[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 5th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19482 68 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 1782)
---------------------------------------
Vector Time (GMT): 2011/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5186502
30 A = 6764133
99 meter
Y = 1236598
93 meter E =
0006563
Z = 4167149
18 I = 51
49126
XDOT = -4220
004607 Wp = 279
34493
YDOT = 5227
357728 meter/sec RA = 334
95764 deg
ZDOT = 3707
098905 TA = 132
55568
MA = 132
50026
Ha = 211
555 n
mi
Hp = 205
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17016083
65 X = 5152045
59
Y = 4057083
10 feet Y = 1294405
06 meter
Z = 13671749
26 Z = 4192261
56
XDOT = -13845
159473 XDOT = -4296
152792
YDOT = 17150
123778 feet/sec YDOT = 5179
741411 meter/sec
ZDOT = 12162
397981 ZDOT = 3686
412903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17397152
34 X = -5302652
03
Y = -735940
82 feet Y = -224314
76 meter
Z = 13773933
20 Z = 4198294
84
XDOT = 10318
176663 XDOT = 3144
980247
YDOT = -18232
404025 feet/sec YDOT = -5557
236747 meter/sec
ZDOT = 12077
832802 ZDOT = 3681
323438
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 11276
55474622
00016717 00000-0 10270-3 0 9009
2 25544 51
6408 335
1993 0016743 283
4330 76
4959 15
60226855 17832
Satellite: ISS
Catalog Number: 25544
Epoch time: 11276
55474622 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 335
1993 deg
Eccentricity:
0016743
Arg of perigee: 283
4330 deg
Mean anomaly: 76
4959 deg
Mean motion: 15
60226855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 325
Coasting Arc #2 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2011/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1868381
83 A = 6759645
11 meter
Y = -3781509
54 meter E =
0004554
Z = -5281157
21 I = 51
44879
XDOT = 6738
562111 Wp = 346
34266
YDOT = -3675
690721 meter/sec RA = 329
88817 deg
ZDOT = 252
249333 TA = 286
03930
MA = 286
08945
Ha = 211
763 n
mi
Hp = 205
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6129861
66 X = -1800302
46
Y = -12406527
35 feet Y = -3802022
51 meter
Z = -17326631
26 Z = -5290068
28
XDOT = 22108
143408 XDOT = 6777
938195
YDOT = -12059
352759 feet/sec YDOT = -3600
115819 meter/sec
ZDOT = 827
589674 ZDOT = 285
081097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8480634
02 X = 2584897
25
Y = 10877744
95 feet Y = 3315536
66 meter
Z = -17362683
75 Z = -5292146
01
XDOT = -18308
078621 XDOT = -5580
302364
YDOT = 15785
815625 feet/sec YDOT = 4811
516602 meter/sec
ZDOT = 961
514589 ZDOT = 293
069647
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 11277
51549937
00016717 00000-0 10270-3 0 9019
2 25544 51
6404 330
3655 0016700 287
5472 72
3859 15
60236266 17982
Satellite: ISS
Catalog Number: 25544
Epoch time: 11277
51549937 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 330
3655 deg
Eccentricity:
0016700
Arg of perigee: 287
5472 deg
Mean anomaly: 72
3859 deg
Mean motion: 15
60236266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 325
Coasting Arc #3 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2011/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2016198
29 A = 6765069
38 meter
Y = 5184917
25 meter E =
0008888
Z = 3859442
78 I = 51
44225
XDOT = -6455
516189 Wp = 330
84116
YDOT = 547
655631 meter/sec RA = 324
82063 deg
ZDOT = -4104
518074 TA = 162
36165
MA = 162
33077
Ha = 211
984 n
mi
Hp = 205
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6614823
78 X = -2092775
66
Y = 17010883
36 feet Y = 5161942
95 meter
Z = 12662213
84 Z = 3849461
78
XDOT = -21179
515056 XDOT = -6441
221404
YDOT = 1796
770443 feet/sec YDOT = 475
