Date: June 27th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4305 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 1198)
---------------------------------------

Vector Time (GMT): 2007/175/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4758912
20                 A    =         6712522
71  meter
 Y    =       -2275777
43  meter          E    =           
0013690
 Z    =        4149951
58                 I    =           51
91603
 XDOT =        -62
200323                 Wp   =           42
54665
 YDOT =      -6734
134167  meter/sec      RA   =           63
61904  deg
 ZDOT =      -3747
222355                 TA   =           85
68263
                                          MA   =           85
52621
                                          Ha   =            184
824  n
mi
                                          Hp   =            176
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15613228
99                 X    =        -4753270
24
 Y    =       -7466461
38  feet           Y    =        -2328963
35  meter
 Z    =       13615326
72                 Z    =         4126846
02
 XDOT =       -204
069302                 XDOT =          31
309792
 YDOT =     -22093
616035  feet/sec       YDOT =       -6734
306305  meter/sec
 ZDOT =     -12294
036597                 ZDOT =       -3747
298431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16769002
71                 X    =         5111192
03
 Y    =       -4549658
75  feet           Y    =        -1386735
99  meter
 Z    =       13527721
18                 Z    =         4123249
42
 XDOT =      14157
480324                 XDOT =        4315
200003
 YDOT =      15456
695476  feet/sec       YDOT =        4711
200781  meter/sec
 ZDOT =     -12295
060433                 ZDOT =       -3747
534420


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   07175
89841288  
00020000  00000-0  20000-3 0  9007
2 25544  51
6335  64
0573 0007460 353
9129   6
1945 15
78306467 11991


Satellite: ISS
Catalog Number: 25544
Epoch time:      07175
89841288   =   yrday
fracday
Element set:     900
Inclination:       51
6335  deg
RA of node:        64
0573  deg
Eccentricity:     
0007460     
Arg of perigee:   353
9129  deg
Mean anomaly:       6
1945  deg
Mean motion:   15
78306467  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1199
Checksum:              310


Coasting Arc #2 (Orbit 1214)
---------------------------------------

Vector Time (GMT): 2007/176/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -792326
57                 A    =         6711761
75  meter
 Y    =        5111676
60  meter          E    =           
0010021
 Z    =        4266337
79                 I    =           51
90136
 XDOT =      -5645
480493                 Wp   =           63
11441
 YDOT =      -3857
440755  meter/sec      RA   =           58
51948  deg
 ZDOT =       3571
372579                 TA   =          350
83914
                                          MA   =          350
85740
                                          Ha   =            184
804  n
mi
                                          Hp   =            176
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2599496
63                 X    =         -870152
43
 Y    =       16770592
51  feet           Y    =         5102380
47  meter
 Z    =       13997171
24                 Z    =         4262300
49
 XDOT =     -18521
917627                 XDOT =       -5619
275630
 YDOT =     -12655
645523  feet/sec       YDOT =       -3920
425788  meter/sec
 ZDOT =      11717
101637                 ZDOT =        3544
009637

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9135758
25                 X    =        -2784579
12
 Y    =      -14316414
87  feet           Y    =        -4363643
25  meter
 Z    =       13982458
47                 Z    =         4261853
34
 XDOT =      21257
176866                 XDOT =        6479
187509
 YDOT =      -2216
350759  feet/sec       YDOT =        -675
543711  meter/sec
 ZDOT =      11613
229454                 ZDOT =        3539
712338


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   07176
91144561  
00020000  00000-0  20000-3 0  9012
2 25544  51
6345  58
8205 0007538 356
7427   3
3688 15
78388488 12158


Satellite: ISS
Catalog Number: 25544
Epoch time:      07176
91144561   =   yrday
fracday
Element set:     901
Inclination:       51
6345  deg
RA of node:        58
8205  deg
Eccentricity:     
0007538     
Arg of perigee:   356
7427  deg
Mean anomaly:       3
3688  deg
Mean motion:   15
78388488  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1215
Checksum:              312


