Date: May 6th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5812 51 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 386)
---------------------------------------

Vector Time (GMT): 2007/124/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2103763
29                 A    =         6715125
04  meter
 Y    =       -4971560
20  meter          E    =           
0016447
 Z    =       -4012371
13                 I    =           51
46634
 XDOT =       6625
729126                 Wp   =          129
80581
 YDOT =       -337
403525  meter/sec      RA   =          329
23003  deg
 ZDOT =       3892
245354                 TA   =          180
50099
                                          MA   =          180
50264
                                          Ha   =            187
829  n
mi
                                          Hp   =            175
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6902110
52                 X    =         2178691
38
 Y    =      -16310893
05  feet           Y    =        -4947615
43  meter
 Z    =      -13163947
27                 Z    =        -4001969
31
 XDOT =      21737
956451                 XDOT =        6610
101394
 YDOT =      -1106
966946  feet/sec       YDOT =        -263
398652  meter/sec
 ZDOT =      12769
833838                 ZDOT =        3924
395776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2108369
12                 X    =         -642630
91
 Y    =      -17614026
80  feet           Y    =        -5368755
37  meter
 Z    =      -13125346
06                 Z    =        -4000605
48
 XDOT =      16929
786968                 XDOT =        5160
199068
 YDOT =     -11631
839656  feet/sec       YDOT =       -3545
384727  meter/sec
 ZDOT =      12890
884295                 ZDOT =        3929
141533


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   07124
47746049  
00020000  00000-0  20000-3 0  9004
2 25544  51
6338 329
7276 0010167 145
3643 214
8186 15
77549773  3878


Satellite: ISS
Catalog Number: 25544
Epoch time:      07124
47746049   =   yrday
fracday
Element set:     900
Inclination:       51
6338  deg
RA of node:       329
7276  deg
Eccentricity:     
0010167     
Arg of perigee:   145
3643  deg
Mean anomaly:     214
8186  deg
Mean motion:   15
77549773  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             387
Checksum:              314


Coasting Arc #2 (Orbit 402)
---------------------------------------

Vector Time (GMT): 2007/125/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5208195
80                 A    =         6714136
05  meter
 Y    =        -390180
17  meter          E    =           
0014288
 Z    =       -4226955
17                 I    =           51
43841
 XDOT =       3339
588631                 Wp   =          113
16827
 YDOT =      -5941
541300  meter/sec      RA   =          324
10441  deg
 ZDOT =      -3581
481332                 TA   =          120
39830
                                          MA   =          120
25700
                                          Ha   =            187
632  n
mi
                                          Hp   =            175
727

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17087256
55                 X    =        -5182911
55
 Y    =       -1280118
66  feet           Y    =         -448279
30  meter
 Z    =      -13867963
14                 Z    =        -4252195
61
 XDOT =      10956
655612                 XDOT =        3423
178065
 YDOT =     -19493
245735  feet/sec       YDOT =       -5903
728387  meter/sec
 ZDOT =     -11750
266836                 ZDOT =       -3565
054956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15243952
81                 X    =        -4646356
82
 Y    =        7654269
21  feet           Y    =         2333021
26  meter
 Z    =      -13963076
57                 Z    =        -4255945
74
 XDOT =        -20
424647                 XDOT =          -6
225432
 YDOT =     -21274
422419  feet/sec       YDOT =       -6484
443953  meter/sec
 ZDOT =     -11689
082484                 ZDOT =       -3562
832341


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   07125
49099870  
00020000  00000-0  20000-3 0  9011
2 25544  51
6329 324
4939 0010091 149
5251 210
6503 15
77568262  4033


Satellite: ISS
Catalog Number: 25544
Epoch time:      07125
49099870   =   yrday
fracday
Element set:     901
Inclination:       51
6329  deg
RA of node:       324
4939  deg
Eccentricity:     
0010091     
Arg of perigee:   149
5251  deg
Mean anomaly:     210
6503  deg
Mean motion:   15
77568262  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             403
Checksum:              286


