[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 16th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12109 4 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
172/13:49:37
925 -0
8 4
2 4
2
N/A 4
1 0
0 221
1
000/00:09:15
850 -0
4 -0
2 209
8
Coasting Arc #1 (Orbit 1774)
---------------------------------------
Vector Time (GMT): 2012/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4766421
42 A = 6773057
38 meter
Y = 202925
34 meter E =
0021914
Z = -4828552
80 I = 51
88720
XDOT = -2887
246812 Wp = 69
49435
YDOT = 6605
327584 meter/sec RA = 129
87999 deg
ZDOT = -2574
472447 TA = 175
20958
MA = 175
18857
Ha = 221
239 n
mi
Hp = 207
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15637865
55 X = 4787254
23
Y = 665765
56 feet Y = 256343
54 meter
Z = -15841708
67 Z = -4805346
91
XDOT = -9472
594526 XDOT = -2948
388036
YDOT = 21671
022258 feet/sec YDOT = 6572
699084 meter/sec
ZDOT = -8446
431912 ZDOT = -2588
646320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2476869
15 X = 754949
72
Y = -15552197
90 feet Y = -4740309
92 meter
Z = -15746113
04 Z = -4799415
25
XDOT = 19303
797037 XDOT = 5883
797337
YDOT = 11679
239147 feet/sec YDOT = 3559
832092 meter/sec
ZDOT = -8505
428179 ZDOT = -2592
454509
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 12167
52066289
00016717 00000-0 10270-3 0 9002
2 25544 51
6343 130
7361 0010548 66
6282 293
5980 15
56375300 17754
Satellite: ISS
Catalog Number: 25544
Epoch time: 12167
52066289 = yrday
fracday
Element set: 900
Inclination: 51
6343 deg
RA of node: 130
7361 deg
Eccentricity:
0010548
Arg of perigee: 66
6282 deg
Mean anomaly: 293
5980 deg
Mean motion: 15
56375300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1775
Checksum: 310
Coasting Arc #2 (Orbit 1790)
---------------------------------------
Vector Time (GMT): 2012/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3325517
31 A = 6770714
14 meter
Y = -2524039
63 meter E =
0012851
Z = 5319888
87 I = 51
89900
XDOT = 4486
960812 Wp = 72
67028
YDOT = -6233
763280 meter/sec RA = 124
87557 deg
ZDOT = -148
753357 TA = 18
76337
MA = 18
71605
Ha = 221
308 n
mi
Hp = 207
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10910489
87 X = -3322888
84
Y = -8280969
91 feet Y = -2561213
71 meter
Z = 17453703
64 Z = 5303739
54
XDOT = 14721
000040 XDOT = 4557
057159
YDOT = -20451
979264 feet/sec YDOT = -6183
195353 meter/sec
ZDOT = -488
035947 ZDOT = -126
786390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9323197
59 X = -2841710
62
Y = 10148973
39 feet Y = 3093407
09 meter
Z = 17387390
50 Z = 5299676
62
XDOT = -18164
697268 XDOT = -5536
599727
YDOT = -15983
919924 feet/sec YDOT = -4871
898793 meter/sec
ZDOT = -396
943721 ZDOT = -120
988446
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 12168
54799531
00016717 00000-0 10270-3 0 9019
2 25544 51
6347 125
5968 0010490 69
8932 290
3350 15
56408215 17912
Satellite: ISS
Catalog Number: 25544
Epoch time: 12168
54799531 = yrday
fracday
Element set: 901
Inclination: 51
6347 deg
RA of node: 125
5968 deg
Eccentricity:
0010490
Arg of perigee: 69
8932 deg
Mean anomaly: 290
3350 deg
Mean motion: 15
56408215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1791
Checksum: 325
Coasting Arc #3 (Orbit 1805)
---------------------------------------
Vector Time (GMT): 2012/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1611265
21 A = 6773311
62 meter
