[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 15th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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
200/03:15:22
043 6
4 7
7 7
8
N/A -2
4 -1
2 219
4
000/00:18:44
085 3
8 0
1 215
5
Coasting Arc #1 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2012/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4661298
34 A = 6775970
92 meter
Y = -2581633
64 meter E =
0011697
Z = -4193146
46 I = 51
57663
XDOT = 5469
500143 Wp = 107
33074
YDOT = -3899
674754 meter/sec RA = 350
35331 deg
ZDOT = -3691
117325 TA = 124
79471
MA = 124
68458
Ha = 219
916 n
mi
Hp = 209
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15292973
55 X = -4611714
28
Y = -8469926
65 feet Y = -2633481
43 meter
Z = -13757042
20 Z = -4215670
61
XDOT = 17944
554274 XDOT = 5530
631132
YDOT = -12794
208509 feet/sec YDOT = -3838
169169 meter/sec
ZDOT = -12109
964978 ZDOT = -3664
398834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2467713
05 X = -752158
94
Y = 17232803
37 feet Y = 5252558
47 meter
Z = -13849613
27 Z = -4221362
13
XDOT = -17138
675230 XDOT = -5223
868210
YDOT = -12066
624380 feet/sec YDOT = -3677
907111 meter/sec
ZDOT = -11999
334741 ZDOT = -3657
397229
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 12195
52278396
00016717 00000-0 10270-3 0 9007
2 25544 51
6377 350
7420 0007264 150
5645 209
5919 15
56122243 22119
Satellite: ISS
Catalog Number: 25544
Epoch time: 12195
52278396 = yrday
fracday
Element set: 900
Inclination: 51
6377 deg
RA of node: 350
7420 deg
Eccentricity:
0007264
Arg of perigee: 150
5645 deg
Mean anomaly: 209
5919 deg
Mean motion: 15
56122243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 300
Coasting Arc #2 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2012/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2440190
34 A = 6772018
98 meter
Y = 3613445
09 meter E =
0010924
Z = 5177590
05 I = 51
53310
XDOT = -6998
556227 Wp = 143
38477
YDOT = 2881
082106 meter/sec RA = 345
33280 deg
ZDOT = 1277
711030 TA = 294
28286
MA = 294
39693
Ha = 219
760 n
mi
Hp = 210
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8005873
82 X = 2374451
28
Y = 11855134
82 feet Y = 3640364
57 meter
Z = 16986843
98 Z = 5189285
10
XDOT = -22961
142476 XDOT = -7036
459722
YDOT = 9452
369113 feet/sec YDOT = 2802
607813 meter/sec
ZDOT = 4191
965320 ZDOT = 1243
620867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8042438
23 X = 2451335
17
Y = -11761433
92 feet Y = -3584885
06 meter
Z = 17034640
15 Z = 5192158
32
XDOT = 16502
902633 XDOT = 5030
084723
YDOT = 17199
311109 feet/sec YDOT = 5242
350026 meter/sec
ZDOT = 4051
059915 ZDOT = 1234
763062
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 12196
55029502
00016717 00000-0 10270-3 0 9015
2 25544 51
6373 345
6028 0007181 155
0161 205
1341 15
56135053 22274
Satellite: ISS
Catalog Number: 25544
Epoch time: 12196
55029502 = yrday
fracday
Element set: 901
Inclination: 51
6373 deg
RA of node: 345
6028 deg
Eccentricity:
0007181
Arg of perigee: 155
0161 deg
Mean anomaly: 205
1341 deg
Mean motion: 15
56135053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 273
Coasting Arc #3 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2012/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 129652
40 A = 6772140
16 meter
Y = -4404140
91 meter E =
0018738
Z = -5158874
63 I = 51
50541
XDOT = 7385
522008 Wp = 119
65636
YDOT = -1447
604864 meter/sec RA = 340
30338 deg
ZDOT = 1416
237153 TA = 164
04057
MA = 163
98145
Ha = 219
741 n
mi
Hp = 210
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 425368
76 X = 203951
20
Y = -14449281
18 feet Y = -4402274
91 meter
Z = -16925441
71 Z = -5158064
93
XDOT = 24230
715249 XDOT = 7394
280812
YDOT = -4749
359789 feet/sec YDOT = -1364
966598 meter/sec
ZDOT = 4646
447352 ZDOT = 1452
136460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13513762
58 X = -4118994
