[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 28th 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) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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 2772)
---------------------------------------
Vector Time (GMT): 2011/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1104572
38 A = 6727758
49 meter
Y = 4597934
75 meter E =
0012604
Z = -4797469
99 I = 51
36845
XDOT = -6063
058416 Wp = 68
18166
YDOT = -4030
817490 meter/sec RA = 229
33361 deg
ZDOT = -2467
786909 TA = 177
55794
MA = 177
55178
Ha = 193
332 n
mi
Hp = 186
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3623925
12 X = -1132600
21
Y = 15085087
78 feet Y = 4585425
88 meter
Z = -15739730
94 Z = -4802904
19
XDOT = -19891
923936 XDOT = -6005
546459
YDOT = -13224
466831 feet/sec YDOT = -4098
296800 meter/sec
ZDOT = -8096
413743 ZDOT = -2497
101175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3049933
59 X = -929619
76
Y = 15188729
32 feet Y = 4629524
70 meter
Z = -15761733
51 Z = -4804176
37
XDOT = -19144
662057 XDOT = -5835
292995
YDOT = -12366
956109 feet/sec YDOT = -3769
448222 meter/sec
ZDOT = -8214
729340 ZDOT = -2503
849503
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 11084
52025157
00016717 00000-0 10270-3 0 9008
2 25544 51
6436 230
1708 0001228 23
5805 336
5414 15
72044411 27738
Satellite: ISS
Catalog Number: 25544
Epoch time: 11084
52025157 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 230
1708 deg
Eccentricity:
0001228
Arg of perigee: 23
5805 deg
Mean anomaly: 336
5414 deg
Mean motion: 15
72044411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 270
Coasting Arc #2 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2011/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5643850
64 A = 6734407
21 meter
Y = 2475375
61 meter E =
0013944
Z = 2700929
02 I = 51
41158
XDOT = -26
242747 Wp = 96
37964
YDOT = 5714
255208 meter/sec RA = 224
15193 deg
ZDOT = -5160
957858 TA = 52
72071
MA = 52
59365
Ha = 193
226 n
mi
Hp = 186
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18516570
35 X = 5602630
59
Y = 8121311
05 feet Y = 2538258
20 meter
Z = 8861315
70 Z = 2728246
31
XDOT = -86
098250 XDOT = -65
067981
YDOT = 18747
556456 feet/sec YDOT = 5713
744463 meter/sec
ZDOT = -16932
276437 ZDOT = -5161
179869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18838118
69 X = 5741858
58
Y = 7209551
32 feet Y = 2197471
24 meter
Z = 8971601
92 Z = 2734544
26
XDOT = 1457
185043 XDOT = 444
150001
YDOT = 17350
029956 feet/sec YDOT = 5288
289131 meter/sec
ZDOT = -16933
242394 ZDOT = -5161
252282
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 11085
53733526
00016717 00000-0 10270-3 0 9017
2 25544 51
6430 224
9620 0001196 25
3133 334
8088 15
72078961 27896
Satellite: ISS
Catalog Number: 25544
Epoch time: 11085
53733526 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 224
9620 deg
Eccentricity:
0001196
Arg of perigee: 25
3133 deg
Mean anomaly: 334
8088 deg
Mean motion: 15
72078961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 307
Coasting Arc #3 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2011/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1090429
70 A = 6729835
46 meter
Y = -5165156
19 meter E =
0010545
Z = 4166167
08 I = 51
42084
XDOT = 6585
798788 Wp = 98
84805
YDOT = 1576
270880 meter/sec RA = 219
06321 deg
ZDOT = 3668
478237 TA = 313
56872
MA = 313
65622
Ha = 193
128 n
mi
Hp = 186
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3577525
27 X = -1052829
09
Y = -16946050
50 feet Y = -5177139
59 meter
Z = 13668527
16 Z = 4160961
44
XDOT = 21606
951403 XDOT = 6549
862613
YDOT = 5171
