[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 16th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 235 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
166/16:14:46
364 -3
8 8
6 8
6
N/A -4
7 0
4 204
8
000/00:39:32
728 6
2 -0
3 199
9
168/16:28:20
578 6
6 9
5 9
5
N/A 3
1 -0
5 206
8
000/00:26:53
157 -6
1 -0
0 205
8
Coasting Arc #1 (Orbit 32)
---------------------------------------
Vector Time (GMT): 2011/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916543
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2035409
47 A = 6738783
29 meter
Y = 4026358
06 meter E =
0011200
Z = -5011648
54 I = 51
62922
XDOT = -7327
531420 Wp = 162
46873
YDOT = -1311
036995 meter/sec RA = 178
40182 deg
ZDOT = 1913
320424 TA = 126
09630
MA = 125
99254
Ha = 200
157 n
mi
Hp = 194
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6677852
58 X = -2055935
82
Y = 13209836
16 feet Y = 4003482
97 meter
Z = -16442416
49 Z = -5021585
81
XDOT = -24040
457416 XDOT = -7321
621191
YDOT = -4301
302478 feet/sec YDOT = -1392
945186 meter/sec
ZDOT = 6277
297978 ZDOT = 1877
737099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11966923
32 X = 3647518
23
Y = 8634532
77 feet Y = 2631805
59 meter
Z = -16482843
70 Z = -5023970
76
XDOT = -7520
011395 XDOT = -2292
099473
YDOT = 22188
526689 feet/sec YDOT = 6763
062935 meter/sec
ZDOT = 6133
103071 ZDOT = 1869
369816
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
51274287
00016717 00000-0 10270-3 0 9006
2 25544 51
6396 179
4119 0011944 231
3343 128
6749 15
67874261 332
Satellite: ISS
Catalog Number: 25544
Epoch time: 11164
51274287 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 179
4119 deg
Eccentricity:
0011944
Arg of perigee: 231
3343 deg
Mean anomaly: 128
6749 deg
Mean motion: 15
67874261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 33
Checksum: 312
Coasting Arc #2 (Orbit 48)
---------------------------------------
Vector Time (GMT): 2011/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916543
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6654617
71 A = 6749506
98 meter
Y = -1020091
36 meter E =
0015318
Z = 303575
80 I = 51
69451
XDOT = 991
592497 Wp = 180
46177
YDOT = 4679
375552 meter/sec RA = 173
32615 deg
ZDOT = -6029
698741 TA = 356
24738
MA = 356
25886
Ha = 199
888 n
mi
Hp = 194
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21832735
28 X = 6664055
26
Y = -3346756
43 feet Y = -945622
67 meter
Z = 995983
61 Z = 335926
82
XDOT = 3253
256223 XDOT = 968
484433
YDOT = 15352
281996 feet/sec YDOT = 4690
336091 meter/sec
ZDOT = -19782
476186 ZDOT = -6024
936797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -141801
09 X = -43220
97
Y = -22080997
47 feet Y = -6730288
03 meter
Z = 1127180
18 Z = 343564
52
XDOT = 14068
073526 XDOT = 4287
948811
YDOT = -1096
681801 feet/sec YDOT = -334
268613 meter/sec
ZDOT = -19763
343072 ZDOT = -6023
866968
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
53252637
00016717 00000-0 10270-3 0 9015
2 25544 51
6380 174
2216 0011822 234
7476 125
2578 15
67913992 490
Satellite: ISS
Catalog Number: 25544
Epoch time: 11165
53252637 = yrday
fracday
Element set: 901
Inclination: 51
6380 deg
RA of node: 174
2216 deg
Eccentricity:
0011822
Arg of perigee: 234
7476 deg
Mean anomaly: 125
2578 deg
Mean motion: 15
67913992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 49
Checksum: 309
Coasting Arc #3 (Orbit 64)
---------------------------------------
Vector Time (GMT): 2011/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916543
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3560726
71 A = 6739657
45 meter
Y = -3130740
25 meter E =
0010351
