[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 20th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 2992)
---------------------------------------
Vector Time (GMT): 2013/137/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4344708
65 A = 6789777
78 meter
Y = -1345153
26 meter E =
0008277
Z = -5046377
33 I = 51
28039
XDOT = 182
117434 Wp = 59
53641
YDOT = -7433
411927 meter/sec RA = 260
01730 deg
ZDOT = 1831
013715 TA = 228
27422
MA = 228
34504
Ha = 227
659 n
mi
Hp = 221
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14254293
47 X = -4304829
83
Y = -4413232
48 feet Y = -1393515
36 meter
Z = -16556356
06 Z = -5067386
87
XDOT = 597
498142 XDOT = 256
331276
YDOT = -24387
834407 feet/sec YDOT = -7430
960494 meter/sec
ZDOT = 6007
262843 ZDOT = 1832
078403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14687323
69 X = -4476696
26
Y = 2010300
28 feet Y = 612739
53 meter
Z = -16643786
98 Z = -5073026
27
XDOT = -9698
326472 XDOT = -2956
049909
YDOT = -21247
940885 feet/sec YDOT = -6476
372382 meter/sec
ZDOT = 6012
684027 ZDOT = 1832
666092
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 13137
43144206
00016717 00000-0 10270-3 0 9006
2 25544 51
6462 260
8253 0009213 322
5344 37
5164 15
50248145 29934
Satellite: ISS
Catalog Number: 25544
Epoch time: 13137
43144206 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 260
8253 deg
Eccentricity:
0009213
Arg of perigee: 322
5344 deg
Mean anomaly: 37
5164 deg
Mean motion: 15
50248145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2993
Checksum: 284
Coasting Arc #2 (Orbit 3008)
---------------------------------------
Vector Time (GMT): 2013/138/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4463301
53 A = 6790471
13 meter
Y = 1516493
23 meter E =
0011175
Z = 4891202
46 I = 51
28826
XDOT = 47
312703 Wp = 3
24166
YDOT = 7305
984171 meter/sec RA = 255
03319 deg
ZDOT = -2297
144352 TA = 109
42435
MA = 109
30356
Ha = 227
894 n
mi
Hp = 221
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14643377
71 X = 4422251
71
Y = 4975371
50 feet Y = 1566175
02 meter
Z = 16047252
16 Z = 4912785
30
XDOT = 155
225404 XDOT = -23
228900
YDOT = 23969
764341 feet/sec YDOT = 7306
118896 meter/sec
ZDOT = -7536
562834 ZDOT = -2297
085646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15250109
34 X = 4648233
33
Y = -1930459
94 feet Y = -588404
19 meter
Z = 16137057
48 Z = 4918575
12
XDOT = 10587
020229 XDOT = 3226
923766
YDOT = 20323
370881 feet/sec YDOT = 6194
563445 meter/sec
ZDOT = -7537
271316 ZDOT = -2297
360297
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 13138
46284648
00016717 00000-0 10270-3 0 9016
2 25544 51
6456 255
7127 0009204 326
7739 33
2833 15
50234376 30090
Satellite: ISS
Catalog Number: 25544
Epoch time: 13138
46284648 = yrday
fracday
Element set: 901
Inclination: 51
6456 deg
RA of node: 255
7127 deg
Eccentricity:
0009204
Arg of perigee: 326
7739 deg
Mean anomaly: 33
2833 deg
Mean motion: 15
50234376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3009
Checksum: 310
Coasting Arc #3 (Orbit 3023)
---------------------------------------
Vector Time (GMT): 2013/139/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4610408
19 A = 6791004
10 meter
Y = -1632795
83 meter E =
0007296
Z = -4714213
90 I = 51
30050
XDOT = -260
750587 Wp = 51
81120
YDOT = -7148
050231 meter/sec RA = 250
05182 deg
ZDOT = 2738
102638 TA = 245
41412
MA = 245
49016
Ha = 227
932 n
mi
Hp = 221
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15126011
13 X = -4568906
63
Y = -5356941
68 feet Y = -1684120
17 meter
Z = -15466581
05 Z = -4736510
33
XDOT = -855
480929 XDOT = -194
101280
YDOT = -23451
608369 feet/sec YDOT = -7150
593507 meter/sec
ZDOT = 8983
