Date:
June 15th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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 2257)
---------------------------------------
Vector Time (GMT): 2010/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3270918
05 A = 6728419
62 meter
Y = 3379782
85 meter E =
0010054
Z = -4818428
59 I = 51
30278
XDOT = -3237
245844 Wp = 24
31598
YDOT = -6553
706113 meter/sec RA = 258
91075 deg
ZDOT = -2392
142059 TA = 222
15982
MA = 222
23719
Ha = 193
465 n
mi
Hp = 189
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10731358
44 X = -3285061
00
Y = 11088526
40 feet Y = 3343127
37 meter
Z = -15808492
76 Z = -4834352
57
XDOT = -10620
885314 XDOT = -3152
099803
YDOT = -21501
660476 feet/sec YDOT = -6589
430373 meter/sec
ZDOT = -7848
235102 ZDOT = -2407
663243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8842477
79 X = 2695187
23
Y = 12566556
36 feet Y = 3830286
38 meter
Z = -15871930
03 Z = -4837764
27
XDOT = -22214
178382 XDOT = -6770
881571
YDOT = 5610
396627 feet/sec YDOT = 1710
048892 meter/sec
ZDOT = -7910
101568 ZDOT = -2410
998958
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 10162
52005891
00016717 00000-0 10270-3 0 9007
2 25544 51
6491 259
6137 0009202 307
4153 52
6171 15
71760772 22589
Satellite: ISS
Catalog Number: 25544
Epoch time: 10162
52005891 = yrday
fracday
Element set: 900
Inclination: 51
6491 deg
RA of node: 259
6137 deg
Eccentricity:
0009202
Arg of perigee: 307
4153 deg
Mean anomaly: 52
6171 deg
Mean motion: 15
71760772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 290
Coasting Arc #2 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2010/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3703471
40 A = 6735232
70 meter
Y = 4925001
84 meter E =
0007526
Z = 2718191
63 I = 51
33245
XDOT = -2832
508352 Wp = 61
72822
YDOT = 4974
566329 meter/sec RA = 253
72811 deg
ZDOT = -5139
699259 TA = 87
14674
MA = 87
06060
Ha = 193
663 n
mi
Hp = 188
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12150496
73 X = 3634919
34
Y = 16158142
53 feet Y = 4966032
40 meter
Z = 8917951
53 Z = 2736017
70
XDOT = -9293
006403 XDOT = -2862
956480
YDOT = 16320
755673 feet/sec YDOT = 4942
722367 meter/sec
ZDOT = -16862
530376 ZDOT = -5153
532574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18024672
55 X = 5493920
19
Y = -9086194
59 feet Y = -2769472
11 meter
Z = 8989007
02 Z = 2739849
34
XDOT = 13798
921179 XDOT = 4205
911175
YDOT = 10590
689927 feet/sec YDOT = 3228
042290 meter/sec
ZDOT = -16917
635276 ZDOT = -5156
495232
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 10163
53732610
00016717 00000-0 10270-3 0 9016
2 25544 51
6485 254
4083 0009100 312
4168 47
6223 15
71785852 22740
Satellite: ISS
Catalog Number: 25544
Epoch time: 10163
53732610 = yrday
fracday
Element set: 901
Inclination: 51
6485 deg
RA of node: 254
4083 deg
Eccentricity:
0009100
Arg of perigee: 312
4168 deg
Mean anomaly: 47
6223 deg
Mean motion: 15
71785852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2274
Checksum: 290
Coasting Arc #3 (Orbit 2289)
---------------------------------------
Vector Time (GMT): 2010/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1514031
17 A = 6731042
87 meter
Y = -5120257
26 meter E =
0005571
Z = 4092389
52 I = 51
32827
XDOT = 4994
156463 Wp = 43
08640
YDOT = 4487
876687 meter/sec RA = 248
63537 deg
ZDOT = 3768
418628 TA = 8
09761
MA = 8
08862
Ha = 193
719 n
mi
Hp = 188
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4967293
86 X = 1551294
22
Y = -16798744
30 feet Y = -5103118
97 meter
Z = 13426474
79 Z = 4099834
12
XDOT = 16385
027765 XDOT = 4925
294758
YDOT = 14724
004877 feet/sec YDOT = 4543
338505 meter/sec
ZDOT = 12363
