[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 30th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 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
There are no maneuvers
Coasting Arc #1 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2011/119/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -409453
27 A = 6724230
89 meter
Y = -5349837
60 meter E =
0007423
Z = -4059610
78 I = 51
90273
XDOT = 6160
299193 Wp = 87
10313
YDOT = 2475
765879 meter/sec RA = 49
23862 deg
ZDOT = -3889
649624 TA = 142
95599
MA = 142
90472
Ha = 189
963 n
mi
Hp = 183
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1343350
62 X = -329878
90
Y = -17551960
63 feet Y = -5353971
56 meter
Z = -13318933
01 Z = -4061406
47
XDOT = 20210
955359 XDOT = 6151
052239
YDOT = 8122
591468 feet/sec YDOT = 2544
602261 meter/sec
ZDOT = -12761
317663 ZDOT = -3859
745163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16677176
39 X = -5083203
36
Y = 5617808
68 feet Y = 1712308
09 meter
Z = -13325985
98 Z = -4061760
53
XDOT = 3193
933006 XDOT = 973
510780
YDOT = -20458
259991 feet/sec YDOT = -6235
677645 meter/sec
ZDOT = -12640
393356 ZDOT = -3852
791895
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 11119
71178676
00016717 00000-0 10270-3 0 9003
2 25544 51
6452 49
7058 0002125 169
8033 190
3174 15
74272232 33273
Satellite: ISS
Catalog Number: 25544
Epoch time: 11119
71178676 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 49
7058 deg
Eccentricity:
0002125
Arg of perigee: 169
8033 deg
Mean anomaly: 190
3174 deg
Mean motion: 15
74272232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 300
Coasting Arc #2 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2011/120/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5572648
02 A = 6726432
61 meter
Y = -1792075
43 meter E =
0013225
Z = 3299806
88 I = 51
89082
XDOT = -876
538939 Wp = 100
30271
YDOT = -6016
420488 meter/sec RA = 44
06827 deg
ZDOT = -4734
085460 TA = 41
08126
MA = 40
98175
Ha = 189
819 n
mi
Hp = 183
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18282965
96 X = -5568224
59
Y = -5879512
58 feet Y = -1854367
36 meter
Z = 10826138
06 Z = 3272745
40
XDOT = -2875
783922 XDOT = -786
199403
YDOT = -19738
912362 feet/sec YDOT = -6025
717462 meter/sec
ZDOT = -15531
776443 ZDOT = -4738
124177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -767269
79 X = -233863
83
Y = 19251089
38 feet Y = 5867732
04 meter
Z = 10716698
77 Z = 3266449
79
XDOT = -16876
347793 XDOT = -5143
910807
YDOT = 8007
703504 feet/sec YDOT = 2440
748028 meter/sec
ZDOT = -15547
870131 ZDOT = -4738
990816
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 11120
72741535
00016717 00000-0 10270-3 0 9017
2 25544 51
6460 44
4880 0002001 173
9446 186
1742 15
74386324 33434
Satellite: ISS
Catalog Number: 25544
Epoch time: 11120
72741535 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 44
4880 deg
Eccentricity:
0002001
Arg of perigee: 173
9446 deg
Mean anomaly: 186
1742 deg
Mean motion: 15
74386324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 285
Coasting Arc #3 (Orbit 3358)
---------------------------------------
Vector Time (GMT): 2011/121/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1081842
32 A = 6723377
55 meter
Y = 5127226
58 meter E =
0010948
Z = 4207271
58 I = 51
85676
XDOT = -6579
255944 Wp = 116
51669
YDOT = -1626
676842 meter/sec RA = 38
99613 deg
ZDOT = 3662
051543 TA = 296
23815
MA = 296
35064
Ha = 189
686 n
mi
Hp = 183
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3549351
45 X = 1003989
80
Y = 16821609
52 feet Y = 5138889
13 meter
Z = 13803384
44 Z = 4212338
11
XDOT = -21585
485382 XDOT = -6578
