[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 16th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19913 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 3103)
---------------------------------------
Vector Time (GMT): 2011/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4730451
84 A = 6724126
75 meter
Y = 592772
27 meter E =
0010353
Z = 4735640
72 I = 51
92021
XDOT = 1834
283032 Wp = 114
48507
YDOT = -6979
780384 meter/sec RA = 121
75202 deg
ZDOT = 2697
167777 TA = 309
06166
MA = 309
15373
Ha = 192
061 n
mi
Hp = 183
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15519855
12 X = -4759733
69
Y = 1944790
90 feet Y = 539710
18 meter
Z = 15536878
99 Z = 4712588
96
XDOT = 6017
988951 XDOT = 1899
093559
YDOT = -22899
541941 feet/sec YDOT = -6958
905703 meter/sec
ZDOT = 8848
975646 ZDOT = 2706
236785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13677792
69 X = -4168991
21
Y = 7775300
45 feet Y = 2369911
58 meter
Z = 15443620
48 Z = 4707215
52
XDOT = -2690
923064 XDOT = -820
193350
YDOT = -22440
571502 feet/sec YDOT = -6839
886194 meter/sec
ZDOT = 8885
780666 ZDOT = 2708
385947
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 11105
55235500
00016717 00000-0 10270-3 0 9000
2 25544 51
6422 122
3918 0002692 103
4244 256
7219 15
73438916 31042
Satellite: ISS
Catalog Number: 25544
Epoch time: 11105
55235500 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 122
3918 deg
Eccentricity:
0002692
Arg of perigee: 103
4244 deg
Mean anomaly: 256
7219 deg
Mean motion: 15
73438916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 276
Coasting Arc #2 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2011/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -905857
19 A = 6730760
83 meter
Y = 6182676
83 meter E =
0007109
Z = -2502949
02 I = 51
95934
XDOT = -5363
496802 Wp = 68
71725
YDOT = 1371
806361 meter/sec RA = 116
60006 deg
ZDOT = 5344
319274 TA = 263
11022
MA = 263
19111
Ha = 191
771 n
mi
Hp = 183
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2971972
40 X = -962766
76
Y = 20284372
80 feet Y = 6172228
57 meter
Z = -8211775
01 Z = -2507488
47
XDOT = -17596
774285 XDOT = -5404
399916
YDOT = 4500
677037 feet/sec YDOT = 1311
600237 meter/sec
ZDOT = 17533
855886 ZDOT = 5318
163734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5407674
87 X = 1648259
30
Y = 19767185
56 feet Y = 6025038
16 meter
Z = -8230253
71 Z = -2508581
33
XDOT = -12997
009558 XDOT = -3961
488513
YDOT = 10791
982190 feet/sec YDOT = 3289
396171 meter/sec
ZDOT = 17428
023328 ZDOT = 5312
061510
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 11106
50501318
00016717 00000-0 10270-3 0 9010
2 25544 51
6427 117
5041 0002713 107
5080 252
6379 15
73534764 31193
Satellite: ISS
Catalog Number: 25544
Epoch time: 11106
50501318 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 117
5041 deg
Eccentricity:
0002713
Arg of perigee: 107
5080 deg
Mean anomaly: 252
6379 deg
Mean motion: 15
73534764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 277
Coasting Arc #3 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2011/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4576144
62 A = 6724271
61 meter
Y = -1755100
95 meter E =
0012484
Z = -4615422
50 I = 51
94907
XDOT = -286
131451 Wp = 77
94229
YDOT = 7082
861633 meter/sec RA = 111
53294 deg
ZDOT = -2981
283289 TA = 162
58623
MA = 162
54338
Ha = 191
681 n
mi
Hp = 183
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15013597
84 X = 4617851
56
Y = -5758205
22 feet Y = -1703694
84 meter
Z = -15142462
27 Z = -4593089
88
XDOT = -938
751481 XDOT = -350
829373
YDOT = 23237
735015 feet/sec YDOT = 7079
