[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 15th 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) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
228/16:15:37
564 -4
5 9
4 9
4
N/A -5
5 0
2 225
2
000/00:31:11
128 6
2 -0
2 217
3
235/13:49:10
282 1
4 9
3 9
3
N/A -6
8 0
2 232
9
000/00:28:20
563 6
2 -0
3 216
3
Coasting Arc #1 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2012/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6241220
52 A = 6785998
72 meter
Y = -2465479
78 meter E =
0015091
Z = 957390
37 I = 51
56110
XDOT = 2561
846968 Wp = 53
34813
YDOT = -4168
500283 meter/sec RA = 195
05368 deg
ZDOT = 5910
096721 TA = 317
04026
MA = 317
15801
Ha = 219
812 n
mi
Hp = 212
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20476445
27 X = -6217837
87
Y = -8088844
44 feet Y = -2535142
29 meter
Z = 3141044
53 Z = 927127
96
XDOT = 8405
009739 XDOT = 2579
560131
YDOT = -13676
182032 feet/sec YDOT = -4139
753335 meter/sec
ZDOT = 19390
081107 ZDOT = 5922
584707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11011569
68 X = 3356326
44
Y = 19084749
78 feet Y = 5817031
73 meter
Z = 3016294
93 Z = 919366
70
XDOT = -13604
013524 XDOT = -4146
503322
YDOT = 4746
389531 feet/sec YDOT = 1446
699529 meter/sec
ZDOT = 19441
991804 ZDOT = 5925
919102
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 12226
56248517
00016717 00000-0 10270-3 0 9008
2 25544 51
6376 195
8023 0001683 36
9779 323
1490 15
55152971 26941
Satellite: ISS
Catalog Number: 25544
Epoch time: 12226
56248517 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 195
8023 deg
Eccentricity:
0001683
Arg of perigee: 36
9779 deg
Mean anomaly: 323
1490 deg
Mean motion: 15
55152971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 323
Coasting Arc #2 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2012/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5218433
07 A = 6782943
75 meter
Y = 3243795
59 meter E =
0005231
Z = -2876602
41 I = 51
58125
XDOT = -4781
063298 Wp = 97
17797
YDOT = 3219
805850 meter/sec RA = 190
06875 deg
ZDOT = -5051
030142 TA = 115
58504
MA = 115
53097
Ha = 219
890 n
mi
Hp = 212
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17120843
39 X = 5195746
05
Y = 10642373
98 feet Y = 3302024
60 meter
Z = -9437671
95 Z = -2851306
96
XDOT = -15685
903208 XDOT = -4792
176182
YDOT = 10563
667488 feet/sec YDOT = 3166
279060 meter/sec
ZDOT = -16571
621200 ZDOT = -5074
282788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7152401
05 X = -2180051
84
Y = -18899268
84 feet Y = -5760497
14 meter
Z = -9333480
09 Z = -2844844
73
XDOT = 17415
914558 XDOT = 5308
370757
YDOT = 1626
511219 feet/sec YDOT = 495
760619 meter/sec
ZDOT = -16667
910495 ZDOT = -5080
379119
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 12227
52639626
00016717 00000-0 10270-3 0 9011
2 25544 51
6383 190
9888 0001907 34
6134 325
5143 15
55143424 27094
Satellite: ISS
Catalog Number: 25544
Epoch time: 12227
52639626 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 190
9888 deg
Eccentricity:
0001907
Arg of perigee: 34
6134 deg
Mean anomaly: 325
5143 deg
Mean motion: 15
55143424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 309
Coasting Arc #3 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2012/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3576555
58 A = 6778305
07 meter
Y = -3772797
37 meter E =
0010360
Z = 4341872
82 I = 51
59692
XDOT = 6498
236655 Wp = 99
48417
YDOT = -2173
