[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 12th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
137/02:03:18
747 -2
8 4
8 4
9
N/A -3
4 -0
5 225
4
000/00:14:33
494 -2
1 0
2 223
4
Coasting Arc #1 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2013/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -539765
68 A = 6795505
80 meter
Y = 6242402
64 meter E =
0008354
Z = 2621278
53 I = 51
33399
XDOT = -5358
187836 Wp = 99
64385
YDOT = 1725
305290 meter/sec RA = 294
49973 deg
ZDOT = -5199
208046 TA = 50
73328
MA = 50
65920
Ha = 224
376 n
mi
Hp = 221
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1770884
76 X = -622263
17
Y = 20480323
63 feet Y = 6235905
26 meter
Z = 8599995
18 Z = 2618456
22
XDOT = -17579
356418 XDOT = -5351
825477
YDOT = 5660
450425 feet/sec YDOT = 1665
422453 meter/sec
ZDOT = -17057
769180 ZDOT = -5225
222642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13904065
39 X = 4237959
13
Y = 15148396
27 feet Y = 4617231
18 meter
Z = 8587354
77 Z = 2617425
73
XDOT = -6488
153444 XDOT = -1977
589170
YDOT = 15710
461227 feet/sec YDOT = 4788
548582 meter/sec
ZDOT = -17166
455581 ZDOT = -5232
335661
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 13130
53750329
00016717 00000-0 10270-3 0 9009
2 25544 51
6442 295
0274 0005257 288
0073 72
0505 15
51013869 28862
Satellite: ISS
Catalog Number: 25544
Epoch time: 13130
53750329 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 295
0274 deg
Eccentricity:
0005257
Arg of perigee: 288
0073 deg
Mean anomaly: 72
0505 deg
Mean motion: 15
51013869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 295
Coasting Arc #2 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2013/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 581438
58 A = 6796640
44 meter
Y = -6461033
89 meter E =
0007001
Z = -2012495
82 I = 51
32734
XDOT = 5147
214218 Wp = 356
67129
YDOT = -1259
258016 meter/sec RA = 289
51904 deg
ZDOT = 5535
782195 TA = 341
02510
MA = 341
05117
Ha = 224
475 n
mi
Hp = 221
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1907606
88 X = 663420
37
Y = -21197617
76 feet Y = -6454073
38 meter
Z = -6602676
57 Z = -2009472
42
XDOT = 16887
185756 XDOT = 5134
021130
YDOT = -4131
423936 feet/sec YDOT = -1201
772703 meter/sec
ZDOT = 18162
015076 ZDOT = 5560
755243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14618483
40 X = -4455713
74
Y = -15474368
39 feet Y = -4716587
48 meter
Z = -6589170
42 Z = -2008379
14
XDOT = 6860
933402 XDOT = 2091
212501
YDOT = -14251
226405 feet/sec YDOT = -4343
773808 meter/sec
ZDOT = 18266
296506 ZDOT = 5567
567175
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 13131
50396733
00016717 00000-0 10270-3 0 9013
2 25544 51
6454 290
2317 0005079 291
5783 68
4827 15
51031536 29014
Satellite: ISS
Catalog Number: 25544
Epoch time: 13131
50396733 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 290
2317 deg
Eccentricity:
0005079
Arg of perigee: 291
5783 deg
Mean anomaly: 68
4827 deg
Mean motion: 15
51031536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 301
Coasting Arc #3 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2013/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -605637
47 A = 6797491
66 meter
Y = 6630733
97 meter E =
0008567
Z = 1346983
08 I = 51
32058
XDOT = -4972
355776 Wp = 122
48069
YDOT = 725
515497 meter/sec RA = 284
53912 deg
ZDOT = -5784
676338 TA = 42
