[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 10th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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
053/10:34:52
615 -2
0 3
0 3
0
N/A -0
7 -0
1 223
9
000/00:07:45
231 -2
1 -0
0 220
2
Coasting Arc #1 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2013/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5469444
95 A = 6787977
21 meter
Y = -708812
50 meter E =
0008045
Z = -3956862
79 I = 51
80605
XDOT = 3628
514048 Wp = 224
10691
YDOT = 5410
244892 meter/sec RA = 26
98031 deg
ZDOT = 4035
845632 TA = 88
01444
MA = 87
92231
Ha = 223
157 n
mi
Hp = 219
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17944373
18 X = 5496185
37
Y = -2325500
34 feet Y = -647500
25 meter
Z = -12981833
31 Z = -3930228
50
XDOT = 11904
573647 XDOT = 3548
141361
YDOT = 17750
147282 feet/sec YDOT = 5450
371856 meter/sec
ZDOT = 13240
963359 ZDOT = 4053
276879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14941364
56 X = 4554127
92
Y = 10345650
75 feet Y = 3153354
35 meter
Z = -12870882
34 Z = -3923044
94
XDOT = -2357
254787 XDOT = -718
491259
YDOT = 20010
150718 feet/sec YDOT = 6099
093939 meter/sec
ZDOT = 13312
783369 ZDOT = 4057
736371
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 13039
50849905
00016717 00000-0 10270-3 0 9003
2 25544 51
6447 27
5249 0012569 251
9324 108
0458 15
52356164 14725
Satellite: ISS
Catalog Number: 25544
Epoch time: 13039
50849905 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 27
5249 deg
Eccentricity:
0012569
Arg of perigee: 251
9324 deg
Mean anomaly: 108
0458 deg
Mean motion: 15
52356164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 312
Coasting Arc #2 (Orbit 1487)
---------------------------------------
Vector Time (GMT): 2013/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6028330
21 A = 6790327
87 meter
Y = 205516
89 meter E =
0004385
Z = 3112770
75 I = 51
78662
XDOT = -2702
528690 Wp = 170
71668
YDOT = -5246
393789 meter/sec RA = 22
01956 deg
ZDOT = -4890
710760 TA = 333
57462
MA = 333
59697
Ha = 222
823 n
mi
Hp = 219
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19777986
24 X = -6045300
86
Y = 674268
01 feet Y = 138009
52 meter
Z = 10212502
46 Z = 3083445
29
XDOT = -8866
563943 XDOT = -2619
904487
YDOT = -17212
578047 feet/sec YDOT = -5276
153338 meter/sec
ZDOT = -16045
638976 ZDOT = -4903
638168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15401709
27 X = -4694440
99
Y = -12525548
12 feet Y = -3817787
07 meter
Z = 10090420
17 Z = 3075560
07
XDOT = 3785
275123 XDOT = 1153
751857
YDOT = -17614
676999 feet/sec YDOT = -5368
953549 meter/sec
ZDOT = -16098
736541 ZDOT = -4906
894898
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 13040
53848538
00016717 00000-0 10270-3 0 9010
2 25544 51
6446 22
4034 0012647 256
2712 103
7032 15
52409108 14880
Satellite: ISS
Catalog Number: 25544
Epoch time: 13040
53848538 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 22
4034 deg
Eccentricity:
0012647
Arg of perigee: 256
2712 deg
Mean anomaly: 103
7032 deg
Mean motion: 15
52409108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1488
Checksum: 284
Coasting Arc #3 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2013/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6449629
04 A = 6792510
81 meter
Y = 244875
25 meter E =
0008447
Z = -2104566
68 I = 51
76536
XDOT = 1617