Y = 4608027
78 meter E =
0020211
Z = -4713175
06 I = 51
92479
XDOT = -5293
871634 Wp = 91
79574
YDOT = 4747
292723 meter/sec RA = 119
87243 deg
ZDOT = 2841
482263 TA = 206
27723
MA = 206
37991
Ha = 221
192 n
mi
Hp = 207
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5286303
18 X = 1582513
21
Y = 15118201
37 feet Y = 4625885
94 meter
Z = -15463172
78 Z = -4705416
67
XDOT = -17368
345256 XDOT = -5360
366730
YDOT = 15575
107358 feet/sec YDOT = 4687
721123 meter/sec
ZDOT = 9322
448368 ZDOT = 2815
603969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15504249
48 X = 4725695
24
Y = -4134935
68 feet Y = -1260328
39 meter
Z = -15431632
50 Z = -4703561
59
XDOT = 13807
517609 XDOT = 4208
531367
YDOT = 17501
738253 feet/sec YDOT = 5334
529819 meter/sec
ZDOT = 9215
356512 ZDOT = 2808
840665
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 12169
51110474
00016717 00000-0 10270-3 0 9021
2 25544 51
6351 120
7781 0010457 73
2684 286
9616 15
56416484 18063
Satellite: ISS
Catalog Number: 25544
Epoch time: 12169
51110474 = yrday
fracday
Element set: 902
Inclination: 51
6351 deg
RA of node: 120
7781 deg
Eccentricity:
0010457
Arg of perigee: 73
2684 deg
Mean anomaly: 286
9616 deg
Mean motion: 15
56416484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1806
Checksum: 308
Coasting Arc #4 (Orbit 1821)
---------------------------------------
Vector Time (GMT): 2012/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 186784
72 A = 6778634
71 meter
Y = -6048170
50 meter E =
0023231
Z = 3036393
52 I = 51
95824
XDOT = 5368
526643 Wp = 87
77284
YDOT = -2343
014750 meter/sec RA = 114
88746 deg
ZDOT = -4963
776392 TA = 57
51350
MA = 57
28915
Ha = 221
147 n
mi
Hp = 207
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 612810
76 X = 239652
57
Y = -19843079
07 feet Y = -6045786
67 meter
Z = 9961920
99 Z = 3037428
31
XDOT = 17613
276389 XDOT = 5418
440673
YDOT = -7687
056265 feet/sec YDOT = -2282
700638 meter/sec
ZDOT = -16285
355617 ZDOT = -4937
575415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19766308
86 X = -6024770
94
Y = -1822045
73 feet Y = -555359
54 meter
Z = 9966763
63 Z = 3037869
55
XDOT = -6670
514526 XDOT = -2033
172828
YDOT = -16727
005219 feet/sec YDOT = -5098
391191 meter/sec
ZDOT = -16177
144371 ZDOT = -4930
793604
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 12170
53840591
00016717 00000-0 10270-3 0 9036
2 25544 51
6360 115
6381 0010469 76
8640 283
3681 15
56461017 18229
Satellite: ISS
Catalog Number: 25544
Epoch time: 12170
53840591 = yrday
fracday
Element set: 903
Inclination: 51
6360 deg
RA of node: 115
6381 deg
Eccentricity:
0010469
Arg of perigee: 76
8640 deg
Mean anomaly: 283
3681 deg
Mean motion: 15
56461017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1822
Checksum: 299
Coasting Arc #5 (Orbit 1836)
---------------------------------------
Vector Time (GMT): 2012/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1729343
86 A = 6782266
43 meter
Y = 6509110
64 meter E =
0019497
Z = -757522
26 I = 51
98255
XDOT = -4764
644919 Wp = 60
29988
YDOT = -583
894161 meter/sec RA = 109
92328 deg
ZDOT = 5984
382903 TA = 291
54379
MA = 291
75149
Ha = 221
111 n
mi
Hp = 207
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5673700
32 X = -1798321
66
Y = 21355349
88 feet Y = 6489386
50 meter
Z = -2485309
25 Z = -766089
75
XDOT = -15632
037137 XDOT = -4786
832324
YDOT = -1915
