[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 11th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 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
348/14:31:55
240 -1
0 1
4 1
4
N/A 0
9 0
1 230
4
000/00:07:50
479 -0
4 0
3 213
3
Coasting Arc #1 (Orbit 543)
---------------------------------------
Vector Time (GMT): 2012/345/17:12:47
095
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3469395
46 A = 6792518
53 meter
Y = 5178820
04 meter E =
0023563
Z = 2699027
44 I = 51
45433
XDOT = -5574
253269 Wp = 58
45645
YDOT = -1024
969568 meter/sec RA = 323
99926 deg
ZDOT = -5153
175340 TA = 91
01064
MA = 90
74066
Ha = 229
659 n
mi
Hp = 213
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11382531
03 X = -3540159
74
Y = 16990879
39 feet Y = 5139627
20 meter
Z = 8855076
90 Z = 2682001
53
XDOT = -18288
232510 XDOT = -5537
344162
YDOT = -3362
761051 feet/sec YDOT = -1087
097555 meter/sec
ZDOT = -16906
743242 ZDOT = -5180
165707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17123713
84 X = -5219307
98
Y = 11237781
77 feet Y = 3425275
88 meter
Z = 8783795
73 Z = 2677300
94
XDOT = -14643
610597 XDOT = -4463
372510
YDOT = -8893
791340 feet/sec YDOT = -2710
827600 meter/sec
ZDOT = -17018
487317 ZDOT = -5187
234934
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 12345
75488246
00016717 00000-0 10270-3 0 9006
2 25544 51
6486 324
4129 0016539 24
8821 335
3125 15
51993870 5449
Satellite: ISS
Catalog Number: 25544
Epoch time: 12345
75488246 = yrday
fracday
Element set: 900
Inclination: 51
6486 deg
RA of node: 324
4129 deg
Eccentricity:
0016539
Arg of perigee: 24
8821 deg
Mean anomaly: 335
3125 deg
Mean motion: 15
51993870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 544
Checksum: 319
Coasting Arc #2 (Orbit 558)
---------------------------------------
Vector Time (GMT): 2012/346/17:12:47
095
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3861351
85 A = 6794076
30 meter
Y = -5273303
61 meter E =
0023856
Z = -1817375
80 I = 51
43655
XDOT = 4922
251964 Wp = 30
95157
YDOT = 1679
177305 meter/sec RA = 319
02119 deg
ZDOT = 5638
929449 TA = 309
01212
MA = 309
22430
Ha = 229
683 n
mi
Hp = 213
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12668477
18 X = 3928860
58
Y = -17300864
85 feet Y = -5229745
89 meter
Z = -5962519
04 Z = -1798453
86
XDOT = 16149
120616 XDOT = 4875
716169
YDOT = 5509
111892 feet/sec YDOT = 1733
960182 meter/sec
ZDOT = 18500
424700 ZDOT = 5662
729030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18220404
39 X = 5553579
26
Y = -11347456
70 feet Y = -3458704
80 meter
Z = -5883363
17 Z = -1793249
09
XDOT = 12015
574889 XDOT = 3662
347226
YDOT = 9741
529698 feet/sec YDOT = 2969
218252 meter/sec
ZDOT = 18598
854550 ZDOT = 5668
930867
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 12346
72073027
00016717 00000-0 10270-3 0 9012
2 25544 51
6494 319
6135 0016565 28
0654 332
1387 15
52028703 5596
Satellite: ISS
Catalog Number: 25544
Epoch time: 12346
72073027 = yrday
fracday
Element set: 901
Inclination: 51
6494 deg
RA of node: 319
6135 deg
Eccentricity:
0016565
Arg of perigee: 28
0654 deg
Mean anomaly: 332
1387 deg
Mean motion: 15
52028703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 559
Checksum: 302
Coasting Arc #3 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2012/347/17:12:47
095
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4219519
05 A = 6795240
