[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 1st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 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
There are no maneuvers
Coasting Arc #1 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2012/306/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -58236
93 A = 6786714
66 meter
Y = -4379704
13 meter E =
0011567
Z = 5190791
90 I = 51
75426
XDOT = 7328
328213 Wp = 234
42781
YDOT = -1734
212475 meter/sec RA = 158
32220 deg
ZDOT = -1389
752289 TA = 228
88274
MA = 228
98265
Ha = 227
209 n
mi
Hp = 219
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -191066
03 X = -34474
17
Y = -14369108
03 feet Y = -4380222
48 meter
Z = 17030157
17 Z = 5190566
73
XDOT = 24043
071566 XDOT = 7353
927149
YDOT = -5689
673476 feet/sec YDOT = -1652
119408 meter/sec
ZDOT = -4559
554755 ZDOT = -1354
088508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8427174
61 X = 2568602
82
Y = 11640805
82 feet Y = 3548117
61 meter
Z = 17029632
79 Z = 5190632
08
XDOT = -15693
718406 XDOT = -4783
445370
YDOT = 17773
278349 feet/sec YDOT = 5417
295241 meter/sec
ZDOT = -4411
709470 ZDOT = -1344
689046
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 12306
53034606
00016717 00000-0 10270-3 0 9006
2 25544 51
6468 159
1693 0015904 234
5184 125
4484 15
51121281 39357
Satellite: ISS
Catalog Number: 25544
Epoch time: 12306
53034606 = yrday
fracday
Element set: 900
Inclination: 51
6468 deg
RA of node: 159
1693 deg
Eccentricity:
0015904
Arg of perigee: 234
5184 deg
Mean anomaly: 125
4484 deg
Mean motion: 15
51121281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 297
Coasting Arc #2 (Orbit 3949)
---------------------------------------
Vector Time (GMT): 2012/307/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -445252
49 A = 6787549
85 meter
Y = 4602529
29 meter E =
0011842
Z = -4971398
60 I = 51
78390
XDOT = -7152
996348 Wp = 187
68046
YDOT = 1671
257742 meter/sec RA = 153
36185 deg
ZDOT = 2175
848309 TA = 103
57687
MA = 103
44493
Ha = 226
854 n
mi
Hp = 219
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1460802
15 X = -472535
36
Y = 15100161
70 feet Y = 4597397
67 meter
Z = -16310362
85 Z = -4973627
91
XDOT = -23467
835789 XDOT = -7181
723090
YDOT = 5483
129076 feet/sec YDOT = 1591
107841 meter/sec
ZDOT = 7138
609937 ZDOT = 2141
028808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7708045
65 X = -2349412
31
Y = -13054479
01 feet Y = -3979005
20 meter
Z = -16320029
80 Z = -4974345
08
XDOT = 14938
107108 XDOT = 4553
135047
YDOT = -17613
465530 feet/sec YDOT = -5368
584294 meter/sec
ZDOT = 6994
247173 ZDOT = 2131
846538
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 12307
49674683
00016717 00000-0 10270-3 0 9018
2 25544 51
6454 154
3719 0015901 238
2716 121
6885 15
51150257 39502
Satellite: ISS
Catalog Number: 25544
Epoch time: 12307
49674683 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 154
3719 deg
Eccentricity:
0015901
Arg of perigee: 238
2716 deg
Mean anomaly: 121
6885 deg
Mean motion: 15
51150257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3950
Checksum: 314
Coasting Arc #3 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2012/308/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 866367
24 A = 6788647
80 meter
Y = -4849514
05 meter E =
0007898
Z = 4675033
22 I = 51
81510
XDOT = 6910
506151 Wp = 240
89442
YDOT = -1563
416168 meter/sec RA = 148
40694 deg
ZDOT = -2909
859458 TA = 237
97026
MA = 238
04701
Ha = 226
549 n
mi
Hp = 219
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2842412
19 X = 897820
41
Y = -15910479
15 feet Y = -4839649
96 meter
Z = 15338035
51 Z = 4679318
44
XDOT = 22672
264275 XDOT = 6941
610712
YDOT = -5129
