[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 14th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 ET - UTC (sec) : 67 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
258/03:09:28
008 -2
3 4
1 4
2
N/A 0
7 -0
6 234
3
000/00:08:56
016 3
4 -0
1 215
4
Coasting Arc #1 (Orbit 3168)
---------------------------------------
Vector Time (GMT): 2012/257/02:36:50
518
Vector Time (MET): N/A
Weight (LBS) : 922601
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -872192
81 A = 6789275
72 meter
Y = 4539008
93 meter E =
0019419
Z = 4955309
70 I = 51
87475
XDOT = -6373
095786 Wp = 78
90239
YDOT = -3656
770780 meter/sec RA = 43
58893 deg
ZDOT = 2224
102483 TA = 349
46766
MA = 349
50828
Ha = 232
177 n
mi
Hp = 214
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2861524
98 X = -946955
70
Y = 14891761
58 feet Y = 4528837
96 meter
Z = 16257577
74 Z = 4950890
64
XDOT = -20909
106909 XDOT = -6342
535447
YDOT = -11997
279463 feet/sec YDOT = -3727
867633 meter/sec
ZDOT = 7296
924158 ZDOT = 2193
217115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5107430
08 X = 1556744
69
Y = 14299532
34 feet Y = 4358497
46 meter
Z = 16238819
38 Z = 4949592
15
XDOT = -23097
485078 XDOT = -7040
113452
YDOT = 94
078162 feet/sec YDOT = 28
675024 meter/sec
ZDOT = 7169
556591 ZDOT = 2185
280849
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 12257
16111426
00016717 00000-0 10270-3 0 9006
2 25544 51
6454 43
9175 0015421 63
0423 297
2301 15
50576629 31696
Satellite: ISS
Catalog Number: 25544
Epoch time: 12257
16111426 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 43
9175 deg
Eccentricity:
0015421
Arg of perigee: 63
0423 deg
Mean anomaly: 297
2301 deg
Mean motion: 15
50576629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3169
Checksum: 286
Coasting Arc #2 (Orbit 3183)
---------------------------------------
Vector Time (GMT): 2012/258/02:36:50
518
Vector Time (MET): N/A
Weight (LBS) : 922601
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1064459
76 A = 6788599
88 meter
Y = -4326257
51 meter E =
0028939
Z = -5148037
96 I = 51
85030
XDOT = 6547
586229 Wp = 71
21080
YDOT = 3575
700794 meter/sec RA = 38
64173 deg
ZDOT = -1649
611834 TA = 182
84599
MA = 182
86249
Ha = 232
214 n
mi
Hp = 214
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3492322
04 X = 1137765
59
Y = -14193758
22 feet Y = -4313944
77 meter
Z = -16889888
33 Z = -5142688
35
XDOT = 21481
582117 XDOT = 6515
128754
YDOT = 11731
301816 feet/sec YDOT = 3648
738318 meter/sec
ZDOT = -5412
112315 ZDOT = -1617
883432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4445069
77 X = -1354857
27
Y = -13952163
48 feet Y = -4252619
43 meter
Z = -16867302
76 Z = -5141153
88
XDOT = 23447
069629 XDOT = 7146
666823
YDOT = -1079
592605 feet/sec YDOT = -329
059826 meter/sec
ZDOT = -5281
254676 ZDOT = -1609
726425
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 12258
12787163
00016717 00000-0 10270-3 0 9011
2 25544 51
6460 39
1233 0015598 66
2309 294
0476 15
50573325 31843
Satellite: ISS
Catalog Number: 25544
Epoch time: 12258
12787163 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 39
1233 deg
Eccentricity:
0015598
Arg of perigee: 66
2309 deg
Mean anomaly: 294
0476 deg
Mean motion: 15
50573325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3184
Checksum: 308
Coasting Arc #3 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2012/258/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2596041
