[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 14th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13723 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 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
172/13:49:37
935 -0
8 4
2 4
2
N/A 4
1 0
0 221
0
000/00:09:15
871 -0
4 -0
2 209
7
Coasting Arc #1 (Orbit 1743)
---------------------------------------
Vector Time (GMT): 2012/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5622742
18 A = 6782432
35 meter
Y = -3637439
57 meter E =
0015332
Z = -1078355
93 I = 51
87530
XDOT = 1814
890137 Wp = 98
45924
YDOT = 4534
946917 meter/sec RA = 139
84045 deg
ZDOT = -5907
640599 TA = 93
20007
MA = 93
02463
Ha = 221
285 n
mi
Hp = 207
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18447316
87 X = 5668237
32
Y = -11933856
86 feet Y = -3574308
10 meter
Z = -3537913
17 Z = -1050930
59
XDOT = 5954
363967 XDOT = 1792
742713
YDOT = 14878
434767 feet/sec YDOT = 4555
118910 meter/sec
ZDOT = -19382
022964 ZDOT = -5898
877222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9037840
46 X = -2754733
77
Y = -20045615
60 feet Y = -6109903
64 meter
Z = -3424617
33 Z = -1043823
36
XDOT = 14156
278386 XDOT = 4314
833652
YDOT = -3120
148513 feet/sec YDOT = -951
021267 meter/sec
ZDOT = -19346
316319 ZDOT = -5896
757214
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 12165
53015917
00016717 00000-0 10270-3 0 9003
2 25544 51
6348 140
6925 0010651 59
7464 300
4742 15
56341602 17443
Satellite: ISS
Catalog Number: 25544
Epoch time: 12165
53015917 = yrday
fracday
Element set: 900
Inclination: 51
6348 deg
RA of node: 140
6925 deg
Eccentricity:
0010651
Arg of perigee: 59
7464 deg
Mean anomaly: 300
4742 deg
Mean motion: 15
56341602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1744
Checksum: 290
Coasting Arc #2 (Orbit 1759)
---------------------------------------
Vector Time (GMT): 2012/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5585111
69 A = 6778287
90 meter
Y = 1974663
49 meter E =
0022706
Z = 3269613
99 I = 51
88445
XDOT = 685
684558 Wp = 76
95968
YDOT = -5986
989184 meter/sec RA = 134
86953 deg
ZDOT = 4764
373145 TA = 320
93284
MA = 321
09661
Ha = 221
232 n
mi
Hp = 207
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18323857
24 X = -5622660
85
Y = 6478554
77 feet Y = 1911996
99 meter
Z = 10727080
00 Z = 3242390
57
XDOT = 2249
621252 XDOT = 729
436899
YDOT = -19642
352966 feet/sec YDOT = -5979
077356 meter/sec
ZDOT = 15631
145488 ZDOT = 4767
809774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3985139
89 X = 1214670
64
Y = 19085372
54 feet Y = 5817221
55 meter
Z = 10614748
07 Z = 3235375
21
XDOT = -17790
890224 XDOT = -5422
663340
YDOT = -5028
806781 feet/sec YDOT = -1532
780307 meter/sec
ZDOT = 15645
834087 ZDOT = 4768
850230
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 12166
55752090
00016717 00000-0 10270-3 0 9017
2 25544 51
6347 135
5537 0010414 64
0252 296
1974 15
56396802 17603
Satellite: ISS
Catalog Number: 25544
Epoch time: 12166
55752090 = yrday
fracday
Element set: 901
Inclination: 51
6347 deg
RA of node: 135
5537 deg
Eccentricity:
0010414
Arg of perigee: 64
0252 deg
Mean anomaly: 296
1974 deg
Mean motion: 15
56396802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1760
Checksum: 304
Coasting Arc #3 (Orbit 1774)
---------------------------------------
Vector Time (GMT): 2012/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4765366
