[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 28th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
060/10:12:39
242 0
8 3
8 3
8
N/A -3
5 -0
3 220
2
000/00:01:14
484 -1
3 0
1 201
1
Coasting Arc #1 (Orbit 75)
---------------------------------------
Vector Time (GMT): 2012/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5612377
24 A = 6768873
87 meter
Y = 1440087
08 meter E =
0025109
Z = -3521710
06 I = 51
40836
XDOT = 1232
814334 Wp = 88
41614
YDOT = -6089
314273 meter/sec RA = 316
59276 deg
ZDOT = -4481
730620 TA = 133
22860
MA = 133
01869
Ha = 220
092 n
mi
Hp = 199
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18413311
16 X = -5610955
94
Y = 4724695
13 feet Y = 1377333
68 meter
Z = -11554166
88 Z = -3548971
16
XDOT = 4044
666450 XDOT = 1322
585692
YDOT = -19978
065200 feet/sec YDOT = -6075
026601 meter/sec
ZDOT = -14703
840617 ZDOT = -4475
523180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18675054
26 X = -5692156
54
Y = -3165119
62 feet Y = -964728
46 meter
Z = -11666015
19 Z = -3555801
43
XDOT = 11689
601841 XDOT = 3562
990641
YDOT = -15195
620977 feet/sec YDOT = -4631
625274 meter/sec
ZDOT = -14677
903868 ZDOT = -4473
825099
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 12058
52467472
00016717 00000-0 10270-3 0 9000
2 25544 51
6435 317
0373 0019896 90
1084 270
2352 15
59326931 763
Satellite: ISS
Catalog Number: 25544
Epoch time: 12058
52467472 = yrday
fracday
Element set: 900
Inclination: 51
6435 deg
RA of node: 317
0373 deg
Eccentricity:
0019896
Arg of perigee: 90
1084 deg
Mean anomaly: 270
2352 deg
Mean motion: 15
59326931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 76
Checksum: 307
Coasting Arc #2 (Orbit 91)
---------------------------------------
Vector Time (GMT): 2012/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3966635
67 A = 6762525
16 meter
Y = 1753220
01 meter E =
0023334
Z = 5169412
75 I = 51
36580
XDOT = -4304
931195 Wp = 98
30014
YDOT = 6269
197633 meter/sec RA = 311
53530 deg
ZDOT = 1169
249833 TA = 340
43746
MA = 340
52684
Ha = 219
923 n
mi
Hp = 199
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13013896
54 X = 3921624
37
Y = 5752034
15 feet Y = 1797326
05 meter
Z = 16960015
59 Z = 5188572
87
XDOT = -14123
790011 XDOT = -4380
394575
YDOT = 20568
233704 feet/sec YDOT = 6220
635376 meter/sec
ZDOT = 3836
121500 ZDOT = 1148
153135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9622764
00 X = 2933018
47
Y = 10353009
62 feet Y = 3155597
33 meter
Z = 17038401
74 Z = 5193304
85
XDOT = -20321
739064 XDOT = -6194
066067
YDOT = 12676
130144 feet/sec YDOT = 3863
684468 meter/sec
ZDOT = 3749
149931 ZDOT = 1142
740899
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 12059
55006266
00016717 00000-0 10270-3 0 9015
2 25544 51
6432 311
8853 0019879 93
9868 266
3560 15
59376864 922
Satellite: ISS
Catalog Number: 25544
Epoch time: 12059
55006266 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 311
8853 deg
Eccentricity:
0019879
Arg of perigee: 93
9868 deg
Mean anomaly: 266
3560 deg
Mean motion: 15
59376864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 92
Checksum: 341
Coasting Arc #3 (Orbit 105)
---------------------------------------
Vector Time (GMT): 2012/060/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4964174
63 A = 6767072
88 meter
Y = 494418
83 meter E =
0026845
Z = -4595359
99 I = 51
35529
XDOT = 2075
224407 Wp = 90
