[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 9th 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) : 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 3779)
---------------------------------------
Vector Time (GMT): 2012/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1970552
12 A = 6764806
62 meter
Y = 3968533
42 meter E =
0019840
Z = 5097982
73 I = 51
89810
XDOT = -5604
142355 Wp = 34
41123
YDOT = -4974
311681 meter/sec RA = 51
95470 deg
ZDOT = 1718
801399 TA = 39
15472
MA = 39
01133
Ha = 220
408 n
mi
Hp = 202
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6465066
01 X = -2039546
78
Y = 13020122
77 feet Y = 3946111
97 meter
Z = 16725665
14 Z = 5088242
37
XDOT = -18386
293817 XDOT = -5556
451416
YDOT = -16319
920212 feet/sec YDOT = -5036
713917 meter/sec
ZDOT = 5639
112202 ZDOT = 1691
693551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13663984
12 X = -4164782
36
Y = 5095251
41 feet Y = 1553032
63 meter
Z = 16685397
83 Z = 5085709
26
XDOT = -2060
723150 XDOT = -628
108416
YDOT = -23492
717300 feet/sec YDOT = -7160
580233 meter/sec
ZDOT = 5528
352054 ZDOT = 1685
041706
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
55102448
00016717 00000-0 10270-3 0 9001
2 25544 51
6396 52
3132 0020532 20
4509 339
7464 15
58761355 37800
Satellite: ISS
Catalog Number: 25544
Epoch time: 12039
55102448 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 52
3132 deg
Eccentricity:
0020532
Arg of perigee: 20
4509 deg
Mean anomaly: 339
7464 deg
Mean motion: 15
58761355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3780
Checksum: 295
Coasting Arc #2 (Orbit 3794)
---------------------------------------
Vector Time (GMT): 2012/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4362662
91 A = 6765123
99 meter
Y = -1142760
42 meter E =
0025981
Z = -5055894
12 I = 51
88003
XDOT = 3860
756741 Wp = 52
81440
YDOT = 6336
506257 meter/sec RA = 46
92413 deg
ZDOT = 1921
245220 TA = 235
64172
MA = 235
88777
Ha = 220
455 n
mi
Hp = 202
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14313198
52 X = 4399677
05
Y = -3749213
98 feet Y = -1093767
81 meter
Z = -16587579
13 Z = -5034611
03
XDOT = 12666
524740 XDOT = 3780
280964
YDOT = 20789
062523 feet/sec YDOT = 6379
229780 meter/sec
ZDOT = 6303
297966 ZDOT = 1939
804266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13244270
39 X = 4036853
62
Y = 6812080
80 feet Y = 2076322
23 meter
Z = -16500208
96 Z = -5029263
69
XDOT = -3947
238964 XDOT = -1203
118436
YDOT = 22949
027293 feet/sec YDOT = 6994
863519 meter/sec
ZDOT = 6378
885428 ZDOT = 1944
284278
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
51267859
00016717 00000-0 10270-3 0 9018
2 25544 51
6401 47
4861 0020542 23
6269 336
5825 15
58764183 37954
Satellite: ISS
Catalog Number: 25544
Epoch time: 12040
51267859 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 47
4861 deg
Eccentricity:
0020542
Arg of perigee: 23
6269 deg
Mean anomaly: 336
5825 deg
Mean motion: 15
58764183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3795
Checksum: 316
Coasting Arc #3 (Orbit 3810)
---------------------------------------
Vector Time (GMT): 2012/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5723618
08 A = 6771667
93 meter
Y = -1868261
32 meter E =
0028199
Z = 3100531
90 I = 51
88030
XDOT = -768
160018 Wp = 52
47508
YDOT = -5854
054791 meter/sec RA = 41
91040 deg
ZDOT = -4898
232051 TA = 91
93756
MA = 91
61458
Ha = 220
465 n
mi
Hp = 201
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18778274
54 X = -5717362
81
Y = -6129466
27 feet Y = -1932231
14 meter
Z = 10172348
74 Z = 3072742
69
XDOT = -2520
210034 XDOT = -678
