Date: September 6th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5651 05 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2345)
---------------------------------------

Vector Time (GMT): 2007/248/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5194499
17                 A    =         6717507
77  meter
 Y    =         956910
01  meter          E    =           
0005766
 Z    =       -4149619
82                 I    =           51
87131
 XDOT =       1799
165716                 Wp   =           30
47351
 YDOT =       6482
028042  meter/sec      RA   =           48
50954  deg
 ZDOT =       3754
089474                 TA   =          277
77299
                                          MA   =          277
83845
                                          Ha   =            187
104  n
mi
                                          Hp   =            180
737

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17042320
10                 X    =         5203570
77
 Y    =        3139468
54  feet           Y    =         1015048
72  meter
 Z    =      -13614238
26                 Z    =        -4124363
03
 XDOT =       5902
774659                 XDOT =        1708
312422
 YDOT =      21266
496201  feet/sec       YDOT =        6501
639186  meter/sec
 ZDOT =      12316
566515                 ZDOT =        3762
609354

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17365137
33                 X    =        -5292893
86
 Y    =       -1163305
60  feet           Y    =         -354575
55  meter
 Z    =      -13518252
32                 Z    =        -4120363
31
 XDOT =      -8309
675208                 XDOT =       -2532
789003
 YDOT =     -19194
460336  feet/sec       YDOT =       -5850
471510  meter/sec
 ZDOT =      12349
664032                 ZDOT =        3764
177597


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   07248
57300578  
00020000  00000-0  20000-3 0  9005
2 25544  51
6353  49
0584 0008755 329
9888  30
0774 15
76553076 23468


Satellite: ISS
Catalog Number: 25544
Epoch time:      07248
57300578   =   yrday
fracday
Element set:     900
Inclination:       51
6353  deg
RA of node:        49
0584  deg
Eccentricity:     
0008755     
Arg of perigee:   329
9888  deg
Mean anomaly:      30
0774  deg
Mean motion:   15
76553076  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2346
Checksum:              315


Coasting Arc #2 (Orbit 2361)
---------------------------------------

Vector Time (GMT): 2007/249/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1166858
80                 A    =         6718119
52  meter
 Y    =       -5339396
03  meter          E    =           
0010235
 Z    =       -3916564
11                 I    =           51
85387
 XDOT =       6336
325568                 Wp   =           14
30087
 YDOT =       1601
797607  meter/sec      RA   =           43
42108  deg
 ZDOT =      -4064
016658                 TA   =          213
48734
                                          MA   =          213
55209
                                          Ha   =            187
109  n
mi
                                          Hp   =            180
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3828276
89                 X    =        -1088040
40
 Y    =      -17517703
50  feet           Y    =        -5352003
69  meter
 Z    =      -12849619
79                 Z    =        -3922041
35
 XDOT =      20788
469712                 XDOT =        6337
685143
 YDOT =       5255
241494  feet/sec       YDOT =        1672
661693  meter/sec
 ZDOT =     -13333
387984                 ZDOT =       -4033
231776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6023828
99                 X    =         1836063
08
 Y    =       16872709
44  feet           Y    =         5142801
84  meter
 Z    =      -12871034
49                 Z    =        -3923091
31
 XDOT =     -20142
128220                 XDOT =       -6139
320681
 YDOT =      -2909
431960  feet/sec       YDOT =        -886
794861  meter/sec
 ZDOT =     -13216
336395                 ZDOT =       -4028
339333


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   07249
58717619  
00020000  00000-0  20000-3 0  9016
2 25544  51
6354  43
8294 0008816 333
8264  26
2453 15
76588956 23623


Satellite: ISS
Catalog Number: 25544
Epoch time:      07249
58717619   =   yrday
fracday
Element set:     901
Inclination:       51
6354  deg
RA of node:        43
8294  deg
Eccentricity:     
0008816     
Arg of perigee:   333
8264  deg
Mean anomaly:      26
2453  deg
Mean motion:   15
76588956  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2362
Checksum:              321