80519
MA = 42
73851
Ha = 224
609 n
mi
Hp = 221
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1986999
58 X = -686282
13
Y = 21754376
53 feet Y = 6623510
35 meter
Z = 4419235
83 Z = 1343845
45
XDOT = -16313
503201 XDOT = -4951
998250
YDOT = 2380
300187 feet/sec YDOT = 670
025686 meter/sec
ZDOT = -18978
596908 ZDOT = -5808
782483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15263710
90 X = 4652379
08
Y = 15631498
66 feet Y = 4764480
79 meter
Z = 4405234
41 Z = 1342715
45
XDOT = -7543
548581 XDOT = -2299
273607
YDOT = 12763
769041 feet/sec YDOT = 3890
396804 meter/sec
ZDOT = -19079
193336 ZDOT = -5815
338129
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 13132
53484779
00016717 00000-0 10270-3 0 9026
2 25544 51
6448 285
1164 0005233 296
2308 63
8305 15
51063569 29175
Satellite: ISS
Catalog Number: 25544
Epoch time: 13132
53484779 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 285
1164 deg
Eccentricity:
0005233
Arg of perigee: 296
2308 deg
Mean anomaly: 63
8305 deg
Mean motion: 15
51063569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 315
Coasting Arc #4 (Orbit 2931)
---------------------------------------
Vector Time (GMT): 2013/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 589968
23 A = 6798038
18 meter
Y = -6732184
78 meter E =
0010887
Z = -669779
78 I = 51
31731
XDOT = 4846
967654 Wp = 13
03721
YDOT = -162
882001 meter/sec RA = 279
55961 deg
ZDOT = 5935
900661 TA = 339
70444
MA = 339
74768
Ha = 224
699 n
mi
Hp = 221
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1935591
30 X = 668458
77
Y = -22087220
42 feet Y = -6725148
47 meter
Z = -2197440
22 Z = -666723
54
XDOT = 15902
124850 XDOT = 4819
593423
YDOT = -534
389768 feet/sec YDOT = -108
833621 meter/sec
ZDOT = 19474
739701 ZDOT = 5959
380599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15828728
38 X = -4824596
41
Y = -15527493
93 feet Y = -4732780
15 meter
Z = -2183770
35 Z = -665613
20
XDOT = 8474
346806 XDOT = 2582
980906
YDOT = -11377
813716 feet/sec YDOT = -3467
957621 meter/sec
ZDOT = 19572
651941 ZDOT = 5965
744312
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 13133
50128746
00016717 00000-0 10270-3 0 9034
2 25544 51
6464 280
3212 0005090 299
8449 60
2196 15
51073032 29322
Satellite: ISS
Catalog Number: 25544
Epoch time: 13133
50128746 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 280
3212 deg
Eccentricity:
0005090
Arg of perigee: 299
8449 deg
Mean anomaly: 60
2196 deg
Mean motion: 15
51073032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2932
Checksum: 290
Coasting Arc #5 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2013/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -577518
43 A = 6798116
20 meter
Y = 6769681
48 meter E =
0006907
Z = -43835
99 I = 51
31308
XDOT = -4768
668653 Wp = 142
53298
YDOT = -442
272899 meter/sec RA = 274
58005 deg
ZDOT = -5980
142841 TA = 37
94060
MA = 37
89196
Ha = 224
858 n
mi
Hp = 220
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1894745
51 X = -652962
60
Y = 22210241
09 feet Y = 6762801
48 meter
Z = -143818
88 Z = -46824
36
XDOT = -15645
238363 XDOT = -4734
318425
YDOT = -1451
026570 feet/sec YDOT = -495
406697 meter/sec
ZDOT = -19619
891209 ZDOT = -6003
225440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16224095
09 X = 4945104
18
Y = 15285927
49 feet Y = 4659150
70 meter
Z = -157202
99 Z = -47915
47
