[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 1st 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 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
153/22:37:05
223 -3
8 6
4 6
4
N/A 1
9 -0
2 189
2
000/00:14:10
446 -4
8 -0
1 183
3
163/14:26:51
050 -9
5 9
5 9
5
N/A 0
3 -0
1 190
8
000/00:33:42
100 -0
9 -0
3 189
9
163/18:35:11
013 2
1 8
5 8
6
N/A 5
6 -0
5 200
5
000/00:40:22
026 -6
1 0
5 193
2
Coasting Arc #1 (Orbit 3811)
---------------------------------------
Vector Time (GMT): 2011/150/11:36:19
571
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2562818
20 A = 6727805
06 meter
Y = -6194680
56 meter E =
0015062
Z = -449427
53 I = 51
34399
XDOT = 4307
100564 Wp = 24
04604
YDOT = -2210
899324 meter/sec RA = 250
59843 deg
ZDOT = 5996
998826 TA = 331
04021
MA = 331
12370
Ha = 188
251 n
mi
Hp = 181
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8408196
18 X = -2491174
34
Y = -20323755
12 feet Y = -6222938
91 meter
Z = -1474499
78 Z = -461704
59
XDOT = 14130
907363 XDOT = 4302
370413
YDOT = -7253
606705 feet/sec YDOT = -2162
761870 meter/sec
ZDOT = 19675
193000 ZDOT = 6017
911261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21844627
81 X = -6658242
56
Y = -2533136
02 feet Y = -772099
86 meter
Z = -1523939
78 Z = -464496
85
XDOT = 284
231059 XDOT = 86
633627
YDOT = -14178
426019 feet/sec YDOT = -4321
584250 meter/sec
ZDOT = 19759
929579 ZDOT = 6022
826536
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 11150
48445304
00016717 00000-0 10270-3 0 9007
2 25544 51
6492 251
4737 0005501 345
7937 14
3071 15
75504653 38128
Satellite: ISS
Catalog Number: 25544
Epoch time: 11150
48445304 = yrday
fracday
Element set: 900
Inclination: 51
6492 deg
RA of node: 251
4737 deg
Eccentricity:
0005501
Arg of perigee: 345
7937 deg
Mean anomaly: 14
3071 deg
Mean motion: 15
75504653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3812
Checksum: 289
Coasting Arc #2 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2011/151/11:36:19
571
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3869210
00 A = 6715583
14 meter
Y = 1644763
00 meter E =
0014988
Z = -5248703
42 I = 51
31482
XDOT = -3122
321997 Wp = 69
48138
YDOT = -7030
617389 meter/sec RA = 245
43381 deg
ZDOT = 103
959773 TA = 201
47902
MA = 201
54198
Ha = 188
255 n
mi
Hp = 181
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12694258
53 X = -3861816
91
Y = 5396204
07 feet Y = 1601537
21 meter
Z = -17220155
57 Z = -5267482
09
XDOT = -10243
838573 XDOT = -3043
977246
YDOT = -23066
330017 feet/sec YDOT = -7065
095054 meter/sec
ZDOT = 341
075372 ZDOT = 88
980664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1166866
27 X = -355660
84
Y = 13648279
86 feet Y = 4159995
70 meter
Z = -17296238
19 Z = -5271893
40
XDOT = -24178
565320 XDOT = -7369
626710
YDOT = -1733
823385 feet/sec YDOT = -528
469368 meter/sec
ZDOT = 280
726081 ZDOT = 85
565310
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 11151
49928580
00016717 00000-0 10270-3 0 9012
2 25544 51
6491 246
2519 0005567 349
1746 10
9298 15
75586182 38282
Satellite: ISS
Catalog Number: 25544
Epoch time: 11151
49928580 = yrday
fracday
Element set: 901
Inclination: 51
6491 deg
RA of node: 246
2519 deg
Eccentricity:
0005567
Arg of perigee: 349
1746 deg
Mean anomaly: 10
9298 deg
Mean motion: 15
75586182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 338
Coasting Arc #3 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2011/152/11:36:19
571
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2853935
13 A = 6727340
67 meter
Y = 6055085
62 meter E =
0006920
Z = -655942
80 I = 51
36816
XDOT = -4615
790616 Wp = 113
68652
