[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 2nd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
125/08:42:01
479 -0
7 8
8 8
9
N/A -6
7 -1
5 216
3
000/00:22:02
959 -5
8 0
1 216
2
Coasting Arc #1 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2012/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2979529
04 A = 6769537
57 meter
Y = 3764212
08 meter E =
0009238
Z = 4778577
37 I = 51
63590
XDOT = -6889
327064 Wp = 345
29853
YDOT = -2116
931490 meter/sec RA =
35462 deg
ZDOT = -2620
424276 TA = 130
57751
MA = 130
49707
Ha = 215
417 n
mi
Hp = 211
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9775357
76 X = -3044613
17
Y = 12349777
17 feet Y = 3730529
34 meter
Z = 15677747
29 Z = 4763944
70
XDOT = -22602
779083 XDOT = -6852
413565
YDOT = -6945
313286 feet/sec YDOT = -2193
765867 meter/sec
ZDOT = -8597
192505 ZDOT = -2653
802813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -165413
95 X = -50418
17
Y = 15809506
56 feet Y = 4818737
60 meter
Z = 15617250
58 Z = 4760137
98
XDOT = -20888
411371 XDOT = -6366
787786
YDOT = 8434
202148 feet/sec YDOT = 2570
744815 meter/sec
ZDOT = -8734
139164 ZDOT = -2662
165617
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 12121
54344089
00016717 00000-0 10270-3 0 9001
2 25544 51
6433
6798 0010447 301
0641 58
9488 15
57627611 10593
Satellite: ISS
Catalog Number: 25544
Epoch time: 12121
54344089 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node:
6798 deg
Eccentricity:
0010447
Arg of perigee: 301
0641 deg
Mean anomaly: 58
9488 deg
Mean motion: 15
57627611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1059
Checksum: 298
Coasting Arc #2 (Orbit 1073)
---------------------------------------
Vector Time (GMT): 2012/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5464980
36 A = 6775712
22 meter
Y = -2748745
64 meter E =
0009241
Z = -2898963
19 I = 51
62570
XDOT = 4503
729297 Wp = 330
15734
YDOT = 3638
201113 meter/sec RA = 355
33903 deg
ZDOT = 5041
470449 TA = 356
73283
MA = 356
73886
Ha = 215
696 n
mi
Hp = 211
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17929725
60 X = 5509393
86
Y = -9018194
35 feet Y = -2687384
61 meter
Z = -9511034
09 Z = -2872306
36
XDOT = 14776
014753 XDOT = 4438
220918
YDOT = 11936
355357 feet/sec YDOT = 3688
198487 meter/sec
ZDOT = 16540
257378 ZDOT = 5063
190319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8297393
26 X = 2529045
47
Y = -18331194
93 feet Y = -5587348
21 meter
Z = -9401234
83 Z = -2865496
38
XDOT = 17580
392109 XDOT = 5358
503515
YDOT = -569
173428 feet/sec YDOT = -173
484061 meter/sec
ZDOT = 16629
144272 ZDOT = 5068
563174
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 12122
50581990
00016717 00000-0 10270-3 0 9013
2 25544 51
6430 355
8565 0010523 304
5402 55
4759 15
57614938 10743
Satellite: ISS
Catalog Number: 25544
Epoch time: 12122
50581990 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 355
8565 deg
Eccentricity:
0010523
Arg of perigee: 304
5402 deg
Mean anomaly: 55
4759 deg
Mean motion: 15
57614938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1074
Checksum: 300
Coasting Arc #3 (Orbit 1089)
---------------------------------------
Vector Time (GMT): 2012/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6655500
73 A = 6779188
35 meter
Y = 1269707
65 meter E =
0002313
Z = 171323
02 I = 51
60712
XDOT = -1042
668696 Wp = 159
94352
YDOT = -4651
778524 meter/sec RA = 350
34720 deg
ZDOT = -6008
106100 TA = 18
20831
MA = 18
20003
Ha = 215
743 n
mi
Hp = 211
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21835632
32 X = -6670036
46
Y = 4165707
51 feet Y = 1195200
45 meter
Z = 562083
41 Z = 138955
12
XDOT = -3420
829056 XDOT = -961
387661
YDOT = -15261
740563 feet/sec YDOT = -4662
984050 meter/sec
ZDOT = -19711
634186 ZDOT = -6012
973795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14050709
49 X = -4282656
25
Y = 17229551
43 feet Y = 5251567
28 meter
Z = 428970
97 Z = 130750
35
XDOT = -11083
