[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 19th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19913 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 123 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 362 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
053/10:36:18
445 -1
3 1
9 1
9
N/A -0
7 -0
2 223
8
000/00:04:36
891 -1
3 -0
0 219
4
Coasting Arc #1 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2013/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2861199
71 A = 6782159
80 meter
Y = 3289665
75 meter E =
0009035
Z = 5202406
06 I = 51
49615
XDOT = -6548
827550 Wp = 282
76979
YDOT = 3783
824154 meter/sec RA = 337
31023 deg
ZDOT = 1212
789833 TA = 155
57903
MA = 155
53620
Ha = 222
801 n
mi
Hp = 218
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9387138
16 X = 2798929
79
Y = 10792866
63 feet Y = 3321313
52 meter
Z = 17068261
36 Z = 5216153
94
XDOT = -21485
654691 XDOT = -6596
543677
YDOT = 12414
121239 feet/sec YDOT = 3710
324304 meter/sec
ZDOT = 3978
969267 ZDOT = 1180
860603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2102785
47 X = 640929
01
Y = 14079843
38 feet Y = 4291536
26 meter
Z = 17125016
28 Z = 5219704
96
XDOT = -23790
067064 XDOT = -7251
212441
YDOT = -1109
513966 feet/sec YDOT = -338
179857 meter/sec
ZDOT = 3845
626913 ZDOT = 1172
147083
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 13049
55028654
00016717 00000-0 10270-3 0 9009
2 25544 51
6479 337
5996 0012823 289
6380 70
3388 15
52633833 16283
Satellite: ISS
Catalog Number: 25544
Epoch time: 13049
55028654 = yrday
fracday
Element set: 900
Inclination: 51
6479 deg
RA of node: 337
5996 deg
Eccentricity:
0012823
Arg of perigee: 289
6380 deg
Mean anomaly: 70
3388 deg
Mean motion: 15
52633833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1628
Checksum: 336
Coasting Arc #2 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2013/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1817365
16 A = 6781694
76 meter
Y = -3817468
85 meter E =
0005695
Z = -5305038
07 I = 51
46710
XDOT = 6839
515343 Wp = 33
63050
YDOT = -3455
340028 meter/sec RA = 332
31492 deg
ZDOT = 148
124682 TA = 237
75762
MA = 237
81283
Ha = 223
075 n
mi
Hp = 218
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5962484
11 X = -1748772
31
Y = -12524504
11 feet Y = -3837408
45 meter
Z = -17404980
54 Z = -5313699
77
XDOT = 22439
354800 XDOT = 6876
925824
YDOT = -11336
417415 feet/sec YDOT = -3378
647091 meter/sec
ZDOT = 485
973365 ZDOT = 181
440900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1483367
28 X = 452130
35
Y = -13746858
70 feet Y = -4190042
53 meter
Z = -17440506
44 Z = -5315866
36
XDOT = 24060
592093 XDOT = 7333
668470
YDOT = 1822
915111 feet/sec YDOT = 555
624526 meter/sec
ZDOT = 625
038366 ZDOT = 190
511694
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 13050
51575764
00016717 00000-0 10270-3 0 9017
2 25544 51
6483 332
7975 0012728 293
6714 66
3102 15
52640060 16438
Satellite: ISS
Catalog Number: 25544
Epoch time: 13050
51575764 = yrday
fracday
Element set: 901
Inclination: 51
6483 deg
RA of node: 332
7975 deg
Eccentricity:
0012728
Arg of perigee: 293
6714 deg
Mean anomaly: 66
3102 deg
Mean motion: 15
52640060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 299
Coasting Arc #3 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2013/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 752701
