[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 12th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 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
292/16:08:51
107 -2
4 5
2 5
2
N/A -4
4 0
0 215
0
000/00:01:38
214 -1
3 0
0 204
4
Coasting Arc #1 (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 = -1796862
40 A = 6769332
85 meter
Y = 6246464
89 meter E =
0005324
Z = 1902566
32 I = 51
35446
XDOT = -5249
190613 Wp = 7
29998
YDOT = 194
418298 meter/sec RA = 299
58412 deg
ZDOT = -5588
950854 TA = 151
61898
MA = 151
58998
Ha = 212
970 n
mi
Hp = 204
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5895217
86 X = -1875820
49
Y = 20493651
21 feet Y = 6225930
01 meter
Z = 6242015
50 Z = 1893644
57
XDOT = -17221
753981 XDOT = -5223
824070
YDOT = 637
855308 feet/sec YDOT = 135
859829 meter/sec
ZDOT = -18336
452934 ZDOT = -5614
390120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -673000
18 X = -205130
46
Y = -21324795
08 feet Y = -6499797
54 meter
Z = 6205342
58 Z = 1891388
42
XDOT = 14526
357664 XDOT = 4427
633816
YDOT = -5830
984947 feet/sec YDOT = -1777
284212 meter/sec
ZDOT = -18440
039997 ZDOT = -5620
524191
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
53572869
00016717 00000-0 10270-3 0 9007
2 25544 51
6389 300
0753 0016269 311
6613 48
3150 15
60502273 18929
Satellite: ISS
Catalog Number: 25544
Epoch time: 11283
53572869 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 300
0753 deg
Eccentricity:
0016269
Arg of perigee: 311
6613 deg
Mean anomaly: 48
3150 deg
Mean motion: 15
60502273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 300
Coasting Arc #2 (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 = 3980706
24 A = 6769269
82 meter
Y = -5135945
48 meter E =
0017175
Z = 1856867
36 I = 51
34042
XDOT = 2965
650335 Wp = 4
46520
YDOT = 4325
329976 meter/sec RA = 294
56309 deg
ZDOT = 5619
157667 TA = 16
13627
MA = 16
08164
Ha = 213
091 n
mi
Hp = 204
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13060059
83 X = 4028821
06
Y = -16850214
83 feet Y = -5091161
56 meter
Z = 6092084
52 Z = 1876323
35
XDOT = 9729
823935 XDOT = 2889
765947
YDOT = 14190
715143 feet/sec YDOT = 4358
070005 meter/sec
ZDOT = 18435
556650 ZDOT = 5633
380228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6849456
25 X = -2087714
27
Y = 20164447
48 feet Y = 6146123
59 meter
Z = 6171580
30 Z = 1881097
67
XDOT = -12233
258609 XDOT = -3728
697224
YDOT = -9802
258829 feet/sec YDOT = -2987
728491 meter/sec
ZDOT = 18493
224013 ZDOT = 5636
734679
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
56034979
00016717 00000-0 10270-3 0 9017
2 25544 51
6388 294
9175 0016307 315
5151 44
4695 15
60531742 19082
Satellite: ISS
Catalog Number: 25544
Epoch time: 11284
56034979 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 294
9175 deg
Eccentricity:
0016307
Arg of perigee: 315
5151 deg
Mean anomaly: 44
4695 deg
Mean motion: 15
60531742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 323
Coasting Arc #3 (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 = -4581058
62 A = 6761236
08 meter
Y = 1727789
61 meter E =
0015878
Z = -4669789
39 I = 51
30187
XDOT = 162
735539 Wp = 358
39018
YDOT = -7146
486183 meter/sec RA = 289
51073 deg
ZDOT = -2787
946953 TA = 243
78091
MA = 243
94423
Ha = 213
287 n
mi
Hp = 204
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15029719
87 X = -4577353
20
Y = 5668601
08 feet Y = 1676581
67 meter
Z = -15320831
34 Z = -4692035
76
XDOT = 533
909248 XDOT = 256
180457
YDOT = -23446
476977 feet/sec YDOT = -7144
144162 meter/sec
ZDOT = -9146
807590 ZDOT = -2786
928702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12111527
18 X = 3691593
49
Y = -10418735
01 feet Y = -3175630
43 meter
Z = -15411497
68 Z = -4697424
49
XDOT = 6676
514206 XDOT = 2035
001530