545776 meter/sec
ZDOT = -13466
266648 ZDOT = -4135
844245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2685043
50 X = 818401
26
Y = -18081820
21 feet Y = -5511338
80 meter
Z = 12621252
91 Z = 3846957
89
XDOT = 18831
778163 XDOT = 5739
925984
YDOT = -6700
549239 feet/sec YDOT = -2042
327408 meter/sec
ZDOT = -13593
864814 ZDOT = -4143
409995
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 11278
54027487
00016717 00000-0 10270-3 0 9025
2 25544 51
6407 325
2094 0016711 291
8056 68
1321 15
60323466 18148
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
54027487 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 325
2094 deg
Eccentricity:
0016711
Arg of perigee: 291
8056 deg
Mean anomaly: 68
1321 deg
Mean motion: 15
60323466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 297
Coasting Arc #4 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2011/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859717
72 A = 6771344
32 meter
Y = -4668633
05 meter E =
0017378
Z = -537486
77 I = 51
43875
XDOT = 3676
451091 Wp = 333
70752
YDOT = 3131
989343 meter/sec RA = 319
79433 deg
ZDOT = 5977
641819 TA = 20
45669
MA = 20
38718
Ha = 212
277 n
mi
Hp = 205
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15943955
79 X = 4914173
12
Y = -15317037
57 feet Y = -4613984
28 meter
Z = -1763408
03 Z = -513745
66
XDOT = 12061
847412 XDOT = 3612
117057
YDOT = 10275
555586 feet/sec YDOT = 3172
742423 meter/sec
ZDOT = 19611
685758 ZDOT = 5995
345484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11771478
47 X = -3587946
64
Y = 18723947
34 feet Y = 5707059
15 meter
Z = -1666452
65 Z = -507934
77
XDOT = -12710
573067 XDOT = -3874
182671
YDOT = -6220
984276 feet/sec YDOT = -1896
156007 meter/sec
ZDOT = 19683
588675 ZDOT = 5999
557828
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 11279
50097976
00016717 00000-0 10270-3 0 9033
2 25544 51
6405 320
3748 0016610 296
1881 63
7567 15
60299934 18291
Satellite: ISS
Catalog Number: 25544
Epoch time: 11279
50097976 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 320
3748 deg
Eccentricity:
0016610
Arg of perigee: 296
1881 deg
Mean anomaly: 63
7567 deg
Mean motion: 15
60299934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1829
Checksum: 338
Coasting Arc #5 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2011/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5622960
81 A = 6767171
25 meter
Y = 2226473
01 meter E =
0012099
Z = -3036179
34 I = 51
40395
XDOT = 328
025217 Wp = 304
40485
YDOT = -5891
848568 meter/sec RA = 314
77551 deg
ZDOT = -4907
378572 TA = 270
62945
MA = 270
76808
Ha = 212
364 n
mi
Hp = 205
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18448034
15 X = -5632690
54
Y = 7304701
48 feet Y = 2163538
93 meter
Z = -9961218
29 Z = -3063519
53
XDOT = 1076
198220 XDOT = 417
723816
YDOT = -19330
211836 feet/sec YDOT = -5887
679319 meter/sec
ZDOT = -16100
323398 ZDOT = -4905
566591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15871438
98 X = 4837614
60
Y = -11813259
28 feet Y = -3600681
43 meter
Z = -10072677
27 Z = -3070152
03
XDOT = 3007
118001 XDOT = 916
569567
YDOT = 17818
891099 feet/sec YDOT = 5431
198007 meter/sec
ZDOT = -16092
599214 ZDOT = -4905
024240
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 11280
52570427
00016717 00000-0 10270-3 0 9045
2 25544 51
6411 315
2184 0016448 299
9401 60
0121 15
60387982 18458
Satellite: ISS
Catalog Number: 25544
Epoch time: 11280
52570427 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 315
2184 deg
Eccentricity:
0016448
Arg of perigee: 299
9401 deg
Mean anomaly: 60
0121 deg
Mean motion: 15