318137 feet/sec YDOT = -1485
964635 meter/sec
ZDOT = -9546
782999 ZDOT = -2876
212313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7303146
07 X = 2225998
92
Y = 14398878
61 feet Y = 4388778
20 meter
Z = 15356247
58 Z = 4680584
26
XDOT = -14110
344417 XDOT = -4300
832978
YDOT = 17163
500602 feet/sec YDOT = 5231
434983 meter/sec
ZDOT = -9407
267077 ZDOT = -2867
335005
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 12308
52755464
00016717 00000-0 10270-3 0 9021
2 25544 51
6459 149
2569 0015976 242
4464 117
5065 15
51184971 39663
Satellite: ISS
Catalog Number: 25544
Epoch time: 12308
52755464 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 149
2569 deg
Eccentricity:
0015976
Arg of perigee: 242
4464 deg
Mean anomaly: 117
5065 deg
Mean motion: 15
51184971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 338
Coasting Arc #4 (Orbit 3980)
---------------------------------------
Vector Time (GMT): 2012/309/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1287087
41 A = 6790139
95 meter
Y = 5124797
31 meter E =
0011567
Z = -4264667
11 I = 51
84429
XDOT = -6613
860707 Wp = 216
10623
YDOT = 1362
696115 meter/sec RA = 143
45248 deg
ZDOT = 3619
505940 TA = 90
88621
MA = 90
75367
Ha = 226
233 n
mi
Hp = 219
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4222727
71 X = -1323581
15
Y = 16813639
45 feet Y = 5110200
26 meter
Z = -13991689
98 Z = -4271008
45
XDOT = -21699
018066 XDOT = -6646
190148
YDOT = 4470
787779 feet/sec YDOT = 1288
555012 meter/sec
ZDOT = 11875
019489 ZDOT = 3587
297019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7002940
86 X = -2134496
37
Y = -15834743
24 feet Y = -4826429
74 meter
Z = -14018452
68 Z = -4272824
38
XDOT = 13342
498869 XDOT = 4066
793655
YDOT = -16336
326755 feet/sec YDOT = -4979
312395 meter/sec
ZDOT = 11741
462865 ZDOT = 3578
797881
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 12309
49392032
00016717 00000-0 10270-3 0 9037
2 25544 51
6445 144
4592 0015922 245
7914 114
1574 15
51201910 39816
Satellite: ISS
Catalog Number: 25544
Epoch time: 12309
49392032 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 144
4592 deg
Eccentricity:
0015922
Arg of perigee: 245
7914 deg
Mean anomaly: 114
1574 deg
Mean motion: 15
51201910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3981
Checksum: 297
Coasting Arc #5 (Orbit 3996)
---------------------------------------
Vector Time (GMT): 2012/310/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1614989
40 A = 6791614
26 meter
Y = -5399504
44 meter E =
0005480
Z = 3789604
63 I = 51
87416
XDOT = 6278
261223 Wp = 222
49070
YDOT = -1100
032041 meter/sec RA = 138
50389 deg
ZDOT = -4250
427332 TA = 272
32925
MA = 272
39199
Ha = 225
903 n
mi
Hp = 219
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5298521
64 X = 1656838
42
Y = -17714909
57 feet Y = -5381210
61 meter
Z = 12433086
04 Z = 3797551
96
XDOT = 20597
969891 XDOT = 6310
743328
YDOT = -3609
029006 feet/sec YDOT = -1029
642997 meter/sec
ZDOT = -13944
971562 ZDOT = -4219
848448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6990032
34 X = 2130561
86
Y = 17093826
48 feet Y = 5210198
31 meter
Z = 12466536
21 Z = 3799800
24
XDOT = -12647
310634 XDOT = -3854
900281
YDOT = 15231
423255 feet/sec YDOT = 4642
537808 meter/sec
ZDOT = -13818
177919 ZDOT = -4211
780630
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 12310
52468957
00016717 00000-0 10270-3 0 9044
2 25544 51
6451 139
3439 0016028 250
1899 109
7525 15
51247949 39971
Satellite: ISS
Catalog Number: 25544
Epoch time: 12310
52468957 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 139
3439 deg
Eccentricity:
0016028
Arg of perigee: 250
1899 deg
Mean anomaly: 109
7525 deg
Mean motion: 15