YDOT = 21361
078605 feet/sec YDOT = 6510
856759 meter/sec
ZDOT = -9142
271722 ZDOT = -2786
564421
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
52090546
00016717 00000-0 10270-3 0 9027
2 25544 51
6383 290
0819 0016274 319
1222 40
8713 15
60575185 19238
Satellite: ISS
Catalog Number: 25544
Epoch time: 11285
52090546 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 290
0819 deg
Eccentricity:
0016274
Arg of perigee: 319
1222 deg
Mean anomaly: 40
8713 deg
Mean motion: 15
60575185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 299
Coasting Arc #4 (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 = 3550321
25 A = 6759271
12 meter
Y = 2650776
22 meter E =
0016814
Z = 5113238
39 I = 51
28585
XDOT = -3000
843875 Wp = 339
01206
YDOT = 6903
413558 meter/sec RA = 284
41860 deg
ZDOT = -1481
298071 TA = 125
39355
MA = 125
23637
Ha = 213
453 n
mi
Hp = 203
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11648035
61 X = 3495576
17
Y = 8696772
39 feet Y = 2690172
41 meter
Z = 16775716
52 Z = 5130353
02
XDOT = -9845
288303 XDOT = -3070
620142
YDOT = 22648
994614 feet/sec YDOT = 6869
466024 meter/sec
ZDOT = -4859
901808 ZDOT = -1496
046519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13890341
00 X = -4233775
94
Y = -4003894
86 feet Y = -1220387
15 meter
Z = 16845251
59 Z = 5134432
68
XDOT = 794
189052 XDOT = 242
068823
YDOT = -23647
513982 feet/sec YDOT = -7207
762262 meter/sec
ZDOT = -4920
321626 ZDOT = -1499
714032
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
54546982
00016717 00000-0 10270-3 0 9031
2 25544 51
6376 284
9229 0016301 322
9902 37
0128 15
60621164 19399
Satellite: ISS
Catalog Number: 25544
Epoch time: 11286
54546982 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 284
9229 deg
Eccentricity:
0016301
Arg of perigee: 322
9902 deg
Mean anomaly: 37
0128 deg
Mean motion: 15
60621164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 314
Coasting Arc #5 (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 = -1399969
06 A = 6766733
71 meter
Y = -5926450
00 meter E =
0016160
Z = -2926485
76 I = 51
30483
XDOT = 4638
349586 Wp = 343
01259
YDOT = -3556
830680 meter/sec RA = 279
34941 deg
ZDOT = 4992
316859 TA = 343
27814
MA = 343
33136
Ha = 213
611 n
mi
Hp = 203
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4593074
34 X = -1319377
63
Y = -19443733
59 feet Y = -5941654
88 meter
Z = -9601331
22 Z = -2933090
82
XDOT = 15217
682368 XDOT = 4653
525731
YDOT = -11669
391996 feet/sec YDOT = -3504
876646 meter/sec
ZDOT = 16378
992321 ZDOT = 5014
887532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11458883
97 X = 3492667
83
Y = 16350477
79 feet Y = 4983625
63 meter
Z = -9627903
38 Z = -2934584
95
XDOT = -8484
425982 XDOT = -2586
053039
YDOT = 15629
174228 feet/sec YDOT = 4763
772305 meter/sec
ZDOT = 16471
077306 ZDOT = 5020
384363
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
50597180
00016717 00000-0 10270-3 0 9045
2 25544 51
6378 280
0876 0016297 326
9452 33
0684 15
60654771 19544
Satellite: ISS
Catalog Number: 25544
Epoch time: 11287
50597180 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 280
0876 deg
Eccentricity:
0016297
Arg of perigee: 326
9452 deg
Mean anomaly: 33
0684 deg
Mean motion: 15
60654771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 333
Coasting Arc #6 (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 = -1136816
29 A = 6769962
04 meter
Y = 6630862
18 meter E =
0006441
Z = -791675
54 I = 51
31210
XDOT = -4639
146300 Wp = 347
37899
YDOT = -1503
758734 meter/sec RA = 274
32109 deg
ZDOT = -5918
124922 TA = 201
23197
MA = 201
25871
Ha = 213
803 n
mi
Hp = 203
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3729712
25 X = -1207033
51
Y = 21754797
17 feet Y = 6617756
96 meter
Z = -2597360
69 Z = -797369
17
XDOT = -15220
