[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 5th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
128/06:37:46
186 2
8 4
1 4
1
N/A -0
8 -0
4 223
9
000/00:13:32
372 2
9 0
1 222
7
137/01:53:25
082 -3
0 4
5 4
5
N/A -0
4 -0
2 226
1
000/00:14:50
164 -3
3 -0
1 223
7
Coasting Arc #1 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2013/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2636907
51 A = 6784314
20 meter
Y = -3339065
48 meter E =
0008498
Z = -5290964
55 I = 51
44918
XDOT = 6364
575111 Wp = 111
67532
YDOT = -4230
898640 meter/sec RA = 329
40789 deg
ZDOT = -505
631651 TA = 153
50413
MA = 153
46066
Ha = 224
054 n
mi
Hp = 220
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8651271
35 X = -2573671
16
Y = -10954939
23 feet Y = -3368199
57 meter
Z = -17358807
58 Z = -5303620
82
XDOT = 20881
151940 XDOT = 6413
869132
YDOT = -13880
901049 feet/sec YDOT = -4159
450340 meter/sec
ZDOT = -1658
896493 ZDOT = -474
593131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13623741
55 X = -4152516
42
Y = -2725941
99 feet Y = -830867
12 meter
Z = -17411096
94 Z = -5306902
35
XDOT = 6571
867460 XDOT = 2003
105202
YDOT = -23157
622507 feet/sec YDOT = -7058
443340 meter/sec
ZDOT = -1528
879504 ZDOT = -466
002473
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 13123
51690732
00016717 00000-0 10270-3 0 9000
2 25544 51
6460 329
8880 0007989 239
0217 121
0150 15
51764260 27779
Satellite: ISS
Catalog Number: 25544
Epoch time: 13123
51690732 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 329
8880 deg
Eccentricity:
0007989
Arg of perigee: 239
0217 deg
Mean anomaly: 121
0150 deg
Mean motion: 15
51764260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 303
Coasting Arc #2 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2013/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1955466
45 A = 6784379
94 meter
Y = 3783691
19 meter E =
0005175
Z = 5284569
81 I = 51
42363
XDOT = -6456
954351 Wp = 240
18319
YDOT = 4088
743966 meter/sec RA = 324
41930 deg
ZDOT = -541
127092 TA = 214
98305
MA = 215
01706
Ha = 223
888 n
mi
Hp = 221
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6415572
34 X = 1887339
83
Y = 12413684
99 feet Y = 3805177
68 meter
Z = 17337827
46 Z = 5293903
78
XDOT = -21184
233436 XDOT = -6499
566995
YDOT = 13414
514324 feet/sec YDOT = 4016
299955 meter/sec
ZDOT = -1775
351351 ZDOT = -572
598286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12970918
09 X = 3953535
83
Y = 5067767
37 feet Y = 1544655
49 meter
Z = 17376202
76 Z = 5296266
60
XDOT = -6505
606092 XDOT = -1982
908737
YDOT = 23157
421081 feet/sec YDOT = 7058
381946 meter/sec
ZDOT = -1907
142880 ZDOT = -581
297150
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 13124
54730910
00016717 00000-0 10270-3 0 9018
2 25544 51
6462 324
7702 0008035 242
8071 117
2262 15
51754877 27933
Satellite: ISS
Catalog Number: 25544
Epoch time: 13124
54730910 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 324
7702 deg
Eccentricity:
0008035
Arg of perigee: 242
8071 deg
Mean anomaly: 117
2262 deg
Mean motion: 15
51754877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2793
Checksum: 295
Coasting Arc #3 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2013/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1287842
33 A = 6785012
32 meter
Y = -4274194
