[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 21st 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19913 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 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
299/12:43:53
237 -4
4 5
5 5
6
N/A -3
3 -0
5 217
9
000/00:01:46
474 0
6 0
3 204
0
Coasting Arc #1 (Orbit 2047)
---------------------------------------
Vector Time (GMT): 2011/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -686247
31 A = 6767742
30 meter
Y = 5820297
90 meter E =
0017311
Z = -3399696
47 I = 51
31794
XDOT = -5188
419101 Wp = 350
27185
YDOT = -3298
218112 meter/sec RA = 249
05026 deg
ZDOT = -4579
054588 TA = 229
72824
MA = 229
87972
Ha = 216
148 n
mi
Hp = 203
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2251467
54 X = -734764
77
Y = 19095465
56 feet Y = 5812352
44 meter
Z = -11153859
81 Z = -3403148
39
XDOT = -17022
372379 XDOT = -5128
907752
YDOT = -10820
925563 feet/sec YDOT = -3355
905644 meter/sec
ZDOT = -15023
144974 ZDOT = -4604
115440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6976355
21 X = -2126393
07
Y = -17908552
63 feet Y = -5458526
84 meter
Z = -11168200
86 Z = -3404067
62
XDOT = 18718
632733 XDOT = 5705
439257
YDOT = 2181
697274 feet/sec YDOT = 664
981329 meter/sec
ZDOT = -15125
053169 ZDOT = -4610
116206
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 11293
52492317
00016717 00000-0 10270-3 0 9006
2 25544 51
6385 249
7875 0018777 335
4479 24
5781 15
59875041 20483
Satellite: ISS
Catalog Number: 25544
Epoch time: 11293
52492317 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 249
7875 deg
Eccentricity:
0018777
Arg of perigee: 335
4479 deg
Mean anomaly: 24
5781 deg
Mean motion: 15
59875041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2048
Checksum: 343
Coasting Arc #2 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2011/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3207114
45 A = 6760896
19 meter
Y = -2910419
46 meter E =
0015797
Z = 5192379
02 I = 51
30769
XDOT = 4090
298506 Wp = 346
75118
YDOT = 6406
970332 meter/sec RA = 243
98309 deg
ZDOT = 1080
587931 TA = 92
95075
MA = 92
76995
Ha = 216
130 n
mi
Hp = 203
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10522029
04 X = 3214197
12
Y = -9548620
27 feet Y = -2874515
62 meter
Z = 17035364
23 Z = 5207976
69
XDOT = 13419
614522 XDOT = 4013
101155
YDOT = 21020
243873 feet/sec YDOT = 6452
278989 meter/sec
ZDOT = 3545
235994 ZDOT = 1100
270861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4531883
40 X = -1381318
06
Y = 13385740
20 feet Y = 4079973
61 meter
Z = 17099031
29 Z = 5211784
74
XDOT = -20890
147427 XDOT = -6367
316936
YDOT = -11637
448779 feet/sec YDOT = -3547
094388 meter/sec
ZDOT = 3625
105179 ZDOT = 1104
932059
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 11294
54995369
00016717 00000-0 10270-3 0 9015
2 25544 51
6387 244
6329 0018759 338
7749 21
2627 15
59932225 20648
Satellite: ISS
Catalog Number: 25544
Epoch time: 11294
54995369 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 244
6329 deg
Eccentricity:
0018759
Arg of perigee: 338
7749 deg
Mean anomaly: 21
2627 deg
Mean motion: 15
59932225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 347
Coasting Arc #3 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2011/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4854276
25 A = 6763193
56 meter
Y = -885840
44 meter E =
0014939
Z = -4622122
21 I = 51
32986
XDOT = -1480
382659 Wp = 17
11650
YDOT = -6953
372326 meter/sec RA = 238
90131 deg
ZDOT = 2903
791305 TA = 281
76702
MA = 281
93458
Ha = 216
259 n
mi
Hp = 203
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15926103
19 X = -4821556
16
Y = -2906300
65 feet Y = -939941
35 meter
Z = -15164442
94 Z = -4645624
97
XDOT = -4856
898489 XDOT = -1416
624891
YDOT = -22812
901333 feet/sec YDOT = -6969
570155 meter/sec
ZDOT = 9526
874360 ZDOT = 2896
754951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15187045