276372 ZDOT = 2736
997666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15821258
67 X = -4822319
64
Y = 2074239
63 feet Y = 632228
24 meter
Z = -15559353
14 Z = -4742490
84
XDOT = -11339
036250 XDOT = -3456
138249
YDOT = -19309
657151 feet/sec YDOT = -5885
583500 meter/sec
ZDOT = 8979
591108 ZDOT = 2736
979370
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 13139
42976961
00016717 00000-0 10270-3 0 9020
2 25544 51
6467 250
9213 0009339 330
1024 29
9592 15
50295158 30246
Satellite: ISS
Catalog Number: 25544
Epoch time: 13139
42976961 = yrday
fracday
Element set: 902
Inclination: 51
6467 deg
RA of node: 250
9213 deg
Eccentricity:
0009339
Arg of perigee: 330
1024 deg
Mean anomaly: 29
9592 deg
Mean motion: 15
50295158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3024
Checksum: 310
Coasting Arc #4 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2013/140/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4784959
62 A = 6791915
72 meter
Y = 1777986
13 meter E =
0012452
Z = 4483001
26 I = 51
31485
XDOT = 416
618739 Wp = 20
03406
YDOT = 6951
450909 meter/sec RA = 245
06969 deg
ZDOT = -3187
542492 TA = 102
25617
MA = 102
11670
Ha = 228
147 n
mi
Hp = 221
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15698686
41 X = 4742944
64
Y = 5833287
82 feet Y = 1831259
56 meter
Z = 14708009
38 Z = 4506144
48
XDOT = 1366
859381 XDOT = 354
339597
YDOT = 22806
597470 feet/sec YDOT = 6955
761638 meter/sec
ZDOT = -10457
816574 ZDOT = -3185
669714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16516809
15 X = 5034323
43
Y = -2197555
73 feet Y = -669814
99 meter
Z = 14804300
26 Z = 4512350
72
XDOT = 11835
960113 XDOT = 3607
600642
YDOT = 18244
093922 feet/sec YDOT = 5560
799827 meter/sec
ZDOT = -10450
895937 ZDOT = -3185
433081
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 13140
46113943
00016717 00000-0 10270-3 0 9030
2 25544 51
6467 245
8086 0009300 334
3710 25
6979 15
50293524 30408
Satellite: ISS
Catalog Number: 25544
Epoch time: 13140
46113943 = yrday
fracday
Element set: 903
Inclination: 51
6467 deg
RA of node: 245
8086 deg
Eccentricity:
0009300
Arg of perigee: 334
3710 deg
Mean anomaly: 25
6979 deg
Mean motion: 15
50293524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 292
Coasting Arc #5 (Orbit 3054)
---------------------------------------
Vector Time (GMT): 2013/141/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4976324
91 A = 6792684
55 meter
Y = -1854186
76 meter E =
0007227
Z = -4235089
57 I = 51
33253
XDOT = -548
933382 Wp = 34
67610
YDOT = -6737
667128 meter/sec RA = 240
09061 deg
ZDOT = 3603
733648 TA = 272
33196
MA = 272
41470
Ha = 228
207 n
mi
Hp = 220
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16326525
30 X = -4934647
85
Y = -6083289
91 feet Y = -1909602
03 meter
Z = -13894650
82 Z = -4259163
36
XDOT = -1800
962539 XDOT = -491
056820
YDOT = -22105
207113 feet/sec YDOT = -6743
482133 meter/sec
ZDOT = 11823
273124 ZDOT = 3601
207342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17151149
31 X = -5227670
31
Y = 2570268
22 feet Y = 783417
75 meter
Z = -13994819
20 Z = -4265620
89
XDOT = -12187
621854 XDOT = -3714
787141
YDOT = -17160
472646 feet/sec YDOT = -5230
512063 meter/sec
ZDOT = 11813
594024 ZDOT = 3600
783458
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 13141
42803078
00016717 00000-0 10270-3 0 9043
2 25544 51
6475 241
0170 0009510 337
5923 22
4812 15
50338774 30557
Satellite: ISS
Catalog Number: 25544
Epoch time: 13141
42803078 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 241
0170 deg
Eccentricity:
0009510
Arg of perigee: 337
5923 deg
Mean anomaly: 22
4812 deg
Mean motion: 15
50338774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3055
