Date:
September 9th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 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
258/09:08:12
999 -0
5 3
8 3
8
N/A 3
2 0
0 195
7
000/00:10:25
998 -2
0 -0
1 188
2
Coasting Arc #1 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2010/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5127956
63 A = 6736320
79 meter
Y = -3588661
68 meter E =
0012479
Z = 2488763
08 I = 51
75244
XDOT = 4682
728203 Wp = 66
74818
YDOT = 2978
516768 meter/sec RA = 163
28151 deg
ZDOT = -5327
751280 TA = 85
18592
MA = 85
04344
Ha = 195
216 n
mi
Hp = 187
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16824004
68 X = 5155614
70
Y = -11773824
41 feet Y = -3531162
91 meter
Z = 8165233
22 Z = 2513742
05
XDOT = 15363
281507 XDOT = 4674
954921
YDOT = 9772
036639 feet/sec YDOT = 3030
837862 meter/sec
ZDOT = -17479
498951 ZDOT = -5305
021923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19038544
86 X = -5802948
47
Y = 7586902
63 feet Y = 2312487
92 meter
Z = 8265217
87 Z = 2519238
41
XDOT = -12242
595210 XDOT = -3731
543020
YDOT = -11687
100414 feet/sec YDOT = -3562
228206 meter/sec
ZDOT = -17388
387864 ZDOT = -5299
980621
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 10251
53686287
00016717 00000-0 10270-3 0 9001
2 25544 51
6461 164
1497 0008616 346
9475 13
1463 15
71581381 36586
Satellite: ISS
Catalog Number: 25544
Epoch time: 10251
53686287 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 164
1497 deg
Eccentricity:
0008616
Arg of perigee: 346
9475 deg
Mean anomaly: 13
1463 deg
Mean motion: 15
71581381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 321
Coasting Arc #2 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2010/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4962802
74 A = 6731261
68 meter
Y = -1614976
80 meter E =
0010049
Z = 4240447
36 I = 51
76433
XDOT = 4688
195216 Wp = 55
96150
YDOT = -4934
031048 meter/sec RA = 158
21899 deg
ZDOT = 3607
147494 TA = 357
43922
MA = 357
44436
Ha = 195
426 n
mi
Hp = 187
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16282161
23 X = -4964974
24
Y = -5298480
30 feet Y = -1670485
56 meter
Z = 13912228
87 Z = 4216332
97
XDOT = 15381
217899 XDOT = 4725
497162
YDOT = -16187
765907 feet/sec YDOT = -4881
395916 meter/sec
ZDOT = 11834
473406 ZDOT = 3630
013815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14852571
24 X = 4527063
71
Y = 8675440
72 feet Y = 2644274
33 meter
Z = 13815593
93 Z = 4210993
03
XDOT = -17785
989514 XDOT = -5421
169604
YDOT = 11455
125069 feet/sec YDOT = 3491
522121 meter/sec
ZDOT = 11925
973673 ZDOT = 3635
036776
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 10252
55424580
00016717 00000-0 10270-3 0 9011
2 25544 51
6462 158
9439 0008650 350
8419 9
2584 15
71616745 36745
Satellite: ISS
Catalog Number: 25544
Epoch time: 10252
55424580 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 158
9439 deg
Eccentricity:
0008650
Arg of perigee: 350
8419 deg
Mean anomaly: 9
2584 deg
Mean motion: 15
71616745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 320
Coasting Arc #3 (Orbit 3688)
---------------------------------------
Vector Time (GMT): 2010/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2905609
10 A = 6732699
09 meter
Y = 4781150
39 meter E =
0008778
Z = -3743424
43 I = 51
79787
XDOT = -6375
409200 Wp = 34
83812
YDOT = -535
433741 meter/sec RA = 153
06133 deg
ZDOT = 4276
623777 TA = 280
11812
MA = 280
21713
Ha = 195