79 A = 6773038
73 meter
Y = 205063
05 meter E =
0021925
Z = -4829483
73 I = 51
88781
XDOT = -2889
166852 Wp = 69
66053
YDOT = 6605
310309 meter/sec RA = 129
87831 deg
ZDOT = -2572
377302 TA = 175
06600
MA = 175
04436
Ha = 221
234 n
mi
Hp = 207
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15634405
49 X = 4786180
30
Y = 672779
04 feet Y = 258469
35 meter
Z = -15844762
89 Z = -4806283
01
XDOT = -9478
893873 XDOT = -2950
317919
YDOT = 21670
965581 feet/sec YDOT = 6572
660282 meter/sec
ZDOT = -8439
558076 ZDOT = -2586
560526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2483438
21 X = 756951
97
Y = -15547969
84 feet Y = -4739021
21 meter
Z = -15749188
75 Z = -4800352
73
XDOT = 19303
317386 XDOT = 5883
651139
YDOT = 11685
052367 feet/sec YDOT = 3561
603961 meter/sec
ZDOT = -8498
592874 ZDOT = -2590
371108
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 12167
52065895
00016717 00000-0 10270-3 0 9026
2 25544 51
6350 130
7343 0010551 66
9621 293
2645 15
56380389 17754
Satellite: ISS
Catalog Number: 25544
Epoch time: 12167
52065895 = yrday
fracday
Element set: 902
Inclination: 51
6350 deg
RA of node: 130
7343 deg
Eccentricity:
0010551
Arg of perigee: 66
9621 deg
Mean anomaly: 293
2645 deg
Mean motion: 15
56380389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1775
Checksum: 314
Coasting Arc #4 (Orbit 1790)
---------------------------------------
Vector Time (GMT): 2012/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3322397
14 A = 6770690
41 meter
Y = -2528237
43 meter E =
0012856
Z = 5319798
08 I = 51
89962
XDOT = 4489
798438 Wp = 72
91784
YDOT = -6231
638275 meter/sec RA = 124
87388 deg
ZDOT = -153
564732 TA = 18
56118
MA = 18
51433
Ha = 221
297 n
mi
Hp = 207
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10900253
09 X = -3319721
52
Y = -8294742
22 feet Y = -2565376
36 meter
Z = 17453405
79 Z = 5303664
03
XDOT = 14730
309837 XDOT = 4559
894185
YDOT = -20445
007464 feet/sec YDOT = -6181
038619 meter/sec
ZDOT = -503
821299 ZDOT = -131
583981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9335896
20 X = -2845581
16
Y = 10137430
11 feet Y = 3089888
70 meter
Z = 17387155
96 Z = 5299605
14
XDOT = -18157
676962 XDOT = -5534
459938
YDOT = -15991
668621 feet/sec YDOT = -4874
260596 meter/sec
ZDOT = -412
672466 ZDOT = -125
782568
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 12168
54798692
00016717 00000-0 10270-3 0 9038
2 25544 51
6354 125
5951 0010490 70
2460 289
9824 15
56416442 17915
Satellite: ISS
Catalog Number: 25544
Epoch time: 12168
54798692 = yrday
fracday
Element set: 903
Inclination: 51
6354 deg
RA of node: 125
5951 deg
Eccentricity:
0010490
Arg of perigee: 70
2460 deg
Mean anomaly: 289
9824 deg
Mean motion: 15
56416442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1791
Checksum: 327
Coasting Arc #5 (Orbit 1805)
---------------------------------------
Vector Time (GMT): 2012/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1604683
93 A = 6773292
57 meter
Y = 4613926
04 meter E =
0020206
Z = -4709631
61 I = 51
92545
XDOT = -5296
270588 Wp = 91
97780
YDOT = 4740
083082 meter/sec RA = 119
87073 deg
ZDOT = 2849
044821 TA = 206
17661
MA = 206
27889
Ha = 221
175 n
mi
Hp = 207
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5264711
06 X = 1575849
25
Y = 15137552
62 feet Y = 4631710
14 meter
Z = -15451547
28 Z = -4701905
38
XDOT = -17376
215840 XDOT = -5362
721624
YDOT = 15551
