[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 30th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
There are no maneuvers
Coasting Arc #1 (Orbit 1992)
---------------------------------------
Vector Time (GMT): 2012/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1436655
14 A = 6775315
09 meter
Y = -4763578
83 meter E =
0017221
Z = -4614682
19 I = 51
93584
XDOT = 5352
630684 Wp = 82
32271
YDOT = 4554
078359 meter/sec RA = 60
20570 deg
ZDOT = -3042
084829 TA = 157
41365
MA = 157
33776
Ha = 221
052 n
mi
Hp = 209
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4713435
51 X = 1512232
88
Y = -15628539
48 feet Y = -4747090
06 meter
Z = -15140033
42 Z = -4607520
02
XDOT = 17561
124290 XDOT = 5316
086063
YDOT = 14941
201966 feet/sec YDOT = 4613
730877 meter/sec
ZDOT = -9980
593270 ZDOT = -3016
169990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16107063
52 X = -4909432
96
Y = -2817706
45 feet Y = -858836
93 meter
Z = -15109975
76 Z = -4605520
61
XDOT = 12419
237500 XDOT = 3785
383590
YDOT = -18173
869032 feet/sec YDOT = -5539
395281 meter/sec
ZDOT = -9874
231388 ZDOT = -3009
665727
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 12181
52147126
00016717 00000-0 10270-3 0 9008
2 25544 51
6406 60
7423 0007601 99
5964 260
6049 15
55860029 19932
Satellite: ISS
Catalog Number: 25544
Epoch time: 12181
52147126 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 60
7423 deg
Eccentricity:
0007601
Arg of perigee: 99
5964 deg
Mean anomaly: 260
6049 deg
Mean motion: 15
55860029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1993
Checksum: 304
Coasting Arc #2 (Orbit 2008)
---------------------------------------
Vector Time (GMT): 2012/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3033860
07 A = 6772358
28 meter
Y = 2913243
48 meter E =
0010455
Z = 5299458
89 I = 51
91037
XDOT = -4739
606518 Wp = 105
76664
YDOT = -6013
431093 meter/sec RA = 55
21055 deg
ZDOT = 588
645795 TA = 338
62242
MA = 338
66606
Ha = 221
137 n
mi
Hp = 209
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9953609
16 X = -3091954
73
Y = 9557885
45 feet Y = 2878991
30 meter
Z = 17386676
14 Z = 5284579
84
XDOT = -15549
890150 XDOT = -4674
870358
YDOT = -19729
104635 feet/sec YDOT = -6066
070444 meter/sec
ZDOT = 1931
252608 ZDOT = 565
777186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10889222
51 X = 3319035
02
Y = 8601945
86 feet Y = 2621873
10 meter
Z = 17324992
84 Z = 5280657
82
XDOT = -16695
005752 XDOT = -5088
637753
YDOT = 17408
376873 feet/sec YDOT = 5306
073271 meter/sec
ZDOT = 1837
621976 ZDOT = 560
107178
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 12182
54915744
00016717 00000-0 10270-3 0 9011
2 25544 51
6409 55
6055 0007651 103
5520 256
6486 15
55876679 20095
Satellite: ISS
Catalog Number: 25544
Epoch time: 12182
54915744 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 55
6055 deg
Eccentricity:
0007651
Arg of perigee: 103
5520 deg
Mean anomaly: 256
6486 deg
Mean motion: 15
55876679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2009
Checksum: 320
Coasting Arc #3 (Orbit 2023)
---------------------------------------
Vector Time (GMT): 2012/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4470222
56 A = 6773552
85 meter
Y = -811661
71 meter E =
0020289
Z = -5042346
15 I = 51
89562
XDOT = 3428
423569 Wp = 105
29644
YDOT = 6550
484356 meter/sec RA = 50
20963 deg
ZDOT = 1986
439201 TA = 183
94895
MA = 183
96499
Ha = 220
924 n
mi
Hp = 209
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14666084
50 X = 4503461
04
Y = -2662932
12 feet Y = -761486
16 meter
Z = -16543130
42 Z = -5020549
43
XDOT = 11248
108821 XDOT = 3345