791752 Wp = 287
91518
YDOT = 5054
383575 meter/sec RA = 17
06134 deg
ZDOT = 5530
249509 TA = 48
83924
MA = 48
76640
Ha = 222
418 n
mi
Hp = 219
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21160200
27 X = 6456634
58
Y = 803396
50 feet Y = 317038
11 meter
Z = -6904746
32 Z = -2073218
84
XDOT = 5307
715721 XDOT = 1534
288621
YDOT = 16582
623279 feet/sec YDOT = 5072
008154 meter/sec
ZDOT = 18143
863220 ZDOT = 5537
905275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15705216
12 X = 4786949
87
Y = 14266391
60 feet Y = 4348396
16 meter
Z = -6774311
81 Z = -2064810
24
XDOT = -5662
554977 XDOT = -1725
946757
YDOT = 14888
912755 feet/sec YDOT = 4538
140608 meter/sec
ZDOT = 18175
046762 ZDOT = 5539
754253
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 13041
50408559
00016717 00000-0 10270-3 0 9024
2 25544 51
6447 17
6021 0012504 259
4615 100
5128 15
52414893 15038
Satellite: ISS
Catalog Number: 25544
Epoch time: 13041
50408559 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 17
6021 deg
Eccentricity:
0012504
Arg of perigee: 259
4615 deg
Mean anomaly: 100
5128 deg
Mean motion: 15
52414893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 276
Coasting Arc #4 (Orbit 1518)
---------------------------------------
Vector Time (GMT): 2013/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6683943
25 A = 6793829
14 meter
Y = -620028
02 meter E =
0009119
Z = 1008569
07 I = 51
74141
XDOT = -438
646774 Wp = 188
50796
YDOT = -4861
639572 meter/sec RA = 12
10440 deg
ZDOT = -5911
349701 TA = 340
58467
MA = 340
61938
Ha = 222
158 n
mi
Hp = 219
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21928947
67 X = -6681412
44
Y = -2034212
68 feet Y = -694757
85 meter
Z = 3308953
66 Z = 976106
09
XDOT = -1439
129836 XDOT = -355
535266
YDOT = -15950
261064 feet/sec YDOT = -4866
080542 meter/sec
ZDOT = -19394
191931 ZDOT = -5913
278316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15751337
12 X = -4801007
56
Y = -15420358
49 feet Y = -4700125
27 meter
Z = 3173935
16 Z = 967415
44
XDOT = 7911
109507 XDOT = 2411
306178
YDOT = -12063
287098 feet/sec YDOT = -3676
889907 meter/sec
ZDOT = -19401
566721 ZDOT = -5913
597537
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 13042
53404509
00016717 00000-0 10270-3 0 9030
2 25544 51
6456 12
4807 0012611 263
9680 96
0035 15
52445666 15199
Satellite: ISS
Catalog Number: 25544
Epoch time: 13042
53404509 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 12
4807 deg
Eccentricity:
0012611
Arg of perigee: 263
9680 deg
Mean anomaly: 96
0035 deg
Mean motion: 15
52445666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1519
Checksum: 293
Coasting Arc #5 (Orbit 1534)
---------------------------------------
Vector Time (GMT): 2013/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6717718
86 A = 6794112
43 meter
Y = 968038
52 meter E =
0008446
Z = 157929
31 I = 51
71266
XDOT = -813
322412 Wp = 335
88671
YDOT = 4682
660533 meter/sec RA = 7
14751 deg
ZDOT = 6014
069324 TA = 25
81164
MA = 25
76952
Ha = 221
905 n
mi
Hp = 219
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22039760
04 X = 6705627
61
Y = 3175979
41 feet Y = 1043092
68 meter
Z = 518140
77 Z = 190533
24
XDOT = -2668
380617 XDOT = -894
838580
YDOT = 15363
059493 feet/sec YDOT = 4673
110205 meter/sec
ZDOT = 19731
198569 ZDOT = 6009
919948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15378033
