[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 11th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16684 06 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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
There are no maneuvers
Coasting Arc #1 (Orbit 3481)
---------------------------------------
Vector Time (GMT): 2011/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1129029
17 A = 6718351
88 meter
Y = 4098895
09 meter E =
0002676
Z = 5202283
26 I = 51
62384
XDOT = -7592
266504 Wp = 178
50630
YDOT = 891
805648 meter/sec RA = 358
90321 deg
ZDOT = 942
421439 TA = 262
49935
MA = 262
52976
Ha = 187
997 n
mi
Hp = 183
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3704163
94 X = 1057838
86
Y = 13447818
54 feet Y = 4111122
23 meter
Z = 17067858
47 Z = 5207595
41
XDOT = -24909
010839 XDOT = -7606
252683
YDOT = 2925
871549 feet/sec YDOT = 806
826061 meter/sec
ZDOT = 3091
933856 ZDOT = 905
504267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12195939
25 X = 3717322
28
Y = 6715401
60 feet Y = 2046854
41 meter
Z = 17089145
50 Z = 5208771
55
XDOT = -14662
563707 XDOT = -4469
149418
YDOT = 19118
915702 feet/sec YDOT = 5827
445506 meter/sec
ZDOT = 2942
496949 ZDOT = 896
873070
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 11129
54911480
00016717 00000-0 10270-3 0 9003
2 25544 51
6481 359
1572 0002990 252
4972 107
5865 15
74704323 34825
Satellite: ISS
Catalog Number: 25544
Epoch time: 11129
54911480 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 359
1572 deg
Eccentricity:
0002990
Arg of perigee: 252
4972 deg
Mean anomaly: 107
5865 deg
Mean motion: 15
74704323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3482
Checksum: 312
Coasting Arc #2 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2011/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6597721
02 A = 6729849
75 meter
Y = -1172888
23 meter E =
0008809
Z = -565076
36 I = 51
63189
XDOT = 1334
385888 Wp = 28
07112
YDOT = 4635
457358 meter/sec RA = 353
74759 deg
ZDOT = 6003
922226 TA = 325
77657
MA = 325
83331
Ha = 187
837 n
mi
Hp = 183
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21646066
35 X = 6613091
16
Y = -3848058
51 feet Y = -1099022
55 meter
Z = -1853925
06 Z = -532987
34
XDOT = 4377
906458 XDOT = 1253
286169
YDOT = 15208
193433 feet/sec YDOT = 4649
925577 meter/sec
ZDOT = 19697
907566 ZDOT = 6010
207869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11905852
56 X = 3628903
86
Y = -18495275
92 feet Y = -5637360
10 meter
Z = -1724014
04 Z = -525479
48
XDOT = 12699
153609 XDOT = 3870
702020
YDOT = 6351
208004 feet/sec YDOT = 1935
848200 meter/sec
ZDOT = 19723
107964 ZDOT = 6011
603308
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 11130
50101121
00016717 00000-0 10270-3 0 9015
2 25544 51
6475 354
2634 0003149 258
3558 101
7252 15
74774515 34977
Satellite: ISS
Catalog Number: 25544
Epoch time: 11130
50101121 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 354
2634 deg
Eccentricity:
0003149
Arg of perigee: 258
3558 deg
Mean anomaly: 101
7252 deg
Mean motion: 15
74774515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 286
Coasting Arc #3 (Orbit 3512)
---------------------------------------
Vector Time (GMT): 2011/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1168367
66 A = 6717721
20 meter
Y = -4024112
45 meter E =
0011819
Z = -5260789
45 I = 51
56026
XDOT = 7482
796959 Wp = 88
74100
YDOT = -1761
971686 meter/sec RA = 348
61034 deg
ZDOT = -314
426982 TA = 178
27024
MA = 178
26615
Ha = 187
653 n
mi
Hp = 183
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3833227
23 X = -1097726
41
Y = -13202468
66 feet Y = -4036782
75 meter
Z = -17259807
