[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 15th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 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
138/04:38:29
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 211
9
143/12:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 210
7
145/00:25:32
425 -2
4 3
4 3
4
N/A -0
5 -0
1 220
2
000/00:07:00
850 -2
2 -0
1 212
1
Coasting Arc #1 (Orbit 1278)
---------------------------------------
Vector Time (GMT): 2012/135/14:55:43
891
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3704509
51 A = 6771751
76 meter
Y = 2145854
66 meter E =
0010412
Z = 5252099
72 I = 51
29256
XDOT = -3065
945382 Wp = 330
69132
YDOT = 6994
196412 meter/sec RA = 289
53791 deg
ZDOT = -686
750893 TA = 125
94780
MA = 125
85116
Ha = 218
555 n
mi
Hp = 212
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12153902
59 X = 3654725
09
Y = 7040205
58 feet Y = 2187002
33 meter
Z = 17231298
29 Z = 5269975
31
XDOT = -10058
875926 XDOT = -3140
591933
YDOT = 22946
838623 feet/sec YDOT = 6959
493754 meter/sec
ZDOT = -2253
119728 ZDOT = -701
826426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5769036
97 X = 1758402
47
Y = -12707108
31 feet Y = -3873126
61 meter
Z = 17304539
70 Z = 5274423
70
XDOT = 22928
913700 XDOT = 6988
732896
YDOT = 7219
083049 feet/sec YDOT = 2200
376513 meter/sec
ZDOT = -2315
715787 ZDOT = -705
830172
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 12135
66901014
00016717 00000-0 10270-3 0 9006
2 25544 51
6398 290
0126 0010964 314
7573 45
2688 15
56111618 12791
Satellite: ISS
Catalog Number: 25544
Epoch time: 12135
66901014 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 290
0126 deg
Eccentricity:
0010964
Arg of perigee: 314
7573 deg
Mean anomaly: 45
2688 deg
Mean motion: 15
56111618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1279
Checksum: 301
Coasting Arc #2 (Orbit 1293)
---------------------------------------
Vector Time (GMT): 2012/136/14:55:43
891
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2566466
10 A = 6774944
64 meter
Y = -4392480
48 meter E =
0005103
Z = -4473083
54 I = 51
29410
XDOT = 4101
503757 Wp = 18
94581
YDOT = -5641
979337 meter/sec RA = 284
49785 deg
ZDOT = 3192
814022 TA = 283
25747
MA = 283
31439
Ha = 218
681 n
mi
Hp = 212
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8420164
37 X = -2495428
27
Y = -14411025
18 feet Y = -4420783
01 meter
Z = -14675470
92 Z = -4485378
99
XDOT = 13456
377154 XDOT = 4148
778537
YDOT = -18510
430897 feet/sec YDOT = -5595
849516 meter/sec
ZDOT = 10475
111622 ZDOT = 3212
853893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13312066
78 X = -4057517
95
Y = 9994622
06 feet Y = 3046360
80 meter
Z = -14725578
76 Z = -4488356
41
XDOT = -19249
903443 XDOT = -5867
370570
YDOT = -10111
596393 feet/sec YDOT = -3082
014581 meter/sec
ZDOT = 10557
970991 ZDOT = 3218
069558
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 12136
63231727
00016717 00000-0 10270-3 0 9012
2 25544 51
6396 285
1964 0010941 318
2955 41
7364 15
56130269 12944
Satellite: ISS
Catalog Number: 25544
Epoch time: 12136
63231727 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 285
1964 deg
Eccentricity:
0010941
Arg of perigee: 318
2955 deg
Mean anomaly: 41
7364 deg
Mean motion: 15
56130269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1294
Checksum: 310
Coasting Arc #3 (Orbit 1309)
---------------------------------------
Vector Time (GMT): 2012/137/14:55:43
891
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1256699
20 A = 6780215
05 meter
Y = 6051443
66 meter E =
0009097
Z = 2790959
85 I = 51
30477
XDOT = -4680
663050 Wp = 46
11656
YDOT = 3323
012717 meter/sec RA = 279
47373 deg