Coasting Arc #3 (Orbit 1229)
---------------------------------------

Vector Time (GMT): 2007/177/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4908961
12                 A    =         6718404
68  meter
 Y    =        4195534
81  meter          E    =           
0014360
 Z    =       -1826299
40                 I    =           51
90738
 XDOT =      -1992
887529                 Wp   =           18
47621
 YDOT =       4800
300413  meter/sec      RA   =           53
32814  deg
 ZDOT =       5696
348887                 TA   =          321
29386
                                          MA   =          321
39668
                                          Ha   =            185
050  n
mi
                                          Hp   =            176
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16105515
48                 X    =         4870553
07
 Y    =       13764877
98  feet           Y    =         4250215
17  meter
 Z    =       -5991795
92                 Z    =        -1802544
00
 XDOT =      -6538
344910                 XDOT =       -2074
089071
 YDOT =      15749
017102  feet/sec       YDOT =        4777
559704  meter/sec
 ZDOT =      18688
808684                 ZDOT =        5686
471067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21196836
34                 X    =        -6460795
72
 Y    =         791956
76  feet           Y    =          241388
42  meter
 Z    =       -5901529
18                 Z    =        -1798786
10
 XDOT =      -5712
797081                 XDOT =       -1741
260550
 YDOT =     -14543
360439  feet/sec       YDOT =       -4432
816262  meter/sec
 ZDOT =      18651
971838                 ZDOT =        5685
121016


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   07177
86115374  
00020000  00000-0  20000-3 0  9028
2 25544  51
6348  53
9119 0007775    
3322 359
7847 15
78350967 12303


Satellite: ISS
Catalog Number: 25544
Epoch time:      07177
86115374   =   yrday
fracday
Element set:     902
Inclination:       51
6348  deg
RA of node:        53
9119  deg
Eccentricity:     
0007775     
Arg of perigee:      
3322  deg
Mean anomaly:     359
7847  deg
Mean motion:   15
78350967  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1230
Checksum:              303


Coasting Arc #4 (Orbit 1245)
---------------------------------------

Vector Time (GMT): 2007/178/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2759185
03                 A    =         6707655
15  meter
 Y    =       -3123411
15  meter          E    =           
0017685
 Z    =       -5269552
22                 I    =           51
85339
 XDOT =       5372
199260                 Wp   =           60
86717
 YDOT =       5493
977079  meter/sec      RA   =           48
19732  deg
 ZDOT =       -436
168205                 TA   =          204
95759
                                          MA   =          205
04320
                                          Ha   =            185
004  n
mi
                                          Hp   =            176
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9052444
34                 X    =         2819505
03
 Y    =      -10247411
92  feet           Y    =        -3092218
02  meter
 Z    =      -17288557
14                 Z    =        -5256002
18
 XDOT =      17625
325655                 XDOT =        5312
484363
 YDOT =      18024
859182  feet/sec       YDOT =        5553
718235  meter/sec
 ZDOT =      -1430
998048                 ZDOT =        -410
213839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         438030
81                 X    =          133511
79
 Y    =       13730329
46  feet           Y    =         4185004
42  meter
 Z    =      -17237650
34                 Z    =        -5254035
82
 XDOT =     -24198
218555                 XDOT =       -7375
617016
 YDOT =       -930
917533  feet/sec       YDOT =        -283
743664  meter/sec
 ZDOT =      -1332
280410                 ZDOT =        -406
079069


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   07178
87416032  
00020000  00000-0  20000-3 0  9036
2 25544  51
6349  48
6757 0007718   3
8561 356
2663 15
78397728 12464


Satellite: ISS
Catalog Number: 25544
Epoch time:      07178
87416032   =   yrday
fracday
Element set:     903
Inclination:       51
6349  deg
RA of node:        48
6757  deg
Eccentricity:     
0007718     
Arg of perigee:     3
8561  deg
Mean anomaly:     356
2663  deg
Mean motion:   15
78397728  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1246
Checksum:              322


