[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 18th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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
There are no maneuvers
Coasting Arc #1 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2012/261/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3945868
70 A = 6796748
65 meter
Y = -4391850
00 meter E =
0022439
Z = -3391959
25 I = 51
78119
XDOT = 5834
417183 Wp = 75
30043
YDOT = -1666
941342 meter/sec RA = 21
16400 deg
ZDOT = -4649
106710 TA = 144
04991
MA = 143
89875
Ha = 234
119 n
mi
Hp = 214
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12945763
44 X = -3879987
34
Y = -14408956
70 feet Y = -4435607
22 meter
Z = -11128475
23 Z = -3410967
69
XDOT = 19141
788658 XDOT = 5875
208137
YDOT = -5468
967656 feet/sec YDOT = -1601
469746 meter/sec
ZDOT = -15252
974771 ZDOT = -4620
663860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19317565
00 X = 5887993
81
Y = -545383
52 feet Y = -166232
90 meter
Z = -11206606
27 Z = -3415773
59
XDOT = -8267
207960 XDOT = -2519
844986
YDOT = 16817
879921 feet/sec YDOT = 5126
089800 meter/sec
ZDOT = -15135
172943 ZDOT = -4613
200713
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
67427639
00016717 00000-0 10270-3 0 9003
2 25544 51
6482 21
5602 0017789 71
8625 288
4461 15
49896651 32399
Satellite: ISS
Catalog Number: 25544
Epoch time: 12261
67427639 = yrday
fracday
Element set: 900
Inclination: 51
6482 deg
RA of node: 21
5602 deg
Eccentricity:
0017789
Arg of perigee: 71
8625 deg
Mean anomaly: 288
4461 deg
Mean motion: 15
49896651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 336
Coasting Arc #2 (Orbit 3254)
---------------------------------------
Vector Time (GMT): 2012/262/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4020943
99 A = 6796028
28 meter
Y = 4115342
30 meter E =
0029367
Z = 3587944
46 I = 51
75100
XDOT = -5955
307787 Wp = 82
12015
YDOT = 1918
222913 meter/sec RA = 16
21971 deg
ZDOT = 4446
634734 TA = 320
23988
MA = 320
45475
Ha = 234
038 n
mi
Hp = 214
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13192073
47 X = 3957196
91
Y = 13501779
18 feet Y = 4159950
94 meter
Z = 11771471
31 Z = 3607322
97
XDOT = -19538
411376 XDOT = -5997
916131
YDOT = 6293
382261 feet/sec YDOT = 1851
389174 meter/sec
ZDOT = 14588
696634 ZDOT = 4417
600102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18755307
93 X = -5716617
86
Y = 1638587
59 feet Y = 499441
50 meter
Z = 11851153
35 Z = 3612231
54
XDOT = 7641
204096 XDOT = 2329
039009
YDOT = -17822
826365 feet/sec YDOT = -5432
397476 meter/sec
ZDOT = 14468
424797 ZDOT = 4409
975878
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
70590770
00016717 00000-0 10270-3 0 9016
2 25544 51
6487 16
4508 0017801 75
3588 284
9535 15
49935253 32557
Satellite: ISS
Catalog Number: 25544
Epoch time: 12262
70590770 = yrday
fracday
Element set: 901
Inclination: 51
6487 deg
RA of node: 16
4508 deg
Eccentricity:
0017801
Arg of perigee: 75
3588 deg
Mean anomaly: 284
9535 deg
Mean motion: 15
49935253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3255
Checksum: 327
Coasting Arc #3 (Orbit 3269)
---------------------------------------
Vector Time (GMT): 2012/263/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4030953
38 A = 6795223
44 meter
Y = -3905864
28 meter E =
0024234
Z = -3855193
27 I = 51
71872
XDOT = 6041
619704 Wp = 77
19345
YDOT = -2144
556771 meter/sec RA = 11
27200 deg
ZDOT = -4161
218088 TA = 148
96412
MA = 148
82073
Ha = 234
143 n
mi
Hp = 214
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13224912
68 X = -3968249
72
Y = -12814515
37 feet Y = -3950590
64 meter
Z = -12648271
88 Z = -3874623
06
XDOT = 19821
586957 XDOT = 6085
366054
YDOT = -7035