ZDOT = -5080
897552 TA = 102
05966
MA = 101
95770
Ha = 218
976 n
mi
Hp = 212
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4123028
88 X = 1175379
28
Y = 19853817
77 feet Y = 6065042
08 meter
Z = 9156692
42 Z = 2796867
57
XDOT = -15356
506068 XDOT = -4692
791559
YDOT = 10902
272695 feet/sec YDOT = 3270
602973 meter/sec
ZDOT = -16669
611390 ZDOT = -5103
665703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19112237
83 X = 5825410
09
Y = -6742475
10 feet Y = -2055106
41 meter
Z = 9180406
20 Z = 2798187
81
XDOT = 12392
103456 XDOT = 3777
113133
YDOT = 12228
080137 feet/sec YDOT = 3727
118826 meter/sec
ZDOT = -16763
461910 ZDOT = -5109
503190
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 12137
65983037
00016717 00000-0 10270-3 0 9024
2 25544 51
6394 280
0582 0010918 322
6046 37
4347 15
56122486 13100
Satellite: ISS
Catalog Number: 25544
Epoch time: 12137
65983037 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 280
0582 deg
Eccentricity:
0010918
Arg of perigee: 322
6046 deg
Mean anomaly: 37
4347 deg
Mean motion: 15
56122486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1310
Checksum: 298
Coasting Arc #4 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2012/138/04:38:29
000
Vector Time (MET): N/A
Weight (LBS) : 926926
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3645341
77 A = 6772930
65 meter
Y = 2885124
79 meter E =
0013024
Z = 4930760
34 I = 51
27899
XDOT = -2538
075928 Wp = 355
16043
YDOT = 6907
143004 meter/sec RA = 276
61082 deg
ZDOT = -2152
803479 TA = 115
99985
MA = 115
86566
Ha = 219
169 n
mi
Hp = 211
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11959782
72 X = 3588855
88
Y = 9465632
52 feet Y = 2925573
25 meter
Z = 16177035
22 Z = 4948332
43
XDOT = -8327
020760 XDOT = -2604
666367
YDOT = 22661
230329 feet/sec YDOT = 6878
388417 meter/sec
ZDOT = -7063
003540 ZDOT = -2165
295041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1187552
56 X = -361966
02
Y = 15129173
44 feet Y = 4611372
07 meter
Z = 16248966
12 Z = 4952684
87
XDOT = -22304
903958 XDOT = -6798
534726
YDOT = 5934
070108 feet/sec YDOT = 1808
704569 meter/sec
ZDOT = -7114
960920 ZDOT = -2168
640088
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 12138
23779812
00016717 00000-0 10270-3 0 9034
2 25544 51
6400 277
1702 0011528 326
2501 33
7917 15
56188351 13197
Satellite: ISS
Catalog Number: 25544
Epoch time: 12138
23779812 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 277
1702 deg
Eccentricity:
0011528
Arg of perigee: 326
2501 deg
Mean anomaly: 33
7917 deg
Mean motion: 15
56188351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 295
Coasting Arc #5 (Orbit 1333)
---------------------------------------
Vector Time (GMT): 2012/139/04:38:29
000
Vector Time (MET): N/A
Weight (LBS) : 926926
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2757164
78 A = 6777793
20 meter
Y = -5022651
29 meter E =
0009195
Z = -3611815
03 I = 51
29290
XDOT = 3648
463635 Wp = 357
35177
YDOT = -5142
397868 meter/sec RA = 271
57699 deg
ZDOT = 4374
544847 TA = 319
54137
MA = 319
60971
Ha = 219
346 n
mi
Hp = 211
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9045816
21 X = -2683249
85
Y = -16478514
72 feet Y = -5053070
14 meter
Z = -11849786
85 Z = -3625030
18
XDOT = 11970
025050 XDOT = 3684
444874
YDOT = -16871
384081 feet/sec YDOT = -5101
397534 meter/sec
ZDOT = 14352
181256 ZDOT = 4392
356374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8325115
89 X = 2537495
32
Y = -16816119
32 feet Y = -5125553
17 meter
Z = -11903623
95 Z = -3628224
58
XDOT = 19408
791742 XDOT = 5915
799723
YDOT = -583
110991 feet/sec YDOT = -177
732230 meter/sec
ZDOT = 14425
832832 ZDOT = 4396
993847
