[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 24th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9956 62 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
091/21:57:19
520 -1
5 3
1 3
1
N/A -1
3 0
0 214
3
000/00:06:39
040 2
4 -0
0 207
8
Coasting Arc #1 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2012/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6399654
55 A = 6772184
27 meter
Y = 651091
52 meter E =
0024707
Z = 2063566
51 I = 51
52830
XDOT = 1262
946859 Wp = 150
05320
YDOT = 5179
233798 meter/sec RA = 200
57759 deg
ZDOT = -5543
321337 TA = 6
98243
MA = 6
94807
Ha = 217
066 n
mi
Hp = 203
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20996241
95 X = 6381874
01
Y = 2136127
04 feet Y = 722557
29 meter
Z = 6770231
33 Z = 2094612
21
XDOT = 4143
526439 XDOT = 1231
865751
YDOT = 16992
236870 feet/sec YDOT = 5193
182294 meter/sec
ZDOT = -18186
749792 ZDOT = -5537
262263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20896610
52 X = 6369286
89
Y = 2645084
20 feet Y = 806221
66 meter
Z = 6897568
09 Z = 2102378
75
XDOT = 4032
692116 XDOT = 1229
164557
YDOT = 15565
783044 feet/sec YDOT = 4744
450672 meter/sec
ZDOT = -18162
176076 ZDOT = -5535
831268
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 12081
53622661
00016717 00000-0 10270-3 0 9000
2 25544 51
6407 201
4687 0016503 182
2412 177
8673 15
59393675 4352
Satellite: ISS
Catalog Number: 25544
Epoch time: 12081
53622661 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 201
4687 deg
Eccentricity:
0016503
Arg of perigee: 182
2412 deg
Mean anomaly: 177
8673 deg
Mean motion: 15
59393675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 435
Checksum: 306
Coasting Arc #2 (Orbit 450)
---------------------------------------
Vector Time (GMT): 2012/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6033682
30 A = 6773184
33 meter
Y = -2782774
87 meter E =
0013759
Z = 1336148
32 I = 51
56188
XDOT = 3105
582435 Wp = 132
20548
YDOT = -3921
234034 meter/sec RA = 195
57573 deg
ZDOT = 5809
838232 TA = 242
37214
MA = 242
51190
Ha = 216
872 n
mi
Hp = 204
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19795545
60 X = -6008607
00
Y = -9129838
80 feet Y = -2850106
84 meter
Z = 4383688
73 Z = 1306898
37
XDOT = 10188
918751 XDOT = 3120
976868
YDOT = -12864
941058 feet/sec YDOT = -3886
418609 meter/sec
ZDOT = 19061
149055 ZDOT = 5824
962891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19756492
47 X = -6021778
91
Y = -9270117
40 feet Y = -2825531
78 meter
Z = 4263828
99 Z = 1299615
07
XDOT = 9488
007455 XDOT = 2891
944672
YDOT = -11351
369913 feet/sec YDOT = -3459
897549 meter/sec
ZDOT = 19123
420025 ZDOT = 5828
818424
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 12082
56155768
00016717 00000-0 10270-3 0 9014
2 25544 51
6416 196
3162 0016304 185
9875 174
1088 15
59448325 4515
Satellite: ISS
Catalog Number: 25544
Epoch time: 12082
56155768 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 196
3162 deg
Eccentricity:
0016304
Arg of perigee: 185
9875 deg
Mean anomaly: 174
1088 deg
Mean motion: 15
59448325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 451
Checksum: 323
Coasting Arc #3 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2012/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3419275
77 A = 6766369
41 meter
Y = 4037671
98 meter E =
0014131
Z = -4212897
16 I = 51
56892
XDOT = -6527
560981 Wp = 161
07749
YDOT = 1732
592786 meter/sec RA = 190
55764 deg
ZDOT = -3653
896482 TA = 71
59389
MA = 71
44030
Ha = 216
719 n
mi
Hp = 204
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11218096
35 X = 3394336
88
Y = 13246955
31 feet Y = 4075768
44 meter
Z = -13821841
08 Z = -4196347
58
XDOT = -21415
882483 XDOT = -6528
700227
YDOT = 5684
359535 feet/sec YDOT = 1659
590711 meter/sec
ZDOT = -11987
849350 ZDOT = -3685
610078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11435104
42 X = 3485419
83
Y = 13131351
55 feet Y = 4002435