947412 feet/sec YDOT = -2076
751354 meter/sec
ZDOT = -13652
290316 ZDOT = -4131
761389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18201270
62 X = 5547747
28
Y = -2407500
24 feet Y = -733806
07 meter
Z = -12728181
00 Z = -3879549
57
XDOT = -6954
096774 XDOT = -2119
608697
YDOT = 18666
957046 feet/sec YDOT = 5689
688508 meter/sec
ZDOT = -13530
250718 ZDOT = -4124
020419
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
67305264
00016717 00000-0 10270-3 0 9026
2 25544 51
6485 11
6598 0017920 78
6890 281
6273 15
49934200 32706
Satellite: ISS
Catalog Number: 25544
Epoch time: 12263
67305264 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 11
6598 deg
Eccentricity:
0017920
Arg of perigee: 78
6890 deg
Mean anomaly: 281
6273 deg
Mean motion: 15
49934200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3270
Checksum: 316
Coasting Arc #4 (Orbit 3285)
---------------------------------------
Vector Time (GMT): 2012/264/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4041219
01 A = 6794474
28 meter
Y = 3654883
13 meter E =
0028208
Z = 4034222
66 I = 51
68637
XDOT = -6135
703322 Wp = 89
07602
YDOT = 2434
493798 meter/sec RA = 6
32276 deg
ZDOT = 3917
547019 TA = 320
24512
MA = 320
45150
Ha = 234
061 n
mi
Hp = 214
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13258592
54 X = 3980451
44
Y = 11991086
39 feet Y = 3699735
04 meter
Z = 13235638
64 Z = 4053707
09
XDOT = -20130
260243 XDOT = -6181
501074
YDOT = 7987
184377 feet/sec YDOT = 2365
624710 meter/sec
ZDOT = 12852
844550 ZDOT = 3887
628347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17519607
43 X = -5339976
34
Y = 3242143
66 feet Y = 988205
39 meter
Z = 13315795
86 Z = 4058654
58
XDOT = 6096
213989 XDOT = 1858
126024
YDOT = -19647
482311 feet/sec YDOT = -5988
552609 meter/sec
ZDOT = 12728
863033 ZDOT = 3879
757452
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
70465957
00016717 00000-0 10270-3 0 9038
2 25544 51
6483 6
5502 0017968 82
1823 278
1367 15
49968929 32867
Satellite: ISS
Catalog Number: 25544
Epoch time: 12264
70465957 = yrday
fracday
Element set: 903
Inclination: 51
6483 deg
RA of node: 6
5502 deg
Eccentricity:
0017968
Arg of perigee: 82
1823 deg
Mean anomaly: 278
1367 deg
Mean motion: 15
49968929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3286
Checksum: 349
Coasting Arc #5 (Orbit 3300)
---------------------------------------
Vector Time (GMT): 2012/265/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3993174
17 A = 6793660
86 meter
Y = -3481047
06 meter E =
0026170
Z = -4278605
64 I = 51
65404
XDOT = 6183
111956 Wp = 80
02954
YDOT = -2694
853905 meter/sec RA = 1
36950 deg
ZDOT = -3592
491239 TA = 153
21073
MA = 153
07533
Ha = 234
140 n
mi
Hp = 214
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13100965
14 X = -3933166
95
Y = -11420758
07 feet Y = -3525365
91 meter
Z = -14037420
07 Z = -4297858
51
XDOT = 20285
800380 XDOT = 6230
238465
YDOT = -8841
384204 feet/sec YDOT = -2625
447167 meter/sec
ZDOT = -11786
388581 ZDOT = -3562
339144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16905155
86 X = 5152691
50
Y = -3748927
20 feet Y = -1142673
01 meter
Z = -14116636
11 Z = -4302750
69
XDOT = -5171
407231 XDOT = -1576
244924
YDOT = 20414
969634 feet/sec YDOT = 6222
482744 meter/sec
ZDOT = -11661
412328 ZDOT = -3554
398478
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
67178110
00016717 00000-0 10270-3 0 9048
2 25544 51
6488 1
7587 0018029 85
5303 274
7907 15
49973617 33011
Satellite: ISS
Catalog Number: 25544
Epoch time: 12265
67178110 = yrday
fracday
Element set: 904
Inclination: 51
6488 deg
RA of node: 1
7587 deg
Eccentricity:
0018029
Arg of perigee: 85
5303 deg
Mean anomaly: 274
7907 deg
Mean motion: 15