64 meter
Y = 5270174
81 meter E =
0020300
Z = 790797
25 I = 51
41797
XDOT = -4195
658562 Wp = 72
38298
YDOT = -2451
597705 meter/sec RA = 314
04412 deg
ZDOT = -5916
747715 TA = 99
05821
MA = 98
82844
Ha = 229
769 n
mi
Hp = 213
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13843566
43 X = -4281979
19
Y = 17290599
77 feet Y = 5222640
17 meter
Z = 2594479
17 Z = 770147
79
XDOT = -13765
283995 XDOT = -4139
189953
YDOT = -8043
299556 feet/sec YDOT = -2498
199671 meter/sec
ZDOT = -19411
901952 ZDOT = -5936
993392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19097866
61 X = -5821029
74
Y = 11239266
80 feet Y = 3425728
52 meter
Z = 2508160
00 Z = 764487
17
XDOT = -9078
136132 XDOT = -2767
015893
YDOT = -10975
077962 feet/sec YDOT = -3345
203763 meter/sec
ZDOT = -19495
498196 ZDOT = -5942
227850
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 12347
75095961
00016717 00000-0 10270-3 0 9028
2 25544 51
6494 314
4937 0016496 32
1191 328
0962 15
52010204 5752
Satellite: ISS
Catalog Number: 25544
Epoch time: 12347
75095961 = yrday
fracday
Element set: 902
Inclination: 51
6494 deg
RA of node: 314
4937 deg
Eccentricity:
0016496
Arg of perigee: 32
1191 deg
Mean anomaly: 328
0962 deg
Mean motion: 15
52010204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 304
Coasting Arc #4 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2012/348/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1299436
46 A = 6786050
04 meter
Y = 4535793
81 meter E =
0023609
Z = 4869347
21 I = 51
36559
XDOT = -5942
763614 Wp = 44
06277
YDOT = 4245
258736 meter/sec RA = 309
58887 deg
ZDOT = -2345
028998 TA = 69
10329
MA = 68
85071
Ha = 230
426 n
mi
Hp = 213
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4263242
98 X = 1224965
41
Y = 14881213
30 feet Y = 4549907
86 meter
Z = 15975548
60 Z = 4875479
58
XDOT = -19497
255953 XDOT = -5978
401646
YDOT = 13928
014225 feet/sec YDOT = 4178
604099 meter/sec
ZDOT = -7693
664690 ZDOT = -2373
984762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10644223
04 X = -3244359
18
Y = 11204149
07 feet Y = 3415024
64 meter
Z = 16000358
19 Z = 4876909
18
XDOT = -21110
663173 XDOT = -6434
530135
YDOT = -8786
173440 feet/sec YDOT = -2678
025665 meter/sec
ZDOT = -7814
282154 ZDOT = -2381
793200
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 12348
65241105
00016717 00000-0 10270-3 0 9032
2 25544 51
6483 310
0137 0017060 38
5707 321
6660 15
51792945 5892
Satellite: ISS
Catalog Number: 25544
Epoch time: 12348
65241105 = yrday
fracday
Element set: 903
Inclination: 51
6483 deg
RA of node: 310
0137 deg
Eccentricity:
0017060
Arg of perigee: 38
5707 deg
Mean anomaly: 321
6660 deg
Mean motion: 15
51792945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 298
Coasting Arc #5 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2012/349/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -837915
83 A = 6787689
12 meter
Y = -5061344
40 meter E =
0022233
Z = -4456569
99 I = 51
35308
XDOT = 5788
088901 Wp = 64
66419
YDOT = -3805
731783 meter/sec RA = 304
59751 deg
ZDOT = 3256
006639 TA = 238
22902
MA = 238
44581
Ha = 230
473 n
mi
Hp = 213
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2749067
67 X = -759607
59
Y = -16605460
62 feet Y = -5070276
07 meter
Z = -14621292
61 Z = -4460450
99
XDOT = 18989
792982 XDOT = 5814
398309
YDOT = -12485
996662 feet/sec YDOT = -3740
859078 meter/sec
ZDOT = 10682
436480 ZDOT = 3284
