[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 16th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
333/20:59:39
337 1
0 3
9 3
9
N/A -2
3 -0
1 228
3
000/00:09:18
675 -3
0 -0
2 218
9
Coasting Arc #1 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2012/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3564986
35 A = 6787740
32 meter
Y = -3183570
38 meter E =
0011189
Z = 4830053
77 I = 51
98319
XDOT = 2503
196372 Wp = 309
17451
YDOT = -6750
867913 meter/sec RA = 93
95220 deg
ZDOT = -2599
199578 TA = 166
37137
MA = 166
34113
Ha = 225
186 n
mi
Hp = 219
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11696149
44 X = -3552586
00
Y = -10444784
72 feet Y = -3223367
21 meter
Z = 15846633
10 Z = 4812764
69
XDOT = 8212
586521 XDOT = 2591
126618
YDOT = -22148
516776 feet/sec YDOT = -6722
383824 meter/sec
ZDOT = -8527
557669 ZDOT = -2586
825598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15427878
78 X = 4702417
45
Y = -3182594
74 feet Y = -970054
88 meter
Z = 15775324
62 Z = 4808318
95
XDOT = 12546
829955 XDOT = 3824
273770
YDOT = 18764
374836 feet/sec YDOT = 5719
381450 meter/sec
ZDOT = -8475
502185 ZDOT = -2583
333066
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 12319
54374096
00016717 00000-0 10270-3 0 9001
2 25544 51
6453 94
5825 0015534 283
1655 76
7763 15
51326443 1378
Satellite: ISS
Catalog Number: 25544
Epoch time: 12319
54374096 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 94
5825 deg
Eccentricity:
0015534
Arg of perigee: 283
1655 deg
Mean anomaly: 76
7763 deg
Mean motion: 15
51326443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 313
Coasting Arc #2 (Orbit 151)
---------------------------------------
Vector Time (GMT): 2012/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3522017
44 A = 6789096
38 meter
Y = 3750817
30 meter E =
0006746
Z = -4422757
80 I = 51
99073
XDOT = -2540
953050 Wp = 282
57186
YDOT = 6389
242309 meter/sec RA = 89
00855 deg
ZDOT = 3392
156681 TA = 21
60317
MA = 21
57472
Ha = 225
513 n
mi
Hp = 219
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11555175
33 X = 3501298
49
Y = 12305831
03 feet Y = 3790087
16 meter
Z = -14510360
25 Z = -4405697
68
XDOT = -8336
460137 XDOT = -2628
688742
YDOT = 20962
081066 feet/sec YDOT = 6360
336988 meter/sec
ZDOT = 11129
122969 ZDOT = 3379
599906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16792441
23 X = -5118336
09
Y = 2237068
84 feet Y = 681858
58 meter
Z = -14440067
49 Z = -4401332
57
XDOT = -11912
404639 XDOT = -3630
900934
YDOT = -17861
050157 feet/sec YDOT = -5444
048088 meter/sec
ZDOT = 11076
331236 ZDOT = 3376
065761
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 12320
50997968
00016717 00000-0 10270-3 0 9019
2 25544 51
6465 89
7865 0015704 287
1504 72
7927 15
51391883 1522
Satellite: ISS
Catalog Number: 25544
Epoch time: 12320
50997968 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 89
7865 deg
Eccentricity:
0015704
Arg of perigee: 287
1504 deg
Mean anomaly: 72
7927 deg
Mean motion: 15
51391883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 152
Checksum: 335
Coasting Arc #3 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2012/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3525633
61 A = 6790831
44 meter
Y = -4287759
75 meter E =
0008100
Z = 3920462
82 I = 51
99566
XDOT = 2613
096524 Wp = 334
25373
YDOT = -5908
132809 meter/sec RA = 84
06623 deg