Coasting Arc #5 (Orbit 1261)
---------------------------------------

Vector Time (GMT): 2007/179/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4208168
37                 A    =         6719061
54  meter
 Y    =       -5120971
27  meter          E    =           
0006865
 Z    =       -1107667
35                 I    =           51
87148
 XDOT =       4349
757251                 Wp   =           88
84552
 YDOT =      -2299
773952  meter/sec      RA   =           43
05114  deg
 ZDOT =      -5924
178958                 TA   =          103
24977
                                          MA   =          103
17319
                                          Ha   =            185
055  n
mi
                                          Hp   =            176
082

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13806326
67                 X    =        -4145211
31
 Y    =      -16801086
84  feet           Y    =        -5167677
11  meter
 Z    =       -3634079
22                 Z    =        -1127958
86
 XDOT =      14270
857123                 XDOT =        4403
928966
 YDOT =      -7545
190132  feet/sec       YDOT =       -2250
828305  meter/sec
 ZDOT =     -19436
282672                 ZDOT =       -5902
916763

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21611636
80                 X    =         6587226
90
 Y    =        2293639
35  feet           Y    =          699101
27  meter
 Z    =       -3711344
78                 Z    =        -1131217
89
 XDOT =      -4780
981474                 XDOT =       -1457
243153
 YDOT =      13890
531339  feet/sec       YDOT =        4233
833952  meter/sec
 ZDOT =     -19356
120346                 ZDOT =       -5899
745481


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   07179
88715276  
00020000  00000-0  20000-3 0  9041
2 25544  51
6344  43
4389 0007682   8
1365 351
9924 15
78420879 12627


Satellite: ISS
Catalog Number: 25544
Epoch time:      07179
88715276   =   yrday
fracday
Element set:     904
Inclination:       51
6344  deg
RA of node:        43
4389  deg
Eccentricity:     
0007682     
Arg of perigee:     8
1365  deg
Mean anomaly:     351
9924  deg
Mean motion:   15
78420879  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1262
Checksum:              320


Coasting Arc #6 (Orbit 1277)
---------------------------------------

Vector Time (GMT): 2007/180/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4754132
91                 A    =         6710180
99  meter
 Y    =         927009
46  meter          E    =           
0014434
 Z    =        4641469
76                 I    =           51
82011
 XDOT =      -3976
348362                 Wp   =           38
07392
 YDOT =      -5948
932602  meter/sec      RA   =           37
86322  deg
 ZDOT =      -2868
879545                 TA   =           80
26364
                                          MA   =           80
10065
                                          Ha   =            185
226  n
mi
                                          Hp   =            175
843

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15597548
92                 X    =        -4786692
84
 Y    =        3041369
63  feet           Y    =          873662
96  meter
 Z    =       15227919
17                 Z    =         4618295
41
 XDOT =     -13045
762343                 XDOT =       -3895
594565
 YDOT =     -19517
495413  feet/sec       YDOT =       -5992
946183  meter/sec
 ZDOT =      -9412
334465                 ZDOT =       -2888
001779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8809413
54                 X    =         2685109
25
 Y    =      -13326148
01  feet           Y    =        -4061809
91  meter
 Z    =       15140376
36                 Z    =         4614786
71
 XDOT =      22060
336040                 XDOT =        6723
990425
 YDOT =       3747
249197  feet/sec       YDOT =        1142
161555  meter/sec
 ZDOT =      -9485
265887                 ZDOT =       -2891
109042


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   07180
90012997  
00020000  00000-0  20000-3 0  9057
2 25544  51
6348  38
2016 0007864  11
7395 348
3952 15
78466537 12784


Satellite: ISS
Catalog Number: 25544
Epoch time:      07180
90012997   =   yrday
fracday
Element set:     905
Inclination:       51
6348  deg
RA of node:        38
2016  deg
Eccentricity:     
0007864     
Arg of perigee:    11
7395  deg
Mean anomaly:     348
3952  deg
Mean motion:   15
78466537  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1278
Checksum:              313


