[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 2nd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15338 57 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
153/22:38:26
098 -5
3 7
3 7
4
N/A 2
0 -1
3 189
3
000/00:16:52
195 -4
7 -0
0 183
9
163/14:26:50
821 -9
2 9
5 9
5
N/A 1
3 -0
0 191
9
000/00:33:41
641 -2
2 -0
3 190
2
163/18:35:10
758 3
6 8
5 8
6
N/A 5
3 -0
5 201
5
000/00:40:21
516 -5
7 0
4 193
2
166/15:04:46
247 8
8 9
8 9
8
N/A -3
9 0
3 205
1
000/00:29:32
493 1
9 0
6 196
1
166/19:08:05
798 -8
5 9
4 9
4
N/A -1
3 0
2 206
3
000/00:36:11
597 3
8 -0
3 205
2
Coasting Arc #1 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2011/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4184892
48 A = 6715788
50 meter
Y = 1011789
95 meter E =
0014123
Z = -5165309
54 I = 51
32976
XDOT = -3015
636090 Wp = 75
47346
YDOT = -6995
923991 meter/sec RA = 240
17388 deg
ZDOT = 1078
820158 TA = 204
83810
MA = 204
90614
Ha = 188
294 n
mi
Hp = 181
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13729962
19 X = -4170803
08
Y = 3319520
84 feet Y = 965071
53 meter
Z = -16946553
61 Z = -5185605
57
XDOT = -9893
819192 XDOT = -2942
422957
YDOT = -22952
506533 feet/sec YDOT = -7029
237476 meter/sec
ZDOT = 3539
436213 ZDOT = 1064
346790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1825021
82 X = -556266
65
Y = 13907097
55 feet Y = 4238883
33 meter
Z = -17028760
75 Z = -5190366
28
XDOT = -23969
728832 XDOT = -7305
973348
YDOT = 1093
193923 feet/sec YDOT = 333
205508 meter/sec
ZDOT = 3481
124636 ZDOT = 1061
046789
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 11152
51408285
00016717 00000-0 10270-3 0 9000
2 25544 51
6487 241
0311 0005688 353
1195 6
9890 15
75642848 38440
Satellite: ISS
Catalog Number: 25544
Epoch time: 11152
51408285 = yrday
fracday
Element set: 900
Inclination: 51
6487 deg
RA of node: 241
0311 deg
Eccentricity:
0005688
Arg of perigee: 353
1195 deg
Mean anomaly: 6
9890 deg
Mean motion: 15
75642848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 314
Coasting Arc #2 (Orbit 3859)
---------------------------------------
Vector Time (GMT): 2011/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2704125
28 A = 6726416
66 meter
Y = 5971164
23 meter E =
0004884
Z = -1510366
28 I = 51
38120
XDOT = -5037
273482 Wp = 101
97332
YDOT = 828
098617 meter/sec RA = 235
02942 deg
ZDOT = -5761
455852 TA = 94
72776
MA = 94
67199
Ha = 188
385 n
mi
Hp = 180
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8871802
11 X = 2644490
73
Y = 19590433
84 feet Y = 6001070
22 meter
Z = -4955269
96 Z = -1497373
41
XDOT = -16526
487802 XDOT = -5018
170774
YDOT = 2716
858979 feet/sec YDOT = 771
876541 meter/sec
ZDOT = -18902
414213 ZDOT = -5785
880545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21458246
83 X = 6540473
63
Y = -1598082
82 feet Y = -487095
64 meter
Z = -4902901
73 Z = -1494404
45
XDOT = -3228
342438 XDOT = -983
998775
YDOT = 14777
612406 feet/sec YDOT = 4504
216261 meter/sec
ZDOT = -19001
339303 ZDOT = -5791
608219
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 11153
52884435
00016717 00000-0 10270-3 0 9018
2 25544 51
6477 235
8082 0005677 357
3225 2
7907 15
75681732 38609
Satellite: ISS
Catalog Number: 25544
Epoch time: 11153
52884435 = yrday
fracday
Element set: 901
Inclination: 51
6477 deg
RA of node: 235
8082 deg
Eccentricity:
0005677
Arg of perigee: 357
3225 deg
Mean anomaly: 2
7907 deg