543820 XDOT = -3378
264156
YDOT = -8545
034813 feet/sec YDOT = -2604
526611 meter/sec
ZDOT = -19731
176919 ZDOT = -6014
062725
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 12123
53233514
00016717 00000-0 10270-3 0 9024
2 25544 51
6429 350
7125 0010373 307
5725 52
4487 15
57619557 10906
Satellite: ISS
Catalog Number: 25544
Epoch time: 12123
53233514 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 350
7125 deg
Eccentricity:
0010373
Arg of perigee: 307
5725 deg
Mean anomaly: 52
4487 deg
Mean motion: 15
57619557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1090
Checksum: 294
Coasting Arc #4 (Orbit 1105)
---------------------------------------
Vector Time (GMT): 2012/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6222268
01 A = 6776005
53 meter
Y = 516764
12 meter E =
0011323
Z = 2612800
54 I = 51
56663
XDOT = -2610
600604 Wp = 27
67384
YDOT = 4975
021041 meter/sec RA = 345
35293 deg
ZDOT = 5233
787705 TA = 1
85154
MA = 1
84735
Ha = 215
824 n
mi
Hp = 210
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20414265
12 X = 6203334
36
Y = 1695420
33 feet Y = 586239
59 meter
Z = 8572180
25 Z = 2642982
57
XDOT = -8564
962611 XDOT = -2691
463291
YDOT = 16322
247511 feet/sec YDOT = 4945
375727 meter/sec
ZDOT = 17171
219505 ZDOT = 5220
908723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16482171
68 X = 5023765
93
Y = -12075359
36 feet Y = -3680569
53 meter
Z = 8696128
89 Z = 2650580
09
XDOT = 3282
194754 XDOT = 1000
412961
YDOT = 16805
794192 feet/sec YDOT = 5122
406070 meter/sec
ZDOT = 17117
817598 ZDOT = 5217
510804
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 12124
55882506
00016717 00000-0 10270-3 0 9039
2 25544 51
6422 345
5666 0010645 311
9579 48
0667 15
57688960 11062
Satellite: ISS
Catalog Number: 25544
Epoch time: 12124
55882506 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 345
5666 deg
Eccentricity:
0010645
Arg of perigee: 311
9579 deg
Mean anomaly: 48
0667 deg
Mean motion: 15
57688960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1106
Checksum: 325
Coasting Arc #5 (Orbit 1118)
---------------------------------------
Vector Time (GMT): 2012/125/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4999244
47 A = 6777124
06 meter
Y = -1810631
03 meter E =
0002807
Z = -4202938
49 I = 51
52300
XDOT = 4796
036803 Wp = 336
11051
YDOT = -4731
675816 meter/sec RA = 340
98845 deg
ZDOT = -3662
929545 TA = 256
27437
MA = 256
30562
Ha = 216
330 n
mi
Hp = 216
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16401720
71 X = -4958208
70
Y = -5940390
52 feet Y = -1866306
30 meter
Z = -13789168
28 Z = -4227125
42
XDOT = 15735
028882 XDOT = 4866
384980
YDOT = -15523
870786 feet/sec YDOT = -4677
650282 meter/sec
ZDOT = -12017
485385 ZDOT = -3639
459158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15751532
33 X = -4801067
05
Y = -7310861
57 feet Y = -2228350
61 meter
Z = -13888353
97 Z = -4233170
29
XDOT = 16540
845399 XDOT = 5041
649678
YDOT = -12971
609432 feet/sec YDOT = -3953
746555 meter/sec
ZDOT = -11920
595806 ZDOT = -3633
397602
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 12125
39286982
00016717 00000-0 10270-3 0 9049
2 25544 51
6394 341
3868 0008743 268
7221 91
2931 15
55709613 11192
Satellite: ISS
Catalog Number: 25544
Epoch time: 12125
39286982 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 341
3868 deg
Eccentricity:
0008743
Arg of perigee: 268
7221 deg
Mean anomaly: 91
2931 deg
Mean motion: 15
55709613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1119
Checksum: 325
Coasting Arc #6 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2012/126/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3097885
08 A = 6773270
24 meter
Y = 3115575
10 meter E =
0005649
Z = 5159906
42 I = 51
48145
XDOT = -6366
847214 Wp = 247
23055
YDOT = 4042
292187 meter/sec RA = 335
96845 deg
ZDOT = 1380
813935 TA = 189
45623
MA = 189
46687
Ha = 216
044 n
mi
Hp = 215