Coasting Arc #3 (Orbit 418)
---------------------------------------

Vector Time (GMT): 2007/126/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3553859
22                 A    =         6719986
25  meter
 Y    =        5296382
27  meter          E    =           
0022455
 Z    =        2073480
48                 I    =           51
43688
 XDOT =      -5208
676322                 Wp   =          127
71366
 YDOT =      -1315
666057  meter/sec      RA   =          318
88245  deg
 ZDOT =      -5539
674838                 TA   =           28
99622
                                          MA   =           28
87167
                                          Ha   =            187
434  n
mi
                                          Hp   =            175
918

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11659643
12                 X    =        -3622892
72
 Y    =       17376582
26  feet           Y    =         5256254
80  meter
 Z    =        6802757
47                 Z    =         2056048
56
 XDOT =     -17088
833079                 XDOT =       -5166
666180
 YDOT =      -4316
489688  feet/sec       YDOT =       -1373
676854  meter/sec
 ZDOT =     -18174
786213                 ZDOT =       -5564
876997

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -729609
30                 X    =         -222384
91
 Y    =       20934215
13  feet           Y    =         6380748
77  meter
 Z    =        6737707
72                 Z    =         2053653
31
 XDOT =     -15171
259844                 XDOT =       -4624
200000
 YDOT =       5380
336810  feet/sec       YDOT =        1639
926660  meter/sec
 ZDOT =     -18269
867346                 ZDOT =       -5568
655567


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   07126
50451391  
00020000  00000-0  20000-3 0  9025
2 25544  51
6336 319
2602 0009893 153
1448 207
0230 15
77646387  4196


Satellite: ISS
Catalog Number: 25544
Epoch time:      07126
50451391   =   yrday
fracday
Element set:     902
Inclination:       51
6336  deg
RA of node:       319
2602  deg
Eccentricity:     
0009893     
Arg of perigee:   153
1448  deg
Mean anomaly:     207
0230  deg
Mean motion:   15
77646387  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             419
Checksum:              283


Coasting Arc #4 (Orbit 434)
---------------------------------------

Vector Time (GMT): 2007/127/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3798528
32                 A    =         6710194
54  meter
 Y    =        1988886
00  meter          E    =           
0013257
 Z    =        5157242
35                 I    =           51
38164
 XDOT =      -4635
057651                 Wp   =          147
67199
 YDOT =       6070
704785  meter/sec      RA   =          313
72982  deg
 ZDOT =       1060
445868                 TA   =          292
12017
                                          MA   =          292
26085
                                          Ha   =            187
360  n
mi
                                          Hp   =            176
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12462363
26                 X    =         3750952
86
 Y    =        6525216
54  feet           Y    =         2031096
67  meter
 Z    =       16920086
45                 Z    =         5175580
41
 XDOT =     -15206
882057                 XDOT =       -4707
748156
 YDOT =      19917
010450  feet/sec       YDOT =        6018
466420  meter/sec
 ZDOT =       3479
153111                 ZDOT =        1037
752722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13927696
02                 X    =         4245161
75
 Y    =       -1248204
34  feet           Y    =         -380452
68  meter
 Z    =       16989395
04                 Z    =         5178367
61
 XDOT =      -2040
630201                 XDOT =        -621
984085
 YDOT =      23978
742342  feet/sec       YDOT =        7308
720666  meter/sec
 ZDOT =       3394
372570                 ZDOT =        1034
604759


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   07127
51800984  
00020000  00000-0  20000-3 0  9034
2 25544  51
6325 314
0258 0010029 156
9563 203
2054 15
77607098  4352


Satellite: ISS
Catalog Number: 25544
Epoch time:      07127
51800984   =   yrday
fracday
Element set:     903
Inclination:       51
6325  deg
RA of node:       314
0258  deg
Eccentricity:     
0010029     
Arg of perigee:   156
9563  deg
Mean anomaly:     203
2054  deg
Mean motion:   15
77607098  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             435
Checksum:              278