153738 meter/sec RA = 185
07382 deg
ZDOT = 3455
801643 TA = 315
40011
MA = 315
48342
Ha = 219
825 n
mi
Hp = 212
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11734106
23 X = -3555192
97
Y = -12377944
14 feet Y = -3812673
26 meter
Z = 14244989
56 Z = 4324550
26
XDOT = 21319
674065 XDOT = 6505
267187
YDOT = -7129
769483 feet/sec YDOT = -2100
447158 meter/sec
ZDOT = 11337
931898 ZDOT = 3487
386177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2138044
82 X = 651676
06
Y = 16981046
53 feet Y = 5175822
98 meter
Z = 14173753
93 Z = 4320160
20
XDOT = -20083
247485 XDOT = -6121
373834
YDOT = -7067
898883 feet/sec YDOT = -2154
295580 meter/sec
ZDOT = 11468
556149 ZDOT = 3495
615914
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 12228
55455244
00016717 00000-0 10270-3 0 9028
2 25544 51
6388 185
8556 0001694 36
0867 324
0400 15
55191437 27251
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
55455244 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 185
8556 deg
Eccentricity:
0001694
Arg of perigee: 36
0867 deg
Mean anomaly: 324
0400 deg
Mean motion: 15
55191437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 313
Coasting Arc #4 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2012/228/16:31:13
128
Vector Time (MET): N/A
Weight (LBS) : 953367
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5704370
18 A = 6791100
05 meter
Y = -2523170
22 meter E =
0015763
Z = 2658714
23 I = 51
62178
XDOT = 4126
612066 Wp = 37
47972
YDOT = -3837
326346 meter/sec RA = 184
13162 deg
ZDOT = 5208
101590 TA = 352
53276
MA = 352
55621
Ha = 225
222 n
mi
Hp = 217
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18715125
27 X = -5688646
78
Y = -8278117
52 feet Y = -2586872
15 meter
Z = 8722815
70 Z = 2631041
39
XDOT = 13538
753496 XDOT = 4143
915888
YDOT = -12589
653367 feet/sec YDOT = -3791
083311 meter/sec
ZDOT = 17086
947473 ZDOT = 5228
190054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20328289
92 X = 6196062
77
Y = -2742461
76 feet Y = -835902
35 meter
Z = 8608727
55 Z = 2623940
16
XDOT = -5082
150345 XDOT = -1549
039425
YDOT = 16268
938366 feet/sec YDOT = 4958
772414 meter/sec
ZDOT = 17170
228974 ZDOT = 5233
485791
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 12228
74744075
00016717 00000-0 10270-3 0 9033
2 25544 51
6412 184
8944 0010286 338
8421 21
2304 15
52518001 27284
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
74744075 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 184
8944 deg
Eccentricity:
0010286
Arg of perigee: 338
8421 deg
Mean anomaly: 21
2304 deg
Mean motion: 15
52518001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 291
Coasting Arc #5 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2012/229/16:31:13
128
Vector Time (MET): N/A
Weight (LBS) : 953367
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5023958
43 A = 6788499
29 meter
Y = 2793393
00 meter E =
0010560
Z = -3622581
94 I = 51
64421
XDOT = -5156
782234 Wp = 10
87147
YDOT = 3557
878124 meter/sec RA = 179
16081 deg
ZDOT = -4400
121736 TA = 211
96424
MA = 212
02835
Ha = 225
220 n
mi
Hp = 217
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16482803
23 X = 5009946
05
Y = 9164675
20 feet Y = 2849495
64 meter
Z = -11885111
34 Z = -3598210
36
XDOT = -16918
576884 XDOT = -5174
809555
YDOT = 11672
828490 feet/sec YDOT = 3500
110927 meter/sec
ZDOT = -14436
094934 ZDOT = -4425
216449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18886910
61 X = -5756730
35