299992 meter/sec
ZDOT = -9781
113154 ZDOT = -2982
830960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11358894
54 X = 3462191
06
Y = -11500851
34 feet Y = -3505459
49 meter
Z = -15052081
06 Z = -4587874
31
XDOT = 7991
138663 XDOT = 2435
699064
YDOT = 20684
086552 feet/sec YDOT = 6304
509581 meter/sec
ZDOT = -9787
520761 ZDOT = -2983
236328
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 11107
52114098
00016717 00000-0 10270-3 0 9029
2 25544 51
6414 112
2884 0002595 110
9126 249
2315 15
73569936 31352
Satellite: ISS
Catalog Number: 25544
Epoch time: 11107
52114098 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 112
2884 deg
Eccentricity:
0002595
Arg of perigee: 110
9126 deg
Mean anomaly: 249
2315 deg
Mean motion: 15
73569936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 295
Coasting Arc #4 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2011/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -394211
18 A = 6729966
95 meter
Y = -6144005
42 meter E =
0016120
Z = 2699468
36 I = 51
97893
XDOT = 5024
001612 Wp = 103
14557
YDOT = -2624
853916 meter/sec RA = 106
37796 deg
ZDOT = -5218
211425 TA = 46
20834
MA = 46
07511
Ha = 191
503 n
mi
Hp = 183
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1293343
76 X = -338592
17
Y = -20157498
11 feet Y = -6148102
65 meter
Z = 8856523
49 Z = 2697688
59
XDOT = 16482
944922 XDOT = 5078
329356
YDOT = -8611
725446 feet/sec YDOT = -2568
368918 meter/sec
ZDOT = -17120
116224 ZDOT = -5193
672381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9884012
67 X = -3012647
06
Y = -17618987
84 feet Y = -5370267
49 meter
Z = 8849465
37 Z = 2697317
05
XDOT = 9984
600467 XDOT = 3043
306222
YDOT = -14187
008977 feet/sec YDOT = -4324
200336 meter/sec
ZDOT = -17020
780440 ZDOT = -5187
933878
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 11108
53722495
00016717 00000-0 10270-3 0 9038
2 25544 51
6409 107
0730 0002505 112
1208 248
0221 15
73665839 31514
Satellite: ISS
Catalog Number: 25544
Epoch time: 11108
53722495 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 107
0730 deg
Eccentricity:
0002505
Arg of perigee: 112
1208 deg
Mean anomaly: 248
0221 deg
Mean motion: 15
73665839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 276
Coasting Arc #5 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2011/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4144512
94 A = 6724292
21 meter
Y = 2785423
40 meter E =
0011415
Z = 4496906
42 I = 51
96741
XDOT = -1166
303216 Wp = 113
77852
YDOT = -6912
359168 meter/sec RA = 101
31435 deg
ZDOT = 3195
830084 TA = 304
38845
MA = 304
49634
Ha = 191
473 n
mi
Hp = 183
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13597483
41 X = -4197197
53
Y = 9138528
22 feet Y = 2738782
40 meter
Z = 14753629
98 Z = 4476644
08
XDOT = -3826
454120 XDOT = -1104
446211
YDOT = -22678
343728 feet/sec YDOT = -6925
055594 meter/sec
ZDOT = 10485
006838 ZDOT = 3190
314402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8180725
39 X = -2493485
10
Y = 14279156
42 feet Y = 4352286
88 meter
Z = 14671580
51 Z = 4471897
74
XDOT = -12543
927280 XDOT = -3823
389035
YDOT = -17973
741850 feet/sec YDOT = -5478
396516 meter/sec
ZDOT = 10462
868696 ZDOT = 3189
082378
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 11109
55326611
00016717 00000-0 10270-3 0 9042
2 25544 51
6405 101
8577 0002449 118
6374 241
5036 15
73711440 31672
Satellite: ISS
Catalog Number: 25544
Epoch time: 11109
55326611 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 101
8577 deg
Eccentricity:
0002449
Arg of perigee: 118
6374 deg
Mean anomaly: 241
5036 deg
Mean motion: 15
