[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 17th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 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 2905)
---------------------------------------
Vector Time (GMT): 2011/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2666253
97 A = 6765858
83 meter
Y = -3343833
58 meter E =
0030832
Z = -5258874
62 I = 51
46657
XDOT = 6494
079528 Wp = 135
76885
YDOT = -3989
312627 meter/sec RA = 333
11448 deg
ZDOT = -780
311534 TA = 126
89141
MA = 126
60845
Ha = 222
594 n
mi
Hp = 201
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8747552
39 X = -2603117
91
Y = -10970582
61 feet Y = -3373295
76 meter
Z = -17253525
66 Z = -5271674
16
XDOT = 21306
035198 XDOT = 6541
996744
YDOT = -13088
296019 feet/sec YDOT = -3916
423851 meter/sec
ZDOT = -2560
077211 ZDOT = -748
647490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12065508
70 X = 3677567
05
Y = -7035639
85 feet Y = -2144463
02 meter
Z = -17305512
86 Z = -5274720
32
XDOT = 9487
708304 XDOT = 2891
853491
YDOT = 22052
303268 feet/sec YDOT = 6721
542036 meter/sec
ZDOT = -2430
379747 ZDOT = -740
779747
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 11348
51735682
00016717 00000-0 10270-3 0 9001
2 25544 51
6406 333
5684 0024639 164
0735 196
1200 15
58146140 29067
Satellite: ISS
Catalog Number: 25544
Epoch time: 11348
51735682 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 333
5684 deg
Eccentricity:
0024639
Arg of perigee: 164
0735 deg
Mean anomaly: 196
1200 deg
Mean motion: 15
58146140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2906
Checksum: 302
Coasting Arc #2 (Orbit 2921)
---------------------------------------
Vector Time (GMT): 2011/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -446280
81 A = 6767789
30 meter
Y = 4759701
03 meter E =
0023465
Z = 4771978
54 I = 51
44663
XDOT = -6981
298256 Wp = 149
82870
YDOT = 1923
530178 meter/sec RA = 328
06133 deg
ZDOT = -2585
893804 TA = 325
56506
MA = 325
71689
Ha = 222
356 n
mi
Hp = 202
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1464175
89 X = -522652
81
Y = 15615817
03 feet Y = 4754283
07 meter
Z = 15656097
57 Z = 4769625
37
XDOT = -22904
521837 XDOT = -6989
726967
YDOT = 6310
794548 feet/sec YDOT = 1845
414082 meter/sec
ZDOT = -8483
903558 ZDOT = -2619
829048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15310509
35 X = -4666643
25
Y = -3449610
49 feet Y = -1051441
28 meter
Z = 15646067
71 Z = 4768921
44
XDOT = -3731
063013 XDOT = -1137
228006
YDOT = -22334
809321 feet/sec YDOT = -6807
649881 meter/sec
ZDOT = -8622
692317 ZDOT = -2628
196618
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 11349
54351031
00016717 00000-0 10270-3 0 9018
2 25544 51
6404 328
4219 0024499 168
0827 192
0912 15
58193088 29228
Satellite: ISS
Catalog Number: 25544
Epoch time: 11349
54351031 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 328
4219 deg
Eccentricity:
0024499
Arg of perigee: 168
0827 deg
Mean anomaly: 192
0912 deg
Mean motion: 15
58193088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 310
Coasting Arc #3 (Orbit 2936)
---------------------------------------
Vector Time (GMT): 2011/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3329454
76 A = 6774331
07 meter
Y = -5242913
90 meter E =
0022920
Z = -2743159
19 I = 51
44347
XDOT = 5617
168194 Wp = 159
80130
YDOT = 882
432253 meter/sec RA = 323
02926 deg
ZDOT = 5122
925131 TA = 169
09019
MA = 169
04040
Ha = 222
229 n
mi
Hp = 202
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10923408
00 X = 3401160
31
Y = -17201161
09 feet Y = -5205280
80 meter
Z = -8999866
10 Z = -2726810
92
XDOT = 18429