333 n
mi
Hp = 186
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9532838
27 X = -2940671
89
Y = 15686188
93 feet Y = 4748461
76 meter
Z = -12281576
22 Z = -3757625
51
XDOT = -20916
696849 XDOT = -6389
723202
YDOT = -1756
672378 feet/sec YDOT = -606
807064 meter/sec
ZDOT = 14030
917902 ZDOT = 4245
617183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12365158
83 X = 3768900
41
Y = -13514288
78 feet Y = -4119155
22 meter
Z = -12338374
65 Z = -3760736
59
XDOT = 19256
300349 XDOT = 5869
320346
YDOT = 4957
942744 feet/sec YDOT = 1511
180948 meter/sec
ZDOT = 13906
688821 ZDOT = 4238
758753
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 10253
50802137
00016717 00000-0 10270-3 0 9026
2 25544 51
6465 154
0637 0008702 353
9323 6
1732 15
71661968 36895
Satellite: ISS
Catalog Number: 25544
Epoch time: 10253
50802137 = yrday
fracday
Element set: 902
Inclination: 51
6465 deg
RA of node: 154
0637 deg
Eccentricity:
0008702
Arg of perigee: 353
9323 deg
Mean anomaly: 6
1732 deg
Mean motion: 15
71661968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3689
Checksum: 305
Coasting Arc #4 (Orbit 3704)
---------------------------------------
Vector Time (GMT): 2010/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5896502
76 A = 6734493
80 meter
Y = -734808
73 meter E =
0008665
Z = -3181552
35 I = 51
83029
XDOT = -1902
346495 Wp = 27
43381
YDOT = 5667
195918 meter/sec RA = 148
00643 deg
ZDOT = -4832
266211 TA = 189
46457
MA = 189
48091
Ha = 195
415 n
mi
Hp = 186
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19345481
49 X = 5919736
80
Y = -2410789
80 feet Y = -668740
79 meter
Z = -10438163
88 Z = -3152850
45
XDOT = -6241
294274 XDOT = -1942
102287
YDOT = 18593
162459 feet/sec YDOT = 5645
700146 meter/sec
ZDOT = -15853
891770 ZDOT = -4841
604802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19523887
11 X = -5950880
79
Y = -1124512
26 feet Y = -342751
34 meter
Z = -10323184
15 Z = -3146506
53
XDOT = 9314
061669 XDOT = 2838
925997
YDOT = -15757
361118 feet/sec YDOT = -4802
843669 meter/sec
ZDOT = -15891
202919 ZDOT = -4843
638650
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 10254
52536022
00016717 00000-0 10270-3 0 9037
2 25544 51
6464 148
8577 0008685 356
8051 3
3054 15
71682261 37052
Satellite: ISS
Catalog Number: 25544
Epoch time: 10254
52536022 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 148
8577 deg
Eccentricity:
0008685
Arg of perigee: 356
8051 deg
Mean anomaly: 3
3054 deg
Mean motion: 15
71682261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3705
Checksum: 303
Coasting Arc #5 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2010/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 402094
59 A = 6729251
59 meter
Y = -4867582
37 meter E =
0014457
Z = 4628449
45 I = 51
83822
XDOT = 6759
065431 Wp = 31
18836
YDOT = -2237
403605 meter/sec RA = 142
85561 deg
ZDOT = -2924
028549 TA = 87
78702
MA = 87
62149
Ha = 195
433 n
mi
Hp = 186
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1319207
98 X = 434010
57
Y = -15969758
42 feet Y = -4862907
26 meter
Z = 15185201
60 Z = 4630480
56
XDOT = 22175
411519 XDOT = 6797
786647
YDOT = -7340
563009 feet/sec YDOT = -2161
603301 meter/sec
ZDOT = -9593
269519 ZDOT = -2891
098619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3818891
24 X = -1163998
05
Y = 15554575
10 feet Y = 4741034
49 meter
Z = 15193258
52 Z = 4630905
20
XDOT = -21997
632472 XDOT = -6704
878377
YDOT = 3892
