[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 19th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 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 2283)
---------------------------------------
Vector Time (GMT): 2012/200/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6106448
77 A = 6787127
94 meter
Y = 2529277
87 meter E =
0007489
Z = -1527537
86 I = 51
47258
XDOT = -653
092073 Wp = 148
26530
YDOT = -5035
083493 meter/sec RA = 326
89707 deg
ZDOT = -5745
321052 TA = 48
46305
MA = 48
39884
Ha = 219
950 n
mi
Hp = 214
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20034280
74 X = -6126857
53
Y = 8298155
75 feet Y = 2460877
86 meter
Z = -5011607
17 Z = -1557251
45
XDOT = -2142
690527 XDOT = -568
831212
YDOT = -16519
302800 feet/sec YDOT = -5041
914911 meter/sec
ZDOT = -18849
478518 ZDOT = -5748
289669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19863451
47 X = -6054380
01
Y = 8627223
94 feet Y = 2629577
86 meter
Z = -5134423
34 Z = -1564972
23
XDOT = -1671
121699 XDOT = -509
357894
YDOT = -15036
309189 feet/sec YDOT = -4583
067041 meter/sec
ZDOT = -18861
136516 ZDOT = -5748
874410
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 12200
21069060
00016717 00000-0 10270-3 0 9006
2 25544 51
6447 327
3047 0001049 270
3088 89
7945 15
54527418 22847
Satellite: ISS
Catalog Number: 25544
Epoch time: 12200
21069060 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 327
3047 deg
Eccentricity:
0001049
Arg of perigee: 270
3088 deg
Mean anomaly: 89
7945 deg
Mean motion: 15
54527418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2284
Checksum: 297
Coasting Arc #2 (Orbit 2299)
---------------------------------------
Vector Time (GMT): 2012/201/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5833528
37 A = 6783679
10 meter
Y = -1359127
37 meter E =
0011898
Z = 3172799
27 I = 51
43641
XDOT = -1256
578802 Wp = 84
02560
YDOT = 5849
565661 meter/sec RA = 321
90463 deg
ZDOT = 4801
815470 TA = 312
74717
MA = 312
84723
Ha = 219
878 n
mi
Hp = 214
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19138872
62 X = 5832880
42
Y = -4459079
29 feet Y = -1293897
21 meter
Z = 10409446
42 Z = 3201136
00
XDOT = -4122
633864 XDOT = -1345
222126
YDOT = 19191
488388 feet/sec YDOT = 5835
017651 meter/sec
ZDOT = 15753
987763 ZDOT = 4795
496528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18913743
46 X = 5764909
01
Y = -5099077
22 feet Y = -1554198
74 meter
Z = 10526448
96 Z = 3208461
64
XDOT = -3941
035502 XDOT = -1201
227621
YDOT = 17944
645311 feet/sec YDOT = 5469
527891 meter/sec
ZDOT = 15727
262435 ZDOT = 4793
669590
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 12201
23922890
00016717 00000-0 10270-3 0 9019
2 25544 51
6446 322
1734 0001024 292
7803 67
3242 15
54569867 23003
Satellite: ISS
Catalog Number: 25544
Epoch time: 12201
23922890 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 322
1734 deg
Eccentricity:
0001024
Arg of perigee: 292
7803 deg
Mean anomaly: 67
3242 deg
Mean motion: 15
54569867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2300
Checksum: 286
Coasting Arc #3 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2012/202/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5115864
25 A = 6779390
91 meter
Y = -85029
83 meter E =
0008636
Z = -4456429
75 I = 51
39876
XDOT = 2930
592049 Wp = 63
56321
YDOT = -6290
830755 meter/sec RA = 316
89910 deg
ZDOT = -3245
332316 TA = 173
62018
MA = 173
60918
Ha = 219
817 n
mi
Hp = 214
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16784331
53 X = -5092885
33
Y = -278969
24 feet Y = -142109
71 meter
Z = -14620832
51 Z = -4481226
06
XDOT = 9614
803312 XDOT = 3016
484366
YDOT = -20639