296260 XDOT = -4593
236394
YDOT = -4933
591648 feet/sec YDOT = -1555
380082 meter/sec
ZDOT = -19416
420349 ZDOT = -5940
550778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5036808
38 X = -1535219
19
Y = -21486965
73 feet Y = -6549227
15 meter
Z = -2620896
98 Z = -798849
40
XDOT = 14266
298494 XDOT = 4348
367781
YDOT = -958
654055 feet/sec YDOT = -292
197756 meter/sec
ZDOT = -19507
646445 ZDOT = -5945
930636
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
53047787
00016717 00000-0 10270-3 0 9053
2 25544 51
6374 274
9284 0016326 330
9024 29
1221 15
60717229 19707
Satellite: ISS
Catalog Number: 25544
Epoch time: 11288
53047787 = yrday
fracday
Element set: 905
Inclination: 51
6374 deg
RA of node: 274
9284 deg
Eccentricity:
0016326
Arg of perigee: 330
9024 deg
Mean anomaly: 29
1221 deg
Mean motion: 15
60717229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 314
Coasting Arc #7 (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 = 3238356
87 A = 6762768
38 meter
Y = -4276657
55 meter E =
0012451
Z = 4107087
93 I = 51
28719
XDOT = 3091
038490 Wp = 13
46947
YDOT = 5945
009926 meter/sec RA = 269
27913 deg
ZDOT = 3762
856909 TA = 37
70684
MA = 37
61964
Ha = 213
762 n
mi
Hp = 203
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10624530
41 X = 3265986
74
Y = -14031028
70 feet Y = -4240289
64 meter
Z = 13474697
94 Z = 4122887
41
XDOT = 10141
202394 XDOT = 3006
050856
YDOT = 19504
625741 feet/sec YDOT = 5979
100737 meter/sec
ZDOT = 12345
331067 ZDOT = 3777
666834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3964754
79 X = -1208457
26
Y = 17096408
80 feet Y = 5210985
40 meter
Z = 13539254
89 Z = 4126764
89
XDOT = -15851
002478 XDOT = -4831
385555
YDOT = -13475
282488 feet/sec YDOT = -4107
266102 meter/sec
ZDOT = 12405
317596 ZDOT = 3781
140803
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
55495158
00016717 00000-0 10270-3 0 9066
2 25544 51
6372 269
7699 0016332 333
9658 26
0675 15
60777821 19860
Satellite: ISS
Catalog Number: 25544
Epoch time: 11289
55495158 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 269
7699 deg
Eccentricity:
0016332
Arg of perigee: 333
9658 deg
Mean anomaly: 26
0675 deg
Mean motion: 15
60777821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 360
Coasting Arc #8 (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 = -4243463
76 A = 6758064
84 meter
Y = 16482
37 meter E =
0016845
Z = -5266502
05 I = 51
27301
XDOT = -476
372246 Wp = 31
41635
YDOT = -7649
937722 meter/sec RA = 264
19073 deg
ZDOT = 374
574344 TA = 242
08552
MA = 242
25619
Ha = 213
967 n
mi
Hp = 202
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13922125
19 X = -4217748
55
Y = 54076
01 feet Y = -30826
98 meter
Z = -17278550
03 Z = -5287054
67
XDOT = -1562
901070 XDOT = -392
613375
YDOT = -25098
220872 feet/sec YDOT = -7654
796478 meter/sec
ZDOT = 1228
918451 ZDOT = 372
463723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12515692
33 X = 3814783
02
Y = -5855498
24 feet Y = -1784755
86 meter
Z = -17362239
80 Z = -5292010
69
XDOT = 11546
047496 XDOT = 3519
235277
YDOT = 21201
359638 feet/sec YDOT = 6462
174418 meter/sec
ZDOT = 1220
723274 ZDOT = 372
076454
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
51536867
00016717 00000-0 10270-3 0 9078
2 25544 51
6372 264
9334 0016295 338
1496 21
8964 15
60790828 20013
Satellite: ISS
Catalog Number: 25544
Epoch time: 11290
51536867 = yrday
fracday
Element set: 907
Inclination: 51
6372 deg
RA of node: 264
9334 deg
Eccentricity:
0016295
Arg of perigee: 338
1496 deg
Mean anomaly: 21
8964 deg
Mean motion: 15
60790828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 325
Coasting Arc #9 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2011/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3784342
99 A = 6764143
67 meter
Y = 4281880
