[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 10th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16684 06 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 235 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
163/14:26:51
724 -9
2 9
5 9
5
N/A 1
3 -0
0 192
0
000/00:33:43
448 -2
2 -0
3 190
3
163/18:35:11
835 3
6 8
5 8
5
N/A 5
3 -0
5 201
5
000/00:40:23
670 -5
7 0
4 193
1
166/15:04:47
021 8
8 9
8 9
8
N/A -3
9 0
3 205
2
000/00:29:34
043 2
0 0
6 196
1
166/19:08:06
734 -8
5 9
4 9
4
N/A -1
3 0
2 206
3
000/00:36:13
467 3
7 -0
3 205
1
Coasting Arc #1 (Orbit 3954)
---------------------------------------
Vector Time (GMT): 2011/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4704543
20 A = 6728618
47 meter
Y = -4173641
55 meter E =
0013406
Z = 2373214
81 I = 51
51218
XDOT = 4925
197843 Wp = 68
87651
YDOT = -2481
503262 meter/sec RA = 204
11832 deg
ZDOT = 5379
804317 TA = 317
93466
MA = 318
03751
Ha = 189
207 n
mi
Hp = 183
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15434853
03 X = -4669051
70
Y = -13693049
72 feet Y = -4226052
39 meter
Z = 7786137
82 Z = 2350446
02
XDOT = 16158
785574 XDOT = 4926
446401
YDOT = -8141
414901 feet/sec YDOT = -2426
420228 meter/sec
ZDOT = 17650
276632 ZDOT = 5403
733659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17084818
02 X = -5207452
53
Y = 11630527
11 feet Y = 3544984
66 meter
Z = 7694028
42 Z = 2345139
86
XDOT = -3086
547385 XDOT = -940
779643
YDOT = -16317
543097 feet/sec YDOT = -4973
587136 meter/sec
ZDOT = 17747
313192 ZDOT = 5409
381061
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 11159
55881987
00016717 00000-0 10270-3 0 9005
2 25544 51
6437 204
8302 0001284 315
3751 44
7309 15
74411105 39555
Satellite: ISS
Catalog Number: 25544
Epoch time: 11159
55881987 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 204
8302 deg
Eccentricity:
0001284
Arg of perigee: 315
3751 deg
Mean anomaly: 44
7309 deg
Mean motion: 15
74411105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3955
Checksum: 304
Coasting Arc #2 (Orbit 3969)
---------------------------------------
Vector Time (GMT): 2011/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4251877
83 A = 6721453
10 meter
Y = 2421963
11 meter E =
0009570
Z = -4617139
42 I = 51
51844
XDOT = -5632
214128 Wp = 106
13676
YDOT = -4366
955080 meter/sec RA = 198
92783 deg
ZDOT = 2898
268996 TA = 192
61692
MA = 192
64089
Ha = 189
051 n
mi
Hp = 183
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13949730
42 X = -4256215
42
Y = 7946073
19 feet Y = 2374392
18 meter
Z = -15148095
22 Z = -4637805
40
XDOT = -18478
392810 XDOT = -5597
042678
YDOT = -14327
280445 feet/sec YDOT = -4429
741523 meter/sec
ZDOT = 9508
756548 ZDOT = 2870
992707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4550079
93 X = 1386864
36
Y = 15312916
83 feet Y = 4667377
05 meter
Z = -15231913
78 Z = -4642687
32
XDOT = -17084
159059 XDOT = -5207
251681
YDOT = 14417
438334 feet/sec YDOT = 4394
435204 meter/sec
ZDOT = 9398
380092 ZDOT = 2864
626252
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 11160
51088215
00016717 00000-0 10270-3 0 9017
2 25544 51
6446 199
9378 0001387 317
4395 42
6661 15
74477176 39708
Satellite: ISS
Catalog Number: 25544
Epoch time: 11160
51088215 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 199
9378 deg
Eccentricity:
0001387
Arg of perigee: 317
4395 deg
Mean anomaly: 42
6661 deg
Mean motion: 15
74477176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3970