663258 feet/sec YDOT = -637
300457 meter/sec
ZDOT = 19633
802174 ZDOT = 5961
182497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21066400
78 X = 6421038
96
Y = 6653467
99 feet Y = 2027977
04 meter
Z = -2521255
23 Z = -768478
59
XDOT = -2165
626591 XDOT = -660
082985
YDOT = 14108
218849 feet/sec YDOT = 4300
185105 meter/sec
ZDOT = 19538
228203 ZDOT = 5955
251956
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 12171
50148592
00016717 00000-0 10270-3 0 9047
2 25544 51
6361 110
8200 0010412 80
4570 279
7760 15
56473397 18375
Satellite: ISS
Catalog Number: 25544
Epoch time: 12171
50148592 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 110
8200 deg
Eccentricity:
0010412
Arg of perigee: 80
4570 deg
Mean anomaly: 279
7760 deg
Mean motion: 15
56473397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1837
Checksum: 296
Coasting Arc #6 (Orbit 1852)
---------------------------------------
Vector Time (GMT): 2012/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2986796
84 A = 6781124
74 meter
Y = -5826123
13 meter E =
0015755
Z = -1766933
77 I = 51
98975
XDOT = 3654
976544 Wp = 108
00758
YDOT = 3589
527837 meter/sec RA = 104
96530 deg
ZDOT = -5703
807327 TA = 91
30362
MA = 91
12312
Ha = 221
084 n
mi
Hp = 207
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9799202
23 X = 3060307
08
Y = -19114577
20 feet Y = -5792311
60 meter
Z = -5797026
80 Z = -1752246
53
XDOT = 11991
392860 XDOT = 3642
273743
YDOT = 11776
666132 feet/sec YDOT = 3630
329982 meter/sec
ZDOT = -18713
278631 ZDOT = -5686
081942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18814475
25 X = -5734652
06
Y = -10397683
38 feet Y = -3169213
89 meter
Z = -5735908
58 Z = -1748304
93
XDOT = 11371
531438 XDOT = 3466
042782
YDOT = -10378
303136 feet/sec YDOT = -3163
306796 meter/sec
ZDOT = -18640
561107 ZDOT = -5681
643025
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 12172
52875558
00016717 00000-0 10270-3 0 9050
2 25544 51
6374 105
6796 0010389 84
1698 276
0640 15
56504315 18536
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
52875558 = yrday
fracday
Element set: 905
Inclination: 51
6374 deg
RA of node: 105
6796 deg
Eccentricity:
0010389
Arg of perigee: 84
1698 deg
Mean anomaly: 276
0640 deg
Mean motion: 15
56504315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1853
Checksum: 330
Coasting Arc #7 (Orbit 1853)
---------------------------------------
Vector Time (GMT): 2012/172/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3516598
18 A = 6773481
97 meter
Y = 2607005
70 meter E =
0020581
Z = -5186912
98 I = 51
95814
XDOT = -2970
300966 Wp = 95
45984
YDOT = 6903
390399 meter/sec RA = 104
54323 deg
ZDOT = 1459
001055 TA = 188
52650
MA = 188
56152
Ha = 221
082 n
mi
Hp = 209
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11537395
61 X = 3512381
48
Y = 8553168
31 feet Y = 2646307
77 meter
Z = -17017431
04 Z = -5169839
39
XDOT = -9745
081909 XDOT = -3054
362792
YDOT = 22648
918631 feet/sec YDOT = 6869
704394 meter/sec
ZDOT = 4786
748867 ZDOT = 1444
368505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2349353
38 X = 716082
91
Y = -14252388
60 feet Y = -4344128
05 meter
Z = -16947303
70 Z = -5165538
17
XDOT = 23580
220648 XDOT = 7187
251254
YDOT = -1720
372256 feet/sec YDOT = -524
369464 meter/sec
ZDOT = 4725
749138 ZDOT = 1440
408337
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 12172
59296120