83809
YDOT = -6740
185275 meter/sec RA = 306
87645 deg
ZDOT = -2982
473963 TA = 149
32645
MA = 149
16924
Ha = 220
248 n
mi
Hp = 201
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16286662
16 X = -4947011
36
Y = 1622109
03 feet Y = 439002
07 meter
Z = -15076640
39 Z = -4619433
84
XDOT = 6808
479024 XDOT = 2164
928326
YDOT = -22113
468751 feet/sec YDOT = -6716
477446 meter/sec
ZDOT = -9785
019564 ZDOT = -2972
174438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11878546
82 X = -3620581
07
Y = -11126574
51 feet Y = -3391379
91 meter
Z = -15175346
87 Z = -4625445
73
XDOT = 20358
596980 XDOT = 6205
300359
YDOT = -8516
156023 feet/sec YDOT = -2595
724356 meter/sec
ZDOT = -9742
266210 ZDOT = -2969
442741
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 12060
44726632
00016717 00000-0 10270-3 0 9022
2 25544 51
6424 307
3756 0017587 103
3793 256
9324 15
58671515 1061
Satellite: ISS
Catalog Number: 25544
Epoch time: 12060
44726632 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 307
3756 deg
Eccentricity:
0017587
Arg of perigee: 103
3793 deg
Mean anomaly: 256
9324 deg
Mean motion: 15
58671515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 106
Checksum: 307
Coasting Arc #4 (Orbit 121)
---------------------------------------
Vector Time (GMT): 2012/061/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3264565
46 A = 6764068
47 meter
Y = 2709987
48 meter E =
0019582
Z = 5251039
89 I = 51
32788
XDOT = -4392
219246 Wp = 101
67113
YDOT = 6292
665500 meter/sec RA = 301
81070 deg
ZDOT = -519
180987 TA = 353
27563
MA = 353
30187
Ha = 219
976 n
mi
Hp = 201
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10710516
62 X = 3208511
14
Y = 8891035
05 feet Y = 2746180
72 meter
Z = 17227821
17 Z = 5266762
53
XDOT = -14410
168129 XDOT = -4459
736623
YDOT = 20645
228020 feet/sec YDOT = 6243
171458 meter/sec
ZDOT = -1703
349696 ZDOT = -540
682256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 522582
28 X = 159283
08
Y = 13830239
76 feet Y = 4215457
08 meter
Z = 17292046
40 Z = 5270615
74
XDOT = -23961
254603 XDOT = -7303
390403
YDOT = 3136
656222 feet/sec YDOT = 956
052816 meter/sec
ZDOT = -1791
973197 ZDOT = -546
193431
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 12061
47309514
00016717 00000-0 10270-3 0 9033
2 25544 51
6419 302
2267 0017350 107
3572 252
9483 15
58728041 1220
Satellite: ISS
Catalog Number: 25544
Epoch time: 12061
47309514 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 302
2267 deg
Eccentricity:
0017350
Arg of perigee: 107
3572 deg
Mean anomaly: 252
9483 deg
Mean motion: 15
58728041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 122
Checksum: 287
Coasting Arc #5 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2012/062/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -941088
03 A = 6769000
77 meter
Y = -5353214
46 meter E =
0024657
Z = -4060680
26 I = 51
32971
XDOT = 5385
559347 Wp = 109
80322
YDOT = -3853
115720 meter/sec RA = 296
74892 deg
ZDOT = 3842
334047 TA = 200
14927
MA = 200
24677
Ha = 220
090 n
mi
Hp = 201
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3087559
14 X = -861431
78
Y = -17563039
55 feet Y = -5363293
10 meter
Z = -13322441
80 Z = -4065058
22
XDOT = 17669
157961 XDOT = 5409
580474
YDOT = -12641
455773 feet/sec YDOT = -3792
756577 meter/sec
ZDOT = 12606
082832 ZDOT = 3868
555002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10763500