83
Y = 5145042
64 feet Y = 1568209
00 meter
Z = -16921583
84 Z = -5157698
75
XDOT = -13430
869162 XDOT = -4093
728921
YDOT = -19451
727705 feet/sec YDOT = -5928
886604 meter/sec
ZDOT = 4794
643268 ZDOT = 1461
407268
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 12197
51357064
00016717 00000-0 10270-3 0 9020
2 25544 51
6383 340
7864 0007254 158
1917 201
9547 15
56167994 22421
Satellite: ISS
Catalog Number: 25544
Epoch time: 12197
51357064 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 340
7864 deg
Eccentricity:
0007254
Arg of perigee: 158
1917 deg
Mean anomaly: 201
9547 deg
Mean motion: 15
56167994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 325
Coasting Arc #4 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2012/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2565931
61 A = 6776390
25 meter
Y = 4753185
39 meter E =
0013444
Z = 4077612
66 I = 51
49100
XDOT = -6648
071862 Wp = 109
36838
YDOT = -296
218923 meter/sec RA = 335
27924 deg
ZDOT = -3832
223781 TA = 20
28174
MA = 20
22838
Ha = 219
691 n
mi
Hp = 210
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8418410
78 X = -2638699
88
Y = 15594440
24 feet Y = 4724084
11 meter
Z = 13377994
29 Z = 4064971
54
XDOT = -21811
259390 XDOT = -6625
649525
YDOT = -971
846859 feet/sec YDOT = -370
435878 meter/sec
ZDOT = -12572
912666 ZDOT = -3864
465017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17702372
86 X = 5395683
25
Y = 1445334
46 feet Y = 440537
94 meter
Z = 13325312
05 Z = 4061555
11
XDOT = 8030
051687 XDOT = 2447
559754
YDOT = 18970
307027 feet/sec YDOT = 5782
149582 meter/sec
ZDOT = -12705
820874 ZDOT = -3872
734202
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 12198
54104863
00016717 00000-0 10270-3 0 9032
2 25544 51
6382 335
6469 0007221 162
0315 198
1095 15
56163349 22586
Satellite: ISS
Catalog Number: 25544
Epoch time: 12198
54104863 = yrday
fracday
Element set: 903
Inclination: 51
6382 deg
RA of node: 335
6469 deg
Eccentricity:
0007221
Arg of perigee: 162
0315 deg
Mean anomaly: 198
1095 deg
Mean motion: 15
56163349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 312
Coasting Arc #5 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2012/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4500929
33 A = 6781287
25 meter
Y = -4578783
81 meter E =
0006350
Z = -2191584
03 I = 51
48190
XDOT = 4900
681946 Wp = 109
95899
YDOT = 2208
124524 meter/sec RA = 330
27352 deg
ZDOT = 5462
130430 TA = 225
65547
MA = 225
70752
Ha = 219
452 n
mi
Hp = 210
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14766828
53 X = 4562441
77
Y = -15022256
58 feet Y = -4528107
39 meter
Z = -7190236
32 Z = -2169570
26
XDOT = 16078
352841 XDOT = 4849
092626
YDOT = 7244
503033 feet/sec YDOT = 2262
637798 meter/sec
ZDOT = 17920
375425 ZDOT = 5485
812353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19863222
58 X = -6054310
24
Y = -7105244
21 feet Y = -2165678
43 meter
Z = -7098930
16 Z = -2163753
91
XDOT = -672
326013 XDOT = -204
924969
YDOT = -16086
439930 feet/sec YDOT = -4903
146891 meter/sec
ZDOT = 18017
768979 ZDOT = 5491
815985
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 12199
50429225
00016717 00000-0 10270-3 0 9042
2 25544 51
6395 330
8298 0007069 165
5697 194
5660 15
56210988 22735
Satellite: ISS
Catalog Number: 25544
Epoch time: 12199
50429225 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 330
8298 deg
Eccentricity:
0007069
Arg of perigee: 165
5697 deg
Mean anomaly: 194
5660 deg
Mean motion: 15
56210988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 341
Coasting Arc #6 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2012/200/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247985
84 A = 6785954
36 meter
Y = -4820853
72 meter E =
0001638
Z = -2179298
00 I = 51
46807
XDOT = 5008
779243 Wp = 359
32708
YDOT = 1942
602556 meter/sec RA = 327
05544 deg
ZDOT = 5467
643935 TA = 336
43038