Mean motion: 15
75681732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3860
Checksum: 321
Coasting Arc #3 (Orbit 3866)
---------------------------------------
Vector Time (GMT): 2011/153/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 375403
92 A = 6725293
25 meter
Y = 5528686
40 meter E =
0005102
Z = -3816426
43 I = 51
36850
XDOT = -6012
516048 Wp = 68
40491
YDOT = -2443
709518 meter/sec RA = 232
72039 deg
ZDOT = -4134
092326 TA = 158
15469
MA = 158
13292
Ha = 189
315 n
mi
Hp = 183
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1231640
16 X = 332092
77
Y = 18138734
90 feet Y = 5532642
88 meter
Z = -12521084
08 Z = -3814706
97
XDOT = -19726
102520 XDOT = -5964
660394
YDOT = -8017
419678 feet/sec YDOT = -2510
676845 meter/sec
ZDOT = -13563
295033 ZDOT = -4163
185434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15094607
92 X = -4600836
49
Y = -10141611
14 feet Y = -3091163
08 meter
Z = -12514340
69 Z = -3814371
04
XDOT = 17676
139248 XDOT = 5387
687243
YDOT = -9437
510337 feet/sec YDOT = -2876
553151 meter/sec
ZDOT = -13680
998707 ZDOT = -4169
968406
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 11153
97281777
00016717 00000-0 10270-3 0 9028
2 25544 51
6450 233
5236 0001371 282
0921 78
0089 15
74196594 38670
Satellite: ISS
Catalog Number: 25544
Epoch time: 11153
97281777 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 233
5236 deg
Eccentricity:
0001371
Arg of perigee: 282
0921 deg
Mean anomaly: 78
0089 deg
Mean motion: 15
74196594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3867
Checksum: 322
Coasting Arc #4 (Orbit 3882)
---------------------------------------
Vector Time (GMT): 2011/154/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5438111
80 A = 6725988
24 meter
Y = 1749346
41 meter E =
0010822
Z = 3542181
71 I = 51
38997
XDOT = 896
872890 Wp = 84
31183
YDOT = 6229
989110 meter/sec RA = 227
51324 deg
ZDOT = -4440
996378 TA = 53
28072
MA = 53
18136
Ha = 189
197 n
mi
Hp = 183
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17841574
13 X = 5400938
82
Y = 5739325
50 feet Y = 1809950
24 meter
Z = 11621331
08 Z = 3568510
07
XDOT = 2942
496357 XDOT = 848
714851
YDOT = 20439
596817 feet/sec YDOT = 6239
749967 meter/sec
ZDOT = -14570
198090 ZDOT = -4436
755297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15285062
91 X = -4658887
18
Y = 10730357
92 feet Y = 3270613
09 meter
Z = 11727882
65 Z = 3574658
63
XDOT = -17358
822468 XDOT = -5290
969088
YDOT = -8775
899488 feet/sec YDOT = -2674
894164 meter/sec
ZDOT = -14553
264717 ZDOT = -4435
835086
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 11154
98851667
00016717 00000-0 10270-3 0 9032
2 25544 51
6441 228
3067 0001377 286
1889 73
9123 15
74220667 38838
Satellite: ISS
Catalog Number: 25544
Epoch time: 11154
98851667 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 228
3067 deg
Eccentricity:
0001377
Arg of perigee: 286
1889 deg
Mean anomaly: 73
9123 deg
Mean motion: 15
74220667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3883
Checksum: 334
Coasting Arc #5 (Orbit 3898)
---------------------------------------
Vector Time (GMT): 2011/155/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1158159
24 A = 6724660
60 meter
Y = -5318531
02 meter E =
0009712
Z = 3941679
92 I = 51
40751
XDOT = 6411
460723 Wp = 98
94809
YDOT = 1558
242799 meter/sec RA = 222
41022 deg
ZDOT = 3976
573249 TA = 309
67724