Y = 1155936
85 feet Y = 352329
55 meter
Z = -11784666
45 Z = -3591966
33
XDOT = 8017
616286 XDOT = 2443
769444
YDOT = -17505
108253 feet/sec YDOT = -5335
556995 meter/sec
ZDOT = -14540
038624 ZDOT = -4431
803773
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 12229
71295743
00016717 00000-0 10270-3 0 9045
2 25544 51
6417 180
0926 0010293 341
0328 19
0439 15
52541278 27430
Satellite: ISS
Catalog Number: 25544
Epoch time: 12229
71295743 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 180
0926 deg
Eccentricity:
0010293
Arg of perigee: 341
0328 deg
Mean anomaly: 19
0439 deg
Mean motion: 15
52541278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 299
Coasting Arc #6 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2012/230/16:31:13
128
Vector Time (MET): N/A
Weight (LBS) : 953367
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4139358
56 A = 6785786
16 meter
Y = -3076142
00 meter E =
0009421
Z = 4400598
63 I = 51
66604
XDOT = 6043
791764 Wp = 43
39782
YDOT = -3301
477893 meter/sec RA = 174
18618 deg
ZDOT = 3379
575540 TA = 12
44513
MA = 12
42188
Ha = 225
462 n
mi
Hp = 216
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13580572
69 X = -4126029
55
Y = -10092329
41 feet Y = -3122356
21 meter
Z = 14437659
54 Z = 4380522
69
XDOT = 19828
713137 XDOT = 6063
843495
YDOT = -10831
620384 feet/sec YDOT = -3233
780220 meter/sec
ZDOT = 11087
846259 ZDOT = 3408
984241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16967192
50 X = 5171600
28
Y = 884460
67 feet Y = 269583
61 meter
Z = 14354970
86 Z = 4375395
12
XDOT = -10451
510859 XDOT = -3185
620510
YDOT = 18692
627771 feet/sec YDOT = 5697
512945 meter/sec
ZDOT = 11209
598004 ZDOT = 3416
685472
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 12230
74283197
00016717 00000-0 10270-3 0 9051
2 25544 51
6421 174
9697 0010324 345
9193 14
1669 15
52555085 27599
Satellite: ISS
Catalog Number: 25544
Epoch time: 12230
74283197 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 174
9697 deg
Eccentricity:
0010324
Arg of perigee: 345
9193 deg
Mean anomaly: 14
1669 deg
Mean motion: 15
52555085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 324
Coasting Arc #7 (Orbit 2773)
---------------------------------------
Vector Time (GMT): 2012/231/16:31:13
128
Vector Time (MET): N/A
Weight (LBS) : 953367
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3159147
93 A = 6783449
03 meter
Y = 3391893
95 meter E =
0016726
Z = -4965820
58 I = 51
68856
XDOT = -6685
906001 Wp = 35
86135
YDOT = 3025
516099 meter/sec RA = 169
20931 deg
ZDOT = -2177
347206 TA = 212
83237
MA = 212
93639
Ha = 225
452 n
mi
Hp = 216
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10364658
58 X = 3145106
71
Y = 11128261
00 feet Y = 3427142
74 meter
Z = -16292062
29 Z = -4950508
13
XDOT = -21935
387142 XDOT = -6708
664152
YDOT = 9926
233921 feet/sec YDOT = 2950
622776 meter/sec
ZDOT = -7143
527578 ZDOT = -2209
881920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14922861
39 X = -4548488
15
Y = -3259007
01 feet Y = -993345
34 meter
Z = -16229070
07 Z = -4946620
56
XDOT = 12203
150609 XDOT = 3719
520306
YDOT = -19478
184900 feet/sec YDOT = -5936
950758 meter/sec
ZDOT = -7278
180635 ZDOT = -2218
389458
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 12231
70832606
00016717 00000-0 10270-3 0 9064
2 25544 51
6418 170
1675 0010408 348
4025 11
6877 15
52601102 27746
Satellite: ISS
Catalog Number: 25544
Epoch time: 12231