Checksum: 284
Coasting Arc #6 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2013/142/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5189835
95 A = 6793726
79 meter
Y = 1953218
37 meter E =
0013457
Z = 3926595
47 I = 51
35253
XDOT = 609
984379 Wp = 36
24267
YDOT = 6491
672945 meter/sec RA = 235
11206 deg
ZDOT = -4017
659778 TA = 96
03130
MA = 95
87793
Ha = 228
396 n
mi
Hp = 220
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17027020
85 X = 5148534
18
Y = 6408196
75 feet Y = 2011023
29 meter
Z = 12882531
06 Z = 3951707
52
XDOT = 2001
261087 XDOT = 556
864878
YDOT = 21298
139584 feet/sec YDOT = 6498
197340 meter/sec
ZDOT = -13181
298485 ZDOT = -4014
825214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17878807
75 X = 5449460
60
Y = -2937594
92 feet Y = -895378
93 meter
Z = 12987024
32 Z = 3958445
01
XDOT = 12252
190173 XDOT = 3734
467565
YDOT = 16088
624054 feet/sec YDOT = 4903
812612 meter/sec
ZDOT = -13170
299234 ZDOT = -4014
307206
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 13142
45936686
00016717 00000-0 10270-3 0 9050
2 25544 51
6479 235
9047 0009426 341
9932 18
0883 15
50351353 30716
Satellite: ISS
Catalog Number: 25544
Epoch time: 13142
45936686 = yrday
fracday
Element set: 905
Inclination: 51
6479 deg
RA of node: 235
9047 deg
Eccentricity:
0009426
Arg of perigee: 341
9932 deg
Mean anomaly: 18
0883 deg
Mean motion: 15
50351353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3071
Checksum: 320
Coasting Arc #7 (Orbit 3085)
---------------------------------------
Vector Time (GMT): 2013/143/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5404632
04 A = 6794641
51 meter
Y = -1973659
77 meter E =
0009003
Z = -3608702
70 I = 51
37473
XDOT = -643
926106 Wp = 19
17650
YDOT = -6245
870242 meter/sec RA = 230
13630 deg
ZDOT = 4391
818463 TA = 297
97105
MA = 298
06213
Ha = 228
477 n
mi
Hp = 220
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17731732
40 X = -5364629
96
Y = -6475261
72 feet Y = -2033873
86 meter
Z = -11839575
79 Z = -3634861
49
XDOT = -2112
618459 XDOT = -595
370332
YDOT = -20491
700268 feet/sec YDOT = -6252
799841 meter/sec
ZDOT = 14408
853226 ZDOT = 4388
807769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18469526
40 X = -5629511
65
Y = 3553905
92 feet Y = 1083230
52 meter
Z = -11948441
34 Z = -3641884
92
XDOT = -12190
709752 XDOT = -3715
728332
YDOT = -15076
114692 feet/sec YDOT = -4595
199758 meter/sec
ZDOT = 14397
086594 ZDOT = 4388
231994
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 13143
42622733
00016717 00000-0 10270-3 0 9064
2 25544 51
6484 231
1128 0009690 345
0887 14
9977 15
50380441 30862
Satellite: ISS
Catalog Number: 25544
Epoch time: 13143
42622733 = yrday
fracday
Element set: 906
Inclination: 51
6484 deg
RA of node: 231
1128 deg
Eccentricity:
0009690
Arg of perigee: 345
0887 deg
Mean anomaly: 14
9977 deg
Mean motion: 15
50380441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3086
Checksum: 310
Coasting Arc #8 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2013/144/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5632799
64 A = 6795691
52 meter
Y = 2012932
38 meter E =
0014052
Z = 3225420
27 I = 51
39872
XDOT = 596
585962 Wp = 51
53492
YDOT = 5977
859758 meter/sec RA = 225
16230 deg
ZDOT = -4749
877508 TA = 91
06992
MA = 90
90892
Ha = 228
639 n
mi
Hp = 220
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18480313
78 X = 5594203
39
Y = 6604108
85 feet Y = 2075705
78 meter
Z = 10582087
51 Z = 3252690
95
XDOT = 1957
303025 XDOT = 552
770024
YDOT = 19612
400780 feet/sec YDOT = 5984
286632 meter/sec
ZDOT = -15583
587624 ZDOT = -4747
085131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19115208