188244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12708893
75 X = 3873670
82
Y = -11015071
72 feet Y = -3357393
86 meter
Z = -14636704
13 Z = -4461267
42
XDOT = 19782
967914 XDOT = 6029
848620
YDOT = 8570
609090 feet/sec YDOT = 2612
321651 meter/sec
ZDOT = 10799
787422 ZDOT = 3291
775206
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 12349
61839390
00016717 00000-0 10270-3 0 9049
2 25544 51
6489 305
2153 0017077 42
0648 318
1812 15
51805468 6047
Satellite: ISS
Catalog Number: 25544
Epoch time: 12349
61839390 = yrday
fracday
Element set: 904
Inclination: 51
6489 deg
RA of node: 305
2153 deg
Eccentricity:
0017077
Arg of perigee: 42
0648 deg
Mean anomaly: 318
1812 deg
Mean motion: 15
51805468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 604
Checksum: 310
Coasting Arc #6 (Orbit 619)
---------------------------------------
Vector Time (GMT): 2012/350/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 351573
40 A = 6789855
70 meter
Y = 5587100
43 meter E =
0027086
Z = 3832995
60 I = 51
34369
XDOT = -5614
566365 Wp = 60
03117
YDOT = 3205
749149 meter/sec RA = 299
60757 deg
ZDOT = -4122
576466 TA = 73
62813
MA = 73
33051
Ha = 230
551 n
mi
Hp = 212
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1153456
03 X = 270451
45
Y = 18330382
00 feet Y = 5590577
94 meter
Z = 12575444
89 Z = 3834507
11
XDOT = -18420
493324 XDOT = -5629
970040
YDOT = 10517
549702 feet/sec YDOT = 3142
877897 meter/sec
ZDOT = -13525
513340 ZDOT = -4149
888634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14824889
88 X = -4518626
43
Y = 10835911
98 feet Y = 3302785
97 meter
Z = 12580970
99 Z = 3834679
96
XDOT = -17983
761278 XDOT = -5481
450438
YDOT = -8634
162756 feet/sec YDOT = -2631
692808 meter/sec
ZDOT = -13639
179837 ZDOT = -4157
222014
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 12350
64876638
00016717 00000-0 10270-3 0 9051
2 25544 51
6487 300
0971 0017077 45
9823 314
2732 15
51812093 6201
Satellite: ISS
Catalog Number: 25544
Epoch time: 12350
64876638 = yrday
fracday
Element set: 905
Inclination: 51
6487 deg
RA of node: 300
0971 deg
Eccentricity:
0017077
Arg of perigee: 45
9823 deg
Mean anomaly: 314
2732 deg
Mean motion: 15
51812093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 620
Checksum: 306
Coasting Arc #7 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2012/351/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -26102
28 A = 6791756
39 meter
Y = -6012154
62 meter E =
0021178
Z = -3160079
96 I = 51
33674
XDOT = 5395
666385 Wp = 54
96610
YDOT = -2533
986266 meter/sec RA = 294
61994 deg
ZDOT = 4811
282180 TA = 268
46074
MA = 268
70335
Ha = 230
538 n
mi
Hp = 212
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -85637
42 X = 56479
65
Y = -19724916
73 feet Y = -6011984
49 meter
Z = -10367716
42 Z = -3160006
72
XDOT = 17702
317536 XDOT = 5400
229026
YDOT = -8313
603235 feet/sec YDOT = -2473
623472 meter/sec
ZDOT = 15785
046523 ZDOT = 4837
504702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16381458
46 X = 4993068
54
Y = -10988634
84 feet Y = -3349335
90 meter
Z = -10366626
29 Z = -3159747
69
XDOT = 15898
037380 XDOT = 4845
721794
YDOT = 8813
699137 feet/sec YDOT = 2686
415497 meter/sec
ZDOT = 15894
105577 ZDOT = 4844
523380
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 12351
61473099
00016717 00000-0 10270-3 0 9064
2 25544 51
6493 295
2990 0017068 49
3723 310
8910 15
51841482 6351