XDOT = -9670
293327 XDOT = -2947
505406
YDOT = 10076
597552 feet/sec YDOT = 3071
346934 meter/sec
ZDOT = -19716
069138 ZDOT = -6009
457873
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 13134
53214206
00016717 00000-0 10270-3 0 9046
2 25544 51
6457 275
2059 0005232 304
6748 55
3909 15
51109323 29488
Satellite: ISS
Catalog Number: 25544
Epoch time: 13134
53214206 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 275
2059 deg
Eccentricity:
0005232
Arg of perigee: 304
6748 deg
Mean anomaly: 55
3909 deg
Mean motion: 15
51109323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 298
Coasting Arc #6 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2013/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 549714
96 A = 6797850
07 meter
Y = -6726298
64 meter E =
0012925
Z = 745011
32 I = 51
31216
XDOT = 4751
721262 Wp = 30
42101
YDOT = 1048
332655 meter/sec RA = 269
60045 deg
ZDOT = 5924
425378 TA = 337
66002
MA = 337
71626
Ha = 224
917 n
mi
Hp = 220
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1803526
77 X = 621269
93
Y = -22067908
94 feet Y = -6719751
34 meter
Z = 2444262
87 Z = 747855
22
XDOT = 15589
636687 XDOT = 4710
865925
YDOT = 3439
411599 feet/sec YDOT = 1101
240611 meter/sec
ZDOT = 19437
091136 ZDOT = 5947
409834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16435565
04 X = -5009560
22
Y = -14834248
98 feet Y = -4521479
09 meter
Z = 2457029
47 Z = 748902
58
XDOT = 11053
685191 XDOT = 3369
163246
YDOT = -8993
107898 feet/sec YDOT = -2741
099287 meter/sec
ZDOT = 19532
783811 ZDOT = 5953
592505
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 13135
56298360
00016717 00000-0 10270-3 0 9054
2 25544 51
6471 270
0910 0005146 308
3420 51
7269 15
51121964 29647
Satellite: ISS
Catalog Number: 25544
Epoch time: 13135
56298360 = yrday
fracday
Element set: 905
Inclination: 51
6471 deg
RA of node: 270
0910 deg
Eccentricity:
0005146
Arg of perigee: 308
3420 deg
Mean anomaly: 51
7269 deg
Mean motion: 15
51121964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 295
Coasting Arc #7 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2013/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -549169
47 A = 6797111
80 meter
Y = 6614515
13 meter E =
0003329
Z = -1457105
27 I = 51
31055
XDOT = -4781
086091 Wp = 157
75550
YDOT = -1661
809267 meter/sec RA = 264
62010 deg
ZDOT = -5749
169727 TA = 38
18951
MA = 38
16593
Ha = 225
102 n
mi
Hp = 220
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1801737
10 X = -616015
31
Y = 21701165
13 feet Y = 6608000
29 meter
Z = -4780529
10 Z = -1459935
14
XDOT = -15685
977989 XDOT = -4734
219927
YDOT = -5452
130140 feet/sec YDOT = -1715
012057 meter/sec
ZDOT = -18862
105404 ZDOT = -5772
282229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16402799
28 X = 4999573
22
Y = 14318295
13 feet Y = 4364216
35 meter
Z = -4793212
23 Z = -1460971
09
XDOT = -12592
501907 XDOT = -3838
194581
YDOT = 8087
318206 feet/sec YDOT = 2465
014589 meter/sec
ZDOT = -18958
256779 ZDOT = -5778
476666
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 13136
52938500
00016717 00000-0 10270-3 0 9069
2 25544 51
6465 265
2955 0005260 312
7650 47
3058 15
51144574 29791
Satellite: ISS
Catalog Number: 25544
Epoch time: 13136
52938500 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 265
2955 deg
Eccentricity:
0005260
Arg of perigee: 312
7650 deg
Mean anomaly: 47
