[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 16th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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
1
000/00:00:00
000 0
0 0
0 212
0
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
419 -2
4 3
4 3
4
N/A -0
5 -0
1 220
2
000/00:07:00
838 -2
2 -0
1 212
2
Coasting Arc #1 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2012/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1480436
75 A = 6783332
96 meter
Y = 6609664
30 meter E =
0000871
Z = -370926
85 I = 51
31368
XDOT = -4611
127722 Wp = 69
42326
YDOT = -1367
139428 meter/sec RA = 280
11149 deg
ZDOT = -5968
746899 TA = 114
59363
MA = 114
58455
Ha = 218
902 n
mi
Hp = 212
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4857075
95 X = -1552435
43
Y = 21685250
32 feet Y = 6592706
58 meter
Z = -1216951
62 Z = -378293
56
XDOT = -15128
371791 XDOT = -4566
502140
YDOT = -4485
365576 feet/sec YDOT = -1418
454239 meter/sec
ZDOT = -19582
502951 ZDOT = -5991
039510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14635425
11 X = 4460877
57
Y = 16720331
80 feet Y = 5096357
13 meter
Z = -1247828
45 Z = -380338
11
XDOT = -11265
240315 XDOT = -3433
645248
YDOT = 8394
939843 feet/sec YDOT = 2558
777664 meter/sec
ZDOT = -19673
966762 ZDOT = -5996
625069
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
53138641
00016717 00000-0 10270-3 0 9002
2 25544 51
6368 280
6985 0011027 321
9512 38
0862 15
56170088 13083
Satellite: ISS
Catalog Number: 25544
Epoch time: 12137
53138641 = yrday
fracday
Element set: 900
Inclination: 51
6368 deg
RA of node: 280
6985 deg
Eccentricity:
0011027
Arg of perigee: 321
9512 deg
Mean anomaly: 38
0862 deg
Mean motion: 15
56170088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 299
Coasting Arc #2 (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 = 3643107
04 A = 6772903
38 meter
Y = 2891185
05 meter E =
0012964
Z = 4928914
91 I = 51
27910
XDOT = -2542
238686 Wp = 354
60900
YDOT = 6903
816109 meter/sec RA = 276
61147 deg
ZDOT = -2158
345605 TA = 116
60767
MA = 116
47479
Ha = 219
119 n
mi
Hp = 211
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11952450
92 X = 3586562
51
Y = 9485515
24 feet Y = 2931608
19 meter
Z = 16170980
67 Z = 4946476
00
XDOT = -8340
678105 XDOT = -2608
764691
YDOT = 22650
315319 feet/sec YDOT = 6875
015332 meter/sec
ZDOT = -7081
186367 ZDOT = -2170
857233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1208105
55 X = -368230
57
Y = 15134281
92 feet Y = 4612929
13 meter
Z = 16242865
82 Z = 4950825
50
XDOT = -22303
088706 XDOT = -6797
981437
YDOT = 5918
231462 feet/sec YDOT = 1803
876950 meter/sec
ZDOT = -7133
225886 ZDOT = -2174
207250
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
23778720
00016717 00000-0 10270-3 0 9019
2 25544 51
6401 277
1710 0011542 325
4941 34
5462 15
56200476 13199
Satellite: ISS
Catalog Number: 25544
Epoch time: 12138
23778720 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 277
1710 deg
Eccentricity:
0011542
Arg of perigee: 325
4941 deg
Mean anomaly: 34
5462 deg
Mean motion: 15
56200476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 282
Coasting Arc #3 (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 = -2751484
25 A = 6777785
02 meter
Y = -5030507
64 meter E =
0009160
Z = -3605084
15 I = 51
29304
XDOT = 3653
905291 Wp = 356
36725
YDOT = -5132
602848 meter/sec RA = 271
57760 deg
ZDOT = 4381
622587 TA = 320
62535
MA = 320
69191
Ha = 219
299 n
mi
Hp = 211
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9027179