Coasting Arc #3 (Orbit 2377)
---------------------------------------

Vector Time (GMT): 2007/250/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5833992
16                 A    =         6721334
95  meter
 Y    =       -1759516
08  meter          E    =           
0011609
 Z    =        2835768
86                 I    =           51
84302
 XDOT =       -769
187048                 Wp   =           59
33872
 YDOT =      -5713
382766  meter/sec      RA   =           38
23053  deg
 ZDOT =      -5106
256847                 TA   =           88
21038
                                          MA   =           88
07742
                                          Ha   =            187
246  n
mi
                                          Hp   =            180
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19140394
22                 X    =        -5827658
85
 Y    =       -5772690
55  feet           Y    =        -1824719
68  meter
 Z    =        9303703
61                 Z    =         2807443
09
 XDOT =      -2523
579555                 XDOT =        -680
437055
 YDOT =     -18744
694113  feet/sec       YDOT =       -5721
487990  meter/sec
 ZDOT =     -16752
811179                 ZDOT =       -5109
777972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19836390
50                 X    =         6046131
82
 Y    =        2861711
88  feet           Y    =          872249
78  meter
 Z    =        9195964
60                 Z    =         2802930
01
 XDOT =       5391
932513                 XDOT =        1643
461030
 YDOT =      16730
291548  feet/sec       YDOT =        5099
392864  meter/sec
 ZDOT =     -16766
845379                 ZDOT =       -5110
534472


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   07250
60132756  
00020000  00000-0  20000-3 0  9025
2 25544  51
6357  38
6002 0008807 337
8983  22
1801 15
76611725 23787


Satellite: ISS
Catalog Number: 25544
Epoch time:      07250
60132756   =   yrday
fracday
Element set:     902
Inclination:       51
6357  deg
RA of node:        38
6002  deg
Eccentricity:     
0008807     
Arg of perigee:   337
8983  deg
Mean anomaly:      22
1801  deg
Mean motion:   15
76611725  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2378
Checksum:              284


Coasting Arc #4 (Orbit 2393)
---------------------------------------

Vector Time (GMT): 2007/251/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          85692
88                 A    =         6714204
41  meter
 Y    =        4625198
05  meter          E    =           
0005664
 Z    =        4862146
29                 I    =           51
79743
 XDOT =      -6960
565207                 Wp   =           29
26830
 YDOT =      -2335
764076  meter/sec      RA   =           33
12940  deg
 ZDOT =       2348
314805                 TA   =           37
94203
                                          MA   =           37
90214
                                          Ha   =            187
311  n
mi
                                          Hp   =            179
812

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         281144
60                 X    =           10347
77
 Y    =       15174534
29  feet           Y    =         4625735
14  meter
 Z    =       15951923
53                 Z    =         4862379
48
 XDOT =     -22836
500022                 XDOT =       -6945
336546
 YDOT =      -7663
267965  feet/sec       YDOT =       -2413
515854  meter/sec
 ZDOT =       7704
444899                 ZDOT =        2314
537908

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2697766
09                 X    =         -822279
10
 Y    =      -14933922
93  feet           Y    =        -4551859
71  meter
 Z    =       15953350
79                 Z    =         4862581
32
 XDOT =      22742
582192                 XDOT =        6931
939052
 YDOT =       3971
739234  feet/sec       YDOT =        1210
586119  meter/sec
 ZDOT =       7575
941306                 ZDOT =        2309
146910


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   07251
61545728  
00020000  00000-0  20000-3 0  9035
2 25544  51
6368  33
3709 0008950 341
4413  18
6423 15
76688343 23941


Satellite: ISS
Catalog Number: 25544
Epoch time:      07251
61545728   =   yrday
fracday
Element set:     903
Inclination:       51
6368  deg
RA of node:        33
3709  deg
Eccentricity:     
0008950     
Arg of perigee:   341
4413  deg
Mean anomaly:      18
6423  deg
Mean motion:   15
76688343  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2394
Checksum:              298


