[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 27th 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) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
091/21:57:19
536 -1
5 3
1 3
1
N/A -1
3 0
0 214
2
000/00:06:39
073 2
4 -0
0 207
7
Coasting Arc #1 (Orbit 512)
---------------------------------------
Vector Time (GMT): 2012/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6485907
17 A = 6772853
12 meter
Y = -1467854
42 meter E =
0023032
Z = 1199590
65 I = 51
68239
XDOT = 2103
819595 Wp = 164
91876
YDOT = 4490
813544 meter/sec RA = 175
44365 deg
ZDOT = -5876
290575 TA = 2
00383
MA = 1
99462
Ha = 215
854 n
mi
Hp = 204
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21279223
01 X = 6496011
59
Y = -4815795
35 feet Y = -1395268
40 meter
Z = 3935664
86 Z = 1231123
75
XDOT = 6902
295259 XDOT = 2081
991916
YDOT = 14733
640236 feet/sec YDOT = 4514
217188 meter/sec
ZDOT = -19279
168553 ZDOT = -5866
123672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20917487
86 X = 6375650
30
Y = -6117171
51 feet Y = -1864513
88 meter
Z = 4065167
75 Z = 1239063
13
XDOT = 7468
431227 XDOT = 2276
377838
YDOT = 12746
319636 feet/sec YDOT = 3885
078225 meter/sec
ZDOT = -19237
695282 ZDOT = -5863
649522
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12086
53445378
00016717 00000-0 10270-3 0 9003
2 25544 51
6409 176
3541 0016022 200
6192 159
4318 15
59590216 5138
Satellite: ISS
Catalog Number: 25544
Epoch time: 12086
53445378 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 176
3541 deg
Eccentricity:
0016022
Arg of perigee: 200
6192 deg
Mean anomaly: 159
4318 deg
Mean motion: 15
59590216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 513
Checksum: 295
Coasting Arc #2 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2012/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6341540
03 A = 6771201
29 meter
Y = -747184
29 meter E =
0011984
Z = 2265766
69 I = 51
70784
XDOT = 2515
867123 Wp = 147
08905
YDOT = -4780
117935 meter/sec RA = 170
45048 deg
ZDOT = 5441
838502 TA = 238
12945
MA = 238
24612
Ha = 215
572 n
mi
Hp = 205
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20805577
52 X = -6343720
19
Y = -2451392
03 feet Y = -818111
33 meter
Z = 7433617
75 Z = 2234954
37
XDOT = 8254
157227 XDOT = 2542
697013
YDOT = -15682
801623 feet/sec YDOT = -4751
833533 meter/sec
ZDOT = 17853
800861 ZDOT = 5454
126063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20978691
08 X = -6394305
04
Y = -799751
69 feet Y = -243764
31 meter
Z = 7307186
15 Z = 2227230
34
XDOT = 6825
672059 XDOT = 2080
464843
YDOT = -14745
304384 feet/sec YDOT = -4494
368776 meter/sec
ZDOT = 17904
511885 ZDOT = 5457
295223
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12087
55965294
00016717 00000-0 10270-3 0 9011
2 25544 51
6410 171
2003 0015878 204
8087 155
2307 15
59653362 5295
Satellite: ISS
Catalog Number: 25544
Epoch time: 12087
55965294 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 171
2003 deg
Eccentricity:
0015878
Arg of perigee: 204
8087 deg
Mean anomaly: 155
2307 deg
Mean motion: 15
59653362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 310
Coasting Arc #3 (Orbit 543)
---------------------------------------
Vector Time (GMT): 2012/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3819139
20 A = 6763657
47 meter
Y = 2897565
94 meter E =
0010713
Z = -4769506
67 I = 51
71157
XDOT = -6147
