[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 8th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
172/13:49:37
930 -0
8 4
2 4
2
N/A 4
1 0
0 221
1
000/00:09:15
860 -0
4 -0
1 209
8
Coasting Arc #1 (Orbit 1634)
---------------------------------------
Vector Time (GMT): 2012/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6742922
11 A = 6783193
35 meter
Y = -19353
32 meter E =
0012868
Z = -751279
40 I = 51
68165
XDOT = -639
862004 Wp = 88
27776
YDOT = 4783
186928 meter/sec RA = 174
78413 deg
ZDOT = -5953
909509 TA = 99
83581
MA = 99
69050
Ha = 221
145 n
mi
Hp = 208
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22122447
86 X = 6746286
91
Y = -63495
14 feet Y = 56069
15 meter
Z = -2464827
42 Z = -718514
47
XDOT = -2099
284790 XDOT = -664
378326
YDOT = 15692
870500 feet/sec YDOT = 4775
895515 meter/sec
ZDOT = -19533
823849 ZDOT = -5957
076673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5854652
69 X = 1784498
14
Y = -21348922
54 feet Y = -6507151
59 meter
Z = -2329947
12 Z = -710167
88
XDOT = 13034
914584 XDOT = 3973
041965
YDOT = 5674
723084 feet/sec YDOT = 1729
655596 meter/sec
ZDOT = -19547
263862 ZDOT = -5958
006025
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 12158
53080079
00016717 00000-0 10270-3 0 9006
2 25544 51
6351 175
6985 0010478 35
5433 324
6417 15
56164780 16352
Satellite: ISS
Catalog Number: 25544
Epoch time: 12158
53080079 = yrday
fracday
Element set: 900
Inclination: 51
6351 deg
RA of node: 175
6985 deg
Eccentricity:
0010478
Arg of perigee: 35
5433 deg
Mean anomaly: 324
6417 deg
Mean motion: 15
56164780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1635
Checksum: 312
Coasting Arc #2 (Orbit 1650)
---------------------------------------
Vector Time (GMT): 2012/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5945685
61 A = 6779729
34 meter
Y = -1302631
79 meter E =
0022173
Z = 2956224
82 I = 51
70004
XDOT = 3516
334885 Wp = 63
27742
YDOT = -4648
480577 meter/sec RA = 169
80257 deg
ZDOT = 5004
761451 TA = 330
55026
MA = 330
67500
Ha = 221
271 n
mi
Hp = 208
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19506842
56 X = -5945038
02
Y = -4273726
36 feet Y = -1369116
95 meter
Z = 9698900
32 Z = 2927342
46
XDOT = 11536
531774 XDOT = 3543
741922
YDOT = -15250
920528 feet/sec YDOT = -4609
006251 meter/sec
ZDOT = 16419
821032 ZDOT = 5021
909442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9040417
78 X = -2755519
34
Y = 17870168
18 feet Y = 5446827
26 meter
Z = 9580096
38 Z = 2920013
38
XDOT = -10593
783406 XDOT = -3228
985182
YDOT = -14234
037107 feet/sec YDOT = -4338
534510 meter/sec
ZDOT = 16490
812034 ZDOT = 5026
399508
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 12159
55827664
00016717 00000-0 10270-3 0 9019
2 25544 51
6347 170
5598 0010563 38
8721 321
3191 15
56185511 16518
Satellite: ISS
Catalog Number: 25544
Epoch time: 12159
55827664 = yrday
fracday
Element set: 901
Inclination: 51
6347 deg
RA of node: 170
5598 deg
Eccentricity:
0010563
Arg of perigee: 38
8721 deg
Mean anomaly: 321
3191 deg
Mean motion: 15
56185511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1651
Checksum: 311
Coasting Arc #3 (Orbit 1665)
---------------------------------------
Vector Time (GMT): 2012/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4231338
77 A = 6774378
22 meter
Y = 2624495
65 meter E =
0020012
Z = -4613399
63 I = 51
71234
XDOT = -5775
702712 Wp = 56
19698
