[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 28th 2013
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) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 3149)
---------------------------------------
Vector Time (GMT): 2013/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 518446
00 A = 6788618
55 meter
Y = -4413745
04 meter E =
0008340
Z = 5126488
08 I = 51
44928
XDOT = 7037
179764 Wp = 30
22224
YDOT = 2619
579844 meter/sec RA = 209
88342 deg
ZDOT = 1549
663286 TA = 44
83377
MA = 44
76642
Ha = 228
925 n
mi
Hp = 219
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1700938
32 X = 542859
68
Y = -14480790
81 feet Y = -4407811
62 meter
Z = 16819186
61 Z = 5129065
37
XDOT = 23087
860118 XDOT = 6999
836148
YDOT = 8594
422059 feet/sec YDOT = 2698
065018 meter/sec
ZDOT = 5084
197132 ZDOT = 1583
759117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12367000
29 X = -3769461
69
Y = -7698256
40 feet Y = -2346428
55 meter
Z = 16830498
63 Z = 5129935
98
XDOT = 17154
256794 XDOT = 5228
617471
YDOT = -16174
668648 feet/sec YDOT = -4930
039004 meter/sec
ZDOT = 5226
167828 ZDOT = 1592
935954
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 13147
55111810
00016717 00000-0 10270-3 0 9005
2 25544 51
6475 210
6712 0010055
9644 359
1524 15
50548912 31501
Satellite: ISS
Catalog Number: 25544
Epoch time: 13147
55111810 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 210
6712 deg
Eccentricity:
0010055
Arg of perigee:
9644 deg
Mean anomaly: 359
1524 deg
Mean motion: 15
50548912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 270
Coasting Arc #2 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2013/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -746980
01 A = 6788193
86 meter
Y = 4259426
90 meter E =
0019272
Z = -5247322
27 I = 51
47394
XDOT = -7172
902009 Wp = 51
62796
YDOT = -2473
169582 meter/sec RA = 204
90953 deg
ZDOT = -977
204720 TA = 208
92109
MA = 209
02803
Ha = 229
143 n
mi
Hp = 218
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2450721
81 X = -769064
21
Y = 13974497
70 feet Y = 4250950
84 meter
Z = -17215624
24 Z = -5251004
17
XDOT = -23533
143073 XDOT = -7139
966381
YDOT = -8114
073433 feet/sec YDOT = -2553
197224 meter/sec
ZDOT = -3206
052230 ZDOT = -1011
970394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11725949
74 X = 3574069
48
Y = 7952796
61 feet Y = 2424012
41 meter
Z = -17231525
47 Z = -5252168
96
XDOT = -16592
885727 XDOT = -5057
511570
YDOT = 17139
152045 feet/sec YDOT = 5224
013543 meter/sec
ZDOT = -3350
860082 ZDOT = -1021
342153
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 13148
51788237
00016717 00000-0 10270-3 0 9016
2 25544 51
6467 205
8780 0010144 4
9352 355
1897 15
50534417 31652
Satellite: ISS
Catalog Number: 25544
Epoch time: 13148
51788237 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 205
8780 deg
Eccentricity:
0010144
Arg of perigee: 4
9352 deg
Mean anomaly: 355
1897 deg
Mean motion: 15
50534417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3165
Checksum: 312
Coasting Arc #3 (Orbit 3180)
---------------------------------------
Vector Time (GMT): 2013/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1048227
35 A = 6787720
35 meter
Y = -4104005
59 meter E =
0010125
Z = 5299821
92 I = 51
50125
XDOT = 7294
217455 Wp = 24
17451
YDOT = 2331
421433 meter/sec RA = 199
93655 deg
ZDOT = 371
481721 TA = 62
32728
MA = 62
22457
Ha = 229
141 n
mi
Hp = 218
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3439066
11 X = 1068296
22
Y = -13464585
26 feet Y = -4092171
97 meter
Z = 17387867
20 Z = 5304962
45
XDOT = 23931
159628 XDOT = 7265
800316
YDOT = 7649
020450 feet/sec YDOT = 2412
831046 meter/sec
