[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 5th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3998)
---------------------------------------
Vector Time (GMT): 2012/310/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4544368
00 A = 6787745
27 meter
Y = 1092774
82 meter E =
0003974
Z = -4918563
80 I = 51
86440
XDOT = -4000
628779 Wp = 234
88802
YDOT = 6106
238752 meter/sec RA = 137
81074 deg
ZDOT = -2340
516458 TA = 12
27682
MA = 12
26714
Ha = 226
155 n
mi
Hp = 219
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14909343
83 X = 4555704
25
Y = 3585219
21 feet Y = 1143656
14 meter
Z = -16137020
33 Z = -4896459
59
XDOT = -13125
422503 XDOT = -4057
242804
YDOT = 20033
591707 feet/sec YDOT = 6061
184665 meter/sec
ZDOT = -7678
859769 ZDOT = -2360
089171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2940485
34 X = -896259
93
Y = 15147265
95 feet Y = 4616886
66 meter
Z = -16045548
78 Z = -4890683
27
XDOT = -19468
301535 XDOT = -5933
938308
YDOT = -11996
959979 feet/sec YDOT = -3656
673402 meter/sec
ZDOT = -7760
543882 ZDOT = -2365
413775
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 12310
65358455
00016717 00000-0 10270-3 0 9005
2 25544 51
6456 138
7047 0015782 248
4636 111
4834 15
51195964 39993
Satellite: ISS
Catalog Number: 25544
Epoch time: 12310
65358455 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 138
7047 deg
Eccentricity:
0015782
Arg of perigee: 248
4636 deg
Mean anomaly: 111
4834 deg
Mean motion: 15
51195964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3999
Checksum: 332
Coasting Arc #2 (Orbit 4014)
---------------------------------------
Vector Time (GMT): 2012/311/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4162633
29 A = 6786671
92 meter
Y = -1472106
66 meter E =
0013525
Z = 5165465
07 I = 51
88322
XDOT = 4139
090093 Wp = 235
87277
YDOT = -6248
830644 meter/sec RA = 132
85805 deg
ZDOT = 1550
184447 TA = 199
18414
MA = 199
23512
Ha = 225
790 n
mi
Hp = 219
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13656933
35 X = -4170955
53
Y = -4829746
26 feet Y = -1518702
27 meter
Z = 16947063
89 Z = 5145222
71
XDOT = 13579
691906 XDOT = 4201
127639
YDOT = -20501
412873 feet/sec YDOT = -6202
197855 meter/sec
ZDOT = 5085
906979 ZDOT = 1570
443044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3996395
00 X = 1218101
20
Y = -14024905
44 feet Y = -4274791
18 meter
Z = 16863336
16 Z = 5139944
86
XDOT = 20252
449555 XDOT = 6172
946624
YDOT = 12005
579882 feet/sec YDOT = 3659
300748 meter/sec
ZDOT = 5170
459686 ZDOT = 1575
956112
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 12311
68436589
00016717 00000-0 10270-3 0 9015
2 25544 51
6459 133
5880 0015913 252
4737 107
4675 15
51217488 40151
Satellite: ISS
Catalog Number: 25544
Epoch time: 12311
68436589 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 133
5880 deg
Eccentricity:
0015913
Arg of perigee: 252
4737 deg
Mean anomaly: 107
4675 deg
Mean motion: 15
51217488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4015
Checksum: 320
Coasting Arc #3 (Orbit 4029)
---------------------------------------
Vector Time (GMT): 2012/312/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3778096
59 A = 6785985
04 meter
Y = 1913481
96 meter E =
0002458
Z = -5301338
37 I = 51
90154
XDOT = -4228
269054 Wp = 199
26731
YDOT = 6352
239511 meter/sec RA = 127
90774 deg
ZDOT = -722
721290 TA = 63
86388
MA = 63
83859
Ha = 225
574 n
mi
Hp = 219
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12395330
02 X = 3782171
93
Y = 6277827
94 feet Y = 1955753
62 meter
Z = -17392842
43 Z = -5282974
43
XDOT = -13872
273798 XDOT = -4295
475997
YDOT = 20840
680809 feet/sec YDOT = 6304
580567 meter/sec
ZDOT = -2371
132840 ZDOT = -743