43 X = 3280714
93
Y = -14201167
96 feet Y = -4328515
99 meter
Z = -13339967
10 Z = -4066021
97
XDOT = 20216
522304 XDOT = 6161
995998
YDOT = 3413
390321 feet/sec YDOT = 1040
401370 meter/sec
ZDOT = 12713
854783 ZDOT = 3875
182938
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 12062
43479458
00016717 00000-0 10270-3 0 9046
2 25544 51
6426 297
3992 0017410 110
6439 249
6585 15
58717987 1372
Satellite: ISS
Catalog Number: 25544
Epoch time: 12062
43479458 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 297
3992 deg
Eccentricity:
0017410
Arg of perigee: 110
6439 deg
Mean anomaly: 249
6585 deg
Mean motion: 15
58717987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 342
Coasting Arc #6 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2012/063/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1441961
55 A = 6775315
91 meter
Y = 6472546
71 meter E =
0031255
Z = 1319471
00 I = 51
33782
XDOT = -5033
965963 Wp = 117
11920
YDOT = 81
190048 meter/sec RA = 291
71957 deg
ZDOT = -5807
682092 TA = 48
40768
MA = 48
14023
Ha = 220
061 n
mi
Hp = 201
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4730844
97 X = -1520641
28
Y = 21235389
48 feet Y = 6455981
96 meter
Z = 4328973
11 Z = 1312274
69
XDOT = -16515
636361 XDOT = -5006
287799
YDOT = 266
371550 feet/sec YDOT = 25
051585 meter/sec
ZDOT = -19054
075106 ZDOT = -5832
069214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18557940
18 X = -5656460
17
Y = 11365926
77 feet Y = 3464334
48 meter
Z = 4298980
54 Z = 1310329
27
XDOT = -10776
870537 XDOT = -3284
790140
YDOT = -10236
634548 feet/sec YDOT = -3120
126210 meter/sec
ZDOT = -19154
038798 ZDOT = -5838
151026
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 12063
46058794
00016717 00000-0 10270-3 0 9057
2 25544 51
6424 292
2494 0017458 114
8627 245
4345 15
58712753 1530
Satellite: ISS
Catalog Number: 25544
Epoch time: 12063
46058794 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 292
2494 deg
Eccentricity:
0017458
Arg of perigee: 114
8627 deg
Mean anomaly: 245
4345 deg
Mean motion: 15
58712753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 321
Coasting Arc #7 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2012/064/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3229512
46 A = 6774435
75 meter
Y = -5660281
60 meter E =
0028174
Z = 1831624
08 I = 51
32514
XDOT = 3535
036753 Wp = 94
81555
YDOT = 3859
128474 meter/sec RA = 286
70604 deg
ZDOT = 5615
951710 TA = 285
46285
MA = 285
77383
Ha = 219
882 n
mi
Hp = 201
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10595513
33 X = 3283669
41
Y = -18570477
70 feet Y = -5623864
27 meter
Z = 6009265
36 Z = 1847444
50
XDOT = 11597
889611 XDOT = 3464
339998
YDOT = 12661
182656 feet/sec YDOT = 3898
264518 meter/sec
ZDOT = 18425
038420 ZDOT = 5632
952437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20587588
75 X = 6275097
05
Y = -5700001
41 feet Y = -1737360
43 meter
Z = 6074536
03 Z = 1851518
58
XDOT = -1218
374253 XDOT = -371
360472
YDOT = 15575
327073 feet/sec YDOT = 4747
359692 meter/sec
ZDOT = 18494
433610 ZDOT = 5637
103364
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 12064
48636013
00016717 00000-0 10270-3 0 9067
2 25544 51
6424 287
1001 0017238 118
0535 242
2365 15
58763438 1697
Satellite: ISS
Catalog Number: 25544
Epoch time: 12064
48636013 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 287