MA = 309
76286
Ha = 189
235 n
mi
Hp = 183
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3799735
02 X = -1117748
22
Y = -17449248
77 feet Y = -5331256
94 meter
Z = 12932020
72 Z = 3936150
92
XDOT = 21034
976124 XDOT = 6374
242237
YDOT = 5112
345141 feet/sec YDOT = 1629
730918 meter/sec
ZDOT = 13046
500162 ZDOT = 4007
629857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16389586
21 X = 4995545
88
Y = 7132267
06 feet Y = 2173915
00 meter
Z = 12909828
01 Z = 3934915
58
XDOT = -15945
254044 XDOT = -4860
113433
YDOT = 12740
501358 feet/sec YDOT = 3883
304814 meter/sec
ZDOT = 13172
224313 ZDOT = 4014
893970
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 11156
00418314
00016717 00000-0 10270-3 0 9046
2 25544 51
6442 223
0888 0001423 294
3360 65
7655 15
74272716 38997
Satellite: ISS
Catalog Number: 25544
Epoch time: 11156
00418314 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 223
0888 deg
Eccentricity:
0001423
Arg of perigee: 294
3360 deg
Mean anomaly: 65
7655 deg
Mean motion: 15
74272716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3899
Checksum: 307
Coasting Arc #6 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2011/156/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5733919
69 A = 6726138
47 meter
Y = -966791
22 meter E =
0003686
Z = -3383123
00 I = 51
43720
XDOT = -1718
942127 Wp = 80
83559
YDOT = -5919
041759 meter/sec RA = 217
20526 deg
ZDOT = 4609
688087 TA = 239
13815
MA = 239
17441
Ha = 189
090 n
mi
Hp = 183
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18812072
46 X = -5706248
19
Y = -3171887
21 feet Y = -1030756
20 meter
Z = -11099484
91 Z = -3410911
14
XDOT = -5639
573907 XDOT = -1675
019397
YDOT = -19419
428343 feet/sec YDOT = -5938
019076 meter/sec
ZDOT = 15123
648581 ZDOT = 4601
443373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13364579
84 X = 4073523
94
Y = -13521552
30 feet Y = -4121369
14 meter
Z = -11212008
44 Z = -3417420
17
XDOT = 18200
848757 XDOT = 5547
618701
YDOT = 5489
653654 feet/sec YDOT = 1673
246434 meter/sec
ZDOT = 15090
468250 ZDOT = 4599
574723
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 11156
95634147
00016717 00000-0 10270-3 0 9055
2 25544 51
6445 218
1970 0001513 299
4126 60
6886 15
74336097 39144
Satellite: ISS
Catalog Number: 25544
Epoch time: 11156
95634147 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 218
1970 deg
Eccentricity:
0001513
Arg of perigee: 299
4126 deg
Mean anomaly: 60
6886 deg
Mean motion: 15
74336097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 323
Coasting Arc #7 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2011/157/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1796235
79 A = 6723739
34 meter
Y = 5004649
17 meter E =
0006854
Z = -4122750
47 I = 51
45473
XDOT = -6689
635111 Wp = 59
64411
YDOT = -679
185194 meter/sec RA = 212
10446 deg
ZDOT = -3740
276827 TA = 171
93329
MA = 171
92226
Ha = 189
059 n
mi
Hp = 183
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5893162
05 X = 1760166
78
Y = 16419452
66 feet Y = 5024534
59 meter
Z = -13526084
22 Z = -4114111
43
XDOT = -21947
621754 XDOT = -6663
373675
YDOT = -2228
297882 feet/sec YDOT = -753
845474 meter/sec
ZDOT = -12271
249432 ZDOT = -3772
711154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16947062
09 X = -5165464
53
Y = -4250368
72 feet Y = -1295512
39 meter
Z = -13491263
51 Z = -4112137
12
XDOT = 13791
297917 XDOT = 4203
