[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 29th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 9 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
180/12:31:32
815 3
3 4
3 4
4
N/A -1
7 -1
0 209
2
000/00:33:05
630 -2
3 -0
1 207
1
182/12:16:32
027 3
3 4
1 4
3
N/A -0
6 -1
0 209
7
000/00:33:04
054 -2
6 -0
4 208
7
Coasting Arc #1 (Orbit 251)
---------------------------------------
Vector Time (GMT): 2011/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2843930
53 A = 6755766
62 meter
Y = 3681118
98 meter E =
0002090
Z = -4899347
50 I = 51
95239
XDOT = -3923
060021 Wp = 28
37329
YDOT = 6167
892507 meter/sec RA = 107
82740 deg
ZDOT = 2359
219051 TA = 264
57100
MA = 264
59484
Ha = 208
341 n
mi
Hp = 204
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9330480
75 X = 2826356
35
Y = 12077162
00 feet Y = 3712824
07 meter
Z = -16073974
75 Z = -4885573
76
XDOT = -12870
931826 XDOT = -4003
199683
YDOT = 20235
867806 feet/sec YDOT = 6123
573998 meter/sec
ZDOT = 7740
219984 ZDOT = 2339
967143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11306116
22 X = 3446104
22
Y = -10338097
03 feet Y = -3151051
98 meter
Z = -16018235
33 Z = -4882358
13
XDOT = 20426
265817 XDOT = 6225
925821
YDOT = 10478
709177 feet/sec YDOT = 3193
910557 meter/sec
ZDOT = 7661
771037 ZDOT = 2335
307812
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 11178
51193182
00016717 00000-0 10270-3 0 9005
2 25544 51
6396 108
6586 0011884 296
8784 63
1157 15
62193246 2523
Satellite: ISS
Catalog Number: 25544
Epoch time: 11178
51193182 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 108
6586 deg
Eccentricity:
0011884
Arg of perigee: 296
8784 deg
Mean anomaly: 63
1157 deg
Mean motion: 15
62193246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 252
Checksum: 322
Coasting Arc #2 (Orbit 267)
---------------------------------------
Vector Time (GMT): 2011/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 68400
60 A = 6764608
97 meter
Y = -6529058
53 meter E =
0002517
Z = 1766481
91 I = 51
99118
XDOT = 4913
074151 Wp = 86
22426
YDOT = -1494
318070 meter/sec RA = 102
80685 deg
ZDOT = -5706
234078 TA = 74
41902
MA = 74
39124
Ha = 208
485 n
mi
Hp = 203
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 224411
41 X = 132823
47
Y = -21420795
71 feet Y = -6527933
74 meter
Z = 5795544
31 Z = 1766969
51
XDOT = 16119
009682 XDOT = 4957
138568
YDOT = -4902
618339 feet/sec YDOT = -1439
129692 meter/sec
ZDOT = -18721
240412 ZDOT = -5682
259621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21341713
31 X = -6504954
22
Y = 1845376
70 feet Y = 562470
82 meter
Z = 5797847
95 Z = 1767184
05
XDOT = -6288
142997 XDOT = -1916
625985
YDOT = -14135
922396 feet/sec YDOT = -4308
629146 meter/sec
ZDOT = -18623
831985 ZDOT = -5676
543989
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 11179
53544435
00016717 00000-0 10270-3 0 9010
2 25544 51
6404 103
4942 0011870 300
7563 59
2425 15
62206768 2682
Satellite: ISS
Catalog Number: 25544
Epoch time: 11179
53544435 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 103
4942 deg
Eccentricity:
0011870
Arg of perigee: 300
7563 deg
Mean anomaly: 59
2425 deg
Mean motion: 15
62206768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 268
Checksum: 296
Coasting Arc #3 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2011/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2767368
01 A = 6763221
04 meter
Y = 5620261
46 meter E =
