[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 31st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 3640)
---------------------------------------
Vector Time (GMT): 2012/030/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1652199
82 A = 6772752
34 meter
Y = -5882471
17 meter E =
0019759
Z = 2937858
09 I = 51
99354
XDOT = 4382
156198 Wp = 25
29580
YDOT = -3761
725559 meter/sec RA = 96
38202 deg
ZDOT = -5037
776145 TA = 121
34030
MA = 121
14677
Ha = 219
240 n
mi
Hp = 204
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5420603
09 X = -1600569
34
Y = -19299446
09 feet Y = -5900658
41 meter
Z = 9638642
04 Z = 2929957
27
XDOT = 14377
152879 XDOT = 4448
366968
YDOT = -12341
619288 feet/sec YDOT = -3712
351373 meter/sec
ZDOT = -16528
136958 ZDOT = -5016
327263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -227732
89 X = -69412
98
Y = -20060279
07 feet Y = -6114373
06 meter
Z = 9606680
95 Z = 2928116
35
XDOT = 15743
773305 XDOT = 4798
702103
YDOT = -8098
758737 feet/sec YDOT = -2468
501663 meter/sec
ZDOT = -16439
934384 ZDOT = -5010
892000
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 12030
63905341
00016717 00000-0 10270-3 0 9004
2 25544 51
6405 97
0429 0020294 346
6782 13
3834 15
58588010 36414
Satellite: ISS
Catalog Number: 25544
Epoch time: 12030
63905341 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 97
0429 deg
Eccentricity:
0020294
Arg of perigee: 346
6782 deg
Mean anomaly: 13
3834 deg
Mean motion: 15
58588010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3641
Checksum: 292
Coasting Arc #2 (Orbit 3656)
---------------------------------------
Vector Time (GMT): 2012/031/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -239429
03 A = 6776390
58 meter
Y = 6752078
48 meter E =
0029094
Z = 93510
56 I = 52
00881
XDOT = -4728
835394 Wp = 10
94415
YDOT = -255
475080 meter/sec RA = 91
41149 deg
ZDOT = 6060
771963 TA = 350
06201
MA = 350
11943
Ha = 219
436 n
mi
Hp = 204
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -785528
32 X = -315368
58
Y = 22152488
44 feet Y = 6748976
43 meter
Z = 306793
17 Z = 92163
08
XDOT = -15514
551819 XDOT = -4755
068690
YDOT = -838
172834 feet/sec YDOT = -308
502596 meter/sec
ZDOT = 19884
422452 ZDOT = 6037
736033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6202403
05 X = -1890492
45
Y = 21281063
34 feet Y = 6486468
11 meter
Z = 300766
09 Z = 91673
50
XDOT = -13398
907936 XDOT = -4083
987139
YDOT = -4197
989402 feet/sec YDOT = -1279
547170 meter/sec
ZDOT = 19790
002277 ZDOT = 6031
992694
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 12031
66494562
00016717 00000-0 10270-3 0 9017
2 25544 51
6413 91
8942 0020345 350
6266 9
4506 15
58595335 36571
Satellite: ISS
Catalog Number: 25544
Epoch time: 12031
66494562 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 91
8942 deg
Eccentricity:
0020345
Arg of perigee: 350
6266 deg
Mean anomaly: 9
4506 deg
Mean motion: 15
58595335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3657
Checksum: 312
Coasting Arc #3 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2012/032/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2090686
85 A = 6772161
23 meter
Y = -5649373
77 meter E =
0019160
Z = -3119258
70 I = 51
99456
XDOT = 4097
664743 Wp = 6
86699
YDOT = 4229
075847 meter/sec RA = 86
43931 deg
ZDOT = -4897
511420 TA = 208
83536
MA = 208
94138
Ha = 219
513 n
mi
Hp = 204
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6859208
84 X = 2168856
37
Y = -18534690
86 feet Y = -5625557
27 meter
Z = -10233788
40 Z = -3108912
64
XDOT = 13443
781966 XDOT = 4073
860533
YDOT = 13874
920759 feet/sec YDOT = 4274
765487 meter/sec