70832606 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 170
1675 deg
Eccentricity:
0010408
Arg of perigee: 348
4025 deg
Mean anomaly: 11
6877 deg
Mean motion: 15
52601102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2774
Checksum: 284
Coasting Arc #8 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2012/232/16:31:13
128
Vector Time (MET): N/A
Weight (LBS) : 953367
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2046630
77 A = 6782056
25 meter
Y = -3743983
83 meter E =
0008657
Z = 5269202
17 I = 51
71398
XDOT = 7123
517440 Wp = 10
69748
YDOT = -2708
953627 meter/sec RA = 164
23056 deg
ZDOT = 850
135568 TA = 71
23003
MA = 71
13613
Ha = 225
582 n
mi
Hp = 216
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6714667
87 X = -2030208
93
Y = -12283411
53 feet Y = -3766778
39 meter
Z = 17287408
71 Z = 5259299
98
XDOT = 23371
120210 XDOT = 7149
150369
YDOT = -8887
643132 feet/sec YDOT = -2629
150646 meter/sec
ZDOT = 2789
158689 ZDOT = 884
803277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12676993
78 X = 3863947
70
Y = 6055198
02 feet Y = 1845624
36 meter
Z = 17246793
00 Z = 5256822
51
XDOT = -13437
107805 XDOT = -4095
630459
YDOT = 19854
449833 feet/sec YDOT = 6051
636309 meter/sec
ZDOT = 2932
609041 ZDOT = 893
859236
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 12232
73817667
00016717 00000-0 10270-3 0 9079
2 25544 51
6421 165
0450 0010338 352
5259 7
5737 15
52601093 27907
Satellite: ISS
Catalog Number: 25544
Epoch time: 12232
73817667 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 165
0450 deg
Eccentricity:
0010338
Arg of perigee: 352
5259 deg
Mean anomaly: 7
5737 deg
Mean motion: 15
52601093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 300
Coasting Arc #9 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2012/233/16:31:13
128
Vector Time (MET): N/A
Weight (LBS) : 953367
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 951694
04 A = 6781758
64 meter
Y = 4120107
42 meter E =
0016799
Z = -5313383
77 I = 51
74124
XDOT = -7276
679766 Wp = 56
24623
YDOT = 2326
061080 meter/sec RA = 159
25177 deg
ZDOT = 510
592089 TA = 218
56560
MA = 218
68573
Ha = 225
626 n
mi
Hp = 216
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3122355
78 X = 931362
42
Y = 13517412
79 feet Y = 4130635
85 meter
Z = -17432361
46 Z = -5308810
16
XDOT = -23873
621280 XDOT = -7304
629762
YDOT = 7631
433990 feet/sec YDOT = 2244
532471 meter/sec
ZDOT = 1675
170895 ZDOT = 475
174572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10621485
37 X = -3237428
74
Y = -8961064
71 feet Y = -2731332
52 meter
Z = -17413791
89 Z = -5307723
77
XDOT = 14037
585031 XDOT = 4278
655917
YDOT = -19543
724023 feet/sec YDOT = -5956
927082 meter/sec
ZDOT = 1528
641915 ZDOT = 465
930056
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 12233
70364888
00016717 00000-0 10270-3 0 9080
2 25544 51
6410 160
2420 0010391 355
4939 4
6118 15
52641587 28055
Satellite: ISS
Catalog Number: 25544
Epoch time: 12233
70364888 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 160
2420 deg
Eccentricity:
0010391
Arg of perigee: 355
4939 deg
Mean anomaly: 4
6118 deg
Mean motion: 15
52641587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 299
Coasting Arc #10 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2012/234/16:31:13
128
Vector Time (MET): N/A
Weight (LBS) : 953367
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 184213
30 A = 6782757
02 meter
Y = -4513007
36 meter E =
0014144
Z = 5060121
