[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 22nd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 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
There are no maneuvers
Coasting Arc #1 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2013/053/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5521967
42 A = 6793776
77 meter
Y = -3728880
47 meter E =
0012951
Z = 1280692
14 I = 51
42916
XDOT = 1799
152824 Wp = 6
85313
YDOT = 4660
692382 meter/sec RA = 317
15271 deg
ZDOT = 5819
229208 TA = 7
11730
MA = 7
09893
Ha = 223
782 n
mi
Hp = 219
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18116691
02 X = 5557033
04
Y = -12233859
80 feet Y = -3666934
21 meter
Z = 4201745
86 Z = 1307602
16
XDOT = 5902
732362 XDOT = 1718
634653
YDOT = 15290
985504 feet/sec YDOT = 4680
361806 meter/sec
ZDOT = 19091
959344 ZDOT = 5827
773265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20323588
88 X = 6194629
89
Y = -7992250
89 feet Y = -2436038
07 meter
Z = 4314179
91 Z = 1314962
04
XDOT = 1726
616707 XDOT = 526
272772
YDOT = 14704
013932 feet/sec YDOT = 4481
783446 meter/sec
ZDOT = 19126
899791 ZDOT = 5829
879056
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
60518867
00016717 00000-0 10270-3 0 9000
2 25544 51
6493 317
4347 0011811 300
0043 59
9936 15
52349632 16919
Satellite: ISS
Catalog Number: 25544
Epoch time: 13053
60518867 = yrday
fracday
Element set: 900
Inclination: 51
6493 deg
RA of node: 317
4347 deg
Eccentricity:
0011811
Arg of perigee: 300
0043 deg
Mean anomaly: 59
9936 deg
Mean motion: 15
52349632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1691
Checksum: 303
Coasting Arc #2 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2013/054/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5476916
65 A = 6792109
29 meter
Y = 3265323
29 meter E =
0006435
Z = -2338680
38 I = 51
40191
XDOT = -909
667028 Wp = 291
95674
YDOT = -5384
425087 meter/sec RA = 312
17297 deg
ZDOT = -5373
255313 TA = 274
18481
MA = 274
25835
Ha = 224
028 n
mi
Hp = 219
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17968886
66 X = -5501662
73
Y = 10713002
92 feet Y = 3203938
41 meter
Z = -7672835
88 Z = -2365346
50
XDOT = -2984
471875 XDOT = -823
288420
YDOT = -17665
436636 feet/sec YDOT = -5394
115029 meter/sec
ZDOT = -17628
790397 ZDOT = -5377
464041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19711112
87 X = -6007947
20
Y = 6884778
43 feet Y = 2098480
47 meter
Z = -7784188
15 Z = -2372620
55
XDOT = 1242
214528 XDOT = 378
626988
YDOT = -16446
533989 feet/sec YDOT = -5012
903560 meter/sec
ZDOT = -17645
610408 ZDOT = -5378
382052
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
57081435
00016717 00000-0 10270-3 0 9014
2 25544 51
6493 312
6348 0011869 302
4922 57
5082 15
52354753 17065
Satellite: ISS
Catalog Number: 25544
Epoch time: 13054
57081435 = yrday
fracday
Element set: 901
Inclination: 51
6493 deg
RA of node: 312
6348 deg
Eccentricity:
0011869
Arg of perigee: 302
4922 deg
Mean anomaly: 57
5082 deg
Mean motion: 15
52354753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 303
Coasting Arc #3 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2013/055/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5309611
05 A = 6789678
39 meter
Y = -2627946
44 meter E =
0008118
Z = 3306040
92 I = 51
37386
XDOT = 91
101154 Wp = 22
12042
YDOT = 6071
080766 meter/sec RA = 307
18663 deg
ZDOT = 4683
162836 TA = 16
47056
MA = 16
44420
Ha = 224
180 n
mi
Hp = 218
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17419983
75 X = 5322543
19
Y = -8621871
51 feet Y = -2568498
38 meter
Z = 10846590
95 Z = 3331865
63
XDOT = 298
888300 XDOT =
457238
