[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 22nd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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 2664)
---------------------------------------
Vector Time (GMT): 2011/077/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2639844
59 A = 6732220
83 meter
Y = -4859998
04 meter E =
0011398
Z = 3829714
53 I = 51
29952
XDOT = 3784
889827 Wp = 95
91544
YDOT = 5301
336458 meter/sec RA = 264
81521 deg
ZDOT = 4106
934228 TA = 310
92571
MA = 311
02434
Ha = 193
578 n
mi
Hp = 187
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8660907
43 X = 2675390
04
Y = -15944875
47 feet Y = -4830278
45 meter
Z = 12564680
20 Z = 3842625
66
XDOT = 12417
617543 XDOT = 3705
377546
YDOT = 17392
836149 feet/sec YDOT = 5343
217356 meter/sec
ZDOT = 13474
193660 ZDOT = 4125
127092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -712316
14 X = -217113
96
Y = -18094989
07 feet Y = -5515352
67 meter
Z = 12616875
05 Z = 3845623
52
XDOT = 18146
494654 XDOT = 5531
051570
YDOT = 8758
305189 feet/sec YDOT = 2669
531422 meter/sec
ZDOT = 13547
541769 ZDOT = 4129
290731
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 11077
65404886
00016717 00000-0 10270-3 0 9004
2 25544 51
6423 265
3131 0000562 11
0007 349
1167 15
71732073 26652
Satellite: ISS
Catalog Number: 25544
Epoch time: 11077
65404886 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 265
3131 deg
Eccentricity:
0000562
Arg of perigee: 11
0007 deg
Mean anomaly: 349
1167 deg
Mean motion: 15
71732073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2665
Checksum: 280
Coasting Arc #2 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2011/078/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3984202
34 A = 6731258
58 meter
Y = -3576188
61 meter E =
0007676
Z = -4087805
47 I = 51
30142
XDOT = 1897
886068 Wp = 104
45401
YDOT = -6424
979026 meter/sec RA = 259
62172 deg
ZDOT = 3775
100873 TA = 204
50599
MA = 204
54249
Ha = 193
631 n
mi
Hp = 187
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13071529
97 X = -3924058
97
Y = -11732902
27 feet Y = -3620406
66 meter
Z = -13411435
26 Z = -4107013
94
XDOT = 6226
660328 XDOT = 1951
251772
YDOT = -21079
327514 feet/sec YDOT = -6403
456806 meter/sec
ZDOT = 12385
501553 ZDOT = 3784
451225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17209726
13 X = -5245524
52
Y = -3204210
18 feet Y = -976643
26 meter
Z = -13488915
86 Z = -4111421
55
XDOT = -6016
686799 XDOT = -1833
886136
YDOT = -19928
227426 feet/sec YDOT = -6074
123720 meter/sec
ZDOT = 12423
340968 ZDOT = 3786
634327
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 11078
60776499
00016717 00000-0 10270-3 0 9013
2 25544 51
6433 260
4322 0000682 17
7968 342
3218 15
71752017 26802
Satellite: ISS
Catalog Number: 25544
Epoch time: 11078
60776499 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 260
4322 deg
Eccentricity:
0000682
Arg of perigee: 17
7968 deg
Mean anomaly: 342
3218 deg
Mean motion: 15
71752017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2680
Checksum: 309
Coasting Arc #3 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2011/079/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -576518
41 A = 6735160
57 meter
Y = 6127768
31 meter E =
0004645
Z = -2736159
92 I = 51
32170
XDOT = -5024
650053 Wp = 113
00564
YDOT = -2759
321759 meter/sec RA = 254
52739 deg
ZDOT = -5129
632614 TA = 98
35032
MA = 98
29765
Ha = 193
565 n
mi
Hp = 187
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1891464
61 X = -631705
72
Y = 20104226
74 feet Y = 6121012
41 meter
Z = -8976902
62 Z = -2739095
47
XDOT = -16485
072351 XDOT = -4968
502615
YDOT = -9052