3058 deg
Mean motion: 15
51144574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2979
Checksum: 314
Coasting Arc #8 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2013/137/02:10:35
494
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3861287
02 A = 6789524
83 meter
Y = 2162758
68 meter E =
0008063
Z = -5155709
85 I = 51
27830
XDOT = -2179
498685 Wp = 58
63273
YDOT = -7206
956553 meter/sec RA = 261
67616 deg
ZDOT = -1388
426915 TA = 197
91248
MA = 197
94092
Ha = 225
394 n
mi
Hp = 223
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12668264
50 X = -3860139
25
Y = 7095664
97 feet Y = 2119585
98 meter
Z = -16915058
57 Z = -5174464
89
XDOT = -7150
586236 XDOT = -2092
002310
YDOT = -23644
870580 feet/sec YDOT = -7230
839802 meter/sec
ZDOT = -4555
206415 ZDOT = -1398
802583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6377580
07 X = -1943886
40
Y = -12942112
47 feet Y = -3944755
88 meter
Z = -16993551
44 Z = -5179634
48
XDOT = 23064
152360 XDOT = 7029
953639
YDOT = -5318
016845 feet/sec YDOT = -1620
931534 meter/sec
ZDOT = -4597
516169 ZDOT = -1401
322928
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 13137
10922875
00016717 00000-0 10270-3 0 9073
2 25544 51
6470 262
4218 0006904 283
8363 76
2019 15
50179780 29887
Satellite: ISS
Catalog Number: 25544
Epoch time: 13137
10922875 = yrday
fracday
Element set: 907
Inclination: 51
6470 deg
RA of node: 262
4218 deg
Eccentricity:
0006904
Arg of perigee: 283
8363 deg
Mean anomaly: 76
2019 deg
Mean motion: 15
50179780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2988
Checksum: 324
Coasting Arc #9 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2013/138/02:10:35
494
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3835790
62 A = 6789100
16 meter
Y = -2007626
55 meter E =
0003731
Z = 5232741
12 I = 51
28216
XDOT = 2476
406002 Wp = 273
64144
YDOT = 7186
633199 meter/sec RA = 256
69315 deg
ZDOT = 942
789462 TA = 167
28663
MA = 167
27722
Ha = 225
533 n
mi
Hp = 223
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12584614
90 X = 3832535
80
Y = -6586701
27 feet Y = -1964750
68 meter
Z = 17167785
82 Z = 5251367
22
XDOT = 8124
691609 XDOT = 2391
279618
YDOT = 23578
192909 feet/sec YDOT = 7213
849934 meter/sec
ZDOT = 3093
141280 ZDOT = 954
613174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6093984
31 X = 1857446
42
Y = 12725505
93 feet Y = 3878734
21 meter
Z = 17245720
91 Z = 5256495
73
XDOT = -22948
504167 XDOT = -6994
704070
YDOT = 6735
785968 feet/sec YDOT = 2053
067563 meter/sec
ZDOT = 3141
505613 ZDOT = 957
530911
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 13138
14068924
00016717 00000-0 10270-3 0 9085
2 25544 51
6467 257
3104 0007041 287
3129 72
7251 15
50204948 30046
Satellite: ISS
Catalog Number: 25544
Epoch time: 13138
14068924 = yrday
fracday
Element set: 908
Inclination: 51
6467 deg
RA of node: 257
3104 deg
Eccentricity:
0007041
Arg of perigee: 287
3129 deg
Mean anomaly: 72
7251 deg
Mean motion: 15
50204948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 295
Coasting Arc #10 (Orbit 3018)
---------------------------------------
Vector Time (GMT): 2013/139/02:10:35
494
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3846116
64 A = 6788843
40 meter
Y = 1857950
30 meter E =
0008947
Z = -5284101
76 I = 51
28995
XDOT = -2766
019493 Wp = 66
13288
YDOT = -7122
208173 meter/sec RA = 251
71009 deg
