[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 30th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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
149/04:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 187
5
000/00:00:00
000 0
0 0
0 181
9
149/05:09:08
700 1
0 1
5 1
6
N/A 0
2 -0
1 188
3
000/00:46:13
400 1
3 0
6 182
2
149/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
4
000/00:00:00
000 0
0 0
0 182
2
Coasting Arc #1 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2011/147/12:07:55
713
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 413670
23 A = 6727132
59 meter
Y = -6616692
80 meter E =
0014207
Z = 1090692
80 I = 51
32377
XDOT = 4810
866248 Wp = 40
51782
YDOT = 1276
080989 meter/sec RA = 266
01005 deg
ZDOT = 5884
559202 TA = 331
48380
MA = 331
56145
Ha = 187
272 n
mi
Hp = 182
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1357185
78 X = 482330
18
Y = -21708309
72 feet Y = -6611683
07 meter
Z = 3578388
46 Z = 1092868
74
XDOT = 15783
681917 XDOT = 4767
652935
YDOT = 4186
617419 feet/sec YDOT = 1329
636986 meter/sec
ZDOT = 19306
296596 ZDOT = 5907
825719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19270006
74 X = -5873498
06
Y = -10084364
46 feet Y = -3073714
29 meter
Z = 3587472
90 Z = 1093461
74
XDOT = 9485
365157 XDOT = 2891
139300
YDOT = -11186
332506 feet/sec YDOT = -3409
594148 meter/sec
ZDOT = 19400
404858 ZDOT = 5913
243401
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 11147
56682532
00016717 00000-0 10270-3 0 9008
2 25544 51
6482 266
4873 0004005 324
2932 35
7964 15
75593159 37664
Satellite: ISS
Catalog Number: 25544
Epoch time: 11147
56682532 = yrday
fracday
Element set: 900
Inclination: 51
6482 deg
RA of node: 266
4873 deg
Eccentricity:
0004005
Arg of perigee: 324
2932 deg
Mean anomaly: 35
7964 deg
Mean motion: 15
75593159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 326
Coasting Arc #2 (Orbit 3780)
---------------------------------------
Vector Time (GMT): 2011/148/12:07:55
713
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4278475
73 A = 6716484
04 meter
Y = -1425865
31 meter E =
0010706
Z = -4986359
04 I = 51
29206
XDOT = 311
341862 Wp = 88
57394
YDOT = -7458
896616 meter/sec RA = 260
81347 deg
ZDOT = 1869
472848 TA = 199
54286
MA = 199
58393
Ha = 187
253 n
mi
Hp = 181
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14036993
86 X = -4237990
33
Y = -4678035
79 feet Y = -1473483
04 meter
Z = -16359445
68 Z = -5007045
90
XDOT = 1021
462801 XDOT = 385
643872
YDOT = -24471
445591 feet/sec YDOT = -7454
999712 meter/sec
ZDOT = 6133
441103 ZDOT = 1871
165229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9775633
35 X = -2979613
05
Y = 10982430
28 feet Y = 3347444
75 meter
Z = -16443110
90 Z = -5011860
20
XDOT = -21318
745531 XDOT = -6497
953638
YDOT = -9800
502783 feet/sec YDOT = -2987
193248 meter/sec
ZDOT = 6140
599985 ZDOT = 1871
654875
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 11148
51818809
00016717 00000-0 10270-3 0 9013
2 25544 51
6483 261
5916 0004092 328
3608 31
7310 15
75674406 37813
Satellite: ISS
Catalog Number: 25544
Epoch time: 11148
51818809 = yrday
fracday
Element set: 901
Inclination: 51
6483 deg
RA of node: 261
5916 deg
Eccentricity:
0004092
Arg of perigee: 328
3608 deg
Mean anomaly: 31
7310 deg
Mean motion: 15
75674406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3781
Checksum: 310
Coasting Arc #3 (Orbit 3791)
---------------------------------------
Vector Time (GMT): 2011/149/04:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 1124139
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 29991
26 A = 6726129
18 meter
Y = 6495203
22 meter E =
0003052
Z = -1744618
08 I = 51
32811
XDOT = -4988
199422 Wp = 127
44147
YDOT = -1497
595721 meter/sec RA = 257
32159 deg
ZDOT = -5669
903386 TA = 71
96423
MA = 71