60387982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 297
Coasting Arc #6 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2011/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4171180
06 A = 6759726
02 meter
Y = 1406410
24 meter E =
0011936
Z = 5137315
41 I = 51
35729
XDOT = -3899
550901 Wp = 303
11002
YDOT = 6456
237338 meter/sec RA = 309
71210 deg
ZDOT = 1407
485154 TA = 133
35624
MA = 133
25673
Ha = 212
527 n
mi
Hp = 204
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13684973
94 X = 4130187
05
Y = 4614206
82 feet Y = 1452826
27 meter
Z = 16854709
35 Z = 5157479
35
XDOT = -12793
802167 XDOT = -3978
293323
YDOT = 21181
881031 feet/sec YDOT = 6412
190048 meter/sec
ZDOT = 4617
733446 ZDOT = 1388
349117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14328716
13 X = -4367392
68
Y = -696873
92 feet Y = -212407
17 meter
Z = 16936732
39 Z = 5162316
03
XDOT = 6443
053245 XDOT = 1963
842629
YDOT = -22848
647784 feet/sec YDOT = -6964
267845 meter/sec
ZDOT = 4539
443514 ZDOT = 1383
622383
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 11281
55040138
00016717 00000-0 10270-3 0 9051
2 25544 51
6397 310
0610 0016364 304
0447 55
9154 15
60419089 18614
Satellite: ISS
Catalog Number: 25544
Epoch time: 11281
55040138 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 310
0610 deg
Eccentricity:
0016364
Arg of perigee: 304
0447 deg
Mean anomaly: 55
9154 deg
Mean motion: 15
60419089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 289
Coasting Arc #7 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2011/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1295328
02 A = 6761640
59 meter
Y = -4704738
08 meter E =
0007083
Z = -4675113
44 I = 51
34618
XDOT = 5699
562259 Wp = 336
18316
YDOT = -4332
505517 meter/sec RA = 304
62745 deg
ZDOT = 2785
686450 TA = 321
45896
MA = 321
50951
Ha = 212
796 n
mi
Hp = 204
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4249763
85 X = -1219911
42
Y = -15435492
38 feet Y = -4718802
08 meter
Z = -15338298
70 Z = -4681222
47
XDOT = 18699
351245 XDOT = 5734
053117
YDOT = -14214
256944 feet/sec YDOT = -4268
576353 meter/sec
ZDOT = 9139
391239 ZDOT = 2813
459393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8480859
90 X = 2584966
10
Y = 13551178
42 feet Y = 4130399
18 meter
Z = -15362906
74 Z = -4682613
98
XDOT = -12696
265707 XDOT = -3869
821787
YDOT = 18417
395411 feet/sec YDOT = 5613
622121 meter/sec
ZDOT = 9252
718117 ZDOT = 2820
228482
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 11282
51102972
00016717 00000-0 10270-3 0 9064
2 25544 51
6406 305
2265 0016479 307
7305 52
2357 15
60443789 18762
Satellite: ISS
Catalog Number: 25544
Epoch time: 11282
51102972 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 305
2265 deg
Eccentricity:
0016479
Arg of perigee: 307
7305 deg
Mean anomaly: 52
2357 deg
Mean motion: 15
60443789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 310
Coasting Arc #8 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2011/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1821528
65 A = 6769348
42 meter
Y = 6247556
23 meter E =
0005359
Z = 1875554
47 I = 51
35476
XDOT = -5237
888340 Wp = 6
78215
YDOT = 156
261651 meter/sec RA = 299
57776 deg
ZDOT = -5600
655886 TA = 152
45035
MA = 152
42193
Ha = 213
000 n
mi
Hp = 204
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5976143
88 X = -1900365
89
Y = 20497231
72 feet Y = 6226746
19 meter
Z = 6153393
94 Z = 1866513
18
XDOT = -17184
673030 XDOT = -5212
039099
YDOT = 512
669459 feet/sec YDOT = 97
832269 meter/sec
ZDOT = -18374
855268 ZDOT = -5626
039067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -597626
