Date: May 23rd 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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 2399)
---------------------------------------

Vector Time (GMT): 2008/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5172740
88                 A    =         6722772
56  meter
 Y    =        3547472
72  meter          E    =           
0000405
 Z    =       -2418907
57                 I    =           51
74261
 XDOT =      -4599
696491                 Wp   =          291
29757
 YDOT =      -3042
073142  meter/sec      RA   =          163
26175  deg
 ZDOT =       5374
318090                 TA   =           41
42950
                                          MA   =           41
42643
                                          Ha   =            185
714  n
mi
                                          Hp   =            181
653

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16970934
64                 X    =        -5200273
97
 Y    =       11638690
02  feet           Y    =         3489474
53  meter
 Z    =       -7936048
44                 Z    =        -2444103
68
 XDOT =     -15090
867754                 XDOT =       -4591
445677
 YDOT =      -9980
554928  feet/sec       YDOT =       -3093
464131  meter/sec
 ZDOT =      17632
277197                 ZDOT =        5351
991967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         463555
47                 X    =          141291
71
 Y    =       20535734
28  feet           Y    =         6259291
81  meter
 Z    =       -8032516
83                 Z    =        -2448311
13
 XDOT =     -15174
480607                 XDOT =       -4625
181689
 YDOT =       7206
412090  feet/sec       YDOT =        2196
514405  meter/sec
 ZDOT =      17546
158192                 ZDOT =        5348
069017


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   08140
50488158  
00020000  00000-0  20000-3 0  9001
2 25544  51
6380 164
2528 0005628 231
6193 128
4466 15
76387894 24004


Satellite: ISS
Catalog Number: 25544
Epoch time:      08140
50488158   =   yrday
fracday
Element set:     900
Inclination:       51
6380  deg
RA of node:       164
2528  deg
Eccentricity:     
0005628     
Arg of perigee:   231
6193  deg
Mean anomaly:     128
4466  deg
Mean motion:   15
76387894  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2400
Checksum:              297


Coasting Arc #2 (Orbit 2415)
---------------------------------------

Vector Time (GMT): 2008/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3446706
34                 A    =         6714630
30  meter
 Y    =        2869495
48  meter          E    =           
0007923
 Z    =       -5004062
91                 I    =           51
74178
 XDOT =      -6213
377095                 Wp   =           88
97136
 YDOT =       4121
344571  meter/sec      RA   =          158
15250  deg
 ZDOT =      -1918
804252                 TA   =          162
53660
                                          MA   =          162
50933
                                          Ha   =            185
583  n
mi
                                          Hp   =            181
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11308091
66                 X    =         3438672
29
 Y    =        9414355
24  feet           Y    =         2907994
32  meter
 Z    =      -16417529
22                 Z    =        -4987337
60
 XDOT =     -20385
095456                 XDOT =       -6249
679450
 YDOT =      13521
471689  feet/sec       YDOT =        4051
660337  meter/sec
 ZDOT =      -6295
289541                 ZDOT =       -1949
076972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14044661
10                 X    =         4280812
70
 Y    =       -4622425
94  feet           Y    =        -1408915
43  meter
 Z    =      -16352949
59                 Z    =        -4984379
03
 XDOT =        246
186690                 XDOT =          75
037703
 YDOT =      23400
608235  feet/sec       YDOT =        7132
505390  meter/sec
 ZDOT =      -6411
227483                 ZDOT =       -1954
142137


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   08141
51919112  
00020000  00000-0  20000-3 0  9013
2 25544  51
6374 159
0251 0005656 236
9262 123
1360 15
76364477 24162


Satellite: ISS
Catalog Number: 25544
Epoch time:      08141
51919112   =   yrday
fracday
Element set:     901
Inclination:       51
6374  deg
RA of node:       159
0251  deg
Eccentricity:     
0005656     
Arg of perigee:   236
9262  deg
Mean anomaly:     123
1360  deg
Mean motion:   15
76364477  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2416
Checksum:              277


