[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 24th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 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
299/12:43:53
238 -4
4 5
5 5
6
N/A -3
3 -0
5 217
9
000/00:01:46
475 0
6 0
3 204
0
Coasting Arc #1 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2011/294/14:01:29
130
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2043900
48 A = 6771903
93 meter
Y = 6342417
31 meter E =
0010305
Z = -1242547
49 I = 51
34688
XDOT = -4968
730774 Wp = 353
90163
YDOT = 458
579171 meter/sec RA = 243
56101 deg
ZDOT = -5817
925509 TA = 199
67388
MA = 199
71367
Ha = 216
247 n
mi
Hp = 203
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6705710
24 X = 1978862
54
Y = 20808455
73 feet Y = 6364909
73 meter
Z = -4076599
37 Z = -1232776
51
XDOT = -16301
610151 XDOT = -4945
226738
YDOT = 1504
524839 feet/sec YDOT = 403
146835 meter/sec
ZDOT = -19087
682116 ZDOT = -5842
006738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21323762
77 X = -6499482
89
Y = -4855514
52 feet Y = -1479960
83 meter
Z = -4037098
23 Z = -1230507
54
XDOT = 6629
861383 XDOT = 2020
781749
YDOT = -13124
144788 feet/sec YDOT = -4000
239331 meter/sec
ZDOT = -19185
788539 ZDOT = -5847
828347
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
61401678
00016717 00000-0 10270-3 0 9007
2 25544 51
6401 244
3122 0018693 339
0831 20
9558 15
59915219 20650
Satellite: ISS
Catalog Number: 25544
Epoch time: 11294
61401678 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 244
3122 deg
Eccentricity:
0018693
Arg of perigee: 339
0831 deg
Mean anomaly: 20
9558 deg
Mean motion: 15
59915219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 301
Coasting Arc #2 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2011/295/14:01:29
130
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 779490
83 A = 6764718
44 meter
Y = -5209695
06 meter E =
0015505
Z = 4230917
14 I = 51
33747
XDOT = 5665
357993 Wp = 15
57573
YDOT = 3753
332103 meter/sec RA = 238
52300 deg
ZDOT = 3589
492023 TA = 37
74261
MA = 37
63395
Ha = 216
274 n
mi
Hp = 203
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2557384
61 X = 817135
49
Y = -17092175
39 feet Y = -5200767
49 meter
Z = 13880961
76 Z = 4234795
81
XDOT = 18587
132522 XDOT = 5605
529142
YDOT = 12314
081704 feet/sec YDOT = 3816
351375 meter/sec
ZDOT = 11776
548633 ZDOT = 3616
868987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13608526
93 X = 4147879
01
Y = 10632273
29 feet Y = 3240716
90 meter
Z = 13896997
32 Z = 4235804
78
XDOT = -19106
749155 XDOT = -5823
737143
YDOT = 8966
898666 feet/sec YDOT = 2733
110714 meter/sec
ZDOT = 11887
892971 ZDOT = 3623
429778
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
63901123
00016717 00000-0 10270-3 0 9011
2 25544 51
6398 239
1567 0018622 342
9843 17
0686 15
59967778 20812
Satellite: ISS
Catalog Number: 25544
Epoch time: 11295
63901123 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 239
1567 deg
Eccentricity:
0018622
Arg of perigee: 342
9843 deg
Mean anomaly: 17
0686 deg
Mean motion: 15
59967778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2081
Checksum: 337
Coasting Arc #3 (Orbit 2095)
---------------------------------------
Vector Time (GMT): 2011/296/14:01:29
130
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3585020
32 A = 6760237
01 meter
Y = 2254018
04 meter E =
0020479
Z = -5277942
46 I = 51
34067
XDOT = -4371
625943 Wp = 31
17193
YDOT = -6296
675257 meter/sec RA = 233
44618 deg
ZDOT = 298
057460 TA = 241
57682
MA = 241
78335
Ha = 216
343 n
mi
Hp = 202
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11761877
69 X = -3584319
08
Y = 7395072
30 feet Y = 2213931
57 meter
Z = -17316084
20 Z = -5295357
24
XDOT = -14342
604801 XDOT = -4302
338297
YDOT = -20658
383388 feet/sec YDOT = -6345
174022 meter/sec
ZDOT = 977
878806 ZDOT = 276
988685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -868577
24 X = -264742
