[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 16th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 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
137/02:28:32
012 1
7 4
7 4
7
N/A -2
7 -0
5 227
8
000/00:15:04
024 3
4 0
1 221
9
Coasting Arc #1 (Orbit 2960)
---------------------------------------
Vector Time (GMT): 2013/135/08:02:13
842
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 997042
69 A = 6797144
62 meter
Y = 6592587
28 meter E =
0008097
Z = 1303957
37 I = 51
31043
XDOT = -4654
832763 Wp = 112
30014
YDOT = 1855
435147 meter/sec RA = 270
41074 deg
ZDOT = -5795
590532 TA = 53
46516
MA = 53
39063
Ha = 225
072 n
mi
Hp = 220
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3271137
44 X = 916914
53
Y = 21629223
37 feet Y = 6603288
74 meter
Z = 4278075
35 Z = 1308606
72
XDOT = -15271
761034 XDOT = -4647
081025
YDOT = 6087
385654 feet/sec YDOT = 1803
425568 meter/sec
ZDOT = -19014
404633 ZDOT = -5818
184547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 569080
67 X = 173455
79
Y = 21864153
77 feet Y = 6664194
07 meter
Z = 4296568
32 Z = 1309594
02
XDOT = -14191
310088 XDOT = -4325
511315
YDOT = 4141
155817 feet/sec YDOT = 1262
224293 meter/sec
ZDOT = -19108
861363 ZDOT = -5824
380943
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 13135
36966328
00016717 00000-0 10270-3 0 9003
2 25544 51
6469 271
0566 0005863 312
0615 48
0037 15
51195007 29614
Satellite: ISS
Catalog Number: 25544
Epoch time: 13135
36966328 = yrday
fracday
Element set: 900
Inclination: 51
6469 deg
RA of node: 271
0566 deg
Eccentricity:
0005863
Arg of perigee: 312
0615 deg
Mean anomaly: 48
0037 deg
Mean motion: 15
51195007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2961
Checksum: 301
Coasting Arc #2 (Orbit 2975)
---------------------------------------
Vector Time (GMT): 2013/136/08:02:13
842
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1009963
87 A = 6797781
18 meter
Y = -6688151
49 meter E =
0012520
Z = -591552
30 I = 51
31168
XDOT = 4679
387801 Wp = 13
85865
YDOT = -1229
254150 meter/sec RA = 265
42884 deg
ZDOT = 5947
020807 TA = 339
73280
MA = 339
78245
Ha = 225
133 n
mi
Hp = 220
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3313529
74 X = -932226
83
Y = -21942754
23 feet Y = -6699010
86 meter
Z = -1940788
37 Z = -596270
17
XDOT = 15352
322183 XDOT = 4663
896571
YDOT = -4032
986055 feet/sec YDOT = -1177
013207 meter/sec
ZDOT = 19511
223119 ZDOT = 5969
715330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -968552
07 X = -295214
67
Y = -22168730
49 feet Y = -6757029
05 meter
Z = -1959565
67 Z = -597275
62
XDOT = 13955
169989 XDOT = 4253
535813
YDOT = -2331
792428 feet/sec YDOT = -710
730332 meter/sec
ZDOT = 19606
017208 ZDOT = 5975
914045
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 13136
33603723
00016717 00000-0 10270-3 0 9019
2 25544 51
6455 266
2596 0005712 314
6114 45
4570 15
51174051 29768
Satellite: ISS
Catalog Number: 25544
Epoch time: 13136
33603723 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 266
2596 deg
Eccentricity:
0005712
Arg of perigee: 314
6114 deg
Mean anomaly: 45
4570 deg
Mean motion: 15
51174051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2976
Checksum: 291
Coasting Arc #3 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2013/137/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1290624
14 A = 6800537
59 meter
Y = -6655317
30 meter E =
0016110
Z = -376760
53 I = 51
31835
XDOT = 4649
345337 Wp = 6
43375
YDOT = -1237
338798 meter/sec RA = 261
57542 deg
ZDOT = 5970
902765 TA = 349
49006
MA = 349
52370
Ha = 227
819 n
mi
Hp = 221
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4234331
17 X = -1214276
82
Y = -21835030
50 feet Y = -6669322
97 meter
Z = -1236090
99 Z = -382845
15
XDOT = 15253
757667 XDOT = 4633
830738
YDOT = -4059
510492 feet/sec YDOT = -1185
433889 meter/sec
ZDOT = 19589
576002 ZDOT = 5993
451292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21568299
