Number: 25544
Epoch time:      08017
56162822   =   yrday
fracday
Element set:     903
Inclination:       51
6383  deg
RA of node:        78
2735  deg
Eccentricity:     
0005848     
Arg of perigee:   293
5796  deg
Mean anomaly:      66
4755  deg
Mean motion:   15
77101416  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             460
Checksum:              304


Coasting Arc #5 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2008/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4409460
61                 A    =         6712675
42  meter
 Y    =        1195517
52  meter          E    =           
0006875
 Z    =       -4924161
72                 I    =           51
93306
 XDOT =        472
268208                 Wp   =           96
74370
 YDOT =       7361
100517  meter/sec      RA   =           72
74643  deg
 ZDOT =       2211
903233                 TA   =          194
64387
                                          MA   =          194
66380
                                          Ha   =            184
136  n
mi
                                          Hp   =            180
978

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14466734
30                 X    =         4419684
94
 Y    =        3922301
57  feet           Y    =         1244884
44  meter
 Z    =      -16155386
23                 Z    =        -4902715
72
 XDOT =       1549
436378                 XDOT =         379
175209
 YDOT =      24150
592248  feet/sec       YDOT =        7365
860884  meter/sec
 ZDOT =       7256
900371                 ZDOT =        2213
972355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2994395
48                 X    =          912691
74
 Y    =       14776701
43  feet           Y    =         4503938
60  meter
 Z    =      -16073271
15                 Z    =        -4899133
05
 XDOT =     -19855
351368                 XDOT =       -6051
911097
 YDOT =      11920
043265  feet/sec       YDOT =        3633
229187  meter/sec
 ZDOT =       7265
539344                 ZDOT =        2214
536392


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   08018
51205831  
00020000  00000-0  20000-3 0  9045
2 25544  51
6384  73
3696 0005839 297
2845  62
7725 15
77177990  4753


Satellite: ISS
Catalog Number: 25544
Epoch time:      08018
51205831   =   yrday
fracday
Element set:     904
Inclination:       51
6384  deg
RA of node:        73
3696  deg
Eccentricity:     
0005839     
Arg of perigee:   297
2845  deg
Mean anomaly:      62
7725  deg
Mean motion:   15
77177990  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             475
Checksum:              320


Coasting Arc #6 (Orbit 490)
---------------------------------------

Vector Time (GMT): 2008/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -40127
49                 A    =         6719281
60  meter
 Y    =       -6062599
44  meter          E    =           
0001304
 Z    =       -2897800
18                 I    =           51
94696
 XDOT =       5277
545607                 Wp   =          329
55127
 YDOT =       2391
281824  meter/sec      RA   =           67
64938  deg
 ZDOT =      -5073
887559                 TA   =          243
65464
                                          MA   =          243
66802
                                          Ha   =            184
143  n
mi
                                          Hp   =            180
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -131651
85                 X    =           41745
22
 Y    =      -19890418
12  feet           Y    =        -6062589
97  meter
 Z    =       -9507218
44                 Z    =        -2897797
15
 XDOT =      17314
782176                 XDOT =        5275
061392
 YDOT =       7845
412809  feet/sec       YDOT =        2450
285197  meter/sec
 ZDOT =     -16646
612727                 ZDOT =       -5048
255256

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17603836
77                 X    =         5365649
45
 Y    =       -9259587
07  feet           Y    =        -2822322
14  meter
 Z    =       -9507799
24                 Z    =        -2897977
21
 XDOT =        410
938438                 XDOT =         125
254036
 YDOT =      17780
245120  feet/sec       YDOT =        5419
418713  meter/sec
 ZDOT =     -16548
367270                 ZDOT =       -5043
942344


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   08019
52581963  
00020000  00000-0  20000-3 0  9051
2 25544  51
6391  68
1385 0005697 302
2832  57
7780 15
77249257  4912