YDOT = 4026
888130 meter/sec RA = 164
80443 deg
ZDOT = -3005
055123 TA = 183
78815
MA = 183
80332
Ha = 221
200 n
mi
Hp = 208
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13882345
03 X = 4224087
36
Y = 8610550
03 feet Y = 2671773
14 meter
Z = -15135825
57 Z = -4592861
37
XDOT = -18949
155879 XDOT = -5805
705140
YDOT = 13211
575230 feet/sec YDOT = 3962
133278 meter/sec
ZDOT = -9859
104735 ZDOT = -3033
185428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11639822
86 X = 3547818
01
Y = -11572463
34 feet Y = -3527286
83 meter
Z = -15051475
25 Z = -4587689
66
XDOT = 7581
672844 XDOT = 2310
893883
YDOT = 20606
331231 feet/sec YDOT = 6280
809759 meter/sec
ZDOT = -9975
273543 ZDOT = -3040
463376
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 12160
52152071
00016717 00000-0 10270-3 0 9022
2 25544 51
6349 165
7417 0010527 42
3474 317
8491 15
56209571 16663
Satellite: ISS
Catalog Number: 25544
Epoch time: 12160
52152071 = yrday
fracday
Element set: 902
Inclination: 51
6349 deg
RA of node: 165
7417 deg
Eccentricity:
0010527
Arg of perigee: 42
3474 deg
Mean anomaly: 317
8491 deg
Mean motion: 15
56209571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1666
Checksum: 299
Coasting Arc #4 (Orbit 1681)
---------------------------------------
Vector Time (GMT): 2012/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1867207
50 A = 6771282
50 meter
Y = -3766979
48 meter E =
0011969
Z = 5298802
72 I = 51
73092
XDOT = 7080
870663 Wp = 57
59308
YDOT = -2947
394057 meter/sec RA = 159
79068 deg
ZDOT = 405
450379 TA = 28
58432
MA = 28
51875
Ha = 221
271 n
mi
Hp = 208
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6126008
86 X = -1850685
85
Y = -12358856
56 feet Y = -3787767
94 meter
Z = 17384523
37 Z = 5289771
68
XDOT = 23231
202964 XDOT = 7111
333181
YDOT = -9669
928007 feet/sec YDOT = -2868
041095 meter/sec
ZDOT = 1330
217780 ZDOT = 439
922444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13416224
57 X = -4089265
25
Y = 3399266
29 feet Y = 1036096
36 meter
Z = 17347647
68 Z = 5287563
01
XDOT = -4147
651115 XDOT = -1264
204060
YDOT = -23790
142581 feet/sec YDOT = -7251
235459 meter/sec
ZDOT = 1472
425051 ZDOT = 448
795155
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 12161
54896627
00016717 00000-0 10270-3 0 9038
2 25544 51
6343 160
6021 0010541 45
7414 314
4603 15
56233811 16829
Satellite: ISS
Catalog Number: 25544
Epoch time: 12161
54896627 = yrday
fracday
Element set: 903
Inclination: 51
6343 deg
RA of node: 160
6021 deg
Eccentricity:
0010541
Arg of perigee: 45
7414 deg
Mean anomaly: 314
4603 deg
Mean motion: 15
56233811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1682
Checksum: 281
Coasting Arc #5 (Orbit 1696)
---------------------------------------
Vector Time (GMT): 2012/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -660187
74 A = 6772880
10 meter
Y = 4608865
72 meter E =
0020068
Z = -4934661
98 I = 51
76474
XDOT = -7177
334661 Wp = 80
36280
YDOT = 1397
795705 meter/sec RA = 154
77727 deg
ZDOT = 2276
894990 TA = 211
81738
MA = 211
93878
Ha = 221
271 n
mi
Hp = 208
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2165970
26 X = -687704
53
Y = 15120950
53 feet Y = 4601329
70 meter
Z = -16189835
89 Z = -4937935
54
XDOT = -23547
685897 XDOT = -7203
492274
YDOT = 4585
943914 feet/sec YDOT = 1317
387835 meter/sec
ZDOT = 7470
127921 ZDOT = 2241
964499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14399141