48 meter E =
0008459
Z = -5116272
84 I = 51
40032
XDOT = 6433
200090 Wp = 135
86628
YDOT = -3841
939026 meter/sec RA = 319
42708 deg
ZDOT = 1585
904050 TA = 149
52207
MA = 149
47288
Ha = 223
679 n
mi
Hp = 221
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4225204
51 X = -1215097
88
Y = -14022947
75 feet Y = -4288189
36 meter
Z = -16785672
05 Z = -5122352
32
XDOT = 21106
299509 XDOT = 6467
979356
YDOT = -12604
786832 feet/sec YDOT = -3769
804418 meter/sec
ZDOT = 5203
097278 ZDOT = 1617
240938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12540683
25 X = -3822400
26
Y = -7509697
90 feet Y = -2288955
92 meter
Z = -16810410
58 Z = -5123813
14
XDOT = 6388
475785 XDOT = 1947
207419
YDOT = -22641
087022 feet/sec YDOT = -6901
003324 meter/sec
ZDOT = 5334
285030 ZDOT = 1625
890077
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 13125
51329726
00016717 00000-0 10270-3 0 9026
2 25544 51
6448 319
9702 0008005 246
1884 113
8429 15
51801997 28089
Satellite: ISS
Catalog Number: 25544
Epoch time: 13125
51329726 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 319
9702 deg
Eccentricity:
0008005
Arg of perigee: 246
1884 deg
Mean anomaly: 113
8429 deg
Mean motion: 15
51801997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2808
Checksum: 319
Coasting Arc #4 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2013/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 678364
13 A = 6786402
48 meter
Y = 4766518
53 meter E =
0001363
Z = 4784104
90 I = 51
38239
XDOT = -6313
233764 Wp = 307
67124
YDOT = 3491
441647 meter/sec RA = 314
43673 deg
ZDOT = -2583
108548 TA = 167
88920
MA = 167
88593
Ha = 223
457 n
mi
Hp = 221
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2225604
11 X = 601773
22
Y = 15638184
16 feet Y = 4773676
29 meter
Z = 15695882
21 Z = 4787214
24
XDOT = -20712
709201 XDOT = -6339
258352
YDOT = 11454
861046 feet/sec YDOT = 3420
697516 meter/sec
ZDOT = -8474
765578 ZDOT = -2613
841456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12342878
34 X = 3762109
32
Y = 9837356
28 feet Y = 2998426
19 meter
Z = 15708170
22 Z = 4787850
28
XDOT = -6307
888864 XDOT = -1922
644526
YDOT = 21653
871707 feet/sec YDOT = 6600
100096 meter/sec
ZDOT = -8603
378404 ZDOT = -2622
309738
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 13126
54367173
00016717 00000-0 10270-3 0 9039
2 25544 51
6449 314
8521 0008104 250
4561 109
5715 15
51803609 28243
Satellite: ISS
Catalog Number: 25544
Epoch time: 13126
54367173 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 314
8521 deg
Eccentricity:
0008104
Arg of perigee: 250
4561 deg
Mean anomaly: 109
5715 deg
Mean motion: 15
51803609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 296
Coasting Arc #5 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2013/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -122568
95 A = 6788197
19 meter
Y = -5256465
57 meter E =
0005209
Z = -4296991
51 I = 51
36711
XDOT = 6107
991179 Wp = 177
25465
YDOT = -3012
958498 meter/sec RA = 309
44505 deg
ZDOT = 3506
567520 TA = 128
64165
MA = 128
59502
Ha = 223
260 n
mi
Hp = 221
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -402129
11 X = -42906
90
Y = -17245621
96 feet Y = -5257390
84 meter
Z = -14097741
16 Z = -4297393
40
XDOT = 20039
341137 XDOT = 6124
194484
YDOT = -9885
034442 feet/sec YDOT = -2944