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10163664
95 X = 3037749
58
Y = 10221703
07 feet Y = 3149881
26 meter
Z = 16928826
84 Z = 5174810
14
XDOT = -20888
606345 XDOT = -6418
283586
YDOT = 13262
113475 feet/sec YDOT = 3970
806547 meter/sec
ZDOT = 4530
229447 ZDOT = 1349
758449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9340823
00 X = 2847082
85
Y = 10884217
10 feet Y = 3317509
37 meter
Z = 16989741
64 Z = 5178473
25
XDOT = -20976
842102 XDOT = -6393
741473
YDOT = 11125
831707 feet/sec YDOT = 3391
153504 meter/sec
ZDOT = 4402
248297 ZDOT = 1341
805281
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 12126
42065494
00016717 00000-0 10270-3 0 9058
2 25544 51
6390 336
2498 0008797 272
3465 87
6682 15
55736660 11352
Satellite: ISS
Catalog Number: 25544
Epoch time: 12126
42065494 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 336
2498 deg
Eccentricity:
0008797
Arg of perigee: 272
3465 deg
Mean anomaly: 87
6682 deg
Mean motion: 15
55736660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1135
Checksum: 334
Coasting Arc #7 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2012/127/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -873640
19 A = 6773045
43 meter
Y = -4255374
52 meter E =
0005290
Z = -5201077
18 I = 51
45373
XDOT = 7023
285785 Wp = 103
18129
YDOT = -2851
709107 meter/sec RA = 330
93847 deg
ZDOT = 1153
272930 TA = 177
90790
MA = 177
90569
Ha = 216
640 n
mi
Hp = 215
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2866273
60 X = -800724
56
Y = -13961202
51 feet Y = -4264736
18 meter
Z = -17063901
50 Z = -5205144
46
XDOT = 23042
276198 XDOT = 7049
049714
YDOT = -9356
001008 feet/sec YDOT = -2773
026381 meter/sec
ZDOT = 3783
703839 ZDOT = 1187
454977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2047565
15 X = -624097
86
Y = -14084824
28 feet Y = -4293054
44 meter
Z = -17080182
55 Z = -5206039
64
XDOT = 22438
441573 XDOT = 6839
236992
YDOT = -8021
728415 feet/sec YDOT = -2445
022821 meter/sec
ZDOT = 3924
411035 ZDOT = 1196
160484
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 12127
38418468
00016717 00000-0 10270-3 0 9068
2 25544 51
6392 331
4338 0008884 276
5827 83
4315 15
55771077 11504
Satellite: ISS
Catalog Number: 25544
Epoch time: 12127
38418468 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 331
4338 deg
Eccentricity:
0008884
Arg of perigee: 276
5827 deg
Mean anomaly: 83
4315 deg
Mean motion: 15
55771077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1150
Checksum: 326
Coasting Arc #8 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2012/128/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1346734
30 A = 6776576
50 meter
Y = 5057280
36 meter E =
0004703
Z = 4307354
57 I = 51
43975
XDOT = -6722
287923 Wp = 6
39191
YDOT = 1188
104186 meter/sec RA = 325
91341 deg
ZDOT = -3491
790659 TA = 119
24943
MA = 119
20240
Ha = 216
895 n
mi
Hp = 215
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4418419
61 X = -1424110
30
Y = 16592127
15 feet Y = 5041787
39 meter
Z = 14131740
72 Z = 4300624
49
XDOT = -22054
750402 XDOT = -6718
111268
YDOT = 3897
979612 feet/sec YDOT = 1112
955015 meter/sec
ZDOT = -11456
006098 ZDOT = -3524
437629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5061838
22 X = -1542848
29
Y = 16431493
01 feet Y = 5008319
07 meter
Z = 14103582
61 Z = 4298771
98
XDOT = -20905
443865 XDOT = -6371
979290
YDOT = 3522
112909 feet/sec YDOT = 1073
540015 meter/sec
ZDOT = -11590
242393 ZDOT = -3532
705881
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 12128
41192914
00016717 00000-0 10270-3 0 9079
2 25544 51
6391 326
2969 0008978 281
2371 78
7774 15
55817343 11666
Satellite: ISS
Catalog Number: 25544
Epoch time: 12128
41192914 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 326
2969 deg
Eccentricity:
0008978
Arg of perigee: 281
2371 deg
Mean anomaly: 78
7774 deg
Mean motion: 15
55817343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1166
Checksum: 339
