[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 20th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 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 213)
---------------------------------------
Vector Time (GMT): 2012/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3602064
72 A = 6795534
05 meter
Y = 5445733
75 meter E =
0017117
Z = -1842133
83 I = 51
99405
XDOT = -3209
064736 Wp = 328
61074
YDOT = 4045
106416 meter/sec RA = 69
25448 deg
ZDOT = 5673
850587 TA = 11
23115
MA = 11
19299
Ha = 226
561 n
mi
Hp = 219
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11817797
63 X = 3549850
41
Y = 17866580
55 feet Y = 5485722
40 meter
Z = -6043746
15 Z = -1824761
69
XDOT = -10528
427610 XDOT = -3281
621971
YDOT = 13271
346508 feet/sec YDOT = 4008
814799 meter/sec
ZDOT = 18614
995364 ZDOT = 5658
084836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21432199
41 X = -6532534
38
Y = 627341
15 feet Y = 191213
58 meter
Z = -5972368
07 Z = -1820377
79
XDOT = -5601
649656 XDOT = -1707
382815
YDOT = -14484
915309 feet/sec YDOT = -4415
002186 meter/sec
ZDOT = 18549
131578 ZDOT = 5653
775305
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 12324
50357646
00016717 00000-0 10270-3 0 9005
2 25544 51
6486 69
9636 0016141 303
6857 56
2755 15
51516629 2144
Satellite: ISS
Catalog Number: 25544
Epoch time: 12324
50357646 = yrday
fracday
Element set: 900
Inclination: 51
6486 deg
RA of node: 69
9636 deg
Eccentricity:
0016141
Arg of perigee: 303
6857 deg
Mean anomaly: 56
2755 deg
Mean motion: 15
51516629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 214
Checksum: 313
Coasting Arc #2 (Orbit 229)
---------------------------------------
Vector Time (GMT): 2012/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3609079
00 A = 6796385
35 meter
Y = -5670253
55 meter E =
0002601
Z = 1017383
50 I = 51
98529
XDOT = 3542
370177 Wp = 322
20786
YDOT = -3316
255965 meter/sec RA = 64
31877 deg
ZDOT = -5922
479328 TA = 206
84172
MA = 206
85518
Ha = 226
636 n
mi
Hp = 218
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11840810
38 X = -3550347
07
Y = -18603194
05 feet Y = -5710284
15 meter
Z = 3337872
37 Z = 999993
18
XDOT = 11621
949398 XDOT = 3607
960303
YDOT = -10880
104872 feet/sec YDOT = -3276
276154 meter/sec
ZDOT = -19430
706458 ZDOT = -5905
111218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22053733
82 X = 6721978
07
Y = -623001
17 feet Y = -189890
76 meter
Z = 3266451
52 Z = 995614
42
XDOT = 3261
265437 XDOT = 994
033705
YDOT = 14054
556370 feet/sec YDOT = 4283
828782 meter/sec
ZDOT = -19358
282037 ZDOT = -5900
404365
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 12325
53412025
00016717 00000-0 10270-3 0 9013
2 25544 51
6482 64
8471 0016010 307
2537 52
7154 15
51558024 2308
Satellite: ISS
Catalog Number: 25544
Epoch time: 12325
53412025 = yrday
fracday
Element set: 901
Inclination: 51
6482 deg
RA of node: 64
8471 deg
Eccentricity:
0016010
Arg of perigee: 307
2537 deg
Mean anomaly: 52
7154 deg
Mean motion: 15
51558024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 230
Checksum: 265
Coasting Arc #3 (Orbit 244)
---------------------------------------
Vector Time (GMT): 2012/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3550899
33 A = 6796778
67 meter
Y = 5778294
85 meter E =
0019544
Z = -144340
77 I = 51
97337
XDOT = -3959
303048 Wp = 348
67678
YDOT = 2586
991936 meter/sec RA = 59
38194 deg
ZDOT = 6041
793529 TA = 9
77538
MA = 9
73741
Ha = 226
985 n
mi
Hp = 218
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11649932
20 X = 3486722
50
Y = 18957660
28 feet Y = 5817644
40 meter
Z = -473558
97 Z = -127246
33
XDOT = -12989
839396 XDOT = -4017
287077
YDOT = 8487