95 meter
Z = -13754155
55 Z = -4192266
61
XDOT = -20326
589361 XDOT = -6195
544437
YDOT = 5065
128519 feet/sec YDOT = 1543
851173 meter/sec
ZDOT = -12118
072991 ZDOT = -3693
588648
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 12083
52278884
00016717 00000-0 10270-3 0 9027
2 25544 51
6417 191
4861 0016285 189
9984 170
0850 15
59456216 4667
Satellite: ISS
Catalog Number: 25544
Epoch time: 12083
52278884 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 191
4861 deg
Eccentricity:
0016285
Arg of perigee: 189
9984 deg
Mean anomaly: 170
0850 deg
Mean motion: 15
59456216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 338
Coasting Arc #4 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2012/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 427535
58 A = 6761655
46 meter
Y = -4180278
94 meter E =
0015753
Z = 5298657
92 I = 51
58441
XDOT = 7638
901608 Wp = 185
59963
YDOT = 761
051359 meter/sec RA = 185
50416 deg
ZDOT = -31
315185 TA = 264
60880
MA = 264
78854
Ha = 216
343 n
mi
Hp = 204
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1402675
79 X = 448508
75
Y = -13714825
92 feet Y = -4175380
07 meter
Z = 17384048
31 Z = 5300786
33
XDOT = 25062
013150 XDOT = 7629
975757
YDOT = 2496
887660 feet/sec YDOT = 846
424367 meter/sec
ZDOT = -102
740108 ZDOT = 5
772601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 922140
56 X = 281068
44
Y = -13744156
37 feet Y = -4189218
86 meter
Z = 17393013
19 Z = 5301390
42
XDOT = 24118
759877 XDOT = 7351
398010
YDOT = 1744
508433 feet/sec YDOT = 531
726170 meter/sec
ZDOT = 49
408944 ZDOT = 15
059846
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 12084
54808157
00016717 00000-0 10270-3 0 9033
2 25544 51
6420 186
3337 0016104 193
8802 166
1912 15
59533256 4828
Satellite: ISS
Catalog Number: 25544
Epoch time: 12084
54808157 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 186
3337 deg
Eccentricity:
0016104
Arg of perigee: 193
8802 deg
Mean anomaly: 166
1912 deg
Mean motion: 15
59533256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 305
Coasting Arc #5 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2012/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4243754
14 A = 6766185
40 meter
Y = 3257736
61 meter E =
0018177
Z = -4156869
71 I = 51
62994
XDOT = -5981
037502 Wp = 172
03530
YDOT = -3004
867008 meter/sec RA = 180
45263 deg
ZDOT = 3735
475235 TA = 136
46786
MA = 136
32426
Ha = 216
119 n
mi
Hp = 204
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13923077
90 X = -4259674
16
Y = 10688112
23 feet Y = 3210190
88 meter
Z = -13638023
99 Z = -4177524
80
XDOT = -19622
826451 XDOT = -5965
138140
YDOT = -9858
487560 feet/sec YDOT = -3071
661377 meter/sec
ZDOT = 12255
496177 ZDOT = 3706
458408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13350751
29 X = -4069308
99
Y = 11292520
77 feet Y = 3441960
33 meter
Z = -13722971
77 Z = -4182761
79
XDOT = -19292
552944 XDOT = -5880
370137
YDOT = -7998
154486 feet/sec YDOT = -2437
837487 meter/sec
ZDOT = 12136
582676 ZDOT = 3699
230400
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 12085
50927787
00016717 00000-0 10270-3 0 9042
2 25544 51
6416 181
5036 0016041 197
2474 162
8138 15
59544943 4973
Satellite: ISS
Catalog Number: 25544
Epoch time: 12085
50927787 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 181
5036 deg
Eccentricity:
0016041
Arg of perigee: 197
2474 deg
Mean anomaly: 162
8138 deg
Mean motion: 15
59544943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 329
Coasting Arc #6 (Orbit 512)
---------------------------------------
Vector Time (GMT): 2012/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6471257
82 A = 6772958
98 meter
Y = -1499248
96 meter E =
0022900
Z = 1240277
25 I = 51
68217
XDOT = 2161
998111 Wp = 164
69931
YDOT = 4477
358334 meter/sec RA = 175
44105 deg
ZDOT = -5865
222346 TA = 1
77180
MA = 1
76370
Ha = 215
909 n
mi
Hp = 204
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21231160
