[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 16th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13723 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 1485)
---------------------------------------
Vector Time (GMT): 2011/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4526599
93 A = 6760154
64 meter
Y = -1888370
28 meter E =
0009390
Z = 4644038
75 I = 51
95156
XDOT = -64
917948 Wp = 146
04966
YDOT = -7094
919678 meter/sec RA = 70
46586 deg
ZDOT = -2952
969553 TA = 333
13080
MA = 333
17941
Ha = 212
701 n
mi
Hp = 203
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14851049
62 X = -4527707
29
Y = -6195440
55 feet Y = -1938995
19 meter
Z = 15236347
62 Z = 4622046
02
XDOT = -212
985393 XDOT = 28
768664
YDOT = -23277
295533 feet/sec YDOT = -7095
122111 meter/sec
ZDOT = -9688
220317 ZDOT = -2953
056613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13981687
47 X = 4261618
34
Y = 8134425
09 feet Y = 2479372
77 meter
Z = 15146847
56 Z = 4616759
14
XDOT = -2361
721171 XDOT = -719
852613
YDOT = 22070
400601 feet/sec YDOT = 6727
058103 meter/sec
ZDOT = -9688
227717 ZDOT = -2952
971808
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 11257
54280186
00016717 00000-0 10270-3 0 9007
2 25544 51
6356 70
9735 0011572 191
6425 168
4465 15
61045659 14868
Satellite: ISS
Catalog Number: 25544
Epoch time: 11257
54280186 = yrday
fracday
Element set: 900
Inclination: 51
6356 deg
RA of node: 70
9735 deg
Eccentricity:
0011572
Arg of perigee: 191
6425 deg
Mean anomaly: 168
4465 deg
Mean motion: 15
61045659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 319
Coasting Arc #2 (Orbit 1500)
---------------------------------------
Vector Time (GMT): 2011/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3807910
93 A = 6768117
89 meter
Y = 5373478
04 meter E =
0005162
Z = -1574801
94 I = 51
96819
XDOT = -3166
567004 Wp = 156
67830
YDOT = 3935
167959 meter/sec RA = 65
45636 deg
ZDOT = 5772
412917 TA = 186
14911
MA = 186
15544
Ha = 212
376 n
mi
Hp = 203
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12493146
10 X = 3755190
77
Y = 17629521
14 feet Y = 5415765
51 meter
Z = -5166673
03 Z = -1556431
61
XDOT = -10388
999356 XDOT = -3238
376926
YDOT = 12910
656032 feet/sec YDOT = 3899
356509 meter/sec
ZDOT = 18938
362587 ZDOT = 5756
854873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10385830
31 X = -3165601
08
Y = -18967819
13 feet Y = -5781391
27 meter
Z = -5092110
71 Z = -1552075
34
XDOT = 10551
961295 XDOT = 3216
237803
YDOT = -10843
231005 feet/sec YDOT = -3305
016810 meter/sec
ZDOT = 18874
785165 ZDOT = 5753
034518
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 11258
50303289
00016717 00000-0 10270-3 0 9015
2 25544 51
6362 66
1348 0011586 194
6871 165
3950 15
61094450 15011
Satellite: ISS
Catalog Number: 25544
Epoch time: 11258
50303289 = yrday
fracday
Element set: 901
Inclination: 51
6362 deg
RA of node: 66
1348 deg
Eccentricity:
0011586
Arg of perigee: 194
6871 deg
Mean anomaly: 165
3950 deg
Mean motion: 15
61094450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1501
Checksum: 300
Coasting Arc #3 (Orbit 1516)
---------------------------------------
Vector Time (GMT): 2011/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1351732
76 A = 6766575
23 meter
Y = -6176414
74 meter E =
0014609
Z = -2386168
90 I = 51
95043
XDOT = 5380
999273 Wp = 178
07009
YDOT = 907
011883 meter/sec RA = 60
47456 deg
ZDOT = -5411
180931 TA = 28
57006
MA = 28
49008
Ha = 212
093 n
mi
Hp = 203
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4434818
76 X = -1270974
77
Y = -20263827
89 feet Y = -6191079
30 meter
Z = -7828638
13 Z = -2392538
99
XDOT = 17654