Z = 4796929
40 I = 51
69095
XDOT = 6413
100530 Wp = 201
21662
YDOT = -3384
786811 meter/sec RA = 168
26271 deg
ZDOT = 2543
554801 TA = 223
79298
MA = 223
87511
Ha = 199
622 n
mi
Hp = 195
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11682174
23 X = -3548756
12
Y = -10271457
50 feet Y = -3170492
48 meter
Z = 15737957
36 Z = 4779659
85
XDOT = 21040
356069 XDOT = 6438
117112
YDOT = -11104
943607 feet/sec YDOT = -3312
932261 meter/sec
ZDOT = 8344
996066 ZDOT = 2574
769714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11695369
44 X = -3564748
60
Y = 10362909
71 feet Y = 3158614
88 meter
Z = 15668049
40 Z = 4775621
46
XDOT = -7566
980843 XDOT = -2306
415761
YDOT = -21387
193215 feet/sec YDOT = -6518
816492 meter/sec
ZDOT = 8471
696475 ZDOT = 2582
173086
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
55229048
00016717 00000-0 10270-3 0 9029
2 25544 51
6373 169
0308 0011813 239
3189 120
6807 15
67937638 653
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
55229048 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 169
0308 deg
Eccentricity:
0011813
Arg of perigee: 239
3189 deg
Mean anomaly: 120
6807 deg
Mean motion: 15
67937638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 65
Checksum: 316
Coasting Arc #4 (Orbit 67)
---------------------------------------
Vector Time (GMT): 2011/166/16:34:32
728
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3918937
45 A = 6750314
05 meter
Y = -2900204
39 meter E =
0006266
Z = 4673535
83 I = 51
69887
XDOT = 6111
418352 Wp = 280
73465
YDOT = -3680
963186 meter/sec RA = 167
29509 deg
ZDOT = 2844
768971 TA = 141
12577
MA = 141
08069
Ha = 204
797 n
mi
Hp = 199
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12857406
32 X = -3908918
68
Y = -9515106
25 feet Y = -2943973
24 meter
Z = 15333122
81 Z = 4654521
42
XDOT = 20050
585144 XDOT = 6138
306029
YDOT = -12076
650873 feet/sec YDOT = -3612
471829 meter/sec
ZDOT = 9333
231532 ZDOT = 2874
522766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6830086
25 X = 2081810
29
Y = 14544939
07 feet Y = 4433297
43 meter
Z = 15256128
89 Z = 4650068
09
XDOT = -22273
601194 XDOT = -6788
993644
YDOT = 558
167535 feet/sec YDOT = 170
129465 meter/sec
ZDOT = 9454
022507 ZDOT = 2881
586060
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
74363953
00016717 00000-0 10270-3 0 9035
2 25544 51
6377 168
0584 0014288 289
3956 70
5657 15
64413251 684
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
74363953 = yrday
fracday
Element set: 903
Inclination: 51
6377 deg
RA of node: 168
0584 deg
Eccentricity:
0014288
Arg of perigee: 289
3956 deg
Mean anomaly: 70
5657 deg
Mean motion: 15
64413251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 68
Checksum: 333
Coasting Arc #5 (Orbit 82)
---------------------------------------
Vector Time (GMT): 2011/167/16:34:32
728
Vector Time (MET): N/A
Weight (LBS) : 914807
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1820346
60 A = 6750019
22 meter
Y = 4482498
59 meter E =
0003336
Z = -4703885
41 I = 51
72782
XDOT = -7168
187832 Wp = 309
07320
YDOT = 1
557181 meter/sec RA = 162
19540 deg
ZDOT = 2776
230671 TA = 348
31188
MA = 348
31962
Ha = 205
040 n
mi
Hp = 199
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5972265
74 X = -1847485
01
Y = 14706360
20 feet Y = 4461991
56 meter
Z = -15432694
92 Z = -4712793
63
XDOT = -23517
676615 XDOT = -7181
158817
YDOT = 5
108862 feet/sec YDOT = -78
674920 meter/sec
ZDOT = 9108
368343 ZDOT = 2741
376345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12015203
64 X = 3662234
07
Y = -10317855
68 feet Y = -3144882
41 meter
Z = -15468994
69 Z = -4714949
58
XDOT = 20148
