Date: May 14th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6189 25 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 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 465)
---------------------------------------

Vector Time (GMT): 2007/129/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3419162
00                 A    =         6709490
86  meter
 Y    =       -2439738
82  meter          E    =           
0020372
 Z    =       -5247532
71                 I    =           51
34415
 XDOT =       4320
806696                 Wp   =          119
12973
 YDOT =      -6364
543410  meter/sec      RA   =          303
37157  deg
 ZDOT =        134
362316                 TA   =          152
20622
                                          MA   =          152
09722
                                          Ha   =            187
054  n
mi
                                          Hp   =            176
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11217723
10                 X    =        -3366134
75
 Y    =       -8004392
47  feet           Y    =        -2477676
86  meter
 Z    =      -17216314
67                 Z    =        -5264014
44
 XDOT =      14175
874988                 XDOT =        4391
002103
 YDOT =     -20881
047934  feet/sec       YDOT =       -6315
833259  meter/sec
 ZDOT =        440
821246                 ZDOT =         155
522784

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13695355
32                 X    =        -4174344
30
 Y    =        -439422
32  feet           Y    =         -133935
92  meter
 Z    =      -17278693
57                 Z    =        -5266545
80
 XDOT =         83
212041                 XDOT =          25
363030
 YDOT =     -24237
888648  feet/sec       YDOT =       -7387
708460  meter/sec
 ZDOT =        519
790785                 ZDOT =         158
432231


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   07129
48157741  
00020000  00000-0  20000-3 0  9005
2 25544  51
6320 303
8876 0010026 164
4761 195
6714 15
77735273  4668


Satellite: ISS
Catalog Number: 25544
Epoch time:      07129
48157741   =   yrday
fracday
Element set:     900
Inclination:       51
6320  deg
RA of node:       303
8876  deg
Eccentricity:     
0010026     
Arg of perigee:   164
4761  deg
Mean anomaly:     195
6714  deg
Mean motion:   15
77735273  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             466
Checksum:              295


Coasting Arc #2 (Orbit 481)
---------------------------------------

Vector Time (GMT): 2007/130/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4027003
22                 A    =         6720548
12  meter
 Y    =        5190547
27  meter          E    =           
0018036
 Z    =       -1371360
16                 I    =           51
36765
 XDOT =      -3147
406970                 Wp   =          156
14089
 YDOT =      -3967
297411  meter/sec      RA   =          298
20180  deg
 ZDOT =      -5816
503787                 TA   =           39
02321
                                          MA   =           38
89321
                                          Ha   =            186
744  n
mi
                                          Hp   =            176
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13211952
82                 X    =        -4078083
54
 Y    =       17029354
57  feet           Y    =         5145229
55  meter
 Z    =       -4499213
11                 Z    =        -1391047
11
 XDOT =     -10326
138352                 XDOT =       -3074
554566
 YDOT =     -13016
067621  feet/sec       YDOT =       -4002
085746  meter/sec
 ZDOT =     -19083
017673                 ZDOT =       -5831
617236

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1075140
25                 X    =         -327702
75
 Y    =       21511192
90  feet           Y    =         6556611
59  meter
 Z    =       -4572765
74                 Z    =        -1393779
00
 XDOT =     -14259
168413                 XDOT =       -4346
194532
 YDOT =      -4752
108092  feet/sec       YDOT =       -1448
442546  meter/sec
 ZDOT =     -19140
427996                 ZDOT =       -5834
002453


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   07130
49498822  
00020000  00000-0  20000-3 0  9017
2 25544  51
6322 298
6536 0009804 168
3443 191
7951 15
77796843  4824


Satellite: ISS
Catalog Number: 25544
Epoch time:      07130
49498822   =   yrday
fracday
Element set:     901
Inclination:       51
6322  deg
RA of node:       298
6536  deg
Eccentricity:     
0009804     
Arg of perigee:   168
3443  deg
Mean anomaly:     191
7951  deg
Mean motion:   15
77796843  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             482
Checksum:              323