73711440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 288
Coasting Arc #6 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2011/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1610278
33 A = 6729327
03 meter
Y = 5878960
19 meter E =
0006399
Z = -2855379
35 I = 51
99012
XDOT = -4415
177189 Wp = 82
48273
YDOT = 3686
407794 meter/sec RA = 96
15834 deg
ZDOT = 5110
568313 TA = 244
94282
MA = 245
00926
Ha = 191
320 n
mi
Hp = 183
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5283065
38 X = 1558290
07
Y = 19287927
14 feet Y = 5896676
67 meter
Z = -9368042
48 Z = -2847682
70
XDOT = -14485
489465 XDOT = -4480
897666
YDOT = 12094
513761 feet/sec YDOT = 3636
667051 meter/sec
ZDOT = 16766
956408 ZDOT = 5088
959558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13626915
77 X = 4153483
93
Y = 14656790
25 feet Y = 4467389
67 meter
Z = -9337065
87 Z = -2845937
68
XDOT = -6301
577978 XDOT = -1920
720968
YDOT = 16462
313716 feet/sec YDOT = 5017
713221 meter/sec
ZDOT = 16679
421201 ZDOT = 5083
887582
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 11110
50576419
00016717 00000-0 10270-3 0 9053
2 25544 51
6408 96
9684 0002561 120
1567 239
9850 15
73762992 31825
Satellite: ISS
Catalog Number: 25544
Epoch time: 11110
50576419 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 96
9684 deg
Eccentricity:
0002561
Arg of perigee: 120
1567 deg
Mean anomaly: 239
9850 deg
Mean motion: 15
73762992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 322
Coasting Arc #7 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2011/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3549894
88 A = 6724136
78 meter
Y = -3590498
02 meter E =
0011059
Z = -4451131
09 I = 51
97567
XDOT = 2452
556896 Wp = 80
23533
YDOT = 6502
970272 meter/sec RA = 91
09472 deg
ZDOT = -3294
694205 TA = 156
84873
MA = 156
79886
Ha = 191
179 n
mi
Hp = 183
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11646636
74 X = 3611403
62
Y = -11779849
13 feet Y = -3550456
88 meter
Z = -14603448
47 Z = -4433736
29
XDOT = 8046
446510 XDOT = 2395
662304
YDOT = 21335
204306 feet/sec YDOT = 6530
078243 meter/sec
ZDOT = -10809
364188 ZDOT = -3282
917584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4710961
15 X = 1435900
96
Y = -15945840
07 feet Y = -4860292
05 meter
Z = -14532953
23 Z = -4429644
15
XDOT = 16126
517099 XDOT = 4915
362412
YDOT = 14557
473130 feet/sec YDOT = 4437
117810 meter/sec
ZDOT = -10761
906730 ZDOT = -3280
229171
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 11111
52171886
00016717 00000-0 10270-3 0 9066
2 25544 51
6411 91
7518 0002521 125
5452 234
5947 15
73832495 31987
Satellite: ISS
Catalog Number: 25544
Epoch time: 11111
52171886 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 91
7518 deg
Eccentricity:
0002521
Arg of perigee: 125
5452 deg
Mean anomaly: 234
5947 deg
Mean motion: 15
73832495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 307
Coasting Arc #8 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2011/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2655201
85 A = 6728793
60 meter
Y = -5454078
35 meter E =
0015489
Z = 2894567
67 I = 51
99179
XDOT = 3661
648360 Wp = 102
94584
YDOT = -4489
070028 meter/sec RA = 85
93764 deg
ZDOT = -5080
462403 TA = 43
92193
MA = 43
79892
Ha = 190
991 n
mi
Hp = 183
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8711292
17 X = -2608077
29
Y = -17893957
85 feet Y = -5483507
04 meter
Z = 9496613
08 Z = 2881782
94
XDOT = 12013
282020 XDOT = 3736
253888
YDOT = -14727
920041 feet/sec YDOT = -4447
705936 meter/sec
ZDOT = -16668
183737 ZDOT = -5062
493007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16425383