367004
YDOT = -5336
866279 feet/sec YDOT = -1700
245084 meter/sec
ZDOT = 12014
604800 ZDOT = 3630
091190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15149109
26 X = 4617448
50
Y = -8093740
40 feet Y = -2466972
07 meter
Z = 13823665
20 Z = 4213453
15
XDOT = 432
533726 XDOT = 131
836280
YDOT = 21176
663430 feet/sec YDOT = 6454
647013 meter/sec
ZDOT = 11885
340660 ZDOT = 3622
651833
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 11121
74300793
00016717 00000-0 10270-3 0 9028
2 25544 51
6449 39
2694 0002078 177
9106 182
2067 15
74376141 33597
Satellite: ISS
Catalog Number: 25544
Epoch time: 11121
74300793 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 39
2694 deg
Eccentricity:
0002078
Arg of perigee: 177
9106 deg
Mean anomaly: 182
2067 deg
Mean motion: 15
74376141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 309
Coasting Arc #4 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2011/122/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5895899
11 A = 6726847
44 meter
Y = 1047820
62 meter E =
0004213
Z = -3069012
56 I = 51
84376
XDOT = 1550
535708 Wp = 101
62502
YDOT = 5701
542455 meter/sec RA = 33
82238 deg
ZDOT = 4930
203474 TA = 222
92247
MA = 222
95535
Ha = 189
509 n
mi
Hp = 183
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19343501
01 X = 5898652
94
Y = 3437731
70 feet Y = 1113767
58 meter
Z = -10068938
85 Z = -3040363
09
XDOT = 5087
059411 XDOT = 1462
714278
YDOT = 18705
847951 feet/sec YDOT = 5718
390387 meter/sec
ZDOT = 16175
208248 ZDOT = 4937
522858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2541445
58 X = -774632
61
Y = -19540991
65 feet Y = -5956094
25 meter
Z = -9953052
79 Z = -3033690
49
XDOT = 14923
267347 XDOT = 4548
611887
YDOT = -10186
363987 feet/sec YDOT = -3104
803743 meter/sec
ZDOT = 16204
569863 ZDOT = 4939
152894
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 11122
69508748
00016717 00000-0 10270-3 0 9034
2 25544 51
6442 34
3767 0002268 184
6399 175
4744 15
74465188 33740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11122
69508748 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 34
3767 deg
Eccentricity:
0002268
Arg of perigee: 184
6399 deg
Mean anomaly: 175
4744 deg
Mean motion: 15
74465188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 338
Coasting Arc #5 (Orbit 3389)
---------------------------------------
Vector Time (GMT): 2011/123/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1572825
39 A = 6722181
25 meter
Y = -4825569
08 meter E =
0008586
Z = -4415624
56 I = 51
80179
XDOT = 6892
228181 Wp = 82
37421
YDOT = 794
231349 meter/sec RA = 28
74479 deg
ZDOT = -3327
322109 TA = 154
26277
MA = 154
22002
Ha = 189
357 n
mi
Hp = 183
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5160188
29 X = -1497297
38
Y = -15831919
57 feet Y = -4842734
92 meter
Z = -14486957
21 Z = -4423082
18
XDOT = 22612
297181 XDOT = 6898
998493
YDOT = 2605
745896 feet/sec YDOT = 871
342394 meter/sec
ZDOT = -10916
411120 ZDOT = -3293
822608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13414651
67 X = -4088785
83
Y = 9821182
40 feet Y = 2993496
40 meter
Z = -14516908
98 Z = -4424753
86
XDOT = -3985
948502 XDOT = -1214
917103
YDOT = -21358
672003 feet/sec YDOT = -6510
123226 meter/sec
ZDOT = -10780
890992 ZDOT = -3286
015574
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 11123
71060281
00016717 00000-0 10270-3 0 9044
2 25544 51
6434 29
1583 0002277 188
0852 172
0275 15
74522119 33909
Satellite: ISS
Catalog Number: 25544
Epoch time: 11123
71060281 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 29
1583 deg
Eccentricity:
0002277
Arg of perigee: 188
0852 deg
Mean anomaly: 172