09 X = 4629011
34
Y = -5341308
77 feet Y = -1628030
91 meter
Z = -15260136
24 Z = -4651289
53
XDOT = 15206
123868 XDOT = 4634
826555
YDOT = 16251
514641 feet/sec YDOT = 4953
461663 meter/sec
ZDOT = 9498
529702 ZDOT = 2895
151853
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 11295
51089154
00016717 00000-0 10270-3 0 9020
2 25544 51
6386 239
7998 0018730 342
4804 17
5703 15
59952315 20798
Satellite: ISS
Catalog Number: 25544
Epoch time: 11295
51089154 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 239
7998 deg
Eccentricity:
0018730
Arg of perigee: 342
4804 deg
Mean anomaly: 17
5703 deg
Mean motion: 15
59952315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2079
Checksum: 332
Coasting Arc #4 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2011/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4958015
19 A = 6770681
87 meter
Y = 4209215
12 meter E =
0015350
Z = 1903556
12 I = 51
37287
XDOT = -1973
154383 Wp = 33
83462
YDOT = 4865
711847 meter/sec RA = 233
85554 deg
ZDOT = -5585
646572 TA = 125
09203
MA = 124
94801
Ha = 216
451 n
mi
Hp = 202
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16266454
03 X = 4901331
16
Y = 13809760
90 feet Y = 4264341
92 meter
Z = 6245262
87 Z = 1927504
42
XDOT = -6473
603620 XDOT = -2000
282642
YDOT = 15963
621545 feet/sec YDOT = 4843
494631 meter/sec
ZDOT = -18325
612113 ZDOT = -5595
298628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21008824
36 X = -6403489
66
Y = -3565205
25 feet Y = -1086674
56 meter
Z = 6342628
93 Z = 1933233
30
XDOT = -2957
946097 XDOT = -901
581971
YDOT = -15439
023633 feet/sec YDOT = -4705
814403 meter/sec
ZDOT = -18365
145369 ZDOT = -5597
696308
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 11296
53585981
00016717 00000-0 10270-3 0 9033
2 25544 51
6394 234
6443 0018704 346
4150 13
6500 15
60012434 20956
Satellite: ISS
Catalog Number: 25544
Epoch time: 11296
53585981 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 234
6443 deg
Eccentricity:
0018704
Arg of perigee: 346
4150 deg
Mean anomaly: 13
6500 deg
Mean motion: 15
60012434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2095
Checksum: 293
Coasting Arc #5 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2011/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3192943
62 A = 6770985
53 meter
Y = -5705121
03 meter E =
0026219
Z = 1692058
17 I = 51
39295
XDOT = 5046
817900 Wp = 21
05256
YDOT = -1134
822259 meter/sec RA = 228
83934 deg
ZDOT = 5693
854309 TA = 357
64850
MA = 357
66081
Ha = 216
527 n
mi
Hp = 202
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10475536
82 X = -3137130
39
Y = -18717588
68 feet Y = -5740514
26 meter
Z = 5551371
94 Z = 1676682
66
XDOT = 16557
801509 XDOT = 5031
472369
YDOT = -3723
170140 feet/sec YDOT = -1078
470920 meter/sec
ZDOT = 18680
624373 ZDOT = 5718
335041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18785774
92 X = 5725904
20
Y = 10385971
95 feet Y = 3165644
25 meter
Z = 5488986
72 Z = 1673043
15
XDOT = -11267
518223 XDOT = -3434
339554
YDOT = 10449
065227 feet/sec YDOT = 3184
875081 meter/sec
ZDOT = 18780
399741 ZDOT = 5724
265841
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 11297
56079553
00016717 00000-0 10270-3 0 9041
2 25544 51
6395 229
4887 0018679 350
1211 9
9575 15
60049580 21113
Satellite: ISS
Catalog Number: 25544
Epoch time: 11297
56079553 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 229
4887 deg
Eccentricity:
0018679
Arg of perigee: 350
1211 deg
Mean anomaly: 9
9575 deg
Mean motion: 15
60049580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 328
Coasting Arc #6 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2011/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 47799
87 A = 6763272
91 meter
Y = 5046824
92 meter E =
0023051
Z = -4519928
89 I = 51
38944
XDOT = -6445
862509 Wp = 18
26370
YDOT = -2739
866075 meter/sec RA = 223
79898 deg
ZDOT = -3110
246970 TA = 220
35958
MA = 220