0010760
Z = 2529505
02 I = 51
99244
XDOT = -3628
729857 Wp = 19
09369
YDOT = -4183
372697 meter/sec RA = 97
82124 deg
ZDOT = 5328
558058 TA = 9
27724
MA = 9
25737
Ha = 208
809 n
mi
Hp = 203
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9079291
36 X = -2842296
99
Y = 18439178
01 feet Y = 5588895
64 meter
Z = 8298900
98 Z = 2515880
27
XDOT = -11905
281684 XDOT = -3607
565922
YDOT = -13724
976039 feet/sec YDOT = -4223
834035 meter/sec
ZDOT = 17482
145858 ZDOT = 5310
980384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19346512
49 X = 5896817
01
Y = 7004938
43 feet Y = 2135105
23 meter
Z = 8243292
23 Z = 2512555
47
XDOT = -11780
868016 XDOT = -3590
808571
YDOT = 12061
729809 feet/sec YDOT = 3676
415246 meter/sec
ZDOT = 17410
989897 ZDOT = 5306
869721
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 11180
55894643
00016717 00000-0 10270-3 0 9024
2 25544 51
6406 98
3291 0011917 304
8124 55
1911 15
62214567 2842
Satellite: ISS
Catalog Number: 25544
Epoch time: 11180
55894643 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 98
3291 deg
Eccentricity:
0011917
Arg of perigee: 304
8124 deg
Mean anomaly: 55
1911 deg
Mean motion: 15
62214567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 300
Coasting Arc #4 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2011/180/12:48:05
630
Vector Time (MET): N/A
Weight (LBS) : 898415
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3166856
95 A = 6765316
21 meter
Y = -5081296
82 meter E =
0003843
Z = -3149033
93 I = 51
98651
XDOT = 3174
290280 Wp = 298
84118
YDOT = 5005
288431 meter/sec RA = 97
65790 deg
ZDOT = -4878
017604 TA = 277
37436
MA = 277
41803
Ha = 209
217 n
mi
Hp = 207
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10389950
61 X = 3238738
98
Y = -16670921
34 feet Y = -5045480
59 meter
Z = -10331476
16 Z = -3133475
78
XDOT = 10414
338190 XDOT = 3141
780663
YDOT = 16421
549969 feet/sec YDOT = 5040
604428 meter/sec
ZDOT = -16003
994765 ZDOT = -4862
674991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19125605
48 X = -5829484
55
Y = -4624777
90 feet Y = -1409632
30 meter
Z = -10268044
41 Z = -3129699
94
XDOT = 11902
351465 XDOT = 3627
836726
YDOT = -13780
974868 feet/sec YDOT = -4200
441140 meter/sec
ZDOT = -15941
956033 ZDOT = -4859
108199
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 11180
55897988
00016717 00000-0 10270-3 0 9030
2 25544 51
6395 98
3307 0008296 290
6223 69
4043 15
60973783 2849
Satellite: ISS
Catalog Number: 25544
Epoch time: 11180
55897988 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 98
3307 deg
Eccentricity:
0008296
Arg of perigee: 290
6223 deg
Mean anomaly: 69
4043 deg
Mean motion: 15
60973783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 343
Coasting Arc #5 (Orbit 299)
---------------------------------------
Vector Time (GMT): 2011/181/12:48:05
630
Vector Time (MET): N/A
Weight (LBS) : 898415
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4148062
13 A = 6757797
40 meter
Y = 1041451
25 meter E =
0004599
Z = 5235864
69 I = 51
96457
XDOT = -514
832398 Wp = 286
31683
YDOT = -7579
985455 meter/sec RA = 92
62917 deg
ZDOT = 1101
899411 TA = 153
19510
MA = 153
17132
Ha = 209
429 n
mi
Hp = 206
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13609127
71 X = -4184834
18
Y = 3416834
80 feet Y = 994858
49 meter
Z = 17178033
75 Z = 5215624
47
XDOT = -1689
082672 XDOT = -435
386050
YDOT = -24868
718683 feet/sec YDOT = -7585
298626 meter/sec