Checksum: 329
Coasting Arc #3 (Orbit 3985)
---------------------------------------
Vector Time (GMT): 2011/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5089294
21 A = 6727494
52 meter
Y = 3466698
27 meter E =
0003664
Z = -2709607
15 I = 51
56906
XDOT = -4821
360596 Wp = 117
97984
YDOT = 3040
348997 meter/sec RA = 193
82652 deg
ZDOT = -5172
816109 TA = 92
96040
MA = 92
91847
Ha = 189
036 n
mi
Hp = 183
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16697159
49 X = 5063313
53
Y = 11373682
00 feet Y = 3523464
85 meter
Z = -8889787
23 Z = -2684945
98
XDOT = -15818
112192 XDOT = -4829
871279
YDOT = 9974
898285 feet/sec YDOT = 2986
386534 meter/sec
ZDOT = -16971
181459 ZDOT = -5196
258790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14678537
88 X = 4474018
34
Y = -13944929
62 feet Y = -4250414
55 meter
Z = -8789969
16 Z = -2679182
60
XDOT = 5382
727887 XDOT = 1640
655460
YDOT = 16408
736644 feet/sec YDOT = 5001
382929 meter/sec
ZDOT = -17066
279887 ZDOT = -5201
802110
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 11161
52638373
00016717 00000-0 10270-3 0 9026
2 25544 51
6449 194
7192 0001337 323
5918 36
5154 15
74547184 39865
Satellite: ISS
Catalog Number: 25544
Epoch time: 11161
52638373 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 194
7192 deg
Eccentricity:
0001337
Arg of perigee: 323
5918 deg
Mean anomaly: 36
5154 deg
Mean motion: 15
74547184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3986
Checksum: 325
Coasting Arc #4 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2011/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4163390
09 A = 6721877
94 meter
Y = -2900979
85 meter E =
0009054
Z = 4404193
48 I = 51
57985
XDOT = 5982
148947 Wp = 60
23626
YDOT = 3557
736982 meter/sec RA = 188
63589 deg
ZDOT = -3302
163163 TA = 62
97857
MA = 62
88618
Ha = 188
859 n
mi
Hp = 183
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13659416
30 X = 4174125
00
Y = -9517650
44 feet Y = -2854362
80 meter
Z = 14449453
67 Z = 4424445
14
XDOT = 19626
472922 XDOT = 5957
962491
YDOT = 11672
365425 feet/sec YDOT = 3624
498165 meter/sec
ZDOT = -10833
868646 ZDOT = -3273
159943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6671315
08 X = -2033416
84
Y = -15174895
05 feet Y = -4625308
01 meter
Z = 14531625
86 Z = 4429239
56
XDOT = 14199
300614 XDOT = 4327
946827
YDOT = -16534
192031 feet/sec YDOT = -5039
621731 meter/sec
ZDOT = -10716
449404 ZDOT = -3266
373778
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 11162
54185120
00016717 00000-0 10270-3 0 9037
2 25544 51
6435 189
5005 0001402 329
2775 30
8306 15
74615974 40021
Satellite: ISS
Catalog Number: 25544
Epoch time: 11162
54185120 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 189
5005 deg
Eccentricity:
0001402
Arg of perigee: 329
2775 deg
Mean anomaly: 30
8306 deg
Mean motion: 15
74615974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 282
Coasting Arc #5 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2011/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5310093
40 A = 6726406
75 meter
Y = -2756442
72 meter E =
0012918
Z = 3060022
93 I = 51
62509
XDOT = 4712
866983 Wp = 78
35044
YDOT = -3607
163894 meter/sec RA = 183
54153 deg
ZDOT = 4914
141307 TA = 317
15921
MA = 317
25980
Ha = 189
089 n
mi
Hp = 183
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17421566
27 X = -5293740
85
Y = -9043447
25 feet Y = -2815732
43 meter
Z = 10039445
32 Z = 3034265