453681 feet/sec YDOT = 4680
484901 meter/sec
ZDOT = 9347
259913 ZDOT = 2823
154980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15521778
16 X = 4731037
98
Y = -4111772
91 feet Y = -1253268
38 meter
Z = -15420140
13 Z = -4700058
71
XDOT = 13784
981226 XDOT = 4201
662278
YDOT = 17506
534305 feet/sec YDOT = 5335
991656 meter/sec
ZDOT = 9240
121139 ZDOT = 2816
388923
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 12169
51109022
00016717 00000-0 10270-3 0 9040
2 25544 51
6357 120
7764 0010452 73
6358 286
5944 15
56427831 18065
Satellite: ISS
Catalog Number: 25544
Epoch time: 12169
51109022 = yrday
fracday
Element set: 904
Inclination: 51
6357 deg
RA of node: 120
7764 deg
Eccentricity:
0010452
Arg of perigee: 73
6358 deg
Mean anomaly: 286
5944 deg
Mean motion: 15
56427831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1806
Checksum: 309
Coasting Arc #6 (Orbit 1821)
---------------------------------------
Vector Time (GMT): 2012/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 197178
06 A = 6778617
62 meter
Y = -6052669
01 meter E =
0023246
Z = 3026634
43 I = 51
95894
XDOT = 5367
979648 Wp = 88
04096
YDOT = -2327
934626 meter/sec RA = 114
88581 deg
ZDOT = -4971
538368 TA = 57
37291
MA = 57
14878
Ha = 221
123 n
mi
Hp = 207
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 646909
66 X = 250142
85
Y = -19857837
97 feet Y = -6050168
42 meter
Z = 9929902
99 Z = 3027719
95
XDOT = 17611
481784 XDOT = 5417
762795
YDOT = -7637
580793 feet/sec YDOT = -2267
627361 meter/sec
ZDOT = -16310
821418 ZDOT = -4945
340364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19778842
63 X = -6028591
23
Y = -1857214
41 feet Y = -566078
95 meter
Z = 9934955
13 Z = 3028174
32
XDOT = -6623
811887 XDOT = -2018
937863
YDOT = -16721
285980 feet/sec YDOT = -5096
647967 meter/sec
ZDOT = -16202
623861 ZDOT = -4938
559753
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 12170
53838279
00016717 00000-0 10270-3 0 9058
2 25544 51
6367 115
6364 0010461 77
2508 282
9815 15
56475527 18222
Satellite: ISS
Catalog Number: 25544
Epoch time: 12170
53838279 = yrday
fracday
Element set: 905
Inclination: 51
6367 deg
RA of node: 115
6364 deg
Eccentricity:
0010461
Arg of perigee: 77
2508 deg
Mean anomaly: 282
9815 deg
Mean motion: 15
56475527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1822
Checksum: 324
Coasting Arc #7 (Orbit 1836)
---------------------------------------
Vector Time (GMT): 2012/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1742813
74 A = 6782225
68 meter
Y = 6507447
34 meter E =
0019508
Z = -740378
50 I = 51
98319
XDOT = -4758
208840 Wp = 60
49557
YDOT = -607
639923 meter/sec RA = 109
92170 deg
ZDOT = 5987
169568 TA = 291
53393
MA = 291
74176
Ha = 221
080 n
mi
Hp = 207
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5717892
85 X = -1811855
23
Y = 21349892
83 feet Y = 6487572
21 meter
Z = -2429063
32 Z = -749011
58
XDOT = -15610
921392 XDOT = -4780
144730
YDOT = -1993
569302 feet/sec YDOT = -660
972841 meter/sec
ZDOT = 19642
944777 ZDOT = 5964
001035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21058865
33 X = 6418742
15
Y = 6697698
06 feet Y = 2041458
37 meter
Z = -2465279
50 Z = -751417
19
XDOT = -2239
233654 XDOT = -682
518418
YDOT = 14084
079256 feet/sec YDOT = 4292
827357 meter/sec
ZDOT = 19547
504485 ZDOT = 5958
079367
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 12171
50145276
00016717 00000-0 10270-3 0 9065