Coasting Arc #5 (Orbit 450)
---------------------------------------

Vector Time (GMT): 2007/128/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4366293
09                 A    =         6721703
77  meter
 Y    =       -5101975
78  meter          E    =           
0012858
 Z    =         295888
67                 I    =           51
40125
 XDOT =       3474
932384                 Wp   =           93
75655
 YDOT =       3335
357459  meter/sec      RA   =          308
54139  deg
 ZDOT =       6008
291246                 TA   =          269
47231
                                          MA   =          269
61965
                                          Ha   =            187
245  n
mi
                                          Hp   =            176
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14325108
55                 X    =         4421582
23
 Y    =      -16738765
67  feet           Y    =        -5052840
34  meter
 Z    =         970763
34                 Z    =          317233
97
 XDOT =      11400
696798                 XDOT =        3408
190366
 YDOT =      10942
773814  feet/sec       YDOT =        3373
842298  meter/sec
 ZDOT =      19712
241622                 ZDOT =        6025
010766

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2540775
38                 X    =          774428
34
 Y    =      -21880999
43  feet           Y    =        -6669328
63  meter
 Z    =        1050579
37                 Z    =          320216
59
 XDOT =      13879
993359                 XDOT =        4230
621976
 YDOT =       2593
948454  feet/sec       YDOT =         790
635489  meter/sec
 ZDOT =      19775
615228                 ZDOT =        6027
607521


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   07128
53148039  
00020000  00000-0  20000-3 0  9044
2 25544  51
6316 308
7909 0009982 161
5237 198
6292 15
77672777  4516


Satellite: ISS
Catalog Number: 25544
Epoch time:      07128
53148039   =   yrday
fracday
Element set:     904
Inclination:       51
6316  deg
RA of node:       308
7909  deg
Eccentricity:     
0009982     
Arg of perigee:   161
5237  deg
Mean anomaly:     198
6292  deg
Mean motion:   15
77672777  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             451
Checksum:              322


Coasting Arc #6 (Orbit 465)
---------------------------------------

Vector Time (GMT): 2007/129/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2272906
77                 A    =         6710605
07  meter
 Y    =       -3851077
71  meter          E    =           
0020244
 Z    =       -5020410
57                 I    =           51
34666
 XDOT =       5215
729757                 Wp   =          128
98029
 YDOT =      -5375
395766  meter/sec      RA   =          303
33947  deg
 ZDOT =       1754
233973                 TA   =          158
04148
                                          MA   =          157
95461
                                          Ha   =            187
103  n
mi
                                          Hp   =            176
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7457043
20                 X    =        -2205286
24
 Y    =      -12634769
37  feet           Y    =        -3876116
10  meter
 Z    =      -16471163
27                 Z    =        -5031288
46
 XDOT =      17111
974267                 XDOT =        5266
928800
 YDOT =     -17635
812879  feet/sec       YDOT =       -5316
784439  meter/sec
 ZDOT =       5755
360805                 ZDOT =        1779
695932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13270173
08                 X    =        -4044748
75
 Y    =       -6146605
96  feet           Y    =        -1873485
50  meter
 Z    =      -16512596
76                 Z    =        -5033039
49
 XDOT =       3465
932844                 XDOT =        1056
416331
 YDOT =     -23268
970286  feet/sec       YDOT =       -7092
382143  meter/sec
 ZDOT =       5850
651747                 ZDOT =        1783
278652


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
48158962  
00020000  00000-0  20000-3 0  9056
2 25544  51
6310 303
8831 0010042 164
7242 195
4228 15
77713504  4664


Satellite: ISS
Catalog Number: 25544
Epoch time:      07129
48158962   =   yrday
fracday
Element set:     905
Inclination:       51
6310  deg
RA of node:       303
8831  deg
Eccentricity:     
0010042     
Arg of perigee:   164
7242  deg
Mean anomaly:     195
4228  deg
Mean motion:   15
77713504  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             466
Checksum:              282