425780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5295252
04 X = -1613992
82
Y = 12947984
52 feet Y = 3946545
68 meter
Z = -17316936
80 Z = -5278202
34
XDOT = -20901
613574 XDOT = -6370
811817
YDOT = -11825
246773 feet/sec YDOT = -3604
335216 meter/sec
ZDOT = -2457
555694 ZDOT = -749
062976
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 12312
65071653
00016717 00000-0 10270-3 0 9021
2 25544 51
6464 128
7932 0015759 256
1443 103
7955 15
51228694 40302
Satellite: ISS
Catalog Number: 25544
Epoch time: 12312
65071653 = yrday
fracday
Element set: 902
Inclination: 51
6464 deg
RA of node: 128
7932 deg
Eccentricity:
0015759
Arg of perigee: 256
1443 deg
Mean anomaly: 103
7955 deg
Mean motion: 15
51228694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4030
Checksum: 307
Coasting Arc #4 (Orbit 4045)
---------------------------------------
Vector Time (GMT): 2012/313/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3443882
06 A = 6785804
49 meter
Y = -2390209
21 meter E =
0013407
Z = 5347397
73 I = 51
91932
XDOT = 4241
158096 Wp = 259
34105
YDOT = -6370
623919 meter/sec RA = 122
95620 deg
ZDOT = -118
809390 TA = 191
77318
MA = 191
80456
Ha = 225
282 n
mi
Hp = 219
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11298825
66 X = -3442875
18
Y = -7841893
73 feet Y = -2428714
99 meter
Z = 17543955
80 Z = 5330669
76
XDOT = 13914
560683 XDOT = 4312
657689
YDOT = -20900
997108 feet/sec YDOT = -6322
796867 meter/sec
ZDOT = -389
794587 ZDOT = -98
031735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6731999
53 X = 2051913
46
Y = -12093720
81 feet Y = -3686166
10 meter
Z = 17474874
62 Z = 5326341
78
XDOT = 21236
536514 XDOT = 6472
896329
YDOT = 11396
149646 feet/sec YDOT = 3473
546412 meter/sec
ZDOT = -303
054411 ZDOT = -92
370985
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 12313
68148164
00016717 00000-0 10270-3 0 9038
2 25544 51
6468 123
6766 0015819 260
2763 99
6602 15
51232334 40468
Satellite: ISS
Catalog Number: 25544
Epoch time: 12313
68148164 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 123
6766 deg
Eccentricity:
0015819
Arg of perigee: 260
2763 deg
Mean anomaly: 99
6602 deg
Mean motion: 15
51232334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4046
Checksum: 310
Coasting Arc #5 (Orbit 4060)
---------------------------------------
Vector Time (GMT): 2012/314/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3131697
83 A = 6785994
11 meter
Y = 2904437
43 meter E =
0003778
Z = -5272493
32 I = 51
93601
XDOT = -4223
340403 Wp = 201
26968
YDOT = 6322
146222 meter/sec RA = 118
00722 deg
ZDOT = 970
477496 TA = 78
00590
MA = 77
96356
Ha = 225
137 n
mi
Hp = 219
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10274599
18 X = 3124600
16
Y = 9528994
18 feet Y = 2939418
08 meter
Z = -17298206
44 Z = -5257296
75
XDOT = -13856
103683 XDOT = -4298
436531
YDOT = 20741
949546 feet/sec YDOT = 6274
498351 meter/sec
ZDOT = 3183
981286 ZDOT = 949
777554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8313737
32 X = -2534027
13
Y = 11376096
02 feet Y = 3467434
07 meter
Z = -17235523
65 Z = -5253387
61
XDOT = -21327
597449 XDOT = -6500
651702
YDOT = -10875
191254 feet/sec YDOT = -3314
758294 meter/sec
ZDOT = 3097
555056 ZDOT = 944
134781
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 12314
64781578
00016717 00000-0 10270-3 0 9048
2 25544 51
6468 118
8814 0015730 263
8378 96
0981 15
51263943 40619
Satellite: ISS
Catalog Number: 25544
Epoch time: 12314
64781578 = yrday
fracday
Element set: 904
Inclination: 51
6468 deg
RA of node: 118
8814 deg
Eccentricity:
0015730
Arg of perigee: 263
8378 deg
Mean anomaly: 96
0981 deg
Mean motion: 15
51263943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4061
Checksum: 331
