[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 10th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 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
228/16:14:36
109 -4
9 9
3 9
3
N/A -5
3 0
2 224
6
000/00:29:08
217 5
9 -0
0 217
3
Coasting Arc #1 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2012/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1833631
52 A = 6775130
86 meter
Y = -3905490
60 meter E =
0003638
Z = 5220682
52 I = 51
39020
XDOT = 6297
588992 Wp = 98
25408
YDOT = 4271
813194 meter/sec RA = 220
06914 deg
ZDOT = 982
692435 TA = 342
30632
MA = 342
31898
Ha = 219
803 n
mi
Hp = 213
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6015851
46 X = 1851806
56
Y = -12813289
36 feet Y = -3884884
23 meter
Z = 17128223
49 Z = 5229634
25
XDOT = 20661
381207 XDOT = 6244
578985
YDOT = 14015
135152 feet/sec YDOT = 4341
940342 meter/sec
ZDOT = 3224
056546 ZDOT = 1013
156881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13098515
65 X = -3992427
57
Y = 5246082
45 feet Y = 1599005
93 meter
Z = 17165500
27 Z = 5232044
48
XDOT = -4982
253766 XDOT = -1518
590948
YDOT = -23411
038252 feet/sec YDOT = -7135
684459 meter/sec
ZDOT = 3349
409350 ZDOT = 1020
899970
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 12221
54996564
00016717 00000-0 10270-3 0 9003
2 25544 51
6379 220
8242 0001548 19
8769 340
2444 15
55008039 26163
Satellite: ISS
Catalog Number: 25544
Epoch time: 12221
54996564 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 220
8242 deg
Eccentricity:
0001548
Arg of perigee: 19
8769 deg
Mean anomaly: 340
2444 deg
Mean motion: 15
55008039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 310
Coasting Arc #2 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2012/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3563380
67 A = 6775301
11 meter
Y = 2549506
49 meter E =
0014461
Z = -5180579
88 I = 51
41486
XDOT = -5536
711304 Wp = 93
79352
YDOT = -5134
204441 meter/sec RA = 215
04327 deg
ZDOT = 1283
822556 TA = 188
57635
MA = 188
60109
Ha = 219
876 n
mi
Hp = 212
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11690881
47 X = -3566459
05
Y = 8364522
60 feet Y = 2509641
47 meter
Z = -16996653
13 Z = -5197897
90
XDOT = -18165
063332 XDOT = -5485
124541
YDOT = -16844
502758 feet/sec YDOT = -5195
830982 meter/sec
ZDOT = 4212
016260 ZDOT = 1257
050846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14195175
53 X = 4326689
50
Y = 1642187
40 feet Y = 500538
72 meter
Z = -17068344
32 Z = -5202431
35
XDOT = 2185
388954 XDOT = 666
106553
YDOT = 23670
233324 feet/sec YDOT = 7214
687117 meter/sec
ZDOT = 4101
964342 ZDOT = 1250
278731
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 12222
51393872
00016717 00000-0 10270-3 0 9015
2 25544 51
6379 216
0122 0001575 20
8786 339
2432 15
55012679 26315
Satellite: ISS
Catalog Number: 25544
Epoch time: 12222
51393872 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 216
0122 deg
Eccentricity:
0001575
Arg of perigee: 20
8786 deg
Mean anomaly: 339
2432 deg
Mean motion: 15
55012679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 294
Coasting Arc #3 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2012/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5057136
75 A = 6778369
32 meter
Y = -1100919
10 meter E =
0010513
Z = 4371725
99 I = 51
45060
XDOT = 4134
620317 Wp = 63
90828
YDOT = 5505
313662 meter/sec RA = 210
02385 deg
ZDOT = -3385
596560 TA = 60
49306
MA = 60
38825
Ha = 219
705 n
mi
Hp = 212
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16591656
01 X = 5047834
92
Y = -3611939
32 feet Y = -1044419
22 meter
Z = 14342933
05 Z = 4396270
49
XDOT = 13565
027286 XDOT = 4089
197793
YDOT = 18062
052697 feet/sec YDOT = 5551
295705 meter/sec
ZDOT = -11107
600263 ZDOT = -3365
621066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14762493
49 X = -4499608
02
Y = -8214551
44 feet Y = -2503795
28 meter
Z = 14444335
00 Z = 4402633
31
XDOT = 1133
119885 XDOT = 345
374941
YDOT = -21485