892909 feet/sec YDOT = -2815
197165 meter/sec
ZDOT = -16829
503328 ZDOT = -5153
905526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9260246
67 X = 2822523
19
Y = 17938532
24 feet Y = 5467664
63 meter
Z = -8988839
99 Z = -2739798
43
XDOT = -17374
056034 XDOT = -5295
612279
YDOT = 500
950277 feet/sec YDOT = 152
689644 meter/sec
ZDOT = -16927
441577 ZDOT = -5159
484193
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 11079
62503196
00016717 00000-0 10270-3 0 9029
2 25544 51
6433 255
2248 0000766 16
0797 344
0389 15
71809434 26967
Satellite: ISS
Catalog Number: 25544
Epoch time: 11079
62503196 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 255
2248 deg
Eccentricity:
0000766
Arg of perigee: 16
0797 deg
Mean anomaly: 344
0389 deg
Mean motion: 15
71809434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 320
Coasting Arc #4 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2011/080/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4556602
47 A = 6728263
52 meter
Y = 1179427
61 meter E =
0007654
Z = 4804058
80 I = 51
30859
XDOT = 673
700790 Wp = 55
88922
YDOT = 7279
093045 meter/sec RA = 249
34321 deg
ZDOT = -2419
077810 TA = 57
88265
MA = 57
80839
Ha = 193
482 n
mi
Hp = 186
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14949483
18 X = 4519737
98
Y = 3869513
16 feet Y = 1230176
69 meter
Z = 15761347
78 Z = 4826105
10
XDOT = 2210
304430 XDOT = 604
005959
YDOT = 23881
538861 feet/sec YDOT = 7286
236835 meter/sec
ZDOT = -7936
606989 ZDOT = -2415
975030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14522330
00 X = 4426406
18
Y = -4974879
97 feet Y = -1516343
41 meter
Z = 15850323
78 Z = 4831178
69
XDOT = 14704
879420 XDOT = 4482
047247
YDOT = 17605
853489 feet/sec YDOT = 5366
264143 meter/sec
ZDOT = -7924
184432 ZDOT = -2415
291415
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 11080
64227007
00016717 00000-0 10270-3 0 9038
2 25544 51
6440 250
0179 0000805 25
6885 334
4317 15
71815159 27123
Satellite: ISS
Catalog Number: 25544
Epoch time: 11080
64227007 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 250
0179 deg
Eccentricity:
0000805
Arg of perigee: 25
6885 deg
Mean anomaly: 334
4317 deg
Mean motion: 15
71815159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 285
Coasting Arc #5 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2011/081/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1752274
30 A = 6737202
40 meter
Y = -6329977
38 meter E =
0014673
Z = 1467475
91 I = 51
35264
XDOT = 5095
084752 Wp = 59
28936
YDOT = -63
888193 meter/sec RA = 244
23493 deg
ZDOT = 5772
973322 TA = 316
92266
MA = 317
03741
Ha = 193
432 n
mi
Hp = 186
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5748931
43 X = -1688489
79
Y = -20767642
31 feet Y = -6349215
62 meter
Z = 4814553
50 Z = 1459118
78
XDOT = 16716
157324 XDOT = 5067
376398
YDOT = -209
606932 feet/sec YDOT = -7
066343 meter/sec
ZDOT = 18940
201188 ZDOT = 5797
657960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16523818
80 X = -5036459
97
Y = -13843101
51 feet Y = -4219377
34 meter
Z = 4780905
53 Z = 1457220
01
XDOT = 12555
205657 XDOT = 3826
826684
YDOT = -8370
510919 feet/sec YDOT = -2551
331728 meter/sec
ZDOT = 19039
849633 ZDOT = 5803
346168
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 11081
65947367
00016717 00000-0 10270-3 0 9049
2 25544 51
6452 244
8109 0000847 20
2450 339
8746 15
71914691 27288
Satellite: ISS
Catalog Number: 25544
Epoch time: 11081
65947367 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 244
8109 deg
Eccentricity:
0000847
Arg of perigee: 20
2450 deg
Mean anomaly: 339
8746 deg
Mean motion: 15
71914691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 321