578176 ZDOT = 3792
513897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15815955
23 X = -4820703
16
Y = -7478666
83 feet Y = -2279497
65 meter
Z = 13456119
28 Z = 4101425
16
XDOT = 16569
621545 XDOT = 5050
420647
YDOT = -12629
235756 feet/sec YDOT = -3849
391058 meter/sec
ZDOT = 12459
630306 ZDOT = 3797
695317
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 10164
55457834
00016717 00000-0 10270-3 0 9022
2 25544 51
6485 249
2015 0009221 316
1011 43
9417 15
71834289 22900
Satellite: ISS
Catalog Number: 25544
Epoch time: 10164
55457834 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 249
2015 deg
Eccentricity:
0009221
Arg of perigee: 316
1011 deg
Mean anomaly: 43
9417 deg
Mean motion: 15
71834289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2290
Checksum: 296
Coasting Arc #4 (Orbit 2304)
---------------------------------------
Vector Time (GMT): 2010/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4798494
34 A = 6731887
98 meter
Y = -2779952
46 meter E =
0005419
Z = -3812180
26 I = 51
34259
XDOT = 466
300398 Wp = 2
98812
YDOT = -6473
234969 meter/sec RA = 243
44498 deg
ZDOT = 4139
122729 TA = 310
50706
MA = 310
55427
Ha = 193
843 n
mi
Hp = 188
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15743091
66 X = -4748533
00
Y = -9120578
94 feet Y = -2833331
99 meter
Z = -12507153
09 Z = -3835370
40
XDOT = 1529
856949 XDOT = 518
543641
YDOT = -21237
647535 feet/sec YDOT = -6467
729223 meter/sec
ZDOT = 13579
798981 ZDOT = 4141
513633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11237269
60 X = -3425119
77
Y = 14227877
99 feet Y = 4336657
21 meter
Z = -12599604
50 Z = -3840359
45
XDOT = -19783
722233 XDOT = -6030
078537
YDOT = -3607
356488 feet/sec YDOT = -1099
522258 meter/sec
ZDOT = 13589
288021 ZDOT = 4142
014989
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 10165
50824266
00016717 00000-0 10270-3 0 9036
2 25544 51
6475 244
3218 0009240 320
3421 39
7056 15
71853357 23059
Satellite: ISS
Catalog Number: 25544
Epoch time: 10165
50824266 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 244
3218 deg
Eccentricity:
0009240
Arg of perigee: 320
3421 deg
Mean anomaly: 39
7056 deg
Mean motion: 15
71853357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2305
Checksum: 289
Coasting Arc #5 (Orbit 2320)
---------------------------------------
Vector Time (GMT): 2010/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 753473
10 A = 6734184
59 meter
Y = 5937059
29 meter E =
0006475
Z = -3094261
73 I = 51
36353
XDOT = -5678
935223 Wp = 351
14203
YDOT = -1814
754569 meter/sec RA = 238
35626 deg
ZDOT = -4857
233975 TA = 224
87088
MA = 224
92325
Ha = 194
173 n
mi
Hp = 188
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2472024
60 X = 702059
05
Y = 19478540
96 feet Y = 5945198
14 meter
Z = -10151777
33 Z = -3090725
24
XDOT = -18631
677242 XDOT = -5634
624892
YDOT = -5953
919188 feet/sec YDOT = -1878
011209 meter/sec
ZDOT = -15935
807004 ZDOT = -4884
714682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19641825
29 X = 5986828
35
Y = -100743
75 feet Y = -30706
70 meter
Z = -10137632
70 Z = -3089950
45
XDOT = -8211
169004 XDOT = -2502
764312
YDOT = 16225
042849 feet/sec YDOT = 4945
393060 meter/sec
ZDOT = -16045
369217 ZDOT = -4890
628537
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 10166
52547222
00016717 00000-0 10270-3 0 9044
2 25544 51
6464 239
1153 0009289 324
6487 35
4058 15
71843423 23215
Satellite: ISS
Catalog Number: 25544
Epoch time: 10166
52547222 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 239
1153 deg
Eccentricity:
0009289
Arg of perigee: 324
6487 deg
Mean anomaly: 35
4058 deg
Mean motion: 15