0275 deg
Mean motion: 15
74522119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 287
Coasting Arc #6 (Orbit 3405)
---------------------------------------
Vector Time (GMT): 2011/124/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6130806
21 A = 6727252
19 meter
Y = -328229
22 meter E =
0013555
Z = 2732249
72 I = 51
79271
XDOT = -2029
565307 Wp = 110
48046
YDOT = -5332
806344 meter/sec RA = 23
56957 deg
ZDOT = -5178
787400 TA = 38
36006
MA = 38
26374
Ha = 189
140 n
mi
Hp = 183
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20114193
60 X = -6139953
22
Y = -1076867
51 feet Y = -396838
90 meter
Z = 8964073
90 Z = 2702443
55
XDOT = -6658
678830 XDOT = -1944
623986
YDOT = -17496
083806 feet/sec YDOT = -5355
026963 meter/sec
ZDOT = -16990
772309 ZDOT = -5188
441149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5692646
94 X = 1735118
79
Y = 19377350
42 feet Y = 5906216
41 meter
Z = 8843478
40 Z = 2695492
22
XDOT = -12906
828376 XDOT = -3934
001289
YDOT = 11587
915874 feet/sec YDOT = 3531
996758 meter/sec
ZDOT = -17029
578401 ZDOT = -5190
615497
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 11124
72607757
00016717 00000-0 10270-3 0 9052
2 25544 51
6441 23
9392 0002252 198
9266 161
1814 15
74619760 34064
Satellite: ISS
Catalog Number: 25544
Epoch time: 11124
72607757 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 23
9392 deg
Eccentricity:
0002252
Arg of perigee: 198
9266 deg
Mean anomaly: 161
1814 deg
Mean motion: 15
74619760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3406
Checksum: 310
Coasting Arc #7 (Orbit 3421)
---------------------------------------
Vector Time (GMT): 2011/125/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1925966
37 A = 6721074
46 meter
Y = 4483867
54 meter E =
0008783
Z = 4618583
69 I = 51
74224
XDOT = -7128
434394 Wp = 131
15712
YDOT = 44
862118 meter/sec RA = 18
48285 deg
ZDOT = 2919
779117 TA = 289
93412
MA = 290
02871
Ha = 189
020 n
mi
Hp = 183
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6318787
31 X = 1853247
22
Y = 14710851
52 feet Y = 4504997
95 meter
Z = 15152833
62 Z = 4627763
84
XDOT = -23387
251948 XDOT = -7142
590193
YDOT = 147
185426 feet/sec YDOT = -34
931713 meter/sec
ZDOT = 9579
327812 ZDOT = 2885
114334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11615560
28 X = 3540422
77
Y = -10967888
61 feet Y = -3343012
45 meter
Z = 15189758
76 Z = 4629838
47
XDOT = 7515
383951 XDOT = 2290
689028
YDOT = 21073
538364 feet/sec YDOT = 6423
214493 meter/sec
ZDOT = 9439
053060 ZDOT = 2877
023373
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 11125
74151746
00016717 00000-0 10270-3 0 9068
2 25544 51
6428 18
7194 0002345 199
0989 161
0087 15
74620438 34221
Satellite: ISS
Catalog Number: 25544
Epoch time: 11125
74151746 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 18
7194 deg
Eccentricity:
0002345
Arg of perigee: 199
0989 deg
Mean anomaly: 161
0087 deg
Mean motion: 15
74620438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3422
Checksum: 313
Coasting Arc #8 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2011/126/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6295252
72 A = 6727885
25 meter
Y = -406226
06 meter E =
0003689
Z = -2338193
48 I = 51
73593
XDOT = 2329
234035 Wp = 60
20411
YDOT = 4944
025387 meter/sec RA = 13
30629 deg
ZDOT = 5420
335462 TA = 273
52343
MA = 273
56562
Ha = 188
943 n
mi
Hp = 183
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20653716
27 X = 6310685
97
Y = -1332762
67 feet Y = -335742
25 meter
Z = -7671238
45 Z = -2307573
38
XDOT = 7641
843947 XDOT = 2247
444615
YDOT = 16220
555733 feet/sec YDOT = 4969
614561 meter/sec
ZDOT = 17783