YDOT = 19918
243984 feet/sec YDOT = 6071
593182 meter/sec
ZDOT = 15364
707466 ZDOT = 4683
384595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18645292
32 X = 5683085
10
Y = -5272213
19 feet Y = -1606970
58 meter
Z = 10954354
38 Z = 3338887
22
XDOT = -3858
152915 XDOT = -1175
965008
YDOT = 18255
520665 feet/sec YDOT = 5564
282699 meter/sec
ZDOT = 15364
864582 ZDOT = 4683
210725
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
60079992
00016717 00000-0 10270-3 0 9025
2 25544 51
6489 307
5132 0011903 307
5973 52
4098 15
52385718 17229
Satellite: ISS
Catalog Number: 25544
Epoch time: 13055
60079992 = yrday
fracday
Element set: 902
Inclination: 51
6489 deg
RA of node: 307
5132 deg
Eccentricity:
0011903
Arg of perigee: 307
5973 deg
Mean anomaly: 52
4098 deg
Mean motion: 15
52385718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 318
Coasting Arc #4 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2013/056/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5067131
05 A = 6787034
66 meter
Y = 1871046
73 meter E =
0010472
Z = -4114838
73 I = 51
34682
XDOT = 618
376003 Wp = 348
53455
YDOT = -6639
722122 meter/sec RA = 302
19525 deg
ZDOT = -3768
883410 TA = 242
35834
MA = 242
46468
Ha = 224
407 n
mi
Hp = 218
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16624445
72 X = -5067688
52
Y = 6138604
74 feet Y = 1814379
26 meter
Z = -13500127
08 Z = -4139455
48
XDOT = 2028
792660 XDOT = 710
884680
YDOT = -21783
865231 feet/sec YDOT = -6632
290265 meter/sec
ZDOT = -12365
103052 ZDOT = -3765
653956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17335388
53 X = -5283826
43
Y = 3279819
57 feet Y = 999689
01 meter
Z = -13602763
79 Z = -4146122
40
XDOT = 5963
970645 XDOT = 1817
818253
YDOT = -19860
084103 feet/sec YDOT = -6053
353635 meter/sec
ZDOT = -12350
843854 ZDOT = -3764
537207
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
56639483
00016717 00000-0 10270-3 0 9039
2 25544 51
6480 302
7128 0012050 310
1415 49
8680 15
52420974 17374
Satellite: ISS
Catalog Number: 25544
Epoch time: 13056
56639483 = yrday
fracday
Element set: 903
Inclination: 51
6480 deg
RA of node: 302
7128 deg
Eccentricity:
0012050
Arg of perigee: 310
1415 deg
Mean anomaly: 49
8680 deg
Mean motion: 15
52420974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 297
Coasting Arc #5 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2013/057/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4756873
55 A = 6784633
48 meter
Y = -949964
05 meter E =
0005176
Z = 4743083
12 I = 51
32308
XDOT = -1238
599452 Wp = 338
52673
YDOT = 7079
239272 meter/sec RA = 297
19667 deg
ZDOT = 2665
713195 TA = 85
04971
MA = 84
99062
Ha = 224
544 n
mi
Hp = 218
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15606540
52 X = 4744102
47
Y = -3116679
96 feet Y = -896840
48 meter
Z = 15561296
33 Z = 4766160
31
XDOT = -4063
646497 XDOT = -1330
618060
YDOT = 23225
850629 feet/sec YDOT = 7064
874321 meter/sec
ZDOT = 8745
778200 ZDOT = 2659
471848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15802599
92 X = 4816632
46
Y = -745054
40 feet Y = -227092
58 meter
Z = 15657409
57 Z = 4772378
44
XDOT = -7621
540036 XDOT = -2323
045403
YDOT = 21189
528985 feet/sec YDOT = 6458
568435 meter/sec
ZDOT = 8718
947961 ZDOT = 2657
535339
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
59634945
00016717 00000-0 10270-3 0 9042
2 25544 51
6477 297
5909 0011968 314
7854 45
2323 15
52427774 17539
Satellite: ISS
Catalog Number: 25544
Epoch time: 13057
59634945 = yrday
fracday
Element set: 904
Inclination: 51
6477 deg
RA of node: 297
5909 deg
Eccentricity:
0011968
Arg of perigee: 314
7854 deg
Mean anomaly: 45
2323 deg