ZDOT = -16067
950853 ZDOT = -4877
663105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10978772
70 X = 3346329
92
Y = -16459805
91 feet Y = -5016948
84 meter
Z = -10190940
86 Z = -3106198
77
XDOT = 8806
817625 XDOT = 2684
318012
YDOT = 15803
784645 feet/sec YDOT = 4816
993560 meter/sec
ZDOT = -15986
897718 ZDOT = -4872
806424
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 12032
62669733
00016717 00000-0 10270-3 0 9029
2 25544 51
6410 87
0669 0020306 354
2831 5
8090 15
58634623 36725
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
62669733 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 87
0669 deg
Eccentricity:
0020306
Arg of perigee: 354
2831 deg
Mean anomaly: 5
8090 deg
Mean motion: 15
58634623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3672
Checksum: 298
Coasting Arc #4 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2012/033/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3558319
65 A = 6765453
85 meter
Y = 2781839
47 meter E =
0017597
Z = 5028266
91 I = 51
96858
XDOT = -2624
715159 Wp = 13
70538
YDOT = -6939
254322 meter/sec RA = 81
43459 deg
ZDOT = 1996
906530 TA = 57
11221
MA = 56
94300
Ha = 219
770 n
mi
Hp = 203
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11674277
06 X = -3613588
10
Y = 9126769
93 feet Y = 2741738
95 meter
Z = 16496938
67 Z = 5010846
86
XDOT = -8611
270207 XDOT = -2556
624332
YDOT = -22766
582422 feet/sec YDOT = -6968
224856 meter/sec
ZDOT = 6551
530610 ZDOT = 1984
321115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13441848
37 X = -4097075
38
Y = 6423544
49 feet Y = 1957896
36 meter
Z = 16425299
03 Z = 5006431
14
XDOT = -3158
350657 XDOT = -962
665280
YDOT = -23102
668197 feet/sec YDOT = -7041
693266 meter/sec
ZDOT = 6500
468534 ZDOT = 1981
342809
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 12033
65254418
00016717 00000-0 10270-3 0 9034
2 25544 51
6401 81
9170 0020366 358
3682 1
7403 15
58662398 36880
Satellite: ISS
Catalog Number: 25544
Epoch time: 12033
65254418 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 81
9170 deg
Eccentricity:
0020366
Arg of perigee: 358
3682 deg
Mean anomaly: 1
7403 deg
Mean motion: 15
58662398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 308
Coasting Arc #5 (Orbit 3702)
---------------------------------------
Vector Time (GMT): 2012/034/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4331797
42 A = 6764972
68 meter
Y = 797816
72 meter E =
0022358
Z = -5142263
11 I = 51
96199
XDOT = 510
929910 Wp = 38
17343
YDOT = 7480
679268 meter/sec RA = 76
41070 deg
ZDOT = 1611
851278 TA = 247
18492
MA = 247
42123
Ha = 219
852 n
mi
Hp = 203
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14211933
80 X = 4347533
63
Y = 2617508
94 feet Y = 846345
74 meter
Z = -16870941
96 Z = -5121181
56
XDOT = 1676
279233 XDOT = 419
411615
YDOT = 24542
910983 feet/sec YDOT = 7485
881030 meter/sec
ZDOT = 5288
225977 ZDOT = 1614
111309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13527917
21 X = 4123309
17
Y = 5360313
43 feet Y = 1633823
53 meter
Z = -16784564
15 Z = -5115935
15
XDOT = -2787
408174 XDOT = -849
602011
YDOT = 23405
556886 feet/sec YDOT = 7134
013739 meter/sec
ZDOT = 5296
901864 ZDOT = 1614
495688
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 12034
61425385
00016717 00000-0 10270-3 0 9045
2 25544 51
6406 77
0907 0020419 1
6480 358
4739 15
58681705 37037
Satellite: ISS
Catalog Number: 25544
Epoch time: 12034
61425385 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 77
0907 deg
Eccentricity:
0020419
Arg of perigee: 1
6480 deg
Mean anomaly: 358
4739 deg
Mean motion: 15
58681705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3703
