[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 17th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
168/16:34:22
400 4
2 9
4 9
7
N/A 6
3 -2
1 207
3
000/00:26:44
799 -6
0 -0
1 204
6
Coasting Arc #1 (Orbit 68)
---------------------------------------
Vector Time (GMT): 2011/166/18:14:28
793
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -614969
22 A = 6747604
74 meter
Y = -4150117
78 meter E =
0012165
Z = 5294402
04 I = 51
69759
XDOT = 7522
537411 Wp = 295
64727
YDOT = -1503
895170 meter/sec RA = 166
92184 deg
ZDOT = -300
463740 TA = 157
23834
MA = 157
18436
Ha = 204
720 n
mi
Hp = 199
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2017615
55 X = -594235
28
Y = -13615871
99 feet Y = -4156879
87 meter
Z = 17370085
44 Z = 5291464
06
XDOT = 24680
240850 XDOT = 7540
254757
YDOT = -4934
039273 feet/sec YDOT = -1419
674466 meter/sec
ZDOT = -985
773426 ZDOT = -263
876592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1289689
21 X = 393097
27
Y = 13718882
37 feet Y = 4181515
34 meter
Z = 17358328
81 Z = 5290818
62
XDOT = -23939
751465 XDOT = -7296
836247
YDOT = 3329
202762 feet/sec YDOT = 1014
741002 meter/sec
ZDOT = -837
353726 ZDOT = -255
225416
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 11166
80753132
00016717 00000-0 10270-3 0 9001
2 25544 51
6433 167
7367 0014228 289
3124 70
6495 15
64409377 699
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
80753132 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 167
7367 deg
Eccentricity:
0014228
Arg of perigee: 289
3124 deg
Mean anomaly: 70
6495 deg
Mean motion: 15
64409377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 69
Checksum: 314
Coasting Arc #2 (Orbit 83)
---------------------------------------
Vector Time (GMT): 2011/167/18:14:28
793
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4779932
62 A = 6756231
27 meter
Y = 3870809
37 meter E =
0011875
Z = -2777033
08 I = 51
75675
XDOT = -5093
554833 Wp = 311
77740
YDOT = -2595
551022 meter/sec RA = 161
84470 deg
ZDOT = 5143
026468 TA = 16
62535
MA = 16
58646
Ha = 204
954 n
mi
Hp = 199
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15682193
63 X = -4809371
27
Y = 12699505
81 feet Y = 3817193
21 meter
Z = -9111000
93 Z = -2800324
58
XDOT = -16711
137904 XDOT = -5089
136020
YDOT = -8515
587342 feet/sec YDOT = -2652
486549 meter/sec
ZDOT = 16873
446416 ZDOT = 5118
292378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16166678
88 X = 4927603
72
Y = -12004756
86 feet Y = -3659049
89 meter
Z = -9205611
85 Z = -2805870
49
XDOT = 15549
008628 XDOT = 4739
337830
YDOT = 8061
671404 feet/sec YDOT = 2457
197444 meter/sec
ZDOT = 16773
231730 ZDOT = 5112
481031
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 11167
76573378
00016717 00000-0 10270-3 0 9010
2 25544 51
6441 162
8855 0014147 293
1196 66
8471 15
64406456 841
Satellite: ISS
Catalog Number: 25544
Epoch time: 11167
76573378 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 162
8855 deg
Eccentricity:
0014147
Arg of perigee: 293
1196 deg
Mean anomaly: 66
8471 deg
Mean motion: 15
64406456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 84
Checksum: 325
Coasting Arc #3 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2011/168/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5581919
61 A = 6760563
12 meter
Y = 825478
96 meter E =
0005856
Z = -3717749
29 I = 51
77028
XDOT = -3642
340443 Wp = 258
58281
YDOT = 5216
261377 meter/sec RA = 157
14484 deg
ZDOT = -4305
909607 TA = 325
87573
MA = 325
91336
Ha = 207
277 n
mi
Hp = 204
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18313384
54 X = 5590334
03
Y = 2708264
30 feet Y = 887947
11 meter
Z = -12197340
18 Z = -3690612
03
XDOT = -11949
935836 XDOT = -3679
481880
YDOT = 17113
718429 feet/sec YDOT = 5175
323641 meter/sec
ZDOT = -14127
000023 ZDOT = -4323
693156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15822785
25 X = -4822784
94
Y = -9748158
25 feet Y = -2971238
63 meter