506351 feet/sec YDOT = 2542
392303 meter/sec
ZDOT = 19822
157249 ZDOT = 6022
418357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22243194
49 X = -6779725
68
Y = 644701
73 feet Y = 196505
09 meter
Z = -403385
89 Z = -122952
02
XDOT = -771
440169 XDOT = -235
134964
YDOT = -13975
919054 feet/sec YDOT = -4259
860128 meter/sec
ZDOT = 19741
496557 ZDOT = 6017
208151
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 12326
50023935
00016717 00000-0 10270-3 0 9020
2 25544 51
6490 60
0492 0016148 311
6494 48
3274 15
51569650 2458
Satellite: ISS
Catalog Number: 25544
Epoch time: 12326
50023935 = yrday
fracday
Element set: 902
Inclination: 51
6490 deg
RA of node: 60
0492 deg
Eccentricity:
0016148
Arg of perigee: 311
6494 deg
Mean anomaly: 48
3274 deg
Mean motion: 15
51569650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 245
Checksum: 292
Coasting Arc #4 (Orbit 260)
---------------------------------------
Vector Time (GMT): 2012/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3454414
30 A = 6796419
71 meter
Y = -5810049
28 meter E =
0005781
Z = -725898
01 I = 51
95561
XDOT = 4408
739198 Wp = 306
04303
YDOT = -1870
386370 meter/sec RA = 54
44540 deg
ZDOT = -5973
377396 TA = 241
74935
MA = 241
80772
Ha = 227
107 n
mi
Hp = 218
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11333380
24 X = -3385662
07
Y = -19061841
48 feet Y = -5848294
29 meter
Z = -2381555
16 Z = -742512
66
XDOT = 14464
367446 XDOT = 4458
344324
YDOT = -6136
438223 feet/sec YDOT = -1820
807725 meter/sec
ZDOT = -19597
694869 ZDOT = -5951
839138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22158556
40 X = 6753927
99
Y = -684352
17 feet Y = -208590
54 meter
Z = -2449725
16 Z = -746676
23
XDOT = -1733
577443 XDOT = -528
394405
YDOT = 14117
598536 feet/sec YDOT = 4303
044034 meter/sec
ZDOT = -19508
151977 ZDOT = -5946
084722
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 12327
53075137
00016717 00000-0 10270-3 0 9036
2 25544 51
6483 54
9327 0016078 315
2506 44
7348 15
51608995 2611
Satellite: ISS
Catalog Number: 25544
Epoch time: 12327
53075137 = yrday
fracday
Element set: 903
Inclination: 51
6483 deg
RA of node: 54
9327 deg
Eccentricity:
0016078
Arg of perigee: 315
2506 deg
Mean anomaly: 44
7348 deg
Mean motion: 15
51608995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 261
Checksum: 311
Coasting Arc #5 (Orbit 276)
---------------------------------------
Vector Time (GMT): 2012/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3250537
37 A = 6795492
67 meter
Y = 5734830
86 meter E =
0018603
Z = 1598886
40 I = 51
93507
XDOT = -4922
802764 Wp = 5
55933
YDOT = 1186
601470 meter/sec RA = 49
50566 deg
ZDOT = 5764
425063 TA = 11
86179
MA = 11
81803
Ha = 227
349 n
mi
Hp = 218
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10664492
67 X = 3178400
53
Y = 18815061
89 feet Y = 5770777
06 meter
Z = 5245690
30 Z = 1614502
46
XDOT = -16150
927702 XDOT = -4963
708485
YDOT = 3893
049443 feet/sec YDOT = 1131
322861 meter/sec
ZDOT = 18912
155720 ZDOT = 5740
410532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21603980
96 X = -6584893
40
Y = 574564
85 feet Y = 175127
37 meter
Z = 5309718
11 Z = 1618402
08
XDOT = 4224
918268 XDOT = 1287
755088
YDOT = -14619
449357 feet/sec YDOT = -4456
008164 meter/sec
ZDOT = 18812
430581 ZDOT = 5734
028841
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 12328
56124684
00016717 00000-0 10270-3 0 9043
2 25544 51
6491 49
8148 0016156 319
5946 40
4005 15
51632131 2775
Satellite: ISS
Catalog Number: 25544
Epoch time: 12328
56124684 = yrday
fracday
Element set: 904
Inclination: 51
6491 deg
RA of node: 49
8148 deg
Eccentricity:
0016156
Arg of perigee: 319
5946 deg