ZDOT = 3615
155548 ZDOT = 1099
589898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7794041
83 X = 2375623
95
Y = 11787911
22 feet Y = 3592955
34 meter
Z = 17095789
59 Z = 5210796
67
XDOT = -22015
495528 XDOT = -6710
323037
YDOT = 9336
272494 feet/sec YDOT = 2845
695856 meter/sec
ZDOT = 3606
177059 ZDOT = 1099
162768
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 11181
58329247
00016717 00000-0 10270-3 0 9043
2 25544 51
6395 93
1710 0008316 294
2413 65
7874 15
61005776 3003
Satellite: ISS
Catalog Number: 25544
Epoch time: 11181
58329247 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 93
1710 deg
Eccentricity:
0008316
Arg of perigee: 294
2413 deg
Mean anomaly: 65
7874 deg
Mean motion: 15
61005776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 300
Checksum: 300
Coasting Arc #6 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2011/182/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3625164
01 A = 6763342
74 meter
Y = -3110919
99 meter E =
0004758
Z = -4792170
29 I = 51
96963
XDOT = 2346
240789 Wp = 47
48696
YDOT = 6810
438824 meter/sec RA = 87
67959 deg
ZDOT = -2644
768332 TA = 196
55648
MA = 196
57202
Ha = 209
723 n
mi
Hp = 208
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11893582
72 X = 3682960
66
Y = -10206430
42 feet Y = -3070057
16 meter
Z = -15722343
47 Z = -4774419
67
XDOT = 7697
640385 XDOT = 2282
758394
YDOT = 22343
959395 feet/sec YDOT = 6836
321451 meter/sec
ZDOT = -8677
061458 ZDOT = -2633
523396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13220842
41 X = -4029712
77
Y = -8550124
29 feet Y = -2606077
88 meter
Z = -15650089
99 Z = -4770147
43
XDOT = 18551
814243 XDOT = 5654
592981
YDOT = -12877
820420 feet/sec YDOT = -3925
159664 meter/sec
ZDOT = -8631
761463 ZDOT = -2630
960894
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 11182
54360439
00016717 00000-0 10270-3 0 9059
2 25544 51
6379 88
3346 0007241 267
0587 92
9740 15
59743837 3156
Satellite: ISS
Catalog Number: 25544
Epoch time: 11182
54360439 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 88
3346 deg
Eccentricity:
0007241
Arg of perigee: 267
0587 deg
Mean anomaly: 92
9740 deg
Mean motion: 15
59743837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 329
Coasting Arc #7 (Orbit 330)
---------------------------------------
Vector Time (GMT): 2011/183/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4223076
56 A = 6761550
28 meter
Y = -964063
95 meter E =
0004643
Z = 5195612
63 I = 51
96143
XDOT = 78
780495 Wp = 303
84317
YDOT = -7556
952420 meter/sec RA = 82
64421 deg
ZDOT = -1336
516984 TA = 158
94078
MA = 158
92165
Ha = 209
582 n
mi
Hp = 208
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13855238
07 X = -4237221
24
Y = -3162939
48 feet Y = -1011368
92 meter
Z = 17045973
18 Z = 5175062
76
XDOT = 258
466192 XDOT = 169
770385
YDOT = -24793
150983 feet/sec YDOT = -7555
562472 meter/sec
ZDOT = -4384
898241 ZDOT = -1335
914530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1226389
45 X = 373803
50
Y = 14258483
75 feet Y = 4345985
85 meter
Z = 16962565
25 Z = 5170189
89
XDOT = -22668
935417 XDOT = -6909
491515
YDOT = 7169
404544 feet/sec YDOT = 2185
234505 meter/sec
ZDOT = -4382
039292 ZDOT = -1335
645576
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 11183
56873803
00016717 00000-0 10270-3 0 9067
2 25544 51
6377 83
1803 0007406 271
0403 88
9904 15
59775232 3319
Satellite: ISS
Catalog Number: 25544
Epoch time: 11183