197091 XDOT = 5396
743652
YDOT = 2975
760770 feet/sec YDOT = 967
273095 meter/sec
ZDOT = -17753
218277 ZDOT = -5385
001719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2352521
63 X = 717048
59
Y = 20599856
73 feet Y = 6278836
33 meter
Z = -7854263
69 Z = -2393979
57
XDOT = -15875
277178 XDOT = -4838
784484
YDOT = -4896
356254 feet/sec YDOT = -1492
409386 meter/sec
ZDOT = -17646
622132 ZDOT = -5378
690426
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 11259
52726207
00016717 00000-0 10270-3 0 9028
2 25544 51
6368 60
9746 0011359 198
6779 161
3962 15
61137887 15178
Satellite: ISS
Catalog Number: 25544
Epoch time: 11259
52726207 = yrday
fracday
Element set: 902
Inclination: 51
6368 deg
RA of node: 60
9746 deg
Eccentricity:
0011359
Arg of perigee: 198
6779 deg
Mean anomaly: 161
3962 deg
Mean motion: 15
61137887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1517
Checksum: 340
Coasting Arc #4 (Orbit 1532)
---------------------------------------
Vector Time (GMT): 2011/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1933257
61 A = 6758338
23 meter
Y = 4112427
28 meter E =
0013872
Z = 5006318
96 I = 51
90691
XDOT = -5414
688164 Wp = 177
54481
YDOT = -5045
002268 meter/sec RA = 55
45180 deg
ZDOT = 2039
515824 TA = 252
64978
MA = 252
80155
Ha = 211
953 n
mi
Hp = 203
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6342708
68 X = -2003419
84
Y = 13492215
48 feet Y = 4090416
45 meter
Z = 16424930
96 Z = 4996756
43
XDOT = -17764
724948 XDOT = -5367
779189
YDOT = -16551
844711 feet/sec YDOT = -5105
290204 meter/sec
ZDOT = 6691
324881 ZDOT = 2013
325386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7529219
09 X = 2294905
98
Y = -12917665
85 feet Y = -3937304
55 meter
Z = 16385754
73 Z = 4994378
04
XDOT = 15441
570021 XDOT = 4706
590543
YDOT = 17410
398133 feet/sec YDOT = 5306
689351 meter/sec
ZDOT = 6584
909416 ZDOT = 2007
080390
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 11260
55147431
00016717 00000-0 10270-3 0 9030
2 25544 51
6367 55
8138 0011446 202
8673 157
1974 15
61147229 15338
Satellite: ISS
Catalog Number: 25544
Epoch time: 11260
55147431 = yrday
fracday
Element set: 903
Inclination: 51
6367 deg
RA of node: 55
8138 deg
Eccentricity:
0011446
Arg of perigee: 202
8673 deg
Mean anomaly: 157
1974 deg
Mean motion: 15
61147229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1533
Checksum: 302
Coasting Arc #5 (Orbit 1547)
---------------------------------------
Vector Time (GMT): 2011/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4708519
64 A = 6759011
01 meter
Y = -278470
32 meter E =
0015167
Z = -4851822
48 I = 51
89242
XDOT = 2958
932948 Wp = 155
88492
YDOT = 6628
142669 meter/sec RA = 50
39735 deg
ZDOT = 2480
338908 TA = 138
43692
MA = 138
32151
Ha = 211
795 n
mi
Hp = 203
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15447899
07 X = 4734853
01
Y = -913616
55 feet Y = -225669
80 meter
Z = -15918052
76 Z = -4828884
39
XDOT = 9707
785262 XDOT = 2872
546735
YDOT = 21745
874898 feet/sec YDOT = 6660
748389 meter/sec
ZDOT = 8137
594841 ZDOT = 2494
503292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15570132
13 X = -4745776
27
Y = -98941
12 feet Y = -30157
25 meter
Z = -15824597
33 Z = -4823337
27
XDOT = -8230
330602 XDOT = -2508
604767
YDOT = -21193
248688 feet/sec YDOT = -6459
702200 meter/sec
ZDOT = 8194
924918 ZDOT = 2497
813115
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 11261
51165675
00016717 00000-0 10270-3 0 9048
2 25544 51
6380 50
9764 0011436 205
8501 154
2085 15
61168940 15486
Satellite: ISS
Catalog Number: 25544
Epoch time: 11261
51165675 = yrday
fracday
Element set: 904
Inclination: 51
6380 deg
RA of node: 50