ZDOT = 1218
772052 ZDOT = 406
847586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10998042
76 X = -3352203
43
Y = -8449899
95 feet Y = -2575529
50 meter
Z = 17409836
41 Z = 5306518
14
XDOT = 15982
894795 XDOT = 4871
586333
YDOT = -18047
356430 feet/sec YDOT = -5500
834240 meter/sec
ZDOT = 1366
124439 ZDOT = 416
394729
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 13149
54908151
00016717 00000-0 10270-3 0 9020
2 25544 51
6467 200
7649 0010211 8
9674 351
1658 15
50589868 31815
Satellite: ISS
Catalog Number: 25544
Epoch time: 13149
54908151 = yrday
fracday
Element set: 902
Inclination: 51
6467 deg
RA of node: 200
7649 deg
Eccentricity:
0010211
Arg of perigee: 8
9674 deg
Mean anomaly: 351
1658 deg
Mean motion: 15
50589868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3181
Checksum: 319
Coasting Arc #4 (Orbit 3195)
---------------------------------------
Vector Time (GMT): 2013/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1331426
45 A = 6787729
96 meter
Y = 4019392
70 meter E =
0019643
Z = -5319761
01 I = 51
53065
XDOT = -7339
456045 Wp = 60
85326
YDOT = -2146
794313 meter/sec RA = 194
96542 deg
ZDOT = 224
862545 TA = 211
23974
MA = 211
35663
Ha = 229
343 n
mi
Hp = 218
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4368197
01 X = -1350431
24
Y = 13186983
91 feet Y = 4004398
02 meter
Z = -17453284
14 Z = -5326274
79
XDOT = -24079
580201 XDOT = -7315
996964
YDOT = -7043
288429 feet/sec YDOT = -2228
737591 meter/sec
ZDOT = 737
738009 ZDOT = 189
264918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10527911
32 X = 3208907
37
Y = 9009627
87 feet Y = 2746134
58 meter
Z = -17480975
54 Z = -5328201
34
XDOT = -15118
057073 XDOT = -4607
983796
YDOT = 18745
846858 feet/sec YDOT = 5713
734122 meter/sec
ZDOT = 589
376271 ZDOT = 179
641887
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 13150
51581967
00016717 00000-0 10270-3 0 9032
2 25544 51
6471 195
9712 0010300 12
7008 347
4400 15
50576359 31969
Satellite: ISS
Catalog Number: 25544
Epoch time: 13150
51581967 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 195
9712 deg
Eccentricity:
0010300
Arg of perigee: 12
7008 deg
Mean anomaly: 347
4400 deg
Mean motion: 15
50576359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3196
Checksum: 295
Coasting Arc #5 (Orbit 3211)
---------------------------------------
Vector Time (GMT): 2013/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1681702
06 A = 6787759
39 meter
Y = -3942497
60 meter E =
0012902
Z = 5259588
46 I = 51
56080
XDOT = 7355
951919 Wp = 27
31822
YDOT = 1983
883503 meter/sec RA = 189
99608 deg
ZDOT = -852
855470 TA = 70
91685
MA = 70
77717
Ha = 229
333 n
mi
Hp = 218
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5517395
21 X = 1700113
21
Y = -12934703
41 feet Y = -3923589
16 meter
Z = 17255867
66 Z = 5267802
49
XDOT = 24133
700522 XDOT = 7337
363944
YDOT = 6508
804145 feet/sec YDOT = 2066
038524 meter/sec
ZDOT = -2798
082251 ZDOT = -817
165843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10022177
20 X = -3054759
61
Y = -9803191
74 feet Y = -2988012
84 meter
Z = 17290649
69 Z = 5270190
03
XDOT = 14250
007024 XDOT = 4343
402141
YDOT = -19310
709664 feet/sec YDOT = -5885
904306 meter/sec
ZDOT = -2649
300014 ZDOT = -807
506644
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 13151
54699139
00016717 00000-0 10270-3 0 9048
2 25544 51
6467 190
8580 0010368 16
9519 343
1977 15
50633273 32128
Satellite: ISS
Catalog Number: 25544
Epoch time: 13151
54699139 = yrday
fracday
Element set: 904
Inclination: 51
6467 deg
RA of node: 190
8580 deg
Eccentricity:
0010368
Arg of perigee: 16
9519 deg
Mean anomaly: 343
1977 deg
Mean motion: 15