2 25544 51
6368 110
8183 0010400 80
8641 279
3689 15
56491265 18372
Satellite: ISS
Catalog Number: 25544
Epoch time: 12171
50145276 = yrday
fracday
Element set: 906
Inclination: 51
6368 deg
RA of node: 110
8183 deg
Eccentricity:
0010400
Arg of perigee: 80
8641 deg
Mean anomaly: 279
3689 deg
Mean motion: 15
56491265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1837
Checksum: 311
Coasting Arc #8 (Orbit 1852)
---------------------------------------
Vector Time (GMT): 2012/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3000935
85 A = 6781030
04 meter
Y = -5811917
02 meter E =
0015721
Z = -1789370
45 I = 51
99024
XDOT = 3639
979982 Wp = 108
09972
YDOT = 3618
770074 meter/sec RA = 104
96365 deg
ZDOT = -5694
939267 TA = 91
46667
MA = 91
28657
Ha = 221
047 n
mi
Hp = 207
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9845590
06 X = 3074395
18
Y = -19067969
21 feet Y = -5777947
66 meter
Z = -5870637
95 Z = -1774614
64
XDOT = 11942
191542 XDOT = 3626
908225
YDOT = 11872
605231 feet/sec YDOT = 3659
402454 meter/sec
ZDOT = -18684
183948 ZDOT = -5677
287626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18766501
73 X = -5720029
73
Y = -10443114
70 feet Y = -3183061
36 meter
Z = -5809238
47 Z = -1770655
88
XDOT = 11462
650852 XDOT = 3493
815980
YDOT = -10329
596247 feet/sec YDOT = -3148
460936 meter/sec
ZDOT = -18611
773293 ZDOT = -5672
868500
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 12172
52870962
00016717 00000-0 10270-3 0 9076
2 25544 51
6380 105
6780 0010374 84
5893 275
6444 15
56525436 18535
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
52870962 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 105
6780 deg
Eccentricity:
0010374
Arg of perigee: 84
5893 deg
Mean anomaly: 275
6444 deg
Mean motion: 15
56525436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1853
Checksum: 325
Coasting Arc #9 (Orbit 1853)
---------------------------------------
Vector Time (GMT): 2012/172/13:54:15
871
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3504485
08 A = 6773446
12 meter
Y = 2634890
55 meter E =
0020533
Z = -5180929
71 I = 51
95883
XDOT = -2988
212723 Wp = 95
75353
YDOT = 6889
985570 meter/sec RA = 104
54120 deg
ZDOT = 1485
834666 TA = 188
49564
MA = 188
53045
Ha = 221
044 n
mi
Hp = 209
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11497654
47 X = 3499928
40
Y = 8644654
02 feet Y = 2674055
26 meter
Z = -16997800
89 Z = -5163915
78
XDOT = -9803
847516 XDOT = -3072
253673
YDOT = 22604
939535 feet/sec YDOT = 6856
099377 meter/sec
ZDOT = 4874
785648 ZDOT = 1471
115150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2448949
14 X = 746439
70
Y = -14258311
01 feet Y = -4345933
20 meter
Z = -16927922
26 Z = -5159630
70
XDOT = 23567
455218 XDOT = 7183
360350
YDOT = -1654
883425 feet/sec YDOT = -504
408468 meter/sec
ZDOT = 4813
428728 ZDOT = 1467
133076
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 12172
59291434
00016717 00000-0 10270-3 0 9085
2 25544 51
6392 105
3577 0006956 84
7167 275
4780 15
55718991 18547
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
59291434 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 105
3577 deg
Eccentricity:
0006956
Arg of perigee: 84
7167 deg
Mean anomaly: 275
4780 deg
Mean motion: 15
55718991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1854
Checksum: 346
Coasting Arc #10 (Orbit 1869)
---------------------------------------