593525 feet/sec YDOT = 1186
462506 meter/sec
ZDOT = -9461
363277 ZDOT = -2883
823527
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 10255
54267552
00016717 00000-0 10270-3 0 9040
2 25544 51
6460 143
6513 0008819
4929 359
6240 15
71762238 37211
Satellite: ISS
Catalog Number: 25544
Epoch time: 10255
54267552 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 143
6513 deg
Eccentricity:
0008819
Arg of perigee:
4929 deg
Mean anomaly: 359
6240 deg
Mean motion: 15
71762238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 305
Coasting Arc #6 (Orbit 3736)
---------------------------------------
Vector Time (GMT): 2010/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5646886
82 A = 6737118
90 meter
Y = 3130413
05 meter E =
0019837
Z = 1880378
35 I = 51
88786
XDOT = -953
320847 Wp = 43
43373
YDOT = -5135
525534 meter/sec RA = 137
79141 deg
ZDOT = 5665
647330 TA = 337
38339
MA = 337
47069
Ha = 195
648 n
mi
Hp = 186
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18526531
55 X = -5690606
57
Y = 10270384
02 feet Y = 3067021
77 meter
Z = 6169220
30 Z = 1852839
34
XDOT = -3127
693068 XDOT = -923
346450
YDOT = -16848
837055 feet/sec YDOT = -5146
018401 meter/sec
ZDOT = 18588
081792 ZDOT = 5661
089009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19864958
34 X = 6054839
30
Y = -7446168
80 feet Y = -2269592
25 meter
Z = 6058913
97 Z = 1846756
98
XDOT = 196
742308 XDOT = 59
967055
YDOT = 15692
025605 feet/sec YDOT = 4782
929404 meter/sec
ZDOT = 18569
737586 ZDOT = 5660
056016
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 10256
55997007
00016717 00000-0 10270-3 0 9058
2 25544 51
6460 138
4444 0008846 4
3593 355
7645 15
71748880 37376
Satellite: ISS
Catalog Number: 25544
Epoch time: 10256
55997007 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 138
4444 deg
Eccentricity:
0008846
Arg of perigee: 4
3593 deg
Mean anomaly: 355
7645 deg
Mean motion: 15
71748880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3737
Checksum: 338
Coasting Arc #7 (Orbit 3751)
---------------------------------------
Vector Time (GMT): 2010/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1956794
11 A = 6726925
91 meter
Y = 3856844
52 meter E =
0016236
Z = -5164026
75 I = 51
87589
XDOT = -5861
515858 Wp = 67
66250
YDOT = 4784
042483 meter/sec RA = 132
66168 deg
ZDOT = 1361
372940 TA = 215
29307
MA = 215
40067
Ha = 195
582 n
mi
Hp = 186
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6419928
18 X = 1938606
70
Y = 12653689
37 feet Y = 3878624
79 meter
Z = -16942344
99 Z = -5154564
86
XDOT = -19230
695073 XDOT = -5921
189580
YDOT = 15695
677439 feet/sec YDOT = 4718
161866 meter/sec
ZDOT = 4466
446655 ZDOT = 1332
752596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4831263
33 X = -1472569
06
Y = -13389379
75 feet Y = -4081082
95 meter
Z = -16904371
94 Z = -5152452
57
XDOT = 20146
585896 XDOT = 6140
679381
YDOT = -12724
608149 feet/sec YDOT = -3878
460564 meter/sec
ZDOT = 4351
814055 ZDOT = 1326
432924
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 10257
51366069
00016717 00000-0 10270-3 0 9064
2 25544 51
6460 133
5632 0008794 7
0931 353
0354 15
71810343 37528
Satellite: ISS
Catalog Number: 25544
Epoch time: 10257
51366069 = yrday
fracday
Element set: 906
Inclination: 51
6460 deg
RA of node: 133
5632 deg
Eccentricity:
0008794
Arg of perigee: 7
0931 deg
Mean anomaly: 353
0354 deg
Mean motion: 15
71810343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3752