833709 Wp = 163
99299
YDOT = 3759
692213 meter/sec RA = 165
42942 deg
ZDOT = -2650
220460 TA = 79
97942
MA = 79
85855
Ha = 215
386 n
mi
Hp = 205
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12529984
25 X = 3809623
46
Y = 9506449
93 feet Y = 2940220
40 meter
Z = -15647987
76 Z = -4750976
70
XDOT = -20170
058099 XDOT = -6176
544201
YDOT = 12334
948206 feet/sec YDOT = 3690
782637 meter/sec
ZDOT = -8694
949015 ZDOT = -2680
156448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13478779
05 X = 4108331
85
Y = 8250162
96 feet Y = 2514649
67 meter
Z = -15572088
60 Z = -4746372
60
XDOT = -18238
718892 XDOT = -5559
161518
YDOT = 13225
141906 feet/sec YDOT = 4031
023253 meter/sec
ZDOT = -8818
059206 ZDOT = -2687
744446
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12088
52075736
00016717 00000-0 10270-3 0 9023
2 25544 51
6400 166
3692 0015805 208
6890 151
3398 15
59662087 5445
Satellite: ISS
Catalog Number: 25544
Epoch time: 12088
52075736 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 166
3692 deg
Eccentricity:
0015805
Arg of perigee: 208
6890 deg
Mean anomaly: 151
3398 deg
Mean motion: 15
59662087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 544
Checksum: 322
Coasting Arc #4 (Orbit 559)
---------------------------------------
Vector Time (GMT): 2012/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -13664
87 A = 6761554
94 meter
Y = -4339318
62 meter E =
0012015
Z = 5187840
04 I = 51
73528
XDOT = 7404
250923 Wp = 205
51199
YDOT = -1556
217486 meter/sec RA = 160
37831 deg
ZDOT = -1293
890398 TA = 256
81834
MA = 256
95243
Ha = 214
964 n
mi
Hp = 205
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -44832
26 X = 9657
89
Y = -14236609
64 feet Y = -4339340
71 meter
Z = 17020472
57 Z = 5187830
56
XDOT = 24292
161820 XDOT = 7427
387994
YDOT = -5105
700414 feet/sec YDOT = -1473
289287 meter/sec
ZDOT = -4245
047239 ZDOT = -1257
864547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1756979
21 X = -535527
26
Y = -14127586
54 feet Y = -4306088
38 meter
Z = 17020689
56 Z = 5187906
18
XDOT = 22554
018262 XDOT = 6874
464766
YDOT = -7694
703763 feet/sec YDOT = -2345
345707 meter/sec
ZDOT = -4097
047350 ZDOT = -1248
780032
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12089
54591076
00016717 00000-0 10270-3 0 9037
2 25544 51
6405 161
2154 0015709 212
8886 147
1294 15
59744150 5600
Satellite: ISS
Catalog Number: 25544
Epoch time: 12089
54591076 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 161
2154 deg
Eccentricity:
0015709
Arg of perigee: 212
8886 deg
Mean anomaly: 147
1294 deg
Mean motion: 15
59744150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 560
Checksum: 311
Coasting Arc #5 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2012/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3714709
62 A = 6768218
10 meter
Y = 4584908
73 meter E =
0013105
Z = -3324290
46 I = 51
78535
XDOT = -5904
079644 Wp = 199
86869
YDOT = -1362
471720 meter/sec RA = 155
34509 deg
ZDOT = 4700
864773 TA = 121
47108
MA = 121
34294
Ha = 214
667 n
mi
Hp = 205
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12187367
52 X = -3749554
28
Y = 15042351
49 feet Y = 4543173
53 meter
Z = -10906464
77 Z = -3342421
23
XDOT = -19370
340040 XDOT = -5911
241111
YDOT = -4470
051575 feet/sec YDOT = -1428
534550 meter/sec
ZDOT = 15422
784687 ZDOT = 4672
165751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10060134
