[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 19th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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
180/12:47:59
537 3
7 7
4 7
5
N/A 4
2 -0
2 211
0
000/00:33:29
075 -5
0 -0
7 206
8
Coasting Arc #1 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2011/168/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5066673
07 A = 6764549
17 meter
Y = 3951047
52 meter E =
0007558
Z = -2104990
05 I = 51
78516
XDOT = -4508
973095 Wp = 288
53337
YDOT = -2823
772142 meter/sec RA = 157
00088 deg
ZDOT = 5538
947117 TA = 48
12231
MA = 48
05785
Ha = 207
270 n
mi
Hp = 204
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16622943
15 X = -5100252
33
Y = 12962754
32 feet Y = 3894201
54 meter
Z = -6906135
33 Z = -2129684
51
XDOT = -14793
218815 XDOT = -4503
968912
YDOT = -9264
344299 feet/sec YDOT = -2874
167260 meter/sec
ZDOT = 18172
398679 ZDOT = 5517
054400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19520689
49 X = 5949906
16
Y = -7867796
92 feet Y = -2398104
50 meter
Z = -7006453
95 Z = -2135567
16
XDOT = 11182
969315 XDOT = 3408
569047
YDOT = 11602
009960 feet/sec YDOT = 3536
292636 meter/sec
ZDOT = 18083
704345 ZDOT = 5511
913084
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
72398002
00016717 00000-0 10270-3 0 9005
2 25544 51
6404 158
0370 0011632 258
2118 101
7735 15
62014372 999
Satellite: ISS
Catalog Number: 25544
Epoch time: 11168
72398002 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 158
0370 deg
Eccentricity:
0011632
Arg of perigee: 258
2118 deg
Mean anomaly: 101
7735 deg
Mean motion: 15
62014372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 99
Checksum: 278
Coasting Arc #2 (Orbit 114)
---------------------------------------
Vector Time (GMT): 2011/169/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6254033
86 A = 6764656
13 meter
Y = -1431699
26 meter E =
0009832
Z = -2125178
09 I = 51
81364
XDOT = -673
455295 Wp = 228
64708
YDOT = 5287
218777 meter/sec RA = 152
00411 deg
ZDOT = -5533
611064 TA = 334
93409
MA = 334
98179
Ha = 207
076 n
mi
Hp = 204
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20518483
78 X = 6279902
17
Y = -4697176
05 feet Y = -1361617
86 meter
Z = -6972369
05 Z = -2094733
79
XDOT = -2209
499000 XDOT = -705
647024
YDOT = 17346
518296 feet/sec YDOT = 5279
508712 meter/sec
ZDOT = -18154
891942 ZDOT = -5536
959985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21074117
41 X = -6423390
99
Y = -813002
23 feet Y = -247803
08 meter
Z = -6848808
10 Z = -2087516
71
XDOT = 6481
374364 XDOT = 1975
522906
YDOT = -14665
180030 feet/sec YDOT = -4469
946873 meter/sec
ZDOT = -18168
680669 ZDOT = -5537
813868
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
74761196
00016717 00000-0 10270-3 0 9017
2 25544 51
6413 152
8733 0011698 261
9499 98
0331 15
62007948 1159
Satellite: ISS
Catalog Number: 25544
Epoch time: 11169
74761196 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 152
8733 deg
Eccentricity:
0011698
Arg of perigee: 261
9499 deg
Mean anomaly: 98
0331 deg
Mean motion: 15
62007948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 115
Checksum: 320
Coasting Arc #3 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2011/170/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4026716
74 A = 6755763
41 meter
Y = -2086544
83 meter E =
0007802
Z = 5014159
33 I = 51
81055
XDOT = 5216
204532 Wp = 238
24623
YDOT = -5264
714973 meter/sec RA = 146
96855 deg
ZDOT = 1996
426670 TA = 192
41846
MA = 192
43769
Ha = 206
634 n
mi
Hp = 204
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13211012
92 X = -4027442
86
Y = -6845619
51 feet Y = -2131578
80 meter
Z = 16450653
98 Z = 4994595
75
XDOT = 17113
531928 XDOT = 5264
989764
YDOT = -17272
686918 feet/sec YDOT = -5206
111717 meter/sec
ZDOT = 6549
956268 ZDOT = 2021
884390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11242172
72 X = 3426614
24
Y = 9879752
35 feet Y = 3011348