Coasting Arc #9 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2012/129/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3243997
71 A = 6781527
77 meter
Y = -5337458
80 meter E =
0007190
Z = -2629156
94 I = 51
43184
XDOT = 5573
864762 Wp = 318
23412
YDOT = 821
085054 meter/sec RA = 320
90226 deg
ZDOT = 5207
494128 TA = 12
01661
MA = 11
99947
Ha = 217
123 n
mi
Hp = 215
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10643037
12 X = 3316213
18
Y = -17511347
77 feet Y = -5300778
40 meter
Z = -8625842
98 Z = -2613222
59
XDOT = 18286
957881 XDOT = 5538
971780
YDOT = 2693
848603 feet/sec YDOT = 883
219898 meter/sec
ZDOT = 17084
954487 ZDOT = 5234
487403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10983811
89 X = 3347865
86
Y = -17332388
12 feet Y = -5282911
90 meter
Z = -8559842
61 Z = -2609040
03
XDOT = 16871
633428 XDOT = 5142
473869
YDOT = 2194
624578 feet/sec YDOT = 668
921571 meter/sec
ZDOT = 17195
765441 ZDOT = 5241
269306
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 12129
37542131
00016717 00000-0 10270-3 0 9086
2 25544 51
6392 321
4801 0009092 284
8638 75
1508 15
55818064 11816
Satellite: ISS
Catalog Number: 25544
Epoch time: 12129
37542131 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 321
4801 deg
Eccentricity:
0009092
Arg of perigee: 284
8638 deg
Mean anomaly: 75
1508 deg
Mean motion: 15
55818064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1181
Checksum: 306
Coasting Arc #10 (Orbit 1196)
---------------------------------------
Vector Time (GMT): 2012/130/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4595034
17 A = 6784357
82 meter
Y = 4964662
75 meter E =
0005730
Z = 461546
35 I = 51
41841
XDOT = -3795
480266 Wp = 167
41001
YDOT = -2956
863962 meter/sec RA = 315
90588 deg
ZDOT = -5972
516707 TA = 7
59454
MA = 7
58586
Ha = 217
264 n
mi
Hp = 215
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15075571
44 X = -4652450
63
Y = 16288263
61 feet Y = 4912957
16 meter
Z = 1514259
69 Z = 439084
67
XDOT = -12452
363079 XDOT = -3733
120543
YDOT = -9700
997251 feet/sec YDOT = -2998
958164 meter/sec
ZDOT = -19594
871087 ZDOT = -5990
803928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15074007
18 X = -4594557
39
Y = 16298069
46 feet Y = 4967651
57 meter
Z = 1421480
57 Z = 433267
28
XDOT = -11150
648004 XDOT = -3398
717512
YDOT = -8595
035174 feet/sec YDOT = -2619
766721 meter/sec
ZDOT = -19669
704342 ZDOT = -5995
325883
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 12130
40312707
00016717 00000-0 10270-3 0 9097
2 25544 51
6392 316
3433 0009016 287
7219 72
2950 15
55812186 11978
Satellite: ISS
Catalog Number: 25544
Epoch time: 12130
40312707 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 316
3433 deg
Eccentricity:
0009016
Arg of perigee: 287
7219 deg
Mean anomaly: 72
2950 deg
Mean motion: 15
55812186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1197
Checksum: 299
Coasting Arc #11 (Orbit 1212)
---------------------------------------
Vector Time (GMT): 2012/131/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5259160
76 A = 6782790
24 meter
Y = -3875090
12 meter E =
0010128
Z = 1799520
99 I = 51
39251
XDOT = 1694
991501 Wp = 24
25702
YDOT = 4920
279376 meter/sec RA = 310
90945 deg
ZDOT = 5639
426921 TA = 355
61096
MA = 355
61983
Ha = 217
356 n
mi
Hp = 214
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17254464
43 X = 5293360
22
Y = -12713550
27 feet Y = -3816087
86 meter
Z = 5903940
24 Z = 1825152
63
XDOT = 5560
995737 XDOT = 1612
450776
YDOT = 16142
648870 feet/sec YDOT = 4938
771865 meter/sec
ZDOT = 18502
056829 ZDOT = 5647
461048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16988590
42 X = 5178122
36
Y = -13018430
09 feet Y = -3968017
49 meter
Z = 6009632
85 Z = 1831736
09
XDOT = 4786
185943 XDOT = 1458
829475
YDOT = 14805
155544 feet/sec YDOT = 4512
611410 meter/sec
ZDOT = 18534
575333 ZDOT = 5649
338561
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 12131
43080919