Coasting Arc #6 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2011/082/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110696
50 A = 6726176
06 meter
Y = 1226030
81 meter E =
0014838
Z = -5193669
45 I = 51
33054
XDOT = -3251
652081 Wp = 93
53889
YDOT = -6900
580023 meter/sec RA = 239
07341 deg
ZDOT = 946
081867 TA = 185
52284
MA = 185
53922
Ha = 193
374 n
mi
Hp = 186
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13486537
07 X = -4098870
81
Y = 4022410
79 feet Y = 1180128
35 meter
Z = -17039597
92 Z = -5213610
53
XDOT = -10668
149873 XDOT = -3178
842702
YDOT = -22639
698239 feet/sec YDOT = -6936
534817 meter/sec
ZDOT = 3103
943133 ZDOT = 930
462583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8564162
97 X = -2610356
87
Y = 11044047
32 feet Y = 3366225
62 meter
Z = -17120119
73 Z = -5218212
49
XDOT = -21038
088512 XDOT = -6412
409378
YDOT = -11607
281121 feet/sec YDOT = -3537
899286 meter/sec
ZDOT = 3040
981495 ZDOT = 926
891160
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 11082
61307572
00016717 00000-0 10270-3 0 9055
2 25544 51
6453 239
9304 0001013 19
3673 340
7527 15
71970909 27432
Satellite: ISS
Catalog Number: 25544
Epoch time: 11082
61307572 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 239
9304 deg
Eccentricity:
0001013
Arg of perigee: 19
3673 deg
Mean anomaly: 340
7527 deg
Mean motion: 15
71970909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 301
Coasting Arc #7 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2011/083/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3833936
81 A = 6737862
65 meter
Y = 5531281
96 meter E =
0011433
Z = -195584
02 I = 51
38697
XDOT = -4045
110041 Wp = 131
85362
YDOT = 2599
524684 meter/sec RA = 233
94278 deg
ZDOT = -6010
364493 TA = 50
27692
MA = 50
17621
Ha = 193
334 n
mi
Hp = 186
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12578532
85 X = 3772750
13
Y = 18147250
54 feet Y = 5573813
25 meter
Z = -641679
85 Z = -177107
67
XDOT = -13271
358402 XDOT = -4044
680642
YDOT = 8528
624290 feet/sec YDOT = 2554
291982 meter/sec
ZDOT = -19719
043612 ZDOT = -6030
014605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20904808
20 X = 6371785
54
Y = 7114862
74 feet Y = 2168610
16 meter
Z = -567156
12 Z = -172869
19
XDOT = -4989
782209 XDOT = -1520
885617
YDOT = 13151
599314 feet/sec YDOT = 4008
607471 meter/sec
ZDOT = -19798
416356 ZDOT = -6034
557305
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 11083
63021989
00016717 00000-0 10270-3 0 9064
2 25544 51
6454 234
7225 0001038 17
6642 342
4556 15
71999266 27597
Satellite: ISS
Catalog Number: 25544
Epoch time: 11083
63021989 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 234
7225 deg
Eccentricity:
0001038
Arg of perigee: 17
6642 deg
Mean anomaly: 342
4556 deg
Mean motion: 15
71999266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 325
Coasting Arc #8 (Orbit 2774)
---------------------------------------
Vector Time (GMT): 2011/084/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2773068
94 A = 6725659
25 meter
Y = -3182728
37 meter E =
0002869
Z = 5233444
53 I = 51
36619
XDOT = 5359
369323 Wp = 89
48121
YDOT = 5506
185646 meter/sec RA = 228
80664 deg
ZDOT = 508
588692 TA = 355
66749
MA = 355
66998
Ha = 193
108 n
mi
Hp = 186
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9097995
22 X = 2783029
80
Y = -10442022
22 feet Y = -3151662
36 meter
Z = 17170093
60 Z = 5246940
29
XDOT = 17583
232688 XDOT = 5294
929175
YDOT = 18064
913536 feet/sec YDOT = 5565
757074 meter/sec
ZDOT = 1668
598071 ZDOT = 534
467576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 790880
95 X = 241060
51
Y = -13758927