51247949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3997
Checksum: 339
Coasting Arc #6 (Orbit 4011)
---------------------------------------
Vector Time (GMT): 2012/311/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1921827
41 A = 6793317
76 meter
Y = 5669571
93 meter E =
0011382
Z = -3206279
03 I = 51
90081
XDOT = -5911
379701 Wp = 250
50715
YDOT = 732
150586 meter/sec RA = 133
55629 deg
ZDOT = 4820
268054 TA = 72
62567
MA = 72
50122
Ha = 225
637 n
mi
Hp = 219
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6305208
03 X = -1969507
30
Y = 18600957
78 feet Y = 5647814
22 meter
Z = -10519288
15 Z = -3215731
21
XDOT = -19394
290359 XDOT = -5942
543525
YDOT = 2402
068851 feet/sec YDOT = 665
871669 meter/sec
ZDOT = 15814
527737 ZDOT = 4791
474715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7064427
38 X = -2153237
46
Y = -18303221
78 feet Y = -5578822
00 meter
Z = -10559007
53 Z = -3218385
49
XDOT = 12138
498637 XDOT = 3699
814385
YDOT = -13772
714383 feet/sec YDOT = -4197
923344 meter/sec
ZDOT = 15695
155152 ZDOT = 4783
883290
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 12311
49101974
00016717 00000-0 10270-3 0 9055
2 25544 51
6439 134
5460 0015904 253
1668 106
7739 15
51256076 40121
Satellite: ISS
Catalog Number: 25544
Epoch time: 12311
49101974 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 134
5460 deg
Eccentricity:
0015904
Arg of perigee: 253
1668 deg
Mean anomaly: 106
7739 deg
Mean motion: 15
51256076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4012
Checksum: 300
Coasting Arc #7 (Orbit 4027)
---------------------------------------
Vector Time (GMT): 2012/312/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2136081
72 A = 6794680
75 meter
Y = -5909399
47 meter E =
0006987
Z = 2577170
25 I = 51
92661
XDOT = 5538
806694 Wp = 200
54443
YDOT = -298
820912 meter/sec RA = 128
61411 deg
ZDOT = -5286
719479 TA = 310
63744
MA = 310
69818
Ha = 225
318 n
mi
Hp = 219
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7008142
12 X = 2189483
60
Y = -19387793
55 feet Y = -5885213
81 meter
Z = 8455282
96 Z = 2587677
27
XDOT = 18171
937972 XDOT = 5567
418586
YDOT = -980
383571 feet/sec YDOT = -236
722687 meter/sec
ZDOT = -17344
880181 ZDOT = -5259
742298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7347749
99 X = 2239594
20
Y = 19242221
46 feet Y = 5865029
10 meter
Z = 8499405
16 Z = 2590618
69
XDOT = -11827
668208 XDOT = -3605
073270
YDOT = 12112
982138 feet/sec YDOT = 3692
036956 meter/sec
ZDOT = -17233
065686 ZDOT = -5252
638421
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 12312
52174983
00016717 00000-0 10270-3 0 9061
2 25544 51
6443 129
4305 0016024 257
8277 102
1080 15
51315329 40281
Satellite: ISS
Catalog Number: 25544
Epoch time: 12312
52174983 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 129
4305 deg
Eccentricity:
0016024
Arg of perigee: 257
8277 deg
Mean anomaly: 102
1080 deg
Mean motion: 15
51315329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4028
Checksum: 286
Coasting Arc #8 (Orbit 4042)
---------------------------------------
Vector Time (GMT): 2012/313/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2322104
06 A = 6796048
69 meter
Y = 6106238
80 meter E =
0011511
Z = -1856451
53 I = 51
94852
XDOT = -5164
026002 Wp = 285
01729
YDOT = -235
773245 meter/sec RA = 123
67282 deg
ZDOT = 5657
499792 TA = 54
67096
MA = 54
56340
Ha = 225
123 n
mi
Hp = 219
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7618451
64 X = -2381194
34
Y = 20033591
87 feet Y = 6079941
12 meter
Z = -6090720
24 Z = -1867876
18
XDOT = -16942
342527 XDOT = -5188
489053
YDOT = -773
534269 feet/sec YDOT = -293
657159 meter/sec
ZDOT = 18561
351022 ZDOT = 5632