Coasting Arc #6 (Orbit 4076)
---------------------------------------
Vector Time (GMT): 2012/315/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2883892
44 A = 6786801
62 meter
Y = -3430260
16 meter E =
0011563
Z = 5107185
78 I = 51
95233
XDOT = 4156
798456 Wp = 282
42679
YDOT = -6171
105482 meter/sec RA = 113
05850 deg
ZDOT = -1798
624473 TA = 184
92723
MA = 184
93862
Ha = 224
982 n
mi
Hp = 219
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9461589
36 X = -2870130
38
Y = -11254134
37 feet Y = -3462432
46 meter
Z = 16755858
87 Z = 5093209
20
XDOT = 13637
790209 XDOT = 4234
233631
YDOT = -20246
409061 feet/sec YDOT = -6124
188681 meter/sec
ZDOT = -5900
998928 ZDOT = -1778
242060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9932495
95 X = 3027424
76
Y = -10929258
38 feet Y = -3331237
95 meter
Z = 16698289
00 Z = 5089638
49
XDOT = 21037
260525 XDOT = 6412
157008
YDOT = 10237
910405 feet/sec YDOT = 3120
515091 meter/sec
ZDOT = -5815
889560 ZDOT = -1772
683138
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 12315
67856422
00016717 00000-0 10270-3 0 9054
2 25544 51
6472 113
7649 0015712 268
0170 91
9182 15
51245701 40777
Satellite: ISS
Catalog Number: 25544
Epoch time: 12315
67856422 = yrday
fracday
Element set: 905
Inclination: 51
6472 deg
RA of node: 113
7649 deg
Eccentricity:
0015712
Arg of perigee: 268
0170 deg
Mean anomaly: 91
9182 deg
Mean motion: 15
51245701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4077
Checksum: 305
Coasting Arc #7 (Orbit 4091)
---------------------------------------
Vector Time (GMT): 2012/316/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2671778
67 A = 6787832
67 meter
Y = 3959230
07 meter E =
0005830
Z = -4820002
65 I = 51
96726
XDOT = -4087
332940 Wp = 237
42043
YDOT = 5937
912644 meter/sec RA = 108
11228 deg
ZDOT = 2606
502940 TA = 58
18351
MA = 58
12675
Ha = 225
000 n
mi
Hp = 219
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8765678
06 X = 2650722
31
Y = 12989599
96 feet Y = 3988989
69 meter
Z = -15813656
98 Z = -4807074
16
XDOT = -13409
884973 XDOT = -4166
090304
YDOT = 19481
340696 feet/sec YDOT = 5891
765253 meter/sec
ZDOT = 8551
518833 ZDOT = 2586
454812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11562124
21 X = -3524135
46
Y = 10656582
29 feet Y = 3248126
28 meter
Z = -15760491
87 Z = -4803797
92
XDOT = -20454
948937 XDOT = -6234
668436
YDOT = -9643
675676 feet/sec YDOT = -2939
392346 meter/sec
ZDOT = 8467
802636 ZDOT = 2580
986243
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 12316
64488156
00016717 00000-0 10270-3 0 9068
2 25544 51
6472 108
9690 0015741 271
5496 88
3852 15
51289317 40923
Satellite: ISS
Catalog Number: 25544
Epoch time: 12316
64488156 = yrday
fracday
Element set: 906
Inclination: 51
6472 deg
RA of node: 108
9690 deg
Eccentricity:
0015741
Arg of perigee: 271
5496 deg
Mean anomaly: 88
3852 deg
Mean motion: 15
51289317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4092
Checksum: 335
Coasting Arc #8 (Orbit 4107)
---------------------------------------
Vector Time (GMT): 2012/317/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2526696
67 A = 6789365
07 meter
Y = -4470951
40 meter E =
0008351
Z = 4449594
48 I = 51
98104
XDOT = 4002
286119 Wp = 304
66760
YDOT = -5599
094541 meter/sec RA = 103
16802 deg
ZDOT = -3353
123724 TA = 179
10952
MA = 179
10803
Ha = 224
992 n
mi
Hp = 219
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8289687
24 X = -2498129
56
Y = -14668475
72 feet Y = -4499046
76 meter
Z = 14598407
07 Z = 4437388
92
XDOT = 13130
859971 XDOT = 4080
888126
YDOT = -18369
732745 feet/sec YDOT = -5553
898996 meter/sec
ZDOT = -11001
062088 ZDOT = -3333
489254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13112275