587605
YDOT = -15633
613029 feet/sec YDOT = -4765
125251 meter/sec
ZDOT = -12402
618352 ZDOT = -3780
318074
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 11157
97194705
00016717 00000-0 10270-3 0 9060
2 25544 51
6447 212
9789 0001647 304
1871 55
9136 15
74382708 39308
Satellite: ISS
Catalog Number: 25544
Epoch time: 11157
97194705 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 212
9789 deg
Eccentricity:
0001647
Arg of perigee: 304
1871 deg
Mean anomaly: 55
9136 deg
Mean motion: 15
74382708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 332
Coasting Arc #8 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2011/158/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5938292
72 A = 6726590
08 meter
Y = 208933
79 meter E =
0011765
Z = 3142847
66 I = 51
49136
XDOT = 2370
700479 Wp = 89
25045
YDOT = 5512
619190 meter/sec RA = 206
90367 deg
ZDOT = -4830
141864 TA = 54
05863
MA = 53
94954
Ha = 189
007 n
mi
Hp = 183
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19482587
65 X = 5920247
72
Y = 685478
31 feet Y = 275238
17 meter
Z = 10311180
00 Z = 3171651
94
XDOT = 7777
888709 XDOT = 2332
344953
YDOT = 18086
020964 feet/sec YDOT = 5538
915832 meter/sec
ZDOT = -15846
922125 ZDOT = -4818
717665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11176976
45 X = -3406742
42
Y = 15896421
93 feet Y = 4845229
40 meter
Z = 10427871
41 Z = 3178415
21
XDOT = -18291
211118 XDOT = -5575
161149
YDOT = -2462
248604 feet/sec YDOT = -750
493374 meter/sec
ZDOT = -15800
826438 ZDOT = -4816
091898
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 11158
98752288
00016717 00000-0 10270-3 0 9079
2 25544 51
6445 207
7606 0001562 311
5638 48
5392 15
74418778 39461
Satellite: ISS
Catalog Number: 25544
Epoch time: 11158
98752288 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 207
7606 deg
Eccentricity:
0001562
Arg of perigee: 311
5638 deg
Mean anomaly: 48
5392 deg
Mean motion: 15
74418778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 344
Coasting Arc #9 (Orbit 3961)
---------------------------------------
Vector Time (GMT): 2011/159/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2303774
93 A = 6722839
61 meter
Y = -4612210
46 meter E =
0008340
Z = 4308894
57 I = 51
50724
XDOT = 6883
646420 Wp = 103
35679
YDOT = -204
529917 meter/sec RA = 201
80392 deg
ZDOT = 3453
971879 TA = 311
66236
MA = 311
73373
Ha = 189
086 n
mi
Hp = 183
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7558316
72 X = -2272960
89
Y = -15131924
07 feet Y = -4637800
76 meter
Z = 14136793
22 Z = 4297777
28
XDOT = 22584
141798 XDOT = 6868
643153
YDOT = -671
029912 feet/sec YDOT = -127
636997 meter/sec
ZDOT = 11331
928738 ZDOT = 3487
376135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16879422
02 X = 5144847
83
Y = 1567026
87 feet Y = 477629
79 meter
Z = 14091903
32 Z = 4295212
13
XDOT = -11283
574940 XDOT = -3439
233642
YDOT = 18198
413493 feet/sec YDOT = 5546
876433 meter/sec
ZDOT = 11467
282108 ZDOT = 3495
227586
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 11160
00306694
00016717 00000-0 10270-3 0 9082
2 25544 51
6449 202
5417 0001661 316
7308 43
3725 15
74457222 39627
Satellite: ISS
Catalog Number: 25544
Epoch time: 11160
00306694 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 202
5417 deg
Eccentricity:
0001661
Arg of perigee: 316
7308 deg
Mean anomaly: 43
3725 deg
Mean motion: 15