847663
YDOT = -19206
216507 feet/sec YDOT = -5862
145818 meter/sec
ZDOT = -16070
315127 ZDOT = -4901
746301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10251763
66 X = -3124737
56
Y = -16952803
00 feet Y = -5167214
36 meter
Z = 10058550
72 Z = 3065846
26
XDOT = 9484
940295 XDOT = 2891
009802
YDOT = -15371
956046 feet/sec YDOT = -4685
372203 meter/sec
ZDOT = -16084
242999 ZDOT = -4902
477266
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
53842645
00016717 00000-0 10270-3 0 9024
2 25544 51
6394 42
3347 0020657 27
3663 332
8575 15
58841052 38115
Satellite: ISS
Catalog Number: 25544
Epoch time: 12041
53842645 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 42
3347 deg
Eccentricity:
0020657
Arg of perigee: 27
3663 deg
Mean anomaly: 332
8575 deg
Mean motion: 15
58841052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3811
Checksum: 303
Coasting Arc #4 (Orbit 3825)
---------------------------------------
Vector Time (GMT): 2012/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5429188
47 A = 6775567
59 meter
Y = 4023840
63 meter E =
0032343
Z = -57971
89 I = 51
87073
XDOT = -2797
544073 Wp = 36
25487
YDOT = 3836
743197 meter/sec RA = 36
92978 deg
ZDOT = 6048
792371 TA = 323
12030
MA = 323
34229
Ha = 220
406 n
mi
Hp = 201
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17812298
13 X = 5384071
18
Y = 13201576
88 feet Y = 4084300
90 meter
Z = -190196
50 Z = -31707
40
XDOT = -9178
294204 XDOT = -2869
622623
YDOT = 12587
740149 feet/sec YDOT = 3805
056744 meter/sec
ZDOT = 19845
119328 ZDOT = 6035
026888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5223296
27 X = 1592060
70
Y = 21547762
89 feet Y = 6567758
13 meter
Z = -82836
86 Z = -25248
68
XDOT = -13632
908438 XDOT = -4155
310492
YDOT = 3330
506275 feet/sec YDOT = 1015
138312 meter/sec
ZDOT = 19788
355536 ZDOT = 6031
490767
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
50005134
00016717 00000-0 10270-3 0 9037
2 25544 51
6396 37
5077 0020459 31
4816 328
7559 15
58879152 38263
Satellite: ISS
Catalog Number: 25544
Epoch time: 12042
50005134 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 37
5077 deg
Eccentricity:
0020459
Arg of perigee: 31
4816 deg
Mean anomaly: 328
7559 deg
Mean motion: 15
58879152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3826
Checksum: 314
Coasting Arc #5 (Orbit 3841)
---------------------------------------
Vector Time (GMT): 2012/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3422817
71 A = 6771529
74 meter
Y = -4986261
43 meter E =
0022568
Z = -3078804
71 I = 51
83191
XDOT = 5791
122116 Wp = 45
43282
YDOT = -943
499980 meter/sec RA = 31
94592 deg
ZDOT = -4916
910781 TA = 169
80908
MA = 169
76325
Ha = 220
574 n
mi
Hp = 201
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11229716
89 X = -3351849
97
Y = -16359125
42 feet Y = -5024140
85 meter
Z = -10101065
32 Z = -3095259
76
XDOT = 18999
744474 XDOT = 5825
127083
YDOT = -3095
472374 feet/sec YDOT = -878
550223 meter/sec
ZDOT = -16131
597052 ZDOT = -4888
695447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1562988
62 X = 476398
93
Y = -19746533
32 feet Y = -6018743
35 meter
Z = -10168113
65 Z = -3099241
04
XDOT = 15375
870049 XDOT = 4686
565191
YDOT = 9452
762119 feet/sec YDOT = 2881
201894 meter/sec
ZDOT = -16015
827770 ZDOT = -4881
624304
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
52576775
00016717 00000-0 10270-3 0 9045
2 25544 51
6393 32
3563 0020666 35
0305 325
2205 15
58858170 38421
Satellite: ISS
Catalog Number: 25544
Epoch time: 12043
52576775 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 32
3563 deg
Eccentricity:
0020666
Arg of perigee: 35