Satellite: ISS
Catalog Number: 25544
Epoch time: 12351
61473099 = yrday
fracday
Element set: 906
Inclination: 51
6493 deg
RA of node: 295
2990 deg
Eccentricity:
0017068
Arg of perigee: 49
3723 deg
Mean anomaly: 310
8910 deg
Mean motion: 15
51841482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 319
Coasting Arc #8 (Orbit 650)
---------------------------------------
Vector Time (GMT): 2012/352/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -326188
77 A = 6793800
11 meter
Y = 6381437
27 meter E =
0027507
Z = 2295541
96 I = 51
33118
XDOT = -5181
801075 Wp = 77
17814
YDOT = 1694
827997 meter/sec RA = 289
63418 deg
ZDOT = -5387
052813 TA = 77
16187
MA = 76
85469
Ha = 230
628 n
mi
Hp = 212
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1070173
13 X = -408674
23
Y = 20936473
97 feet Y = 6377328
26 meter
Z = 7531305
64 Z = 2293757
45
XDOT = -17000
659694 XDOT = -5174
199016
YDOT = 5560
459308 feet/sec YDOT = 1636
924732 meter/sec
ZDOT = -17674
057786 ZDOT = -5412
206971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17834291
92 X = -5435892
18
Y = 11024655
49 feet Y = 3360314
99 meter
Z = 7523083
19 Z = 2293035
76
XDOT = -13396
757485 XDOT = -4083
331681
YDOT = -9403
526715 feet/sec YDOT = -2866
194943 meter/sec
ZDOT = -17778
576692 ZDOT = -5418
910176
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 12352
64508459
00016717 00000-0 10270-3 0 9078
2 25544 51
6489 290
1803 0017064 53
3278 306
9439 15
51831093 6516
Satellite: ISS
Catalog Number: 25544
Epoch time: 12352
64508459 = yrday
fracday
Element set: 907
Inclination: 51
6489 deg
RA of node: 290
1803 deg
Eccentricity:
0017064
Arg of perigee: 53
3278 deg
Mean anomaly: 306
9439 deg
Mean motion: 15
51831093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 651
Checksum: 318
Coasting Arc #9 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2012/353/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 533562
09 A = 6795020
53 meter
Y = -6611116
23 meter E =
0025198
Z = -1444106
07 I = 51
32675
XDOT = 4986
732329 Wp = 50
12436
YDOT = -838
282350 meter/sec RA = 284
65012 deg
ZDOT = 5762
964846 TA = 294
06278
MA = 294
32623
Ha = 230
577 n
mi
Hp = 212
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1750531
81 X = 614464
43
Y = -21690013
87 feet Y = -6604697
17 meter
Z = -4737880
82 Z = -1441317
92
XDOT = 16360
670371 XDOT = 4967
740560
YDOT = -2750
270178 feet/sec YDOT = -782
624089 meter/sec
ZDOT = 18907
364980 ZDOT = 5787
143830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18640888
35 X = 5681742
77
Y = -11231906
12 feet Y = -3423484
98 meter
Z = -4725478
19 Z = -1440325
75
XDOT = 10904
800109 XDOT = 3323
783073
YDOT = 10215
729732 feet/sec YDOT = 3113
754422 meter/sec
ZDOT = 19007
730017 ZDOT = 5793
556109
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 12353
61103096
00016717 00000-0 10270-3 0 9085
2 25544 51
6493 285
3820 0017036 56
4432 303
8344 15
51869895 6669
Satellite: ISS
Catalog Number: 25544
Epoch time: 12353
61103096 = yrday
fracday
Element set: 908
Inclination: 51
6493 deg
RA of node: 285
3820 deg
Eccentricity:
0017036
Arg of perigee: 56
4432 deg
Mean anomaly: 303
8344 deg
Mean motion: 15
51869895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 318
Coasting Arc #10 (Orbit 681)
---------------------------------------
Vector Time (GMT): 2012/354/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -786902
67 A = 6795887
