Date: December 28th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 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


There are no maneuvers



Coasting Arc #1 (Orbit 1768)
---------------------------------------

Vector Time (GMT): 2008/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2186597
35                 A    =         6732575
48  meter
 Y    =        5114955
86  meter          E    =           
0013807
 Z    =       -3807222
80                 I    =           51
82271
 XDOT =      -6421
624539                 Wp   =          106
86839
 YDOT =        378
093693  meter/sec      RA   =          145
70360  deg
 ZDOT =       4204
685921                 TA   =          207
20239
                                          MA   =          207
27478
                                          Ha   =            196
415  n
mi
                                          Hp   =            184
727

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7173875
82                 X    =        -2225136
26
 Y    =       16781351
24  feet           Y    =         5090288
88  meter
 Z    =      -12490888
44                 Z    =        -3817938
52
 XDOT =     -21068
321979                 XDOT =       -6445
800833
 YDOT =       1240
464871  feet/sec       YDOT =         306
147856  meter/sec
 ZDOT =      13794
901314                 ZDOT =        4173
430887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16482709
47                 X    =        -5023929
84
 Y    =       -7769581
42  feet           Y    =        -2368168
42  meter
 Z    =      -12532135
92                 Z    =        -3819795
03
 XDOT =       -957
555170                 XDOT =        -291
862816
 YDOT =     -19978
157310  feet/sec       YDOT =       -6089
342348  meter/sec
 ZDOT =      13673
438875                 ZDOT =        4167
664169


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   08354
50819197  
00010596  00000-0  82463-4 0  9000
2 25544  51
6389 146
6585 0007537 107
9744 252
2240 15
71643793 17699


Satellite: ISS
Catalog Number: 25544
Epoch time:      08354
50819197   =   yrday
fracday
Element set:     900
Inclination:       51
6389  deg
RA of node:       146
6585  deg
Eccentricity:     
0007537     
Arg of perigee:   107
9744  deg
Mean anomaly:     252
2240  deg
Mean motion:   15
71643793  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1769
Checksum:              339


Coasting Arc #2 (Orbit 1784)
---------------------------------------

Vector Time (GMT): 2008/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5764751
47                 A    =         6734696
83  meter
 Y    =       -1559845
43  meter          E    =           
0011986
 Z    =       -3118058
89                 I    =           51
85334
 XDOT =      -1057
193918                 Wp   =          109
07783
 YDOT =       5837
532401  meter/sec      RA   =          140
64992  deg
 ZDOT =      -4893
918360                 TA   =          106
97349
                                          MA   =          106
84209
                                          Ha   =            196
392  n
mi
                                          Hp   =            184
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18913226
61                 X    =         5796912
53
 Y    =       -5117603
12  feet           Y    =        -1495200
55  meter
 Z    =      -10229851
99                 Z    =        -3089975
56
 XDOT =      -3468
483983                 XDOT =       -1098
617669
 YDOT =      19152
009188  feet/sec       YDOT =        5825
479055  meter/sec
 ZDOT =     -16056
162598                 ZDOT =       -4899
154357

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4681236
14                 X    =         1426840
77
 Y    =       19084162
13  feet           Y    =         5816852
62  meter
 Z    =      -10120803
25                 Z    =        -3084820
83
 XDOT =     -17677
728458                 XDOT =       -5388
171634
 YDOT =      -4155
773165  feet/sec       YDOT =       -1266
679661  meter/sec
 ZDOT =     -16076
059128                 ZDOT =       -4899
982822


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   08355
52554367  
00010596  00000-0  82463-4 0  9019
2 25544  51
6387 141
4517 0007477 110
9350 249
2613 15
71666491 17853


Satellite: ISS
Catalog Number: 25544
Epoch time:      08355
52554367   =   yrday
fracday
Element set:     901
Inclination:       51
6387  deg
RA of node:       141
4517  deg
Eccentricity:     
0007477     
Arg of perigee:   110
9350  deg
Mean anomaly:     249
2613  deg
Mean motion:   15
71666491  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1785
Checksum:              322