029508 XDOT = 5581
997066
YDOT = 2895
118939 feet/sec YDOT = 945
049923 meter/sec
ZDOT = 16807
497150 ZDOT = 5150
127814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15957463
93 X = 4863835
00
Y = 12718718
14 feet Y = 3876665
29 meter
Z = -8932632
82 Z = -2722666
48
XDOT = -3871
949954 XDOT = -1180
170346
YDOT = 16759
296093 feet/sec YDOT = 5108
233449 meter/sec
ZDOT = 16918
537604 ZDOT = 5156
770262
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
50551215
00016717 00000-0 10270-3 0 9023
2 25544 51
6404 323
5966 0024505 171
2661 188
8925 15
58212166 29375
Satellite: ISS
Catalog Number: 25544
Epoch time: 11350
50551215 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 323
5966 deg
Eccentricity:
0024505
Arg of perigee: 171
2661 deg
Mean anomaly: 188
8925 deg
Mean motion: 15
58212166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2937
Checksum: 302
Coasting Arc #4 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2011/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5135469
38 A = 6777386
45 meter
Y = 4383506
91 meter E =
0034270
Z = -220822
83 I = 51
43098
XDOT = -2973
059225 Wp = 162
68817
YDOT = -3772
191939 meter/sec RA = 318
02236 deg
ZDOT = -6010
465149 TA = 19
70794
MA = 19
57583
Ha = 221
925 n
mi
Hp = 202
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16848652
81 X = -5183032
22
Y = 14381584
36 feet Y = 4325813
01 meter
Z = -724484
35 Z = -245886
20
XDOT = -9754
131314 XDOT = -2901
459166
YDOT = -12375
957806 feet/sec YDOT = -3805
037877 meter/sec
ZDOT = -19719
373849 ZDOT = -6024
734513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12850701
50 X = -3916893
82
Y = -18039043
74 feet Y = -5498300
53 meter
Z = -827236
10 Z = -252141
56
XDOT = 11858
069046 XDOT = 3614
339445
YDOT = -7576
257895 feet/sec YDOT = -2309
243407 meter/sec
ZDOT = -19777
336438 ZDOT = -6028
132146
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
53162874
00016717 00000-0 10270-3 0 9037
2 25544 51
6410 318
4488 0024404 175
3523 184
7863 15
58243257 29533
Satellite: ISS
Catalog Number: 25544
Epoch time: 11351
53162874 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 318
4488 deg
Eccentricity:
0024404
Arg of perigee: 175
3523 deg
Mean anomaly: 184
7863 deg
Mean motion: 15
58243257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2953
Checksum: 314
Coasting Arc #5 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2011/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5562023
41 A = 6773080
30 meter
Y = -2359607
91 meter E =
0026891
Z = 3077816
29 I = 51
39546
XDOT = -205
781778 Wp = 150
10446
YDOT = 5915
998423 meter/sec RA = 313
01215 deg
ZDOT = 4866
051522 TA = 245
40555
MA = 245
68598
Ha = 221
754 n
mi
Hp = 202
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18248108
31 X = 5573044
13
Y = -7741495
77 feet Y = -2297348
49 meter
Z = 10097822
49 Z = 3104863
30
XDOT = -675
137068 XDOT = -295
558795
YDOT = 19409
443644 feet/sec YDOT = 5913
195024 meter/sec
ZDOT = 15964
735964 ZDOT = 4864
834067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6440379
83 X = 1963027
77
Y = 18686847
85 feet Y = 5695751
22 meter
Z = 10208499
29 Z = 3111550
58
XDOT = -17945
076865 XDOT = -5469
659429
YDOT = -2606
968025 feet/sec YDOT = -794
603854 meter/sec
ZDOT = 15959
260107 ZDOT = 4864
382481
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
55772419
00016717 00000-0 10270-3 0 9043
2 25544 51
6409 313
3023 0024540 179
4689 180
6496 15
58314067 29691
Satellite: ISS
Catalog Number: 25544
Epoch time: 11352
55772419 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 313
3023 deg
Eccentricity:
0024540
Arg of perigee: 179
4689 deg
Mean anomaly: 180
