[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 14th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 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
291/15:24:13
182 0
2 1
1 1
1
N/A -0
8 0
0 231
1
000/00:00:22
363 0
8 0
0 217
3
Coasting Arc #1 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2012/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2097956
62 A = 6792713
87 meter
Y = -5132320
88 meter E =
0025102
Z = 3923628
95 I = 51
29868
XDOT = 4349
287261 Wp = 136
91149
YDOT = 4868
083943 meter/sec RA = 257
69463 deg
ZDOT = 4008
878880 TA = 270
83522
MA = 271
12283
Ha = 231
900 n
mi
Hp = 215
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6883059
79 X = 2136131
04
Y = -16838323
09 feet Y = -5108646
28 meter
Z = 12872798
39 Z = 3933914
22
XDOT = 14269
315160 XDOT = 4275
053607
YDOT = 15971
404012 feet/sec YDOT = 4916
305827 meter/sec
ZDOT = 13152
489763 ZDOT = 4029
826857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -426484
56 X = -129992
49
Y = 18155294
03 feet Y = 5533733
62 meter
Z = 12915803
67 Z = 3936736
96
XDOT = -17587
143179 XDOT = -5360
561241
YDOT = -9908
621476 feet/sec YDOT = -3020
147826 meter/sec
ZDOT = 13238
628671 ZDOT = 4035
134019
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 12286
55589836
00016717 00000-0 10270-3 0 9005
2 25544 51
6444 258
2528 0017590 159
3800 200
8065 15
50723105 36252
Satellite: ISS
Catalog Number: 25544
Epoch time: 12286
55589836 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 258
2528 deg
Eccentricity:
0017590
Arg of perigee: 159
3800 deg
Mean anomaly: 200
8065 deg
Mean motion: 15
50723105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3625
Checksum: 311
Coasting Arc #2 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2012/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2129865
18 A = 6791364
91 meter
Y = 4793368
18 meter E =
0019135
Z = -4317000
38 I = 51
30192
XDOT = -4512
291509 Wp = 135
75150
YDOT = -5117
887942 meter/sec RA = 252
70881 deg
ZDOT = -3479
215182 TA = 98
76111
MA = 98
54435
Ha = 231
765 n
mi
Hp = 215
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6987746
66 X = -2162335
96
Y = 15726273
54 feet Y = 4769368
58 meter
Z = -14163387
08 Z = -4327426
84
XDOT = -14804
106000 XDOT = -4437
825323
YDOT = -16790
970939 feet/sec YDOT = -5167
931291 meter/sec
ZDOT = -11414
747972 ZDOT = -3500
954514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 614273
31 X = 187230
50
Y = -17161916
36 feet Y = -5230952
11 meter
Z = -14206938
85 Z = -4330274
96
XDOT = 18636
973376 XDOT = 5680
549485
YDOT = 10128
671334 feet/sec YDOT = 3087
219023 meter/sec
ZDOT = -11504
142513 ZDOT = -3506
462638
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 12287
52256074
00016717 00000-0 10270-3 0 9019
2 25544 51
6447 253
4572 0017505 162
2800 197
8965 15
50709834 36404
Satellite: ISS
Catalog Number: 25544
Epoch time: 12287
52256074 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 253
4572 deg
Eccentricity:
0017505
Arg of perigee: 162
2800 deg
Mean anomaly: 197
8965 deg
Mean motion: 15
50709834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3640
Checksum: 317
Coasting Arc #3 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2012/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2141972
16 A = 6790095
27 meter
Y = -4504826
84 meter E =
0023592
Z = 4606913
59 I = 51
30873
XDOT = 4709
878417 Wp = 150