9764 deg
Eccentricity:
0011436
Arg of perigee: 205
8501 deg
Mean anomaly: 154
2085 deg
Mean motion: 15
61168940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 298
Coasting Arc #6 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2011/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5507777
70 A = 6767278
51 meter
Y = -3378347
39 meter E =
0016867
Z = 1973122
43 I = 51
89963
XDOT = 1130
268367 Wp = 154
30609
YDOT = -5125
244465 meter/sec RA = 45
37791 deg
ZDOT = -5617
304100 TA = 3
90813
MA = 3
89497
Ha = 211
614 n
mi
Hp = 204
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18070136
80 X = -5479176
11
Y = -11083816
88 feet Y = -3439778
72 meter
Z = 6473498
79 Z = 1946435
18
XDOT = 3708
229552 XDOT = 1214
783798
YDOT = -16815
106514 feet/sec YDOT = -5112
132811 meter/sec
ZDOT = -18429
475393 ZDOT = -5611
607721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17557233
13 X = 5351444
66
Y = 11938075
12 feet Y = 3638725
30 meter
Z = 6364978
75 Z = 1940045
52
XDOT = -3749
707121 XDOT = -1142
910731
YDOT = 15333
485290 feet/sec YDOT = 4673
646316 meter/sec
ZDOT = -18405
977812 ZDOT = -5610
142037
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 11262
53583319
00016717 00000-0 10270-3 0 9051
2 25544 51
6375 45
8154 0011417 210
1474 149
9026 15
61187970 15641
Satellite: ISS
Catalog Number: 25544
Epoch time: 11262
53583319 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 45
8154 deg
Eccentricity:
0011417
Arg of perigee: 210
1474 deg
Mean anomaly: 149
9026 deg
Mean motion: 15
61187970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 306
Coasting Arc #7 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2011/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3746931
86 A = 6766912
45 meter
Y = 5263686
84 meter E =
0008066
Z = 2014778
77 I = 51
87863
XDOT = -5056
462242 Wp = 123
30408
YDOT = 1453
364446 meter/sec RA = 40
39118 deg
ZDOT = 5586
243112 TA = 258
93090
MA = 259
02163
Ha = 211
268 n
mi
Hp = 204
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12293083
53 X = 3678006
36
Y = 17269313
79 feet Y = 5305202
02 meter
Z = 6610166
56 Z = 2032813
74
XDOT = -16589
443050 XDOT = -5099
475216
YDOT = 4768
256055 feet/sec YDOT = 1396
579720 meter/sec
ZDOT = 18327
569265 ZDOT = 5561
574267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11716983
08 X = -3571336
44
Y = -17637710
64 feet Y = -5375974
20 meter
Z = 6683328
06 Z = 2037078
39
XDOT = 15552
030525 XDOT = 4740
258904
YDOT = -3399
720817 feet/sec YDOT = -1036
234905 meter/sec
ZDOT = 18226
992875 ZDOT = 5555
587428
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 11263
55998986
00016717 00000-0 10270-3 0 9065
2 25544 51
6389 40
6549 0011436 213
8522 146
1906 15
61257123 15804
Satellite: ISS
Catalog Number: 25544
Epoch time: 11263
55998986 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 40
6549 deg
Eccentricity:
0011436
Arg of perigee: 213
8522 deg
Mean anomaly: 146
1906 deg
Mean motion: 15
61257123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 323
Coasting Arc #8 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2011/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 30321
54 A = 6758502
90 meter
Y = -4680607
35 meter E =
0007017
Z = -4877292
37 I = 51
82684
XDOT = 6836
996252 Wp = 138
73975
YDOT = 2538
530373 meter/sec RA = 35
36810 deg
ZDOT = -2400
764269 TA = 107
86177
MA = 107
78522
Ha = 211
024 n
mi
Hp = 204
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 99480
10 X = 106351
70
Y = -15356323
32 feet Y = -4679843
38 meter
Z = -16001615
40 Z = -4876960
19
XDOT = 22431
090064 XDOT = 6819
764214
YDOT = 8328
511723 feet/sec YDOT = 2614
889392 meter/sec