Coasting Arc #3 (Orbit 497)
---------------------------------------

Vector Time (GMT): 2007/131/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2110047
72                 A    =         6712158
40  meter
 Y    =        4417335
69  meter          E    =           
0010805
 Z    =        4581615
52                 I    =           51
32599
 XDOT =      -4782
930221                 Wp   =          125
28097
 YDOT =       5305
332100  meter/sec      RA   =          292
97977  deg
 ZDOT =      -2913
688825                 TA   =          353
64469
                                          MA   =          353
65838
                                          Ha   =            186
668  n
mi
                                          Hp   =            176
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6922728
73                 X    =         2038238
84
 Y    =       14492571
15  feet           Y    =         4440529
69  meter
 Z    =       15031546
98                 Z    =         4591691
98
 XDOT =     -15692
028284                 XDOT =       -4827
745495
 YDOT =      17405
945211  feet/sec       YDOT =        5251
596264  meter/sec
 ZDOT =      -9559
346538                 ZDOT =       -2937
033005

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14034486
96                 X    =         4277711
63
 Y    =        7735196
82  feet           Y    =         2357687
99  meter
 Z    =       15070039
88                 Z    =         4593348
15
 XDOT =      -1906
827834                 XDOT =        -581
201124
 YDOT =      22245
118544  feet/sec       YDOT =        6780
312132  meter/sec
 ZDOT =      -9646
659410                 ZDOT =       -2940
301788


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   07131
50837513  
00020000  00000-0  20000-3 0  9025
2 25544  51
6314 293
4186 0009944 172
6509 187
4803 15
77793417  4984


Satellite: ISS
Catalog Number: 25544
Epoch time:      07131
50837513   =   yrday
fracday
Element set:     902
Inclination:       51
6314  deg
RA of node:       293
4186  deg
Eccentricity:     
0009944     
Arg of perigee:   172
6509  deg
Mean anomaly:     187
4803  deg
Mean motion:   15
77793417  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             498
Checksum:              311


Coasting Arc #4 (Orbit 513)
---------------------------------------

Vector Time (GMT): 2007/132/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4225008
66                 A    =         6715564
20  meter
 Y    =       -3810707
16  meter          E    =           
0016641
 Z    =        3566438
65                 I    =           51
32799
 XDOT =       1745
296738                 Wp   =          130
23703
 YDOT =       6077
682327  meter/sec      RA   =          287
84009  deg
 ZDOT =       4402
255504                 TA   =          272
62786
                                          MA   =          272
81834
                                          Ha   =            186
496  n
mi
                                          Hp   =            176
568

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13861576
96                 X    =         4249981
25
 Y    =      -12502320
08  feet           Y    =        -3763321
25  meter
 Z    =       11700914
22                 Z    =         3587024
45
 XDOT =       5726
039167                 XDOT =        1655
819935
 YDOT =      19939
902646  feet/sec       YDOT =        6096
698751  meter/sec
 ZDOT =      14443
095485                 ZDOT =        4410
517131

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3537863
15                 X    =         1078340
69
 Y    =      -18279077
93  feet           Y    =        -5571462
95  meter
 Z    =       11778011
34                 Z    =         3589937
86
 XDOT =      15145
543713                 XDOT =        4616
361724
 YDOT =      12308
867104  feet/sec       YDOT =        3751
742693  meter/sec
 ZDOT =      14474
955395                 ZDOT =        4411
966404


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   07132
52173504  
00020000  00000-0  20000-3 0  9032
2 25544  51
6311 288
1831 0009974 176
6666 183
4567 15
77871425  5148


Satellite: ISS
Catalog Number: 25544
Epoch time:      07132
52173504   =   yrday
fracday
Element set:     903
Inclination:       51
6311  deg
RA of node:       288
1831  deg
Eccentricity:     
0009974     
Arg of perigee:   176
6666  deg
Mean anomaly:     183
4567  deg
Mean motion:   15
77871425  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             514
Checksum:              302