Mean motion: 15
52427774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 345
Coasting Arc #6 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2013/058/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4433022
94 A = 6782816
75 meter
Y = -35680
63 meter E =
0012757
Z = -5140742
77 I = 51
30291
XDOT = 1740
235142 Wp = 24
87483
YDOT = -7319
213670 meter/sec RA = 292
19318 deg
ZDOT = -1439
803878 TA = 231
13189
MA = 231
24577
Ha = 224
703 n
mi
Hp = 218
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14544038
51 X = -4407322
44
Y = -117062
43 feet Y = -85110
47 meter
Z = -16865953
97 Z = -5162215
30
XDOT = 5709
432881 XDOT = 1828
944904
YDOT = -24013
168210 feet/sec YDOT = -7299
257456 meter/sec
ZDOT = -4723
766003 ZDOT = -1431
133620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14294729
68 X = -4357033
61
Y = -2045172
02 feet Y = -623368
43 meter
Z = -16955268
74 Z = -5167965
91
XDOT = 8744
179893 XDOT = 2665
226031
YDOT = -21989
905154 feet/sec YDOT = -6702
523091 meter/sec
ZDOT = -4686
814369 ZDOT = -1428
541020
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
56191457
00016717 00000-0 10270-3 0 9057
2 25544 51
6462 292
7892 0012103 317
7522 42
2697 15
52487354 17685
Satellite: ISS
Catalog Number: 25544
Epoch time: 13058
56191457 = yrday
fracday
Element set: 905
Inclination: 51
6462 deg
RA of node: 292
7892 deg
Eccentricity:
0012103
Arg of perigee: 317
7522 deg
Mean anomaly: 42
2697 deg
Mean motion: 15
52487354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 326
Coasting Arc #7 (Orbit 1783)
---------------------------------------
Vector Time (GMT): 2013/059/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4091279
84 A = 6782142
15 meter
Y = 1130848
94 meter E =
0010527
Z = 5293925
41 I = 51
29005
XDOT = -2172
693130 Wp = 330
78901
YDOT = 7347
052008 meter/sec RA = 287
18628 deg
ZDOT = 118
812419 TA = 118
12562
MA = 118
01919
Ha = 224
866 n
mi
Hp = 217
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13422834
11 X = 4052614
11
Y = 3710134
31 feet Y = 1176384
69 meter
Z = 17368521
69 Z = 5313706
26
XDOT = -7128
258300 XDOT = -2255
265104
YDOT = 24104
501339 feet/sec YDOT = 7322
293916 meter/sec
ZDOT = 389
804525 ZDOT = 108
056251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12792738
23 X = 3899226
61
Y = 5236717
19 feet Y = 1596151
40 meter
Z = 17450666
45 Z = 5318963
13
XDOT = -9507
162037 XDOT = -2897
782989
YDOT = 22177
301779 feet/sec YDOT = 6759
641582 meter/sec
ZDOT = 344
182554 ZDOT = 104
906842
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
59183731
00016717 00000-0 10270-3 0 9068
2 25544 51
6463 287
6674 0012048 321
4961 38
5330 15
52484974 17849
Satellite: ISS
Catalog Number: 25544
Epoch time: 13059
59183731 = yrday
fracday
Element set: 906
Inclination: 51
6463 deg
RA of node: 287
6674 deg
Eccentricity:
0012048
Arg of perigee: 321
4961 deg
Mean anomaly: 38
5330 deg
Mean motion: 15
52484974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1784
Checksum: 331
Coasting Arc #8 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2013/060/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3781167
22 A = 6782471
94 meter
Y = -2197726
96 meter E =
0010329
Z = -5188782
01 I = 51
28201
XDOT = 2520
097487 Wp = 42
39513
YDOT = -7136
377188 meter/sec RA = 282
17738 deg
ZDOT = 1195
077792 TA = 239
08555
MA = 239
18714
Ha = 224
963 n
mi
Hp = 217
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12405404
26 X = -3731105
16
Y = -7210390
29 feet Y = -2239731
03 meter
Z = -17023563
01 Z = -5207028
64
XDOT = 8268
036374 XDOT = 2593
905339
YDOT = -23413
310983 feet/sec YDOT = -7107
783053 meter/sec
ZDOT = 3920
858898 ZDOT = 1207