21 X = 4687224
52
Y = 16099537
89 feet Y = 4907139
15 meter
Z = 653690
88 Z = 199244
98
XDOT = -10503
981441 XDOT = -3201
613543
YDOT = 9245
606899 feet/sec YDOT = 2818
060983 meter/sec
ZDOT = 19713
304500 ZDOT = 6008
615212
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 13043
56398979
00016717 00000-0 10270-3 0 9048
2 25544 51
6456 7
3594 0012583 267
0706 92
9006 15
52478808 15352
Satellite: ISS
Catalog Number: 25544
Epoch time: 13043
56398979 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 7
3594 deg
Eccentricity:
0012583
Arg of perigee: 267
0706 deg
Mean anomaly: 92
9006 deg
Mean motion: 15
52478808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1535
Checksum: 334
Coasting Arc #6 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2013/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6536117
64 A = 6793348
94 meter
Y = -1282949
31 meter E =
0009855
Z = -1306408
18 I = 51
68082
XDOT = 2059
208871 Wp = 227
41488
YDOT = -4532
222323 meter/sec RA = 2
18822 deg
ZDOT = -5830
147377 TA = 326
78551
MA = 326
84733
Ha = 221
887 n
mi
Hp = 218
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21443955
50 X = -6514939
58
Y = -4209151
27 feet Y = -1355921
99 meter
Z = -4286116
08 Z = -1338107
95
XDOT = 6755
934615 XDOT = 2138
056898
YDOT = -14869
495809 feet/sec YDOT = -4508
754633 meter/sec
ZDOT = -19127
780109 ZDOT = -5819
952161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14535399
58 X = -4430389
79
Y = -16282988
33 feet Y = -4963054
84 meter
Z = -4417852
78 Z = -1346561
53
XDOT = 13268
646072 XDOT = 4044
283323
YDOT = -6648
002097 feet/sec YDOT = -2026
311039 meter/sec
ZDOT = -19084
749528 ZDOT = -5817
031656
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 13044
52955122
00016717 00000-0 10270-3 0 9055
2 25544 51
6467 2
5585 0012653 271
4849 88
4853 15
52483452 15504
Satellite: ISS
Catalog Number: 25544
Epoch time: 13044
52955122 = yrday
fracday
Element set: 905
Inclination: 51
6467 deg
RA of node: 2
5585 deg
Eccentricity:
0012653
Arg of perigee: 271
4849 deg
Mean anomaly: 88
4853 deg
Mean motion: 15
52483452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 313
Coasting Arc #7 (Orbit 1565)
---------------------------------------
Vector Time (GMT): 2013/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6135774
56 A = 6791473
34 meter
Y = 1615034
17 meter E =
0004705
Z = 2413977
18 I = 51
64444
XDOT = -3265
123761 Wp = 6
90463
YDOT = 4402
570529 meter/sec RA = 357
22452 deg
ZDOT = 5357
198376 TA = 20
06188
MA = 20
04339
Ha = 221
884 n
mi
Hp = 218
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20130493
97 X = 6105532
60
Y = 5298668
54 feet Y = 1683479
38 meter
Z = 7919872
62 Z = 2443710
20
XDOT = -10712
348298 XDOT = -3340
135032
YDOT = 14444
129032 feet/sec YDOT = 4365
638919 meter/sec
ZDOT = 17576
110157 ZDOT = 5341
154339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13091850
12 X = 3990395
92
Y = 16122799
64 feet Y = 4914229
33 meter
Z = 8043373
08 Z = 2451620
12
XDOT = -16081
988381 XDOT = -4901
790058
YDOT = 4329
509569 feet/sec YDOT = 1319
634517 meter/sec
ZDOT = 17508
762493 ZDOT = 5336
670808
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 13045
55946808
00016717 00000-0 10270-3 0 9061
2 25544 51
6469 357
4373 0012673 274
8694 85
1011 15
52517131 15669
Satellite: ISS
Catalog Number: 25544
Epoch time: 13045