208514 feet/sec YDOT = -6257
578513 meter/sec
ZDOT = -10647
415734 ZDOT = -3230
887868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16687308
32 X = -5086291
58
Y = 570318
80 feet Y = 173833
17 meter
Z = -14723071
34 Z = -4487592
14
XDOT = 8657
984062 XDOT = 2638
953542
YDOT = -19889
040227 feet/sec YDOT = -6062
179461 meter/sec
ZDOT = -10587
144463 ZDOT = -3226
961632
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 12202
20346539
00016717 00000-0 10270-3 0 9028
2 25544 51
6442 317
3632 0001238 292
7285 67
3737 15
54612913 23159
Satellite: ISS
Catalog Number: 25544
Epoch time: 12202
20346539 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 317
3632 deg
Eccentricity:
0001238
Arg of perigee: 292
7285 deg
Mean anomaly: 67
3737 deg
Mean motion: 15
54612913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 291
Coasting Arc #4 (Orbit 2330)
---------------------------------------
Vector Time (GMT): 2012/203/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4051283
40 A = 6776415
68 meter
Y = 1668364
28 meter E =
0003047
Z = 5167664
05 I = 51
36745
XDOT = -4231
715419 Wp = 125
54730
YDOT = 6266
474032 meter/sec RA = 311
88060 deg
ZDOT = 1292
140834 TA = 311
98724
MA = 312
01319
Ha = 219
739 n
mi
Hp = 214
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13291612
20 X = 4007223
47
Y = 5473636
09 feet Y = 1713421
54 meter
Z = 16954278
39 Z = 5187237
70
XDOT = -13883
580772 XDOT = -4307
750710
YDOT = 20559
298004 feet/sec YDOT = 6218
727137 meter/sec
ZDOT = 4239
307197 ZDOT = 1271
399513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13529908
57 X = 4123916
13
Y = 4564228
76 feet Y = 1391176
92 meter
Z = 17034805
33 Z = 5192208
67
XDOT = -12144
452427 XDOT = -3701
629100
YDOT = 20472
172219 feet/sec YDOT = 6239
918092 meter/sec
ZDOT = 4153
084871 ZDOT = 1265
860269
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 12203
23196868
00016717 00000-0 10270-3 0 9031
2 25544 51
6443 312
2321 0001127 301
0278 59
0764 15
54630184 23318
Satellite: ISS
Catalog Number: 25544
Epoch time: 12203
23196868 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 312
2321 deg
Eccentricity:
0001127
Arg of perigee: 301
0278 deg
Mean anomaly: 59
0764 deg
Mean motion: 15
54630184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2331
Checksum: 273
Coasting Arc #5 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2012/204/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2789220
74 A = 6775990
53 meter
Y = -3275634
46 meter E =
0013379
Z = -5246630
41 I = 51
34558
XDOT = 5084
220912 Wp = 93
86193
YDOT = -5667
427269 meter/sec RA = 306
85404 deg
ZDOT = 836
435825 TA = 184
17084
MA = 184
18200
Ha = 219
760 n
mi
Hp = 214
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9150986
67 X = -2726898
14
Y = -10746832
22 feet Y = -3306476
53 meter
Z = -17213354
37 Z = -5260028
86
XDOT = 16680
514802 XDOT = 5143
154236
YDOT = -18593
921486 feet/sec YDOT = -5610
242881 meter/sec
ZDOT = 2744
212023 ZDOT = 861
277152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9928791
07 X = -3026295
52
Y = -9937875
82 feet Y = -3029064
55 meter
Z = -17268244
29 Z = -5263360
86
XDOT = 14293
379547 XDOT = 4356
622086
YDOT = -19222
287303 feet/sec YDOT = -5858
953170 meter/sec
ZDOT = 2847
263001 ZDOT = 867
845763
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 12204
19617243
00016717 00000-0 10270-3 0 9043
2 25544 51
6430 307
4207 0001275 304
7010 55
4023 15
54682957 23460
Satellite: ISS
Catalog Number: 25544
Epoch time: 12204
19617243 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 307
4207 deg
Eccentricity:
0001275
Arg of perigee: 304
7010 deg
Mean anomaly: 55
4023 deg
Mean motion: 15