Coasting Arc #3 (Orbit 1800)
---------------------------------------

Vector Time (GMT): 2008/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -344193
52                 A    =         6729394
34  meter
 Y    =       -4813078
65  meter          E    =           
0013887
 Z    =        4678752
66                 I    =           51
85712
 XDOT =       6416
825190                 Wp   =           88
59348
 YDOT =      -3204
246231  meter/sec      RA   =          135
50164  deg
 ZDOT =      -2816
707687                 TA   =           29
14138
                                          MA   =           29
06396
                                          Ha   =            196
431  n
mi
                                          Hp   =            184
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1129243
83                 X    =         -313076
04
 Y    =      -15790940
44  feet           Y    =        -4816754
10  meter
 Z    =       15350238
39                 Z    =         4677155
66
 XDOT =      21052
576084                 XDOT =        6465
861858
 YDOT =     -10512
618867  feet/sec       YDOT =       -3132
215118  meter/sec
 ZDOT =      -9241
166952                 ZDOT =       -2785
415680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15797496
85                 X    =         4815077
04
 Y    =       -1126965
62  feet           Y    =         -343499
12  meter
 Z    =       15343658
36                 Z    =         4676747
07
 XDOT =      10309
317606                 XDOT =        3142
280006
 YDOT =      20013
378138  feet/sec       YDOT =        6100
077656  meter/sec
 ZDOT =      -9119
760683                 ZDOT =       -2779
703056


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   08356
54288810  
00010596  00000-0  82463-4 0  9020
2 25544  51
6385 136
2448 0007571 115
2270 244
9677 15
71636893 18014


Satellite: ISS
Catalog Number: 25544
Epoch time:      08356
54288810   =   yrday
fracday
Element set:     902
Inclination:       51
6385  deg
RA of node:       136
2448  deg
Eccentricity:     
0007571     
Arg of perigee:   115
2270  deg
Mean anomaly:     244
9677  deg
Mean motion:   15
71636893  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1801
Checksum:              324


Coasting Arc #4 (Orbit 1816)
---------------------------------------

Vector Time (GMT): 2008/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5166063
10                 A    =         6737418
94  meter
 Y    =        3944188
31  meter          E    =           
0019445
 Z    =        1752213
10                 I    =           51
90608
 XDOT =      -1749
591864                 Wp   =           83
27633
 YDOT =      -4853
026912  meter/sec      RA   =          130
43822  deg
 ZDOT =       5714
080742                 TA   =          296
03755
                                          MA   =          296
23763
                                          Ha   =            196
251  n
mi
                                          Hp   =            184
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16949025
93                 X    =        -5218295
72
 Y    =       12940250
37  feet           Y    =         3886126
15  meter
 Z    =        5748730
63                 Z    =         1726989
70
 XDOT =      -5740
130787                 XDOT =       -1722
952726
 YDOT =     -15922
004304  feet/sec       YDOT =       -4872
443583  meter/sec
 ZDOT =      18746
984062                 ZDOT =        5705
645280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13134184
39                 X    =        -4003299
40
 Y    =      -16832329
32  feet           Y    =        -5130493
98  meter
 Z    =        5650960
41                 Z    =         1722412
73
 XDOT =      14626
261861                 XDOT =        4458
084615
 YDOT =      -5072
336121  feet/sec       YDOT =       -1546
048050  meter/sec
 ZDOT =      18713
819519                 ZDOT =        5703
972189


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   08357
56022014  
00010596  00000-0  82463-4 0  9036
2 25544  51
6398 131
0385 0007506 119
4198 240
7714 15
71710656 18177


Satellite: ISS
Catalog Number: 25544
Epoch time:      08357
56022014   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:       131
0385  deg
Eccentricity:     
0007506     
Arg of perigee:   119
4198  deg
Mean anomaly:     240
7714  deg
Mean motion:   15
71710656  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1817
Checksum:              303