Coasting Arc #5 (Orbit 2408)
---------------------------------------

Vector Time (GMT): 2007/252/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6217209
82                 A    =         6724006
15  meter
 Y    =        2234044
06  meter          E    =           
0016663
 Z    =       -1196243
20                 I    =           51
80567
 XDOT =       -637
759787                 Wp   =           11
79322
 YDOT =       4919
651840  meter/sec      RA   =           27
95531  deg
 ZDOT =       5903
392529                 TA   =          335
10331
                                          MA   =          335
18360
                                          Ha   =            187
582  n
mi
                                          Hp   =            179
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20397670
02                 X    =         6197577
39
 Y    =        7329540
87  feet           Y    =         2303458
59  meter
 Z    =       -3924682
42                 Z    =        -1166088
17
 XDOT =      -2092
387752                 XDOT =        -721
401913
 YDOT =      16140
590025  feet/sec       YDOT =        4912
052639  meter/sec
 ZDOT =      19368
085724                 ZDOT =        5900
090954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21413336
22                 X    =        -6526784
88
 Y    =       -3484771
21  feet           Y    =        -1062158
27  meter
 Z    =       -3809940
29                 Z    =        -1161269
80
 XDOT =      -1031
838132                 XDOT =        -314
504262
 YDOT =     -14709
803292  feet/sec       YDOT =       -4483
548043  meter/sec
 ZDOT =      19356
130680                 ZDOT =        5899
748631


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   07252
56618834  
00020000  00000-0  20000-3 0  9040
2 25544  51
6372  28
4691 0009128 345
9423  14
1486 15
76668363 24096


Satellite: ISS
Catalog Number: 25544
Epoch time:      07252
56618834   =   yrday
fracday
Element set:     904
Inclination:       51
6372  deg
RA of node:        28
4691  deg
Eccentricity:     
0009128     
Arg of perigee:   345
9423  deg
Mean anomaly:      14
1486  deg
Mean motion:   15
76668363  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2409
Checksum:              308


Coasting Arc #6 (Orbit 2424)
---------------------------------------

Vector Time (GMT): 2007/253/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1269557
40                 A    =         6712384
10  meter
 Y    =       -3974516
30  meter          E    =           
0016462
 Z    =       -5269917
20                 I    =           51
74119
 XDOT =       7182
899805                 Wp   =           53
87411
 YDOT =       2741
738504  meter/sec      RA   =           22
82339  deg
 ZDOT =       -328
580857                 TA   =          212
95737
                                          MA   =          213
06010
                                          Ha   =            187
588  n
mi
                                          Hp   =            179
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4165214
55                 X    =         1339506
74
 Y    =      -13039751
63  feet           Y    =        -3959928
61  meter
 Z    =      -17289754
60                 Z    =        -5263579
60
 XDOT =      23565
944243                 XDOT =        7153
303601
 YDOT =       8995
205067  feet/sec       YDOT =        2821
896247  meter/sec
 ZDOT =      -1078
021185                 ZDOT =        -293
758721

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1579899
85                 X    =         -481553
47
 Y    =       13627296
86  feet           Y    =         4153600
08  meter
 Z    =      -17266164
76                 Z    =        -5262727
02
 XDOT =     -23897
204572                 XDOT =       -7283
867954
 YDOT =      -4005
175327  feet/sec       YDOT =       -1220
777440  meter/sec
 ZDOT =       -945
503489                 ZDOT =        -288
189464


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   07253
58028061  
00020000  00000-0  20000-3 0  9051
2 25544  51
6376  23
2406 0009171 349
6355  10
4619 15
76722088 24250


Satellite: ISS
Catalog Number: 25544
Epoch time:      07253
58028061   =   yrday
fracday
Element set:     905
Inclination:       51
6376  deg
RA of node:        23
2406  deg
Eccentricity:     
0009171     
Arg of perigee:   349
6355  deg
Mean anomaly:      10
4619  deg
Mean motion:   15
76722088  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2425
Checksum:              283