Mean anomaly: 40
4005 deg
Mean motion: 15
51632131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 277
Checksum: 302
Coasting Arc #6 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2012/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2989519
60 A = 6794021
95 meter
Y = -5605574
84 meter E =
0010817
Z = -2418859
15 I = 51
90909
XDOT = 5424
867656 Wp = 328
19671
YDOT = -566
703670 meter/sec RA = 44
56416 deg
ZDOT = -5371
511806 TA = 238
68262
MA = 238
78857
Ha = 227
544 n
mi
Hp = 218
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9808135
18 X = -2914864
19
Y = -18390993
58 feet Y = -5638588
06 meter
Z = -7935889
59 Z = -2433201
15
XDOT = 17798
122232 XDOT = 5456
895582
YDOT = -1859
264008 feet/sec YDOT = -505
860241 meter/sec
ZDOT = -17623
070230 ZDOT = -5345
079723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20817358
97 X = 6345131
01
Y = -360288
23 feet Y = -109815
85 meter
Z = -7994639
59 Z = -2436766
15
XDOT = -6486
131628 XDOT = -1976
972920
YDOT = 15285
355892 feet/sec YDOT = 4658
976476 meter/sec
ZDOT = -17513
400809 ZDOT = -5338
084566
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 12329
52732214
00016717 00000-0 10270-3 0 9055
2 25544 51
6483 45
0181 0016156 323
2252 36
7790 15
51654700 2925
Satellite: ISS
Catalog Number: 25544
Epoch time: 12329
52732214 = yrday
fracday
Element set: 905
Inclination: 51
6483 deg
RA of node: 45
0181 deg
Eccentricity:
0016156
Arg of perigee: 323
2252 deg
Mean anomaly: 36
7790 deg
Mean motion: 15
51654700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 292
Checksum: 284
Coasting Arc #7 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2012/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2589403
32 A = 6792059
65 meter
Y = 5395184
50 meter E =
0014909
Z = 3192396
01 I = 51
88128
XDOT = -5953
319088 Wp = 14
94706
YDOT = -
138986 meter/sec RA = 39
61761 deg
ZDOT = 4838
077642 TA = 21
79827
MA = 21
73489
Ha = 227
709 n
mi
Hp = 217
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8495417
72 X = 2513372
51
Y = 17700736
56 feet Y = 5423715
62 meter
Z = 10473740
19 Z = 3204790
98
XDOT = -19531
886771 XDOT = -5976
377862
YDOT = -
455990 feet/sec YDOT = -66
841803 meter/sec
ZDOT = 15872
958142 ZDOT = 4809
100048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19605958
89 X = -5975896
27
Y = -173531
84 feet Y = -52892
50 meter
Z = 10524433
15 Z = 3207847
22
XDOT = 8583
812260 XDOT = 2616
345977
YDOT = -16216
703438 feet/sec YDOT = -4942
851208 meter/sec
ZDOT = 15752
809181 ZDOT = 4801
456238
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 12330
55778604
00016717 00000-0 10270-3 0 9064
2 25544 51
6490 39
9000 0016218 327
2077 32
8067 15
51692766 3089
Satellite: ISS
Catalog Number: 25544
Epoch time: 12330
55778604 = yrday
fracday
Element set: 906
Inclination: 51
6490 deg
RA of node: 39
9000 deg
Eccentricity:
0016218
Arg of perigee: 327
2077 deg
Mean anomaly: 32
8067 deg
Mean motion: 15
51692766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 307
Coasting Arc #8 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2012/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2134356
40 A = 6790073
37 meter
Y = -5167332
70 meter E =
0015973
Z = -3864844
37 I = 51
84978
XDOT = 6413
154092 Wp = 353
40640
YDOT = 469
561771 meter/sec RA = 34
66763 deg
ZDOT = -4152
299318 TA = 232
90483
MA = 233
05094
Ha = 227
942 n
mi
Hp = 217
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7002481
63 X = -2057640
62
Y = -16953191
28 feet Y = -5190771
28 meter
Z = -12679935
60 Z = -3875027
11
XDOT = 21040
531799 XDOT = 6427
598082
YDOT = 1540
556991 feet/sec YDOT = 541
358632 meter/sec
ZDOT = -13623
029260 ZDOT = -4121