70 X = 5826315
61
Y = -4162908
65 feet Y = -1268854
56 meter
Z = 10695597
94 Z = 3260018
25
XDOT = 11835
187410 XDOT = 3607
365123
YDOT = 14145
316122 feet/sec YDOT = 4311
492354 meter/sec
ZDOT = -15572
696712 ZDOT = -4746
557958
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 13144
45753051
00016717 00000-0 10270-3 0 9077
2 25544 51
6483 226
0010 0009563 349
6912 10
4042 15
50406629 31022
Satellite: ISS
Catalog Number: 25544
Epoch time: 13144
45753051 = yrday
fracday
Element set: 907
Inclination: 51
6483 deg
RA of node: 226
0010 deg
Eccentricity:
0009563
Arg of perigee: 349
6912 deg
Mean anomaly: 10
4042 deg
Mean motion: 15
50406629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3102
Checksum: 273
Coasting Arc #9 (Orbit 3116)
---------------------------------------
Vector Time (GMT): 2013/145/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5844525
16 A = 6796624
30 meter
Y = -1969967
98 meter E =
0012179
Z = -2842032
79 I = 51
42441
XDOT = -523
440333 Wp = 13
98835
YDOT = -5729
525673 meter/sec RA = 220
19045 deg
ZDOT = 5064
007846 TA = 313
64604
MA = 313
74697
Ha = 228
734 n
mi
Hp = 219
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19174951
32 X = -5808256
11
Y = -6463149
55 feet Y = -2035122
01 meter
Z = -9324254
56 Z = -2870337
62
XDOT = -1717
323926 XDOT = -483
932653
YDOT = -18797
656408 feet/sec YDOT = -5735
158827 meter/sec
ZDOT = 16614
198971 ZDOT = 5061
560244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19552996
56 X = -5959753
35
Y = 4991979
51 feet Y = 1521555
35 meter
Z = -9442099
85 Z = -2877952
03
XDOT = -11400
497271 XDOT = -3474
871568
YDOT = -13346
183714 feet/sec YDOT = -4067
916796 meter/sec
ZDOT = 16604
713381 ZDOT = 5061
116638
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 13145
42436068
00016717 00000-0 10270-3 0 9082
2 25544 51
6485 221
2088 0009857 352
6356 7
4648 15
50421409 31175
Satellite: ISS
Catalog Number: 25544
Epoch time: 13145
42436068 = yrday
fracday
Element set: 908
Inclination: 51
6485 deg
RA of node: 221
2088 deg
Eccentricity:
0009857
Arg of perigee: 352
6356 deg
Mean anomaly: 7
4648 deg
Mean motion: 15
50421409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3117
Checksum: 311
Coasting Arc #10 (Orbit 3132)
---------------------------------------
Vector Time (GMT): 2013/146/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6058280
72 A = 6797530
02 meter
Y = 1945012
86 meter E =
0014080
Z = 2390789
71 I = 51
45095
XDOT = 364
925128 Wp = 65
26168
YDOT = 5471
565652 meter/sec RA = 215
22107 deg
ZDOT = -5345
446955 TA = 88
01116
MA = 87
84991
Ha = 228
871 n
mi
Hp = 219
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19876249
07 X = 6024466
95
Y = 6381275
79 feet Y = 2012570
99 meter
Z = 7843798
26 Z = 2420138
78
XDOT = 1197
260918 XDOT = 329
680824
YDOT = 17951
330880 feet/sec YDOT = 5475
450129 meter/sec
ZDOT = -17537
555628 ZDOT = -5343
759035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20007451
15 X = 6098271
11
Y = -5792712
93 feet Y = -1765618
90 meter
Z = 7966021
85 Z = 2428043
46
XDOT = 10694
837580 XDOT = 3259
786494
YDOT = 12694
238989 feet/sec YDOT = 3869
204044 meter/sec
ZDOT = -17531
204373 ZDOT = -5343
511093
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 13146
45563160
00016717 00000-0 10270-3 0 9091
2 25544 51
6477 216
0969 0009712 357
3892 2
7207 15
50459868 31330
Satellite: ISS
Catalog Number: 25544
Epoch time: 13146
45563160 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 216
0969 deg
Eccentricity:
0009712
Arg of perigee: 357
3892 deg
Mean anomaly: 2
7207 deg
Mean motion: 15
50459868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3133
Checksum: 325
Coasting Arc #11 (Orbit 3147)