74457222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3962
Checksum: 293
Coasting Arc #10 (Orbit 3976)
---------------------------------------
Vector Time (GMT): 2011/160/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6057436
45 A = 6727043
49 meter
Y = 569592
86 meter E =
0004371
Z = -2868101
29 I = 51
55112
XDOT = -2866
041471 Wp = 42
18897
YDOT = -5046
123406 meter/sec RA = 196
60835 deg
ZDOT = 5058
575439 TA = 284
82321
MA = 284
87163
Ha = 188
883 n
mi
Hp = 183
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19873479
17 X = -6049422
78
Y = 1868742
98 feet Y = 501899
99 meter
Z = -9409781
12 Z = -2897508
90
XDOT = -9403
023199 XDOT = -2833
975461
YDOT = -16555
522985 feet/sec YDOT = -5077
994393 meter/sec
ZDOT = 16596
376112 ZDOT = 5044
729591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8641630
93 X = 2633969
11
Y = -17930767
88 feet Y = -5465298
05 meter
Z = -9528962
88 Z = -2904427
88
XDOT = 17775
946630 XDOT = 5418
108533
YDOT = -209
950159 feet/sec YDOT = -63
992808 meter/sec
ZDOT = 16540
439731 ZDOT = 5041
526030
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 11160
95511071
00016717 00000-0 10270-3 0 9094
2 25544 51
6448 197
6491 0001862 317
2861 42
8158 15
74512647 39778
Satellite: ISS
Catalog Number: 25544
Epoch time: 11160
95511071 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 197
6491 deg
Eccentricity:
0001862
Arg of perigee: 317
2861 deg
Mean anomaly: 42
8158 deg
Mean motion: 15
74512647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3977
Checksum: 326
Coasting Arc #11 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2011/161/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2650488
27 A = 6721721
26 meter
Y = 4209141
27 meter E =
0009479
Z = -4530482
78 I = 51
56257
XDOT = -6968
278203 Wp = 59
10796
YDOT = 1074
416794 meter/sec RA = 191
50969 deg
ZDOT = -3078
440250 TA = 180
17149
MA = 180
17181
Ha = 188
872 n
mi
Hp = 183
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8695827
64 X = 2625232
27
Y = 13809518
60 feet Y = 4238639
91 meter
Z = -14863788
66 Z = -4517667
51
XDOT = -22861
805127 XDOT = -6964
820020
YDOT = 3524
989480 feet/sec YDOT = 996
512935 meter/sec
ZDOT = -10099
869588 ZDOT = -3112
283887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16352789
14 X = -4984330
13
Y = 665927
21 feet Y = 202974
61 meter
Z = -14811997
30 Z = -4514696
78
XDOT = 8446
067929 XDOT = 2574
361505
YDOT = -20296
593620 feet/sec YDOT = -6186
401735 meter/sec
ZDOT = -10237
055591 ZDOT = -3120
254544
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 11161
97059494
00016717 00000-0 10270-3 0 9105
2 25544 51
6441 192
4301 0001914 319
1011 41
0008 15
74562500 39936
Satellite: ISS
Catalog Number: 25544
Epoch time: 11161
97059494 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 192
4301 deg
Eccentricity:
0001914
Arg of perigee: 319
1011 deg
Mean anomaly: 41
0008 deg
Mean motion: 15
74562500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 275
Coasting Arc #12 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2011/162/22:46:52
195
Vector Time (MET): N/A
Weight (LBS) : 904691
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6100897
80 A = 6727590
15 meter
Y = -1315390
72 meter E =
0012510
Z = 2498317
02 I = 51
61375
XDOT = 3173
215435 Wp = 98
35589
YDOT = 4586
532591 meter/sec RA = 186
32169 deg
ZDOT = -5313
357025 TA = 53
34233
MA = 53
22740
Ha = 188
821 n
mi