ZDOT = -488
064561 TA = 199
16423
MA = 199
19791
Ha = 225
817 n
mi
Hp = 223
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12618492
93 X = -3840937
79
Y = 6095637
46 feet Y = 1814969
67 meter
Z = -17336291
86 Z = -5302773
42
XDOT = -9074
867104 XDOT = -2683
800941
YDOT = -23366
824715 feet/sec YDOT = -7152
679827 meter/sec
ZDOT = -1601
261683 ZDOT = -501
302224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5820303
02 X = -1774028
36
Y = -12640925
26 feet Y = -3852954
02 meter
Z = -17414397
97 Z = -5307908
50
XDOT = 22637
101844 XDOT = 6899
788642
YDOT = -8129
143386 feet/sec YDOT = -2477
762904 meter/sec
ZDOT = -1655
543447 ZDOT = -504
609643
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 13139
10767315
00016717 00000-0 10270-3 0 9093
2 25544 51
6472 252
5184 0007019 292
0975 67
9431 15
50219035 30199
Satellite: ISS
Catalog Number: 25544
Epoch time: 13139
10767315 = yrday
fracday
Element set: 909
Inclination: 51
6472 deg
RA of node: 252
5184 deg
Eccentricity:
0007019
Arg of perigee: 292
0975 deg
Mean anomaly: 67
9431 deg
Mean motion: 15
50219035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3019
Checksum: 306
Coasting Arc #11 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2013/140/02:10:35
494
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3893413
44 A = 6788677
39 meter
Y = -1694785
50 meter E =
0005032
Z = 5300209
60 I = 51
30014
XDOT = 3039
686112 Wp = 306
82384
YDOT = 7030
527388 meter/sec RA = 246
72731 deg
ZDOT = 18
156297 TA = 143
01949
MA = 142
98479
Ha = 225
958 n
mi
Hp = 223
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12773666
15 X = 3886328
20
Y = -5560319
88 feet Y = -1651286
61 meter
Z = 17389139
10 Z = 5319106
46
XDOT = 9972
723464 XDOT = 2960
755124
YDOT = 23066
034739 feet/sec YDOT = 7064
077747 meter/sec
ZDOT = 59
567902 ZDOT = 32
731419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5500855
54 X = 1676660
77
Y = 12691322
95 feet Y = 3868315
23 meter
Z = 17468164
55 Z = 5324296
55
XDOT = -22186
066592 XDOT = -6762
313097
YDOT = 9465
153179 feet/sec YDOT = 2884
978689 meter/sec
ZDOT = 119
450138 ZDOT = 36
408402
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 13140
13910881
00016717 00000-0 10270-3 0 9108
2 25544 51
6472 247
4067 0007145 295
6698 64
3714 15
50245999 30354
Satellite: ISS
Catalog Number: 25544
Epoch time: 13140
13910881 = yrday
fracday
Element set: 910
Inclination: 51
6472 deg
RA of node: 247
4067 deg
Eccentricity:
0007145
Arg of perigee: 295
6698 deg
Mean anomaly: 64
3714 deg
Mean motion: 15
50245999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 316
Coasting Arc #12 (Orbit 3049)
---------------------------------------
Vector Time (GMT): 2013/141/02:10:35
494
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3972182
38 A = 6788711
26 meter
Y = 1554547
57 meter E =
0008944
Z = -5288501
52 I = 51
31369
XDOT = -3295
558530 Wp = 72
38163
YDOT = -6895
888731 meter/sec RA = 241
74519 deg
ZDOT = 451
539208 TA = 201
93232
MA = 201
97063
Ha = 226
183 n
mi
Hp = 222
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13032094
43 X = -3963579
90
Y = 5100221
67 feet Y = 1510176
33 meter
Z = -17350726
78 Z = -5307777
43
XDOT = -10812
199902 XDOT = -3220
395775
YDOT = -22624
306859 feet/sec YDOT = -6932
321496 meter/sec
ZDOT = 1481
427847 ZDOT = 435
711828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5261551