Checksum: 306
Coasting Arc #6 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2012/035/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4170224
16 A = 6771148
37 meter
Y = -4149044
37 meter E =
0024856
Z = 3362006
48 I = 51
97431
XDOT = 1925
127405 Wp = 35
56805
YDOT = -5758
804103 meter/sec RA = 71
40093 deg
ZDOT = -4681
948090 TA = 105
38912
MA = 105
11438
Ha = 219
856 n
mi
Hp = 203
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13681837
79 X = -4139850
28
Y = -13612350
28 feet Y = -4195508
67 meter
Z = 11030204
99 Z = 3341821
79
XDOT = 6316
034792 XDOT = 2012
123772
YDOT = -18893
714250 feet/sec YDOT = -5736
789555 meter/sec
ZDOT = -15360
722080 ZDOT = -4672
385009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11101223
76 X = -3383653
00
Y = -15844979
39 feet Y = -4829549
72 meter
Z = 10947769
04 Z = 3336880
00
XDOT = 8519
888967 XDOT = 2596
862157
YDOT = -16639
558690 feet/sec YDOT = -5071
737489 meter/sec
ZDOT = -15321
047641 ZDOT = -4669
855321
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 12035
64005415
00016717 00000-0 10270-3 0 9058
2 25544 51
6396 71
9402 0020546 5
4744 354
6632 15
58766167 37197
Satellite: ISS
Catalog Number: 25544
Epoch time: 12035
64005415 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 71
9402 deg
Eccentricity:
0020546
Arg of perigee: 5
4744 deg
Mean anomaly: 354
6632 deg
Mean motion: 15
58766167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3719
Checksum: 309
Coasting Arc #7 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2012/036/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2975840
67 A = 6775702
09 meter
Y = 6053750
01 meter E =
0030503
Z = -391756
79 I = 51
97914
XDOT = -4108
192822 Wp = 21
01706
YDOT = 2399
398418 meter/sec RA = 66
42523 deg
ZDOT = 6043
120917 TA = 334
76238
MA = 334
91111
Ha = 219
850 n
mi
Hp = 202
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9763256
78 X = 2909828
27
Y = 19861384
56 feet Y = 6086658
61 meter
Z = -1285291
31 Z = -377460
87
XDOT = -13478
322906 XDOT = -4164
073409
YDOT = 7872
042054 feet/sec YDOT = 2353
145501 meter/sec
ZDOT = 19826
512195 ZDOT = 6023
028336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6438262
94 X = 1962382
54
Y = 21177596
92 feet Y = 6454931
54 meter
Z = -1227156
26 Z = -374037
23
XDOT = -13146
221932 XDOT = -4006
968445
YDOT = 5106
443273 feet/sec YDOT = 1556
443910 meter/sec
ZDOT = 19743
924575 ZDOT = 6017
948211
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 12036
60172184
00016717 00000-0 10270-3 0 9064
2 25544 51
6394 67
1134 0020329 9
5394 350
6143 15
58812240 37343
Satellite: ISS
Catalog Number: 25544
Epoch time: 12036
60172184 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 67
1134 deg
Eccentricity:
0020329
Arg of perigee: 9
5394 deg
Mean anomaly: 350
6143 deg
Mean motion: 15
58812240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3734
Checksum: 291
Coasting Arc #8 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2012/037/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -863632
00 A = 6772467
67 meter
Y = -6131759
35 meter E =
0019647
Z = -2775194
60 I = 51
95461
XDOT = 5442
703730 Wp = 26
29411
YDOT = 1566
849591 meter/sec RA = 61
45145 deg
ZDOT = -5152
480750 TA = 184
99247
MA = 185
01209
Ha = 220
038 n
mi
Hp = 202
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2833438
33 X = -781520
37
Y = -20117320
72 feet Y = -6140957
91 meter
Z = -9104969
15 Z = -2779190
52
XDOT = 17856
639533 XDOT = 5449
807274
YDOT = 5140
582647 feet/sec YDOT = 1627
752971 meter/sec
ZDOT = -16904
464404 ZDOT = -5126
023834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 154934