492388 feet/sec YDOT = 1649
716531 meter/sec
ZDOT = 12035
689753 ZDOT = 3700
384203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4770491
43 X = -1454045
79
Y = -16666807
13 feet Y = -5080042
81 meter
Z = 13647560
27 Z = 4159776
37
XDOT = 20613
781114 XDOT = 6283
080484
YDOT = 4086
203062 feet/sec YDOT = 1245
474693 meter/sec
ZDOT = 12164
532526 ZDOT = 3707
749514
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 11086
55437765
00016717 00000-0 10270-3 0 9027
2 25544 51
6441 219
7540 0001250 23
0935 337
0284 15
72183060 28056
Satellite: ISS
Catalog Number: 25544
Epoch time: 11086
55437765 = yrday
fracday
Element set: 902
Inclination: 51
6441 deg
RA of node: 219
7540 deg
Eccentricity:
0001250
Arg of perigee: 23
0935 deg
Mean anomaly: 337
0284 deg
Mean motion: 15
72183060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 287
Coasting Arc #4 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2011/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5651143
83 A = 6731418
36 meter
Y = -289951
60 meter E =
0006230
Z = -3651090
91 I = 51
45134
XDOT = -2498
463269 Wp = 88
39180
YDOT = -5840
330098 meter/sec RA = 213
87686 deg
ZDOT = 4337
463769 TA = 227
72109
MA = 227
77392
Ha = 193
104 n
mi
Hp = 186
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18540498
14 X = -5629745
48
Y = -951284
79 feet Y = -353026
73 meter
Z = -11978644
73 Z = -3678491
73
XDOT = -8197
057970 XDOT = -2454
040172
YDOT = -19161
187984 feet/sec YDOT = -5868
020749 meter/sec
ZDOT = 14230
524177 ZDOT = 4325
434732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18483651
92 X = -5633817
11
Y = 588180
60 feet Y = 179277
45 meter
Z = -12089317
54 Z = -3684823
99
XDOT = -9804
678832 XDOT = -2988
466108
YDOT = -17057
233867 feet/sec YDOT = -5199
044883 meter/sec
ZDOT = 14181
995377 ZDOT = 4322
672191
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 11087
50782101
00016717 00000-0 10270-3 0 9031
2 25544 51
6444 214
8719 0001468 23
3580 336
7649 15
72198543 28203
Satellite: ISS
Catalog Number: 25544
Epoch time: 11087
50782101 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 214
8719 deg
Eccentricity:
0001468
Arg of perigee: 23
3580 deg
Mean anomaly: 336
7649 deg
Mean motion: 15
72198543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 308
Coasting Arc #5 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2011/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3207063
54 A = 6732151
66 meter
Y = 4850073
85 meter E =
0005692
Z = -3399186
96 I = 51
48064
XDOT = -6109
528547 Wp = 77
39746
YDOT = 819
905456 meter/sec RA = 208
79361 deg
ZDOT = -4599
597013 TA = 142
77235
MA = 142
73288
Ha = 193
078 n
mi
Hp = 186
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10521862
00 X = 3169103
11
Y = 15912315
78 feet Y = 4885724
64 meter
Z = -11152188
18 Z = -3383699
91
XDOT = -20044
384997 XDOT = -6095
899148
YDOT = 2689
978530 feet/sec YDOT = 751
660811 meter/sec
ZDOT = -15090
541381 ZDOT = -4629
243600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12131456
58 X = 3697667
97
Y = 14769211
94 feet Y = 4501655
80 meter
Z = -11089671
52 Z = -3380131
88
XDOT = -18506
228939 XDOT = -5640
698580
YDOT = 3793
182376 feet/sec YDOT = 1156
161988 meter/sec
ZDOT = -15210
305391 ZDOT = -4636
101083
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 11088
52478779
00016717 00000-0 10270-3 0 9048
2 25544 51
6447 209
6629 0001473 27
7840 332
3401 15
72269203 28368
Satellite: ISS
Catalog Number: 25544
Epoch time: 11088
52478779 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 209
6629 deg
Eccentricity:
0001473
Arg of perigee: 27
7840 deg
Mean anomaly: 332
3401 deg
Mean motion: 15