ZDOT = -4107
806149 TA = 158
68211
MA = 158
64835
Ha = 225
592 n
mi
Hp = 219
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11567039
40 X = -3496469
98
Y = -14067453
24 feet Y = -4327022
81 meter
Z = 12862410
82 Z = 3903405
69
XDOT = 8573
151326 XDOT = 2698
923412
YDOT = -19383
637824 feet/sec YDOT = -5878
431346 meter/sec
ZDOT = -13477
054294 ZDOT = -4094
903590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18198331
48 X = 5546851
43
Y = -1520442
93 feet Y = -463431
00 meter
Z = 12792194
42 Z = 3899060
86
XDOT = 10852
419170 XDOT = 3307
817363
YDOT = 16852
290190 feet/sec YDOT = 5136
578050 meter/sec
ZDOT = -13422
868643 ZDOT = -4091
290363
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 12321
54061411
00016717 00000-0 10270-3 0 9020
2 25544 51
6470 84
6699 0015605 291
0237 68
9245 15
51409890 1689
Satellite: ISS
Catalog Number: 25544
Epoch time: 12321
54061411 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 84
6699 deg
Eccentricity:
0015605
Arg of perigee: 291
0237 deg
Mean anomaly: 68
9245 deg
Mean motion: 15
51409890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 168
Checksum: 303
Coasting Arc #4 (Orbit 182)
---------------------------------------
Vector Time (GMT): 2012/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3541843
36 A = 6792571
18 meter
Y = 4750302
61 meter E =
0012069
Z = -3304765
45 I = 51
99846
XDOT = -2749
468976 Wp = 306
81228
YDOT = 5357
525489 meter/sec RA = 79
12605 deg
ZDOT = 4749
334509 TA = 15
00695
MA = 14
97117
Ha = 226
006 n
mi
Hp = 219
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11620220
98 X = 3504515
23
Y = 15584982
32 feet Y = 4789701
21 meter
Z = -10842406
32 Z = -3287649
50
XDOT = -9020
567508 XDOT = -2832
245065
YDOT = 17577
183363 feet/sec YDOT = 5326
316083 meter/sec
ZDOT = 15581
806133 ZDOT = 4735
776829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19452491
20 X = -5929119
32
Y = 1021539
92 feet Y = 311365
37 meter
Z = -10772001
98 Z = -3283306
20
XDOT = -9443
446839 XDOT = -2878
362596
YDOT = -15945
408705 feet/sec YDOT = -4860
160573 meter/sec
ZDOT = 15524
956691 ZDOT = 4732
006799
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 12322
50681120
00016717 00000-0 10270-3 0 9033
2 25544 51
6477 79
8733 0015795 295
3307 64
6208 15
51447491 1834
Satellite: ISS
Catalog Number: 25544
Epoch time: 12322
50681120 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 79
8733 deg
Eccentricity:
0015795
Arg of perigee: 295
3307 deg
Mean anomaly: 64
6208 deg
Mean motion: 15
51447491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 183
Checksum: 311
Coasting Arc #5 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2012/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3580611
04 A = 6794178
28 meter
Y = -5153128
28 meter E =
0004449
Z = 2612117
14 I = 51
99761
XDOT = 2941
443604 Wp = 353
85482
YDOT = -4715
146870 meter/sec RA = 74
18795 deg
ZDOT = -5266
426792 TA = 156
95513
MA = 156
93517
Ha = 226
065 n
mi
Hp = 219
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11747411
55 X = -3535410
75
Y = -16906588
83 feet Y = -5192916
30 meter
Z = 8569938
13 Z = 2594832
09
XDOT = 9650
405524 XDOT = 3019
534090
YDOT = -15469
641963 feet/sec YDOT = -4681
816939 meter/sec
ZDOT = -17278
303123 ZDOT = -5251
947797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20603616
11 X = 6279982
19
Y = -733663
02 feet Y = -223620