MA = 336
43788
Ha = 219
382 n
mi
Hp = 215
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13936961
42 X = 4312164
25
Y = -15816449
21 feet Y = -4772990
98 meter
Z = -7149927
81 Z = -2158506
56
XDOT = 16433
002766 XDOT = 4960
124282
YDOT = 6373
367967 feet/sec YDOT = 1998
341086 meter/sec
ZDOT = 17938
464355 ZDOT = 5491
858011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17238460
41 X = 5254282
73
Y = -12184455
23 feet Y = -3713821
95 meter
Z = -7063636
45 Z = -2152996
39
XDOT = 13534
950244 XDOT = 4125
452834
YDOT = 8695
003136 feet/sec YDOT = 2650
236956 meter/sec
ZDOT = 18038
085437 ZDOT = 5498
008441
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 12200
14644606
00016717 00000-0 10270-3 0 9058
2 25544 51
6425 327
6198 0005185 234
2518 125
8153 15
54612061 22836
Satellite: ISS
Catalog Number: 25544
Epoch time: 12200
14644606 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 327
6198 deg
Eccentricity:
0005185
Arg of perigee: 234
2518 deg
Mean anomaly: 125
8153 deg
Mean motion: 15
54612061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 288
Coasting Arc #7 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2012/201/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5161934
49 A = 6787952
91 meter
Y = 4381646
62 meter E =
0012312
Z = 355007
38 I = 51
44970
XDOT = -3340
124460 Wp = 155
15941
YDOT = -3444
694008 meter/sec RA = 322
06872 deg
ZDOT = -5986
200566 TA = 21
00171
MA = 20
95119
Ha = 219
273 n
mi
Hp = 215
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16935480
61 X = -5212271
83
Y = 14375481
04 feet Y = 4323641
18 meter
Z = 1164722
37 Z = 329809
65
XDOT = -10958
413583 XDOT = -3272
277905
YDOT = -11301
489526 feet/sec YDOT = -3481
665331 meter/sec
ZDOT = -19639
765635 ZDOT = -6002
262012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19613613
77 X = -5978229
48
Y = 10440470
21 feet Y = 3182255
32 meter
Z = 1060317
70 Z = 323184
84
XDOT = -7423
098936 XDOT = -2262
560556
YDOT = -11920
231309 feet/sec YDOT = -3633
286503 meter/sec
ZDOT = -19705
601074 ZDOT = -6006
267207
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 12201
17496065
00016717 00000-0 10270-3 0 9067
2 25544 51
6426 322
4887 0005235 237
5917 122
4730 15
54587786 22996
Satellite: ISS
Catalog Number: 25544
Epoch time: 12201
17496065 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 322
4887 deg
Eccentricity:
0005235
Arg of perigee: 237
5917 deg
Mean anomaly: 122
4730 deg
Mean motion: 15
54587786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 327
Coasting Arc #8 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2012/202/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5579798
28 A = 6786846
11 meter
Y = -3550830
71 meter E =
0008771
Z = 1503579
78 I = 51
42323
XDOT = 1526
268259 Wp = 60
63456
YDOT = 4841
244177 meter/sec RA = 317
08111 deg
ZDOT = 5747
887415 TA = 315
83847
MA = 315
90846
Ha = 218
959 n
mi
Hp = 215
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18306424
81 X = 5611785
80
Y = -11649707
05 feet Y = -3488255
23 meter
Z = 4933004
52 Z = 1530763
00
XDOT = 5007
441794 XDOT = 1444
097681
YDOT = 15883
347038 feet/sec YDOT = 4857
851892 meter/sec
ZDOT = 18857
898344 ZDOT = 5755
102658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20204635
67 X = 6158372
95
Y = -7841623
95 feet Y = -2390126
98 meter
Z = 5045495
87 Z = 1537867
14
XDOT = 1112
298470 XDOT = 339
028574
YDOT = 15061
966700 feet/sec YDOT = 4590
887450 meter/sec
ZDOT = 18887
104534 ZDOT = 5756
789462
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 12202
20345836
00016717 00000-0 10270-3 0 9072
2 25544 51
6427 317
3570 0005137 244
7305 115
3316 15
54638206 23155
Satellite: ISS
Catalog Number: 25544
Epoch time: 12202
20345836 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 317
3570 deg
Eccentricity:
0005137
Arg of perigee: 244
7305 deg
Mean anomaly: 115
3316 deg
Mean motion: 15