Satellite: ISS
Catalog Number: 25544
Epoch time:      08019
52581963   =   yrday
fracday
Element set:     905
Inclination:       51
6391  deg
RA of node:        68
1385  deg
Eccentricity:     
0005697     
Arg of perigee:   302
2832  deg
Mean anomaly:      57
7780  deg
Mean motion:   15
77249257  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             491
Checksum:              315


Coasting Arc #7 (Orbit 506)
---------------------------------------

Vector Time (GMT): 2008/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4790530
75                 A    =         6716788
89  meter
 Y    =       -2879594
58  meter          E    =           
0008498
 Z    =        3722778
28                 I    =           51
92617
 XDOT =        478
141750                 Wp   =           56
41389
 YDOT =      -6373
342604  meter/sec      RA   =           62
46013  deg
 ZDOT =      -4302
958304                 TA   =           78
82286
                                          MA   =           78
72734
                                          Ha   =            184
265  n
mi
                                          Hp   =            180
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15716964
39                 X    =        -4776058
86
 Y    =       -9447488
79  feet           Y    =        -2933084
65  meter
 Z    =       12213839
51                 Z    =         3699541
07
 XDOT =       1568
706528                 XDOT =         570
276479
 YDOT =     -20909
916680  feet/sec       YDOT =       -6367
479966  meter/sec
 ZDOT =     -14117
317270                 ZDOT =       -4300
412686

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         768443
66                 X    =          234221
63
 Y    =      -18380888
99  feet           Y    =        -5602494
96  meter
 Z    =       12124698
10                 Z    =         3695607
98
 XDOT =      17821
436279                 XDOT =        5431
973778
 YDOT =      -8586
481281  feet/sec       YDOT =       -2617
159495  meter/sec
 ZDOT =     -14108
200978                 ZDOT =       -4300
179658


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   08020
53954611  
00020000  00000-0  20000-3 0  9069
2 25544  51
6385  62
9072 0005797 306
8606  53
2027 15
77319405  5076


Satellite: ISS
Catalog Number: 25544
Epoch time:      08020
53954611   =   yrday
fracday
Element set:     906
Inclination:       51
6385  deg
RA of node:        62
9072  deg
Eccentricity:     
0005797     
Arg of perigee:   306
8606  deg
Mean anomaly:      53
2027  deg
Mean motion:   15
77319405  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             507
Checksum:              287


Coasting Arc #8 (Orbit 522)
---------------------------------------

Vector Time (GMT): 2008/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -980666
45                 A    =         6714063
94  meter
 Y    =        4931726
80  meter          E    =           
0004327
 Z    =        4445282
71                 I    =           51
90230
 XDOT =      -5660
971143                 Wp   =           85
19534
 YDOT =      -4079
554492  meter/sec      RA   =           57
36801  deg
 ZDOT =       3274
765750                 TA   =          332
11860
                                          MA   =          332
14179
                                          Ha   =            184
439  n
mi
                                          Hp   =            180
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3217409
63                 X    =        -1057334
70
 Y    =       16180206
04  feet           Y    =         4920331
17  meter
 Z    =       14584260
85                 Z    =         4440333
19
 XDOT =     -18572
739972                 XDOT =       -5630
840008
 YDOT =     -13384
365131  feet/sec       YDOT =       -4142
690650  meter/sec
 ZDOT =      10743
982121                 ZDOT =        3247
338118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15708268
18                 X    =        -4787880
14
 Y    =        5093030
56  feet           Y    =         1552355
71  meter
 Z    =       14565809
53                 Z    =         4439658
74
 XDOT =       2848
566611                 XDOT =         868
243103
 YDOT =     -21662
491949  feet/sec       YDOT =       -6602
727546  meter/sec
 ZDOT =      10638
690983                 ZDOT =        3242
673012


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   08021
55324087  
00020000  00000-0  20000-3 0  9071
2 25544  51
6381  57
6751 0005584 312
1734  47
8957 15
77344484  5237


Satellite: ISS
Catalog Number: 25544
Epoch time:      08021
55324087   =   yrday
fracday
Element set:     907
Inclination:       51
6381  deg
RA of node:        57
6751  deg
Eccentricity:     
0005584     
Arg of perigee:   312
1734  deg
Mean anomaly:      47
8957  deg
Mean motion:   15
77344484  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             523
Checksum:              300