6496 deg
Mean motion: 15
58314067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 328
Coasting Arc #6 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2011/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4571821
29 A = 6766634
98 meter
Y = -584410
50 meter E =
0023701
Z = -4957127
56 I = 51
35398
XDOT = 3101
513081 Wp = 151
89504
YDOT = -6697
718935 meter/sec RA = 307
96828 deg
ZDOT = -2095
436207 TA = 97
77200
MA = 97
50283
Ha = 221
482 n
mi
Hp = 202
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14999413
69 X = -4540865
55
Y = -1917357
28 feet Y = -635362
01 meter
Z = -16263541
86 Z = -4979262
43
XDOT = 10175
567850 XDOT = 3186
357094
YDOT = -21974
143486 feet/sec YDOT = -6662
561386 meter/sec
ZDOT = -6874
790706 ZDOT = -2080
163327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2709528
08 X = 825864
16
Y = -14777339
76 feet Y = -4504133
16 meter
Z = -16353903
23 Z = -4984669
71
XDOT = 20321
332238 XDOT = 6193
942066
YDOT = 11175
775517 feet/sec YDOT = 3406
376378 meter/sec
ZDOT = -6811
841103 ZDOT = -2076
249168
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
51967408
00016717 00000-0 10270-3 0 9055
2 25544 51
6410 308
4753 0024336 182
8820 177
2198 15
58298851 29846
Satellite: ISS
Catalog Number: 25544
Epoch time: 11353
51967408 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 308
4753 deg
Eccentricity:
0024336
Arg of perigee: 182
8820 deg
Mean anomaly: 177
2198 deg
Mean motion: 15
58298851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 335
Coasting Arc #7 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2011/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2640945
18 A = 6765757
50 meter
Y = 3500411
77 meter E =
0021617
Z = 5147378
45 I = 51
33372
XDOT = -4969
977594 Wp = 177
58563
YDOT = 5698
193356 meter/sec RA = 302
90505 deg
ZDOT = -1346
087341 TA = 285
26716
MA = 285
50603
Ha = 221
259 n
mi
Hp = 203
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8664518
30 X = 2576601
39
Y = 11484290
58 feet Y = 3529584
22 meter
Z = 16887724
57 Z = 5160052
26
XDOT = -16305
700767 XDOT = -5026
787448
YDOT = 18694
860093 feet/sec YDOT = 5642
298493 meter/sec
ZDOT = -4416
297052 ZDOT = -1370
369149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11786856
13 X = -3592633
75
Y = 8141972
40 feet Y = 2481673
19 meter
Z = 16939195
87 Z = 5163066
90
XDOT = -17501
050711 XDOT = -5334
320257
YDOT = -16083
412715 feet/sec YDOT = -4902
224195 meter/sec
ZDOT = -4515
958744 ZDOT = -1376
464225
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
54573407
00016717 00000-0 10270-3 0 9062
2 25544 51
6414 303
3287 0024284 186
7304 173
3528 15
58326560 30001
Satellite: ISS
Catalog Number: 25544
Epoch time: 11354
54573407 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 303
3287 deg
Eccentricity:
0024284
Arg of perigee: 186
7304 deg
Mean anomaly: 173
3528 deg
Mean motion: 15
58326560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 297
Coasting Arc #8 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2011/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -230121
40 A = 6771563
40 meter
Y = -5741343
11 meter E =
0024579
Z = -3606849
79 I = 51
33761
XDOT = 5533
575901 Wp = 177
61119
YDOT = -2983
486718 meter/sec RA = 297
85187 deg
ZDOT = 4372
984737 TA = 139
47678
MA = 139
29352
Ha = 221
107 n
mi
Hp = 203
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -754991
47 X = -148381
93
Y = -18836427
53 feet Y = -5743459
03 meter
Z = -11833496
69 Z = -3607769
84
XDOT = 18154
776579 XDOT = 5545
283276
YDOT = -9788
342252 feet/sec YDOT = -2921
541918 meter/sec
ZDOT = 14347
062784 ZDOT = 4399