31 meter
Y = 6734209
34 meter E =
0024589
Z = 443605
86 I = 51
32241
XDOT = -4812
292496 Wp = 89
73654
YDOT = -150
919451 meter/sec RA = 279
66717 deg
ZDOT = -5957
834330 TA = 85
46614
MA = 85
18529
Ha = 230
657 n
mi
Hp = 212
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2581701
69 X = -864302
46
Y = 22093862
67 feet Y = 6724976
92 meter
Z = 1455399
80 Z = 439595
45
XDOT = -15788
361206 XDOT = -4781
305524
YDOT = -495
142556 feet/sec YDOT = -204
559977 meter/sec
ZDOT = -19546
700559 ZDOT = -5981
136878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19253532
25 X = -5868476
63
Y = 11142531
73 feet Y = 3396243
67 meter
Z = 1437923
06 Z = 438278
95
XDOT = -8163
395475 XDOT = -2488
202941
YDOT = -11447
638114 feet/sec YDOT = -3489
240097 meter/sec
ZDOT = -19643
306983 ZDOT = -5987
279968
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 12354
64136575
00016717 00000-0 10270-3 0 9098
2 25544 51
6491 280
2630 0016980 60
5893 299
6951 15
51846112 6825
Satellite: ISS
Catalog Number: 25544
Epoch time: 12354
64136575 = yrday
fracday
Element set: 909
Inclination: 51
6491 deg
RA of node: 280
2630 deg
Eccentricity:
0016980
Arg of perigee: 60
5893 deg
Mean anomaly: 299
6951 deg
Mean motion: 15
51846112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 682
Checksum: 327
Coasting Arc #11 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2012/355/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 932715
00 A = 6795744
42 meter
Y = -6701992
84 meter E =
0029728
Z = 477514
04 I = 51
31823
XDOT = 4700
803852 Wp = 57
68832
YDOT = 1097
407262 meter/sec RA = 274
68402 deg
ZDOT = 5963
711180 TA = 307
48543
MA = 307
75538
Ha = 230
594 n
mi
Hp = 212
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3060088
57 X = 1005269
12
Y = -21988165
48 feet Y = -6691156
99 meter
Z = 1566647
12 Z = 482221
03
XDOT = 15422
584815 XDOT = 4659
212711
YDOT = 3600
417527 feet/sec YDOT = 1149
741753 meter/sec
ZDOT = 19565
981562 ZDOT = 5986
446476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19256642
42 X = 5869424
61
Y = -11043599
91 feet Y = -3366089
25 meter
Z = 1587000
44 Z = 483717
73
XDOT = 5710
534072 XDOT = 1740
570785
YDOT = 12902
083060 feet/sec YDOT = 3932
554917 meter/sec
ZDOT = 19660
119652 ZDOT = 5992
404470
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 12355
67168922
00016717 00000-0 10270-3 0 9105
2 25544 51
6491 275
1444 0017000 63
6271 296
6624 15
51893753 6983
Satellite: ISS
Catalog Number: 25544
Epoch time: 12355
67168922 = yrday
fracday
Element set: 910
Inclination: 51
6491 deg
RA of node: 275
1444 deg
Eccentricity:
0017000
Arg of perigee: 63
6271 deg
Mean anomaly: 296
6624 deg
Mean motion: 15
51893753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 698
Checksum: 322
Coasting Arc #12 (Orbit 712)
---------------------------------------
Vector Time (GMT): 2012/356/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1154497
26 A = 6794941
72 meter
Y = 6533525
02 meter E =
0020643
Z = -1484417
20 I = 51
31386
XDOT = -4607
362175 Wp = 90
28039
YDOT = -2102
439854 meter/sec RA = 269
70033 deg
ZDOT = -5739
967938 TA = 105
96248
MA = 105
73495
Ha = 230
628 n
mi
Hp = 212
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3787720
68 X = -1220259
74
Y = 21435449
55 feet Y = 6520247
10 meter
Z = -4870135
19 Z = -1490185
07
XDOT = -15116
017634 XDOT = -4555
626322
YDOT = -6897
768550 feet/sec YDOT = -2153