474144 XDOT = 6141
254919
YDOT = 10022
924650 feet/sec YDOT = 3054
987433 meter/sec
ZDOT = 8967
011459 ZDOT = 2733
145093
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 11167
70183075
00016717 00000-0 10270-3 0 9048
2 25544 51
6379 163
2067 0014274 293
5375 66
4283 15
64417631 838
Satellite: ISS
Catalog Number: 25544
Epoch time: 11167
70183075 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 163
2067 deg
Eccentricity:
0014274
Arg of perigee: 293
5375 deg
Mean anomaly: 66
4283 deg
Mean motion: 15
64417631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 83
Checksum: 310
Coasting Arc #6 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2011/168/16:34:32
000
Vector Time (MET): N/A
Weight (LBS) : 913944
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5986766
66 A = 6764343
30 meter
Y = -3072198
08 meter E =
0007008
Z = 644013
34 I = 51
78779
XDOT = 2690
714447 Wp = 157
64666
YDOT = 3984
376064 meter/sec RA = 157
15585 deg
ZDOT = -5990
927948 TA = 15
38893
MA = 15
36763
Ha = 205
946 n
mi
Hp = 204
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19641622
91 X = 6017547
16
Y = -10079390
03 feet Y = -3005078
44 meter
Z = 2112904
66 Z = 673170
94
XDOT = 8827
803304 XDOT = 2675
062924
YDOT = 13072
099947 feet/sec YDOT = 4014
378863 meter/sec
ZDOT = -19655
275419 ZDOT = -5977
893879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22063955
54 X = -6725093
65
Y = 234560
61 feet Y = 71494
07 meter
Z = 2231292
72 Z = 680098
02
XDOT = -2136
799833 XDOT = -651
296589
YDOT = -14083
111822 feet/sec YDOT = -4292
532483 meter/sec
ZDOT = -19602
558759 ZDOT = -5974
859910
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 11168
72393949
00016717 00000-0 10270-3 0 9055
2 25544 51
6380 158
0328 0007954 282
2382 77
7885 15
62695002 990
Satellite: ISS
Catalog Number: 25544
Epoch time: 11168
72393949 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 158
0328 deg
Eccentricity:
0007954
Arg of perigee: 282
2382 deg
Mean anomaly: 77
7885 deg
Mean motion: 15
62695002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 99
Checksum: 339
Coasting Arc #7 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2011/168/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6392900
18 A = 6764836
20 meter
Y = -1039816
93 meter E =
0007439
Z = -1935264
98 I = 51
78316
XDOT = -862
075156 Wp = 209
56687
YDOT = 5165
229947 meter/sec RA = 157
15409 deg
ZDOT = -5620
186616 TA = 351
80285
MA = 351
81499
Ha = 206
770 n
mi
Hp = 205
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20974081
95 X = 6413453
54
Y = -3411472
86 feet Y = -968212
36 meter
Z = -6349294
56 Z = -1904158
88
XDOT = -2828
330564 XDOT = -892
468137
YDOT = 16946
292477 feet/sec YDOT = 5155
420802 meter/sec
ZDOT = -18438
932466 ZDOT = -5624
447400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20509792
11 X = -6251384
64
Y = -5699604
90 feet Y = -1737239
57 meter
Z = -6223080
72 Z = -1896795
00
XDOT = 9147
492822 XDOT = 2788
155812
YDOT = -12754
951942 feet/sec YDOT = -3887
709352 meter/sec
ZDOT = -18456
413214 ZDOT = -5625
514748
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 11168
72395146
00016717 00000-0 10270-3 0 9067
2 25544 51
6379 158
0329 0008136 263
0010 97
0221 15
62057998 992
Satellite: ISS
Catalog Number: 25544
Epoch time: 11168
72395146 = yrday
fracday
Element set: 906
Inclination: 51
6379 deg
RA of node: 158
0329 deg
Eccentricity:
0008136
Arg of perigee: 263
0010 deg
Mean anomaly: 97
0221 deg
Mean motion: 15
62057998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 99
Checksum: 313
Coasting Arc #8 (Orbit 114)
---------------------------------------
