[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 5th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
There are no maneuvers
Coasting Arc #1 (Orbit 832)
---------------------------------------
Vector Time (GMT): 2011/215/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3277343
12 A = 6768386
82 meter
Y = -5215981
73 meter E =
0024005
Z = 2769059
32 I = 51
30833
XDOT = 3237
484008 Wp = 58
65133
YDOT = 4754
821271 meter/sec RA = 281
04087 deg
ZDOT = 5104
368813 TA = 333
03594
MA = 333
16047
Ha = 215
429 n
mi
Hp = 201
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10752438
07 X = 3321974
28
Y = -17112800
96 feet Y = -5179082
98 meter
Z = 9084840
30 Z = 2785088
74
XDOT = 10621
666693 XDOT = 3159
278339
YDOT = 15599
807321 feet/sec YDOT = 4790
587447 meter/sec
ZDOT = 16746
616842 ZDOT = 5119
906376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6984411
73 X = -2128848
69
Y = 18933799
42 feet Y = 5771022
06 meter
Z = 9150215
12 Z = 2788985
57
XDOT = -12099
404132 XDOT = -3687
898379
YDOT = -12618
962040 feet/sec YDOT = -3846
259630 meter/sec
ZDOT = 16809
487995 ZDOT = 5123
531941
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 11215
72692996
00016717 00000-0 10270-3 0 9007
2 25544 51
6375 281
4583 0012442 35
9969 324
2022 15
60209013 8330
Satellite: ISS
Catalog Number: 25544
Epoch time: 11215
72692996 = yrday
fracday
Element set: 900
Inclination: 51
6375 deg
RA of node: 281
4583 deg
Eccentricity:
0012442
Arg of perigee: 35
9969 deg
Mean anomaly: 324
2022 deg
Mean motion: 15
60209013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 833
Checksum: 301
Coasting Arc #2 (Orbit 847)
---------------------------------------
Vector Time (GMT): 2011/216/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4230996
55 A = 6760820
86 meter
Y = 1629709
56 meter E =
0024343
Z = -5036629
66 I = 51
27781
XDOT = -687
050900 Wp = 58
36975
YDOT = -7410
444913 meter/sec RA = 275
97674 deg
ZDOT = -1814
604008 TA = 193
92109
MA = 193
98832
Ha = 215
583 n
mi
Hp = 201
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13881222
26 X = -4224439
06
Y = 5346816
16 feet Y = 1582432
77 meter
Z = -16524375
54 Z = -5057167
64
XDOT = -2254
104002 XDOT = -595
319884
YDOT = -24312
483310 feet/sec YDOT = -7417
614996 meter/sec
ZDOT = -5953
425223 ZDOT = -1817
719028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12262085
97 X = 3737483
80
Y = -8255380
23 feet Y = -2516239
89 meter
Z = -16607880
85 Z = -5062082
08
XDOT = 6926
630664 XDOT = 2111
237027
YDOT = 22329
771729 feet/sec YDOT = 6806
114423 meter/sec
ZDOT = -5965
709316 ZDOT = -1818
348200
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 11216
68769718
00016717 00000-0 10270-3 0 9011
2 25544 51
6370 276
6237 0012471 39
5047 320
7015 15
60208464 8484
Satellite: ISS
Catalog Number: 25544
Epoch time: 11216
68769718 = yrday
fracday
Element set: 901
Inclination: 51
6370 deg
RA of node: 276
6237 deg
Eccentricity:
0012471
Arg of perigee: 39
5047 deg
Mean anomaly: 320
7015 deg
Mean motion: 15
60208464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 848
Checksum: 309
Coasting Arc #3 (Orbit 863)
---------------------------------------
Vector Time (GMT): 2011/217/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3844944
32 A = 6761468
35 meter
Y = 2713598
89 meter E =
0019149
Z = 4847228
15 I = 51
27759
XDOT = -1989
721310 Wp = 48
26630
YDOT = 7041
897495 meter/sec RA = 270
88667 deg
ZDOT = -2345
380913 TA = 64
86289
MA = 64
66436
Ha = 215
522 n
mi
Hp = 201
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12614646
70 X = 3790767
82
Y = 8902883
51 feet Y = 2756292
28 meter
Z = 15902979
48 Z = 4865775
24
XDOT = -6527
957054 XDOT = -2056
923965
YDOT = 23103
338238 feet/sec YDOT = 7019