52 meter
Z = 16371360
09 Z = 4989990
56
XDOT = -20045
445906 XDOT = -6109
851912
YDOT = 11775
052880 feet/sec YDOT = 3589
036118 meter/sec
ZDOT = 6653
446838 ZDOT = 2027
970596
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
77123331
00016717 00000-0 10270-3 0 9026
2 25544 51
6415 147
7091 0011618 266
1043 93
8785 15
62044762 1314
Satellite: ISS
Catalog Number: 25544
Epoch time: 11170
77123331 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 147
7091 deg
Eccentricity:
0011618
Arg of perigee: 266
1043 deg
Mean anomaly: 93
8785 deg
Mean motion: 15
62044762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 131
Checksum: 284
Coasting Arc #4 (Orbit 145)
---------------------------------------
Vector Time (GMT): 2011/171/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -201814
15 A = 6756892
69 meter
Y = 4851022
07 meter E =
0003835
Z = -4699616
07 I = 51
84000
XDOT = -6711
969877 Wp = 201
32921
YDOT = 2451
949135 meter/sec RA = 141
90019 deg
ZDOT = 2814
964955 TA = 96
47651
MA = 96
43284
Ha = 206
529 n
mi
Hp = 204
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -662119
91 X = -233214
62
Y = 15915426
75 feet Y = 4848590
28 meter
Z = -15418687
90 Z = -4700672
14
XDOT = -22020
898546 XDOT = -6752
563615
YDOT = 8044
452542 feet/sec YDOT = 2376
664488 meter/sec
ZDOT = 9235
449329 ZDOT = 2782
260309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4163918
98 X = 1269162
51
Y = -15370850
16 feet Y = -4685035
13 meter
Z = -15423160
90 Z = -4700979
44
XDOT = 22204
377131 XDOT = 6767
894150
YDOT = -3132
376358 feet/sec YDOT = -954
748314 meter/sec
ZDOT = 9102
651274 ZDOT = 2774
488108
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
73086895
00016717 00000-0 10270-3 0 9037
2 25544 51
6420 142
8678 0011710 270
1045 89
8770 15
62063047 1469
Satellite: ISS
Catalog Number: 25544
Epoch time: 11171
73086895 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 142
8678 deg
Eccentricity:
0011710
Arg of perigee: 270
1045 deg
Mean anomaly: 89
8770 deg
Mean motion: 15
62063047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 146
Checksum: 300
Coasting Arc #5 (Orbit 161)
---------------------------------------
Vector Time (GMT): 2011/172/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4023187
24 A = 6765573
94 meter
Y = -5255014
08 meter E =
0006190
Z = 1384232
46 I = 51
89198
XDOT = 4586
382503 Wp = 175
54776
YDOT = 1975
325833 meter/sec RA = 136
87907 deg
ZDOT = -5835
317706 TA = 349
37137
MA = 349
38444
Ha = 206
586 n
mi
Hp = 204
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13199433
19 X = 4074926
52
Y = -17240859
83 feet Y = -5209735
21 meter
Z = 4541445
07 Z = 1403902
01
XDOT = 15047
186688 XDOT = 4592
299793
YDOT = 6480
727797 feet/sec YDOT = 2026
647278 meter/sec
ZDOT = -19144
743131 ZDOT = -5813
022687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16498744
89 X = -5028817
44
Y = 14090083
29 feet Y = 4294657
39 meter
Z = 4621469
22 Z = 1408623
82
XDOT = -12435
571200 XDOT = -3790
362102
YDOT = -8316
204534 feet/sec YDOT = -2534
779142 meter/sec
ZDOT = -19054
348639 ZDOT = -5807
765465
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
75447145
00016717 00000-0 10270-3 0 9040
2 25544 51
6419 137
7041 0011628 273
3236 86
6590 15
62041582 1622
Satellite: ISS
Catalog Number: 25544
Epoch time: 11172
75447145 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 137
7041 deg
Eccentricity:
0011628
Arg of perigee: 273
3236 deg
Mean anomaly: 86
6590 deg
Mean motion: 15
62041582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 162
Checksum: 296
Coasting Arc #6 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2011/173/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5473765
55 A = 6762970
77 meter
Y = 2775299
60 meter E =
0004331
Z = 2834487
66 I = 51
90477
XDOT = -253
746288 Wp = 22
59384
YDOT = -5723
500624 meter/sec RA = 131
88608 deg
ZDOT = 5115
291257 TA = 9
60026
MA = 9
59199
Ha = 207
010 n
mi
Hp = 204