83 A = 6782372
71 meter
Y = 4378311
13 meter E =
0011412
Z = 5133343
09 I = 51
44299
XDOT = -6889
993601 Wp = 319
00494
YDOT = 2977
851299 meter/sec RA = 327
31840 deg
ZDOT = -1523
068940 TA = 145
76414
MA = 145
69051
Ha = 223
352 n
mi
Hp = 218
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2469494
19 X = 678750
75
Y = 14364537
84 feet Y = 4386315
05 meter
Z = 16841676
80 Z = 5136819
78
XDOT = -22604
965882 XDOT = -6915
381968
YDOT = 9769
853343 feet/sec YDOT = 2900
661045 meter/sec
ZDOT = -4996
945340 ZDOT = -1556
601079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5188009
19 X = -1581305
20
Y = 13603494
39 feet Y = 4146345
09 meter
Z = 16855560
72 Z = 5137574
91
XDOT = -23430
823624 XDOT = -7141
715041
YDOT = -2544
591053 feet/sec YDOT = -775
591353 meter/sec
ZDOT = -5136
841299 ZDOT = -1565
709228
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 13051
54557114
00016717 00000-0 10270-3 0 9021
2 25544 51
6482 327
6759 0012830 297
3849 62
5997 15
52686043 16592
Satellite: ISS
Catalog Number: 25544
Epoch time: 13051
54557114 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 327
6759 deg
Eccentricity:
0012830
Arg of perigee: 297
3849 deg
Mean anomaly: 62
5997 deg
Mean motion: 15
52686043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1659
Checksum: 337
Coasting Arc #4 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2013/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 241881
13 A = 6784213
58 meter
Y = -4903249
98 meter E =
0003177
Z = -4680204
74 I = 51
42467
XDOT = 6729
276226 Wp = 342
51222
YDOT = -2356
260646 meter/sec RA = 322
32175 deg
ZDOT = 2818
806433 TA = 315
52761
MA = 315
55311
Ha = 223
566 n
mi
Hp = 218
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 793573
26 X = 319427
03
Y = -16086778
13 feet Y = -4900111
75 meter
Z = -15355002
42 Z = -4678841
13
XDOT = 22077
677908 XDOT = 6741
431586
YDOT = -7730
513930 feet/sec YDOT = -2280
941548 meter/sec
ZDOT = 9248
052601 ZDOT = 2851
525609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8633697
38 X = 2631550
96
Y = -13603947
74 feet Y = -4146483
27 meter
Z = -15348686
06 Z = -4678279
51
XDOT = 21998
171443 XDOT = 6705
042656
YDOT = 3382
155217 feet/sec YDOT = 1030
880910 meter/sec
ZDOT = 9384
480510 ZDOT = 2860
389659
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 13052
51100333
00016717 00000-0 10270-3 0 9037
2 25544 51
6489 322
8735 0012793 301
0142 58
9753 15
52698800 16747
Satellite: ISS
Catalog Number: 25544
Epoch time: 13052
51100333 = yrday
fracday
Element set: 903
Inclination: 51
6489 deg
RA of node: 322
8735 deg
Eccentricity:
0012793
Arg of perigee: 301
0142 deg
Mean anomaly: 58
9753 deg
Mean motion: 15
52698800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1674
Checksum: 298
Coasting Arc #5 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2013/053/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4775055
90 A = 6794415
62 meter
Y = 4812459
83 meter E =
0002668
Z = 423525
46 I = 51
43213
XDOT = -3659
546455 Wp = 190
52959
YDOT = -3106
359451 meter/sec RA = 317
63175 deg
ZDOT = -5971
130834 TA = 344
89649
MA = 344
90445
Ha = 223
787 n
mi
Hp = 219
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15666193
91 X = -4830572
29
Y = 15788910
22 feet Y = 4758751
78 meter
Z = 1389519
22 Z = 400194
05
XDOT = -12006
386008 XDOT = -3595
533013
YDOT = -10191
468015 feet/sec YDOT = -3146