903272 feet/sec YDOT = -6548
903317 meter/sec
ZDOT = -11025
618104 ZDOT = -3360
608398
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 12223
54216205
00016717 00000-0 10270-3 0 9024
2 25544 51
6372 210
8783 0001624 21
5505 338
5716 15
55065606 26477
Satellite: ISS
Catalog Number: 25544
Epoch time: 12223
54216205 = yrday
fracday
Element set: 902
Inclination: 51
6372 deg
RA of node: 210
8783 deg
Eccentricity:
0001624
Arg of perigee: 21
5505 deg
Mean anomaly: 338
5716 deg
Mean motion: 15
55065606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 285
Coasting Arc #4 (Orbit 2661)
---------------------------------------
Vector Time (GMT): 2012/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6101924
76 A = 6782812
53 meter
Y = -256707
72 meter E =
0005944
Z = -2951154
97 I = 51
49214
XDOT = -2180
249402 Wp = 58
51180
YDOT = -5397
285115 meter/sec RA = 205
02019 deg
ZDOT = 4987
920519 TA = 267
70856
MA = 267
77662
Ha = 219
844 n
mi
Hp = 212
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20019438
18 X = -6084264
79
Y = -842216
94 feet Y = -324844
37 meter
Z = -9682266
96 Z = -2980754
66
XDOT = -7153
049218 XDOT = -2143
963749
YDOT = -17707
628329 feet/sec YDOT = -5421
463348 meter/sec
ZDOT = 16364
568632 ZDOT = 4977
416978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14642108
29 X = 4462914
61
Y = 13591000
09 feet Y = 4142536
83 meter
Z = -9804433
15 Z = -2988391
22
XDOT = -4977
331708 XDOT = -1517
090705
YDOT = 17112
124114 feet/sec YDOT = 5215
775430 meter/sec
ZDOT = 16321
665822 ZDOT = 4974
843743
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 12224
50610834
00016717 00000-0 10270-3 0 9038
2 25544 51
6370 206
0660 0001715 28
4578 331
6669 15
55065705 26621
Satellite: ISS
Catalog Number: 25544
Epoch time: 12224
50610834 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 206
0660 deg
Eccentricity:
0001715
Arg of perigee: 28
4578 deg
Mean anomaly: 331
6669 deg
Mean motion: 15
55065705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2662
Checksum: 293
Coasting Arc #5 (Orbit 2677)
---------------------------------------
Vector Time (GMT): 2012/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6530361
13 A = 6785946
17 meter
Y = 1485100
46 meter E =
0013572
Z = 1059121
05 I = 51
53111
XDOT = -155
853496 Wp = 116
00299
YDOT = 4918
939551 meter/sec RA = 200
03059 deg
ZDOT = -5883
552312 TA = 52
48875
MA = 52
36546
Ha = 219
806 n
mi
Hp = 212
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21425069
31 X = 6508124
17
Y = 4872376
85 feet Y = 1558002
64 meter
Z = 3474806
58 Z = 1090790
90
XDOT = -511
330366 XDOT = -182
265904
YDOT = 16138
253120 feet/sec YDOT = 4917
049292 meter/sec
ZDOT = -19302
993151 ZDOT = -5884
373360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13426877
14 X = -4092512
15
Y = -17365706
59 feet Y = -5293067
37 meter
Z = 3605431
54 Z = 1098935
53
XDOT = 9293
939572 XDOT = 2832
792782
YDOT = -11229
034009 feet/sec YDOT = -3422
609566 meter/sec
ZDOT = -19306
795764 ZDOT = -5884
711349
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 12225
53430214
00016717 00000-0 10270-3 0 9045
2 25544 51
6370 200
9315 0001771 27
0110 333
1135 15
55117145 26788
Satellite: ISS
Catalog Number: 25544
Epoch time: 12225
53430214 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 200
9315 deg
Eccentricity:
0001771
Arg of perigee: 27
0110 deg
Mean anomaly: 333
1135 deg
Mean motion: 15
55117145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2678
Checksum: 257
Coasting Arc #6 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2012/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6240231
67 A = 6785970
25 meter
Y = -2467012
43 meter E =
0014958
Z = 960155
23 I = 51
56025
XDOT = 2565
232378 Wp = 53
38268
YDOT = -4167
278920 meter/sec RA = 195
04955 deg
ZDOT = 5909
412493 TA = 317
03610
MA = 317
15283
Ha = 219
753 n
mi
Hp = 212
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20473201
02 X = -6216845
39
Y = -8093872