50633273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3212
Checksum: 320
Coasting Arc #6 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2013/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1988865
44 A = 6788239
19 meter
Y = 3940160
51 meter E =
0018661
Z = -5170916
55 I = 51
59368
XDOT = -7295
219184 Wp = 67
64459
YDOT = -1795
253179 meter/sec RA = 185
02935 deg
ZDOT = 1449
094690 TA = 216
27810
MA = 216
40478
Ha = 229
508 n
mi
Hp = 217
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6525149
08 X = -2007658
29
Y = 12927035
78 feet Y = 3917815
00 meter
Z = -16964949
30 Z = -5180623
73
XDOT = -23934
446143 XDOT = -7281
641425
YDOT = -5889
938251 feet/sec YDOT = -1876
757094 meter/sec
ZDOT = 4754
247672 ZDOT = 1413
687841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9825656
91 X = 2994860
23
Y = 10571131
22 feet Y = 3222080
79 meter
Z = -17005968
97 Z = -5183419
34
XDOT = -13201
827798 XDOT = -4023
917113
YDOT = 19622
998647 feet/sec YDOT = 5981
089988 meter/sec
ZDOT = 4606
608841 ZDOT = 1404
094375
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 13152
51370352
00016717 00000-0 10270-3 0 9050
2 25544 51
6478 186
0645 0010437 20
2713 339
8851 15
50619041 32276
Satellite: ISS
Catalog Number: 25544
Epoch time: 13152
51370352 = yrday
fracday
Element set: 905
Inclination: 51
6478 deg
RA of node: 186
0645 deg
Eccentricity:
0010437
Arg of perigee: 20
2713 deg
Mean anomaly: 339
8851 deg
Mean motion: 15
50619041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 290
Coasting Arc #7 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2013/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2353344
78 A = 6788782
56 meter
Y = -3949523
28 meter E =
0015890
Z = 4990950
37 I = 51
62548
XDOT = 7194
226165 Wp = 36
43167
YDOT = 1648
619326 meter/sec RA = 180
06441 deg
ZDOT = -2071
726900 TA = 73
82045
MA = 73
64564
Ha = 229
491 n
mi
Hp = 217
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7720947
44 X = 2373089
39
Y = -12957753
53 feet Y = -3923096
61 meter
Z = 16374509
10 Z = 5002430
52
XDOT = 23603
104216 XDOT = 7185
320232
YDOT = 5408
856056 feet/sec YDOT = 1729
020039 meter/sec
ZDOT = -6797
004264 ZDOT = -2036
799207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9630795
26 X = -2935466
39
Y = -11540182
36 feet Y = -3517447
58 meter
Z = 16422939
08 Z = 5005711
83
XDOT = 12218
736773 XDOT = 3724
270968
YDOT = -19736
665840 feet/sec YDOT = -6015
735748 meter/sec
ZDOT = -6651
335368 ZDOT = -2027
327020
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 13153
54484779
00016717 00000-0 10270-3 0 9064
2 25544 51
6465 180
9510 0010507 24
5807 335
5843 15
50678309 32439
Satellite: ISS
Catalog Number: 25544
Epoch time: 13153
54484779 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 180
9510 deg
Eccentricity:
0010507
Arg of perigee: 24
5807 deg
Mean anomaly: 335
5843 deg
Mean motion: 15
50678309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3243
Checksum: 317
Coasting Arc #8 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2013/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2649735
69 A = 6789689
66 meter
Y = 4029602
87 meter E =
0016702
Z = -4790440
60 I = 51
65992
XDOT = -7025
512730 Wp = 70
20978
YDOT = -1494
918365 meter/sec RA = 175
10312 deg
ZDOT = 2641
556842 TA = 225
82941
MA = 225
96681
Ha = 229
638 n
mi
Hp = 217
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8693358
57 X = -2671327
71
Y = 13220481
87 feet Y = 3999851
49 meter
Z = -15716668
63 Z = -4803365
07
XDOT = -23049
582447 XDOT = -7021
106193
YDOT = -4904
587812 feet/sec YDOT = -1573
457639 meter/sec
ZDOT = 8666
525073 ZDOT = 2607
437721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9763563