353353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7639667
64 X = -2328570
70
Y = -20010863
18 feet Y = -6099311
10 meter
Z = -6138673
73 Z = -1871067
75
XDOT = 11803
473671 XDOT = 3597
698775
YDOT = -10194
607919 feet/sec YDOT = -3107
316494 meter/sec
ZDOT = 18457
168830 ZDOT = 5625
745060
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 12313
48804371
00016717 00000-0 10270-3 0 9079
2 25544 51
6435 124
6325 0015836 260
5321 99
4040 15
51312515 40437
Satellite: ISS
Catalog Number: 25544
Epoch time: 12313
48804371 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 124
6325 deg
Eccentricity:
0015836
Arg of perigee: 260
5321 deg
Mean anomaly: 99
4040 deg
Mean motion: 15
51312515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4043
Checksum: 280
Coasting Arc #9 (Orbit 4058)
---------------------------------------
Vector Time (GMT): 2012/314/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2428098
07 A = 6796774
44 meter
Y = -6243862
24 meter E =
0009712
Z = 1115806
95 I = 51
96761
XDOT = 4816
014748 Wp = 207
06177
YDOT = 822
781272 meter/sec RA = 118
73561 deg
ZDOT = -5904
498456 TA = 320
89905
MA = 320
96920
Ha = 224
873 n
mi
Hp = 219
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7966201
03 X = 2492317
34
Y = -20485112
34 feet Y = -6216350
61 meter
Z = 3660783
97 Z = 1127759
08
XDOT = 15800
573320 XDOT = 4835
139594
YDOT = 2699
413621 feet/sec YDOT = 876
743604 meter/sec
ZDOT = -19371
714093 ZDOT = -5881
055589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8021635
39 X = 2444994
47
Y = 20454431
25 feet Y = 6234510
64 meter
Z = 3710947
84 Z = 1131096
90
XDOT = -12051
328676 XDOT = -3673
244980
YDOT = 8206
322674 feet/sec YDOT = 2501
287151 meter/sec
ZDOT = -19274
646182 ZDOT = -5874
912156
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 12314
51873405
00016717 00000-0 10270-3 0 9089
2 25544 51
6434 119
5163 0015916 265
4172 94
5161 15
51384782 40598
Satellite: ISS
Catalog Number: 25544
Epoch time: 12314
51873405 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 119
5163 deg
Eccentricity:
0015916
Arg of perigee: 265
4172 deg
Mean anomaly: 94
5161 deg
Mean motion: 15
51384782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4059
Checksum: 311
Coasting Arc #10 (Orbit 4073)
---------------------------------------
Vector Time (GMT): 2012/315/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2513844
94 A = 6797295
51 meter
Y = 6301662
58 meter E =
0011141
Z = -310561
50 I = 51
98293
XDOT = -4493
245336 Wp = 314
57576
YDOT = -1489
219459 meter/sec RA = 113
79870 deg
ZDOT = 6027
531482 TA = 42
09683
MA = 42
01130
Ha = 224
786 n
mi
Hp = 219
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8247522
77 X = -2582615
94
Y = 20674745
99 feet Y = 6273166
66 meter
Z = -1018902
56 Z = -322941
28
XDOT = -14741
618558 XDOT = -4505
539717
YDOT = -4885
890612 feet/sec YDOT = -1539
534195 meter/sec
ZDOT = 19775
365756 ZDOT = 6005
673180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8287704
85 X = -2526092
44
Y = -20656043
39 feet Y = -6295962
03 meter
Z = -1070857
44 Z = -326397
35
XDOT = 12625
940677 XDOT = 3848
386718
YDOT = -6106
587720 feet/sec YDOT = -1861
287937 meter/sec
ZDOT = 19684
930744 ZDOT = 5999
966891
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 12315
48499042
00016717 00000-0 10270-3 0 9098
2 25544 51
6434 114
7183 0015730 267
9221 92
0129 15
51376213 40747
Satellite: ISS
Catalog Number: 25544
Epoch time: 12315
48499042 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 114
7183 deg
Eccentricity:
0015730
Arg of perigee: 267
9221 deg
Mean anomaly: 92
0129 deg
Mean motion: 15
51376213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4074
Checksum: 299
Coasting Arc #11 (Orbit 4089)