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17958548
38 X = -5518161
99
Y = 9105313
65 feet Y = 2713840
09 meter
Z = 9299500
21 Z = 2807788
74
XDOT = -832
500946 XDOT = -214
575134
YDOT = -18777
889186 feet/sec YDOT = -5726
119690 meter/sec
ZDOT = 16782
451632 ZDOT = 5114
153109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19433640
63 X = 5923373
66
Y = -5454843
69 feet Y = -1662636
36 meter
Z = 9191038
73 Z = 2801428
61
XDOT = -3108
894381 XDOT = -947
591007
YDOT = 17186
621260 feet/sec YDOT = 5238
482160 meter/sec
ZDOT = 16778
062136 ZDOT = 5113
953339
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
77806157
00016717 00000-0 10270-3 0 9056
2 25544 51
6419 132
5391 0011731 278
4591 81
5236 15
62073683 1783
Satellite: ISS
Catalog Number: 25544
Epoch time: 11173
77806157 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 132
5391 deg
Eccentricity:
0011731
Arg of perigee: 278
4591 deg
Mean anomaly: 81
5236 deg
Mean motion: 15
62073683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 178
Checksum: 313
Coasting Arc #7 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2011/174/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4024794
12 A = 6754577
02 meter
Y = 1463523
42 meter E =
0005244
Z = -5226278
20 I = 51
89624
XDOT = -3831
084956 Wp = 29
07995
YDOT = 6562
481739 meter/sec RA = 126
84543 deg
ZDOT = -1108
634201 TA = 230
32541
MA = 230
37168
Ha = 207
229 n
mi
Hp = 204
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13204705
12 X = 4033517
81
Y = 4801586
03 feet Y = 1508580
46 meter
Z = -17146582
02 Z = -5206704
47
XDOT = -12569
176365 XDOT = -3898
797631
YDOT = 21530
451898 feet/sec YDOT = 6519
261735 meter/sec
ZDOT = -3637
251316 ZDOT = -1127
409311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12253021
23 X = -3734720
87
Y = -7070983
11 feet Y = -2155235
65 meter
Z = -17067202
74 Z = -5202083
40
XDOT = 15629
685811 XDOT = 4763
928235
YDOT = -18088
365724 feet/sec YDOT = -5513
333873 meter/sec
ZDOT = -3713
720528 ZDOT = -1131
942017
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
73766675
00016717 00000-0 10270-3 0 9064
2 25544 51
6416 127
6976 0011844 281
9332 78
0497 15
62129157 1936
Satellite: ISS
Catalog Number: 25544
Epoch time: 11174
73766675 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 127
6976 deg
Eccentricity:
0011844
Arg of perigee: 281
9332 deg
Mean anomaly: 78
0497 deg
Mean motion: 15
62129157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 334
Coasting Arc #8 (Orbit 208)
---------------------------------------
Vector Time (GMT): 2011/175/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -704811
34 A = 6758308
95 meter
Y = -5201615
25 meter E =
0006458
Z = 4262527
40 I = 51
92677
XDOT = 5647
330150 Wp = 342
40972
YDOT = -3733
413944 meter/sec RA = 121
78583 deg
ZDOT = -3617
560835 TA = 144
38737
MA = 144
34426
Ha = 207
446 n
mi
Hp = 204
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2312373
17 X = -667300
06
Y = -17065666
83 feet Y = -5209287
65 meter
Z = 13984669
95 Z = 4259193
93
XDOT = 18527
986058 XDOT = 5706
231625
YDOT = -12248
733411 feet/sec YDOT = -3669
932302 meter/sec
ZDOT = -11868
637910 ZDOT = -3589
983488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -352510
66 X = -107445
25
Y = 17228807
65 feet Y = 5251340
57 meter
Z = 13971362
52 Z = 4258471
30
XDOT = -19056
282904 XDOT = -5808
355029
YDOT = 9156
040935 feet/sec YDOT = 2790
761277 meter/sec
ZDOT = -11756
549076 ZDOT = -3583
396158
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
76123559
00016717 00000-0 10270-3 0 9077
2 25544 51
6418 122
5334 0011969 285
9641 74
0197 15
62165427 2096
Satellite: ISS
Catalog Number: 25544
Epoch time: 11175
76123559 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 122
5334 deg
Eccentricity:
0011969
Arg of perigee: 285
9641 deg
Mean anomaly: 74
0197 deg
Mean motion: 15
62165427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 209
Checksum: 317