Coasting Arc #9 (Orbit 537)
---------------------------------------

Vector Time (GMT): 2008/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4999647
75                 A    =         6721011
63  meter
 Y    =        4086556
95  meter          E    =           
0009780
 Z    =       -1842517
15                 I    =           51
91042
 XDOT =      -1875
449104                 Wp   =            3
58470
 YDOT =       4853
469730  meter/sec      RA   =           52
18507  deg
 ZDOT =       5686
762061                 TA   =          336
01177
                                          MA   =          336
05730
                                          Ha   =            184
464  n
mi
                                          Hp   =            179
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16403043
81                 X    =         4962530
01
 Y    =       13407339
07  feet           Y    =         4142258
51  meter
 Z    =       -6045003
79                 Z    =        -1818319
32
 XDOT =      -6153
048243                 XDOT =       -1957
206381
 YDOT =      15923
457119  feet/sec       YDOT =        4832
039656  meter/sec
 ZDOT =      18657
355844                 ZDOT =        5677
453342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3218206
10                 X    =         -980909
22
 Y    =       20966039
83  feet           Y    =         6390448
94  meter
 Z    =       -5952056
90                 Z    =        -1814186
94
 XDOT =     -15368
794011                 XDOT =       -4684
408414
 YDOT =       2917
063696  feet/sec       YDOT =         889
121014  meter/sec
 ZDOT =      18622
224231                 ZDOT =        5676
053946


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   08022
50354802  
00020000  00000-0  20000-3 0  9086
2 25544  51
6389  52
7703 0005566 315
6756  44
3963 15
77423311  5382


Satellite: ISS
Catalog Number: 25544
Epoch time:      08022
50354802   =   yrday
fracday
Element set:     908
Inclination:       51
6389  deg
RA of node:        52
7703  deg
Eccentricity:     
0005566     
Arg of perigee:   315
6756  deg
Mean anomaly:      44
3963  deg
Mean motion:   15
77423311  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             538
Checksum:              290


Coasting Arc #10 (Orbit 553)
---------------------------------------

Vector Time (GMT): 2008/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2384051
22                 A    =         6710539
49  meter
 Y    =       -3472199
51  meter          E    =           
0012484
 Z    =       -5234197
91                 I    =           51
85626
 XDOT =       5669
059642                 Wp   =           61
64106
 YDOT =       5142
185592  meter/sec      RA   =           47
06424  deg
 ZDOT =       -824
715205                 TA   =          200
50465
                                          MA   =          200
55480
                                          Ha   =            184
538  n
mi
                                          Hp   =            179
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7821690
34                 X    =         2448126
68
 Y    =      -11391730
68  feet           Y    =        -3445181
03  meter
 Z    =      -17172565
31                 Z    =        -5222461
18
 XDOT =      18599
277042                 XDOT =        5615
143792
 YDOT =      16870
687637  feet/sec       YDOT =        5205
278844  meter/sec
 ZDOT =      -2705
758548                 ZDOT =        -797
306347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13850069
41                 X    =         4221501
16
 Y    =         808775
12  feet           Y    =          246514
66  meter
 Z    =      -17128012
94                 Z    =        -5220618
34
 XDOT =      -4615
865655                 XDOT =       -1406
915852
 YDOT =      23673
189052  feet/sec       YDOT =        7215
588023  meter/sec
 ZDOT =      -2600
420998                 ZDOT =        -792
608320


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   08023
51717574  
00020000  00000-0  20000-3 0  9098
2 25544  51
6389  47
5378 0005638 319
6745  40
4001 15
77434274  5542


Satellite: ISS
Catalog Number: 25544
Epoch time:      08023
51717574   =   yrday
fracday
Element set:     909
Inclination:       51
6389  deg
RA of node:        47
5378  deg
Eccentricity:     
0005638     
Arg of perigee:   319
6745  deg
Mean anomaly:      40
4001  deg
Mean motion:   15
77434274  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             554
Checksum:              302