Coasting Arc #3 (Orbit 2431)
---------------------------------------

Vector Time (GMT): 2008/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5580612
54                 A    =         6725024
41  meter
 Y    =       -3631381
11  meter          E    =           
0012332
 Z    =         889763
81                 I    =           51
80269
 XDOT =       3294
233220                 Wp   =          149
31840
 YDOT =       3593
375225  meter/sec      RA   =          152
98328  deg
 ZDOT =      -5970
227294                 TA   =           20
97824
                                          MA   =           20
92769
                                          Ha   =            185
335  n
mi
                                          Hp   =            181
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18309096
24                 X    =         5616482
07
 Y    =      -11913980
02  feet           Y    =        -3568775
09  meter
 Z    =        2919172
61                 Z    =          916961
39
 XDOT =      10807
851773                 XDOT =        3282
809415
 YDOT =      11789
288797  feet/sec       YDOT =        3630
150300  meter/sec
 ZDOT =     -19587
359887                 ZDOT =       -5954
250843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -696030
87                 X    =         -212150
21
 Y    =      -21818852
96  feet           Y    =        -6650386
38  meter
 Z    =        3023357
50                 Z    =          921519
37
 XDOT =      14152
226525                 XDOT =        4313
598645
 YDOT =      -3168
313250  feet/sec       YDOT =        -965
701879  meter/sec
 ZDOT =     -19525
581013                 ZDOT =       -5951
397093


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   08142
53348893  
00020000  00000-0  20000-3 0  9029
2 25544  51
6362 153
7971 0005511 240
9279 119
1334 15
76388414 24323


Satellite: ISS
Catalog Number: 25544
Epoch time:      08142
53348893   =   yrday
fracday
Element set:     902
Inclination:       51
6362  deg
RA of node:       153
7971  deg
Eccentricity:     
0005511     
Arg of perigee:   240
9279  deg
Mean anomaly:     119
1334  deg
Mean motion:   15
76388414  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2432
Checksum:              294


Coasting Arc #4 (Orbit 2447)
---------------------------------------

Vector Time (GMT): 2008/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2301521
61                 A    =         6713257
31  meter
 Y    =       -3458884
86  meter          E    =           
0003707
 Z    =        5275565
83                 I    =           51
78821
 XDOT =       6481
193808                 Wp   =          226
63401
 YDOT =      -4162
645682  meter/sec      RA   =          147
84994  deg
 ZDOT =         95
828403                 TA   =          222
44450
                                          MA   =          222
47317
                                          Ha   =            185
189  n
mi
                                          Hp   =            181
982

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7550923
93                 X    =        -2288300
79
 Y    =      -11348047
43  feet           Y    =        -3484548
75  meter
 Z    =       17308286
84                 Z    =         5264416
45
 XDOT =      21263
759213                 XDOT =        6526
793945
 YDOT =     -13656
974022  feet/sec       YDOT =       -4089
914319  meter/sec
 ZDOT =        314
397649                 ZDOT =         127
424473

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13656530
00                 X    =        -4162510
34
 Y    =         887576
96  feet           Y    =          270533
46  meter
 Z    =       17265075
19                 Z    =         5262394
92
 XDOT =      -1015
417243                 XDOT =        -309
499176
 YDOT =     -24250
989822  feet/sec       YDOT =       -7391
701698  meter/sec
 ZDOT =        435
456503                 ZDOT =         132
727142


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   08143
54777419  
00020000  00000-0  20000-3 0  9032
2 25544  51
6357 148
5688 0005554 245
8770 114
1813 15
76406053 24485


Satellite: ISS
Catalog Number: 25544
Epoch time:      08143
54777419   =   yrday
fracday
Element set:     903
Inclination:       51
6357  deg
RA of node:       148
5688  deg
Eccentricity:     
0005554     
Arg of perigee:   245
8770  deg
Mean anomaly:     114
1813  deg
Mean motion:   15
76406053  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2448
Checksum:              309