90 Z = -5266293
89
XDOT = 24549
858791 XDOT = 7503
470955
YDOT = -5780
747000 feet/sec YDOT = -1678
178905 meter/sec
ZDOT = -1031
584587 ZDOT = -278
025307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12322341
34 X = -3755849
64
Y = -6032936
93 feet Y = -1838839
18 meter
Z = -17281879
36 Z = -5267516
83
XDOT = 11641
057627 XDOT = 3548
194365
YDOT = -21247
427532 feet/sec YDOT = -6476
215912 meter/sec
ZDOT = -884
197305 ZDOT = -269
503339
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 11131
51632990
00016717 00000-0 10270-3 0 9021
2 25544 51
6466 349
0429 0003225 263
3066 96
7723 15
74842630 35135
Satellite: ISS
Catalog Number: 25544
Epoch time: 11131
51632990 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 349
0429 deg
Eccentricity:
0003225
Arg of perigee: 263
3066 deg
Mean anomaly: 96
7723 deg
Mean motion: 15
74842630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3513
Checksum: 300
Coasting Arc #4 (Orbit 3528)
---------------------------------------
Vector Time (GMT): 2011/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6453384
50 A = 6729714
66 meter
Y = 1887348
07 meter E =
0010287
Z = -34871
31 I = 51
57116
XDOT = -1317
828795 Wp = 149
05736
YDOT = -4602
861920 meter/sec RA = 343
46222 deg
ZDOT = -6034
166194 TA = 31
32196
MA = 31
26072
Ha = 187
558 n
mi
Hp = 183
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21172521
34 X = -6473840
16
Y = 6192086
83 feet Y = 1815068
03 meter
Z = -114407
18 Z = -66271
69
XDOT = -4323
585287 XDOT = -1236
947709
YDOT = -15101
253020 feet/sec YDOT = -4617
146374 meter/sec
ZDOT = -19797
133183 ZDOT = -6040
371841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9172657
30 X = -2795825
94
Y = 20060775
07 feet Y = 6114524
24 meter
Z = -241557
05 Z = -73626
59
XDOT = -12708
211442 XDOT = -3873
462847
YDOT = -6034
579865 feet/sec YDOT = -1839
339943 meter/sec
ZDOT = -19822
013315 ZDOT = -6041
749658
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 11132
53161113
00016717 00000-0 10270-3 0 9039
2 25544 51
6468 343
8238 0003302 265
9806 94
0980 15
74864943 35297
Satellite: ISS
Catalog Number: 25544
Epoch time: 11132
53161113 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 343
8238 deg
Eccentricity:
0003302
Arg of perigee: 265
9806 deg
Mean anomaly: 94
0980 deg
Mean motion: 15
74864943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3529
Checksum: 310
Coasting Arc #5 (Orbit 3544)
---------------------------------------
Vector Time (GMT): 2011/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1122383
41 A = 6717508
43 meter
Y = 4044144
89 meter E =
0001307
Z = 5245819
36 I = 51
50073
XDOT = -7259
779575 Wp = 317
35705
YDOT = 2541
248894 meter/sec RA = 338
30763 deg
ZDOT = -404
944915 TA = 136
49999
MA = 136
48969
Ha = 187
404 n
mi
Hp = 183
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3682360
28 X = 1051594
08
Y = 13268191
89 feet Y = 4056300
18 meter
Z = 17210693
45 Z = 5251100
07
XDOT = -23818
174459 XDOT = -7285
689569
YDOT = 8337
430754 feet/sec YDOT = 2459
920765 meter/sec
ZDOT = -1328
559432 ZDOT = -440
276199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12476432
45 X = 3802816
61
Y = 5763190
06 feet Y = 1756620
33 meter
Z = 17231858
17 Z = 5252270
37
XDOT = -8451
886934 XDOT = -2576
135137
YDOT = 22705
931292 feet/sec YDOT = 6920
767858 meter/sec
ZDOT = -1471
640405 ZDOT = -448
555995
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 11133
54685220
00016717 00000-0 10270-3 0 9042
2 25544 51
6461 338
6028 0003381 271
1963 88
8813 15
74930310 35455
Satellite: ISS
Catalog Number: 25544
Epoch time: 11133
54685220 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 338
