[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 19th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 2939)
---------------------------------------
Vector Time (GMT): 2011/350/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3611614
69 A = 6775124
09 meter
Y = 5190066
95 meter E =
0032740
Z = 2371187
36 I = 51
44536
XDOT = -5357
340673 Wp = 148
98495
YDOT = -1269
197602 meter/sec RA = 322
22325 deg
ZDOT = -5376
467299 TA = 4
33499
MA = 4
30670
Ha = 222
169 n
mi
Hp = 202
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11849129
56 X = -3680901
37
Y = 17027778
70 feet Y = 5149292
12 meter
Z = 7779486
10 Z = 2353474
22
XDOT = -17576
577011 XDOT = -5316
632302
YDOT = -4164
034127 feet/sec YDOT = -1328
878757 meter/sec
ZDOT = -17639
328409 ZDOT = -5402
394328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19841787
04 X = -6047776
69
Y = 6146384
55 feet Y = 1873418
01 meter
Z = 7706683
28 Z = 2348997
06
XDOT = -10790
358543 XDOT = -3288
901284
YDOT = -12561
200067 feet/sec YDOT = -3828
653780 meter/sec
ZDOT = -17745
124452 ZDOT = -5408
713933
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 11350
69790345
00016717 00000-0 10270-3 0 9000
2 25544 51
6436 322
6339 0024426 172
0140 188
1409 15
58215386 29408
Satellite: ISS
Catalog Number: 25544
Epoch time: 11350
69790345 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 322
6339 deg
Eccentricity:
0024426
Arg of perigee: 172
0140 deg
Mean anomaly: 188
1409 deg
Mean motion: 15
58215386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2940
Checksum: 302
Coasting Arc #2 (Orbit 2955)
---------------------------------------
Vector Time (GMT): 2011/351/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5278268
29 A = 6777167
07 meter
Y = -4222827
50 meter E =
0020209
Z = 609094
68 I = 51
42934
XDOT = 2567
973909 Wp = 142
56298
YDOT = 4084
872430 meter/sec RA = 317
21815 deg
ZDOT = 5946
773560 TA = 224
02831
MA = 224
18943
Ha = 221
931 n
mi
Hp = 202
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17317153
17 X = 5322137
62
Y = -13854420
93 feet Y = -4163557
40 meter
Z = 1998342
13 Z = 634842
82
XDOT = 8425
111251 XDOT = 2493
216886
YDOT = 13401
812436 feet/sec YDOT = 4113
170810 meter/sec
ZDOT = 19510
411942 ZDOT = 5959
067376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22156312
40 X = 6753244
02
Y = -702616
58 feet Y = -214157
53 meter
Z = 2103876
25 Z = 641261
48
XDOT = -1446
035332 XDOT = -440
751569
YDOT = 14090
936285 feet/sec YDOT = 4294
917380 meter/sec
ZDOT = 19560
278562 ZDOT = 5961
972906
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 11351
72401254
00016717 00000-0 10270-3 0 9014
2 25544 51
6434 317
4866 0024328 175
9324 184
2033 15
58256558 29563
Satellite: ISS
Catalog Number: 25544
Epoch time: 11351
72401254 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 317
4866 deg
Eccentricity:
0024328
Arg of perigee: 175
9324 deg
Mean anomaly: 184
2033 deg
Mean motion: 15
58256558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2956
Checksum: 311
Coasting Arc #3 (Orbit 2970)
---------------------------------------
Vector Time (GMT): 2011/352/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5483662
43 A = 6772113
08 meter
Y = 1963860
16 meter E =
0024601
Z = -3434877
93 I = 51
39205
XDOT = 644
164785 Wp = 167
47279
YDOT = -6142
706233 meter/sec RA = 312
20390 deg
ZDOT = -4570
125550 TA = 53
07170
MA = 52
84659
Ha = 221
593 n
mi
Hp = 202
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17991018
46 X = -5488529
08
Y = 6443110
77 feet Y = 1902511
45 meter
Z = -11269284
56 Z = -3461529
35
XDOT = 2113
401525 XDOT = 735
006767
YDOT = -20153
235671 feet/sec YDOT = -6134
994620 meter/sec
ZDOT = -14993
850230 ZDOT = -4566