93098
Ha = 187
498 n
mi
Hp = 181
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 98396
53 X = -34166
43
Y = 21309721
86 feet Y = 6495180
04 meter
Z = -5723812
60 Z = -1744627
61
XDOT = -16365
483669 XDOT = -4943
538561
YDOT = -4913
371789 feet/sec YDOT = -1553
126552 meter/sec
ZDOT = -18602
045230 ZDOT = -5694
028033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15475655
83 X = -4716979
90
Y = 14649726
87 feet Y = 4465236
75 meter
Z = -5724118
95 Z = -1744711
45
XDOT = -6441
952428 XDOT = -1963
507100
YDOT = -14100
644019 feet/sec YDOT = -4297
876297 meter/sec
ZDOT = -18699
624099 ZDOT = -5699
645425
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 11149
21583329
00016717 00000-0 10270-3 0 9028
2 25544 51
6482 258
0039 0004685 331
8433 28
2477 15
75659122 37927
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
21583329 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 258
0039 deg
Eccentricity:
0004685
Arg of perigee: 331
8433 deg
Mean anomaly: 28
2477 deg
Mean motion: 15
75659122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3792
Checksum: 319
Coasting Arc #4 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2011/149/05:32:15
400
Vector Time (MET): N/A
Weight (LBS) : 1123503
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940905
83 A = 6716399
60 meter
Y = -1527242
65 meter E =
0004413
Z = 5219071
42 I = 51
29134
XDOT = 2141
893662 Wp = 6
53288
YDOT = 7380
479277 meter/sec RA = 257
08479 deg
ZDOT = 546
675523 TA = 78
27476
MA = 78
22524
Ha = 188
343 n
mi
Hp = 182
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12929481
06 X = 3932337
21
Y = -5010638
61 feet Y = -1483221
45 meter
Z = 17122937
73 Z = 5238195
63
XDOT = 7027
210177 XDOT = 2056
548847
YDOT = 24214
170857 feet/sec YDOT = 7403
953992 meter/sec
ZDOT = 1793
554864 ZDOT = 556
874371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13561618
38 X = 4133581
28
Y = 2387805
94 feet Y = 727803
25 meter
Z = 17200403
07 Z = 5242682
86
XDOT = -6419
198801 XDOT = -1956
571795
YDOT = 23343
913631 feet/sec YDOT = 7115
224875 meter/sec
ZDOT = 1834
529017 ZDOT = 559
164444
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 11149
27926814
00016717 00000-0 10270-3 0 9035
2 25544 51
6471 257
6758 0005888 339
5328 20
5599 15
75331591 37930
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
27926814 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 257
6758 deg
Eccentricity:
0005888
Arg of perigee: 339
5328 deg
Mean anomaly: 20
5599 deg
Mean motion: 15
75331591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 349
Coasting Arc #5 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2011/149/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 467399
87 A = 6727608
05 meter
Y = 6586943
41 meter E =
0003737
Z = -1283414
10 I = 51
32861
XDOT = -4967
758493 Wp = 116
53671
YDOT = -780
249429 meter/sec RA = 256
99265 deg
ZDOT = -5828
430358 TA = 77
60741
MA = 77
56558
Ha = 188
424 n
mi
Hp = 182
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1533464
15 X = 399943
34
Y = 21610706
72 feet Y = 6591793
11 meter
Z = -4210676
18 Z = -1281306
67
XDOT = -16298
420252 XDOT = -4930
350547
YDOT = -2559
873454 feet/sec YDOT = -835
592208 meter/sec
ZDOT = -19122
146845 ZDOT = -5852
473255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7495755
74 X = -2284706
35
Y = 20328730
39 feet Y = 6196197
02 meter
Z = -4202418
08 Z = -1280897
03
XDOT = -12203
139244 XDOT = -3719
516841
YDOT = -8462
720255 feet/sec YDOT = -2579
437134 meter/sec
ZDOT = -19219
424730 ZDOT = -5858
080658
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 11149
27926745
00016717 00000-0 10270-3 0 9049
2 25544 51
6462 257
6757 0005903 339
0022 21
0899 15
75353537 37936
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
27926745 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 257