Coasting Arc #5 (Orbit 1831)
---------------------------------------

Vector Time (GMT): 2008/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2558983
50                 A    =         6727079
93  meter
 Y    =        3443697
28  meter          E    =           
0021402
 Z    =       -5199918
72                 I    =           51
88973
 XDOT =      -5115
819531                 Wp   =          106
93662
 YDOT =       5604
376332  meter/sec      RA   =          125
31350  deg
 ZDOT =       1191
890701                 TA   =          174
44910
                                          MA   =          174
42534
                                          Ha   =            196
180  n
mi
                                          Hp   =            184
938

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8395615
14                 X    =         2545545
81
 Y    =       11298219
41  feet           Y    =         3472238
88  meter
 Z    =      -17060100
80                 Z    =        -5187519
24
 XDOT =     -16784
184812                 XDOT =       -5183
898406
 YDOT =      18387
061456  feet/sec       YDOT =        5546
787466  meter/sec
 ZDOT =       3910
402561                 ZDOT =        1166
873218

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11049913
50                 X    =        -3368013
63
 Y    =        8814020
29  feet           Y    =         2686513
38  meter
 Z    =      -17011631
69                 Z    =        -5185145
34
 XDOT =     -18218
576130                 XDOT =       -5553
022004
 YDOT =     -15466
665354  feet/sec       YDOT =       -4714
239600  meter/sec
 ZDOT =       3813
540792                 ZDOT =        1162
367233


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   08358
51396373  
00010596  00000-0  82463-4 0  9045
2 25544  51
6401 126
1582 0007466 121
7517 238
4374 15
71714750 18324


Satellite: ISS
Catalog Number: 25544
Epoch time:      08358
51396373   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       126
1582  deg
Eccentricity:     
0007466     
Arg of perigee:   121
7517  deg
Mean anomaly:     238
4374  deg
Mean motion:   15
71714750  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1832
Checksum:              309


Coasting Arc #6 (Orbit 1847)
---------------------------------------

Vector Time (GMT): 2008/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3598372
94                 A    =         6738643
04  meter
 Y    =       -5678898
56  meter          E    =           
0018896
 Z    =        -319665
80                 I    =           51
94495
 XDOT =       3865
941679                 Wp   =          132
81047
 YDOT =       2777
005932  meter/sec      RA   =          120
22677  deg
 ZDOT =      -6052
799049                 TA   =           50
64753
                                          MA   =           50
48025
                                          Ha   =            196
133  n
mi
                                          Hp   =            184
963

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11805685
50                 X    =         3663160
76
 Y    =      -18631556
94  feet           Y    =        -5638297
17  meter
 Z    =       -1048772
32                 Z    =         -302028
28
 XDOT =      12683
535691                 XDOT =        3864
005012
 YDOT =       9110
911851  feet/sec       YDOT =        2820
227216  meter/sec
 ZDOT =     -19858
264596                 ZDOT =       -6034
022461

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19153587
54                 X    =         5838013
48
 Y    =       10944750
45  feet           Y    =         3335959
94  meter
 Z    =        -980596
51                 Z    =         -298885
82
 XDOT =      -7716
161690                 XDOT =       -2351
886083
 YDOT =      11805
220392  feet/sec       YDOT =        3598
231176  meter/sec
 ZDOT =     -19785
044917                 ZDOT =       -6030
481691


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   08359
53128039  
00010596  00000-0  82463-4 0  9051
2 25544  51
6403 120
9505 0007375 125
4436 234
7416 15
71717604 18487


Satellite: ISS
Catalog Number: 25544
Epoch time:      08359
53128039   =   yrday
fracday
Element set:     905
Inclination:       51
6403  deg
RA of node:       120
9505  deg
Eccentricity:     
0007375     
Arg of perigee:   125
4436  deg
Mean anomaly:     234
7416  deg
Mean motion:   15
71717604  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1848
Checksum:              308