64 X = -182156
60
Y = -21352975
94 feet Y = -6508387
07 meter
Z = 6116234
28 Z = 1864228
21
XDOT = 14527
394363 XDOT = 4427
949802
YDOT = -5705
888073 feet/sec YDOT = -1739
154685 meter/sec
ZDOT = -18478
211855 ZDOT = -5632
158973
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 11283
53567264
00016717 00000-0 10270-3 0 9077
2 25544 51
6390 300
0689 0016357 311
9621 48
0140 15
60511900 18922
Satellite: ISS
Catalog Number: 25544
Epoch time: 11283
53567264 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 300
0689 deg
Eccentricity:
0016357
Arg of perigee: 311
9621 deg
Mean anomaly: 48
0140 deg
Mean motion: 15
60511900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 293
Coasting Arc #9 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2011/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3995965
90 A = 6769192
22 meter
Y = -5112925
25 meter E =
0017211
Z = 1887057
89 I = 51
34041
XDOT = 2938
423345 Wp = 4
57901
YDOT = 4360
691056 meter/sec RA = 294
55669 deg
ZDOT = 5606
191523 TA = 16
37333
MA = 16
31781
Ha = 213
121 n
mi
Hp = 204
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13110124
36 X = 4043675
52
Y = -16774689
13 feet Y = -5067972
95 meter
Z = 6191134
83 Z = 1906587
03
XDOT = 9640
496540 XDOT = 2862
208554
YDOT = 14306
729187 feet/sec YDOT = 4393
124768 meter/sec
ZDOT = 18393
016808 ZDOT = 5620
281007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6920758
16 X = -2109447
09
Y = 20109059
80 feet Y = 6129241
43 meter
Z = 6270927
13 Z = 1911378
59
XDOT = -12190
701637 XDOT = -3715
725859
YDOT = -9935
698892 feet/sec YDOT = -3028
401022 meter/sec
ZDOT = 18450
140419 ZDOT = 5623
602800
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 11284
56028723
00016717 00000-0 10270-3 0 9084
2 25544 51
6389 294
9110 0016396 315
8211 44
1635 15
60541548 19086
Satellite: ISS
Catalog Number: 25544
Epoch time: 11284
56028723 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 294
9110 deg
Eccentricity:
0016396
Arg of perigee: 315
8211 deg
Mean anomaly: 44
1635 deg
Mean motion: 15
60541548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 314
Coasting Arc #10 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2011/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579800
83 A = 6761140
31 meter
Y = 1685939
97 meter E =
0016005
Z = -4686214
90 I = 51
30181
XDOT = 196
846529 Wp = 358
81031
YDOT = -7159
477616 meter/sec RA = 289
50385 deg
ZDOT = -2752
199911 TA = 243
74593
MA = 243
91050
Ha = 213
315 n
mi
Hp = 204
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15025593
29 X = -4575547
75
Y = 5531299
12 feet Y = 1634749
16 meter
Z = -15374720
80 Z = -4708453
82
XDOT = 645
821946 XDOT = 290
260529
YDOT = -23489
099791 feet/sec YDOT = -7156
754316 meter/sec
ZDOT = -9029
527268 ZDOT = -2751
016019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12154131
74 X = 3704579
35
Y = -10288131
71 feet Y = -3135822
55 meter
Z = -15465354
54 Z = -4713840
06
XDOT = 6596
013520 XDOT = 2010
464921
YDOT = 21435
933089 feet/sec YDOT = 6533
672405 meter/sec
ZDOT = -9024
316328 ZDOT = -2750
611617
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 11285
52083661
00016717 00000-0 10270-3 0 9094
2 25544 51
6385 290
0754 0016363 319
4225 40
5710 15
60585488 19234
Satellite: ISS
Catalog Number: 25544
Epoch time: 11285
52083661 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 290
0754 deg
Eccentricity:
0016363
Arg of perigee: 319
4225 deg
Mean anomaly: 40
5710 deg
Mean motion: 15
60585488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 312