41 X = -5006456
86
Y = -11281126
09 feet Y = -3438487
23 meter
Z = 9445050
15 Z = 2878851
29
XDOT = 2495
647659 XDOT = 760
673407
YDOT = -17581
038254 feet/sec YDOT = -5358
700460 meter/sec
ZDOT = -16595
323263 ZDOT = -5058
254531
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 11112
53762718
00016717 00000-0 10270-3 0 9079
2 25544 51
6412 86
5361 0002348 129
5924 230
5446 15
73922576 32140
Satellite: ISS
Catalog Number: 25544
Epoch time: 11112
53762718 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 86
5361 deg
Eccentricity:
0002348
Arg of perigee: 129
5924 deg
Mean anomaly: 230
5446 deg
Mean motion: 15
73922576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 303
Coasting Arc #9 (Orbit 3229)
---------------------------------------
Vector Time (GMT): 2011/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2829868
19 A = 6723675
00 meter
Y = 4193286
08 meter E =
0011435
Z = 4423078
90 I = 51
97281
XDOT = -3591
856069 Wp = 116
28935
YDOT = -5947
282217 meter/sec RA = 80
87491 deg
ZDOT = 3328
708266 TA = 300
38906
MA = 300
50205
Ha = 190
806 n
mi
Hp = 183
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9284344
44 X = -2898034
48
Y = 13757500
25 feet Y = 4161259
52 meter
Z = 14511413
71 Z = 4409165
95
XDOT = -11784
304688 XDOT = -3541
255712
YDOT = -19512
080764 feet/sec YDOT = -5987
165698 meter/sec
ZDOT = 10920
958879 ZDOT = 3311
381795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1120991
41 X = -341678
18
Y = 16608619
54 feet Y = 5062307
24 meter
Z = 14454968
96 Z = 4405874
54
XDOT = -18882
509242 XDOT = -5755
388817
YDOT = -10751
518351 feet/sec YDOT = -3277
062793 meter/sec
ZDOT = 10851
035906 ZDOT = 3307
395744
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 11113
55348889
00016717 00000-0 10270-3 0 9082
2 25544 51
6419 81
3205 0002366 138
6455 221
4888 15
74017625 32305
Satellite: ISS
Catalog Number: 25544
Epoch time: 11113
55348889 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 81
3205 deg
Eccentricity:
0002366
Arg of perigee: 138
6455 deg
Mean anomaly: 221
4888 deg
Mean motion: 15
74017625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3230
Checksum: 311
Coasting Arc #10 (Orbit 3244)
---------------------------------------
Vector Time (GMT): 2011/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3582409
01 A = 6728475
15 meter
Y = 4909788
87 meter E =
0005747
Z = -2891190
90 I = 51
98305
XDOT = -2816
607381 Wp = 87
32452
YDOT = 5043
215815 meter/sec RA = 75
71550 deg
ZDOT = 5083
224461 TA = 239
63316
MA = 239
69000
Ha = 190
716 n
mi
Hp = 183
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11753310
41 X = 3541285
40
Y = 16108231
19 feet Y = 4949619
64 meter
Z = -9485534
46 Z = -2873887
45
XDOT = -9240
837863 XDOT = -2897
485551
YDOT = 16545
983645 feet/sec YDOT = 5011
266527 meter/sec
ZDOT = 16677
245607 ZDOT = 5069
345036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18470599
44 X = 5629838
71
Y = 7600845
36 feet Y = 2316737
66 meter
Z = -9415672
46 Z = -2869896
96
XDOT = 1197
413236 XDOT = 364
971554
YDOT = 17643
237269 feet/sec YDOT = 5377
658720 meter/sec
ZDOT = 16620
900194 ZDOT = 5066
050379
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 11114
50581878
00016717 00000-0 10270-3 0 9096
2 25544 51
6417 76
4297 0002388 138
0862 222
0485 15
74041100 32450
Satellite: ISS
Catalog Number: 25544
Epoch time: 11114
50581878 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 76
4297 deg
Eccentricity:
0002388
Arg of perigee: 138
0862 deg
Mean anomaly: 222
0485 deg
Mean motion: 15
74041100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3245
Checksum: 300
Coasting Arc #11 (Orbit 3260)