54 meter E =
0017780
Z = 3628368
35 I = 51
29811
XDOT = -2420
700514 Wp = 22
15192
YDOT = 5840
321516 meter/sec RA = 259
10796 deg
ZDOT = -4344
295961 TA = 114
46738
MA = 114
28184
Ha = 214
121 n
mi
Hp = 202
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12415823
45 X = 3718554
71
Y = 14048164
49 feet Y = 4323831
62 meter
Z = 11904095
62 Z = 3646593
02
XDOT = -7941
930820 XDOT = -2464
724146
YDOT = 19161
159828 feet/sec YDOT = 5813
005511 meter/sec
ZDOT = -14252
939503 ZDOT = -4356
162944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17232563
15 X = -5252485
25
Y = -7264652
93 feet Y = -2214266
21 meter
Z = 11978091
48 Z = 3650922
28
XDOT = -1809
840392 XDOT = -551
639351
YDOT = -19412
132138 feet/sec YDOT = -5916
817876 meter/sec
ZDOT = -14301
563184 ZDOT = -4359
116458
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 11291
53978061
00016717 00000-0 10270-3 0 9088
2 25544 51
6371 259
7743 0016391 341
7155 18
3410 15
60861389 20172
Satellite: ISS
Catalog Number: 25544
Epoch time: 11291
53978061 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 259
7743 deg
Eccentricity:
0016391
Arg of perigee: 341
7155 deg
Mean anomaly: 18
3410 deg
Mean motion: 15
60861389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 314
Coasting Arc #10 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2011/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1898444
15 A = 6769683
04 meter
Y = -6480733
60 meter E =
0024617
Z = -58969
69 I = 51
32388
XDOT = 4599
416089 Wp = 10
50600
YDOT = -1398
169646 meter/sec RA = 254
07326 deg
ZDOT = 6004
655440 TA = 348
85314
MA = 348
90757
Ha = 214
110 n
mi
Hp = 202
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6228491
32 X = -1825547
75
Y = -21262249
33 feet Y = -6501555
58 meter
Z = -193470
13 Z = -68015
17
XDOT = 15089
947797 XDOT = 4585
539028
YDOT = -4587
170756 feet/sec YDOT = -1346
813570 meter/sec
ZDOT = 19700
313122 ZDOT = 6026
965961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15151560
19 X = 4618195
55
Y = 16164532
54 feet Y = 4926949
52 meter
Z = -229984
62 Z = -70099
31
XDOT = -10111
774025 XDOT = -3082
068723
YDOT = 9743
267945 feet/sec YDOT = 2969
748070 meter/sec
ZDOT = 19791
242845 ZDOT = 6032
370819
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 11292
50013738
00016717 00000-0 10270-3 0 9098
2 25544 51
6371 254
9378 0016200 345
5532 14
5159 15
60915001 20329
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
50013738 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 254
9378 deg
Eccentricity:
0016200
Arg of perigee: 345
5532 deg
Mean anomaly: 14
5159 deg
Mean motion: 15
60915001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 281
Coasting Arc #11 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2011/292/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3365865
59 A = 6761337
69 meter
Y = 2942127
23 meter E =
0018238
Z = -5081435
42 I = 51
29167
XDOT = -3377
409066 Wp = 17
10762
YDOT = -6693
070142 meter/sec RA = 253
21141 deg
ZDOT = -1622
455734 TA = 237
07720
MA = 237
25276
Ha = 215
050 n
mi
Hp = 204
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11042866
12 X = -3373829
94
Y = 9652648
38 feet Y = 2904443
36 meter
Z = -16671376
04 Z = -5097806
39
XDOT = -11080
738404 XDOT = -3294
433145
YDOT = -21958
891542 feet/sec YDOT = -6730
374507 meter/sec
ZDOT = -5323
017501 ZDOT = -1638
661583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9538953
01 X = -2907472
88
Y = -11040585
39 feet Y = -3365170
43 meter
Z = -16738194
10 Z = -5101801
56
XDOT = 21266
350980 XDOT = 6481
983779
YDOT = -10126
777579 feet/sec YDOT = -3086
641806 meter/sec
ZDOT = -5388
684581 ZDOT = -1642
471060
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 11292
69220924
00016717 00000-0 10270-3 0 9107
2 25544 51
6407 253