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 12139
20107024
00016717 00000-0 10270-3 0 9043
2 25544 51
6402 272
3527 0011592 329
8368 30
2117 15
56170660 13347
Satellite: ISS
Catalog Number: 25544
Epoch time: 12139
20107024 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 272
3527 deg
Eccentricity:
0011592
Arg of perigee: 329
8368 deg
Mean anomaly: 30
2117 deg
Mean motion: 15
56170660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1334
Checksum: 274
Coasting Arc #6 (Orbit 1349)
---------------------------------------
Vector Time (GMT): 2012/140/04:38:29
000
Vector Time (MET): N/A
Weight (LBS) : 926926
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1620791
71 A = 6782379
82 meter
Y = 6404233
78 meter E =
0008236
Z = 1540679
89 I = 51
30845
XDOT = -4440
796379 Wp = 62
24002
YDOT = 2507
096766 meter/sec RA = 266
56307 deg
ZDOT = -5722
384898 TA = 100
84275
MA = 100
75005
Ha = 219
577 n
mi
Hp = 211
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5317558
10 X = 1541573
39
Y = 21011265
67 feet Y = 6421915
43 meter
Z = 5054724
06 Z = 1548361
80
XDOT = -14569
541925 XDOT = -4440
702613
YDOT = 8225
383091 feet/sec YDOT = 2457
437956 meter/sec
ZDOT = -18774
228669 ZDOT = -5743
958095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13868841
01 X = -4227222
74
Y = 16646044
72 feet Y = 5073714
43 meter
Z = 5085704
36 Z = 1550122
69
XDOT = -13945
339381 XDOT = -4250
539443
YDOT = -5828
458594 feet/sec YDOT = -1776
514180 meter/sec
ZDOT = -18863
096853 ZDOT = -5749
471921
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 12140
22854637
00016717 00000-0 10270-3 0 9057
2 25544 51
6403 267
2143 0011458 333
9764 26
0812 15
56169174 13503
Satellite: ISS
Catalog Number: 25544
Epoch time: 12140
22854637 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 267
2143 deg
Eccentricity:
0011458
Arg of perigee: 333
9764 deg
Mean anomaly: 26
0812 deg
Mean motion: 15
56169174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1350
Checksum: 294
Coasting Arc #7 (Orbit 1365)
---------------------------------------
Vector Time (GMT): 2012/141/04:38:29
000
Vector Time (MET): N/A
Weight (LBS) : 926926
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -321279
85 A = 6782946
03 meter
Y = -6710607
63 meter E =
0019699
Z = 833246
34 I = 51
31369
XDOT = 4867
382059 Wp = 18
64197
YDOT = 504
592930 meter/sec RA = 261
55923 deg
ZDOT = 5920
123468 TA = 350
43041
MA = 350
46789
Ha = 219
645 n
mi
Hp = 211
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1054067
73 X = -250264
38
Y = -22016429
22 feet Y = -6713803
38 meter
Z = 2733747
84 Z = 831857
47
XDOT = 15969
101242 XDOT = 4832
618687
YDOT = 1655
488614 feet/sec YDOT = 558
828121 meter/sec
ZDOT = 19422
977258 ZDOT = 5943
685033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16923105
39 X = 5158162
52
Y = -14123405
00 feet Y = -4304813
84 meter
Z = 2728649
25 Z = 831692
29
XDOT = 7201
091451 XDOT = 2194
892674
YDOT = 12412
751120 feet/sec YDOT = 3783
406541 meter/sec
ZDOT = 19519
746436 ZDOT = 5949
618714
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 12141
25600489
00016717 00000-0 10270-3 0 9066
2 25544 51
6403 262
0750 0011704 337
3483 22
7153 15
56228972 13660
Satellite: ISS
Catalog Number: 25544
Epoch time: 12141
25600489 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 262
0750 deg
Eccentricity:
0011704
Arg of perigee: 337
3483 deg
Mean anomaly: 22
7153 deg
Mean motion: 15
56228972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1366
Checksum: 290
Coasting Arc #8 (Orbit 1380)
---------------------------------------
Vector Time (GMT): 2012/142/04:38:29
000
Vector Time (MET): N/A
Weight (LBS) : 926926
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1091414