56873803 = yrday
fracday
Element set: 906
Inclination: 51
6377 deg
RA of node: 83
1803 deg
Eccentricity:
0007406
Arg of perigee: 271
0403 deg
Mean anomaly: 88
9904 deg
Mean motion: 15
59775232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 331
Checksum: 310
Coasting Arc #8 (Orbit 345)
---------------------------------------
Vector Time (GMT): 2011/184/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3667046
67 A = 6768399
08 meter
Y = 4621103
39 meter E =
0002921
Z = -3314549
98 I = 51
97934
XDOT = -2593
461675 Wp = 291
46933
YDOT = 5456
243018 meter/sec RA = 77
62537 deg
ZDOT = 4735
458749 TA = 30
08424
MA = 30
06746
Ha = 209
900 n
mi
Hp = 208
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12030993
01 X = 3631201
22
Y = 15161100
35 feet Y = 4661910
59 meter
Z = -10874507
80 Z = -3296822
20
XDOT = -8508
732529 XDOT = -2677
285238
YDOT = 17901
059770 feet/sec YDOT = 5426
771980 meter/sec
ZDOT = 15536
281984 ZDOT = 4722
657146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10491563
95 X = 3197828
69
Y = -16312147
51 feet Y = -4971942
56 meter
Z = -10802759
19 Z = -3292681
00
XDOT = 18523
780272 XDOT = 5646
048227
YDOT = 1654
705912 feet/sec YDOT = 504
354362 meter/sec
ZDOT = 15483
986371 ZDOT = 4719
519046
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 11184
52979453
00016717 00000-0 10270-3 0 9073
2 25544 51
6378 78
3477 0007402 275
0315 84
9995 15
59752410 3460
Satellite: ISS
Catalog Number: 25544
Epoch time: 11184
52979453 = yrday
fracday
Element set: 907
Inclination: 51
6378 deg
RA of node: 78
3477 deg
Eccentricity:
0007402
Arg of perigee: 275
0315 deg
Mean anomaly: 84
9995 deg
Mean motion: 15
59752410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 346
Checksum: 337
Coasting Arc #9 (Orbit 361)
---------------------------------------
Vector Time (GMT): 2011/185/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1990632
07 A = 6773107
99 meter
Y = -6468504
09 meter E =
0007674
Z = -37627
94 I = 51
98719
XDOT = 4528
455433 Wp = 170
88027
YDOT = -1359
431416 meter/sec RA = 72
64566 deg
ZDOT = -6048
525835 TA = 9
52404
MA = 9
50950
Ha = 209
992 n
mi
Hp = 208
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6530945
10 X = -1917969
27
Y = -21222126
28 feet Y = -6490358
26 meter
Z = -123451
25 Z = -47122
54
XDOT = 14857
137249 XDOT = 4572
702370
YDOT = -4460
076825 feet/sec YDOT = -1308
543337 meter/sec
ZDOT = -19844
244864 ZDOT = -6026
419711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17789827
36 X = -5422339
38
Y = 13286949
89 feet Y = 4049862
33 meter
Z = -161656
44 Z = -49272
88
XDOT = -8268
930938 XDOT = -2520
370150
YDOT = -11306
230179 feet/sec YDOT = -3446
138959 meter/sec
ZDOT = -19754
379796 ZDOT = -6021
134962
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 11185
55491278
00016717 00000-0 10270-3 0 9082
2 25544 51
6376 73
1934 0007391 277
4036 82
6279 15
59725202 3629
Satellite: ISS
Catalog Number: 25544
Epoch time: 11185
55491278 = yrday
fracday
Element set: 908
Inclination: 51
6376 deg
RA of node: 73
1934 deg
Eccentricity:
0007391
Arg of perigee: 277
4036 deg
Mean anomaly: 82
6279 deg
Mean motion: 15
59725202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 362
Checksum: 325
Coasting Arc #10 (Orbit 377)
---------------------------------------
Vector Time (GMT): 2011/186/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -449406
86 A = 6768168
93 meter
Y = 5847521
57 meter E =
0005610