108713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18292221
29 X = 5575469
05
Y = 885947
63 feet Y = 270036
84 meter
Z = -12721475
84 Z = -3877505
84
XDOT = -10254
599587 XDOT = -3125
601954
YDOT = 17161
960286 feet/sec YDOT = 5230
965495 meter/sec
ZDOT = -13493
768165 ZDOT = -4112
900537
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 12331
52383346
00016717 00000-0 10270-3 0 9078
2 25544 51
6482 35
1030 0016242 331
1550 28
8703 15
51695471 3233
Satellite: ISS
Catalog Number: 25544
Epoch time: 12331
52383346 = yrday
fracday
Element set: 907
Inclination: 51
6482 deg
RA of node: 35
1030 deg
Eccentricity:
0016242
Arg of perigee: 331
1550 deg
Mean anomaly: 28
8703 deg
Mean motion: 15
51695471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 275
Coasting Arc #9 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2012/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1526883
20 A = 6787882
86 meter
Y = 4893213
76 meter E =
0011640
Z = 4441795
30 I = 51
81775
XDOT = -6847
249843 Wp = 7
76347
YDOT = -884
594292 meter/sec RA = 29
71179 deg
ZDOT = 3338
487989 TA = 48
65745
MA = 48
55737
Ha = 228
101 n
mi
Hp = 217
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5009459
31 X = 1450475
08
Y = 16053850
93 feet Y = 4909860
81 meter
Z = 14572819
23 Z = 4449027
71
XDOT = -22464
730456 XDOT = -6853
067174
YDOT = -2902
212245 feet/sec YDOT = -961
197264 meter/sec
ZDOT = 10953
044583 ZDOT = 3305
209471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16667847
70 X = -5080359
98
Y = -2036616
85 feet Y = -620760
81 meter
Z = 14602154
55 Z = 4450736
71
XDOT = 11667
763144 XDOT = 3556
334206
YDOT = -18187
230547 feet/sec YDOT = -5543
467871 meter/sec
ZDOT = 10815
183557 ZDOT = 3296
467948
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 12332
55426670
00016717 00000-0 10270-3 0 9081
2 25544 51
6486 29
9849 0016320 335
0924 24
9438 15
51741396 3398
Satellite: ISS
Catalog Number: 25544
Epoch time: 12332
55426670 = yrday
fracday
Element set: 908
Inclination: 51
6486 deg
RA of node: 29
9849 deg
Eccentricity:
0016320
Arg of perigee: 335
0924 deg
Mean anomaly: 24
9438 deg
Mean motion: 15
51741396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 323
Coasting Arc #10 (Orbit 353)
---------------------------------------
Vector Time (GMT): 2012/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -892001
22 A = 6786229
68 meter
Y = -4642615
28 meter E =
0019560
Z = -4880429
87 I = 51
78476
XDOT = 7159
707820 Wp = 15
90566
YDOT = 1194
848387 meter/sec RA = 24
75193 deg
ZDOT = -2429
181311 TA = 230
18467
MA = 230
35700
Ha = 228
308 n
mi
Hp = 216
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2926513
18 X = -816311
75
Y = -15231677
44 feet Y = -4652166
61 meter
Z = -16011909
03 Z = -4884579
77
XDOT = 23489
855053 XDOT = 7157
615278
YDOT = 3920
106258 feet/sec YDOT = 1274
901207 meter/sec
ZDOT = -7969
754956 ZDOT = -2394
404105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15125877
69 X = 4610367
52
Y = 3353360
24 feet Y = 1022104
20 meter
Z = -16028490
48 Z = -4885483
90
XDOT = -12566
969318 XDOT = -3830
412248
YDOT = 19028
596606 feet/sec YDOT = 5799
916246 meter/sec
ZDOT = -7825
723114 ZDOT = -2385
280405
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 12333
52028582
00016717 00000-0 10270-3 0 9090
2 25544 51
6482 25
1872 0016340 339
0817 20
9664 15
51736838 3544
Satellite: ISS
Catalog Number: 25544
Epoch time: 12333
52028582 = yrday
fracday
Element set: 909
Inclination: 51
6482 deg
RA of node: 25
1872 deg
Eccentricity:
0016340
Arg of perigee: 339
0817 deg
Mean anomaly: 20
9664 deg
Mean motion: 15
51736838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 354
Checksum: 308