Coasting Arc #11 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2011/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3530860
93 A = 6759283
68 meter
Y = 2695475
74 meter E =
0016949
Z = 5103400
45 I = 51
28617
XDOT = -3029
765737 Wp = 339
53755
YDOT = 6881
338961 meter/sec RA = 284
41152 deg
ZDOT = -1524
263052 TA = 125
29366
MA = 125
13502
Ha = 213
481 n
mi
Hp = 203
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11584189
40 X = 3475665
25
Y = 8843424
35 feet Y = 2734651
79 meter
Z = 16743439
81 Z = 5120419
44
XDOT = -9940
176303 XDOT = -3099
084292
YDOT = 22576
571395 feet/sec YDOT = 6847
070560 meter/sec
ZDOT = -5000
863032 ZDOT = -1539
150892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13883221
06 X = -4231605
78
Y = -4163603
96 feet Y = -1269066
49 meter
Z = 16812583
09 Z = 5124475
33
XDOT = 896
235951 XDOT = 273
172718
YDOT = -23613
933781 feet/sec YDOT = -7197
527016 meter/sec
ZDOT = -5061
849145 ZDOT = -1542
851619
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 11286
54539408
00016717 00000-0 10270-3 0 9104
2 25544 51
6377 284
9164 0016390 323
2897 36
7135 15
60631989 19393
Satellite: ISS
Catalog Number: 25544
Epoch time: 11286
54539408 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 284
9164 deg
Eccentricity:
0016390
Arg of perigee: 323
2897 deg
Mean anomaly: 36
7135 deg
Mean motion: 15
60631989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 341
Coasting Arc #12 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2011/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1367606
04 A = 6766789
70 meter
Y = -5951293
69 meter E =
0016407
Z = -2890887
39 I = 51
30530
XDOT = 4650
714486 Wp = 343
26136
YDOT = -3502
788497 meter/sec RA = 279
34276 deg
ZDOT = 5019
203323 TA = 343
49270
MA = 343
54606
Ha = 213
636 n
mi
Hp = 203
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4486896
46 X = -1286912
15
Y = -19525241
75 feet Y = -5966136
09 meter
Z = -9484538
68 Z = -2897334
98
XDOT = 15258
249625 XDOT = 4665
154789
YDOT = -11492
088246 feet/sec YDOT = -3450
700304 meter/sec
ZDOT = 16467
202502 ZDOT = 5041
832275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11391413
57 X = 3472102
86
Y = 16465432
50 feet Y = 5018663
83 meter
Z = -9510468
37 Z = -2898790
76
XDOT = -8579
309925 XDOT = -2614
973665
YDOT = 15484
505019 feet/sec YDOT = 4719
677130 meter/sec
ZDOT = 16559
521842 ZDOT = 5047
342257
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 11287
50588943
00016717 00000-0 10270-3 0 9110
2 25544 51
6379 280
0811 0016382 327
2469 32
7670 15
60666379 19549
Satellite: ISS
Catalog Number: 25544
Epoch time: 11287
50588943 = yrday
fracday
Element set: 911
Inclination: 51
6379 deg
RA of node: 280
0811 deg
Eccentricity:
0016382
Arg of perigee: 327
2469 deg
Mean anomaly: 32
7670 deg
Mean motion: 15
60666379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 333
Coasting Arc #13 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2011/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1171924
57 A = 6769897
86 meter
Y = 6619154
26 meter E =
0006637
Z = -837436
98 I = 51
31216
XDOT = -4627
791039 Wp = 347
04724
YDOT = -1569
023381 meter/sec RA = 274
31463 deg
ZDOT = -5909
967683 TA = 202
06552
MA = 202
09411
Ha = 213
828 n
mi
Hp = 203
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3844896
89 X = -1241785
95
Y = 21716385
36 feet Y = 6605658
43 meter
Z = -2747496
67 Z = -843300
31
XDOT = -15183
041468 XDOT = -4581
191803
YDOT = -5147
714506 feet/sec YDOT = -1620
513893 meter/sec
ZDOT = -19389
657753 ZDOT = -5932
336697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4916585
39 X = -1498575
23
Y = -21496001
99 feet Y = -6551981
41 meter
Z = -2771723