49 meter
Z = 8498882
61 Z = 2590459
42
XDOT = 7644
243242 XDOT = 2329
965340
YDOT = 15088
987222 feet/sec YDOT = 4599
123305 meter/sec
ZDOT = -17217
700956 ZDOT = -5247
955252
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 12323
53740031
00016717 00000-0 10270-3 0 9045
2 25544 51
6478 74
7569 0015659 299
0482 60
9100 15
51488831 1990
Satellite: ISS
Catalog Number: 25544
Epoch time: 12323
53740031 = yrday
fracday
Element set: 904
Inclination: 51
6478 deg
RA of node: 74
7569 deg
Eccentricity:
0015659
Arg of perigee: 299
0482 deg
Mean anomaly: 60
9100 deg
Mean motion: 15
51488831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 199
Checksum: 319
Coasting Arc #6 (Orbit 213)
---------------------------------------
Vector Time (GMT): 2012/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3596695
75 A = 6795565
09 meter
Y = 5453009
93 meter E =
0016841
Z = -1831824
24 I = 51
99378
XDOT = -3217
172632 Wp = 328
99918
YDOT = 4032
434807 meter/sec RA = 69
25049 deg
ZDOT = 5677
988999 TA = 10
96092
MA = 10
92427
Ha = 226
473 n
mi
Hp = 219
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11800182
91 X = 3544350
40
Y = 17890452
52 feet Y = 5492937
80 meter
Z = -6009922
06 Z = -1814478
50
XDOT = -10555
028320 XDOT = -3289
607672
YDOT = 13229
772990 feet/sec YDOT = 3996
053207 meter/sec
ZDOT = 18628
572833 ZDOT = 5662
184157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21443055
74 X = -6535843
39
Y = 599596
90 feet Y = 182757
13 meter
Z = -5938654
34 Z = -1810101
84
XDOT = -5554
278396 XDOT = -1692
944055
YDOT = -14484
818425 feet/sec YDOT = -4414
972656 meter/sec
ZDOT = 18562
548476 ZDOT = 5657
864776
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 12324
50355552
00016717 00000-0 10270-3 0 9054
2 25544 51
6484 69
9594 0015837 303
5184 56
4454 15
51511368 2141
Satellite: ISS
Catalog Number: 25544
Epoch time: 12324
50355552 = yrday
fracday
Element set: 905
Inclination: 51
6484 deg
RA of node: 69
9594 deg
Eccentricity:
0015837
Arg of perigee: 303
5184 deg
Mean anomaly: 56
4454 deg
Mean motion: 15
51511368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 214
Checksum: 309
Coasting Arc #7 (Orbit 229)
---------------------------------------
Vector Time (GMT): 2012/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602854
72 A = 6796383
28 meter
Y = -5675942
57 meter E =
0002300
Z = 1006445
81 I = 51
98500
XDOT = 3550
624741 Wp = 322
51433
YDOT = -3303
444852 meter/sec RA = 64
31477 deg
ZDOT = -5924
959224 TA = 206
65407
MA = 206
66590
Ha = 226
536 n
mi
Hp = 219
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11820389
51 X = -3544006
50
Y = -18621858
84 feet Y = -5715902
92 meter
Z = 3301987
56 Z = 989086
01
XDOT = 11649
031304 XDOT = 3616
083045
YDOT = -10838
073661 feet/sec YDOT = -3263
373470 meter/sec
ZDOT = -19438
842599 ZDOT = -5907
551333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22059150
26 X = 6723629
00
Y = -595703
45 feet Y = -181570
41 meter
Z = 3230693
98 Z = 984715
52
XDOT = 3213
257846 XDOT = 979
400992
YDOT = 14055
854690 feet/sec YDOT = 4284
224510 meter/sec
ZDOT = -19366
254782 ZDOT = -5902
834457
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 12325
53409965
00016717 00000-0 10270-3 0 9067
2 25544 51
6480 64
8429 0015708 307
1162 52
8554 15
51561919 2307
Satellite: ISS
Catalog Number: 25544
Epoch time: 12325
53409965 = yrday
fracday
Element set: 906