21 X = 6574017
60
Y = -5426365
53 feet Y = -1653956
21 meter
Z = -1260580
98 Z = -384225
08
XDOT = 4492
067725 XDOT = 1369
182243
YDOT = 13312
355366 feet/sec YDOT = 4057
605916 meter/sec
ZDOT = 19683
764477 ZDOT = 5999
611412
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
10912272
00016717 00000-0 10270-3 0 9028
2 25544 51
6495 262
4250 0009644 322
8834 37
1649 15
50260753 29887
Satellite: ISS
Catalog Number: 25544
Epoch time: 13137
10912272 = yrday
fracday
Element set: 902
Inclination: 51
6495 deg
RA of node: 262
4250 deg
Eccentricity:
0009644
Arg of perigee: 322
8834 deg
Mean anomaly: 37
1649 deg
Mean motion: 15
50260753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2988
Checksum: 309
Coasting Arc #4 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2013/138/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1521470
86 A = 6800540
99 meter
Y = 6627473
59 meter E =
0003180
Z = -69803
01 I = 51
32418
XDOT = -4676
632841 Wp = 98
95550
YDOT = 1013
139506 meter/sec RA = 256
59982 deg
ZDOT = -5976
709970 TA = 81
79786
MA = 81
76179
Ha = 227
975 n
mi
Hp = 221
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4991702
30 X = 1447587
03
Y = 21743679
75 feet Y = 6644074
53 meter
Z = -229012
50 Z = -62591
03
XDOT = -15343
283600 XDOT = -4658
580934
YDOT = 3323
948509 feet/sec YDOT = 960
943571 meter/sec
ZDOT = -19608
628510 ZDOT = -5999
384934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21325051
73 X = -6499875
77
Y = 6554341
62 feet Y = 1997763
33 meter
Z = -199805
96 Z = -60900
86
XDOT = -3937
976939 XDOT = -1200
295371
YDOT = -13386
243565 feet/sec YDOT = -4080
127039 meter/sec
ZDOT = -19703
317281 ZDOT = -6005
571107
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
14051004
00016717 00000-0 10270-3 0 9031
2 25544 51
6497 257
3136 0009573 326
3098 33
7443 15
50276649 30042
Satellite: ISS
Catalog Number: 25544
Epoch time: 13138
14051004 = yrday
fracday
Element set: 903
Inclination: 51
6497 deg
RA of node: 257
3136 deg
Eccentricity:
0009573
Arg of perigee: 326
3098 deg
Mean anomaly: 33
7443 deg
Mean motion: 15
50276649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 297
Coasting Arc #5 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2013/139/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1741464
45 A = 6800318
05 meter
Y = -6541478
64 meter E =
0017535
Z = 511797
17 I = 51
33189
XDOT = 4760
334165 Wp = 17
13631
YDOT = -798
205190 meter/sec RA = 251
62390 deg
ZDOT = 5959
766814 TA = 348
40468
MA = 348
44502
Ha = 228
103 n
mi
Hp = 221
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5713466
06 X = -1670673
00
Y = -21461544
09 feet Y = -6560556
99 meter
Z = 1679124
58 Z = 503509
01
XDOT = 15617
894242 XDOT = 4739
954838
YDOT = -2618
783432 feet/sec YDOT = -745
086211 meter/sec
ZDOT = 19553
040729 ZDOT = 5982
842806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20862604
28 X = 6358921
79
Y = -7622690
02 feet Y = -2323395
92 meter
Z = 1645408
06 Z = 501520
38
XDOT = 3438
723315 XDOT = 1048
122866
YDOT = 13678
786290 feet/sec YDOT = 4169
294061 meter/sec
ZDOT = 19649
376665 ZDOT = 5989
130007
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
17187670
00016717 00000-0 10270-3 0 9045
2 25544 51
6498 252
2015 0009813 330
6957 29
3642 15
50322162 30204
Satellite: ISS
Catalog Number: 25544
Epoch time: 13139
17187670 = yrday
fracday
Element set: 904
Inclination: 51
6498 deg
RA of node: 252
2015 deg
Eccentricity:
0009813
Arg of perigee: 330
6957 deg
Mean anomaly: 29
3642 deg
Mean motion: 15
50322162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 293
Coasting Arc #6 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2013/140/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1934735
34 A = 6800001
19 meter
Y = 6446791
56 meter E =
0002097
Z = -973798
16 I = 51
34172
XDOT = -4871
902261 Wp = 60
07156
YDOT = 575
709874 meter/sec RA = 246
64904 deg
