[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 8th 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 28)
---------------------------------------
Vector Time (GMT): 2012/312/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1581422
13 A = 6787451
56 meter
Y = -4319678
30 meter E =
0010068
Z = 4999403
84 I = 51
90069
XDOT = 5754
740928 Wp = 267
19422
YDOT = -4575
326220 meter/sec RA = 128
33872 deg
ZDOT = -2137
097199 TA = 203
55803
MA = 203
60417
Ha = 225
601 n
mi
Hp = 220
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5188392
82 X = -1557287
39
Y = -14172172
92 feet Y = -4337227
66 meter
Z = 16402243
58 Z = 4991780
00
XDOT = 18880
383623 XDOT = 5815
857165
YDOT = -15010
912795 feet/sec YDOT = -4510
631453 meter/sec
ZDOT = -7011
473750 ZDOT = -2108
991923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14970880
69 X = 4563124
43
Y = 2159621
89 feet Y = 658252
75 meter
Z = 16371080
12 Z = 4989905
22
XDOT = 4247
789557 XDOT = 1294
726257
YDOT = 22713
590515 feet/sec YDOT = 6923
102389 meter/sec
ZDOT = -6894
561174 ZDOT = -2101
462246
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
58630064
00016717 00000-0 10270-3 0 9008
2 25544 51
6429 129
1136 0015703 255
8093 104
1314 15
51166354 292
Satellite: ISS
Catalog Number: 25544
Epoch time: 12312
58630064 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 129
1136 deg
Eccentricity:
0015703
Arg of perigee: 255
8093 deg
Mean anomaly: 104
1314 deg
Mean motion: 15
51166354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 29
Checksum: 274
Coasting Arc #2 (Orbit 43)
---------------------------------------
Vector Time (GMT): 2012/313/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1254128
65 A = 6788590
67 meter
Y = 4755846
30 meter E =
0008426
Z = -4677447
04 I = 51
92406
XDOT = -5598
553621 Wp = 220
40070
YDOT = 4349
065317 meter/sec RA = 123
38965 deg
ZDOT = 2911
681645 TA = 78
50358
MA = 78
40897
Ha = 225
302 n
mi
Hp = 219
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4114595
30 X = 1223576
94
Y = 15603170
29 feet Y = 4769699
74 meter
Z = -15345954
86 Z = -4671428
85
XDOT = -18367
958074 XDOT = -5660
914211
YDOT = 14268
586997 feet/sec YDOT = 4286
110235 meter/sec
ZDOT = 9552
761304 ZDOT = 2884
332006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15771028
59 X = -4807009
52
Y = -3523309
47 feet Y = -1073904
73 meter
Z = -15321491
30 Z = -4669990
55
XDOT = -4329
812693 XDOT = -1319
726909
YDOT = -21796
564827 feet/sec YDOT = -6643
592959 meter/sec
ZDOT = 9438
990320 ZDOT = 2877
004250
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
55264746
00016717 00000-0 10270-3 0 9017
2 25544 51
6439 124
3170 0015658 259
3339 100
6049 15
51215538 441
Satellite: ISS
Catalog Number: 25544
Epoch time: 12313
55264746 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 124
3170 deg
Eccentricity:
0015658
Arg of perigee: 259
3339 deg
Mean anomaly: 100
6049 deg
Mean motion: 15
51215538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 44
Checksum: 292
Coasting Arc #3 (Orbit 59)
---------------------------------------
Vector Time (GMT): 2012/314/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1007038
62 A = 6790132
09 meter
Y = -5177970
50 meter E =
0006123
Z = 4281405
23 I = 51
94427
XDOT = 5407
854293 Wp = 279
24646
YDOT = -4039
210129 meter/sec RA = 118
44365 deg
ZDOT = -3616
512039 TA = 207
59161
MA = 207
62412
Ha = 225
156 n
mi
Hp = 219
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3303932
48 X = -969861
15
Y = -16988092
18 feet Y = -5189023
75 meter
Z = 14046605
09 Z = 4276603
54
XDOT = 17742
304111 XDOT = 5470
188215
YDOT = -13252
001734 feet/sec YDOT = -3978
387770 meter/sec
ZDOT = -11865