55946808 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 357
4373 deg
Eccentricity:
0012673
Arg of perigee: 274
8694 deg
Mean anomaly: 85
1011 deg
Mean motion: 15
52517131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1566
Checksum: 324
Coasting Arc #8 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2013/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5541766
70 A = 6789000
54 meter
Y = -1959310
40 meter E =
0007897
Z = -3392572
79 I = 51
60627
XDOT = 4354
465055 Wp = 284
54452
YDOT = -4290
328867 meter/sec RA = 352
25450 deg
ZDOT = -4624
263275 TA = 295
08351
MA = 295
16545
Ha = 222
122 n
mi
Hp = 218
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18181649
28 X = -5502965
39
Y = -6428183
71 feet Y = -2021065
22 meter
Z = -11130488
14 Z = -3419399
47
XDOT = 14286
302674 XDOT = 4424
579945
YDOT = -14075
882109 feet/sec YDOT = -4241
242814 meter/sec
ZDOT = -15171
467439 ZDOT = -4602
939305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11107238
29 X = -3385486
23
Y = -15685404
14 feet Y = -4780911
18 meter
Z = -11241843
16 Z = -3426513
79
XDOT = 18718
203170 XDOT = 5705
308326
YDOT = -2419
817158 feet/sec YDOT = -737
560270 meter/sec
ZDOT = -15082
169373 ZDOT = -4597
045225
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 13046
52500291
00016717 00000-0 10270-3 0 9072
2 25544 51
6473 352
6363 0012682 279
1283 80
8434 15
52533990 15811
Satellite: ISS
Catalog Number: 25544
Epoch time: 13046
52500291 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 352
6363 deg
Eccentricity:
0012682
Arg of perigee: 279
1283 deg
Mean anomaly: 80
8434 deg
Mean motion: 15
52533990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 307
Coasting Arc #9 (Orbit 1596)
---------------------------------------
Vector Time (GMT): 2013/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4762329
92 A = 6786233
46 meter
Y = 2359544
97 meter E =
0002828
Z = 4222230
84 I = 51
56732
XDOT = -5296
577425 Wp = 266
91061
YDOT = 4164
214791 meter/sec RA = 347
27746 deg
ZDOT = 3648
947039 TA = 145
65745
MA = 145
63916
Ha = 222
272 n
mi
Hp = 218
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15624442
01 X = 4715080
82
Y = 7741289
26 feet Y = 2412536
40 meter
Z = 13852463
38 Z = 4245250
64
XDOT = -17377
222524 XDOT = -5360
474303
YDOT = 13662
122018 feet/sec YDOT = 4104
628088 meter/sec
ZDOT = 11971
611019 ZDOT = 3623
061584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8508179
69 X = 2593293
17
Y = 15133005
82 feet Y = 4612540
17 meter
Z = 13947921
07 Z = 4251326
34
XDOT = -21008
495697 XDOT = -6403
389488
YDOT = 883
119609 feet/sec YDOT = 269
174857 meter/sec
ZDOT = 11863
354937 ZDOT = 3615
950585
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 13047
55489143
00016717 00000-0 10270-3 0 9089
2 25544 51
6475 347
5150 0012719 282
3531 77
6197 15
52564730 15976
Satellite: ISS
Catalog Number: 25544
Epoch time: 13047
55489143 = yrday
fracday
Element set: 908
Inclination: 51
6475 deg
RA of node: 347
5150 deg
Eccentricity:
0012719
Arg of perigee: 282
3531 deg
Mean anomaly: 77
6197 deg
Mean motion: 15
52564730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1597
Checksum: 329
Coasting Arc #10 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2013/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3859433
03 A = 6783863
06 meter
Y = -2796178
92 meter E =
0007219
Z = -4829667
49 I = 51
53001
XDOT = 6036
313113 Wp = 351