35 X = -3066328
95
Y = 16491286
35 feet Y = 5026544
08 meter
Z = -10981184
39 Z = -3347065
00
XDOT = -18677
259927 XDOT = -5692
828826
YDOT = -1164
441245 feet/sec YDOT = -354
921691 meter/sec
ZDOT = 15305
025031 ZDOT = 4664
971629
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12090
50697344
00016717 00000-0 10270-3 0 9041
2 25544 51
6396 156
3836 0015539 215
9461 144
0650 15
59765506 5751
Satellite: ISS
Catalog Number: 25544
Epoch time: 12090
50697344 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 156
3836 deg
Eccentricity:
0015539
Arg of perigee: 215
9461 deg
Mean anomaly: 144
0650 deg
Mean motion: 15
59765506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 326
Coasting Arc #6 (Orbit 590)
---------------------------------------
Vector Time (GMT): 2012/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5877914
28 A = 6772937
79 meter
Y = -3337179
70 meter E =
0020324
Z = -9167
19 I = 51
82901
XDOT = 2337
623265 Wp = 183
43319
YDOT = 4135
791405 meter/sec RA = 150
35322 deg
ZDOT = -6043
343778 TA = 356
66565
MA = 356
67918
Ha = 214
360 n
mi
Hp = 205
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19284495
65 X = 5914838
96
Y = -10948752
29 feet Y = -3271242
77 meter
Z = -30076
08 Z = 19477
24
XDOT = 7669
367667 XDOT = 2320
559357
YDOT = 13568
869438 feet/sec YDOT = 4161
836348 meter/sec
ZDOT = -19827
243367 ZDOT = -6032
029474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17462840
56 X = 5322673
80
Y = -13667821
79 feet Y = -4165952
08 meter
Z = 87753
90 Z = 26747
39
XDOT = 8705
162276 XDOT = 2653
333462
YDOT = 11000
068468 feet/sec YDOT = 3352
820869 meter/sec
ZDOT = -19781
028780 ZDOT = -6029
257572
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12091
53208379
00016717 00000-0 10270-3 0 9052
2 25544 51
6401 151
2296 0015329 219
9395 140
0634 15
59787922 5911
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
53208379 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 151
2296 deg
Eccentricity:
0015329
Arg of perigee: 219
9395 deg
Mean anomaly: 140
0634 deg
Mean motion: 15
59787922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 591
Checksum: 317
Coasting Arc #7 (Orbit 597)
---------------------------------------
Vector Time (GMT): 2012/091/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5898158
47 A = 6774555
68 meter
Y = 3313446
32 meter E =
0001047
Z = 361880
90 I = 51
84028
XDOT = -2044
490107 Wp = 252
20355
YDOT = -4294
976773 meter/sec RA = 148
26472 deg
ZDOT = 6017
190501 TA = 111
69175
MA = 111
68060
Ha = 214
172 n
mi
Hp = 207
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19350913
63 X = -5936529
66
Y = 10870886
87 feet Y = 3247274
94 meter
Z = 1187273
28 Z = 333134
61
XDOT = -6707
644709 XDOT = -2025
540874
YDOT = -14091
131144 feet/sec YDOT = -4317
733154 meter/sec
ZDOT = 19741
438651 ZDOT = 6007
304834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21965724
21 X = 6695152
74
Y = -3226114
08 feet Y = -983319
57 meter
Z = 1069020
78 Z = 325837
53
XDOT = 1099
605735 XDOT = 335
159828
YDOT = 13998
289072 feet/sec YDOT = 4266
678509 meter/sec
ZDOT = 19701
099316 ZDOT = 6004
895071
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12091
98058696
00016717 00000-0 10270-3 0 9067
2 25544 51
6405 148
9751 0013695 230
5474 129
4470 15
59207353 5986
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