57 X = 2975934
18
Y = 12381963
17 feet Y = 3774022
37 meter
Z = -15771148
07 Z = -4807045
93
XDOT = -11152
248508 XDOT = -3399
205345
YDOT = 19597
094271 feet/sec YDOT = 5973
194334 meter/sec
ZDOT = 8524
201497 ZDOT = 2598
176616
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 13154
51153368
00016717 00000-0 10270-3 0 9070
2 25544 51
6475 176
1577 0010548 27
6194 332
5515 15
50661393 32582
Satellite: ISS
Catalog Number: 25544
Epoch time: 13154
51153368 = yrday
fracday
Element set: 907
Inclination: 51
6475 deg
RA of node: 176
1577 deg
Eccentricity:
0010548
Arg of perigee: 27
6194 deg
Mean anomaly: 332
5515 deg
Mean motion: 15
50661393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 316
Coasting Arc #9 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2013/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2991122
42 A = 6790659
42 meter
Y = -4119069
47 meter E =
0018550
Z = 4489094
35 I = 51
69252
XDOT = 6809
429694 Wp = 48
59040
YDOT = 1404
730206 meter/sec RA = 170
14316 deg
ZDOT = -3227
589328 TA = 73
96330
MA = 73
75909
Ha = 229
611 n
mi
Hp = 217
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9813393
76 X = 3015153
34
Y = -13514007
45 feet Y = -4085486
89 meter
Z = 14727999
83 Z = 4503683
15
XDOT = 22340
648604 XDOT = 6808
894567
YDOT = 4608
694901 feet/sec YDOT = 1480
874841 meter/sec
ZDOT = -10589
203832 ZDOT = -3194
510458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9911958
73 X = -3021165
02
Y = -13374238
79 feet Y = -4076467
98 meter
Z = 14789451
79 Z = 4507824
91
XDOT = 10234
583987 XDOT = 3119
501199
YDOT = -19216
806620 feet/sec YDOT = -5857
282658 meter/sec
ZDOT = -10451
201065 ZDOT = -3185
526085
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 13155
54265003
00016717 00000-0 10270-3 0 9085
2 25544 51
6458 171
0435 0010603 31
6701 328
5086 15
50723520 32748
Satellite: ISS
Catalog Number: 25544
Epoch time: 13155
54265003 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 171
0435 deg
Eccentricity:
0010603
Arg of perigee: 31
6701 deg
Mean anomaly: 328
5086 deg
Mean motion: 15
50723520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 277
Coasting Arc #10 (Orbit 3288)
---------------------------------------
Vector Time (GMT): 2013/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3242664
45 A = 6791861
75 meter
Y = 4267907
05 meter E =
0014779
Z = -4178840
98 I = 51
72676
XDOT = -6545
468029 Wp = 66
14059
YDOT = -1323
990627 meter/sec RA = 165
18772 deg
ZDOT = 3743
195903 TA = 242
30643
MA = 242
45645
Ha = 229
740 n
mi
Hp = 217
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10638662
91 X = -3269848
15
Y = 14002319
71 feet Y = 4231493
98 meter
Z = -13710108
20 Z = -4194659
34
XDOT = -21474
632642 XDOT = -6548
360083
YDOT = -4343
801271 feet/sec YDOT = -1397
202749 meter/sec
ZDOT = 12280
826455 ZDOT = 3711
391004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10368770
44 X = 3160401
23
Y = 14138725
82 feet Y = 4309483
63 meter
Z = -13776726
90 Z = -4199146
36
XDOT = -9334
008532 XDOT = -2845
005801
YDOT = 18630
403893 feet/sec YDOT = 5678
547107 meter/sec
ZDOT = 12148
121822 ZDOT = 3702
747531
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 13156
50930940
00016717 00000-0 10270-3 0 9092
2 25544 51
6461 166
2503 0010636 34
8283 325
3562 15
50704380 32893
Satellite: ISS
Catalog Number: 25544
Epoch time: 13156
50930940 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 166
2503 deg
Eccentricity:
0010636
Arg of perigee: 34
8283 deg
Mean anomaly: 325
3562 deg
Mean motion: 15
50704380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3289
Checksum: 299
Coasting Arc #11 (Orbit 3304)
---------------------------------------