925249 meter/sec
ZDOT = -19590
324259 ZDOT = -5988
752505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22207879
29 X = -6768961
61
Y = -1338413
19 feet Y = -407948
34 meter
Z = 1291831
48 Z = 393750
24
XDOT = -296
091999 XDOT = -90
248841
YDOT = -14036
823937 feet/sec YDOT = -4278
423936 meter/sec
ZDOT = -19663
230322 ZDOT = -5993
352602
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 13053
47642588
00016717 00000-0 10270-3 0 9047
2 25544 51
6479 318
0716 0011682 299
3677 60
6307 15
52356231 16890
Satellite: ISS
Catalog Number: 25544
Epoch time: 13053
47642588 = yrday
fracday
Element set: 904
Inclination: 51
6479 deg
RA of node: 318
0716 deg
Eccentricity:
0011682
Arg of perigee: 299
3677 deg
Mean anomaly: 60
6307 deg
Mean motion: 15
52356231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 331
Coasting Arc #6 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2013/054/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4975225
80 A = 6794171
64 meter
Y = -4556492
18 meter E =
0014469
Z = 716459
27 I = 51
40929
XDOT = 2785
080802 Wp = 2
69675
YDOT = 3973
662206 meter/sec RA = 312
65385 deg
ZDOT = 5940
598737 TA = 5
06818
MA = 5
05355
Ha = 223
966 n
mi
Hp = 219
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16322919
29 X = 5022327
41
Y = -14949121
33 feet Y = -4500592
66 meter
Z = 2350588
16 Z = 740742
67
XDOT = 9137
404205 XDOT = 2711
582324
YDOT = 13036
949494 feet/sec YDOT = 4004
396255 meter/sec
ZDOT = 19490
153336 ZDOT = 5953
949251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22033257
80 X = 6715736
98
Y = 1990347
22 feet Y = 606657
83 meter
Z = 2452194
14 Z = 747428
77
XDOT = -3422
199432 XDOT = -1043
086387
YDOT = 13839
349733 feet/sec YDOT = 4218
233799 meter/sec
ZDOT = 19545
184207 ZDOT = 5957
372146
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 13054
50641744
00016717 00000-0 10270-3 0 9056
2 25544 51
6475 312
9506 0011774 303
5640 56
4387 15
52384779 17054
Satellite: ISS
Catalog Number: 25544
Epoch time: 13054
50641744 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 312
9506 deg
Eccentricity:
0011774
Arg of perigee: 303
5640 deg
Mean anomaly: 56
4387 deg
Mean motion: 15
52384779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 314
Coasting Arc #7 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2013/055/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5052064
24 A = 6792847
89 meter
Y = 4157376
72 meter E =
0005155
Z = -1825369
95 I = 51
38585
XDOT = -1940
035119 Wp = 285
71732
YDOT = -4831
314123 meter/sec RA = 307
67352 deg
ZDOT = -5619
501537 TA = 274
39876
MA = 274
45765
Ha = 224
168 n
mi
Hp = 218
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16575013
92 X = -5089310
48
Y = 13639687
40 feet Y = 4100672
92 meter
Z = -5988746
56 Z = -1850002
75
XDOT = -6364
944616 XDOT = -1858
568748
YDOT = -15850
768121 feet/sec YDOT = -4852
553881 meter/sec
ZDOT = -18436
684832 ZDOT = -5628
727475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21268843
92 X = -6482743
63
Y = -2676594
97 feet Y = -815826
15 meter
Z = -6091745
40 Z = -1856764
00
XDOT = 7050
637119 XDOT = 2149
034194
YDOT = -13871
870512 feet/sec YDOT = -4228
146132 meter/sec
ZDOT = -18474
455262 ZDOT = -5631
013964
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 13055
47201539
00016717 00000-0 10270-3 0 9068
2 25544 51
6481 308
1501 0011777 306
6285 53
3783 15
52417245 17203