9718 0016522 331
6535 28
3721 15
59958185 20351
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
69220924 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 253
9718 deg
Eccentricity:
0016522
Arg of perigee: 331
6535 deg
Mean anomaly: 28
3721 deg
Mean motion: 15
59958185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 312
Coasting Arc #12 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2011/293/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4614635
15 A = 6762246
64 meter
Y = 1132466
17 meter E =
0018603
Z = 4819495
60 I = 51
30473
XDOT = 794
639720 Wp = 357
20850
YDOT = 7228
652232 meter/sec RA = 248
12608 deg
ZDOT = -2441
544640 TA = 116
95306
MA = 116
76293
Ha = 215
139 n
mi
Hp = 204
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15139879
10 X = 4578216
28
Y = 3715440
20 feet Y = 1183866
44 meter
Z = 15811993
45 Z = 4841825
17
XDOT = 2607
085697 XDOT = 725
609128
YDOT = 23716
050631 feet/sec YDOT = 7237
152297 meter/sec
ZDOT = -8010
317060 ZDOT = -2437
852257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3611823
68 X = -1100883
86
Y = 15069591
28 feet Y = 4593211
42 meter
Z = 15902884
02 Z = 4847199
05
XDOT = -22597
773961 XDOT = -6887
801503
YDOT = 3083
149367 feet/sec YDOT = 939
743927 meter/sec
ZDOT = -7995
626863 ZDOT = -2437
067068
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 11293
71719295
00016717 00000-0 10270-3 0 9116
2 25544 51
6402 248
8164 0016584 335
0944 24
9410 15
60017662 20517
Satellite: ISS
Catalog Number: 25544
Epoch time: 11293
71719295 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 248
8164 deg
Eccentricity:
0016584
Arg of perigee: 335
0944 deg
Mean anomaly: 24
9410 deg
Mean motion: 15
60017662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 297
Coasting Arc #13 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2011/294/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4410790
81 A = 6769812
93 meter
Y = -4554572
76 meter E =
0019413
Z = -2337701
88 I = 51
34299
XDOT = 2299
464800 Wp = 354
43728
YDOT = -4982
253720 meter/sec RA = 243
07247 deg
ZDOT = 5383
583768 TA = 339
26707
MA = 339
34571
Ha = 215
221 n
mi
Hp = 203
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14471098
44 X = -4348176
62
Y = -14942824
01 feet Y = -4603546
98 meter
Z = -7669625
58 Z = -2358977
29
XDOT = 7544
175854 XDOT = 2328
853741
YDOT = -16345
976773 feet/sec YDOT = -4956
375029 meter/sec
ZDOT = 17662
676403 ZDOT = 5394
826365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14590731
48 X = 4447254
95
Y = -14780993
44 feet Y = -4505246
80 meter
Z = -7756070
12 Z = -2364050
17
XDOT = 15441
980982 XDOT = 4706
715803
YDOT = 5976
827035 feet/sec YDOT = 1821
736880 meter/sec
ZDOT = 17708
701274 ZDOT = 5397
612148
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 11294
67808723
00016717 00000-0 10270-3 0 9128
2 25544 51
6406 243
9830 0016513 338
6455 21
4010 15
60038292 20661
Satellite: ISS
Catalog Number: 25544
Epoch time: 11294
67808723 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 243
9830 deg
Eccentricity:
0016513
Arg of perigee: 338
6455 deg
Mean anomaly: 21
4010 deg
Mean motion: 15
60038292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 293
Coasting Arc #14 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2011/295/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2627659
56 A = 6771492
07 meter
Y = 6118398
09 meter E =
0008380
Z = -1260693
41 I = 51
36331
XDOT = -4911
139507 Wp = 3
43954
YDOT = 909
605833 meter/sec RA = 238
05358 deg
ZDOT = -5815
571551 TA = 190
33779
MA = 190
35503
Ha = 215
404 n
mi
Hp = 203
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8620930
31 X = 2565171
42
Y = 20073484
56 feet Y = 6147432
70 meter
Z = -4136133
25 Z = -1248080
39
XDOT = -16112
662425 XDOT = -4892
694590
YDOT = 2984