44660
YDOT = 5277
564417 meter/sec RA = 247
72521 deg
ZDOT = 2944
129892 TA = 269
92579
MA = 270
19613
Ha = 231
563 n
mi
Hp = 215
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7027467
72 X = 2169807
04
Y = -14779615
60 feet Y = -4480717
77 meter
Z = 15114545
90 Z = 4617387
57
XDOT = 15452
357010 XDOT = 4636
211307
YDOT = 17314
843887 feet/sec YDOT = 5329
821679 meter/sec
ZDOT = 9659
218807 ZDOT = 2966
831185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -714526
06 X = -217787
54
Y = 16309147
93 feet Y = 4971028
29 meter
Z = 15158264
53 Z = 4620239
03
XDOT = -19680
998570 XDOT = -5998
768364
YDOT = -10007
628164 feet/sec YDOT = -3050
325064 meter/sec
ZDOT = 9752
581545 ZDOT = 2972
586855
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 12288
55364796
00016717 00000-0 10270-3 0 9025
2 25544 51
6453 248
3444 0017485 166
7620 193
3994 15
50772194 36567
Satellite: ISS
Catalog Number: 25544
Epoch time: 12288
55364796 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 248
3444 deg
Eccentricity:
0017485
Arg of perigee: 166
7620 deg
Mean anomaly: 193
3994 deg
Mean motion: 15
50772194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3656
Checksum: 346
Coasting Arc #4 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2280475
42 A = 6788979
00 meter
Y = 4126292
13 meter E =
0019956
Z = -4892650
05 I = 51
31792
XDOT = -4882
053948 Wp = 133
25482
YDOT = -5423
275922 meter/sec RA = 242
73826 deg
ZDOT = -2317
661792 TA = 114
03290
MA = 113
82391
Ha = 231
417 n
mi
Hp = 216
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7481874
72 X = -2302678
98
Y = 13537703
82 feet Y = 4100665
79 meter
Z = -16052001
47 Z = -4903783
13
XDOT = -16017
237363 XDOT = -4809
787927
YDOT = -17792
900008 feet/sec YDOT = -5477
466270 meter/sec
ZDOT = -7603
877271 ZDOT = -2341
203116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1342485
17 X = 409189
48
Y = -15360779
88 feet Y = -4681965
71 meter
Z = -16098409
87 Z = -4906795
33
XDOT = 20640
661457 XDOT = 6291
273612
YDOT = 9807
931892 feet/sec YDOT = 2989
457641 meter/sec
ZDOT = -7700
704856 ZDOT = -2347
174840
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 12289
52027919
00016717 00000-0 10270-3 0 9037
2 25544 51
6458 243
5488 0017402 169
8573 190
2933 15
50760888 36710
Satellite: ISS
Catalog Number: 25544
Epoch time: 12289
52027919 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 243
5488 deg
Eccentricity:
0017402
Arg of perigee: 169
8573 deg
Mean anomaly: 190
2933 deg
Mean motion: 15
50760888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 341
Coasting Arc #5 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2012/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2399685
20 A = 6788005
68 meter
Y = -3812323
72 meter E =
0021209
Z = 5077831
94 I = 51
33074
XDOT = 5071
325219 Wp = 163
37920
YDOT = 5487
164620 meter/sec RA = 237
75448 deg
ZDOT = 1701
305294 TA = 269
97894
MA = 270
22198
Ha = 231
200 n
mi
Hp = 216
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7872982
94 X = 2417469
40
Y = -12507623
75 feet Y = -3785389
13 meter
Z = 16659553
60 Z = 5089533
30
XDOT = 16638
206100 XDOT = 5001
324897
YDOT = 18002
508596 feet/sec YDOT = 5543
484076 meter/sec
ZDOT = 5581
710281 ZDOT = 1725
771806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1859105
68 X = -566655
41
Y = 14606237
69 feet Y = 4451981
25 meter
Z = 16708284