Z = -12087296
39 Z = -3684207
94
XDOT = 16947
521802 XDOT = 5165
604645
YDOT = -9883
093734 feet/sec YDOT = -3012
366970 meter/sec
ZDOT = -14199
334430 ZDOT = -4327
957134
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 11168
72397793
00016717 00000-0 10270-3 0 9023
2 25544 51
6392 158
0361 0011551 258
7345 101
2514 15
62056834 991
Satellite: ISS
Catalog Number: 25544
Epoch time: 11168
72397793 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 158
0361 deg
Eccentricity:
0011551
Arg of perigee: 258
7345 deg
Mean anomaly: 101
2514 deg
Mean motion: 15
62056834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 99
Checksum: 308
Coasting Arc #4 (Orbit 114)
---------------------------------------
Vector Time (GMT): 2011/169/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1792232
02 A = 6754266
25 meter
Y = -3782293
65 meter E =
0009290
Z = 5309046
08 I = 51
77710
XDOT = 6841
148516 Wp = 262
35886
YDOT = -3475
203652 meter/sec RA = 152
08304 deg
ZDOT = -167
836526 TA = 189
22766
MA = 189
24474
Ha = 206
842 n
mi
Hp = 204
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5880026
31 X = -1775594
52
Y = -12409099
92 feet Y = -3802243
34 meter
Z = 17418130
19 Z = 5300379
32
XDOT = 22444
712980 XDOT = 6880
315772
YDOT = -11401
586786 feet/sec YDOT = -3398
482750 meter/sec
ZDOT = -550
644771 ZDOT = -134
508105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 834914
80 X = 254482
03
Y = 13750706
01 feet Y = 4191215
19 meter
Z = 17383116
26 Z = 5298373
84
XDOT = -24091
499728 XDOT = -7343
089117
YDOT = 1981
743804 feet/sec YDOT = 604
035512 meter/sec
ZDOT = -415
305403 ZDOT = -126
585087
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 11169
74758553
00016717 00000-0 10270-3 0 9032
2 25544 51
6392 152
8718 0011710 262
5611 97
4215 15
62093245 1155
Satellite: ISS
Catalog Number: 25544
Epoch time: 11169
74758553 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 152
8718 deg
Eccentricity:
0011710
Arg of perigee: 262
5611 deg
Mean anomaly: 97
4215 deg
Mean motion: 15
62093245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 115
Checksum: 301
Coasting Arc #5 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2011/170/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2771794
43 A = 6761000
82 meter
Y = 5075911
28 meter E =
0006541
Z = -3497521
47 I = 51
82689
XDOT = -6188
237018 Wp = 259
75708
YDOT = -242
880110 meter/sec RA = 147
02512 deg
ZDOT = 4543
377899 TA = 59
07627
MA = 59
01198
Ha = 206
511 n
mi
Hp = 204
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9093813
74 X = -2811358
15
Y = 16653252
22 feet Y = 5044694
68 meter
Z = -11474807
96 Z = -3511082
03
XDOT = -20302
614888 XDOT = -6207
131763
YDOT = -796
850755 feet/sec YDOT = -312
187037 meter/sec
ZDOT = 14906
095470 ZDOT = 4513
269923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14454784
16 X = 4405818
21
Y = -12239987
47 feet Y = -3730748
18 meter
Z = -11530021
56 Z = -3514350
57
XDOT = 17818
805451 XDOT = 5431
171902
YDOT = 7091
042303 feet/sec YDOT = 2161
349694 meter/sec
ZDOT = 14783
949720 ZDOT = 4506
147875
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 11170
70720989
00016717 00000-0 10270-3 0 9043
2 25544 51
6401 148
0299 0011589 266
2399 93
7433 15
62087476 1302
Satellite: ISS
Catalog Number: 25544
Epoch time: 11170
70720989 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 148
0299 deg
Eccentricity:
0011589
Arg of perigee: 266
2399 deg
Mean anomaly: 93
7433 deg
Mean motion: 15
62087476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 319
Coasting Arc #6 (Orbit 145)
---------------------------------------
Vector Time (GMT): 2011/171/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5568180
97 A = 6766239
17 meter
Y = -3793167
04 meter E =
0009476
Z = -555665
53 I = 51
86931
XDOT = 2267
705187 Wp = 207
90629
YDOT = 4214
043611 meter/sec RA = 142
02454 deg
ZDOT = -6009
430544 TA = 338
09173
MA = 338
13222
Ha = 206
505 n
mi
Hp = 204