---------------------------------------
Vector Time (GMT): 2012/316/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2543405
47 A = 6797057
40 meter
Y = -6278742
02 meter E =
0011231
Z = -482117
75 I = 51
99397
XDOT = 4222
105661 Wp = 228
06938
YDOT = 2178
420096 meter/sec RA = 108
86384 deg
ZDOT = -6013
989179 TA = 317
09960
MA = 317
18716
Ha = 224
689 n
mi
Hp = 219
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8344506
12 X = 2615768
72
Y = -20599547
32 feet Y = -6249895
48 meter
Z = -1581751
14 Z = -469585
67
XDOT = 13852
052695 XDOT = 4226
647737
YDOT = 7147
047558 feet/sec YDOT = 2225
659519 meter/sec
ZDOT = -19730
935627 ZDOT = -5993
466842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8508695
96 X = 2593450
53
Y = 20536257
11 feet Y = 6259451
17 meter
Z = -1529152
08 Z = -466085
56
XDOT = -13470
475986 XDOT = -4105
801081
YDOT = 4097
451590 feet/sec YDOT = 1248
903245 meter/sec
ZDOT = -19646
109486 ZDOT = -5988
134171
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 12316
51564072
00016717 00000-0 10270-3 0 9101
2 25544 51
6432 109
6015 0015744 272
8178 87
1171 15
51442275 40905
Satellite: ISS
Catalog Number: 25544
Epoch time: 12316
51564072 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 109
6015 deg
Eccentricity:
0015744
Arg of perigee: 272
8178 deg
Mean anomaly: 87
1171 deg
Mean motion: 15
51442275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4090
Checksum: 290
Coasting Arc #12 (Orbit 4105)
---------------------------------------
Vector Time (GMT): 2012/317/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2574108
98 A = 6796427
25 meter
Y = 6147990
09 meter E =
0009313
Z = 1303750
47 I = 52
00160
XDOT = -3993
749872 Wp = 336
13655
YDOT = -2909
606057 meter/sec RA = 103
92842 deg
ZDOT = 5858
236846 TA = 37
96303
MA = 37
89741
Ha = 224
733 n
mi
Hp = 219
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8445239
42 X = -2648999
29
Y = 20170571
17 feet Y = 6118786
07 meter
Z = 4277396
55 Z = 1291063
22
XDOT = -13102
853912 XDOT = -3989
376089
YDOT = -9545
951632 feet/sec YDOT = -2954
242168 meter/sec
ZDOT = 19219
937158 ZDOT = 5838
845436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8472413
54 X = -2582391
65
Y = -20170396
46 feet Y = -6147936
84 meter
Z = 4224150
45 Z = 1287521
06
XDOT = 14600
066546 XDOT = 4450
100283
YDOT = -2140
206309 feet/sec YDOT = -652
334883 meter/sec
ZDOT = 19139
878450 ZDOT = 5833
834952
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 12317
54627157
00016717 00000-0 10270-3 0 9110
2 25544 51
6439 104
4836 0015660 275
6108 84
3257 15
51449315 41061
Satellite: ISS
Catalog Number: 25544
Epoch time: 12317
54627157 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 104
4836 deg
Eccentricity:
0015660
Arg of perigee: 275
6108 deg
Mean anomaly: 84
3257 deg
Mean motion: 15
51449315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4106
Checksum: 305
Coasting Arc #13 (Orbit 4120)
---------------------------------------
Vector Time (GMT): 2012/318/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2579625
20 A = 6795235
05 meter
Y = -5929170
29 meter E =
0011354
Z = -2075249
24 I = 52
00467
XDOT = 3827
920647 Wp = 258
59279
YDOT = 3621
367642 meter/sec RA = 98
99313 deg
ZDOT = -5564
766878 TA = 304
22356
MA = 304
33108
Ha = 224
824 n
mi
Hp = 219
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8463337
27 X = 2655816
10
Y = -19452658
42 feet Y = -5899897
25 meter
Z = -6808560
49 Z = -2062532
22
XDOT = 12558
794774 XDOT = 3814
174468
YDOT = 11881
127434 feet/sec YDOT = 3664
097119 meter/sec
ZDOT = -18257
109180 ZDOT = -5546
203739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8273925
17 X = 2521892
39
Y = 19552493