775858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18297584
65 X = -5577103
80
Y = -5283902
15 feet Y = -1610533
38 meter
Z = -11378311
39 Z = -3468109
31
XDOT = 13212
402102 XDOT = 4027
140161
YDOT = -13703
916730 feet/sec YDOT = -4176
953819 meter/sec
ZDOT = -14979
646301 ZDOT = -4565
796192
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 11352
68597104
00016717 00000-0 10270-3 0 9021
2 25544 51
6442 312
6608 0024303 179
6571 180
4604 15
58289515 29719
Satellite: ISS
Catalog Number: 25544
Epoch time: 11352
68597104 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 312
6608 deg
Eccentricity:
0024303
Arg of perigee: 179
6571 deg
Mean anomaly: 180
4604 deg
Mean motion: 15
58289515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2971
Checksum: 314
Coasting Arc #4 (Orbit 2986)
---------------------------------------
Vector Time (GMT): 2011/353/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4383493
39 A = 6766065
28 meter
Y = 932704
45 meter E =
0027351
Z = 5073296
20 I = 51
35207
XDOT = -3385
801602 Wp = 173
85050
YDOT = 6678
538812 meter/sec RA = 307
15744 deg
ZDOT = 1670
052111 TA = 259
81067
MA = 260
11926
Ha = 221
424 n
mi
Hp = 202
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14381539
99 X = 4348092
62
Y = 3060053
99 feet Y = 981525
09 meter
Z = 16644672
58 Z = 5094505
41
XDOT = -11108
272971 XDOT = -3468
343563
YDOT = 21911
216574 feet/sec YDOT = 6640
215068 meter/sec
ZDOT = 5479
173593 ZDOT = 1653
403755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9962102
34 X = 3036448
79
Y = 10679907
51 feet Y = 3255235
81 meter
Z = 16731223
53 Z = 5099676
93
XDOT = -20893
968079 XDOT = -6368
481470
YDOT = 10872
401736 feet/sec YDOT = 3313
908049 meter/sec
ZDOT = 5410
607735 ZDOT = 1649
153238
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 11353
71204060
00016717 00000-0 10270-3 0 9033
2 25544 51
6438 307
5136 0024326 183
4049 176
6944 15
58330470 29879
Satellite: ISS
Catalog Number: 25544
Epoch time: 11353
71204060 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 307
5136 deg
Eccentricity:
0024326
Arg of perigee: 183
4049 deg
Mean anomaly: 176
6944 deg
Mean motion: 15
58330470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2987
Checksum: 306
Coasting Arc #5 (Orbit 3001)
---------------------------------------
Vector Time (GMT): 2011/354/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2300875
43 A = 6766243
12 meter
Y = -3912536
62 meter E =
0028890
Z = -5034077
92 I = 51
33573
XDOT = 5117
506495 Wp = 160
16167
YDOT = -5399
177428 meter/sec RA = 302
09089 deg
ZDOT = 1833
702951 TA = 127
81857
MA = 127
55670
Ha = 221
234 n
mi
Hp = 203
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7548803
89 X = -2232498
85
Y = -12836406
24 feet Y = -3937883
64 meter
Z = -16516003
68 Z = -5045089
93
XDOT = 16789
719471 XDOT = 5168
592964
YDOT = -17713
836705 feet/sec YDOT = -5341
664858 meter/sec
ZDOT = 6016
085796 ZDOT = 1858
687561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 979469
50 X = 298542
30
Y = -14809509
39 feet Y = -4513938
46 meter
Z = -16560652
59 Z = -5047686
91
XDOT = 22705
616389 XDOT = 6920
671875
YDOT = -5426
678355 feet/sec YDOT = -1654
051563 meter/sec
ZDOT = 6118
593045 ZDOT = 1864
947160
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 11354
67396230
00016717 00000-0 10270-3 0 9041
2 25544 51
6442 302
6869 0024239 187
1422 172
9391 15
58358601 30022
Satellite: ISS
Catalog Number: 25544
Epoch time: 11354
67396230 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 302
6869 deg
Eccentricity:
0024239
Arg of perigee: 187
1422 deg
Mean anomaly: 172
9391 deg
Mean motion: 15
58358601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3002