46 X = 4388858
32
Y = 5054702
73 feet Y = 1540673
39 meter
Z = -16203705
24 Z = -4938889
36
XDOT = 135
022837 XDOT = 41
154961
YDOT = 22983
312319 feet/sec YDOT = 7005
313595 meter/sec
ZDOT = 7326
148513 ZDOT = 2233
010067
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 12162
51218207
00016717 00000-0 10270-3 0 9049
2 25544 51
6344 155
7849 0010561 48
8733 311
3331 15
56233410 16978
Satellite: ISS
Catalog Number: 25544
Epoch time: 12162
51218207 = yrday
fracday
Element set: 904
Inclination: 51
6344 deg
RA of node: 155
7849 deg
Eccentricity:
0010561
Arg of perigee: 48
8733 deg
Mean anomaly: 311
3331 deg
Mean motion: 15
56233410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1697
Checksum: 291
Coasting Arc #6 (Orbit 1712)
---------------------------------------
Vector Time (GMT): 2012/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3015792
52 A = 6777746
08 meter
Y = -4947817
47 meter E =
0021627
Z = 3504941
29 I = 51
80827
XDOT = 6171
760498 Wp = 71
61162
YDOT = 530
649325 meter/sec RA = 149
77782 deg
ZDOT = -4531
788649 TA = 67
20134
MA = 66
97302
Ha = 221
176 n
mi
Hp = 207
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9894332
42 X = 3053869
66
Y = -16232996
95 feet Y = -4913880
42 meter
Z = 11499151
20 Z = 3519683
93
XDOT = 20248
558064 XDOT = 6187
382386
YDOT = 1740
975476 feet/sec YDOT = 599
753520 meter/sec
ZDOT = -14868
072997 ZDOT = -4501
768502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14154237
75 X = -4314211
67
Y = -12635492
13 feet Y = -3851298
00 meter
Z = 11560293
02 Z = 3523577
31
XDOT = 4520
765866 XDOT = 1377
929436
YDOT = -18642
160311 feet/sec YDOT = -5682
130463 meter/sec
ZDOT = -14744
468788 ZDOT = -4494
114087
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 12163
53959603
00016717 00000-0 10270-3 0 9055
2 25544 51
6339 150
6449 0010558 52
0253 308
1853 15
56300160 17131
Satellite: ISS
Catalog Number: 25544
Epoch time: 12163
53959603 = yrday
fracday
Element set: 905
Inclination: 51
6339 deg
RA of node: 150
6449 deg
Eccentricity:
0010558
Arg of perigee: 52
0253 deg
Mean anomaly: 308
1853 deg
Mean motion: 15
56300160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1713
Checksum: 290
Coasting Arc #7 (Orbit 1727)
---------------------------------------
Vector Time (GMT): 2012/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4709450
96 A = 6782096
75 meter
Y = 4667199
08 meter E =
0018891
Z = -1399336
75 I = 51
84848
XDOT = -4273
601554 Wp = 48
55398
YDOT = -2584
795161 meter/sec RA = 144
80136 deg
ZDOT = 5824
618068 TA = 296
22181
MA = 296
41588
Ha = 221
236 n
mi
Hp = 207
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15450954
60 X = -4754492
83
Y = 15312332
93 feet Y = 4614283
36 meter
Z = -4590999
83 Z = -1422324
12
XDOT = -14021
002474 XDOT = -4272
675006
YDOT = -8480
299085 feet/sec YDOT = -2632
580572 meter/sec
ZDOT = 19109
639331 ZDOT = 5803
859038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12529728
84 X = 3819061
35
Y = 17757344
44 feet Y = 5412438
59 meter
Z = -4686089
08 Z = -1428319
95
XDOT = -9420
180218 XDOT = -2871
270930
YDOT = 11614
037365 feet/sec YDOT = 3539
958589 meter/sec
ZDOT = 19024
350063 ZDOT = 5798
621899
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 12164
50278294
00016717 00000-0 10270-3 0 9064
2 25544 51
6336 145
8276 0010640 56
6637 303
5534 15
56319187 17280
Satellite: ISS
Catalog Number: 25544
Epoch time: 12164