196978 ZDOT = -3590
088786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16698721
64 X = 5089770
36
Y = 4605198
24 feet Y = 1403664
42 meter
Z = 14027230
84 Z = 4275499
96
XDOT = 4169
573445 XDOT = 1270
885986
YDOT = 20652
458315 feet/sec YDOT = 6294
869294 meter/sec
ZDOT = -11755
284910 ZDOT = -3583
010841
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
58341005
00016717 00000-0 10270-3 0 9026
2 25544 51
6431 119
2008 0015667 263
2115 96
7253 15
51202983 602
Satellite: ISS
Catalog Number: 25544
Epoch time: 12314
58341005 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 119
2008 deg
Eccentricity:
0015667
Arg of perigee: 263
2115 deg
Mean anomaly: 96
7253 deg
Mean motion: 15
51202983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 60
Checksum: 272
Coasting Arc #4 (Orbit 74)
---------------------------------------
Vector Time (GMT): 2012/315/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 792167
01 A = 6791728
79 meter
Y = 5585201
62 meter E =
0010050
Z = -3775626
11 I = 51
96479
XDOT = -5224
184657 Wp = 257
83436
YDOT = 3635
983531 meter/sec RA = 113
50026 deg
ZDOT = 4270
901175 TA = 57
23987
MA = 57
14306
Ha = 224
993 n
mi
Hp = 219
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2598973
12 X = 747994
82
Y = 18324152
31 feet Y = 5593812
97 meter
Z = -12387224
76 Z = -3771885
26
XDOT = -17139
713443 XDOT = -5285
202289
YDOT = 11929
079827 feet/sec YDOT = 3577
222463 meter/sec
ZDOT = 14012
142962 ZDOT = 4245
373321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17668953
95 X = -5385497
16
Y = -5541379
60 feet Y = -1689012
50 meter
Z = -12372297
06 Z = -3771076
14
XDOT = -3677
501128 XDOT = -1120
902344
YDOT = -19407
490560 feet/sec YDOT = -5915
403123 meter/sec
ZDOT = 13905
971760 ZDOT = 4238
540193
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
54974090
00016717 00000-0 10270-3 0 9030
2 25544 51
6443 114
4043 0015634 266
9629 92
9733 15
51239559 751
Satellite: ISS
Catalog Number: 25544
Epoch time: 12315
54974090 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 114
4043 deg
Eccentricity:
0015634
Arg of perigee: 266
9629 deg
Mean anomaly: 92
9733 deg
Mean motion: 15
51239559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 75
Checksum: 315
Coasting Arc #5 (Orbit 90)
---------------------------------------
Vector Time (GMT): 2012/316/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -652321
55 A = 6793395
94 meter
Y = -5950564
11 meter E =
0002944
Z = 3213551
87 I = 51
98103
XDOT = 5040
137071 Wp = 257
98047
YDOT = -3156
585377 meter/sec RA = 108
55970 deg
ZDOT = -4826
301981 TA = 245
12254
MA = 245
15315
Ha = 224
961 n
mi
Hp = 219
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2140162
55 X = -601343
76
Y = -19522848
14 feet Y = -5957573
65 meter
Z = 10543149
18 Z = 3210506
85
XDOT = 16535
882780 XDOT = 5098
505821
YDOT = -10356
251238 feet/sec YDOT = -3099
897209 meter/sec
ZDOT = -15834
324086 ZDOT = -4801
674650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18653825
72 X = 5685686
08
Y = 6165180
25 feet Y = 1879146
94 meter
Z = 10531155
12 Z = 3209896
08
XDOT = 2898
015377 XDOT = 883
315087
YDOT = 18080
031828 feet/sec YDOT = 5510
793701 meter/sec
ZDOT = -15731
923512 ZDOT = -4795
090286
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
58048605
00016717 00000-0 10270-3 0 9040
2 25544 51
6438 109
2878 0015648 270
7741 89
1617 15
51236856 910
Satellite: ISS
Catalog Number: 25544
Epoch time: 12316
58048605 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 109
2878 deg
Eccentricity:
0015648
Arg of perigee: 270
7741 deg
Mean anomaly: 89
1617 deg
Mean motion: 15
51236856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 91