672663 meter/sec
ZDOT = -18831
915807 ZDOT = -5762
224775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19074813
21 X = -5814003
07
Y = 10475465
69 feet Y = 3192921
94 meter
Z = -4894860
73 Z = -1491953
55
XDOT = -3235
487134 XDOT = -986
176478
YDOT = -14627
889032 feet/sec YDOT = -4458
580577 meter/sec
ZDOT = -18923
949171 ZDOT = -5768
019707
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 12356
63761030
00016717 00000-0 10270-3 0 9112
2 25544 51
6491 270
3452 0016852 67
5260 292
7674 15
51872817 7132
Satellite: ISS
Catalog Number: 25544
Epoch time: 12356
63761030 = yrday
fracday
Element set: 911
Inclination: 51
6491 deg
RA of node: 270
3452 deg
Eccentricity:
0016852
Arg of perigee: 67
5260 deg
Mean anomaly: 292
7674 deg
Mean motion: 15
51872817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 713
Checksum: 308
Coasting Arc #13 (Orbit 728)
---------------------------------------
Vector Time (GMT): 2012/357/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1315509
93 A = 6793439
69 meter
Y = -6220348
79 meter E =
0030736
Z = 2351144
27 I = 51
30994
XDOT = 4591
562581 Wp = 71
72118
YDOT = 3015
981239 meter/sec RA = 264
71425 deg
ZDOT = 5361
939563 TA = 314
66131
MA = 314
91142
Ha = 230
600 n
mi
Hp = 212
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4315977
45 X = 1373548
05
Y = -20407968
48 feet Y = -6205313
59 meter
Z = 7713727
93 Z = 2357675
52
XDOT = 15064
181696 XDOT = 4531
448835
YDOT = 9894
951572 feet/sec YDOT = 3066
990478 meter/sec
ZDOT = 17591
665234 ZDOT = 5384
099416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18427426
35 X = 5616679
55
Y = -9752558
32 feet Y = -2972579
78 meter
Z = 7741576
17 Z = 2359632
42
XDOT = 1229
062617 XDOT = 374
618286
YDOT = 16484
504589 feet/sec YDOT = 5024
476999 meter/sec
ZDOT = 17683
189677 ZDOT = 5389
836214
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 12357
66791639
00016717 00000-0 10270-3 0 9125
2 25544 51
6488 265
2263 0016961 70
5586 289
7396 15
51909627 7291
Satellite: ISS
Catalog Number: 25544
Epoch time: 12357
66791639 = yrday
fracday
Element set: 912
Inclination: 51
6488 deg
RA of node: 265
2263 deg
Eccentricity:
0016961
Arg of perigee: 70
5586 deg
Mean anomaly: 289
7396 deg
Mean motion: 15
51909627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 729
Checksum: 360
Coasting Arc #14 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2012/358/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1581637
29 A = 6791350
35 meter
Y = 5774080
64 meter E =
0021041
Z = -3228765
87 I = 51
30644
XDOT = -4567
253673 Wp = 79
49844
YDOT = -3891
247419 meter/sec RA = 259
72583 deg
ZDOT = -4744
246618 TA = 137
95935
MA = 137
79770
Ha = 230
583 n
mi
Hp = 212
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5189098
73 X = -1630402
07
Y = 18943834
12 feet Y = 5756121
40 meter
Z = -10593063
89 Z = -3236567
38
XDOT = -14984
428060 XDOT = -4500
354941
YDOT = -12766
559772 feet/sec YDOT = -3941
946856 meter/sec
ZDOT = -15565
113576 ZDOT = -4766
272017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17704279
98 X = -5396264
54
Y = 8464785
42 feet Y = 2580066
59 meter
Z = -10626122
42 Z = -3238842
11
XDOT = 591
838061 XDOT = 180
392241
YDOT = -18322
257216 feet/sec YDOT = -5584
623999 meter/sec
ZDOT = -15655
981023 ZDOT = -4771
943016
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 12358
63381981
00016717 00000-0 10270-3 0 9139
2 25544 51
6484 260