1001 deg
Eccentricity:
0017238
Arg of perigee: 118
0535 deg
Mean anomaly: 242
2365 deg
Mean motion: 15
58763438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 298
Coasting Arc #8 (Orbit 183)
---------------------------------------
Vector Time (GMT): 2012/065/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4212215
39 A = 6767451
62 meter
Y = 2979467
95 meter E =
0023771
Z = -4395985
44 I = 51
29434
XDOT = -1330
202979 Wp = 103
94396
YDOT = -6769
405063 meter/sec RA = 281
66867 deg
ZDOT = -3334
323383 TA = 132
26509
MA = 132
06327
Ha = 219
676 n
mi
Hp = 201
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13819604
30 X = -4223865
10
Y = 9775157
32 feet Y = 2932298
84 meter
Z = -14422524
40 Z = -4416476
29
XDOT = -4364
183003 XDOT = -1238
210225
YDOT = -22209
334197 feet/sec YDOT = -6783
766142 meter/sec
ZDOT = -10939
381179 ZDOT = -3340
561281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16671265
83 X = -5081401
82
Y = -2483532
23 feet Y = -756980
63 meter
Z = -14506734
20 Z = -4421652
58
XDOT = 12128
128561 XDOT = 3696
653585
YDOT = -17764
149150 feet/sec YDOT = -5414
512661 meter/sec
ZDOT = -10964
456537 ZDOT = -3341
966352
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 12065
44800304
00016717 00000-0 10270-3 0 9071
2 25544 51
6423 282
2719 0017051 121
9173 238
3643 15
58805073 1846
Satellite: ISS
Catalog Number: 25544
Epoch time: 12065
44800304 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 282
2719 deg
Eccentricity:
0017051
Arg of perigee: 121
9173 deg
Mean anomaly: 238
3643 deg
Mean motion: 15
58805073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 184
Checksum: 291
Coasting Arc #9 (Orbit 199)
---------------------------------------
Vector Time (GMT): 2012/066/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4175920
46 A = 6763617
27 meter
Y = 648833
42 meter E =
0018889
Z = 5266522
82 I = 51
27656
XDOT = -1004
298578 Wp = 120
49414
YDOT = 7622
097376 meter/sec RA = 276
59926 deg
ZDOT = -151
753813 TA = 330
90282
MA = 331
00795
Ha = 219
467 n
mi
Hp = 201
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13700526
44 X = 4142771
67
Y = 2128718
56 feet Y = 695346
37 meter
Z = 17278618
17 Z = 5286728
23
XDOT = -3294
942841 XDOT = -1088
718594
YDOT = 25006
881155 feet/sec YDOT = 7610
394654 meter/sec
ZDOT = -497
879964 ZDOT = -156
838435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8503594
19 X = 2591895
51
Y = 10819303
43 feet Y = 3297723
68 meter
Z = 17361396
04 Z = 5291753
51
XDOT = -18653
851740 XDOT = -5685
694010
YDOT = 15447
148982 feet/sec YDOT = 4708
291010 meter/sec
ZDOT = -519
262612 ZDOT = -158
271244
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 12066
47373685
00016717 00000-0 10270-3 0 9083
2 25544 51
6420 277
1223 0017040 125
7491 234
5252 15
58853377 2002
Satellite: ISS
Catalog Number: 25544
Epoch time: 12066
47373685 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 277
1223 deg
Eccentricity:
0017040
Arg of perigee: 125
7491 deg
Mean anomaly: 234
5252 deg
Mean motion: 15
58853377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 200
Checksum: 299
Coasting Arc #10 (Orbit 214)
---------------------------------------
Vector Time (GMT): 2012/067/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3274417
77 A = 6767948
87 meter
Y = -4180256
50 meter E =
0024725
Z = -4223149
05 I = 51
28790
XDOT = 3049
818291 Wp = 123
02820