50278294 = yrday
fracday
Element set: 906
Inclination: 51
6336 deg
RA of node: 145
8276 deg
Eccentricity:
0010640
Arg of perigee: 56
6637 deg
Mean anomaly: 303
5534 deg
Mean motion: 15
56319187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1728
Checksum: 318
Coasting Arc #8 (Orbit 1743)
---------------------------------------
Vector Time (GMT): 2012/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5621419
06 A = 6782444
89 meter
Y = -3640572
55 meter E =
0015272
Z = -1074953
76 I = 51
87436
XDOT = 1819
441837 Wp = 98
23510
YDOT = 4532
179587 meter/sec RA = 139
83523 deg
ZDOT = -5908
308645 TA = 93
38698
MA = 93
21227
Ha = 221
280 n
mi
Hp = 207
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18442975
90 X = 5666932
80
Y = -11944135
66 feet Y = -3577455
77 meter
Z = -3526751
17 Z = -1047534
79
XDOT = 5969
297365 XDOT = 1797
328265
YDOT = 14869
355601 feet/sec YDOT = 4552
402669 meter/sec
ZDOT = -19384
214716 ZDOT = -5899
523074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9048662
32 X = -2758032
27
Y = -20042793
37 feet Y = -6109043
42 meter
Z = -3413481
34 Z = -1040429
11
XDOT = 14149
742283 XDOT = 4312
841448
YDOT = -3135
495596 feet/sec YDOT = -955
699058 meter/sec
ZDOT = -19348
416406 ZDOT = -5897
397321
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 12165
53016558
00016717 00000-0 10270-3 0 9072
2 25544 51
6339 140
6868 0010637 59
2430 300
9770 15
56338304 17442
Satellite: ISS
Catalog Number: 25544
Epoch time: 12165
53016558 = yrday
fracday
Element set: 907
Inclination: 51
6339 deg
RA of node: 140
6868 deg
Eccentricity:
0010637
Arg of perigee: 59
2430 deg
Mean anomaly: 300
9770 deg
Mean motion: 15
56338304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1744
Checksum: 308
Coasting Arc #9 (Orbit 1759)
---------------------------------------
Vector Time (GMT): 2012/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5585486
40 A = 6778312
26 meter
Y = 1979742
60 meter E =
0022682
Z = 3265904
68 I = 51
88352
XDOT = 679
494025 Wp = 76
70225
YDOT = -5985
145090 meter/sec RA = 134
86425 deg
ZDOT = 4767
594278 TA = 321
14025
MA = 321
30311
Ha = 221
231 n
mi
Hp = 207
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18325086
61 X = -5623074
31
Y = 6495218
51 feet Y = 1917071
69 meter
Z = 10714910
36 Z = 3238679
34
XDOT = 2229
311106 XDOT = 723
210558
YDOT = -19636
302790 feet/sec YDOT = -5977
302689 meter/sec
ZDOT = 15641
713509 ZDOT = 4771
000747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4001502
80 X = 1219658
05
Y = 19088725
72 feet Y = 5818243
60 meter
Z = 10602570
08 Z = 3231663
36
XDOT = -17787
348273 XDOT = -5421
583753
YDOT = -5009
003610 feet/sec YDOT = -1526
744300 meter/sec
ZDOT = 15656
277697 ZDOT = 4772
033442
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 12166
55753001
00016717 00000-0 10270-3 0 9087
2 25544 51
6338 135
5480 0010402 63
5058 296
7161 15
56391917 17601
Satellite: ISS
Catalog Number: 25544
Epoch time: 12166
55753001 = yrday
fracday
Element set: 908
Inclination: 51
6338 deg
RA of node: 135
5480 deg
Eccentricity:
0010402
Arg of perigee: 63
5058 deg
Mean anomaly: 296
7161 deg
Mean motion: 15
56391917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1760
Checksum: 302
Coasting Arc #10 (Orbit 1774)
---------------------------------------
Vector Time (GMT): 2012/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4768661
26 A = 6773069
06 meter
Y = 197334
28 meter E =