55
XDOT = 15462
162017 XDOT = 4728
980463
YDOT = -11834
527212 feet/sec YDOT = -3554
372378 meter/sec
ZDOT = 16122
510850 ZDOT = 4937
075260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12028606
39 X = -3666319
23
Y = 15578540
09 feet Y = 4748339
02 meter
Z = 9935144
11 Z = 3028231
93
XDOT = -7753
486604 XDOT = -2363
262717
YDOT = -16359
489524 feet/sec YDOT = -4986
372407 meter/sec
ZDOT = 16215
590980 ZDOT = 4942
512131
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 11163
55728698
00016717 00000-0 10270-3 0 9043
2 25544 51
6430 184
2812 0001408 338
9871 21
1235 15
74625736 40182
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
55728698 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 184
2812 deg
Eccentricity:
0001408
Arg of perigee: 338
9871 deg
Mean anomaly: 21
1235 deg
Mean motion: 15
74625736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 309
Coasting Arc #6 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2011/163/14:43:43
448
Vector Time (MET): N/A
Weight (LBS) : 903960
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5319494
66 A = 6734144
23 meter
Y = 2394773
64 meter E =
0005806
Z = -3360759
47 I = 51
62367
XDOT = -4710
201812 Wp = 255
15393
YDOT = -3926
080634 meter/sec RA = 182
90673 deg
ZDOT = 4649
692602 TA = 65
29583
MA = 65
23539
Ha = 191
995 n
mi
Hp = 190
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17452410
30 X = -5329552
00
Y = 7856868
88 feet Y = 2335232
09 meter
Z = -11026113
74 Z = -3386625
91
XDOT = -15453
418020 XDOT = -4688
537136
YDOT = -12880
841975 feet/sec YDOT = -3978
632534 meter/sec
ZDOT = 15254
896989 ZDOT = 4626
862245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15635812
29 X = 4765795
59
Y = 10932225
03 feet Y = 3332142
19 meter
Z = -11131038
96 Z = -3392740
68
XDOT = -2333
778664 XDOT = -711
335737
YDOT = 18803
031585 feet/sec YDOT = 5731
164027 meter/sec
ZDOT = 15162
499382 ZDOT = 4621
529812
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 11163
62076664
00016717 00000-0 10270-3 0 9051
2 25544 51
6412 183
9549 0010600 261
8636 98
1323 15
71557806 40194
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
62076664 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 183
9549 deg
Eccentricity:
0010600
Arg of perigee: 261
8636 deg
Mean anomaly: 98
1323 deg
Mean motion: 15
71557806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 309
Coasting Arc #7 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2011/163/18:55:23
670
Vector Time (MET): N/A
Weight (LBS) : 902207
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4232077
50 A = 6742523
47 meter
Y = 3350403
86 meter E =
0008913
Z = -4035552
51 I = 51
62408
XDOT = -5978
809393 Wp = 169
54433
YDOT = 2871
619402 meter/sec RA = 182
06439 deg
ZDOT = -3895
824190 TA = 60
25640
MA = 60
16774
Ha = 201
540 n
mi
Hp = 193
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13884768
69 X = 4213902
27
Y = 10992138
66 feet Y = 3397628
52 meter
Z = -13240001
66 Z = -4015036
50
XDOT = -19615
516380 XDOT = -5991
550638
YDOT = 9421
323496 feet/sec YDOT = 2804
690086 meter/sec
ZDOT = -12781
575427 ZDOT = -3924
900042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14663872
63 X = -4469548
38
Y = -10038760
75 feet Y = -3059814
28 meter
Z = -13156963
17 Z = -4010242
37
XDOT = 18136
829438 XDOT = 5528
105613
YDOT = -9629
594908 feet/sec YDOT = -2935
100528 meter/sec
ZDOT = -12899
528700 ZDOT = -3931
776348