---------------------------------------
Vector Time (GMT): 2013/147/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6237745
66 A = 6798335
33 meter
Y = -1840947
18 meter E =
0015809
Z = -1950318
30 I = 51
47932
XDOT = -186
839169 Wp = 16
52531
YDOT = -5252
572006 meter/sec RA = 210
25331 deg
ZDOT = 5581
569556 TA = 321
93572
MA = 322
04731
Ha = 228
978 n
mi
Hp = 219
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20465044
80 X = -6207222
01
Y = -6039852
94 feet Y = -1910530
65 meter
Z = -6398682
08 Z = -1980547
00
XDOT = -612
989401 XDOT = -155
203813
YDOT = -17232
847789 feet/sec YDOT = -5254
485219 meter/sec
ZDOT = 18312
236077 ZDOT = 5580
738045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20198846
03 X = -6156608
27
Y = 6758483
84 feet Y = 2059985
87 meter
Z = -6524609
55 Z = -1988700
99
XDOT = -9979
526903 XDOT = -3041
759800
YDOT = -12230
334661 feet/sec YDOT = -3727
806005 meter/sec
ZDOT = 18309
427131 ZDOT = 5580
713389
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 13147
42243195
00016717 00000-0 10270-3 0 9104
2 25544 51
6478 211
3041 0010005
2129 359
9024 15
50462186 31481
Satellite: ISS
Catalog Number: 25544
Epoch time: 13147
42243195 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 211
3041 deg
Eccentricity:
0010005
Arg of perigee:
2129 deg
Mean anomaly: 359
9024 deg
Mean motion: 15
50462186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3148
Checksum: 269
Coasting Arc #12 (Orbit 3163)
---------------------------------------
Vector Time (GMT): 2013/148/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6406913
59 A = 6798931
53 meter
Y = 1758042
49 meter E =
0013404
Z = 1442747
77 I = 51
50767
XDOT = -72
791893 Wp = 76
36237
YDOT = 5037
301241 meter/sec RA = 205
28835 deg
ZDOT = -5766
559116 TA = 87
90597
MA = 87
75249
Ha = 229
084 n
mi
Hp = 219
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21020057
71 X = 6379770
11
Y = 5767855
93 feet Y = 1829536
69 meter
Z = 4733424
46 Z = 1473806
33
XDOT = -238
818545 XDOT = -101
102233
YDOT = 16526
578874 feet/sec YDOT = 5036
329639 meter/sec
ZDOT = -18919
157206 ZDOT = -5766
980891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20377366
38 X = 6211021
27
Y = -7657151
09 feet Y = -2333899
65 meter
Z = 4862846
08 Z = 1482195
49
XDOT = 9046
977540 XDOT = 2757
518754
YDOT = 11961
427439 feet/sec YDOT = 3645
843083 meter/sec
ZDOT = -18921
547671 ZDOT = -5767
287730
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 13148
45367131
00016717 00000-0 10270-3 0 9116
2 25544 51
6467 206
1917 0009878 4
9334 355
1913 15
50512847 31641
Satellite: ISS
Catalog Number: 25544
Epoch time: 13148
45367131 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 206
1917 deg
Eccentricity:
0009878
Arg of perigee: 4
9334 deg
Mean anomaly: 355
1913 deg
Mean motion: 15
50512847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3164
Checksum: 311
Coasting Arc #13 (Orbit 3178)
---------------------------------------
Vector Time (GMT): 2013/149/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6526036
84 A = 6799469
23 meter
Y = -1605879
20 meter E =
0019155
Z = -957852
29 I = 51
53779
XDOT = 341
677479 Wp = 23
34409
YDOT = -4877
792635 meter/sec RA = 200
32489 deg
ZDOT = 5907
616144 TA = 326
27476
MA = 326
39648
Ha = 229
210 n
mi
Hp = 218
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21410882
02 X = -6502941
53
Y = -5268632
55 feet Y = -1678728
23 meter
Z = -3142560
02 Z = -989499
26
XDOT = 1120
989105 XDOT = 367
499014
YDOT = -16003
256676 feet/sec YDOT = -4873
828006 meter/sec
ZDOT = 19381
942730 ZDOT = 5909
338206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20262701
76 X = -6176071
50
Y = 8646430
89 feet Y = 2635432
14 meter