91 Z = 5092685
24
XDOT = -21525
918358 XDOT = -6561
099916
YDOT = -9321
290787 feet/sec YDOT = -2841
129432 meter/sec
ZDOT = 5682
363134 ZDOT = 1731
984283
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 12290
55133337
00016717 00000-0 10270-3 0 9045
2 25544 51
6465 238
4363 0017393 174
1950 185
9406 15
50820855 36874
Satellite: ISS
Catalog Number: 25544
Epoch time: 12290
55133337 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 238
4363 deg
Eccentricity:
0017393
Arg of perigee: 174
1950 deg
Mean anomaly: 185
9406 deg
Mean motion: 15
50820855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 323
Coasting Arc #6 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2012/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2647863
70 A = 6787375
64 meter
Y = 3433132
98 meter E =
0021422
Z = -5232807
11 I = 51
34578
XDOT = -5205
434790 Wp = 135
98308
YDOT = -5520
631575 meter/sec RA = 232
76776 deg
ZDOT = -1005
539310 TA = 124
43357
MA = 124
23092
Ha = 231
052 n
mi
Hp = 216
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8687216
87 X = -2660636
44
Y = 11263559
64 feet Y = 3403451
26 meter
Z = -17168002
32 Z = -5245701
83
XDOT = -17078
198131 XDOT = -5138
430239
YDOT = -18112
308317 feet/sec YDOT = -5578
467399 meter/sec
ZDOT = -3299
013483 ZDOT = -1030
664740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2876432
26 X = 876736
55
Y = -13864240
59 feet Y = -4225820
53 meter
Z = -17221637
17 Z = -5249155
01
XDOT = 22196
158852 XDOT = 6765
389218
YDOT = 8759
957486 feet/sec YDOT = 2670
035042 meter/sec
ZDOT = -3402
395895 ZDOT = -1037
050269
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 12291
51793297
00016717 00000-0 10270-3 0 9050
2 25544 51
6467 233
6409 0017327 177
4556 182
6686 15
50811716 37027
Satellite: ISS
Catalog Number: 25544
Epoch time: 12291
51793297 = yrday
fracday
Element set: 905
Inclination: 51
6467 deg
RA of node: 233
6409 deg
Eccentricity:
0017327
Arg of perigee: 177
4556 deg
Mean anomaly: 182
6686 deg
Mean motion: 15
50811716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 331
Coasting Arc #7 (Orbit 3703)
---------------------------------------
Vector Time (GMT): 2012/291/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5246723
53 A = 6797101
33 meter
Y = -3613791
45 meter E =
0013401
Z = -2394891
27 I = 51
38122
XDOT = 1239
717529 Wp = 161
81246
YDOT = -5337
982045 meter/sec RA = 232
03300 deg
ZDOT = 5334
471653 TA = 171
42072
MA = 171
39779
Ha = 231
061 n
mi
Hp = 217
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17213659
87 X = -5194289
26
Y = -11856271
15 feet Y = -3672170
51 meter
Z = -7857254
83 Z = -2420252
77
XDOT = 4067
314729 XDOT = 1273
401477
YDOT = -17513
064452 feet/sec YDOT = -5323
930187 meter/sec
ZDOT = 17501
547418 ZDOT = 5340
576347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15456473
76 X = 4711133
20
Y = -14011602
89 feet Y = -4270736
56 meter
Z = -7961790
52 Z = -2426753
75
XDOT = 15126
994620 XDOT = 4610
707960
YDOT = 6719
380966 feet/sec YDOT = 2048
067318 meter/sec
ZDOT = 17527
281935 ZDOT = 5342
315534
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 12291
64681105
00016717 00000-0 10270-3 0 9069
2 25544 51
6489 233
0028 0016453 179
3502 180
7673 15
50605920 37048
Satellite: ISS
Catalog Number: 25544
Epoch time: 12291
64681105 = yrday
fracday
Element set: 906
Inclination: 51
6489 deg
RA of node: 233
0028 deg