Checksum: 296
Coasting Arc #8 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2010/258/09:13:25
998
Vector Time (MET): N/A
Weight (LBS) : 826418
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4480094
18 A = 6729787
33 meter
Y = 638777
76 meter E =
0015442
Z = -4994204
13 I = 51
89561
XDOT = -3222
085316 Wp = 50
12069
YDOT = 6674
620103 meter/sec RA = 128
17887 deg
ZDOT = -2031
146754 TA = 200
22238
MA = 200
28361
Ha = 195
656 n
mi
Hp = 188
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14698471
71 X = 4496879
20
Y = 2095727
56 feet Y = 688970
63 meter
Z = -16385184
16 Z = -4972399
09
XDOT = -10571
146051 XDOT = -3286
615735
YDOT = 21898
359919 feet/sec YDOT = 6638
227973 meter/sec
ZDOT = -6663
867303 ZDOT = -2046
956482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8301480
12 X = -2530291
14
Y = -12424940
22 feet Y = -3787121
78 meter
Z = -16297781
85 Z = -4967563
91
XDOT = 22437
069939 XDOT = 6838
818917
YDOT = -6142
913266 feet/sec YDOT = -1872
359963 meter/sec
ZDOT = -6727
146005 ZDOT = -2050
434102
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 10258
40376230
00016717 00000-0 10270-3 0 9075
2 25544 51
6455 129
0074 0006617 355
1292 4
9804 15
71097605 37666
Satellite: ISS
Catalog Number: 25544
Epoch time: 10258
40376230 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 129
0074 deg
Eccentricity:
0006617
Arg of perigee: 355
1292 deg
Mean anomaly: 4
9804 deg
Mean motion: 15
71097605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 305
Coasting Arc #9 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2010/259/09:13:25
998
Vector Time (MET): N/A
Weight (LBS) : 826418
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1461460
95 A = 6737421
34 meter
Y = -6024991
08 meter E =
0013686
Z = 2631579
22 I = 51
93909
XDOT = 5536
455260 Wp = 74
74201
YDOT = -963
963457 meter/sec RA = 123
04667 deg
ZDOT = -5255
605167 TA = 75
50572
MA = 75
35392
Ha = 195
712 n
mi
Hp = 187
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4794819
38 X = 1515941
20
Y = -19767031
10 feet Y = -6008343
47 meter
Z = 8633790
09 Z = 2638811
43
XDOT = 18164
223293 XDOT = 5572
353674
YDOT = -3162
609767 feet/sec YDOT = -901
850886 meter/sec
ZDOT = -17242
799103 ZDOT = -5228
621957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17727465
16 X = -5403331
38
Y = 9947996
46 feet Y = 3032149
32 meter
Z = 8662706
74 Z = 2640393
01
XDOT = -14005
079381 XDOT = -4268
748195
YDOT = -9962
128991 feet/sec YDOT = -3036
456916 meter/sec
ZDOT = -17134
652000 ZDOT = -5222
641930
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 10259
42147454
00016717 00000-0 10270-3 0 9083
2 25544 51
6453 123
8040 0006582 358
4510 1
6630 15
71101482 37827
Satellite: ISS
Catalog Number: 25544
Epoch time: 10259
42147454 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 123
8040 deg
Eccentricity:
0006582
Arg of perigee: 358
4510 deg
Mean anomaly: 1
6630 deg
Mean motion: 15
71101482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3782
Checksum: 284
Coasting Arc #10 (Orbit 3797)
---------------------------------------
Vector Time (GMT): 2010/260/09:13:25
998
Vector Time (MET): N/A
Weight (LBS) : 826418
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4834231
94 A = 6733294
54 meter
Y = 2331900
85 meter E =
0011606
Z = 4053359
92 I = 51
94155
XDOT = 71
717769 Wp = 68
07674
YDOT = -6640
973324 meter/sec RA = 118
00154 deg
ZDOT = 3901
478528 TA = 341
86472
MA = 341
90609
Ha = 195