Coasting Arc #9 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2011/176/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2653088
57 A = 6766003
21 meter
Y = 6191534
46 meter E =
0012879
Z = -538311
81 I = 51
96655
XDOT = -4556
482124 Wp = 341
66785
YDOT = -1426
555767 meter/sec RA = 116
77926 deg
ZDOT = 6021
960639 TA = 12
52745
MA = 12
49547
Ha = 207
796 n
mi
Hp = 204
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8704358
82 X = -2719511
29
Y = 20313433
26 feet Y = 6161494
69 meter
Z = -1766114
86 Z = -551361
06
XDOT = -14949
088334 XDOT = -4569
445079
YDOT = -4680
301074 feet/sec YDOT = -1477
582393 meter/sec
ZDOT = 19757
088712 ZDOT = 5999
793545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11495372
52 X = 3503789
54
Y = -18869736
24 feet Y = -5751495
61 meter
Z = -1819357
00 Z = -554540
01
XDOT = 12872
398646 XDOT = 3923
507107
YDOT = 5937
308576 feet/sec YDOT = 1809
691654 meter/sec
ZDOT = 19667
175584 ZDOT = 5994
555118
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
72082310
00016717 00000-0 10270-3 0 9084
2 25544 51
6411 117
6908 0011948 289
2914 70
6951 15
62142888 2241
Satellite: ISS
Catalog Number: 25544
Epoch time: 11176
72082310 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 117
6908 deg
Eccentricity:
0011948
Arg of perigee: 289
2914 deg
Mean anomaly: 70
6951 deg
Mean motion: 15
62142888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 309
Coasting Arc #10 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2011/177/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4443603
07 A = 6760870
36 meter
Y = -3672782
90 meter E =
0007826
Z = -3531670
89 I = 51
96119
XDOT = 1393
940812 Wp = 310
21117
YDOT = 6046
547774 meter/sec RA = 111
78608 deg
ZDOT = -4522
766474 TA = 271
33779
MA = 271
42745
Ha = 208
059 n
mi
Hp = 204
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14578750
24 X = 4501498
83
Y = -12049812
65 feet Y = -3622767
59 meter
Z = -11586846
76 Z = -3509943
74
XDOT = 4573
296626 XDOT = 1348
194363
YDOT = 19837
755165 feet/sec YDOT = 6061
880556 meter/sec
ZDOT = -14838
472683 ZDOT = -4516
104918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16041886
01 X = -4889566
85
Y = 10121058
29 feet Y = 3084898
57 meter
Z = -11498479
63 Z = -3504736
59
XDOT = -1403
309844 XDOT = -427
728841
YDOT = -19094
946965 feet/sec YDOT = -5820
139835 meter/sec
ZDOT = -14811
711245 ZDOT = -4514
609588
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
74437165
00016717 00000-0 10270-3 0 9090
2 25544 51
6403 112
5265 0012027 292
7621 67
2265 15
62144318 2403
Satellite: ISS
Catalog Number: 25544
Epoch time: 11177
74437165 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 112
5265 deg
Eccentricity:
0012027
Arg of perigee: 292
7621 deg
Mean anomaly: 67
2265 deg
Mean motion: 15
62144318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 287
Coasting Arc #11 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2011/178/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4017153
89 A = 6754087
68 meter
Y = -1107582
27 meter E =
0009736
Z = 5322416
39 I = 51
94919
XDOT = 2143
425141 Wp = 301
97517
YDOT = -7370
039237 meter/sec RA = 106
73736 deg
ZDOT = 89
231154 TA = 147
20921
MA = 147
14875
Ha = 208
374 n
mi
Hp = 204
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13179638
75 X = -4030325
48
Y = -3633800
09 feet Y = -1152579
05 meter
Z = 17461996
02 Z = 5302868
86
XDOT = 7032
234714 XDOT = 2225
245568
YDOT = -24179
918755 feet/sec YDOT = -7345
612686 meter/sec
ZDOT = 292
753130 ZDOT = 99
841441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12813468
68 X = 3905545
25
Y = 5048333
29 feet Y = 1538731
99 meter
Z = 17382693
61 Z = 5298245
01
XDOT = -9236
046585 XDOT = -2815
146999
YDOT = 22343
369028 feet/sec YDOT = 6810
258880 meter/sec
ZDOT = 336
182176 ZDOT = 102
468327
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
76790980
00016717 00000-0 10270-3 0 9102
2 25544 51
6407 107
3612 0011935 296
7654 63