53086
Ha = 216
592 n
mi
Hp = 202
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 156823
71 X = 13319
25
Y = 16557824
54 feet Y = 5047166
30 meter
Z = -14829163
02 Z = -4519780
83
XDOT = -21147
842878 XDOT = -6399
636326
YDOT = -8989
061926 feet/sec YDOT = -2811
689442 meter/sec
ZDOT = -10204
222342 ZDOT = -3141
449217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9160975
44 X = -2792265
31
Y = -13793986
11 feet Y = -4204406
97 meter
Z = -14828779
43 Z = -4519811
97
XDOT = 21592
178960 XDOT = 6581
296147
YDOT = -3173
149389 feet/sec YDOT = -967
175934 meter/sec
ZDOT = -10331
216172 ZDOT = -3148
954689
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 11298
52164228
00016717 00000-0 10270-3 0 9053
2 25544 51
6404 224
6555 0018643 353
8236 6
2688 15
60121928 21269
Satellite: ISS
Catalog Number: 25544
Epoch time: 11298
52164228 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 224
6555 deg
Eccentricity:
0018643
Arg of perigee: 353
8236 deg
Mean anomaly: 6
2688 deg
Mean motion: 15
60121928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2126
Checksum: 306
Coasting Arc #7 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2011/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3452030
33 A = 6760070
59 meter
Y = -2567992
55 meter E =
0020477
Z = 5215177
18 I = 51
40211
XDOT = 5438
674944 Wp = 5
88186
YDOT = 5335
141245 meter/sec RA = 218
72160 deg
ZDOT = -952
555125 TA = 93
36921
MA = 93
13494
Ha = 216
533 n
mi
Hp = 201
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11325558
81 X = 3455154
47
Y = -8425172
40 feet Y = -2529372
09 meter
Z = 17110161
35 Z = 5231955
33
XDOT = 17843
421731 XDOT = 5383
239590
YDOT = 17503
744241 feet/sec YDOT = 5395
649836 meter/sec
ZDOT = -3125
180856 ZDOT = -926
268250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4656874
74 X = -1419415
42
Y = 13236979
58 feet Y = 4034631
38 meter
Z = 17178629
84 Z = 5236046
37
XDOT = -23608
673023 XDOT = -7195
923537
YDOT = -4302
321187 feet/sec YDOT = -1311
347498 meter/sec
ZDOT = -3018
318984 ZDOT = -919
983626
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 11299
54651328
00016717 00000-0 10270-3 0 9069
2 25544 51
6404 219
4999 0018607 357
1371 2
9676 15
60181134 21423
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
54651328 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 219
4999 deg
Eccentricity:
0018607
Arg of perigee: 357
1371 deg
Mean anomaly: 2
9676 deg
Mean motion: 15
60181134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 316
Coasting Arc #8 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2011/299/12:44:46
474
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2956514
31 A = 6762842
62 meter
Y = 3032684
73 meter E =
0020403
Z = -5279800
50 I = 51
40283
XDOT = -5794
089637 Wp = 28
50169
YDOT = -5011
993534 meter/sec RA = 218
56833 deg
ZDOT = 383
849985 TA = 245
06328
MA = 245
27542
Ha = 217
917 n
mi
Hp = 204
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9699850
09 X = -2964557
62
Y = 9949753
06 feet Y = 2999577
93 meter
Z = -17322180
13 Z = -5294183
34
XDOT = -19009
480436 XDOT = -5739
478626
YDOT = -16443
548341 feet/sec YDOT = -5076
481230 meter/sec
ZDOT = 1259
350346 ZDOT = 355
834433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -237312
53 X = -72332
86
Y = -13819921
81 feet Y = -4212312
17 meter
Z = -17380910
40 Z = -5297701
49
XDOT = 24068
078586 XDOT = 7335
950353
YDOT = -1778
987428 feet/sec YDOT = -542
235368 meter/sec
ZDOT = 1145
431307 ZDOT = 349
127462
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 11299
54651529
00016717 00000-0 10270-3 0 9073
2 25544 51
6412 219
4987 0019392 344
4389 15
6168 15
59137480 21429
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
54651529 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 219
4987 deg
Eccentricity:
0019392
Arg of perigee: 344
4389 deg
Mean anomaly: 15
6168 deg
Mean motion: 15
59137480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 336