Satellite: ISS
Catalog Number: 25544
Epoch time: 13055
47201539 = yrday
fracday
Element set: 906
Inclination: 51
6481 deg
RA of node: 308
1501 deg
Eccentricity:
0011777
Arg of perigee: 306
6285 deg
Mean anomaly: 53
3783 deg
Mean motion: 15
52417245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 295
Coasting Arc #8 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2013/056/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5009348
65 A = 6790674
44 meter
Y = -3566224
23 meter E =
0010556
Z = 2864575
35 I = 51
36046
XDOT = 1152
420354 Wp = 23
11541
YDOT = 5664
724886 meter/sec RA = 302
68799 deg
ZDOT = 5040
175757 TA = 9
61100
MA = 9
59082
Ha = 224
267 n
mi
Hp = 218
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16434870
91 X = 5034939
58
Y = -11700210
72 feet Y = -3510063
11 meter
Z = 9398213
08 Z = 2888972
40
XDOT = 3780
906674 XDOT = 1064
507231
YDOT = 18585
055399 feet/sec YDOT = 5677
121028 meter/sec
ZDOT = 16536
009700 ZDOT = 5045
559785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19810932
03 X = 6038372
08
Y = 3549717
48 feet Y = 1081953
89 meter
Z = 9500147
35 Z = 2895644
91
XDOT = -10473
932059 XDOT = -3192
454491
YDOT = 14169
109664 feet/sec YDOT = 4318
744625 meter/sec
ZDOT = 16557
702247 ZDOT = 5046
787645
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 13056
50196790
00016717 00000-0 10270-3 0 9076
2 25544 51
6476 303
0287 0011802 310
9750 49
0380 15
52445645 17363
Satellite: ISS
Catalog Number: 25544
Epoch time: 13056
50196790 = yrday
fracday
Element set: 907
Inclination: 51
6476 deg
RA of node: 303
0287 deg
Eccentricity:
0011802
Arg of perigee: 310
9750 deg
Mean anomaly: 49
0380 deg
Mean motion: 15
52445645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 303
Coasting Arc #9 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2013/057/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4890159
89 A = 6788000
83 meter
Y = 2833615
13 meter E =
0010052
Z = -3765466
02 I = 51
33659
XDOT = -450
426391 Wp = 344
22065
YDOT = -6384
363880 meter/sec RA = 297
69727 deg
ZDOT = -4207
291184 TA = 241
02107
MA = 241
12186
Ha = 224
497 n
mi
Hp = 218
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16043831
67 X = -4903191
22
Y = 9296637
56 feet Y = 2778856
93 meter
Z = -12353891
15 Z = -3789253
60
XDOT = -1477
776872 XDOT = -358
564056
YDOT = -20946
075723 feet/sec YDOT = -6388
887754 meter/sec
ZDOT = -13803
448766 ZDOT = -4209
255312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17886989
08 X = -5451954
27
Y = -4628637
60 feet Y = -1410808
74 meter
Z = -12453191
02 Z = -3795732
62
XDOT = 13410
763639 XDOT = 4087
600757
YDOT = -14560
793806 feet/sec YDOT = -4438
129952 meter/sec
ZDOT = -13810
835904 ZDOT = -4209
542784
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 13057
46752880
00016717 00000-0 10270-3 0 9081
2 25544 51
6479 298
2279 0011916 314
1495 45
8676 15
52493059 17511
Satellite: ISS
Catalog Number: 25544
Epoch time: 13057
46752880 = yrday
fracday
Element set: 908
Inclination: 51
6479 deg
RA of node: 298
2279 deg
Eccentricity:
0011916
Arg of perigee: 314
1495 deg
Mean anomaly: 45
8676 deg
Mean motion: 15
52493059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 346
Coasting Arc #10 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2013/058/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4703906
98 A = 6785363
72 meter
Y = -1914162
06 meter E =