564459 meter/sec
ZDOT = 11504
486615 ZDOT = 3536
279541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12350912
01 X = -3764557
98
Y = -12041670
64 feet Y = -3670301
21 meter
Z = -14098674
80 Z = -4297276
08
XDOT = 6370
031180 XDOT = 1941
585504
YDOT = -20167
786413 feet/sec YDOT = -6147
141299 meter/sec
ZDOT = 11628
770714 ZDOT = 3544
449314
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 13127
50963555
00016717 00000-0 10270-3 0 9043
2 25544 51
6441 310
0518 0007992 253
3754 106
6520 15
51836692 28395
Satellite: ISS
Catalog Number: 25544
Epoch time: 13127
50963555 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 310
0518 deg
Eccentricity:
0007992
Arg of perigee: 253
3754 deg
Mean anomaly: 106
6520 deg
Mean motion: 15
51836692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 312
Coasting Arc #6 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2013/128/06:44:32
372
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3401245
73 A = 6798062
41 meter
Y = -5826638
18 meter E =
0009624
Z = -779680
65 I = 51
38232
XDOT = 4504
497146 Wp = 341
57481
YDOT = 1835
340747 meter/sec RA = 305
57049 deg
ZDOT = 5923
405855 TA = 9
97614
MA = 9
95705
Ha = 223
852 n
mi
Hp = 222
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11158942
70 X = 3469935
22
Y = -19116266
98 feet Y = -5788219
24 meter
Z = -2558007
37 Z = -762990
54
XDOT = 14778
533943 XDOT = 4454
864293
YDOT = 6021
459144 feet/sec YDOT = 1885
435340 meter/sec
ZDOT = 19433
746243 ZDOT = 5945
168191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19854941
03 X = 6051786
03
Y = -9802559
31 feet Y = -2987820
08 meter
Z = -2487612
31 Z = -758224
23
XDOT = 8203
505406 XDOT = 2500
428448
YDOT = 11651
868831 feet/sec YDOT = 3551
489620 meter/sec
ZDOT = 19524
205556 ZDOT = 5950
977853
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 13128
28239772
00016717 00000-0 10270-3 0 9057
2 25544 51
6488 306
2158 0009726 277
0236 82
9809 15
51045633 28515
Satellite: ISS
Catalog Number: 25544
Epoch time: 13128
28239772 = yrday
fracday
Element set: 905
Inclination: 51
6488 deg
RA of node: 306
2158 deg
Eccentricity:
0009726
Arg of perigee: 277
0236 deg
Mean anomaly: 82
9809 deg
Mean motion: 15
51045633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 326
Coasting Arc #7 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2013/129/06:44:32
372
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3395707
15 A = 6798354
60 meter
Y = 5883587
49 meter E =
0006781
Z = 89570
40 I = 51
36625
XDOT = -4182
803374 Wp = 186
20331
YDOT = -2323
741602 meter/sec RA = 300
59517 deg
ZDOT = -5984
585429 TA = 352
82962
MA = 352
83931
Ha = 224
255 n
mi
Hp = 222
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11140771
50 X = -3461681
43
Y = 19303108
55 feet Y = 5845245
66 meter
Z = 293866
13 Z = 72913
88
XDOT = -13723
108182 XDOT = -4127
435807
YDOT = -7623
824155 feet/sec YDOT = -2370
206639 meter/sec
ZDOT = -19634
466631 ZDOT = -6004
771103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19756352
79 X = -6021736
33
Y = 10317445
02 feet Y = 3144757
24 meter
Z = 223605
09 Z = 68154
83
XDOT = -6638
801519 XDOT = -2023
506703
YDOT = -12289
553591 feet/sec YDOT = -3745
855934 meter/sec
ZDOT = -19718
284646 ZDOT = -6010
133160
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 13129
31327590