6757 deg
Eccentricity:
0005903
Arg of perigee: 339
0022 deg
Mean anomaly: 21
0899 deg
Mean motion: 15
75353537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 329
Coasting Arc #6 (Orbit 3808)
---------------------------------------
Vector Time (GMT): 2011/150/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4460593
28 A = 6717426
27 meter
Y = 886142
16 meter E =
0009456
Z = 4943874
68 I = 51
30256
XDOT = 751
941345 Wp = 19
23477
YDOT = 7402
119736 meter/sec RA = 251
79391 deg
ZDOT = -1995
298023 TA = 90
20282
MA = 90
09446
Ha = 188
359 n
mi
Hp = 181
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14634492
38 X = 4426335
96
Y = 2907290
54 feet Y = 935831
11 meter
Z = 16220061
28 Z = 4965461
43
XDOT = 2466
999165 XDOT = 678
806464
YDOT = 24285
169737 feet/sec YDOT = 7410
119709 meter/sec
ZDOT = -6546
253356 ZDOT = -1991
821844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12189359
96 X = 3715316
92
Y = 8437969
26 feet Y = 2571893
03 meter
Z = 16307399
29 Z = 4970495
30
XDOT = -6721
191646 XDOT = -2048
619214
YDOT = 22396
571201 feet/sec YDOT = 6826
474902 meter/sec
ZDOT = -6532
486200 ZDOT = -1991
101794
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 11150
29420699
00016717 00000-0 10270-3 0 9051
2 25544 51
6459 252
4525 0005896 342
4670 17
6290 15
75399746 38092
Satellite: ISS
Catalog Number: 25544
Epoch time: 11150
29420699 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 252
4525 deg
Eccentricity:
0005896
Arg of perigee: 342
4670 deg
Mean anomaly: 17
6290 deg
Mean motion: 15
75399746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3809
Checksum: 337
Coasting Arc #7 (Orbit 3824)
---------------------------------------
Vector Time (GMT): 2011/151/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -805595
54 A = 6725903
63 meter
Y = -6296588
24 meter E =
0015731
Z = 2193752
08 I = 51
34161
XDOT = 5294
499983 Wp = 49
45409
YDOT = 1232
551341 meter/sec RA = 246
66035 deg
ZDOT = 5466
465681 TA = 335
27222
MA = 335
34755
Ha = 188
427 n
mi
Hp = 181
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2643029
98 X = -745782
99
Y = -20658097
90 feet Y = -6305262
76 meter
Z = 7197349
34 Z = 2189982
89
XDOT = 17370
406769 XDOT = 5253
768407
YDOT = 4043
803613 feet/sec YDOT = 1291
529178 meter/sec
ZDOT = 17934
598690 ZDOT = 5492
087930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5386649
11 X = 1641850
65
Y = -20123179
09 feet Y = -6133544
99 meter
Z = 7182348
41 Z = 2189179
79
XDOT = 12952
293839 XDOT = 3947
859162
YDOT = 9923
520903 feet/sec YDOT = 3024
689171 meter/sec
ZDOT = 18038
264683 ZDOT = 5498
063075
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 11151
30911106
00016717 00000-0 10270-3 0 9063
2 25544 51
6451 247
2292 0005870 346
6838 13
4170 15
75473389 38256
Satellite: ISS
Catalog Number: 25544
Epoch time: 11151
30911106 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 247
2292 deg
Eccentricity:
0005870
Arg of perigee: 346
6838 deg
Mean anomaly: 13
4170 deg
Mean motion: 15
75473389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3825
Checksum: 303
Coasting Arc #8 (Orbit 3839)
---------------------------------------
Vector Time (GMT): 2011/152/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4807438
12 A = 6718804
34 meter
Y = -1248785
04 meter E =
0009085
Z = -4531002
69 I = 51
33124
XDOT = -1038
980912 Wp = 75
91965
YDOT = -6995
841956 meter/sec RA = 241
44888 deg
ZDOT = 3037
751041 TA = 224
40582
MA = 224
47870
Ha = 188
455 n
mi
Hp = 181
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15772434
78 X = -4771105
64
Y = -4097063
77 feet Y = -1302340
89 meter
Z = -14865494
38 Z = -4554269
42
XDOT = -3408
730025 XDOT = -975
431845
YDOT = -22952
237387 feet/sec YDOT = -7007
105612 meter/sec
ZDOT = 9966
374805 ZDOT = 3032
856911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13105078