Coasting Arc #7 (Orbit 1863)
---------------------------------------

Vector Time (GMT): 2008/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3979530
97                 A    =         6726579
11  meter
 Y    =       -1243417
47  meter          E    =           
0009921
 Z    =        5272064
85                 I    =           51
91977
 XDOT =       2901
864427                 Wp   =          124
52557
 YDOT =      -7118
454962  meter/sec      RA   =          115
13110  deg
 ZDOT =        505
362674                 TA   =          320
65797
                                          MA   =          320
73001
                                          Ha   =            196
092  n
mi
                                          Hp   =            185
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13056203
97                 X    =        -3990941
92
 Y    =       -4079453
66  feet           Y    =        -1287983
55  meter
 Z    =       17296800
70                 Z    =         5252704
31
 XDOT =       9520
552582                 XDOT =        2978
793516
 YDOT =     -23354
511030  feet/sec       YDOT =       -7085
574583  meter/sec
 ZDOT =       1658
014021                 ZDOT =         519
645690

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3241928
07                 X    =          988139
67
 Y    =      -13386503
88  feet           Y    =        -4080206
38  meter
 Z    =       17221415
01                 Z    =         5249087
30
 XDOT =      22931
375280                 XDOT =        6989
483185
 YDOT =       7783
466938  feet/sec       YDOT =        2372
400723  meter/sec
 ZDOT =       1713
056000                 ZDOT =         522
139469


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   08360
54858740  
00010596  00000-0  82463-4 0  9064
2 25544  51
6416 115
7443 0007238 129
0487 231
1320 15
71757423 18644


Satellite: ISS
Catalog Number: 25544
Epoch time:      08360
54858740   =   yrday
fracday
Element set:     906
Inclination:       51
6416  deg
RA of node:       115
7443  deg
Eccentricity:     
0007238     
Arg of perigee:   129
0487  deg
Mean anomaly:     231
1320  deg
Mean motion:   15
71757423  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1864
Checksum:              308


Coasting Arc #8 (Orbit 1878)
---------------------------------------

Vector Time (GMT): 2008/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1379466
38                 A    =         6738031
38  meter
 Y    =        6488385
44  meter          E    =           
0011396
 Z    =       -1182791
49                 I    =           51
97007
 XDOT =      -4925
144568                 Wp   =           77
18969
 YDOT =         20
696842  meter/sec      RA   =          110
01927  deg
 ZDOT =       5907
567977                 TA   =          269
93360
                                          MA   =          270
06419
                                          Ha   =            195
977  n
mi
                                          Hp   =            185
139

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4525808
33                 X    =        -1446172
26
 Y    =       21287353
82  feet           Y    =         6472586
68  meter
 Z    =       -3880549
50                 Z    =        -1189653
88
 XDOT =     -16158
610786                 XDOT =       -4953
707822
 YDOT =         67
903026  feet/sec       YDOT =         -34
539660  meter/sec
 ZDOT =      19381
784701                 ZDOT =        5883
572265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21579879
55                 X    =        -6577547
29
 Y    =       -2781880
10  feet           Y    =         -847917
05  meter
 Z    =       -3906786
35                 Z    =        -1190788
48
 XDOT =      -1575
440034                 XDOT =        -480
194122
 YDOT =     -14638
419860  feet/sec       YDOT =       -4461
790373  meter/sec
 ZDOT =      19288
451468                 ZDOT =        5879
120007


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   08361
50230651  
00010596  00000-0  82463-4 0  9077
2 25544  51
6423 110
8638 0007249 131
4040 228
7746 15
71726177 18790


Satellite: ISS
Catalog Number: 25544
Epoch time:      08361
50230651   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:       110
8638  deg
Eccentricity:     
0007249     
Arg of perigee:   131
4040  deg
Mean anomaly:     228
7746  deg
Mean motion:   15
71726177  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1879
Checksum:              307