54638206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 281
Coasting Arc #9 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2012/203/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5519997
68 A = 6783403
08 meter
Y = 2306315
76 meter E =
0002695
Z = -3194253
34 I = 51
39018
XDOT = 263
504867 Wp = 188
77051
YDOT = -5988
342719 meter/sec RA = 312
08575 deg
ZDOT = -4781
147622 TA = 28
29726
MA = 28
28262
Ha = 218
687 n
mi
Hp = 215
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18110228
59 X = -5529860
47
Y = 7566652
77 feet Y = 2244532
80 meter
Z = -10479833
80 Z = -3221092
49
XDOT = 864
517281 XDOT = 353
673423
YDOT = -19646
793697 feet/sec YDOT = -5984
891552 meter/sec
ZDOT = -15686
179863 ZDOT = -4779
648955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19109104
43 X = -5824455
03
Y = 4211820
61 feet Y = 1283762
92 meter
Z = -10590761
32 Z = -3228064
05
XDOT = 4770
648292 XDOT = 1454
093599
YDOT = -17764
715103 feet/sec YDOT = -5414
685164 meter/sec
ZDOT = -15679
335136 ZDOT = -4779
061349
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 12203
16766133
00016717 00000-0 10270-3 0 9086
2 25544 51
6426 312
5468 0005333 248
5419 111
5165 15
54645816 23305
Satellite: ISS
Catalog Number: 25544
Epoch time: 12203
16766133 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 312
5468 deg
Eccentricity:
0005333
Arg of perigee: 248
5419 deg
Mean anomaly: 111
5165 deg
Mean motion: 15
54645816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 295
Coasting Arc #10 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2012/204/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5042449
27 A = 6779161
05 meter
Y = -746562
20 meter E =
0005905
Z = 4468794
31 I = 51
35632
XDOT = -1856
267853 Wp = 144
16572
YDOT = 6712
527508 meter/sec RA = 307
07592 deg
ZDOT = 3209
101998 TA = 273
40162
MA = 273
46916
Ha = 218
516 n
mi
Hp = 215
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16543468
73 X = 5028714
72
Y = -2449351
05 feet Y = -690251
42 meter
Z = 14661398
66 Z = 4493256
46
XDOT = -6090
117628 XDOT = -1946
779559
YDOT = 22022
728043 feet/sec YDOT = 6691
263327 meter/sec
ZDOT = 10528
549863 ZDOT = 3199
864990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16632857
78 X = 5069695
05
Y = 251781
06 feet Y = 76742
87 meter
Z = 14762348
64 Z = 4499563
87
XDOT = -9625
398958 XDOT = -2933
821603
YDOT = 19521
238528 feet/sec YDOT = 5950
073503 meter/sec
ZDOT = 10489
727742 ZDOT = 3197
269016
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 12204
19613102
00016717 00000-0 10270-3 0 9098
2 25544 51
6424 307
4149 0005082 253
5609 106
4985 15
54671071 23462
Satellite: ISS
Catalog Number: 25544
Epoch time: 12204
19613102 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 307
4149 deg
Eccentricity:
0005082
Arg of perigee: 253
5609 deg
Mean anomaly: 106
4985 deg
Mean motion: 15
54671071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 294
Coasting Arc #11 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2012/205/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4247284
76 A = 6776075
48 meter
Y = -1036274
08 meter E =
0008923
Z = -5184949
83 I = 51
32795
XDOT = 3158
657871 Wp = 82
08173
YDOT = -6875
269056 meter/sec RA = 302
05283 deg
ZDOT = -1213
921198 TA = 176
21474
MA = 176
20799
Ha = 218
301 n
mi
Hp = 215
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13934661
28 X = -4210194
33
Y = -3399849
33 feet Y = -1083562
27 meter
Z = -17010990
25 Z = -5205492
59
XDOT = 10363
050758 XDOT = 3241
200651
YDOT = -22556
657009 feet/sec YDOT = -6839
485414 meter/sec
ZDOT = -3982
681095 ZDOT = -1198
376580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13190402
76 X = -4020434
76
Y = -5372321
29 feet Y = -1637483
53 meter
Z = -17095583
90 Z = -5210733
97
XDOT = 13159
397888 XDOT = 4010
984476
YDOT = -19848
572528 feet/sec YDOT = -6049
844907 meter/sec
ZDOT = -3917
844065 ZDOT = -1194
158871