29 X = -2677514
59
Y = -16504290
15 feet Y = -5060862
66 meter
Z = -11827703
90 Z = -3618271
56
XDOT = 11987
878252 XDOT = 3689
742213
YDOT = -16839
248190 feet/sec YDOT = -5091
542470 meter/sec
ZDOT = 14375
402188 ZDOT = 4399
460199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8356841
71 X = 2547165
35
Y = -16815797
43 feet Y = -5125455
06 meter
Z = -11881426
35 Z = -3621458
75
XDOT = 19392
701497 XDOT = 5910
895416
YDOT = -552
457018 feet/sec YDOT = -168
388899 meter/sec
ZDOT = 14449
160046 ZDOT = 4404
103982
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
20105249
00016717 00000-0 10270-3 0 9028
2 25544 51
6404 272
3534 0011603 329
0818 30
9651 15
56180653 13345
Satellite: ISS
Catalog Number: 25544
Epoch time: 12139
20105249 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 272
3534 deg
Eccentricity:
0011603
Arg of perigee: 329
0818 deg
Mean anomaly: 30
9651 deg
Mean motion: 15
56180653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1334
Checksum: 277
Coasting Arc #4 (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 = 1611941
02 A = 6782372
48 meter
Y = 6409150
39 meter E =
0008051
Z = 1529380
01 I = 51
30858
XDOT = -4444
937764 Wp = 62
28006
YDOT = 2490
783770 meter/sec RA = 266
56372 deg
ZDOT = -5726
320431 TA = 100
93045
MA = 100
83985
Ha = 219
533 n
mi
Hp = 211
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5288520
40 X = 1532723
27
Y = 21027396
30 feet Y = 6426733
08 meter
Z = 5017650
94 Z = 1537018
92
XDOT = -14583
129146 XDOT = -4444
642156
YDOT = 8171
862761 feet/sec YDOT = 2441
079776 meter/sec
ZDOT = -18787
140523 ZDOT = -5747
913258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13898842
67 X = -4236367
24
Y = 16632256
23 feet Y = 5069511
70 meter
Z = 5048454
13 Z = 1538768
82
XDOT = -13911
042589 XDOT = -4240
085781
YDOT = -5868
705938 feet/sec YDOT = -1788
781570 meter/sec
ZDOT = -18876
087877 ZDOT = -5753
431585
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
22852275
00016717 00000-0 10270-3 0 9031
2 25544 51
6404 267
2150 0011465 333
2071 26
8489 15
56176811 13508
Satellite: ISS
Catalog Number: 25544
Epoch time: 12140
22852275 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 267
2150 deg
Eccentricity:
0011465
Arg of perigee: 333
2071 deg
Mean anomaly: 26
8489 deg
Mean motion: 15
56176811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1350
Checksum: 283
Coasting Arc #5 (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 = -309534
97 A = 6782919
53 meter
Y = -6709411
13 meter E =
0019594
Z = 847443
39 I = 51
31373
XDOT = 4868
305360 Wp = 18
40757
YDOT = 525
241602 meter/sec RA = 261
55987 deg
ZDOT = 5917
505486 TA = 350
82068
MA = 350
85645
Ha = 219
607 n
mi
Hp = 211
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1015534
69 X = -238602
73
Y = -22012503
70 feet Y = -6712476
01 meter
Z = 2780326
08 Z = 846111
37
XDOT = 15972
130446 XDOT = 4833
323739
YDOT = 1723
233603 feet/sec YDOT = 579
485898 meter/sec
ZDOT = 19414
388077 ZDOT = 5941
071008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16943022
80 X = 5164233
35
Y = -14090515
88 feet Y = -4294789
24 meter
Z = 2775461
00 Z = 845960
51
XDOT = 7151
288609 XDOT = 2179
712768
YDOT = 12454
586662 feet/sec YDOT = 3796
158015 meter/sec
ZDOT = 19511
171643 ZDOT = 5947
005117
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
25597689
00016717 00000-0 10270-3 0 9041
2 25544 51
6404 262
0757 0011711 336
5974 23
4646 15
56234561 13668
Satellite: ISS
Catalog Number: 25544
Epoch time: 12141