71 A = 6779274
57 meter
Y = 5958680
85 meter E =
0009708
Z = -3055534
18 I = 51
30630
XDOT = -4832
277061 Wp = 2
18058
YDOT = -3393
268214 meter/sec RA = 256
55059 deg
ZDOT = -4882
234192 TA = 213
05947
MA = 213
12019
Ha = 219
855 n
mi
Hp = 211
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3580756
91 X = -1143121
43
Y = 19549477
87 feet Y = 5946187
18 meter
Z = -10024718
43 Z = -3060961
30
XDOT = -15853
927365 XDOT = -4770
256508
YDOT = -11132
769731 feet/sec YDOT = -3446
958452 meter/sec
ZDOT = -16017
828714 ZDOT = -4905
559270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17563763
27 X = -5353435
04
Y = 9276836
37 feet Y = 2827579
72 meter
Z = -10047557
48 Z = -3062495
52
XDOT = -266
735992 XDOT = -81
301130
YDOT = -17989
050608 feet/sec YDOT = -5483
062625 meter/sec
ZDOT = -16113
372690 ZDOT = -4911
355996
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 12142
21923608
00016717 00000-0 10270-3 0 9075
2 25544 51
6397 257
2580 0011736 340
4219 19
6482 15
56220407 13818
Satellite: ISS
Catalog Number: 25544
Epoch time: 12142
21923608 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 257
2580 deg
Eccentricity:
0011736
Arg of perigee: 340
4219 deg
Mean anomaly: 19
6482 deg
Mean motion: 15
56220407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1381
Checksum: 297
Coasting Arc #9 (Orbit 1396)
---------------------------------------
Vector Time (GMT): 2012/143/04:38:29
000
Vector Time (MET): N/A
Weight (LBS) : 926926
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2511416
27 A = 6773960
66 meter
Y = -4232686
27 meter E =
0008965
Z = 4647029
25 I = 51
29650
XDOT = 4306
529948 Wp = 28
38149
YDOT = 5679
452772 meter/sec RA = 251
52221 deg
ZDOT = 2851
146056 TA = 33
22742
MA = 33
17116
Ha = 219
972 n
mi
Hp = 210
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8239554
70 X = 2535985
84
Y = -13886765
98 feet Y = -4204465
21 meter
Z = 15246158
97 Z = 4659288
97
XDOT = 14129
035263 XDOT = 4228
850659
YDOT = 18633
375237 feet/sec YDOT = 5727
176401 meter/sec
ZDOT = 9354
153726 ZDOT = 2871
879243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15916657
75 X = 4851397
28
Y = -2417043
60 feet Y = -736714
89 meter
Z = 15296921
28 Z = 4662501
61
XDOT = -5788
377833 XDOT = -1764
297563
YDOT = 21505
274810 feet/sec YDOT = 6554
807762 meter/sec
ZDOT = 9438
851473 ZDOT = 2876
961929
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 12143
24666900
00016717 00000-0 10270-3 0 9089
2 25544 51
6395 252
1184 0011850 345
2823 14
7984 15
56230569 13971
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
24666900 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 252
1184 deg
Eccentricity:
0011850
Arg of perigee: 345
2823 deg
Mean anomaly: 14
7984 deg
Mean motion: 15
56230569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1397
Checksum: 314
Coasting Arc #10 (Orbit 1401)
---------------------------------------
Vector Time (GMT): 2012/143/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 947811
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4243381
31 A = 6771234
67 meter
Y = -627550
70 meter E =
0012462
Z = 5240681
52 I = 51
29199
XDOT = 2046
483371 Wp = 359
67730
YDOT = 7353
574998 meter/sec RA = 249
84612 deg
ZDOT = -764
233162 TA = 97
72824
MA = 97
58672
Ha = 219
712 n
mi
Hp = 210
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13921854
69 X = 4224624
95
Y = -2058893
38 feet Y = -580204
07 meter
Z = 17193837
00 Z = 5261250
31
XDOT = 6714
184288 XDOT = 1967
814618
YDOT = 24125
902224 feet/sec YDOT = 7376
020268 meter/sec
ZDOT = -2507
326647 ZDOT = -754
481539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3448725
14 X = 1051171
42
Y = -13536889