0305 deg
Mean anomaly: 325
2205 deg
Mean motion: 15
58858170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 300
Coasting Arc #6 (Orbit 3857)
---------------------------------------
Vector Time (GMT): 2012/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 178048
69 A = 6764734
98 meter
Y = 4517770
35 meter E =
0021755
Z = 5013028
93 I = 51
78294
XDOT = -7185
660019 Wp = 52
95802
YDOT = -1903
473446 meter/sec RA = 26
92857 deg
ZDOT = 1977
577270 TA = 17
97981
MA = 17
90298
Ha = 220
607 n
mi
Hp = 200
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 584149
24 X = 103164
93
Y = 14822081
21 feet Y = 4519342
88 meter
Z = 16446945
30 Z = 5013711
82
XDOT = -23575
000063 XDOT = -7173
447469
YDOT = -6244
991620 feet/sec YDOT = -1983
759572 meter/sec
ZDOT = 6488
114404 ZDOT = 1942
699746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8715020
58 X = -2656338
27
Y = 12000182
13 feet Y = 3657655
51 meter
Z = 16449357
93 Z = 5013764
30
XDOT = -13935
859398 XDOT = -4247
649944
YDOT = -18787
418121 feet/sec YDOT = -5726
405043 meter/sec
ZDOT = 6345
275578 ZDOT = 1934
039996
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
55146617
00016717 00000-0 10270-3 0 9058
2 25544 51
6392 27
2063 0020605 38
3361 321
9255 15
58888850 38582
Satellite: ISS
Catalog Number: 25544
Epoch time: 12044
55146617 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 27
2063 deg
Eccentricity:
0020605
Arg of perigee: 38
3361 deg
Mean anomaly: 321
9255 deg
Mean motion: 15
58888850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3858
Checksum: 314
Coasting Arc #7 (Orbit 3872)
---------------------------------------
Vector Time (GMT): 2012/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3275046
01 A = 6764533
16 meter
Y = -3023382
07 meter E =
0029512
Z = -5108259
15 I = 51
75464
XDOT = 6313
021114 Wp = 64
88348
YDOT = 3986
869624 meter/sec RA = 21
88803 deg
ZDOT = 1707
698486 TA = 221
49661
MA = 221
72106
Ha = 220
683 n
mi
Hp = 200
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10744901
60 X = 3333425
15
Y = -9919232
52 feet Y = -2986432
14 meter
Z = -16759380
40 Z = -5092207
46
XDOT = 20712
011530 XDOT = 6259
674421
YDOT = 13080
280919 feet/sec YDOT = 4057
167462 meter/sec
ZDOT = 5602
685322 ZDOT = 1738
236878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14629348
46 X = 4459025
41
Y = -1427114
60 feet Y = -434984
53 meter
Z = -16693304
74 Z = -5088119
29
XDOT = 8587
842176 XDOT = 2617
574295
YDOT = 21804
965758 feet/sec YDOT = 6646
153563 meter/sec
ZDOT = 5727
548190 ZDOT = 1745
756688
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 12045
51304313
00016717 00000-0 10270-3 0 9065
2 25544 51
6395 22
3782 0020656 42
0133 318
2602 15
58887834 38737
Satellite: ISS
Catalog Number: 25544
Epoch time: 12045
51304313 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 22
3782 deg
Eccentricity:
0020656
Arg of perigee: 42
0133 deg
Mean anomaly: 318
2602 deg
Mean motion: 15
58887834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 296
Coasting Arc #8 (Orbit 3888)
---------------------------------------
Vector Time (GMT): 2012/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5893750
32 A = 6771059
34 meter
Y = 859860
34 meter E =
0030759
Z = 3212411
81 I = 51
74829
XDOT = -3362
876349 Wp = 63
26277
YDOT = -4966
661762 meter/sec RA = 16
86348 deg
ZDOT = -4791
497193 TA = 79
54536
MA = 79
19889
Ha = 220
694 n
mi
Hp = 200
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19336451
17 X = -5918532
35
Y = 2821064
09 feet Y = 793814
22 meter
Z = 10539408
82 Z = 3183720
46
XDOT = -11033
058887 XDOT = -3283
812535
YDOT = -16294
822055 feet/sec YDOT = -5003