ZDOT = -5876
640356 TA = 130
49419
MA = 130
47592
Ha = 228
239 n
mi
Hp = 221
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6347556
87 X = 1867232
64
Y = 21150890
95 feet Y = 6468049
58 meter
Z = -3194875
86 Z = -964563
11
XDOT = -15983
931301 XDOT = -4849
430369
YDOT = 1888
811924 feet/sec YDOT = 521
354944 meter/sec
ZDOT = -19280
316127 ZDOT = -5900
253340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20350764
53 X = -6202913
03
Y = 8587050
66 feet Y = 2617333
04 meter
Z = -3157188
94 Z = -962311
19
XDOT = -2942
709983 XDOT = -896
938003
YDOT = -14088
630209 feet/sec YDOT = -4294
214488 meter/sec
ZDOT = -19378
866145 ZDOT = -5906
678401
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
13876549
00016717 00000-0 10270-3 0 9054
2 25544 51
6500 247
4094 0009731 333
5234 26
5419 15
50328128 30355
Satellite: ISS
Catalog Number: 25544
Epoch time: 13140
13876549 = yrday
fracday
Element set: 905
Inclination: 51
6500 deg
RA of node: 247
4094 deg
Eccentricity:
0009731
Arg of perigee: 333
5234 deg
Mean anomaly: 26
5419 deg
Mean motion: 15
50328128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 293
Coasting Arc #7 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2013/141/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2100682
24 A = 6799410
20 meter
Y = -6295321
46 meter E =
0018020
Z = 1423078
61 I = 51
35326
XDOT = 5039
628594 Wp = 27
50676
YDOT = -374
284830 meter/sec RA = 241
67374 deg
ZDOT = 5769
919606 TA = 348
06541
MA = 348
10806
Ha = 228
375 n
mi
Hp = 220
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6892002
10 X = -2037043
52
Y = -20653941
80 feet Y = -6318456
82 meter
Z = 4668893
09 Z = 1413027
95
XDOT = 16534
214548 XDOT = 5015
410183
YDOT = -1227
968601 feet/sec YDOT = -318
064064 meter/sec
ZDOT = 18930
182434 ZDOT = 5794
343251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19638298
36 X = 5985753
34
Y = -9423612
73 feet Y = -2872317
16 meter
Z = 4627777
90 Z = 1410546
71
XDOT = 2561
678935 XDOT = 780
799740
YDOT = 14706
860817 feet/sec YDOT = 4482
651177 meter/sec
ZDOT = 19032
091834 ZDOT = 5800
981591
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
17009418
00016717 00000-0 10270-3 0 9063
2 25544 51
6501 242
2969 0009998 338
0117 22
0604 15
50381410 30513
Satellite: ISS
Catalog Number: 25544
Epoch time: 13141
17009418 = yrday
fracday
Element set: 906
Inclination: 51
6501 deg
RA of node: 242
2969 deg
Eccentricity:
0009998
Arg of perigee: 338
0117 deg
Mean anomaly: 22
0604 deg
Mean motion: 15
50381410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 280
Coasting Arc #8 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2013/142/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2232222
18 A = 6798746
84 meter
Y = 6142035
46 meter E =
0003997
Z = -1884792
91 I = 51
36659
XDOT = -5224
981420 Wp = 17
61283
YDOT = 183
366355 meter/sec RA = 236
69999 deg
ZDOT = -5589
965537 TA = 183
16535
MA = 183
16788
Ha = 228
486 n
mi
Hp = 220
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7323563
59 X = 2172530
72
Y = 20151034
98 feet Y = 6166663
89 meter
Z = -6183703
76 Z = -1874093
52
XDOT = -17142
327494 XDOT = -5199
488432
YDOT = 601
595654 feet/sec YDOT = 125
080061 meter/sec
ZDOT = -18339
781945 ZDOT = -5615
286617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18913197
48 X = -5764742
59
Y = 10125714
44 feet Y = 3086317
76 meter
Z = -6139857
88 Z = -1871428
68
XDOT = -2253
659648 XDOT = -686
915461
YDOT = -15395
310053 feet/sec YDOT = -4692
490504 meter/sec
ZDOT = -18445
415811 ZDOT = -5622
162739
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
13694788
00016717 00000-0 10270-3 0 9071
2 25544 51
6502 237
5049 0009922 340
6682 19
4092 15
50386326 30661
Satellite: ISS
Catalog Number: 25544
Epoch time: 13142
13694788 = yrday
fracday
Element set: 907
Inclination: 51
6502 deg
RA of node: 237
5049 deg
Eccentricity:
0009922
Arg of perigee: 340
6682 deg
Mean anomaly: 19