Coasting Arc #5 (Orbit 2463)
---------------------------------------

Vector Time (GMT): 2008/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5644174
59                 A    =         6724942
16  meter
 Y    =        3573369
50  meter          E    =           
0008142
 Z    =         733314
37                 I    =           51
85270
 XDOT =      -2001
388201                 Wp   =           41
45363
 YDOT =      -4398
950880  meter/sec      RA   =          142
71561  deg
 ZDOT =       5999
686432                 TA   =          326
52201
                                          MA   =          326
57344
                                          Ha   =            184
880  n
mi
                                          Hp   =            182
003

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18517633
17                 X    =        -5687275
41
 Y    =       11723653
23  feet           Y    =         3510012
01  meter
 Z    =        2405887
06                 Z    =          705790
67
 XDOT =      -6566
234255                 XDOT =       -1981
195295
 YDOT =     -14432
253542  feet/sec       YDOT =       -4421
219642  meter/sec
 ZDOT =      19684
010604                 ZDOT =        5990
011932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1163333
15                 X    =          354583
94
 Y    =       21897256
54  feet           Y    =         6674283
79  meter
 Z    =        2300410
29                 Z    =          701165
06
 XDOT =     -14257
728114                 XDOT =       -4345
755529
 YDOT =      -1317
897698  feet/sec       YDOT =        -401
695218  meter/sec
 ZDOT =      19646
373339                 ZDOT =        5988
214594


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   08144
56204570  
00020000  00000-0  20000-3 0  9049
2 25544  51
6361 143
3417 0005661 248
8779 111
1780 15
76472979 24642


Satellite: ISS
Catalog Number: 25544
Epoch time:      08144
56204570   =   yrday
fracday
Element set:     904
Inclination:       51
6361  deg
RA of node:       143
3417  deg
Eccentricity:     
0005661     
Arg of perigee:   248
8779  deg
Mean anomaly:     111
1780  deg
Mean motion:   15
76472979  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2464
Checksum:              303


Coasting Arc #6 (Orbit 2478)
---------------------------------------

Vector Time (GMT): 2008/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1228764
09                 A    =         6714208
74  meter
 Y    =        4256887
80  meter          E    =           
0008964
 Z    =       -5052551
38                 I    =           51
83825
 XDOT =      -6371
055856                 Wp   =          120
46144
 YDOT =       3942
173109  meter/sec      RA   =          137
55413  deg
 ZDOT =       1769
812785                 TA   =          166
55162
                                          MA   =          166
52772
                                          Ha   =            184
702  n
mi
                                          Hp   =            182
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4031378
23                 X    =         1205616
05
 Y    =       13966167
31  feet           Y    =         4270499
91  meter
 Z    =      -16576612
14                 Z    =        -5046637
57
 XDOT =     -20902
414226                 XDOT =       -6423
261807
 YDOT =      12933
638810  feet/sec       YDOT =        3870
636140  meter/sec
 ZDOT =       5806
472391                 ZDOT =        1738
735881

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14253145
36                 X    =         4344358
70
 Y    =        2986820
84  feet           Y    =          910382
99  meter
 Z    =      -16553448
54                 Z    =        -5045491
12
 XDOT =       1683
583655                 XDOT =         513
156298
 YDOT =      23525
060509  feet/sec       YDOT =        7170
438443  meter/sec
 ZDOT =       5687
353790                 ZDOT =        1733
505435


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   08145
51291792  
00020000  00000-0  20000-3 0  9058
2 25544  51
6357 138
4401 0005590 254
9661 105
0885 15
76419532 24794


Satellite: ISS
Catalog Number: 25544
Epoch time:      08145
51291792   =   yrday
fracday
Element set:     905
Inclination:       51
6357  deg
RA of node:       138
4401  deg
Eccentricity:     
0005590     
Arg of perigee:   254
9661  deg
Mean anomaly:     105
0885  deg
Mean motion:   15
76419532  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2479
Checksum:              304