825440 meter/sec
ZDOT = -15720
135149 ZDOT = -4807
641621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17371160
57 X = -5294729
74
Y = -9086632
84 feet Y = -2769605
69 meter
Z = 10421697
02 Z = 3176533
25
XDOT = 29
151305 XDOT = 8
885318
YDOT = -18347
028776 feet/sec YDOT = -5592
174371 meter/sec
ZDOT = -15785
892257 ZDOT = -4811
539960
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 12046
53870727
00016717 00000-0 10270-3 0 9076
2 25544 51
6394 17
2270 0020667 45
5215 314
7625 15
58948351 38897
Satellite: ISS
Catalog Number: 25544
Epoch time: 12046
53870727 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 17
2270 deg
Eccentricity:
0020667
Arg of perigee: 45
5215 deg
Mean anomaly: 314
7625 deg
Mean motion: 15
58948351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 327
Coasting Arc #9 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2012/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6640362
98 A = 6775272
74 meter
Y = 1259069
50 meter E =
0032498
Z = -169801
23 I = 51
73344
XDOT = -756
707189 Wp = 47
23704
YDOT = 4703
309174 meter/sec RA = 11
87185 deg
ZDOT = 6032
388615 TA = 310
92983
MA = 311
21074
Ha = 220
658 n
mi
Hp = 200
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21785967
79 X = 6626615
13
Y = 4130805
46 feet Y = 1333249
27 meter
Z = -557090
66 Z = -137576
66
XDOT = -2482
635135 XDOT = -838
547711
YDOT = 15430
804376 feet/sec YDOT = 4694
389578 meter/sec
ZDOT = 19791
301229 ZDOT = 6028
513878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15505934
28 X = 4726208
77
Y = 15855207
57 feet Y = 4832667
27 meter
Z = -425077
98 Z = -129563
77
XDOT = -9808
386907 XDOT = -2989
596329
YDOT = 10036
047253 feet/sec YDOT = 3058
987203 meter/sec
ZDOT = 19774
999302 ZDOT = 6027
419787
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 12047
50025165
00016717 00000-0 10270-3 0 9083
2 25544 51
6395 12
3991 0020633 49
5618 310
7333 15
58977311 39046
Satellite: ISS
Catalog Number: 25544
Epoch time: 12047
50025165 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 12
3991 deg
Eccentricity:
0020633
Arg of perigee: 49
5618 deg
Mean anomaly: 310
7333 deg
Mean motion: 15
58977311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 303
Coasting Arc #10 (Orbit 3919)
---------------------------------------
Vector Time (GMT): 2012/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5254944
66 A = 6771210
93 meter
Y = -3043180
60 meter E =
0023576
Z = -3027726
77 I = 51
69123
XDOT = 4783
714007 Wp = 61
36588
YDOT = -3358
208670 meter/sec RA = 6
87865 deg
ZDOT = -4945
520967 TA = 153
29015
MA = 153
16852
Ha = 220
660 n
mi
Hp = 200
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17240632
07 X = -5205816
98
Y = -9984188
32 feet Y = -3101669
95 meter
Z = -9933486
79 Z = -3053135
11
XDOT = 15694
599761 XDOT = 4844
934282
YDOT = -11017
744979 feet/sec YDOT = -3304
371940 meter/sec
ZDOT = -16225
462489 ZDOT = -4922
133753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8685173
04 X = -2647240
74
Y = -17872213
87 feet Y = -5447450
79 meter
Z = -10037395
64 Z = -3059398
19
XDOT = 17950
659003 XDOT = 5471
360864
YDOT = 302
005276 feet/sec YDOT = 92
051208 meter/sec
ZDOT = -16129
275593 ZDOT = -4916
203201
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 12048
52588093
00016717 00000-0 10270-3 0 9091
2 25544 51
6404 7
2475 0020684 52
9070 307
3972 15
59003009 39207
Satellite: ISS
Catalog Number: 25544
Epoch time: 12048
52588093 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 7
2475 deg
Eccentricity:
0020684
Arg of perigee: 52
9070 deg
Mean anomaly: 307
3972 deg
Mean motion: 15