54682957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 277
Coasting Arc #6 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2012/205/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1438064
88 A = 6778423
44 meter
Y = 4723531
68 meter E =
0007669
Z = 4640716
78 I = 51
33671
XDOT = -5503
087382 Wp = 54
75987
YDOT = 4505
971276 meter/sec RA = 301
83067 deg
ZDOT = -2873
371311 TA = 63
94641
MA = 63
86748
Ha = 219
644 n
mi
Hp = 214
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4718060
64 X = 1362595
28
Y = 15497151
19 feet Y = 4739190
87 meter
Z = 15225448
76 Z = 4647519
60
XDOT = -18054
748629 XDOT = -5539
107097
YDOT = 14783
370327 feet/sec YDOT = 4444
231045 meter/sec
ZDOT = -9427
071229 ZDOT = -2900
191983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6186994
97 X = 1885796
07
Y = 14943341
49 feet Y = 4554730
49 meter
Z = 15252990
51 Z = 4649111
51
XDOT = -15299
505145 XDOT = -4663
289168
YDOT = 16096
036913 feet/sec YDOT = 4906
072051 meter/sec
ZDOT = -9538
147853 ZDOT = -2907
227466
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 12205
22463906
00016717 00000-0 10270-3 0 9054
2 25544 51
6431 302
2895 0001419 307
7917 52
3107 15
54721988 23621
Satellite: ISS
Catalog Number: 25544
Epoch time: 12205
22463906 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 302
2895 deg
Eccentricity:
0001419
Arg of perigee: 307
7917 deg
Mean anomaly: 52
3107 deg
Mean motion: 15
54721988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2362
Checksum: 299
Coasting Arc #7 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2012/206/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -148554
50 A = 6782527
88 meter
Y = -5835857
39 meter E =
0004017
Z = -3455698
72 I = 51
33362
XDOT = 5494
738937 Wp = 79
27158
YDOT = -2823
223804 meter/sec RA = 296
81510 deg
ZDOT = 4536
783816 TA = 240
00506
MA = 240
04494
Ha = 219
715 n
mi
Hp = 214
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -487383
55 X = -66498
88
Y = -19146513
74 feet Y = -5837059
70 meter
Z = -11337594
21 Z = -3456221
27
XDOT = 18027
358718 XDOT = 5503
861993
YDOT = -9262
545290 feet/sec YDOT = -2761
727367 meter/sec
ZDOT = 14884
461340 ZDOT = 4563
498784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2702291
96 X = -823658
59
Y = -18960204
96 feet Y = -5779070
47 meter
Z = -11339127
82 Z = -3456166
16
XDOT = 15318
750881 XDOT = 4669
155268
YDOT = -11140
714315 feet/sec YDOT = -3395
689723 meter/sec
ZDOT = 14994
915160 ZDOT = 4570
450141
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 12206
18881196
00016717 00000-0 10270-3 0 9066
2 25544 51
6414 297
4775 0001359 311
6622 48
4415 15
54724860 23770
Satellite: ISS
Catalog Number: 25544
Epoch time: 12206
18881196 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 297
4775 deg
Eccentricity:
0001359
Arg of perigee: 311
6622 deg
Mean anomaly: 48
4415 deg
Mean motion: 15
54724860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 320
Coasting Arc #8 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2012/207/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1039805
97 A = 6786078
76 meter
Y = 6456296
08 meter E =
0012587
Z = 1791551
99 I = 51
33335
XDOT = -5152
369505 Wp = 111
31388
YDOT = 741
135974 meter/sec RA = 291
81237 deg
ZDOT = -5633
753368 TA = 48
90654
MA = 48
79790
Ha = 219
667 n
mi
Hp = 213
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3411436
92 X = -1120627
22
Y = 21182073
76 feet Y = 6444216
35 meter
Z = 5877795
24 Z = 1786304
65
XDOT = -16904
099427 XDOT = -5132
906796
YDOT = 2431
548471 feet/sec YDOT = 683
628037 meter/sec
ZDOT = -18483
442809 ZDOT = -5658
735865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -523342