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 12205
16030567
00016717 00000-0 10270-3 0 9106
2 25544 51
6413 302
6035 0005228 258
4052 101
6515 15
54729386 23615
Satellite: ISS
Catalog Number: 25544
Epoch time: 12205
16030567 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 302
6035 deg
Eccentricity:
0005228
Arg of perigee: 258
4052 deg
Mean anomaly: 101
6515 deg
Mean motion: 15
54729386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 275
Coasting Arc #12 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2012/206/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3243904
23 A = 6775868
64 meter
Y = 2848455
67 meter E =
0002466
Z = 5224686
25 I = 51
31206
XDOT = -4110
666770 Wp = 296
80812
YDOT = 6404
682264 meter/sec RA = 297
02399 deg
ZDOT = -938
798911 TA = 162
22022
MA = 162
21158
Ha = 218
080 n
mi
Hp = 215
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10642730
40 X = 3186431
05
Y = 9345326
99 feet Y = 2884409
49 meter
Z = 17141359
10 Z = 5240305
32
XDOT = -13486
439533 XDOT = -4177
419307
YDOT = 21012
737086 feet/sec YDOT = 6358
341033 meter/sec
ZDOT = -3080
048922 ZDOT = -958
930045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9253697
36 X = 2820526
96
Y = 10619338
34 feet Y = 3236774
33 meter
Z = 17205457
77 Z = 5244223
53
XDOT = -15273
775403 XDOT = -4655
446743
YDOT = 18439
432913 feet/sec YDOT = 5620
339152 meter/sec
ZDOT = -3163
737231 ZDOT = -964
307108
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 12206
18874568
00016717 00000-0 10270-3 0 9117
2 25544 51
6414 297
4718 0005260 262
0870 97
9686 15
54742792 23779
Satellite: ISS
Catalog Number: 25544
Epoch time: 12206
18874568 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 297
4718 deg
Eccentricity:
0005260
Arg of perigee: 262
0870 deg
Mean anomaly: 97
9686 deg
Mean motion: 15
54742792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 340
Coasting Arc #13 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2012/207/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2145613
31 A = 6778494
59 meter
Y = -4507173
84 meter E =
0005760
Z = -4591467
47 I = 51
30671
XDOT = 4700
424918 Wp = 131
50291
YDOT = -5271
067718 meter/sec RA = 291
99628 deg
ZDOT = 2976
449589 TA = 168
34403
MA = 168
33069
Ha = 218
083 n
mi
Hp = 215
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7039413
75 X = -2072749
55
Y = -14787315
75 feet Y = -4530759
83 meter
Z = -15063869
65 Z = -4601713
89
XDOT = 15421
341594 XDOT = 4744
558919
YDOT = -17293
529260 feet/sec YDOT = -5218
258005 meter/sec
ZDOT = 9765
254556 ZDOT = 2999
390858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5262462
71 X = -1603998
63
Y = -15468169
25 feet Y = -4714697
99 meter
Z = -15105642
92 Z = -4604199
96
XDOT = 16058
376812 XDOT = 4894
593252
YDOT = -15096
775926 feet/sec YDOT = -4601
497302 meter/sec
ZDOT = 9860
402839 ZDOT = 3005
450785
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 12207
15289496
00016717 00000-0 10270-3 0 9126
2 25544 51
6400 292
6592 0005294 266
3246 93
7302 15
54763984 23924
Satellite: ISS
Catalog Number: 25544
Epoch time: 12207
15289496 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 292
6592 deg
Eccentricity:
0005294
Arg of perigee: 266
3246 deg
Mean anomaly: 93
7302 deg
Mean motion: 15
54763984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 324
Coasting Arc #14 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2012/208/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1027526
48 A = 6782562
73 meter
Y = 5806778
64 meter E =
0007156
Z = 3344673
65 I = 51
31066
XDOT = -4968
239755 Wp = 90
21589
YDOT = 3554
930541 meter/sec RA = 286
98037 deg
ZDOT = -4636
914190 TA = 50
58182
MA = 50
51849
Ha = 217
925 n
mi
Hp = 215
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3371149
85 X = 946269
92
Y = 19051111
03 feet Y = 5817814
55 meter
Z = 10973338
74 Z = 3349468
27
XDOT = -16299
999195 XDOT = -4985