49973617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3301
Checksum: 323
Coasting Arc #6 (Orbit 3316)
---------------------------------------
Vector Time (GMT): 2012/266/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3947585
68 A = 6792926
97 meter
Y = 3271689
78 meter E =
0026788
Z = 4434493
29 I = 51
62063
XDOT = -6236
461548 Wp = 95
72741
YDOT = 3015
260378 meter/sec RA = 356
41484 deg
ZDOT = 3307
282230 TA = 320
83536
MA = 321
02892
Ha = 234
066 n
mi
Hp = 214
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12951396
60 X = 3889165
74
Y = 10733890
35 feet Y = 3315507
70 meter
Z = 14548862
51 Z = 4453528
50
XDOT = -20460
831852 XDOT = -6285
781389
YDOT = 9892
586542 feet/sec YDOT = 2945
244764 meter/sec
ZDOT = 10850
663484 ZDOT = 3276
865751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16189095
70 X = -4934436
37
Y = 4310759
43 feet Y = 1313919
47 meter
Z = 14627201
02 Z = 4458370
87
XDOT = 4078
468055 XDOT = 1243
117063
YDOT = -21293
035709 feet/sec YDOT = -6490
117284 meter/sec
ZDOT = 10724
558032 ZDOT = 3268
845288
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
70336362
00016717 00000-0 10270-3 0 9059
2 25544 51
6479 356
6487 0018125 88
9940 271
3288 15
50002873 33174
Satellite: ISS
Catalog Number: 25544
Epoch time: 12266
70336362 = yrday
fracday
Element set: 905
Inclination: 51
6479 deg
RA of node: 356
6487 deg
Eccentricity:
0018125
Arg of perigee: 88
9940 deg
Mean anomaly: 271
3288 deg
Mean motion: 15
50002873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3317
Checksum: 327
Coasting Arc #7 (Orbit 3331)
---------------------------------------
Vector Time (GMT): 2012/267/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3853412
44 A = 6792167
24 meter
Y = -3148407
59 meter E =
0028063
Z = -4648696
44 I = 51
58920
XDOT = 6231
963720 Wp = 83
84565
YDOT = -3297
480694 meter/sec RA = 351
45645 deg
ZDOT = -2944
974385 TA = 156
75408
MA = 156
62692
Ha = 234
103 n
mi
Hp = 214
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12642429
26 X = -3795337
59
Y = -10329421
24 feet Y = -3191174
39 meter
Z = -15251628
75 Z = -4667274
90
XDOT = 20446
075197 XDOT = 6282
679671
YDOT = -10818
506215 feet/sec YDOT = -3227
507579 meter/sec
ZDOT = -9661
989452 ZDOT = -2914
576442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15601943
70 X = 4755472
44
Y = -4557308
53 feet Y = -1389067
64 meter
Z = -15328092
90 Z = -4672002
72
XDOT = -2931
668118 XDOT = -893
572442
YDOT = 21900
203697 feet/sec YDOT = 6675
182087 meter/sec
ZDOT = -9535
930640 ZDOT = -2906
551659
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
67046155
00016717 00000-0 10270-3 0 9065
2 25544 51
6491 351
8572 0018082 92
4033 267
9188 15
50011114 33320
Satellite: ISS
Catalog Number: 25544
Epoch time: 12267
67046155 = yrday
fracday
Element set: 906
Inclination: 51
6491 deg
RA of node: 351
8572 deg
Eccentricity:
0018082
Arg of perigee: 92
4033 deg
Mean anomaly: 267
9188 deg
Mean motion: 15
50011114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3332
Checksum: 299
Coasting Arc #8 (Orbit 3347)
---------------------------------------
Vector Time (GMT): 2012/268/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3765451
12 A = 6791489
29 meter
Y = 2993939
12 meter E =
0025116
Z = 4774811
88 I = 51
55609
XDOT = -6232
960844 Wp = 101
84593
YDOT = 3635
201961 meter/sec RA = 346
49639 deg
ZDOT = 2619
259498 TA = 322
23891
MA = 322
41489
Ha = 234
022 n
mi
Hp = 214
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12353842
24 X = 3708497
52
Y = 9822634
90 feet Y = 3035728
63 meter
Z = 15665393
30 Z = 4792965
66
XDOT = -20449
346602 XDOT = -6285
870910
YDOT = 11926
515620 feet/sec YDOT = 3565
205453 meter/sec
ZDOT = 8593
371058 ZDOT = 2588