Coasting Arc #7 (Orbit 2494)
---------------------------------------

Vector Time (GMT): 2008/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5418670
37                 A    =         6722893
84  meter
 Y    =       -3222886
04  meter          E    =           
0005394
 Z    =       -2323911
31                 I    =           51
88846
 XDOT =        866
331595                 Wp   =          194
51599
 YDOT =       5380
983829  meter/sec      RA   =          132
45043  deg
 ZDOT =      -5444
925759                 TA   =           11
56011
                                          MA   =           11
54773
                                          Ha   =            184
586  n
mi
                                          Hp   =            182
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17777789
93                 X    =         5465595
62
 Y    =      -10573773
10  feet           Y    =        -3162028
66  meter
 Z    =       -7624380
95                 Z    =        -2297473
84
 XDOT =       2842
295260                 XDOT =         832
546710
 YDOT =      17654
146421  feet/sec       YDOT =        5390
483526  meter/sec
 ZDOT =     -17863
929656                 ZDOT =       -5440
798402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1219913
72                 X    =         -371829
70
 Y    =      -20685783
70  feet           Y    =        -6305026
87  meter
 Z    =       -7523020
69                 Z    =        -2293016
71
 XDOT =      15528
837683                 XDOT =        4733
189726
 YDOT =       5572
100172  feet/sec       YDOT =        1698
376133  meter/sec
 ZDOT =     -17847
524413                 ZDOT =       -5439
925441


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   08146
52716796  
00020000  00000-0  20000-3 0  9067
2 25544  51
6356 133
2117 0005506 259
3150 100
7395 15
76459468 24957


Satellite: ISS
Catalog Number: 25544
Epoch time:      08146
52716796   =   yrday
fracday
Element set:     906
Inclination:       51
6356  deg
RA of node:       133
2117  deg
Eccentricity:     
0005506     
Arg of perigee:   259
3150  deg
Mean anomaly:     100
7395  deg
Mean motion:   15
76459468  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2495
Checksum:              306


Coasting Arc #8 (Orbit 2510)
---------------------------------------

Vector Time (GMT): 2008/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -352656
52                 A    =         6716978
69  meter
 Y    =       -5131176
41  meter          E    =           
0004349
 Z    =        4318757
76                 I    =           51
88752
 XDOT =       5993
475380                 Wp   =           54
19256
 YDOT =      -3354
249096  meter/sec      RA   =          127
26884  deg
 ZDOT =      -3490
895531                 TA   =           70
99197
                                          MA   =           70
94485
                                          Ha   =            184
324  n
mi
                                          Hp   =            182
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1157009
57                 X    =         -316232
46
 Y    =      -16834568
28  feet           Y    =        -5134916
91  meter
 Z    =       14169152
75                 Z    =         4317132
37
 XDOT =      19663
633136                 XDOT =        6047
495832
 YDOT =     -11004
754252  feet/sec       YDOT =       -3286
924139  meter/sec
 ZDOT =     -11453
069328                 ZDOT =       -3461
648394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15637892
77                 X    =        -4766429
72
 Y    =       -6355243
25  feet           Y    =        -1937078
14  meter
 Z    =       14162395
37                 Z    =         4316698
11
 XDOT =      -1579
444206                 XDOT =        -481
414594
 YDOT =     -21422
341104  feet/sec       YDOT =       -6529
529568  meter/sec
 ZDOT =     -11340
905075                 ZDOT =       -3456
707867


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   08147
54140475  
00020000  00000-0  20000-3 0  9076
2 25544  51
6354 127
9837 0005665 264
3884  95
6634 15
76487582 25115


Satellite: ISS
Catalog Number: 25544
Epoch time:      08147
54140475   =   yrday
fracday
Element set:     907
Inclination:       51
6354  deg
RA of node:       127
9837  deg
Eccentricity:     
0005665     
Arg of perigee:   264
3884  deg
Mean anomaly:      95
6634  deg
Mean motion:   15
76487582  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2511
Checksum:              323