92 A = 6797495
67 meter
Y = 5344381
65 meter E =
0029798
Z = 3266762
98 I = 51
87279
XDOT = -6016
860666 Wp = 70
20263
YDOT = -7
201739 meter/sec RA = 38
52681 deg
ZDOT = 4767
879233 TA = 327
56584
MA = 327
74863
Ha = 234
323 n
mi
Hp = 215
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8517197
91 X = 2520217
91
Y = 17534060
53 feet Y = 5372988
63 meter
Z = 10717726
30 Z = 3279189
55
XDOT = -19740
356515 XDOT = -6039
494067
YDOT = -23
627752 feet/sec YDOT = -74
612030 meter/sec
ZDOT = 15642
648403 ZDOT = 4738
594831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17906835
22 X = 5458003
38
Y = 7631446
54 feet Y = 2326064
91 meter
Z = 10768559
42 Z = 3282256
91
XDOT = -14386
716015 XDOT = -4385
071041
YDOT = 11738
657057 feet/sec YDOT = 3577
942671 meter/sec
ZDOT = 15521
521804 ZDOT = 4730
959846
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 12258
19235573
00016717 00000-0 10270-3 0 9022
2 25544 51
6472 38
8049 0018115 58
8365 301
4559 15
49763105 31855
Satellite: ISS
Catalog Number: 25544
Epoch time: 12258
19235573 = yrday
fracday
Element set: 902
Inclination: 51
6472 deg
RA of node: 38
8049 deg
Eccentricity:
0018115
Arg of perigee: 58
8365 deg
Mean anomaly: 301
4559 deg
Mean motion: 15
49763105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 321
Coasting Arc #4 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2012/259/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2759649
38 A = 6796709
34 meter
Y = -5142873
06 meter E =
0022851
Z = -3510070
68 I = 51
84738
XDOT = 6142
028626 Wp = 66
77152
YDOT = -205
238734 meter/sec RA = 33
58870 deg
ZDOT = -4542
997848 TA = 154
17766
MA = 154
06342
Ha = 234
304 n
mi
Hp = 215
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9053967
80 X = -2684884
53
Y = -16872943
10 feet Y = -5173315
60 meter
Z = -11515979
92 Z = -3523294
61
XDOT = 20151
012554 XDOT = 6165
935940
YDOT = -673
355427 feet/sec YDOT = -136
421658 meter/sec
ZDOT = -14904
848583 ZDOT = -4513
102165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17985862
89 X = -5482091
01
Y = -6475277
33 feet Y = -1973664
53 meter
Z = -11570127
70 Z = -3526574
92
XDOT = 14077
566939 XDOT = 4290
842403
YDOT = -12777
195685 feet/sec YDOT = -3894
489245 meter/sec
ZDOT = -14781
177333 ZDOT = -4505
302851
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 12259
15959385
00016717 00000-0 10270-3 0 9034
2 25544 51
6483 34
0143 0018085 62
0863 298
2117 15
49801108 32003
Satellite: ISS
Catalog Number: 25544
Epoch time: 12259
15959385 = yrday
fracday
Element set: 903
Inclination: 51
6483 deg
RA of node: 34
0143 deg
Eccentricity:
0018085
Arg of perigee: 62
0863 deg
Mean anomaly: 298
2117 deg
Mean motion: 15
49801108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 301
Coasting Arc #5 (Orbit 3215)
---------------------------------------
Vector Time (GMT): 2012/260/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2921819
40 A = 6796154
80 meter
Y = 4890205
35 meter E =
0028920
Z = 3675980
91 I = 51
81978
XDOT = -6299
537363 Wp = 76
71385
YDOT = 467
645347 meter/sec RA = 28
64914 deg
ZDOT = 4362
705898 TA = 326
89790
MA = 327
07856
Ha = 234
321 n
mi
Hp = 215
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9586021
66 X = 2849061
84
Y = 16043980
82 feet Y = 4922472
65 meter
Z = 12060304
83 Z = 3689997
60
XDOT = -20667
773502 XDOT = -6325
491540
YDOT = 1534
269510 feet/sec YDOT = 397
055464 meter/sec