59003009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 302
Coasting Arc #11 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2012/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2101763
13 A = 6764272
28 meter
Y = 4022875
71 meter E =
0023257
Z = 4994189
98 I = 51
63856
XDOT = -7308
878183 Wp = 69
26352
YDOT = 1343
223293 meter/sec RA = 1
85130 deg
ZDOT = 1994
503236 TA = 1
43526
MA = 1
42860
Ha = 220
516 n
mi
Hp = 200
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6895548
34 X = 2032362
35
Y = 13198411
12 feet Y = 4045990
97 meter
Z = 16385137
73 Z = 5004231
32
XDOT = -23979
259131 XDOT = -7333
043745
YDOT = 4406
900567 feet/sec YDOT = 1261
355832 meter/sec
ZDOT = 6543
645787 ZDOT = 1958
939297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1471781
97 X = -448599
15
Y = 14772989
87 feet Y = 4502807
31 meter
Z = 16425955
36 Z = 5006631
19
XDOT = -21477
861841 XDOT = -6546
452289
YDOT = -9251
124357 feet/sec YDOT = -2819
742704 meter/sec
ZDOT = 6397
711220 ZDOT = 1950
022380
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 12049
55149068
00016717 00000-0 10270-3 0 9102
2 25544 51
6408 2
0975 0020450 56
6411 303
6698 15
59056756 39368
Satellite: ISS
Catalog Number: 25544
Epoch time: 12049
55149068 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 2
0975 deg
Eccentricity:
0020450
Arg of perigee: 56
6411 deg
Mean anomaly: 303
6698 deg
Mean motion: 15
59056756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 314
Coasting Arc #12 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2012/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1726414
48 A = 6764151
88 meter
Y = -4136425
15 meter E =
0031558
Z = -5090429
64 I = 51
60744
XDOT = 7392
760939 Wp = 76
37388
YDOT = 966
159851 meter/sec RA = 356
79838 deg
ZDOT = 1738
480155 TA = 210
37640
MA = 210
55964
Ha = 220
660 n
mi
Hp = 199
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5664089
50 X = 1797267
94
Y = -13570948
65 feet Y = -4116723
36 meter
Z = -16700884
66 Z = -5081870
79
XDOT = 24254
465022 XDOT = 7372
962805
YDOT = 3169
815784 feet/sec YDOT = 1048
719634 meter/sec
ZDOT = 5703
675048 ZDOT = 1774
344670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12073404
01 X = 3679973
54
Y = -8465717
29 feet Y = -2580350
63 meter
Z = -16665432
85 Z = -5079623
93
XDOT = 18256
466198 XDOT = 5564
570897
YDOT = 14624
707845 feet/sec YDOT = 4457
610951 meter/sec
ZDOT = 5850
638065 ZDOT = 1783
274482
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 12050
51298555
00016717 00000-0 10270-3 0 9117
2 25544 51
6411 357
2682 0020561 60
0938 300
2257 15
59036949 39511
Satellite: ISS
Catalog Number: 25544
Epoch time: 12050
51298555 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 357
2682 deg
Eccentricity:
0020561
Arg of perigee: 60
0938 deg
Mean anomaly: 300
2257 deg
Mean motion: 15
59036949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 302
Coasting Arc #13 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2012/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5032926
28 A = 6770836
73 meter
Y = 3244950
64 meter E =
0032403
Z = 3142245
56 I = 51
60055
XDOT = -5075
194312 Wp = 75
30803
YDOT = -3139
258615 meter/sec RA = 351
76349 deg
ZDOT = -4837
333339 TA = 68
32980
MA = 67
98504
Ha = 220
685 n
mi
Hp = 199
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16512225
32 X = -5084101
79
Y = 10646163
52 feet Y = 3188383
41 meter
Z = 10309204
61 Z = 3117672
05
XDOT = -16650
899974 XDOT = -5016
215304
YDOT = -10299
404905 feet/sec YDOT = -3195
683096 meter/sec
ZDOT = -15870
516204 ZDOT = -4861
844235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19690191
49 X = -6001570
36