0005459
Z = 4496922
69 I = 51
31414
XDOT = -176
319464 Wp = 2
08769
YDOT = 6982
282941 meter/sec RA = 292
69926 deg
ZDOT = 3161
751815 TA = 56
04657
MA = 55
99470
Ha = 224
575 n
mi
Hp = 218
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15432765
69 X = 4703117
38
Y = -6280059
25 feet Y = -1861563
82 meter
Z = 14753683
37 Z = 4519771
90
XDOT = -578
475931 XDOT = -269
742479
YDOT = 22907
752432 feet/sec YDOT = 6979
789295 meter/sec
ZDOT = 10373
201492 ZDOT = 3160
667422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15426382
05 X = 4701961
25
Y = 6067591
06 feet Y = 1849401
76 meter
Z = 14848961
23 Z = 4525963
38
XDOT = -15857
315476 XDOT = -4833
309757
YDOT = 14984
973257 feet/sec YDOT = 4567
419849 meter/sec
ZDOT = 10367
844521 ZDOT = 3160
119010
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 13058
49744246
00016717 00000-0 10270-3 0 9093
2 25544 51
6475 293
1058 0011884 318
2345 41
7899 15
52508665 17678
Satellite: ISS
Catalog Number: 25544
Epoch time: 13058
49744246 = yrday
fracday
Element set: 909
Inclination: 51
6475 deg
RA of node: 293
1058 deg
Eccentricity:
0011884
Arg of perigee: 318
2345 deg
Mean anomaly: 41
7899 deg
Mean motion: 15
52508665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1767
Checksum: 345
Coasting Arc #11 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2013/059/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4497959
95 A = 6783173
96 meter
Y = 907501
57 meter E =
0013596
Z = -5003731
18 I = 51
29639
XDOT = 704
149497 Wp = 21
23959
YDOT = -7370
636311 meter/sec RA = 287
69640 deg
ZDOT = -1958
986006 TA = 229
56851
MA = 229
68718
Ha = 224
771 n
mi
Hp = 217
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14757086
45 X = -4483466
95
Y = 2977367
34 feet Y = 857282
94 meter
Z = -16416440
89 Z = -5025546
60
XDOT = 2310
201761 XDOT = 796
033334
YDOT = -24181
877660 feet/sec YDOT = -7362
248570 meter/sec
ZDOT = -6427
119441 ZDOT = -1955
341206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12783050
47 X = -3896273
78
Y = -7761361
99 feet Y = -2365663
14 meter
Z = -16507293
20 Z = -5031422
97
XDOT = 17572
756276 XDOT = 5356
176113
YDOT = -15232
403154 feet/sec YDOT = -4642
836481 meter/sec
ZDOT = -6411
074214 ZDOT = -1954
095421
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 13059
46296680
00016717 00000-0 10270-3 0 9107
2 25544 51
6474 288
3043 0012047 321
5618 38
4675 15
52567915 17824
Satellite: ISS
Catalog Number: 25544
Epoch time: 13059
46296680 = yrday
fracday
Element set: 910
Inclination: 51
6474 deg
RA of node: 288
3043 deg
Eccentricity:
0012047
Arg of perigee: 321
5618 deg
Mean anomaly: 38
4675 deg
Mean motion: 15
52567915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1782
Checksum: 325
Coasting Arc #12 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2013/060/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4273119
19 A = 6781974
10 meter
Y = 232535
08 meter E =
0009614
Z = 5264238
63 I = 51
28416
XDOT = -1179
126630 Wp = 333
64769
YDOT = 7546
107352 meter/sec RA = 282
68852 deg
ZDOT = 632
703119 TA = 110
33030
MA = 110
22697
Ha = 224
874 n
mi
Hp = 217
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14019419
92 X = 4244629
22
Y = 762910
36 feet Y = 280161
10 meter
Z = 17271124
11 Z = 5284927
72
XDOT = -3868
525690 XDOT = -1266
494659
YDOT = 24757
570052 feet/sec YDOT = 7532
433188 meter/sec
ZDOT = 2075
797635 ZDOT = 626