895110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18846657
39 X = 5744461
17
Y = -327149
08 feet Y = -99715
04 meter
Z = -11836770
54 Z = -3607847
66
XDOT = 9420
366081 XDOT = 2871
327582
YDOT = 16875
085822 feet/sec YDOT = 5143
526159 meter/sec
ZDOT = 14457
234296 ZDOT = 4406
565013
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
50764687
00016717 00000-0 10270-3 0 9072
2 25544 51
6413 298
5018 0024226 190
4816 169
5836 15
58349653 30156
Satellite: ISS
Catalog Number: 25544
Epoch time: 11355
50764687 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 298
5018 deg
Eccentricity:
0024226
Arg of perigee: 190
4816 deg
Mean anomaly: 169
5836 deg
Mean motion: 15
58349653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 332
Coasting Arc #9 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2011/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1968998
33 A = 6776749
38 meter
Y = 6407108
79 meter E =
0031854
Z = 839179
39 I = 51
34303
XDOT = -4847
958980 Wp = 170
89605
YDOT = -712
973602 meter/sec RA = 292
83065 deg
ZDOT = -5931
588592 TA = 359
95028
MA = 359
95059
Ha = 220
857 n
mi
Hp = 203
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6459968
27 X = -2044574
14
Y = 21020698
12 feet Y = 6384667
56 meter
Z = 2753213
24 Z = 829431
28
XDOT = -15905
377231 XDOT = -4810
811395
YDOT = -2339
152237 feet/sec YDOT = -766
977937 meter/sec
ZDOT = -19460
592495 ZDOT = -5955
049910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21009797
04 X = -6403786
14
Y = -6512293
78 feet Y = -1984947
14 meter
Z = 2712854
67 Z = 826878
10
XDOT = 1892
268573 XDOT = 576
763461
YDOT = -14251
234290 feet/sec YDOT = -4343
776212 meter/sec
ZDOT = -19556
369115 ZDOT = -5960
781306
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
53366993
00016717 00000-0 10270-3 0 9085
2 25544 51
6424 293
3541 0024282 194
1552 165
8926 15
58371412 30317
Satellite: ISS
Catalog Number: 25544
Epoch time: 11356
53366993 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 293
3541 deg
Eccentricity:
0024282
Arg of perigee: 194
1552 deg
Mean anomaly: 165
8926 deg
Mean motion: 15
58371412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 316
Coasting Arc #10 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2011/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3575297
45 A = 6774739
94 meter
Y = -5322510
19 meter E =
0019514
Z = 2217762
04 I = 51
32598
XDOT = 3151
421477 Wp = 162
83545
YDOT = 4391
001784 meter/sec RA = 287
81829 deg
ZDOT = 5427
110050 TA = 221
91698
MA = 222
06653
Ha = 220
611 n
mi
Hp = 203
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11729978
50 X = 3623775
63
Y = -17462303
77 feet Y = -5282258
30 meter
Z = 7276122
18 Z = 2235247
75
XDOT = 10339
309308 XDOT = 3075
722355
YDOT = 14406
173832 feet/sec YDOT = 4425
818839 meter/sec
ZDOT = 17805
479167 ZDOT = 5442
236405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17640899
35 X = 5376946
12
Y = 11413675
53 feet Y = 3478888
30 meter
Z = 7347998
60 Z = 2239669
97
XDOT = -13414
600175 XDOT = -4088
770133
YDOT = 9167
015701 feet/sec YDOT = 2794
106386 meter/sec
ZDOT = 17866
906364 ZDOT = 5445
833060
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
55967247
00016717 00000-0 10270-3 0 9098
2 25544 51
6422 288
2062 0024232 198
2007 161
8283 15
58422560 30471
Satellite: ISS
Catalog Number: 25544
Epoch time: 11357
55967247 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 288
2062 deg
Eccentricity:
0024232
Arg of perigee: 198
2007 deg
Mean anomaly: 161
8283 deg
Mean motion: 15
58422560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3047
Checksum: 313