---------------------------------------
Vector Time (GMT): 2011/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2110766
22 A = 6723148
32 meter
Y = -4560178
27 meter E =
0010543
Z = -4476293
50 I = 51
95811
XDOT = 4548
501317 Wp = 81
70831
YDOT = 5286
678579 meter/sec RA = 70
64930 deg
ZDOT = -3245
914115 TA = 155
91937
MA = 155
87004
Ha = 190
520 n
mi
Hp = 183
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6925086
03 X = 2183347
07
Y = -14961214
81 feet Y = -4536168
61 meter
Z = -14686002
29 Z = -4465863
11
XDOT = 14922
904584 XDOT = 4504
814615
YDOT = 17344
745995 feet/sec YDOT = 5337
298397 meter/sec
ZDOT = -10649
324524 ZDOT = -3223
923725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2087145
96 X = -636162
09
Y = -16391505
15 feet Y = -4996130
77 meter
Z = -14643626
91 Z = -4463377
48
XDOT = 20748
216466 XDOT = 6324
056379
YDOT = 6777
880971 feet/sec YDOT = 2065
898120 meter/sec
ZDOT = -10560
509339 ZDOT = -3218
843246
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 11115
52159032
00016717 00000-0 10270-3 0 9104
2 25544 51
6425 71
2123 0002361 143
9541 216
1781 15
74132488 32611
Satellite: ISS
Catalog Number: 25544
Epoch time: 11115
52159032 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 71
2123 deg
Eccentricity:
0002361
Arg of perigee: 143
9541 deg
Mean anomaly: 216
1781 deg
Mean motion: 15
74132488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3261
Checksum: 269
Coasting Arc #12 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2011/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4347764
07 A = 6728316
96 meter
Y = -4311326
32 meter E =
0015247
Z = 2770589
37 I = 51
96510
XDOT = 2002
700694 Wp = 106
98372
YDOT = -5353
070820 meter/sec RA = 65
48921 deg
ZDOT = -5168
340683 TA = 41
45539
MA = 41
33982
Ha = 190
406 n
mi
Hp = 183
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14264317
80 X = -4312689
84
Y = -14144771
40 feet Y = -4359749
49 meter
Z = 9089860
12 Z = 2749553
27
XDOT = 6570
540335 XDOT = 2087
517714
YDOT = -17562
568306 feet/sec YDOT = -5330
201280 meter/sec
ZDOT = -16956
498305 ZDOT = -5158
405451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19736925
16 X = -6015814
79
Y = -3941682
53 feet Y = -1201424
84 meter
Z = 9004876
54 Z = 2744686
37
XDOT = -4371
363845 XDOT = -1332
391700
YDOT = -16899
406174 feet/sec YDOT = -5150
939002 meter/sec
ZDOT = -16916
093619 ZDOT = -5156
025335
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 11116
53731431
00016717 00000-0 10270-3 0 9116
2 25544 51
6428 65
9953 0002325 149
0229 211
1072 15
74205129 32773
Satellite: ISS
Catalog Number: 25544
Epoch time: 11116
53731431 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 65
9953 deg
Eccentricity:
0002325
Arg of perigee: 149
0229 deg
Mean anomaly: 211
1072 deg
Mean motion: 15
74205129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 283
Coasting Arc #13 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2011/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1405330
18 A = 6722321
30 meter
Y = 4741260
25 meter E =
0010506
Z = 4548961
18 I = 51
93279
XDOT = -5377
286627 Wp = 123
06726
YDOT = -4569
641939 meter/sec RA = 60
41996 deg
ZDOT = 3090
868736 TA = 296
24111
MA = 296
34906
Ha = 190
142 n
mi
Hp = 182
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4610663
33 X = -1480341
46
Y = 15555315
78 feet Y = 4725125
73 meter
Z = 14924413
33 Z = 4541951
73
XDOT = -17642
016493 XDOT = -5340
803250
YDOT = -14992
263580 feet/sec YDOT = -4629
569932 meter/sec
ZDOT = 10140
645458 ZDOT = 3064
834636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4894675
16 X = 1491896
99