Coasting Arc #9 (Orbit 1894)
---------------------------------------

Vector Time (GMT): 2008/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4368013
65                 A    =         6728060
93  meter
 Y    =       -1284662
16  meter          E    =           
0017278
 Z    =       -4967590
45                 I    =           51
94586
 XDOT =       -244
049110                 Wp   =           95
91603
 YDOT =       7379
733867  meter/sec      RA   =          104
95191  deg
 ZDOT =      -2131
103138                 TA   =          153
50868
                                          MA   =          153
42027
                                          Ha   =            195
908  n
mi
                                          Hp   =            185
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14330753
46                 X    =         4406185
84
 Y    =       -4214770
88  feet           Y    =        -1235602
26  meter
 Z    =      -16297868
92                 Z    =        -4946278
23
 XDOT =       -800
686058                 XDOT =        -316
199908
 YDOT =      24211
725287  feet/sec       YDOT =        7376
601703  meter/sec
 ZDOT =      -6991
808194                 ZDOT =       -2132
462765

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5598776
61                 X    =         1706507
11
 Y    =       13945648
23  feet           Y    =         4250633
58  meter
 Z    =      -16215052
13                 Z    =        -4942347
89
 XDOT =     -23153
780307                 XDOT =       -7057
272238
 YDOT =       1191
275441  feet/sec       YDOT =         363
100754  meter/sec
 ZDOT =      -6996
585569                 ZDOT =       -2132
559281


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   08362
51959734  
00010596  00000-0  82463-4 0  9080
2 25544  51
6427 105
6575 0007197 136
0768 224
0967 15
71737077 18959


Satellite: ISS
Catalog Number: 25544
Epoch time:      08362
51959734   =   yrday
fracday
Element set:     908
Inclination:       51
6427  deg
RA of node:       105
6575  deg
Eccentricity:     
0007197     
Arg of perigee:   136
0768  deg
Mean anomaly:     224
0967  deg
Mean motion:   15
71737077  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1895
Checksum:              349


Coasting Arc #10 (Orbit 1910)
---------------------------------------

Vector Time (GMT): 2008/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -936768
99                 A    =         6735846
28  meter
 Y    =       -6162099
70  meter          E    =           
0020280
 Z    =        2524455
47                 I    =           51
97848
 XDOT =       4736
370748                 Wp   =          115
99644
 YDOT =      -2914
786677  meter/sec      RA   =           99
81842  deg
 ZDOT =      -5333
162756                 TA   =           35
54466
                                          MA   =           35
40972
                                          Ha   =            195
909  n
mi
                                          Hp   =            185
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3073389
08                 X    =         -880057
00
 Y    =      -20216862
55  feet           Y    =        -6172258
50  meter
 Z    =        8282334
22                 Z    =         2520041
48
 XDOT =      15539
274106                 XDOT =        4794
519658
 YDOT =      -9562
948414  feet/sec       YDOT =       -2861
495879  meter/sec
 ZDOT =     -17497
253137                 ZDOT =       -5310
012881

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19726837
88                 X    =         6012740
19
 Y    =       -5413897
00  feet           Y    =        -1650155
81  meter
 Z    =        8264738
24                 Z    =         2519092
22
 XDOT =      10895
182683                 XDOT =        3320
851682
 YDOT =      13004
218994  feet/sec       YDOT =        3963
685950  meter/sec
 ZDOT =     -17407
389827                 ZDOT =       -5305
772419


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   08363
53688020  
00010596  00000-0  82463-4 0  9091
2 25544  51
6426 100
4516 0007328 138
7563 221
4153 15
71746732 19119


Satellite: ISS
Catalog Number: 25544
Epoch time:      08363
53688020   =   yrday
fracday
Element set:     909
Inclination:       51
6426  deg
RA of node:       100
4516  deg
Eccentricity:     
0007328     
Arg of perigee:   138
7563  deg
Mean anomaly:     221
4153  deg
Mean motion:   15
71746732  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1911
Checksum:              300