Coasting Arc #9 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2011/300/12:44:46
474
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5450091
98 A = 6767729
77 meter
Y = -230158
32 meter E =
0022182
Z = 4015698
98 I = 51
44352
XDOT = 3138
923991 Wp = 17
36499
YDOT = 5807
256102 meter/sec RA = 213
50864 deg
ZDOT = -3900
929496 TA = 113
33673
MA = 113
10318
Ha = 218
032 n
mi
Hp = 203
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17880879
21 X = 5432752
50
Y = -755112
61 feet Y = -169308
93 meter
Z = 13174865
41 Z = 4042134
15
XDOT = 10298
307057 XDOT = 3092
703355
YDOT = 19052
677501 feet/sec YDOT = 5842
098966 meter/sec
ZDOT = -12798
325119 ZDOT = -3885
792560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11838649
63 X = -3608420
41
Y = 13315119
87 feet Y = 4058448
54 meter
Z = 13282585
31 Z = 4048532
00
XDOT = -19934
443299 XDOT = -6076
018318
YDOT = -4932
600756 feet/sec YDOT = -1503
456710 meter/sec
ZDOT = -12736
907674 ZDOT = -3882
209459
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 11300
57203262
00016717 00000-0 10270-3 0 9087
2 25544 51
6407 214
3475 0019364 348
1984 11
8715 15
59173834 21586
Satellite: ISS
Catalog Number: 25544
Epoch time: 11300
57203262 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 214
3475 deg
Eccentricity:
0019364
Arg of perigee: 348
1984 deg
Mean anomaly: 11
8715 deg
Mean motion: 15
59173834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 307
Coasting Arc #10 (Orbit 2172)
---------------------------------------
Vector Time (GMT): 2011/301/12:44:46
474
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6235227
99 A = 6773956
79 meter
Y = -2327597
86 meter E =
0026564
Z = -1166426
93 I = 51
49104
XDOT = 742
527040 Wp = 6
34238
YDOT = -4911
667855 meter/sec RA = 208
48657 deg
ZDOT = 5870
565390 TA = 340
91301
MA = 341
01236
Ha = 218
070 n
mi
Hp = 203
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20456784
74 X = -6203070
47
Y = -7636475
92 feet Y = -2397144
19 meter
Z = -3826860
01 Z = -1196640
34
XDOT = 2436
112335 XDOT = 768
876226
YDOT = -16114
395849 feet/sec YDOT = -4903
217188 meter/sec
ZDOT = 19260
385139 ZDOT = 5874
236638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19534502
63 X = 5954116
40
Y = -9707850
96 feet Y = -2958952
97 meter
Z = -3949873
50 Z = -1203921
44
XDOT = 9476
429661 XDOT = 2888
415761
YDOT = 11276
019827 feet/sec YDOT = 3436
930843 meter/sec
ZDOT = 19275
566136 ZDOT = 5875
192558
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 11301
53342633
00016717 00000-0 10270-3 0 9091
2 25544 51
6412 209
5177 0019380 351
4716 8
6107 15
59220537 21734
Satellite: ISS
Catalog Number: 25544
Epoch time: 11301
53342633 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 209
5177 deg
Eccentricity:
0019380
Arg of perigee: 351
4716 deg
Mean anomaly: 8
6107 deg
Mean motion: 15
59220537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2173
Checksum: 289
Coasting Arc #11 (Orbit 2188)
---------------------------------------
Vector Time (GMT): 2011/302/12:44:46
474
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4971817
36 A = 6772496
19 meter
Y = 4059319
99 meter E =
0014733
Z = -2191042
46 I = 51
51327
XDOT = -4632
381824 Wp = 10
01542
YDOT = 2721
372471 meter/sec RA = 203
48263 deg
ZDOT = -5461
063450 TA = 194
36057
MA = 194
40248
Ha = 218
218 n
mi
Hp = 203
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16311736
73 X = 4936699
62
Y = 13317978
97 feet Y = 4114721
60 meter
Z = -7188459
50 Z = -2166974
07
XDOT = -15198
103097 XDOT = -4635
939051
YDOT = 8928
387371 feet/sec YDOT = 2669
550588 meter/sec
ZDOT = -17916
874835 ZDOT = -5483
576594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20845855
71 X = -6353816
82
Y = 3207744
62 feet Y = 977720
56 meter
Z = -7090553
07 Z = -2161200
58
XDOT = 3725
371875 XDOT = 1135
493348
YDOT = -15661
498643 feet/sec YDOT = -4773
624786 meter/sec
ZDOT = -18008
750402 ZDOT = -5489