Checksum: 324
Coasting Arc #6 (Orbit 105)
---------------------------------------
Vector Time (GMT): 2012/317/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 538580
83 A = 6794910
14 meter
Y = 6264866
14 meter E =
0012429
Z = -2558122
45 I = 51
99650
XDOT = -4891
877151 Wp = 291
63185
YDOT = 2592
529688 meter/sec RA = 103
62174 deg
ZDOT = 5303
036393 TA = 39
79796
MA = 39
70686
Ha = 224
998 n
mi
Hp = 219
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1766997
47 X = 480912
92
Y = 20554022
78 feet Y = 6270566
44 meter
Z = -8392790
18 Z = -2555646
07
XDOT = -16049
465718 XDOT = -4946
265529
YDOT = 8505
674831 feet/sec YDOT = 2537
521587 meter/sec
ZDOT = 17398
413363 ZDOT = 5279
139015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19545536
11 X = -5957479
41
Y = -6612338
22 feet Y = -2015440
69 meter
Z = -8383201
11 Z = -2555199
70
XDOT = -1762
878725 XDOT = -537
325435
YDOT = -16788
394948 feet/sec YDOT = -5117
102780 meter/sec
ZDOT = 17299
086287 ZDOT = 5272
761500
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
54680059
00016717 00000-0 10270-3 0 9053
2 25544 51
6452 104
4912 0015646 274
7695 85
1670 15
51264050 1061
Satellite: ISS
Catalog Number: 25544
Epoch time: 12317
54680059 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 104
4912 deg
Eccentricity:
0015646
Arg of perigee: 274
7695 deg
Mean anomaly: 85
1670 deg
Mean motion: 15
51264050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 106
Checksum: 298
Coasting Arc #7 (Orbit 121)
---------------------------------------
Vector Time (GMT): 2012/318/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -483140
19 A = 6796166
36 meter
Y = -6514171
38 meter E =
0004257
Z = 1870980
66 I = 52
00707
XDOT = 4771
764559 Wp = 219
91388
YDOT = -1975
754334 meter/sec RA = 98
68631 deg
ZDOT = -5657
046696 TA = 299
63551
MA = 299
67790
Ha = 225
085 n
mi
Hp = 219
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1585105
60 X = -419350
53
Y = -21371953
36 feet Y = -6519217
54 meter
Z = 6138387
99 Z = 1868788
29
XDOT = 15655
395534 XDOT = 4820
984705
YDOT = -6482
133643 feet/sec YDOT = -1922
118128 meter/sec
ZDOT = -18559
864487 ZDOT = -5633
745459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20335040
29 X = 6198120
28
Y = 6772130
54 feet Y = 2064145
39 meter
Z = 6130019
71 Z = 1868430
01
XDOT = 371
464825 XDOT = 113
222479
YDOT = 15566
437165 feet/sec YDOT = 4744
650048 meter/sec
ZDOT = -18463
063504 ZDOT = -5627
541756
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
57752818
00016717 00000-0 10270-3 0 9061
2 25544 51
6453 99
3751 0015665 278
5117 81
4259 15
51272346 1224
Satellite: ISS
Catalog Number: 25544
Epoch time: 12318
57752818 = yrday
fracday
Element set: 906
Inclination: 51
6453 deg
RA of node: 99
3751 deg
Eccentricity:
0015665
Arg of perigee: 278
5117 deg
Mean anomaly: 81
4259 deg
Mean motion: 15
51272346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 122
Checksum: 319
Coasting Arc #8 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2012/319/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 434050
61 A = 6797083
07 meter
Y = 6682294
94 meter E =
0014391
Z = -1114739
04 I = 52
01538
XDOT = -4709
725756 Wp = 318
93418
YDOT = 1297
237050 meter/sec RA = 93
75245 deg
ZDOT = 5909
853390 TA = 29
04068
MA = 28
96070
Ha = 225
308 n
mi
Hp = 219
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1424050
55 X = 364710
83
Y = 21923539
83 feet Y = 6686761
13 meter
Z = -3657280
33 Z = -1112798
45
XDOT = -15451
856155 XDOT = -4752
591214
YDOT = 4256
027067 feet/sec YDOT = 1244
329960 meter/sec
ZDOT = 19389
282777 ZDOT = 5886
869071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20895515