916 n
mi
Hp = 187
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15860341
02 X = -4879638
76
Y = 7650593
34 feet Y = 2277587
82 meter
Z = 13298424
94 Z = 4029765
01
XDOT = 235
294518 XDOT = 127
020471
YDOT = -21787
970223 feet/sec YDOT = -6639
861988 meter/sec
ZDOT = 12800
126404 ZDOT = 3901
961484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16552007
30 X = 5045051
82
Y = 6214424
54 feet Y = 1894156
60 meter
Z = 13203866
23 Z = 4024538
43
XDOT = -15387
887772 XDOT = -4690
228193
YDOT = 13752
436893 feet/sec YDOT = 4191
742765 meter/sec
ZDOT = 12801
986596 ZDOT = 3902
045515
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 10260
43916415
00016717 00000-0 10270-3 0 9098
2 25544 51
6459 118
6002 0006686 2
0671 358
0518 15
71140230 37983
Satellite: ISS
Catalog Number: 25544
Epoch time: 10260
43916415 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 118
6002 deg
Eccentricity:
0006686
Arg of perigee: 2
0671 deg
Mean anomaly: 358
0518 deg
Mean motion: 15
71140230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3798
Checksum: 295
Coasting Arc #11 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2010/261/09:13:25
998
Vector Time (MET): N/A
Weight (LBS) : 826418
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1262987
53 A = 6733034
89 meter
Y = 5212026
93 meter E =
0008693
Z = -4074453
04 I = 51
95486
XDOT = -5093
087503 Wp = 60
48394
YDOT = 4260
831057 meter/sec RA = 112
85899 deg
ZDOT = 3882
044312 TA = 249
32567
MA = 249
41889
Ha = 195
834 n
mi
Hp = 187
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4143659
87 X = 1224404
62
Y = 17099825
89 feet Y = 5225934
48 meter
Z = -13367628
10 Z = -4068411
48
XDOT = -16709
604667 XDOT = -5159
212497
YDOT = 13979
104519 feet/sec YDOT = 4203
507568 meter/sec
ZDOT = 12736
365854 ZDOT = 3857
141452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9166805
93 X = 2794042
45
Y = -15039684
24 feet Y = -4584095
76 meter
Z = -13343350
80 Z = -4067053
33
XDOT = 20648
667237 XDOT = 6293
713774
YDOT = 1404
399023 feet/sec YDOT = 428
060822 meter/sec
ZDOT = 12636
576591 ZDOT = 3851
628545
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 10261
39322746
00016717 00000-0 10270-3 0 9104
2 25544 51
6463 113
7219 0006750 4
4166 355
7054 15
71183560 38131
Satellite: ISS
Catalog Number: 25544
Epoch time: 10261
39322746 = yrday
fracday
Element set: 910
Inclination: 51
6463 deg
RA of node: 113
7219 deg
Eccentricity:
0006750
Arg of perigee: 4
4166 deg
Mean anomaly: 355
7054 deg
Mean motion: 15
71183560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3813
Checksum: 289
Coasting Arc #12 (Orbit 3828)
---------------------------------------
Vector Time (GMT): 2010/262/09:13:25
998
Vector Time (MET): N/A
Weight (LBS) : 826418
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3764940
13 A = 6737159
04 meter
Y = -4918386
63 meter E =
0006070
Z = -2659846
07 I = 51
97950
XDOT = 2724
772370 Wp = 52
94425
YDOT = 4918
385930 meter/sec RA = 107
81522 deg
ZDOT = -5242
468050 TA = 157
11342
MA = 157
08635
Ha = 195
820 n
mi
Hp = 187
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12352165
77 X = 3832579
58
Y = -16136439
07 feet Y = -4875906
80 meter
Z = -8726529
11 Z = -2641391
49
XDOT = 8939
541897 XDOT = 2695
038345
YDOT = 16136
436777 feet/sec YDOT = 4948
689356 meter/sec
ZDOT = -17199
698327 ZDOT = -5229
303763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20144812
61 X = -6140138
88
Y = 2903817