00016717 00000-0 10270-3 0 9060
2 25544 51
6386 105
3594 0006972 84
2154 275
9794 15
55697892 18544
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
59296120 = yrday
fracday
Element set: 906
Inclination: 51
6386 deg
RA of node: 105
3594 deg
Eccentricity:
0006972
Arg of perigee: 84
2154 deg
Mean anomaly: 275
9794 deg
Mean motion: 15
55697892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1854
Checksum: 348
Coasting Arc #8 (Orbit 1869)
---------------------------------------
Vector Time (GMT): 2012/173/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2525390
31 A = 6777303
48 meter
Y = -4687670
81 meter E =
0017179
Z = 4180247
03 I = 51
97773
XDOT = 3891
304714 Wp = 80
30520
YDOT = -5454
183120 meter/sec RA = 99
55641 deg
ZDOT = -3749
537627 TA = 48
07848
MA = 47
93213
Ha = 221
110 n
mi
Hp = 209
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8285401
27 X = -2493090
66
Y = -15379497
41 feet Y = -4715731
35 meter
Z = 13714721
23 Z = 4168056
61
XDOT = 12766
747749 XDOT = 3970
219561
YDOT = -17894
301575 feet/sec YDOT = -5410
226318 meter/sec
ZDOT = -12301
632635 ZDOT = -3730
443154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9667860
88 X = -2946764
00
Y = 14597005
50 feet Y = 4449167
28 meter
Z = 13664929
19 Z = 4165070
42
XDOT = -20761
040593 XDOT = -6327
965173
YDOT = -2259
557208 feet/sec YDOT = -688
713037 meter/sec
ZDOT = -12222
369120 ZDOT = -3725
378108
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 12173
62074933
00016717 00000-0 10270-3 0 9072
2 25544 51
6384 100
2231 0006973 87
6335 272
5616 15
55726248 18705
Satellite: ISS
Catalog Number: 25544
Epoch time: 12173
62074933 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 100
2231 deg
Eccentricity:
0006973
Arg of perigee: 87
6335 deg
Mean anomaly: 272
5616 deg
Mean motion: 15
55726248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1870
Checksum: 311
Coasting Arc #9 (Orbit 1884)
---------------------------------------
Vector Time (GMT): 2012/174/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1446447
72 A = 6782021
98 meter
Y = 6148084
81 meter E =
0011450
Z = -2474510
05 I = 51
99861
XDOT = -4455
116284 Wp = 72
62244
YDOT = 3194
654336 meter/sec RA = 94
58606 deg
ZDOT = 5356
824813 TA = 259
80100
MA = 259
93015
Ha = 220
979 n
mi
Hp = 209
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4745563
39 X = 1389611
57
Y = 20170881
93 feet Y = 6163942
44 meter
Z = -8118471
30 Z = -2467620
53
XDOT = -14616
523240 XDOT = -4516
530445
YDOT = 10481
149395 feet/sec YDOT = 3144
490334 meter/sec
ZDOT = 17574
884556 ZDOT = 5335
033531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15337747
44 X = 4674945
42
Y = -13949508
75 feet Y = -4251810
27 meter
Z = -8090681
99 Z = -2466039
87
XDOT = 15277
117844 XDOT = 4656
465519
YDOT = 6701
604367 feet/sec YDOT = 2042
649011 meter/sec
ZDOT = 17484
717967 ZDOT = 5329
342036
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 12174
58428617
00016717 00000-0 10270-3 0 9081
2 25544 51
6391 95
4075 0006885 91
3795 268
8147 15
55752946 18855
Satellite: ISS
Catalog Number: 25544
Epoch time: 12174
58428617 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 95
4075 deg
Eccentricity:
0006885
Arg of perigee: 91
3795 deg
Mean anomaly: 268
8147 deg
Mean motion: 15
55752946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1885
Checksum: 360
Coasting Arc #10 (Orbit 1900)