Coasting Arc #9 (Orbit 2526)
---------------------------------------

Vector Time (GMT): 2008/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5009726
61                 A    =         6719116
25  meter
 Y    =        2527240
78  meter          E    =           
0006249
 Z    =        3692283
54                 I    =           51
91212
 XDOT =         -9
665253                 Wp   =          103
09214
 YDOT =      -6367
541730  meter/sec      RA   =          122
18368  deg
 ZDOT =       4337
759477                 TA   =          301
20774
                                          MA   =          301
26897
                                          Ha   =            184
220  n
mi
                                          Hp   =            181
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16436110
93                 X    =        -5055550
78
 Y    =        8291472
36  feet           Y    =         2470962
52  meter
 Z    =       12113791
14                 Z    =         3667835
19
 XDOT =        -31
710146                 XDOT =          40
466211
 YDOT =     -20890
884941  feet/sec       YDOT =       -6367
369992  meter/sec
 ZDOT =      14231
494347                 ZDOT =        4337
833590

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         431159
44                 X    =          131417
40
 Y    =       18465427
08  feet           Y    =         5628262
17  meter
 Z    =       12019995
70                 Z    =         3663694
69
 XDOT =     -17583
151888                 XDOT =       -5359
344696
 YDOT =      -8869
273299  feet/sec       YDOT =       -2703
354502  meter/sec
 ZDOT =      14231
153814                 ZDOT =        4337
655683


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   08148
55562834  
00020000  00000-0  20000-3 0  9086
2 25544  51
6358 122
7559 0005755 267
2490  92
8016 15
76537215 25277


Satellite: ISS
Catalog Number: 25544
Epoch time:      08148
55562834   =   yrday
fracday
Element set:     908
Inclination:       51
6358  deg
RA of node:       122
7559  deg
Eccentricity:     
0005755     
Arg of perigee:   267
2490  deg
Mean anomaly:      92
8016  deg
Mean motion:   15
76537215  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2527
Checksum:              315


Coasting Arc #10 (Orbit 2541)
---------------------------------------

Vector Time (GMT): 2008/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -261954
20                 A    =         6720752
07  meter
 Y    =        5934279
98  meter          E    =           
0001658
 Z    =       -3141548
48                 I    =           51
93180
 XDOT =      -5481
240770                 Wp   =          317
13193
 YDOT =       2341
060652  meter/sec      RA   =          116
99757  deg
 ZDOT =       4878
925608                 TA   =            6
43806
                                          MA   =            6
43593
                                          Ha   =            184
248  n
mi
                                          Hp   =            181
966

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -859429
79                 X    =         -313031
62
 Y    =       19469422
52  feet           Y    =         5931065
38  meter
 Z    =      -10306917
58                 Z    =        -3142944
54
 XDOT =     -17983
073394                 XDOT =       -5530
712578
 YDOT =       7680
645185  feet/sec       YDOT =        2279
489190  meter/sec
 ZDOT =      16006
973779                 ZDOT =        4852
177641

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17407259
63                 X    =         5305732
73
 Y    =        8757029
93  feet           Y    =         2669142
72  meter
 Z    =      -10311708
00                 Z    =        -3143008
60
 XDOT =        183
854820                 XDOT =          56
038949
 YDOT =      18363
591591  feet/sec       YDOT =        5597
222717  meter/sec
 ZDOT =      15904
307394                 ZDOT =        4847
632894


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   08149
50645368  
00020000  00000-0  20000-3 0  9097
2 25544  51
6356 117
8541 0005591 272
8227  87
2298 15
76502821 25421


Satellite: ISS
Catalog Number: 25544
Epoch time:      08149
50645368   =   yrday
fracday
Element set:     909
Inclination:       51
6356  deg
RA of node:       117
8541  deg
Eccentricity:     
0005591     
Arg of perigee:   272
8227  deg
Mean anomaly:      87
2298  deg
Mean motion:   15
76502821  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2542
Checksum:              310