2281 15
62153961 2567
Satellite: ISS
Catalog Number: 25544
Epoch time: 11178
76790980 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 107
3612 deg
Eccentricity:
0011935
Arg of perigee: 296
7654 deg
Mean anomaly: 63
2281 deg
Mean motion: 15
62153961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 313
Coasting Arc #12 (Orbit 270)
---------------------------------------
Vector Time (GMT): 2011/179/17:16:26
699
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1801147
79 A = 6760300
89 meter
Y = 5390270
94 meter E =
0007071
Z = -3652109
68 I = 51
97726
XDOT = -4439
519246 Wp = 316
02784
YDOT = 4466
637687 meter/sec RA = 101
68685 deg
ZDOT = 4402
865821 TA =
63752
MA =
63662
Ha = 208
563 n
mi
Hp = 203
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5909277
53 X = 1758480
13
Y = 17684615
95 feet Y = 5410174
57 meter
Z = -11981987
15 Z = -3643462
38
XDOT = -14565
351857 XDOT = -4510
524377
YDOT = 14654
323120 feet/sec YDOT = 4416
594474 meter/sec
ZDOT = 14445
097838 ZDOT = 4381
127012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4346468
78 X = -1324803
68
Y = -18155083
71 feet Y = -5533669
51 meter
Z = -11947148
74 Z = -3641490
94
XDOT = 14601
240361 XDOT = 4450
458062
YDOT = -12943
418314 feet/sec YDOT = -3945
153902 meter/sec
ZDOT = 14356
614958 ZDOT = 4375
896239
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
72746581
00016717 00000-0 10270-3 0 9118
2 25544 51
6398 102
5181 0012002 300
0375 59
9591 15
62192476 2716
Satellite: ISS
Catalog Number: 25544
Epoch time: 11179
72746581 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 102
5181 deg
Eccentricity:
0012002
Arg of perigee: 300
0375 deg
Mean anomaly: 59
9591 deg
Mean motion: 15
62192476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 271
Checksum: 298
Coasting Arc #13 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2011/180/13:04:44
075
Vector Time (MET): N/A
Weight (LBS) : 913479
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3898239
94 A = 6761025
34 meter
Y = 1761489
79 meter E =
0002072
Z = -5235958
30 I = 51
96367
XDOT = -1847
840964 Wp = 181
64311
YDOT = 7370
440987 meter/sec RA = 97
56108 deg
ZDOT = 1101
803728 TA = 98
86631
MA = 98
84285
Ha = 210
970 n
mi
Hp = 206
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12789501
13 X = 3903688
10
Y = 5779165
97 feet Y = 1805113
73 meter
Z = -17178340
89 Z = -5217007
18
XDOT = -6062
470355 XDOT = -1935
473658
YDOT = 24181
236833 feet/sec YDOT = 7349
287116 meter/sec
ZDOT = 3614
841626 ZDOT = 1092
615500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 364644
79 X = 111143
73
Y = -14123447
70 feet Y = -4304826
86 meter
Z = -17101483
95 Z = -5212532
31
XDOT = 23628
679561 XDOT = 7202
021530
YDOT = -3729
473803 feet/sec YDOT = -1136
743615 meter/sec
ZDOT = 3577
155961 ZDOT = 1090
317137
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
55910573
00016717 00000-0 10270-3 0 9126
2 25544 51
6417 98
3244 0014219 270
1016 89
8511 15
59886370 2848
Satellite: ISS
Catalog Number: 25544
Epoch time: 11180
55910573 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 98
3244 deg
Eccentricity:
0014219
Arg of perigee: 270
1016 deg
Mean anomaly: 89
8511 deg
Mean motion: 15
59886370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 308
Coasting Arc #14 (Orbit 299)
---------------------------------------
Vector Time (GMT): 2011/181/13:04:44
075
Vector Time (MET): N/A
Weight (LBS) : 913479
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2462063
00 A = 6767631
53 meter
Y = -5280098
28 meter E =
0002055
Z = 3446371
56 I = 51
98862
XDOT = 3822
492228 Wp = 301
03727
YDOT = -4793
287051 meter/sec RA = 92
54068 deg
ZDOT = -4613
905876 TA = 198
70600
MA = 198
71355
Ha = 210
893 n
mi
Hp = 206
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8077634
52 X = -2419578
62
Y = -17323157
08 feet Y = -5307393
68 meter
Z = 11306993
31 Z = 3434513
15
XDOT = 12540
984999 XDOT = 3898
220894
YDOT = -15726