Inclination: 51
6480 deg
RA of node: 64
8429 deg
Eccentricity:
0015708
Arg of perigee: 307
1162 deg
Mean anomaly: 52
8554 deg
Mean motion: 15
51561919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 230
Checksum: 308
Coasting Arc #8 (Orbit 244)
---------------------------------------
Vector Time (GMT): 2012/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3542419
13 A = 6796740
17 meter
Y = 5783959
99 meter E =
0019285
Z = -130703
09 I = 51
97304
XDOT = -3969
393654 Wp = 349
27925
YDOT = 2570
417934 meter/sec RA = 59
37788 deg
ZDOT = 6042
050158 TA = 9
31921
MA = 9
28348
Ha = 226
871 n
mi
Hp = 218
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11622110
01 X = 3478113
33
Y = 18976246
68 feet Y = 5823213
98 meter
Z = -428815
92 Z = -113650
16
XDOT = -13022
945059 XDOT = -4027
192846
YDOT = 8433
129706 feet/sec YDOT = 2525
706495 meter/sec
ZDOT = 19822
999206 ZDOT = 6022
626415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22245293
82 X = -6780365
56
Y = 611077
96 feet Y = 186256
56 meter
Z = -358815
67 Z = -109367
02
XDOT = -710
247640 XDOT = -216
483481
YDOT = -13977
343664 feet/sec YDOT = -4260
294349 meter/sec
ZDOT = 19742
139147 ZDOT = 6017
404012
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 12326
50021322
00016717 00000-0 10270-3 0 9073
2 25544 51
6487 60
0450 0015844 311
5682 48
4111 15
51583251 2452
Satellite: ISS
Catalog Number: 25544
Epoch time: 12326
50021322 = yrday
fracday
Element set: 907
Inclination: 51
6487 deg
RA of node: 60
0450 deg
Eccentricity:
0015844
Arg of perigee: 311
5682 deg
Mean anomaly: 48
4111 deg
Mean motion: 15
51583251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 245
Checksum: 269
Coasting Arc #9 (Orbit 260)
---------------------------------------
Vector Time (GMT): 2012/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3439985
34 A = 6796341
42 meter
Y = -5815838
81 meter E =
0005538
Z = -745818
33 I = 51
95524
XDOT = 4423
274129 Wp = 305
33483
YDOT = -1846
261786 meter/sec RA = 54
44122 deg
ZDOT = -5970
382904 TA = 242
67306
MA = 242
72945
Ha = 226
981 n
mi
Hp = 218
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11286041
14 X = -3371072
67
Y = -19080836
00 feet Y = -5853921
57 meter
Z = -2446910
54 Z = -762362
49
XDOT = 14512
054230 XDOT = 4472
593862
YDOT = -6057
289324 feet/sec YDOT = -1796
522198 meter/sec
ZDOT = -19587
870420 ZDOT = -5948
774728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22152089
56 X = 6751956
90
Y = -633379
87 feet Y = -193054
18 meter
Z = -2514787
53 Z = -766507
24
XDOT = -1822
171667 XDOT = -555
397924
YDOT = 14121
461760 feet/sec YDOT = 4304
221544 meter/sec
ZDOT = -19498
040616 ZDOT = -5943
002780
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 12327
53071316
00016717 00000-0 10270-3 0 9086
2 25544 51
6481 54
9283 0015775 315
2000 44
7877 15
51631565 2618
Satellite: ISS
Catalog Number: 25544
Epoch time: 12327
53071316 = yrday
fracday
Element set: 908
Inclination: 51
6481 deg
RA of node: 54
9283 deg
Eccentricity:
0015775
Arg of perigee: 315
2000 deg
Mean anomaly: 44
7877 deg
Mean motion: 15
51631565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 261
Checksum: 298
Coasting Arc #10 (Orbit 276)
---------------------------------------
Vector Time (GMT): 2012/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3227428
47 A = 6795360
53 meter
Y = 5740186
33 meter E =
0018326