YDOT = -6026
785721 meter/sec RA = 271
52973 deg
ZDOT = 3603
056278 TA = 184
05914
MA = 184
07924
Ha = 219
464 n
mi
Hp = 201
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10742840
47 X = -3206915
21
Y = -13714752
29 feet Y = -4216496
18 meter
Z = -13855475
90 Z = -4238891
23
XDOT = 10005
965523 XDOT = 3099
481835
YDOT = -19772
919033 feet/sec YDOT = -5992
402614 meter/sec
ZDOT = 11821
050782 ZDOT = 3617
993304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1240158
29 X = 378000
25
Y = -17325725
16 feet Y = -5280881
03 meter
Z = -13919716
92 Z = -4242729
72
XDOT = 19341
523195 XDOT = 5895
296270
YDOT = -8156
605748 feet/sec YDOT = -2486
133432 meter/sec
ZDOT = 11882
694854 ZDOT = 3621
845392
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 12067
43534462
00016717 00000-0 10270-3 0 9093
2 25544 51
6412 272
2933 0016881 129
2717 230
9939 15
58867860 2159
Satellite: ISS
Catalog Number: 25544
Epoch time: 12067
43534462 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 272
2933 deg
Eccentricity:
0016881
Arg of perigee: 129
2717 deg
Mean anomaly: 230
9939 deg
Mean motion: 15
58867860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 215
Checksum: 326
Coasting Arc #11 (Orbit 230)
---------------------------------------
Vector Time (GMT): 2012/068/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1623930
71 A = 6774559
33 meter
Y = 6377348
68 meter E =
0030653
Z = 1537024
34 I = 51
31015
XDOT = -4449
066895 Wp = 125
97153
YDOT = 2530
919286 meter/sec RA = 266
49439 deg
ZDOT = -5738
202960 TA = 37
08753
MA = 36
87609
Ha = 219
386 n
mi
Hp = 201
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5327856
66 X = 1545030
80
Y = 20923059
96 feet Y = 6395067
54 meter
Z = 5042730
76 Z = 1544720
66
XDOT = -14596
676166 XDOT = -4449
162951
YDOT = 8303
540966 feet/sec YDOT = 2481
165718 meter/sec
ZDOT = -18826
125196 ZDOT = -5759
816629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9715620
33 X = -2961321
08
Y = 19273100
31 feet Y = 5874440
97 meter
Z = 5073850
08 Z = 1546509
50
XDOT = -14973
531251 XDOT = -4563
932325
YDOT = -2515
132922 feet/sec YDOT = -766
612514 meter/sec
ZDOT = -18914
892537 ZDOT = -5765
259245
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 12068
46104056
00016717 00000-0 10270-3 0 9101
2 25544 51
6410 267
1429 0016975 132
9409 227
3174 15
58874811 2316
Satellite: ISS
Catalog Number: 25544
Epoch time: 12068
46104056 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 267
1429 deg
Eccentricity:
0016975
Arg of perigee: 132
9409 deg
Mean anomaly: 227
3174 deg
Mean motion: 15
58874811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 231
Checksum: 301
Coasting Arc #12 (Orbit 246)
---------------------------------------
Vector Time (GMT): 2012/069/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 371674
36 A = 6774167
58 meter
Y = -6552870
83 meter E =
0024755
Z = 1671632
00 I = 51
31161
XDOT = 4857
941116 Wp = 104
35022
YDOT = 1743
224289 meter/sec RA = 261
47766 deg
ZDOT = 5676
646336 TA = 274
08294
MA = 274
36586
Ha = 219
168 n
mi
Hp = 201
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1219404
06 X = 436801
91
Y = -21498920
05 feet Y = -6548350
15 meter
Z = 5484356
96 Z = 1673596
68
XDOT = 15938
127022 XDOT = 4810
511320
YDOT = 5719
239792 feet/sec YDOT = 1797
284395 meter/sec
ZDOT = 18624
167770 ZDOT = 5700
130356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14720541