Y = 15495788
31 feet Y = 4723116
28 meter
Z = 14895867
82 Z = 4540260
51
XDOT = -21943
989456 XDOT = -6688
527986
YDOT = -2749
316573 feet/sec YDOT = -837
991691 meter/sec
ZDOT = 10035
448631 ZDOT = 3058
804743
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 11117
55298871
00016717 00000-0 10270-3 0 9126
2 25544 51
6433 60
7782 0002415 158
5529 201
5736 15
74308417 32932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11117
55298871 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 60
7782 deg
Eccentricity:
0002415
Arg of perigee: 158
5529 deg
Mean anomaly: 201
5736 deg
Mean motion: 15
74308417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 312
Coasting Arc #14 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2011/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5013816
54 A = 6728350
50 meter
Y = 3660355
97 meter E =
0004882
Z = -2597495
32 I = 51
93686
XDOT = -1250
660072 Wp = 77
55996
YDOT = 5455
033427 meter/sec RA = 55
25785 deg
ZDOT = 5282
386902 TA = 253
08234
MA = 253
13587
Ha = 190
014 n
mi
Hp = 183
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16449529
31 X = 4985131
31
Y = 12009041
89 feet Y = 3716263
03 meter
Z = -8521966
26 Z = -2573207
90
XDOT = -4103
215458 XDOT = -1337
227335
YDOT = 17897
091296 feet/sec YDOT = 5440
563953 meter/sec
ZDOT = 17330
665688 ZDOT = 5276
100701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20405922
20 X = 6219725
09
Y = 256409
84 feet Y = 78153
72 meter
Z = -8423811
72 Z = -2567577
81
XDOT = 6935
605628 XDOT = 2113
972595
YDOT = 15546
854727 feet/sec YDOT = 4738
681321 meter/sec
ZDOT = 17305
014909 ZDOT = 5274
568544
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 11118
50514213
00016717 00000-0 10270-3 0 9134
2 25544 51
6431 55
8861 0002291 161
0269 199
0980 15
74335284 33086
Satellite: ISS
Catalog Number: 25544
Epoch time: 11118
50514213 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 55
8861 deg
Eccentricity:
0002291
Arg of perigee: 161
0269 deg
Mean anomaly: 199
0980 deg
Mean motion: 15
74335284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 294
Coasting Arc #15 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2011/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 826718
17 A = 6721401
66 meter
Y = -4752530
84 meter E =
0011134
Z = -4690590
36 I = 51
89713
XDOT = 6055
714834 Wp = 82
62444
YDOT = 3822
549478 meter/sec RA = 50
18206 deg
ZDOT = -2809
964276 TA = 159
74002
MA = 159
69580
Ha = 189
824 n
mi
Hp = 182
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2712329
94 X = 902586
66
Y = -15592292
77 feet Y = -4742861
92 meter
Z = -15389076
00 Z = -4686389
69
XDOT = 19867
830819 XDOT = 6026
170687
YDOT = 12541
172829 feet/sec YDOT = 3890
102876 meter/sec
ZDOT = -9219
042899 ZDOT = -2780
617262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6974113
75 X = -2125709
87
Y = -14225569
25 feet Y = -4335953
51 meter
Z = -15371886
82 Z = -4685351
10
XDOT = 22442
857004 XDOT = 6840
582815
YDOT = -1184
018309 feet/sec YDOT = -360
888780 meter/sec
ZDOT = -9100
426676 ZDOT = -2773
810051
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 11119
52072429
00016717 00000-0 10270-3 0 9146
2 25544 51
6442 50
6676 0002346 164
6819 195
4416 15
74435588 33246
Satellite: ISS
Catalog Number: 25544
Epoch time: 11119
52072429 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 50
6676 deg
Eccentricity:
0002346
Arg of perigee: 164
6819 deg
Mean anomaly: 195
4416 deg
Mean motion: 15
74435588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 316
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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