Hp = 183
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20016068
91 X = 6103016
83
Y = -4315586
35 feet Y = -1247155
25 meter
Z = 8196578
17 Z = 2527960
46
XDOT = 10410
811796 XDOT = 3147
503680
YDOT = 15047
679103 feet/sec YDOT = 4621
874348 meter/sec
ZDOT = -17432
273703 ZDOT = -5298
003243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5955658
95 X = -1815284
85
Y = 19540029
52 feet Y = 5955801
00 meter
Z = 8316764
20 Z = 2534949
73
XDOT = -16838
064795 XDOT = -5132
242150
YDOT = 2289
715123 feet/sec YDOT = 697
905169 meter/sec
ZDOT = -17370
204953 ZDOT = -5294
438470
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 11162
98604871
00016717 00000-0 10270-3 0 9113
2 25544 51
6442 187
2113 0001892 327
2556 32
8490 15
74630033 40098
Satellite: ISS
Catalog Number: 25544
Epoch time: 11162
98604871 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 187
2113 deg
Eccentricity:
0001892
Arg of perigee: 327
2556 deg
Mean anomaly: 32
8490 deg
Mean motion: 15
74630033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 295
Coasting Arc #13 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2011/163/14:43:41
641
Vector Time (MET): N/A
Weight (LBS) : 903229
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5333971
42 A = 6734202
52 meter
Y = 2382988
07 meter E =
0005895
Z = -3346015
73 I = 51
62312
XDOT = -4688
791896 Wp = 257
03421
YDOT = -3935
496481 meter/sec RA = 182
90026 deg
ZDOT = 4663
541678 TA = 63
62195
MA = 63
56144
Ha = 191
938 n
mi
Hp = 190
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17499906
23 X = -5343967
51
Y = 7818202
33 feet Y = 2323284
97 meter
Z = -10977741
89 Z = -3371952
35
XDOT = -15383
175513 XDOT = -4667
090798
YDOT = -12911
733862 feet/sec YDOT = -3987
808761 meter/sec
ZDOT = 15300
333590 ZDOT = 4640
815419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15625538
34 X = 4762664
09
Y = 10995115
64 feet Y = 3351311
25 meter
Z = -11082951
16 Z = -3378083
51
XDOT = -2394
114436 XDOT = -729
726080
YDOT = 18758
992042 feet/sec YDOT = 5717
740774 meter/sec
ZDOT = 15208
358232 ZDOT = 4635
507589
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 11163
62070908
00016717 00000-0 10270-3 0 9124
2 25544 51
6404 183
9483 0010687 262
5080 97
4868 15
71552440 40193
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
62070908 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 183
9483 deg
Eccentricity:
0010687
Arg of perigee: 262
5080 deg
Mean anomaly: 97
4868 deg
Mean motion: 15
71552440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 311
Coasting Arc #14 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2011/163/18:55:21
516
Vector Time (MET): N/A
Weight (LBS) : 901478
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216096
85 A = 6742502
26 meter
Y = 3357795
66 meter E =
0008786
Z = -4046110
33 I = 51
62326
XDOT = -5993
587023 Wp = 170
04383
YDOT = 2860
377964 meter/sec RA = 182
05788 deg
ZDOT = -3881
352654 TA = 59
93546
MA = 59
84835
Ha = 201
512 n
mi
Hp = 193
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13832338
75 X = 4197891
44
Y = 11016389
98 feet Y = 3404841
45 meter
Z = -13274640
20 Z = -4025672
03
XDOT = -19663
999419 XDOT = -6006
271766
YDOT = 9384
442138 feet/sec YDOT = 2793
283709 meter/sec
ZDOT = -12734
096635 ZDOT = -3910
500161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14611798
02 X = -4453676
04
Y = -10068723
96 feet Y = -3068947