Coasting Arc #7 (Orbit 481)
---------------------------------------

Vector Time (GMT): 2007/130/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4616209
91                 A    =         6718282
53  meter
 Y    =        4068130
50  meter          E    =           
0013707
 Z    =       -2684979
89                 I    =           51
35851
 XDOT =      -1785
320599                 Wp   =          153
60072
 YDOT =      -5426
787306  meter/sec      RA   =          298
19312  deg
 ZDOT =      -5175
101710                 TA   =           57
20011
                                          MA   =           57
06815
                                          Ha   =            186
803  n
mi
                                          Hp   =            176
376

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15145045
62                 X    =        -4648314
07
 Y    =       13346884
85  feet           Y    =         4016330
13  meter
 Z    =       -8808989
14                 Z    =        -2707483
20
 XDOT =      -5857
351047                 XDOT =       -1699
365023
 YDOT =     -17804
420295  feet/sec       YDOT =       -5446
270808  meter/sec
 ZDOT =     -16978
680152                 ZDOT =       -5183
566400

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4403983
13                 X    =        -1342334
06
 Y    =       19662767
76  feet           Y    =         5993211
61  meter
 Z    =       -8893285
57                 Z    =        -2710673
44
 XDOT =     -13672
787908                 XDOT =       -4167
465754
 YDOT =     -10723
770600  feet/sec       YDOT =       -3268
605279  meter/sec
 ZDOT =     -17011
215128                 ZDOT =       -5185
018371


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
49501739  
00020000  00000-0  20000-3 0  9064
2 25544  51
6311 298
6493 0009867 168
4139 191
7255 15
77760248  4823


Satellite: ISS
Catalog Number: 25544
Epoch time:      07130
49501739   =   yrday
fracday
Element set:     906
Inclination:       51
6311  deg
RA of node:       298
6493  deg
Eccentricity:     
0009867     
Arg of perigee:   168
4139  deg
Mean anomaly:     191
7255  deg
Mean motion:   15
77760248  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             482
Checksum:              319


Coasting Arc #8 (Orbit 497)
---------------------------------------

Vector Time (GMT): 2007/131/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         918904
16                 A    =         6715346
75  meter
 Y    =        5492385
12  meter          E    =           
0015354
 Z    =        3734893
31                 I    =           51
33558
 XDOT =      -5257
272359                 Wp   =          123
34689
 YDOT =       3752
559901  meter/sec      RA   =          292
95739  deg
 ZDOT =      -4220
802071                 TA   =           11
14339
                                          MA   =           11
10943
                                          Ha   =            186
718  n
mi
                                          Hp   =            176
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3014777
42                 X    =          839275
69
 Y    =       18019636
21  feet           Y    =         5502215
41  meter
 Z    =       12253586
97                 Z    =         3739164
22
 XDOT =     -17248
268894                 XDOT =       -5278
339304
 YDOT =      12311
548233  feet/sec       YDOT =        3693
652554  meter/sec
 ZDOT =     -13847
775824                 ZDOT =       -4246
393010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13170894
39                 X    =         4014488
61
 Y    =       12645669
24  feet           Y    =         3854399
98  meter
 Z    =       12270336
44                 Z    =         3739998
55
 XDOT =      -5424
137004                 XDOT =       -1653
276959
 YDOT =      19192
350385  feet/sec       YDOT =        5849
828397  meter/sec
 ZDOT =     -13943
739583                 ZDOT =       -4250
051825


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
50842282  
00020000  00000-0  20000-3 0  9079
2 25544  51
6305 293
4142 0009944 173
0946 187
0357 15
77769376  4983


Satellite: ISS
Catalog Number: 25544
Epoch time:      07131
50842282   =   yrday
fracday
Element set:     907
Inclination:       51
6305  deg
RA of node:       293
4142  deg
Eccentricity:     
0009944     
Arg of perigee:   173
0946  deg
Mean anomaly:     187
0357  deg
Mean motion:   15
77769376  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             498
Checksum:              314