6028 deg
Eccentricity:
0003381
Arg of perigee: 271
1963 deg
Mean anomaly: 88
8813 deg
Mean motion: 15
74930310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3545
Checksum: 301
Coasting Arc #6 (Orbit 3560)
---------------------------------------
Vector Time (GMT): 2011/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6194721
49 A = 6729092
99 meter
Y = -2518849
72 meter E =
0011139
Z = 690261
42 I = 51
51104
XDOT = 1239
681531 Wp = 40
05390
YDOT = 4699
118537 meter/sec RA = 333
16501 deg
ZDOT = 5977
316764 TA = 327
48365
MA = 327
55221
Ha = 187
303 n
mi
Hp = 183
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20323889
39 X = 6219074
12
Y = -8263942
64 feet Y = -2449440
44 meter
Z = 2264637
21 Z = 720414
92
XDOT = 4067
196625 XDOT = 1158
005778
YDOT = 15417
055566 feet/sec YDOT = 4712
524563 meter/sec
ZDOT = 19610
619306 ZDOT = 5983
140971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6323901
27 X = 1927525
11
Y = -20995081
51 feet Y = -6399300
84 meter
Z = 2386762
38 Z = 727485
17
XDOT = 12947
722632 XDOT = 3946
465858
YDOT = 6147
876043 feet/sec YDOT = 1873
872618 meter/sec
ZDOT = 19633
948050 ZDOT = 5984
427366
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 11134
56205402
00016717 00000-0 10270-3 0 9056
2 25544 51
6448 333
3811 0003477 275
6115 84
4652 15
75004749 35616
Satellite: ISS
Catalog Number: 25544
Epoch time: 11134
56205402 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 333
3811 deg
Eccentricity:
0003477
Arg of perigee: 275
6115 deg
Mean anomaly: 84
4652 deg
Mean motion: 15
75004749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3561
Checksum: 296
Coasting Arc #7 (Orbit 3575)
---------------------------------------
Vector Time (GMT): 2011/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1034337
61 A = 6717564
33 meter
Y = -4196118
76 meter E =
0010816
Z = -5152281
09 I = 51
44470
XDOT = 6901
919757 Wp = 99
31783
YDOT = -3181
053049 meter/sec RA = 327
99189 deg
ZDOT = 1205
553048 TA = 182
23698
MA = 182
24182
Ha = 187
240 n
mi
Hp = 183
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3393496
11 X = -962309
62
Y = -13766793
83 feet Y = -4207282
34 meter
Z = -16903809
36 Z = -5157131
27
XDOT = 22644
093692 XDOT = 6931
121463
YDOT = -10436
525752 feet/sec YDOT = -3103
708382 meter/sec
ZDOT = 3955
226535 ZDOT = 1239
153960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12884243
01 X = -3927117
27
Y = -5863455
86 feet Y = -1787181
35 meter
Z = -16923219
74 Z = -5158197
38
XDOT = 5239
965212 XDOT = 1597
141397
YDOT = -23318
659133 feet/sec YDOT = -7107
527304 meter/sec
ZDOT = 4091
330454 ZDOT = 1247
037522
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 11135
51377061
00016717 00000-0 10270-3 0 9064
2 25544 51
6437 328
4855 0003438 279
1472 80
9302 15
75070064 35761
Satellite: ISS
Catalog Number: 25544
Epoch time: 11135
51377061 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 328
4855 deg
Eccentricity:
0003438
Arg of perigee: 279
1472 deg
Mean anomaly: 80
9302 deg
Mean motion: 15
75070064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3576
Checksum: 309
Coasting Arc #8 (Orbit 3591)
---------------------------------------
Vector Time (GMT): 2011/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5846992
53 A = 6727993
93 meter
Y = 2996646
30 meter E =
0006016
Z = -1432724
31 I = 51
45530
XDOT = -1117
605369 Wp = 163
42880
YDOT = -4946
138351 meter/sec RA = 322
85935 deg
ZDOT = -5795
861532 TA = 32
37893
MA = 32
34203
Ha = 187
151 n
mi
Hp = 183
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19183046
37 X = -5873106
99
Y = 9831516
74 feet Y = 2931115
79 meter
Z = -4700539
09 Z = -1461192
73
XDOT = -3666