Eccentricity:
0016453
Arg of perigee: 179
3502 deg
Mean anomaly: 180
7673 deg
Mean motion: 15
50605920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3704
Checksum: 301
Coasting Arc #8 (Orbit 3719)
---------------------------------------
Vector Time (GMT): 2012/292/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5419592
62 A = 6798102
42 meter
Y = 3612701
16 meter E =
0024992
Z = 1887302
97 I = 51
40341
XDOT = -1411
692002 Wp = 151
53547
YDOT = 5050
847990 meter/sec RA = 227
06010 deg
ZDOT = -5605
479001 TA = 7
60374
MA = 7
56592
Ha = 230
902 n
mi
Hp = 217
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17780815
68 X = 5369623
54
Y = 11852694
10 feet Y = 3673027
08 meter
Z = 6191938
87 Z = 1913510
24
XDOT = -4631
535439 XDOT = -1440
835945
YDOT = 16571
023589 feet/sec YDOT = 5034
898486 meter/sec
ZDOT = -18390
679136 ZDOT = -5612
408001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15331445
44 X = -4673024
57
Y = 14840513
96 feet Y = 4523388
65 meter
Z = 6299983
89 Z = 1920235
09
XDOT = -14160
303290 XDOT = -4316
060443
YDOT = -6796
843518 feet/sec YDOT = -2071
677904 meter/sec
ZDOT = -18419
798162 ZDOT = -5614
354480
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 12292
67798486
00016717 00000-0 10270-3 0 9075
2 25544 51
6486 227
8903 0016542 182
9307 177
1750 15
50583492 37203
Satellite: ISS
Catalog Number: 25544
Epoch time: 12292
67798486 = yrday
fracday
Element set: 907
Inclination: 51
6486 deg
RA of node: 227
8903 deg
Eccentricity:
0016542
Arg of perigee: 182
9307 deg
Mean anomaly: 177
1750 deg
Mean motion: 15
50583492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3720
Checksum: 342
Coasting Arc #9 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2012/293/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5612398
10 A = 6798591
01 meter
Y = -3596906
09 meter E =
0010028
Z = -1369916
52 I = 51
42719
XDOT = 1627
819030 Wp = 161
61624
YDOT = -4740
007289 meter/sec RA = 222
08817 deg
ZDOT = 5778
855413 TA = 183
46345
MA = 183
47039
Ha = 230
662 n
mi
Hp = 217
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18413379
58 X = -5565104
74
Y = -11800873
00 feet Y = -3659403
02 meter
Z = -4494476
76 Z = -1397066
86
XDOT = 5340
613617 XDOT = 1652
628908
YDOT = -15551
205016 feet/sec YDOT = -4721
665190 meter/sec
ZDOT = 18959
499387 ZDOT = 5786
823766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15147854
72 X = 4617066
12
Y = -15742830
05 feet Y = -4798414
60 meter
Z = -4606438
10 Z = -1404042
33
XDOT = 13090
902432 XDOT = 3990
107061
YDOT = 7040
887501 feet/sec YDOT = 2146
062510 meter/sec
ZDOT = 18992
890093 ZDOT = 5789
032900
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 12293
64469173
00016717 00000-0 10270-3 0 9082
2 25544 51
6486 223
0964 0016402 187
0919 173
0002 15
50658752 37351
Satellite: ISS
Catalog Number: 25544
Epoch time: 12293
64469173 = yrday
fracday
Element set: 908
Inclination: 51
6486 deg
RA of node: 223
0964 deg
Eccentricity:
0016402
Arg of perigee: 187
0919 deg
Mean anomaly: 173
0002 deg
Mean motion: 15
50658752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3735
Checksum: 317
Coasting Arc #10 (Orbit 3750)
---------------------------------------
Vector Time (GMT): 2012/294/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5734484
29 A = 6799243
28 meter
Y = 3529322
03 meter E =
0025331
Z = 811232
83 I = 51
45175
XDOT = -1914