252829 ZDOT = 5431
452712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8793305
87 X = -2680199
63
Y = -18786059
17 feet Y = -5725990
83 meter
Z = -7547311
06 Z = -2300420
41
XDOT = 10984
071896 XDOT = 3347
945114
YDOT = -12292
862294 feet/sec YDOT = -3746
864427 meter/sec
ZDOT = 17827
989445 ZDOT = 5433
971183
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 11126
69345471
00016717 00000-0 10270-3 0 9074
2 25544 51
6426 13
8254 0002521 200
2611 159
8453 15
74697207 34371
Satellite: ISS
Catalog Number: 25544
Epoch time: 11126
69345471 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 13
8254 deg
Eccentricity:
0002521
Arg of perigee: 200
2611 deg
Mean anomaly: 159
8453 deg
Mean motion: 15
74697207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 299
Coasting Arc #9 (Orbit 3452)
---------------------------------------
Vector Time (GMT): 2011/127/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2089424
80 A = 6719733
87 meter
Y = -4171167
55 meter E =
0010799
Z = -4846055
87 I = 51
67916
XDOT = 7261
562377 Wp = 82
70787
YDOT = -862
286803 meter/sec RA = 8
20996 deg
ZDOT = -2391
883180 TA = 163
96486
MA = 163
93065
Ha = 188
779 n
mi
Hp = 182
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6855068
24 X = -2019085
32
Y = -13684932
91 feet Y = -4194139
10 meter
Z = -15899133
44 Z = -4856035
83
XDOT = 23824
023546 XDOT = 7282
284336
YDOT = -2829
024943 feet/sec YDOT = -780
967557 meter/sec
ZDOT = -7847
385762 ZDOT = -2356
556036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10080323
51 X = -3072482
61
Y = 11461998
70 feet Y = 3493617
20 meter
Z = -15939305
42 Z = -4858300
29
XDOT = -10870
524331 XDOT = -3313
335816
YDOT = -20259
521905 feet/sec YDOT = -6175
102277 meter/sec
ZDOT = -7704
385557 ZDOT = -2348
296718
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 11127
70881795
00016717 00000-0 10270-3 0 9082
2 25544 51
6426 8
6060 0002458 202
1412 157
9646 15
74768087 34533
Satellite: ISS
Catalog Number: 25544
Epoch time: 11127
70881795 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 8
6060 deg
Eccentricity:
0002458
Arg of perigee: 202
1412 deg
Mean anomaly: 157
9646 deg
Mean motion: 15
74768087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3453
Checksum: 319
Coasting Arc #10 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2011/128/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6373022
64 A = 6728410
87 meter
Y = 1106244
58 meter E =
0013976
Z = 1824598
59 I = 51
67793
XDOT = -2431
328591 Wp = 124
36290
YDOT = -4616
774312 meter/sec RA = 3
03504 deg
ZDOT = -5670
157141 TA = 35
39132
MA = 35
29864
Ha = 188
546 n
mi
Hp = 182
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20908866
93 X = -6393782
81
Y = 3629411
35 feet Y = 1034861
37 meter
Z = 5986215
85 Z = 1793588
02
XDOT = -7976
799838 XDOT = -2351
977571
YDOT = -15146
897349 feet/sec YDOT = -4643
518832 meter/sec
ZDOT = -18602
877758 ZDOT = -5681
776142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11639678
11 X = 3547773
89
Y = 17786471
47 feet Y = 5421316
50 meter
Z = 5860669
73 Z = 1786332
13
XDOT = -9488
297641 XDOT = -2892
033121
YDOT = 12379
684643 feet/sec YDOT = 3773
327879 meter/sec
ZDOT = -18649
659303 ZDOT = -5684
416156
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 11128
72414118
00016717 00000-0 10270-3 0 9097
2 25544 51
6423 3
3851 0002535 213
2156 146
8848 15
74836743 34697
Satellite: ISS
Catalog Number: 25544
Epoch time: 11128
72414118 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 3
3851 deg
Eccentricity:
0002535
Arg of perigee: 213
2156 deg
Mean anomaly: 146
8848 deg
Mean motion: 15