72269203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 320
Coasting Arc #6 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2011/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859857
31 A = 6728668
29 meter
Y = -1648798
77 meter E =
0010817
Z = 4346030
23 I = 51
49752
XDOT = 4749
291376 Wp = 65
15058
YDOT = 5022
828050 meter/sec RA = 203
61147 deg
ZDOT = -3394
169644 TA = 59
17964
MA = 59
07324
Ha = 192
990 n
mi
Hp = 186
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15944413
76 X = 4856821
35
Y = -5409444
78 feet Y = -1594469
43 meter
Z = 14258629
37 Z = 4369631
89
XDOT = 15581
664619 XDOT = 4709
260221
YDOT = 16479
094652 feet/sec YDOT = 5075
713335 meter/sec
ZDOT = -11135
727177 ZDOT = -3371
195645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15113907
11 X = 4606718
89
Y = -7233794
15 feet Y = -2204860
46 meter
Z = 14353987
89 Z = 4375095
51
XDOT = 16947
380491 XDOT = 5165
561574
YDOT = 13424
921117 feet/sec YDOT = 4091
915957 meter/sec
ZDOT = -11042
956929 ZDOT = -3365
893272
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 11089
54171543
00016717 00000-0 10270-3 0 9051
2 25544 51
6453 204
4545 0001663 33
9926 326
1342 15
72312074 28528
Satellite: ISS
Catalog Number: 25544
Epoch time: 11089
54171543 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 204
4545 deg
Eccentricity:
0001663
Arg of perigee: 33
9926 deg
Mean anomaly: 326
1342 deg
Mean motion: 15
72312074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 293
Coasting Arc #7 (Orbit 2867)
---------------------------------------
Vector Time (GMT): 2011/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4970923
16 A = 6734020
79 meter
Y = -3770788
53 meter E =
0015193
Z = 2513379
19 I = 51
54546
XDOT = 4828
002162 Wp = 71
36300
YDOT = -2819
263411 meter/sec RA = 198
52571 deg
ZDOT = 5297
766249 TA = 317
13606
MA = 317
25439
Ha = 192
998 n
mi
Hp = 185
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16308803
02 X = -4940597
45
Y = -12371353
45 feet Y = -3826206
57 meter
Z = 8245994
72 Z = 2489304
77
XDOT = 15839
902106 XDOT = 4833
433536
YDOT = -9249
551872 feet/sec YDOT = -2765
242801 meter/sec
ZDOT = 17381
122865 ZDOT = 5321
233953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17873095
93 X = -5447719
64
Y = -10058529
72 feet Y = -3065839
86 meter
Z = 8148760
20 Z = 2483742
11
XDOT = 13615
217232 XDOT = 4149
918212
YDOT = -9977
900441 feet/sec YDOT = -3041
264054 meter/sec
ZDOT = 17475
953597 ZDOT = 5326
670656
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 11090
55860043
00016717 00000-0 10270-3 0 9065
2 25544 51
6460 199
2452 0001746 33
6402 326
4871 15
72413921 28682
Satellite: ISS
Catalog Number: 25544
Epoch time: 11090
55860043 = yrday
fracday
Element set: 906
Inclination: 51
6460 deg
RA of node: 199
2452 deg
Eccentricity:
0001746
Arg of perigee: 33
6402 deg
Mean anomaly: 326
4871 deg
Mean motion: 15
72413921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2868
Checksum: 301
Coasting Arc #8 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2011/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3462142
61 A = 6726206
51 meter
Y = 3136674
04 meter E =
0012913
Z = -4850799
49 I = 51
54971
XDOT = -6445
136519 Wp = 99
37112
YDOT = -3460
784630 meter/sec RA = 193
35682 deg
ZDOT = 2365
493263 TA = 193
74390
MA = 193
77909
Ha = 192
877 n
mi
Hp = 185
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11358735
61 X = -3473396
01
Y = 10290925
32 feet Y = 3097894
78 meter
Z = -15914696
50 Z = -4867646
18
XDOT = -21145
461021 XDOT = -6417
449421
YDOT = -11354
280283 feet/sec YDOT = -3532
702977 meter/sec
ZDOT = 7760
804668 ZDOT = 2334
250628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9574046