79 feet Y = -2536663
86 meter
Z = 3150115
58 Z = 929897
63
XDOT = 8416
116725 XDOT = 2582
934955
YDOT = -13672
174934 feet/sec YDOT = -4138
494173 meter/sec
ZDOT = 19387
836262 ZDOT = 5921
916899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11005945
02 X = 3354612
04
Y = 19086701
62 feet Y = 5817626
65 meter
Z = 3025385
98 Z = 922137
65
XDOT = -13610
083547 XDOT = -4148
353465
YDOT = 4736
743444 feet/sec YDOT = 1443
759402 meter/sec
ZDOT = 19439
814661 ZDOT = 5925
255509
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 12226
56247933
00016717 00000-0 10270-3 0 9054
2 25544 51
6367 195
7980 0001553 35
6450 324
4807 15
55162003 26943
Satellite: ISS
Catalog Number: 25544
Epoch time: 12226
56247933 = yrday
fracday
Element set: 905
Inclination: 51
6367 deg
RA of node: 195
7980 deg
Eccentricity:
0001553
Arg of perigee: 35
6450 deg
Mean anomaly: 324
4807 deg
Mean motion: 15
55162003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 311
Coasting Arc #7 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2012/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5213492
60 A = 6782892
92 meter
Y = 3246803
78 meter E =
0005129
Z = -2881874
19 I = 51
58037
XDOT = -4788
010519 Wp = 97
99978
YDOT = 3215
869951 meter/sec RA = 190
06444 deg
ZDOT = -5047
121039 TA = 114
83195
MA = 114
77860
Ha = 219
822 n
mi
Hp = 212
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17104634
52 X = 5190797
93
Y = 10652243
38 feet Y = 3304977
50 meter
Z = -9454967
82 Z = -2856602
76
XDOT = -15708
695928 XDOT = -4799
097864
YDOT = 10550
754432 feet/sec YDOT = 3162
265615 meter/sec
ZDOT = -16558
796059 ZDOT = -5070
407372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7133618
17 X = -2174326
82
Y = -18897297
39 feet Y = -5759896
25 meter
Z = -9350875
39 Z = -2850146
82
XDOT = 17426
345338 XDOT = 5311
550059
YDOT = 1649
307086 feet/sec YDOT = 502
708800 meter/sec
ZDOT = -16655
224148 ZDOT = -5076
512320
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 12227
52638340
00016717 00000-0 10270-3 0 9068
2 25544 51
6375 190
9843 0001776 33
0778 327
0486 15
55156493 27094
Satellite: ISS
Catalog Number: 25544
Epoch time: 12227
52638340 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 190
9843 deg
Eccentricity:
0001776
Arg of perigee: 33
0778 deg
Mean anomaly: 327
0486 deg
Mean motion: 15
55156493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 326
Coasting Arc #8 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2012/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3564386
32 A = 6778230
41 meter
Y = -3776774
66 meter E =
0010224
Z = 4348474
39 I = 51
59598
XDOT = 6506
778948 Wp = 100
14108
YDOT = -2164
407547 meter/sec RA = 185
06924 deg
ZDOT = 3445
014451 TA = 314
86789
MA = 314
95088
Ha = 219
748 n
mi
Hp = 212
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11694180
85 X = -3543012
21
Y = -12390992
97 feet Y = -3816514
40 meter
Z = 14266648
26 Z = 4331210
98
XDOT = 21347
699960 XDOT = 6513
763444
YDOT = -7101
074629 feet/sec YDOT = -2091
605698 meter/sec
ZDOT = 11302
540851 ZDOT = 3476
640371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2098298
41 X = 639561
36
Y = 16967860
35 feet Y = 5171803
83 meter
Z = 14195657
23 Z = 4326836
32
XDOT = -20089
839217 XDOT = -6123
382993
YDOT = -7104
864876 feet/sec YDOT = -2165
562814 meter/sec
ZDOT = 11433
335323 ZDOT = 3484
880607
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 12228
55452937
00016717 00000-0 10270-3 0 9079
2 25544 51
6380 185
8510 0001560 34
2049 325
9204 15
55208703 27254
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
55452937 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 185
8510 deg
Eccentricity:
0001560
Arg of perigee: 34
2049 deg
Mean anomaly: 325
9204 deg
Mean motion: 15
55208703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 297
Coasting Arc #9 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2012/228/16:29:10
217
Vector Time (MET): N/A
Weight (LBS) : 953457