82 X = 6481516
74
Y = -4918795
80 feet Y = -1426825
88 meter
Z = 4069151
07 Z = 1271739
56
XDOT = 7093
169655 XDOT = 2140
262799
YDOT = 14689
495847 feet/sec YDOT = 4501
413084 meter/sec
ZDOT = -19242
855465 ZDOT = -5854
772587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20862356
96 X = 6358846
40
Y = -6216954
55 feet Y = -1894927
75 meter
Z = 4198365
22 Z = 1279661
72
XDOT = 7648
720060 XDOT = 2331
329874
YDOT = 12694
524363 feet/sec YDOT = 3869
291026 meter/sec
ZDOT = -19200
220520 ZDOT = -5852
227214
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 12086
53453494
00016717 00000-0 10270-3 0 9056
2 25544 51
6408 176
3513 0015974 200
8137 159
2370 15
59538388 5130
Satellite: ISS
Catalog Number: 25544
Epoch time: 12086
53453494 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 176
3513 deg
Eccentricity:
0015974
Arg of perigee: 200
8137 deg
Mean anomaly: 159
2370 deg
Mean motion: 15
59538388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 513
Checksum: 320
Coasting Arc #7 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2012/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6366419
66 A = 6771475
27 meter
Y = -699161
62 meter E =
0011742
Z = 2211335
72 I = 51
70811
XDOT = 2434
252668 Wp = 146
73679
YDOT = -4789
450965 meter/sec RA = 170
44827 deg
ZDOT = 5470
539988 TA = 237
83421
MA = 237
94817
Ha = 215
642 n
mi
Hp = 205
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20887203
61 X = -6368870
55
Y = -2293837
34 feet Y = -770368
40 meter
Z = 7255038
44 Z = 2180401
87
XDOT = 7986
393267 XDOT = 2461
053562
YDOT = -15713
421802 feet/sec YDOT = -4762
079387 meter/sec
ZDOT = 17947
965840 ZDOT = 5482
430997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21046560
83 X = -6414991
74
Y = -636348
51 feet Y = -193959
03 meter
Z = 7128105
26 Z = 2172646
48
XDOT = 6567
678028 XDOT = 2001
828263
YDOT = -14749
722809 feet/sec YDOT = -4495
715512 meter/sec
ZDOT = 17997
049688 ZDOT = 5485
500745
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 12087
55977080
00016717 00000-0 10270-3 0 9062
2 25544 51
6410 171
1976 0015839 205
0065 155
0325 15
59593910 5299
Satellite: ISS
Catalog Number: 25544
Epoch time: 12087
55977080 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 171
1976 deg
Eccentricity:
0015839
Arg of perigee: 205
0065 deg
Mean anomaly: 155
0325 deg
Mean motion: 15
59593910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 315
Coasting Arc #8 (Orbit 543)
---------------------------------------
Vector Time (GMT): 2012/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3901672
30 A = 6763995
57 meter
Y = 2846552
81 meter E =
0010598
Z = -4733396
27 I = 51
71197
XDOT = -6080
785981 Wp = 165
35450
YDOT = 3809
592072 meter/sec RA = 165
42851 deg
ZDOT = -2732
666153 TA = 77
74132
MA = 77
62267
Ha = 215
472 n
mi
Hp = 205
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12800762
14 X = 3892545
45
Y = 9339084
03 feet Y = 2890132
39 meter
Z = -15529515
31 Z = -4714464
40
XDOT = -19950
085239 XDOT = -6109
658943
YDOT = 12498
661653 feet/sec YDOT = 3741
431351 meter/sec
ZDOT = -8965
440135 ZDOT = -2762
276823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13731525
05 X = 4185368
84
Y = 8057660
71 feet Y = 2455974
98 meter
Z = -15451963
36 Z = -4709758
43
XDOT = -18016
457333 XDOT = -5491
416195
YDOT = 13348
387174 feet/sec YDOT = 4068
588411 meter/sec
ZDOT = -9087
217761 ZDOT = -2769
783974
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 12088
52091385
00016717 00000-0 10270-3 0 9076
2 25544 51
6399 166
3668 0015778 208
8808 151
1476 15
59596381 5443
Satellite: ISS
Catalog Number: 25544
Epoch time: 12088
52091385 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 166
3668 deg
Eccentricity:
0015778
Arg of perigee: 208
8808 deg
Mean anomaly: 151
1476 deg
Mean motion: 15
59596381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 544
Checksum: 353
Coasting Arc #9 (Orbit 559)