Z = 3371739
25 I = 51
96062
XDOT = -5234
835199 Wp = 70
35197
YDOT = -3104
000582 meter/sec RA = 67
66334 deg
ZDOT = 4680
996363 TA = 328
90787
MA = 328
94105
Ha = 210
539 n
mi
Hp = 208
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1474431
94 X = -531140
59
Y = 19184782
05 feet Y = 5842038
69 meter
Z = 11062136
66 Z = 3369358
14
XDOT = -17174
656165 XDOT = -5222
475647
YDOT = -10183
728943 feet/sec YDOT = -3162
471065 meter/sec
ZDOT = 15357
599616 ZDOT = 4655
595665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18497239
52 X = 5637958
61
Y = -5320064
64 feet Y = -1621555
70 meter
Z = 11052136
53 Z = 3368691
21
XDOT = -3831
640892 XDOT = -1167
884144
YDOT = 18398
846214 feet/sec YDOT = 5607
968326 meter/sec
ZDOT = 15254
601431 ZDOT = 4649
602516
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 11186
58002094
00016717 00000-0 10270-3 0 9091
2 25544 51
6373 68
0378 0007445 283
7416 76
2911 15
59757555 3788
Satellite: ISS
Catalog Number: 25544
Epoch time: 11186
58002094 = yrday
fracday
Element set: 909
Inclination: 51
6373 deg
RA of node: 68
0378 deg
Eccentricity:
0007445
Arg of perigee: 283
7416 deg
Mean anomaly: 76
2911 deg
Mean motion: 15
59757555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 378
Checksum: 333
Coasting Arc #11 (Orbit 392)
---------------------------------------
Vector Time (GMT): 2011/187/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2990157
60 A = 6761348
88 meter
Y = -3108449
59 meter E =
0008082
Z = -5213519
97 I = 51
92520
XDOT = 4311
178597 Wp = 56
01355
YDOT = 6225
030836 meter/sec RA = 62
64118 deg
ZDOT = -1235
873727 TA = 202
16143
MA = 202
19639
Ha = 210
705 n
mi
Hp = 208
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9810228
34 X = 3050020
65
Y = -10198325
43 feet Y = -3074676
65 meter
Z = -17104724
32 Z = -5198848
85
XDOT = 14144
286734 XDOT = 4247
252253
YDOT = 20423
329513 feet/sec YDOT = 6272
883738 meter/sec
ZDOT = -4054
703828 ZDOT = -1215
085005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13134341
51 X = -4003347
29
Y = -5456790
54 feet Y = -1663229
76 meter
Z = -17044956
02 Z = -5195302
59
XDOT = 13366
812088 XDOT = 4074
204324
YDOT = -19739
579084 feet/sec YDOT = -6016
623705 meter/sec
ZDOT = -3970
619772 ZDOT = -1210
244907
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 11187
54105070
00016717 00000-0 10270-3 0 9108
2 25544 51
6367 63
2049 0007589 287
0047 73
0276 15
59809095 3932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11187
54105070 = yrday
fracday
Element set: 910
Inclination: 51
6367 deg
RA of node: 63
2049 deg
Eccentricity:
0007589
Arg of perigee: 287
0047 deg
Mean anomaly: 73
0276 deg
Mean motion: 15
59809095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 393
Checksum: 314
Coasting Arc #12 (Orbit 408)
---------------------------------------
Vector Time (GMT): 2011/188/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4791263
56 A = 6763323
55 meter
Y = -624933
12 meter E =
0006294
Z = 4735408
07 I = 51
91774
XDOT = -1831
198755 Wp = 357
76761
YDOT = -6922
866821 meter/sec RA = 57
60231 deg
ZDOT = -2760
399800 TA = 119
45457
MA = 119
39175
Ha = 210
870 n
mi
Hp = 208
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15719368
62 X = -4806922
89
Y = -2050305
51 feet Y = -678599
93 meter
Z = 15536115
73 Z = 4712094
22
XDOT = -6007
869932 XDOT = -1740
240412
YDOT = -22712
817655 feet/sec YDOT = -6942
835573 meter/sec
ZDOT = -9056
429791 ZDOT = -2769