270237
YDOT = 21491
090408 feet/sec YDOT = 6588
357821 meter/sec
ZDOT = 6517
188979 ZDOT = 2002
893516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4975848
86 X = -1516638
73
Y = -14156100
12 feet Y = -4314779
32 meter
Z = -16453150
57 Z = -5014920
29
XDOT = 18405
983626 XDOT = 5610
143809
YDOT = -14116
851673 feet/sec YDOT = -4302
816390 meter/sec
ZDOT = 6584
300082 ZDOT = 2006
894665
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 12183
51260322
00016717 00000-0 10270-3 0 9025
2 25544 51
6404 50
7889 0007501 106
7945 253
4032 15
55896325 20240
Satellite: ISS
Catalog Number: 25544
Epoch time: 12183
51260322 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 50
7889 deg
Eccentricity:
0007501
Arg of perigee: 106
7945 deg
Mean anomaly: 253
4032 deg
Mean motion: 15
55896325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2024
Checksum: 289
Coasting Arc #4 (Orbit 2039)
---------------------------------------
Vector Time (GMT): 2012/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5451855
99 A = 6777978
82 meter
Y = -1249145
41 meter E =
0018432
Z = 3811885
02 I = 51
89074
XDOT = -1529
818135 Wp = 93
07509
YDOT = -6234
532756 meter/sec RA = 45
21948 deg
ZDOT = -4214
487712 TA = 41
22055
MA = 41
08151
Ha = 220
907 n
mi
Hp = 209
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17886666
63 X = -5455999
75
Y = -4098246
09 feet Y = -1310135
31 meter
Z = 12506184
43 Z = 3785390
01
XDOT = -5019
088368 XDOT = -1439
515718
YDOT = -20454
503793 feet/sec YDOT = -6251
134442 meter/sec
ZDOT = -13827
059424 ZDOT = -4221
701266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -875654
17 X = -266899
39
Y = 18403240
16 feet Y = 5609307
60 meter
Z = 12397059
92 Z = 3778623
86
XDOT = -17927
288102 XDOT = -5464
237414
YDOT = 8517
809280 feet/sec YDOT = 2596
228269 meter/sec
ZDOT = -13856
091703 ZDOT = -4223
336751
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 12184
54026776
00016717 00000-0 10270-3 0 9033
2 25544 51
6405 45
6520 0007382 109
6954 250
4997 15
55943607 20406
Satellite: ISS
Catalog Number: 25544
Epoch time: 12184
54026776 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 45
6520 deg
Eccentricity:
0007382
Arg of perigee: 109
6954 deg
Mean anomaly: 250
4997 deg
Mean motion: 15
55943607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2040
Checksum: 313
Coasting Arc #5 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2012/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5803534
88 A = 6782658
18 meter
Y = 2945965
84 meter E =
0011491
Z = -1912815
71 I = 51
88262
XDOT = -764
255694 Wp = 76
75053
YDOT = 5142
424972 meter/sec RA = 40
24484 deg
ZDOT = 5632
133653 TA = 262
24736
MA = 262
37784
Ha = 220
829 n
mi
Hp = 209
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19040468
75 X = 5779453
06
Y = 9665242
25 feet Y = 3010730
25 meter
Z = -6275642
08 Z = -1884680
70
XDOT = -2507
400572 XDOT = -849
061835
YDOT = 16871
473006 feet/sec YDOT = 5133
403411 meter/sec
ZDOT = 18478
128782 ZDOT = 5628
215905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5806985
18 X = 1769969
08
Y = -20583343
43 feet Y = -6273803
08 meter
Z = -6159946
28 Z = -1877551
63
XDOT = 15560
379087 XDOT = 4742
803546
YDOT = -1104
041112 feet/sec YDOT = -336
511731 meter/sec
ZDOT = 18461
375131 ZDOT = 5627
027140
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 12185
50369527
00016717 00000-0 10270-3 0 9045
2 25544 51
6392 40
8352 0007342 113
8724 246
3200 15
55907244 20553
Satellite: ISS
Catalog Number: 25544
Epoch time: 12185
50369527 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 40
8352 deg
Eccentricity:
0007342
Arg of perigee: 113
8724 deg