74836743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 308
Coasting Arc #11 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2011/129/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2120252
49 A = 6718625
54 meter
Y = 3912397
01 meter E =
0005906
Z = 5032507
51 I = 51
61470
XDOT = -7307
805195 Wp = 150
48603
YDOT = 1670
964310 meter/sec RA = 357
92461 deg
ZDOT = 1773
880961 TA = 282
39718
MA = 282
46328
Ha = 188
389 n
mi
Hp = 182
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6956208
95 X = 2051898
71
Y = 12835948
21 feet Y = 3935724
50 meter
Z = 16510851
41 Z = 5042641
88
XDOT = -23975
738828 XDOT = -7334
564297
YDOT = 5482
166370 feet/sec YDOT = 1589
094281 meter/sec
ZDOT = 5819
819427 ZDOT = 1738
314726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8866494
30 X = 2702507
46
Y = -11540640
56 feet Y = -3517587
24 meter
Z = 16551662
08 Z = 5044946
60
XDOT = 14054
530610 XDOT = 4283
820930
YDOT = 18965
998689 feet/sec YDOT = 5780
836401 meter/sec
ZDOT = 5675
809840 ZDOT = 1729
986839
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 11129
73942922
00016717 00000-0 10270-3 0 9100
2 25544 51
6424 358
1643 0002550 214
0558 146
0442 15
74864220 34851
Satellite: ISS
Catalog Number: 25544
Epoch time: 11129
73942922 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 358
1643 deg
Eccentricity:
0002550
Arg of perigee: 214
0558 deg
Mean anomaly: 146
0442 deg
Mean motion: 15
74864220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 295
Coasting Arc #12 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2011/130/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6359520
71 A = 6728890
47 meter
Y = -1802220
00 meter E =
0006619
Z = -1244648
27 I = 51
62038
XDOT = 2385
157018 Wp = 37
85882
YDOT = 4380
178386 meter/sec RA = 352
75464 deg
ZDOT = 5866
098954 TA = 308
48735
MA = 308
54670
Ha = 188
332 n
mi
Hp = 182
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20864569
24 X = 6385247
10
Y = -5912795
29 feet Y = -1730960
09 meter
Z = -4083491
69 Z = -1213691
28
XDOT = 7825
318299 XDOT = 2307
503296
YDOT = 14370
663997 feet/sec YDOT = 4406
416258 meter/sec
ZDOT = 19245
731477 ZDOT = 5877
497591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14284361
02 X = -4353873
24
Y = -16347982
63 feet Y = -4982865
11 meter
Z = -3958130
41 Z = -1206438
15
XDOT = 8496
751629 XDOT = 2589
809897
YDOT = -12077
379636 feet/sec YDOT = -3681
185313 meter/sec
ZDOT = 19291
635256 ZDOT = 5880
090426
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 11130
69122527
00016717 00000-0 10270-3 0 9119
2 25544 51
6437 353
2702 0002628 215
6134 144
4855 15
74930539 35005
Satellite: ISS
Catalog Number: 25544
Epoch time: 11130
69122527 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 353
2702 deg
Eccentricity:
0002628
Arg of perigee: 215
6134 deg
Mean anomaly: 144
4855 deg
Mean motion: 15
74930539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 288
Coasting Arc #13 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2011/131/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2007924
63 A = 6717554
85 meter
Y = -3777935
92 meter E =
0012780
Z = -5189875
86 I = 51
55300
XDOT = 7227
707234 Wp = 89
63638
YDOT = -2424
972960 meter/sec RA = 347
62972 deg
ZDOT = -1033
208808 TA = 170
50195
MA = 170
47776
Ha = 188
122 n
mi
Hp = 182
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6587679
24 X = -1940318
25
Y = -12394802
88 feet Y = -3800011
63 meter
Z = -17027151
78 Z = -5199466
25
XDOT = 23712
950244 XDOT = 7259
305718
YDOT = -7955
948032 feet/sec YDOT = -2343
971651 meter/sec
ZDOT = -3389
792676 ZDOT = -998
019813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8233714
18 X = -2509636