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 11163
81162651
00016717 00000-0 10270-3 0 9065
2 25544 51
6432 182
9801 0012113 204
9694 155
0881 15
67941087 40228
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
81162651 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 182
9801 deg
Eccentricity:
0012113
Arg of perigee: 204
9694 deg
Mean anomaly: 155
0881 deg
Mean motion: 15
67941087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 297
Coasting Arc #8 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2011/164/18:55:23
670
Vector Time (MET): N/A
Weight (LBS) : 902207
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2960227
56 A = 6739907
61 meter
Y = -3855379
16 meter E =
0007079
Z = 4664811
34 I = 51
64556
XDOT = 6901
620165 Wp = 170
69447
YDOT = 1876
376997 meter/sec RA = 176
92891 deg
ZDOT = -2835
140013 TA = 307
30256
MA = 307
36706
Ha = 201
198 n
mi
Hp = 193
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9712032
67 X = 2980458
16
Y = -12648881
75 feet Y = -3822163
82 meter
Z = 15304499
16 Z = 4679240
69
XDOT = 22643
110777 XDOT = 6893
897906
YDOT = 6156
092509 feet/sec YDOT = 1953
512434 meter/sec
ZDOT = -9301
640463 ZDOT = -2801
630106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8528397
62 X = -2599455
59
Y = 13408432
45 feet Y = 4086890
21 meter
Z = 15363133
01 Z = 4682682
94
XDOT = -22156
098468 XDOT = -6753
178813
YDOT = -3613
666674 feet/sec YDOT = -1101
445602 meter/sec
ZDOT = -9165
865780 ZDOT = -2793
755890
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 11164
83138382
00016717 00000-0 10270-3 0 9073
2 25544 51
6423 177
7907 0012098 209
0905 150
9582 15
67971332 40385
Satellite: ISS
Catalog Number: 25544
Epoch time: 11164
83138382 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 177
7907 deg
Eccentricity:
0012098
Arg of perigee: 209
0905 deg
Mean anomaly: 150
9582 deg
Mean motion: 15
67971332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 322
Coasting Arc #9 (Orbit 4053)
---------------------------------------
Vector Time (GMT): 2011/165/18:55:23
670
Vector Time (MET): N/A
Weight (LBS) : 902207
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6706158
53 A = 6749192
11 meter
Y = 476022
36 meter E =
0004110
Z = 604673
84 I = 51
70741
XDOT = 201
948624 Wp = 117
20996
YDOT = -4807
106592 meter/sec RA = 171
86768 deg
ZDOT = 5991
064442 TA = 249
34373
MA = 249
38780
Ha = 201
026 n
mi
Hp = 193
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22001832
45 X = -6713920
49
Y = 1561753
14 feet Y = 400986
50 meter
Z = 1983838
06 Z = 572076
45
XDOT = 662
561102 XDOT = 226
584015
YDOT = -15771
347087 feet/sec YDOT = -4804
711704 meter/sec
ZDOT = 19655
723234 ZDOT = 5992
104414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21743908
19 X = 6627543
22
Y = -3772153
39 feet Y = -1149752
35 meter
Z = 1851656
71 Z = 564384
96
XDOT = 772
302866 XDOT = 235
397914
YDOT = 14159
395103 feet/sec YDOT = 4315
783627 meter/sec
ZDOT = 19660
118534 ZDOT = 5992
404129
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 11165
85111847
00016717 00000-0 10270-3 0 9084
2 25544 51
6426 172
5998 0012076 213
1034 146
9371 15
67990059 40542
Satellite: ISS
Catalog Number: 25544
Epoch time: 11165
85111847 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 172
5998 deg
Eccentricity:
0012076
Arg of perigee: 213
1034 deg
Mean anomaly: 146
9371 deg
Mean motion: 15
67990059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4054
Checksum: 320