Vector Time (GMT): 2013/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3526565
03 A = 6793074
02 meter
Y = -4416849
93 meter E =
0020486
Z = 3761014
98 I = 51
75936
XDOT = 6232
817424 Wp = 62
07379
YDOT = 1326
753951 meter/sec RA = 160
23335 deg
ZDOT = -4259
075116 TA = 73
06917
MA = 72
84469
Ha = 229
700 n
mi
Hp = 216
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11570095
23 X = 3557422
87
Y = -14490977
46 feet Y = -4377241
58 meter
Z = 12339287
99 Z = 3778221
35
XDOT = 20448
876064 XDOT = 6238
207830
YDOT = 4352
867294 feet/sec YDOT = 1396
483908 meter/sec
ZDOT = -13973
343558 ZDOT = -4228
783005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10825695
33 X = -3299671
94
Y = -14995553
97 feet Y = -4570644
85 meter
Z = 12411738
04 Z = 3783097
76
XDOT = 8669
500964 XDOT = 2642
463894
YDOT = -17792
944933 feet/sec YDOT = -5423
289616 meter/sec
ZDOT = -13846
945391 ZDOT = -4220
548955
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 13157
54039724
00016717 00000-0 10270-3 0 9109
2 25544 51
6447 161
1354 0010660 38
3443 321
8464 15
50768105 33055
Satellite: ISS
Catalog Number: 25544
Epoch time: 13157
54039724 = yrday
fracday
Element set: 910
Inclination: 51
6447 deg
RA of node: 161
1354 deg
Eccentricity:
0010660
Arg of perigee: 38
3443 deg
Mean anomaly: 321
8464 deg
Mean motion: 15
50768105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3305
Checksum: 288
Coasting Arc #12 (Orbit 3319)
---------------------------------------
Vector Time (GMT): 2013/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3705094
52 A = 6794358
25 meter
Y = 4607601
44 meter E =
0014449
Z = -3349193
39 I = 51
79201
XDOT = -5900
210286 Wp = 56
18354
YDOT = -1350
104252 meter/sec RA = 155
28381 deg
ZDOT = 4692
177403 TA = 264
96881
MA = 265
13376
Ha = 229
816 n
mi
Hp = 216
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12155821
92 X = -3740072
69
Y = 15116802
64 feet Y = 4565973
62 meter
Z = -10988167
30 Z = -3367276
94
XDOT = -19357
645294 XDOT = -5907
468178
YDOT = -4429
475892 feet/sec YDOT = -1416
125338 meter/sec
ZDOT = 15394
282818 ZDOT = 4663
496589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11535879
94 X = 3516136
21
Y = 15541100
52 feet Y = 4736927
44 meter
Z = -11064321
83 Z = -3372405
29
XDOT = -8106
720083 XDOT = -2470
928281
YDOT = 16840
179832 feet/sec YDOT = 5132
886813 meter/sec
ZDOT = 15274
606032 ZDOT = 4655
699918
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 13158
50702975
00016717 00000-0 10270-3 0 9112
2 25544 51
6446 156
3419 0010709 42
0269 318
1701 15
50751169 33206
Satellite: ISS
Catalog Number: 25544
Epoch time: 13158
50702975 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 156
3419 deg
Eccentricity:
0010709
Arg of perigee: 42
0269 deg
Mean anomaly: 318
1701 deg
Mean motion: 15
50751169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3320
Checksum: 292
Coasting Arc #13 (Orbit 3335)
---------------------------------------
Vector Time (GMT): 2013/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3905602
84 A = 6795562
34 meter
Y = -4782600
77 meter E =
0021393
Z = 2827069
56 I = 51
82337
XDOT = 5524
114179 Wp = 75
69563
YDOT = 1471
954432 meter/sec RA = 150
33545 deg
ZDOT = -5103
944738 TA = 72
32888
MA = 72
09541
Ha = 229
774 n
mi
Hp = 216
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12813657
60 X = 3945059
39
Y = -15690947
41 feet Y = -4738705
65 meter
Z = 9275162
58 Z = 2846137
93
XDOT = 18123
734183 XDOT = 5532
037677
YDOT = 4829
246825 feet/sec YDOT = 1533
773591 meter/sec
ZDOT = -16745
225519 ZDOT = -5077
089413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12200027
86 X = -3718568
49
Y = -16126338