06 meter
Z = -13191916
92 Z = -4020896
28
XDOT = 18187
430666 XDOT = 5543
528867
YDOT = -9596
865211 feet/sec YDOT = -2925
124516 meter/sec
ZDOT = -12852
339958 ZDOT = -3917
393219
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 11163
81156945
00016717 00000-0 10270-3 0 9132
2 25544 51
6424 182
9734 0012103 205
7375 154
3184 15
67935606 40226
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
81156945 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 182
9734 deg
Eccentricity:
0012103
Arg of perigee: 205
7375 deg
Mean anomaly: 154
3184 deg
Mean motion: 15
67935606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 302
Coasting Arc #15 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2011/164/18:55:21
516
Vector Time (MET): N/A
Weight (LBS) : 901478
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2976259
76 A = 6739959
43 meter
Y = -3851365
53 meter E =
0006980
Z = 4658099
13 I = 51
64496
XDOT = 6892
527282 Wp = 171
33354
YDOT = 1887
527650 meter/sec RA = 176
92233 deg
ZDOT = -2849
519437 TA = 306
81925
MA = 306
88326
Ha = 201
173 n
mi
Hp = 193
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9764631
74 X = 2996476
89
Y = -12635713
68 feet Y = -3817970
98 meter
Z = 15282477
46 Z = 4672606
33
XDOT = 22613
278484 XDOT = 6884
750864
YDOT = 6192
676016 feet/sec YDOT = 1964
561105 meter/sec
ZDOT = -9348
817051 ZDOT = -2816
053833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8584149
07 X = -2616448
64
Y = 13398373
78 feet Y = 4083824
33 meter
Z = 15341426
77 Z = 4676066
88
XDOT = -22129
774869 XDOT = -6745
155380
YDOT = -3652
155173 feet/sec YDOT = -1113
176897 meter/sec
ZDOT = -9213
222359 ZDOT = -2808
190175
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 11164
83133132
00016717 00000-0 10270-3 0 9149
2 25544 51
6415 177
7840 0012089 209
8597 150
1875 15
67962752 40380
Satellite: ISS
Catalog Number: 25544
Epoch time: 11164
83133132 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 177
7840 deg
Eccentricity:
0012089
Arg of perigee: 209
8597 deg
Mean anomaly: 150
1875 deg
Mean motion: 15
67962752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 323
Coasting Arc #16 (Orbit 4053)
---------------------------------------
Vector Time (GMT): 2011/165/18:55:21
516
Vector Time (MET): N/A
Weight (LBS) : 901478
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6705690
85 A = 6749218
66 meter
Y = 467772
03 meter E =
0003979
Z = 615868
38 I = 51
70671
XDOT = 217
568856 Wp = 116
76926
YDOT = -4808
367547 meter/sec RA = 171
86127 deg
ZDOT = 5989
567652 TA = 249
90641
MA = 249
94923
Ha = 201
003 n
mi
Hp = 193
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22000298
07 X = -6713414
97
Y = 1534685
15 feet Y = 392741
62 meter
Z = 2020565
55 Z = 583273
35
XDOT = 713
808584 XDOT = 242
224458
YDOT = -15775
484077 feet/sec YDOT = -4805
797870 meter/sec
ZDOT = 19650
812507 ZDOT = 5990
683556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21745916
40 X = 6628155
32
Y = -3741676
94 feet Y = -1140463
13 meter
Z = 1888394
07 Z = 575582
51
XDOT = 721
452541 XDOT = 219
898734
YDOT = 14168
688217 feet/sec YDOT = 4318
616169 meter/sec
ZDOT = 19655
515718 ZDOT = 5991
001191
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 11165
85107233
00016717 00000-0 10270-3 0 9156
2 25544 51
6418 172
5930 0012067 213
8832 146
1558 15
67978886 40545
Satellite: ISS
Catalog Number: 25544
Epoch time: 11165