Coasting Arc #11 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2012/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 114302
12 A = 6784793
78 meter
Y = 4379702
30 meter E =
0013228
Z = 5178941
64 I = 51
75221
XDOT = -7389
034504 Wp = 354
45572
YDOT = -1469
557509 meter/sec RA = 19
78686 deg
ZDOT = 1418
998878 TA = 81
98698
MA = 81
83690
Ha = 228
483 n
mi
Hp = 216
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 375006
94 X = 40160
35
Y = 14369102
04 feet Y = 4380565
49 meter
Z = 16991278
35 Z = 5179317
22
XDOT = -24242
239187 XDOT = -7378
945713
YDOT = -4821
382903 feet/sec YDOT = -1552
130027 meter/sec
ZDOT = 4655
508130 ZDOT = 1383
127088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13422411
91 X = -4091151
15
Y = -5139830
69 feet Y = -1566620
39 meter
Z = 16992241
25 Z = 5179235
13
XDOT = 13198
795684 XDOT = 4022
992925
YDOT = -19710
597661 feet/sec YDOT = -6007
790167 meter/sec
ZDOT = 4506
975872 ZDOT = 1373
726246
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 12334
55068905
00016717 00000-0 10270-3 0 9109
2 25544 51
6481 20
0689 0016403 343
2281 16
8326 15
51784094 3709
Satellite: ISS
Catalog Number: 25544
Epoch time: 12334
55068905 = yrday
fracday
Element set: 910
Inclination: 51
6481 deg
RA of node: 20
0689 deg
Eccentricity:
0016403
Arg of perigee: 343
2281 deg
Mean anomaly: 16
8326 deg
Mean motion: 15
51784094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 292
Coasting Arc #12 (Orbit 384)
---------------------------------------
Vector Time (GMT): 2012/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 640767
51 A = 6784238
90 meter
Y = -4173528
30 meter E =
0020041
Z = -5320470
33 I = 51
72159
XDOT = 7464
004749 Wp = 33
05364
YDOT = 1658
996561 meter/sec RA = 14
81878 deg
ZDOT = -386
745045 TA = 233
16478
MA = 233
34876
Ha = 228
647 n
mi
Hp = 216
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2102255
60 X = 713235
11
Y = -13692678
15 feet Y = -4165957
15 meter
Z = -17455611
32 Z = -5317181
84
XDOT = 24488
204558 XDOT = 7446
777498
YDOT = 5442
902102 feet/sec YDOT = 1742
367439 meter/sec
ZDOT = -1268
848574 ZDOT = -350
526487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11986897
40 X = 3653606
33
Y = 6979892
41 feet Y = 2127471
21 meter
Z = -17441406
84 Z = -5316140
80
XDOT = -13367
870674 XDOT = -4074
526981
YDOT = 20032
559443 feet/sec YDOT = 6105
924118 meter/sec
ZDOT = -1118
904620 ZDOT = -341
042128
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 12335
51667957
00016717 00000-0 10270-3 0 9119
2 25544 51
6484 15
2706 0016445 346
9742 13
0983 15
51780860 3857
Satellite: ISS
Catalog Number: 25544
Epoch time: 12335
51667957 = yrday
fracday
Element set: 911
Inclination: 51
6484 deg
RA of node: 15
2706 deg
Eccentricity:
0016445
Arg of perigee: 346
9742 deg
Mean anomaly: 13
0983 deg
Mean motion: 15
51780860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 385
Checksum: 320
Coasting Arc #13 (Orbit 400)
---------------------------------------
Vector Time (GMT): 2012/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1506235
56 A = 6784229
99 meter
Y = 3977732
37 meter E =
0017757
Z = 5287053
88 I = 51
69156
XDOT = -7404
283471 Wp =
28729
YDOT = -1847
915192 meter/sec RA = 9
84723 deg
ZDOT = -701
775157 TA = 96
51549
MA = 96
31330
Ha = 228
807 n
mi
Hp = 216
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4941717
73 X = -1576287
00
Y = 13050303
05 feet Y = 3960496
54 meter
Z = 17345977
30 Z = 5279566
80
XDOT = -24292
268605 XDOT = -7379
660292
YDOT = -6062
713885 feet/sec YDOT = -1930
576777 meter/sec
ZDOT = -2302
411934 ZDOT = -737
685519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10528018
65 X = -3208940
08
Y = -9218820
74 feet Y = -2809896