Mean anomaly: 246
3200 deg
Mean motion: 15
55907244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 292
Coasting Arc #6 (Orbit 2070)
---------------------------------------
Vector Time (GMT): 2012/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5333354
89 A = 6784079
70 meter
Y = -4161514
91 meter E =
0018347
Z = -403283
31 I = 51
86320
XDOT = 3194
074907 Wp = 129
83788
YDOT = -3528
870723 meter/sec RA = 35
28148 deg
ZDOT = -6018
791235 TA = 54
50124
MA = 54
33021
Ha = 220
775 n
mi
Hp = 209
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17497883
49 X = -5284464
56
Y = -13653264
14 feet Y = -4220882
36 meter
Z = -1323107
96 Z = -429073
99
XDOT = 10479
248383 XDOT = 3262
535509
YDOT = -11577
659854 feet/sec YDOT = -3492
768844 meter/sec
ZDOT = -19746
690405 ZDOT = -6003
109102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9685003
09 X = -2951988
94
Y = 19962385
82 feet Y = 6084535
20 meter
Z = -1428996
26 Z = -435558
06
XDOT = -12087
453303 XDOT = -3684
255767
YDOT = -7231
438848 feet/sec YDOT = -2204
142561 meter/sec
ZDOT = -19681
600590 ZDOT = -5998
951860
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 12186
53134069
00016717 00000-0 10270-3 0 9051
2 25544 51
6389 35
6976 0007412 118
4453 241
7448 15
55908709 20719
Satellite: ISS
Catalog Number: 25544
Epoch time: 12186
53134069 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 35
6976 deg
Eccentricity:
0007412
Arg of perigee: 118
4453 deg
Mean anomaly: 241
7448 deg
Mean motion: 15
55908709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2071
Checksum: 324
Coasting Arc #7 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2012/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4085610
83 A = 6781092
43 meter
Y = 4744918
67 meter E =
0019432
Z = 2587558
56 I = 51
82749
XDOT = -5318
476225 Wp = 92
09657
YDOT = 1687
771172 meter/sec RA = 30
31200 deg
ZDOT = 5267
871523 TA = 296
96906
MA = 297
16738
Ha = 220
585 n
mi
Hp = 209
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13404235
02 X = 4019678
99
Y = 15567318
48 feet Y = 4790237
50 meter
Z = 8489365
36 Z = 2607246
42
XDOT = -17449
068980 XDOT = -5362
543596
YDOT = 5537
306995 feet/sec YDOT = 1628
049552 meter/sec
ZDOT = 17283
043055 ZDOT = 5241
928282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12141514
41 X = 3700733
59
Y = -16529449
46 feet Y = -5038176
20 meter
Z = 8570015
95 Z = 2612140
86
XDOT = 8162
790605 XDOT = 2488
018576
YDOT = 14959
617165 feet/sec YDOT = 4559
691312 meter/sec
ZDOT = 17175
844714 ZDOT = 5235
197469
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 12187
55897337
00016717 00000-0 10270-3 0 9069
2 25544 51
6380 30
5589 0007267 122
5856 237
6000 15
55968096 20875
Satellite: ISS
Catalog Number: 25544
Epoch time: 12187
55897337 = yrday
fracday
Element set: 906
Inclination: 51
6380 deg
RA of node: 30
5589 deg
Eccentricity:
0007267
Arg of perigee: 122
5856 deg
Mean anomaly: 237
6000 deg
Mean motion: 15
55968096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 338
Coasting Arc #8 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2012/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2098123
12 A = 6775971
73 meter
Y = -4773079
87 meter E =
0014229
Z = -4339332
55 I = 51
78255
XDOT = 6813
404881 Wp = 94
26567
YDOT = 176
196863 meter/sec RA = 25
32547 deg
ZDOT = -3499
088023 TA = 140
24386
MA = 140
13950
Ha = 220
603 n
mi
Hp = 209
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6883606
03 X = -2023514
51
Y = -15659710
85 feet Y = -4796124
73 meter
Z = -14236655
35 Z = -4349344
28
XDOT = 22353
690554 XDOT = 6827
925690
YDOT = 578
073696 feet/sec YDOT = 252
470170 meter/sec