108441 Wp = 162
42514
YDOT = 4479
293612 meter/sec RA = 217
11918 deg
ZDOT = -5932
171287 TA = 8
77753
MA = 8
73332
Ha = 230
556 n
mi
Hp = 217
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18813924
83 X = 5690651
63
Y = 11579140
52 feet Y = 3593203
55 meter
Z = 2661525
02 Z = 838984
54
XDOT = -6279
883335 XDOT = -1935
237019
YDOT = 14695
845183 feet/sec YDOT = 4457
770604 meter/sec
ZDOT = -19462
504222 ZDOT = -5941
521479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14729508
23 X = -4489554
11
Y = 16445650
17 feet Y = 5012634
17 meter
Z = 2775996
43 Z = 846123
71
XDOT = -12169
792998 XDOT = -3709
352906
YDOT = -7594
875544 feet/sec YDOT = -2314
918066 meter/sec
ZDOT = -19501
587908 ZDOT = -5944
083994
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 12294
67583170
00016717 00000-0 10270-3 0 9091
2 25544 51
6482 217
9835 0016547 190
6781 169
4021 15
50624706 37513
Satellite: ISS
Catalog Number: 25544
Epoch time: 12294
67583170 = yrday
fracday
Element set: 909
Inclination: 51
6482 deg
RA of node: 217
9835 deg
Eccentricity:
0016547
Arg of perigee: 190
6781 deg
Mean anomaly: 169
4021 deg
Mean motion: 15
50624706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3751
Checksum: 328
Coasting Arc #11 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2012/295/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5861307
06 A = 6799226
14 meter
Y = -3447003
23 meter E =
0008320
Z = -252065
60 I = 51
47688
XDOT = 2228
354627 Wp = 154
25330
YDOT = -4221
411523 meter/sec RA = 212
15066 deg
ZDOT = 5979
033157 TA = 203
03275
MA = 203
07007
Ha = 230
242 n
mi
Hp = 218
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19230010
03 X = -5821101
83
Y = -11309065
72 feet Y = -3512323
23 meter
Z = -826986
87 Z = -280442
11
XDOT = 7310
874761 XDOT = 2246
348599
YDOT = -13849
775339 feet/sec YDOT = -4196
391870 meter/sec
ZDOT = 19616
250516 ZDOT = 5989
902364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14246285
71 X = 4342267
88
Y = -17161708
58 feet Y = -5230888
77 meter
Z = -944067
17 Z = -287751
67
XDOT = 11264
377911 XDOT = 3433
382387
YDOT = 8279
842049 feet/sec YDOT = 2523
695856 meter/sec
ZDOT = 19661
595531 ZDOT = 5992
854318
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 12295
64250672
00016717 00000-0 10270-3 0 9109
2 25544 51
6477 213
1889 0016395 194
8526 165
2145 15
50713228 37663
Satellite: ISS
Catalog Number: 25544
Epoch time: 12295
64250672 = yrday
fracday
Element set: 910
Inclination: 51
6477 deg
RA of node: 213
1889 deg
Eccentricity:
0016395
Arg of perigee: 194
8526 deg
Mean anomaly: 165
2145 deg
Mean motion: 15
50713228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 326
Coasting Arc #12 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2012/296/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5900009
52 A = 6799361
15 meter
Y = 3329916
61 meter E =
0024202
Z = -335127
42 I = 51
50285
XDOT = -2606
659390 Wp = 174
25728
YDOT = 4021
340337 meter/sec RA = 207
18523 deg
ZDOT = -5994
836272 TA = 9
36207
MA = 9
31703
Ha = 230
159 n
mi
Hp = 218
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19356986
62 X = 5863963
18
Y = 10924923
27 feet Y = 3395692
64 meter
Z = -1099499
42 Z = -306552
89
XDOT = -8552
032119 XDOT = -2622
311280
YDOT = 13193
373809 feet/sec YDOT = 3992
103239 meter/sec
ZDOT = -19668
098004 ZDOT = -6007
537639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13588576