Vector Time (GMT): 2012/173/13:54:15
871
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2504768
39 A = 6777304
86 meter
Y = -4716367
60 meter E =
0017231
Z = 4160268
02 I = 51
97856
XDOT = 3908
274303 Wp = 80
74743
YDOT = -5422
315547 meter/sec RA = 99
55441 deg
ZDOT = -3778
086849 TA = 47
98106
MA = 47
83450
Ha = 221
066 n
mi
Hp = 209
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8217744
08 X = -2472052
33
Y = -15473646
97 feet Y = -4744195
19 meter
Z = 13649173
28 Z = 4148178
78
XDOT = 12822
422255 XDOT = 3986
970224
YDOT = -17789
749169 feet/sec YDOT = -5378
170200 meter/sec
ZDOT = -12395
298061 ZDOT = -3758
910466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9782901
63 X = -2981828
42
Y = 14580989
02 feet Y = 4444285
45 meter
Z = 13599801
27 Z = 4145219
43
XDOT = -20696
185818 XDOT = -6308
197437
YDOT = -2349
794972 feet/sec YDOT = -716
217507 meter/sec
ZDOT = -12315
700015 ZDOT = -3753
825365
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 12173
62068741
00016717 00000-0 10270-3 0 9094
2 25544 51
6390 100
2214 0006955 88
1790 272
0160 15
55749950 18708
Satellite: ISS
Catalog Number: 25544
Epoch time: 12173
62068741 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 100
2214 deg
Eccentricity:
0006955
Arg of perigee: 88
1790 deg
Mean anomaly: 272
0160 deg
Mean motion: 15
55749950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1870
Checksum: 306
Coasting Arc #11 (Orbit 1884)
---------------------------------------
Vector Time (GMT): 2012/174/13:54:15
871
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1416461
41 A = 6782016
96 meter
Y = 6169396
51 meter E =
0011454
Z = -2438261
72 I = 51
99946
XDOT = -4467
315700 Wp = 72
31007
YDOT = 3141
682106 meter/sec RA = 94
58422 deg
ZDOT = 5378
117252 TA = 260
55073
MA = 260
68022
Ha = 220
927 n
mi
Hp = 209
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4647183
11 X = 1359213
09
Y = 20240802
20 feet Y = 6184916
51 meter
Z = -7999546
32 Z = -2431518
87
XDOT = -14656
547572 XDOT = -4528
240041
YDOT = 10307
355992 feet/sec YDOT = 3091
384419 meter/sec
ZDOT = 17644
741639 ZDOT = 5356
267889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15446853
46 X = 4708200
94
Y = -13896591
61 feet Y = -4235681
12 meter
Z = -7972363
87 Z = -2429976
51
XDOT = 15148
420066 XDOT = 4617
238436
YDOT = 6813
056685 feet/sec YDOT = 2076
619678 meter/sec
ZDOT = 17554
340886 ZDOT = 5350
563102
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 12174
58420821
00016717 00000-0 10270-3 0 9103
2 25544 51
6397 95
4058 0006863 91
9519 268
2421 15
55780451 18859
Satellite: ISS
Catalog Number: 25544
Epoch time: 12174
58420821 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 95
4058 deg
Eccentricity:
0006863
Arg of perigee: 91
9519 deg
Mean anomaly: 268
2421 deg
Mean motion: 15
55780451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1885
Checksum: 326
Coasting Arc #12 (Orbit 1900)
---------------------------------------
Vector Time (GMT): 2012/175/13:54:15
871
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -212710
05 A = 6784576
83 meter
Y = -6771047
67 meter E =
0018502
Z = 216134
49 I = 52
00909
XDOT = 4716
367103 Wp = 120
07641
YDOT = -352
995274 meter/sec RA = 89
62854 deg
ZDOT = -6041
452636 TA = 57
60466
MA = 57
42577
Ha = 220
938 n
mi
Hp = 209
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -697867
63 X = -138028
92
Y = -22214723
32 feet Y = -6773008
79 meter
Z = 709102