Coasting Arc #7 (Orbit 2440)
---------------------------------------

Vector Time (GMT): 2007/254/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6203534
77                 A    =         6724154
43  meter
 Y    =       -2514601
92  meter          E    =           
0005917
 Z    =        -649561
15                 I    =           51
75408
 XDOT =       2334
108158                 Wp   =           81
03885
 YDOT =      -4220
005785  meter/sec      RA   =           17
67843  deg
 ZDOT =      -6000
257468                 TA   =          106
02539
                                          MA   =          105
96022
                                          Ha   =            187
671  n
mi
                                          Hp   =            179
042

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20352804
35                 X    =        -6171799
62
 Y    =       -8250006
28  feet           Y    =        -2583795
95  meter
 Z    =       -2131106
12                 Z    =         -679620
50
 XDOT =       7657
835163                 XDOT =        2410
271446
 YDOT =     -13845
163337  feet/sec       YDOT =       -4193
479059  meter/sec
 ZDOT =     -19685
884080                 ZDOT =       -5988
733116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21642300
39                 X    =         6596573
16
 Y    =        3661880
64  feet           Y    =         1116141
22  meter
 Z    =       -2245512
33                 Z    =         -684432
16
 XDOT =      -4327
545505                 XDOT =       -1319
035870
 YDOT =      13617
929230  feet/sec       YDOT =        4150
744829  meter/sec
 ZDOT =     -19642
635469                 ZDOT =       -5987
075291


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   07254
59435284  
00020000  00000-0  20000-3 0  9063
2 25544  51
6376  18
0113 0009155 353
7187   6
3861 15
76749460 24412


Satellite: ISS
Catalog Number: 25544
Epoch time:      07254
59435284   =   yrday
fracday
Element set:     906
Inclination:       51
6376  deg
RA of node:        18
0113  deg
Eccentricity:     
0009155     
Arg of perigee:   353
7187  deg
Mean anomaly:       6
3861  deg
Mean motion:   15
76749460  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2441
Checksum:              297


Coasting Arc #8 (Orbit 2456)
---------------------------------------

Vector Time (GMT): 2007/255/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2810271
63                 A    =         6713229
88  meter
 Y    =        3446324
88  meter          E    =           
0013168
 Z    =        5029069
68                 I    =           51
69034
 XDOT =      -6878
624772                 Wp   =           17
77987
 YDOT =      -2975
312604  meter/sec      RA   =           12
50599  deg
 ZDOT =      -1791
345004                 TA   =           89
52906
                                          MA   =           89
37818
                                          Ha   =            187
839  n
mi
                                          Hp   =            178
714

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9220051
29                 X    =        -2873030
41
 Y    =       11306840
16  feet           Y    =         3414548
32  meter
 Z    =       16499572
43                 Z    =         5015264
67
 XDOT =     -22567
666575                 XDOT =       -6836
141115
 YDOT =      -9761
524292  feet/sec       YDOT =       -3051
995874  meter/sec
 ZDOT =      -5877
116156                 ZDOT =       -1824
657945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6425173
93                 X    =         1958393
01
 Y    =      -13163746
57  feet           Y    =        -4012309
96  meter
 Z    =       16447576
92                 Z    =         5013221
45
 XDOT =      23227
502452                 XDOT =        7079
742747
 YDOT =       3779
898864  feet/sec       YDOT =        1152
113174  meter/sec
 ZDOT =      -6003
921926                 ZDOT =       -1829
995403


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   07255
60840363  
00020000  00000-0  20000-3 0  9075
2 25544  51
6383  12
7818 0009359 357
6611   2
4508 15
76806601 24577


Satellite: ISS
Catalog Number: 25544
Epoch time:      07255
60840363   =   yrday
fracday
Element set:     907
Inclination:       51
6383  deg
RA of node:        12
7818  deg
Eccentricity:     
0009359     
Arg of perigee:   357
6611  deg
Mean anomaly:       2
4508  deg
Mean motion:   15
76806601  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2457
Checksum:              294