25597689 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 262
0757 deg
Eccentricity:
0011711
Arg of perigee: 336
5974 deg
Mean anomaly: 23
4646 deg
Mean motion: 15
56234561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1366
Checksum: 313
Coasting Arc #6 (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 = -1104080
84 A = 6779230
98 meter
Y = 5949695
22 meter E =
0009708
Z = -3068236
56 I = 51
30626
XDOT = -4828
623825 Wp = 1
40340
YDOT = -3413
281575 meter/sec RA = 256
55113 deg
ZDOT = -4872
032734 TA = 214
00575
MA = 214
06800
Ha = 219
821 n
mi
Hp = 211
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3622312
46 X = -1155624
43
Y = 19519997
45 feet Y = 5937060
82 meter
Z = -10066392
90 Z = -3073724
81
XDOT = -15841
941682 XDOT = -4766
429307
YDOT = -11198
430364 feet/sec YDOT = -3466
929988 meter/sec
ZDOT = -15984
359362 ZDOT = -4895
339643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17566000
71 X = -5354117
02
Y = 9226141
03 feet Y = 2812127
78 meter
Z = -10089482
37 Z = -3075274
23
XDOT = -211
466008 XDOT = -64
454839
YDOT = -18020
076775 feet/sec YDOT = -5492
519401 meter/sec
ZDOT = -16079
826875 ZDOT = -4901
131231
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
21920529
00016717 00000-0 10270-3 0 9052
2 25544 51
6399 257
2587 0011743 339
6727 20
3958 15
56223972 13816
Satellite: ISS
Catalog Number: 25544
Epoch time: 12142
21920529 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 257
2587 deg
Eccentricity:
0011743
Arg of perigee: 339
6727 deg
Mean anomaly: 20
3958 deg
Mean motion: 15
56223972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1381
Checksum: 322
Coasting Arc #7 (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 = 2523413
50 A = 6773924
97 meter
Y = -4216958
62 meter E =
0008833
Z = 4654978
50 I = 51
29647
XDOT = 4297
462579 Wp = 27
38329
YDOT = 5694
417245 meter/sec RA = 251
52260 deg
ZDOT = 2834
548575 TA = 34
40583
MA = 34
34867
Ha = 219
940 n
mi
Hp = 210
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8278915
67 X = 2547767
69
Y = -13835166
07 feet Y = -4188604
61 meter
Z = 15272239
17 Z = 4667295
98
XDOT = 14099
286676 XDOT = 4219
697256
YDOT = 18682
471275 feet/sec YDOT = 5742
038998 meter/sec
ZDOT = 9299
700049 ZDOT = 2855
237506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15901263
58 X = 4846705
14
Y = -2354095
27 feet Y = -717528
24 meter
Z = 15323237
45 Z = 4670522
78
XDOT = -5840
447261 XDOT = -1780
168325
YDOT = 21514
465262 feet/sec YDOT = 6557
609012 meter/sec
ZDOT = 9384
214575 ZDOT = 2860
308602
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
24663665
00016717 00000-0 10270-3 0 9062
2 25544 51
6397 252
1191 0011852 344
5399 15
5391 15
56231993 13976
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
24663665 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 252
1191 deg
Eccentricity:
0011852
Arg of perigee: 344
5399 deg
Mean anomaly: 15
5391 deg
Mean motion: 15
56231993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1397
Checksum: 322
Coasting Arc #8 (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 = 4249095
73 A = 6771242
87 meter
Y = -607111
98 meter E =
0012463
Z = 5238615
73 I = 51
29211
XDOT = 2031
279026 Wp = 359
08098
YDOT = 7355
687564 meter/sec RA = 249
84644 deg
ZDOT = -782
902263 TA = 98
50476
MA = 98
36349
Ha = 219
684 n
mi
Hp = 210
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13940602
79 X = 4230120
43
Y = -1991837
19 feet Y = -559702
66 meter
Z = 17187059
48 Z = 5259211
76
XDOT = 6664
301266 XDOT = 1952
678471