271566 meter/sec
ZDOT = -7694
819268 ZDOT = -2355
209827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14274623
62 X = -4350905
28
Y = -5676981
18 feet Y = -1730343
87 meter
Z = 15978185
37 Z = 4870150
90
XDOT = 397
280515 XDOT = 121
091101
YDOT = -22940
298751 feet/sec YDOT = -6992
203059 meter/sec
ZDOT = -7735
090539 ZDOT = -2357
655596
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 11217
71250621
00016717 00000-0 10270-3 0 9025
2 25544 51
6364 271
4664 0012509 42
6836 317
5290 15
60238315 8642
Satellite: ISS
Catalog Number: 25544
Epoch time: 11217
71250621 = yrday
fracday
Element set: 902
Inclination: 51
6364 deg
RA of node: 271
4664 deg
Eccentricity:
0012509
Arg of perigee: 42
6836 deg
Mean anomaly: 317
5290 deg
Mean motion: 15
60238315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 864
Checksum: 291
Coasting Arc #4 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2011/218/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2330177
63 A = 6769189
15 meter
Y = -5894473
49 meter E =
0018273
Z = -2366110
55 I = 51
30408
XDOT = 4034
195972 Wp = 46
49681
YDOT = -3731
623613 meter/sec RA = 265
82952 deg
ZDOT = 5361
686515 TA = 286
88159
MA = 287
08188
Ha = 215
671 n
mi
Hp = 201
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7644939
73 X = -2252597
27
Y = -19338823
79 feet Y = -5920097
03 meter
Z = -7762829
88 Z = -2377242
38
XDOT = 13235
551088 XDOT = 4049
578018
YDOT = -12242
859624 feet/sec YDOT = -3686
425109 meter/sec
ZDOT = 17590
835023 ZDOT = 5381
321585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12262574
39 X = 3737632
67
Y = 16773932
91 feet Y = 5112694
75 meter
Z = -7807764
13 Z = -2379806
51
XDOT = -8364
817448 XDOT = -2549
596358
YDOT = 14282
060221 feet/sec YDOT = 4353
171955 meter/sec
ZDOT = 17670
778295 ZDOT = 5386
053224
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 11218
67325722
00016717 00000-0 10270-3 0 9037
2 25544 51
6363 266
6330 0012645 46
5810 313
6397 15
60241776 8799
Satellite: ISS
Catalog Number: 25544
Epoch time: 11218
67325722 = yrday
fracday
Element set: 903
Inclination: 51
6363 deg
RA of node: 266
6330 deg
Eccentricity:
0012645
Arg of perigee: 46
5810 deg
Mean anomaly: 313
6397 deg
Mean motion: 15
60241776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 879
Checksum: 310
Coasting Arc #5 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2011/219/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3929
18 A = 6770798
03 meter
Y = 6644080
37 meter E =
0015117
Z = -1320885
67 I = 51
31291
XDOT = -4888
097355 Wp = 85
50846
YDOT = -1138
707656 meter/sec RA = 260
80563 deg
ZDOT = -5798
521282 TA = 108
95749
MA = 108
79360
Ha = 215
742 n
mi
Hp = 201
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12891
02 X = -63949
96
Y = 21798163
95 feet Y = 6643744
89 meter
Z = -4333614
39 Z = -1321030
92
XDOT = -16037
064813 XDOT = -4846
832967
YDOT = -3735
917505 feet/sec YDOT = -1193
138148 meter/sec
ZDOT = -19024
019953 ZDOT = -5822
167249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5937947
92 X = -1809886
53
Y = -20973626
89 feet Y = -6392761
48 meter
Z = -4334522
03 Z = -1321162
31
XDOT = 14809
936186 XDOT = 4514
068549
YDOT = -279
605375 feet/sec YDOT = -85
223718 meter/sec
ZDOT = -19120
027702 ZDOT = -5827
784444
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 11219
69804933
00016717 00000-0 10270-3 0 9047
2 25544 51
6363 261
4753 0012688 49
7700 310
4564 15
60263730 8954
Satellite: ISS
Catalog Number: 25544
Epoch time: 11219
69804933 = yrday
fracday
Element set: 904
Inclination: 51
6363 deg
RA of node: 261
4753 deg
Eccentricity:
0012688
Arg of perigee: 49
7700 deg
Mean anomaly: 310
4564 deg
Mean motion: 15
60263730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 895