ZDOT = 14313
339560 ZDOT = 4332
039895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17913309
72 X = 5459976
80
Y = 5198606
46 feet Y = 1584535
25 meter
Z = 12117751
85 Z = 3693490
76
XDOT = -13711
671586 XDOT = -4179
317499
YDOT = 14009
657767 feet/sec YDOT = 4270
143687 meter/sec
ZDOT = 14186
462069 ZDOT = 4324
033639
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 12260
19130242
00016717 00000-0 10270-3 0 9044
2 25544 51
6484 28
9048 0018133 65
7585 294
5458 15
49804800 32161
Satellite: ISS
Catalog Number: 25544
Epoch time: 12260
19130242 = yrday
fracday
Element set: 904
Inclination: 51
6484 deg
RA of node: 28
9048 deg
Eccentricity:
0018133
Arg of perigee: 65
7585 deg
Mean anomaly: 294
5458 deg
Mean motion: 15
49804800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3216
Checksum: 309
Coasting Arc #6 (Orbit 3230)
---------------------------------------
Vector Time (GMT): 2012/261/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3020695
48 A = 6795350
56 meter
Y = -4687731
52 meter E =
0024529
Z = -3909768
18 I = 51
79133
XDOT = 6406
018600 Wp = 69
77099
YDOT = -715
450850 meter/sec RA = 23
70710 deg
ZDOT = -4104
193541 TA = 157
16396
MA = 157
05469
Ha = 234
282 n
mi
Hp = 214
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9910418
25 X = -2949058
90
Y = -15379696
58 feet Y = -4721110
78 meter
Z = -12827323
44 Z = -3924268
06
XDOT = 21017
121390 XDOT = 6433
480176
YDOT = -2347
279690 feet/sec YDOT = -643
661740 meter/sec
ZDOT = -13465
201907 ZDOT = -4073
006413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17766912
52 X = -5415354
94
Y = -4190386
78 feet Y = -1277229
89 meter
Z = -12886782
43 Z = -3927891
28
XDOT = 13200
457899 XDOT = 4023
499568
YDOT = -15083
522771 feet/sec YDOT = -4597
457740 meter/sec
ZDOT = -13336
150700 ZDOT = -4064
858733
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 12261
15851524
00016717 00000-0 10270-3 0 9055
2 25544 51
6493 24
1144 0018022 68
9118 291
3957 15
49838033 32311
Satellite: ISS
Catalog Number: 25544
Epoch time: 12261
15851524 = yrday
fracday
Element set: 905
Inclination: 51
6493 deg
RA of node: 24
1144 deg
Eccentricity:
0018022
Arg of perigee: 68
9118 deg
Mean anomaly: 291
3957 deg
Mean motion: 15
49838033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3231
Checksum: 300
Coasting Arc #7 (Orbit 3246)
---------------------------------------
Vector Time (GMT): 2012/262/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3116284
20 A = 6794747
72 meter
Y = 4441189
34 meter E =
0027766
Z = 4064359
28 I = 51
76129
XDOT = -6541
399061 Wp = 83
08378
YDOT = 1013
784059 meter/sec RA = 18
76329 deg
ZDOT = 3888
251389 TA = 326
67545
MA = 326
84995
Ha = 234
293 n
mi
Hp = 214
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10224029
53 X = 3046646
35
Y = 14570831
18 feet Y = 4475648
68 meter
Z = 13334512
07 Z = 4079328
54
XDOT = -21461
283010 XDOT = -6571
137667
YDOT = 3326
063185 feet/sec YDOT = 940
468222 meter/sec
ZDOT = 12756
730279 ZDOT = 3856
400906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17482241
25 X = 5328587
13
Y = 3093446
60 feet Y = 942882
52 meter
Z = 13395930
06 Z = 4083079
48
XDOT = -12613
413222 XDOT = -3844
568350
YDOT = 16336
406363 feet/sec YDOT = 4979
336660 meter/sec
ZDOT = 12624
910642 ZDOT = 3848
072764
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 12262
19019678
00016717 00000-0 10270-3 0 9067
2 25544 51
6494 19
0050 0018126 72