500231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11522911
98 X = -3512183
57
Y = -8397937
46 feet Y = -2559691
34 meter
Z = -17099199
59 Z = -5211836
04
XDOT = 9916
632983 XDOT = 3022
589733
YDOT = -21637
918294 feet/sec YDOT = -6595
237496 meter/sec
ZDOT = 3973
379419 ZDOT = 1211
086047
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
55737389
00016717 00000-0 10270-3 0 9071
2 25544 51
6448 282
8644 0012083 324
9227 35
1128 15
52535289 17998
Satellite: ISS
Catalog Number: 25544
Epoch time: 13060
55737389 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 282
8644 deg
Eccentricity:
0012083
Arg of perigee: 324
9227 deg
Mean anomaly: 35
1128 deg
Mean motion: 15
52535289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1799
Checksum: 333
Coasting Arc #9 (Orbit 1814)
---------------------------------------
Vector Time (GMT): 2013/061/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3478040
08 A = 6784035
13 meter
Y = 3284360
16 meter E =
0013869
Z = 4816028
44 I = 51
28225
XDOT = -2842
829847 Wp = 359
11351
YDOT = 6667
261615 meter/sec RA = 277
17081 deg
ZDOT = -2480
272618 TA = 115
47508
MA = 115
33154
Ha = 225
171 n
mi
Hp = 217
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11410892
65 X = 3417660
29
Y = 10775459
83 feet Y = 3322916
65 meter
Z = 15800618
24 Z = 4832777
41
XDOT = -9326
869577 XDOT = -2905
124847
YDOT = 21874
217897 feet/sec YDOT = 6635
122756 meter/sec
ZDOT = -8137
377357 ZDOT = -2494
234728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10388935
95 X = 3166547
68
Y = 11670254
70 feet Y = 3557093
63 meter
Z = 15869899
42 Z = 4837145
34
XDOT = -10192
557340 XDOT = -3106
691477
YDOT = 20279
301411 feet/sec YDOT = 6181
131070 meter/sec
ZDOT = -8196
241714 ZDOT = -2498
214475
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
58726430
00016717 00000-0 10270-3 0 9081
2 25544 51
6452 277
7426 0012153 328
2336 31
8081 15
52549275 18150
Satellite: ISS
Catalog Number: 25544
Epoch time: 13061
58726430 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 277
7426 deg
Eccentricity:
0012153
Arg of perigee: 328
2336 deg
Mean anomaly: 31
8081 deg
Mean motion: 15
52549275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1815
Checksum: 305
Coasting Arc #10 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2013/062/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3216867
02 A = 6786273
67 meter
Y = -4236639
96 meter E =
0008133
Z = -4210229
98 I = 51
28598
XDOT = 3137
439141 Wp = 13
64008
YDOT = -5979
865191 meter/sec RA = 272
16643 deg
ZDOT = 3629
384173 TA = 293
66999
MA = 293
75533
Ha = 225
237 n
mi
Hp = 217
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10554025
65 X = -3148800
85
Y = -13899737
41 feet Y = -4272232
73 meter
Z = -13813090
47 Z = -4225691
51
XDOT = 10293
435503 XDOT = 3186
443594
YDOT = -19618
980285 feet/sec YDOT = -5944
506101 meter/sec
ZDOT = 11907
428389 ZDOT = 3644
744982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9542059
55 X = -2908419
75
Y = -14552391
82 feet Y = -4435569
03 meter
Z = -13876909
52 Z = -4229682
02
XDOT = 10413
447837 XDOT = 3174
018901
YDOT = -18215
808259 feet/sec YDOT = -5552
178357 meter/sec
ZDOT = 11972
026858 ZDOT = 3649
073786
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
55277270
00016717 00000-0 10270-3 0 9093
2 25544 51
6440 272
9394 0012071 332
0654 27
9856 15
52572912 18300
Satellite: ISS
Catalog Number: 25544
Epoch time: 13062
55277270 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 272
9394 deg
Eccentricity:
0012071
Arg of perigee: 332
0654 deg
Mean anomaly: 27
9856 deg
Mean motion: 15
52572912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 307