YDOT = 24132
833214 feet/sec YDOT = 7377
963193 meter/sec
ZDOT = -2568
576979 ZDOT = -773
224337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3517827
87 X = 1072233
93
Y = -13528269
11 feet Y = -4123416
43 meter
Z = 17271758
94 Z = 5264432
13
XDOT = 23851
065408 XDOT = 7269
804736
YDOT = 2921
756534 feet/sec YDOT = 890
551392 meter/sec
ZDOT = -2529
459632 ZDOT = -770
979296
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
56770481
00016717 00000-0 10270-3 0 9073
2 25544 51
6404 250
5105 0011352 344
6887 15
3921 15
56297124 14022
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
56770481 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 250
5105 deg
Eccentricity:
0011352
Arg of perigee: 344
6887 deg
Mean anomaly: 15
3921 deg
Mean motion: 15
56297124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1402
Checksum: 289
Coasting Arc #9 (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 = -4788125
52 A = 6774649
98 meter
Y = -1898397
87 meter E =
0010133
Z = -4401688
03 I = 51
31472
XDOT = -306
976666 Wp = 39
29944
YDOT = -6905
243374 meter/sec RA = 244
80661 deg
ZDOT = 3323
985580 TA = 264
36756
MA = 264
48312
Ha = 219
804 n
mi
Hp = 210
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15709073
22 X = -4745158
77
Y = -6228339
47 feet Y = -1951700
88 meter
Z = -14441233
70 Z = -4424844
62
XDOT = -1007
141292 XDOT = -245
885341
YDOT = -22654
997945 feet/sec YDOT = -6908
334995 meter/sec
ZDOT = 10905
464500 ZDOT = 3322
641848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11580238
07 X = -3529656
56
Y = 12194758
19 feet Y = 3716962
30 meter
Z = -14536243
80 Z = -4430647
11
XDOT = -20546
432817 XDOT = -6262
552723
YDOT = -6563
770135 feet/sec YDOT = -2000
637137 meter/sec
ZDOT = 10900
551984 ZDOT = 3322
488245
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
53090607
00016717 00000-0 10270-3 0 9087
2 25544 51
6400 245
6943 0011323 348
6428 11
4468 15
56307664 14176
Satellite: ISS
Catalog Number: 25544
Epoch time: 12144
53090607 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 245
6943 deg
Eccentricity:
0011323
Arg of perigee: 348
6428 deg
Mean anomaly: 11
4468 deg
Mean motion: 15
56307664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1417
Checksum: 297
Coasting Arc #10 (Orbit 1424)
---------------------------------------
Vector Time (GMT): 2012/145/00:29:02
838
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -279303
46 A = 6779269
66 meter
Y = 5726162
64 meter E =
0010452
Z = -3629679
91 I = 51
32995
XDOT = -5524
313275 Wp = 13
02601
YDOT = -3034
619682 meter/sec RA = 242
34924 deg
ZDOT = -4354
762499 TA = 210
22039
MA = 210
28071
Ha = 220
203 n
mi
Hp = 212
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -916349
92 X = -325681
51
Y = 18786622
83 feet Y = 5722780
41 meter
Z = -11908398
66 Z = -3631148
74
XDOT = -18124
387384 XDOT = -5468
814335
YDOT = -9956
101319 feet/sec YDOT = -3096
085140 meter/sec
ZDOT = -14287
278541 ZDOT = -4381
465140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17166188
42 X = -5232254
23
Y = -7677437
50 feet Y = -2340082
95 meter
Z = -11914939
42 Z = -3631673
54
XDOT = 15320
503916 XDOT = 4669
689594
YDOT = -11874
193866 feet/sec YDOT = -3619
254290 meter/sec
ZDOT = -14396
770212 ZDOT = -4388
135561
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
04461768
00016717 00000-0 10270-3 0 9095
2 25544 51
6395 243
1267 0009860 341
9348 18
1454 15
55667011 14253
Satellite: ISS
Catalog Number: 25544
Epoch time: 12145
04461768 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 243