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18268310
28 X = 5612882
35
Y = -12444773
74 feet Y = -3730650
24 meter
Z = -1823049
62 Z = -528507
53
XDOT = 7439
977647 XDOT = 2249
606757
YDOT = 13825
602399 feet/sec YDOT = 4239
302019 meter/sec
ZDOT = -19715
979474 ZDOT = -5998
457607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21461375
23 X = -6541427
17
Y = 5329453
53 feet Y = 1624417
44 meter
Z = -1712706
09 Z = -522032
82
XDOT = -1903
297739 XDOT = -580
125151
YDOT = -14023
305019 feet/sec YDOT = -4274
303370 meter/sec
ZDOT = -19671
618595 ZDOT = -5995
909348
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 11171
73079795
00016717 00000-0 10270-3 0 9050
2 25544 51
6405 142
8659 0011651 269
5930 90
3892 15
62065796 1465
Satellite: ISS
Catalog Number: 25544
Epoch time: 11171
73079795 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 142
8659 deg
Eccentricity:
0011651
Arg of perigee: 269
5930 deg
Mean anomaly: 90
3892 deg
Mean motion: 15
62065796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 146
Checksum: 329
Coasting Arc #7 (Orbit 161)
---------------------------------------
Vector Time (GMT): 2011/172/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5235437
36 A = 6758571
97 meter
Y = 301263
98 meter E =
0002763
Z = 4266457
04 I = 51
86721
XDOT = 2576
941569 Wp = 224
26219
YDOT = -6269
966107 meter/sec RA = 137
01356 deg
ZDOT = 3604
411071 TA = 189
09046
MA = 189
09547
Ha = 206
608 n
mi
Hp = 204
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17176631
74 X = -5259142
51
Y = 988398
90 feet Y = 242585
13 meter
Z = 13997562
48 Z = 4240965
99
XDOT = 8454
532708 XDOT = 2629
352614
YDOT = -20570
754945 feet/sec YDOT = -6240
856531 meter/sec
ZDOT = 11825
495641 ZDOT = 3617
056344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16615886
13 X = 5064522
09
Y = 4776129
51 feet Y = 1455764
27 meter
Z = 13894109
58 Z = 4234924
60
XDOT = -14367
506376 XDOT = -4379
215943
YDOT = 15427
418714 feet/sec YDOT = 4702
277224 meter/sec
ZDOT = 11877
055305 ZDOT = 3620
126457
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 11172
75437405
00016717 00000-0 10270-3 0 9060
2 25544 51
6407 137
7012 0011595 274
3683 85
6149 15
62102374 1623
Satellite: ISS
Catalog Number: 25544
Epoch time: 11172
75437405 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 137
7012 deg
Eccentricity:
0011595
Arg of perigee: 274
3683 deg
Mean anomaly: 85
6149 deg
Mean motion: 15
62102374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 162
Checksum: 297
Coasting Arc #8 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2011/173/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2210578
84 A = 6754492
85 meter
Y = 3671974
45 meter E =
0002620
Z = -5222741
01 I = 51
87562
XDOT = -5698
982537 Wp = 100
32660
YDOT = 5024
700114 meter/sec RA = 131
95107 deg
ZDOT = 1120
600509 TA = 180
36245
MA = 180
36264
Ha = 206
850 n
mi
Hp = 204
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7252555
25 X = 2194724
78
Y = 12047160
27 feet Y = 3696606
39 meter
Z = -17134977
07 Z = -5212040
21
XDOT = -18697
449269 XDOT = -5760
189778
YDOT = 16485
236593 feet/sec YDOT = 4960
628279 meter/sec
ZDOT = 3676
510856 ZDOT = 1092
766893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3193445
80 X = -973362
28
Y = -13748339
17 feet Y = -4190493
78 meter
Z = -17091698
03 Z = -5209549
56
XDOT = 21951
509608 XDOT = 6690
820129
YDOT = -9528
700853 feet/sec YDOT = -2904
348020 meter/sec
ZDOT = 3563
354596 ZDOT = 1086
110481
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 11173
71396567
00016717 00000-0 10270-3 0 9071
2 25544 51
6408 132
8595 0011721 278
0103 81
9724 15
62145627 1777
Satellite: ISS
Catalog Number: 25544
Epoch time: 11173
71396567 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 132
8595 deg
Eccentricity:
0011721
Arg of perigee: 278
0103 deg
Mean anomaly: 81
9724 deg
Mean motion: 15
62145627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 177