Vector Time (GMT): 2011/169/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4003675
95 A = 6755906
06 meter
Y = -2284926
10 meter E =
0004762
Z = 4942439
20 I = 51
78108
XDOT = 5506
506171 Wp = 213
88119
YDOT = -4876
198579 meter/sec RA = 152
11899 deg
ZDOT = 2203
456024 TA = 214
67894
MA = 214
71000
Ha = 206
073 n
mi
Hp = 205
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13135419
78 X = -4001837
05
Y = -7496476
70 feet Y = -2329688
17 meter
Z = 16215351
69 Z = 4922993
68
XDOT = 18065
965129 XDOT = 5549
919661
YDOT = -15998
026835 feet/sec YDOT = -4814
379110 meter/sec
ZDOT = 7229
186430 ZDOT = 2230
310920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9089277
15 X = 2770411
67
Y = 12193060
88 feet Y = 3716444
96 meter
Z = 16136553
34 Z = 4918421
46
XDOT = -22052
109610 XDOT = -6721
483009
YDOT = 6714
571463 feet/sec YDOT = 2046
601382 meter/sec
ZDOT = 7338
317844 ZDOT = 2236
719279
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 11169
74754543
00016717 00000-0 10270-3 0 9071
2 25544 51
6379 152
8682 0008149 266
6748 93
3476 15
62097224 1153
Satellite: ISS
Catalog Number: 25544
Epoch time: 11169
74754543 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 152
8682 deg
Eccentricity:
0008149
Arg of perigee: 266
6748 deg
Mean anomaly: 93
3476 deg
Mean motion: 15
62097224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 115
Checksum: 338
Coasting Arc #9 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2011/170/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -428652
36 A = 6756435
77 meter
Y = 4759193
02 meter E =
0004413
Z = -4780367
67 I = 51
81029
XDOT = -6923
792910 Wp = 142
07577
YDOT = 2021
499554 meter/sec RA = 147
04767 deg
ZDOT = 2631
280123 TA = 153
78674
MA = 153
76440
Ha = 205
647 n
mi
Hp = 205
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1406339
77 X = -458616
88
Y = 15614150
31 feet Y = 4754232
71 meter
Z = -15683620
98 Z = -4782522
14
XDOT = -22715
856003 XDOT = -6958
665220
YDOT = 6632
216384 feet/sec YDOT = 1943
878134 meter/sec
ZDOT = 8632
808802 ZDOT = 2597
560382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7255695
58 X = 2211536
01
Y = -13887201
13 feet Y = -4232818
90 meter
Z = -15692545
21 Z = -4783087
78
XDOT = 22546
745106 XDOT = 6872
247908
YDOT = 2171
837239 feet/sec YDOT = 661
975990 meter/sec
ZDOT = 8495
922265 ZDOT = 2589
557106
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 11170
70715282
00016717 00000-0 10270-3 0 9087
2 25544 51
6388 148
0264 0008142 270
9881 89
0343 15
62108135 1301
Satellite: ISS
Catalog Number: 25544
Epoch time: 11170
70715282 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 148
0264 deg
Eccentricity:
0008142
Arg of perigee: 270
9881 deg
Mean anomaly: 89
0343 deg
Mean motion: 15
62108135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 292
Coasting Arc #10 (Orbit 145)
---------------------------------------
Vector Time (GMT): 2011/171/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4360969
55 A = 6765195
02 meter
Y = -4932790
96 meter E =
0007285
Z = 1534406
10 I = 51
86452
XDOT = 4542
984144 Wp = 144
07568
YDOT = 2214
575918 meter/sec RA = 142
02170 deg
ZDOT = -5784
239073 TA = 19
15275
MA = 19
12538
Ha = 206
158 n
mi
Hp = 205
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14307642
88 X = 4408351
08
Y = -16183697
38 feet Y = -4883759
22 meter
Z = 5034140
73 Z = 1555705
90
XDOT = 14904
803621 XDOT = 4545
981117
YDOT = 7265
669023 feet/sec YDOT = 2265
395802 meter/sec
ZDOT = -18977
162314 ZDOT = -5762
161975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19265547
33 X = -5872138
83
Y = 9725214
73 feet Y = 2964245
45 meter
Z = 5120758
08 Z = 1560807