65 Z = 215281
74
XDOT = 15473
645350 XDOT = 4749
311559
YDOT = -1158
120977 feet/sec YDOT = -300
069005 meter/sec
ZDOT = -19821
038831 ZDOT = -6018
460980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18907915
90 X = -5763132
77
Y = 11682280
41 feet Y = 3560759
07 meter
Z = 706271
08 Z = 215271
43
XDOT = -7926
621421 XDOT = -2416
034209
YDOT = -11561
973373 feet/sec YDOT = -3524
089484 meter/sec
ZDOT = -19726
202498 ZDOT = -6012
546521
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 12175
61194782
00016717 00000-0 10270-3 0 9113
2 25544 51
6396 90
2689 0006823 97
0441 263
1489 15
55758716 19014
Satellite: ISS
Catalog Number: 25544
Epoch time: 12175
61194782 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 90
2689 deg
Eccentricity:
0006823
Arg of perigee: 97
0441 deg
Mean anomaly: 263
1489 deg
Mean motion: 15
55758716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1901
Checksum: 331
Coasting Arc #13 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2012/176/13:54:15
871
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -966835
28 A = 6782768
90 meter
Y = 6402755
11 meter E =
0020048
Z = 1993057
10 I = 52
00215
XDOT = -4628
374235 Wp = 77
81181
YDOT = -2457
682695 meter/sec RA = 84
67358 deg
ZDOT = 5606
889134 TA = 304
10745
MA = 304
29751
Ha = 220
820 n
mi
Hp = 209
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3172031
74 X = -1048042
07
Y = 21006414
40 feet Y = 6391489
10 meter
Z = 6538901
24 Z = 1988163
71
XDOT = -15184
954840 XDOT = -4627
784701
YDOT = -8063
263434 feet/sec YDOT = -2509
437325 meter/sec
ZDOT = 18395
305559 ZDOT = 5584
406068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19676746
22 X = 5997472
25
Y = -8026759
78 feet Y = -2446556
38 meter
Z = 6518070
76 Z = 1986707
97
XDOT = 347
974554 XDOT = 106
062644
YDOT = 15831
329915 feet/sec YDOT = 4825
389358 meter/sec
ZDOT = 18302
849353 ZDOT = 5578
708483
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 12176
63966835
00016717 00000-0 10270-3 0 9123
2 25544 51
6394 85
1317 0006715 98
6007 261
5908 15
55812044 19178
Satellite: ISS
Catalog Number: 25544
Epoch time: 12176
63966835 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 85
1317 deg
Eccentricity:
0006715
Arg of perigee: 98
6007 deg
Mean anomaly: 261
5908 deg
Mean motion: 15
55812044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 325
Coasting Arc #14 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2012/177/13:54:15
871
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2173205
74 A = 6777963
34 meter
Y = -5106470
45 meter E =
0012534
Z = -3902266
32 I = 51
98225
XDOT = 4174
219416 Wp = 88
74480
YDOT = 4922
643214 meter/sec RA = 79
70619 deg
ZDOT = -4128
216404 TA = 138
15045
MA = 138
05456
Ha = 220
692 n
mi
Hp = 209
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7129940
10 X = 2249102
04
Y = -16753511
99 feet Y = -5081743
61 meter
Z = -12802711
01 Z = -3891525
15
XDOT = 13694
945589 XDOT = 4138
917003
YDOT = 16150
404246 feet/sec YDOT = 4969
124912 meter/sec
ZDOT = -13544
017074 ZDOT = -4108
023646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18034291
08 X = -5496851
92
Y = 2725089
60 feet Y = 830607
31 meter
Z = -12757893
67 Z = -3888605
99
XDOT = 6639
105794 XDOT = 2023
599446
YDOT = -18912
211146 feet/sec YDOT = -5764
441957 meter/sec
ZDOT = -13461
259967 ZDOT = -4102
992038
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 12177
60314026