34
Y = -13777124
53 feet Y = -4199267
56 meter
Z = -17387123
00 Z = -5299595
09
XDOT = 24009
788878 XDOT = 7318
183650
YDOT = -2566
731131 feet/sec YDOT = -782
339649 meter/sec
ZDOT = 892
334246 ZDOT = 271
983478
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
59991126
00016717 00000-0 10270-3 0 9020
2 25544 51
6406 234
3238 0018623 346
4982 13
5674 15
60032719 20962
Satellite: ISS
Catalog Number: 25544
Epoch time: 11296
59991126 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 234
3238 deg
Eccentricity:
0018623
Arg of perigee: 346
4982 deg
Mean anomaly: 13
5674 deg
Mean motion: 15
60032719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2096
Checksum: 316
Coasting Arc #4 (Orbit 2111)
---------------------------------------
Vector Time (GMT): 2011/297/14:01:29
130
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5380262
89 A = 6765645
74 meter
Y = 1410494
90 meter E =
0021578
Z = 3861182
37 I = 51
37805
XDOT = 1284
858973 Wp = 21
79849
YDOT = 6361
439544 meter/sec RA = 228
37372 deg
ZDOT = -4087
138733 TA = 111
32331
MA = 111
09283
Ha = 216
454 n
mi
Hp = 202
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17651781
13 X = 5345333
29
Y = 4627607
93 feet Y = 1470465
35 meter
Z = 12667921
15 Z = 3887235
21
XDOT = 4215
416579 XDOT = 1233
483576
YDOT = 20870
864645 feet/sec YDOT = 6375
519992 meter/sec
ZDOT = -13409
247811 ZDOT = -4081
022147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12289441
00 X = -3745821
62
Y = 13389218
62 feet Y = 4081033
83 meter
Z = 12773990
10 Z = 3893512
18
XDOT = -19489
346725 XDOT = -5940
352882
YDOT = -5034
933465 feet/sec YDOT = -1534
647720 meter/sec
ZDOT = -13384
608481 ZDOT = -4079
628665
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
62483753
00016717 00000-0 10270-3 0 9038
2 25544 51
6404 229
1681 0018572 350
3037 9
7758 15
60073496 21128
Satellite: ISS
Catalog Number: 25544
Epoch time: 11297
62483753 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 229
1681 deg
Eccentricity:
0018572
Arg of perigee: 350
3037 deg
Mean anomaly: 9
7758 deg
Mean motion: 15
60073496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2112
Checksum: 310
Coasting Arc #5 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2011/298/14:01:29
130
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5229299
37 A = 6771767
77 meter
Y = -4225684
77 meter E =
0027017
Z = -647175
92 I = 51
42088
XDOT = 2586
754130 Wp = 10
50037
YDOT = -4105
214442 meter/sec RA = 223
34476 deg
ZDOT = 5968
431239 TA = 342
45934
MA = 342
55247
Ha = 216
485 n
mi
Hp = 202
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17156494
01 X = -5178514
33
Y = -13863795
16 feet Y = -4283878
09 meter
Z = -2123280
59 Z = -672456
79
XDOT = 8486
726147 XDOT = 2603
472919
YDOT = -13468
551318 feet/sec YDOT = -4076
193831 meter/sec
ZDOT = 19581
467319 ZDOT = 5981
038923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20105634
40 X = 6128197
37
Y = -9048006
58 feet Y = -2757832
41 meter
Z = -2226087
49 Z = -678511
47
XDOT = 7586
026806 XDOT = 2312
220970
YDOT = 12076
833333 feet/sec YDOT = 3681
018800 meter/sec
ZDOT = 19633
007860 ZDOT = 5984
140796
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 11298
58567292
00016717 00000-0 10270-3 0 9046
2 25544 51
6414 224
3344 0018592 353
5519 6
5395 15
60125305 21279
Satellite: ISS
Catalog Number: 25544
Epoch time: 11298
58567292 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 224
3344 deg
Eccentricity:
0018592
Arg of perigee: 353
5519 deg
Mean anomaly: 6
5395 deg
Mean motion: 15
60125305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2127
Checksum: 309
Coasting Arc #6 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2011/299/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2974550
84 A = 6762787
60 meter
Y = 3016979
31 meter E =
0020283
Z = -5278474
38 I = 51
40266
XDOT = -5782
268665 Wp = 28
42195
YDOT = -5024
182473 meter/sec RA = 218
56867 deg