06
XDOT = -10538
152944 XDOT = -3212
029017
YDOT = -10917
043748 feet/sec YDOT = -3327
514934 meter/sec
ZDOT = -18887
667654 ZDOT = -5756
961101
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 11171
73072032
00016717 00000-0 10270-3 0 9091
2 25544 51
6388 142
8620 0008111 274
1297 85
8933 15
62106296 1464
Satellite: ISS
Catalog Number: 25544
Epoch time: 11171
73072032 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 142
8620 deg
Eccentricity:
0008111
Arg of perigee: 274
1297 deg
Mean anomaly: 85
8933 deg
Mean motion: 15
62106296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 146
Checksum: 299
Coasting Arc #11 (Orbit 161)
---------------------------------------
Vector Time (GMT): 2011/172/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5704345
63 A = 6763082
76 meter
Y = 2408227
39 meter E =
0006652
Z = 2709928
43 I = 51
88115
XDOT = 84
969801 Wp = 52
50627
YDOT = -5654
470647 meter/sec RA = 137
02752 deg
ZDOT = 5199
064649 TA = 338
13288
MA = 338
16126
Ha = 206
805 n
mi
Hp = 205
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18715044
70 X = -5744015
14
Y = 7901008
48 feet Y = 2344215
82 meter
Z = 8890841
32 Z = 2682120
90
XDOT = 278
772312 XDOT = 122
937005
YDOT = -18551
412884 feet/sec YDOT = -5653
308751 meter/sec
ZDOT = 17057
298717 ZDOT = 5199
569026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20350893
02 X = 6202952
19
Y = -717926
39 feet Y = -218823
96 meter
Z = 8777905
66 Z = 2675505
64
XDOT = -6807
905688 XDOT = -2075
049654
YDOT = 15793
655233 feet/sec YDOT = 4813
906115 meter/sec
ZDOT = 17059
567203 ZDOT = 5199
756083
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 11172
75427229
00016717 00000-0 10270-3 0 9108
2 25544 51
6392 137
6969 0008151 279
2156 80
8079 15
62137525 1624
Satellite: ISS
Catalog Number: 25544
Epoch time: 11172
75427229 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 137
6969 deg
Eccentricity:
0008151
Arg of perigee: 279
2156 deg
Mean anomaly: 80
8079 deg
Mean motion: 15
62137525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 162
Checksum: 316
Coasting Arc #12 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2011/173/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3964994
91 A = 6754492
16 meter
Y = 1698997
36 meter E =
0007210
Z = -5203440
56 I = 51
87462
XDOT = -4302
830844 Wp = 54
76952
YDOT = 6235
624031 meter/sec RA = 131
98660 deg
ZDOT = -1239
861552 TA = 203
36672
MA = 203
39951
Ha = 206
965 n
mi
Hp = 205
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13008513
48 X = 3970978
91
Y = 5574138
32 feet Y = 1743370
35 meter
Z = -17071655
38 Z = -5184164
03
XDOT = -14116
899096 XDOT = -4366
216016
YDOT = 20458
084092 feet/sec YDOT = 6187
152885 meter/sec
ZDOT = -4067
787245 ZDOT = -1260
917871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10443543
16 X = -3183191
96
Y = -9689550
52 feet Y = -2953375
00 meter
Z = -16993495
09 Z = -5179617
30
XDOT = 19488
756447 XDOT = 5940
172965
YDOT = -13704
409515 feet/sec YDOT = -4177
104020 meter/sec
ZDOT = -4153
488191 ZDOT = -1265
983201
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 11173
71383785
00016717 00000-0 10270-3 0 9114
2 25544 51
6395 132
8551 0008246 282
7733 77
2502 15
62196432 1775
Satellite: ISS
Catalog Number: 25544
Epoch time: 11173
71383785 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 132
8551 deg
Eccentricity:
0008246
Arg of perigee: 282
7733 deg
Mean anomaly: 77
2502 deg
Mean motion: 15
62196432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 177
Checksum: 313
Coasting Arc #13 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2011/174/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -329858