62 X = -6368953
16
Y = -6789713
62 feet Y = -2069504
71 meter
Z = -3649990
99 Z = -1112517
25
XDOT = 1327
548482 XDOT = 404
636777
YDOT = -14515
065225 feet/sec YDOT = -4424
191880 meter/sec
ZDOT = 19293
859653 ZDOT = 5880
768422
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
54382660
00016717 00000-0 10270-3 0 9074
2 25544 51
6468 94
5786 0015672 282
7338 77
2061 15
51286405 1376
Satellite: ISS
Catalog Number: 25544
Epoch time: 12319
54382660 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 94
5786 deg
Eccentricity:
0015672
Arg of perigee: 282
7338 deg
Mean anomaly: 77
2061 deg
Mean motion: 15
51286405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 324
Coasting Arc #9 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2012/320/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -418193
78 A = 6797480
11 meter
Y = -6772770
24 meter E =
0006749
Z = 356916
83 I = 52
01823
XDOT = 4692
562959 Wp = 234
21508
YDOT = -602
847459 meter/sec RA = 88
82034 deg
ZDOT = -6024
770279 TA = 301
96391
MA = 302
02951
Ha = 225
462 n
mi
Hp = 219
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1372026
83 X = -344162
02
Y = -22220374
81 feet Y = -6777032
84 meter
Z = 1170986
97 Z = 355064
56
XDOT = 15395
547766 XDOT = 4728
222980
YDOT = -1977
845993 feet/sec YDOT = -550
172476 meter/sec
ZDOT = -19766
306690 ZDOT = -6001
886936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21263006
30 X = 6480964
32
Y = 6597589
32 feet Y = 2010945
22 meter
Z = 1164088
94 Z = 354814
31
XDOT = -3176
052030 XDOT = -968
060659
YDOT = 13658
159457 feet/sec YDOT = 4163
007003 meter/sec
ZDOT = -19671
371024 ZDOT = -5995
833888
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
57453669
00016717 00000-0 10270-3 0 9088
2 25544 51
6470 89
4632 0015685 286
4114 73
5313 15
51309002 1535
Satellite: ISS
Catalog Number: 25544
Epoch time: 12320
57453669 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 89
4632 deg
Eccentricity:
0015685
Arg of perigee: 286
4114 deg
Mean anomaly: 73
5313 deg
Mean motion: 15
51309002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 297
Coasting Arc #10 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2012/321/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 379004
89 A = 6797445
07 meter
Y = 6763487
56 meter E =
0014649
Z = 439672
08 I = 52
01762
XDOT = -4743
118091 Wp = 340
63426
YDOT = -121
198047 meter/sec RA = 83
88785 deg
ZDOT = 6023
704506 TA = 24
07921
MA = 24
01079
Ha = 225
779 n
mi
Hp = 219
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1243454
38 X = 301210
13
Y = 22189919
83 feet Y = 6767290
83 meter
Z = 1442493
69 Z = 441324
82
XDOT = -15561
411060 XDOT = -4770
672578
YDOT = -397
631388 feet/sec YDOT = -174
393060 meter/sec
ZDOT = 19762
810059 ZDOT = 6000
595335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21295872
33 X = -6490981
89
Y = -6356651
91 feet Y = -1937507
50 meter
Z = 1448553
49 Z = 441519
10
XDOT = 5222
638545 XDOT = 1591
860228
YDOT = -13067
624116 feet/sec YDOT = -3983
011831 meter/sec
ZDOT = 19667
013685 ZDOT = 5994
505771
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
60523799
00016717 00000-0 10270-3 0 9096
2 25544 51
6481 84
3469 0015667 290
9278 69
0196 15
51313975 1690
Satellite: ISS
Catalog Number: 25544
Epoch time: 12321
60523799 = yrday
fracday
Element set: 909
Inclination: 51
6481 deg
RA of node: 84
3469 deg
Eccentricity:
0015667
Arg of perigee: 290
9278 deg
Mean anomaly: 69
0196 deg
Mean motion: 15
51313975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 340
Coasting Arc #11 (Orbit 183)
---------------------------------------
Vector Time (GMT): 2012/322/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -345219