98058696 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 148
9751 deg
Eccentricity:
0013695
Arg of perigee: 230
5474 deg
Mean anomaly: 129
4470 deg
Mean motion: 15
59207353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 598
Checksum: 337
Coasting Arc #8 (Orbit 612)
---------------------------------------
Vector Time (GMT): 2012/092/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5733712
92 A = 6769420
87 meter
Y = -867646
89 meter E =
0009994
Z = -3479268
43 I = 51
84964
XDOT = -1881
883701 Wp = 218
57896
YDOT = 5881
130310 meter/sec RA = 143
27666 deg
ZDOT = -4568
486443 TA = 2
28240
MA = 2
27784
Ha = 213
978 n
mi
Hp = 207
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18811394
10 X = 5759890
39
Y = -2846610
52 feet Y = -803382
89 meter
Z = -11414922
67 Z = -3451350
81
XDOT = -6174
159124 XDOT = -1925
315270
YDOT = 19295
046948 feet/sec YDOT = 5859
842699 meter/sec
ZDOT = -14988
472581 ZDOT = -4577
734485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18717147
71 X = -5704986
62
Y = -3774367
62 feet Y = -1150427
25 meter
Z = -11300209
27 Z = -3444303
78
XDOT = 12033
364170 XDOT = 3667
769399
YDOT = -14690
241848 feet/sec YDOT = -4477
585715 meter/sec
ZDOT = -15026
811346 ZDOT = -4580
172098
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12092
94195609
00016717 00000-0 10270-3 0 9071
2 25544 51
6414 144
1458 0013732 234
3757 125
6120 15
59246698 6139
Satellite: ISS
Catalog Number: 25544
Epoch time: 12092
94195609 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 144
1458 deg
Eccentricity:
0013732
Arg of perigee: 234
3757 deg
Mean anomaly: 125
6120 deg
Mean motion: 15
59246698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 613
Checksum: 314
Coasting Arc #9 (Orbit 628)
---------------------------------------
Vector Time (GMT): 2012/093/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3786978
75 A = 6762928
83 meter
Y = -2098918
07 meter E =
0012613
Z = 5204026
26 I = 51
85203
XDOT = 4931
408567 Wp = 220
17679
YDOT = -5735
489685 meter/sec RA = 138
25301 deg
ZDOT = 1267
629384 TA = 217
64671
MA = 217
73506
Ha = 213
580 n
mi
Hp = 207
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12424470
96 X = -3788506
63
Y = -6886214
16 feet Y = -2141274
42 meter
Z = 17073576
96 Z = 5185625
88
XDOT = 16179
161964 XDOT = 4989
019629
YDOT = -18817
223377 feet/sec YDOT = -5680
021375 meter/sec
ZDOT = 4158
889055 ZDOT = 1291
726348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9605488
71 X = 2927752
96
Y = 10587385
70 feet Y = 3227035
16 meter
Z = 16998126
50 Z = 5181028
96
XDOT = -20625
748749 XDOT = -6286
728219
YDOT = 11835
568320 feet/sec YDOT = 3607
481224 meter/sec
ZDOT = 4258
215420 ZDOT = 1297
904060
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12093
96739575
00016717 00000-0 10270-3 0 9081
2 25544 51
6412 138
9938 0013666 238
0984 121
8843 15
59290403 6290
Satellite: ISS
Catalog Number: 25544
Epoch time: 12093
96739575 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 138
9938 deg
Eccentricity:
0013666
Arg of perigee: 238
0984 deg
Mean anomaly: 121
8843 deg
Mean motion: 15
59290403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 629
Checksum: 345
Coasting Arc #10 (Orbit 643)
---------------------------------------
Vector Time (GMT): 2012/094/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 783857
64 A = 6764387
47 meter
Y = 4686460
57 meter E =
0010020
Z = -4817585