---------------------------------------
Vector Time (GMT): 2012/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -141782
17 A = 6761676
30 meter
Y = -4311744
66 meter E =
0012236
Z = 5209383
21 I = 51
73488
XDOT = 7402
327874 Wp = 206
10738
YDOT = -1652
494780 meter/sec RA = 160
37836 deg
ZDOT = -1178
071435 TA = 255
09785
MA = 255
23338
Ha = 215
064 n
mi
Hp = 205
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -465164
61 X = -118862
88
Y = -14146143
90 feet Y = -4313201
70 meter
Z = 17091152
26 Z = 5208750
36
XDOT = 24285
852606 XDOT = 7425
979057
YDOT = -5421
570799 feet/sec YDOT = -1569
585204 meter/sec
ZDOT = -3865
063763 ZDOT = -1142
053671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2164805
34 X = -659832
67
Y = -13990121
49 feet Y = -4264189
03 meter
Z = 17088808
31 Z = 5208668
77
XDOT = 22519
765448 XDOT = 6864
024509
YDOT = -7977
813424 feet/sec YDOT = -2431
637532 meter/sec
ZDOT = -3717
091401 ZDOT = -1132
969459
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 12089
54611296
00016717 00000-0 10270-3 0 9089
2 25544 51
6405 161
2133 0015691 213
0783 146
9392 15
59670999 5601
Satellite: ISS
Catalog Number: 25544
Epoch time: 12089
54611296 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 161
2133 deg
Eccentricity:
0015691
Arg of perigee: 213
0783 deg
Mean anomaly: 146
9392 deg
Mean motion: 15
59670999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 560
Checksum: 324
Coasting Arc #10 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2012/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3586591
29 A = 6768154
57 meter
Y = 4613086
74 meter E =
0013370
Z = -3424504
12 I = 51
78429
XDOT = -6004
769328 Wp = 198
65495
YDOT = -1235
417001 meter/sec RA = 155
34455 deg
ZDOT = 4607
435304 TA = 121
28861
MA = 121
15762
Ha = 214
773 n
mi
Hp = 205
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11767031
79 X = -3621273
75
Y = 15134799
02 feet Y = 4572785
14 meter
Z = -11235249
74 Z = -3442012
11
XDOT = -19700
686773 XDOT = -6012
890205
YDOT = -4053
205384 feet/sec YDOT = -1302
611175 meter/sec
ZDOT = 15116
257560 ZDOT = 4578
244800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9629370
78 X = -2935032
21
Y = 16527964
97 feet Y = 5037723
72 meter
Z = -11307413
84 Z = -3446499
74
XDOT = -18946
020279 XDOT = -5774
746981
YDOT = -739
819225 feet/sec YDOT = -225
496900 meter/sec
ZDOT = 14996
472265 ZDOT = 4570
924746
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 12090
50722268
00016717 00000-0 10270-3 0 9090
2 25544 51
6395 156
3818 0015523 216
1111 143
8998 15
59688131 5758
Satellite: ISS
Catalog Number: 25544
Epoch time: 12090
50722268 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 156
3818 deg
Eccentricity:
0015523
Arg of perigee: 216
1111 deg
Mean anomaly: 143
8998 deg
Mean motion: 15
59688131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 322
Coasting Arc #11 (Orbit 590)
---------------------------------------
Vector Time (GMT): 2012/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5814455
49 A = 6773169
47 meter
Y = -3443957
73 meter E =
0020231
Z = 148631
09 I = 51
82889
XDOT = 2534
978790 Wp = 182
34848
YDOT = 4021
214924 meter/sec RA = 150
35200 deg
ZDOT = -6040
835309 TA = 356
04880
MA = 356
06475
Ha = 214
472 n
mi
Hp = 205
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19076297
53 X = 5851812
36
Y = -11299073
93 feet Y = -3378728
02 meter
Z = 487634
80 Z = 176968
30
XDOT = 8316
859547 XDOT = 2519
169246
YDOT = 13192
962349 feet/sec YDOT = 4049
473833 meter/sec
ZDOT = -19819
013481 ZDOT = -6028
559210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17202244
38 X = 5243244
09
Y = -13983193
70 feet Y = -4262077
44 meter
Z = 604209
57 Z = 184163
08
XDOT = 9267
217155 XDOT = 2824
647789
YDOT = 10551
968599 feet/sec YDOT = 3216
240029 meter/sec
ZDOT = -19768
842364 ZDOT = -6025
543152
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 12091
53238762
00016717 00000-0 10270-3 0 9107