75 X = 3996621
65
Y = -10649495
21 feet Y = -3245966
14 meter
Z = 14548300
93 Z = 4434322
12
XDOT = 19493
156814 XDOT = 5941
514197
YDOT = 9083
842859 feet/sec YDOT = 2768
755303 meter/sec
ZDOT = -10919
077991 ZDOT = -3328
134972
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 12317
67561276
00016717 00000-0 10270-3 0 9078
2 25544 51
6475 103
8530 0015662 275
7687 84
1678 15
51267755 41083
Satellite: ISS
Catalog Number: 25544
Epoch time: 12317
67561276 = yrday
fracday
Element set: 907
Inclination: 51
6475 deg
RA of node: 103
8530 deg
Eccentricity:
0015662
Arg of perigee: 275
7687 deg
Mean anomaly: 84
1678 deg
Mean motion: 15
51267755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4108
Checksum: 335
Coasting Arc #9 (Orbit 4122)
---------------------------------------
Vector Time (GMT): 2012/318/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2416358
76 A = 6790961
67 meter
Y = 4947867
11 meter E =
0009209
Z = -3966107
94 I = 51
99307
XDOT = -3945
776753 Wp = 274
15743
YDOT = 5178
543006 meter/sec RA = 98
22608 deg
ZDOT = 4049
027599 TA = 37
96185
MA = 37
89697
Ha = 225
221 n
mi
Hp = 219
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7927686
20 X = 2380118
12
Y = 16233159
82 feet Y = 4974685
83 meter
Z = -13012165
15 Z = -3954456
90
XDOT = -12945
461787 XDOT = -4023
060904
YDOT = 16989
970491 feet/sec YDOT = 5133
986627 meter/sec
ZDOT = 13284
211284 ZDOT = 4029
671031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14533230
84 X = -4429728
76
Y = 10788381
16 feet Y = 3288298
58 meter
Z = -12964419
05 Z = -3951554
93
XDOT = -18264
759106 XDOT = -5567
098575
YDOT = -8708
858193 feet/sec YDOT = -2654
459977 meter/sec
ZDOT = 13203
405544 ZDOT = 4024
398010
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 12318
64191363
00016717 00000-0 10270-3 0 9083
2 25544 51
6479 99
0567 0015814 279
4390 80
4974 15
51298762 41231
Satellite: ISS
Catalog Number: 25544
Epoch time: 12318
64191363 = yrday
fracday
Element set: 908
Inclination: 51
6479 deg
RA of node: 99
0567 deg
Eccentricity:
0015814
Arg of perigee: 279
4390 deg
Mean anomaly: 80
4974 deg
Mean motion: 15
51298762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4123
Checksum: 338
Coasting Arc #10 (Orbit 4138)
---------------------------------------
Vector Time (GMT): 2012/319/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2363245
38 A = 6792682
38 meter
Y = -5379235
81 meter E =
0004582
Z = 3414923
39 I = 52
00243
XDOT = 3905
018283 Wp = 321
99391
YDOT = -4666
359682 meter/sec RA = 93
28709 deg
ZDOT = -4647
911489 TA = 178
38798
MA = 178
38650
Ha = 225
307 n
mi
Hp = 219
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7753429
74 X = -2319507
38
Y = -17648411
44 feet Y = -5405418
73 meter
Z = 11203816
90 Z = 3403548
48
XDOT = 12811
739773 XDOT = 3979
487376
YDOT = -15309
579009 feet/sec YDOT = -4622
274687 meter/sec
ZDOT = -15249
053440 ZDOT = -4628
759944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15769730
28 X = 4806613
79
Y = -11132765
70 feet Y = -3393266
99 meter
Z = 11157273
28 Z = 3400736
90
XDOT = 16733
401107 XDOT = 5100
340657
YDOT = 8499
936728 feet/sec YDOT = 2590
780715 meter/sec
ZDOT = -15169
135967 ZDOT = -4623
552643
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 12319
67262737
00016717 00000-0 10270-3 0 9092
2 25544 51
6482 93
9412 0015695 283
6767 76
2637 15
51300112 41398
Satellite: ISS
Catalog Number: 25544
Epoch time: 12319
67262737 = yrday
fracday
Element set: 909
Inclination: 51
6482 deg
RA of node: 93
9412 deg
Eccentricity:
0015695
Arg of perigee: 283
6767 deg
Mean anomaly: 76
2637 deg
Mean motion: 15
51300112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4139
Checksum: 324
Coasting Arc #11 (Orbit 4153)