Coasting Arc #10 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2011/166/15:19:34
043
Vector Time (MET): N/A
Weight (LBS) : 900925
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3393583
15 A = 6749491
83 meter
Y = -4098848
52 meter E =
0012566
Z = 4138944
90 I = 51
70553
XDOT = 6520
166605 Wp = 108
92672
YDOT = 1596
526161 meter/sec RA = 167
51241 deg
ZDOT = -3759
645240 TA = 19
60483
MA = 19
55655
Ha = 205
152 n
mi
Hp = 196
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11133802
97 X = 3419058
83
Y = -13447665
75 feet Y = -4060757
80 meter
Z = 13579215
54 Z = 4155491
96
XDOT = 21391
622719 XDOT = 6520
092991
YDOT = 5237
946723 feet/sec YDOT = 1669
438965 meter/sec
ZDOT = -12334
794094 ZDOT = -3727
970171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17378085
17 X = -5296840
36
Y = 986121
68 feet Y = 300569
89 meter
Z = 13646468
30 Z = 4159443
54
XDOT = -10624
019892 XDOT = -3238
201263
YDOT = -18066
298998 feet/sec YDOT = -5506
607935 meter/sec
ZDOT = -12206
412796 ZDOT = -3720
514620
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 11166
67974175
00016717 00000-0 10270-3 0 9097
2 25544 51
6395 168
3819 0006935 163
7270 196
4112 15
65333904 40676
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
67974175 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 168
3819 deg
Eccentricity:
0006935
Arg of perigee: 163
7270 deg
Mean anomaly: 196
4112 deg
Mean motion: 15
65333904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 337
Coasting Arc #11 (Orbit 4069)
---------------------------------------
Vector Time (GMT): 2011/166/19:26:13
467
Vector Time (MET): N/A
Weight (LBS) : 899353
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6614318
74 A = 6765741
62 meter
Y = 508135
69 meter E =
0007808
Z = 1304617
88 I = 51
73541
XDOT = 777
231433 Wp = 37
15754
YDOT = -4921
970646 meter/sec RA = 166
68338 deg
ZDOT = 5845
465762 TA = 337
06959
MA = 337
10443
Ha = 206
348 n
mi
Hp = 205
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21700520
82 X = -6625846
80
Y = 1667111
85 feet Y = 434105
64 meter
Z = 4280242
38 Z = 1272457
69
XDOT = 2549
971892 XDOT = 803
815950
YDOT = -16148
197656 feet/sec YDOT = -4913
131703 meter/sec
ZDOT = 19178
037278 ZDOT = 5849
305130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20616633
21 X = 6283949
80
Y = -7053073
47 feet Y = -2149776
79 meter
Z = 4149810
87 Z = 1264862
35
XDOT = 1170
722446 XDOT = 356
836202
YDOT = 14739
231978 feet/sec YDOT = 4492
517907 meter/sec
ZDOT = 19193
792528 ZDOT = 5850
267963
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 11166
87140342
00016717 00000-0 10270-3 0 9102
2 25544 51
6418 167
4131 0007228 263
2068 96
8266 15
62041485 40700
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
87140342 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 167
4131 deg
Eccentricity:
0007228
Arg of perigee: 263
2068 deg
Mean anomaly: 96
8266 deg
Mean motion: 15
62041485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4070
Checksum: 296
Coasting Arc #12 (Orbit 4084)
---------------------------------------
Vector Time (GMT): 2011/167/19:26:13
467
Vector Time (MET): N/A
Weight (LBS) : 899353
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4226374
35 A = 6757094
76 meter
Y = 2471430
79 meter E =
0004085
Z = -4660765
65 I = 51
73630
XDOT = -5684
257863 Wp = 39
53332
YDOT = 4280
527365 meter/sec RA = 161
65448 deg
ZDOT = -2882
974583 TA = 201
88690
MA = 201
90435
Ha = 206
037 n
mi