88 feet Y = -4126044
04 meter
Z = 17278426
37 Z = 5266464
36
XDOT = 23863
206046 XDOT = 7273
505203
YDOT = 2878
462551 feet/sec YDOT = 877
355385 meter/sec
ZDOT = -2467
906232 ZDOT = -752
217819
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 12143
56773734
00016717 00000-0 10270-3 0 9099
2 25544 51
6403 250
5098 0011348 345
4586 14
6240 15
56296618 14025
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
56773734 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 250
5098 deg
Eccentricity:
0011348
Arg of perigee: 345
4586 deg
Mean anomaly: 14
6240 deg
Mean motion: 15
56296618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1402
Checksum: 308
Coasting Arc #11 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2012/144/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 947811
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4787324
72 A = 6774610
74 meter
Y = -1879138
98 meter E =
0010270
Z = -4410955
76 I = 51
31452
XDOT = -324
032789 Wp = 40
13635
YDOT = -6911
867946 meter/sec RA = 244
80619 deg
ZDOT = 3308
268004 TA = 263
35005
MA = 263
46695
Ha = 219
831 n
mi
Hp = 210
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15706445
93 X = -4744528
36
Y = -6165154
13 feet Y = -1932433
99 meter
Z = -14471639
64 Z = -4434108
87
XDOT = -1063
099701 XDOT = -262
789766
YDOT = -22676
732107 feet/sec YDOT = -6915
149450 meter/sec
ZDOT = 10853
897651 ZDOT = 3306
841782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11520520
83 X = -3511454
75
Y = 12215588
61 feet Y = 3723311
41 meter
Z = -14566637
14 Z = -4439911
00
XDOT = -20585
744384 XDOT = -6274
534888
YDOT = -6524
517884 feet/sec YDOT = -1988
673051 meter/sec
ZDOT = 10848
646666 ZDOT = 3306
667504
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 12144
53093835
00016717 00000-0 10270-3 0 9106
2 25544 51
6399 245
6936 0011322 349
4267 10
6647 15
56309246 14172
Satellite: ISS
Catalog Number: 25544
Epoch time: 12144
53093835 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 245
6936 deg
Eccentricity:
0011322
Arg of perigee: 349
4267 deg
Mean anomaly: 10
6647 deg
Mean motion: 15
56309246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1417
Checksum: 312
Coasting Arc #12 (Orbit 1424)
---------------------------------------
Vector Time (GMT): 2012/145/00:29:02
850
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -264430
26 A = 6779298
98 meter
Y = 5734343
69 meter E =
0010458
Z = -3618022
30 I = 51
32999
XDOT = -5525
221543 Wp = 13
73510
YDOT = -3014
857936 meter/sec RA = 242
34872 deg
ZDOT = -4367
174850 TA = 209
33774
MA = 209
39650
Ha = 220
224 n
mi
Hp = 212
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -867553
35 X = -310957
53
Y = 18813463
54 feet Y = 5731126
95 meter
Z = -11870151
92 Z = -3619419
24
XDOT = -18127
367266 XDOT = -5469
883218
YDOT = -9891
266194 feet/sec YDOT = -3076
334447 meter/sec
ZDOT = -14328
001478 ZDOT = -4393
882292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17208983
78 X = -5245298
25
Y = -7642095
01 feet Y = -2329310
56 meter
Z = -11876397
89 Z = -3619926
08
XDOT = 15263
760637 XDOT = 4652
394242
YDOT = -11897
415215 feet/sec YDOT = -3626
332157 meter/sec
ZDOT = -14437
514617 ZDOT = -4400
554455
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 12145
04464936
00016717 00000-0 10270-3 0 9118
2 25544 51
6394 243
1260 0009830 342
8517 17
2303 15
55669355 14256
Satellite: ISS
Catalog Number: 25544
Epoch time: 12145
04464936 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 243
1260 deg
Eccentricity:
0009830
Arg of perigee: 342
8517 deg
Mean anomaly: 17
2303 deg
Mean motion: 15
55669355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1425
Checksum: 298