5852 287
7278 15
49845520 32473
Satellite: ISS
Catalog Number: 25544
Epoch time: 12262
19019678 = yrday
fracday
Element set: 906
Inclination: 51
6494 deg
RA of node: 19
0050 deg
Eccentricity:
0018126
Arg of perigee: 72
5852 deg
Mean anomaly: 287
7278 deg
Mean motion: 15
49845520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3247
Checksum: 324
Coasting Arc #8 (Orbit 3261)
---------------------------------------
Vector Time (GMT): 2012/263/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3152698
75 A = 6793953
14 meter
Y = -4254772
52 meter E =
0026253
Z = -4282873
74 I = 51
73015
XDOT = 6616
399268 Wp = 73
32081
YDOT = -1294
097085 meter/sec RA = 13
81658 deg
ZDOT = -3595
830224 TA = 159
90221
MA = 159
79864
Ha = 234
233 n
mi
Hp = 214
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10343499
84 X = -3084081
20
Y = -13959227
42 feet Y = -4289644
70 meter
Z = -14051423
02 Z = -4298022
51
XDOT = 21707
346681 XDOT = 6647
846321
YDOT = -4245
725343 feet/sec YDOT = -1219
932887 meter/sec
ZDOT = -11797
343254 ZDOT = -3563
611172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17171895
35 X = -5233993
70
Y = -2285375
57 feet Y = -696582
47 meter
Z = -14113595
45 Z = -4301823
89
XDOT = 11871
252811 XDOT = 3618
357857
YDOT = -17387
895397 feet/sec YDOT = -5299
830517 meter/sec
ZDOT = -11663
973895 ZDOT = -3555
179243
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 12263
15738382
00016717 00000-0 10270-3 0 9075
2 25544 51
6496 14
2145 0017937 75
7164 284
5977 15
49876161 32620
Satellite: ISS
Catalog Number: 25544
Epoch time: 12263
15738382 = yrday
fracday
Element set: 907
Inclination: 51
6496 deg
RA of node: 14
2145 deg
Eccentricity:
0017937
Arg of perigee: 75
7164 deg
Mean anomaly: 284
5977 deg
Mean motion: 15
49876161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3262
Checksum: 339
Coasting Arc #9 (Orbit 3277)
---------------------------------------
Vector Time (GMT): 2012/264/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3185757
27 A = 6793341
34 meter
Y = 4031098
91 meter E =
0026375
Z = 4421144
18 I = 51
69842
XDOT = -6717
432947 Wp = 89
20256
YDOT = 1624
010158 meter/sec RA = 8
86789 deg
ZDOT = 3342
801642 TA = 327
01412
MA = 327
17839
Ha = 234
243 n
mi
Hp = 214
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10451959
54 X = 3118966
74
Y = 13225390
12 feet Y = 4066350
90 meter
Z = 14505066
21 Z = 4436458
10
XDOT = -22038
822006 XDOT = -6751
332471
YDOT = 5328
117316 feet/sec YDOT = 1548
702330 meter/sec
ZDOT = 10967
196989 ZDOT = 3310
085826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16743080
14 X = 5103290
83
Y = 1412711
41 feet Y = 430594
44 meter
Z = 14567939
52 Z = 4440307
97
XDOT = -11041
826606 XDOT = -3365
548750
YDOT = 18599
363079 feet/sec YDOT = 5669
085867 meter/sec
ZDOT = 10831
739637 ZDOT = 3301
514241
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 12264
18903798
00016717 00000-0 10270-3 0 9085
2 25544 51
6495 9
1049 0018089 79
3837 280
9350 15
49883603 32782
Satellite: ISS
Catalog Number: 25544
Epoch time: 12264
18903798 = yrday
fracday
Element set: 908
Inclination: 51
6495 deg
RA of node: 9
1049 deg
Eccentricity:
0018089
Arg of perigee: 79
3837 deg
Mean anomaly: 280
9350 deg
Mean motion: 15
49883603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3278
Checksum: 351
Coasting Arc #10 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2012/265/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3166598