08 X = -159514
66
Y = 21454745
65 feet Y = 6539406
48 meter
Z = 5855478
60 Z = 1784749
88
XDOT = -14737
391436 XDOT = -4491
956910
YDOT = 4737
923635 feet/sec YDOT = 1444
119124 meter/sec
ZDOT = -18586
529832 ZDOT = -5665
174293
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 12207
21724418
00016717 00000-0 10270-3 0 9075
2 25544 51
6416 292
3458 0001544 320
6793 39
4247 15
54782740 23931
Satellite: ISS
Catalog Number: 25544
Epoch time: 12207
21724418 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 292
3458 deg
Eccentricity:
0001544
Arg of perigee: 320
6793 deg
Mean anomaly: 39
4247 deg
Mean motion: 15
54782740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2393
Checksum: 310
Coasting Arc #9 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2012/208/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2026325
24 A = 6787491
83 meter
Y = -6470487
67 meter E =
0012510
Z = 84793
41 I = 51
32600
XDOT = 4550
472306 Wp = 39
87095
YDOT = 1509
829267 meter/sec RA = 286
81517 deg
ZDOT = 5987
806467 TA = 321
04680
MA = 321
13686
Ha = 219
725 n
mi
Hp = 213
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6648048
69 X = 2098117
06
Y = -21228634
09 feet Y = -6447426
64 meter
Z = 278193
61 Z = 94811
16
XDOT = 14929
371082 XDOT = 4504
163608
YDOT = 4953
508095 feet/sec YDOT = 1560
456191 meter/sec
ZDOT = 19645
034342 ZDOT = 6009
799962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3308140
42 X = 1008321
20
Y = -21997330
35 feet Y = -6704786
29 meter
Z = 320176
54 Z = 97589
81
XDOT = 13790
135012 XDOT = 4203
233152
YDOT = 2381
128436 feet/sec YDOT = 725
767947 meter/sec
ZDOT = 19735
561502 ZDOT = 6015
399146
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 12208
24566120
00016717 00000-0 10270-3 0 9084
2 25544 51
6401 287
2124 0001410 322
0157 38
0896 15
54760298 24097
Satellite: ISS
Catalog Number: 25544
Epoch time: 12208
24566120 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 287
2124 deg
Eccentricity:
0001410
Arg of perigee: 322
0157 deg
Mean anomaly: 38
0896 deg
Mean motion: 15
54760298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 285
Coasting Arc #10 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2012/209/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2846097
30 A = 6785658
42 meter
Y = 5828514
82 meter E =
0005323
Z = -1988062
95 I = 51
31232
XDOT = -3759
286374 Wp = 137
27810
YDOT = -3723
500308 meter/sec RA = 281
81828 deg
ZDOT = -5547
218047 TA = 64
77273
MA = 64
71756
Ha = 219
717 n
mi
Hp = 213
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9337589
58 X = -2901403
91
Y = 19122423
96 feet Y = 5796378
92 meter
Z = -6522516
24 Z = -2002022
96
XDOT = -12333
616712 XDOT = -3690
423019
YDOT = -12216
208361 feet/sec YDOT = -3765
153490 meter/sec
ZDOT = -18199
534274 ZDOT = -5565
313449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5900973
78 X = -1798616
81
Y = 20427285
51 feet Y = 6226236
62 meter
Z = -6580684
64 Z = -2005792
68
XDOT = -12636
784196 XDOT = -3851
691823
YDOT = -9524
207293 feet/sec YDOT = -2902
978383 meter/sec
ZDOT = -18273
761681 ZDOT = -5569
842560
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 12209
20978480
00016717 00000-0 10270-3 0 9098
2 25544 51
6399 282
4011 0001425 329
3019 30
8050 15
54803078 24241
Satellite: ISS
Catalog Number: 25544
Epoch time: 12209
20978480 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 282
4011 deg
Eccentricity:
0001425
Arg of perigee: 329
3019 deg
Mean anomaly: 30
8050 deg
Mean motion: 15
54803078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2424
Checksum: 293
Coasting Arc #11 (Orbit 2439)
---------------------------------------