00016717 00000-0 10270-3 0 9069
2 25544 51
6490 301
1009 0009728 280
2496 79
7558 15
51027593 28670
Satellite: ISS
Catalog Number: 25544
Epoch time: 13129
31327590 = yrday
fracday
Element set: 906
Inclination: 51
6490 deg
RA of node: 301
1009 deg
Eccentricity:
0009728
Arg of perigee: 280
2496 deg
Mean anomaly: 79
7558 deg
Mean motion: 15
51027593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 323
Coasting Arc #8 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2013/130/06:44:32
372
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3358115
65 A = 6798026
51 meter
Y = -5870445
72 meter E =
0010718
Z = 612522
78 I = 51
35112
XDOT = 3905
376865 Wp = 4
00424
YDOT = 2854
062486 meter/sec RA = 295
61780 deg
ZDOT = 5946
663799 TA = 2
62790
MA = 2
62227
Ha = 224
532 n
mi
Hp = 222
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11017439
81 X = 3420535
12
Y = -19259992
53 feet Y = -5832544
17 meter
Z = 2009589
18 Z = 628987
93
XDOT = 12812
916224 XDOT = 3844
283989
YDOT = 9363
722068 feet/sec YDOT = 2897
393049 meter/sec
ZDOT = 19510
051833 ZDOT = 5965
487876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19436016
78 X = 5924097
91
Y = -10690582
13 feet Y = -3258489
43 meter
Z = 2079049
31 Z = 633694
23
XDOT = 5163
163530 XDOT = 1573
732244
YDOT = 13193
715316 feet/sec YDOT = 4021
444428 meter/sec
ZDOT = 19588
121050 ZDOT = 5970
459296
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 13130
34413900
00016717 00000-0 10270-3 0 9076
2 25544 51
6492 295
9851 0009863 285
4183 74
5878 15
51084033 28835
Satellite: ISS
Catalog Number: 25544
Epoch time: 13130
34413900 = yrday
fracday
Element set: 907
Inclination: 51
6492 deg
RA of node: 295
9851 deg
Eccentricity:
0009863
Arg of perigee: 285
4183 deg
Mean anomaly: 74
5878 deg
Mean motion: 15
51084033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 325
Coasting Arc #9 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2013/131/06:44:32
372
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3298851
25 A = 6797501
80 meter
Y = 5794394
22 meter E =
0005606
Z = -1305596
13 I = 51
33702
XDOT = -3675
614827 Wp = 226
04754
YDOT = -3401
602204 meter/sec RA = 290
64017 deg
ZDOT = -5797
771497 TA = 328
19918
MA = 328
23302
Ha = 224
825 n
mi
Hp = 222
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10823002
79 X = -3357057
88
Y = 19010479
71 feet Y = 5757179
00 meter
Z = -4283451
87 Z = -1321763
03
XDOT = -12059
103763 XDOT = -3609
139661
YDOT = -11160
112219 feet/sec YDOT = -3442
333249 meter/sec
ZDOT = -19021
560030 ZDOT = -5815
466358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18942970
76 X = -5773817
49
Y = 10913781
66 feet Y = 3326520
65 meter
Z = -4351656
80 Z = -1326384
99
XDOT = -3839
557025 XDOT = -1170
296981
YDOT = -14293
146568 feet/sec YDOT = -4356
551074 meter/sec
ZDOT = -19094
848696 ZDOT = -5820
109883
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 13131
31056284
00016717 00000-0 10270-3 0 9083
2 25544 51
6493 291
1901 0009919 288
1657 71
8414 15
51065855 28981
Satellite: ISS
Catalog Number: 25544
Epoch time: 13131
31056284 = yrday
fracday
Element set: 908
Inclination: 51
6493 deg
RA of node: 291
1901 deg
Eccentricity:
0009919
Arg of perigee: 288
1657 deg
Mean anomaly: 71
8414 deg
Mean motion: 15
51065855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 328