44 feet Y = 885083
56 meter
Z = -8652591
78 Z = -2637309
97
XDOT = 4994
612454 XDOT = 1522
357876
YDOT = -16398
270144 feet/sec YDOT = -4998
192740 meter/sec
ZDOT = -17146
868963 ZDOT = -5226
365660
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 10262
41087397
00016717 00000-0 10270-3 0 9119
2 25544 51
6464 108
5179 0006658 7
0237 353
1017 15
71194153 38292
Satellite: ISS
Catalog Number: 25544
Epoch time: 10262
41087397 = yrday
fracday
Element set: 911
Inclination: 51
6464 deg
RA of node: 108
5179 deg
Eccentricity:
0006658
Arg of perigee: 7
0237 deg
Mean anomaly: 353
1017 deg
Mean motion: 15
71194153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3829
Checksum: 305
Coasting Arc #13 (Orbit 3844)
---------------------------------------
Vector Time (GMT): 2010/263/09:13:25
998
Vector Time (MET): N/A
Weight (LBS) : 826418
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3278687
59 A = 6729257
68 meter
Y = -3134765
62 meter E =
0011926
Z = 4968340
76 I = 51
96186
XDOT = 3189
119868 Wp = 31
99903
YDOT = -6684
256514 meter/sec RA = 102
68486 deg
ZDOT = -2100
695765 TA = 78
33946
MA = 78
20564
Ha = 195
872 n
mi
Hp = 187
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10756849
06 X = -3267525
57
Y = -10284664
09 feet Y = -3171367
03 meter
Z = 16300330
58 Z = 4952440
36
XDOT = 10462
991694 XDOT = 3273
832185
YDOT = -21929
975440 feet/sec YDOT = -6648
120390 meter/sec
ZDOT = -6892
046472 ZDOT = -2084
996758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 855185
10 X = 260660
42
Y = 14927424
50 feet Y = 4549878
99 meter
Z = 16236549
83 Z = 4948900
39
XDOT = -21590
345098 XDOT = -6580
737186
YDOT = 8708
592445 feet/sec YDOT = 2654
378977 meter/sec
ZDOT = -6829
168955 ZDOT = -2081
530697
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 10263
42849610
00016717 00000-0 10270-3 0 9126
2 25544 51
6462 103
3135 0006843 10
1937 349
9363 15
71295328 38454
Satellite: ISS
Catalog Number: 25544
Epoch time: 10263
42849610 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 103
3135 deg
Eccentricity:
0006843
Arg of perigee: 10
1937 deg
Mean anomaly: 349
9363 deg
Mean motion: 15
71295328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3845
Checksum: 304
Coasting Arc #14 (Orbit 3860)
---------------------------------------
Vector Time (GMT): 2010/264/09:13:25
998
Vector Time (MET): N/A
Weight (LBS) : 826418
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1621865
29 A = 6739504
34 meter
Y = 6458779
36 meter E =
0019342
Z = 961473
55 I = 52
00145
XDOT = -4435
551214 Wp = 41
68071
YDOT = -2010
353181 meter/sec RA = 97
61954 deg
ZDOT = 5968
614115 TA = 328
76697
MA = 328
88176
Ha = 195
922 n
mi
Hp = 186
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5321080
35 X = -1698638
67
Y = 21190221
01 feet Y = 6440213
52 meter
Z = 3154440
77 Z = 953407
41
XDOT = -14552
333380 XDOT = -4441
735823
YDOT = -6595
646920 feet/sec YDOT = -2059
988165 meter/sec
ZDOT = 19582
067307 ZDOT = 5947
051419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18206128
32 X = 5549227
91
Y = -12086309
52 feet Y = -3683907
14 meter
Z = 3122158
37 Z = 951633
87
XDOT = 5534
851681 XDOT = 1687
022793
YDOT = 13419
742845 feet/sec YDOT = 4090
337619 meter/sec
ZDOT = 19495
595440 ZDOT = 5942
257490
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 10264
44609754
00016717 00000-0 10270-3 0 9133
2 25544 51
6459 98
1088 0006862 13
9587 346
1763 15
71294417 38610
Satellite: ISS
Catalog Number: 25544