ZDOT = -7876
523193 ZDOT = -2367
592196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -403354
07 X = -122942
32
Y = 15353045
13 feet Y = 4679608
15 meter
Z = -15999986
52 Z = -4876795
89
XDOT = -21244
075965 XDOT = -6475
194354
YDOT = -8601
564814 feet/sec YDOT = -2621
756955 meter/sec
ZDOT = -7741
540989 ZDOT = -2359
621693
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 11264
52012166
00016717 00000-0 10270-3 0 9071
2 25544 51
6391 35
8174 0011230 218
1790 141
8571 15
61257963 15952
Satellite: ISS
Catalog Number: 25544
Epoch time: 11264
52012166 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 35
8174 deg
Eccentricity:
0011230
Arg of perigee: 218
1790 deg
Mean anomaly: 141
8571 deg
Mean motion: 15
61257963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 297
Coasting Arc #9 (Orbit 1610)
---------------------------------------
Vector Time (GMT): 2011/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4038213
26 A = 6758238
07 meter
Y = 2166988
33 meter E =
0005318
Z = 4967075
11 I = 51
80065
XDOT = -5349
808373 Wp = 202
01438
YDOT = -5077
324147 meter/sec RA = 30
30608 deg
ZDOT = -2139
842940 TA = 268
72152
MA = 268
78245
Ha = 210
897 n
mi
Hp = 204
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13248731
17 X = -4086273
85
Y = 7109541
76 feet Y = 2121562
12 meter
Z = 16296178
20 Z = 4947340
71
XDOT = -17551
864740 XDOT = -5282
240209
YDOT = -16657
887621 feet/sec YDOT = -5136
771305 meter/sec
ZDOT = -7020
482087 ZDOT = -2165
667765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13320380
13 X = 4060051
86
Y = -7159593
07 feet Y = -2182243
97 meter
Z = 16215658
67 Z = 4942532
76
XDOT = 17048
570005 XDOT = 5196
404138
YDOT = 15622
074531 feet/sec YDOT = 4761
608317 meter/sec
ZDOT = -7125
382712 ZDOT = -2171
816651
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 11265
54424418
00016717 00000-0 10270-3 0 9082
2 25544 51
6395 30
6562 0011118 221
5444 138
4869 15
61252498 16118
Satellite: ISS
Catalog Number: 25544
Epoch time: 11265
54424418 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 30
6562 deg
Eccentricity:
0011118
Arg of perigee: 221
5444 deg
Mean anomaly: 138
4869 deg
Mean motion: 15
61252498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1611
Checksum: 304
Coasting Arc #10 (Orbit 1625)
---------------------------------------
Vector Time (GMT): 2011/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6305610
66 A = 6766506
56 meter
Y = 1040821
16 meter E =
0004932
Z = -2225513
70 I = 51
80277
XDOT = 1067
052256 Wp = 230
70245
YDOT = 5269
119467 meter/sec RA = 25
27547 deg
ZDOT = 5476
412261 TA = 104
56027
MA = 104
50556
Ha = 210
483 n
mi
Hp = 204
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20687699
03 X = 6304314
42
Y = 3414767
57 feet Y = 1111326
94 meter
Z = -7301554
14 Z = -2194884
47
XDOT = 3500
827611 XDOT = 981
449369
YDOT = 17287
137358 feet/sec YDOT = 5280
573685 meter/sec
ZDOT = 17967
231829 ZDOT = 5481
387636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20798170
43 X = -6339282
35
Y = -2980474
76 feet Y = -908448
71 meter
Z = -7176844
61 Z = -2187502
24
XDOT = -3970
277703 XDOT = -1210
140644
YDOT = -15696
708096 feet/sec YDOT = -4784
356628 meter/sec
ZDOT = 17987
187062 ZDOT = 5482
494617
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 11266
50433863
00016717 00000-0 10270-3 0 9094
2 25544 51
6402 25
8176 0011077 226
2787 133
7453 15
61302485 16265
Satellite: ISS
Catalog Number: 25544
Epoch time: 11266
50433863 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 25
8176 deg
Eccentricity:
0011077
Arg of perigee: 226
2787 deg
Mean anomaly: 133
7453 deg
Mean motion: 15