Coasting Arc #10 (Orbit 2913)
---------------------------------------
Vector Time (GMT): 2013/132/06:44:32
372
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3230013
98 A = 6796393
79 meter
Y = -5632276
82 meter E =
0009816
Z = 1986152
49 I = 51
32375
XDOT = 3501
312839 Wp = 22
13971
YDOT = 3964
604165 meter/sec RA = 285
65954 deg
ZDOT = 5548
586735 TA = 359
86598
MA = 359
86625
Ha = 225
009 n
mi
Hp = 222
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10597158
72 X = 3283106
89
Y = -18478598
50 feet Y = -5595860
04 meter
Z = 6516248
33 Z = 2001972
47
XDOT = 11487
246847 XDOT = 3429
765581
YDOT = 13007
231514 feet/sec YDOT = 4003
357653 meter/sec
ZDOT = 18204
024720 ZDOT = 5565
422545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18282036
79 X = 5572364
82
Y = -10892719
40 feet Y = -3320100
87 meter
Z = 6582982
77 Z = 2006493
15
XDOT = 2707
795753 XDOT = 825
336145
YDOT = 15588
438749 feet/sec YDOT = 4751
356131 meter/sec
ZDOT = 18273
659060 ZDOT = 5569
811281
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 13132
34140075
00016717 00000-0 10270-3 0 9090
2 25544 51
6491 286
0740 0010027 293
4625 66
5472 15
51118312 29140
Satellite: ISS
Catalog Number: 25544
Epoch time: 13132
34140075 = yrday
fracday
Element set: 909
Inclination: 51
6491 deg
RA of node: 286
0740 deg
Eccentricity:
0010027
Arg of perigee: 293
4625 deg
Mean anomaly: 66
5472 deg
Mean motion: 15
51118312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2914
Checksum: 284
Coasting Arc #11 (Orbit 2928)
---------------------------------------
Vector Time (GMT): 2013/133/06:44:32
372
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3163573
34 A = 6795130
90 meter
Y = 5406717
78 meter E =
0005264
Z = -2631020
28 I = 51
31189
XDOT = -3379
315438 Wp = 287
00501
YDOT = -4507
713089 meter/sec RA = 280
67837 deg
ZDOT = -5189
811567 TA = 282
73740
MA = 282
79624
Ha = 225
280 n
mi
Hp = 221
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10379177
64 X = -3211016
34
Y = 17738575
40 feet Y = 5371075
62 meter
Z = -8631956
30 Z = -2646503
71
XDOT = -11086
992906 XDOT = -3303
447018
YDOT = -14789
084939 feet/sec YDOT = -4545
078164 meter/sec
ZDOT = -17026
940838 ZDOT = -5206
044229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17535844
18 X = -5344925
30
Y = 10665223
64 feet Y = 3250760
17 meter
Z = -8697254
09 Z = -2650923
05
XDOT = -1819
696223 XDOT = -554
643409
YDOT = -16958
700008 feet/sec YDOT = -5169
011763 meter/sec
ZDOT = -17093
992773 ZDOT = -5210
248997
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 13133
30779992
00016717 00000-0 10270-3 0 9105
2 25544 51
6488 281
2791 0010109 296
3197 63
6915 15
51116712 29294
Satellite: ISS
Catalog Number: 25544
Epoch time: 13133
30779992 = yrday
fracday
Element set: 910
Inclination: 51
6488 deg
RA of node: 281
2791 deg
Eccentricity:
0010109
Arg of perigee: 296
3197 deg
Mean anomaly: 63
6915 deg
Mean motion: 15
51116712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2929
Checksum: 323
Coasting Arc #12 (Orbit 2944)
---------------------------------------
Vector Time (GMT): 2013/134/06:44:32
372
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3114163
61 A = 6793528
47 meter
Y = -5089685
52 meter E =
0007087
Z = 3237876
41 I = 51
30171
XDOT = 3310
142801 Wp = 34
12106
YDOT = 5037
396283 meter/sec RA = 275