Checksum: 307
Coasting Arc #6 (Orbit 3017)
---------------------------------------
Vector Time (GMT): 2011/355/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -63400
58 A = 6772396
91 meter
Y = 5903489
43 meter E =
0025587
Z = 3284692
34 I = 51
34119
XDOT = -5525
177328 Wp = 161
06311
YDOT = 2549
585847 meter/sec RA = 297
04359 deg
ZDOT = -4702
472257 TA = 340
42984
MA = 340
52787
Ha = 221
005 n
mi
Hp = 203
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -208007
15 X = -145366
39
Y = 19368403
63 feet Y = 5902321
76 meter
Z = 10776549
67 Z = 3284185
94
XDOT = -18127
222205 XDOT = -5530
432769
YDOT = 8364
782962 feet/sec YDOT = 2487
771096 meter/sec
ZDOT = -15428
058587 ZDOT = -4729
326187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10756410
88 X = -3278554
04
Y = 16110035
84 feet Y = 4910338
93 meter
Z = 10773983
43 Z = 3283910
15
XDOT = -18508
513116 XDOT = -5641
394798
YDOT = -1996
119983 feet/sec YDOT = -608
417371 meter/sec
ZDOT = -15537
963612 ZDOT = -4735
971309
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 11355
69999330
00016717 00000-0 10270-3 0 9055
2 25544 51
6441 297
5397 0024202 190
7319 169
3322 15
58374782 30183
Satellite: ISS
Catalog Number: 25544
Epoch time: 11355
69999330 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 297
5397 deg
Eccentricity:
0024202
Arg of perigee: 190
7319 deg
Mean anomaly: 169
3322 deg
Mean motion: 15
58374782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3018
Checksum: 332
Coasting Arc #7 (Orbit 3032)
---------------------------------------
Vector Time (GMT): 2011/356/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2236223
35 A = 6776754
31 meter
Y = -6395134
98 meter E =
0015159
Z = -406524
04 I = 51
34397
XDOT = 4641
391785 Wp = 174
34042
YDOT = 1244
237678 meter/sec RA = 292
02460 deg
ZDOT = 5962
394533 TA = 181
26057
MA = 181
26439
Ha = 220
770 n
mi
Hp = 203
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7336690
80 X = 2309543
65
Y = -20981413
96 feet Y = -6369718
14 meter
Z = -1333740
30 Z = -395483
25
XDOT = 15227
663336 XDOT = 4598
169224
YDOT = 4082
144612 feet/sec YDOT = 1295
898063 meter/sec
ZDOT = 19561
661855 ZDOT = 5984
837648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17331702
74 X = 5282702
99
Y = -13920434
61 feet Y = -4242948
47 meter
Z = -1288102
28 Z = -392613
58
XDOT = 9646
928672 XDOT = 2940
383859
YDOT = 10193
719639 feet/sec YDOT = 3107
045746 meter/sec
ZDOT = 19653
235612 ZDOT = 5990
306215
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 11356
66187714
00016717 00000-0 10270-3 0 9069
2 25544 51
6445 292
7127 0024253 194
7064 165
3388 15
58435130 30332
Satellite: ISS
Catalog Number: 25544
Epoch time: 11356
66187714 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 292
7127 deg
Eccentricity:
0024253
Arg of perigee: 194
7064 deg
Mean anomaly: 165
3388 deg
Mean motion: 15
58435130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3033
Checksum: 315
Coasting Arc #8 (Orbit 3048)
---------------------------------------
Vector Time (GMT): 2011/357/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3724073
44 A = 6773919
16 meter
Y = 4990318
77 meter E =
0026218
Z = -2624980
11 I = 51
32375
XDOT = -2870
638452 Wp = 188
19416
YDOT = -4872
828176 meter/sec RA = 287
01077 deg
ZDOT = -5210
184035 TA = 21
64623
MA = 21
53561
Ha = 220
522 n
mi
Hp = 203
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12218088
70 X = -3766847
76
Y = 16372436
91 feet Y = 4948435
13 meter
Z = -8612139
47 Z = -2643174
74
XDOT = -9418
105156 XDOT = -2790
626128
YDOT = -15986
969083 feet/sec YDOT = -4904
481255 meter/sec
ZDOT = -17093
779643 ZDOT = -5223
935937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18853589