761969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9869451
24 X = 3008208
74
Y = 9835702
02 feet Y = 2997921
98 meter
Z = 17357153
95 Z = 5290460
52
XDOT = -18666
381813 XDOT = -5689
513176
YDOT = 15163
758765 feet/sec YDOT = 4621
913672 meter/sec
ZDOT = 2050
187015 ZDOT = 624
897002
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 13060
49284105
00016717 00000-0 10270-3 0 9112
2 25544 51
6474 283
1819 0012034 325
1396 34
8967 15
52584270 17981
Satellite: ISS
Catalog Number: 25544
Epoch time: 13060
49284105 = yrday
fracday
Element set: 911
Inclination: 51
6474 deg
RA of node: 283
1819 deg
Eccentricity:
0012034
Arg of perigee: 325
1396 deg
Mean anomaly: 34
8967 deg
Mean motion: 15
52584270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 317
Coasting Arc #13 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2013/061/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4069887
33 A = 6781905
25 meter
Y = -1361545
32 meter E =
0012121
Z = -5257475
88 I = 51
27815
XDOT = 1584
699371 Wp = 42
26769
YDOT = -7461
151917 meter/sec RA = 277
67914 deg
ZDOT = 715
271154 TA = 234
54868
MA = 234
66189
Ha = 225
029 n
mi
Hp = 217
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13352648
74 X = -4028820
45
Y = -4467012
22 feet Y = -1406828
26 meter
Z = -17248936
62 Z = -5277147
08
XDOT = 5199
144919 XDOT = 1664
539200
YDOT = -24478
844871 feet/sec YDOT = -7442
984332 meter/sec
ZDOT = 2346
690138 ZDOT = 723
164107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7113343
43 X = -2168147
08
Y = -12034279
89 feet Y = -3668048
51 meter
Z = -17330599
93 Z = -5282366
86
XDOT = 19034
774148 XDOT = 5801
799160
YDOT = -14633
342562 feet/sec YDOT = -4460
242813 meter/sec
ZDOT = 2380
403506 ZDOT = 725
546989
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 13061
45832967
00016717 00000-0 10270-3 0 9125
2 25544 51
6470 278
3796 0012178 328
5163 31
5259 15
52623655 18132
Satellite: ISS
Catalog Number: 25544
Epoch time: 13061
45832967 = yrday
fracday
Element set: 912
Inclination: 51
6470 deg
RA of node: 278
3796 deg
Eccentricity:
0012178
Arg of perigee: 328
5163 deg
Mean anomaly: 31
5259 deg
Mean motion: 15
52623655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1813
Checksum: 321
Coasting Arc #14 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2013/062/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3869414
84 A = 6783038
91 meter
Y = 2531000
89 meter E =
0014171
Z = 4968126
21 I = 51
27953
XDOT = -1985
423204 Wp = 357
15094
YDOT = 7107
097858 meter/sec RA = 272
67042 deg
ZDOT = -2060
701139 TA = 113
08958
MA = 112
94014
Ha = 225
180 n
mi
Hp = 216
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12694930
56 X = 3816691
35
Y = 8303808
70 feet Y = 2573976
71 meter
Z = 16299626
67 Z = 4986795
14
XDOT = -6513
855656 XDOT = -2054
738436
YDOT = 23317
250191 feet/sec YDOT = 7084
507885 meter/sec
ZDOT = -6760
830509 ZDOT = -2070
515017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4363130
51 X = 1329882
18
Y = 14441250
39 feet Y = 4401693
12 meter
Z = 16376987
21 Z = 4991705
70
XDOT = -18841
463942 XDOT = -5742
878209
YDOT = 13457
425351 feet/sec YDOT = 4101
823247 meter/sec
ZDOT = -6802
487845 ZDOT = -2073
398295
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 13062
48816404
00016717 00000-0 10270-3 0 9138
2 25544 51
6473 273
2573 0012279 331
9449 28
1040 15
52669292 18293
Satellite: ISS