Hp = 205
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13866057
57 X = 4221065
20
Y = 8108368
74 feet Y = 2518663
91 meter
Z = -15291225
87 Z = -4640246
48
XDOT = -18649
139971 XDOT = -5717
696216
YDOT = 14043
724951 feet/sec YDOT = 4216
776143 meter/sec
ZDOT = -9458
578027 ZDOT = -2910
668885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15615454
31 X = -4759590
47
Y = -4087304
09 feet Y = -1245810
29 meter
Z = -15208100
36 Z = -4635428
99
XDOT = 13870
291002 XDOT = 4227
664697
YDOT = -17358
172896 feet/sec YDOT = -5290
771099 meter/sec
ZDOT = -9571
061855 ZDOT = -2917
259653
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 11167
83103053
00016717 00000-0 10270-3 0 9118
2 25544 51
6421 162
5719 0007339 267
0651 92
9667 15
62086609 40850
Satellite: ISS
Catalog Number: 25544
Epoch time: 11167
83103053 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 162
5719 deg
Eccentricity:
0007339
Arg of perigee: 267
0651 deg
Mean anomaly: 92
9667 deg
Mean motion: 15
62086609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4085
Checksum: 312
Coasting Arc #13 (Orbit 4100)
---------------------------------------
Vector Time (GMT): 2011/168/19:26:13
467
Vector Time (MET): N/A
Weight (LBS) : 899353
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 411600
79 A = 6755307
58 meter
Y = -4496363
27 meter E =
0004282
Z = 5027997
47 I = 51
75982
XDOT = 7280
060502 Wp = 320
31400
YDOT = -1495
178994 meter/sec RA = 156
58053 deg
ZDOT = -1930
726892 TA = 148
36978
MA = 148
34404
Ha = 205
756 n
mi
Hp = 204
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1350396
29 X = 437424
58
Y = -14751848
00 feet Y = -4491617
03 meter
Z = 16496054
69 Z = 5030058
90
XDOT = 23884
712932 XDOT = 7305
617823
YDOT = -4905
442893 feet/sec YDOT = -1413
625683 meter/sec
ZDOT = -6334
405815 ZDOT = -1895
298951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2981847
90 X = 908867
24
Y = 14500604
72 feet Y = 4419784
32 meter
Z = 16504588
93 Z = 5030598
70
XDOT = -20492
723656 XDOT = -6246
182170
YDOT = 11268
885518 feet/sec YDOT = 3434
756306 meter/sec
ZDOT = -6190
641822 ZDOT = -1886
907627
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 11168
85461657
00016717 00000-0 10270-3 0 9129
2 25544 51
6426 157
4076 0007404 270
8567 89
1741 15
62137959 41010
Satellite: ISS
Catalog Number: 25544
Epoch time: 11168
85461657 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 157
4076 deg
Eccentricity:
0007404
Arg of perigee: 270
8567 deg
Mean anomaly: 89
1741 deg
Mean motion: 15
62137959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4101
Checksum: 323
Coasting Arc #14 (Orbit 4115)
---------------------------------------
Vector Time (GMT): 2011/169/19:26:13
467
Vector Time (MET): N/A
Weight (LBS) : 899353
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4619931
43 A = 6764140
33 meter
Y = 4436908
53 meter E =
0006106
Z = -2160625
53 I = 51
81657
XDOT = -4813
504516 Wp = 328
41445
YDOT = -2325
116228 meter/sec RA = 151
54121 deg
ZDOT = 5515
785030 TA = 7
59293
MA = 7
58369
Ha = 205
997 n
mi
Hp = 204
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15157255
34 X = -4658706
64
Y = 14556786
51 feet Y = 4385029
20 meter
Z = -7088666
45 Z = -2183162
32
XDOT = -15792
337652 XDOT = -4813
941188
YDOT = -7628
334081 feet/sec YDOT = -2378
947103 meter/sec
ZDOT = 18096
407578 ZDOT = 5492
399896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10052307
02 X = 3063943
18
Y = -18419732