Checksum: 315
Coasting Arc #6 (Orbit 910)
---------------------------------------
Vector Time (GMT): 2011/220/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2397805
05 A = 6763415
72 meter
Y = -4606145
47 meter E =
0019606
Z = 4314110
32 I = 51
29406
XDOT = 4222
497448 Wp = 76
97780
YDOT = 5429
380942 meter/sec RA = 255
76266 deg
ZDOT = 3441
200612 TA = 337
99451
MA = 338
07857
Ha = 215
575 n
mi
Hp = 200
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7866814
47 X = 2428176
81
Y = -15112025
84 feet Y = -4579162
33 meter
Z = 14153905
23 Z = 4325832
03
XDOT = 13853
338085 XDOT = 4144
754759
YDOT = 17812
929601 feet/sec YDOT = 5476
164491 meter/sec
ZDOT = 11290
028253 ZDOT = 3461
524840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3113554
48 X = -949011
41
Y = 16709558
66 feet Y = 5093073
48 meter
Z = 14201744
82 Z = 4328691
82
XDOT = -17102
002567 XDOT = -5212
690382
YDOT = -12876
763407 feet/sec YDOT = -3924
837486 meter/sec
ZDOT = 11372
348750 ZDOT = 3466
291899
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 11220
72283106
00016717 00000-0 10270-3 0 9057
2 25544 51
6360 256
3194 0012472 53
1377 307
0921 15
60297650 9119
Satellite: ISS
Catalog Number: 25544
Epoch time: 11220
72283106 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 256
3194 deg
Eccentricity:
0012472
Arg of perigee: 53
1377 deg
Mean anomaly: 307
0921 deg
Mean motion: 15
60297650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 911
Checksum: 280
Coasting Arc #7 (Orbit 925)
---------------------------------------
Vector Time (GMT): 2011/221/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4202967
60 A = 6759660
08 meter
Y = 756666
86 meter E =
0025911
Z = -5261205
02 I = 51
28959
XDOT = -2066
624161 Wp = 77
22475
YDOT = -7351
564677 meter/sec RA = 250
67762 deg
ZDOT = 601
775364 TA = 198
50608
MA = 198
60049
Ha = 215
795 n
mi
Hp = 200
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13789263
77 X = -4185558
95
Y = 2482502
82 feet Y = 709764
51 meter
Z = -17261171
34 Z = -5281580
28
XDOT = -6780
262995 XDOT = -1987
187196
YDOT = -24119
306682 feet/sec YDOT = -7374
230824 meter/sec
ZDOT = 1974
328621 ZDOT = 591
928215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12285446
29 X = 3744604
03
Y = -6519836
28 feet Y = -1987246
10 meter
Z = -17343995
96 Z = -5286449
97
XDOT = 13319
485807 XDOT = 4059
779274
YDOT = 20022
262131 feet/sec YDOT = 6102
785498 meter/sec
ZDOT = 1934
651800 ZDOT = 589
681869
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 11221
68355772
00016717 00000-0 10270-3 0 9063
2 25544 51
6359 251
4846 0012644 56
6476 303
5888 15
60268117 9261
Satellite: ISS
Catalog Number: 25544
Epoch time: 11221
68355772 = yrday
fracday
Element set: 906
Inclination: 51
6359 deg
RA of node: 251
4846 deg
Eccentricity:
0012644
Arg of perigee: 56
6476 deg
Mean anomaly: 303
5888 deg
Mean motion: 15
60268117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 926
Checksum: 328
Coasting Arc #8 (Orbit 941)
---------------------------------------
Vector Time (GMT): 2011/222/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4666906
01 A = 6765788
20 meter
Y = 3301741
11 meter E =
0023938
Z = 3605450
07 I = 51
32134
XDOT = -1012
599729 Wp = 72
50842
YDOT = 6237
763944 meter/sec RA = 245
60227 deg
ZDOT = -4370
548385 TA = 64
38735
MA = 64
14019
Ha = 215
717 n
mi
Hp = 200
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15311371
44 X = 4612124
25
Y = 10832483
97 feet Y = 3353622
73 meter
Z = 11828904
44 Z = 3627988
54
XDOT = -3322
177587 XDOT = -1061
045541
YDOT = 20465
104802 feet/sec YDOT = 6226
169885 meter/sec
ZDOT = -14339
069505 ZDOT = -4375
584685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17905018
42 X = -5457449