00016717 00000-0 10270-3 0 9100
2 25544 51
6388 311
2050 0009261 292
7270 67
2905 15
55889803 12130
Satellite: ISS
Catalog Number: 25544
Epoch time: 12131
43080919 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 311
2050 deg
Eccentricity:
0009261
Arg of perigee: 292
7270 deg
Mean anomaly: 67
2905 deg
Mean motion: 15
55889803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1213
Checksum: 294
Coasting Arc #12 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2012/132/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5237262
37 A = 6778174
49 meter
Y = 2147852
44 meter E =
0006017
Z = -3730878
47 I = 51
35732
XDOT = 418
972862 Wp = 333
81630
YDOT = -6369
470300 meter/sec RA = 305
90101 deg
ZDOT = -4247
090286 TA = 250
97947
MA = 251
04467
Ha = 217
609 n
mi
Hp = 214
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17182619
33 X = -5242767
04
Y = 7046759
97 feet Y = 2089255
58 meter
Z = -12240414
92 Z = -3756334
16
XDOT = 1374
582880 XDOT = 510
797891
YDOT = -20897
212270 feet/sec YDOT = -6364
271403 meter/sec
ZDOT = -13934
023249 ZDOT = -4244
832279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16850380
79 X = -5135996
07
Y = 7641164
30 feet Y = 2329026
88 meter
Z = -12345212
27 Z = -3762820
70
XDOT = 1283
378539 XDOT = 391
173779
YDOT = -19707
618727 feet/sec YDOT = -6006
882188 meter/sec
ZDOT = -13924
120450 ZDOT = -4244
071913
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 12132
39424392
00016717 00000-0 10270-3 0 9114
2 25544 51
6380 306
3891 0009364 296
0920 63
9269 15
55899309 12287
Satellite: ISS
Catalog Number: 25544
Epoch time: 12132
39424392 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 306
3891 deg
Eccentricity:
0009364
Arg of perigee: 296
0920 deg
Mean anomaly: 63
9269 deg
Mean motion: 15
55899309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 325
Coasting Arc #13 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2012/133/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4604851
08 A = 6773532
31 meter
Y = 49256
86 meter E =
0003307
Z = 4969396
73 I = 51
32484
XDOT = -2287
077308 Wp = 295
53825
YDOT = 7026
921942 meter/sec RA = 300
87173 deg
ZDOT = 2052
120542 TA = 134
43176
MA = 134
40469
Ha = 217
738 n
mi
Hp = 214
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15107779
12 X = 4579817
77
Y = 161603
86 feet Y = 100610
97 meter
Z = 16303795
06 Z = 4991706
14
XDOT = -7503
534476 XDOT = -2375
452559
YDOT = 23054
205847 feet/sec YDOT = 7000
852207 meter/sec
ZDOT = 6732
678944 ZDOT = 2040
795636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14996260
27 X = 4570860
13
Y = -621457
08 feet Y = -189420
12 meter
Z = 16395450
83 Z = 4997333
41
XDOT = -6375
321252 XDOT = -1943
197918
YDOT = 22323
627716 feet/sec YDOT = 6804
241728 meter/sec
ZDOT = 6685
468995 ZDOT = 2037
730950
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 12133
42188819
00016717 00000-0 10270-3 0 9121
2 25544 51
6380 301
2509 0009285 300
9539 59
0702 15
55912644 12444
Satellite: ISS
Catalog Number: 25544
Epoch time: 12133
42188819 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 301
2509 deg
Eccentricity:
0009285
Arg of perigee: 300
9539 deg
Mean anomaly: 59
0702 deg
Mean motion: 15
55912644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 299
Coasting Arc #14 (Orbit 1258)
---------------------------------------
Vector Time (GMT): 2012/134/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3537209
78 A = 6772045
52 meter
Y = -2378056
12 meter E =
0008081
Z = -5268141
33 I = 51
30433
XDOT = 3710
841271 Wp = 58
75581
YDOT = -6688
021726 meter/sec RA = 295
82891 deg
ZDOT = 532
132378 TA = 216
31862
MA = 216
37349
Ha = 217
828 n
mi
Hp = 213
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11605018
97 X = -3484763
44
Y = -7802021
40 feet Y = -2417318
00 meter
Z = -17283928
25 Z = -5285197
68
XDOT = 12174
676086 XDOT = 3782
767301
YDOT = -21942
328496 feet/sec YDOT = -6646
122656 meter/sec
ZDOT = 1745