1267 deg
Eccentricity:
0009860
Arg of perigee: 341
9348 deg
Mean anomaly: 18
1454 deg
Mean motion: 15
55667011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1425
Checksum: 312
Coasting Arc #11 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2012/146/00:29:02
838
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1891049
25 A = 6774620
07 meter
Y = -4291543
19 meter E =
0006847
Z = 4883971
42 I = 51
32895
XDOT = 5373
805787 Wp = 28
56003
YDOT = 4975
201278 meter/sec RA = 237
32332 deg
ZDOT = 2295
572342 TA = 38
93818
MA = 38
88888
Ha = 220
229 n
mi
Hp = 211
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6204229
81 X = 1915172
26
Y = -14079866
11 feet Y = -4270261
98 meter
Z = 16023528
29 Z = 4893216
21
XDOT = 17630
596414 XDOT = 5306
621249
YDOT = 16322
838838 feet/sec YDOT = 5034
918592 meter/sec
ZDOT = 7531
405320 ZDOT = 2321
515552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11041520
08 X = 3365455
32
Y = 10657796
45 feet Y = 3248496
36 meter
Z = 16061904
15 Z = 4895668
39
XDOT = -20677
873585 XDOT = -6302
615869
YDOT = 9934
603393 feet/sec YDOT = 3028
067114 meter/sec
ZDOT = 7637
621747 ZDOT = 2327
947108
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
07243474
00016717 00000-0 10270-3 0 9103
2 25544 51
6389 237
9902 0009847 345
6071 14
4800 15
55679440 14413
Satellite: ISS
Catalog Number: 25544
Epoch time: 12146
07243474 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 237
9902 deg
Eccentricity:
0009847
Arg of perigee: 345
6071 deg
Mean anomaly: 14
4800 deg
Mean motion: 15
55679440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 310
Coasting Arc #12 (Orbit 1455)
---------------------------------------
Vector Time (GMT): 2012/147/00:29:02
838
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3460861
37 A = 6772771
97 meter
Y = 2447147
92 meter E =
0016112
Z = -5293550
78 I = 51
34066
XDOT = -4580
151878 Wp = 54
08050
YDOT = -6139
861327 meter/sec RA = 232
28666 deg
ZDOT = 165
690700 TA = 217
45025
MA = 217
56263
Ha = 220
395 n
mi
Hp = 211
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11354532
05 X = -3462253
71
Y = 8028700
53 feet Y = 2408439
17 meter
Z = -17367292
60 Z = -5310366
68
XDOT = -15026
745006 XDOT = -4511
959179
YDOT = -20143
901993 feet/sec YDOT = -6190
698150 meter/sec
ZDOT = 543
604659 ZDOT = 143
605485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3799995
46 X = -1158238
62
Y = -13286536
44 feet Y = -4049736
31 meter
Z = -17436635
75 Z = -5314686
58
XDOT = 23043
516607 XDOT = 7023
663862
YDOT = -7144
164078 feet/sec YDOT = -2177
541211 meter/sec
ZDOT = 453
331591 ZDOT = 138
175469
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
03600227
00016717 00000-0 10270-3 0 9114
2 25544 51
6392 233
1751 0009962 349
2090 10
8848 15
55706113 14562
Satellite: ISS
Catalog Number: 25544
Epoch time: 12147
03600227 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 233
1751 deg
Eccentricity:
0009962
Arg of perigee: 349
2090 deg
Mean anomaly: 10
8848 deg
Mean motion: 15
55706113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1456
Checksum: 290
Coasting Arc #13 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2012/148/00:29:02
838
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4811368
83 A = 6774918
68 meter
Y = -393148
39 meter E =
0014545
Z = 4754661
85 I = 51
36732
XDOT = 3139
366112 Wp = 21
20396
YDOT = 6486
625806 meter/sec RA = 227
25142 deg
ZDOT = -2624
606892 TA = 94
86079
MA = 94
69470
Ha = 220
456 n
mi
Hp = 211