0021893
Z = -4826571
12 I = 51
88689
XDOT = -2881
831955 Wp = 69
39183
YDOT = 6605
886505 meter/sec RA = 129
87302 deg
ZDOT = -2579
124396 TA = 175
26292
MA = 175
24217
Ha = 221
237 n
mi
Hp = 207
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15645214
11 X = 4789546
80
Y = 647422
16 feet Y = 250777
81 meter
Z = -15835207
08 Z = -4803354
22
XDOT = -9454
829249 XDOT = -2942
957234
YDOT = 21672
855988 feet/sec YDOT = 6573
318647 meter/sec
ZDOT = -8461
694214 ZDOT = -2593
271925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2459492
66 X = 749653
36
Y = -15561575
58 feet Y = -4743168
24 meter
Z = -15739565
58 Z = -4797419
59
XDOT = 19306
995473 XDOT = 5884
772220
YDOT = 11662
979276 feet/sec YDOT = 3554
876083 meter/sec
ZDOT = -8520
582001 ZDOT = -2597
073394
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 12167
52067155
00016717 00000-0 10270-3 0 9094
2 25544 51
6341 130
7285 0010541 66
4417 293
7843 15
56374037 17754
Satellite: ISS
Catalog Number: 25544
Epoch time: 12167
52067155 = yrday
fracday
Element set: 909
Inclination: 51
6341 deg
RA of node: 130
7285 deg
Eccentricity:
0010541
Arg of perigee: 66
4417 deg
Mean anomaly: 293
7843 deg
Mean motion: 15
56374037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1775
Checksum: 312
Coasting Arc #11 (Orbit 1790)
---------------------------------------
Vector Time (GMT): 2012/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3329342
79 A = 6770712
84 meter
Y = -2518811
51 meter E =
0012837
Z = 5319986
76 I = 51
89865
XDOT = 4482
853297 Wp = 72
56971
YDOT = -6236
827966 meter/sec RA = 124
86858 deg
ZDOT = -143
413584 TA = 18
81337
MA = 18
76597
Ha = 221
303 n
mi
Hp = 207
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10923040
66 X = -3326772
97
Y = -8263817
30 feet Y = -2556028
70 meter
Z = 17454024
80 Z = 5303818
71
XDOT = 14707
523940 XDOT = 4552
958280
YDOT = -20462
034009 feet/sec YDOT = -6186
305925 meter/sec
ZDOT = -470
517008 ZDOT = -121
466551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9307362
66 X = -2836884
14
Y = 10163152
02 feet Y = 3097728
74 meter
Z = 17387634
02 Z = 5299750
85
XDOT = -18175
004079 XDOT = -5539
741243
YDOT = -15972
546582 feet/sec YDOT = -4868
432198 meter/sec
ZDOT = -379
506625 ZDOT = -115
673619
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 12168
54800426
00016717 00000-0 10270-3 0 9105
2 25544 51
6345 125
5893 0010482 69
7137 290
5142 15
56408548 17914
Satellite: ISS
Catalog Number: 25544
Epoch time: 12168
54800426 = yrday
fracday
Element set: 910
Inclination: 51
6345 deg
RA of node: 125
5893 deg
Eccentricity:
0010482
Arg of perigee: 69
7137 deg
Mean anomaly: 290
5142 deg
Mean motion: 15
56408548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1791
Checksum: 313
Coasting Arc #12 (Orbit 1805)
---------------------------------------
Vector Time (GMT): 2012/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1615686
50 A = 6773298
25 meter
Y = 4604388
46 meter E =
0020205
Z = -4715188
87 I = 51
92440
XDOT = -5291
831056 Wp = 91
72145
YDOT = 4752
192229 meter/sec RA = 119
86538 deg
ZDOT = 2837
130813 TA = 206
30470
MA = 206
40745
Ha = 221
185 n
mi
Hp = 207
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5300808
74 X = 1586984
66
Y = 15106261
36 feet Y = 4622296
34 meter
Z = -15469779
77 Z = -4707408
88
XDOT = -17361
650446 XDOT = -5358
359953
YDOT = 15591
181853 feet/sec YDOT = 4692
643260 meter/sec
ZDOT = 9308