30 feet Y = -5614334
40 meter
Z = -7180264
66 Z = -2188544
67
XDOT = 16113
227199 XDOT = 4911
311650
YDOT = 1773
836451 feet/sec YDOT = 540
665350 meter/sec
ZDOT = 18001
627247 ZDOT = 5486
895985
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 11169
81421461
00016717 00000-0 10270-3 0 9136
2 25544 51
6425 152
5656 0007424 274
8574 85
1735 15
62121647 41165
Satellite: ISS
Catalog Number: 25544
Epoch time: 11169
81421461 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 152
5656 deg
Eccentricity:
0007424
Arg of perigee: 274
8574 deg
Mean anomaly: 85
1735 deg
Mean motion: 15
62121647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4116
Checksum: 305
Coasting Arc #15 (Orbit 4131)
---------------------------------------
Vector Time (GMT): 2011/170/19:26:13
467
Vector Time (MET): N/A
Weight (LBS) : 899353
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6091375
67 A = 6764335
35 meter
Y = -2032562
19 meter E =
0005094
Z = -2115458
80 I = 51
84304
XDOT = -150
999303 Wp = 218
98911
YDOT = 5316
939882 meter/sec RA = 146
54620 deg
ZDOT = -5540
037638 TA = 344
45893
MA = 344
47456
Ha = 206
229 n
mi
Hp = 205
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19984828
31 X = 6123927
82
Y = -6668511
12 feet Y = -1964262
42 meter
Z = -6940481
62 Z = -2085788
51
XDOT = -495
404539 XDOT = -183
530999
YDOT = 17444
028483 feet/sec YDOT = 5315
070205 meter/sec
ZDOT = -18175
976502 ZDOT = -5540
849449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16888458
44 X = -5147602
13
Y = 12660961
55 feet Y = 3859061
08 meter
Z = -6820022
89 Z = -2078742
98
XDOT = -4227
823213 XDOT = -1288
640515
YDOT = -15438
171226 feet/sec YDOT = -4705
554590 meter/sec
ZDOT = -18179
474752 ZDOT = -5541
103904
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 11170
83776855
00016717 00000-0 10270-3 0 9141
2 25544 51
6424 147
4017 0007492 277
2930 82
7375 15
62124034 41320
Satellite: ISS
Catalog Number: 25544
Epoch time: 11170
83776855 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 147
4017 deg
Eccentricity:
0007492
Arg of perigee: 277
2930 deg
Mean anomaly: 82
7375 deg
Mean motion: 15
62124034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4132
Checksum: 305
Coasting Arc #16 (Orbit 4147)
---------------------------------------
Vector Time (GMT): 2011/171/19:26:13
467
Vector Time (MET): N/A
Weight (LBS) : 899353
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4180575
41 A = 6755401
21 meter
Y = -1718805
83 meter E =
0002871
Z = 5022837
07 I = 51
83795
XDOT = 4720
422241 Wp = 233
17187
YDOT = -5728
758621 meter/sec RA = 141
51099 deg
ZDOT = 1967
593348 TA = 197
80496
MA = 197
81503
Ha = 206
695 n
mi
Hp = 205
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13715798
58 X = -4185444
41
Y = -5639126
74 feet Y = -1765583
40 meter
Z = 16479124
24 Z = 5002516
04
XDOT = 15486
949608 XDOT = 4774
573397
YDOT = -18795
139833 feet/sec YDOT = -5675
669455 meter/sec
ZDOT = 6455
358753 ZDOT = 1990
655714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14903320
18 X = 4542531
99
Y = 722868
08 feet Y = 220330
19 meter
Z = 16396735
23 Z = 4997724
90
XDOT = -8264
934230 XDOT = -2519
151953
YDOT = 21775
861788 feet/sec YDOT = 6637
282673 meter/sec
ZDOT = 6549
159777 ZDOT = 1996
183900
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 11171
86130514
00016717 00000-0 10270-3 0 9152
2 25544 51
6423 142
2365 0007354 282
4160 77
6174 15
62153637 41486
Satellite: ISS
Catalog Number: 25544