76 feet Y = -4193721
18 meter
Z = 17224629
85 Z = 5250067
18
XDOT = 23932
623522 XDOT = 7294
663649
YDOT = 3596
182827 feet/sec YDOT = 1096
116526 meter/sec
ZDOT = 1773
024295 ZDOT = 540
417805
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 11084
64733050
00016717 00000-0 10270-3 0 9076
2 25544 51
6460 229
5152 0001169 15
2528 344
8669 15
72082168 27751
Satellite: ISS
Catalog Number: 25544
Epoch time: 11084
64733050 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 229
5152 deg
Eccentricity:
0001169
Arg of perigee: 15
2528 deg
Mean anomaly: 344
8669 deg
Mean motion: 15
72082168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2775
Checksum: 311
Coasting Arc #9 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2011/085/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5355895
20 A = 6737140
01 meter
Y = -3937704
20 meter E =
0010892
Z = -1063518
11 I = 51
42582
XDOT = 2124
409346 Wp = 35
82273
YDOT = -4471
067544 meter/sec RA = 223
65436 deg
ZDOT = 5894
773169 TA = 312
51948
MA = 312
61142
Ha = 193
248 n
mi
Hp = 186
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17571834
64 X = -5306298
66
Y = -12918977
03 feet Y = -3997319
80 meter
Z = -3489232
63 Z = -1089416
10
XDOT = 6969
846936 XDOT = 2145
612389
YDOT = -14668
856772 feet/sec YDOT = -4447
192326 meter/sec
ZDOT = 19339
806986 ZDOT = 5905
145101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21778456
86 X = -6638073
65
Y = 792282
29 feet Y = 241487
64 meter
Z = -3593771
00 Z = -1095381
40
XDOT = -3692
929715 XDOT = -1125
604977
YDOT = -14161
886016 feet/sec YDOT = -4316
542858 meter/sec
ZDOT = 19381
746591 ZDOT = 5907
556361
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 11085
60084421
00016717 00000-0 10270-3 0 9085
2 25544 51
6459 224
6336 0001401 18
7320 341
3894 15
72073586 27909
Satellite: ISS
Catalog Number: 25544
Epoch time: 11085
60084421 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 224
6336 deg
Eccentricity:
0001401
Arg of perigee: 18
7320 deg
Mean anomaly: 341
3894 deg
Mean motion: 15
72073586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 298
Coasting Arc #10 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2011/086/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -854397
65 A = 6726639
26 meter
Y = 4425819
71 meter E =
0013904
Z = -5005568
15 I = 51
41353
XDOT = -6642
499300 Wp = 71
51426
YDOT = -3390
505760 meter/sec RA = 218
54391 deg
ZDOT = -1863
906369 TA = 180
41414
MA = 180
41529
Ha = 193
187 n
mi
Hp = 186
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2803141
88 X = -879508
72
Y = 14520405
89 feet Y = 4416124
66 meter
Z = -16422467
68 Z = -5009779
98
XDOT = -21792
976707 XDOT = -6595
037948
YDOT = -11123
706563 feet/sec YDOT = -3464
520941 meter/sec
ZDOT = -6115
178377 ZDOT = -1896
059684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7131882
87 X = 2173797
90
Y = 12933500
41 feet Y = 3942130
93 meter
Z = -16439527
06 Z = -5010767
85
XDOT = -22926
810318 XDOT = -6988
091785
YDOT = 4704
128109 feet/sec YDOT = 1433
818248 meter/sec
ZDOT = -6245
001658 ZDOT = -1903
476505
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 11086
61789247
00016717 00000-0 10270-3 0 9096
2 25544 51
6457 219
4260 0001325 18
5794 341
5416 15
72129563 28060
Satellite: ISS
Catalog Number: 25544
Epoch time: 11086
61789247 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 219
4260 deg
Eccentricity:
0001325
Arg of perigee: 18
5794 deg
Mean anomaly: 341
5416 deg
Mean motion: 15
72129563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 320
Coasting Arc #11 (Orbit 2821)
---------------------------------------