841134 ZDOT = 550
334072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12013374
75 X = -3661676
62
Y = -6986226
56 feet Y = -2129401
85 meter
Z = -17353778
97 Z = -5289431
83
XDOT = 10102
319716 XDOT = 3079
187049
YDOT = -21857
425462 feet/sec YDOT = -6662
143281 meter/sec
ZDOT = 1821
263083 ZDOT = 555
120988
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 12134
38528304
00016717 00000-0 10270-3 0 9135
2 25544 51
6365 296
4333 0009388 304
1888 55
8375 15
55987307 12598
Satellite: ISS
Catalog Number: 25544
Epoch time: 12134
38528304 = yrday
fracday
Element set: 913
Inclination: 51
6365 deg
RA of node: 296
4333 deg
Eccentricity:
0009388
Arg of perigee: 304
1888 deg
Mean anomaly: 55
8375 deg
Mean motion: 15
55987307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1259
Checksum: 337
Coasting Arc #15 (Orbit 1274)
---------------------------------------
Vector Time (GMT): 2012/135/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2190700
79 A = 6774971
76 meter
Y = 4514221
36 meter E =
0009268
Z = 4556717
97 I = 51
30241
XDOT = -4618
276019 Wp = 1
83089
YDOT = 5314
271758 meter/sec RA = 290
78919 deg
ZDOT = -3035
138775 TA = 118
69541
MA = 118
60221
Ha = 218
054 n
mi
Hp = 213
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7187338
54 X = 2117923
37
Y = 14810437
53 feet Y = 4538312
12 meter
Z = 14949862
11 Z = 4567183
68
XDOT = -15151
824210 XDOT = -4662
613924
YDOT = 17435
274798 feet/sec YDOT = 5262
379487 meter/sec
ZDOT = -9957
804380 ZDOT = -3057
681903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8351445
55 X = 2545520
61
Y = 14141622
88 feet Y = 4310366
66 meter
Z = 14992435
81 Z = 4569694
43
XDOT = -12494
156640 XDOT = -3808
218944
YDOT = 18066
319488 feet/sec YDOT = 5506
614180 meter/sec
ZDOT = -10050
925303 ZDOT = -3063
522032
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 12135
41288454
00016717 00000-0 10270-3 0 9140
2 25544 51
6369 291
2956 0009549 307
6445 52
3842 15
56019354 12750
Satellite: ISS
Catalog Number: 25544
Epoch time: 12135
41288454 = yrday
fracday
Element set: 914
Inclination: 51
6369 deg
RA of node: 291
2956 deg
Eccentricity:
0009549
Arg of perigee: 307
6445 deg
Mean anomaly: 52
3842 deg
Mean motion: 15
56019354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1275
Checksum: 324
Coasting Arc #16 (Orbit 1289)
---------------------------------------
Vector Time (GMT): 2012/136/08:53:02
959
Vector Time (MET): N/A
Weight (LBS) : 911677
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -765604
03 A = 6780024
48 meter
Y = -6040897
65 meter E =
0008442
Z = -2968982
43 I = 51
30821
XDOT = 4990
946503 Wp = 339
83203
YDOT = -3066
998345 meter/sec RA = 285
76330 deg
ZDOT = 4956
895620 TA = 346
00851
MA = 346
03188
Ha = 218
155 n
mi
Hp = 213
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2511824
26 X = -683573
79
Y = -19819218
00 feet Y = -6049000
39 meter
Z = -9740756
00 Z = -2972502
59
XDOT = 16374
496400 XDOT = 5000
791631
YDOT = -10062
330527 feet/sec YDOT = -3011
131533 meter/sec
ZDOT = 16262
780905 ZDOT = 4981
165525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4494002
04 X = -1369771
82
Y = -19458767
46 feet Y = -5931032
32 meter
Z = -9754655
57 Z = -2973219
02
XDOT = 13725
466618 XDOT = 4183
522225
YDOT = -11366
673179 feet/sec YDOT = -3464
561985 meter/sec
ZDOT = 16362
780814 ZDOT = 4987
375592
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 12136
37624300
00016717 00000-0 10270-3 0 9151
2 25544 51
6354 286
4773 0009469 311
3336 48
7002 15
56037103 12905
Satellite: ISS
Catalog Number: 25544
Epoch time: 12136
37624300 = yrday
fracday
Element set: 915
Inclination: 51
6354 deg
RA of node: 286
4773 deg
Eccentricity:
0009469
Arg of perigee: 311
3336 deg
Mean anomaly: 48
7002 deg
Mean motion: 15
56037103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1290
Checksum: 290
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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