32 X = 47223
98
Y = -20308160
01 feet Y = -6189927
17 meter
Z = -9120858
59 Z = -2780037
70
XDOT = 15548
003068 XDOT = 4739
031335
YDOT = 7666
846382 feet/sec YDOT = 2336
854777 meter/sec
ZDOT = -16796
095731 ZDOT = -5119
449979
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 12037
62747681
00016717 00000-0 10270-3 0 9078
2 25544 51
6387 61
9622 0020564 13
2923 346
8770 15
58808984 37501
Satellite: ISS
Catalog Number: 25544
Epoch time: 12037
62747681 = yrday
fracday
Element set: 907
Inclination: 51
6387 deg
RA of node: 61
9622 deg
Eccentricity:
0020564
Arg of perigee: 13
2923 deg
Mean anomaly: 346
8770 deg
Mean motion: 15
58808984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3750
Checksum: 333
Coasting Arc #9 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2012/038/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1729696
99 A = 6765427
52 meter
Y = 4325518
98 meter E =
0019896
Z = 4890193
62 I = 51
91560
XDOT = -5461
315545 Wp = 35
28296
YDOT = -4861
158806 meter/sec RA = 56
44665 deg
ZDOT = 2379
190366 TA = 31
62710
MA = 31
50769
Ha = 220
153 n
mi
Hp = 202
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5674858
90 X = -1801692
03
Y = 14191335
23 feet Y = 4305774
02 meter
Z = 16043942
32 Z = 4881616
09
XDOT = -17917
701920 XDOT = -5418
108436
YDOT = -15948
683748 feet/sec YDOT = -4921
988954 meter/sec
ZDOT = 7805
742670 ZDOT = 2352
765380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7531898
87 X = -2295722
77
Y = 13341935
80 feet Y = 4066622
03 meter
Z = 16008415
06 Z = 4879364
91
XDOT = -14815
349822 XDOT = -4515
718626
YDOT = -17556
271458 feet/sec YDOT = -5351
151540 meter/sec
ZDOT = 7697
771927 ZDOT = 2346
280883
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 12038
65320644
00016717 00000-0 10270-3 0 9089
2 25544 51
6384 56
8119 0020548 16
6019 343
5805 15
58850681 37668
Satellite: ISS
Catalog Number: 25544
Epoch time: 12038
65320644 = yrday
fracday
Element set: 908
Inclination: 51
6384 deg
RA of node: 56
8119 deg
Eccentricity:
0020548
Arg of perigee: 16
6019 deg
Mean anomaly: 343
5805 deg
Mean motion: 15
58850681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 321
Coasting Arc #10 (Orbit 3780)
---------------------------------------
Vector Time (GMT): 2012/039/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4084561
17 A = 6764165
36 meter
Y = -1434819
13 meter E =
0026947
Z = -5212083
22 I = 51
89373
XDOT = 3884
784111 Wp = 50
94454
YDOT = 6480
487990 meter/sec RA = 51
41581 deg
ZDOT = 1281
357977 TA = 231
20323
MA = 231
44420
Ha = 220
225 n
mi
Hp = 202
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13400791
25 X = 4125620
48
Y = -4707411
85 feet Y = -1388913
74 meter
Z = -17100010
58 Z = -5192141
35
XDOT = 12745
354696 XDOT = 3805
804891
YDOT = 21261
443537 feet/sec YDOT = 6523
488508 meter/sec
ZDOT = 4203
930371 ZDOT = 1300
037411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13941004
72 X = 4249218
24
Y = -3191151
38 feet Y = -972662
94 meter
Z = -17018114
90 Z = -5187121
42
XDOT = 10065
816888 XDOT = 3068
060988
YDOT = 21517
561000 feet/sec YDOT = 6558
552593 meter/sec
ZDOT = 4280
003637 ZDOT = 1304
545108
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 12039
61480619
00016717 00000-0 10270-3 0 9096
2 25544 51
6385 51
9834 0020586 20
4307 339
7667 15
58860457 37816
Satellite: ISS
Catalog Number: 25544
Epoch time: 12039
61480619 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 51
9834 deg
Eccentricity:
0020586
Arg of perigee: 20
4307 deg
Mean anomaly: 339
7667 deg
Mean motion: 15
58860457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3781
Checksum: 336