45 X = -5746574
06
Y = 7783799
22 feet Y = 2372502
00 meter
Z = -8686884
52 Z = -2647762
40
XDOT = 802
135561 XDOT = 244
490919
YDOT = -17127
039577 feet/sec YDOT = -5220
321663 meter/sec
ZDOT = -17149
553139 ZDOT = -5227
183797
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 11357
68786824
00016717 00000-0 10270-3 0 9070
2 25544 51
6445 287
5651 0024341 198
8904 161
1351 15
58408504 30498
Satellite: ISS
Catalog Number: 25544
Epoch time: 11357
68786824 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 287
5651 deg
Eccentricity:
0024341
Arg of perigee: 198
8904 deg
Mean anomaly: 161
1351 deg
Mean motion: 15
58408504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3049
Checksum: 332
Coasting Arc #9 (Orbit 3064)
---------------------------------------
Vector Time (GMT): 2011/358/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4338681
87 A = 6767139
88 meter
Y = -2151101
88 meter E =
0026009
Z = 4739966
34 I = 51
29344
XDOT = 643
026266 Wp = 185
29645
YDOT = 7166
726992 meter/sec RA = 281
96781 deg
ZDOT = 2639
528646 TA = 238
38821
MA = 238
64229
Ha = 220
247 n
mi
Hp = 203
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14234520
57 X = 4339387
78
Y = -7057420
88 feet Y = -2102580
85 meter
Z = 15551070
67 Z = 4761044
84
XDOT = 2109
666228 XDOT = 550
016482
YDOT = 23512
883833 feet/sec YDOT = 7173
397261 meter/sec
ZDOT = 8659
870886 ZDOT = 2642
427603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15774536
48 X = 4808078
72
Y = 949405
15 feet Y = 289378
69 meter
Z = 15637365
28 Z = 4766268
94
XDOT = -9892
944811 XDOT = -3015
369578
YDOT = 20247
515188 feet/sec YDOT = 6171
442629 meter/sec
ZDOT = 8671
125552 ZDOT = 2642
959068
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 11358
71383969
00016717 00000-0 10270-3 0 9089
2 25544 51
6443 282
4170 0024095 202
4129 157
5975 15
58451962 30658
Satellite: ISS
Catalog Number: 25544
Epoch time: 11358
71383969 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 282
4170 deg
Eccentricity:
0024095
Arg of perigee: 202
4129 deg
Mean anomaly: 157
5975 deg
Mean motion: 15
58451962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3065
Checksum: 331
Coasting Arc #10 (Orbit 3079)
---------------------------------------
Vector Time (GMT): 2011/359/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4037700
29 A = 6764863
97 meter
Y = -1495524
27 meter E =
0023682
Z = -5223857
98 I = 51
28016
XDOT = 1604
192752 Wp = 170
94102
YDOT = -7450
330292 meter/sec RA = 276
89689 deg
ZDOT = 870
537989 TA = 107
55234
MA = 107
29346
Ha = 219
900 n
mi
Hp = 203
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13247048
20 X = -3995300
77
Y = -4906575
70 feet Y = -1540438
51 meter
Z = -17138641
67 Z = -5243370
06
XDOT = 5263
099579 XDOT = 1683
155746
YDOT = -24443
340853 feet/sec YDOT = -7431
949840 meter/sec
ZDOT = 2856
095764 ZDOT = 878
521795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9119692
25 X = -2779682
20
Y = -10660911
55 feet Y = -3249445
84 meter
Z = -17218245
78 Z = -5248121
31
XDOT = 15654
232079 XDOT = 4771
409938
YDOT = -18176
094188 feet/sec YDOT = -5540
073508 meter/sec
ZDOT = 2889
317962 ZDOT = 880
664115
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 11359
67566792
00016717 00000-0 10270-3 0 9093
2 25544 51
6433 277
5895 0024156 206
3329 153
6600 15
58518674 30802
Satellite: ISS
Catalog Number: 25544
Epoch time: 11359
67566792 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 277
5895 deg
Eccentricity:
0024156
Arg of perigee: 206
3329 deg
Mean anomaly: 153
6600 deg
Mean motion: 15
58518674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3080
Checksum: 339
Coasting Arc #11 (Orbit 3095)
---------------------------------------