23 Z = -844821
24
XDOT = 14314
719275 XDOT = 4363
126435
YDOT = -755
725153 feet/sec YDOT = -230
345027 meter/sec
ZDOT = -19480
648926 ZDOT = -5937
701793
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 11288
53038824
00016717 00000-0 10270-3 0 9123
2 25544 51
6375 274
9218 0016413 331
1987 28
8261 15
60728303 19708
Satellite: ISS
Catalog Number: 25544
Epoch time: 11288
53038824 = yrday
fracday
Element set: 912
Inclination: 51
6375 deg
RA of node: 274
9218 deg
Eccentricity:
0016413
Arg of perigee: 331
1987 deg
Mean anomaly: 28
8261 deg
Mean motion: 15
60728303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 315
Coasting Arc #14 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2011/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3263562
72 A = 6762624
71 meter
Y = -4226970
48 meter E =
0012456
Z = 4138367
76 I = 51
28698
XDOT = 3056
611456 Wp = 12
98986
YDOT = 5990
683404 meter/sec RA = 269
27205 deg
ZDOT = 3718
234545 TA = 38
73274
MA = 38
64350
Ha = 213
788 n
mi
Hp = 203
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10707226
76 X = 3290483
15
Y = -13868013
37 feet Y = -4190324
67 meter
Z = 13577322
06 Z = 4154287
97
XDOT = 10028
252810 XDOT = 2971
332423
YDOT = 19654
473110 feet/sec YDOT = 6024
387600 meter/sec
ZDOT = 12198
932234 ZDOT = 3732
876511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4105771
31 X = -1251439
09
Y = 16980536
30 feet Y = 5175667
47 meter
Z = 13642367
93 Z = 4158193
75
XDOT = -15817
596403 XDOT = -4821
203384
YDOT = -13647
368631 feet/sec YDOT = -4159
717959 meter/sec
ZDOT = 12258
232480 ZDOT = 3736
309260
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 11289
55485449
00016717 00000-0 10270-3 0 9136
2 25544 51
6373 269
7632 0016420 334
2713 25
7625 15
60788867 19865
Satellite: ISS
Catalog Number: 25544
Epoch time: 11289
55485449 = yrday
fracday
Element set: 913
Inclination: 51
6373 deg
RA of node: 269
7632 deg
Eccentricity:
0016420
Arg of perigee: 334
2713 deg
Mean anomaly: 25
7625 deg
Mean motion: 15
60788867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 345
Coasting Arc #15 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2011/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4247512
05 A = 6758047
06 meter
Y = -51830
87 meter E =
0016844
Z = -5262865
71 I = 51
27323
XDOT = -428
140025 Wp = 31
47489
YDOT = -7649
671634 meter/sec RA = 264
18318 deg
ZDOT = 435
638162 TA = 242
61225
MA = 242
78374
Ha = 213
991 n
mi
Hp = 202
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13935406
98 X = -4221050
31
Y = -170048
79 feet Y = -99181
32 meter
Z = -17266619
79 Z = -5283436
18
XDOT = -1404
658874 XDOT = -344
684356
YDOT = -25097
347879 feet/sec YDOT = -7653
992721 meter/sec
ZDOT = 1429
259062 ZDOT = 433
761120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12622003
39 X = 3847186
63
Y = -5657740
97 feet Y = -1724479
45 meter
Z = -17350378
69 Z = -5288395
42
XDOT = 11417
608156 XDOT = 3480
086966
YDOT = 21258
802238 feet/sec YDOT = 6479
682922 meter/sec
ZDOT = 1422
014977 ZDOT = 433
430165
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 11290
51526437
00016717 00000-0 10270-3 0 9148
2 25544 51
6373 264
9267 0016382 338
4437 21
6028 15
60802418 20012
Satellite: ISS
Catalog Number: 25544
Epoch time: 11290
51526437 = yrday
fracday
Element set: 914
Inclination: 51
6373 deg
RA of node: 264
9267 deg
Eccentricity:
0016382
Arg of perigee: 338
4437 deg
Mean anomaly: 21
6028 deg
Mean motion: 15
60802418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 294
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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