Vector Time (GMT): 2011/087/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6070698
15 A = 6735242
77 meter
Y = 1931516
13 meter E =
0014338
Z = 2167942
52 I = 51
46738
XDOT = 251
569041 Wp = 103
24330
YDOT = 5397
042753 meter/sec RA = 213
37379 deg
ZDOT = -5485
770958 TA = 52
43630
MA = 52
30615
Ha = 193
164 n
mi
Hp = 186
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19916988
69 X = 6038117
08
Y = 6336995
18 feet Y = 1999220
34 meter
Z = 7112672
32 Z = 2197354
22
XDOT = 825
357746 XDOT = 217
848040
YDOT = 17706
833178 feet/sec YDOT = 5399
667021 meter/sec
ZDOT = -17997
936213 ZDOT = -5484
631140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19240553
17 X = 5864520
60
Y = -8058614
39 feet Y = -2456265
67 meter
Z = 7231452
27 Z = 2204146
65
XDOT = 11601
192528 XDOT = 3536
043482
YDOT = 11473
649778 feet/sec YDOT = 3497
168452 meter/sec
ZDOT = -17993
385392 ZDOT = -5484
383867
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 11087
63490832
00016717 00000-0 10270-3 0 9100
2 25544 51
6452 214
2182 0001483 28
1720 331
9522 15
72184777 28229
Satellite: ISS
Catalog Number: 25544
Epoch time: 11087
63490832 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 214
2182 deg
Eccentricity:
0001483
Arg of perigee: 28
1720 deg
Mean anomaly: 331
9522 deg
Mean motion: 15
72184777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2822
Checksum: 293
Coasting Arc #12 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2011/088/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1311775
71 A = 6728239
34 meter
Y = -4797329
05 meter E =
0008953
Z = 4525077
47 I = 51
47110
XDOT = 6994
607530 Wp = 103
92006
YDOT = 988
677653 meter/sec RA = 208
28171 deg
ZDOT = 3068
643667 TA = 315
42618
MA = 315
49815
Ha = 193
088 n
mi
Hp = 186
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4303726
08 X = -1280015
24
Y = -15739268
53 feet Y = -4811820
14 meter
Z = 14846054
70 Z = 4518782
53
XDOT = 22948
187436 XDOT = 6968
125406
YDOT = 3243
693088 feet/sec YDOT = 1066
747798 meter/sec
ZDOT = 10067
728565 ZDOT = 3102
558528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13702592
41 X = -4176550
17
Y = -8901613
73 feet Y = -2713211
86 meter
Z = 14820668
22 Z = 4517339
67
XDOT = 18665
049809 XDOT = 5689
107182
YDOT = -11702
236568 feet/sec YDOT = -3566
841706 meter/sec
ZDOT = 10204
719355 ZDOT = 3110
398459
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 11088
65188880
00016717 00000-0 10270-3 0 9111
2 25544 51
6457 209
0091 0001536 25
6831 334
4408 15
72268607 28382
Satellite: ISS
Catalog Number: 25544
Epoch time: 11088
65188880 = yrday
fracday
Element set: 911
Inclination: 51
6457 deg
RA of node: 209
0091 deg
Eccentricity:
0001536
Arg of perigee: 25
6831 deg
Mean anomaly: 334
4408 deg
Mean motion: 15
72268607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 317
Coasting Arc #13 (Orbit 2852)
---------------------------------------
Vector Time (GMT): 2011/089/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5949326
72 A = 6732624
98 meter
Y = 183443
44 meter E =
0005746
Z = -3148353
75 I = 51
51360
XDOT = -2716
536291 Wp = 66
70605
YDOT = -5335
163449 meter/sec RA = 203
10230 deg
ZDOT = 4831
675943 TA = 256
61496
MA = 256
67903
Ha = 193
021 n
mi
Hp = 186
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19518788
44 X = -5935641
91
Y = 601848
56 feet Y = 116990
65 meter
Z = -10329244
60 Z = -3177221
98
XDOT = -8912
520640 XDOT = -2680
146681
YDOT = -17503
817090 feet/sec YDOT = -5365
337442 meter/sec
ZDOT = 15851
955192 ZDOT = 4818
568124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13966362
77 X = -4256947
37
Y = 13559615
36 feet Y = 4132970
76 meter
Z = -10445868
08 Z = -3183900
59
XDOT = -17463