Vector Time (GMT): 2011/360/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2970667
70 A = 6769910
41 meter
Y = 4663593
59 meter E =
0018990
Z = 3892087
55 I = 51
29517
XDOT = -3428
832845 Wp = 183
60394
YDOT = 5551
666773 meter/sec RA = 271
83764 deg
ZDOT = -4054
766399 TA = 308
86973
MA = 309
03900
Ha = 219
538 n
mi
Hp = 204
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9746285
10 X = 2899390
97
Y = 15300503
91 feet Y = 4696414
42 meter
Z = 12769316
10 Z = 3906346
23
XDOT = -11249
451591 XDOT = -3470
960886
YDOT = 18214
129833 feet/sec YDOT = 5513
088402 meter/sec
ZDOT = -13303
039366 ZDOT = -4071
525020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1355377
68 X = 413119
12
Y = 18049279
59 feet Y = 5501420
42 meter
Z = 12827212
65 Z = 3909734
41
XDOT = -17094
751315 XDOT = -5210
480201
YDOT = 10741
096976 feet/sec YDOT = 3273
886358 meter/sec
ZDOT = -13371
956567 ZDOT = -4075
772362
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 11360
70159943
00016717 00000-0 10270-3 0 9107
2 25544 51
6435 272
4423 0024112 210
5264 149
4489 15
58569602 30964
Satellite: ISS
Catalog Number: 25544
Epoch time: 11360
70159943 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 272
4423 deg
Eccentricity:
0024112
Arg of perigee: 210
5264 deg
Mean anomaly: 149
4489 deg
Mean motion: 15
58569602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3096
Checksum: 305
Coasting Arc #12 (Orbit 3110)
---------------------------------------
Vector Time (GMT): 2011/361/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1298593
65 A = 6775898
94 meter
Y = -6555239
73 meter E =
0014929
Z = -1163374
80 I = 51
31340
XDOT = 4569
442595 Wp = 211
55906
YDOT = -1948
667556 meter/sec RA = 266
80820 deg
ZDOT = 5832
973078 TA = 135
74823
MA = 135
62876
Ha = 219
451 n
mi
Hp = 204
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4260477
87 X = -1219543
79
Y = -21506692
02 feet Y = -6569319
29 meter
Z = -3816846
46 Z = -1169491
88
XDOT = 14991
609565 XDOT = 4562
558394
YDOT = -6393
266259 feet/sec YDOT = -1897
608310 meter/sec
ZDOT = 19137
050782 ZDOT = 5855
154089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5991628
24 X = 1826248
29
Y = -21085594
37 feet Y = -6426889
16 meter
Z = -3841339
83 Z = -1170840
38
XDOT = 14618
366831 XDOT = 4455
678210
YDOT = 623
351497 feet/sec YDOT = 189
997536 meter/sec
ZDOT = 19227
843074 ZDOT = 5860
646569
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 11361
66339394
00016717 00000-0 10270-3 0 9114
2 25544 51
6417 267
6143 0024174 213
9938 145
9669 15
58554444 31119
Satellite: ISS
Catalog Number: 25544
Epoch time: 11361
66339394 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 267
6143 deg
Eccentricity:
0024174
Arg of perigee: 213
9938 deg
Mean anomaly: 145
9669 deg
Mean motion: 15
58554444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3111
Checksum: 327
Coasting Arc #13 (Orbit 3126)
---------------------------------------
Vector Time (GMT): 2011/362/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -660085
00 A = 6774816
34 meter
Y = 6431855
85 meter E =
0026605
Z = -1962098
24 I = 51
31173
XDOT = -4824
982577 Wp = 203
22053
YDOT = -2195
523472 meter/sec RA = 261
79477 deg
ZDOT = -5572
132576 TA = 358
62015
MA = 358
62748
Ha = 219
158 n
mi
Hp = 204
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2165633
19 X = -722426
89
Y = 21101889
27 feet Y = 6424125
95 meter
Z = -6437330
18 Z = -1965455
80
XDOT = -15829
995333 XDOT = -4773
005287
YDOT = -7203
160999 feet/sec YDOT = -2249
188344 meter/sec
ZDOT = -18281
274857 ZDOT = -5595
445823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11168902
32 X = -3404281
43
Y = 18029205
41 feet Y = 5495301
81 meter
Z = -6451533