684283 XDOT = -1034
057853
YDOT = -16227
488028 feet/sec YDOT = -4958
168467 meter/sec
ZDOT = -19015
293739 ZDOT = -5801
088437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3650775
14 X = -1112756
26
Y = 21218442
41 feet Y = 6467381
25 meter
Z = -4815869
57 Z = -1467877
05
XDOT = -13559
493405 XDOT = -4132
933590
YDOT = -6645
114035 feet/sec YDOT = -2025
430758 meter/sec
ZDOT = -19036
187064 ZDOT = -5802
229817
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 11136
52889634
00016717 00000-0 10270-3 0 9071
2 25544 51
6438 323
2646 0003553 285
6271 74
4500 15
75139960 35927
Satellite: ISS
Catalog Number: 25544
Epoch time: 11136
52889634 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 323
2646 deg
Eccentricity:
0003553
Arg of perigee: 285
6271 deg
Mean anomaly: 74
4500 deg
Mean motion: 15
75139960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3592
Checksum: 322
Coasting Arc #9 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2011/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 933018
65 A = 6718267
01 meter
Y = 4470847
38 meter E =
0004806
Z = 4926992
09 I = 51
39821
XDOT = -6461
242262 Wp = 21
32036
YDOT = 3642
860606 meter/sec RA = 317
66808 deg
ZDOT = -2076
997381 TA = 88
89104
MA = 88
83598
Ha = 187
126 n
mi
Hp = 183
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3061084
81 X = 859020
60
Y = 14668134
45 feet Y = 4480866
67 meter
Z = 16164672
22 Z = 4931345
53
XDOT = -21198
301385 XDOT = -6491
407363
YDOT = 11951
642409 feet/sec YDOT = 3570
438644 meter/sec
ZDOT = -6814
295870 ZDOT = -2108
459491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13615444
00 X = 4149987
33
Y = 6211427
95 feet Y = 1893243
24 meter
Z = 16182054
37 Z = 4932290
17
XDOT = -2291
566974 XDOT = -698
469614
YDOT = 23150
960701 feet/sec YDOT = 7056
412822 meter/sec
ZDOT = -6941
775111 ZDOT = -2115
853054
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 11137
54398344
00016717 00000-0 10270-3 0 9088
2 25544 51
6433 318
0420 0003572 287
1857 72
8916 15
75162726 36089
Satellite: ISS
Catalog Number: 25544
Epoch time: 11137
54398344 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 318
0420 deg
Eccentricity:
0003572
Arg of perigee: 287
1857 deg
Mean anomaly: 72
8916 deg
Mean motion: 15
75162726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 321
Coasting Arc #10 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2011/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5419371
31 A = 6726463
97 meter
Y = -3310247
72 meter E =
0011504
Z = 2198422
10 I = 51
40456
XDOT = 1031
506558 Wp = 60
07244
YDOT = 5330
272844 meter/sec RA = 312
54242 deg
ZDOT = 5467
554351 TA = 324
67167
MA = 324
74785
Ha = 187
024 n
mi
Hp = 183
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17780089
59 X = 5445304
68
Y = -10860392
78 feet Y = -3249500
31 meter
Z = 7212670
95 Z = 2224812
29
XDOT = 3384
207868 XDOT = 945
265051
YDOT = 17487
771797 feet/sec YDOT = 5341
324857 meter/sec
ZDOT = 17938
170442 ZDOT = 5472
356686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1263104
75 X = 384994
33
Y = -20758856
21 feet Y = -6327299
37 meter
Z = 7319617
13 Z = 2231019
30
XDOT = 14696
453548 XDOT = 4479
479041
YDOT = 7243
863961 feet/sec YDOT = 2207
929735 meter/sec
ZDOT = 17957
324409 ZDOT = 5473
392480
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 11138
55902969
00016717 00000-0 10270-3 0 9095
2 25544 51
6431 312
8191 0003560 291
2162 68
8621 15
75247826 36247
Satellite: ISS
Catalog Number: 25544
Epoch time: 11138
55902969 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 312
8191 deg
Eccentricity:
0003560
Arg of perigee: 291
2162 deg
Mean anomaly: 68
8621 deg