Epoch time: 11171
86130514 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 142
2365 deg
Eccentricity:
0007354
Arg of perigee: 282
4160 deg
Mean anomaly: 77
6174 deg
Mean motion: 15
62153637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4148
Checksum: 292
Coasting Arc #17 (Orbit 4162)
---------------------------------------
Vector Time (GMT): 2011/172/19:26:13
467
Vector Time (MET): N/A
Weight (LBS) : 899353
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 183168
01 A = 6756593
53 meter
Y = 4883768
98 meter E =
0003300
Z = -4668718
80 I = 51
86470
XDOT = -6449
257130 Wp = 119
28111
YDOT = 3003
204371 meter/sec RA = 136
44227 deg
ZDOT = 2888
468477 TA = 179
29186
MA = 179
29139
Ha = 206
815 n
mi
Hp = 205
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 600944
91 X = 151222
72
Y = 16022864
11 feet Y = 4885639
17 meter
Z = -15317318
88 Z = -4667906
03
XDOT = -21158
980084 XDOT = -6496
391737
YDOT = 9853
032714 feet/sec YDOT = 2930
820998 meter/sec
ZDOT = 9476
602615 ZDOT = 2857
024123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6237244
87 X = -1901112
24
Y = -14774479
12 feet Y = -4503261
24 meter
Z = -15314212
68 Z = -4667772
03
XDOT = 15369
606114 XDOT = 4684
655943
YDOT = -16179
052837 feet/sec YDOT = -4931
375305 meter/sec
ZDOT = 9348
884313 ZDOT = 2849
539939
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 11172
82085272
00016717 00000-0 10270-3 0 9160
2 25544 51
6413 137
3938 0007495 285
3627 74
6702 15
62214452 41636
Satellite: ISS
Catalog Number: 25544
Epoch time: 11172
82085272 = yrday
fracday
Element set: 916
Inclination: 51
6413 deg
RA of node: 137
3938 deg
Eccentricity:
0007495
Arg of perigee: 285
3627 deg
Mean anomaly: 74
6702 deg
Mean motion: 15
62214452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4163
Checksum: 310
Coasting Arc #18 (Orbit 4178)
---------------------------------------
Vector Time (GMT): 2011/173/19:26:13
467
Vector Time (MET): N/A
Weight (LBS) : 899353
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3607854
46 A = 6765126
15 meter
Y = -5578337
58 meter E =
0006638
Z = 1257438
19 I = 51
91501
XDOT = 4653
791622 Wp = 133
96048
YDOT = 1682
633961 meter/sec RA = 131
42351 deg
ZDOT = -5873
414642 TA = 32
37246
MA = 32
33175
Ha = 206
980 n
mi
Hp = 204
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11836792
84 X = 3663855
99
Y = -18301632
48 feet Y = -5537679
37 meter
Z = 4125453
38 Z = 1275100
48
XDOT = 15268
345216 XDOT = 4663
162005
YDOT = 5520
452628 feet/sec YDOT = 1734
728500 meter/sec
ZDOT = -19269
733076 ZDOT = -5850
783725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4320824
59 X = -1316987
34
Y = 21349273
15 feet Y = 6507258
46 meter
Z = 4197355
42 Z = 1279353
93
XDOT = -14780
329049 XDOT = -4505
044294
YDOT = 788
413656 feet/sec YDOT = 240
308482 meter/sec
ZDOT = -19177
958732 ZDOT = -5845
441822
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 11173
84435394
00016717 00000-0 10270-3 0 9178
2 25544 51
6415 132
2298 0007510 289
8028 70
2319 15
62248732 41794
Satellite: ISS
Catalog Number: 25544
Epoch time: 11173
84435394 = yrday
fracday
Element set: 917
Inclination: 51
6415 deg
RA of node: 132
2298 deg
Eccentricity:
0007510
Arg of perigee: 289
8028 deg
Mean anomaly: 70
2319 deg
Mean motion: 15
62248732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4179
Checksum: 316
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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