Coasting Arc #9 (Orbit 2472)
---------------------------------------

Vector Time (GMT): 2007/256/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5660028
03                 A    =         6721538
72  meter
 Y    =        2665427
52  meter          E    =           
0018854
 Z    =        2424348
64                 I    =           51
69015
 XDOT =      -4072
863450                 Wp   =           46
18493
 YDOT =       3751
118982  meter/sec      RA   =            7
38969  deg
 ZDOT =       5371
688281                 TA   =          341
23348
                                          MA   =          341
30290
                                          Ha   =            187
820  n
mi
                                          Hp   =            178
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18569645
77                 X    =         5618025
05
 Y    =        8744840
93  feet           Y    =         2728486
48  meter
 Z    =        7953899
74                 Z    =         2451742
97
 XDOT =     -13362
412893                 XDOT =       -4140
601140
 YDOT =      12306
820806  feet/sec       YDOT =        3705
195575  meter/sec
 ZDOT =      17623
649217                 ZDOT =        5351
737404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20120427
32                 X    =        -6132706
25
 Y    =       -3847385
98  feet           Y    =        -1172683
25  meter
 Z    =        8058196
66                 Z    =         2456138
34
 XDOT =       9685
258415                 XDOT =        2952
066765
 YDOT =     -13808
345834  feet/sec       YDOT =       -4208
783810  meter/sec
 ZDOT =      17548
362606                 ZDOT =        5348
740922


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   07256
62243463  
00020000  00000-0  20000-3 0  9087
2 25544  51
6383   7
5528 0009365   1
8742 358
2456 15
76820032 24733


Satellite: ISS
Catalog Number: 25544
Epoch time:      07256
62243463   =   yrday
fracday
Element set:     908
Inclination:       51
6383  deg
RA of node:         7
5528  deg
Eccentricity:     
0009365     
Arg of perigee:     1
8742  deg
Mean anomaly:     358
2456  deg
Mean motion:   15
76820032  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2473
Checksum:              292


Coasting Arc #10 (Orbit 2487)
---------------------------------------

Vector Time (GMT): 2007/257/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4235140
50                 A    =         6716538
17  meter
 Y    =       -3137191
64  meter          E    =           
0010693
 Z    =       -4165953
47                 I    =           51
64427
 XDOT =       5969
145511                 Wp   =           50
78042
 YDOT =       3159
660925  meter/sec      RA   =            2
18884  deg
 ZDOT =       3701
822732                 TA   =          256
96162
                                          MA   =          257
08102
                                          Ha   =            187
991  n
mi
                                          Hp   =            178
250

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13894817
91                 X    =         4290143
91
 Y    =      -10292623
49  feet           Y    =        -3089524
63  meter
 Z    =      -13667826
34                 Z    =        -4145245
17
 XDOT =      19583
810732                 XDOT =        5915
387124
 YDOT =      10366
341619  feet/sec       YDOT =        3226
110942  meter/sec
 ZDOT =      12145
087703                 ZDOT =        3730
690310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10729265
11                 X    =        -3270280
00
 Y    =       13638891
06  feet           Y    =         4157134
00  meter
 Z    =      -13589593
84                 Z    =        -4142108
20
 XDOT =     -20575
378587                 XDOT =       -6271
375393
 YDOT =      -4017
785536  feet/sec       YDOT =       -1224
621031  meter/sec
 ZDOT =      12255
029181                 ZDOT =        3735
332895


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   07257
57306968  
00020000  00000-0  20000-3 0  9093
2 25544  51
6379   2
6513 0009430   5
5329 354
5939 15
76867279 24888


Satellite: ISS
Catalog Number: 25544
Epoch time:      07257
57306968   =   yrday
fracday
Element set:     909
Inclination:       51
6379  deg
RA of node:         2
6513  deg
Eccentricity:     
0009430     
Arg of perigee:     5
5329  deg
Mean anomaly:     354
5939  deg
Mean motion:   15
76867279  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2488
Checksum:              333