007384 feet/sec YDOT = -4750
117313 meter/sec
ZDOT = -15137
486470 ZDOT = -4595
153358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12600640
12 X = -3840675
11
Y = 14409863
58 feet Y = 4392126
42 meter
Z = 11259118
46 Z = 3431779
31
XDOT = -18422
158701 XDOT = -5615
073972
YDOT = -4343
781854 feet/sec YDOT = -1323
984709 meter/sec
ZDOT = -15061
085309 ZDOT = -4590
618802
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
58414149
00016717 00000-0 10270-3 0 9139
2 25544 51
6417 93
1705 0014194 273
9978 85
9555 15
59881033 3008
Satellite: ISS
Catalog Number: 25544
Epoch time: 11181
58414149 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 93
1705 deg
Eccentricity:
0014194
Arg of perigee: 273
9978 deg
Mean anomaly: 85
9555 deg
Mean motion: 15
59881033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 300
Checksum: 321
Coasting Arc #15 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2011/182/13:04:44
075
Vector Time (MET): N/A
Weight (LBS) : 913479
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 348431
49 A = 6772581
07 meter
Y = 6756012
58 meter E =
0011948
Z = -77358
39 I = 52
00641
XDOT = -4717
731008 Wp = 331
17695
YDOT = 316
910865 meter/sec RA = 87
55944 deg
ZDOT = 6051
610623 TA = 27
99171
MA = 27
92750
Ha = 211
068 n
mi
Hp = 206
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1143147
94 X = 273234
35
Y = 22165395
59 feet Y = 6759488
51 meter
Z = -253800
49 Z = -75847
14
XDOT = -15478
120105 XDOT = -4750
321346
YDOT = 1039
733810 feet/sec YDOT = 263
970996 meter/sec
ZDOT = 19854
365562 ZDOT = 6028
613101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19670997
68 X = 5995720
09
Y = -10279411
31 feet Y = -3133164
57 meter
Z = -248026
72 Z = -75598
55
XDOT = 6697
581801 XDOT = 2041
422933
YDOT = 12309
419788 feet/sec YDOT = 3751
911152 meter/sec
ZDOT = 19760
954124 ZDOT = 6023
138817
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 11182
54510272
00016717 00000-0 10270-3 0 9141
2 25544 51
6424 88
3375 0014350 277
8269 82
1257 15
59907419 3156
Satellite: ISS
Catalog Number: 25544
Epoch time: 11182
54510272 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 88
3375 deg
Eccentricity:
0014350
Arg of perigee: 277
8269 deg
Mean anomaly: 82
1257 deg
Mean motion: 15
59907419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 311
Coasting Arc #16 (Orbit 330)
---------------------------------------
Vector Time (GMT): 2011/183/13:04:44
075
Vector Time (MET): N/A
Weight (LBS) : 913479
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1881828
57 A = 6767955
47 meter
Y = -5591303
59 meter E =
0009869
Z = -3311242
79 I = 51
98855
XDOT = 4287
894925 Wp = 284
33623
YDOT = 4256
706378 meter/sec RA = 82
58052 deg
ZDOT = -4736
793394 TA = 294
06894
MA = 294
17216
Ha = 211
313 n
mi
Hp = 206
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6173978
23 X = 1960296
87
Y = -18344171
87 feet Y = -5569820
54 meter
Z = -10863657
44 Z = -3301911
36
XDOT = 14067
896735 XDOT = 4262
987002
YDOT = 13965
572107 feet/sec YDOT = 4304
517750 meter/sec
ZDOT = -15540
660741 ZDOT = -4716
022953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19238917
40 X = -5864022
02
Y = 2306361
55 feet Y = 702979
00 meter
Z = -10825454
05 Z = -3299598
39
XDOT = 6636
928774 XDOT = 2022
935890
YDOT = -17404
145515 feet/sec YDOT = -5304
783553 meter/sec
ZDOT = -15456
536389 ZDOT = -4711
152291
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 11183
57011974
00016717 00000-0 10270-3 0 9151
2 25544 51
6424 83
1835 0014511 281
4195 78
5331 15
59899839 3314
Satellite: ISS
Catalog Number: 25544
Epoch time: 11183
57011974 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 83
1835 deg
Eccentricity:
0014511
Arg of perigee: 281
4195 deg
Mean anomaly: 78
5331 deg
Mean motion: 15
59899839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 331
Checksum: 319
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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