57 A = 6792585
01 meter
Y = -3876970
77 meter E =
0027958
Z = -4618113
32 I = 51
66555
XDOT = 6748
590830 Wp = 77
53943
YDOT = -1929
473086 meter/sec RA = 3
91570 deg
ZDOT = -3017
241721 TA = 162
27948
MA = 162
18178
Ha = 234
168 n
mi
Hp = 214
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10389102
92 X = -3100576
17
Y = -12719720
36 feet Y = -3912012
74 meter
Z = -15151290
43 Z = -4633336
08
XDOT = 22141
046031 XDOT = 6784
322238
YDOT = -6330
292277 feet/sec YDOT = -1853
806513 meter/sec
ZDOT = -9899
087012 ZDOT = -2984
370180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16344021
05 X = -4981657
62
Y = -836436
84 feet Y = -254945
95 meter
Z = -15213799
54 Z = -4637166
10
XDOT = 10059
498733 XDOT = 3066
135214
YDOT = -19557
894031 feet/sec YDOT = -5961
246101 meter/sec
ZDOT = -9762
952342 ZDOT = -2975
747874
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 12265
15619887
00016717 00000-0 10270-3 0 9097
2 25544 51
6489 4
3138 0017858 82
5927 277
7252 15
49915905 32933
Satellite: ISS
Catalog Number: 25544
Epoch time: 12265
15619887 = yrday
fracday
Element set: 909
Inclination: 51
6489 deg
RA of node: 4
3138 deg
Eccentricity:
0017858
Arg of perigee: 82
5927 deg
Mean anomaly: 277
7252 deg
Mean motion: 15
49915905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 354
Coasting Arc #11 (Orbit 3308)
---------------------------------------
Vector Time (GMT): 2012/266/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3145751
36 A = 6792012
28 meter
Y = 3691526
21 meter E =
0024817
Z = 4734349
27 I = 51
63331
XDOT = -6803
709691 Wp = 94
92893
YDOT = 2282
286888 meter/sec RA = 358
96177 deg
ZDOT = 2726
771107 TA = 328
05839
MA = 328
20860
Ha = 234
170 n
mi
Hp = 214
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10320706
57 X = 3081239
62
Y = 12111306
46 feet Y = 3726343
47 meter
Z = 15532641
96 Z = 4749474
40
XDOT = -22321
882188 XDOT = -6841
971137
YDOT = 7487
817873 feet/sec YDOT = 2205
989756 meter/sec
ZDOT = 8946
099434 ZDOT = 2693
625777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15850011
05 X = 4831083
37
Y = 210030
94 feet Y = 64017
43 meter
Z = 15594766
15 Z = 4753284
72
XDOT = -8986
942168 XDOT = -2739
219973
YDOT = 20655
458753 feet/sec YDOT = 6295
783828 meter/sec
ZDOT = 8808
793040 ZDOT = 2684
920119
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 12266
18782546
00016717 00000-0 10270-3 0 9106
2 25544 51
6489 359
2038 0018019 86
2523 274
0688 15
49919426 33090
Satellite: ISS
Catalog Number: 25544
Epoch time: 12266
18782546 = yrday
fracday
Element set: 910
Inclination: 51
6489 deg
RA of node: 359
2038 deg
Eccentricity:
0018019
Arg of perigee: 86
2523 deg
Mean anomaly: 274
0688 deg
Mean motion: 15
49919426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 340
Coasting Arc #12 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2012/267/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3082464
71 A = 6791332
61 meter
Y = -3583723
54 meter E =
0029536
Z = -4903066
22 I = 51
60007
XDOT = 6780
590241 Wp = 82
48253
YDOT = -2601
106629 meter/sec RA = 354
00393 deg
ZDOT = -2370
177094 TA = 164
24193
MA = 164
14982
Ha = 234
095 n
mi
Hp = 214
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10113073
20 X = -3018343
65
Y = -11757623
15 feet Y = -3617835
29 meter
Z = -16086175
25 Z = -4917884
79
XDOT = 22246
030973 XDOT = 6820
686205
YDOT = -8533
814399 feet/sec YDOT = -2525