851383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14937838
62 X = -4553053
21
Y = 4859602
22 feet Y = 1481206
76 meter
Z = 15740119
61 Z = 4797588
46
XDOT = 1628
903101 XDOT = 496
489665
YDOT = -22594
993937 feet/sec YDOT = -6886
954152 meter/sec
ZDOT = 8467
236690 ZDOT = 2580
813743
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
70201977
00016717 00000-0 10270-3 0 9076
2 25544 51
6478 346
7468 0018192 95
8199 264
5026 15
50037513 33486
Satellite: ISS
Catalog Number: 25544
Epoch time: 12268
70201977 = yrday
fracday
Element set: 907
Inclination: 51
6478 deg
RA of node: 346
7468 deg
Eccentricity:
0018192
Arg of perigee: 95
8199 deg
Mean anomaly: 264
5026 deg
Mean motion: 15
50037513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3348
Checksum: 336
Coasting Arc #9 (Orbit 3362)
---------------------------------------
Vector Time (GMT): 2012/269/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3641520
05 A = 6790857
29 meter
Y = -2932235
68 meter E =
0029728
Z = -4951201
57 I = 51
52589
XDOT = 6167
436247 Wp = 88
58498
YDOT = -3922
766100 meter/sec RA = 341
53333 deg
ZDOT = -2223
764702 TA = 159
64868
MA = 159
52996
Ha = 234
034 n
mi
Hp = 214
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11947244
27 X = -3584408
81
Y = -9620195
79 feet Y = -2972638
55 meter
Z = -16244099
65 Z = -4968752
85
XDOT = 20234
370888 XDOT = 6221
645559
YDOT = -12869
967520 feet/sec YDOT = -3853
495082 meter/sec
ZDOT = -7295
815951 ZDOT = -2193
671666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14461860
88 X = 4407975
20
Y = -4877206
46 feet Y = -1486572
53 meter
Z = -16316342
22 Z = -4973221
11
XDOT = -306
000065 XDOT = -93
268820
YDOT = 22963
535007 feet/sec YDOT = 6999
285470 meter/sec
ZDOT = -7170
959469 ZDOT = -2185
708446
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
66909439
00016717 00000-0 10270-3 0 9081
2 25544 51
6490 341
9557 0018074 99
3058 261
0137 15
50044478 33638
Satellite: ISS
Catalog Number: 25544
Epoch time: 12269
66909439 = yrday
fracday
Element set: 908
Inclination: 51
6490 deg
RA of node: 341
9557 deg
Eccentricity:
0018074
Arg of perigee: 99
3058 deg
Mean anomaly: 261
0137 deg
Mean motion: 15
50044478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3363
Checksum: 333
Coasting Arc #10 (Orbit 3378)
---------------------------------------
Vector Time (GMT): 2012/270/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3528244
25 A = 6790278
41 meter
Y = 2841672
41 meter E =
0023299
Z = 5040713
40 I = 51
49442
XDOT = -6108
600315 Wp = 107
12521
YDOT = 4260
366454 meter/sec RA = 336
56811 deg
ZDOT = 1860
105673 TA = 324
75963
MA = 324
91346
Ha = 233
923 n
mi
Hp = 214
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11575604
51 X = 3471719
26
Y = 9323072
21 feet Y = 2880811
95 meter
Z = 16537773
61 Z = 5057715
79
XDOT = -20041
339617 XDOT = -6164
822564
YDOT = 13977
580229 feet/sec YDOT = 4191
742122 meter/sec
ZDOT = 6102
708901 ZDOT = 1830
293414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13927959
86 X = -4245242
17
Y = 4960504
59 feet Y = 1511961
80 meter
Z = 16607756
61 Z = 5062044
21
XDOT = -1151
494417 XDOT = -350
975498
YDOT = -23402
239825 feet/sec YDOT = -7133
002699 meter/sec
ZDOT = 5978
985547 ZDOT = 1822
394795
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
70062837
00016717 00000-0 10270-3 0 9091
2 25544 51
6476 336
8450 0018141 102
6959 257
6221 15
50071855 33791
Satellite: ISS
Catalog Number: 25544
Epoch time: 12270
70062837 = yrday
fracday
Element set: 909
Inclination: 51
6476 deg
RA of node: 336
8450 deg
Eccentricity:
0018141
Arg of perigee: 102
6959 deg
Mean anomaly: 257
6221 deg
Mean motion: 15
50071855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3379
Checksum: 316
Coasting Arc #11 (Orbit 3393)