08
Y = 11310085
01 feet Y = 3447313
91 meter
Z = -17065769
30 Z = -5201646
48
XDOT = -16831
266225 XDOT = -5130
169945
YDOT = -17142
537968 feet/sec YDOT = -5225
045573 meter/sec
ZDOT = -3247
280415 ZDOT = -989
771071
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 11131
70643766
00016717 00000-0 10270-3 0 9126
2 25544 51
6441 348
0506 0002550 220
2997 139
7978 15
75006746 35162
Satellite: ISS
Catalog Number: 25544
Epoch time: 11131
70643766 = yrday
fracday
Element set: 912
Inclination: 51
6441 deg
RA of node: 348
0506 deg
Eccentricity:
0002550
Arg of perigee: 220
2997 deg
Mean anomaly: 139
7978 deg
Mean motion: 15
75006746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 312
Coasting Arc #14 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2011/132/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6245765
02 A = 6729056
53 meter
Y = 2424516
11 meter E =
0013003
Z = 542022
90 I = 51
56175
XDOT = -2196
832414 Wp = 140
91447
YDOT = -4302
124962 meter/sec RA = 342
46595 deg
ZDOT = -6002
543392 TA = 33
17654
MA = 33
09507
Ha = 187
893 n
mi
Hp = 182
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20491355
05 X = -6275045
29
Y = 7954449
19 feet Y = 2354508
45 meter
Z = 1778290
36 Z = 511609
68
XDOT = -7207
455428 XDOT = -2119
402489
YDOT = -14114
583210 feet/sec YDOT = -4326
258270 meter/sec
ZDOT = -19693
383831 ZDOT = -6013
027648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16474623
60 X = 5021465
27
Y = 14566351
66 feet Y = 4439823
99 meter
Z = 1655109
30 Z = 504477
31
XDOT = -8226
883480 XDOT = -2507
554085
YDOT = 11574
319494 feet/sec YDOT = 3527
852582 meter/sec
ZDOT = -19735
591322 ZDOT = -6015
408235
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 11132
72161134
00016717 00000-0 10270-3 0 9134
2 25544 51
6435 342
8285 0002644 228
6048 131
4888 15
75059109 35322
Satellite: ISS
Catalog Number: 25544
Epoch time: 11132
72161134 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 342
8285 deg
Eccentricity:
0002644
Arg of perigee: 228
6048 deg
Mean anomaly: 131
4888 deg
Mean motion: 15
75059109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 300
Coasting Arc #15 (Orbit 3547)
---------------------------------------
Vector Time (GMT): 2011/133/16:32:00
105
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1815779
09 A = 6716950
92 meter
Y = 3771122
18 meter E =
0001889
Z = 5253286
75 I = 51
49340
XDOT = -7043
532955 Wp = 171
41138
YDOT = 3113
635569 meter/sec RA = 337
32148 deg
ZDOT = 197
570089 TA = 276
69975
MA = 276
72125
Ha = 187
687 n
mi
Hp = 182
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5957280
49 X = 1747954
92
Y = 12372448
08 feet Y = 3791048
01 meter
Z = 17235192
76 Z = 5261943
22
XDOT = -23108
703920 XDOT = -7078
786500
YDOT = 10215
339792 feet/sec YDOT = 3034
673389 meter/sec
ZDOT = 648
195831 ZDOT = 163
266627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8119557
23 X = 2474841
04
Y = -11019864
19 feet Y = -3358854
61 meter
Z = 17270029
40 Z = 5263904
96
XDOT = 19147
351930 XDOT = 5836
112868
YDOT = 14915
538334 feet/sec YDOT = 4546
256084 meter/sec
ZDOT = 509
246221 ZDOT = 155
218248
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 11133
73674798
00016717 00000-0 10270-3 0 9142
2 25544 51
6444 337
6076 0002623 233
9626 126
1295 15
75105364 35485
Satellite: ISS
Catalog Number: 25544
Epoch time: 11133
73674798 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 337
6076 deg
Eccentricity:
0002623
Arg of perigee: 233
9626 deg
Mean anomaly: 126
1295 deg
Mean motion: 15
75105364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 321
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list