4092 deg
Mean motion: 15
50386326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 316
Coasting Arc #9 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2013/143/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2320111
91 A = 6797828
94 meter
Y = -5938450
91 meter E =
0017456
Z = 2324710
51 I = 51
38132
XDOT = 5462
012913 Wp = 37
30348
YDOT = -22
735133 meter/sec RA = 231
72560 deg
ZDOT = 5385
486532 TA = 348
70125
MA = 348
74039
Ha = 228
627 n
mi
Hp = 220
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7611915
72 X = -2264827
51
Y = -19483106
65 feet Y = -5964086
89 meter
Z = 7627002
99 Z = 2313573
29
XDOT = 17919
989871 XDOT = 5435
699363
YDOT = -74
590333 feet/sec YDOT = 38
197087 meter/sec
ZDOT = 17668
919067 ZDOT = 5411
957182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18029640
51 X = 5495434
43
Y = -10637660
61 feet Y = -3242358
95 meter
Z = 7581300
70 Z = 2310780
45
XDOT = 2107
455032 XDOT = 642
352294
YDOT = 16260
948142 feet/sec YDOT = 4956
336994 meter/sec
ZDOT = 17779
335458 ZDOT = 5419
141448
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
16823990
00016717 00000-0 10270-3 0 9085
2 25544 51
6499 232
3920 0010165 345
0844 15
0006 15
50437045 30827
Satellite: ISS
Catalog Number: 25544
Epoch time: 13143
16823990 = yrday
fracday
Element set: 908
Inclination: 51
6499 deg
RA of node: 232
3920 deg
Eccentricity:
0010165
Arg of perigee: 345
0844 deg
Mean anomaly: 15
0006 deg
Mean motion: 15
50437045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 286
Coasting Arc #10 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2013/144/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2369100
91 A = 6796844
07 meter
Y = 5743803
45 meter E =
0007582
Z = -2767746
47 I = 51
39733
XDOT = -5699
679454 Wp = 15
05270
YDOT = -110
959828 meter/sec RA = 226
75294 deg
ZDOT = -5105
000027 TA = 196
32582
MA = 196
35026
Ha = 228
710 n
mi
Hp = 220
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7772640
77 X = 2318141
64
Y = 18844499
51 feet Y = 5770011
55 meter
Z = -9080533
02 Z = -2756360
60
XDOT = -18699
735742 XDOT = -5673
215800
YDOT = -364
041432 feet/sec YDOT = -174
548818 meter/sec
ZDOT = -16748
687754 ZDOT = -5132
624907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17185440
07 X = -5238122
13
Y = 11001678
79 feet Y = 3353311
69 meter
Z = -9033764
43 Z = -2753491
40
XDOT = -2088
269222 XDOT = -636
504459
YDOT = -17120
290514 feet/sec YDOT = -5218
264549 meter/sec
ZDOT = -16863
912909 ZDOT = -5140
120655
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
13505928
00016717 00000-0 10270-3 0 9092
2 25544 51
6493 227
6000 0010106 347
9021 12
1885 15
50450630 30974
Satellite: ISS
Catalog Number: 25544
Epoch time: 13144
13505928 = yrday
fracday
Element set: 909
Inclination: 51
6493 deg
RA of node: 227
6000 deg
Eccentricity:
0010106
Arg of perigee: 347
9021 deg
Mean anomaly: 12
1885 deg
Mean motion: 15
50450630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 280
Coasting Arc #11 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2013/145/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2360084
55 A = 6795699
99 meter
Y = -5510006
07 meter E =
0015910
Z = 3179053
53 I = 51
41486
XDOT = 5980
701686 Wp = 45
92740
YDOT = 209
293286 meter/sec RA = 221
77942 deg
ZDOT = 4798
627136 TA = 350
89949
MA = 350
92829
Ha = 228
853 n
mi
Hp = 219
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7743059
54 X = -2313738
34
Y = -18077447
72 feet Y = -5536139
25 meter
Z = 10429965
64 Z = 3167700
17
XDOT = 19621
724691 XDOT = 5954
605942
YDOT = 686
657764 feet/sec YDOT = 276
026802 meter/sec
ZDOT = 15743
527348 ZDOT = 4827
618046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16244793
62 X = 4951413
10
Y = -11127762
00 feet Y = -3391741
86 meter
Z = 10383297
34 Z = 3164829
03
XDOT = 2256
058200 XDOT = 687
646539
YDOT = 18109
237775 feet/sec YDOT = 5519
695674 meter/sec
ZDOT = 15864