05 A = 6796833
90 meter
Y = -6678479
05 meter E =
0008719
Z = -1204353
98 I = 52
01153
XDOT = 4839
282987 Wp = 264
79431
YDOT = 816
921795 meter/sec RA = 78
95572 deg
ZDOT = -5881
416438 TA = 288
20196
MA = 288
29685
Ha = 225
968 n
mi
Hp = 219
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1132608
42 X = -264662
69
Y = -21911020
50 feet Y = -6681889
01 meter
Z = -3951292
60 Z = -1205835
81
XDOT = 15876
912687 XDOT = 4858
359251
YDOT = 2680
189616 feet/sec YDOT = 871
144709 meter/sec
ZDOT = -19295
985688 ZDOT = -5857
860756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21097518
71 X = 6430523
70
Y = 6018970
33 feet Y = 1834582
16 meter
Z = -3956644
36 Z = -1205985
20
XDOT = -7256
349903 XDOT = -2211
735450
YDOT = 12737
353651 feet/sec YDOT = 3882
345393 meter/sec
ZDOT = -19198
413604 ZDOT = -5851
676466
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
57151163
00016717 00000-0 10270-3 0 9107
2 25544 51
6480 79
5516 0015689 294
3094 65
6418 15
51338844 1844
Satellite: ISS
Catalog Number: 25544
Epoch time: 12322
57151163 = yrday
fracday
Element set: 910
Inclination: 51
6480 deg
RA of node: 79
5516 deg
Eccentricity:
0015689
Arg of perigee: 294
3094 deg
Mean anomaly: 65
6418 deg
Mean motion: 15
51338844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 184
Checksum: 315
Coasting Arc #12 (Orbit 199)
---------------------------------------
Vector Time (GMT): 2012/323/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 254484
39 A = 6795765
93 meter
Y = 6489733
98 meter E =
0012715
Z = 1973644
48 I = 52
00175
XDOT = -4996
389174 Wp = 355
91186
YDOT = -1507
894476 meter/sec RA = 74
02092 deg
ZDOT = 5617
041481 TA = 25
73998
MA = 25
67676
Ha = 226
279 n
mi
Hp = 219
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 834922
54 X = 172308
31
Y = 21291778
15 feet Y = 6492120
22 meter
Z = 6475211
54 Z = 1974681
45
XDOT = -16392
352932 XDOT = -5006
442800
YDOT = -4947
160353 feet/sec YDOT = -1563
823688 meter/sec
ZDOT = 18428
613782 ZDOT = 5592
744539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20512702
99 X = -6252271
87
Y = -5763705
52 feet Y = -1756777
44 meter
Z = 6478733
82 Z = 1974718
07
XDOT = 9342
590252 XDOT = 2847
621509
YDOT = -12701
591114 feet/sec YDOT = -3871
444971 meter/sec
ZDOT = 18328
046572 ZDOT = 5586
388595
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
60219494
00016717 00000-0 10270-3 0 9115
2 25544 51
6484 74
4349 0015668 298
6495 61
3080 15
51351440 2009
Satellite: ISS
Catalog Number: 25544
Epoch time: 12323
60219494 = yrday
fracday
Element set: 911
Inclination: 51
6484 deg
RA of node: 74
4349 deg
Eccentricity:
0015668
Arg of perigee: 298
6495 deg
Mean anomaly: 61
3080 deg
Mean motion: 15
51351440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 200
Checksum: 298
Coasting Arc #13 (Orbit 214)
---------------------------------------
Vector Time (GMT): 2012/324/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -145671
84 A = 6794363
29 meter
Y = -6243070
74 meter E =
0010800
Z = -2677139
62 I = 51
98733
XDOT = 5183
097460 Wp = 300
56097
YDOT = 2127
555096 meter/sec RA = 69
08529 deg
ZDOT = -5222
479575 TA = 269
44597
MA = 269
56972
Ha = 226
510 n
mi
Hp = 219
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -477926
00 X = -62844
64
Y = -20482515
55 feet Y = -6244236
55 meter
Z = -8783266
47 Z = -2677646
28
XDOT = 17004
912926 XDOT = 5184
291309
YDOT = 6980
167637 feet/sec YDOT = 2185
522548 meter/sec
ZDOT = -17134
119342 ZDOT = -5197
297152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19726865
96 X = 6012748
74
Y = 5530729
02 feet Y = 1685766
21 meter
Z = -8784612
80 Z = -2677549
98
XDOT = -11234