79694
YDOT = -4008
655300 meter/sec RA = 342
29278 deg
ZDOT = -2495
371152 TA = 253
58864
MA = 253
66800
Ha = 222
598 n
mi
Hp = 218
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12662181
86 X = -3804417
79
Y = -9173815
35 feet Y = -2839030
15 meter
Z = -15845365
77 Z = -4848282
27
XDOT = 19804
176879 XDOT = 6092
811808
YDOT = -13151
756233 feet/sec YDOT = -3940
837673 meter/sec
ZDOT = -8186
913228 ZDOT = -2465
910218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5493685
74 X = -1674475
41
Y = -14555439
56 feet Y = -4436497
98 meter
Z = -15922435
43 Z = -4853158
32
XDOT = 22753
614238 XDOT = 6935
301620
YDOT = 259
827030 feet/sec YDOT = 79
195279 meter/sec
ZDOT = -8063
806063 ZDOT = -2457
848088
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 13048
52040001
00016717 00000-0 10270-3 0 9094
2 25544 51
6476 342
7133 0012677 286
6069 73
3691 15
52581351 16129
Satellite: ISS
Catalog Number: 25544
Epoch time: 13048
52040001 = yrday
fracday
Element set: 909
Inclination: 51
6476 deg
RA of node: 342
7133 deg
Eccentricity:
0012677
Arg of perigee: 286
6069 deg
Mean anomaly: 73
3691 deg
Mean motion: 15
52581351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 297
Coasting Arc #11 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2013/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2846139
44 A = 6782186
84 meter
Y = 3298254
35 meter E =
0009048
Z = 5205256
59 I = 51
49594
XDOT = -6556
903672 Wp = 283
21725
YDOT = 3774
799669 meter/sec RA = 337
30244 deg
ZDOT = 1197
116408 TA = 155
28472
MA = 155
24135
Ha = 222
839 n
mi
Hp = 218
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9337727
83 X = 2783760
75
Y = 10821044
46 feet Y = 3329733
11 meter
Z = 17077613
47 Z = 5218931
04
XDOT = -21512
151154 XDOT = -6604
442148
YDOT = 12384
513349 feet/sec YDOT = 3701
210499 meter/sec
ZDOT = 3927
547269 ZDOT = 1165
148377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2045911
10 X = 623593
70
Y = 14077330
05 feet Y = 4290770
20 meter
Z = 17134061
76 Z = 5222462
03
XDOT = -23796
625040 XDOT = -7253
211312
YDOT = -1144
373696 feet/sec YDOT = -348
805103 meter/sec
ZDOT = 3794
044717 ZDOT = 1156
424830
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 13049
55025976
00016717 00000-0 10270-3 0 9104
2 25544 51
6477 337
5919 0012812 289
8720 70
1051 15
52620427 16284
Satellite: ISS
Catalog Number: 25544
Epoch time: 13049
55025976 = yrday
fracday
Element set: 910
Inclination: 51
6477 deg
RA of node: 337
5919 deg
Eccentricity:
0012812
Arg of perigee: 289
8720 deg
Mean anomaly: 70
1051 deg
Mean motion: 15
52620427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1628
Checksum: 312
Coasting Arc #12 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2013/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1808769
79 A = 6781763
38 meter
Y = -3821899
25 meter E =
0005742
Z = -5304892
02 I = 51
46695
XDOT = 6842
100426 Wp = 33
67210
YDOT = -3449
694709 meter/sec RA = 332
30730 deg
ZDOT = 157
189381 TA = 237
80245
MA = 237
85814
Ha = 223
132 n
mi
Hp = 218
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5934284
07 X = -1740128
75
Y = -12539039
55 feet Y = -3841742
47 meter
Z = -17404501
38 Z = -5313511
85
XDOT = 22447
836042 XDOT = 6879
403554
YDOT = -11317
896028 feet/sec YDOT = -3372
973464 meter/sec
ZDOT = 515
713191 ZDOT = 190
517896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1515014