029743 XDOT = -5322
731466
YDOT = -5838
812111 feet/sec YDOT = -1779
669931 meter/sec
ZDOT = 15799
043777 ZDOT = 4815
548543
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 11089
60528007
00016717 00000-0 10270-3 0 9127
2 25544 51
6453 204
1269 0001691 26
5591 333
5658 15
72297343 28539
Satellite: ISS
Catalog Number: 25544
Epoch time: 11089
60528007 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 204
1269 deg
Eccentricity:
0001691
Arg of perigee: 26
5591 deg
Mean anomaly: 333
5658 deg
Mean motion: 15
72297343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2853
Checksum: 310
Coasting Arc #14 (Orbit 2868)
---------------------------------------
Vector Time (GMT): 2011/090/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3357421
20 A = 6730408
92 meter
Y = 4348199
92 meter E =
0007940
Z = -3897150
96 I = 51
53430
XDOT = -6399
943845 Wp = 65
46548
YDOT = 1307
780766 meter/sec RA = 198
02218 deg
ZDOT = -4057
684965 TA = 162
17824
MA = 162
15038
Ha = 193
079 n
mi
Hp = 186
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11015161
40 X = 3327480
74
Y = 14265747
77 feet Y = 4385576
80 meter
Z = -12785928
34 Z = -3880913
98
XDOT = -20997
191094 XDOT = -6394
380726
YDOT = 4290
619310 feet/sec YDOT = 1236
243360 meter/sec
ZDOT = -13312
614715 ZDOT = -4088
762223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17858735
50 X = 5443342
58
Y = 2753777
02 feet Y = 839351
23 meter
Z = -12720360
94 Z = -3877166
01
XDOT = -12059
024168 XDOT = -3675
590566
YDOT = 16179
969321 feet/sec YDOT = 4931
654649 meter/sec
ZDOT = -13438
178202 ZDOT = -4095
956716
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 11090
62219826
00016717 00000-0 10270-3 0 9138
2 25544 51
6448 198
9180 0001788 30
9651 329
1617 15
72333329 28696
Satellite: ISS
Catalog Number: 25544
Epoch time: 11090
62219826 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 198
9180 deg
Eccentricity:
0001788
Arg of perigee: 30
9651 deg
Mean anomaly: 329
1617 deg
Mean motion: 15
72333329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2869
Checksum: 328
Coasting Arc #15 (Orbit 2884)
---------------------------------------
Vector Time (GMT): 2011/091/14:22:09
985
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5082801
67 A = 6729898
45 meter
Y = -2025044
14 meter E =
0012423
Z = 3911321
10 I = 51
56415
XDOT = 4867
871976 Wp = 72
69285
YDOT = 4395
013500 meter/sec RA = 192
84138 deg
ZDOT = -4036
232559 TA = 59
36770
MA = 59
24526
Ha = 192
870 n
mi
Hp = 185
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16675858
48 X = 5086067
94
Y = -6643845
60 feet Y = -1968186
45 meter
Z = 12832418
30 Z = 3936021
38
XDOT = 15970
708582 XDOT = 4837
971490
YDOT = 14419
335629 feet/sec YDOT = 4449
281349 meter/sec
ZDOT = -13242
232804 ZDOT = -4012
657703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7224382
60 X = 2201991
82
Y = -16354254
93 feet Y = -4984776
90 meter
Z = 12932228
81 Z = 3941743
34
XDOT = 20363
518832 XDOT = 6206
800540
YDOT = -1437
050807 feet/sec YDOT = -438
013086 meter/sec
ZDOT = -13147
013016 ZDOT = -4007
209567
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 11091
63908150
00016717 00000-0 10270-3 0 9146
2 25544 51
6457 193
7088 0001985 29
0175 331
1098 15
72430645 28858
Satellite: ISS
Catalog Number: 25544
Epoch time: 11091
63908150 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 193
7088 deg
Eccentricity:
0001985
Arg of perigee: 29
0175 deg
Mean anomaly: 331
1098 deg
Mean motion: 15
72430645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2885
Checksum: 318
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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