61 X = -3994427
96
Y = -9539644
22 feet Y = -2907683
56 meter
Z = -14959634
24 Z = -4559696
52
XDOT = 4453
105917 XDOT = 1357
306684
YDOT = -21678
494814 feet/sec YDOT = -6607
605219 meter/sec
ZDOT = 9946
844859 ZDOT = 3031
798313
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 11152
26055293
00016717 00000-0 10270-3 0 9076
2 25544 51
6448 242
3324 0005851 351
7012 8
4054 15
75518805 38409
Satellite: ISS
Catalog Number: 25544
Epoch time: 11152
26055293 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 242
3324 deg
Eccentricity:
0005851
Arg of perigee: 351
7012 deg
Mean anomaly: 8
4054 deg
Mean motion: 15
75518805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3840
Checksum: 289
Coasting Arc #9 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2011/153/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 939311
94 A = 6723464
40 meter
Y = 5892016
84 meter E =
0006338
Z = -3108702
68 I = 51
36319
XDOT = -5747
454499 Wp = 39
43994
YDOT = -1640
361627 meter/sec RA = 236
32928 deg
ZDOT = -4846
236333 TA = 176
82737
MA = 176
82335
Ha = 188
599 n
mi
Hp = 181
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3081732
08 X = 888458
08
Y = 19330763
90 feet Y = 5902236
97 meter
Z = -10199155
77 Z = -3104262
02
XDOT = -18856
478016 XDOT = -5705
142185
YDOT = -5381
763869 feet/sec YDOT = -1704
395769 meter/sec
ZDOT = -15899
725501 ZDOT = -4874
055169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3800047
38 X = -1158254
44
Y = 19211891
22 feet Y = 5855784
44 meter
Z = -10181412
47 Z = -3103294
52
XDOT = -14302
272976 XDOT = -4359
332803
YDOT = -11313
695999 feet/sec YDOT = -3448
414540 meter/sec
ZDOT = -16012
290984 ZDOT = -4880
546292
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 11153
27538963
00016717 00000-0 10270-3 0 9089
2 25544 51
6448 237
1099 0006030 356
4502 3
6618 15
75589494 38568
Satellite: ISS
Catalog Number: 25544
Epoch time: 11153
27538963 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 237
1099 deg
Eccentricity:
0006030
Arg of perigee: 356
4502 deg
Mean anomaly: 3
6618 deg
Mean motion: 15
75589494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 331
Coasting Arc #10 (Orbit 3871)
---------------------------------------
Vector Time (GMT): 2011/154/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5255061
06 A = 6720954
14 meter
Y = 1580387
77 meter E =
0013454
Z = 3877133
50 I = 51
37227
XDOT = 1056
975211 Wp = 54
55087
YDOT = 6466
385876 meter/sec RA = 231
11085 deg
ZDOT = -4050
883146 TA = 77
83366
MA = 77
68299
Ha = 188
547 n
mi
Hp = 180
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17241013
99 X = 5218163
82
Y = 5184999
24 feet Y = 1638946
09 meter
Z = 12720254
27 Z = 3902573
32
XDOT = 3467
766440 XDOT = 1004
266798
YDOT = 21215
176759 feet/sec YDOT = 6477
911595 meter/sec
ZDOT = -13290
299037 ZDOT = -4045
875273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14460426
67 X = 4407538
05
Y = 10602035
17 feet Y = 3231500
32 meter
Z = 12823203
96 Z = 3908512
57
XDOT = -2941
431959 XDOT = -896
548461
YDOT = 20131
447171 feet/sec YDOT = 6136
065098 meter/sec
ZDOT = -13270
275389 ZDOT = -4044
779939
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 11154
29019228
00016717 00000-0 10270-3 0 9091
2 25544 51
6439 231
8860 0005902 359
3416
7739 15
75606331 38728
Satellite: ISS
Catalog Number: 25544
Epoch time: 11154
29019228 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 231
8860 deg
Eccentricity:
0005902
Arg of perigee: 359
3416 deg
Mean anomaly:
7739 deg
Mean motion: 15
75606331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3872
Checksum: 313
Coasting Arc #11 (Orbit 3887)
---------------------------------------
Vector Time (GMT): 2011/155/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -841035
01 A = 6720652
68 meter