Vector Time (GMT): 2012/210/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3456161
09 A = 6781683
50 meter
Y = -4580367
17 meter E =
0011154
Z = 3604763
63 I = 51
29361
XDOT = 2862
248036 Wp = 88
35477
YDOT = 5613
761157 meter/sec RA = 276
81035 deg
ZDOT = 4377
388522 TA = 314
62079
MA = 314
71171
Ha = 219
578 n
mi
Hp = 213
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11339111
18 X = 3489611
82
Y = -15027451
33 feet Y = -4541531
56 meter
Z = 11826652
33 Z = 3621634
17
XDOT = 9390
577545 XDOT = 2777
996857
YDOT = 18417
851566 feet/sec YDOT = 5645
297069 meter/sec
ZDOT = 14361
510898 ZDOT = 4391
089032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8250490
99 X = 2514749
65
Y = -16872093
87 feet Y = -5142614
21 meter
Z = 11896692
31 Z = 3626111
82
XDOT = 11359
712011 XDOT = 3462
440221
YDOT = 15747
118903 feet/sec YDOT = 4799
721841 meter/sec
ZDOT = 14417
427407 ZDOT = 4394
431874
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 12210
23816663
00016717 00000-0 10270-3 0 9109
2 25544 51
6394 277
2677 0001354 326
5146 33
5921 15
54838181 24405
Satellite: ISS
Catalog Number: 25544
Epoch time: 12210
23816663 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 277
2677 deg
Eccentricity:
0001354
Arg of perigee: 326
5146 deg
Mean anomaly: 33
5921 deg
Mean motion: 15
54838181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2440
Checksum: 298
Coasting Arc #12 (Orbit 2454)
---------------------------------------
Vector Time (GMT): 2012/211/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3912323
53 A = 6777495
90 meter
Y = 2830434
12 meter E =
0011432
Z = -4766747
85 I = 51
27714
XDOT = -1867
847899 Wp = 65
19353
YDOT = -6959
294014 meter/sec RA = 271
78987 deg
ZDOT = -2599
510466 TA = 179
02427
MA = 179
02203
Ha = 219
768 n
mi
Hp = 213
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12835707
13 X = -3920527
73
Y = 9286201
18 feet Y = 2786638
76 meter
Z = -15638936
51 Z = -4785773
14
XDOT = -6128
109905 XDOT = -1777
261126
YDOT = -22832
329442 feet/sec YDOT = -6979
674656 meter/sec
ZDOT = -8528
577643 ZDOT = -2608
365042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10574230
32 X = -3223025
40
Y = 11692104
42 feet Y = 3563753
43 meter
Z = -15717684
06 Z = -4790750
10
XDOT = -9759
890534 XDOT = -2974
814635
YDOT = -20338
912419 feet/sec YDOT = -6199
300505 meter/sec
ZDOT = -8564
382662 ZDOT = -2610
423835
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 12211
20226104
00016717 00000-0 10270-3 0 9113
2 25544 51
6394 272
4563 0001271 342
6573 17
4536 15
54855997 24550
Satellite: ISS
Catalog Number: 25544
Epoch time: 12211
20226104 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 272
4563 deg
Eccentricity:
0001271
Arg of perigee: 342
6573 deg
Mean anomaly: 17
4536 deg
Mean motion: 15
54855997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2455
Checksum: 297
Coasting Arc #13 (Orbit 2470)
---------------------------------------
Vector Time (GMT): 2012/212/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4187592
59 A = 6775395
32 meter
Y = -775603
09 meter E =
0002301
Z = 5267579
48 I = 51
26935
XDOT = 812
867543 Wp = 82
48530
YDOT = 7613
888099 meter/sec RA = 266
75782 deg
ZDOT = 474
983832 TA = 2
96331
MA = 2
96195
Ha = 219
716 n
mi
Hp = 213
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13738820
82 X = 4170366
02
Y = -2544629
55 feet Y = -728871
73 meter
Z = 17282084
91 Z = 5287880
35
XDOT = 2666
888263 XDOT = 725
359739
YDOT = 24979
947831 feet/sec YDOT = 7622
488752 meter/sec
ZDOT = 1558
345904 ZDOT = 478
720935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12733132
49 X = 3881058
78
Y = -5494909
11 feet Y = -1674848
30 meter