15 feet Y = 5959599
91 meter
Z = -6755195
57 Z = -2058983
61
XDOT = -15912
464350 XDOT = -4850
119134
YDOT = 425
505921 feet/sec YDOT = 129
694205 meter/sec
ZDOT = -18180
564997 ZDOT = -5541
436211
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 12318
51246824
00016717 00000-0 10270-3 0 9127
2 25544 51
6443 99
6867 0015642 280
0626 79
8760 15
51484776 41215
Satellite: ISS
Catalog Number: 25544
Epoch time: 12318
51246824 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 99
6867 deg
Eccentricity:
0015642
Arg of perigee: 280
0626 deg
Mean anomaly: 79
8760 deg
Mean motion: 15
51484776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4121
Checksum: 326
Coasting Arc #14 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2012/319/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2615895
21 A = 6793564
12 meter
Y = 5589363
09 meter E =
0006203
Z = 2834267
73 I = 52
00447
XDOT = -3705
734420 Wp = 340
34496
YDOT = -4328
035269 meter/sec RA = 94
05583 deg
ZDOT = 5123
879328 TA = 51
63380
MA = 51
57808
Ha = 224
985 n
mi
Hp = 219
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8582333
35 X = -2691970
83
Y = 18337805
41 feet Y = 5559685
00 meter
Z = 9298778
64 Z = 2821374
98
XDOT = -12157
921325 XDOT = -3681
953342
YDOT = -14199
590778 feet/sec YDOT = -4369
342410 meter/sec
ZDOT = 16810
627718 ZDOT = 5105
934072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7696069
63 X = -2345762
02
Y = -18753794
15 feet Y = -5716156
46 meter
Z = 9244704
13 Z = 2817785
82
XDOT = 17384
259591 XDOT = 5298
722323
YDOT = 1101
820831 feet/sec YDOT = 335
834989 meter/sec
ZDOT = 16736
728221 ZDOT = 5101
354762
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 12319
54305686
00016717 00000-0 10270-3 0 9134
2 25544 51
6455 94
5691 0015668 283
3096 76
6308 15
51520290 41374
Satellite: ISS
Catalog Number: 25544
Epoch time: 12319
54305686 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 94
5691 deg
Eccentricity:
0015668
Arg of perigee: 283
3096 deg
Mean anomaly: 76
6308 deg
Mean motion: 15
51520290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4137
Checksum: 322
Coasting Arc #15 (Orbit 4151)
---------------------------------------
Vector Time (GMT): 2012/320/11:37:28
591
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2658218
68 A = 6791757
50 meter
Y = -5172869
38 meter E =
0011089
Z = -3503977
75 I = 52
00028
XDOT = 3639
002505 Wp = 296
59182
YDOT = 4969
124844 meter/sec RA = 89
11746 deg
ZDOT = -4559
240733 TA = 284
31910
MA = 284
44220
Ha = 225
205 n
mi
Hp = 219
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8721189
91 X = 2732887
14
Y = -16971356
24 feet Y = -5142725
78 meter
Z = -11495989
98 Z = -3490882
94
XDOT = 11938
984596 XDOT = 3605
314508
YDOT = 16302
903032 feet/sec YDOT = 5009
630403 meter/sec
ZDOT = -14958
138889 ZDOT = -4541
643704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6892974
91 X = 2100978
75
Y = 17827838
12 feet Y = 5433925
06 meter
Z = -11441108
18 Z = -3487249
77
XDOT = -18881
712103 XDOT = -5755
145849
YDOT = -2286
314076 feet/sec YDOT = -696
868530 meter/sec
ZDOT = -14885
760544 ZDOT = -4537
179814
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 12320
50921553
00016717 00000-0 10270-3 0 9140
2 25544 51
6461 89
7726 0015660 287
5202 72
4238 15
51529568 41523
Satellite: ISS
Catalog Number: 25544
Epoch time: 12320
50921553 = yrday
fracday
Element set: 914
Inclination: 51
6461 deg
RA of node: 89
7726 deg
Eccentricity:
0015660
Arg of perigee: 287
5202 deg
Mean anomaly: 72
4238 deg
Mean motion: 15
51529568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4152
Checksum: 307
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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