61302485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1626
Checksum: 303
Coasting Arc #11 (Orbit 1641)
---------------------------------------
Vector Time (GMT): 2011/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5475393
68 A = 6767001
62 meter
Y = -3530796
77 meter E =
0013406
Z = -1795364
73 I = 51
77739
XDOT = 3988
381391 Wp = 196
65886
YDOT = -3296
834830 meter/sec RA = 20
28131 deg
ZDOT = -5682
005528 TA = 3
10630
MA = 3
09799
Ha = 210
170 n
mi
Hp = 205
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17963890
03 X = -5426783
16
Y = -11583978
89 feet Y = -3591754
35 meter
Z = -5890304
22 Z = -1821845
60
XDOT = 13085
240785 XDOT = 4052
552819
YDOT = -10816
387238 feet/sec YDOT = -3251
876077 meter/sec
ZDOT = -18641
750419 ZDOT = -5662
473883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18356286
43 X = 5594996
10
Y = 10892968
66 feet Y = 3320176
85 meter
Z = -5997964
49 Z = -1828179
58
XDOT = -11981
468623 XDOT = -3651
951636
YDOT = 9973
557282 feet/sec YDOT = 3039
940259 meter/sec
ZDOT = -18561
993723 ZDOT = -5657
695687
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 11267
52842231
00016717 00000-0 10270-3 0 9102
2 25544 51
6404 20
6567 0011069 230
0470 129
9715 15
61345902 16424
Satellite: ISS
Catalog Number: 25544
Epoch time: 11267
52842231 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 20
6567 deg
Eccentricity:
0011069
Arg of perigee: 230
0470 deg
Mean anomaly: 129
9715 deg
Mean motion: 15
61345902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1642
Checksum: 280
Coasting Arc #12 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2011/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1836928
36 A = 6758447
06 meter
Y = 4413633
38 meter E =
0010370
Z = 4783539
31 I = 51
72134
XDOT = -7215
759189 Wp = 193
70873
YDOT = 166
300288 meter/sec RA = 15
25252 deg
ZDOT = 2608
787002 TA = 230
58614
MA = 230
67799
Ha = 209
865 n
mi
Hp = 205
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6026667
84 X = 1764200
21
Y = 14480424
46 feet Y = 4433768
97 meter
Z = 15694026
62 Z = 4792285
89
XDOT = -23673
750620 XDOT = -7229
755479
YDOT = 545
604619 feet/sec YDOT = 85
531310 meter/sec
ZDOT = 8559
012475 ZDOT = 2573
698931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6723284
78 X = -2049257
20
Y = -14131154
24 feet Y = -4307175
81 meter
Z = 15729393
21 Z = 4794319
05
XDOT = 22628
020977 XDOT = 6897
020794
YDOT = -1366
266946 feet/sec YDOT = -416
438165 meter/sec
ZDOT = 8416
079562 ZDOT = 2565
221050
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 11268
55248532
00016717 00000-0 10270-3 0 9111
2 25544 51
6414 15
4956 0011036 234
3533 125
6596 15
61401244 16589
Satellite: ISS
Catalog Number: 25544
Epoch time: 11268
55248532 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 15
4956 deg
Eccentricity:
0011036
Arg of perigee: 234
3533 deg
Mean anomaly: 125
6596 deg
Mean motion: 15
61401244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 294
Coasting Arc #13 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2011/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2885914
74 A = 6757522
87 meter
Y = -3504128
33 meter E =
0009583
Z = -5011148
71 I = 51
68893
XDOT = 6861
681639 Wp = 160
28185
YDOT = 2817
073301 meter/sec RA = 10
18297 deg
ZDOT = 1974
020580 TA = 128
89387
MA = 128
80837
Ha = 209
620 n
mi
Hp = 205
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9468224
20 X = 2949227
41
Y = -11496484
01 feet Y = -3471502
93 meter
Z = -16440776
62 Z = -4996974
66
XDOT = 22512
078869 XDOT = 6820
081135
YDOT = 9242
366472 feet/sec YDOT = 2893
572489 meter/sec
ZDOT = 6476
445471 ZDOT = 2007
253275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8709184