---------------------------------------
Vector Time (GMT): 2012/320/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2328745
07 A = 6794359
13 meter
Y = 5741404
82 meter E =
0013290
Z = -2768706
02 I = 52
00919
XDOT = -3921
052873 Wp = 303
42251
YDOT = 4088
253854 meter/sec RA = 88
34973 deg
ZDOT = 5169
042046 TA = 25
40056
MA = 25
33529
Ha = 225
699 n
mi
Hp = 219
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7640239
73 X = 2277820
44
Y = 18836630
00 feet Y = 5767161
77 meter
Z = -9083681
18 Z = -2757516
13
XDOT = -12864
346697 XDOT = -3991
587739
YDOT = 13412
906344 feet/sec YDOT = 4044
011439 meter/sec
ZDOT = 16958
799365 ZDOT = 5149
822297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16763860
91 X = -5109624
81
Y = 11532280
86 feet Y = 3515039
21 meter
Z = -9037954
53 Z = -2754768
54
XDOT = -15028
102310 XDOT = -4580
565584
YDOT = -8589
942143 feet/sec YDOT = -2618
214365 meter/sec
ZDOT = 16878
648406 ZDOT = 5144
612034
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 12320
63891223
00016717 00000-0 10270-3 0 9100
2 25544 51
6486 89
1449 0015903 287
5858 72
3556 15
51298693 41549
Satellite: ISS
Catalog Number: 25544
Epoch time: 12320
63891223 = yrday
fracday
Element set: 910
Inclination: 51
6486 deg
RA of node: 89
1449 deg
Eccentricity:
0015903
Arg of perigee: 287
5858 deg
Mean anomaly: 72
3556 deg
Mean motion: 15
51298693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4154
Checksum: 333
Coasting Arc #12 (Orbit 4169)
---------------------------------------
Vector Time (GMT): 2012/321/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2330868
12 A = 6795655
06 meter
Y = -6036633
86 meter E =
0001867
Z = 2078523
85 I = 52
01190
XDOT = 3974
848224 Wp = 297
25263
YDOT = -3449
057545 meter/sec RA = 83
41499 deg
ZDOT = -5562
643745 TA = 219
91575
MA = 219
92948
Ha = 225
805 n
mi
Hp = 219
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7647205
12 X = -2273289
14
Y = -19805229
20 feet Y = -6062377
29 meter
Z = 6819303
97 Z = 2067339
84
XDOT = 13040
840629 XDOT = 4040
143378
YDOT = -11315
805593 feet/sec YDOT = -3404
242821 meter/sec
ZDOT = -18250
143520 ZDOT = -5543
175451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17507422
02 X = 5336262
23
Y = -12034853
17 feet Y = -3668223
25 meter
Z = 6773643
02 Z = 2064606
39
XDOT = 13159
406279 XDOT = 4010
987034
YDOT = 8922
746258 feet/sec YDOT = 2719
653060 meter/sec
ZDOT = -18169
022765 ZDOT = -5537
918139
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 12321
66960851
00016717 00000-0 10270-3 0 9119
2 25544 51
6484 84
0296 0015758 291
7581 68
1893 15
51335996 41702
Satellite: ISS
Catalog Number: 25544
Epoch time: 12321
66960851 = yrday
fracday
Element set: 911
Inclination: 51
6484 deg
RA of node: 84
0296 deg
Eccentricity:
0015758
Arg of perigee: 291
7581 deg
Mean anomaly: 68
1893 deg
Mean motion: 15
51335996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4170
Checksum: 335
Coasting Arc #13 (Orbit 4184)
---------------------------------------
Vector Time (GMT): 2012/322/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2322892
69 A = 6796839
95 meter
Y = 6238232
14 meter E =
0016565
Z = -1319279
31 I = 52
01106
XDOT = -4103
756628 Wp = 327
35290
YDOT = 2771
184325 meter/sec RA = 78
48055 deg
ZDOT = 5857
425081 TA = 18
36658
MA = 18
30684
Ha = 226
264 n
mi
Hp = 219
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7621039
00 X = 2259371
66
Y = 20466640
88 feet Y = 6263853
09 meter
Z = -4328344
20 Z = -1308148
59
XDOT = -13463
768466 XDOT = -4162
893958
YDOT = 9091
812089 feet/sec YDOT = 2724
962542 meter/sec
ZDOT = 19217
273888 ZDOT = 5837
345514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17949196
65 X = -5470915
14
Y = 12457166
96 feet Y = 3796944
49 meter