63 X = -2918169
41
Y = 11878124
96 feet Y = 3620452
49 meter
Z = -15982783
30 Z = -4871552
35
XDOT = -21801
056023 XDOT = -6644
961876
YDOT = -7313
728691 feet/sec YDOT = -2229
224505 meter/sec
ZDOT = 7634
599154 ZDOT = 2327
025822
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 11091
51189582
00016717 00000-0 10270-3 0 9075
2 25544 51
6462 194
3626 0001877 34
7795 325
3490 15
72487097 28832
Satellite: ISS
Catalog Number: 25544
Epoch time: 11091
51189582 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 194
3626 deg
Eccentricity:
0001877
Arg of perigee: 34
7795 deg
Mean anomaly: 325
3490 deg
Mean motion: 15
72487097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 341
Coasting Arc #9 (Orbit 2898)
---------------------------------------
Vector Time (GMT): 2011/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6149629
55 A = 6735286
58 meter
Y = 2201864
04 meter E =
0007714
Z = -1634789
80 I = 51
61021
XDOT = -3006
771223 Wp = 129
28550
YDOT = 4155
761864 meter/sec RA = 188
26259 deg
ZDOT = -5736
119426 TA = 68
75903
MA = 68
67666
Ha = 192
887 n
mi
Hp = 185
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20175949
96 X = 6132492
33
Y = 7223963
40 feet Y = 2270536
93 meter
Z = -5363483
58 Z = -1604956
82
XDOT = -9864
734982 XDOT = -3025
153276
YDOT = 13634
389316 feet/sec YDOT = 4122
034896 meter/sec
ZDOT = -18819
289457 ZDOT = -5750
771418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21135958
34 X = 6442240
10
Y = 3715402
79 feet Y = 1132454
77 meter
Z = -5242957
87 Z = -1598053
56
XDOT = -7044
272030 XDOT = -2147
094115
YDOT = 13540
668811 feet/sec YDOT = 4127
195853 meter/sec
ZDOT = -18878
519355 ZDOT = -5754
172699
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 11092
52870534
00016717 00000-0 10270-3 0 9082
2 25544 51
6459 189
1532 0001908 36
3447 323
7845 15
72517379 28993
Satellite: ISS
Catalog Number: 25544
Epoch time: 11092
52870534 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 189
1532 deg
Eccentricity:
0001908
Arg of perigee: 36
3447 deg
Mean anomaly: 323
7845 deg
Mean motion: 15
72517379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2899
Checksum: 339
Coasting Arc #10 (Orbit 2914)
---------------------------------------
Vector Time (GMT): 2011/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1730160
50 A = 6724608
43 meter
Y = -3979933
03 meter E =
0006238
Z = 5133606
49 I = 51
60625
XDOT = 7436
155442 Wp = 48
92680
YDOT = 1478
931003 meter/sec RA = 183
10986 deg
ZDOT = -1354
516839 TA = 54
06921
MA = 54
01135
Ha = 192
690 n
mi
Hp = 185
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5676379
59 X = 1749598
07
Y = -13057523
06 feet Y = -3960476
10 meter
Z = 16842540
97 Z = 5142059
26
XDOT = 24396
835441 XDOT = 7425
645096
YDOT = 4852
135835 feet/sec YDOT = 1562
027695 meter/sec
ZDOT = -4443
952884 ZDOT = -1318
417587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3057627
89 X = 931964
98
Y = -13864286
41 feet Y = -4225834
50 meter
Z = 16876725
22 Z = 5144025
85
XDOT = 23888
132652 XDOT = 7281
102832
YDOT = 16
004520 feet/sec YDOT = 4
878178 meter/sec
ZDOT = -4298
094790 ZDOT = -1310
059292
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 11093
54547366
00016717 00000-0 10270-3 0 9090
2 25544 51
6463 183
9432 0002050 35
4190 324
7108 15
72616028 29156
Satellite: ISS
Catalog Number: 25544
Epoch time: 11093
54547366 = yrday
fracday
Element set: 909
Inclination: 51
6463 deg
RA of node: 183
9432 deg
Eccentricity:
0002050
Arg of perigee: 35
4190 deg
Mean anomaly: 324
7108 deg
Mean motion: 15
72616028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2915
Checksum: 300
Coasting Arc #11 (Orbit 2930)