00016717 00000-0 10270-3 0 9131
2 25544 51
6391 80
3155 0006505 103
1994 256
9885 15
55832736 19325
Satellite: ISS
Catalog Number: 25544
Epoch time: 12177
60314026 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 80
3155 deg
Eccentricity:
0006505
Arg of perigee: 103
1994 deg
Mean anomaly: 256
9885 deg
Mean motion: 15
55832736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 310
Coasting Arc #15 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2012/178/13:54:15
871
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3247365
27 A = 6773501
23 meter
Y = 3116628
36 meter E =
0012144
Z = 5053697
17 I = 51
96122
XDOT = -3365
836047 Wp = 114
32718
YDOT = -6629
334083 meter/sec RA = 74
72057 deg
ZDOT = 1917
050303 TA = 317
14295
MA = 317
23753
Ha = 220
781 n
mi
Hp = 209
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10654085
52 X = -3306524
36
Y = 10225158
67 feet Y = 3079983
09 meter
Z = 16580371
29 Z = 5037778
22
XDOT = -11042
769183 XDOT = -3300
767899
YDOT = -21749
783737 feet/sec YDOT = -6666
609301 meter/sec
ZDOT = 6289
535116 ZDOT = 1900
856716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14425349
33 X = 4396846
48
Y = 3486528
52 feet Y = 1062693
89 meter
Z = 16514403
88 Z = 5033590
30
XDOT = -12004
198838 XDOT = -3658
879806
YDOT = 20056
221945 feet/sec YDOT = 6113
136449 meter/sec
ZDOT = 6223
453029 ZDOT = 1896
908483
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 12178
63082823
00016717 00000-0 10270-3 0 9143
2 25544 51
6392 75
1782 0006643 106
2968 253
8917 15
55860202 19480
Satellite: ISS
Catalog Number: 25544
Epoch time: 12178
63082823 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 75
1782 deg
Eccentricity:
0006643
Arg of perigee: 106
2968 deg
Mean anomaly: 253
8917 deg
Mean motion: 15
55860202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1948
Checksum: 327
Coasting Arc #16 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2012/179/13:54:15
871
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4162412
76 A = 6772334
75 meter
Y = -728008
81 meter E =
0020950
Z = -5310452
96 I = 51
94799
XDOT = 2141
663862 Wp = 99
64558
YDOT = 7319
174267 meter/sec RA = 69
72233 deg
ZDOT = 674
131152 TA = 176
78156
MA = 176
76806
Ha = 220
502 n
mi
Hp = 209
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13656209
83 X = 4196041
17
Y = -2388480
34 feet Y = -681273
59 meter
Z = -17422745
92 Z = -5290150
48
XDOT = 7026
456239 XDOT = 2056
385399
YDOT = 24013
038933 feet/sec YDOT = 7342
646797 meter/sec
ZDOT = 2211
716377 ZDOT = 684
328843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9648990
24 X = -2941012
22
Y = -10099838
76 feet Y = -3078430
85 meter
Z = -17338951
09 Z = -5284912
29
XDOT = 15302
849849 XDOT = 4664
308634
YDOT = -18494
102304 feet/sec YDOT = -5637
002382 meter/sec
ZDOT = 2252
990129 ZDOT = 686
711391
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 12179
59426849
00016717 00000-0 10270-3 0 9150
2 25544 51
6385 70
3608 0006454 110
0443 250
1406 15
55910808 19635
Satellite: ISS
Catalog Number: 25544
Epoch time: 12179
59426849 = yrday
fracday
Element set: 915
Inclination: 51
6385 deg
RA of node: 70
3608 deg
Eccentricity:
0006454
Arg of perigee: 110
0443 deg
Mean anomaly: 250
1406 deg
Mean motion: 15
55910808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 309
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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