171960 ZDOT = 2811
262352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15493529
85 X = 4722427
90
Y = -4150402
97 feet Y = -1265042
83 meter
Z = -15438150
14 Z = -4705548
16
XDOT = 13822
960983 XDOT = 4213
238508
YDOT = 17497
066064 feet/sec YDOT = 5333
105736 meter/sec
ZDOT = 9201
120149 ZDOT = 2804
501421
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 12169
51111299
00016717 00000-0 10270-3 0 9117
2 25544 51
6349 120
7705 0010447 73
0967 287
1331 15
56418346 18063
Satellite: ISS
Catalog Number: 25544
Epoch time: 12169
51111299 = yrday
fracday
Element set: 911
Inclination: 51
6349 deg
RA of node: 120
7705 deg
Eccentricity:
0010447
Arg of perigee: 73
0967 deg
Mean anomaly: 287
1331 deg
Mean motion: 15
56418346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1806
Checksum: 304
Coasting Arc #13 (Orbit 1821)
---------------------------------------
Vector Time (GMT): 2012/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 182937
54 A = 6778617
37 meter
Y = -6046869
28 meter E =
0023212
Z = 3039224
77 I = 51
95785
XDOT = 5368
385180 Wp = 87
67867
YDOT = -2348
114565 meter/sec RA = 114
88032 deg
ZDOT = -4961
498570 TA = 57
57045
MA = 57
34615
Ha = 221
137 n
mi
Hp = 207
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 600188
77 X = 235777
37
Y = -19838809
99 feet Y = -6044528
63 meter
Z = 9971209
87 Z = 3040240
80
XDOT = 17612
812271 XDOT = 5418
345182
YDOT = -7703
787943 feet/sec YDOT = -2287
801779 meter/sec
ZDOT = -16277
882449 ZDOT = -4935
298170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19762860
14 X = -6023719
77
Y = -1809119
85 feet Y = -551419
73 meter
Z = 9975975
09 Z = 3040677
21
XDOT = -6686
301433 XDOT = -2037
984677
YDOT = -16727
819888 feet/sec YDOT = -5098
639502 meter/sec
ZDOT = -16169
673084 ZDOT = -4928
516356
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 12170
53841237
00016717 00000-0 10270-3 0 9124
2 25544 51
6358 115
6305 0010457 76
7007 283
5313 15
56464490 18227
Satellite: ISS
Catalog Number: 25544
Epoch time: 12170
53841237 = yrday
fracday
Element set: 912
Inclination: 51
6358 deg
RA of node: 115
6305 deg
Eccentricity:
0010457
Arg of perigee: 76
7007 deg
Mean anomaly: 283
5313 deg
Mean motion: 15
56464490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1822
Checksum: 295
Coasting Arc #14 (Orbit 1836)
---------------------------------------
Vector Time (GMT): 2012/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1726920
15 A = 6782250
69 meter
Y = 6509492
24 meter E =
0019489
Z = -759511
92 I = 51
98217
XDOT = -4765
516046 Wp = 60
20785
YDOT = -580
513916 meter/sec RA = 109
91607 deg
ZDOT = 5984
048511 TA = 291
61418
MA = 291
82170
Ha = 221
098 n
mi
Hp = 207
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5665748
54 X = -1795892
74
Y = 21356601
84 feet Y = 6489795
23 meter
Z = -2491837
00 Z = -768067
62
XDOT = -15634
895165 XDOT = -4787
739560
YDOT = -1904
573214 feet/sec YDOT = -633
930155 meter/sec
ZDOT = 19632
705087 ZDOT = 5960
843785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21068025
62 X = 6421534
21
Y = 6645544
02 feet Y = 2025561
82 meter
Z = -2527734
44 Z = -770453
46
XDOT = -2155
260325 XDOT = -656
923347
YDOT = 14111
468473 feet/sec YDOT = 4301
175591 meter/sec
ZDOT = 19537
112984 ZDOT = 5954
912038
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 12171
50148973
00016717 00000-0 10270-3 0 9130
2 25544 51
6359 110
8123 0010399 80
3013 279
9314 15