453238 ZDOT = 4835
485347
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
16631571
00016717 00000-0 10270-3 0 9102
2 25544 51
6487 222
4868 0010286 352
0699 8
0288 15
50487319 31133
Satellite: ISS
Catalog Number: 25544
Epoch time: 13145
16631571 = yrday
fracday
Element set: 910
Inclination: 51
6487 deg
RA of node: 222
4868 deg
Eccentricity:
0010286
Arg of perigee: 352
0699 deg
Mean anomaly: 8
0288 deg
Mean motion: 15
50487319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 309
Coasting Arc #12 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2013/146/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2312633
12 A = 6794489
28 meter
Y = 5298899
00 meter E =
0011604
Z = -3583189
45 I = 51
43319
XDOT = -6240
021714 Wp = 22
43067
YDOT = -268
690289 meter/sec RA = 216
80738 deg
ZDOT = -4418
979350 TA = 199
92645
MA = 199
97180
Ha = 228
907 n
mi
Hp = 219
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7587379
01 X = 2270614
22
Y = 17384839
23 feet Y = 5324525
85 meter
Z = -11755870
89 Z = -3572056
09
XDOT = -20472
512184 XDOT = -6215
086884
YDOT = -881
529821 feet/sec YDOT = -338
330145 meter/sec
ZDOT = -14497
963748 ZDOT = -4449
232709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15404251
82 X = -4695215
96
Y = 11116850
45 feet Y = 3388416
02 meter
Z = -11710086
15 Z = -3569234
26
XDOT = -2576
812542 XDOT = -785
412463
YDOT = -18995
119076 feet/sec YDOT = -5789
712294 meter/sec
ZDOT = -14624
166986 ZDOT = -4457
446097
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
13310143
00016717 00000-0 10270-3 0 9110
2 25544 51
6473 217
6941 0010230 355
3629 4
7425 15
50515144 31284
Satellite: ISS
Catalog Number: 25544
Epoch time: 13146
13310143 = yrday
fracday
Element set: 911
Inclination: 51
6473 deg
RA of node: 217
6941 deg
Eccentricity:
0010230
Arg of perigee: 355
3629 deg
Mean anomaly: 4
7425 deg
Mean motion: 15
50515144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 268
Coasting Arc #13 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2013/147/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2196533
99 A = 6793261
07 meter
Y = -5063256
52 meter E =
0013682
Z = 3944768
22 I = 51
45376
XDOT = 6531
326101 Wp = 52
11184
YDOT = 292
946544 meter/sec RA = 211
83457 deg
ZDOT = 4011
511015 TA = 355
91710
MA = 355
92825
Ha = 229
050 n
mi
Hp = 219
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7206476
34 X = -2158915
08
Y = -16611734
00 feet Y = -5087609
74 meter
Z = 12942152
94 Z = 3934188
26
XDOT = 21428
235238 XDOT = 6508
077896
YDOT = 961
110710 feet/sec YDOT = 365
853421 meter/sec
ZDOT = 13161
125378 ZDOT = 4043
183437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14541613
17 X = 4432283
69
Y = -10841999
16 feet Y = -3304641
34 meter
Z = 12898638
35 Z = 3931504
97
XDOT = 3082
200449 XDOT = 939
454697
YDOT = 19953
856567 feet/sec YDOT = 6081
935482 meter/sec
ZDOT = 13293
266836 ZDOT = 4051
787732
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
16432297
00016717 00000-0 10270-3 0 9120
2 25544 51
6467 212
5804 0010342 359
2315
8819 15
50532546 31445
Satellite: ISS
Catalog Number: 25544
Epoch time: 13147
16432297 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 212
5804 deg
Eccentricity:
0010342
Arg of perigee: 359
2315 deg
Mean anomaly:
8819 deg
Mean motion: 15
50532546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 289
Coasting Arc #14 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2013/148/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2048861
21 A = 6791987
34 meter
Y = 4865414
44 meter E =
0015491
Z = -4288880
00 I = 51
47499
XDOT = -6775
874411 Wp = 32
69744
YDOT = -272
958207 meter/sec RA = 206
86304 deg
ZDOT = -3539
838845 TA = 201
00789
MA = 201
07159
Ha = 229
072 n
mi
Hp = 218
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6721985
59 X = 2015137
10
Y = 15962645
81 feet Y = 4888138
08 meter
Z = -14071128
59 Z = -4279008
08
XDOT = -22230
559090 XDOT = -6755