Coasting Arc #7 (Orbit 1293)
---------------------------------------

Vector Time (GMT): 2007/181/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2456753
00                 A    =         6713441
18  meter
 Y    =        5030466
53  meter          E    =           
0015100
 Z    =        3688068
79                 I    =           51
80757
 XDOT =      -6387
395054                 Wp   =           65
18661
 YDOT =        -59
746443  meter/sec      RA   =           32
75410  deg
 ZDOT =       4328
865304                 TA   =          339
23793
                                          MA   =          339
29920
                                          Ha   =            185
150  n
mi
                                          Hp   =            175
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8060213
25                 X    =         2382403
20
 Y    =       16504155
29  feet           Y    =         5057522
78  meter
 Z    =       12099963
21                 Z    =         3699824
12
 XDOT =     -20956
020519                 XDOT =       -6407
280874
 YDOT =       -196
018515  feet/sec       YDOT =        -131
286044  meter/sec
 ZDOT =      14202
313991                 ZDOT =        4297
787316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17477429
95                 X    =        -5327120
65
 Y    =       -5550055
81  feet           Y    =        -1691657
01  meter
 Z    =       12144941
83                 Z    =         3701778
27
 XDOT =      14205
757056                 XDOT =        4329
914751
 YDOT =     -13859
996880  feet/sec       YDOT =       -4224
527049  meter/sec
 ZDOT =      14084
771464                 ZDOT =        4293
038342


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   07181
91309277  
00020000  00000-0  20000-3 0  9060
2 25544  51
6345  32
9644 0007786  15
3477 344
7923 15
78486039 12948


Satellite: ISS
Catalog Number: 25544
Epoch time:      07181
91309277   =   yrday
fracday
Element set:     906
Inclination:       51
6345  deg
RA of node:        32
9644  deg
Eccentricity:     
0007786     
Arg of perigee:    15
3477  deg
Mean anomaly:     344
7923  deg
Mean motion:   15
78486039  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1294
Checksum:              320


Coasting Arc #8 (Orbit 1308)
---------------------------------------

Vector Time (GMT): 2007/182/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6129001
77                 A    =         6716641
43  meter
 Y    =         903255
42  meter          E    =           
0012599
 Z    =       -2583724
32                 I    =           51
79250
 XDOT =       1417
924124                 Wp   =           30
56364
 YDOT =       5430
553195  meter/sec      RA   =           27
54775  deg
 ZDOT =       5283
844212                 TA   =          300
10510
                                          MA   =          300
22994
                                          Ha   =            185
383  n
mi
                                          Hp   =            175
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20108273
51                 X    =         6130997
00
 Y    =        2963436
40  feet           Y    =          971805
06  meter
 Z    =       -8476785
82                 Z    =        -2553945
00
 XDOT =       4651
982034                 XDOT =        1331
425903
 YDOT =      17816
775573  feet/sec       YDOT =        5445
924465  meter/sec
 ZDOT =      17335
446889                 ZDOT =        5290
523439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15795218
22                 X    =        -4814382
51
 Y    =       12866005
11  feet           Y    =         3921558
36  meter
 Z    =       -8364060
64                 Z    =        -2549365
68
 XDOT =     -15279
245200                 XDOT =       -4657
113937
 YDOT =      -7518
646586  feet/sec       YDOT =       -2291
683479  meter/sec
 ZDOT =      17361
271629                 ZDOT =        5291
715592


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   07182
86273339  
00020000  00000-0  20000-3 0  9075
2 25544  51
6340  28
0551 0007939  17
9909 342
1536 15
78468281 13092


Satellite: ISS
Catalog Number: 25544
Epoch time:      07182
86273339   =   yrday
fracday
Element set:     907
Inclination:       51
6340  deg
RA of node:        28
0551  deg
Eccentricity:     
0007939     
Arg of perigee:    17
9909  deg
Mean anomaly:     342
1536  deg
Mean motion:   15
78468281  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1309
Checksum:              309