Z = 1626369
59 I = 51
93461
XDOT = -4942
552489 Wp = 6
40801
YDOT = 1151
808408 meter/sec RA = 49
50130 deg
ZDOT = 5754
430694 TA = 11
32244
MA = 11
28127
Ha = 227
207 n
mi
Hp = 218
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10588676
10 X = 3155099
96
Y = 18832632
31 feet Y = 5775873
03 meter
Z = 5335858
24 Z = 1641872
92
XDOT = -16215
723388 XDOT = -4983
019127
YDOT = 3778
898975 feet/sec YDOT = 1096
311399 meter/sec
ZDOT = 18879
365793 ZDOT = 5730
321283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21583718
50 X = -6578717
40
Y = 498864
76 feet Y = 152053
98 meter
Z = 5399417
94 Z = 1645742
59
XDOT = 4350
510466 XDOT = 1326
035590
YDOT = -14624
491008 feet/sec YDOT = -4457
544859 meter/sec
ZDOT = 18779
251637 ZDOT = 5723
915899
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 12328
56119019
00016717 00000-0 10270-3 0 9094
2 25544 51
6489 49
8102 0015850 319
5869 40
4104 15
51664444 2778
Satellite: ISS
Catalog Number: 25544
Epoch time: 12328
56119019 = yrday
fracday
Element set: 909
Inclination: 51
6489 deg
RA of node: 49
8102 deg
Eccentricity:
0015850
Arg of perigee: 319
5869 deg
Mean anomaly: 40
4104 deg
Mean motion: 15
51664444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 277
Checksum: 316
Coasting Arc #11 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2012/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2952336
80 A = 6793826
87 meter
Y = -5608926
47 meter E =
0010631
Z = -2455767
87 I = 51
90851
XDOT = 5450
897533 Wp = 328
72077
YDOT = -518
215586 meter/sec RA = 44
55950 deg
ZDOT = -5350
263559 TA = 238
60392
MA = 238
70794
Ha = 227
389 n
mi
Hp = 218
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9686144
36 X = -2877467
37
Y = -18401989
73 feet Y = -5641522
69 meter
Z = -8056981
19 Z = -2469928
71
XDOT = 17883
522089 XDOT = 5482
278099
YDOT = -1700
182370 feet/sec YDOT = -457
084695 meter/sec
ZDOT = -17553
358134 ZDOT = -5323
706593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20771523
79 X = 6331160
45
Y = -245906
12 feet Y = -74952
19 meter
Z = -8114979
62 Z = -2473445
79
XDOT = -6658
111255 XDOT = -2029
392310
YDOT = 15292
307752 feet/sec YDOT = 4661
095403 meter/sec
ZDOT = -17443
177112 ZDOT = -5316
680384
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 12329
52724250
00016717 00000-0 10270-3 0 9102
2 25544 51
6481 45
0134 0015851 323
2531 36
7533 15
51695545 2929
Satellite: ISS
Catalog Number: 25544
Epoch time: 12329
52724250 = yrday
fracday
Element set: 910
Inclination: 51
6481 deg
RA of node: 45
0134 deg
Eccentricity:
0015851
Arg of perigee: 323
2531 deg
Mean anomaly: 36
7533 deg
Mean motion: 15
51695545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 292
Checksum: 285
Coasting Arc #12 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2012/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2534054
43 A = 6791789
77 meter
Y = 5394617
36 meter E =
0014534
Z = 3237348
21 I = 51
88054
XDOT = -5983
997948 Wp = 15
80528
YDOT = -64
162839 meter/sec RA = 39
61249 deg
ZDOT = 4799
497242 TA = 21
54555
MA = 21
48445
Ha = 227
539 n
mi
Hp = 217
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8313826
88 X = 2457815
70
Y = 17698875
86 feet Y = 5422528
37 meter
Z = 10621221
17 Z = 3249473
79
XDOT = -19632
539199 XDOT = -6006
151095
YDOT = -210
508003 feet/sec YDOT = -131
203662 meter/sec
ZDOT = 15746
382029 ZDOT = 4770