067122
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 11302
55888351
00016717 00000-0 10270-3 0 9108
2 25544 51
6410 204
3661 0019257 354
9609 5
1350 15
59246719 21894
Satellite: ISS
Catalog Number: 25544
Epoch time: 11302
55888351 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 204
3661 deg
Eccentricity:
0019257
Arg of perigee: 354
9609 deg
Mean anomaly: 5
1350 deg
Mean motion: 15
59246719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2189
Checksum: 306
Coasting Arc #12 (Orbit 2204)
---------------------------------------
Vector Time (GMT): 2011/303/12:44:46
474
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1862469
10 A = 6765069
04 meter
Y = -4524972
17 meter E =
0017246
Z = 4657968
26 I = 51
51686
XDOT = 7136
764075 Wp = 24
28421
YDOT = -11
026395 meter/sec RA = 198
45148 deg
ZDOT = 2854
569515 TA = 37
45394
MA = 37
33388
Ha = 218
334 n
mi
Hp = 202
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6110462
91 X = -1834359
46
Y = -14845709
22 feet Y = -4545642
40 meter
Z = 15282048
11 Z = 4648988
40
XDOT = 23414
580299 XDOT = 7122
489751
YDOT = -36
175835 feet/sec YDOT = 68
701380 meter/sec
ZDOT = 9365
385549 ZDOT = 2889
205778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15263076
55 X = 4652185
73
Y = 5087479
54 feet Y = 1550663
76 meter
Z = 15245651
17 Z = 4646874
48
XDOT = -14960
139813 XDOT = -4559
850615
YDOT = 16509
034739 feet/sec YDOT = 5031
953788 meter/sec
ZDOT = 9506
565842 ZDOT = 2897
601269
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 11303
58430997
00016717 00000-0 10270-3 0 9112
2 25544 51
6407 199
2136 0019335 359
1247
9871 15
59304832 22052
Satellite: ISS
Catalog Number: 25544
Epoch time: 11303
58430997 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 199
2136 deg
Eccentricity:
0019335
Arg of perigee: 359
1247 deg
Mean anomaly:
9871 deg
Mean motion: 15
59304832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2205
Checksum: 308
Coasting Arc #13 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2011/304/12:44:46
474
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1963227
47 A = 6762374
33 meter
Y = 3811660
39 meter E =
0023245
Z = -5240252
22 I = 51
53738
XDOT = -7201
224001 Wp = 41
10016
YDOT = -2467
640157 meter/sec RA = 193
39109 deg
ZDOT = 922
452758 TA = 237
62494
MA = 237
85011
Ha = 218
314 n
mi
Hp = 202
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6441035
02 X = -1980247
81
Y = 12505447
47 feet Y = 3789611
32 meter
Z = -17192428
54 Z = -5249830
95
XDOT = -23626
062996 XDOT = -7177
576305
YDOT = -8095
932273 feet/sec YDOT = -2548
036453 meter/sec
ZDOT = 3026
419811 ZDOT = 887
526205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5477457
21 X = -1669528
96
Y = -12904280
30 feet Y = -3933224
64 meter
Z = -17231649
95 Z = -5252206
91
XDOT = 20486
876149 XDOT = 6244
399850
YDOT = -12462
234270 feet/sec YDOT = -3798
489005 meter/sec
ZDOT = 2884
148637 ZDOT = 879
088505
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 11304
54561872
00016717 00000-0 10270-3 0 9127
2 25544 51
6404 194
3834 0019345 2
1754 357
9482 15
59372852 22206
Satellite: ISS
Catalog Number: 25544
Epoch time: 11304
54561872 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 194
3834 deg
Eccentricity:
0019345
Arg of perigee: 2
1754 deg
Mean anomaly: 357
9482 deg
Mean motion: 15
59372852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 307
Coasting Arc #14 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2011/305/12:44:46
474
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5296378
43 A = 6768222
54 meter
Y = -2138456
90 meter E =
0024525
Z = 3637467
41 I = 51
58737
XDOT = 4713
537353 Wp = 34
52545
YDOT = 4190
017545 meter/sec RA = 188
34303 deg
ZDOT = -4365
656339 TA = 102
19660
MA = 101
92180
Ha = 218
364 n
mi
Hp = 202
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17376569
66 X = 5302227
12
Y = -7015934
72 feet Y = -2079196
88 meter
Z = 11933948