Coasting Arc #9 (Orbit 1324)
---------------------------------------

Vector Time (GMT): 2007/183/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         170043
02                 A    =         6707907
96  meter
 Y    =       -4319864
56  meter          E    =           
0019580
 Z    =       -5145281
84                 I    =           51
73639
 XDOT =       7338
444259                 Wp   =           59
54179
 YDOT =       1887
556214  meter/sec      RA   =           22
41985  deg
 ZDOT =      -1336
251085                 TA   =          197
64539
                                          MA   =          197
71349
                                          Ha   =            185
361  n
mi
                                          Hp   =            175
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         557883
91                 X    =          243330
16
 Y    =      -14172783
99  feet           Y    =        -4317552
30  meter
 Z    =      -16880845
93                 Z    =        -5144278
59
 XDOT =      24076
260691                 XDOT =        7323
283079
 YDOT =       6192
769730  feet/sec       YDOT =        1969
534299  meter/sec
 ZDOT =      -4384
025870                 ZDOT =       -1300
637979

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10184951
99                 X    =         3104373
37
 Y    =        9877181
49  feet           Y    =         3010564
92  meter
 Z    =      -16877500
96                 Z    =        -5144262
29
 XDOT =     -19883
771212                 XDOT =       -6060
573465
 YDOT =      13209
197991  feet/sec       YDOT =        4026
163548  meter/sec
 ZDOT =      -4249
127014                 ZDOT =       -1295
133914


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   07183
87566896  
00020000  00000-0  20000-3 0  9081
2 25544  51
6333  22
8174 0007931  21
9481 338
2023 15
78487213 13250


Satellite: ISS
Catalog Number: 25544
Epoch time:      07183
87566896   =   yrday
fracday
Element set:     908
Inclination:       51
6333  deg
RA of node:        22
8174  deg
Eccentricity:     
0007931     
Arg of perigee:    21
9481  deg
Mean anomaly:     338
2023  deg
Mean motion:   15
78487213  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1325
Checksum:              303


Coasting Arc #10 (Orbit 1340)
---------------------------------------

Vector Time (GMT): 2007/184/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6318163
60                 A    =         6719213
76  meter
 Y    =       -2257579
76  meter          E    =           
0011322
 Z    =        -358358
75                 I    =           51
74806
 XDOT =       1902
202796                 Wp   =           95
82237
 YDOT =      -4391
531188  meter/sec      RA   =           17
24922  deg
 ZDOT =      -6035
168754                 TA   =           88
07203
                                          MA   =           87
94237
                                          Ha   =            185
438  n
mi
                                          Hp   =            175
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20728883
20                 X    =        -6290708
62
 Y    =       -7406757
73  feet           Y    =        -2328079
44  meter
 Z    =       -1175717
67                 Z    =         -388985
55
 XDOT =       6240
822820                 XDOT =        1980
485421
 YDOT =     -14407
910722  feet/sec       YDOT =       -4369
821012  meter/sec
 ZDOT =     -19800
422421                 ZDOT =       -6025
738573

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19089970
31                 X    =         5818622
95
 Y    =      -10946837
84  feet           Y    =        -3336596
17  meter
 Z    =       -1291799
42                 Z    =         -393740
46
 XDOT =       6032
539743                 XDOT =        1838
718114
 YDOT =      12794
870460  feet/sec       YDOT =        3899
876516  meter/sec
 ZDOT =     -19765
213078                 ZDOT =       -6024
436946


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   07184
88858991  
00020000  00000-0  20000-3 0  9094
2 25544  51
6335  17
5795 0008133  26
4596 333
6983 15
78541016 13418


Satellite: ISS
Catalog Number: 25544
Epoch time:      07184
88858991   =   yrday
fracday
Element set:     909
Inclination:       51
6335  deg
RA of node:        17
5795  deg
Eccentricity:     
0008133     
Arg of perigee:    26
4596  deg
Mean anomaly:     333
6983  deg
Mean motion:   15
78541016  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1341
Checksum:              324