YDOT = 1534
752786 meter/sec RA = 240
27250 deg
ZDOT = -5967
681900 TA = 73
48510
MA = 73
40909
Ha = 188
319 n
mi
Hp = 181
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9363304
25 X = 2789200
37
Y = 19865766
46 feet Y = 6086638
20 meter
Z = -2152043
31 Z = -642234
54
XDOT = -15143
670001 XDOT = -4603
619250
YDOT = 5035
278168 feet/sec YDOT = 1483
205199 meter/sec
ZDOT = -19579
008859 ZDOT = -5990
075837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21955915
02 X = 6692162
90
Y = 701922
85 feet Y = 213946
09 meter
Z = -2096791
36 Z = -639102
01
XDOT = -2311
392793 XDOT = -704
512523
YDOT = 14068
738902 feet/sec YDOT = 4288
151617 meter/sec
ZDOT = -19669
729996 ZDOT = -5995
333703
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
51407951
00016717 00000-0 10270-3 0 9021
2 25544 51
6485 241
0292 0005544 353
4528 6
6563 15
75636461 38448
Satellite: ISS
Catalog Number: 25544
Epoch time: 11152
51407951 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 241
0292 deg
Eccentricity:
0005544
Arg of perigee: 353
4528 deg
Mean anomaly: 6
6563 deg
Mean motion: 15
75636461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 303
Coasting Arc #4 (Orbit 3859)
---------------------------------------
Vector Time (GMT): 2011/153/11:36:19
571
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4239605
14 A = 6715773
81 meter
Y = -1052448
35 meter E =
0008925
Z = 5099820
37 I = 51
34679
XDOT = 3374
169922 Wp = 21
66307
YDOT = 6784
881187 meter/sec RA = 235
08604 deg
ZDOT = -1395
874808 TA = 81
80124
MA = 81
70002
Ha = 188
187 n
mi
Hp = 180
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13909465
67 X = 4226284
56
Y = -3452914
52 feet Y = -1005113
84 meter
Z = 16731694
13 Z = 5120383
97
XDOT = 11070
111294 XDOT = 3304
830248
YDOT = 22260
108880 feet/sec YDOT = 6822
225737 meter/sec
ZDOT = -4579
641758 ZDOT = -1379
650275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2977759
22 X = 907621
01
Y = -13918848
10 feet Y = -4242464
90 meter
Z = 16814995
09 Z = 5125210
50
XDOT = 23857
226706 XDOT = 7271
682700
YDOT = -384
906284 feet/sec YDOT = -117
319435 meter/sec
ZDOT = -4514
221605 ZDOT = -1375
934745
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
52883218
00016717 00000-0 10270-3 0 9038
2 25544 51
6488 235
8057 0005751 356
7634 3
3492 15
75737561 38601
Satellite: ISS
Catalog Number: 25544
Epoch time: 11153
52883218 = yrday
fracday
Element set: 903
Inclination: 51
6488 deg
RA of node: 235
8057 deg
Eccentricity:
0005751
Arg of perigee: 356
7634 deg
Mean anomaly: 3
3492 deg
Mean motion: 15
75737561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3860
Checksum: 323
Coasting Arc #5 (Orbit 3866)
---------------------------------------
Vector Time (GMT): 2011/153/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1328581
86 A = 6726763
75 meter
Y = 5825659
37 meter E =
0003722
Z = -3092656
43 I = 51
37830
XDOT = -5832
756951 Wp = 92
48806
YDOT = -1248
778375 meter/sec RA = 232
72820 deg
ZDOT = -4863
236095 TA = 123
55112
MA = 123
51557
Ha = 189
224 n
mi
Hp = 183
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4358864
36 X = 1278363
10
Y = 19113055
69 feet Y = 5840236
12 meter
Z = -10146510
61 Z = -3086323
15
XDOT = -19136
341702 XDOT = -5794
734543
YDOT = -4097
041914 feet/sec YDOT = -1313
790384 meter/sec
ZDOT = -15955
498998 ZDOT = -4891
479612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17680511
81 X = -5389020
00
Y = -8498421
48 feet Y = -2590318
87 meter
Z = -10121097
20 Z = -3084910
43
XDOT = 14481
512127 XDOT = 4413
964896
YDOT = -11010
205916 feet/sec YDOT = -3355
910763 meter/sec
ZDOT = -16069
809859 ZDOT = -4898
078045