---------------------------------------
Vector Time (GMT): 2012/175/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -251831
36 A = 6784654
80 meter
Y = -6767942
89 meter E =
0018604
Z = 266504
66 I = 52
00845
XDOT = 4713
896377 Wp = 119
57588
YDOT = -425
244785 meter/sec RA = 89
63027 deg
ZDOT = -6038
735212 TA = 57
56434
MA = 57
38455
Ha = 220
997 n
mi
Hp = 209
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -826218
37 X = -177426
73
Y = -22204537
06 feet Y = -6770343
04 meter
Z = 874359
12 Z = 265461
20
XDOT = 15465
539295 XDOT = 4747
635726
YDOT = -1395
160057 feet/sec YDOT = -372
341702 meter/sec
ZDOT = -19812
123399 ZDOT = -6015
753637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18834612
70 X = -5740789
95
Y = 11789307
92 feet Y = 3593381
05 meter
Z = 870740
85 Z = 265401
81
XDOT = -8120
218535 XDOT = -2475
042609
YDOT = -11442
099499 feet/sec YDOT = -3487
551927 meter/sec
ZDOT = -19717
321328 ZDOT = -6009
839541
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 12175
61204487
00016717 00000-0 10270-3 0 9094
2 25544 51
6390 90
2707 0006850 96
4403 263
7531 15
55728380 19018
Satellite: ISS
Catalog Number: 25544
Epoch time: 12175
61204487 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 90
2707 deg
Eccentricity:
0006850
Arg of perigee: 96
4403 deg
Mean anomaly: 263
7531 deg
Mean motion: 15
55728380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1901
Checksum: 306
Coasting Arc #11 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2012/176/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -920182
17 A = 6782958
16 meter
Y = 6427209
85 meter E =
0020074
Z = 1936206
95 I = 52
00187
XDOT = -4640
599890 Wp = 77
12227
YDOT = -2374
592323 meter/sec RA = 84
67554 deg
ZDOT = 5632
410133 TA = 304
14037
MA = 304
33060
Ha = 220
882 n
mi
Hp = 209
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3018970
37 X = -1001389
73
Y = 21086646
49 feet Y = 6416465
55 meter
Z = 6352385
01 Z = 1931540
20
XDOT = -15225
065256 XDOT = -4641
062555
YDOT = -7790
657229 feet/sec YDOT = -2426
489554 meter/sec
ZDOT = 18479
035868 ZDOT = 5609
865128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19666451
87 X = 5994334
53
Y = -8200239
16 feet Y = -2499432
90 meter
Z = 6332486
55 Z = 1930141
90
XDOT = 590
104093 XDOT = 179
863727
YDOT = 15727
006533 feet/sec YDOT = 4793
591591 meter/sec
ZDOT = 18386
315790 ZDOT = 5604
149053
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 12176
63978651
00016717 00000-0 10270-3 0 9100
2 25544 51
6388 85
1336 0006742 97
9948 262
1971 15
55779311 19174
Satellite: ISS
Catalog Number: 25544
Epoch time: 12176
63978651 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 85
1336 deg
Eccentricity:
0006742
Arg of perigee: 97
9948 deg
Mean anomaly: 262
1971 deg
Mean motion: 15
55779311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 348
Coasting Arc #12 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2012/177/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2122953
25 A = 6778234
29 meter
Y = -5165388
66 meter E =
0012408
Z = -3852207
47 I = 51
98220
XDOT = 4207
051504 Wp = 89
22103
YDOT = 4843
752620 meter/sec RA = 79
70881 deg
ZDOT = -4187
885539 TA = 136
89387
MA = 136
79664
Ha = 220
764 n
mi
Hp = 209
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6965069
71 X = 2199268
95
Y = -16946813
18 feet Y = -5141221
42 meter
Z = -12638475
96 Z = -3841709
42