Catalog Number: 25544
Epoch time: 13062
48816404 = yrday
fracday
Element set: 913
Inclination: 51
6473 deg
RA of node: 273
2573 deg
Eccentricity:
0012279
Arg of perigee: 331
9449 deg
Mean anomaly: 28
1040 deg
Mean motion: 15
52669292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1829
Checksum: 315
Coasting Arc #15 (Orbit 1843)
---------------------------------------
Vector Time (GMT): 2013/063/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3696537
51 A = 6785175
43 meter
Y = -3573631
49 meter E =
0008693
Z = -4426125
00 I = 51
28545
XDOT = 2370
045975 Wp = 24
11873
YDOT = -6507
901158 meter/sec RA = 267
66454 deg
ZDOT = 3285
154805 TA = 279
14691
MA = 279
24525
Ha = 225
293 n
mi
Hp = 216
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12127747
73 X = -3634800
89
Y = -11724512
77 feet Y = -3614623
58 meter
Z = -14521407
48 Z = -4443932
15
XDOT = 7775
741387 XDOT = 2426
684280
YDOT = -21351
381752 feet/sec YDOT = -6481
080930 meter/sec
ZDOT = 10778
066944 ZDOT = 3296
806163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2034009
67 X = -619966
15
Y = -16681262
88 feet Y = -5084448
93 meter
Z = -14595068
12 Z = -4448576
76
XDOT = 18170
280509 XDOT = 5538
301499
YDOT = -11659
982358 feet/sec YDOT = -3553
962623 meter/sec
ZDOT = 10827
293662 ZDOT = 3300
159108
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 13063
45361701
00016717 00000-0 10270-3 0 9142
2 25544 51
6464 268
4546 0012308 335
3930 24
6633 15
52674032 18449
Satellite: ISS
Catalog Number: 25544
Epoch time: 13063
45361701 = yrday
fracday
Element set: 914
Inclination: 51
6464 deg
RA of node: 268
4546 deg
Eccentricity:
0012308
Arg of perigee: 335
3930 deg
Mean anomaly: 24
6633 deg
Mean motion: 15
52674032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1844
Checksum: 295
Coasting Arc #16 (Orbit 1859)
---------------------------------------
Vector Time (GMT): 2013/064/10:38:36
891
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3510184
61 A = 6787770
49 meter
Y = 4547829
73 meter E =
0014527
Z = 3620367
70 I = 51
29713
XDOT = -2795
317370 Wp = 30
61343
YDOT = 5644
053039 meter/sec RA = 262
66412 deg
ZDOT = -4359
655755 TA = 106
29423
MA = 106
13440
Ha = 225
493 n
mi
Hp = 216
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11516353
71 X = 3441482
35
Y = 14920701
22 feet Y = 4586698
89 meter
Z = 11877846
78 Z = 3637252
55
XDOT = -9170
988746 XDOT = -2837
044825
YDOT = 18517
234379 feet/sec YDOT = 5612
560493 meter/sec
ZDOT = -14303
332529 ZDOT = -4373
336664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -109012
07 X = -33226
88
Y = 18803742
05 feet Y = 5731380
58 meter
Z = 11947567
67 Z = 3641618
63
XDOT = -17156
717405 XDOT = -5229
367465
YDOT = 9066
732307 feet/sec YDOT = 2763
540007 meter/sec
ZDOT = -14360
898408 ZDOT = -4377
201835
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 13064
48341179
00016717 00000-0 10270-3 0 9154
2 25544 51
6466 263
3324 0012495 339
1207 20
9433 15
52738583 18602
Satellite: ISS
Catalog Number: 25544
Epoch time: 13064
48341179 = yrday
fracday
Element set: 915
Inclination: 51
6466 deg
RA of node: 263
3324 deg
Eccentricity:
0012495
Arg of perigee: 339
1207 deg
Mean anomaly: 20
9433 deg
Mean motion: 15
52738583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1860
Checksum: 310
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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