075383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4186935
81 X = 1276178
04
Y = 15385192
67 feet Y = 4689406
73 meter
Z = 15441457
49 Z = 4706556
24
XDOT = -17557
111001 XDOT = -5351
407433
YDOT = 13922
429568 feet/sec YDOT = 4243
556532 meter/sec
ZDOT = -9091
264137 ZDOT = -2771
017309
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 11188
56614137
00016717 00000-0 10270-3 0 9111
2 25544 51
6373 58
0501 0007716 290
6856 69
3472 15
59838928 4095
Satellite: ISS
Catalog Number: 25544
Epoch time: 11188
56614137 = yrday
fracday
Element set: 911
Inclination: 51
6373 deg
RA of node: 58
0501 deg
Eccentricity:
0007716
Arg of perigee: 290
6856 deg
Mean anomaly: 69
3472 deg
Mean motion: 15
59838928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 409
Checksum: 330
Coasting Arc #13 (Orbit 423)
---------------------------------------
Vector Time (GMT): 2011/189/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5097941
54 A = 6770956
77 meter
Y = 3892747
12 meter E =
0008474
Z = -2150785
95 I = 51
92503
XDOT = -1557
828760 Wp = 340
05384
YDOT = 5094
905714 meter/sec RA = 52
59441 deg
ZDOT = 5530
271766 TA = 356
12668
MA = 356
13324
Ha = 211
208 n
mi
Hp = 208
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16725529
98 X = 5064481
27
Y = 12771480
04 feet Y = 3949568
54 meter
Z = -7056384
34 Z = -2126101
13
XDOT = -5110
986744 XDOT = -1641
550127
YDOT = 16715
569928 feet/sec YDOT = 5077
016432 meter/sec
ZDOT = 18143
936239 ZDOT = 5522
501047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4991973
13 X = 1521553
41
Y = -20477693
79 feet Y = -6241601
07 meter
Z = -6956355
14 Z = -2120297
05
XDOT = 15915
059271 XDOT = 4850
910066
YDOT = -2271
469417 feet/sec YDOT = -692
343878 meter/sec
ZDOT = 18112
069135 ZDOT = 5520
558672
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 11189
52715776
00016717 00000-0 10270-3 0 9120
2 25544 51
6364 53
2167 0007764 294
3637 65
6707 15
59805026 4241
Satellite: ISS
Catalog Number: 25544
Epoch time: 11189
52715776 = yrday
fracday
Element set: 912
Inclination: 51
6364 deg
RA of node: 53
2167 deg
Eccentricity:
0007764
Arg of perigee: 294
3637 deg
Mean anomaly: 65
6707 deg
Mean motion: 15
59805026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 424
Checksum: 325
Coasting Arc #14 (Orbit 439)
---------------------------------------
Vector Time (GMT): 2011/190/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3589074
13 A = 6772005
12 meter
Y = -5565481
34 meter E =
0003636
Z = -1404056
44 I = 51
90930
XDOT = 4737
269286 Wp = 207
01334
YDOT = -1584
335596 meter/sec RA = 47
61661 deg
ZDOT = -5826
674974 TA = 348
26620
MA = 348
27467
Ha = 211
246 n
mi
Hp = 208
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11775177
58 X = -3519752
46
Y = -18259453
22 feet Y = -5605228
77 meter
Z = -4606484
39 Z = -1421324
44
XDOT = 15542
222066 XDOT = 4782
938389
YDOT = -5197
951430 feet/sec YDOT = -1531
104472 meter/sec
ZDOT = -19116
387711 ZDOT = -5803
550661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11718471
95 X = -3571790
25
Y = 18278182
79 feet Y = 5571190
12 meter
Z = -4676279
11 Z = -1425329
87
XDOT = -9907
650722 XDOT = -3019
851940
YDOT = -11220
905094 feet/sec YDOT = -3420
131873 meter/sec
ZDOT = -19022
366483 ZDOT = -5798
017304
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 11190
55223318
00016717 00000-0 10270-3 0 9132
2 25544 51
6362 48
0624 0007716 297
3989 62
6381 15
59806334 4405