---------------------------------------
Vector Time (GMT): 2011/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6678267
23 A = 6735882
99 meter
Y = -351585
87 meter E =
0015575
Z = 738730
82 I = 51
67442
XDOT = 920
618629 Wp = 50
97122
YDOT = -4763
073704 meter/sec RA = 178
00421 deg
ZDOT = 5981
350747 TA = 317
07414
MA = 317
19559
Ha = 192
817 n
mi
Hp = 185
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21910325
57 X = -6677428
03
Y = -1153496
96 feet Y = -426261
55 meter
Z = 2423657
54 Z = 706289
68
XDOT = 3020
402325 XDOT = 944
755303
YDOT = -15626
882232 feet/sec YDOT = -4752
643281 meter/sec
ZDOT = 19623
854158 ZDOT = 5985
882207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21704418
97 X = -6615506
90
Y = 3305961
97 feet Y = 1007657
21 meter
Z = 2292564
19 Z = 698773
56
XDOT = -77
323855 XDOT = -23
568311
YDOT = -14307
549998 feet/sec YDOT = -4360
941239 meter/sec
ZDOT = 19642
203321 ZDOT = 5986
943572
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 11094
56220513
00016717 00000-0 10270-3 0 9107
2 25544 51
6460 178
7339 0002237 39
6868 320
4458 15
72626309 29318
Satellite: ISS
Catalog Number: 25544
Epoch time: 11094
56220513 = yrday
fracday
Element set: 910
Inclination: 51
6460 deg
RA of node: 178
7339 deg
Eccentricity:
0002237
Arg of perigee: 39
6868 deg
Mean anomaly: 320
4458 deg
Mean motion: 15
72626309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2931
Checksum: 309
Coasting Arc #12 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2011/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 102251
90 A = 6723890
59 meter
Y = 4189065
19 meter E =
0016448
Z = -5272550
42 I = 51
66410
XDOT = -7649
498501 Wp = 86
78019
YDOT = 657
210910 meter/sec RA = 172
87170 deg
ZDOT = 375
718542 TA = 186
78128
MA = 186
80357
Ha = 192
733 n
mi
Hp = 185
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 335472
11 X = 81014
68
Y = 13743652
19 feet Y = 4190089
49 meter
Z = -17298393
75 Z = -5272105
57
XDOT = -25096
779858 XDOT = -7658
104214
YDOT = 2156
203773 feet/sec YDOT = 571
621489 meter/sec
ZDOT = 1232
672382 ZDOT = 338
536027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3439725
30 X = 1048428
27
Y = 13312765
50 feet Y = 4057730
92 meter
Z = -17296632
85 Z = -5272013
69
XDOT = -23050
335979 XDOT = -7025
742407
YDOT = 7353
863937 feet/sec YDOT = 2241
457728 meter/sec
ZDOT = 1082
398498 ZDOT = 329
915062
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 11095
51535278
00016717 00000-0 10270-3 0 9111
2 25544 51
6448 173
8498 0002241 40
0555 320
0773 15
72684745 29460
Satellite: ISS
Catalog Number: 25544
Epoch time: 11095
51535278 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 173
8498 deg
Eccentricity:
0002241
Arg of perigee: 40
0555 deg
Mean anomaly: 320
0773 deg
Mean motion: 15
72684745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 315
Coasting Arc #13 (Orbit 2961)
---------------------------------------
Vector Time (GMT): 2011/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6567127
46 A = 6735704
49 meter
Y = -1474495
34 meter E =
0012762
Z = 60656
94 I = 51
73425
XDOT = 1105
572638 Wp = 123
28277
YDOT = 4638
210862 meter/sec RA = 167
75273 deg
ZDOT = -6043
716780 TA = 56
05959
MA = 55
93832
Ha = 192
729 n
mi
Hp = 185
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21545693
78 X = 6582832
80
Y = -4837583
14 feet Y = -1400969
92 meter
Z = 199005
72 Z = 92598
56
XDOT = 3627
206819 XDOT = 1082
984655
YDOT = 15217
227238 feet/sec YDOT = 4650
447413 meter/sec
ZDOT = -19828
467126 ZDOT = -6038
400986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19795145
51 X = 6033560
35
Y = -9782805
63 feet Y = -2981799
16 meter
Z = 328119