Coasting Arc #11 (Orbit 569)
---------------------------------------

Vector Time (GMT): 2008/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4741366
65                 A    =         6722140
79  meter
 Y    =       -4739732
11  meter          E    =           
0005730
 Z    =        -458208
36                 I    =           51
87410
 XDOT =       3659
492814                 Wp   =          132
56208
 YDOT =      -3082
078130  meter/sec      RA   =           41
91526  deg
 ZDOT =      -6037
141848                 TA   =           52
41060
                                          MA   =           52
35858
                                          Ha   =            184
595  n
mi
                                          Hp   =            179
439

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15555664
85                 X    =        -4685788
02
 Y    =      -15550302
20  feet           Y    =        -4792441
99  meter
 Z    =       -1503308
28                 Z    =         -481106
46
 XDOT =      12006
210019                 XDOT =        3723
011564
 YDOT =     -10111
804887  feet/sec       YDOT =       -3040
800162  meter/sec
 ZDOT =     -19806
895828                 ZDOT =       -6019
210432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4781087
34                 X    =         1457275
42
 Y    =      -21462975
79  feet           Y    =        -6541915
02  meter
 Z    =       -1591357
02                 Z    =         -485045
62
 XDOT =      13469
832907                 XDOT =        4105
605070
 YDOT =       4452
258343  feet/sec       YDOT =        1357
048343  meter/sec
 ZDOT =     -19738
611817                 ZDOT =       -6016
328882


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   08024
53076916  
00020000  00000-0  20000-3 0  9101
2 25544  51
6378  42
3047 0005547 324
9445  35
1354 15
77496665  5703


Satellite: ISS
Catalog Number: 25544
Epoch time:      08024
53076916   =   yrday
fracday
Element set:     910
Inclination:       51
6378  deg
RA of node:        42
3047  deg
Eccentricity:     
0005547     
Arg of perigee:   324
9445  deg
Mean anomaly:      35
1354  deg
Mean motion:   15
77496665  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             570
Checksum:              296


Coasting Arc #12 (Orbit 585)
---------------------------------------

Vector Time (GMT): 2008/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4016584
36                 A    =         6711143
24  meter
 Y    =        1928088
69  meter          E    =           
0008218
 Z    =        5019612
18                 I    =           51
81447
 XDOT =      -5002
190773                 Wp   =           12
02633
 YDOT =      -5559
395525  meter/sec      RA   =           36
74676  deg
 ZDOT =      -1858
795139                 TA   =           95
89176
                                          MA   =           95
79808
                                          Ha   =            184
734  n
mi
                                          Hp   =            179
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13177770
22                 X    =        -4062229
74
 Y    =        6325750
28  feet           Y    =         1882917
61  meter
 Z    =       16468543
91                 Z    =         4999989
32
 XDOT =     -16411
387051                 XDOT =       -4930
623540
 YDOT =     -18239
486629  feet/sec       YDOT =       -5614
932668  meter/sec
 ZDOT =      -6098
409250                 ZDOT =       -1882
921437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12590815
78                 X    =        -3837680
65
 Y    =       -7589490
15  feet           Y    =        -2313276
60  meter
 Z    =       16393678
06                 Z    =         4996793
07
 XDOT =       5644
801767                 XDOT =        1720
535578
 YDOT =     -22797
966226  feet/sec       YDOT =       -6948
820106  meter/sec
 ZDOT =      -6191
237333                 ZDOT =       -1887
089139


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   08025
54432715  
00020000  00000-0  20000-3 0  9117
2 25544  51
6373  37
0715 0005605 329
2136  30
8699 15
77564639  5869


Satellite: ISS
Catalog Number: 25544
Epoch time:      08025
54432715   =   yrday
fracday
Element set:     911
Inclination:       51
6373  deg
RA of node:        37
0715  deg
Eccentricity:     
0005605     
Arg of perigee:   329
2136  deg
Mean anomaly:      30
8699  deg
Mean motion:   15
77564639  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             586
Checksum:              298

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

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