122902
YDOT = -895
532175 feet/sec YDOT = -348
613834 meter/sec
ZDOT = -11613
644506 ZDOT = -3572
705170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13838680
72 X = -4218029
88
Y = 10470092
80 feet Y = 3191284
29 meter
Z = -14030533
99 Z = -4276506
76
XDOT = -3730
489268 XDOT = -1137
053129
YDOT = -20707
209517 feet/sec YDOT = -6311
557461 meter/sec
ZDOT = -11750
791520 ZDOT = -3581
641255
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
13107580
00016717 00000-0 10270-3 0 9133
2 25544 51
6453 207
7869 0010266 3
0935 357
0278 15
50574209 31598
Satellite: ISS
Catalog Number: 25544
Epoch time: 13148
13107580 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 207
7869 deg
Eccentricity:
0010266
Arg of perigee: 3
0935 deg
Mean anomaly: 357
0278 deg
Mean motion: 15
50574209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 305
Coasting Arc #15 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2013/149/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1826942
06 A = 6790845
70 meter
Y = -4659326
52 meter E =
0011376
Z = 4578675
96 I = 51
49889
XDOT = 7039
163494 Wp = 53
48637
YDOT = 224
016725 meter/sec RA = 201
89127 deg
ZDOT = 3038
041655 TA = 6
11451
MA = 6
10064
Ha = 229
214 n
mi
Hp = 218
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5993904
41 X = -1796946
66
Y = -15286504
34 feet Y = -4679589
32 meter
Z = 15021902
76 Z = 4569873
19
XDOT = 23094
368418 XDOT = 7021
377334
YDOT = 734
963008 feet/sec YDOT = 302
633313 meter/sec
ZDOT = 9967
328263 ZDOT = 3072
194118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13190185
36 X = 4020368
50
Y = -9834043
52 feet Y = -2997416
46 meter
Z = 14985735
41 Z = 4567652
15
XDOT = 4531
092934 XDOT = 1381
077126
YDOT = 21476
618256 feet/sec YDOT = 6546
073244 meter/sec
ZDOT = 10109
869341 ZDOT = 3081
488175
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
16226306
00016717 00000-0 10270-3 0 9146
2 25544 51
6452 202
6727 0010336 6
7630 353
3658 15
50574623 31753
Satellite: ISS
Catalog Number: 25544
Epoch time: 13149
16226306 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 202
6727 deg
Eccentricity:
0010336
Arg of perigee: 6
7630 deg
Mean anomaly: 353
3658 deg
Mean motion: 15
50574623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 293
Coasting Arc #16 (Orbit 3189)
---------------------------------------
Vector Time (GMT): 2013/150/02:36:04
024
Vector Time (MET): N/A
Weight (LBS) : 880022
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1587313
43 A = 6789705
48 meter
Y = 4505227
01 meter E =
0018742
Z = -4841930
64 I = 51
52363
XDOT = -7231
631294 Wp = 43
86877
YDOT = -133
546974 meter/sec RA = 196
92107 deg
ZDOT = -2487
573088 TA = 201
54505
MA = 201
62402
Ha = 229
210 n
mi
Hp = 218
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5207721
24 X = 1560337
83
Y = 14780928
50 feet Y = 4522826
95 meter
Z = -15885599
21 Z = -4834284
74
XDOT = -23725
824457 XDOT = -7217
516515
YDOT = -438
146239 feet/sec YDOT = -214
336495 meter/sec
ZDOT = -8161
329030 ZDOT = -2522
669433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12747929
91 X = -3885569
04
Y = 9169624
60 feet Y = 2794901
58 meter
Z = -15854234
07 Z = -4832370
54
XDOT = -5427
127552 XDOT = -1654
188478
YDOT = -21951
297699 feet/sec YDOT = -6690
755539 meter/sec
ZDOT = -8307
839462 ZDOT = -2532
229468
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
12898374
00016717 00000-0 10270-3 0 9155
2 25544 51
6445 197
8788 0010239 11
0520 349
0854 15
50627868 31903
Satellite: ISS
Catalog Number: 25544
Epoch time: 13150
12898374 = yrday
fracday
Element set: 915
Inclination: 51
6445 deg
RA of node: 197
8788 deg
Eccentricity:
0010239
Arg of perigee: 11
0520 deg
Mean anomaly: 349
0854 deg
Mean motion: 15
50627868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3190
Checksum: 322
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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