Coasting Arc #11 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2013/063/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2952348
44 A = 6788893
68 meter
Y = 5107232
76 meter E =
0013208
Z = 3365120
69 I = 51
29535
XDOT = -3451
244324 Wp = 33
73662
YDOT = 5047
487318 meter/sec RA = 267
16813 deg
ZDOT = -4613
097871 TA = 106
84812
MA = 106
70322
Ha = 225
447 n
mi
Hp = 216
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9686182
55 X = 2878672
13
Y = 16756012
99 feet Y = 5139836
03 meter
Z = 11040422
21 Z = 3379283
57
XDOT = -11322
980064 XDOT = -3485
020878
YDOT = 16559
997764 feet/sec YDOT = 5008
704202 meter/sec
ZDOT = -15134
835535 ZDOT = -4629
945925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8804428
37 X = 2683589
77
Y = 17198166
24 feet Y = 5242001
07 meter
Z = 11098745
23 Z = 3382897
55
XDOT = -10755
475251 XDOT = -3278
268857
YDOT = 15360
126253 feet/sec YDOT = 4681
766482 meter/sec
ZDOT = -15205
510044 ZDOT = -4634
639462
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
58263052
00016717 00000-0 10270-3 0 9102
2 25544 51
6444 267
8175 0012245 335
2941 24
7623 15
52616658 18461
Satellite: ISS
Catalog Number: 25544
Epoch time: 13063
58263052 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 267
8175 deg
Eccentricity:
0012245
Arg of perigee: 335
2941 deg
Mean anomaly: 24
7623 deg
Mean motion: 15
52616658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 307
Coasting Arc #12 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2013/064/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2700986
91 A = 6791330
19 meter
Y = -5755076
82 meter E =
0015168
Z = -2362241
87 I = 51
30515
XDOT = 3787
842324 Wp = 359
46847
YDOT = -3971
810729 meter/sec RA = 262
17376 deg
ZDOT = 5360
026118 TA = 334
02696
MA = 334
10301
Ha = 225
500 n
mi
Hp = 216
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8861505
61 X = -2624956
67
Y = -18881485
62 feet Y = -5784855
97 meter
Z = -7750137
37 Z = -2375177
88
XDOT = 12427
304212 XDOT = 3805
937180
YDOT = -13030
875095 feet/sec YDOT = -3929
351228 meter/sec
ZDOT = 17585
387526 ZDOT = 5378
471068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8229707
70 X = -2508414
91
Y = -19143718
30 feet Y = -5835005
34 meter
Z = -7803292
31 Z = -2378443
50
XDOT = 11316
892368 XDOT = 3449
388794
YDOT = -12045
177178 feet/sec YDOT = -3671
370004 meter/sec
ZDOT = 17662
580255 ZDOT = 5383
554462
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
54810985
00016717 00000-0 10270-3 0 9113
2 25544 51
6436 263
0146 0012041 339
4787 20
5880 15
52616314 18611
Satellite: ISS
Catalog Number: 25544
Epoch time: 13064
54810985 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 263
0146 deg
Eccentricity:
0012041
Arg of perigee: 339
4787 deg
Mean anomaly: 20
5880 deg
Mean motion: 15
52616314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 298
Coasting Arc #13 (Orbit 1876)
---------------------------------------
Vector Time (GMT): 2013/065/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2406314
75 A = 6792877
78 meter
Y = 6239583
61 meter E =
0009279
Z = 1201981
94 I = 51
31608
XDOT = -4158
554986 Wp = 60
35021
YDOT = 2732
586343 meter/sec RA = 257
18502 deg
ZDOT = -5821
311726 TA = 106
55164
MA = 106
44969
Ha = 225
703 n
mi
Hp = 216
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7894733
42 X = 2330524
74
Y = 20471074
83 feet Y = 6266068
84 meter
Z = 3943510
31 Z = 1213486
94
XDOT = -13643
553104 XDOT = -4160
524370
YDOT = 8965
178291 feet/sec YDOT = 2686
071397 meter/sec
ZDOT = -19098
791752 ZDOT = -5841
518238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7593124
18 X = 2314384
25