057766 meter/sec
ZDOT = -7776
171567 ZDOT = -2337
139735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15444662
45 X = -4707533
11
Y = 127919
14 feet Y = 38989
75 meter
Z = -16147043
82 Z = -4921618
96
XDOT = 7779
909250 XDOT = 2371
316339
YDOT = -21444
540503 feet/sec YDOT = -6536
295945 meter/sec
ZDOT = -7639
276482 ZDOT = -2328
451472
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 12267
15496027
00016717 00000-0 10270-3 0 9111
2 25544 51
6479 354
4120 0017805 89
6130 270
7061 15
49956070 33242
Satellite: ISS
Catalog Number: 25544
Epoch time: 12267
15496027 = yrday
fracday
Element set: 911
Inclination: 51
6479 deg
RA of node: 354
4120 deg
Eccentricity:
0017805
Arg of perigee: 89
6130 deg
Mean anomaly: 270
7061 deg
Mean motion: 15
49956070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 307
Coasting Arc #13 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2012/268/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3020630
24 A = 6790847
25 meter
Y = 3449078
30 meter E =
0023210
Z = 4990984
00 I = 51
56859
XDOT = -6780
385879 Wp = 100
06322
YDOT = 2963
884977 meter/sec RA = 349
04492 deg
ZDOT = 2043
309399 TA = 330
00705
MA = 330
13980
Ha = 234
079 n
mi
Hp = 214
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9910204
18 X = 2957592
40
Y = 11315873
68 feet Y = 3482504
71 meter
Z = 16374619
42 Z = 5005504
72
XDOT = -22245
360494 XDOT = -6822
950636
YDOT = 9724
032078 feet/sec YDOT = 2887
824606 meter/sec
ZDOT = 6703
770993 ZDOT = 2010
267092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14968020
78 X = 4562252
73
Y = -512194
67 feet Y = -156116
94 meter
Z = 16434272
60 Z = 5009166
29
XDOT = -6488
538010 XDOT = -1977
706385
YDOT = 22352
330244 feet/sec YDOT = 6812
990258 meter/sec
ZDOT = 6566
817507 ZDOT = 2001
565976
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 12268
18655933
00016717 00000-0 10270-3 0 9129
2 25544 51
6480 349
3018 0017934 93
2785 267
0418 15
49954212 33402
Satellite: ISS
Catalog Number: 25544
Epoch time: 12268
18655933 = yrday
fracday
Element set: 912
Inclination: 51
6480 deg
RA of node: 349
3018 deg
Eccentricity:
0017934
Arg of perigee: 93
2785 deg
Mean anomaly: 267
0418 deg
Mean motion: 15
49954212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 325
Coasting Arc #14 (Orbit 3354)
---------------------------------------
Vector Time (GMT): 2012/269/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2928608
24 A = 6790291
34 meter
Y = -3398034
70 meter E =
0030857
Z = -5124537
34 I = 51
53627
XDOT = 6696
078489 Wp = 88
13847
YDOT = -3280
386262 meter/sec RA = 344
08183 deg
ZDOT = -1659
237298 TA = 165
79944
MA = 165
71250
Ha = 234
022 n
mi
Hp = 214
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9608294
75 X = -2865499
29
Y = -11148407
82 feet Y = -3430431
78 meter
Z = -16812786
55 Z = -5138610
77
XDOT = 21968
761448 XDOT = 6740
322951
YDOT = -10762
422120 feet/sec YDOT = -3205
259285 meter/sec
ZDOT = -5443
691922 ZDOT = -1626
600447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14637588
32 X = -4461536
92
Y = 632509
16 feet Y = 192788
79 meter
Z = -16870597
41 Z = -5142158
09
XDOT = 5099
667506 XDOT = 1554
378656
YDOT = -22898
684769 feet/sec YDOT = -6979
519117 meter/sec
ZDOT = -5308
385076 ZDOT = -1617
995771
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 12269
15366838
00016717 00000-0 10270-3 0 9131
2 25544 51
6468 344
5097 0017796 96
8053 263
5123 15
49995527 33559