86 X = 461776
53
Y = -13744678
37 feet Y = -4189377
97 meter
Z = -17439852
49 Z = -5315667
04
XDOT = 24058
248742 XDOT = 7332
954217
YDOT = 1840
749623 feet/sec YDOT = 561
060485 meter/sec
ZDOT = 654
828581 ZDOT = 199
591751
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 13050
51574242
00016717 00000-0 10270-3 0 9118
2 25544 51
6481 332
7898 0012721 293
9569 66
0250 15
52616956 16432
Satellite: ISS
Catalog Number: 25544
Epoch time: 13050
51574242 = yrday
fracday
Element set: 911
Inclination: 51
6481 deg
RA of node: 332
7898 deg
Eccentricity:
0012721
Arg of perigee: 293
9569 deg
Mean anomaly: 66
0250 deg
Mean motion: 15
52616956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 314
Coasting Arc #13 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2013/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 754654
02 A = 6782467
08 meter
Y = 4377683
75 meter E =
0011436
Z = 5133698
08 I = 51
44284
XDOT = -6889
381216 Wp = 319
35253
YDOT = 2979
864408 meter/sec RA = 327
31105 deg
ZDOT = -1521
712106 TA = 145
40366
MA = 145
32920
Ha = 223
428 n
mi
Hp = 218
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2475899
02 X = 680708
09
Y = 14362479
50 feet Y = 4385709
52 meter
Z = 16842841
46 Z = 5137184
26
XDOT = -22602
956745 XDOT = -6914
798730
YDOT = 9776
458031 feet/sec YDOT = 2902
680839 meter/sec
ZDOT = -4992
493785 ZDOT = -1555
241341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5181445
29 X = -1579304
53
Y = 13604936
64 feet Y = 4146784
69 meter
Z = 16856764
98 Z = 5137941
97
XDOT = -23432
331323 XDOT = -7142
174587
YDOT = -2538
365096 feet/sec YDOT = -773
693681 meter/sec
ZDOT = -5132
377914 ZDOT = -1564
348788
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 13051
54557467
00016717 00000-0 10270-3 0 9123
2 25544 51
6480 327
6683 0012825 297
7254 62
2597 15
52653233 16592
Satellite: ISS
Catalog Number: 25544
Epoch time: 13051
54557467 = yrday
fracday
Element set: 912
Inclination: 51
6480 deg
RA of node: 327
6683 deg
Eccentricity:
0012825
Arg of perigee: 297
7254 deg
Mean anomaly: 62
2597 deg
Mean motion: 15
52653233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1659
Checksum: 329
Coasting Arc #14 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2013/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 225635
27 A = 6784310
98 meter
Y = -4897891
14 meter E =
0003219
Z = -4686813
77 I = 51
42445
XDOT = 6729
606057 Wp = 344
37665
YDOT = -2371
539918 meter/sec RA = 322
31473 deg
ZDOT = 2804
915600 TA = 313
51266
MA = 313
53941
Ha = 223
659 n
mi
Hp = 218
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 740273
19 X = 303154
56
Y = -16069196
65 feet Y = -4894934
74 meter
Z = -15376685
58 Z = -4685529
15
XDOT = 22078
760029 XDOT = 6741
999724
YDOT = -7780
642776 feet/sec YDOT = -2296
215800 meter/sec
ZDOT = 9202
479001 ZDOT = 2837
636957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8578719
18 X = 2614793
61
Y = -13614578
55 feet Y = -4149723
54 meter
Z = -15370698
53 Z = -4684988
91
XDOT = 22023
074307 XDOT = 6712
633049
YDOT = 3343
086253 feet/sec YDOT = 1018
972690 meter/sec
ZDOT = 9338
917979 ZDOT = 2846
502200
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 13052
51103046
00016717 00000-0 10270-3 0 9132
2 25544 51
6486 322
8660 0012791 301
4029 58
5871 15
52656386 16747
Satellite: ISS
Catalog Number: 25544
Epoch time: 13052