Epoch time: 10264
44609754 = yrday
fracday
Element set: 913
Inclination: 51
6459 deg
RA of node: 98
1088 deg
Eccentricity:
0006862
Arg of perigee: 13
9587 deg
Mean anomaly: 346
1763 deg
Mean motion: 15
71294417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3861
Checksum: 337
Coasting Arc #15 (Orbit 3875)
---------------------------------------
Vector Time (GMT): 2010/265/09:13:25
998
Vector Time (MET): N/A
Weight (LBS) : 826418
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4142868
93 A = 6727698
58 meter
Y = 292780
46 meter E =
0018190
Z = -5307173
06 I = 51
96439
XDOT = -418
264081 Wp = 69
39268
YDOT = 7672
157545 meter/sec RA = 92
51805 deg
ZDOT = 103
274720 TA = 201
54670
MA = 201
62335
Ha = 195
925 n
mi
Hp = 186
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13592089
66 X = 4165068
46
Y = 960565
82 feet Y = 339232
06 meter
Z = -17411985
11 Z = -5286993
06
XDOT = -1372
257482 XDOT = -504
526166
YDOT = 25171
120556 feet/sec YDOT = 7666
997959 meter/sec
ZDOT = 338
827820 ZDOT = 101
032426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9656342
66 X = -2943253
24
Y = -9758779
83 feet Y = -2974476
09 meter
Z = -17331072
56 Z = -5282510
92
XDOT = 16931
409386 XDOT = 5160
693581
YDOT = -17301
342931 feet/sec YDOT = -5273
449325 meter/sec
ZDOT = 329
898754 ZDOT = 100
553140
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 10265
40007669
00016717 00000-0 10270-3 0 9148
2 25544 51
6453 93
2290 0006902 16
8616 343
2774 15
71340500 38766
Satellite: ISS
Catalog Number: 25544
Epoch time: 10265
40007669 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 93
2290 deg
Eccentricity:
0006902
Arg of perigee: 16
8616 deg
Mean anomaly: 343
2774 deg
Mean motion: 15
71340500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3876
Checksum: 298
Coasting Arc #16 (Orbit 3891)
---------------------------------------
Vector Time (GMT): 2010/266/09:13:25
998
Vector Time (MET): N/A
Weight (LBS) : 826418
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -894860
21 A = 6739534
20 meter
Y = -6633756
36 meter E =
0013313
Z = 762218
28 I = 52
00434
XDOT = 4631
165442 Wp = 97
43467
YDOT = -1323
994740 meter/sec RA = 87
42067 deg
ZDOT = -5998
815344 TA = 74
31113
MA = 74
16430
Ha = 195
988 n
mi
Hp = 186
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2935893
07 X = -824316
56
Y = -21764292
53 feet Y = -6643368
71 meter
Z = 2500716
15 Z = 758043
11
XDOT = 15194
112342 XDOT = 4674
767778
YDOT = -4343
814764 feet/sec YDOT = -1271
963139 meter/sec
ZDOT = -19681
152703 ZDOT = -5976
210918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11828687
70 X = -3605384
01
Y = 18505937
14 feet Y = 5640609
64 meter
Z = 2483931
71 Z = 757102
38
XDOT = -13136
583414 XDOT = -4004
030624
YDOT = -5728
551362 feet/sec YDOT = -1746
062455 meter/sec
ZDOT = -19590
531200 ZDOT = -5971
193910
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 10266
41763295
00016717 00000-0 10270-3 0 9155
2 25544 51
6453 88
0245 0006821 21
2723 338
8721 15
71330533 38922
Satellite: ISS
Catalog Number: 25544
Epoch time: 10266
41763295 = yrday
fracday
Element set: 915
Inclination: 51
6453 deg
RA of node: 88
0245 deg
Eccentricity:
0006821
Arg of perigee: 21
2723 deg
Mean anomaly: 338
8721 deg
Mean motion: 15
71330533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3892
Checksum: 301
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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