Satellite: ISS
Catalog Number: 25544
Epoch time: 11190
55223318 = yrday
fracday
Element set: 913
Inclination: 51
6362 deg
RA of node: 48
0624 deg
Eccentricity:
0007716
Arg of perigee: 297
3989 deg
Mean anomaly: 62
6381 deg
Mean motion: 15
59806334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 440
Checksum: 311
Coasting Arc #15 (Orbit 455)
---------------------------------------
Vector Time (GMT): 2011/191/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 596905
46 A = 6764842
46 meter
Y = 5164169
49 meter E =
0002828
Z = 4325834
12 I = 51
86383
XDOT = -6463
484050 Wp = 66
50198
YDOT = -2197
298825 meter/sec RA = 42
61457 deg
ZDOT = 3514
290338 TA = 347
90985
MA = 347
91663
Ha = 211
515 n
mi
Hp = 208
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1958351
24 X = 518100
32
Y = 16942813
28 feet Y = 5170403
16 meter
Z = 14192369
15 Z = 4328543
25
XDOT = -21205
656333 XDOT = -6455
504765
YDOT = -7208
985645 feet/sec YDOT = -2269
533357 meter/sec
ZDOT = 11529
823942 ZDOT = 3482
909895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14476267
51 X = 4412366
34
Y = -9001586
33 feet Y = -2743683
51 meter
Z = 14203046
37 Z = 4329088
53
XDOT = 2021
993267 XDOT = 616
303548
YDOT = 21246
733849 feet/sec YDOT = 6476
004477 meter/sec
ZDOT = 11402
503792 ZDOT = 3475
483156
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 11191
57730027
00016717 00000-0 10270-3 0 9146
2 25544 51
6358 42
9062 0007786 302
5213 57
5189 15
59814046 4560
Satellite: ISS
Catalog Number: 25544
Epoch time: 11191
57730027 = yrday
fracday
Element set: 914
Inclination: 51
6358 deg
RA of node: 42
9062 deg
Eccentricity:
0007786
Arg of perigee: 302
5213 deg
Mean anomaly: 57
5189 deg
Mean motion: 15
59814046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 456
Checksum: 310
Coasting Arc #16 (Orbit 470)
---------------------------------------
Vector Time (GMT): 2011/192/12:33:04
054
Vector Time (MET): N/A
Weight (LBS) : 897710
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2874143
61 A = 6760766
06 meter
Y = -3055206
80 meter E =
0009295
Z = -5309308
46 I = 51
82637
XDOT = 5890
537110 Wp = 66
61644
YDOT = 4901
338695 meter/sec RA = 37
57291 deg
ZDOT = 372
457962 TA = 206
89994
MA = 206
94816
Ha = 211
578 n
mi
Hp = 207
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9429605
01 X = 2933885
38
Y = -10023644
36 feet Y = -3022731
44 meter
Z = -17418991
00 Z = -5295201
38
XDOT = 19325
909153 XDOT = 5833
482272
YDOT = 16080
507530 feet/sec YDOT = 4966
891189 meter/sec
ZDOT = 1221
974940 ZDOT = 400
936246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13229039
34 X = -4032211
19
Y = -4047621
40 feet Y = -1233715
00 meter
Z = -17361492
56 Z = -5291782
93
XDOT = 5454
139080 XDOT = 1662
421592
YDOT = -23504
157376 feet/sec YDOT = -7164
067168 meter/sec
ZDOT = 1337
331988 ZDOT = 407
618790
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 11192
53829130
00016717 00000-0 10270-3 0 9158
2 25544 51
6346 38
0727 0007686 305
4533 54
5904 15
59861284 4712
Satellite: ISS
Catalog Number: 25544
Epoch time: 11192
53829130 = yrday
fracday
Element set: 915
Inclination: 51
6346 deg
RA of node: 38
0727 deg
Eccentricity:
0007686
Arg of perigee: 305
4533 deg
Mean anomaly: 54
5904 deg
Mean motion: 15
59861284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 471
Checksum: 314
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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