93 I = 51
77295
XDOT = 7203
840064 Wp = 18
08174
YDOT = -1828
347727 meter/sec RA = 154
27602 deg
ZDOT = -1878
382582 TA = 90
17401
MA = 90
01193
Ha = 225
661 n
mi
Hp = 215
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 604374
35 X = 210084
17
Y = -14806454
61 feet Y = -4510802
46 meter
Z = 16601449
90 Z = 5061079
90
XDOT = 23634
645880 XDOT = 7232
874337
YDOT = -5998
516166 feet/sec YDOT = -1747
627662 meter/sec
ZDOT = -6162
672513 ZDOT = -1843
316194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8592272
51 X = 2618924
66
Y = 12067547
15 feet Y = 3678188
37 meter
Z = 16605772
01 Z = 5061439
31
XDOT = -14282
881456 XDOT = -4353
422268
YDOT = 18515
883716 feet/sec YDOT = 5643
641357 meter/sec
ZDOT = -6017
621942 ZDOT = -1834
171168
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 12234
73347394
00016717 00000-0 10270-3 0 9098
2 25544 51
6410 155
1194 0010367 358
7708 1
3416 15
52658721 28210
Satellite: ISS
Catalog Number: 25544
Epoch time: 12234
73347394 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 155
1194 deg
Eccentricity:
0010367
Arg of perigee: 358
7708 deg
Mean anomaly: 1
3416 deg
Mean motion: 15
52658721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 302
Coasting Arc #11 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2012/235/14:03:20
563
Vector Time (MET): N/A
Weight (LBS) : 952122
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2405557
56 A = 6788658
21 meter
Y = -3447725
60 meter E =
0018814
Z = 5322870
28 I = 51
79404
XDOT = 6495
568886 Wp = 24
23356
YDOT = -4064
824428 meter/sec RA = 149
84015 deg
ZDOT = 319
011400 TA = 62
82786
MA = 62
63619
Ha = 232
929 n
mi
Hp = 216
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7892249
21 X = -2392682
83
Y = -11311435
68 feet Y = -3474553
85 meter
Z = 17463485
17 Z = 5311215
62
XDOT = 21310
921541 XDOT = 6538
990144
YDOT = -13336
038150 feet/sec YDOT = -3991
944140 meter/sec
ZDOT = 1046
625329 ZDOT = 350
672124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8255778
03 X = 2516361
14
Y = 11124225
46 feet Y = 3390663
92 meter
Z = 17415602
96 Z = 5308275
78
XDOT = -20182
007146 XDOT = -6151
475778
YDOT = 13218
222545 feet/sec YDOT = 4028
914232 meter/sec
ZDOT = 1177
796912 ZDOT = 358
992499
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 12235
63466337
00016717 00000-0 10270-3 0 9109
2 25544 51
6415 150
6374 0018629 16
1233 344
0507 15
50263138 28357
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
63466337 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 150
6374 deg
Eccentricity:
0018629
Arg of perigee: 16
1233 deg
Mean anomaly: 344
0507 deg
Mean motion: 15
50263138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2835
Checksum: 290
Coasting Arc #12 (Orbit 2849)
---------------------------------------
Vector Time (GMT): 2012/236/14:03:20
563
Vector Time (MET): N/A
Weight (LBS) : 952122
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2297487
40 A = 6788602
25 meter
Y = 3523803
84 meter E =
0027324
Z = -5346102
80 I = 51
81934
XDOT = -6317
524667 Wp = 50
71216
YDOT = 4306
070023 meter/sec RA = 144
89255 deg
ZDOT = 140
637915 TA = 220
52659
MA = 220
73037
Ha = 232
998 n
mi
Hp = 216
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7537688
31 X = 2283882
85
Y = 11561036
23 feet Y = 3549419
62 meter
Z = -17539707
36 Z = -5334974
84
XDOT = -20726
786966 XDOT = -6365
889684
YDOT = 14127
526321 feet/sec YDOT = 4235
153109 meter/sec
ZDOT = 461
410481 ZDOT = 109