Checksum: 312
Coasting Arc #9 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2011/174/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1686870
95 A = 6762727
35 meter
Y = -5913966
03 meter E =
0001842
Z = 2811773
31 I = 51
92249
XDOT = 5650
865500 Wp = 86
00771
YDOT = -829
294802 meter/sec RA = 126
91028 deg
ZDOT = -5131
370500 TA = 62
10633
MA = 62
08767
Ha = 207
082 n
mi
Hp = 204
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5534353
51 X = 1739217
65
Y = -19402775
70 feet Y = -5894810
04 meter
Z = 9224978
06 Z = 2820094
61
XDOT = 18539
584973 XDOT = 5684
646029
YDOT = -2720
783472 feet/sec YDOT = -765
913955 meter/sec
ZDOT = -16835
205054 ZDOT = -5103
836725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11014132
75 X = -3357107
66
Y = 16886589
62 feet Y = 5147032
52 meter
Z = 9258993
72 Z = 2822141
29
XDOT = -17372
690436 XDOT = -5295
196045
YDOT = -2156
270491 feet/sec YDOT = -657
231246 meter/sec
ZDOT = -16723
425558 ZDOT = -5097
300110
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 11174
73752062
00016717 00000-0 10270-3 0 9081
2 25544 51
6406 127
6953 0011653 281
9624 78
0226 15
62141027 1932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11174
73752062 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 127
6953 deg
Eccentricity:
0011653
Arg of perigee: 281
9624 deg
Mean anomaly: 78
0226 deg
Mean motion: 15
62141027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 297
Coasting Arc #10 (Orbit 208)
---------------------------------------
Vector Time (GMT): 2011/175/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4394038
37 A = 6765212
49 meter
Y = 4930872
17 meter E =
0010059
Z = 1434149
61 I = 51
94816
XDOT = -2777
361704 Wp = 4
30535
YDOT = -4167
657314 meter/sec RA = 121
91920 deg
ZDOT = 5826
868663 TA = 11
32761
MA = 11
30499
Ha = 207
494 n
mi
Hp = 204
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14416136
40 X = -4455816
60
Y = 16177402
12 feet Y = 4881389
77 meter
Z = 4705215
24 Z = 1412653
90
XDOT = -9112
079080 XDOT = -2758
857586
YDOT = -13673
416383 feet/sec YDOT = -4198
612685 meter/sec
ZDOT = 19117
023171 ZDOT = 5813
420703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18416036
29 X = 5613207
86
Y = -11454181
96 feet Y = -3491234
66 meter
Z = 4617759
36 Z = 1407493
05
XDOT = 4166
808260 XDOT = 1270
043158
YDOT = 14374
867889 feet/sec YDOT = 4381
459733 meter/sec
ZDOT = 19062
619343 ZDOT = 5810
286376
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 11175
76106216
00016717 00000-0 10270-3 0 9090
2 25544 51
6405 122
5296 0011856 285
9614 74
0237 15
62168536 2093
Satellite: ISS
Catalog Number: 25544
Epoch time: 11175
76106216 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 122
5296 deg
Eccentricity:
0011856
Arg of perigee: 285
9614 deg
Mean anomaly: 74
0237 deg
Mean motion: 15
62168536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 209
Checksum: 307
Coasting Arc #11 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2011/176/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4697839
97 A = 6756481
92 meter
Y = -1047736
74 meter E =
0007637
Z = -4744174
11 I = 51
93361
XDOT = -1189
948009 Wp = 353
76878
YDOT = 7076
473237 meter/sec RA = 116
90138 deg
ZDOT = -2733
326800 TA = 249
30998
MA = 249
39187
Ha = 207
767 n
mi
Hp = 204
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15412860
79 X = 4732253
17
Y = -3437456
48 feet Y = -995009
59 meter
Z = -15564875
70 Z = -4721268
53
XDOT = -3904
028901 XDOT = -1255
712037
YDOT = 23216
775711 feet/sec YDOT = 7062
799167 meter/sec
ZDOT = -8967
607611 ZDOT = -2739
266386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15862727
47 X = -4834959
33
Y = -795807
95 feet Y = -242562
26 meter
Z = -15471855
33 Z = -4715821
51
XDOT = 9809
432352 XDOT = 2989
914981
YDOT = -20208
070990 feet/sec YDOT = -6159
420038 meter/sec
ZDOT = -8992
030574 ZDOT = -2740
770919
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 11176