Z = -3274475
73 Z = -998060
20
XDOT = -8187
433160 XDOT = -2495
529627
YDOT = -11912
811064 feet/sec YDOT = -3631
024812 meter/sec
ZDOT = 19389
737059 ZDOT = 5909
991855
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 13149
42044254
00016717 00000-0 10270-3 0 9123
2 25544 51
6471 201
3984 0010142 7
7825 352
3481 15
50503395 31792
Satellite: ISS
Catalog Number: 25544
Epoch time: 13149
42044254 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 201
3984 deg
Eccentricity:
0010142
Arg of perigee: 7
7825 deg
Mean anomaly: 352
3481 deg
Mean motion: 15
50503395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3179
Checksum: 289
Coasting Arc #14 (Orbit 3194)
---------------------------------------
Vector Time (GMT): 2013/150/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6623736
94 A = 6799610
99 meter
Y = 1482340
78 meter E =
0012065
Z = 410355
14 I = 51
56720
XDOT = -679
447209 Wp = 82
99193
YDOT = 4733
523962 meter/sec RA = 195
36425 deg
ZDOT = -5978
877497 TA = 92
58975
MA = 92
45163
Ha = 229
277 n
mi
Hp = 218
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21731420
39 X = 6604675
39
Y = 4863322
78 feet Y = 1556304
97 meter
Z = 1346309
50 Z = 442486
49
XDOT = -2229
157509 XDOT = -703
284221
YDOT = 15529
934258 feet/sec YDOT = 4725
793169 meter/sec
ZDOT = -19615
739821 ZDOT = -5982
235700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20123314
31 X = 6133586
20
Y = -9517356
96 feet Y = -2900890
40 meter
Z = 1480279
54 Z = 451189
20
XDOT = 7189
079839 XDOT = 2191
231535
YDOT = 12076
278084 feet/sec YDOT = 3680
849560 meter/sec
ZDOT = -19630
344137 ZDOT = -5983
328893
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 13150
45165107
00016717 00000-0 10270-3 0 9130
2 25544 51
6464 196
2855 0010063 12
3297 347
8099 15
50566554 31958
Satellite: ISS
Catalog Number: 25544
Epoch time: 13150
45165107 = yrday
fracday
Element set: 913
Inclination: 51
6464 deg
RA of node: 196
2855 deg
Eccentricity:
0010063
Arg of perigee: 12
3297 deg
Mean anomaly: 347
8099 deg
Mean motion: 15
50566554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3195
Checksum: 312
Coasting Arc #15 (Orbit 3210)
---------------------------------------
Vector Time (GMT): 2013/151/10:02:39
122
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6659716
09 A = 6799765
33 meter
Y = -1305212
89 meter E =
0021688
Z = 102128
31 I = 51
59758
XDOT = 1013
770192 Wp = 32
59173
YDOT = -4657
299486 meter/sec RA = 190
40516 deg
ZDOT = 6009
905909 TA = 328
50847
MA = 328
63812
Ha = 229
433 n
mi
Hp = 218
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21849462
23 X = -6645122
06
Y = -4282194
52 feet Y = -1379604
44 meter
Z = 335066
63 Z = 69811
29
XDOT = 3326
017690 XDOT = 1036
579213
YDOT = -15279
853956 feet/sec YDOT = -4645
835747 meter/sec
ZDOT = 19717
539071 ZDOT = 6014
885808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19691411
82 X = -6001942
32
Y = 10395029
85 feet Y = 3168405
10 meter
Z = 200284
94 Z = 61046
85
XDOT = -6346
870157 XDOT = -1934
526024
YDOT = -12464
220192 feet/sec YDOT = -3799
094314 meter/sec
ZDOT = 19738
904204 ZDOT = 6016
418001
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 13151
48284461
00016717 00000-0 10270-3 0 9140
2 25544 51
6468 191
1724 0010284 15
6823 344
4645 15
50547814 32114
Satellite: ISS
Catalog Number: 25544
Epoch time: 13151
48284461 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 191
1724 deg
Eccentricity:
0010284
Arg of perigee: 15
6823 deg
Mean anomaly: 344
4645 deg
Mean motion: 15
50547814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3211
Checksum: 298
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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