94 X = 4486821
18
Y = -15713147
43 feet Y = -4789367
34 meter
Z = 5492842
95 Z = 1674218
53
XDOT = 7306
258013 XDOT = 2226
947442
YDOT = 13476
658128 feet/sec YDOT = 4107
685397 meter/sec
ZDOT = 18720
316850 ZDOT = 5705
952576
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 12069
48671291
00016717 00000-0 10270-3 0 9115
2 25544 51
6401 261
9916 0016736 137
2060 223
0402 15
58947087 2475
Satellite: ISS
Catalog Number: 25544
Epoch time: 12069
48671291 = yrday
fracday
Element set: 911
Inclination: 51
6401 deg
RA of node: 261
9916 deg
Eccentricity:
0016736
Arg of perigee: 137
2060 deg
Mean anomaly: 223
0402 deg
Mean motion: 15
58947087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 247
Checksum: 304
Coasting Arc #13 (Orbit 261)
---------------------------------------
Vector Time (GMT): 2012/070/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2455209
27 A = 6767343
34 meter
Y = 4599687
48 meter E =
0021128
Z = -4324325
98 I = 51
29341
XDOT = -4156
526402 Wp = 117
73846
YDOT = -5441
161730 meter/sec RA = 256
43961 deg
ZDOT = -3450
303218 TA = 117
15334
MA = 116
93775
Ha = 219
023 n
mi
Hp = 202
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8055148
54 X = -2485454
89
Y = 15090838
20 feet Y = 4572062
15 meter
Z = -14187421
21 Z = -4336327
29
XDOT = -13636
897643 XDOT = -4078
612567
YDOT = -17851
580479 feet/sec YDOT = -5487
207376 meter/sec
ZDOT = -11319
892447 ZDOT = -3470
305424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15688077
92 X = -4781726
15
Y = 6715366
83 feet Y = 2046843
81 meter
Z = -14236916
64 Z = -4339412
19
XDOT = 1175
738936 XDOT = 358
365228
YDOT = -21268
466048 feet/sec YDOT = -6482
628451 meter/sec
ZDOT = -11401
530623 ZDOT = -3475
186534
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 12070
44826464
00016717 00000-0 10270-3 0 9128
2 25544 51
6392 257
1618 0016638 140
7090 219
5276 15
58943649 2629
Satellite: ISS
Catalog Number: 25544
Epoch time: 12070
44826464 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 257
1618 deg
Eccentricity:
0016638
Arg of perigee: 140
7090 deg
Mean anomaly: 219
5276 deg
Mean motion: 15
58943649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 262
Checksum: 321
Coasting Arc #14 (Orbit 277)
---------------------------------------
Vector Time (GMT): 2012/071/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4024258
61 A = 6763277
01 meter
Y = -1286414
49 meter E =
0018076
Z = 5270712
38 I = 51
28870
XDOT = 2404
401602 Wp = 137
98417
YDOT = 7300
337417 meter/sec RA = 251
36952 deg
ZDOT = -67
106223 TA = 312
58073
MA = 312
73312
Ha = 218
850 n
mi
Hp = 202
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13202948
19 X = 4012740
55
Y = -4220519
98 feet Y = -1241476
59 meter
Z = 17292363
46 Z = 5290234
19
XDOT = 7888
456700 XDOT = 2322
915043
YDOT = 23951
238246 feet/sec YDOT = 7326
769298 meter/sec
ZDOT = -220
164774 ZDOT = -55
624456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12918682
97 X = 3937614
57
Y = 4739333
28 feet Y = 1444548
79 meter
Z = 17372472
89 Z = 5295129
74
XDOT = -8184
337624 XDOT = -2494
586108
YDOT = 22788
696706 feet/sec YDOT = 6945
994756 meter/sec
ZDOT = -173
569391 ZDOT = -52
903950
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 12071
47389909
00016717 00000-0 10270-3 0 9131
2 25544 51
6397 252
0110 0016642 144
3736 215
8533 15
58969893 2788
Satellite: ISS
Catalog Number: 25544