51103046 = yrday
fracday
Element set: 913
Inclination: 51
6486 deg
RA of node: 322
8660 deg
Eccentricity:
0012791
Arg of perigee: 301
4029 deg
Mean anomaly: 58
5871 deg
Mean motion: 15
52656386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1674
Checksum: 303
Coasting Arc #15 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2013/053/10:38:45
231
Vector Time (MET): N/A
Weight (LBS) : 902838
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4787750
59 A = 6795189
58 meter
Y = 4802037
59 meter E =
0003349
Z = 402089
68 I = 51
43231
XDOT = -3638
356086 Wp = 180
71171
YDOT = -3127
702314 meter/sec RA = 317
62465 deg
ZDOT = -5973
125979 TA = 354
94650
MA = 354
94988
Ha = 223
931 n
mi
Hp = 220
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15707843
13 X = -4843045
36
Y = 15754716
50 feet Y = 4748188
81 meter
Z = 1319191
85 Z = 378697
14
XDOT = -11936
863799 XDOT = -3574
095867
YDOT = -10261
490530 feet/sec YDOT = -3168
029768 meter/sec
ZDOT = -19596
870009 ZDOT = -5990
644110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22210271
17 X = -6769690
65
Y = -1378439
39 feet Y = -420148
33 meter
Z = 1221251
17 Z = 372237
36
XDOT = -210
007942 XDOT = -64
010421
YDOT = -14030
615335 feet/sec YDOT = -4276
531554 meter/sec
ZDOT = -19669
342557 ZDOT = -5995
215611
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 13053
47648838
00016717 00000-0 10270-3 0 9142
2 25544 51
6479 318
0643 0010903 297
3675 62
6366 15
52093117 16898
Satellite: ISS
Catalog Number: 25544
Epoch time: 13053
47648838 = yrday
fracday
Element set: 914
Inclination: 51
6479 deg
RA of node: 318
0643 deg
Eccentricity:
0010903
Arg of perigee: 297
3675 deg
Mean anomaly: 62
6366 deg
Mean motion: 15
52093117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 334
Coasting Arc #16 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2013/054/10:38:45
231
Vector Time (MET): N/A
Weight (LBS) : 902838
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4943244
57 A = 6795005
48 meter
Y = -4603116
25 meter E =
0013835
Z = 648275
42 I = 51
40958
XDOT = 2857
628982 Wp = 4
01246
YDOT = 3905
906586 meter/sec RA = 312
64794 deg
ZDOT = 5949
873117 TA = 3
00827
MA = 2
99995
Ha = 224
123 n
mi
Hp = 219
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16217994
00 X = 4991201
13
Y = -15102087
44 feet Y = -4547569
59 meter
Z = 2126887
87 Z = 672405
55
XDOT = 9375
423168 XDOT = 2784
837718
YDOT = 12814
654155 feet/sec YDOT = 3937
455870 meter/sec
ZDOT = 19520
581093 ZDOT = 5963
577779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22077730
15 X = 6729292
15
Y = 1797355
89 feet Y = 547834
08 meter
Z = 2227862
16 Z = 679052
39
XDOT = -3102
374130 XDOT = -945
603635
YDOT = 13864
214912 feet/sec YDOT = 4225
812705 meter/sec
ZDOT = 19577
093947 ZDOT = 5967
098235
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 13054
50665784
00016717 00000-0 10270-3 0 9157
2 25544 51
6476 312
9445 0010995 301
6634 58
3445 15
52112588 17045
Satellite: ISS
Catalog Number: 25544
Epoch time: 13054
50665784 = yrday
fracday
Element set: 915
Inclination: 51
6476 deg
RA of node: 312
9445 deg
Eccentricity:
0010995
Arg of perigee: 301
6634 deg
Mean anomaly: 58
3445 deg
Mean motion: 15
52112588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1704
Checksum: 316
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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