Coasting Arc #9 (Orbit 513)
---------------------------------------

Vector Time (GMT): 2007/132/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4477272
25                 A    =         6712528
19  meter
 Y    =       -2268981
58  meter          E    =           
0015989
 Z    =        4456372
36                 I    =           51
31636
 XDOT =        397
788262                 Wp   =          146
55560
 YDOT =       7019
317170  meter/sec      RA   =          287
81926  deg
 ZDOT =       3155
713165                 TA   =          271
71250
                                          MA   =          271
89563
                                          Ha   =            186
500  n
mi
                                          Hp   =            176
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14689213
43                 X    =         4480663
12
 Y    =       -7444165
29  feet           Y    =        -2218895
43  meter
 Z    =       14620644
24                 Z    =         4478131
30
 XDOT =       1305
079600                 XDOT =         303
937646
 YDOT =      23029
255808  feet/sec       YDOT =        7023
240593  meter/sec
 ZDOT =      10353
389648                 ZDOT =        3157
417947

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6962641
29                 X    =         2122213
06
 Y    =      -14842992
71  feet           Y    =        -4524144
18  meter
 Z    =       14702347
42                 Z    =         4481275
49
 XDOT =      14037
677572                 XDOT =        4278
684124
 YDOT =      16907
311923  feet/sec       YDOT =        5153
348674  meter/sec
 ZDOT =      10360
660277                 ZDOT =        3157
929252


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
52180511  
00020000  00000-0  20000-3 0  9083
2 25544  51
6301 288
1789 0009922 177
0028 183
1198 15
77831197  5148


Satellite: ISS
Catalog Number: 25544
Epoch time:      07132
52180511   =   yrday
fracday
Element set:     908
Inclination:       51
6301  deg
RA of node:       288
1789  deg
Eccentricity:     
0009922     
Arg of perigee:   177
0028  deg
Mean anomaly:     183
1198  deg
Mean motion:   15
77831197  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             514
Checksum:              293


Coasting Arc #10 (Orbit 528)
---------------------------------------

Vector Time (GMT): 2007/133/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         162049
47                 A    =         6720135
65  meter
 Y    =       -6532542
50  meter          E    =           
0006081
 Z    =       -1582268
32                 I    =           51
33558
 XDOT =       4981
099330                 Wp   =          125
21420
 YDOT =      -1261
834565  meter/sec      RA   =          282
59232  deg
 ZDOT =       5731
789780                 TA   =          217
24415
                                          MA   =          217
28634
                                          Ha   =            186
451  n
mi
                                          Hp   =            176
798

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         531658
36                 X    =          242771
75
 Y    =      -21432226
06  feet           Y    =        -6530278
97  meter
 Z    =       -5191169
02                 Z    =        -1581285
26
 XDOT =      16342
189402                 XDOT =        4966
994722
 YDOT =      -4139
877182  feet/sec       YDOT =       -1206
212219  meter/sec
 ZDOT =      18805
084580                 ZDOT =        5755
954013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13007623
82                 X    =        -3964723
74
 Y    =      -17042738
12  feet           Y    =        -5194626
58  meter
 Z    =       -5188256
96                 Z    =        -1581380
72
 XDOT =       8805
355165                 XDOT =        2683
872254
 YDOT =     -12460
953852  feet/sec       YDOT =       -3798
098734  meter/sec
 ZDOT =      18895
971010                 ZDOT =        5759
491964


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
47183146  
00020000  00000-0  20000-3 0  9096
2 25544  51
6310 283
2708 0009962 179
6691 180
4482 15
77851876  5291


Satellite: ISS
Catalog Number: 25544
Epoch time:      07133
47183146   =   yrday
fracday
Element set:     909
Inclination:       51
6310  deg
RA of node:       283
2708  deg
Eccentricity:     
0009962     
Arg of perigee:   179
6691  deg
Mean anomaly:     180
4482  deg
Mean motion:   15
77851876  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             529
Checksum:              319