Coasting Arc #13 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2012/146/00:29:02
850
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1877437
72 A = 6774632
09 meter
Y = -4304001
38 meter E =
0006949
Z = 4878084
20 I = 51
32895
XDOT = 5380
019788 Wp = 30
02373
YDOT = 4961
382962 meter/sec RA = 237
32289 deg
ZDOT = 2311
362874 TA = 37
31085
MA = 37
26260
Ha = 220
247 n
mi
Hp = 211
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6159572
56 X = 1901729
65
Y = -14120739
43 feet Y = -4282871
43 meter
Z = 16004213
24 Z = 4887263
27
XDOT = 17650
983557 XDOT = 5312
912601
YDOT = 16277
503155 feet/sec YDOT = 5021
170195 meter/sec
ZDOT = 7583
211530 ZDOT = 2337
336458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11095431
79 X = 3381887
61
Y = 10630419
49 feet Y = 3240151
86 meter
Z = 16042320
04 Z = 4889699
15
XDOT = -20644
451426 XDOT = -6292
428795
YDOT = 9965
390742 feet/sec YDOT = 3037
451098 meter/sec
ZDOT = 7689
554017 ZDOT = 2343
776064
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 12146
07246409
00016717 00000-0 10270-3 0 9126
2 25544 51
6388 237
9895 0009818 346
5339 13
5551 15
55683706 14411
Satellite: ISS
Catalog Number: 25544
Epoch time: 12146
07246409 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 237
9895 deg
Eccentricity:
0009818
Arg of perigee: 346
5339 deg
Mean anomaly: 13
5551 deg
Mean motion: 15
55683706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 331
Coasting Arc #14 (Orbit 1455)
---------------------------------------
Vector Time (GMT): 2012/147/00:29:02
850
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3450761
63 A = 6772752
27 meter
Y = 2460774
08 meter E =
0016263
Z = -5293964
54 I = 51
34057
XDOT = -4589
879928 Wp = 54
32947
YDOT = -6132
812595 meter/sec RA = 232
28620 deg
ZDOT = 150
757133 TA = 217
05822
MA = 217
17064
Ha = 220
409 n
mi
Hp = 211
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11321396
43 X = -3452305
08
Y = 8073405
77 feet Y = 2422177
43 meter
Z = -17368650
06 Z = -5310731
74
XDOT = -15058
661182 XDOT = -4521
692783
YDOT = -20120
776230 feet/sec YDOT = -6183
758232 meter/sec
ZDOT = 494
610015 ZDOT = 128
624647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3853226
61 X = -1174463
47
Y = -13270263
07 feet Y = -4044776
18 meter
Z = -17437794
17 Z = -5315039
66
XDOT = 23033
489170 XDOT = 7020
607499
YDOT = -7177
836014 feet/sec YDOT = -2187
804417 meter/sec
ZDOT = 404
142001 ZDOT = 123
182482
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 12147
03602821
00016717 00000-0 10270-3 0 9138
2 25544 51
6391 233
1743 0009935 350
1229 9
9727 15
55712537 14569
Satellite: ISS
Catalog Number: 25544
Epoch time: 12147
03602821 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 233
1743 deg
Eccentricity:
0009935
Arg of perigee: 350
1229 deg
Mean anomaly: 9
9727 deg
Mean motion: 15
55712537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1456
Checksum: 301
Coasting Arc #15 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2012/148/00:29:02
850
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4805662
38 A = 6774875
07 meter
Y = -404795
32 meter E =
0014583
Z = 4759247
31 I = 51
36717
XDOT = 3150
517678 Wp = 21
68782
YDOT = 6485
780338 meter/sec RA = 227
25083 deg
ZDOT = -2613
717616 TA = 94
26098
MA = 94
09431
Ha = 220
463 n
mi
Hp = 211
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15766608
86 X = 4786712
31
Y = -1328068
63 feet Y = -351161
79 meter
Z = 15614328
45 Z = 4782547
00
XDOT = 10336
344088 XDOT = 3090
455085
YDOT = 21278
806882 feet/sec YDOT = 6520
675770 meter/sec
ZDOT = -8575
189028 ZDOT = -2598
557845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3732035
82 X = -1137524
52
Y = 15278078
79 feet Y = 4656758