09 X = -4141797
99
Y = 17596672
75 feet Y = 5363465
85 meter
Z = -981573
45 Z = -299183
59
XDOT = -10563
554569 XDOT = -3219
771433
YDOT = -9244
997390 feet/sec YDOT = -2817
875204 meter/sec
ZDOT = -19721
006195 ZDOT = -6010
962688
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 12296
67361262
00016717 00000-0 10270-3 0 9112
2 25544 51
6475 208
0757 0016540 198
6028 161
4520 15
50674855 37824
Satellite: ISS
Catalog Number: 25544
Epoch time: 12296
67361262 = yrday
fracday
Element set: 911
Inclination: 51
6475 deg
RA of node: 208
0757 deg
Eccentricity:
0016540
Arg of perigee: 198
6028 deg
Mean anomaly: 161
4520 deg
Mean motion: 15
50674855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3782
Checksum: 320
Coasting Arc #13 (Orbit 3797)
---------------------------------------
Vector Time (GMT): 2012/297/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5931409
99 A = 6798781
59 meter
Y = -3205016
47 meter E =
0008691
Z = 911124
57 I = 51
52868
XDOT = 2989
208996 Wp = 148
67789
YDOT = -3844
915632 meter/sec RA = 202
21970 deg
ZDOT = 5901
938160 TA = 221
17150
MA = 221
23709
Ha = 229
807 n
mi
Hp = 218
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19460006
53 X = -5899556
07
Y = -10515145
89 feet Y = -3271167
03 meter
Z = 2989253
85 Z = 882387
35
XDOT = 9807
116130 XDOT = 3003
310906
YDOT = -12614
552599 feet/sec YDOT = -3811
409198 meter/sec
ZDOT = 19363
314172 ZDOT = 5916
494250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12891742
69 X = 3929403
17
Y = -17993283
24 feet Y = -5484352
73 meter
Z = 2870629
63 Z = 874967
91
XDOT = 9975
976297 XDOT = 3040
677575
YDOT = 10264
236462 feet/sec YDOT = 3128
539274 meter/sec
ZDOT = 19423
882579 ZDOT = 5920
399410
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 12297
70469801
00016717 00000-0 10270-3 0 9126
2 25544 51
6468 202
9608 0016446 202
8411 157
2010 15
50768665 37980
Satellite: ISS
Catalog Number: 25544
Epoch time: 12297
70469801 = yrday
fracday
Element set: 912
Inclination: 51
6468 deg
RA of node: 202
9608 deg
Eccentricity:
0016446
Arg of perigee: 202
8411 deg
Mean anomaly: 157
2010 deg
Mean motion: 15
50768665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3798
Checksum: 320
Coasting Arc #14 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2012/298/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5862435
04 A = 6798302
66 meter
Y = 3067057
13 meter E =
0021522
Z = -1498753
21 I = 51
55489
XDOT = -3422
519813 Wp = 186
30770
YDOT = 3730
416374 meter/sec RA = 197
25727 deg
ZDOT = -5766
433706 TA = 10
07683
MA = 10
03375
Ha = 229
696 n
mi
Hp = 218
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19233710
76 X = 5834983
55
Y = 10062523
40 feet Y = 3132460
94 meter
Z = -4917169
34 Z = -1470340
34
XDOT = -11228
739544 XDOT = -3435
967358
YDOT = 12238
898864 feet/sec YDOT = 3692
067979 meter/sec
ZDOT = -18918
745754 ZDOT = -5783
093310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12106853
10 X = -3690168
83
Y = 18048655
93 feet Y = 5501230
33 meter
Z = -4799863
36 Z = -1462998
35
XDOT = -9633
988696 XDOT = -2936
439755
YDOT = -11500
390483 feet/sec YDOT = -3505
319019 meter/sec
ZDOT = -18988
011162 ZDOT = -5787
545802
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 12298
67132865
00016717 00000-0 10270-3 0 9131
2 25544 51
6465 198
1670 0016492 206
4937 153
5373 15
50738657 38133
Satellite: ISS