XDOT = 13802
662415 XDOT = 4172
918679
YDOT = 15891
576836 feet/sec YDOT = 4890
608011 meter/sec
ZDOT = -13739
781952 ZDOT = -4167
530451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18110866
59 X = -5520192
14
Y = 2967983
19 feet Y = 904641
28 meter
Z = -12594655
01 Z = -3838850
85
XDOT = 6379
526547 XDOT = 1944
479691
YDOT = -18862
439444 feet/sec YDOT = -5749
271543 meter/sec
ZDOT = -13656
347346 ZDOT = -4162
454671
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 12177
60328016
00016717 00000-0 10270-3 0 9113
2 25544 51
6385 80
3175 0006537 102
5631 257
6254 15
55795502 19323
Satellite: ISS
Catalog Number: 25544
Epoch time: 12177
60328016 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 80
3175 deg
Eccentricity:
0006537
Arg of perigee: 102
5631 deg
Mean anomaly: 257
6254 deg
Mean motion: 15
55795502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 300
Coasting Arc #13 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2012/178/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3199527
36 A = 6773736
13 meter
Y = 3209939
28 meter E =
0012398
Z = 5025935
09 I = 51
96102
XDOT = -3424
137089 Wp = 113
87716
YDOT = -6572
018945 meter/sec RA = 74
72401 deg
ZDOT = 2008
779810 TA = 316
67249
MA = 316
76991
Ha = 220
859 n
mi
Hp = 209
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10497137
02 X = -3259598
58
Y = 10531296
84 feet Y = 3173823
86 meter
Z = 16489288
34 Z = 5010246
32
XDOT = -11234
045566 XDOT = -3360
151118
YDOT = -21561
741947 feet/sec YDOT = -6609
952180 meter/sec
ZDOT = 6590
484941 ZDOT = 1992
300376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14597056
31 X = 4449182
76
Y = 3188157
34 feet Y = 971750
36 meter
Z = 16424260
37 Z = 5006114
56
XDOT = -11763
242996 XDOT = -3585
436465
YDOT = 20103
871007 feet/sec YDOT = 6127
659883 meter/sec
ZDOT = 6523
218170 ZDOT = 1988
276898
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 12178
63099327
00016717 00000-0 10270-3 0 9128
2 25544 51
6386 75
1802 0006680 105
5875 254
6016 15
55820043 19484
Satellite: ISS
Catalog Number: 25544
Epoch time: 12178
63099327 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 75
1802 deg
Eccentricity:
0006680
Arg of perigee: 105
5875 deg
Mean anomaly: 254
6016 deg
Mean motion: 15
55820043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1948
Checksum: 316
Coasting Arc #14 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2012/179/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4126677
82 A = 6772411
05 meter
Y = -848073
92 meter E =
0021059
Z = -5320702
46 I = 51
94724
XDOT = 2227
947892 Wp = 98
83132
YDOT = 7302
683738 meter/sec RA = 69
72629 deg
ZDOT = 562
740629 TA = 176
53223
MA = 176
51761
Ha = 220
587 n
mi
Hp = 209
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13538969
24 X = 4161701
28
Y = -2782394
74 feet Y = -801730
51 meter
Z = -17456372
91 Z = -5300570
21
XDOT = 7309
540329 XDOT = 2143
388528
YDOT = 23958
936147 feet/sec YDOT = 7327
125180 meter/sec
ZDOT = 1846
261907 ZDOT = 573
359230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9910977
34 X = -3020865
89
Y = -9783275
36 feet Y = -2981942
33 meter
Z = -17373267
26 Z = -5295371
86
XDOT = 15122
118473 XDOT = 4609
221710
YDOT = -18681
801300 feet/sec YDOT = -5694
213036 meter/sec
ZDOT = 1889
273046 ZDOT = 575
850425
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 12179
59445889
00016717 00000-0 10270-3 0 9133