Coasting Arc #5 (Orbit 528)
---------------------------------------

Vector Time (GMT): 2007/133/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -985248
13                 A    =         6717587
98  meter
 Y    =       -6013792
58  meter          E    =           
0008886
 Z    =       -2840700
57                 I    =           51
32827
 XDOT =       4855
177618                 Wp   =          151
52505
 YDOT =      -3182
702712  meter/sec      RA   =          282
60144  deg
 ZDOT =       5052
668694                 TA   =          175
71265
                                          MA   =          175
70503
                                          Ha   =            186
391  n
mi
                                          Hp   =            176
713

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3232441
37                 X    =         -904127
98
 Y    =      -19730290
61  feet           Y    =        -6024356
49  meter
 Z    =       -9319883
74                 Z    =        -2845290
18
 XDOT =      15929
060427                 XDOT =        4865
860893
 YDOT =     -10441
938031  feet/sec       YDOT =       -3128
349868  meter/sec
 ZDOT =      16576
997027                 ZDOT =        5076
281321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14617168
58                 X    =        -4455312
98
 Y    =      -13628470
56  feet           Y    =        -4153957
83  meter
 Z    =       -9337903
98                 Z    =        -2846193
13
 XDOT =       5104
333231                 XDOT =        1555
800769
 YDOT =     -16896
206148  feet/sec       YDOT =       -5149
963634  meter/sec
 ZDOT =      16665
572502                 ZDOT =        5079
666499


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   07133
47173877  
00020000  00000-0  20000-3 0  9041
2 25544  51
6319 283
2749 0009942 179
4511 180
6667 15
77891065  5293


Satellite: ISS
Catalog Number: 25544
Epoch time:      07133
47173877   =   yrday
fracday
Element set:     904
Inclination:       51
6319  deg
RA of node:       283
2749  deg
Eccentricity:     
0009942     
Arg of perigee:   179
4511  deg
Mean anomaly:     180
6667  deg
Mean motion:   15
77891065  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             529
Checksum:              326


Coasting Arc #6 (Orbit 544)
---------------------------------------

Vector Time (GMT): 2007/134/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4227354
09                 A    =         6710056
84  meter
 Y    =        1569638
17  meter          E    =           
0013966
 Z    =       -4977705
39                 I    =           51
29884
 XDOT =       -552
390770                 Wp   =          117
95260
 YDOT =      -7444
211166  meter/sec      RA   =          277
45239  deg
 ZDOT =      -1888
774095                 TA   =          133
78571
                                          MA   =          133
67008
                                          Ha   =            186
084  n
mi
                                          Hp   =            176
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13869271
95                 X    =        -4220410
54
 Y    =        5149731
51  feet           Y    =         1522404
64  meter
 Z    =      -16331054
43                 Z    =        -4998225
34
 XDOT =      -1812
305675                 XDOT =        -459
931954
 YDOT =     -24423
264981  feet/sec       YDOT =       -7449
871235  meter/sec
 ZDOT =      -6196
765402                 ZDOT =       -1891
233515

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7503363
54                 X    =        -2287025
21
 Y    =       12651131
04  feet           Y    =         3856064
74  meter
 Z    =      -16408174
70                 Z    =        -5001211
65
 XDOT =     -15777
029311                 XDOT =       -4808
838534
 YDOT =     -17363
143751  feet/sec       YDOT =       -5292
286215  meter/sec
 ZDOT =      -6206
932718                 ZDOT =       -1891
873092


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   07134
48505042  
00020000  00000-0  20000-3 0  9057
2 25544  51
6324 278
0404 0009798 182
9339 177
1770 15
77944801  5456


Satellite: ISS
Catalog Number: 25544
Epoch time:      07134
48505042   =   yrday
fracday
Element set:     905
Inclination:       51
6324  deg
RA of node:       278
0404  deg
Eccentricity:     
0009798     
Arg of perigee:   182
9339  deg
Mean anomaly:     177
1770  deg
Mean motion:   15
77944801  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             545
Checksum:              305