Y = -5381522
15 meter E =
0011924
Z = 3924281
23 I = 51
39199
XDOT = 6303
460287 Wp = 71
48499
YDOT = 1933
363341 meter/sec RA = 225
99638 deg
ZDOT = 3996
074178 TA = 336
93720
MA = 336
99068
Ha = 188
552 n
mi
Hp = 180
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2759301
20 X = -799858
70
Y = -17655912
57 feet Y = -5390697
54 meter
Z = 12874938
43 Z = 3920294
61
XDOT = 20680
643987 XDOT = 6261
960377
YDOT = 6343
055580 feet/sec YDOT = 2003
619759 meter/sec
ZDOT = 13110
479585 ZDOT = 4026
595874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2897418
70 X = 883133
22
Y = -17645398
93 feet Y = -5378317
59 meter
Z = 12859000
47 Z = 3919423
34
XDOT = 16247
900014 XDOT = 4952
359924
YDOT = 12326
899677 feet/sec YDOT = 3757
239022 meter/sec
ZDOT = 13234
010719 ZDOT = 4033
726467
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 11155
30495968
00016717 00000-0 10270-3 0 9105
2 25544 51
6438 226
6621 0005859 3
4936 356
6268 15
75694245 38887
Satellite: ISS
Catalog Number: 25544
Epoch time: 11155
30495968 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 226
6621 deg
Eccentricity:
0005859
Arg of perigee: 3
4936 deg
Mean anomaly: 356
6268 deg
Mean motion: 15
75694245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 346
Coasting Arc #12 (Orbit 3902)
---------------------------------------
Vector Time (GMT): 2011/156/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5735851
98 A = 6723156
10 meter
Y = -1750976
20 meter E =
0008792
Z = -3034882
98 I = 51
42405
XDOT = -802
065351 Wp = 36
89030
YDOT = -5872
530962 meter/sec RA = 220
78106 deg
ZDOT = 4918
313939 TA = 287
83030
MA = 287
92620
Ha = 188
568 n
mi
Hp = 180
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18818411
99 X = -5701103
08
Y = -5744672
58 feet Y = -1814923
22 meter
Z = -9956965
17 Z = -3062663
49
XDOT = -2631
448003 XDOT = -760
230134
YDOT = -19266
833864 feet/sec YDOT = -5881
266984 meter/sec
ZDOT = 16136
200586 ZDOT = 4914
518240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16169054
67 X = -4928327
86
Y = -11110514
53 feet Y = -3386484
83 meter
Z = -10069418
38 Z = -3069158
72
XDOT = 2370
025500 XDOT = 722
383773
YDOT = -18017
560424 feet/sec YDOT = -5491
752417 meter/sec
ZDOT = 16121
046043 ZDOT = 4913
694834
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 11156
25627475
00016717 00000-0 10270-3 0 9111
2 25544 51
6446 221
7650 0005896 8
6470 351
4795 15
75726541 39036
Satellite: ISS
Catalog Number: 25544
Epoch time: 11156
25627475 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 221
7650 deg
Eccentricity:
0005896
Arg of perigee: 8
6470 deg
Mean anomaly: 351
4795 deg
Mean motion: 15
75726541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3903
Checksum: 321
Coasting Arc #13 (Orbit 3918)
---------------------------------------
Vector Time (GMT): 2011/157/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 469974
87 A = 6717835
30 meter
Y = 4869727
28 meter E =
0014738
Z = -4617882
23 I = 51
43064
XDOT = -6825
133497 Wp = 50
34991
YDOT = -2073
343219 meter/sec RA = 215
66462 deg
ZDOT = -2877
861863 TA = 191
04380
MA = 191
07619
Ha = 188
686 n
mi
Hp = 180
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1541912
32 X = 437918
40
Y = 15976795
54 feet Y = 4874804
21 meter
Z = -15150532
24 Z = -4615676
31
XDOT = -22392
170265 XDOT = -6787
461674
YDOT = -6802
307149 feet/sec YDOT = -2149
454985 meter/sec
ZDOT = -9441
804013 ZDOT = -2910
926923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2966607
04 X = -904221
82
Y = 15782904
94 feet Y = 4810629
43 meter
Z = -15141772
38 Z = -4615212
22
XDOT = -18336
661438 XDOT = -5589
014406
YDOT = -12643
282168 feet/sec YDOT = -3853
672405 meter/sec
ZDOT = -9575
667271 ZDOT = -2918
663384
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 11157
27097684
00016717 00000-0 10270-3 0 9128