01 feet Y = -4915307
82 meter
Z = 9355470
88 Z = 2851547
52
XDOT = 7854
766085 XDOT = 2394
132703
YDOT = -15662
623816 feet/sec YDOT = -4773
967739 meter/sec
ZDOT = -16633
179183 ZDOT = -5069
793015
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 13159
53808858
00016717 00000-0 10270-3 0 9124
2 25544 51
6440 151
2266 0010702 44
9491 315
2524 15
50810937 33362
Satellite: ISS
Catalog Number: 25544
Epoch time: 13159
53808858 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 151
2266 deg
Eccentricity:
0010702
Arg of perigee: 44
9491 deg
Mean anomaly: 315
2524 deg
Mean motion: 15
50810937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3336
Checksum: 300
Coasting Arc #14 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2013/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3993878
34 A = 6796662
07 meter
Y = 4978003
01 meter E =
0016449
Z = -2328407
54 I = 51
85314
XDOT = -5160
175933 Wp = 48
38042
YDOT = -1618
101191 meter/sec RA = 145
39161 deg
ZDOT = 5427
122122 TA = 285
78265
MA = 285
96397
Ha = 229
859 n
mi
Hp = 216
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13103275
40 X = -4037935
78
Y = 16332030
86 feet Y = 4933094
94 meter
Z = -7639132
36 Z = -2347915
83
XDOT = -16929
711065 XDOT = -5168
062075
YDOT = -5308
730941 feet/sec YDOT = -1675
850415 meter/sec
ZDOT = 17805
518774 ZDOT = 5402
034934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13034527
11 X = 3972923
86
Y = 16348385
72 feet Y = 4982987
97 meter
Z = -7721320
41 Z = -2353458
46
XDOT = -7757
039328 XDOT = -2364
345587
YDOT = 14490
544481 feet/sec YDOT = 4416
717958 meter/sec
ZDOT = 17700
868437 ZDOT = 5395
224699
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 13160
50469364
00016717 00000-0 10270-3 0 9139
2 25544 51
6440 146
4330 0010750 49
2489 310
9594 15
50804860 33512
Satellite: ISS
Catalog Number: 25544
Epoch time: 13160
50469364 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 146
4330 deg
Eccentricity:
0010750
Arg of perigee: 49
2489 deg
Mean anomaly: 310
9594 deg
Mean motion: 15
50804860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 295
Coasting Arc #15 (Orbit 3366)
---------------------------------------
Vector Time (GMT): 2013/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4098448
27 A = 6797591
44 meter
Y = -5136864
87 meter E =
0021038
Z = 1721955
05 I = 51
88160
XDOT = 4764
010833 Wp = 88
28575
YDOT = 1868
908291 meter/sec RA = 140
44904 deg
ZDOT = -5702
883643 TA = 72
91904
MA = 72
68870
Ha = 229
837 n
mi
Hp = 216
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13446352
60 X = 4147220
39
Y = -16853231
19 feet Y = -5090760
98 meter
Z = 5649458
84 Z = 1741982
72
XDOT = 15629
956801 XDOT = 4770
461338
YDOT = 6131
588882 feet/sec YDOT = 1922
219346 meter/sec
ZDOT = -18710
248171 ZDOT = -5679
724524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13751403
53 X = -4191427
80
Y = -16576308
52 feet Y = -5052458
84 meter
Z = 5733853
99 Z = 1747678
70
XDOT = 8014
008969 XDOT = 2442
669934
YDOT = -13154
800693 feet/sec YDOT = -4009
583251 meter/sec
ZDOT = -18613
678572 ZDOT = -5673
449229
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 13161
53572299
00016717 00000-0 10270-3 0 9146
2 25544 51
6443 141
3176 0010726 51
7825 308
4290 15
50849667 33678
Satellite: ISS
Catalog Number: 25544
Epoch time: 13161
53572299 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 141
3176 deg
Eccentricity:
0010726
Arg of perigee: 51
7825 deg
Mean anomaly: 308
4290 deg
Mean motion: 15
50849667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3367
Checksum: 318
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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