73 X = -2654559
51
Y = 12160109
15 feet Y = 3706401
27 meter
Z = -16382838
48 Z = -4993489
17
XDOT = -22196
391627 XDOT = -6765
460168
YDOT = -6955
383149 feet/sec YDOT = -2120
000784 meter/sec
ZDOT = 6611
635612 ZDOT = 2015
226535
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 11269
51252868
00016717 00000-0 10270-3 0 9126
2 25544 51
6415 10
6579 0010860 238
1521 121
8579 15
61430464 16733
Satellite: ISS
Catalog Number: 25544
Epoch time: 11269
51252868 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 10
6579 deg
Eccentricity:
0010860
Arg of perigee: 238
1521 deg
Mean anomaly: 121
8579 deg
Mean motion: 15
61430464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 303
Coasting Arc #14 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2011/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6211781
94 A = 6765983
74 meter
Y = 1290492
55 meter E =
0010008
Z = 2331429
17 I = 51
68689
XDOT = -2979
912711 Wp = 157
84562
YDOT = -4563
919509 meter/sec RA = 5
14286 deg
ZDOT = -5414
883307 TA = 356
07602
MA = 356
08386
Ha = 209
450 n
mi
Hp = 205
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20379862
00 X = -6237076
56
Y = 4233899
46 feet Y = 1220887
48 meter
Z = 7649045
82 Z = 2301190
48
XDOT = -9776
616507 XDOT = -2902
351849
YDOT = -14973
489204 feet/sec YDOT = -4596
809750 meter/sec
ZDOT = -17765
365181 ZDOT = -5429
170853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19964154
83 X = 6085074
39
Y = -6047082
27 feet Y = -1843150
68 meter
Z = 7525815
54 Z = 2293868
58
XDOT = 10530
966472 XDOT = 3209
838581
YDOT = 12592
082005 feet/sec YDOT = 3838
066595 meter/sec
ZDOT = -17823
282195 ZDOT = -5432
536413
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 11270
53655589
00016717 00000-0 10270-3 0 9138
2 25544 51
6414 5
4972 0010822 241
9736 118
0326 15
61413272 16892
Satellite: ISS
Catalog Number: 25544
Epoch time: 11270
53655589 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 5
4972 deg
Eccentricity:
0010822
Arg of perigee: 241
9736 deg
Mean anomaly: 118
0326 deg
Mean motion: 15
61413272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 304
Coasting Arc #15 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2011/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6397409
16 A = 6766773
48 meter
Y = 1374237
96 meter E =
0003276
Z = 1717908
98 I = 51
66040
XDOT = -2497
964109 Wp = 59
90210
YDOT = 4499
253201 meter/sec RA =
13956 deg
ZDOT = 5696
630430 TA = 318
98810
MA = 319
01273
Ha = 208
983 n
mi
Hp = 205
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20988875
19 X = 6373221
28
Y = 4508654
73 feet Y = 1445642
66 meter
Z = 5636184
32 Z = 1748929
09
XDOT = -8195
420304 XDOT = -2575
763549
YDOT = 14761
329398 feet/sec YDOT = 4470
885064 meter/sec
ZDOT = 18689
732382 ZDOT = 5684
305691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21315997
71 X = -6497116
10
Y = -2247237
40 feet Y = -684957
96 meter
Z = 5762429
07 Z = 1756388
38
XDOT = 6521
464384 XDOT = 1987
742344
YDOT = -14010
053216 feet/sec YDOT = -4270
264220 meter/sec
ZDOT = 18639
268836 ZDOT = 5681
249141
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 11271
56056181
00016717 00000-0 10270-3 0 9146
2 25544 51
6419
3354 0010749 246
7472 113
2553 15
61462663 17059
Satellite: ISS
Catalog Number: 25544
Epoch time: 11271
56056181 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node:
3354 deg
Eccentricity:
0010749
Arg of perigee: 246
7472 deg
Mean anomaly: 113
2553 deg
Mean motion: 15
61462663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 289
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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