---------------------------------------
Vector Time (GMT): 2012/271/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3394049
17 A = 6789840
66 meter
Y = -2847268
06 meter E =
0031001
Z = -5171807
69 I = 51
46586
XDOT = 5978
415898 Wp = 94
14044
YDOT = -4533
603736 meter/sec RA = 331
60044 deg
ZDOT = -1437
145405 TA = 161
99895
MA = 161
88893
Ha = 233
940 n
mi
Hp = 214
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11135331
92 X = -3336834
68
Y = -9341430
65 feet Y = -2884903
18 meter
Z = -16967873
00 Z = -5188156
51
XDOT = 19614
225388 XDOT = 6035
648600
YDOT = -14874
028004 feet/sec YDOT = -4466
429531 meter/sec
ZDOT = -4715
043979 ZDOT = -1407
962934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13632902
70 X = 4155308
74
Y = -4807723
82 feet Y = -1465394
22 meter
Z = -17035152
28 Z = -5192314
42
XDOT = 2576
101479 XDOT = 785
195731
YDOT = 23470
474560 feet/sec YDOT = 7153
800646 meter/sec
ZDOT = -4593
905348 ZDOT = -1400
222350
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
66768007
00016717 00000-0 10270-3 0 9101
2 25544 51
6480 332
0540 0018027 106
2061 254
1075 15
50074568 33941
Satellite: ISS
Catalog Number: 25544
Epoch time: 12271
66768007 = yrday
fracday
Element set: 910
Inclination: 51
6480 deg
RA of node: 332
0540 deg
Eccentricity:
0018027
Arg of perigee: 106
2061 deg
Mean anomaly: 254
1075 deg
Mean motion: 15
50074568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3394
Checksum: 286
Coasting Arc #12 (Orbit 3409)
---------------------------------------
Vector Time (GMT): 2012/272/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3274703
97 A = 6789409
64 meter
Y = 2824211
73 meter E =
0021560
Z = 5217882
75 I = 51
43730
XDOT = -5857
940531 Wp = 111
18743
YDOT = 4850
728545 meter/sec RA = 326
63038 deg
ZDOT = 1039
789145 TA = 328
77293
MA = 328
90083
Ha = 233
783 n
mi
Hp = 214
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10743779
42 X = 3217532
24
Y = 9265786
51 feet Y = 2860512
54 meter
Z = 17119037
90 Z = 5233651
94
XDOT = -19218
964998 XDOT = -5916
798094
YDOT = 15914
463730 feet/sec YDOT = 4784
892444 meter/sec
ZDOT = 3411
381710 ZDOT = 1011
187797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13290014
46 X = -4050796
41
Y = 4736391
20 feet Y = 1443652
04 meter
Z = 17183921
80 Z = 5237659
36
XDOT = -4106
216017 XDOT = -1251
574642
YDOT = -23599
519484 feet/sec YDOT = -7193
133539 meter/sec
ZDOT = 3292
622155 ZDOT = 1003
591233
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 12272
69918973
00016717 00000-0 10270-3 0 9115
2 25544 51
6466 326
9430 0018017 109
6278 250
6819 15
50105286 34109
Satellite: ISS
Catalog Number: 25544
Epoch time: 12272
69918973 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 326
9430 deg
Eccentricity:
0018017
Arg of perigee: 109
6278 deg
Mean anomaly: 250
6819 deg
Mean motion: 15
50105286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3410
Checksum: 318
Coasting Arc #13 (Orbit 3424)
---------------------------------------
Vector Time (GMT): 2012/273/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3151013
28 A = 6789212
86 meter
Y = -2896590
86 meter E =
0031725
Z = -5296760
65 I = 51
41153
XDOT = 5666
091223 Wp = 100
39067
YDOT = -5088
568365 meter/sec RA = 321
65803 deg
ZDOT = -596
641182 TA = 163
92505
MA = 163
82416
Ha = 233
824 n
mi
Hp = 214
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10337970
09 X = -3092658
11
Y = -9503250
85 feet Y = -2931501
88 meter
Z = -17377823
67 Z = -5311926
14
XDOT = 18589
538134 XDOT = 5725
469908
YDOT = -16694
778100 feet/sec YDOT = -5024
874671 meter/sec
ZDOT = -1957
484192 ZDOT = -568
970412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13222194
56 X = 4030124
90
Y = -4493003