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
97280040
00016717 00000-0 10270-3 0 9042
2 25544 51
6474 233
5230 0001220 328
0788 32
0301 15
74447136 38673
Satellite: ISS
Catalog Number: 25544
Epoch time: 11153
97280040 = yrday
fracday
Element set: 904
Inclination: 51
6474 deg
RA of node: 233
5230 deg
Eccentricity:
0001220
Arg of perigee: 328
0788 deg
Mean anomaly: 32
0301 deg
Mean motion: 15
74447136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3867
Checksum: 279
Coasting Arc #6 (Orbit 3882)
---------------------------------------
Vector Time (GMT): 2011/154/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5230995
92 A = 6723217
80 meter
Y = 818981
06 meter E =
0010102
Z = 4137897
74 I = 51
38559
XDOT = 1922
421197 Wp = 67
77186
YDOT = 6477
026380 meter/sec RA = 227
52140 deg
ZDOT = -3701
245175 TA = 60
22214
MA = 60
12171
Ha = 189
088 n
mi
Hp = 183
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17162060
09 X = 5201347
97
Y = 2686945
73 feet Y = 877310
77 meter
Z = 13575779
99 Z = 4163238
05
XDOT = 6307
156157 XDOT = 1867
830941
YDOT = 21250
086548 feet/sec YDOT = 6498
219452 meter/sec
ZDOT = -12143
192831 ZDOT = -3692
037561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12572972
52 X = -3832242
02
Y = 11869306
70 feet Y = 3617764
68 meter
Z = 13678366
39 Z = 4169166
08
XDOT = -19848
118785 XDOT = -6049
706606
YDOT = -7032
348289 feet/sec YDOT = -2143
459758 meter/sec
ZDOT = -12106
156575 ZDOT = -3689
956524
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
98833201
00016717 00000-0 10270-3 0 9058
2 25544 51
6465 228
3053 0001252 333
4396 26
6703 15
74488269 38833
Satellite: ISS
Catalog Number: 25544
Epoch time: 11154
98833201 = yrday
fracday
Element set: 905
Inclination: 51
6465 deg
RA of node: 228
3053 deg
Eccentricity:
0001252
Arg of perigee: 333
4396 deg
Mean anomaly: 26
6703 deg
Mean motion: 15
74488269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3883
Checksum: 315
Coasting Arc #7 (Orbit 3898)
---------------------------------------
Vector Time (GMT): 2011/155/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1986121
84 A = 6725718
09 meter
Y = -5461210
91 meter E =
0012180
Z = 3374410
67 I = 51
41606
XDOT = 6140
180816 Wp = 84
09378
YDOT = 625
072144 meter/sec RA = 222
41564 deg
ZDOT = 4612
636753 TA = 315
87684
MA = 315
97395
Ha = 189
169 n
mi
Hp = 183
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6516147
76 X = -1941298
13
Y = -17917358
62 feet Y = -5483170
84 meter
Z = 11070901
16 Z = 3364870
14
XDOT = 20144
950184 XDOT = 6110
327517
YDOT = 2050
761627 feet/sec YDOT = 693
567727 meter/sec
ZDOT = 15133
322680 ZDOT = 4642
393230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18297107
47 X = 5576958
36
Y = 5436663
67 feet Y = 1657095
09 meter
Z = 11032466
65 Z = 3362695
84
XDOT = -13238
531566 XDOT = -4035
104421
YDOT = 13513
330226 feet/sec YDOT = 4118
863053 meter/sec
ZDOT = 15253
816269 ZDOT = 4649
363199
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
00382709
00016717 00000-0 10270-3 0 9066
2 25544 51
6466 223
0864 0001347 338
9015 21
2093 15
74540181 38991
Satellite: ISS
Catalog Number: 25544
Epoch time: 11156
00382709 = yrday
fracday
Element set: 906
Inclination: 51
6466 deg
RA of node: 223
0864 deg
Eccentricity:
0001347
Arg of perigee: 338
9015 deg
Mean anomaly: 21
2093 deg
Mean motion: 15
74540181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3899
Checksum: 301
Coasting Arc #8 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2011/156/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5481800
78 A = 6723753
62 meter
Y = -268118
36 meter E =
0006035
Z = -3889853
57 I = 51