Y = 20575762
78 feet Y = 6271492
50 meter
Z = 3990669
77 Z = 1216356
15
XDOT = -12144
946565 XDOT = -3701
779713
YDOT = 8226
675958 feet/sec YDOT = 2507
490832 meter/sec
ZDOT = -19183
172548 ZDOT = -5847
030993
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 13065
57793505
00016717 00000-0 10270-3 0 9126
2 25544 51
6435 257
8924 0012343 343
0920 16
9819 15
52691772 18779
Satellite: ISS
Catalog Number: 25544
Epoch time: 13065
57793505 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 257
8924 deg
Eccentricity:
0012343
Arg of perigee: 343
0920 deg
Mean anomaly: 16
9819 deg
Mean motion: 15
52691772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1877
Checksum: 329
Coasting Arc #14 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2013/066/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2069543
65 A = 6793590
56 meter
Y = -6456298
35 meter E =
0021041
Z = 4292
93 I = 51
32559
XDOT = 4569
896897 Wp = 16
55640
YDOT = -1456
070340 meter/sec RA = 252
19789 deg
ZDOT = 5992
177457 TA = 343
49007
MA = 343
55849
Ha = 225
746 n
mi
Hp = 216
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6789841
39 X = -1997214
99
Y = -21182081
18 feet Y = -6479036
87 meter
Z = 14084
42 Z = -5584
35
XDOT = 14993
100055 XDOT = 4556
731524
YDOT = -4777
133661 feet/sec YDOT = -1405
040023 meter/sec
ZDOT = 19659
374860 ZDOT = 6014
345310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6868095
31 X = -2093395
45
Y = -21156825
92 feet Y = -6448600
54 meter
Z = -26293
45 Z = -8014
24
XDOT = 13311
060922 XDOT = 4057
211369
YDOT = -4329
890055 feet/sec YDOT = -1319
750489 meter/sec
ZDOT = 19751
775393 ZDOT = 6020
341140
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 13066
54338413
00016717 00000-0 10270-3 0 9138
2 25544 51
6431 253
0896 0012014 347
1498 12
9346 15
52666483 18920
Satellite: ISS
Catalog Number: 25544
Epoch time: 13066
54338413 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 253
0896 deg
Eccentricity:
0012014
Arg of perigee: 347
1498 deg
Mean anomaly: 12
9346 deg
Mean motion: 15
52666483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 312
Coasting Arc #15 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2013/067/13:02:26
808
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1641766
54 A = 6792734
69 meter
Y = 6477022
43 meter E =
0006186
Z = -1243548
13 I = 51
33351
XDOT = -4981
606127 Wp = 36
98212
YDOT = 148
890917 meter/sec RA = 247
21203 deg
ZDOT = -5811
652566 TA = 156
57020
MA = 156
54201
Ha = 225
932 n
mi
Hp = 215
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5386373
17 X = 1575257
77
Y = 21250073
57 feet Y = 6495009
70 meter
Z = -4079882
32 Z = -1235734
93
XDOT = -16343
852124 XDOT = -4954
669957
YDOT = 488
487260 feet/sec YDOT = 93
333496 meter/sec
ZDOT = -19067
101595 ZDOT = -5835
786848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5854347
84 X = 1784405
22
Y = 21132054
90 feet Y = 6441050
33 meter
Z = -4048079
74 Z = -1233854
70
XDOT = -14671
280299 XDOT = -4471
806235
YDOT = 399
244761 feet/sec YDOT = 121
689803 meter/sec
ZDOT = -19167
544923 ZDOT = -5842
267692
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 13067
57317691
00016717 00000-0 10270-3 0 9148
2 25544 51
6429 247
9669 0012257 351
3461 8
7478 15
52733335 19081
Satellite: ISS
Catalog Number: 25544
Epoch time: 13067
57317691 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 247
9669 deg
Eccentricity:
0012257
Arg of perigee: 351
3461 deg
Mean anomaly: 8
7478 deg
Mean motion: 15
52733335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 333
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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