372806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19524367
59 X = -5951027
24
Y = -336779
36 feet Y = -102650
35 meter
Z = 10670797
22 Z = 3252458
99
XDOT = 8804
492364 XDOT = 2683
609273
YDOT = -16220
436092 feet/sec YDOT = -4943
988921 meter/sec
ZDOT = 15625
632535 ZDOT = 4762
692797
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 12330
55767581
00016717 00000-0 10270-3 0 9112
2 25544 51
6488 39
8951 0015912 327
2668 32
7496 15
51743387 3087
Satellite: ISS
Catalog Number: 25544
Epoch time: 12330
55767581 = yrday
fracday
Element set: 911
Inclination: 51
6488 deg
RA of node: 39
8951 deg
Eccentricity:
0015912
Arg of perigee: 327
2668 deg
Mean anomaly: 32
7496 deg
Mean motion: 15
51743387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 333
Coasting Arc #13 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2012/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2054395
06 A = 6789734
08 meter
Y = -5160640
68 meter E =
0015853
Z = -3916204
81 I = 51
84889
XDOT = 6446
446039 Wp = 354
63946
YDOT = 550
657502 meter/sec RA = 34
66188 deg
ZDOT = -4090
648535 TA = 232
47847
MA = 232
62266
Ha = 227
758 n
mi
Hp = 217
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6740141
27 X = -1977510
55
Y = -16931235
81 feet Y = -5183184
13 meter
Z = -12848440
98 Z = -3925998
68
XDOT = 21149
757345 XDOT = 6459
681233
YDOT = 1806
619102 feet/sec YDOT = 622
819893 meter/sec
ZDOT = -13420
762911 ZDOT = -4059
299127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18161071
33 X = 5535494
54
Y = 1115391
91 feet Y = 339971
45 meter
Z = -12888369
76 Z = -3928375
10
XDOT = -10524
653323 XDOT = -3207
914333
YDOT = 17156
993561 feet/sec YDOT = 5229
451637 meter/sec
ZDOT = -13290
854065 ZDOT = -4051
052319
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 12331
52368893
00016717 00000-0 10270-3 0 9124
2 25544 51
6480 35
0978 0015934 331
2525 28
7747 15
51754243 3231
Satellite: ISS
Catalog Number: 25544
Epoch time: 12331
52368893 = yrday
fracday
Element set: 912
Inclination: 51
6480 deg
RA of node: 35
0978 deg
Eccentricity:
0015934
Arg of perigee: 331
2525 deg
Mean anomaly: 28
7747 deg
Mean motion: 15
51754243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 309
Coasting Arc #14 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2012/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1417936
75 A = 6787487
73 meter
Y = 4878076
64 meter E =
0011272
Z = 4494113
99 I = 51
81677
XDOT = -6877
416237 Wp = 7
41510
YDOT = -983
408370 meter/sec RA = 29
70522 deg
ZDOT = 3247
312105 TA = 50
03881
MA = 49
93986
Ha = 227
903 n
mi
Hp = 217
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4652023
45 X = 1341451
84
Y = 16004188
44 feet Y = 4893504
95 meter
Z = 14744468
46 Z = 4500816
94
XDOT = -22563
701564 XDOT = -6881
683445
YDOT = -3226
405412 feet/sec YDOT = -1060
340007 meter/sec
ZDOT = 10653
911107 ZDOT = 3213
890797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16476661
54 X = -5022086
44
Y = -2343899
66 feet Y = -714420
62 meter
Z = 14771610
57 Z = 4502386
90
XDOT = 11981
045169 XDOT = 3651
822568
YDOT = -18158
016112 feet/sec YDOT = -5534
563311 meter/sec
ZDOT = 10515
471214 ZDOT = 3205
115626
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 12332
55407959
00016717 00000-0 10270-3 0 9136
2 25544 51
6484 29
9794 0016010 335
2259 24
8122 15
51809670 3393
Satellite: ISS
Catalog Number: 25544
Epoch time: 12332