43418
XDOT = -2577
695324 Wp = 96
27465
YDOT = -6013
531840 meter/sec RA = 217
20891 deg
ZDOT = 4051
858856 TA = 216
03298
MA = 216
07367
Ha = 189
025 n
mi
Hp = 182
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17984910
69 X = -5459499
12
Y = -879653
42 feet Y = -329293
94 meter
Z = -12761986
78 Z = -3916429
86
XDOT = -8457
005655 XDOT = -2529
942346
YDOT = -19729
435171 feet/sec YDOT = -6042
090763 meter/sec
ZDOT = 13293
500185 ZDOT = 4039
451634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11173624
95 X = 3405720
88
Y = -14022193
62 feet Y = -4273964
61 meter
Z = -12869627
06 Z = -3922662
33
XDOT = 19977
539252 XDOT = 6089
153964
YDOT = 3778
369081 feet/sec YDOT = 1151
646896 meter/sec
ZDOT = 13243
462645 ZDOT = 4036
607414
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
95582052
00016717 00000-0 10270-3 0 9074
2 25544 51
6469 218
1938 0001443 340
8767 19
2342 15
74607931 39143
Satellite: ISS
Catalog Number: 25544
Epoch time: 11156
95582052 = yrday
fracday
Element set: 907
Inclination: 51
6469 deg
RA of node: 218
1938 deg
Eccentricity:
0001443
Arg of perigee: 340
8767 deg
Mean anomaly: 19
2342 deg
Mean motion: 15
74607931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 321
Coasting Arc #9 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2011/157/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2461086
26 A = 6724347
80 meter
Y = 5039367
18 meter E =
0005854
Z = -3716843
03 I = 51
46186
XDOT = -6406
868908 Wp = 63
36140
YDOT = -12
531601 meter/sec RA = 212
10708 deg
ZDOT = -4261
841269 TA = 161
57056
MA = 161
54935
Ha = 188
995 n
mi
Hp = 182
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8074430
00 X = 2422607
81
Y = 16533356
89 feet Y = 5066673
84 meter
Z = -12194366
89 Z = -3704980
01
XDOT = -21019
911116 XDOT = -6385
549489
YDOT = -41
114176 feet/sec YDOT = -84
057386 meter/sec
ZDOT = -13982
418860 ZDOT = -4292
913851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18228130
88 X = -5555934
29
Y = -2729284
41 feet Y = -831885
89 meter
Z = -12146486
95 Z = -3702249
22
XDOT = 11768
543762 XDOT = 3587
052139
YDOT = -15848
669663 feet/sec YDOT = -4830
674513 meter/sec
ZDOT = -14108
294768 ZDOT = -4300
208245
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
97124614
00016717 00000-0 10270-3 0 9084
2 25544 51
6472 212
9747 0001526 341
2109 18
8998 15
74656890 39302
Satellite: ISS
Catalog Number: 25544
Epoch time: 11157
97124614 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 212
9747 deg
Eccentricity:
0001526
Arg of perigee: 341
2109 deg
Mean anomaly: 18
8998 deg
Mean motion: 15
74656890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 330
Coasting Arc #10 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2011/158/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5706417
06 A = 6724573
17 meter
Y = -263154
56 meter E =
0012043
Z = 3539800
74 I = 51
48989
XDOT = 3026
186790 Wp = 79
35265
YDOT = 5509
599405 meter/sec RA = 206
90280 deg
ZDOT = -4453
858493 TA = 58
33744
MA = 58
22003
Ha = 188
905 n
mi
Hp = 182
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18721840
74 X = 5691739
96
Y = -863367
98 feet Y = -199424
36 meter
Z = 11613519
47 Z = 3567486
70
XDOT = 9928
434351 XDOT = 2985
988407
YDOT = 18076
113535 feet/sec YDOT = 5543
215752 meter/sec
ZDOT = -14612
396630 ZDOT = -4439
254434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9648997
57 X = -2941014
46
Y = 15985351
18 feet Y = 4872335
04 meter
Z = 11725696
26 Z = 3573992
22
XDOT = -19427
620215 XDOT = -5921
538642
YDOT = -1015
756646 feet/sec YDOT = -309
602626 meter/sec
ZDOT = -14553
417859 ZDOT = -4435
881763