71843423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2321
Checksum: 303
Coasting Arc #6 (Orbit 2336)
---------------------------------------
Vector Time (GMT): 2010/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4888581
35 A = 6728807
69 meter
Y = 378176
02 meter E =
0011912
Z = 4611673
48 I = 51
36355
XDOT = 2204
623013 Wp = 11
42942
YDOT = 6785
116258 meter/sec RA = 233
17079 deg
ZDOT = -2880
628249 TA = 107
27643
MA = 107
14605
Ha = 194
232 n
mi
Hp = 187
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16038652
72 X = 4861586
73
Y = 1240734
99 feet Y = 432691
44 meter
Z = 15130162
34 Z = 4635356
47
XDOT = 7233
015135 XDOT = 2142
580198
YDOT = 22260
880113 feet/sec YDOT = 6809
423194 meter/sec
ZDOT = -9450
880081 ZDOT = -2870
067986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2936349
08 X = 894999
20
Y = -15725441
75 feet Y = -4793114
65 meter
Z = 15224583
83 Z = 4640453
15
XDOT = 21764
623752 XDOT = 6633
857320
YDOT = -5085
361015 feet/sec YDOT = -1550
018037 meter/sec
ZDOT = -9408
714363 ZDOT = -2867
776138
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 10167
54268687
00016717 00000-0 10270-3 0 9053
2 25544 51
6469 233
9082 0009509 328
4179 31
6411 15
71906718 23373
Satellite: ISS
Catalog Number: 25544
Epoch time: 10167
54268687 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 233
9082 deg
Eccentricity:
0009509
Arg of perigee: 328
4179 deg
Mean anomaly: 31
6411 deg
Mean motion: 15
71906718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2337
Checksum: 330
Coasting Arc #7 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2010/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3062068
60 A = 6736710
89 meter
Y = -5678852
64 meter E =
0016551
Z = 1900089
87 I = 51
40799
XDOT = 5195
711056 Wp = 32
29972
YDOT = -920
207227 meter/sec RA = 228
07261 deg
ZDOT = 5614
156409 TA = 348
88930
MA = 348
92581
Ha = 194
543 n
mi
Hp = 187
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10046156
83 X = -3007569
29
Y = -18631406
30 feet Y = -5712790
03 meter
Z = 6233890
66 Z = 1885346
11
XDOT = 17046
296116 XDOT = 5178
342470
YDOT = -3019
052583 feet/sec YDOT = -862
203508 meter/sec
ZDOT = 18419
148323 ZDOT = 5639
354686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19459769
29 X = -5931337
68
Y = 8372703
71 feet Y = 2552000
09 meter
Z = 6175044
29 Z = 1882153
50
XDOT = -878
031888 XDOT = -267
624119
YDOT = -15720
524214 feet/sec YDOT = -4791
615781 meter/sec
ZDOT = 18519
605019 ZDOT = 5644
775610
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 10168
55989263
00016717 00000-0 10270-3 0 9066
2 25544 51
6462 228
7013 0009461 333
9388 26
1296 15
71871070 23532
Satellite: ISS
Catalog Number: 25544
Epoch time: 10168
55989263 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 228
7013 deg
Eccentricity:
0009461
Arg of perigee: 333
9388 deg
Mean anomaly: 26
1296 deg
Mean motion: 15
71871070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 322
Coasting Arc #8 (Orbit 2367)
---------------------------------------
Vector Time (GMT): 2010/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3952374
56 A = 6726768
21 meter
Y = 1896059
60 meter E =
0011827
Z = -5109656
05 I = 51
39575
XDOT = -4689
123170 Wp = 58
65626
YDOT = -5924
885626 meter/sec RA = 222
90704 deg
ZDOT = 1437
018694 TA = 225
12795
MA = 225
22405
Ha = 194
622 n
mi
Hp = 187
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12967108
14 X = -3948461
20
Y = 6220667
99 feet Y = 1851884
25 meter
Z = -16763963
41 Z = -5128846
90
XDOT = -15384
262369 XDOT = -4629
502270
YDOT = -19438
601136 feet/sec YDOT = -5976
989001 meter/sec
ZDOT = 4714
628262 ZDOT = 1414
383160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5271316