00 A = 6757918
07 meter
Y = -5192135
11 meter E =
0005582
Z = 4315299
26 I = 51
90590
XDOT = 5956
309916 Wp = 13
36400
YDOT = -3318
340846 meter/sec RA = 126
92411 deg
ZDOT = -3531
099609 TA = 112
42197
MA = 112
36283
Ha = 207
064 n
mi
Hp = 205
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1082211
30 X = -292736
90
Y = -17034564
01 feet Y = -5195616
70 meter
Z = 14157805
96 Z = 4313786
42
XDOT = 19541
699200 XDOT = 6010
126938
YDOT = -10886
945032 feet/sec YDOT = -3251
432477 meter/sec
ZDOT = -11584
972469 ZDOT = -3502
033591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4395898
38 X = -1339869
83
Y = 16498223
73 feet Y = 5028658
59 meter
Z = 14151880
20 Z = 4313493
09
XDOT = -20873
017020 XDOT = -6362
095588
YDOT = 4292
004889 feet/sec YDOT = 1308
203090 meter/sec
ZDOT = -11466
871836 ZDOT = -3495
102535
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 11174
73736058
00016717 00000-0 10270-3 0 9123
2 25544 51
6394 127
6902 0008350 286
9542 73
0700 15
62228894 1936
Satellite: ISS
Catalog Number: 25544
Epoch time: 11174
73736058 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 127
6902 deg
Eccentricity:
0008350
Arg of perigee: 286
9542 deg
Mean anomaly: 73
0700 deg
Mean motion: 15
62228894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 313
Coasting Arc #14 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2011/175/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3143353
13 A = 6765704
99 meter
Y = 5951446
19 meter E =
0011078
Z = -610820
54 I = 51
94929
XDOT = -4459
743233 Wp = 355
69904
YDOT = -1738
938010 meter/sec RA = 121
91487 deg
ZDOT = 6011
008954 TA = 357
71027
MA = 357
71534
Ha = 207
256 n
mi
Hp = 205
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10312838
35 X = -3206702
47
Y = 19525742
10 feet Y = 5915941
17 meter
Z = -2004004
40 Z = -626244
12
XDOT = -14631
703521 XDOT = -4469
167004
YDOT = -5705
177198 feet/sec YDOT = -1788
862969 meter/sec
ZDOT = 19721
157984 ZDOT = 5989
320438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15790967
98 X = 4813087
04
Y = -15427206
44 feet Y = -4702212
52 meter
Z = -2066858
66 Z = -629978
52
XDOT = 11165
697412 XDOT = 3403
304571
YDOT = 8800
220924 feet/sec YDOT = 2682
307338 meter/sec
ZDOT = 19633
204243 ZDOT = 5984
200653
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 11175
69690023
00016717 00000-0 10270-3 0 9131
2 25544 51
6394 122
8473 0008370 289
9650 70
0605 15
62232582 2088
Satellite: ISS
Catalog Number: 25544
Epoch time: 11175
69690023 = yrday
fracday
Element set: 913
Inclination: 51
6394 deg
RA of node: 122
8473 deg
Eccentricity:
0008370
Arg of perigee: 289
9650 deg
Mean anomaly: 70
0605 deg
Mean motion: 15
62232582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 303
Coasting Arc #15 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2011/176/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4750183
17 A = 6760734
36 meter
Y = -3298747
23 meter E =
0004581
Z = -3502817
14 I = 51
94705
XDOT = 888
405981 Wp = 322
41984
YDOT = 6119
184546 meter/sec RA = 116
92043 deg
ZDOT = -4551
259404 TA = 258
72083
MA = 258
77231
Ha = 207
455 n
mi
Hp = 205
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15584590
45 X = 4803733
42
Y = -10822661
53 feet Y = -3245327
92 meter
Z = -11492182
22 Z = -3479611
08
XDOT = 2914
717786 XDOT = 842
023268
YDOT = 20076
064785 feet/sec YDOT = 6128
860500 meter/sec
ZDOT = -14931
953425 ZDOT = -4547
055382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18120450
90 X = -5523113
43
Y = 5815338
68 feet Y = 1772515
23 meter
Z = -11397842
33 Z = -3474062
34
XDOT = 3374
329496 XDOT = 1028