Coasting Arc #7 (Orbit 560)
---------------------------------------

Vector Time (GMT): 2007/135/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          16412
80                 A    =         6720812
52  meter
 Y    =        6699221
67  meter          E    =           
0019970
 Z    =         348095
04                 I    =           51
33260
 XDOT =      -4826
385690                 Wp   =          155
18639
 YDOT =        329
658144  meter/sec      RA   =          272
24265  deg
 ZDOT =      -6010
602475                 TA   =           21
00297
                                          MA   =           20
92107
                                          Ha   =            185
842  n
mi
                                          Hp   =            177
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          53847
77                 X    =          -60191
11
 Y    =       21979073
73  feet           Y    =         6698976
87  meter
 Z    =        1142044
11                 Z    =          347989
31
 XDOT =     -15834
598721                 XDOT =       -4800
514159
 YDOT =       1081
555591  feet/sec       YDOT =         275
831989  meter/sec
 ZDOT =     -19719
824392                 ZDOT =       -6033
986738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14111088
85                 X    =         4301059
88
 Y    =       16851077
66  feet           Y    =         5136208
47  meter
 Z    =        1142453
46                 Z    =          348219
81
 XDOT =     -10155
902264                 XDOT =       -3095
519010
 YDOT =       9871
087014  feet/sec       YDOT =        3008
707322  meter/sec
 ZDOT =     -19807
889330                 ZDOT =       -6037
444668


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   07135
49833603  
00020000  00000-0  20000-3 0  9067
2 25544  51
6319 272
8039 0009674 187
9575 172
1438 15
77987429  5613


Satellite: ISS
Catalog Number: 25544
Epoch time:      07135
49833603   =   yrday
fracday
Element set:     906
Inclination:       51
6319  deg
RA of node:       272
8039  deg
Eccentricity:     
0009674     
Arg of perigee:   187
9575  deg
Mean anomaly:     172
1438  deg
Mean motion:   15
77987429  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             561
Checksum:              332


Coasting Arc #8 (Orbit 576)
---------------------------------------

Vector Time (GMT): 2007/136/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4180315
99                 A    =         6709220
98  meter
 Y    =        1026683
20  meter          E    =           
0007486
 Z    =        5143915
64                 I    =           51
29443
 XDOT =       -503
610729                 Wp   =          169
23559
 YDOT =       7611
968716  meter/sec      RA   =          267
04704  deg
 ZDOT =      -1117
020192                 TA   =          291
42387
                                          MA   =          291
50371
                                          Ha   =            185
714  n
mi
                                          Hp   =            177
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13714947
46                 X    =         4143535
98
 Y    =        3368383
20  feet           Y    =         1073223
54  meter
 Z    =       16876363
66                 Z    =         5164134
88
 XDOT =      -1652
266172                 XDOT =        -583
265032
 YDOT =      24973
650644  feet/sec       YDOT =        7605
891830  meter/sec
 ZDOT =      -3664
764411                 ZDOT =       -1119
659317

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12511072
95                 X    =         3813375
04
 Y    =       -6351174
90  feet           Y    =        -1935838
11  meter
 Z    =       16952671
48                 Z    =         5167174
27
 XDOT =      14621
546245                 XDOT =        4456
647296
 YDOT =      19057
638746  feet/sec       YDOT =        5808
768290  meter/sec
 ZDOT =      -3673
795620                 ZDOT =       -1119
772905


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   07136
51159956  
00020000  00000-0  20000-3 0  9074
2 25544  51
6328 267
5688 0009668 190
7763 169
3196 15
77967972  5775


Satellite: ISS
Catalog Number: 25544
Epoch time:      07136
51159956   =   yrday
fracday
Element set:     907
Inclination:       51
6328  deg
RA of node:       267
5688  deg
Eccentricity:     
0009668     
Arg of perigee:   190
7763  deg
Mean anomaly:     169
3196  deg
Mean motion:   15
77967972  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             577
Checksum:              361