4271 0016776 74
3420 285
9581 15
51911963 7443
Satellite: ISS
Catalog Number: 25544
Epoch time: 12358
63381981 = yrday
fracday
Element set: 913
Inclination: 51
6484 deg
RA of node: 260
4271 deg
Eccentricity:
0016776
Arg of perigee: 74
3420 deg
Mean anomaly: 285
9581 deg
Mean motion: 15
51911963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 326
Coasting Arc #15 (Orbit 759)
---------------------------------------
Vector Time (GMT): 2012/359/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1829009
77 A = 6789208
22 meter
Y = -5215769
25 meter E =
0027500
Z = 3917334
42 I = 51
30541
XDOT = 4604
873854 Wp = 86
35706
YDOT = 4649
411395 meter/sec RA = 254
73422 deg
ZDOT = 4017
766216 TA = 321
44833
MA = 321
64441
Ha = 230
597 n
mi
Hp = 212
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6000688
22 X = 1868168
11
Y = -17112103
85 feet Y = -5195097
56 meter
Z = 12852147
05 Z = 3926314
28
XDOT = 15107
853851 XDOT = 4533
023487
YDOT = 15253
974392 feet/sec YDOT = 4700
503844 meter/sec
ZDOT = 13181
647690 ZDOT = 4039
962447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16718137
96 X = 5095688
45
Y = -6954222
57 feet Y = -2119647
04 meter
Z = 12890022
98 Z = 3928879
01
XDOT = -1910
315367 XDOT = -582
264124
YDOT = 20147
727158 feet/sec YDOT = 6141
027238 meter/sec
ZDOT = 13273
141277 ZDOT = 4045
653461
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 12359
66410940
00016717 00000-0 10270-3 0 9142
2 25544 51
6481 255
3080 0016929 77
6635 282
6410 15
51919922 7601
Satellite: ISS
Catalog Number: 25544
Epoch time: 12359
66410940 = yrday
fracday
Element set: 914
Inclination: 51
6481 deg
RA of node: 255
3080 deg
Eccentricity:
0016929
Arg of perigee: 77
6635 deg
Mean anomaly: 282
6410 deg
Mean motion: 15
51919922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 760
Checksum: 317
Coasting Arc #16 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2012/360/14:35:50
479
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2195955
86 A = 6786938
14 meter
Y = 4562724
26 meter E =
0026444
Z = -4544591
02 I = 51
30595
XDOT = -4586
862830 Wp = 77
19772
YDOT = -5276
691696 meter/sec RA = 249
73916 deg
ZDOT = -3090
917229 TA = 161
64832
MA = 161
55273
Ha = 230
551 n
mi
Hp = 211
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7204579
61 X = -2224737
43
Y = 14969567
79 feet Y = 4538007
28 meter
Z = -14910075
51 Z = -4555328
27
XDOT = -15048
762566 XDOT = -4512
501884
YDOT = -17311
980631 feet/sec YDOT = -5327
568753 meter/sec
ZDOT = -10140
804556 ZDOT = -3113
019936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15827574
14 X = -4824244
60
Y = 4912772
68 feet Y = 1497413
11 meter
Z = -14955160
99 Z = -4558333
07
XDOT = 2934
348734 XDOT = 894
389494
YDOT = -21598
392035 feet/sec YDOT = -6583
189892 meter/sec
ZDOT = -10231
846677 ZDOT = -3118
666867
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 12360
62999581
00016717 00000-0 10270-3 0 9154
2 25544 51
6469 250
5085 0016750 81
4323 278
8726 15
51947111 7752
Satellite: ISS
Catalog Number: 25544
Epoch time: 12360
62999581 = yrday
fracday
Element set: 915
Inclination: 51
6469 deg
RA of node: 250
5085 deg
Eccentricity:
0016750
Arg of perigee: 81
4323 deg
Mean anomaly: 278
8726 deg
Mean motion: 15
51947111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 330
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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