Mean motion: 15
75247826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 316
Coasting Arc #11 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2011/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -886158
68 A = 6719365
22 meter
Y = -4855972
15 meter E =
0006883
Z = -4565612
83 I = 51
36176
XDOT = 5946
826822 Wp = 107
10625
YDOT = -3878
329300 meter/sec RA = 307
33609 deg
ZDOT = 2972
427188 TA = 192
51621
MA = 192
53331
Ha = 187
078 n
mi
Hp = 182
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2907344
77 X = -809613
34
Y = -15931667
15 feet Y = -4865453
09 meter
Z = -14979044
70 Z = -4569732
56
XDOT = 19510
586686 XDOT = 5975
313450
YDOT = -12724
177494 feet/sec YDOT = -3811
669412 meter/sec
ZDOT = 9752
057702 ZDOT = 3001
385723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14786873
30 X = -4507038
98
Y = -6567106
41 feet Y = -2001654
03 meter
Z = -14995464
09 Z = -4570617
46
XDOT = -159
998641 XDOT = -48
767586
YDOT = -22163
131144 feet/sec YDOT = -6755
322373 meter/sec
ZDOT = 9869
429123 ZDOT = 3008
201997
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 11139
51059978
00016717 00000-0 10270-3 0 9107
2 25544 51
6438 307
9230 0003486 295
5430 64
5373 15
75307758 36399
Satellite: ISS
Catalog Number: 25544
Epoch time: 11139
51059978 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 307
9230 deg
Eccentricity:
0003486
Arg of perigee: 295
5430 deg
Mean anomaly: 64
5373 deg
Mean motion: 15
75307758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 330
Coasting Arc #12 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2011/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4971181
74 A = 6724238
39 meter
Y = 3396881
25 meter E =
0001358
Z = -2995709
42 I = 51
36172
XDOT = -1000
325798 Wp = 67
37513
YDOT = -5819
180302 meter/sec RA = 302
21805 deg
ZDOT = -4939
748488 TA = 147
39555
MA = 147
38717
Ha = 187
089 n
mi
Hp = 182
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16309651
37 X = -4994244
20
Y = 11144623
53 feet Y = 3341161
94 meter
Z = -9828442
99 Z = -3019915
03
XDOT = -3281
908786 XDOT = -911
183814
YDOT = -19091
798890 feet/sec YDOT = -5829
867457 meter/sec
ZDOT = -16206
523910 ZDOT = -4944
392349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 499163
92 X = 152145
16
Y = 19698220
32 feet Y = 6004017
55 meter
Z = -9926560
56 Z = -3025615
66
XDOT = -16311
827990 XDOT = -4971
845171
YDOT = -7760
883615 feet/sec YDOT = -2365
517326 meter/sec
ZDOT = -16225
020101 ZDOT = -4945
386127
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 11140
52556799
00016717 00000-0 10270-3 0 9114
2 25544 51
6441 302
7010 0003598 302
4883 57
5933 15
75389277 36554
Satellite: ISS
Catalog Number: 25544
Epoch time: 11140
52556799 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 302
7010 deg
Eccentricity:
0003598
Arg of perigee: 302
4883 deg
Mean anomaly: 57
5933 deg
Mean motion: 15
75389277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 322
Coasting Arc #13 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2011/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 894417
80 A = 6721137
48 meter
Y = 5315248
59 meter E =
0008732
Z = 4011839
81 I = 51
33529
XDOT = -5436
782646 Wp = 60
07423
YDOT = 3845
540344 meter/sec RA = 297
00040 deg
ZDOT = -3872
232233 TA = 70
04685
MA = 69
95282
Ha = 187
084 n
mi
Hp = 182
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2934441
59 X = 815426
43
Y = 17438479
62 feet Y = 5324808
35 meter
Z = 13162204
09 Z = 4015993
67
XDOT = -17837
213406 XDOT = -5460
569569
YDOT = 12616
602178 feet/sec YDOT = 3784
610421 meter/sec
ZDOT = -12704
173993 ZDOT = -3898
701385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16301861