2 25544 51
6447 216
5415 0006019 12
6575 347
4739 15
75788511 39192
Satellite: ISS
Catalog Number: 25544
Epoch time: 11157
27097684 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 216
5415 deg
Eccentricity:
0006019
Arg of perigee: 12
6575 deg
Mean anomaly: 347
4739 deg
Mean motion: 15
75788511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3919
Checksum: 334
Coasting Arc #14 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2011/158/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6168119
66 A = 6725288
63 meter
Y = 1832167
39 meter E =
0014736
Z = 1944399
44 I = 51
48139
XDOT = 204
926790 Wp = 88
54367
YDOT = 5288
419085 meter/sec RA = 210
46117 deg
ZDOT = -5596
449603 TA = 69
75841
MA = 69
60004
Ha = 188
661 n
mi
Hp = 180
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20236613
07 X = 6137728
11
Y = 6011047
86 feet Y = 1900972
90 meter
Z = 6379263
26 Z = 1974290
37
XDOT = 672
331989 XDOT = 172
961804
YDOT = 17350
456314 feet/sec YDOT = 5290
532610 meter/sec
ZDOT = -18361
055128 ZDOT = -5595
531116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17857853
15 X = 5443073
64
Y = 11188900
00 feet Y = 3410376
72 meter
Z = 6500292
48 Z = 1981289
15
XDOT = -3065
106067 XDOT = -934
244329
YDOT = 15625
807390 feet/sec YDOT = 4762
746093 meter/sec
ZDOT = -18357
518749 ZDOT = -5595
371715
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 11158
28564544
00016717 00000-0 10270-3 0 9135
2 25544 51
6440 211
3161 0005949 15
8986 344
2364 15
75822138 39359
Satellite: ISS
Catalog Number: 25544
Epoch time: 11158
28564544 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 211
3161 deg
Eccentricity:
0005949
Arg of perigee: 15
8986 deg
Mean anomaly: 344
2364 deg
Mean motion: 15
75822138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 318
Coasting Arc #15 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2011/159/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 170232
95 A = 6715495
05 meter
Y = -4388776
43 meter E =
0006546
Z = 5074388
24 I = 51
47743
XDOT = 7261
862459 Wp = 65
07458
YDOT = 2072
419171 meter/sec RA = 205
33162 deg
ZDOT = 1549
955745 TA = 10
04095
MA = 10
02788
Ha = 188
595 n
mi
Hp = 179
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 558507
05 X = 194646
08
Y = -14398872
80 feet Y = -4386736
77 meter
Z = 16648255
37 Z = 5075274
10
XDOT = 23825
008068 XDOT = 7230
619174
YDOT = 6799
275496 feet/sec YDOT = 2153
450889 meter/sec
ZDOT = 5085
156645 ZDOT = 1585
158047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4051287
86 X = 1234832
54
Y = -13823966
46 feet Y = -4213544
98 meter
Z = 16651993
66 Z = 5075527
67
XDOT = 20323
546815 XDOT = 6194
617069
YDOT = 12248
641563 feet/sec YDOT = 3733
385948 meter/sec
ZDOT = 5227
709762 ZDOT = 1593
405935
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
30027966
00016717 00000-0 10270-3 0 9142
2 25544 51
6452 206
0916 0005989 18
9132 341
2253 15
75907141 39512
Satellite: ISS
Catalog Number: 25544
Epoch time: 11159
30027966 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 206
0916 deg
Eccentricity:
0005989
Arg of perigee: 18
9132 deg
Mean anomaly: 341
2253 deg
Mean motion: 15
75907141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 308
Coasting Arc #16 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2011/160/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6445159
99 A = 6726446
13 meter
Y = -1751653
76 meter E =
0016431
Z = -725398
62 I = 51
54402
XDOT = 646
104320 Wp = 34
09603
YDOT = -4820
804423 meter/sec RA = 200
15274 deg
ZDOT = 5978
804825 TA = 317
97858
MA = 318
10450
Ha = 188
665 n
mi
Hp = 179
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21145538
04 X = -6421569
79
Y = -5746895
55 feet Y = -1823595
50 meter
Z = -2379916
74 Z = -756652
07
XDOT = 2119
764830 XDOT = 670
919509
YDOT = -15816
287477 feet/sec YDOT = -4813