72062245
00016717 00000-0 10270-3 0 9102
2 25544 51
6400 117
6877 0011969 289
5574 70
4290 15
62186636 2245
Satellite: ISS
Catalog Number: 25544
Epoch time: 11176
72062245 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 117
6877 deg
Eccentricity:
0011969
Arg of perigee: 289
5574 deg
Mean anomaly: 70
4290 deg
Mean motion: 15
62186636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 311
Coasting Arc #12 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2011/177/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2723738
53 A = 6755363
90 meter
Y = -3677356
22 meter E =
0009967
Z = 4976848
10 I = 51
94356
XDOT = 4226
543529 Wp = 324
39396
YDOT = -6037
704430 meter/sec RA = 111
83904 deg
ZDOT = -2142
348775 TA = 146
40008
MA = 146
33683
Ha = 207
965 n
mi
Hp = 204
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8936150
04 X = -2706591
86
Y = -12064816
98 feet Y = -3707719
58 meter
Z = 16328241
80 Z = 4963657
26
XDOT = 13866
612628 XDOT = 4304
151337
YDOT = -19808
741569 feet/sec YDOT = -5990
006405 meter/sec
ZDOT = -7028
703331 ZDOT = -2121
628572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5752828
92 X = 1753462
25
Y = 13930533
06 feet Y = 4246026
48 meter
Z = 16274866
35 Z = 4960579
26
XDOT = -17378
957251 XDOT = -5297
106170
YDOT = 15311
998536 feet/sec YDOT = 4667
097154 meter/sec
ZDOT = -6944
314531 ZDOT = -2116
627069
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 11177
74414187
00016717 00000-0 10270-3 0 9112
2 25544 51
6405 112
5227 0011990 293
2255 66
7639 15
62226931 2401
Satellite: ISS
Catalog Number: 25544
Epoch time: 11177
74414187 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 112
5227 deg
Eccentricity:
0011990
Arg of perigee: 293
2255 deg
Mean anomaly: 66
7639 deg
Mean motion: 15
62226931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 297
Coasting Arc #13 (Orbit 254)
---------------------------------------
Vector Time (GMT): 2011/178/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -352110
90 A = 6764311
51 meter
Y = 6456467
12 meter E =
0012511
Z = -1957786
18 I = 51
98281
XDOT = -5031
521331 Wp = 329
47899
YDOT = 1434
399655 meter/sec RA = 106
81363 deg
ZDOT = 5630
198968 TA = 8
93910
MA = 8
91684
Ha = 208
309 n
mi
Hp = 204
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1155219
47 X = -414771
61
Y = 21182634
90 feet Y = 6452179
57 meter
Z = -6423183
00 Z = -1959647
87
XDOT = -16507
615916 XDOT = -5074
537614
YDOT = 4706
035612 feet/sec YDOT = 1377
892675 meter/sec
ZDOT = 18471
781391 ZDOT = 5605
651565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5996213
84 X = 1827645
98
Y = -20346567
94 feet Y = -6201633
91 meter
Z = -6431051
68 Z = -1960184
55
XDOT = 15773
021332 XDOT = 4807
616902
YDOT = -1163
919798 feet/sec YDOT = -354
762754 meter/sec
ZDOT = 18372
058953 ZDOT = 5599
803569
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 11178
70368207
00016717 00000-0 10270-3 0 9121
2 25544 51
6397 107
6797 0012065 296
9782 63
0143 15
62203666 2553
Satellite: ISS
Catalog Number: 25544
Epoch time: 11178
70368207 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 107
6797 deg
Eccentricity:
0012065
Arg of perigee: 296
9782 deg
Mean anomaly: 63
0143 deg
Mean motion: 15
62203666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 255
Checksum: 318
Coasting Arc #14 (Orbit 270)
---------------------------------------
Vector Time (GMT): 2011/179/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3037262
05 A = 6763604
12 meter
Y = -5569962
16 meter E =
0006616
Z = -2342564
82 I = 51
98794
XDOT = 3462
290860 Wp = 287
28748
YDOT = 4178
317458 meter/sec RA = 101
82863 deg
ZDOT = -5431
330240 TA = 278
79341
MA = 278
86832
Ha = 208
471 n
mi
Hp = 203
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9964770
50 X = 3110700
44
Y = -18274154
08 feet Y = -5535586
61 meter
Z = -7685580
13 Z = -2327632
46
XDOT = 11359
221983 XDOT = 3441
695150
YDOT = 13708
390610 feet/sec YDOT = 4216