42 meter
Z = 15710162
04 Z = 4788457
39
XDOT = -22364
511714 XDOT = -6816
703170
YDOT = 3344
356605 feet/sec YDOT = 1019
359893 meter/sec
ZDOT = -8513
403100 ZDOT = -2594
885265
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 12148
06381620
00016717 00000-0 10270-3 0 9144
2 25544 51
6387 228
0376 0010073 353
4111 6
6908 15
55751307 14721
Satellite: ISS
Catalog Number: 25544
Epoch time: 12148
06381620 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 228
0376 deg
Eccentricity:
0010073
Arg of perigee: 353
4111 deg
Mean anomaly: 6
6908 deg
Mean motion: 15
55751307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 289
Coasting Arc #16 (Orbit 1486)
---------------------------------------
Vector Time (GMT): 2012/149/00:29:02
850
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5670560
35 A = 6779632
84 meter
Y = -1480148
26 meter E =
0010897
Z = -3401958
21 I = 51
40471
XDOT = -1177
208884 Wp = 24
02299
YDOT = -6026
039666 meter/sec RA = 222
23043 deg
ZDOT = 4599
043092 TA = 296
01081
MA = 296
12300
Ha = 220
587 n
mi
Hp = 211
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18604200
61 X = -5637061
58
Y = -4856129
45 feet Y = -1543372
43 meter
Z = -11161280
21 Z = -3429424
37
XDOT = -3862
233872 XDOT = -1132
078176
YDOT = -19770
471344 feet/sec YDOT = -6038
951931 meter/sec
ZDOT = 15088
724054 ZDOT = 4593
433438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10229048
73 X = 3117814
05
Y = -16202892
63 feet Y = -4938641
67 meter
Z = -11274097
83 Z = -3436345
02
XDOT = 18858
886854 XDOT = 5748
188713
YDOT = 1456
461242 feet/sec YDOT = 443
929386 meter/sec
ZDOT = 15066
156543 ZDOT = 4592
164514
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 12149
02735689
00016717 00000-0 10270-3 0 9150
2 25544 51
6390 223
2219 0010102 356
8848 3
2241 15
55736831 14879
Satellite: ISS
Catalog Number: 25544
Epoch time: 12149
02735689 = yrday
fracday
Element set: 915
Inclination: 51
6390 deg
RA of node: 223
2219 deg
Eccentricity:
0010102
Arg of perigee: 356
8848 deg
Mean anomaly: 3
2241 deg
Mean motion: 15
55736831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1487
Checksum: 303
Coasting Arc #17 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2012/150/00:29:02
850
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5884290
68 A = 6783811
47 meter
Y = 3072876
65 meter E =
0012744
Z = 1396691
37 I = 51
44164
XDOT = -1173
209150 Wp = 75
59122
YDOT = 4895
616769 meter/sec RA = 217
22893 deg
ZDOT = -5780
706770 TA = 89
14308
MA = 88
99707
Ha = 220
801 n
mi
Hp = 210
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19305415
61 X = 5842706
96
Y = 10081616
30 feet Y = 3138445
84 meter
Z = 4582320
75 Z = 1425176
34
XDOT = -3849
111385 XDOT = -1199
784197
YDOT = 16061
734807 feet/sec YDOT = 4882
348980 meter/sec
ZDOT = -18965
573394 ZDOT = -5786
470456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15167956
46 X = -4623193
13
Y = 15594430
53 feet Y = 4753182
43 meter
Z = 4699208
01 Z = 1432318
60
XDOT = -13187
934383 XDOT = -4019
682400
YDOT = -7059
210277 feet/sec YDOT = -2151
647292 meter/sec
ZDOT = -18989
676166 ZDOT = -5788
053295
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 12150
05512148
00016717 00000-0 10270-3 0 9169
2 25544 51
6390 218
0851 0009983 1
2689 358
8488 15
55727796 15033
Satellite: ISS
Catalog Number: 25544
Epoch time: 12150
05512148 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 218
0851 deg
Eccentricity:
0009983
Arg of perigee: 1
2689 deg
Mean anomaly: 358
8488 deg
Mean motion: 15
55727796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 326
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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