98 Z = -1966427
56
XDOT = -9649
966646 XDOT = -2941
309834
YDOT = -12555
802648 feet/sec YDOT = -3827
008647 meter/sec
ZDOT = -18376
384653 ZDOT = -5601
122042
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 11362
68928861
00016717 00000-0 10270-3 0 9121
2 25544 51
6409 262
4662 0024263 217
7915 142
1537 15
58566031 31270
Satellite: ISS
Catalog Number: 25544
Epoch time: 11362
68928861 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 262
4662 deg
Eccentricity:
0024263
Arg of perigee: 217
7915 deg
Mean anomaly: 142
1537 deg
Mean motion: 15
58566031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3127
Checksum: 315
Coasting Arc #14 (Orbit 3142)
---------------------------------------
Vector Time (GMT): 2011/363/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2580108
20 A = 6768080
13 meter
Y = -4458261
78 meter E =
0022478
Z = 4408766
17 I = 51
29407
XDOT = 4036
408924 Wp = 198
94342
YDOT = 5613
654187 meter/sec RA = 256
75645 deg
ZDOT = 3298
333582 TA = 217
49163
MA = 217
64862
Ha = 218
877 n
mi
Hp = 204
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8464921
93 X = 2608352
98
Y = -14626843
11 feet Y = -4429251
76 meter
Z = 14464455
93 Z = 4421368
47
XDOT = 13242
811429 XDOT = 3957
313488
YDOT = 18417
500612 feet/sec YDOT = 5658
349348 meter/sec
ZDOT = 10821
304403 ZDOT = 3317
750346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13779845
21 X = 4200096
82
Y = -9706348
60 feet Y = -2958495
05 meter
Z = 14516287
08 Z = 4424564
30
XDOT = 3436
317062 XDOT = 1047
389441
YDOT = 21259
207975 feet/sec YDOT = 6479
806591 meter/sec
ZDOT = 10900
247354 ZDOT = 3322
395394
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 11363
71516431
00016717 00000-0 10270-3 0 9133
2 25544 51
6402 257
3158 0024122 221
7593 138
1722 15
58590601 31436
Satellite: ISS
Catalog Number: 25544
Epoch time: 11363
71516431 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 257
3158 deg
Eccentricity:
0024122
Arg of perigee: 221
7593 deg
Mean anomaly: 138
1722 deg
Mean motion: 15
58590601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3143
Checksum: 283
Coasting Arc #15 (Orbit 3157)
---------------------------------------
Vector Time (GMT): 2011/364/15:52:00
514
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4073627
04 A = 6764214
95 meter
Y = 1147682
22 meter E =
0017560
Z = -5275152
58 I = 51
28854
XDOT = -2291
179071 Wp = 187
14109
YDOT = -7326
228409 meter/sec RA = 251
68723 deg
ZDOT = 158
191813 TA = 84
47210
MA = 84
27184
Ha = 218
475 n
mi
Hp = 204
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13364918
10 X = -4060532
50
Y = 3765361
60 feet Y = 1102201
90 meter
Z = -17306931
04 Z = -5294910
12
XDOT = -7516
991702 XDOT = -2209
853897
YDOT = -24036
182443 feet/sec YDOT = -7351
395075 meter/sec
ZDOT = 519
002010 ZDOT = 147
258580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13642826
95 X = -4158333
66
Y = -1966664
87 feet Y = -599439
45 meter
Z = -17387764
31 Z = -5299790
56
XDOT = 2785
691787 XDOT = 849
078857
YDOT = -24019
294781 feet/sec YDOT = -7321
081049 meter/sec
ZDOT = 474
843353 ZDOT = 144
732254
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 11364
67690381
00016717 00000-0 10270-3 0 9147
2 25544 51
6390 252
4872 0024164 224
9336 134
9864 15
58651307 31585
Satellite: ISS
Catalog Number: 25544
Epoch time: 11364
67690381 = yrday
fracday
Element set: 914
Inclination: 51
6390 deg
RA of node: 252
4872 deg
Eccentricity:
0024164
Arg of perigee: 224
9336 deg
Mean anomaly: 134
9864 deg
Mean motion: 15
58651307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3158
Checksum: 326
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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