920726 meter/sec
ZDOT = -17819
324934 ZDOT = -5414
559727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13706161
50 X = -4177638
03
Y = 15694424
01 feet Y = 4783660
44 meter
Z = -7624676
55 Z = -2324001
41
XDOT = -7105
851284 XDOT = -2165
863471
YDOT = -14852
939413 feet/sec YDOT = -4527
175933 meter/sec
ZDOT = -17751
445624 ZDOT = -5410
640626
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 11179
72717995
00016717 00000-0 10270-3 0 9137
2 25544 51
6393 102
5154 0012029 300
2756 59
7210 15
62217706 2715
Satellite: ISS
Catalog Number: 25544
Epoch time: 11179
72717995 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 102
5154 deg
Eccentricity:
0012029
Arg of perigee: 300
2756 deg
Mean anomaly: 59
7210 deg
Mean motion: 15
62217706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 271
Checksum: 296
Coasting Arc #15 (Orbit 286)
---------------------------------------
Vector Time (GMT): 2011/180/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4194925
72 A = 6754827
25 meter
Y = 1375887
95 meter E =
0006856
Z = 5116379
17 I = 51
96370
XDOT = -423
797427 Wp = 304
09841
YDOT = -7482
590744 meter/sec RA = 96
79784 deg
ZDOT = 1670
069650 TA = 129
90112
MA = 129
84083
Ha = 208
840 n
mi
Hp = 203
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13762879
64 X = -4234853
68
Y = 4514068
08 feet Y = 1328753
52 meter
Z = 16786020
89 Z = 5095903
61
XDOT = -1390
411506 XDOT = -348
207004
YDOT = -24549
182232 feet/sec YDOT = -7486
907574 meter/sec
ZDOT = 5479
231135 ZDOT = 1668
193034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14483298
40 X = 4414509
35
Y = -1677592
63 feet Y = -511330
23 meter
Z = 16702811
58 Z = 5091016
97
XDOT = -3592
850452 XDOT = -1095
100818
YDOT = 23287
860694 feet/sec YDOT = 7098
139940 meter/sec
ZDOT = 5471
997498 ZDOT = 1667
864837
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 11180
75066722
00016717 00000-0 10270-3 0 9148
2 25544 51
6394 97
3492 0011951 304
7340 55
2691 15
62213391 2870
Satellite: ISS
Catalog Number: 25544
Epoch time: 11180
75066722 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 97
3492 deg
Eccentricity:
0011951
Arg of perigee: 304
7340 deg
Mean anomaly: 55
2691 deg
Mean motion: 15
62213391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 287
Checksum: 302
Coasting Arc #16 (Orbit 301)
---------------------------------------
Vector Time (GMT): 2011/181/16:47:44
799
Vector Time (MET): N/A
Weight (LBS) : 913632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3430562
80 A = 6757049
15 meter
Y = 3657644
46 meter E =
0003917
Z = -4526506
78 I = 51
97334
XDOT = -2686
520513 Wp = 355
13542
YDOT = 6454
934156 meter/sec RA = 91
73751 deg
ZDOT = 3183
447334 TA = 306
58589
MA = 306
62193
Ha = 208
941 n
mi
Hp = 203
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11255127
31 X = 3411396
07
Y = 12000145
86 feet Y = 3695900
80 meter
Z = -14850744
04 Z = -4509887
13
XDOT = -8814
043677 XDOT = -2773
965614
YDOT = 21177
605499 feet/sec YDOT = 6424
402311 meter/sec
ZDOT = 10444
381017 ZDOT = 3170
185180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8980514
47 X = -2737260
81
Y = -13857343
67 feet Y = -4223718
35 meter
Z = -14783449
40 Z = -4505995
38
XDOT = 11558
831440 XDOT = 3523
131823
YDOT = -18562
819396 feet/sec YDOT = -5657
947352 meter/sec
ZDOT = 10390
184901 ZDOT = 3166
928358
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 11181
71017363
00016717 00000-0 10270-3 0 9153
2 25544 51
6385 92
5060 0011970 307
6637 52
3433 15
62272555 3027
Satellite: ISS
Catalog Number: 25544
Epoch time: 11181
71017363 = yrday
fracday
Element set: 915
Inclination: 51
6385 deg
RA of node: 92
5060 deg
Eccentricity:
0011970
Arg of perigee: 307
6637 deg
Mean anomaly: 52
3433 deg
Mean motion: 15
62272555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 302
Checksum: 284
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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