50 X = 1606697
27
Y = 13284772
27 feet Y = 4049198
59 meter
Z = -16840460
83 Z = -5132972
46
XDOT = -19535
414573 XDOT = -5954
394362
YDOT = 13578
342162 feet/sec YDOT = 4138
678691 meter/sec
ZDOT = 4624
301961 ZDOT = 1409
487238
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 10169
51350930
00016717 00000-0 10270-3 0 9077
2 25544 51
6460 223
8198 0009557 337
2768 22
7970 15
71890542 23687
Satellite: ISS
Catalog Number: 25544
Epoch time: 10169
51350930 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 223
8198 deg
Eccentricity:
0009557
Arg of perigee: 337
2768 deg
Mean anomaly: 22
7970 deg
Mean motion: 15
71890542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2368
Checksum: 328
Coasting Arc #9 (Orbit 2383)
---------------------------------------
Vector Time (GMT): 2010/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4989450
90 A = 6737873
02 meter
Y = 4487658
18 meter E =
0004257
Z = -613878
60 I = 51
45722
XDOT = -3621
886580 Wp = 79
18685
YDOT = 3214
309604 meter/sec RA = 217
78995 deg
ZDOT = -5974
383229 TA = 107
50163
MA = 107
45510
Ha = 194
796 n
mi
Hp = 186
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16369589
56 X = 4941880
38
Y = 14723287
98 feet Y = 4543187
28 meter
Z = -2014037
40 Z = -589754
86
XDOT = -11882
829986 XDOT = -3628
537880
YDOT = 10545
635183 feet/sec YDOT = 3173
770997 meter/sec
ZDOT = -19600
994845 ZDOT = -5991
994167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15606535
29 X = 4756871
96
Y = -15541980
98 feet Y = -4737195
80 meter
Z = -1917785
51 Z = -584541
02
XDOT = 8744
854489 XDOT = 2665
431648
YDOT = 11193
905914 feet/sec YDOT = 3411
902523 meter/sec
ZDOT = -19671
179637 ZDOT = -5995
775553
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 10170
53068883
00016717 00000-0 10270-3 0 9085
2 25544 51
6467 218
6126 0009586 342
1950 17
8875 15
71945891 23842
Satellite: ISS
Catalog Number: 25544
Epoch time: 10170
53068883 = yrday
fracday
Element set: 908
Inclination: 51
6467 deg
RA of node: 218
6126 deg
Eccentricity:
0009586
Arg of perigee: 342
1950 deg
Mean anomaly: 17
8875 deg
Mean motion: 15
71945891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2384
Checksum: 341
Coasting Arc #10 (Orbit 2399)
---------------------------------------
Vector Time (GMT): 2010/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2218031
34 A = 6725917
59 meter
Y = -3557744
46 meter E =
0009099
Z = 5259202
72 I = 51
44108
XDOT = 6503
924694 Wp =
58062
YDOT = 4118
454367 meter/sec RA = 212
65170 deg
ZDOT = 52
023732 TA = 88
97635
MA = 88
87210
Ha = 194
830 n
mi
Hp = 186
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7277005
70 X = 2232101
45
Y = -11672389
97 feet Y = -3532863
11 meter
Z = 17254602
08 Z = 5270011
69
XDOT = 21338
335609 XDOT = 6457
135278
YDOT = 13511
989393 feet/sec YDOT = 4190
923510 meter/sec
ZDOT = 170
681536 ZDOT = 83
506834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11389883
36 X = -3471636
45
Y = -7614606
72 feet Y = -2320932
13 meter
Z = 17297662
10 Z = 5272327
41
XDOT = 13760
154532 XDOT = 4194
095101
YDOT = -19975
890149 feet/sec YDOT = -6088
651317 meter/sec
ZDOT = 296
284569 ZDOT = 90
307537
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 10171
54785563
00016717 00000-0 10270-3 0 9099
2 25544 51
6461 213
4056 0009568 346
0023 14
0873 15
71959401 24003
Satellite: ISS
Catalog Number: 25544
Epoch time: 10171
54785563 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 213
4056 deg
Eccentricity:
0009568
Arg of perigee: 346
0023 deg
Mean anomaly: 14
0873 deg
Mean motion: 15
71959401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2400
Checksum: 296
Coasting Arc #11 (Orbit 2414)