85107233 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 172
5930 deg
Eccentricity:
0012067
Arg of perigee: 213
8832 deg
Mean anomaly: 146
1558 deg
Mean motion: 15
67978886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4054
Checksum: 325
Coasting Arc #17 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2011/166/15:19:32
493
Vector Time (MET): N/A
Weight (LBS) : 900197
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3405429
75 A = 6749555
74 meter
Y = -4096348
21 meter E =
0012469
Z = 4131909
75 I = 51
70493
XDOT = 6511
939760 Wp = 108
78922
YDOT = 1605
825212 meter/sec RA = 167
50585 deg
ZDOT = -3769
681118 TA = 19
86534
MA = 19
81682
Ha = 205
121 n
mi
Hp = 196
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11172669
79 X = 3430910
77
Y = -13439462
63 feet Y = -4058124
98 meter
Z = 13556134
34 Z = 4148514
38
XDOT = 21364
631757 XDOT = 6511
811526
YDOT = 5268
455419 feet/sec YDOT = 1678
645715 meter/sec
ZDOT = -12367
720205 ZDOT = -3738
046146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17398595
11 X = -5303091
79
Y = 949915
18 feet Y = 289534
15 meter
Z = 13623620
44 Z = 4152479
51
XDOT = -10583
884223 XDOT = -3225
967911
YDOT = -18066
980726 feet/sec YDOT = -5506
815725 meter/sec
ZDOT = -12239
501841 ZDOT = -3730
600161
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 11166
67970212
00016717 00000-0 10270-3 0 9163
2 25544 51
6387 168
3752 0006827 164
4635 195
6734 15
65320494 40677
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
67970212 = yrday
fracday
Element set: 916
Inclination: 51
6387 deg
RA of node: 168
3752 deg
Eccentricity:
0006827
Arg of perigee: 164
4635 deg
Mean anomaly: 195
6734 deg
Mean motion: 15
65320494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 334
Coasting Arc #18 (Orbit 4069)
---------------------------------------
Vector Time (GMT): 2011/166/19:26:11
597
Vector Time (MET): N/A
Weight (LBS) : 898627
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6613107
00 A = 6765771
54 meter
Y = 501672
14 meter E =
0007830
Z = 1313137
78 I = 51
73469
XDOT = 789
046642 Wp = 36
27016
YDOT = -4923
096859 meter/sec RA = 166
67694 deg
ZDOT = 5842
984019 TA = 338
05205
MA = 338
08556
Ha = 206
291 n
mi
Hp = 205
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21696545
28 X = -6624604
26
Y = 1645905
97 feet Y = 427655
81 meter
Z = 4308194
80 Z = 1280983
55
XDOT = 2588
735701 XDOT = 815
654930
YDOT = -16151
892581 feet/sec YDOT = -4914
125658 meter/sec
ZDOT = 19169
895074 ZDOT = 5846
880842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20619213
79 X = 6284736
36
Y = -7028779
33 feet Y = -2142371
94 meter
Z = 4177787
70 Z = 1273389
69
XDOT = 1133
626245 XDOT = 345
529279
YDOT = 14752
562276 feet/sec YDOT = 4496
580982 meter/sec
ZDOT = 19185
883359 ZDOT = 5847
857248
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 11166
87136542
00016717 00000-0 10270-3 0 9176
2 25544 51
6411 167
4063 0007317 264
1441 95
8881 15
62027894 40701
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
87136542 = yrday
fracday
Element set: 917
Inclination: 51
6411 deg
RA of node: 167
4063 deg
Eccentricity:
0007317
Arg of perigee: 264
1441 deg
Mean anomaly: 95
8881 deg
Mean motion: 15
62027894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4070
Checksum: 311
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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