ZDOT = 404
962689 TA = 245
34556
MA = 245
55693
Ha = 217
863 n
mi
Hp = 203
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9759025
07 X = -2982423
63
Y = 9898226
09 feet Y = 2983671
77 meter
Z = -17317829
33 Z = -5292944
42
XDOT = -18970
697719 XDOT = -5727
624798
YDOT = -16483
538298 feet/sec YDOT = -5088
537794 meter/sec
ZDOT = 1328
617745 ZDOT = 377
004644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -159012
78 X = -48467
10
Y = -13825275
05 feet Y = -4213943
84 meter
Z = -17376914
20 Z = -5296483
45
XDOT = 24068
783954 XDOT = 7336
165349
YDOT = -1729
295838 feet/sec YDOT = -527
089372 meter/sec
ZDOT = 1214
933536 ZDOT = 370
311742
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 11299
54647900
00016717 00000-0 10270-3 0 9059
2 25544 51
6410 219
4995 0019363 344
1930 15
8619 15
59158133 21424
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
54647900 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 219
4995 deg
Eccentricity:
0019363
Arg of perigee: 344
1930 deg
Mean anomaly: 15
8619 deg
Mean motion: 15
59158133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 317
Coasting Arc #7 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2011/300/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5463642
89 A = 6767717
90 meter
Y = -204852
92 meter E =
0022079
Z = 3998641
31 I = 51
44353
XDOT = 3108
407206 Wp = 17
42938
YDOT = 5808
529967 meter/sec RA = 213
50893 deg
ZDOT = -3923
362367 TA = 113
55460
MA = 113
32251
Ha = 217
971 n
mi
Hp = 203
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17925337
58 X = 5446102
30
Y = -672089
63 feet Y = -143853
12 meter
Z = 13118901
93 Z = 4025141
82
XDOT = 10198
186373 XDOT = 3062
283572
YDOT = 19056
856847 feet/sec YDOT = 5843
032115 meter/sec
ZDOT = -12871
923776 ZDOT = -3908
373450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11929455
73 X = -3636098
11
Y = 13289566
10 feet Y = 4050659
75 meter
Z = 13226886
95 Z = 4031555
14
XDOT = -19869
983051 XDOT = -6056
370834
YDOT = -5000
499931 feet/sec YDOT = -1524
152379 meter/sec
ZDOT = -12811
109490 ZDOT = -3904
826172
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 11300
57198133
00016717 00000-0 10270-3 0 9065
2 25544 51
6406 214
3481 0019328 347
9474 12
1216 15
59198082 21585
Satellite: ISS
Catalog Number: 25544
Epoch time: 11300
57198133 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 214
3481 deg
Eccentricity:
0019328
Arg of perigee: 347
9474 deg
Mean anomaly: 12
1216 deg
Mean motion: 15
59198082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 304
Coasting Arc #8 (Orbit 2172)
---------------------------------------
Vector Time (GMT): 2011/301/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6230677
06 A = 6773911
06 meter
Y = -2356292
79 meter E =
0026582
Z = -1132059
18 I = 51
49096
XDOT = 789
665851 Wp = 6
32265
YDOT = -4894
000478 meter/sec RA = 208
48698 deg
ZDOT = 5879
274005 TA = 341
31409
MA = 341
41149
Ha = 218
003 n
mi
Hp = 203
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20441853
86 X = -6198365
96
Y = -7730619
39 feet Y = -2425787
37 meter
Z = -3714104
92 Z = -1162250
11
XDOT = 2590
767228 XDOT = 815
771667
YDOT = -16056
432015 feet/sec YDOT = -4885
024037 meter/sec
ZDOT = 19288
956708 ZDOT = 5883
173667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19593524
59 X = 5972106
29
Y = -9633144
36 feet Y = -2936182
40 meter
Z = -3837025
50 Z = -1169525
37
XDOT = 9334
025385 XDOT = 2845
010937
YDOT = 11344
950743 feet/sec YDOT = 3457
940987 meter/sec
ZDOT = 19305
067691 ZDOT = 5884
184632
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 11301
53335865
00016717 00000-0 10270-3 0 9078
2 25544 51
6410 209
5182 0019342 351
2129 8
8685 15
59248508 21733
Satellite: ISS
Catalog Number: 25544
Epoch time: 11301
53335865 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 209
5182 deg
Eccentricity:
0019342
Arg of perigee: 351
2129 deg
Mean anomaly: 8
8685 deg