989472 XDOT = -3424
424791
YDOT = 12914
144674 feet/sec YDOT = 3936
231297 meter/sec
ZDOT = -17029
953806 ZDOT = -5190
729920
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
56845265
00016717 00000-0 10270-3 0 9123
2 25544 51
6479 69
6395 0015718 302
1341 57
8285 15
51359869 2153
Satellite: ISS
Catalog Number: 25544
Epoch time: 12324
56845265 = yrday
fracday
Element set: 912
Inclination: 51
6479 deg
RA of node: 69
6395 deg
Eccentricity:
0015718
Arg of perigee: 302
1341 deg
Mean anomaly: 57
8285 deg
Mean motion: 15
51359869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 215
Checksum: 330
Coasting Arc #14 (Orbit 230)
---------------------------------------
Vector Time (GMT): 2012/325/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -50570
01 A = 6792557
88 meter
Y = 5903280
04 meter E =
0009509
Z = 3349704
41 I = 51
97014
XDOT = -5407
058332 Wp = 358
61348
YDOT = -2712
779589 meter/sec RA = 64
14512 deg
ZDOT = 4708
702895 TA = 40
18023
MA = 40
10997
Ha = 226
786 n
mi
Hp = 219
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -165912
11 X = -132850
23
Y = 19367716
68 feet Y = 5902254
44 meter
Z = 10989843
86 Z = 3349258
96
XDOT = -17739
692690 XDOT = -5399
195625
YDOT = -8900
195503 feet/sec YDOT = -2773
200792 meter/sec
ZDOT = 15448
500311 ZDOT = 4682
454465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18567207
19 X = -5659284
75
Y = -5518261
64 feet Y = -1681966
15 meter
Z = 10987276
73 Z = 3348921
95
XDOT = 13032
325475 XDOT = 3972
252805
YDOT = -13368
806806 feet/sec YDOT = -4074
812314 meter/sec
ZDOT = 15339
987216 ZDOT = 4675
628103
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 12325
59911783
00016717 00000-0 10270-3 0 9137
2 25544 51
6482 64
5222 0015739 306
2572 53
7125 15
51389430 2317
Satellite: ISS
Catalog Number: 25544
Epoch time: 12325
59911783 = yrday
fracday
Element set: 913
Inclination: 51
6482 deg
RA of node: 64
5222 deg
Eccentricity:
0015739
Arg of perigee: 306
2572 deg
Mean anomaly: 53
7125 deg
Mean motion: 15
51389430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 231
Checksum: 298
Coasting Arc #15 (Orbit 245)
---------------------------------------
Vector Time (GMT): 2012/326/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 277043
08 A = 6790839
97 meter
Y = -5537143
28 meter E =
0013291
Z = -3926030
91 I = 51
94944
XDOT = 5631
485983 Wp = 333
83384
YDOT = 3194
303396 meter/sec RA = 59
20358 deg
ZDOT = -4090
865376 TA = 253
38002
MA = 253
52600
Ha = 227
047 n
mi
Hp = 219
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 908933
98 X = 358011
98
Y = -18166480
59 feet Y = -5533592
48 meter
Z = -12880678
83 Z = -3924488
38
XDOT = 18476
003880 XDOT = 5615
220798
YDOT = 10479
998017 feet/sec YDOT = 3257
187264 meter/sec
ZDOT = -13421
474331 ZDOT = -4063
547046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17304800
47 X = 5274503
18
Y = 5619017
71 feet Y = 1712676
60 meter
Z = -12873600
33 Z = -3923873
38
XDOT = -14482
566733 XDOT = -4414
286340
YDOT = 13983
755052 feet/sec YDOT = 4262
248540 meter/sec
ZDOT = -13308
588382 ZDOT = -4056
457739
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 12326
56535995
00016717 00000-0 10270-3 0 9143
2 25544 51
6475 59
7266 0015786 309
9961 49
9803 15
51378316 2464
Satellite: ISS
Catalog Number: 25544
Epoch time: 12326
56535995 = yrday
fracday
Element set: 914
Inclination: 51
6475 deg
RA of node: 59
7266 deg
Eccentricity:
0015786
Arg of perigee: 309
9961 deg
Mean anomaly: 49
9803 deg
Mean motion: 15
51378316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 246
Checksum: 351
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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