2 25544 51
6400 151
2282 0015320 220
1643 139
8381 15
59702776 5915
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
53238762 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 151
2282 deg
Eccentricity:
0015320
Arg of perigee: 220
1643 deg
Mean anomaly: 139
8381 deg
Mean motion: 15
59702776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 591
Checksum: 286
Coasting Arc #12 (Orbit 597)
---------------------------------------
Vector Time (GMT): 2012/091/22:00:39
040
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5837742
99 A = 6774845
74 meter
Y = 3432908
62 meter E =
0001581
Z = 192299
75 I = 51
84032
XDOT = -2256
732476 Wp = 261
94157
YDOT = -4172
890769 meter/sec RA = 148
26366 deg
ZDOT = 6027
126680 TA = 100
12715
MA = 100
10932
Ha = 214
305 n
mi
Hp = 207
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19152700
09 X = -5876630
74
Y = 11262823
57 feet Y = 3367409
95 meter
Z = 630904
69 Z = 163845
70
XDOT = -7403
977939 XDOT = -2239
180926
YDOT = -13690
586511 feet/sec YDOT = -4198
028390 meter/sec
ZDOT = 19774
037664 ZDOT = 6016
206551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21917689
92 X = 6680511
89
Y = -3664149
05 feet Y = -1116832
63 meter
Z = 513845
11 Z = 156619
99
XDOT = 1861
343704 XDOT = 567
337561
YDOT = 13876
943787 feet/sec YDOT = 4229
692466 meter/sec
ZDOT = 19729
442729 ZDOT = 6013
534144
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 12091
98091607
00016717 00000-0 10270-3 0 9112
2 25544 51
6405 148
9738 0013767 230
9223 129
0709 15
59119077 5983
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
98091607 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 148
9738 deg
Eccentricity:
0013767
Arg of perigee: 230
9223 deg
Mean anomaly: 129
0709 deg
Mean motion: 15
59119077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 598
Checksum: 329
Coasting Arc #13 (Orbit 612)
---------------------------------------
Vector Time (GMT): 2012/092/22:00:39
040
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5792480
27 A = 6770152
24 meter
Y = -1062965
58 meter E =
0010714
Z = -3324766
76 I = 51
85104
XDOT = -1634
531205 Wp = 218
46330
YDOT = 5839
654677 meter/sec RA = 143
27755 deg
ZDOT = -4714
786183 TA =
22952
MA =
22903
Ha = 214
128 n
mi
Hp = 207
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19004200
35 X = 5820086
93
Y = -3487419
88 feet Y = -998036
41 meter
Z = -10908027
43 Z = -3296560
17
XDOT = -5362
635186 XDOT = -1676
806681
YDOT = 19158
972037 feet/sec YDOT = 5821
139567 meter/sec
ZDOT = -15468
458605 ZDOT = -4722
829793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19114362
14 X = -5826057
58
Y = -3237004
31 feet Y = -986638
91 meter
Z = -10792115
35 Z = -3289436
76
XDOT = 11260
667282 XDOT = 3432
251388
YDOT = -14811
576444 feet/sec YDOT = -4514
568500 meter/sec
ZDOT = -15501
848114 ZDOT = -4724
963305
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 12092
94234232
00016717 00000-0 10270-3 0 9123
2 25544 51
6414 144
1449 0013818 234
7247 125
2616 15
59148243 6135
Satellite: ISS
Catalog Number: 25544
Epoch time: 12092
94234232 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 144
1449 deg
Eccentricity:
0013818
Arg of perigee: 234
7247 deg
Mean anomaly: 125
2616 deg
Mean motion: 15
59148243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 613
Checksum: 292
Coasting Arc #14 (Orbit 628)
---------------------------------------
Vector Time (GMT): 2012/093/22:00:39
040
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3974583
79 A = 6763476
96 meter
Y = -1874820
00 meter E =
0012645
Z = 5150177
22 I = 51
85275
XDOT = 4738
523229 Wp = 217
96575
YDOT = -5833
995869 meter/sec RA = 138
25697 deg
ZDOT = 1525
404185 TA = 217
34002
MA = 217
42797
Ha = 213
733 n
mi
Hp = 208
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13039973
07 X = -3978342
06
Y = -6150984
25 feet Y = -1919286
74 meter
Z = 16896906
91 Z = 5130860
03
XDOT = 15546
336054 XDOT = 4795