Coasting Arc #11 (Orbit 3796)
---------------------------------------
Vector Time (GMT): 2012/040/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5501487
74 A = 6770200
55 meter
Y = -1758730
22 meter E =
0028173
Z = 3533207
22 I = 51
89481
XDOT = -960
425461 Wp = 46
64655
YDOT = -6134
077781 meter/sec RA = 46
39703 deg
ZDOT = -4507
424053 TA = 91
81143
MA = 91
48873
Ha = 220
242 n
mi
Hp = 201
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18049500
47 X = -5498575
51
Y = -5770112
27 feet Y = -1820234
73 meter
Z = 11591887
20 Z = 3506489
06
XDOT = -3151
002168 XDOT = -869
866055
YDOT = -20124
927102 feet/sec YDOT = -6144
311807 meter/sec
ZDOT = -14788
136656 ZDOT = -4511
869273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17503578
74 X = -5335090
80
Y = -7431567
28 feet Y = -2265141
71 meter
Z = 11482467
11 Z = 3499855
97
XDOT = -1715
857965 XDOT = -522
993508
YDOT = -19046
974375 feet/sec YDOT = -5805
517789 meter/sec
ZDOT = -14805
862989 ZDOT = -4512
827039
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 12040
64048727
00016717 00000-0 10270-3 0 9103
2 25544 51
6386 46
8321 0020636 23
9891 336
2221 15
58928302 37972
Satellite: ISS
Catalog Number: 25544
Epoch time: 12040
64048727 = yrday
fracday
Element set: 910
Inclination: 51
6386 deg
RA of node: 46
8321 deg
Eccentricity:
0020636
Arg of perigee: 23
9891 deg
Mean anomaly: 336
2221 deg
Mean motion: 15
58928302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3797
Checksum: 309
Coasting Arc #12 (Orbit 3811)
---------------------------------------
Vector Time (GMT): 2012/041/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5335882
84 A = 6775200
89 meter
Y = 4108432
05 meter E =
0031364
Z = -571639
45 I = 51
89059
XDOT = -2512
736005 Wp = 32
23225
YDOT = 4075
958392 meter/sec RA = 41
41255 deg
ZDOT = 6016
259684 TA = 321
59683
MA = 321
81968
Ha = 220
251 n
mi
Hp = 201
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17506177
30 X = 5292321
80
Y = 13479107
77 feet Y = 4167857
58 meter
Z = -1875457
53 Z = -545824
58
XDOT = -8243
884530 XDOT = -2587
352522
YDOT = 13372
566902 feet/sec YDOT = 4047
442668 meter/sec
ZDOT = 19738
384791 ZDOT = 6003
871618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16442574
80 X = 5011696
80
Y = 14770882
64 feet Y = 4502165
03 meter
Z = -1769940
88 Z = -539477
98
XDOT = -8278
261285 XDOT = -2523
214040
YDOT = 11500
603430 feet/sec YDOT = 3505
383925 meter/sec
ZDOT = 19687
250321 ZDOT = 6000
673898
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 12041
60204062
00016717 00000-0 10270-3 0 9117
2 25544 51
6390 42
0039 0020580 27
9823 332
2434 15
58962024 38127
Satellite: ISS
Catalog Number: 25544
Epoch time: 12041
60204062 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 42
0039 deg
Eccentricity:
0020580
Arg of perigee: 27
9823 deg
Mean anomaly: 332
2434 deg
Mean motion: 15
58962024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3812
Checksum: 268
Coasting Arc #13 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2012/042/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3468803
24 A = 6772068
82 meter
Y = -5178732
52 meter E =
0021011
Z = -2682531
67 I = 51
85845
XDOT = 5521
885512 Wp = 44
45982
YDOT = -1006
534408 meter/sec RA = 36
43282 deg
ZDOT = -5207
302568 TA = 165
71434
MA = 165
65483
Ha = 220
259 n
mi
Hp = 201
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11380588
05 X = -3397604
86
Y = -16990592
24 feet Y = -5217124
90 meter
Z = -8800956
91 Z = -2699209
42
XDOT = 18116
422284 XDOT = 5558
025923
YDOT = -3302
278243 feet/sec YDOT = -944
583567 meter/sec
ZDOT = -17084
326012 ZDOT = -5180
390033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10308126