69350 deg
ZDOT = 4735
424232 TA = 3
54958
MA = 3
54456
Ha = 225
439 n
mi
Hp = 221
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10217072
22 X = 3155117
22
Y = -16698443
29 feet Y = -5054632
21 meter
Z = 10622954
11 Z = 3253104
04
XDOT = 10860
048561 XDOT = 3230
563874
YDOT = 16526
890693 feet/sec YDOT = 5073
967117 meter/sec
ZDOT = 15536
168740 ZDOT = 4751
311828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16714715
43 X = 5094645
26
Y = -10123096
40 feet Y = -3085519
78 meter
Z = 10687138
75 Z = 3257439
89
XDOT = 1176
992144 XDOT = 358
747205
YDOT = 18411
981010 feet/sec YDOT = 5611
971812 meter/sec
ZDOT = 15601
718564 ZDOT = 4755
403818
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 13134
33861307
00016717 00000-0 10270-3 0 9112
2 25544 51
6484 276
1627 0010177 301
3655 58
6500 15
51145626 29450
Satellite: ISS
Catalog Number: 25544
Epoch time: 13134
33861307 = yrday
fracday
Element set: 911
Inclination: 51
6484 deg
RA of node: 276
1627 deg
Eccentricity:
0010177
Arg of perigee: 301
3655 deg
Mean anomaly: 58
6500 deg
Mean motion: 15
51145626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2945
Checksum: 296
Coasting Arc #13 (Orbit 2959)
---------------------------------------
Vector Time (GMT): 2013/135/06:44:32
372
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3089899
56 A = 6791846
14 meter
Y = 4722446
64 meter E =
0007614
Z = -3782805
74 I = 51
29320
XDOT = -3285
311755 Wp = 340
32174
YDOT = -5508
967102 meter/sec RA = 270
70769 deg
ZDOT = -4184
340037 TA = 245
19878
MA = 245
27800
Ha = 225
664 n
mi
Hp = 221
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10137465
74 X = -3124101
31
Y = 15493591
34 feet Y = 4687702
43 meter
Z = -12410779
97 Z = -3797899
11
XDOT = -10778
581874 XDOT = -3203
138558
YDOT = -18074
039049 feet/sec YDOT = -5545
245817 meter/sec
ZDOT = -13728
149727 ZDOT = -4200
100667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15919023
09 X = -4852118
24
Y = 9371355
74 feet Y = 2856389
23 meter
Z = -12474351
24 Z = -3802182
26
XDOT = -815
631134 XDOT = -248
604370
YDOT = -19787
047682 feet/sec YDOT = -6031
092134 meter/sec
ZDOT = -13793
117101 ZDOT = -4204
142092
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
30498752
00016717 00000-0 10270-3 0 9121
2 25544 51
6474 271
3674 0010220 304
3831 55
6353 15
51168957 29608
Satellite: ISS
Catalog Number: 25544
Epoch time: 13135
30498752 = yrday
fracday
Element set: 912
Inclination: 51
6474 deg
RA of node: 271
3674 deg
Eccentricity:
0010220
Arg of perigee: 304
3831 deg
Mean anomaly: 55
6353 deg
Mean motion: 15
51168957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2960
Checksum: 303
Coasting Arc #14 (Orbit 2975)
---------------------------------------
Vector Time (GMT): 2013/136/06:44:32
372
Vector Time (MET): N/A
Weight (LBS) : 904584
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3107926
42 A = 6790188
22 meter
Y = -4269739
00 meter E =
0003843
Z = 4264563
34 I = 51
28799
XDOT = 3296
264401 Wp = 22
33127
YDOT = 5940
424292 meter/sec RA = 265
71837 deg
ZDOT = 3547
817939 TA = 31
29300
MA = 31
27013
Ha = 225
829 n
mi
Hp = 221
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10196608
98 X = 3134724
32
Y = -14008330
04 feet Y = -4234834
59 meter
Z = 13991349
54 Z = 4279726
35
XDOT = 10814
515750 XDOT = 3212
357845