830181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8102114
58 X = -2469524
53
Y = -11244156
19 feet Y = -3427218
81 meter
Z = -17494008
37 Z = -5332173
75
XDOT = 19326
257368 XDOT = 5890
643246
YDOT = -14356
394387 feet/sec YDOT = -4375
829009 meter/sec
ZDOT = 333
726267 ZDOT = 101
719766
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 12236
60161102
00016717 00000-0 10270-3 0 9110
2 25544 51
6413 145
8447 0018688 19
4421 340
7438 15
50277252 28507
Satellite: ISS
Catalog Number: 25544
Epoch time: 12236
60161102 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 145
8447 deg
Eccentricity:
0018688
Arg of perigee: 19
4421 deg
Mean anomaly: 340
7438 deg
Mean motion: 15
50277252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2850
Checksum: 291
Coasting Arc #13 (Orbit 2865)
---------------------------------------
Vector Time (GMT): 2012/237/14:03:20
563
Vector Time (MET): N/A
Weight (LBS) : 952122
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2111293
96 A = 6788640
06 meter
Y = -3666922
10 meter E =
0020895
Z = 5301708
00 I = 51
84408
XDOT = 6164
161298 Wp = 28
67561
YDOT = -4515
636958 meter/sec RA = 139
94539 deg
ZDOT = -649
547024 TA = 67
61866
MA = 67
39740
Ha = 233
066 n
mi
Hp = 215
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6926817
45 X = -2095887
16
Y = -12030584
33 feet Y = -3690445
78 meter
Z = 17394055
10 Z = 5291488
88
XDOT = 20223
626306 XDOT = 6217
353288
YDOT = -14815
081884 feet/sec YDOT = -4446
408056 meter/sec
ZDOT = -2131
059791 ZDOT = -619
472738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7710481
30 X = 2350154
70
Y = 11606944
53 feet Y = 3537796
69 meter
Z = 17352124
63 Z = 5288927
59
XDOT = -18508
197903 XDOT = -5641
298721
YDOT = 15387
585052 feet/sec YDOT = 4690
135924 meter/sec
ZDOT = -2006
369841 ZDOT = -611
541527
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 12237
63300954
00016717 00000-0 10270-3 0 9125
2 25544 51
6414 140
7318 0018641 23
0749 337
1234 15
50300479 28661
Satellite: ISS
Catalog Number: 25544
Epoch time: 12237
63300954 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 140
7318 deg
Eccentricity:
0018641
Arg of perigee: 23
0749 deg
Mean anomaly: 337
1234 deg
Mean motion: 15
50300479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2866
Checksum: 290
Coasting Arc #14 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2012/238/14:03:20
563
Vector Time (MET): N/A
Weight (LBS) : 952122
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2038955
22 A = 6788883
89 meter
Y = 3800557
78 meter E =
0026775
Z = -5259872
50 I = 51
86694
XDOT = -5932
005650 Wp = 57
05253
YDOT = 4696
826098 meter/sec RA = 135
00051 deg
ZDOT = 1112
484648 TA = 223
49913
MA = 223
71064
Ha = 233
127 n
mi
Hp = 215
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6689485
63 X = 2021856
13
Y = 12469021
59 feet Y = 3823263
11 meter
Z = -17256799
53 Z = -5250008
91
XDOT = -19461
960793 XDOT = -5989
489806
YDOT = 15409
534442 feet/sec YDOT = 4630
169294 meter/sec
ZDOT = 3649
884015 ZDOT = 1083
527891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7704131
50 X = -2348219
28
Y = -11927552
59 feet Y = -3635518
03 meter
Z = -17216349
63 Z = -5247543
37
XDOT = 17413
068909 XDOT = 5307
503403
YDOT = -16255
511161 feet/sec YDOT = -4954
679802 meter/sec
ZDOT = 3529
778323 ZDOT = 1075
876433
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 12238
59993601
00016717 00000-0 10270-3 0 9139
2 25544 51
6408 135