Epoch time: 12071
47389909 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 252
0110 deg
Eccentricity:
0016642
Arg of perigee: 144
3736 deg
Mean anomaly: 215
8533 deg
Mean motion: 15
58969893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 278
Checksum: 333
Coasting Arc #15 (Orbit 292)
---------------------------------------
Vector Time (GMT): 2012/072/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4741780
29 A = 6767438
91 meter
Y = -2367648
69 meter E =
0023659
Z = -4233476
81 I = 51
31284
XDOT = 169
176555 Wp = 135
81502
YDOT = -6761
980608 meter/sec RA = 246
29856 deg
ZDOT = 3587
768833 TA = 171
09762
MA = 171
05559
Ha = 218
782 n
mi
Hp = 202
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15557021
94 X = -4694387
08
Y = -7767876
29 feet Y = -2420409
56 meter
Z = -13889359
60 Z = -4256396
83
XDOT = 555
041191 XDOT = 227
349252
YDOT = -22184
975748 feet/sec YDOT = -6759
763220 meter/sec
ZDOT = 11770
895123 ZDOT = 3588
732530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7676800
04 X = -2339888
65
Y = -15518146
15 feet Y = -4729930
95 meter
Z = -13983169
35 Z = -4262070
02
XDOT = 12610
689968 XDOT = 3843
738302
YDOT = -16862
236560 feet/sec YDOT = -5139
609704 meter/sec
ZDOT = 11775
280552 ZDOT = 3589
105512
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 12072
43541109
00016717 00000-0 10270-3 0 9141
2 25544 51
6386 247
1805 0016584 148
0097 212
2069 15
59019522 2936
Satellite: ISS
Catalog Number: 25544
Epoch time: 12072
43541109 = yrday
fracday
Element set: 914
Inclination: 51
6386 deg
RA of node: 247
1805 deg
Eccentricity:
0016584
Arg of perigee: 148
0097 deg
Mean anomaly: 212
2069 deg
Mean motion: 15
59019522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 293
Checksum: 301
Coasting Arc #16 (Orbit 308)
---------------------------------------
Vector Time (GMT): 2012/073/10:13:16
484
Vector Time (MET): N/A
Weight (LBS) : 886205
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4173708
47 A = 6773960
95 meter
Y = 5092741
42 meter E =
0028959
Z = 1514666
86 I = 51
34900
XDOT = -2967
049483 Wp = 136
23201
YDOT = 4155
525387 meter/sec RA = 241
26506 deg
ZDOT = -5751
149016 TA = 27
08627
MA = 26
93546
Ha = 218
436 n
mi
Hp = 202
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13693269
25 X = 4109092
32
Y = 16708469
22 feet Y = 5139053
21 meter
Z = 4969379
45 Z = 1534785
22
XDOT = -9734
414315 XDOT = -2985
359189
YDOT = 13633
613475 feet/sec YDOT = 4122
243286 meter/sec
ZDOT = -18868
599135 ZDOT = -5765
607486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1220379
40 X = 371971
64
Y = 21549151
81 feet Y = 6568181
47 meter
Z = 5051537
29 Z = 1539708
57
XDOT = -14227
033649 XDOT = -4336
399856
YDOT = 5276
969741 feet/sec YDOT = 1608
420377 meter/sec
ZDOT = -18928
142408 ZDOT = -5769
297806
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 12073
46100253
00016717 00000-0 10270-3 0 9157
2 25544 51
6391 242
0298 0016324 151
7507 208
4537 15
59084564 3094
Satellite: ISS
Catalog Number: 25544
Epoch time: 12073
46100253 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 242
0298 deg
Eccentricity:
0016324
Arg of perigee: 151
7507 deg
Mean anomaly: 208
4537 deg
Mean motion: 15
59084564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 309
Checksum: 295
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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