56478387 18372
Satellite: ISS
Catalog Number: 25544
Epoch time: 12171
50148973 = yrday
fracday
Element set: 913
Inclination: 51
6359 deg
RA of node: 110
8123 deg
Eccentricity:
0010399
Arg of perigee: 80
3013 deg
Mean anomaly: 279
9314 deg
Mean motion: 15
56478387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1837
Checksum: 316
Coasting Arc #15 (Orbit 1852)
---------------------------------------
Vector Time (GMT): 2012/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2986008
36 A = 6781105
64 meter
Y = -5826548
84 meter E =
0015731
Z = -1766834
30 I = 51
98936
XDOT = 3655
519258 Wp = 107
94192
YDOT = 3588
973004 meter/sec RA = 104
95802 deg
ZDOT = -5703
805390 TA = 91
36828
MA = 91
18806
Ha = 221
068 n
mi
Hp = 207
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9796615
34 X = 3059522
93
Y = -19115973
90 feet Y = -5792746
11 meter
Z = -5796700
46 Z = -1752150
88
XDOT = 11993
173418 XDOT = 3642
822612
YDOT = 11774
845813 feet/sec YDOT = 3629
781252 meter/sec
ZDOT = -18713
272276 ZDOT = -5686
077353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18815948
19 X = -5735101
01
Y = -10395137
16 feet Y = -3168437
81 meter
Z = -5735597
93 Z = -1748210
25
XDOT = 11369
950470 XDOT = 3465
560903
YDOT = -10380
029485 feet/sec YDOT = -3163
832987 meter/sec
ZDOT = -18640
543774 ZDOT = -5681
637742
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 12172
52875552
00016717 00000-0 10270-3 0 9144
2 25544 51
6372 105
6719 0010375 84
0235 276
2101 15
56510943 18538
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
52875552 = yrday
fracday
Element set: 914
Inclination: 51
6372 deg
RA of node: 105
6719 deg
Eccentricity:
0010375
Arg of perigee: 84
0235 deg
Mean anomaly: 276
2101 deg
Mean motion: 15
56510943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1853
Checksum: 296
Coasting Arc #16 (Orbit 1853)
---------------------------------------
Vector Time (GMT): 2012/172/13:54:15
860
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3516870
25 A = 6773462
61 meter
Y = 2606728
47 meter E =
0020561
Z = -5186821
72 I = 51
95775
XDOT = -2969
564895 Wp = 95
39581
YDOT = 6903
701695 meter/sec RA = 104
53595 deg
ZDOT = 1459
177858 TA = 188
59216
MA = 188
62742
Ha = 221
066 n
mi
Hp = 209
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11538288
21 X = 3512656
18
Y = 8552258
75 feet Y = 2646033
59 meter
Z = -17017131
63 Z = -5169746
80
XDOT = -9742
666978 XDOT = -3053
631116
YDOT = 22649
939945 feet/sec YDOT = 6870
023897 meter/sec
ZDOT = 4787
328932 ZDOT = 1444
548874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2348128
55 X = 715709
58
Y = -14252772
28 feet Y = -4344244
99 meter
Z = -16946998
79 Z = -5165445
23
XDOT = 23580
009460 XDOT = 7187
186883
YDOT = -1722
913320 feet/sec YDOT = -525
143980 meter/sec
ZDOT = 4726
343854 ZDOT = 1440
589607
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 12172
59296086
00016717 00000-0 10270-3 0 9151
2 25544 51
6383 105
3517 0006958 83
9965 276
1981 15
55704630 18546
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
59296086 = yrday
fracday
Element set: 915
Inclination: 51
6383 deg
RA of node: 105
3517 deg
Eccentricity:
0006958
Arg of perigee: 83
9965 deg
Mean anomaly: 276
1981 deg
Mean motion: 15
55704630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1854
Checksum: 341
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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