61
Y = -5386965
49 feet Y = -1641947
08 meter
Z = 11920348
26 Z = 3633322
15
XDOT = -3875
463578 XDOT = -1181
241299
YDOT = -19118
188997 feet/sec YDOT = -5827
224006 meter/sec
ZDOT = -14359
809426 ZDOT = -4376
869913
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 11222
70832218
00016717 00000-0 10270-3 0 9073
2 25544 51
6356 246
3277 0012648 59
8226 300
4181 15
60306157 9428
Satellite: ISS
Catalog Number: 25544
Epoch time: 11222
70832218 = yrday
fracday
Element set: 907
Inclination: 51
6356 deg
RA of node: 246
3277 deg
Eccentricity:
0012648
Arg of perigee: 59
8226 deg
Mean anomaly: 300
4181 deg
Mean motion: 15
60306157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 942
Checksum: 295
Coasting Arc #9 (Orbit 956)
---------------------------------------
Vector Time (GMT): 2011/223/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3490280
03 A = 6771359
81 meter
Y = -5786954
15 meter E =
0023880
Z = -245925
80 I = 51
35337
XDOT = 4006
388122 Wp = 54
21125
YDOT = -2653
166869 meter/sec RA = 240
57205 deg
ZDOT = 5994
123678 TA = 303
11993
MA = 303
34889
Ha = 215
772 n
mi
Hp = 200
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11451049
98 X = -3424115
15
Y = -18986070
05 feet Y = -5825614
63 meter
Z = -806843
17 Z = -262720
73
XDOT = 13144
317986 XDOT = 4006
641000
YDOT = -8704
615711 feet/sec YDOT = -2608
363909 meter/sec
ZDOT = 19665
760098 ZDOT = 6013
586658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17163362
27 X = 5231392
82
Y = 14032178
10 feet Y = 4277007
88 meter
Z = -874854
90 Z = -266655
77
XDOT = -8317
583287 XDOT = -2535
199386
YDOT = 11325
019924 feet/sec YDOT = 3451
866073 meter/sec
ZDOT = 19744
970355 ZDOT = 6018
266964
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 11223
66903056
00016717 00000-0 10270-3 0 9089
2 25544 51
6354 241
4937 0012660 63
8737 296
3720 15
60320989 9578
Satellite: ISS
Catalog Number: 25544
Epoch time: 11223
66903056 = yrday
fracday
Element set: 908
Inclination: 51
6354 deg
RA of node: 241
4937 deg
Eccentricity:
0012660
Arg of perigee: 63
8737 deg
Mean anomaly: 296
3720 deg
Mean motion: 15
60320989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 957
Checksum: 321
Coasting Arc #10 (Orbit 972)
---------------------------------------
Vector Time (GMT): 2011/224/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 815626
04 A = 6766698
20 meter
Y = 5859110
33 meter E =
0016944
Z = -3304447
01 I = 51
35439
XDOT = -5789
494849 Wp = 74
60115
YDOT = -1824
427207 meter/sec RA = 235
54594 deg
ZDOT = -4679
551877 TA = 144
03703
MA = 143
92289
Ha = 215
814 n
mi
Hp = 200
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2675938
44 X = 766099
67
Y = 19222802
92 feet Y = 5867954
35 meter
Z = -10841361
58 Z = -3300604
91
XDOT = -18994
405673 XDOT = -5745
931674
YDOT = -5985
653567 feet/sec YDOT = -1888
925142 meter/sec
ZDOT = -15352
860488 ZDOT = -4707
570713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9338970
13 X = -2846518
09
Y = -17023327
65 feet Y = -5188710
27 meter
Z = -10825981
36 Z = -3299759
12
XDOT = 18557
331094 XDOT = 5656
274517
YDOT = -377
219300 feet/sec YDOT = -114
976443 meter/sec
ZDOT = -15466
666731 ZDOT = -4714
240020
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 11224
69377659
00016717 00000-0 10270-3 0 9098
2 25544 51
6361 236
3360 0012677 66
9434 293
3057 15
60336135 9733
Satellite: ISS
Catalog Number: 25544
Epoch time: 11224
69377659 = yrday
fracday
Element set: 909
Inclination: 51
6361 deg
RA of node: 236
3360 deg
Eccentricity:
0012677
Arg of perigee: 66
9434 deg
Mean anomaly: 293
3057 deg
Mean motion: 15
60336135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 973
Checksum: 325
Coasting Arc #11 (Orbit 988)
---------------------------------------