Coasting Arc #11 (Orbit 2503)
---------------------------------------

Vector Time (GMT): 2007/258/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4618893
37                 A    =         6717189
16  meter
 Y    =       -2891915
47  meter          E    =           
0014120
 Z    =       -3942995
66                 I    =           51
61696
 XDOT =       5585
606781                 Wp   =           34
83039
 YDOT =      -3458
780728  meter/sec      RA   =          357
08223  deg
 ZDOT =      -4001
945295                 TA   =          193
57119
                                          MA   =          193
60920
                                          Ha   =            188
069  n
mi
                                          Hp   =            177
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15153849
64                 X    =        -4567057
67
 Y    =       -9487911
65  feet           Y    =        -2943276
92  meter
 Z    =      -12936337
47                 Z    =        -3965308
44
 XDOT =      18325
481564                 XDOT =        5643
309196
 YDOT =     -11347
705802  feet/sec       YDOT =       -3395
996885  meter/sec
 ZDOT =     -13129
741783                 ZDOT =       -3974
669780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17147494
02                 X    =         5226556
18
 Y    =        4839006
59  feet           Y    =         1474929
21  meter
 Z    =      -13021363
90                 Z    =        -3968911
72
 XDOT =     -14089
102882                 XDOT =       -4294
358559
 YDOT =      14834
376030  feet/sec       YDOT =        4521
517814  meter/sec
 ZDOT =     -13026
621006                 ZDOT =       -3970
514083


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   07258
58706013  
00020000  00000-0  20000-3 0  9102
2 25544  51
6372 357
4215 0009505   9
1245 351
0091 15
76862852 25043


Satellite: ISS
Catalog Number: 25544
Epoch time:      07258
58706013   =   yrday
fracday
Element set:     910
Inclination:       51
6372  deg
RA of node:       357
4215  deg
Eccentricity:     
0009505     
Arg of perigee:     9
1245  deg
Mean anomaly:     351
0091  deg
Mean motion:   15
76862852  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2504
Checksum:              277


Coasting Arc #12 (Orbit 2519)
---------------------------------------

Vector Time (GMT): 2007/259/13:32:04
852
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5414663
43                 A    =         6720764
98  meter
 Y    =        2929071
45  meter          E    =           
0016964
 Z    =        2692829
08                 I    =           51
60081
 XDOT =      -4491
090119                 Wp   =           66
38957
 YDOT =      -3507
897548  meter/sec      RA   =          351
87351  deg
 ZDOT =      -5182
562354                 TA   =           82
85557
                                          MA   =           82
66271
                                          Ha   =            188
183  n
mi
                                          Hp   =            177
714

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17764643
80                 X    =        -5460095
75
 Y    =        9609814
46  feet           Y    =         2868267
68  meter
 Z    =        8834741
07                 Z    =         2666413
86
 XDOT =     -14734
547633                 XDOT =       -4426
354229
 YDOT =     -11508
850224  feet/sec       YDOT =       -3557
757668  meter/sec
 ZDOT =     -17003
157331                 ZDOT =       -5204
222981

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14124701
50                 X    =         4305209
02
 Y    =      -14497566
11  feet           Y    =        -4418858
15  meter
 Z    =        8734823
25                 Z    =         2662374
13
 XDOT =      16353
492380                 XDOT =        4984
544477
 YDOT =       5573
995808  feet/sec       YDOT =        1698
953922  meter/sec
 ZDOT =     -17085
777108                 ZDOT =       -5207
744862


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   07259
60102851  
00020000  00000-0  20000-3 0  9117
2 25544  51
6375 352
1915 0009760  13
0097 347
1318 15
76930650 25205


Satellite: ISS
Catalog Number: 25544
Epoch time:      07259
60102851   =   yrday
fracday
Element set:     911
Inclination:       51
6375  deg
RA of node:       352
1915  deg
Eccentricity:     
0009760     
Arg of perigee:    13
0097  deg
Mean anomaly:     347
1318  deg
Mean motion:   15
76930650  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2520
Checksum:              274

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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