56 meter
Z = 17314389
39 Z = 5277425
89
XDOT = 13350
644264 XDOT = 4069
276372
YDOT = -19957
216074 feet/sec YDOT = -6082
959459 meter/sec
ZDOT = -2451
052064 ZDOT = -747
080669
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 12336
54705285
00016717 00000-0 10270-3 0 9121
2 25544 51
6476 10
1519 0016478 351
2506 8
8356 15
51833145 4017
Satellite: ISS
Catalog Number: 25544
Epoch time: 12336
54705285 = yrday
fracday
Element set: 912
Inclination: 51
6476 deg
RA of node: 10
1519 deg
Eccentricity:
0016478
Arg of perigee: 351
2506 deg
Mean anomaly: 8
8356 deg
Mean motion: 15
51833145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 401
Checksum: 292
Coasting Arc #14 (Orbit 415)
---------------------------------------
Vector Time (GMT): 2012/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2286385
57 A = 6785098
56 meter
Y = -3853479
89 meter E =
0017596
Z = -5101359
28 I = 51
66520
XDOT = 7189
758502 Wp = 39
72934
YDOT = 1990
431983 meter/sec RA = 4
87505 deg
ZDOT = 1735
368770 TA = 246
96650
MA = 247
15215
Ha = 228
969 n
mi
Hp = 215
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7501265
01 X = 2354087
47
Y = -12642650
55 feet Y = -3827533
13 meter
Z = -16736743
05 Z = -5090087
92
XDOT = 23588
446530 XDOT = 7158
536630
YDOT = 6530
288659 feet/sec YDOT = 2070
657642 meter/sec
ZDOT = 5693
467093 ZDOT = 1770
220840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9464459
50 X = 2884767
26
Y = 11318541
34 feet Y = 3449891
40 meter
Z = -16689481
29 Z = -5086953
90
XDOT = -13044
265166 XDOT = -3975
892023
YDOT = 19435
192427 feet/sec YDOT = 5923
846652 meter/sec
ZDOT = 5837
699362 ZDOT = 1779
330765
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 12337
51301501
00016717 00000-0 10270-3 0 9133
2 25544 51
6487 5
3534 0016561 354
7448 5
3527 15
51824960 4161
Satellite: ISS
Catalog Number: 25544
Epoch time: 12337
51301501 = yrday
fracday
Element set: 913
Inclination: 51
6487 deg
RA of node: 5
3534 deg
Eccentricity:
0016561
Arg of perigee: 354
7448 deg
Mean anomaly: 5
3527 deg
Mean motion: 15
51824960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 416
Checksum: 288
Coasting Arc #15 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2012/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3127315
80 A = 6786508
32 meter
Y = 3742909
08 meter E =
0021244
Z = 4722141
86 I = 51
63882
XDOT = -6807
308602 Wp = 18
13829
YDOT = -2174
215189 meter/sec RA = 359
90131 deg
ZDOT = -2761
808804 TA = 99
35247
MA = 99
11221
Ha = 229
068 n
mi
Hp = 215
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10260222
45 X = -3191876
56
Y = 12279885
45 feet Y = 3707576
18 meter
Z = 15492591
41 Z = 4706792
88
XDOT = -22333
689640 XDOT = -6769
073832
YDOT = -7133
251932 feet/sec YDOT = -2250
124795 meter/sec
ZDOT = -9061
052508 ZDOT = -2794
785830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8458530
53 X = -2578160
10
Y = -13656671
01 feet Y = -4162553
32 meter
Z = 15428439
27 Z = 4702588
29
XDOT = 12702
886200 XDOT = 3871
839714
YDOT = -18344
477941 feet/sec YDOT = -5591
396876 meter/sec
ZDOT = -9197
484211 ZDOT = -2803
393188
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 12338
54335831
00016717 00000-0 10270-3 0 9141
2 25544 51
6475
2343 0016590 358
9540 1
1574 15
51888590 4324
Satellite: ISS
Catalog Number: 25544
Epoch time: 12338
54335831 = yrday
fracday
Element set: 914
Inclination: 51
6475 deg
RA of node:
2343 deg
Eccentricity:
0016590
Arg of perigee: 358
9540 deg
Mean anomaly: 1
1574 deg
Mean motion: 15
51888590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 299
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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