ZDOT = -11479
947582 ZDOT = -3465
954124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13538867
25 X = -4126646
74
Y = 10399424
64 feet Y = 3169744
63 meter
Z = -14277393
75 Z = -4351749
61
XDOT = -4132
187301 XDOT = -1259
490689
YDOT = -20903
891331 feet/sec YDOT = -6371
506078 meter/sec
ZDOT = -11343
309656 ZDOT = -3457
440783
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 12188
52237188
00016717 00000-0 10270-3 0 9070
2 25544 51
6370 25
7416 0007335 125
2185 234
9656 15
55961669 21024
Satellite: ISS
Catalog Number: 25544
Epoch time: 12188
52237188 = yrday
fracday
Element set: 907
Inclination: 51
6370 deg
RA of node: 25
7416 deg
Eccentricity:
0007335
Arg of perigee: 125
2185 deg
Mean anomaly: 234
9656 deg
Mean motion: 15
55961669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 318
Coasting Arc #9 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2012/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -274056
93 A = 6772450
20 meter
Y = 4292012
14 meter E =
0011056
Z = 5224940
37 I = 51
74274
XDOT = -7379
856934 Wp = 126
18517
YDOT = -1812
829003 meter/sec RA = 20
31982 deg
ZDOT = 1094
063857 TA = 313
31312
MA = 313
40525
Ha = 220
633 n
mi
Hp = 209
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -899136
89 X = -347411
88
Y = 14081404
67 feet Y = 4288536
83 meter
Z = 17142192
81 Z = 5223431
26
XDOT = -24212
129049 XDOT = -7364
351649
YDOT = -5947
601715 feet/sec YDOT = -1895
268547 meter/sec
ZDOT = 3589
448350 ZDOT = 1058
250918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13859948
72 X = 4224512
37
Y = -2688242
16 feet Y = -819376
21 meter
Z = 17135470
65 Z = 5222891
46
XDOT = 354
732651 XDOT = 108
122512
YDOT = 23935
957718 feet/sec YDOT = 7295
679912 meter/sec
ZDOT = 3441
955183 ZDOT = 1049
107940
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 12189
54998696
00016717 00000-0 10270-3 0 9082
2 25544 51
6373 20
6033 0007355 128
7051 231
4762 15
55936798 21180
Satellite: ISS
Catalog Number: 25544
Epoch time: 12189
54998696 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 20
6033 deg
Eccentricity:
0007355
Arg of perigee: 128
7051 deg
Mean anomaly: 231
4762 deg
Mean motion: 15
55936798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 336
Coasting Arc #10 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2012/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2751177
57 A = 6772767
09 meter
Y = -3460674
73 meter E =
0020301
Z = -5148785
19 I = 51
71468
XDOT = 6817
512603 Wp = 112
28847
YDOT = 3125
477160 meter/sec RA = 15
30469 deg
ZDOT = 1539
442461 TA = 172
56917
MA = 172
53904
Ha = 220
499 n
mi
Hp = 209
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9026173
15 X = 2814682
38
Y = -11353919
72 feet Y = -3429553
87 meter
Z = -16892339
85 Z = -5135266
29
XDOT = 22367
167333 XDOT = 6774
578019
YDOT = 10254
190158 feet/sec YDOT = 3201
474631 meter/sec
ZDOT = 5050
664243 ZDOT = 1572
457158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13435335
69 X = -4095090
32
Y = -5636408
15 feet Y = -1717977
20 meter
Z = -16836184
20 Z = -5131668
94
XDOT = 3272
992371 XDOT = 997
608075
YDOT = -23320
003122 feet/sec YDOT = -7107
936952 meter/sec
ZDOT = 5186
458350 ZDOT = 1580
832505
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 12190
51336410
00016717 00000-0 10270-3 0 9092
2 25544 51
6368 15
7854 0007403 132
7481 227
4297 15
55993873 21338
Satellite: ISS
Catalog Number: 25544
Epoch time: 12190
51336410 = yrday
fracday
Element set: 909
Inclination: 51
6368 deg
RA of node: 15
7854 deg
Eccentricity:
0007403
Arg of perigee: 132
7481 deg
Mean anomaly: 227
4297 deg
Mean motion: 15