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15785330
82 X = 4792310
38
Y = -1289856
92 feet Y = -339451
65 meter
Z = 15599284
30 Z = 4777989
00
XDOT = 10299
757586 XDOT = 3079
347791
YDOT = 21281
580728 feet/sec YDOT = 6521
396783 meter/sec
ZDOT = -8610
914999 ZDOT = -2609
501187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3774261
64 X = -1150394
95
Y = 15283742
37 feet Y = 4658484
68 meter
Z = 15695229
81 Z = 4783906
05
XDOT = -22355
148304 XDOT = -6813
849203
YDOT = 3312
057424 feet/sec YDOT = 1009
515103 meter/sec
ZDOT = -8549
351444 ZDOT = -2605
842320
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
06379518
00016717 00000-0 10270-3 0 9125
2 25544 51
6389 228
0385 0010101 352
5156 7
5846 15
55742831 14727
Satellite: ISS
Catalog Number: 25544
Epoch time: 12148
06379518 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 228
0385 deg
Eccentricity:
0010101
Arg of perigee: 352
5156 deg
Mean anomaly: 7
5846 deg
Mean motion: 15
55742831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 306
Coasting Arc #14 (Orbit 1486)
---------------------------------------
Vector Time (GMT): 2012/149/00:29:02
838
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5672020
29 A = 6779679
99 meter
Y = -1488057
94 meter E =
0010866
Z = -3395951
26 I = 51
40485
XDOT = -1167
764637 Wp = 23
10380
YDOT = -6023
654653 meter/sec RA = 222
23117 deg
ZDOT = 4604
727257 TA = 297
01442
MA = 297
12531
Ha = 220
582 n
mi
Hp = 211
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18608990
45 X = -5638462
14
Y = -4882079
85 feet Y = -1551298
11 meter
Z = -11141572
38 Z = -3423424
37
XDOT = -3831
248808 XDOT = -1122
688913
YDOT = -19762
646499 feet/sec YDOT = -6036
461615 meter/sec
ZDOT = 15107
372889 ZDOT = 4599
163349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10255283
03 X = 3125810
27
Y = -16199725
67 feet Y = -4937676
38 meter
Z = -11254417
92 Z = -3430346
58
XDOT = 18842
330284 XDOT = 5743
142271
YDOT = 1481
630576 feet/sec YDOT = 451
600999 meter/sec
ZDOT = 15084
993290 ZDOT = 4597
905955
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
02734165
00016717 00000-0 10270-3 0 9136
2 25544 51
6392 223
2227 0010129 355
9866 4
1205 15
55726612 14875
Satellite: ISS
Catalog Number: 25544
Epoch time: 12149
02734165 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 223
2227 deg
Eccentricity:
0010129
Arg of perigee: 355
9866 deg
Mean anomaly: 4
1205 deg
Mean motion: 15
55726612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1487
Checksum: 295
Coasting Arc #15 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2012/150/00:29:02
838
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5883569
58 A = 6783851
09 meter
Y = 3076104
47 meter E =
0012588
Z = 1393047
61 I = 51
44174
XDOT = -1178
128008 Wp = 75
31851
YDOT = 4893
005764 meter/sec RA = 217
22979 deg
ZDOT = -5781
814414 TA = 89
45681
MA = 89
31257
Ha = 220
800 n
mi
Hp = 211
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19303049
81 X = 5841967
52
Y = 10092206
26 feet Y = 3141665
49 meter
Z = 4570366
17 Z = 1421529
04
XDOT = -3865
249371 XDOT = -1204
668112
YDOT = 16053
168518 feet/sec YDOT = 4879
683165 meter/sec
ZDOT = -18969
207395 ZDOT = -5787
601911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15177463
30 X = -4626090
81
Y = 15589195
25 feet Y = 4751586
71 meter
Z = 4687238
58 Z = 1428670
32
XDOT = -13175
496305 XDOT = -4015
891274
YDOT = -7071
526961 feet/sec YDOT = -2155
401418 meter/sec
ZDOT = -18993
407872 ZDOT = -5789
190719
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