62 X = 4968807
42
Y = 6820922
60 feet Y = 2079017
21 meter
Z = 13178750
25 Z = 4016883
08
XDOT = 1783
028311 XDOT = 543
467029
YDOT = 20558
758382 feet/sec YDOT = 6266
309555 meter/sec
ZDOT = -12811
473723 ZDOT = -3904
937191
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 11141
54049673
00016717 00000-0 10270-3 0 9126
2 25544 51
6435 297
4780 0003610 304
2676 55
8146 15
75409604 36718
Satellite: ISS
Catalog Number: 25544
Epoch time: 11141
54049673 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 297
4780 deg
Eccentricity:
0003610
Arg of perigee: 304
2676 deg
Mean anomaly: 55
8146 deg
Mean motion: 15
75409604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 308
Coasting Arc #14 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2011/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4533656
25 A = 6721676
29 meter
Y = -3248940
63 meter E =
0008606
Z = 3743117
29 I = 51
32605
XDOT = 1076
687428 Wp = 84
64973
YDOT = 6362
876710 meter/sec RA = 291
88375 deg
ZDOT = 4211
248530 TA = 320
89215
MA = 320
95433
Ha = 186
896 n
mi
Hp = 182
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14874200
29 X = 4551466
25
Y = -10659254
04 feet Y = -3198143
35 meter
Z = 12280568
53 Z = 3765184
64
XDOT = 3532
439068 XDOT = 984
999082
YDOT = 20875
579756 feet/sec YDOT = 6374
403780 meter/sec
ZDOT = 13816
432186 ZDOT = 4216
257022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1507659
22 X = -459534
53
Y = -18176450
01 feet Y = -5540181
96 meter
Z = 12370025
19 Z = 3770383
68
XDOT = 18343
080431 XDOT = 5590
970915
YDOT = 7911
539033 feet/sec YDOT = 2411
437097 meter/sec
ZDOT = 13836
394516 ZDOT = 4217
333048
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 11142
55538287
00016717 00000-0 10270-3 0 9133
2 25544 51
6443 292
2551 0003695 307
8882 52
1947 15
75513121 36873
Satellite: ISS
Catalog Number: 25544
Epoch time: 11142
55538287 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 292
2551 deg
Eccentricity:
0003695
Arg of perigee: 307
8882 deg
Mean anomaly: 52
1947 deg
Mean motion: 15
75513121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 320
Coasting Arc #15 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2011/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1013358
36 A = 6723040
67 meter
Y = -5778302
34 meter E =
0003557
Z = -3282398
80 I = 51
32141
XDOT = 4978
827101 Wp = 34
18808
YDOT = -3535
354884 meter/sec RA = 286
66297 deg
ZDOT = 4691
876271 TA = 287
09518
MA = 287
13413
Ha = 187
063 n
mi
Hp = 182
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3324666
55 X = -932723
71
Y = -18957684
83 feet Y = -5789183
19 meter
Z = -10769024
95 Z = -3287126
32
XDOT = 16334
734582 XDOT = 4995
197864
YDOT = -11598
933346 feet/sec YDOT = -3479
587486 meter/sec
ZDOT = 15393
294854 ZDOT = 4716
102800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18044454
61 X = -5499949
77
Y = -6666202
97 feet Y = -2031858
67 meter
Z = -10787887
46 Z = -3288148
10
XDOT = -2397
955048 XDOT = -730
896699
YDOT = -18550
495739 feet/sec YDOT = -5654
191101 meter/sec
ZDOT = 15491
500126 ZDOT = 4721
809238
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 11143
50680300
00016717 00000-0 10270-3 0 9144
2 25544 51
6452 287
3592 0003722 313
7492 46
3363 15
75554908 37020
Satellite: ISS
Catalog Number: 25544
Epoch time: 11143
50680300 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 287
3592 deg
Eccentricity:
0003722
Arg of perigee: 313
7492 deg
Mean anomaly: 46
3363 deg
Mean motion: 15
75554908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 298
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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