---------------------------------------
Vector Time (GMT): 2010/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6172309
47 A = 6737778
85 meter
Y = -2577230
27 meter E =
0018389
Z = -711113
95 I = 51
50733
XDOT = 1277
200622 Wp = 16
23013
YDOT = -4692
579693 meter/sec RA = 207
51266 deg
ZDOT = 5975
507423 TA = 336
00711
MA = 336
09268
Ha = 195
054 n
mi
Hp = 186
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20250359
14 X = -6139577
18
Y = -8455479
88 feet Y = -2646069
59 meter
Z = -2333051
02 Z = -741020
13
XDOT = 4190
290753 XDOT = 1300
550829
YDOT = -15395
602667 feet/sec YDOT = -4678
167602 meter/sec
ZDOT = 19604
683147 ZDOT = 5981
768133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8877044
02 X = -2705723
02
Y = 20054908
43 feet Y = 6112736
09 meter
Z = -2452355
97 Z = -747478
10
XDOT = -13843
932971 XDOT = -4219
630770
YDOT = -3748
252463 feet/sec YDOT = -1142
467351 meter/sec
ZDOT = 19629
594201 ZDOT = 5983
100313
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 10172
50143908
00016717 00000-0 10270-3 0 9109
2 25544 51
6464 208
5240 0009732 350
0258 10
0709 15
71949639 24156
Satellite: ISS
Catalog Number: 25544
Epoch time: 10172
50143908 = yrday
fracday
Element set: 910
Inclination: 51
6464 deg
RA of node: 208
5240 deg
Eccentricity:
0009732
Arg of perigee: 350
0258 deg
Mean anomaly: 10
0709 deg
Mean motion: 15
71949639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2415
Checksum: 289
Coasting Arc #12 (Orbit 2430)
---------------------------------------
Vector Time (GMT): 2010/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 47238
78 A = 6726710
93 meter
Y = 4405105
04 meter E =
0017536
Z = -5096972
07 I = 51
49786
XDOT = -7336
134117 Wp = 45
32501
YDOT = -1705
256862 meter/sec RA = 202
40320 deg
ZDOT = -1532
891583 TA = 209
86061
MA = 209
96078
Ha = 195
172 n
mi
Hp = 186
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 154982
88 X = 22736
93
Y = 14452444
34 feet Y = 4405497
16 meter
Z = -16722349
32 Z = -5096801
34
XDOT = -24068
681486 XDOT = -7309
073821
YDOT = -5594
674745 feet/sec YDOT = -1787
142321 meter/sec
ZDOT = -5029
171859 ZDOT = -1568
465349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14452739
99 X = 4405195
15
Y = -200017
74 feet Y = -60965
41 meter
Z = -16721615
76 Z = -5096748
48
XDOT = -5698
790262 XDOT = -1736
991272
YDOT = 22963
668271 feet/sec YDOT = 6999
326089 meter/sec
ZDOT = -5171
084297 ZDOT = -1576
146494
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 10173
51858195
00016717 00000-0 10270-3 0 9113
2 25544 51
6467 203
3169 0009623 353
8259 6
2783 15
71975028 24311
Satellite: ISS
Catalog Number: 25544
Epoch time: 10173
51858195 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 203
3169 deg
Eccentricity:
0009623
Arg of perigee: 353
8259 deg
Mean anomaly: 6
2783 deg
Mean motion: 15
71975028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2431
Checksum: 318
Coasting Arc #13 (Orbit 2446)
---------------------------------------
Vector Time (GMT): 2010/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6438738
70 A = 6736126
50 meter
Y = 386259
24 meter E =
0013554
Z = 1939811
02 I = 51
55701
XDOT = 1392
907664 Wp = 71
13602
YDOT = 5087
114939 meter/sec RA = 197
24431 deg
ZDOT = -5600
217730 TA = 87
29033
MA = 87
13519
Ha = 195
275 n
mi
Hp = 185
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21124470
81 X = 6424517
64
Y = 1267254
74 feet Y = 458181
17 meter
Z = 6364209
38 Z = 1971056
10
XDOT = 4569
907035 XDOT = 1363
124072
YDOT = 16690
009641 feet/sec YDOT = 5102
525804 meter/sec
ZDOT = -18373
417750 ZDOT = -5593
522322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 983049
30 X = 299633
43
Y = -21101675
86 feet Y = -6431790