Coasting Arc #11 (Orbit 2557)
---------------------------------------

Vector Time (GMT): 2008/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4564549
89                 A    =         6715403
40  meter
 Y    =       -1462602
76  meter          E    =           
0006482
 Z    =       -4709456
26                 I    =           51
92665
 XDOT =       -552
435184                 Wp   =           48
57678
 YDOT =       7166
732523  meter/sec      RA   =          111
90886  deg
 ZDOT =      -2759
425560                 TA   =          194
33224
                                          MA   =          194
35063
                                          Ha   =            184
232  n
mi
                                          Hp   =            182
045

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14975557
38                 X    =         4603443
62
 Y    =       -4798565
48  feet           Y    =        -1411341
44  meter
 Z    =      -15450971
99                 Z    =        -4687187
11
 XDOT =      -1812
451391                 XDOT =        -619
128727
 YDOT =      23512
901978  feet/sec       YDOT =        7160
182231  meter/sec
 ZDOT =      -9053
233464                 ZDOT =       -2762
270650

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1568719
54                 X    =          478145
72
 Y    =      -15731126
05  feet           Y    =        -4794847
22  meter
 Z    =      -15365444
26                 Z    =        -4683387
41
 XDOT =      19739
321590                 XDOT =        6016
545221
 YDOT =      10826
900262  feet/sec       YDOT =        3300
039200  meter/sec
 ZDOT =      -9063
484138                 ZDOT =       -2762
549965


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   08150
52065342  
00020000  00000-0  20000-3 0  9101
2 25544  51
6361 112
6253 0005652 276
7710  83
2811 15
76538327 25582


Satellite: ISS
Catalog Number: 25544
Epoch time:      08150
52065342   =   yrday
fracday
Element set:     910
Inclination:       51
6361  deg
RA of node:       112
6253  deg
Eccentricity:     
0005652     
Arg of perigee:   276
7710  deg
Mean anomaly:      83
2811  deg
Mean motion:   15
76538327  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2558
Checksum:              275


Coasting Arc #12 (Orbit 2573)
---------------------------------------

Vector Time (GMT): 2008/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         641683
61                 A    =         6723777
25  meter
 Y    =       -6492822
25  meter          E    =           
0008749
 Z    =        1605022
61                 I    =           51
96512
 XDOT =       5005
485809                 Wp   =          127
07326
 YDOT =       -938
633523  meter/sec      RA   =          106
73931  deg
 ZDOT =      -5781
964000                 TA   =           35
27165
                                          MA   =           35
21379
                                          Ha   =            184
321  n
mi
                                          Hp   =            181
925

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2105261
19                 X    =          706442
65
 Y    =      -21301910
28  feet           Y    =        -6485284
65  meter
 Z    =        5265822
22                 Z    =         1608296
62
 XDOT =      16422
197536                 XDOT =        5043
697900
 YDOT =      -3079
506309  feet/sec       YDOT =        -882
445087  meter/sec
 ZDOT =     -18969
698162                 ZDOT =       -5757
554249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18907418
46                 X    =        -5762981
15
 Y    =      -10029295
80  feet           Y    =        -3056929
36  meter
 Z    =        5277797
19                 Z    =         1608672
58
 XDOT =       2714
521987                 XDOT =         827
386302
 YDOT =     -15078
725099  feet/sec       YDOT =       -4595
995410  meter/sec
 ZDOT =     -18875
880120                 ZDOT =       -5753
368260


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   08151
53484002  
00020000  00000-0  20000-3 0  9112
2 25544  51
6363 107
3969 0005712 281
2940  78
7583 15
76559814 25749


Satellite: ISS
Catalog Number: 25544
Epoch time:      08151
53484002   =   yrday
fracday
Element set:     911
Inclination:       51
6363  deg
RA of node:       107
3969  deg
Eccentricity:     
0005712     
Arg of perigee:   281
2940  deg
Mean anomaly:      78
7583  deg
Mean motion:   15
76559814  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2574
Checksum:              303

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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