55 I = 51
87951
XDOT = -6223
270230 Wp = 186
33427
YDOT = 3686
347637 meter/sec RA = 133
21477 deg
ZDOT = 2563
215568 TA = 108
84379
MA = 108
73510
Ha = 213
174 n
mi
Hp = 207
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2571711
43 X = 754797
14
Y = 15375526
80 feet Y = 4695063
09 meter
Z = -15805726
88 Z = -4813848
76
XDOT = -20417
553247 XDOT = -6276
480686
YDOT = 12094
316395 feet/sec YDOT = 3616
457970 meter/sec
ZDOT = 8409
499895 ZDOT = 2532
853579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2215352
71 X = 675239
51
Y = -15446313
78 feet Y = -4708036
44 meter
Z = -15790665
89 Z = -4812994
96
XDOT = 22078
136996 XDOT = 6729
416156
YDOT = -5337
063515 feet/sec YDOT = -1626
736959 meter/sec
ZDOT = 8284
555382 ZDOT = 2525
132481
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12094
92872552
00016717 00000-0 10270-3 0 9092
2 25544 51
6413 134
1635 0013665 242
1841 117
7930 15
59322974 6447
Satellite: ISS
Catalog Number: 25544
Epoch time: 12094
92872552 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 134
1635 deg
Eccentricity:
0013665
Arg of perigee: 242
1841 deg
Mean anomaly: 117
7930 deg
Mean motion: 15
59322974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 644
Checksum: 313
Coasting Arc #11 (Orbit 659)
---------------------------------------
Vector Time (GMT): 2012/095/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2183246
06 A = 6771608
07 meter
Y = -5906899
60 meter E =
0009162
Z = 2473610
41 I = 51
92351
XDOT = 5500
411676 Wp = 174
28671
YDOT = -206
111001 meter/sec RA = 128
20729 deg
ZDOT = -5354
122867 TA = 338
03926
MA = 338
07850
Ha = 212
879 n
mi
Hp = 207
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7162880
78 X = 2237119
67
Y = -19379591
88 feet Y = -5882183
65 meter
Z = 8115519
72 Z = 2484348
16
XDOT = 18045
970064 XDOT = 5528
316842
YDOT = -676
217196 feet/sec YDOT = -144
446656 meter/sec
ZDOT = -17566
019905 ZDOT = -5327
334237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12474233
12 X = -3802146
25
Y = 16448253
23 feet Y = 5013427
58 meter
Z = 8159998
56 Z = 2487167
56
XDOT = -16356
183962 XDOT = -4985
364872
YDOT = -3756
122618 feet/sec YDOT = -1144
866174 meter/sec
ZDOT = -17455
962775 ZDOT = -5320
577454
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12095
95412374
00016717 00000-0 10270-3 0 9100
2 25544 51
6409 129
0118 0013550 245
6932 114
2809 15
59330331 6604
Satellite: ISS
Catalog Number: 25544
Epoch time: 12095
95412374 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 129
0118 deg
Eccentricity:
0013550
Arg of perigee: 245
6932 deg
Mean anomaly: 114
2809 deg
Mean motion: 15
59330331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 660
Checksum: 288
Coasting Arc #12 (Orbit 675)
---------------------------------------
Vector Time (GMT): 2012/096/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4252898
53 A = 6773732
39 meter
Y = 5190448
57 meter E =
0003667
Z = 910990
13 I = 51
94885
XDOT = -3180
732841 Wp = 329
48668
YDOT = -3648
782864 meter/sec RA = 123
23023 deg
ZDOT = 5953
761713 TA = 40
34972
MA = 40
32252
Ha = 212
468 n
mi
Hp = 207
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13953079
15 X = -4315048
51
Y = 17029030
74 feet Y = 5142542
64 meter
Z = 2988812
76 Z = 890177
96
XDOT = -10435
475199 XDOT = -3168
617288
YDOT = -11971
072387 feet/sec YDOT = -3684
283301 meter/sec
ZDOT = 19533
338952 ZDOT = 5938