9386 0018664 26
3993 333
8105 15
50307442 28811
Satellite: ISS
Catalog Number: 25544
Epoch time: 12238
59993601 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 135
9386 deg
Eccentricity:
0018664
Arg of perigee: 26
3993 deg
Mean anomaly: 333
8105 deg
Mean motion: 15
50307442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 324
Coasting Arc #15 (Orbit 2896)
---------------------------------------
Vector Time (GMT): 2012/239/14:03:20
563
Vector Time (MET): N/A
Weight (LBS) : 952122
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1898382
54 A = 6789264
02 meter
Y = -4003556
50 meter E =
0023174
Z = 5137107
48 I = 51
88964
XDOT = 5728
567430 Wp = 35
31435
YDOT = -4831
278003 meter/sec RA = 130
05667 deg
ZDOT = -1626
162466 TA = 70
44634
MA = 70
19625
Ha = 233
171 n
mi
Hp = 215
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6228289
17 X = -1878427
45
Y = -13135027
89 feet Y = -4024673
87 meter
Z = 16854027
17 Z = 5127933
77
XDOT = 18794
512566 XDOT = 5790
065451
YDOT = -15850
649617 feet/sec YDOT = -4766
873727 meter/sec
ZDOT = -5335
178694 ZDOT = -1598
184364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7507458
73 X = 2288273
42
Y = 12498959
58 feet Y = 3809682
88 meter
Z = 16816445
77 Z = 5125652
67
XDOT = -16384
647044 XDOT = -4994
040419
YDOT = 16961
044309 feet/sec YDOT = 5169
726305 meter/sec
ZDOT = -5219
088984 ZDOT = -1590
778322
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 12239
63131187
00016717 00000-0 10270-3 0 9149
2 25544 51
6412 130
8259 0018618 29
9862 330
2351 15
50335163 28974
Satellite: ISS
Catalog Number: 25544
Epoch time: 12239
63131187 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 130
8259 deg
Eccentricity:
0018618
Arg of perigee: 29
9862 deg
Mean anomaly: 330
2351 deg
Mean motion: 15
50335163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2897
Checksum: 307
Coasting Arc #16 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2012/240/14:03:20
563
Vector Time (MET): N/A
Weight (LBS) : 952122
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1878889
17 A = 6789792
95 meter
Y = 4178238
87 meter E =
0025621
Z = -5026944
58 I = 51
90923
XDOT = -5462
268501 Wp = 61
74778
YDOT = 4934
207440 meter/sec RA = 125
11466 deg
ZDOT = 2079
406861 TA = 228
34955
MA = 228
56921
Ha = 233
232 n
mi
Hp = 215
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6164334
55 X = 1856446
95
Y = 13708132
78 feet Y = 4199124
27 meter
Z = -16492600
32 Z = -5017871
70
XDOT = -17920
828416 XDOT = -5527
138983
YDOT = 16188
344621 feet/sec YDOT = 4872
762252 meter/sec
ZDOT = 6822
200988 ZDOT = 2052
714260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7717875
99 X = -2352408
60
Y = -12944897
07 feet Y = -3945604
63 meter
Z = -16455449
54 Z = -5015621
02
XDOT = 15152
239054 XDOT = 4618
402464
YDOT = -17482
440771 feet/sec YDOT = -5328
647947 meter/sec
ZDOT = 6711
401741 ZDOT = 2045
635251
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 12240
59821753
00016717 00000-0 10270-3 0 9152
2 25544 51
6403 126
0323 0018618 33
4957 326
7367 15
50335974 29123
Satellite: ISS
Catalog Number: 25544
Epoch time: 12240
59821753 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 126
0323 deg
Eccentricity:
0018618
Arg of perigee: 33
4957 deg
Mean anomaly: 326
7367 deg
Mean motion: 15
50335974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 309
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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