Catalog Number: 25544
Epoch time: 12298
67132865 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 198
1670 deg
Eccentricity:
0016492
Arg of perigee: 206
4937 deg
Mean anomaly: 153
5373 deg
Mean motion: 15
50738657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3813
Checksum: 338
Coasting Arc #15 (Orbit 3828)
---------------------------------------
Vector Time (GMT): 2012/299/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5779854
55 A = 6797231
16 meter
Y = -2933530
52 meter E =
0010290
Z = 2062116
15 I = 51
58085
XDOT = 3832
048609 Wp = 153
71912
YDOT = -3651
300493 meter/sec RA = 192
29427 deg
ZDOT = 5526
847611 TA = 229
04587
MA = 229
13497
Ha = 229
353 n
mi
Hp = 218
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18962777
38 X = -5756639
07
Y = -9624443
97 feet Y = -2998034
49 meter
Z = 6765472
94 Z = 2034094
09
XDOT = 12572
337955 XDOT = 3845
744805
YDOT = -11979
332327 feet/sec YDOT = -3608
371080 meter/sec
ZDOT = 18132
702136 ZDOT = 5545
497399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11334341
08 X = 3454707
16
Y = -18036125
92 feet Y = -5497411
18 meter
Z = 6649762
85 Z = 2026847
72
XDOT = 9463
619079 XDOT = 2884
511095
YDOT = 12685
270214 feet/sec YDOT = 3866
470361 meter/sec
ZDOT = 18210
200841 ZDOT = 5550
469216
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 12299
70238155
00016717 00000-0 10270-3 0 9146
2 25544 51
6459 193
0518 0016515 210
4938 149
5254 15
50819042 38291
Satellite: ISS
Catalog Number: 25544
Epoch time: 12299
70238155 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 193
0518 deg
Eccentricity:
0016515
Arg of perigee: 210
4938 deg
Mean anomaly: 149
5254 deg
Mean motion: 15
50819042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3829
Checksum: 321
Coasting Arc #16 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2012/300/15:24:24
363
Vector Time (MET): N/A
Weight (LBS) : 891765
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5592145
04 A = 6796171
53 meter
Y = 2811353
89 meter E =
0017536
Z = -2617986
08 I = 51
60640
XDOT = -4273
148871 Wp = 197
45391
YDOT = 3632
120098 meter/sec RA = 187
33385 deg
ZDOT = -5234
519642 TA = 12
04049
MA = 11
99863
Ha = 229
186 n
mi
Hp = 219
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18346932
54 X = 5573010
10
Y = 9223602
00 feet Y = 2873781
54 meter
Z = -8589193
18 Z = -2590865
89
XDOT = -14019
517292 XDOT = -4288
017791
YDOT = 11916
404521 feet/sec YDOT = 3584
251492 meter/sec
ZDOT = -17173
620872 ZDOT = -5255
315235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10577228
69 X = -3223939
30
Y = 17655547
97 feet Y = 5381411
02 meter
Z = -8477196
83 Z = -2583849
59
XDOT = -9550
511979 XDOT = -2910
996051
YDOT = -13997
289920 feet/sec YDOT = -4266
373968 meter/sec
ZDOT = -17260
004609 ZDOT = -5260
849405
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 12300
66898104
00016717 00000-0 10270-3 0 9151
2 25544 51
6453 188
2577 0016412 214
0417 145
9683 15
50809310 38444
Satellite: ISS
Catalog Number: 25544
Epoch time: 12300
66898104 = yrday
fracday
Element set: 915
Inclination: 51
6453 deg
RA of node: 188
2577 deg
Eccentricity:
0016412
Arg of perigee: 214
0417 deg
Mean anomaly: 145
9683 deg
Mean motion: 15
50809310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 309
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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