Z = 17365889
17 Z = 5293123
02
XDOT = 7714
151365 XDOT = 2351
273336
YDOT = 22845
704350 feet/sec YDOT = 6963
370686 meter/sec
ZDOT = 1572
992324 ZDOT = 479
448060
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 12212
23061221
00016717 00000-0 10270-3 0 9125
2 25544 51
6388 267
3231 0001288 347
8822 12
2300 15
54824700 24718
Satellite: ISS
Catalog Number: 25544
Epoch time: 12212
23061221 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 267
3231 deg
Eccentricity:
0001288
Arg of perigee: 347
8822 deg
Mean anomaly: 12
2300 deg
Mean motion: 15
54824700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2471
Checksum: 267
Coasting Arc #14 (Orbit 2485)
---------------------------------------
Vector Time (GMT): 2012/213/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4303483
96 A = 6776113
66 meter
Y = -1349012
59 meter E =
0012950
Z = -5068882
79 I = 51
27552
XDOT = 311
072117 Wp = 98
17510
YDOT = -7457
217594 meter/sec RA = 261
72427 deg
ZDOT = 1722
514561 TA = 188
56648
MA = 188
58860
Ha = 219
768 n
mi
Hp = 213
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14119041
88 X = -4263456
22
Y = -4425894
33 feet Y = -1396912
52 meter
Z = -16630192
89 Z = -5089691
39
XDOT = 1020
577812 XDOT = 386
069732
YDOT = -24465
936987 feet/sec YDOT = -7453
319825 meter/sec
ZDOT = 5651
294491 ZDOT = 1724
207141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14667831
46 X = -4470755
03
Y = -965934
79 feet Y = -294416
92 meter
Z = -16715887
36 Z = -5095002
47
XDOT = -4931
884968 XDOT = -1503
238538
YDOT = -22928
377237 feet/sec YDOT = -6988
569382 meter/sec
ZDOT = 5659
012847 ZDOT = 1724
867116
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 12213
19467359
00016717 00000-0 10270-3 0 9134
2 25544 51
6392 262
5114 0001179 351
5039 8
6094 15
54893537 24860
Satellite: ISS
Catalog Number: 25544
Epoch time: 12213
19467359 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 262
5114 deg
Eccentricity:
0001179
Arg of perigee: 351
5039 deg
Mean anomaly: 8
6094 deg
Mean motion: 15
54893537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2486
Checksum: 318
Coasting Arc #15 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2012/214/04:21:27
656
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4202910
07 A = 6779686
65 meter
Y = 3320066
64 meter E =
0010517
Z = 4150622
11 I = 51
29193
XDOT = -1502
610443 Wp = 68
82313
YDOT = 6547
808247 meter/sec RA = 256
69771 deg
ZDOT = -3704
688029 TA = 59
45933
MA = 59
35557
Ha = 219
704 n
mi
Hp = 213
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13789075
02 X = 4145309
74
Y = 10892607
08 feet Y = 3366743
81 meter
Z = 13617526
60 Z = 4170899
50
XDOT = -4929
824288 XDOT = -1557
721610
YDOT = 21482
310522 feet/sec YDOT = 6530
697263 meter/sec
ZDOT = -12154
488284 ZDOT = -3712
120826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16026865
96 X = 4884988
74
Y = 7046333
04 feet Y = 2147722
31 meter
Z = 13700849
18 Z = 4176018
83
XDOT = 1285
852260 XDOT = 391
927769
YDOT = 20841
189259 feet/sec YDOT = 6352
394486 meter/sec
ZDOT = -12185
781832 ZDOT = -3714
226302
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 12214
22299081
00016717 00000-0 10270-3 0 9145
2 25544 51
6382 257
3782 0001195 353
9437 6
1701 15
54897685 25023
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
22299081 = yrday
fracday
Element set: 914
Inclination: 51
6382 deg
RA of node: 257
3782 deg
Eccentricity:
0001195
Arg of perigee: 353
9437 deg
Mean anomaly: 6
1701 deg
Mean motion: 15
54897685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 312
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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