Coasting Arc #11 (Orbit 544)
---------------------------------------

Vector Time (GMT): 2007/134/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4207516
07                 A    =         6709047
96  meter
 Y    =        -174402
29  meter          E    =           
0017158
 Z    =       -5234836
39                 I    =           51
29402
 XDOT =        724
713314                 Wp   =          122
30968
 YDOT =      -7655
568620  meter/sec      RA   =          277
42201  deg
 ZDOT =       -337
289799                 TA   =          144
52843
                                          MA   =          144
41421
                                          Ha   =            186
193  n
mi
                                          Hp   =            176
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13804186
58                 X    =        -4179822
76
 Y    =        -572185
99  feet           Y    =         -221297
94  meter
 Z    =      -17174660
06                 Z    =        -5255209
66
 XDOT =       2377
668352                 XDOT =         811
903658
 YDOT =     -25116
694946  feet/sec       YDOT =       -7646
976943  meter/sec
 ZDOT =      -1106
593830                 ZDOT =        -333
557732

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10892651
19                 X    =        -3320080
08
 Y    =        8342057
22  feet           Y    =         2542659
04  meter
 Z    =      -17251438
88                 Z    =        -5258238
57
 XDOT =     -13650
826018                 XDOT =       -4160
771770
 YDOT =     -20019
333608  feet/sec       YDOT =       -6101
892884  meter/sec
 ZDOT =      -1093
459889                 ZDOT =        -333
286574


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
48517016  
00020000  00000-0  20000-3 0  9107
2 25544  51
6314 278
0363 0009872 183
0779 177
0327 15
77899369  5457


Satellite: ISS
Catalog Number: 25544
Epoch time:      07134
48517016   =   yrday
fracday
Element set:     910
Inclination:       51
6314  deg
RA of node:       278
0363  deg
Eccentricity:     
0009872     
Arg of perigee:   183
0779  deg
Mean anomaly:     177
0327  deg
Mean motion:   15
77899369  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             545
Checksum:              316


Coasting Arc #12 (Orbit 560)
---------------------------------------

Vector Time (GMT): 2007/135/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 464586
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1067782
78                 A    =         6720532
45  meter
 Y    =        6546198
86  meter          E    =           
0017947
 Z    =       -1013737
51                 I    =           51
33057
 XDOT =      -4667
711962                 Wp   =          164
64529
 YDOT =      -1670
219856  meter/sec      RA   =          272
23858  deg
 ZDOT =      -5909
703200                 TA   =           26
51232
                                          MA   =           26
42063
                                          Ha   =            185
914  n
mi
                                          Hp   =            177
158

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3503224
34                 X    =        -1135979
30
 Y    =       21477030
40  feet           Y    =         6533877
10  meter
 Z    =       -3325910
46                 Z    =        -1019089
98
 XDOT =     -15314
015622                 XDOT =       -4619
979459
 YDOT =      -5479
723937  feet/sec       YDOT =       -1722
149410  meter/sec
 ZDOT =     -19388
790026                 ZDOT =       -5932
263686

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11402762
68                 X    =         3475562
07
 Y    =       18530600
35  feet           Y    =         5648126
99  meter
 Z    =       -3345287
67                 Z    =        -1019643
68
 XDOT =     -13737
552001                 XDOT =       -4187
205850
 YDOT =       4961
822677  feet/sec       YDOT =        1512
363552  meter/sec
 ZDOT =     -19473
992366                 ZDOT =       -5935
672873


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
49848534  
00020000  00000-0  20000-3 0  9112
2 25544  51
6312 272
7999 0009679 187
8049 172
2967 15
77942780  5619


Satellite: ISS
Catalog Number: 25544
Epoch time:      07135
49848534   =   yrday
fracday
Element set:     911
Inclination:       51
6312  deg
RA of node:       272
7999  deg
Eccentricity:     
0009679     
Arg of perigee:   187
8049  deg
Mean anomaly:     172
2967  deg
Mean motion:   15
77942780  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             561
Checksum:              343

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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