83 Z = 100010
92
XDOT = 6515
905726 XDOT = 1986
048065
YDOT = 12460
036597 feet/sec YDOT = 3797
819155 meter/sec
ZDOT = -19807
027993 ZDOT = -6037
182132
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 11096
53200670
00016717 00000-0 10270-3 0 9120
2 25544 51
6442 168
6392 0002410 45
9209 314
2152 15
72759475 29624
Satellite: ISS
Catalog Number: 25544
Epoch time: 11096
53200670 = yrday
fracday
Element set: 912
Inclination: 51
6442 deg
RA of node: 168
6392 deg
Eccentricity:
0002410
Arg of perigee: 45
9209 deg
Mean anomaly: 314
2152 deg
Mean motion: 15
72759475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2962
Checksum: 298
Coasting Arc #14 (Orbit 2977)
---------------------------------------
Vector Time (GMT): 2011/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1787907
56 A = 6723500
98 meter
Y = -3786772
72 meter E =
0004311
Z = 5256448
14 I = 51
72369
XDOT = 7202
775603 Wp = 83
83079
YDOT = -2680
808299 meter/sec RA = 162
63824 deg
ZDOT = 518
747875 TA = 1
24859
MA = 1
24752
Ha = 192
632 n
mi
Hp = 184
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5865838
46 X = -1770965
34
Y = -12423795
02 feet Y = -3806671
26 meter
Z = 17245564
76 Z = 5247803
71
XDOT = 23631
153554 XDOT = 7229
697579
YDOT = -8795
302819 feet/sec YDOT = -2600
111946 meter/sec
ZDOT = 1701
928723 ZDOT = 553
804727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8912964
79 X = -2716671
67
Y = -10512864
94 feet Y = -3204321
23 meter
Z = 17210664
63 Z = 5245810
58
XDOT = 19866
911059 XDOT = 6055
434491
YDOT = -13825
692281 feet/sec YDOT = -4214
071007 meter/sec
ZDOT = 1843
663566 ZDOT = 561
948655
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 11097
54861949
00016717 00000-0 10270-3 0 9135
2 25544 51
6443 163
4279 0002354 46
5311 313
6047 15
72840513 29787
Satellite: ISS
Catalog Number: 25544
Epoch time: 11097
54861949 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 163
4279 deg
Eccentricity:
0002354
Arg of perigee: 46
5311 deg
Mean anomaly: 313
6047 deg
Mean motion: 15
72840513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2978
Checksum: 316
Coasting Arc #15 (Orbit 2992)
---------------------------------------
Vector Time (GMT): 2011/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5892619
97 A = 6735170
66 meter
Y = 3143607
71 meter E =
0012870
Z = -825943
46 I = 51
79107
XDOT = -2904
006186 Wp = 41
01940
YDOT = -3889
474034 meter/sec RA = 157
50737 deg
ZDOT = 5976
521440 TA = 309
99441
MA = 310
10732
Ha = 192
663 n
mi
Hp = 184
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19332742
67 X = -5923322
12
Y = 10313673
60 feet Y = 3077541
18 meter
Z = -2709788
26 Z = -854644
62
XDOT = -9527
579351 XDOT = -2889
330535
YDOT = -12760
741581 feet/sec YDOT = -3921
866191 meter/sec
ZDOT = 19608
009974 ZDOT = 5962
449443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15827278
44 X = -4824154
47
Y = 15132136
65 feet Y = 4612275
25 meter
Z = -2825854
27 Z = -861320
38
XDOT = -11619
855529 XDOT = -3541
731965
YDOT = -8538
871579 feet/sec YDOT = -2602
648057 meter/sec
ZDOT = 19551
169653 ZDOT = 5959
196510
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 11098
50166070
00016717 00000-0 10270-3 0 9146
2 25544 51
6435 158
5425 0002668 46
9550 313
1835 15
72834258 29939
Satellite: ISS
Catalog Number: 25544
Epoch time: 11098
50166070 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 158
5425 deg
Eccentricity:
0002668
Arg of perigee: 46
9550 deg
Mean anomaly: 313
1835 deg
Mean motion: 15
72834258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2993
Checksum: 319
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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