41 X = -1603720
87
Y = -12859265
82 feet Y = -3919504
22 meter
Z = -17431317
38 Z = -5313065
54
XDOT = 21548
167585 XDOT = 6567
881480
YDOT = -10722
034443 feet/sec YDOT = -3268
076098 meter/sec
ZDOT = 1416
296817 ZDOT = 431
687270
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 13141
10606968
00016717 00000-0 10270-3 0 9115
2 25544 51
6475 242
6144 0007179 300
1231 59
9208 15
50255864 30509
Satellite: ISS
Catalog Number: 25544
Epoch time: 13141
10606968 = yrday
fracday
Element set: 911
Inclination: 51
6475 deg
RA of node: 242
6144 deg
Eccentricity:
0007179
Arg of perigee: 300
1231 deg
Mean anomaly: 59
9208 deg
Mean motion: 15
50255864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3050
Checksum: 288
Coasting Arc #13 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2013/142/02:10:35
494
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4089030
37 A = 6788837
17 meter
Y = -1406639
93 meter E =
0006583
Z = 5236982
09 I = 51
33000
XDOT = 3521
098483 Wp = 332
04618
YDOT = 6737
700291 meter/sec RA = 236
76412 deg
ZDOT = -934
314944 TA = 126
97238
MA = 126
91210
Ha = 226
320 n
mi
Hp = 222
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13415453
97 X = 4079015
45
Y = -4614960
40 feet Y = -1360970
00 meter
Z = 17181699
78 Z = 5256822
26
XDOT = 11552
160378 XDOT = 3450
033111
YDOT = 22105
315914 feet/sec YDOT = 6776
678119 meter/sec
ZDOT = -3065
337742 ZDOT = -917
381789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5008393
12 X = 1526558
22
Y = 13165548
24 feet Y = 4012859
10 meter
Z = 17264628
87 Z = 5262258
88
XDOT = -20790
240076 XDOT = -6336
865175
YDOT = 11859
563889 feet/sec YDOT = 3614
795073 meter/sec
ZDOT = -2995
567423 ZDOT = -913
048950
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 13142
13748122
00016717 00000-0 10270-3 0 9129
2 25544 51
6478 237
5028 0007285 303
7938 56
2518 15
50286399 30665
Satellite: ISS
Catalog Number: 25544
Epoch time: 13142
13748122 = yrday
fracday
Element set: 912
Inclination: 51
6478 deg
RA of node: 237
5028 deg
Eccentricity:
0007285
Arg of perigee: 303
7938 deg
Mean anomaly: 56
2518 deg
Mean motion: 15
50286399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 318
Coasting Arc #14 (Orbit 3080)
---------------------------------------
Vector Time (GMT): 2013/143/02:10:35
494
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4227987
37 A = 6789181
79 meter
Y = 1297769
23 meter E =
0008068
Z = -5157415
92 I = 51
34854
XDOT = -3719
814107 Wp = 76
16637
YDOT = -6543
018060 meter/sec RA = 231
78406 deg
ZDOT = 1406
778311 TA = 207
41927
MA = 207
46186
Ha = 226
508 n
mi
Hp = 222
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13871349
64 X = -4217131
17
Y = 4257773
07 feet Y = 1250550
22 meter
Z = -16920655
91 Z = -5177929
12
XDOT = -12204
114525 XDOT = -3653
206105
YDOT = -21466
594684 feet/sec YDOT = -6584
243024 meter/sec
ZDOT = 4615
414405 ZDOT = 1388
868780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4898843
14 X = -1493167
39
Y = -13551228
52 feet Y = -4130414
45 meter
Z = -17006384
40 Z = -5183545
96
XDOT = 19879
387630 XDOT = 6059
237350
YDOT = -12870
640862 feet/sec YDOT = -3922
971335 meter/sec
ZDOT = 4541
540403 ZDOT = 1384
261515
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 13143
10441987
00016717 00000-0 10270-3 0 9137
2 25544 51
6475 232
7104 0007340 307
8550 52
1936 15
50289935 30816
Satellite: ISS