Z = -4282933
44 Z = -1305438
11
XDOT = -11252
429714 XDOT = -3429
740577
YDOT = -9611
478120 feet/sec YDOT = -2929
578531 meter/sec
ZDOT = 19133
688317 ZDOT = 5831
948199
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 12322
63587733
00016717 00000-0 10270-3 0 9122
2 25544 51
6484 79
2330 0015939 295
9053 64
0455 15
51302647 41850
Satellite: ISS
Catalog Number: 25544
Epoch time: 12322
63587733 = yrday
fracday
Element set: 912
Inclination: 51
6484 deg
RA of node: 79
2330 deg
Eccentricity:
0015939
Arg of perigee: 295
9053 deg
Mean anomaly: 64
0455 deg
Mean motion: 15
51302647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4185
Checksum: 316
Coasting Arc #14 (Orbit 4200)
---------------------------------------
Vector Time (GMT): 2012/323/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2324720
54 A = 6797237
42 meter
Y = -6363894
82 meter E =
0003683
Z = 546820
55 I = 52
00577
XDOT = 4276
918341 Wp = 264
26131
YDOT = -2075
199866 meter/sec RA = 73
54737 deg
ZDOT = -6003
582696 TA = 269
87966
MA = 269
92186
Ha = 226
357 n
mi
Hp = 219
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7627035
88 X = -2256041
70
Y = -20878920
00 feet Y = -6389507
31 meter
Z = 1794030
68 Z = 535693
61
XDOT = 14031
884321 XDOT = 4328
970095
YDOT = -6808
398512 feet/sec YDOT = -2027
081394 meter/sec
ZDOT = -19696
793621 ZDOT = -5982
679091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18132689
69 X = 5526843
82
Y = -12863409
01 feet Y = -3920767
07 meter
Z = 1748655
51 Z = 532990
20
XDOT = 9356
249876 XDOT = 2851
784962
YDOT = 10539
150453 feet/sec YDOT = 3212
333058 meter/sec
ZDOT = -19609
867115 ZDOT = -5977
087497
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 12323
66655609
00016717 00000-0 10270-3 0 9135
2 25544 51
6482 74
1173 0015797 299
9100 60
0481 15
51368433 42015
Satellite: ISS
Catalog Number: 25544
Epoch time: 12323
66655609 = yrday
fracday
Element set: 913
Inclination: 51
6482 deg
RA of node: 74
1173 deg
Eccentricity:
0015797
Arg of perigee: 299
9100 deg
Mean anomaly: 60
0481 deg
Mean motion: 15
51368433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4201
Checksum: 304
Coasting Arc #15 (Orbit 4216)
---------------------------------------
Vector Time (GMT): 2012/324/15:12:00
321
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2280534
69 A = 6797468
36 meter
Y = 6385750
87 meter E =
0017733
Z = 262557
23 I = 51
99626
XDOT = -4528
606836 Wp = 347
56450
YDOT = 1372
865525 meter/sec RA = 68
61308 deg
ZDOT = 6037
180665 TA = 15
25004
MA = 15
19666
Ha = 226
792 n
mi
Hp = 219
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7482069
21 X = 2207682
94
Y = 20950626
22 feet Y = 6410845
89 meter
Z = 861408
22 Z = 273459
26
XDOT = -14857
633975 XDOT = -4572
949433
YDOT = 4504
151986 feet/sec YDOT = 1321
975725 meter/sec
ZDOT = 19807
023180 ZDOT = 6015
073039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18022867
43 X = -5493369
99
Y = 13038704
75 feet Y = 3974197
21 meter
Z = 905842
73 Z = 276100
86
XDOT = -7564
897462 XDOT = -2305
780746
YDOT = -11806
319091 feet/sec YDOT = -3598
566059 meter/sec
ZDOT = 19715
184354 ZDOT = 6009
188191
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 12324
69722718
00016717 00000-0 10270-3 0 9146
2 25544 51
6479 69
0004 0015894 304
4449 55
5200 15
51324298 42179
Satellite: ISS
Catalog Number: 25544
Epoch time: 12324
69722718 = yrday
fracday
Element set: 914
Inclination: 51
6479 deg
RA of node: 69
0004 deg
Eccentricity:
0015894
Arg of perigee: 304
4449 deg
Mean anomaly: 55
5200 deg
Mean motion: 15
51324298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4217
Checksum: 309
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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