24 feet Y = -1369467
39 meter
Z = -17440202
13 Z = -5315773
61
XDOT = 5535
645405 XDOT = 1687
264719
YDOT = 23332
843128 feet/sec YDOT = 7111
850585 meter/sec
ZDOT = -1842
556013 ZDOT = -561
611073
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 12273
66621870
00016717 00000-0 10270-3 0 9121
2 25544 51
6464 322
1516 0017965 113
0818 247
2228 15
50104513 34254
Satellite: ISS
Catalog Number: 25544
Epoch time: 12273
66621870 = yrday
fracday
Element set: 912
Inclination: 51
6464 deg
RA of node: 322
1516 deg
Eccentricity:
0017965
Arg of perigee: 113
0818 deg
Mean anomaly: 247
2228 deg
Mean motion: 15
50104513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3425
Checksum: 289
Coasting Arc #14 (Orbit 3440)
---------------------------------------
Vector Time (GMT): 2012/274/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3045347
95 A = 6788980
12 meter
Y = 2938448
85 meter E =
0020190
Z = 5292792
57 I = 51
38708
XDOT = -5488
814460 Wp = 113
75880
YDOT = 5363
849080 meter/sec RA = 316
68369 deg
ZDOT = 171
724787 TA = 334
55101
MA = 334
65030
Ha = 233
622 n
mi
Hp = 214
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9991299
04 X = 2986551
74
Y = 9640580
21 feet Y = 2972175
76 meter
Z = 17364805
01 Z = 5307443
72
XDOT = -18007
921456 XDOT = -5549
220402
YDOT = 17597
930051 feet/sec YDOT = 5302
132003 meter/sec
ZDOT = 563
401532 ZDOT = 144
912621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13105664
11 X = -3994606
42
Y = 4348845
96 feet Y = 1325528
25 meter
Z = 17425051
03 Z = 5311155
55
XDOT = -7036
485013 XDOT = -2144
720632
YDOT = -23127
715502 feet/sec YDOT = -7049
327685 meter/sec
ZDOT = 452
001458 ZDOT = 137
770044
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 12274
69770396
00016717 00000-0 10270-3 0 9134
2 25544 51
6455 317
0403 0017883 116
5989 243
6997 15
50138801 34416
Satellite: ISS
Catalog Number: 25544
Epoch time: 12274
69770396 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 317
0403 deg
Eccentricity:
0017883
Arg of perigee: 116
5989 deg
Mean anomaly: 243
6997 deg
Mean motion: 15
50138801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3441
Checksum: 334
Coasting Arc #15 (Orbit 3455)
---------------------------------------
Vector Time (GMT): 2012/275/15:34:39
949
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2952110
95 A = 6789049
27 meter
Y = -3070540
80 meter E =
0031743
Z = -5313354
48 I = 51
36563
XDOT = 5245
395909 Wp = 107
22145
YDOT = -5546
020705 meter/sec RA = 311
70713 deg
ZDOT = 282
859902 TA = 165
54113
MA = 165
45010
Ha = 233
678 n
mi
Hp = 214
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9685403
37 X = -2891744
62
Y = -10073952
75 feet Y = -3103216
24 meter
Z = -17432265
36 Z = -5327548
94
XDOT = 17209
304164 XDOT = 5305
648722
YDOT = -18195
605988 feet/sec YDOT = -5487
026488 meter/sec
ZDOT = 928
018052 ZDOT = 308
489203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13281151
36 X = 4048094
94
Y = -4106712
21 feet Y = -1251725
88 meter
Z = -17490608
09 Z = -5331137
35
XDOT = 8361
490831 XDOT = 2548
582405
YDOT = 22526
607559 feet/sec YDOT = 6866
109984 meter/sec
ZDOT = 1034
541826 ZDOT = 315
328349
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 12275
66471008
00016717 00000-0 10270-3 0 9141
2 25544 51
6453 312
2483 0017883 119
9736 240
3193 15
50137475 34560
Satellite: ISS
Catalog Number: 25544
Epoch time: 12275
66471008 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 312
2483 deg
Eccentricity:
0017883
Arg of perigee: 119
9736 deg
Mean anomaly: 240
3193 deg
Mean motion: 15
50137475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3456
Checksum: 315
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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