02 X = -3141916
81
Y = -17627813
98 feet Y = -5372957
70 meter
Z = -8868909
97 Z = -2703243
76
XDOT = 17097
049259 XDOT = 5211
180614
YDOT = -1474
327716 feet/sec YDOT = -449
375088 meter/sec
ZDOT = -16973
890289 ZDOT = -5173
641760
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 12042
62767192
00016717 00000-0 10270-3 0 9129
2 25544 51
6402 36
8525 0020659 31
4972 328
7416 15
59007498 38287
Satellite: ISS
Catalog Number: 25544
Epoch time: 12042
62767192 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 36
8525 deg
Eccentricity:
0020659
Arg of perigee: 31
4972 deg
Mean anomaly: 328
7416 deg
Mean motion: 15
59007498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 320
Coasting Arc #14 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2012/043/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 317424
94 A = 6764842
23 meter
Y = 4674003
55 meter E =
0021980
Z = 4860116
46 I = 51
81043
XDOT = -7007
571095 Wp = 52
68268
YDOT = -2042
958044 meter/sec RA = 31
42150 deg
ZDOT = 2427
943468 TA = 13
67044
MA = 13
61101
Ha = 220
184 n
mi
Hp = 200
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1041420
40 X = 241526
62
Y = 15334657
32 feet Y = 4677129
08 meter
Z = 15945263
99 Z = 4861473
88
XDOT = -22990
718816 XDOT = -6995
999779
YDOT = -6702
618253 feet/sec YDOT = -2121
256194 meter/sec
ZDOT = 7965
693794 ZDOT = 2393
929605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 305408
62 X = 93088
55
Y = 15361578
32 feet Y = 4682209
07 meter
Z = 15950434
24 Z = 4861692
36
XDOT = -21619
471542 XDOT = -6589
614926
YDOT = -7677
727294 feet/sec YDOT = -2340
171279 meter/sec
ZDOT = 7826
402278 ZDOT = 2385
487414
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 12043
65327552
00016717 00000-0 10270-3 0 9136
2 25544 51
6409 31
7025 0020429 35
1430 325
1069 15
59074259 38440
Satellite: ISS
Catalog Number: 25544
Epoch time: 12043
65327552 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 31
7025 deg
Eccentricity:
0020429
Arg of perigee: 35
1430 deg
Mean anomaly: 325
1069 deg
Mean motion: 15
59074259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 290
Coasting Arc #15 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2012/044/14:25:26
468
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3122088
36 A = 6763602
41 meter
Y = -3024364
93 meter E =
0029891
Z = -5202134
37 I = 51
77963
XDOT = 6243
977363 Wp = 62
60518
YDOT = 4240
681808 meter/sec RA = 26
38113 deg
ZDOT = 1301
080910 TA = 219
77219
MA = 219
99170
Ha = 220
304 n
mi
Hp = 200
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10243072
04 X = 3180945
91
Y = -9922457
12 feet Y = -2989122
89 meter
Z = -17067369
97 Z = -5186824
50
XDOT = 20485
490036 XDOT = 6189
772848
YDOT = 13912
998057 feet/sec YDOT = 4310
202779 meter/sec
ZDOT = 4268
638156 ZDOT = 1331
281761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10585867
14 X = 3226572
30
Y = -9667610
82 feet Y = -2946687
78 meter
Z = -17004338
15 Z = -5182922
27
XDOT = 19408
129027 XDOT = 5915
597727
YDOT = 13637
113999 feet/sec YDOT = 4156
592347 meter/sec
ZDOT = 4392
100820 ZDOT = 1338
712330
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 12044
61475711
00016717 00000-0 10270-3 0 9145
2 25544 51
6411 26
8734 0020559 38
7536 321
5090 15
59066902 38591
Satellite: ISS
Catalog Number: 25544
Epoch time: 12044
61475711 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 26
8734 deg
Eccentricity:
0020559
Arg of perigee: 38
7536 deg
Mean anomaly: 321
5090 deg
Mean motion: 15
59066902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 310
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