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6148279
18 A = 6791801
35 meter
Y = -2037144
27 meter E =
0016567
Z = 2006725
61 I = 51
62521
XDOT = 3208
859926 Wp = 32
35103
YDOT = -4190
439616 meter/sec RA = 184
12984 deg
ZDOT = 5569
888530 TA = 349
82774
MA = 349
86123
Ha = 224
582 n
mi
Hp = 217
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20171519
61 X = -6134790
47
Y = -6683544
19 feet Y = -2105822
75 meter
Z = 6583745
43 Z = 1976890
91
XDOT = 10527
755664 XDOT = 3228
423101
YDOT = -13748
161470 feet/sec YDOT = -4154
446827 meter/sec
ZDOT = 18273
912499 ZDOT = 5585
524172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20769123
08 X = 6330428
71
Y = -4669978
29 feet Y = -1423409
38 meter
Z = 6460688
79 Z = 1969217
94
XDOT = -2197
570520 XDOT = -669
819495
YDOT = 15632
507321 feet/sec YDOT = 4764
788232 meter/sec
ZDOT = 18338
831817 ZDOT = 5589
675938
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 12228
74740784
00016717 00000-0 10270-3 0 9081
2 25544 51
6404 184
8897 0009748 335
0194 25
0485 15
52715699 27283
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
74740784 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 184
8897 deg
Eccentricity:
0009748
Arg of perigee: 335
0194 deg
Mean anomaly: 25
0485 deg
Mean motion: 15
52715699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 348
Coasting Arc #10 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2012/229/16:29:10
217
Vector Time (MET): N/A
Weight (LBS) : 953457
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5549184
33 A = 6789377
54 meter
Y = 2381841
57 meter E =
0007662
Z = -3112774
51 I = 51
64822
XDOT = -4419
227272 Wp = 4
40685
YDOT = 3920
015919 meter/sec RA = 179
16048 deg
ZDOT = -4872
021129 TA = 211
34310
MA = 211
38879
Ha = 224
583 n
mi
Hp = 217
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18205985
33 X = 5537258
49
Y = 7814440
85 feet Y = 2443829
28 meter
Z = -10212514
79 Z = -3085846
39
XDOT = -14498
777139 XDOT = -4439
066577
YDOT = 12860
944617 feet/sec YDOT = 3870
486384 meter/sec
ZDOT = -15984
321288 ZDOT = -4893
537314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19635305
57 X = -5984841
14
Y = 3038715
46 feet Y = 926200
47 meter
Z = -10101476
60 Z = -3078930
07
XDOT = 5633
957798 XDOT = 1717
230337
YDOT = -17100
990279 feet/sec YDOT = -5212
381837 meter/sec
ZDOT = -16073
512576 ZDOT = -4899
206633
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 12229
71280075
00016717 00000-0 10270-3 0 9092
2 25544 51
6410 180
0870 0009712 337
1260 22
9458 15
52734464 27431
Satellite: ISS
Catalog Number: 25544
Epoch time: 12229
71280075 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 180
0870 deg
Eccentricity:
0009712
Arg of perigee: 337
1260 deg
Mean anomaly: 22
9458 deg
Mean motion: 15
52734464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 297
Coasting Arc #11 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2012/230/16:29:10
217
Vector Time (MET): N/A
Weight (LBS) : 953457
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4707931
25 A = 6786487
62 meter
Y = -2732213
95 meter E =
0010435
Z = 4041140
91 I = 51
66948
XDOT = 5486
250314 Wp = 47
09733
YDOT = -3667
676342 meter/sec RA = 174
18693 deg
ZDOT = 3912
321459 TA = 2
35688
MA = 2
35197
Ha = 224
843 n
mi
Hp = 216
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15445968
66 X = -4696659
72
Y = -8963956
52 feet Y = -2784797
80 meter
Z = 13258336
33 Z = 4018297
93
XDOT = 17999
508903 XDOT = 5507
850481
YDOT = -12033
058865 feet/sec YDOT = -3606
204768 meter/sec
ZDOT = 12835
700326 ZDOT = 3939
025477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17904473
36 X = 5457283
48
Y = -920813
39 feet Y = -280663
92 meter
Z = 13164189
42 Z = 4012444
93
XDOT = -8564
036817 XDOT = -2610
318422
YDOT = 18536
965500 feet/sec YDOT = 5650
067084 meter/sec
ZDOT = 12946
308174 ZDOT = 3946
034731
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 12230
74254036
00016717 00000-0 10270-3 0 9107
2 25544 51
6413 174