Coasting Arc #11 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2011/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4308032
39 A = 6767869
31 meter
Y = 2570091
26 meter E =
0018965
Z = -4533756
08 I = 51
29577
XDOT = -944
678266 Wp = 178
28755
YDOT = -6975
251630 meter/sec RA = 282
78015 deg
ZDOT = -3075
452583 TA = 60
94041
MA = 60
75057
Ha = 220
198 n
mi
Hp = 203
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14133964
54 X = -4314427
51
Y = 8432057
94 feet Y = 2521881
13 meter
Z = -14874527
82 Z = -4554699
46
XDOT = -3099
338142 XDOT = -851
669545
YDOT = -22884
683827 feet/sec YDOT = -6985
295095 meter/sec
ZDOT = -10090
067529 ZDOT = -3079
816935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8885857
18 X = -2708409
27
Y = -13760485
94 feet Y = -4194196
11 meter
Z = -14960304
20 Z = -4559900
72
XDOT = 21770
264516 XDOT = 6635
576625
YDOT = -3136
864316 feet/sec YDOT = -956
116243 meter/sec
ZDOT = -10107
323195 ZDOT = -3080
712110
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
52153339
00016717 00000-0 10270-3 0 9107
2 25544 51
6429 283
3798 0024125 201
7100 158
3035 15
58460950 30623
Satellite: ISS
Catalog Number: 25544
Epoch time: 11358
52153339 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 283
3798 deg
Eccentricity:
0024125
Arg of perigee: 201
7100 deg
Mean anomaly: 158
3035 deg
Mean motion: 15
58460950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 294
Coasting Arc #12 (Orbit 3077)
---------------------------------------
Vector Time (GMT): 2011/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4142624
51 A = 6764675
35 meter
Y = 919207
69 meter E =
0022623
Z = 5274197
61 I = 51
27954
XDOT = -1287
644558 Wp = 200
72270
YDOT = 7555
039816 meter/sec RA = 277
71450 deg
ZDOT = -326
571065 TA = 252
28168
MA = 252
52874
Ha = 219
957 n
mi
Hp = 203
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13591287
75 X = 4106417
12
Y = 3015773
25 feet Y = 965329
86 meter
Z = 17303797
95 Z = 5294234
39
XDOT = -4224
555636 XDOT = -1370
444414
YDOT = 24786
876037 feet/sec YDOT = 7540
177672 meter/sec
ZDOT = -1071
427378 ZDOT = -333
026394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2340281
32 X = -713317
75
Y = 13619975
07 feet Y = 4151368
40 meter
Z = 17385591
07 Z = 5299128
16
XDOT = -23973
177391 XDOT = -7307
024469
YDOT = -2805
637298 feet/sec YDOT = -855
158248 meter/sec
ZDOT = -1098
414509 ZDOT = -334
796742
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
54749922
00016717 00000-0 10270-3 0 9110
2 25544 51
6427 278
2329 0024202 205
8830 154
1116 15
58503529 30786
Satellite: ISS
Catalog Number: 25544
Epoch time: 11359
54749922 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 278
2329 deg
Eccentricity:
0024202
Arg of perigee: 205
8830 deg
Mean anomaly: 154
1116 deg
Mean motion: 15
58503529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3078
Checksum: 310
Coasting Arc #13 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2011/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3152224
19 A = 6769134
46 meter
Y = -4305208
03 meter E =
0024131
Z = -4177537
20 I = 51
29162
XDOT = 3208
052228 Wp = 190
25102
YDOT = -5923
475039 meter/sec RA = 272
64915 deg
ZDOT = 3657
190811 TA = 117
56447
MA = 117
31913
Ha = 219
775 n
mi
Hp = 204
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10341942
89 X = -3083554
86
Y = -14124698
27 feet Y = -4340073
67 meter
Z = -13705830
72 Z = -4192684
18
XDOT = 10525
105734 XDOT = 3256
285620
YDOT = -19433
973225 feet/sec YDOT = -5887
331399 meter/sec
ZDOT = 11998
657516 ZDOT = 3672
891670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13405787
88 X = 4086084
14
Y = -11182874
81 feet Y = -3408540
24 meter