Vector Time (GMT): 2011/225/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2413878
33 A = 6759632
59 meter
Y = -3587154
76 meter E =
0015139
Z = 5182672
72 I = 51
34942
XDOT = 5487
517026 Wp = 82
54950
YDOT = 5275
845600 meter/sec RA = 230
47906 deg
ZDOT = 1094
973622 TA = 356
94166
MA = 356
95091
Ha = 215
638 n
mi
Hp = 200
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7919548
32 X = 2428635
37
Y = -11768880
45 feet Y = -3560078
85 meter
Z = 17003519
43 Z = 5194434
83
XDOT = 18003
664784 XDOT = 5422
794608
YDOT = 17309
204723 feet/sec YDOT = 5336
848469 meter/sec
ZDOT = 3592
433143 ZDOT = 1121
474116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2931421
85 X = -893497
38
Y = 13820265
01 feet Y = 4212416
78 meter
Z = 17051466
41 Z = 5197286
96
XDOT = -22086
299849 XDOT = -6731
904194
YDOT = -9252
995519 feet/sec YDOT = -2820
313034 meter/sec
ZDOT = 3699
947309 ZDOT = 1127
743940
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 11225
71851194
00016717 00000-0 10270-3 0 9105
2 25544 51
6363 231
1797 0012506 70
6612 289
5895 15
60373808 9895
Satellite: ISS
Catalog Number: 25544
Epoch time: 11225
71851194 = yrday
fracday
Element set: 910
Inclination: 51
6363 deg
RA of node: 231
1797 deg
Eccentricity:
0012506
Arg of perigee: 70
6612 deg
Mean anomaly: 289
5895 deg
Mean motion: 15
60373808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 989
Checksum: 324
Coasting Arc #12 (Orbit 1003)
---------------------------------------
Vector Time (GMT): 2011/226/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5003807
59 A = 6762307
80 meter
Y = 121298
89 meter E =
0021702
Z = -4565952
14 I = 51
37838
XDOT = -2912
823622 Wp = 90
37586
YDOT = -6405
598402 meter/sec RA = 225
39602 deg
ZDOT = 3034
346601 TA = 210
01377
MA = 210
13833
Ha = 215
787 n
mi
Hp = 200
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16416691
57 X = -4982612
06
Y = 397962
22 feet Y = 65461
73 meter
Z = -14980157
95 Z = -4590208
56
XDOT = -9556
507946 XDOT = -2855
718433
YDOT = -21015
742789 feet/sec YDOT = -6437
852056 meter/sec
ZDOT = 9955
205385 ZDOT = 3020
335209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14919328
93 X = 4547411
46
Y = -6641970
81 feet Y = -2024472
70 meter
Z = -15078763
74 Z = -4596007
19
XDOT = 16470
799231 XDOT = 5020
299606
YDOT = 14616
767115 feet/sec YDOT = 4455
190617 meter/sec
ZDOT = 9898
484443 ZDOT = 3017
058058
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 11226
67919439
00016717 00000-0 10270-3 0 9119
2 25544 51
6364 226
3444 0012604 74
0278 286
2266 15
60350389 10040
Satellite: ISS
Catalog Number: 25544
Epoch time: 11226
67919439 = yrday
fracday
Element set: 911
Inclination: 51
6364 deg
RA of node: 226
3444 deg
Eccentricity:
0012604
Arg of perigee: 74
0278 deg
Mean anomaly: 286
2266 deg
Mean motion: 15
60350389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1004
Checksum: 303
Coasting Arc #13 (Orbit 1019)
---------------------------------------
Vector Time (GMT): 2011/227/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5747146
30 A = 6770053
31 meter
Y = 3161382
34 meter E =
0025197
Z = 1645245
60 I = 51
42733
XDOT = -1110
883144 Wp = 98
17219
YDOT = 5024
687804 meter/sec RA = 220
35338 deg
ZDOT = -5703
306769 TA = 63
69707
MA = 63
43844
Ha = 215
797 n
mi
Hp = 200
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18855466
87 X = 5703375
83
Y = 10371989
31 feet Y = 3225405
74 meter
Z = 5397787
39 Z = 1673058
26
XDOT = -3644
629737 XDOT = -1139
282568
YDOT = 16485
196207 feet/sec YDOT = 5012
106312 meter/sec
ZDOT = -18711
636380 ZDOT = -5708
772419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21400526
82 X = -6522880
57
Y = -1972840
70 feet Y = -601321
85 meter
Z = 5510739