9631 0009780 342
1838 17
8970 15
52757669 27594
Satellite: ISS
Catalog Number: 25544
Epoch time: 12230
74254036 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 174
9631 deg
Eccentricity:
0009780
Arg of perigee: 342
1838 deg
Mean anomaly: 17
8970 deg
Mean motion: 15
52757669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 325
Coasting Arc #12 (Orbit 2773)
---------------------------------------
Vector Time (GMT): 2012/231/16:29:10
217
Vector Time (MET): N/A
Weight (LBS) : 953457
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3723518
24 A = 6783740
11 meter
Y = 3112427
25 meter E =
0015134
Z = -4752385
04 I = 51
69071
XDOT = -6306
657751 Wp = 30
83605
YDOT = 3385
532798 meter/sec RA = 169
21037 deg
ZDOT = -2715
202327 TA = 212
24591
MA = 212
33853
Ha = 224
811 n
mi
Hp = 216
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12216267
20 X = 3711523
32
Y = 10211375
48 feet Y = 3153998
63 meter
Z = -15591814
45 Z = -4734325
96
XDOT = -20691
134355 XDOT = -6330
857136
YDOT = 11107
391071 feet/sec YDOT = 3314
872378 meter/sec
ZDOT = -8908
144117 ZDOT = -2745
898221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15914144
24 X = -4850631
17
Y = -1600851
37 feet Y = -487939
50 meter
Z = -15517452
73 Z = -4729719
59
XDOT = 10807
361193 XDOT = 3294
083692
YDOT = -19573
092878 feet/sec YDOT = -5965
878709 meter/sec
ZDOT = -9035
228896 ZDOT = -2753
937767
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 12231
70790566
00016717 00000-0 10270-3 0 9118
2 25544 51
6411 170
1601 0009852 344
4468 15
6380 15
52803909 27748
Satellite: ISS
Catalog Number: 25544
Epoch time: 12231
70790566 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 170
1601 deg
Eccentricity:
0009852
Arg of perigee: 344
4468 deg
Mean anomaly: 15
6380 deg
Mean motion: 15
52803909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2774
Checksum: 300
Coasting Arc #13 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2012/232/16:29:10
217
Vector Time (MET): N/A
Weight (LBS) : 953457
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2575167
58 A = 6781828
41 meter
Y = -3526472
65 meter E =
0007246
Z = 5186067
52 I = 51
71442
XDOT = 6901
147414 Wp = 14
15056
YDOT = -3058
830888 meter/sec RA = 164
23063 deg
ZDOT = 1353
289962 TA = 62
89456
MA = 62
82066
Ha = 224
962 n
mi
Hp = 216
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8448712
54 X = -2560734
87
Y = -11569792
15 feet Y = -3555188
76 meter
Z = 17014657
22 Z = 5173592
91
XDOT = 22641
559757 XDOT = 6928
265090
YDOT = -10035
534411 feet/sec YDOT = -2981
506256 meter/sec
ZDOT = 4439
927697 ZDOT = 1386
881049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13634389
67 X = 4155761
97
Y = 4591950
90 feet Y = 1399626
63 meter
Z = 16963395
88 Z = 5170443
06
XDOT = -12466
058256 XDOT = -3799
654556
YDOT = 20177
326282 feet/sec YDOT = 6150
049051 meter/sec
ZDOT = 4578
957547 ZDOT = 1395
666260
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 12232
73761612
00016717 00000-0 10270-3 0 9123
2 25544 51
6413 165
0365 0009782 348
8075 11
2858 15
52809309 27904
Satellite: ISS
Catalog Number: 25544
Epoch time: 12232
73761612 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 165
0365 deg
Eccentricity:
0009782
Arg of perigee: 348
8075 deg
Mean anomaly: 11
2858 deg
Mean motion: 15
52809309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 311
Coasting Arc #14 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2012/233/16:29:10
217
Vector Time (MET): N/A
Weight (LBS) : 953457
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1408396
31 A = 6781055
36 meter
Y = 3962321
94 meter E =
0016541
Z = -5331239
03 I = 51
74020
XDOT = -7182
443421 Wp = 54
67561
YDOT = 2651
468355 meter/sec RA = 159
24978 deg
ZDOT = 82
706476 TA = 216
05675
MA = 216
16843
Ha = 224
979 n
mi
Hp = 216
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4620722
82 X = 1389881
88
Y = 12999743
90 feet Y = 3977967
66 meter
Z = -17490941
70 Z = -5324442
38
XDOT = -23564