Mean motion: 15
59248508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2173
Checksum: 305
Coasting Arc #9 (Orbit 2188)
---------------------------------------
Vector Time (GMT): 2011/302/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4936778
54 A = 6772326
88 meter
Y = 4079518
28 meter E =
0014799
Z = -2231848
07 I = 51
51283
XDOT = -4679
995755 Wp = 9
51031
YDOT = 2682
370922 meter/sec RA = 203
48278 deg
ZDOT = -5439
858227 TA = 195
35095
MA = 195
39589
Ha = 218
142 n
mi
Hp = 203
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16196779
97 X = 4901635
78
Y = 13384246
32 feet Y = 4134527
92 meter
Z = -7322336
18 Z = -2207949
97
XDOT = -15354
316783 XDOT = -4683
216334
YDOT = 8800
429535 feet/sec YDOT = 2630
018473 meter/sec
ZDOT = -17847
303893 ZDOT = -5462
601867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20818500
51 X = -6345478
95
Y = 3078627
69 feet Y = 938365
72 meter
Z = -7225124
66 Z = -2202218
00
XDOT = 3915
901752 XDOT = 1193
566854
YDOT = -15693
938811 feet/sec YDOT = -4783
512550 meter/sec
ZDOT = -17940
117079 ZDOT = -5468
147686
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 11302
55879590
00016717 00000-0 10270-3 0 9080
2 25544 51
6408 204
3665 0019215 354
6891 5
4058 15
59279038 21897
Satellite: ISS
Catalog Number: 25544
Epoch time: 11302
55879590 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 204
3665 deg
Eccentricity:
0019215
Arg of perigee: 354
6891 deg
Mean anomaly: 5
4058 deg
Mean motion: 15
59279038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2189
Checksum: 331
Coasting Arc #10 (Orbit 2204)
---------------------------------------
Vector Time (GMT): 2011/303/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1795343
26 A = 6764857
19 meter
Y = -4524815
78 meter E =
0017076
Z = 4684464
27 I = 51
51631
XDOT = 7158
896958 Wp = 23
57556
YDOT = 43
785649 meter/sec RA = 198
45076 deg
ZDOT = 2797
813765 TA = 38
77507
MA = 38
65265
Ha = 218
247 n
mi
Hp = 202
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5890233
78 X = -1767369
07
Y = -14845196
12 feet Y = -4544736
13 meter
Z = 15368977
27 Z = 4675810
18
XDOT = 23487
194743 XDOT = 7144
283783
YDOT = 143
653704 feet/sec YDOT = 123
759034 meter/sec
ZDOT = 9179
179018 ZDOT = 2832
556729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15118230
38 X = 4608036
62
Y = 5252669
19 feet Y = 1601013
57 meter
Z = 15333908
20 Z = 4673775
22
XDOT = -15132
059712 XDOT = -4612
251800
YDOT = 16456
920330 feet/sec YDOT = 5016
069317 meter/sec
ZDOT = 9320
791746 ZDOT = 2840
977324
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 11303
58419992
00016717 00000-0 10270-3 0 9091
2 25544 51
6405 199
2137 0019283 358
8491 1
2617 15
59340970 22055
Satellite: ISS
Catalog Number: 25544
Epoch time: 11303
58419992 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 199
2137 deg
Eccentricity:
0019283
Arg of perigee: 358
8491 deg
Mean anomaly: 1
2617 deg
Mean motion: 15
59340970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2205
Checksum: 320
Coasting Arc #11 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2011/304/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2045726
61 A = 6762306
93 meter
Y = 3782916
61 meter E =
0022979
Z = -5229064
96 I = 51
53735
XDOT = -7171
877700 Wp = 41
05314
YDOT = -2523
507910 meter/sec RA = 193
38974 deg
ZDOT = 999
650439 TA = 238
41814
MA = 238
64267
Ha = 218
221 n
mi
Hp = 202
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6711701
47 X = -2062473
74
Y = 12411143
73 feet Y = 3759946
51 meter
Z = -17155724
94 Z = -5239043
82
XDOT = -23529
782480 XDOT = -7147
982478
YDOT = -8279
225425 feet/sec YDOT = -2603
574655 meter/sec
ZDOT = 3279
693042 ZDOT = 964
867052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5230778
26 X = -1594341
21
Y = -13050634
06 feet Y = -3977833
26 meter
Z = -17196576
21 Z = -5241516
43
XDOT = 20555
283722 XDOT = 6265
250479
YDOT = -12289
658262 feet/sec YDOT = -3745