Coasting Arc #9 (Orbit 592)
---------------------------------------

Vector Time (GMT): 2007/137/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         926609
88                 A    =         6718377
75  meter
 Y    =       -6262009
34  meter          E    =           
0011905
 Z    =        2250527
27                 I    =           51
33043
 XDOT =       4768
937392                 Wp   =          115
28336
 YDOT =       2666
731513  meter/sec      RA   =          261
88716  deg
 ZDOT =       5429
193875                 TA   =          270
12360
                                          MA   =          270
26002
                                          Ha   =            185
515  n
mi
                                          Hp   =            177
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3040058
65                 X    =          985630
84
 Y    =      -20544650
06  feet           Y    =        -6251317
82  meter
 Z    =        7383619
65                 Z    =         2255171
21
 XDOT =      15646
120053                 XDOT =        4712
388623
 YDOT =       8749
119138  feet/sec       YDOT =        2719
743411  meter/sec
 ZDOT =      17812
315862                 ZDOT =        5452
224884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11455231
22                 X    =        -3491554
47
 Y    =      -17316310
81  feet           Y    =        -5278011
54  meter
 Z    =        7400371
57                 Z    =         2255633
26
 XDOT =      16158
940186                 XDOT =        4925
244969
 YDOT =      -3001
731896  feet/sec       YDOT =        -914
927882  meter/sec
 ZDOT =      17899
421555                 ZDOT =        5455
743690


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   07137
52483284  
00020000  00000-0  20000-3 0  9081
2 25544  51
6340 262
3336 0009757 195
6430 164
4435 15
78080077  5939


Satellite: ISS
Catalog Number: 25544
Epoch time:      07137
52483284   =   yrday
fracday
Element set:     908
Inclination:       51
6340  deg
RA of node:       262
3336  deg
Eccentricity:     
0009757     
Arg of perigee:   195
6430  deg
Mean anomaly:     164
4435  deg
Mean motion:   15
78080077  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             593
Checksum:              302


Coasting Arc #10 (Orbit 607)
---------------------------------------

Vector Time (GMT): 2007/138/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4115291
73                 A    =         6713595
56  meter
 Y    =       -3508446
79  meter          E    =           
0011820
 Z    =       -3989762
90                 I    =           51
31980
 XDOT =       1684
989381                 Wp   =          162
19272
 YDOT =      -6419
577694  meter/sec      RA   =          256
65195  deg
 ZDOT =       3899
068538                 TA   =          148
29868
                                          MA   =          148
22745
                                          Ha   =            185
282  n
mi
                                          Hp   =            177
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13501613
29                 X    =        -4056372
11
 Y    =      -11510652
19  feet           Y    =        -3554136
15  meter
 Z    =      -13089773
29                 Z    =        -4009612
75
 XDOT =       5528
180385                 XDOT =        1737
707581
 YDOT =     -21061
606606  feet/sec       YDOT =       -6400
441119  meter/sec
 ZDOT =      12792
219612                 ZDOT =        3907
381257

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17673817
67                 X    =        -5386979
63
 Y    =         670656
93  feet           Y    =          204416
23  meter
 Z    =      -13165000
12                 Z    =        -4012692
04
 XDOT =     -10249
467445                 XDOT =       -3124
037677
 YDOT =     -17876
609058  feet/sec       YDOT =       -5448
790441  meter/sec
 ZDOT =      12822
782043                 ZDOT =        3908
383967


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   07138
47472026  
00020000  00000-0  20000-3 0  9099
2 25544  51
6342 257
4261 0009516 199
8111 160
2686 15
78070354  6084


Satellite: ISS
Catalog Number: 25544
Epoch time:      07138
47472026   =   yrday
fracday
Element set:     909
Inclination:       51
6342  deg
RA of node:       257
4261  deg
Eccentricity:     
0009516     
Arg of perigee:   199
8111  deg
Mean anomaly:     160
2686  deg
Mean motion:   15
78070354  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             608
Checksum:              295