82 Z = 1679673
50
XDOT = -3503
983107 XDOT = -1068
014051
YDOT = -14959
617574 feet/sec YDOT = -4559
691436 meter/sec
ZDOT = -18734
032380 ZDOT = -5710
133069
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 11227
70391180
00016717 00000-0 10270-3 0 9122
2 25544 51
6372 221
1867 0012658 77
9216 282
3357 15
60368188 10206
Satellite: ISS
Catalog Number: 25544
Epoch time: 11227
70391180 = yrday
fracday
Element set: 912
Inclination: 51
6372 deg
RA of node: 221
1867 deg
Eccentricity:
0012658
Arg of perigee: 77
9216 deg
Mean anomaly: 282
3357 deg
Mean motion: 15
60368188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1020
Checksum: 302
Coasting Arc #14 (Orbit 1035)
---------------------------------------
Vector Time (GMT): 2011/228/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4157973
38 A = 6769513
47 meter
Y = -4927790
58 meter E =
0026447
Z = 2026309
65 I = 51
44926
XDOT = 4972
357716 Wp = 74
83906
YDOT = -1892
739030 meter/sec RA = 215
33954 deg
ZDOT = 5546
730557 TA = 307
70336
MA = 307
94284
Ha = 215
815 n
mi
Hp = 200
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13641644
95 X = -4112404
11
Y = -16167291
93 feet Y = -4974032
72 meter
Z = 6647997
54 Z = 2006221
40
XDOT = 16313
509567 XDOT = 4966
208582
YDOT = -6209
773719 feet/sec YDOT = -1837
169304 meter/sec
ZDOT = 18197
934897 ZDOT = 5570
870976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19165829
42 X = 5841744
81
Y = 9012422
17 feet Y = 2746986
28 meter
Z = 6566498
75 Z = 2001468
82
XDOT = -11496
339769 XDOT = -3504
084362
YDOT = 10987
861721 feet/sec YDOT = 3349
100253 meter/sec
ZDOT = 18296
140573 ZDOT = 5576
663647
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 11228
72861882
00016717 00000-0 10270-3 0 9137
2 25544 51
6372 216
0299 0012617 81
4834 278
7751 15
60380483 10365
Satellite: ISS
Catalog Number: 25544
Epoch time: 11228
72861882 = yrday
fracday
Element set: 913
Inclination: 51
6372 deg
RA of node: 216
0299 deg
Eccentricity:
0012617
Arg of perigee: 81
4834 deg
Mean anomaly: 278
7751 deg
Mean motion: 15
60380483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1036
Checksum: 316
Coasting Arc #15 (Orbit 1050)
---------------------------------------
Vector Time (GMT): 2011/229/16:02:39
721
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 644985
83 A = 6761471
28 meter
Y = 4775058
53 meter E =
0023715
Z = -4765511
53 I = 51
44893
XDOT = -7000
796794 Wp = 78
90281
YDOT = -1667
480368 meter/sec RA = 210
29521 deg
ZDOT = -2624
978731 TA = 165
14532
MA = 165
07553
Ha = 215
770 n
mi
Hp = 200
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2116095
25 X = 614691
95
Y = 15666202
54 feet Y = 4782101
63 meter
Z = -15634880
33 Z = -4762451
96
XDOT = -22968
493420 XDOT = -6968
878885
YDOT = -5470
736117 feet/sec YDOT = -1745
589171 meter/sec
ZDOT = -8612
134943 ZDOT = -2658
910567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8753157
71 X = -2667962
47
Y = -13178536
08 feet Y = -4016817
80 meter
Z = -15622600
96 Z = -4761768
77
XDOT = 22072
952491 XDOT = 6727
835919
YDOT = -4313
851998 feet/sec YDOT = -1314
862089 meter/sec
ZDOT = -8750
034631 ZDOT = -2667
010555
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 11229
68927183
00016717 00000-0 10270-3 0 9141
2 25544 51
6382 211
1946 0012660 85
0162 275
2439 15
60415275 10513
Satellite: ISS
Catalog Number: 25544
Epoch time: 11229
68927183 = yrday
fracday
Element set: 914
Inclination: 51
6382 deg
RA of node: 211
1946 deg
Eccentricity:
0012660
Arg of perigee: 85
0162 deg
Mean anomaly: 275
2439 deg
Mean motion: 15
60415275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1051
Checksum: 298
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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