339613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18131158
13 X = 5526377
00
Y = -12507721
55 feet Y = -3812353
53 meter
Z = 2902983
67 Z = 884829
42
XDOT = 5925
082843 XDOT = 1805
965251
YDOT = 13097
317097 feet/sec YDOT = 3992
062251 meter/sec
ZDOT = 19470
218316 ZDOT = 5934
522543
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 12096
97949711
00016717 00000-0 10270-3 0 9114
2 25544 51
6406 123
8582 0013672 250
2233 109
7448 15
59393175 6769
Satellite: ISS
Catalog Number: 25544
Epoch time: 12096
97949711 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 123
8582 deg
Eccentricity:
0013672
Arg of perigee: 250
2233 deg
Mean anomaly: 109
7448 deg
Mean motion: 15
59393175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 676
Checksum: 327
Coasting Arc #13 (Orbit 690)
---------------------------------------
Vector Time (GMT): 2012/097/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4869582
71 A = 6767601
27 meter
Y = -2588562
65 meter E =
0007309
Z = -3914981
00 I = 51
94343
XDOT = 153
706415 Wp = 253
91533
YDOT = 6493
126512 meter/sec RA = 118
24256 deg
ZDOT = -4097
694242 TA = 333
40543
MA = 333
44291
Ha = 212
326 n
mi
Hp = 207
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15976321
22 X = 4917184
96
Y = -8492659
60 feet Y = -2533842
22 meter
Z = -12844425
86 Z = -3891208
58
XDOT = 504
286140 XDOT = 100
993475
YDOT = 21302
908503 feet/sec YDOT = 6494
550179 meter/sec
ZDOT = -13443
878747 ZDOT = -4097
076269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17708758
07 X = -5397629
46
Y = 4033808
77 feet Y = 1229504
91 meter
Z = -12746593
93 Z = -3885161
83
XDOT = 5259
147285 XDOT = 1602
988092
YDOT = -19432
405455 feet/sec YDOT = -5922
997183 meter/sec
ZDOT = -13441
768540 ZDOT = -4097
051051
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 12097
94076634
00016717 00000-0 10270-3 0 9128
2 25544 51
6398 119
0277 0013788 254
0186 105
9450 15
59398900 6913
Satellite: ISS
Catalog Number: 25544
Epoch time: 12097
94076634 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 119
0277 deg
Eccentricity:
0013788
Arg of perigee: 254
0186 deg
Mean anomaly: 105
9450 deg
Mean motion: 15
59398900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 691
Checksum: 335
Coasting Arc #14 (Orbit 706)
---------------------------------------
Vector Time (GMT): 2012/098/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4055205
52 A = 6762039
03 meter
Y = -1091869
63 meter E =
0011411
Z = 5309325
60 I = 51
93882
XDOT = 2631
000736 Wp = 249
52292
YDOT = -7184
371588 meter/sec RA = 113
21722 deg
ZDOT = 529
082130 TA = 195
43299
MA = 195
46781
Ha = 211
847 n
mi
Hp = 207
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13304480
06 X = -4068486
53
Y = -3582249
43 feet Y = -1137291
28 meter
Z = 17419047
24 Z = 5289593
11
XDOT = 8631
892178 XDOT = 2708
572087
YDOT = -23570
772926 feet/sec YDOT = -7154
516343 meter/sec
ZDOT = 1735
833759 ZDOT = 542
052602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12137988
12 X = 3699658
78
Y = 6732462
11 feet Y = 2052054
45 meter
Z = 17338053
68 Z = 5284638
76
XDOT = -13599
304346 XDOT = -4145
067965
YDOT = 19884
244822 feet/sec YDOT = 6060
717822 meter/sec
ZDOT = 1789
612091 ZDOT = 545
473765
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 12098
96609886
00016717 00000-0 10270-3 0 9133
2 25544 51
6399 113
8744 0013596 257
7239 102
2394 15
59437911 7072