887838 meter/sec
ZDOT = 3138
008029 ZDOT = 956
464847
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 11304
54548537
00016717 00000-0 10270-3 0 9108
2 25544 51
6402 194
3834 0019292 1
8925 358
2300 15
59412022 22208
Satellite: ISS
Catalog Number: 25544
Epoch time: 11304
54548537 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 194
3834 deg
Eccentricity:
0019292
Arg of perigee: 1
8925 deg
Mean anomaly: 358
2300 deg
Mean motion: 15
59412022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 280
Coasting Arc #12 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2011/305/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5360447
31 A = 6768288
35 meter
Y = -2080600
11 meter E =
0024341
Z = 3576945
36 I = 51
58780
XDOT = 4619
546761 Wp = 35
02539
YDOT = 4227
266526 meter/sec RA = 188
34204 deg
ZDOT = -4429
514405 TA = 102
58931
MA = 102
31698
Ha = 218
270 n
mi
Hp = 202
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17586769
39 X = 5365938
28
Y = -6826115
85 feet Y = -2020625
62 meter
Z = 11735385
04 Z = 3602999
96
XDOT = 15155
993312 XDOT = 4593
451264
YDOT = 13868
984666 feet/sec YDOT = 4278
779248 meter/sec
ZDOT = -14532
527577 ZDOT = -4407
135811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5762088
62 X = -1756284
61
Y = 17893626
94 feet Y = 5453977
49 meter
Z = 11841707
09 Z = 3609352
32
XDOT = -19073
371148 XDOT = -5813
563526
YDOT = 3489
406169 feet/sec YDOT = 1063
571000 meter/sec
ZDOT = -14441
476149 ZDOT = -4401
761930
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 11305
57082547
00016717 00000-0 10270-3 0 9117
2 25544 51
6402 189
2303 0019360 5
6123 354
5246 15
59474580 22362
Satellite: ISS
Catalog Number: 25544
Epoch time: 11305
57082547 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 189
2303 deg
Eccentricity:
0019360
Arg of perigee: 5
6123 deg
Mean anomaly: 354
5246 deg
Mean motion: 15
59474580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 293
Coasting Arc #13 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2011/306/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6740317
43 A = 6773672
67 meter
Y = -30097
29 meter E =
0029223
Z = -457291
99 I = 51
63582
XDOT = -376
415931 Wp = 21
10416
YDOT = -4786
340461 meter/sec RA = 183
33428 deg
ZDOT = 6008
727268 TA = 333
94346
MA = 334
09026
Ha = 218
304 n
mi
Hp = 202
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22113902
34 X = -6737258
46
Y = -98744
38 feet Y = -105454
55 meter
Z = -1500301
79 Z = -490029
27
XDOT = -1234
960405 XDOT = -352
055692
YDOT = -15703
216736 feet/sec YDOT = -4790
413506 meter/sec
ZDOT = 19713
672138 ZDOT = 6006
957847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13733296
85 X = 4185908
88
Y = -17320872
33 feet Y = -5279401
89 meter
Z = -1633790
69 Z = -497979
40
XDOT = 11920
881919 XDOT = 3633
484809
YDOT = 7634
286146 feet/sec YDOT = 2326
930417 meter/sec
ZDOT = 19706
669950 ZDOT = 6006
593001
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 11306
53205305
00016717 00000-0 10270-3 0 9124
2 25544 51
6400 184
3991 0019274 8
8997 351
2496 15
59497684 22515
Satellite: ISS
Catalog Number: 25544
Epoch time: 11306
53205305 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 184
3991 deg
Eccentricity:
0019274
Arg of perigee: 8
8997 deg
Mean anomaly: 351
2496 deg
Mean motion: 15
59497684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2251
Checksum: 323
Coasting Arc #14 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2011/307/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5740376
48 A = 6770161
81 meter
Y = 2137979
35 meter E =
0018559
Z = -2912283
30 I = 51
65392
XDOT = -4077
205916 Wp = 26
66042
YDOT = 4095
898214 meter/sec RA = 178
33579 deg
ZDOT = -5025
871147 TA = 186
53358
MA = 186
55781
Ha = 218
383 n
mi
Hp = 201
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18833256
18 X = 5730190
00
Y = 7014367
94 feet Y = 2202114
73 meter
Z = -9554735
23 Z = -2884421