997938
YDOT = -19140
406394 feet/sec YDOT = -5780
685257 meter/sec
ZDOT = 5004
606905 ZDOT = 1548
563804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10425694
85 X = 3177751
79
Y = 10092155
06 feet Y = 3076088
86 meter
Z = 16817677
04 Z = 5126027
96
XDOT = -20163
818345 XDOT = -6145
931832
YDOT = 12288
859546 feet/sec YDOT = 3745
644390 meter/sec
ZDOT = 5100
089181 ZDOT = 1554
507182
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 12093
96784717
00016717 00000-0 10270-3 0 9135
2 25544 51
6412 138
9933 0013731 238
4626 121
5189 15
59185223 6298
Satellite: ISS
Catalog Number: 25544
Epoch time: 12093
96784717 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 138
9933 deg
Eccentricity:
0013731
Arg of perigee: 238
4626 deg
Mean anomaly: 121
5189 deg
Mean motion: 15
59185223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 629
Checksum: 327
Coasting Arc #15 (Orbit 643)
---------------------------------------
Vector Time (GMT): 2012/094/22:00:39
040
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1060259
57 A = 6764254
00 meter
Y = 4516338
81 meter E =
0009823
Z = -4925826
52 I = 51
87793
XDOT = -6170
431219 Wp = 182
66359
YDOT = 3949
723190 meter/sec RA = 133
21928 deg
ZDOT = 2283
468087 TA = 109
61434
MA = 109
50829
Ha = 213
337 n
mi
Hp = 208
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3478541
88 X = 1033606
66
Y = 14817384
55 feet Y = 4528045
68 meter
Z = -16160848
15 Z = -4920741
11
XDOT = -20244
196914 XDOT = -6225
231774
YDOT = 12958
409416 feet/sec YDOT = 3880
415477 meter/sec
ZDOT = 7491
693200 ZDOT = 2253
358894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1178399
44 X = 359176
15
Y = -15196456
02 feet Y = -4631879
79 meter
Z = -16140237
00 Z = -4919544
24
XDOT = 22193
285597 XDOT = 6764
513450
YDOT = -6138
427623 feet/sec YDOT = -1870
992739 meter/sec
ZDOT = 7367
770883 ZDOT = 2245
696565
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 12094
92924182
00016717 00000-0 10270-3 0 9145
2 25544 51
6413 134
1635 0013746 242
5468 117
4290 15
59216135 6443
Satellite: ISS
Catalog Number: 25544
Epoch time: 12094
92924182 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 134
1635 deg
Eccentricity:
0013746
Arg of perigee: 242
5468 deg
Mean anomaly: 117
4290 deg
Mean motion: 15
59216135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 644
Checksum: 302
Coasting Arc #16 (Orbit 659)
---------------------------------------
Vector Time (GMT): 2012/095/22:00:39
040
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1900555
38 A = 6771326
61 meter
Y = -5886958
75 meter E =
0008083
Z = 2741466
53 I = 51
92143
XDOT = 5633
768625 Wp = 174
62676
YDOT = -591
699180 meter/sec RA = 128
20937 deg
ZDOT = -5182
894807 TA = 334
39540
MA = 334
43540
Ha = 213
030 n
mi
Hp = 208
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6235417
92 X = 1952925
83
Y = -19314169
13 feet Y = -5865412
39 meter
Z = 8994312
77 Z = 2750827
33
XDOT = 18483
492865 XDOT = 5665
143816
YDOT = -1941
270276 feet/sec YDOT = -528
524131 meter/sec
ZDOT = -17004
248054 ZDOT = -5155
449855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11563175
12 X = -3524455
78
Y = 16658652
39 feet Y = 5077557
25 meter
Z = 9033134
00 Z = 2753299
24
XDOT = -17126
198059 XDOT = -5220
065168
YDOT = -2740
048108 feet/sec YDOT = -835
166663 meter/sec
ZDOT = -16891
470723 ZDOT = -5148
520276
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 12095
95471349
00016717 00000-0 10270-3 0 9152
2 25544 51
6409 129
0122 0013630 246
2086 113
7640 15
59221679 6606
Satellite: ISS
Catalog Number: 25544
Epoch time: 12095
95471349 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 129
0122 deg
Eccentricity:
0013630
Arg of perigee: 246
2086 deg
Mean anomaly: 113
7640 deg
Mean motion: 15
59221679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 660
Checksum: 302
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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