Z = -13767383
27 Z = -4196298
42
XDOT = 19274
955544 XDOT = 5875
006450
YDOT = 8148
059550 feet/sec YDOT = 2483
528551 meter/sec
ZDOT = 12063
282859 ZDOT = 3676
888615
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
50932681
00016717 00000-0 10270-3 0 9125
2 25544 51
6429 273
4055 0024118 209
2282 150
7525 15
58511787 30934
Satellite: ISS
Catalog Number: 25544
Epoch time: 11360
50932681 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 273
4055 deg
Eccentricity:
0024118
Arg of perigee: 209
2282 deg
Mean anomaly: 150
7525 deg
Mean motion: 15
58511787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 303
Coasting Arc #14 (Orbit 3108)
---------------------------------------
Vector Time (GMT): 2011/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1577462
44 A = 6775471
11 meter
Y = 6364523
89 meter E =
0026501
Z = 1637727
09 I = 51
31229
XDOT = -4467
280655 Wp = 181
29609
YDOT = 2568
611205 meter/sec RA = 267
61721 deg
ZDOT = -5707
061807 TA = 340
61804
MA = 340
71863
Ha = 219
516 n
mi
Hp = 204
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5175401
71 X = 1498220
20
Y = 20880983
89 feet Y = 6381720
81 meter
Z = 5373120
39 Z = 1645198
44
XDOT = -14656
432595 XDOT = -4467
948021
YDOT = 8427
202117 feet/sec YDOT = 2518
652184 meter/sec
ZDOT = -18723
956060 ZDOT = -5728
764798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20374062
02 X = -6210014
10
Y = 6882888
17 feet Y = 2097904
31 meter
Z = 5403160
29 Z = 1646883
26
XDOT = -9118
911785 XDOT = -2779
444312
YDOT = -12295
884093 feet/sec YDOT = -3747
785472 meter/sec
ZDOT = -18812
842549 ZDOT = -5734
154409
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
53525793
00016717 00000-0 10270-3 0 9132
2 25544 51
6427 268
2579 0024165 212
9801 146
9848 15
58510172 31095
Satellite: ISS
Catalog Number: 25544
Epoch time: 11361
53525793 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 268
2579 deg
Eccentricity:
0024165
Arg of perigee: 212
9801 deg
Mean anomaly: 146
9848 deg
Mean motion: 15
58510172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3109
Checksum: 321
Coasting Arc #15 (Orbit 3124)
---------------------------------------
Vector Time (GMT): 2011/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 361293
93 A = 6775515
76 meter
Y = -6604284
80 meter E =
0012876
Z = 1509290
42 I = 51
31498
XDOT = 4832
185735 Wp = 189
71100
YDOT = 1575
341042 meter/sec RA = 262
60322 deg
ZDOT = 5731
284193 TA = 186
84807
MA = 186
86568
Ha = 219
233 n
mi
Hp = 204
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1185347
54 X = 427785
78
Y = -21667601
05 feet Y = -6599872
93 meter
Z = 4951740
23 Z = 1511206
53
XDOT = 15853
627740 XDOT = 4786
369804
YDOT = 5168
441738 feet/sec YDOT = 1629
120882 meter/sec
ZDOT = 18803
425831 ZDOT = 5754
647351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21672856
64 X = 6605886
70
Y = -1046291
38 feet Y = -318909
61 meter
Z = 4960068
04 Z = 1511828
74
XDOT = -3624
229616 XDOT = -1104
665187
YDOT = 14601
902548 feet/sec YDOT = 4450
659897 meter/sec
ZDOT = 18898
784870 ZDOT = 5760
349628
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
56116942
00016717 00000-0 10270-3 0 9149
2 25544 51
6425 263
1088 0024065 217
1183 142
8309 15
58552997 31257
Satellite: ISS
Catalog Number: 25544
Epoch time: 11362
56116942 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 263
1088 deg
Eccentricity:
0024065
Arg of perigee: 217
1183 deg
Mean anomaly: 142
8309 deg
Mean motion: 15
58552997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3125
Checksum: 310
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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