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
98663718
00016717 00000-0 10270-3 0 9090
2 25544 51
6469 207
7554 0001581 350
2970 9
8163 15
74717961 39461
Satellite: ISS
Catalog Number: 25544
Epoch time: 11158
98663718 = yrday
fracday
Element set: 909
Inclination: 51
6469 deg
RA of node: 207
7554 deg
Eccentricity:
0001581
Arg of perigee: 350
2970 deg
Mean anomaly: 9
8163 deg
Mean motion: 15
74717961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 345
Coasting Arc #11 (Orbit 3961)
---------------------------------------
Vector Time (GMT): 2011/159/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2775690
51 A = 6722935
06 meter
Y = -4581782
68 meter E =
0010321
Z = 4053835
39 I = 51
51283
XDOT = 6652
274752 Wp = 94
47859
YDOT = -625
795342 meter/sec RA = 201
80312 deg
ZDOT = 3838
410387 TA = 315
95779
MA = 316
03996
Ha = 189
020 n
mi
Hp = 182
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9106596
17 X = -2743942
61
Y = -15032095
42 feet Y = -4612644
99 meter
Z = 13299984
86 Z = 4040427
80
XDOT = 21825
048399 XDOT = 6640
131822
YDOT = -2053
134323 feet/sec YDOT = -551
473802 meter/sec
ZDOT = 12593
209932 ZDOT = 3870
697550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17611365
51 X = 5367944
21
Y = 414482
02 feet Y = 126334
12 meter
Z = 13245814
19 Z = 4037324
16
XDOT = -10018
949717 XDOT = -3053
775874
YDOT = 18112
914729 feet/sec YDOT = 5520
816410 meter/sec
ZDOT = 12724
051226 ZDOT = 3878
290814
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
00199279
00016717 00000-0 10270-3 0 9104
2 25544 51
6473 202
5355 0001649 353
7163 6
3979 15
74751861 39627
Satellite: ISS
Catalog Number: 25544
Epoch time: 11160
00199279 = yrday
fracday
Element set: 910
Inclination: 51
6473 deg
RA of node: 202
5355 deg
Eccentricity:
0001649
Arg of perigee: 353
7163 deg
Mean anomaly: 6
3979 deg
Mean motion: 15
74751861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3962
Checksum: 315
Coasting Arc #12 (Orbit 3976)
---------------------------------------
Vector Time (GMT): 2011/160/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5892419
66 A = 6725484
62 meter
Y = 838391
17 meter E =
0004924
Z = -3132549
79 I = 51
55127
XDOT = -3284
289057 Wp = 58
99043
YDOT = -4996
536968 meter/sec RA = 196
60344 deg
ZDOT = 4848
681886 TA = 264
51804
MA = 264
57421
Ha = 188
799 n
mi
Hp = 182
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19332085
49 X = -5886139
36
Y = 2750627
19 feet Y = 772533
95 meter
Z = -10277394
32 Z = -3161159
93
XDOT = -10775
226566 XDOT = -3251
726818
YDOT = -16392
837822 feet/sec YDOT = -5033
082260 meter/sec
ZDOT = 15907
748971 ZDOT = 4832
805395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7815016
02 X = 2382016
88
Y = -17827620
10 feet Y = -5433858
61 meter
Z = -10393353
62 Z = -3167894
18
XDOT = 18359
698081 XDOT = 5596
035975
YDOT = -1173
091419 feet/sec YDOT = -357
558264 meter/sec
ZDOT = 15843
582544 ZDOT = 4829
123959
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
95385552
00016717 00000-0 10270-3 0 9110
2 25544 51
6472 197
6420 0001744 350
5800 9
5331 15
74815699 39775
Satellite: ISS
Catalog Number: 25544
Epoch time: 11160
95385552 = yrday
fracday
Element set: 911
Inclination: 51
6472 deg
RA of node: 197
6420 deg
Eccentricity:
0001744
Arg of perigee: 350
5800 deg
Mean anomaly: 9
5331 deg
Mean motion: 15
74815699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3977
Checksum: 319
Coasting Arc #13 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2011/161/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2902239
59 A = 6721301
49 meter
Y = 4165681
71 meter E =
0009798
Z = -4414574
08 I = 51
56664
XDOT = -6835