Coasting Arc #11 (Orbit 623)
---------------------------------------

Vector Time (GMT): 2007/139/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2079922
27                 A    =         6712280
59  meter
 Y    =        4694479
96  meter          E    =           
0007130
 Z    =       -4323919
24                 I    =           51
32372
 XDOT =      -4598
001448                 Wp   =          140
39038
 YDOT =      -5163
169544  meter/sec      RA   =          251
51277  deg
 ZDOT =      -3402
385191                 TA   =           95
20726
                                          MA   =           95
12589
                                          Ha   =            184
992  n
mi
                                          Hp   =            177
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6823891
96                 X    =        -2111257
08
 Y    =       15401837
13  feet           Y    =         4671046
67  meter
 Z    =      -14186086
74                 Z    =        -4334098
85
 XDOT =     -15085
306587                 XDOT =       -4523
396119
 YDOT =     -16939
532625  feet/sec       YDOT =       -5214
169227  meter/sec
 ZDOT =     -11162
681074                 ZDOT =       -3424
542140

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5781743
28                 X    =         1762275
35
 Y    =       15788585
63  feet           Y    =         4812360
90  meter
 Z    =      -14223893
76                 Z    =        -4335442
82
 XDOT =     -21414
810981                 XDOT =       -6527
234387
 YDOT =      -2265
128743  feet/sec       YDOT =        -690
411241  meter/sec
 ZDOT =     -11246
812089                 ZDOT =       -3428
028325


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   07139
48790815  
00020000  00000-0  20000-3 0  9102
2 25544  51
6343 252
1906 0009486 204
0364 156
0360 15
78111973  6241


Satellite: ISS
Catalog Number: 25544
Epoch time:      07139
48790815   =   yrday
fracday
Element set:     910
Inclination:       51
6343  deg
RA of node:       252
1906  deg
Eccentricity:     
0009486     
Arg of perigee:   204
0364  deg
Mean anomaly:     156
0360  deg
Mean motion:   15
78111973  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             624
Checksum:              285


Coasting Arc #12 (Orbit 639)
---------------------------------------

Vector Time (GMT): 2007/140/11:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3813751
22                 A    =         6719067
43  meter
 Y    =        5239927
00  meter          E    =           
0016656
 Z    =        1731158
53                 I    =           51
35733
 XDOT =      -3136
312144                 Wp   =          149
53099
 YDOT =       4164
605293  meter/sec      RA   =          246
28322  deg
 ZDOT =      -5686
616805                 TA   =           11
17521
                                          MA   =           11
13827
                                          Ha   =            184
779  n
mi
                                          Hp   =            177
998

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12512307
16                 X    =         3746464
48
 Y    =       17191361
55  feet           Y    =         5282198
00  meter
 Z    =        5679653
97                 Z    =         1749523
21
 XDOT =     -10289
738004                 XDOT =       -3155
023670
 YDOT =      13663
403193  feet/sec       YDOT =        4129
429624  meter/sec
 ZDOT =     -18656
879280                 ZDOT =       -5701
897790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20966175
81                 X    =         6390490
39
 Y    =        3423709
38  feet           Y    =         1043546
62  meter
 Z    =        5749512
82                 Z    =         1752451
51
 XDOT =       2634
585235                 XDOT =         803
021579
 YDOT =      15345
525657  feet/sec       YDOT =        4677
316220  meter/sec
 ZDOT =     -18713
981058                 ZDOT =       -5704
021426


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   07140
50107187  
00020000  00000-0  20000-3 0  9112
2 25544  51
6342 246
9552 0009431 207
5844 152
4822 15
78146586  6408


Satellite: ISS
Catalog Number: 25544
Epoch time:      07140
50107187   =   yrday
fracday
Element set:     911
Inclination:       51
6342  deg
RA of node:       246
9552  deg
Eccentricity:     
0009431     
Arg of perigee:   207
5844  deg
Mean anomaly:     152
4822  deg
Mean motion:   15
78146586  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             640
Checksum:              282

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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