55993873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 314
Coasting Arc #11 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2012/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4872519
97 A = 6776984
35 meter
Y = 2369685
74 meter E =
0015823
Z = 4055111
56 I = 51
69952
XDOT = -5224
020913 Wp = 100
93011
YDOT = -4070
478747 meter/sec RA = 10
29834 deg
ZDOT = -3888
476733 TA = 29
29394
MA = 29
20531
Ha = 220
486 n
mi
Hp = 209
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15985957
89 X = -4918354
76
Y = 7774559
52 feet Y = 2314941
62 meter
Z = 13304171
78 Z = 4031330
16
XDOT = -17139
176225 XDOT = -5159
226570
YDOT = -13354
589064 feet/sec YDOT = -4128
534408 meter/sec
ZDOT = -12757
469595 ZDOT = -3913
697468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12138858
68 X = 3699924
13
Y = 13086250
94 feet Y = 3988689
29 meter
Z = 13205822
90 Z = 4025134
82
XDOT = -6820
653455 XDOT = -2078
935173
YDOT = 19338
436585 feet/sec YDOT = 5894
355471 meter/sec
ZDOT = -12861
004724 ZDOT = -3920
034240
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 12191
54095687
00016717 00000-0 10270-3 0 9106
2 25544 51
6372 10
6477 0007275 137
1603 223
0119 15
56002229 21499
Satellite: ISS
Catalog Number: 25544
Epoch time: 12191
54095687 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 10
6477 deg
Eccentricity:
0007275
Arg of perigee: 137
1603 deg
Mean anomaly: 223
0119 deg
Mean motion: 15
56002229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 289
Coasting Arc #12 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2012/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6305797
04 A = 6781806
55 meter
Y = -1171072
24 meter E =
0009014
Z = -2213896
90 I = 51
68573
XDOT = 2767
915599 Wp = 96
64101
YDOT = 4597
777872 meter/sec RA = 5
30734 deg
ZDOT = 5469
849970 TA = 238
78539
MA = 238
87376
Ha = 220
367 n
mi
Hp = 209
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20688310
51 X = 6329178
09
Y = -3842100
52 feet Y = -1100425
99 meter
Z = -7263441
28 Z = -2183207
14
XDOT = 9081
087923 XDOT = 2689
725476
YDOT = 15084
573070 feet/sec YDOT = 4628
292792 meter/sec
ZDOT = 17945
702002 ZDOT = 5483
106739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10064520
82 X = -3067665
95
Y = -18528296
24 feet Y = -5647424
69 meter
Z = -7136747
61 Z = -2175280
67
XDOT = 10221
562994 XDOT = 3115
532401
YDOT = -12462
223304 feet/sec YDOT = -3798
485663 meter/sec
ZDOT = 17999
832808 ZDOT = 5486
349040
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 12192
50431637
00016717 00000-0 10270-3 0 9113
2 25544 51
6372 5
8303 0007437 140
1872 219
9829 15
56024474 21640
Satellite: ISS
Catalog Number: 25544
Epoch time: 12192
50431637 = yrday
fracday
Element set: 911
Inclination: 51
6372 deg
RA of node: 5
8303 deg
Eccentricity:
0007437
Arg of perigee: 140
1872 deg
Mean anomaly: 219
9829 deg
Mean motion: 15
56024474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 297
Coasting Arc #13 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2012/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6772379
22 A = 6783654
55 meter
Y = -121021
94 meter E =
0018970
Z = -103835
40 I = 51
66214
XDOT = 167
404181 Wp = 137
95818
YDOT = -4759
769901 meter/sec RA =
32914 deg
ZDOT = -6019
849443 TA = 43
16156
MA = 43
01301
Ha = 220
101 n
mi
Hp = 209
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22219091
93 X = -6770018
18
Y = -397053
60 feet Y = -196741
67 meter
Z = -340667
32 Z = -136729
43
XDOT = 549
226315 XDOT = 249
859386
YDOT = -15616
042982 feet/sec YDOT = -4757
436295 meter/sec
ZDOT = -19750
162215 ZDOT = -6018
836363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6856139