Coasting Arc #11 (Orbit 1356)
---------------------------------------

Vector Time (GMT): 2007/185/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3110062
31                 A    =         6708584
32  meter
 Y    =        3317287
55  meter          E    =           
0013966
 Z    =        4927986
92                 I    =           51
68488
 XDOT =      -6718
858739                 Wp   =           40
51136
 YDOT =      -3141
992410  meter/sec      RA   =           12
06304  deg
 ZDOT =      -2111
481459                 TA   =           69
98723
                                          MA   =           69
83691
                                          Ha   =            185
477  n
mi
                                          Hp   =            174
930

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10203616
52                 X    =        -3170864
47
 Y    =       10883489
32  feet           Y    =         3282168
45  meter
 Z    =       16167936
10                 Z    =         4912731
23
 XDOT =     -22043
499801                 XDOT =       -6672
968120
 YDOT =     -10308
374048  feet/sec       YDOT =       -3216
869589  meter/sec
 ZDOT =      -6927
432607                 ZDOT =       -2144
010151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1846424
27                 X    =         -562790
12
 Y    =      -14866276
47  feet           Y    =        -4531241
07  meter
 Z    =       16110581
28                 Z    =         4910505
17
 XDOT =      20869
206211                 XDOT =        6360
934053
 YDOT =     -10282
063883  feet/sec       YDOT =       -3133
973072  meter/sec
 ZDOT =      -7050
803540                 ZDOT =       -2149
084919


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   07185
90149462  
00020000  00000-0  20000-3 0  9106
2 25544  51
6339  12
3416 0008086  28
7206 331
4403 15
78590359 13579


Satellite: ISS
Catalog Number: 25544
Epoch time:      07185
90149462   =   yrday
fracday
Element set:     910
Inclination:       51
6339  deg
RA of node:        12
3416  deg
Eccentricity:     
0008086     
Arg of perigee:    28
7206  deg
Mean anomaly:     331
4403  deg
Mean motion:   15
78590359  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1357
Checksum:              287


Coasting Arc #12 (Orbit 1372)
---------------------------------------

Vector Time (GMT): 2007/186/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5015146
33                 A    =         6714736
80  meter
 Y    =        3128208
26  meter          E    =           
0019101
 Z    =        3162278
99                 I    =           51
67686
 XDOT =      -5073
826236                 Wp   =           66
16911
 YDOT =       3231
919399  meter/sec      RA   =            6
93804  deg
 ZDOT =       4834
400861                 TA   =          330
79372
                                          MA   =          330
90039
                                          Ha   =            185
515  n
mi
                                          Hp   =            174
702

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16453892
16                 X    =         4964431
90
 Y    =       10263150
45  feet           Y    =         3184006
51  meter
 Z    =       10374931
08                 Z    =         3186519
50
 XDOT =     -16646
411537                 XDOT =       -5133
073329
 YDOT =      10603
410102  feet/sec       YDOT =        3174
849189  meter/sec
 ZDOT =      15860
895212                 ZDOT =        4809
608944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18241678
44                 X    =        -5560063
59
 Y    =        6433205
03  feet           Y    =         1960840
89  meter
 Z    =       10466950
85                 Z    =         3190326
62
 XDOT =       2598
478700                 XDOT =         792
016308
 YDOT =     -18366
400674  feet/sec       YDOT =       -5598
078925  meter/sec
 ZDOT =      15767
463141                 ZDOT =        4805
922765


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   07186
91438790  
00020000  00000-0  20000-3 0  9114
2 25544  51
6336   7
1038 0008268  33
9891 326
1802 15
78575491 13730


Satellite: ISS
Catalog Number: 25544
Epoch time:      07186
91438790   =   yrday
fracday
Element set:     911
Inclination:       51
6336  deg
RA of node:         7
1038  deg
Eccentricity:     
0008268     
Arg of perigee:    33
9891  deg
Mean anomaly:     326
1802  deg
Mean motion:   15
78575491  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1373
Checksum:              306

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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