Catalog Number: 25544
Epoch time: 13143
10441987 = yrday
fracday
Element set: 913
Inclination: 51
6475 deg
RA of node: 232
7104 deg
Eccentricity:
0007340
Arg of perigee: 307
8550 deg
Mean anomaly: 52
1936 deg
Mean motion: 15
50289935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3081
Checksum: 297
Coasting Arc #15 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2013/144/02:10:35
494
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4403145
29 A = 6789607
04 meter
Y = -1186733
10 meter E =
0008120
Z = 5033323
24 I = 51
37009
XDOT = 3874
250995 Wp = 353
43485
YDOT = 6331
676108 meter/sec RA = 226
80595 deg
ZDOT = -1888
729489 TA = 115
00769
MA = 114
92334
Ha = 226
650 n
mi
Hp = 222
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14446014
72 X = 4391637
27
Y = -3893481
31 feet Y = -1137559
15 meter
Z = 16513527
68 Z = 5054685
74
XDOT = 12710
797228 XDOT = 3812
336025
YDOT = 20773
215577 feet/sec YDOT = 6374
654405 meter/sec
ZDOT = -6196
619058 ZDOT = -1870
058137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4804743
96 X = 1464485
96
Y = 14064310
25 feet Y = 4286801
76 meter
Z = 16602793
35 Z = 5060531
41
XDOT = -18886
132136 XDOT = -5756
493075
YDOT = 13705
369660 feet/sec YDOT = 4177
396672 meter/sec
ZDOT = -6119
533168 ZDOT = -1865
233710
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 13144
13580796
00016717 00000-0 10270-3 0 9144
2 25544 51
6476 227
5989 0007441 311
5743 48
4769 15
50324111 30973
Satellite: ISS
Catalog Number: 25544
Epoch time: 13144
13580796 = yrday
fracday
Element set: 914
Inclination: 51
6476 deg
RA of node: 227
5989 deg
Eccentricity:
0007441
Arg of perigee: 311
5743 deg
Mean anomaly: 48
4769 deg
Mean motion: 15
50324111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 321
Coasting Arc #16 (Orbit 3111)
---------------------------------------
Vector Time (GMT): 2013/145/02:10:35
494
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4586743
92 A = 6790244
11 meter
Y = 1127594
26 meter E =
0006539
Z = -4883098
81 I = 51
39269
XDOT = -3995
974546 Wp = 74
20708
YDOT = -6095
097139 meter/sec RA = 221
82876 deg
ZDOT = 2350
369754 TA = 218
89615
MA = 218
94322
Ha = 226
802 n
mi
Hp = 222
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15048372
46 X = -4575290
80
Y = 3699456
24 feet Y = 1076367
00 meter
Z = -16020665
40 Z = -4905353
29
XDOT = -13110
152710 XDOT = -3938
938544
YDOT = -19997
037859 feet/sec YDOT = -6139
464008 meter/sec
ZDOT = 7711
186856 ZDOT = 2331
095135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4901847
46 X = -1494083
11
Y = -14598739
67 feet Y = -4449695
85 meter
Z = -16113655
75 Z = -4911442
27
XDOT = 17795
471203 XDOT = 5424
059623
YDOT = -14382
934755 feet/sec YDOT = -4383
918513 meter/sec
ZDOT = 7631
544749 ZDOT = 2326
094840
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 13145
10272504
00016717 00000-0 10270-3 0 9158
2 25544 51
6465 222
8061 0007463 315
3445 44
7104 15
50321361 31129
Satellite: ISS
Catalog Number: 25544
Epoch time: 13145
10272504 = yrday
fracday
Element set: 915
Inclination: 51
6465 deg
RA of node: 222
8061 deg
Eccentricity:
0007463
Arg of perigee: 315
3445 deg
Mean anomaly: 44
7104 deg
Mean motion: 15
50321361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3112
Checksum: 261
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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