Satellite: ISS
Catalog Number: 25544
Epoch time: 12098
96609886 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 113
8744 deg
Eccentricity:
0013596
Arg of perigee: 257
7239 deg
Mean anomaly: 102
2394 deg
Mean motion: 15
59437911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 707
Checksum: 349
Coasting Arc #15 (Orbit 721)
---------------------------------------
Vector Time (GMT): 2012/099/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2184055
58 A = 6765275
63 meter
Y = 4576227
58 meter E =
0007120
Z = -4477416
58 I = 51
96044
XDOT = -4447
263061 Wp = 221
36907
YDOT = 5332
907762 meter/sec RA = 108
18460 deg
ZDOT = 3273
086258 TA = 81
44764
MA = 81
36696
Ha = 211
561 n
mi
Hp = 207
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7165536
68 X = 2154471
56
Y = 15013870
02 feet Y = 4600485
41 meter
Z = -14689686
94 Z = -4466878
46
XDOT = -14590
758074 XDOT = -4522
466334
YDOT = 17496
416541 feet/sec YDOT = 5282
755393 meter/sec
ZDOT = 10738
471974 ZDOT = 3251
298401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3669570
29 X = -1118485
02
Y = -16265181
82 feet Y = -4957627
42 meter
Z = -14646713
82 Z = -4464318
37
XDOT = 17048
624565 XDOT = 5196
420767
YDOT = -13459
505024 feet/sec YDOT = -4102
457131 meter/sec
ZDOT = 10648
576339 ZDOT = 3245
686068
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 12099
92732671
00016717 00000-0 10270-3 0 9140
2 25544 51
6390 109
0421 0013709 261
4871 98
4730 15
59490360 7226
Satellite: ISS
Catalog Number: 25544
Epoch time: 12099
92732671 = yrday
fracday
Element set: 914
Inclination: 51
6390 deg
RA of node: 109
0421 deg
Eccentricity:
0013709
Arg of perigee: 261
4871 deg
Mean anomaly: 98
4730 deg
Mean motion: 15
59490360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 722
Checksum: 310
Coasting Arc #16 (Orbit 737)
---------------------------------------
Vector Time (GMT): 2012/100/22:00:39
073
Vector Time (MET): N/A
Weight (LBS) : 886297
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 108360
30 A = 6772332
09 meter
Y = -6531141
66 meter E =
0006971
Z = 1771971
09 I = 51
99353
XDOT = 4922
680407 Wp = 187
43941
YDOT = -1463
839888 meter/sec RA = 103
18962 deg
ZDOT = -5705
688958 TA = 333
15381
MA = 333
18987
Ha = 211
277 n
mi
Hp = 207
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 355512
81 X = 172776
86
Y = -21427630
11 feet Y = -6529569
69 meter
Z = 5813553
43 Z = 1772654
13
XDOT = 16150
526270 XDOT = 4966
400768
YDOT = -4802
624306 feet/sec YDOT = -1408
547123 meter/sec
ZDOT = -18719
451962 ZDOT = -5681
668286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4801653
05 X = -1463543
85
Y = 20884818
69 feet Y = 6365692
74 meter
Z = 5816837
72 Z = 1772972
14
XDOT = -15386
511769 XDOT = -4689
808787
YDOT = 1640
264352 feet/sec YDOT = 499
952574 meter/sec
ZDOT = -18620
645428 ZDOT = -5675
572726
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 12100
95261554
00016717 00000-0 10270-3 0 9154
2 25544 51
6396 103
8897 0013642 265
6593 94
3004 15
59529315 7383
Satellite: ISS
Catalog Number: 25544
Epoch time: 12100
95261554 = yrday
fracday
Element set: 915
Inclination: 51
6396 deg
RA of node: 103
8897 deg
Eccentricity:
0013642
Arg of perigee: 265
6593 deg
Mean anomaly: 94
3004 deg
Mean motion: 15
59529315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 738
Checksum: 321
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list