55407959 = yrday
fracday
Element set: 913
Inclination: 51
6484 deg
RA of node: 29
9794 deg
Eccentricity:
0016010
Arg of perigee: 335
2259 deg
Mean anomaly: 24
8122 deg
Mean motion: 15
51809670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 313
Coasting Arc #15 (Orbit 353)
---------------------------------------
Vector Time (GMT): 2012/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -748336
97 A = 6785811
86 meter
Y = -4617238
61 meter E =
0019388
Z = -4927821
02 I = 51
78378
XDOT = 7180
796071 Wp = 17
57282
YDOT = 1311
939894 meter/sec RA = 24
74436 deg
ZDOT = -2304
074406 TA = 229
81572
MA = 229
98561
Ha = 228
094 n
mi
Hp = 216
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2455173
79 X = -672711
73
Y = -15148420
63 feet Y = -4625183
74 meter
Z = -16167391
79 Z = -4931273
14
XDOT = 23559
042228 XDOT = 7176
784868
YDOT = 4304
264743 feet/sec YDOT = 1392
217798 meter/sec
ZDOT = -7559
299232 ZDOT = -2269
199404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14864585
60 X = 4530725
69
Y = 3755491
07 feet Y = 1144673
68 meter
Z = -16181083
55 Z = -4931994
27
XDOT = -12917
312667 XDOT = -3937
196901
YDOT = 18958
783218 feet/sec YDOT = 5778
637125 meter/sec
ZDOT = -7414
877682 ZDOT = -2260
054718
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 12333
52005322
00016717 00000-0 10270-3 0 9143
2 25544 51
6480 25
1814 0016028 339
2492 20
8007 15
51813585 3547
Satellite: ISS
Catalog Number: 25544
Epoch time: 12333
52005322 = yrday
fracday
Element set: 914
Inclination: 51
6480 deg
RA of node: 25
1814 deg
Eccentricity:
0016028
Arg of perigee: 339
2492 deg
Mean anomaly: 20
8007 deg
Mean motion: 15
51813585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 354
Checksum: 274
Coasting Arc #16 (Orbit 359)
---------------------------------------
Vector Time (GMT): 2012/333/21:04:18
675
Vector Time (MET): N/A
Weight (LBS) : 906113
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5290202
04 A = 6796626
72 meter
Y = -3837513
67 meter E =
0006907
Z = -1880765
94 I = 51
80306
XDOT = 4205
178930 Wp = 351
74335
YDOT = -3033
563110 meter/sec RA = 22
86997 deg
ZDOT = -5629
378411 TA = 208
86012
MA = 208
89834
Ha = 228
272 n
mi
Hp = 218
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17356305
91 X = -5237760
48
Y = -12590267
95 feet Y = -3896378
64 meter
Z = -6170491
92 Z = -1906338
90
XDOT = 13796
518798 XDOT = 4266
135058
YDOT = -9952
634876 feet/sec YDOT = -2986
196875 meter/sec
ZDOT = -18469
089275 ZDOT = -5608
801669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20896776
78 X = -6369337
56
Y = -4665583
25 feet Y = -1422069
78 meter
Z = -6276003
97 Z = -1912926
01
XDOT = 8463
957370 XDOT = 2579
814206
YDOT = -13140
578856 feet/sec YDOT = -4005
248435 meter/sec
ZDOT = -18383
364493 ZDOT = -5603
249498
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 12333
90645253
00016717 00000-0 10270-3 0 9159
2 25544 51
6487 23
2626 0013394 336
3982 23
6554 15
51089996 3605
Satellite: ISS
Catalog Number: 25544
Epoch time: 12333
90645253 = yrday
fracday
Element set: 915
Inclination: 51
6487 deg
RA of node: 23
2626 deg
Eccentricity:
0013394
Arg of perigee: 336
3982 deg
Mean anomaly: 23
6554 deg
Mean motion: 15
51089996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 360
Checksum: 318
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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