495630
YDOT = -18761
989228 feet/sec YDOT = -5718
654317 meter/sec
ZDOT = -14915
160890 ZDOT = -4546
141039
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 11176
72039391
00016717 00000-0 10270-3 0 9142
2 25544 51
6389 117
6824 0008521 293
1560 66
8699 15
62223044 2246
Satellite: ISS
Catalog Number: 25544
Epoch time: 11176
72039391 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 117
6824 deg
Eccentricity:
0008521
Arg of perigee: 293
1560 deg
Mean anomaly: 66
8699 deg
Mean motion: 15
62223044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 312
Coasting Arc #16 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2011/177/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3907570
44 A = 6753770
57 meter
Y = -1447046
13 meter E =
0006238
Z = 5319396
94 I = 51
93714
XDOT = 2784
994671 Wp = 305
76374
YDOT = -7154
940710 meter/sec RA = 111
87046 deg
ZDOT = 103
093575 TA = 143
28054
MA = 143
23779
Ha = 207
629 n
mi
Hp = 204
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12820112
98 X = -3916939
58
Y = -4747526
67 feet Y = -1490796
13 meter
Z = 17452089
71 Z = 5300390
96
XDOT = 9137
121624 XDOT = 2864
294800
YDOT = -23474
214929 feet/sec YDOT = -7123
353831 meter/sec
ZDOT = 338
233514 ZDOT = 116
814667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11132262
65 X = 3393113
65
Y = 8102570
38 feet Y = 2469663
45 meter
Z = 17375005
71 Z = 5295901
74
XDOT = -14619
529101 XDOT = -4456
032470
YDOT = 19266
298255 feet/sec YDOT = 5872
367708 meter/sec
ZDOT = 394
262418 ZDOT = 120
171185
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 11177
74387248
00016717 00000-0 10270-3 0 9153
2 25544 51
6391 112
5167 0008420 297
5599 62
4703 15
62263571 2406
Satellite: ISS
Catalog Number: 25544
Epoch time: 11177
74387248 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 112
5167 deg
Eccentricity:
0008420
Arg of perigee: 297
5599 deg
Mean anomaly: 62
4703 deg
Mean motion: 15
62263571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 313
Coasting Arc #17 (Orbit 254)
---------------------------------------
Vector Time (GMT): 2011/178/16:41:47
157
Vector Time (MET): N/A
Weight (LBS) : 913626
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1296965
00 A = 6760054
37 meter
Y = 5544702
73 meter E =
0004002
Z = -3638280
93 I = 51
96811
XDOT = -4826
131872 Wp = 331
40302
YDOT = 4026
147755 meter/sec RA = 106
81852 deg
ZDOT = 4416
832150 TA = 345
47519
MA = 345
48669
Ha = 207
785 n
mi
Hp = 204
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4255134
50 X = 1252540
79
Y = 18191281
91 feet Y = 5558958
39 meter
Z = -11936617
23 Z = -3632087
26
XDOT = -15833
765985 XDOT = -4892
250528
YDOT = 13209
146179 feet/sec YDOT = 3971
808594 meter/sec
ZDOT = 14490
919127 ZDOT = 4393
226844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 495228
73 X = 150945
72
Y = -18691627
31 feet Y = -5697208
00 meter
Z = -11911740
22 Z = -3630698
42
XDOT = 17418
458542 XDOT = 5309
146164
YDOT = -8709
037855 feet/sec YDOT = -2654
514738 meter/sec
ZDOT = 14394
896515 ZDOT = 4387
564458
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 11178
70336943
00016717 00000-0 10270-3 0 9167
2 25544 51
6384 107
6733 0008572 300
8112 59
2201 15
62290533 2550
Satellite: ISS
Catalog Number: 25544
Epoch time: 11178
70336943 = yrday
fracday
Element set: 916
Inclination: 51
6384 deg
RA of node: 107
6733 deg
Eccentricity:
0008572
Arg of perigee: 300
8112 deg
Mean anomaly: 59
2201 deg
Mean motion: 15
62290533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 255
Checksum: 291
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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