2 25544 51
6379 70
3630 0006494 109
3063 250
8794 15
55868682 19635
Satellite: ISS
Catalog Number: 25544
Epoch time: 12179
59445889 = yrday
fracday
Element set: 913
Inclination: 51
6379 deg
RA of node: 70
3630 deg
Eccentricity:
0006494
Arg of perigee: 109
3063 deg
Mean anomaly: 250
8794 deg
Mean motion: 15
55868682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 352
Coasting Arc #15 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2012/180/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4713731
39 A = 6775225
14 meter
Y = -1541985
18 meter E =
0013684
Z = 4604697
09 I = 51
94618
XDOT = -681
774200 Wp = 85
66151
YDOT = -7018
648547 meter/sec RA = 64
73248 deg
ZDOT = -3039
517325 TA = 34
56062
MA = 34
47174
Ha = 220
578 n
mi
Hp = 209
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15464998
00 X = -4718506
94
Y = -5059006
51 feet Y = -1594724
28 meter
Z = 15107273
92 Z = 4581786
11
XDOT = -2236
791994 XDOT = -588
474206
YDOT = -23027
062162 feet/sec YDOT = -7025
750552 meter/sec
ZDOT = -9972
169700 ZDOT = -3042
603546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4732619
38 X = 1442502
39
Y = 15658946
23 feet Y = 4772846
81 meter
Z = 15012966
13 Z = 4575952
08
XDOT = -16518
349635 XDOT = -5034
792969
YDOT = 14592
317955 feet/sec YDOT = 4447
738513 meter/sec
ZDOT = -9984
137534 ZDOT = -3043
165120
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 12180
62214109
00016717 00000-0 10270-3 0 9149
2 25544 51
6384 65
2259 0006336 113
1635 247
0187 15
55912190 19799
Satellite: ISS
Catalog Number: 25544
Epoch time: 12180
62214109 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 65
2259 deg
Eccentricity:
0006336
Arg of perigee: 113
1635 deg
Mean anomaly: 247
0187 deg
Mean motion: 15
55912190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 302
Coasting Arc #16 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2012/181/13:54:15
850
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4873133
02 A = 6780258
51 meter
Y = 3586512
38 meter E =
0010042
Z = -3069968
67 I = 51
94797
XDOT = -1125
261208 Wp = 98
23318
YDOT = 5747
351110 meter/sec RA = 59
75228 deg
ZDOT = 4940
576240 TA = 226
69524
MA = 226
77902
Ha = 220
450 n
mi
Hp = 209
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15987969
23 X = 4847579
01
Y = 11766772
90 feet Y = 3640864
32 meter
Z = -10072075
68 Z = -3046356
65
XDOT = -3691
801865 XDOT = -1213
445961
YDOT = 18856
138813 feet/sec YDOT = 5734
273987 meter/sec
ZDOT = 16209
239633 ZDOT = 4934
896341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 150490
44 X = 45869
49
Y = -19899584
65 feet Y = -6065393
40 meter
Z = -9975103
84 Z = -3040411
65
XDOT = 16058
835493 XDOT = 4894
733058
YDOT = -7971
171419 feet/sec YDOT = -2429
613049 meter/sec
ZDOT = 16185
185033 ZDOT = 4933
244398
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 12181
58558150
00016717 00000-0 10270-3 0 9153
2 25544 51
6374 60
4090 0006356 117
2842 242
8959 15
55899300 19949
Satellite: ISS
Catalog Number: 25544
Epoch time: 12181
58558150 = yrday
fracday
Element set: 915
Inclination: 51
6374 deg
RA of node: 60
4090 deg
Eccentricity:
0006356
Arg of perigee: 117
2842 deg
Mean anomaly: 242
8959 deg
Mean motion: 15
55899300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1994
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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