19 Z = 3663211
63
XDOT = 15464
361395 XDOT = 4687
541182
YDOT = 13746
776723 feet/sec YDOT = 4242
581883 meter/sec
ZDOT = -14323
019484 ZDOT = -4342
820893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5481437
57 X = -1670742
17
Y = 17849475
53 feet Y = 5440520
14 meter
Z = 12039007
37 Z = 3669489
45
XDOT = -19175
656750 XDOT = -5844
740177
YDOT = 3784
259693 feet/sec YDOT = 1153
442354 meter/sec
ZDOT = -14230
103733 ZDOT = -4337
335618
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 11305
57098604
00016717 00000-0 10270-3 0 9130
2 25544 51
6404 189
2305 0019420 5
8788 354
2592 15
59432875 22364
Satellite: ISS
Catalog Number: 25544
Epoch time: 11305
57098604 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 189
2305 deg
Eccentricity:
0019420
Arg of perigee: 5
8788 deg
Mean anomaly: 354
2592 deg
Mean motion: 15
59432875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 318
Coasting Arc #15 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2011/306/12:44:46
474
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6733146
03 A = 6773764
77 meter
Y = 47771
70 meter E =
0029129
Z = -555043
53 I = 51
63586
XDOT = -518
263734 Wp = 20
86444
YDOT = -4786
107164 meter/sec RA = 183
33477 deg
ZDOT = 5998
010744 TA = 333
12124
MA = 333
27186
Ha = 218
409 n
mi
Hp = 202
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22090374
10 X = -6730483
47
Y = 156731
29 feet Y = -27507
59 meter
Z = -1821008
95 Z = -587746
94
XDOT = -1700
340336 XDOT = -493
843501
YDOT = -15702
451325 feet/sec YDOT = -4791
766102 meter/sec
ZDOT = 19678
512938 ZDOT = 5995
552367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13516685
59 X = 4119885
77
Y = -17458663
79 feet Y = -5321400
72 meter
Z = -1954363
18 Z = -595689
90
XDOT = 12197
597003 XDOT = 3717
827567
YDOT = 7283
831037 feet/sec YDOT = 2220
111700 meter/sec
ZDOT = 19668
701438 ZDOT = 5995
020198
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 11306
53224148
00016717 00000-0 10270-3 0 9142
2 25544 51
6401 184
3995 0019339 9
1894 350
9612 15
59449801 22516
Satellite: ISS
Catalog Number: 25544
Epoch time: 11306
53224148 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 184
3995 deg
Eccentricity:
0019339
Arg of perigee: 9
1894 deg
Mean anomaly: 350
9612 deg
Mean motion: 15
59449801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2251
Checksum: 312
Coasting Arc #16 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2011/307/12:44:46
474
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5816447
49 A = 6770539
69 meter
Y = 2060027
66 meter E =
0018290
Z = -2816505
85 I = 51
65490
XDOT = -3937
262882 Wp = 27
27810
YDOT = 4146
570911 meter/sec RA = 178
33713 deg
ZDOT = -5095
337973 TA = 184
68985
MA = 184
70701
Ha = 218
495 n
mi
Hp = 201
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19082832
99 X = 5806661
76
Y = 6758620
92 feet Y = 2125015
95 meter
Z = -9240504
76 Z = -2788273
13
XDOT = -12917
529140 XDOT = -3958
585584
YDOT = 13604
235272 feet/sec YDOT = 4102
422667 meter/sec
ZDOT = -16716
988101 ZDOT = -5114
517261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16947871
61 X = -5165711
27
Y = 11167631
28 feet Y = 3403894
02 meter
Z = -9125462
14 Z = -2781440
86
XDOT = -2282
584041 XDOT = -695
731616
YDOT = -17195
621985 feet/sec YDOT = -5241
225581 meter/sec
ZDOT = -16795
385102 ZDOT = -5119
233379
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 11307
55755185
00016717 00000-0 10270-3 0 9156
2 25544 51
6395 179
2466 0019211 12
6718 347
4916 15
59473565 22676
Satellite: ISS
Catalog Number: 25544
Epoch time: 11307
55755185 = yrday
fracday
Element set: 915
Inclination: 51
6395 deg
RA of node: 179
2466 deg
Eccentricity:
0019211
Arg of perigee: 12
6718 deg
Mean anomaly: 347
4916 deg
Mean motion: 15
59473565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 336
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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