18 X = 2089751
22
Y = 21135946
89 feet Y = 6442236
61 meter
Z = -476294
46 Z = -145174
55
XDOT = -13443
579685 XDOT = -4097
603088
YDOT = 3950
225048 feet/sec YDOT = 1204
028595 meter/sec
ZDOT = -19745
426868 ZDOT = -6018
406109
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 12193
53188750
00016717 00000-0 10270-3 0 9123
2 25544 51
6372
6923 0007168 142
9527 217
2123 15
56081098 21800
Satellite: ISS
Catalog Number: 25544
Epoch time: 12193
53188750 = yrday
fracday
Element set: 912
Inclination: 51
6372 deg
RA of node:
6923 deg
Eccentricity:
0007168
Arg of perigee: 142
9527 deg
Mean anomaly: 217
2123 deg
Mean motion: 15
56081098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 297
Coasting Arc #14 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2012/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6207374
06 A = 6781286
80 meter
Y = 1364903
25 meter E =
0017417
Z = 2353655
82 I = 51
62359
XDOT = -3052
219074 Wp = 97
55346
YDOT = 4528
654346 meter/sec RA = 355
34743 deg
ZDOT = 5387
103886 TA = 288
74092
MA = 288
92984
Ha = 220
145 n
mi
Hp = 209
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20365400
47 X = 6180216
61
Y = 4478029
04 feet Y = 1434165
86 meter
Z = 7721967
91 Z = 2383745
02
XDOT = -10013
842105 XDOT = -3128
801793
YDOT = 14857
789850 feet/sec YDOT = 4494
093771 meter/sec
ZDOT = 17674
225349 ZDOT = 5372
090865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2734099
70 X = -833353
59
Y = -20625177
62 feet Y = -6286554
14 meter
Z = 7845878
91 Z = 2391423
89
XDOT = 15919
189206 XDOT = 4852
168870
YDOT = 4634
034678 feet/sec YDOT = 1412
453770 meter/sec
ZDOT = 17611
787154 ZDOT = 5368
072725
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 12194
55945012
00016717 00000-0 10270-3 0 9139
2 25544 51
6372 355
5540 0007440 147
7219 212
4391 15
56062847 21963
Satellite: ISS
Catalog Number: 25544
Epoch time: 12194
55945012 = yrday
fracday
Element set: 913
Inclination: 51
6372 deg
RA of node: 355
5540 deg
Eccentricity:
0007440
Arg of perigee: 147
7219 deg
Mean anomaly: 212
4391 deg
Mean motion: 15
56062847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 306
Coasting Arc #15 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2012/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4658885
75 A = 6776080
19 meter
Y = -2583245
98 meter E =
0011832
Z = -4195076
94 I = 51
57691
XDOT = 5472
014513 Wp = 107
46133
YDOT = -3898
419423 meter/sec RA = 350
34901 deg
ZDOT = -3688
491829 TA = 124
69612
MA = 124
58458
Ha = 220
028 n
mi
Hp = 209
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15285058
22 X = -4609274
46
Y = -8475216
47 feet Y = -2635066
64 meter
Z = -13763375
77 Z = -4217589
30
XDOT = 17952
803519 XDOT = 5533
118524
YDOT = -12790
089971 feet/sec YDOT = -3836
885872 meter/sec
ZDOT = -12101
351144 ZDOT = -3661
761189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2475499
16 X = -754532
14
Y = 17227269
22 feet Y = 5250871
66 meter
Z = -13855898
05 Z = -4223277
73
XDOT = -17138
165434 XDOT = -5223
712824
YDOT = -12075
184330 feet/sec YDOT = -3680
516184 meter/sec
ZDOT = -11990
670966 ZDOT = -3654
756510
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
52277937
00016717 00000-0 10270-3 0 9142
2 25544 51
6380 350
7374 0007382 150
0812 210
0765 15
56082382 22118
Satellite: ISS
Catalog Number: 25544
Epoch time: 12195
52277937 = yrday
fracday
Element set: 914
Inclination: 51
6380 deg
RA of node: 350
7374 deg
Eccentricity:
0007382
Arg of perigee: 150
0812 deg
Mean anomaly: 210
0765 deg
Mean motion: 15
56082382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 294
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