05511367
00016717 00000-0 10270-3 0 9149
2 25544 51
6391 218
0860 0010008
3566 359
7593 15
55715643 15033
Satellite: ISS
Catalog Number: 25544
Epoch time: 12150
05511367 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 218
0860 deg
Eccentricity:
0010008
Arg of perigee:
3566 deg
Mean anomaly: 359
7593 deg
Mean motion: 15
55715643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 286
Coasting Arc #16 (Orbit 1518)
---------------------------------------
Vector Time (GMT): 2012/151/00:29:02
838
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5304355
11 A = 6784300
21 meter
Y = -4125856
14 meter E =
0021349
Z = 829102
87 I = 51
46856
XDOT = 3542
588366 Wp = 32
26095
YDOT = -3351
616033 meter/sec RA = 212
23825 deg
ZDOT = 5933
055520 TA = 336
74468
MA = 336
84113
Ha = 220
848 n
mi
Hp = 210
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17402739
85 X = -5261852
34
Y = -13536273
44 feet Y = -4184935
13 meter
Z = 2720153
78 Z = 803437
29
XDOT = 11622
665244 XDOT = 3550
981792
YDOT = -10996
115593 feet/sec YDOT = -3311
954030 meter/sec
ZDOT = 19465
405250 ZDOT = 5950
285623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17724234
27 X = 5402346
61
Y = -13133884
27 feet Y = -4003207
93 meter
Z = 2614936
52 Z = 797032
65
XDOT = 6535
892820 XDOT = 1992
140132
YDOT = 12745
764747 feet/sec YDOT = 3884
909095 meter/sec
ZDOT = 19536
538224 ZDOT = 5954
736851
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 12151
08287145
00016717 00000-0 10270-3 0 9158
2 25544 51
6392 212
9487 0010205 3
2328 356
8889 15
55770774 15198
Satellite: ISS
Catalog Number: 25544
Epoch time: 12151
08287145 = yrday
fracday
Element set: 915
Inclination: 51
6392 deg
RA of node: 212
9487 deg
Eccentricity:
0010205
Arg of perigee: 3
2328 deg
Mean anomaly: 356
8889 deg
Mean motion: 15
55770774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1519
Checksum: 320
Coasting Arc #17 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2012/152/00:29:02
838
Vector Time (MET): N/A
Weight (LBS) : 947501
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3953404
37 A = 6780986
45 meter
Y = 4668320
86 meter E =
0009707
Z = -2940826
63 I = 51
48322
XDOT = -5589
185761 Wp = 33
05839
YDOT = 1589
515535 meter/sec RA = 207
24403 deg
ZDOT = -4990
244454 TA = 180
56613
MA = 180
56723
Ha = 220
960 n
mi
Hp = 210
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12970486
78 X = 3915194
50
Y = 15316013
32 feet Y = 4712316
83 meter
Z = -9648381
32 Z = -2921713
40
XDOT = -18337
223624 XDOT = -5582
302820
YDOT = 5214
945981 feet/sec YDOT = 1527
052610 meter/sec
ZDOT = -16372
193090 ZDOT = -5017
380030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18108908
06 X = -5519595
18
Y = 8739837
45 feet Y = 2663902
45 meter
Z = -9570148
57 Z = -2916981
28
XDOT = 197
093718 XDOT = 60
074165
YDOT = -17642
189308 feet/sec YDOT = -5377
339301 meter/sec
ZDOT = -16483
928649 ZDOT = -5024
301452
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 12152
04638591
00016717 00000-0 10270-3 0 9161
2 25544 51
6388 208
1333 0010144 6
1920 353
9358 15
55757674 15342
Satellite: ISS
Catalog Number: 25544
Epoch time: 12152
04638591 = yrday
fracday
Element set: 916
Inclination: 51
6388 deg
RA of node: 208
1333 deg
Eccentricity:
0010144
Arg of perigee: 6
1920 deg
Mean anomaly: 353
9358 deg
Mean motion: 15
55757674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 307
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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