097493
YDOT = 11663
157942 feet/sec YDOT = 3499
278614 meter/sec
ZDOT = -15212
973065 ZDOT = -4661
090300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1500257
15 X = 457278
38
Y = 19277909
78 feet Y = 5875906
90 meter
Z = 10992500
57 Z = 3350514
17
XDOT = -15824
567771 XDOT = -4823
328256
YDOT = 9979
229155 feet/sec YDOT = 3041
669046 meter/sec
ZDOT = -15313
029718 ZDOT = -4667
411458
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 12208
18130571
00016717 00000-0 10270-3 0 9130
2 25544 51
6403 287
5272 0005389 272
0961 87
9574 15
54817538 24087
Satellite: ISS
Catalog Number: 25544
Epoch time: 12208
18130571 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 287
5272 deg
Eccentricity:
0005389
Arg of perigee: 272
0961 deg
Mean anomaly: 87
9574 deg
Mean motion: 15
54817538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2408
Checksum: 321
Coasting Arc #15 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2012/209/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 34329
43 A = 6786245
67 meter
Y = -6575078
07 meter E =
0006596
Z = -1661690
44 I = 51
31326
XDOT = 4951
670759 Wp = 355
10855
YDOT = -1409
400549 meter/sec RA = 281
97488 deg
ZDOT = 5683
882845 TA = 346
59732
MA = 346
61484
Ha = 218
024 n
mi
Hp = 215
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 112629
35 X = 115922
83
Y = -21571778
45 feet Y = -6574237
83 meter
Z = -5451740
28 Z = -1661326
01
XDOT = 16245
638973 XDOT = 4939
452052
YDOT = -4624
017549 feet/sec YDOT = -1354
096673 meter/sec
ZDOT = 18647
909596 ZDOT = 5707
907939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1801647
48 X = 549142
15
Y = -21497260
51 feet Y = -6552365
00 meter
Z = -5449554
10 Z = -1661024
09
XDOT = 14871
086719 XDOT = 4532
707232
YDOT = -3502
095123 feet/sec YDOT = -1067
438593 meter/sec
ZDOT = 18747
120809 ZDOT = 5714
122422
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 12209
14542999
00016717 00000-0 10270-3 0 9149
2 25544 51
6388 282
7144 0005356 274
5701 85
4840 15
54785927 24239
Satellite: ISS
Catalog Number: 25544
Epoch time: 12209
14542999 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 282
7144 deg
Eccentricity:
0005356
Arg of perigee: 274
5701 deg
Mean anomaly: 85
4840 deg
Mean motion: 15
54785927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 332
Coasting Arc #16 (Orbit 2438)
---------------------------------------
Vector Time (GMT): 2012/210/03:24:44
085
Vector Time (MET): N/A
Weight (LBS) : 907911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1030747
60 A = 6787276
92 meter
Y = 6698339
10 meter E =
0008064
Z = -261348
53 I = 51
31179
XDOT = -4706
867381 Wp = 160
35192
YDOT = -955
186943 meter/sec RA = 276
97844 deg
ZDOT = -5978
983136 TA = 22
47779
MA = 22
44248
Ha = 218
087 n
mi
Hp = 215
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3381717
84 X = -1104303
63
Y = 21976178
15 feet Y = 6686401
39 meter
Z = -857442
68 Z = -266533
81
XDOT = -15442
478285 XDOT = -4666
792106
YDOT = -3133
815431 feet/sec YDOT = -1007
597375 meter/sec
ZDOT = -19616
086403 ZDOT = -6001
751490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4680415
06 X = -1426590
51
Y = 21735772
28 feet Y = 6625063
39 meter
Z = -879515
78 Z = -268076
41
XDOT = -13523
200530 XDOT = -4121
871521
YDOT = -3701
586896 feet/sec YDOT = -1128
243686 meter/sec
ZDOT = -19709
875365 ZDOT = -6007
570011
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 12210
17381443
00016717 00000-0 10270-3 0 9150
2 25544 51
6389 277
5824 0005286 279
0689 80
9866 15
54824023 24390
Satellite: ISS
Catalog Number: 25544
Epoch time: 12210
17381443 = yrday
fracday
Element set: 915
Inclination: 51
6389 deg
RA of node: 277
5824 deg
Eccentricity:
0005286
Arg of perigee: 279
0689 deg
Mean anomaly: 80
9866 deg
Mean motion: 15
54824023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2439
Checksum: 334
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