731554 Wp = 59
66980
YDOT = 1274
473202 meter/sec RA = 191
50477 deg
ZDOT = -3291
900850 TA = 177
22346
MA = 177
21801
Ha = 188
780 n
mi
Hp = 182
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9521783
42 X = 2876887
79
Y = 13666934
75 feet Y = 4197995
04 meter
Z = -14483510
77 Z = -4400536
03
XDOT = -22426
940794 XDOT = -6833
483331
YDOT = 4181
342525 feet/sec YDOT = 1198
044818 meter/sec
ZDOT = -10800
199639 ZDOT = -3325
103488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16658899
04 X = -5077632
43
Y = 1253455
65 feet Y = 382053
28 meter
Z = -14426762
66 Z = -4397277
26
XDOT = 7953
208154 XDOT = 2424
137845
YDOT = -20132
764132 feet/sec YDOT = -6136
466507 meter/sec
ZDOT = -10934
794763 ZDOT = -3332
925444
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
96914244
00016717 00000-0 10270-3 0 9129
2 25544 51
6466 192
4219 0001745 351
4848 8
6285 15
74869155 39932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11161
96914244 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 192
4219 deg
Eccentricity:
0001745
Arg of perigee: 351
4848 deg
Mean anomaly: 8
6285 deg
Mean motion: 15
74869155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 335
Coasting Arc #14 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2011/162/22:44:10
446
Vector Time (MET): N/A
Weight (LBS) : 904800
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6037567
07 A = 6726459
76 meter
Y = -1403326
39 meter E =
0013445
Z = 2598898
15 I = 51
61554
XDOT = 3327
226005 Wp = 95
20307
YDOT = 4551
971139 meter/sec RA = 186
31307 deg
ZDOT = -5249
647237 TA = 55
24029
MA = 55
11379
Ha = 188
707 n
mi
Hp = 182
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19808290
92 X = 6040185
51
Y = -4604089
21 feet Y = -1335796
35 meter
Z = 8526568
73 Z = 2628235
12
XDOT = 10916
095817 XDOT = 3301
579782
YDOT = 14934
288515 feet/sec YDOT = 4589
035495 meter/sec
ZDOT = -17223
252091 ZDOT = -5233
545111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5831116
05 X = -1777324
17
Y = 19429913
64 feet Y = 5922237
68 meter
Z = 8645515
74 Z = 2635153
20
XDOT = -17018
994472 XDOT = -5187
389515
YDOT = 2558
759672 feet/sec YDOT = 779
909948 meter/sec
ZDOT = -17158
149195 ZDOT = -5229
803875
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
98439436
00016717 00000-0 10270-3 0 9138
2 25544 51
6467 187
2019 0001815 359
7521
3642 15
74947906 40096
Satellite: ISS
Catalog Number: 25544
Epoch time: 11162
98439436 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 187
2019 deg
Eccentricity:
0001815
Arg of perigee: 359
7521 deg
Mean anomaly:
3642 deg
Mean motion: 15
74947906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 318
Coasting Arc #15 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2011/163/14:43:42
100
Vector Time (MET): N/A
Weight (LBS) : 903320
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5970164
11 A = 6735293
08 meter
Y = 1741088
07 meter E =
0006865
Z = -2575961
48 I = 51
63232
XDOT = -3544
785341 Wp = 301
55529
YDOT = -4353
224049 meter/sec RA = 182
88450 deg
ZDOT = 5266
478181 TA = 29
22936
MA = 29
19097
Ha = 190
756 n
mi
Hp = 189
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19587152
58 X = -5976675
89
Y = 5712231
20 feet Y = 1674290
04 meter
Z = -8451317
20 Z = -2604980
39
XDOT = -11629
873165 XDOT = -3521
427144
YDOT = -14282
231133 feet/sec YDOT = -4392
734178 meter/sec
ZDOT = 17278
471722 ZDOT = 5249
313524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14889380
20 X = 4538283
09
Y = 13877663
40 feet Y = 4229911
80 meter
Z = -8568997
01 Z = -2611830
29
XDOT = -5272
453249 XDOT = -1607
043750
YDOT = 16296
312142 feet/sec YDOT = 4967