11
XDOT = -13376
659829 XDOT = -4098
289045
YDOT = 13437
986265 feet/sec YDOT = 4050
186383 meter/sec
ZDOT = -16489
078566 ZDOT = -5045
729700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17002018
83 X = -5182215
34
Y = 10815767
46 feet Y = 3296645
92 meter
Z = -9441207
09 Z = -2877679
92
XDOT = -1897
561305 XDOT = -578
376686
YDOT = -17458
194672 feet/sec YDOT = -5321
257736 meter/sec
ZDOT = -16570
243392 ZDOT = -5050
610186
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 11307
55733136
00016717 00000-0 10270-3 0 9136
2 25544 51
6393 179
2460 0019149 12
3624 347
7998 15
59524452 22676
Satellite: ISS
Catalog Number: 25544
Epoch time: 11307
55733136 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 179
2460 deg
Eccentricity:
0019149
Arg of perigee: 12
3624 deg
Mean anomaly: 347
7998 deg
Mean motion: 15
59524452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 326
Coasting Arc #15 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2011/308/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2590960
72 A = 6762821
60 meter
Y = -3695710
22 meter E =
0018313
Z = 5023058
14 I = 51
65997
XDOT = 7061
829013 Wp = 34
21982
YDOT = -2357
709582 meter/sec RA = 173
30231 deg
ZDOT = 1919
353260 TA = 37
28466
MA = 37
15768
Ha = 218
533 n
mi
Hp = 201
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8500527
31 X = -2573843
37
Y = -12125033
53 feet Y = -3724588
03 meter
Z = 16479849
53 Z = 5010512
83
XDOT = 23168
730357 XDOT = 7078
344559
YDOT = -7735
267658 feet/sec YDOT = -2278
647463 meter/sec
ZDOT = 6297
090747 ZDOT = 1953
700197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14862939
63 X = 4530224
00
Y = 216346
66 feet Y = 65942
46 meter
Z = 16428848
50 Z = 5007513
02
XDOT = -7396
279098 XDOT = -2254
385869
YDOT = 22151
940959 feet/sec YDOT = 6751
911604 meter/sec
ZDOT = 6437
274893 ZDOT = 1962
081387
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 11308
58257869
00016717 00000-0 10270-3 0 9145
2 25544 51
6393 174
0917 0019240 16
4638 343
7139 15
59562393 22835
Satellite: ISS
Catalog Number: 25544
Epoch time: 11308
58257869 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 174
0917 deg
Eccentricity:
0019240
Arg of perigee: 16
4638 deg
Mean anomaly: 343
7139 deg
Mean motion: 15
59562393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 334
Coasting Arc #16 (Orbit 2297)
---------------------------------------
Vector Time (GMT): 2011/309/12:44:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1401096
51 A = 6762620
02 meter
Y = 4334548
97 meter E =
0024018
Z = -5010079
67 I = 51
68902
XDOT = -7397
437847 Wp = 52
41820
YDOT = -86
700469 meter/sec RA = 168
24701 deg
ZDOT = 2014
632750 TA = 237
03054
MA = 237
26167
Ha = 218
410 n
mi
Hp = 201
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4596773
32 X = -1425123
75
Y = 14220961
18 feet Y = 4318746
48 meter
Z = -16437269
25 Z = -5016944
85
XDOT = -24269
809209 XDOT = -7405
705404
YDOT = -284
450357 feet/sec YDOT = -169
469292 meter/sec
ZDOT = 6609
687500 ZDOT = 1978
675419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9028035
78 X = -2751745
30
Y = -11871519
26 feet Y = -3618439
07 meter
Z = -16465463
34 Z = -5018673
22
XDOT = 13378
112886 XDOT = 4077
648808
YDOT = -19042
831695 feet/sec YDOT = -5804
255101 meter/sec
ZDOT = 6463
032260 ZDOT = 1969
932233
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 11309
54371761
00016717 00000-0 10270-3 0 9151
2 25544 51
6381 169
2596 0019156 19
6101 340
5787 15
59640392 22983
Satellite: ISS
Catalog Number: 25544
Epoch time: 11309
54371761 = yrday
fracday
Element set: 915
Inclination: 51
6381 deg
RA of node: 169
2596 deg
Eccentricity:
0019156
Arg of perigee: 19
6101 deg
Mean anomaly: 340
5787 deg
Mean motion: 15
59640392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2298
Checksum: 328
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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