441072 meter/sec
ZDOT = 19615
501395 ZDOT = 5982
003450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19201012
10 X = -5852468
49
Y = -10529160
30 feet Y = -3209288
06 meter
Z = -2506493
29 Z = -763979
15
XDOT = 4877
156299 XDOT = 1486
557240
YDOT = -13508
491585 feet/sec YDOT = -4117
388235 meter/sec
ZDOT = 19628
623064 ZDOT = 5982
804310
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
25147036
00016717 00000-0 10270-3 0 9150
2 25544 51
6462 201
1941 0006074 23
6835 336
4608 15
75925990 39664
Satellite: ISS
Catalog Number: 25544
Epoch time: 11160
25147036 = yrday
fracday
Element set: 915
Inclination: 51
6462 deg
RA of node: 201
1941 deg
Eccentricity:
0006074
Arg of perigee: 23
6835 deg
Mean anomaly: 336
4608 deg
Mean motion: 15
75925990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 308
Coasting Arc #17 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2011/161/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1020054
23 A = 6714408
79 meter
Y = 4058332
53 meter E =
0018754
Z = -5266395
44 I = 51
53352
XDOT = -7439
876136 Wp = 72
88817
YDOT = -1948
621714 meter/sec RA = 195
00447 deg
ZDOT = -55
328847 TA = 196
55472
MA = 196
61603
Ha = 188
685 n
mi
Hp = 179
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3346634
63 X = -1039776
16
Y = 13314739
28 feet Y = 4046815
89 meter
Z = -17278200
26 Z = -5271398
41
XDOT = -24409
042440 XDOT = -7417
264541
YDOT = -6393
115859 feet/sec YDOT = -2031
692496 meter/sec
ZDOT = -181
525089 ZDOT = -91
417198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6055903
55 X = -1845839
40
Y = 12292380
03 feet Y = 3746717
43 meter
Z = -17298609
05 Z = -5272616
04
XDOT = -21541
138195 XDOT = -6565
738922
YDOT = -11097
758425 feet/sec YDOT = -3382
596768 meter/sec
ZDOT = -327
697524 ZDOT = -99
882205
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
26604032
00016717 00000-0 10270-3 0 9167
2 25544 51
6463 195
9702 0006124 27
4045 332
7441 15
76000870 39825
Satellite: ISS
Catalog Number: 25544
Epoch time: 11161
26604032 = yrday
fracday
Element set: 916
Inclination: 51
6463 deg
RA of node: 195
9702 deg
Eccentricity:
0006124
Arg of perigee: 27
4045 deg
Mean anomaly: 332
7441 deg
Mean motion: 15
76000870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 286
Coasting Arc #18 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2011/162/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6486375
10 A = 6726192
84 meter
Y = 1651180
04 meter E =
0010644
Z = -652113
48 I = 51
60380
XDOT = -1742
909308 Wp = 107
19109
YDOT = 4514
361907 meter/sec RA = 189
85371 deg
ZDOT = -5988
821721 TA = 79
91619
MA = 79
79612
Ha = 188
683 n
mi
Hp = 179
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21280758
19 X = 6470597
07
Y = 5417257
36 feet Y = 1723626
49 meter
Z = -2139479
91 Z = -620640
54
XDOT = -5718
206390 XDOT = -1764
167380
YDOT = 14810
898644 feet/sec YDOT = 4494
753452 meter/sec
ZDOT = -19648
365228 ZDOT = -5997
339973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19776937
13 X = 6028010
44
Y = 9571801
13 feet Y = 2917484
99 meter
Z = -2011989
45 Z = -613254
39
XDOT = -7754
732154 XDOT = -2363
642360
YDOT = 11946
210190 feet/sec YDOT = 3641
204866 meter/sec
ZDOT = -19683
039025 ZDOT = -5999
390295
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
28057661
00016717 00000-0 10270-3 0 9171
2 25544 51
6463 190
7444 0006092 31
0508 329
1016 15
76045390 39981
Satellite: ISS
Catalog Number: 25544
Epoch time: 11162
28057661 = yrday
fracday
Element set: 917
Inclination: 51
6463 deg
RA of node: 190
7444 deg
Eccentricity:
0006092
Arg of perigee: 31
0508 deg
Mean anomaly: 329
1016 deg
Mean motion: 15
76045390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 306
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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