115941 meter/sec
ZDOT = 17209
053135 ZDOT = 5245
319396
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
61892226
00016717 00000-0 10270-3 0 9140
2 25544 51
6428 183
9383 0009921 273
0232 86
9795 15
71866901 40195
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
61892226 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 183
9383 deg
Eccentricity:
0009921
Arg of perigee: 273
0232 deg
Mean anomaly: 86
9795 deg
Mean motion: 15
71866901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 329
Coasting Arc #16 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2011/163/18:55:22
026
Vector Time (MET): N/A
Weight (LBS) : 901547
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3206283
09 A = 6739556
37 meter
Y = 3751442
01 meter E =
0007039
Z = -4589605
02 I = 51
61900
XDOT = -6758
658172 Wp = 153
48208
YDOT = 2128
992836 meter/sec RA = 182
03537 deg
ZDOT = -2989
321221 TA = 86
83301
MA = 86
75247
Ha = 200
542 n
mi
Hp = 193
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10519301
47 X = 3186391
13
Y = 12307880
62 feet Y = 3787186
10 meter
Z = -15057759
24 Z = -4574076
47
XDOT = -22174
075367 XDOT = -6767
440933
YDOT = 6984
884631 feet/sec YDOT = 2053
364770 meter/sec
ZDOT = -9807
484320 ZDOT = -3022
176116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11402883
99 X = -3475599
04
Y = -11575899
18 feet Y = -3528334
07 meter
Z = -14994950
37 Z = -4570460
87
XDOT = 20758
394353 XDOT = 6327
158599
YDOT = -7605
189462 feet/sec YDOT = -2318
061748 meter/sec
ZDOT = -9940
728887 ZDOT = -3029
934165
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
80973713
00016717 00000-0 10270-3 0 9153
2 25544 51
6448 182
9633 0011721 213
3450 146
6973 15
68252305 40223
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
80973713 = yrday
fracday
Element set: 915
Inclination: 51
6448 deg
RA of node: 182
9633 deg
Eccentricity:
0011721
Arg of perigee: 213
3450 deg
Mean anomaly: 146
6973 deg
Mean motion: 15
68252305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 300
Coasting Arc #17 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2011/164/18:55:22
026
Vector Time (MET): N/A
Weight (LBS) : 901547
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4118910
82 A = 6741304
21 meter
Y = -3445620
00 meter E =
0007573
Z = 4067622
47 I = 51
65503
XDOT = 6078
599870 Wp = 155
55331
YDOT = 2722
790866 meter/sec RA = 176
89693 deg
ZDOT = -3853
022290 TA = 334
10466
MA = 334
14254
Ha = 200
227 n
mi
Hp = 193
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13513486
95 X = 4137374
36
Y = -11304527
57 feet Y = -3399457
33 meter
Z = 13345218
07 Z = 4087676
52
XDOT = 19942
912959 XDOT = 6066
418742
YDOT = 8933
040898 feet/sec YDOT = 2790
698042 meter/sec
ZDOT = -12641
149246 ZDOT = -3823
521326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12442101
25 X = -3792352
46
Y = 12386323
58 feet Y = 3775351
43 meter
Z = 13426638
56 Z = 4092439
43
XDOT = -19791
302136 XDOT = -6032
388891
YDOT = -6321
975345 feet/sec YDOT = -1926
938085 meter/sec
ZDOT = -12521
656734 ZDOT = -3816
600972
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
82929428
00016717 00000-0 10270-3 0 9161
2 25544 51
6440 177
7728 0011730 217
2235 142
8113 15
68264858 40383
Satellite: ISS
Catalog Number: 25544
Epoch time: 11164
82929428 = yrday
fracday
Element set: 916
Inclination: 51
6440 deg
RA of node: 177
7728 deg
Eccentricity:
0011730
Arg of perigee: 217
2235 deg
Mean anomaly: 142
8113 deg
Mean motion: 15
68264858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 318
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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