Coasting Arc #11 (Orbit 1926)
---------------------------------------

Vector Time (GMT): 2008/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3650022
32                 A    =         6730652
90  meter
 Y    =        3717568
36  meter          E    =           
0016421
 Z    =        4254793
43                 I    =           51
96584
 XDOT =      -2296
749306                 Wp   =          121
62509
 YDOT =      -6404
033182  meter/sec      RA   =           94
76924  deg
 ZDOT =       3606
596539                 TA   =          291
79991
                                          MA   =          291
97453
                                          Ha   =            195
753  n
mi
                                          Hp   =            185
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11975138
84                 X    =        -3711990
27
 Y    =       12196746
59  feet           Y    =         3676404
61  meter
 Z    =       13959296
04                 Z    =         4236911
84
 XDOT =      -7535
266753                 XDOT =       -2242
487643
 YDOT =     -21010
607553  feet/sec       YDOT =       -6429
413880  meter/sec
 ZDOT =      11832
665809                 ZDOT =        3595
569954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13676264
20                 X    =        -4168525
33
 Y    =      -10346732
62  feet           Y    =        -3153684
10  meter
 Z    =       13889976
43                 Z    =         4233664
81
 XDOT =      19073
694835                 XDOT =        5813
662186
 YDOT =      -9302
833027  feet/sec       YDOT =       -2835
503507  meter/sec
 ZDOT =      11789
325866                 ZDOT =        3593
386524


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   08364
55415182  
00010596  00000-0  82463-4 0  9103
2 25544  51
6431  95
2447 0007195 142
5714 217
5951 15
71804392 19278


Satellite: ISS
Catalog Number: 25544
Epoch time:      08364
55415182   =   yrday
fracday
Element set:     910
Inclination:       51
6431  deg
RA of node:        95
2447  deg
Eccentricity:     
0007195     
Arg of perigee:   142
5714  deg
Mean anomaly:     217
5951  deg
Mean motion:   15
71804392  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1927
Checksum:              311


Coasting Arc #12 (Orbit 1941)
---------------------------------------

Vector Time (GMT): 2008/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2930081
09                 A    =         6732554
44  meter
 Y    =        4807446
68  meter          E    =           
0011925
 Z    =       -3706340
77                 I    =           51
97318
 XDOT =      -3355
579862                 Wp   =          125
93810
 YDOT =       5385
761276  meter/sec      RA   =           89
62443  deg
 ZDOT =       4335
855371                 TA   =          189
79169
                                          MA   =          189
81495
                                          Ha   =            195
603  n
mi
                                          Hp   =            185
499

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9613126
93                 X    =         2894110
16
 Y    =       15772462
85  feet           Y    =         4840011
87  meter
 Z    =      -12159910
68                 Z    =        -3692193
41
 XDOT =     -11009
120281                 XDOT =       -3436
617459
 YDOT =      17669
820458  feet/sec       YDOT =        5347
783604  meter/sec
 ZDOT =      14225
247280                 ZDOT =        4319
357995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14159133
73                 X    =        -4315703
96
 Y    =       11918279
57  feet           Y    =         3632691
61  meter
 Z    =      -12104534
91                 Z    =        -3689462
24
 XDOT =     -18252
233447                 XDOT =       -5563
280755
 YDOT =      -7310
754401  feet/sec       YDOT =       -2228
317941  meter/sec
 ZDOT =      14161
421398                 ZDOT =        4316
401242


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   08365
50783866  
00010596  00000-0  82463-4 0  9117
2 25544  51
6429  90
3645 0007101 145
6591 214
5031 15
71799401 19422


Satellite: ISS
Catalog Number: 25544
Epoch time:      08365
50783866   =   yrday
fracday
Element set:     911
Inclination:       51
6429  deg
RA of node:        90
3645  deg
Eccentricity:     
0007101     
Arg of perigee:   145
6591  deg
Mean anomaly:     214
5031  deg
Mean motion:   15
71799401  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1942
Checksum:              309

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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