Satellite: ISS
Catalog Number: 25544
Epoch time: 12269
15366838 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 344
5097 deg
Eccentricity:
0017796
Arg of perigee: 96
8053 deg
Mean anomaly: 263
5123 deg
Mean motion: 15
49995527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3355
Checksum: 354
Coasting Arc #15 (Orbit 3370)
---------------------------------------
Vector Time (GMT): 2012/270/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2842090
97 A = 6789939
09 meter
Y = 3322659
05 meter E =
0021730
Z = 5177558
31 I = 51
50646
XDOT = -6634
936583 Wp = 104
34901
YDOT = 3636
500251 meter/sec RA = 339
11803 deg
ZDOT = 1298
531047 TA = 333
11368
MA = 333
22612
Ha = 233
981 n
mi
Hp = 214
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9324445
43 X = 2779573
75
Y = 10901112
36 feet Y = 3354092
05 meter
Z = 16986739
87 Z = 5191212
82
XDOT = -21768
164643 XDOT = -6681
415509
YDOT = 11930
775102 feet/sec YDOT = 3562
044503 meter/sec
ZDOT = 4260
272465 ZDOT = 1266
185678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14255602
08 X = 4345107
51
Y = -805406
73 feet Y = -245487
97 meter
Z = 17042828
22 Z = 5194654
04
XDOT = -3641
062290 XDOT = -1109
795786
YDOT = 23546
806491 feet/sec YDOT = 7177
066618 meter/sec
ZDOT = 4126
139589 ZDOT = 1257
647347
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 12270
18523999
00016717 00000-0 10270-3 0 9140
2 25544 51
6470 339
3995 0017874 100
4885 259
8281 15
49989091 33713
Satellite: ISS
Catalog Number: 25544
Epoch time: 12270
18523999 = yrday
fracday
Element set: 914
Inclination: 51
6470 deg
RA of node: 339
3995 deg
Eccentricity:
0017874
Arg of perigee: 100
4885 deg
Mean anomaly: 259
8281 deg
Mean motion: 15
49989091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3371
Checksum: 357
Coasting Arc #16 (Orbit 3385)
---------------------------------------
Vector Time (GMT): 2012/271/03:13:56
016
Vector Time (MET): N/A
Weight (LBS) : 922208
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2739498
80 A = 6789553
79 meter
Y = -3333964
75 meter E =
0031786
Z = -5269139
64 I = 51
47627
XDOT = 6487
495644 Wp = 94
42914
YDOT = -3932
202928 meter/sec RA = 334
15015 deg
ZDOT = -891
966190 TA = 167
02782
MA = 166
94587
Ha = 233
950 n
mi
Hp = 214
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8987856
94 X = -2676417
84
Y = -10938204
56 feet Y = -3364247
45 meter
Z = -17287203
55 Z = -5282294
37
XDOT = 21284
434526 XDOT = 6535
317153
YDOT = -12900
928243 feet/sec YDOT = -3859
388424 meter/sec
ZDOT = -2926
398262 ZDOT = -860
333648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14070725
94 X = -4288757
27
Y = 754908
27 feet Y = 230096
04 meter
Z = -17341224
96 Z = -5285605
37
XDOT = 2140
013625 XDOT = 652
276153
YDOT = -23790
568756 feet/sec YDOT = -7251
365357 meter/sec
ZDOT = -2795
190328 ZDOT = -851
974012
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 12271
15232354
00016717 00000-0 10270-3 0 9151
2 25544 51
6458 334
6073 0017840 104
1247 256
1888 15
50034515 33863
Satellite: ISS
Catalog Number: 25544
Epoch time: 12271
15232354 = yrday
fracday
Element set: 915
Inclination: 51
6458 deg
RA of node: 334
6073 deg
Eccentricity:
0017840
Arg of perigee: 104
1247 deg
Mean anomaly: 256
1888 deg
Mean motion: 15
50034515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3386
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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