446918 XDOT = -7211
960637
YDOT = 8699
043158 feet/sec YDOT = 2570
984766 meter/sec
ZDOT = 271
346706 ZDOT = 47
742924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11451260
42 X = -3490344
18
Y = -7757812
18 feet Y = -2364581
15 meter
Z = -17463174
04 Z = -5322775
45
XDOT = 13423
515089 XDOT = 4091
487399
YDOT = -20029
181845 feet/sec YDOT = -6104
894626 meter/sec
ZDOT = 126
667553 ZDOT = 38
608270
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 12233
70295422
00016717 00000-0 10270-3 0 9133
2 25544 51
6402 160
2326 0009838 351
6463 8
4523 15
52859225 28057
Satellite: ISS
Catalog Number: 25544
Epoch time: 12233
70295422 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 160
2326 deg
Eccentricity:
0009838
Arg of perigee: 351
6463 deg
Mean anomaly: 8
4523 deg
Mean motion: 15
52859225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 294
Coasting Arc #15 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2012/234/16:29:10
217
Vector Time (MET): N/A
Weight (LBS) : 953457
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -185057
63 A = 6781754
05 meter
Y = -4411878
38 meter E =
0012815
Z = 5147374
97 I = 51
77093
XDOT = 7203
487773 Wp = 13
79901
YDOT = -2120
071374 meter/sec RA = 154
27118 deg
ZDOT = -1545
218820 TA = 91
14196
MA = 90
99514
Ha = 225
015 n
mi
Hp = 215
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -607144
45 X = -160714
01
Y = -14474666
60 feet Y = -4413811
43 meter
Z = 16887713
17 Z = 5146535
34
XDOT = 23633
490069 XDOT = 7234
165759
YDOT = -6955
614744 feet/sec YDOT = -2039
346040 meter/sec
ZDOT = -5069
615551 ZDOT = -1510
150135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9255056
03 X = 2820941
08
Y = 11150502
66 feet Y = 3398673
21 meter
Z = 16884598
96 Z = 5146425
76
XDOT = -13940
046947 XDOT = -4248
926309
YDOT = 19091
669536 feet/sec YDOT = 5819
140875 meter/sec
ZDOT = -4924
531989 ZDOT = -1500
997350
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 12234
73263394
00016717 00000-0 10270-3 0 9141
2 25544 51
6403 155
1090 0009799 354
9379 5
1672 15
52875525 28215
Satellite: ISS
Catalog Number: 25544
Epoch time: 12234
73263394 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 155
1090 deg
Eccentricity:
0009799
Arg of perigee: 354
9379 deg
Mean anomaly: 5
1672 deg
Mean motion: 15
52875525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 320
Coasting Arc #16 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2012/235/16:29:10
217
Vector Time (MET): N/A
Weight (LBS) : 953457
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -923802
37 A = 6783635
33 meter
Y = 4829957
86 meter E =
0011594
Z = -4678438
22 I = 51
80285
XDOT = -6938
305468 Wp = 57
90930
YDOT = 1468
681467 meter/sec RA = 149
29616 deg
ZDOT = 2897
537813 TA = 240
80014
MA = 240
91617
Ha = 225
107 n
mi
Hp = 215
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3030847
67 X = -955016
55
Y = 15846318
44 feet Y = 4819452
64 meter
Z = -15349206
77 Z = -4683001
99
XDOT = -22763
469382 XDOT = -6968
288448
YDOT = 4818
508749 feet/sec YDOT = 1390
925474 meter/sec
ZDOT = 9506
357654 ZDOT = 2863
759036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7408264
00 X = -2258038
87
Y = -14311463
93 feet Y = -4362134
21 meter
Z = -15368461
83 Z = -4684307
17
XDOT = 14013
672762 XDOT = 4271
367458
YDOT = -17272
941016 feet/sec YDOT = -5264
792422 meter/sec
ZDOT = 9366
643425 ZDOT = 2854
952916
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 12235
69794518
00016717 00000-0 10270-3 0 9155
2 25544 51
6387 150
3042 0009780 358
4760 1
6360 15
52893783 28360
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
69794518 = yrday
fracday
Element set: 915
Inclination: 51
6387 deg
RA of node: 150
3042 deg
Eccentricity:
0009780
Arg of perigee: 358
4760 deg
Mean anomaly: 1
6360 deg
Mean motion: 15
52893783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 329
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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