Y = 602994
15 feet Y = 183792
62 meter
Z = 10208175
15 Z = 3111451
79
XDOT = -8852
608425 XDOT = -2698
275048
YDOT = -15913
227499 feet/sec YDOT = -4850
351742 meter/sec
ZDOT = -15970
739621 ZDOT = -4867
881437
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 12051
53856064
00016717 00000-0 10270-3 0 9126
2 25544 51
6417 352
1170 0020579 63
8843 296
4427 15
59084218 39672
Satellite: ISS
Catalog Number: 25544
Epoch time: 12051
53856064 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 352
1170 deg
Eccentricity:
0020579
Arg of perigee: 63
8843 deg
Mean anomaly: 296
4427 deg
Mean motion: 15
59084218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 322
Coasting Arc #14 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2012/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6574845
76 A = 6774937
35 meter
Y = -1586855
45 meter E =
0032110
Z = -49205
89 I = 51
58446
XDOT = 1142
021639 Wp = 58
86263
YDOT = 4635
453469 meter/sec RA = 346
76158 deg
ZDOT = 6019
677937 TA = 300
60539
MA = 300
92169
Ha = 220
635 n
mi
Hp = 199
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21571016
29 X = 6592340
67
Y = -5206218
67 feet Y = -1513233
65 meter
Z = -161436
65 Z = -17223
84
XDOT = 3746
790154 XDOT = 1060
860747
YDOT = 15208
180674 feet/sec YDOT = 4647
770957 meter/sec
ZDOT = 19749
599530 ZDOT = 6025
028162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21287377
74 X = 6488392
74
Y = 6267866
95 feet Y = 1910445
85 meter
Z = -30182
46 Z = -9199
61
XDOT = -4000
176351 XDOT = -1219
253752
YDOT = 13434
658897 feet/sec YDOT = 4094
884032 meter/sec
ZDOT = 19771
140105 ZDOT = 6026
243504
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 12052
50002059
00016717 00000-0 10270-3 0 9132
2 25544 51
6417 347
2887 0020530 67
4280 292
9045 15
59094551 39829
Satellite: ISS
Catalog Number: 25544
Epoch time: 12052
50002059 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 347
2887 deg
Eccentricity:
0020530
Arg of perigee: 67
4280 deg
Mean anomaly: 292
9045 deg
Mean motion: 15
59094551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 305
Coasting Arc #15 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2012/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5961568
60 A = 6770434
77 meter
Y = -680806
30 meter E =
0024647
Z = -3163804
45 I = 51
54161
XDOT = 3123
938734 Wp = 75
90925
YDOT = -5062
859855 meter/sec RA = 341
75688 deg
ZDOT = -4822
703726 TA = 140
64787
MA = 140
46852
Ha = 220
575 n
mi
Hp = 199
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19558952
11 X = -5938143
93
Y = -2233616
46 feet Y = -747341
57 meter
Z = -10379935
86 Z = -3192707
82
XDOT = 10249
142827 XDOT = 3203
747518
YDOT = -16610
432595 feet/sec YDOT = -5027
480282 meter/sec
ZDOT = -15822
518785 ZDOT = -4807
333794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15970123
64 X = -4867693
69
Y = -11402811
32 feet Y = -3475576
89 meter
Z = -10498369
56 Z = -3199903
04
XDOT = 16268
040717 XDOT = 4958
498811
YDOT = -8351
757414 feet/sec YDOT = -2545
615660 meter/sec
ZDOT = -15759
083239 ZDOT = -4803
368571
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 12053
52555968
00016717 00000-0 10270-3 0 9148
2 25544 51
6426 342
1371 0020559 71
2598 289
0786 15
59141219 39987
Satellite: ISS
Catalog Number: 25544
Epoch time: 12053
52555968 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 342
1371 deg
Eccentricity:
0020559
Arg of perigee: 71
2598 deg
Mean anomaly: 289
0786 deg
Mean motion: 15
59141219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 339
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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