271105 feet/sec YDOT = 854
789118 meter/sec
ZDOT = -19079
959158 ZDOT = -5839
385388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19698827
42 X = -6004202
60
Y = 9467920
58 feet Y = 2885822
19 meter
Z = -4085033
43 Z = -1245118
19
XDOT = -2951
471888 XDOT = -899
608632
YDOT = -14423
800235 feet/sec YDOT = -4396
374312 meter/sec
ZDOT = -19177
001798 ZDOT = -5845
150148
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 11295
70300939
00016717 00000-0 10270-3 0 9130
2 25544 51
6405 238
8275 0016351 342
0135 18
0440 15
60052614 20821
Satellite: ISS
Catalog Number: 25544
Epoch time: 11295
70300939 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 238
8275 deg
Eccentricity:
0016351
Arg of perigee: 342
0135 deg
Mean anomaly: 18
0440 deg
Mean motion: 15
60052614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 275
Coasting Arc #15 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2011/296/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 341812
37 A = 6764159
90 meter
Y = -5223011
92 meter E =
0014178
Z = 4271521
54 I = 51
35632
XDOT = 5994
237559 Wp = 23
12033
YDOT = 3270
283375 meter/sec RA = 233
01481 deg
ZDOT = 3527
926836 TA = 30
92765
MA = 30
84422
Ha = 215
498 n
mi
Hp = 203
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1121431
67 X = 379441
13
Y = -17135865
89 feet Y = -5218978
78 meter
Z = 14014178
28 Z = 4273273
97
XDOT = 19666
133723 XDOT = 5940
084812
YDOT = 10729
276165 feet/sec YDOT = 3337
012157 meter/sec
ZDOT = 11574
563109 ZDOT = 3556
915422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17166474
36 X = 5232341
38
Y = 32518
79 feet Y = 9911
73 meter
Z = 14021547
78 Z = 4273767
76
XDOT = -9562
596739 XDOT = -2914
679486
YDOT = 18938
333122 feet/sec YDOT = 5772
403936 meter/sec
ZDOT = 11692
503661 ZDOT = 3563
875116
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 11296
72789846
00016717 00000-0 10270-3 0 9142
2 25544 51
6406 233
6708 0016471 346
4171 13
6539 15
60112957 20981
Satellite: ISS
Catalog Number: 25544
Epoch time: 11296
72789846 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 233
6708 deg
Eccentricity:
0016471
Arg of perigee: 346
4171 deg
Mean anomaly: 13
6539 deg
Mean motion: 15
60112957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 327
Coasting Arc #16 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2011/297/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3452155
04 A = 6759789
22 meter
Y = 2465435
20 meter E =
0019364
Z = -5272278
42 I = 51
36142
XDOT = -4866
118935 Wp = 37
75274
YDOT = -5913
577006 meter/sec RA = 227
93686 deg
ZDOT = 436
776116 TA = 236
33526
MA = 236
52010
Ha = 215
489 n
mi
Hp = 202
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11325967
97 X = -3453855
16
Y = 8088698
16 feet Y = 2426821
10 meter
Z = -17297501
39 Z = -5289053
68
XDOT = -15964
957137 XDOT = -4801
752308
YDOT = -19401
499364 feet/sec YDOT = -5967
632998 meter/sec
ZDOT = 1432
992506 ZDOT = 413
292935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8913769
78 X = -2716917
03
Y = -10577181
72 feet Y = -3223924
99 meter
Z = -17365945
92 Z = -5293140
32
XDOT = 17365
790209 XDOT = 5293
092856
YDOT = -16745
638197 feet/sec YDOT = -5104
070522 meter/sec
ZDOT = 1337
587440 ZDOT = 407
696652
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 11297
68870073
00016717 00000-0 10270-3 0 9152
2 25544 51
6403 228
8369 0016463 349
3767 10
7038 15
60198038 21135
Satellite: ISS
Catalog Number: 25544
Epoch time: 11297
68870073 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 228
8369 deg
Eccentricity:
0016463
Arg of perigee: 349
3767 deg
Mean anomaly: 10
7038 deg
Mean motion: 15
60198038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 321
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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