80 meter
Z = 6488856
02 Z = 1977803
32
XDOT = 15086
050836 XDOT = 4598
228295
YDOT = -4974
653373 feet/sec YDOT = -1516
274348 meter/sec
ZDOT = -18346
650060 ZDOT = -5592
058938
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 10174
53571165
00016717 00000-0 10270-3 0 9126
2 25544 51
6452 198
1093 0009738 358
4718 1
6412 15
72018587 24474
Satellite: ISS
Catalog Number: 25544
Epoch time: 10174
53571165 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 198
1093 deg
Eccentricity:
0009738
Arg of perigee: 358
4718 deg
Mean anomaly: 1
6412 deg
Mean motion: 15
72018587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2447
Checksum: 314
Coasting Arc #14 (Orbit 2462)
---------------------------------------
Vector Time (GMT): 2010/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2372468
24 A = 6728583
21 meter
Y = -4264511
97 meter E =
0010017
Z = 4622730
39 I = 51
55981
XDOT = 7095
199190 Wp = 52
33339
YDOT = -817
297177 meter/sec RA = 192
15775 deg
ZDOT = 2889
186703 TA = 9
07002
MA = 9
05194
Ha = 195
460 n
mi
Hp = 185
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7783688
47 X = -2347061
78
Y = -13991180
99 feet Y = -4290901
21 meter
Z = 15166438
27 Z = 4611265
76
XDOT = 23278
212565 XDOT = 7089
775862
YDOT = -2681
421186 feet/sec YDOT = -737
985344 meter/sec
ZDOT = 9478
959000 ZDOT = 2923
641886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13742539
88 X = -4188726
15
Y = 8298695
68 feet Y = 2529442
44 meter
Z = 15120649
76 Z = 4608774
05
XDOT = -2787
146817 XDOT = -849
522350
YDOT = -22126
490419 feet/sec YDOT = -6744
154280 meter/sec
ZDOT = 9616
417116 ZDOT = 2931
083937
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 10175
55282936
00016717 00000-0 10270-3 0 9135
2 25544 51
6444 192
9014 0009774 2
6350 357
4862 15
72017652 24631
Satellite: ISS
Catalog Number: 25544
Epoch time: 10175
55282936 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 192
9014 deg
Eccentricity:
0009774
Arg of perigee: 2
6350 deg
Mean anomaly: 357
4862 deg
Mean motion: 15
72017652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2463
Checksum: 310
Coasting Arc #15 (Orbit 2477)
---------------------------------------
Vector Time (GMT): 2010/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5725356
62 A = 6733529
15 meter
Y = 1751336
45 meter E =
0012144
Z = -3072890
56 I = 51
60754
XDOT = -3971
722303 Wp = 26
90812
YDOT = -4404
749098 meter/sec RA = 186
98803 deg
ZDOT = 4907
797185 TA = 297
45957
MA = 297
58300
Ha = 195
406 n
mi
Hp = 185
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18783978
42 X = -5729587
37
Y = 5745854
49 feet Y = 1687289
08 meter
Z = -10081661
94 Z = -3100714
17
XDOT = -13030
584984 XDOT = -3946
013517
YDOT = -14451
276567 feet/sec YDOT = -4449
020535 meter/sec
ZDOT = 16101
696800 ZDOT = 4888
564152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6635235
96 X = 2022419
92
Y = 18427581
40 feet Y = 5616726
81 meter
Z = -10192668
15 Z = -3106725
25
XDOT = -12462
108710 XDOT = -3798
450735
YDOT = 13318
349401 feet/sec YDOT = 4059
432897 meter/sec
ZDOT = 16024
901683 ZDOT = 4884
390033
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 10176
50636449
00016717 00000-0 10270-3 0 9144
2 25544 51
6451 188
0202 0009827 5
9584 354
1693 15
72052402 24782
Satellite: ISS
Catalog Number: 25544
Epoch time: 10176
50636449 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 188
0202 deg
Eccentricity:
0009827
Arg of perigee: 5
9584 deg
Mean anomaly: 354
1693 deg
Mean motion: 15
72052402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2478
Checksum: 310
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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