YDOT = 19489
581012 feet/sec YDOT = 5976
815867 meter/sec
ZDOT = 11639
822635 ZDOT = 3563
627516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15159827
84 X = 4620715
53
Y = -8282178
73 feet Y = -2524408
08 meter
Z = 14055146
47 Z = 4284008
64
XDOT = 689
206247 XDOT = 210
070064
YDOT = 21111
749324 feet/sec YDOT = 6434
861194 meter/sec
ZDOT = 11704
948494 ZDOT = 3567
668301
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
33577586
00016717 00000-0 10270-3 0 9139
2 25544 51
6471 266
2509 0010261 309
0829 50
9409 15
51168251 29763
Satellite: ISS
Catalog Number: 25544
Epoch time: 13136
33577586 = yrday
fracday
Element set: 913
Inclination: 51
6471 deg
RA of node: 266
2509 deg
Eccentricity:
0010261
Arg of perigee: 309
0829 deg
Mean anomaly: 50
9409 deg
Mean motion: 15
51168251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2976
Checksum: 316
Coasting Arc #15 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2013/137/02:00:50
164
Vector Time (MET): N/A
Weight (LBS) : 904105
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1996058
19 A = 6795411
90 meter
Y = 5500977
02 meter E =
0004633
Z = -3454849
09 I = 51
30014
XDOT = -4312
936119 Wp = 315
17395
YDOT = -4416
267745 meter/sec RA = 261
71566 deg
ZDOT = -4533
014136 TA = 265
47495
MA = 265
52788
Ha = 226
056 n
mi
Hp = 223
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6548747
36 X = -2040640
11
Y = 18047824
87 feet Y = 5478406
72 meter
Z = -11334806
73 Z = -3464653
88
XDOT = -14150
052883 XDOT = -4241
211601
YDOT = -14489
067404 feet/sec YDOT = -4464
096486 meter/sec
ZDOT = -14872
093622 ZDOT = -4553
792115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17319290
84 X = -5278919
85
Y = -8228434
42 feet Y = -2508026
81 meter
Z = -11376420
79 Z = -3467533
06
XDOT = 15207
113746 XDOT = 4635
128270
YDOT = -11295
891149 feet/sec YDOT = -3442
987622 meter/sec
ZDOT = -14958
149545 ZDOT = -4559
243981
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
10887473
00016717 00000-0 10270-3 0 9145
2 25544 51
6479 262
4154 0008804 290
6582 69
3624 15
50299495 29886
Satellite: ISS
Catalog Number: 25544
Epoch time: 13137
10887473 = yrday
fracday
Element set: 914
Inclination: 51
6479 deg
RA of node: 262
4154 deg
Eccentricity:
0008804
Arg of perigee: 290
6582 deg
Mean anomaly: 69
3624 deg
Mean motion: 15
50299495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2988
Checksum: 345
Coasting Arc #16 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2013/138/02:00:50
164
Vector Time (MET): N/A
Weight (LBS) : 904105
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1855343
98 A = 6794412
72 meter
Y = -5328541
41 meter E =
0004090
Z = 3780382
14 I = 51
30169
XDOT = 4522
244543 Wp = 56
21038
YDOT = 4549
039270 meter/sec RA = 256
73536 deg
ZDOT = 4191
499314 TA = 349
28584
MA = 349
29455
Ha = 226
195 n
mi
Hp = 223
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6087086
55 X = 1896426
76
Y = -17482091
25 feet Y = -5307564
20 meter
Z = 12402828
56 Z = 3789494
93
XDOT = 14836
760312 XDOT = 4450
678771
YDOT = 14924
669521 feet/sec YDOT = 4599
209580 meter/sec
ZDOT = 13751
638168 ZDOT = 4213
294460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16932542
03 X = 5161038
81
Y = 7416448
45 feet Y = 2260533
49 meter
Z = 12441527
47 Z = 3792177
57
XDOT = -15538
609610 XDOT = -4736
168209
YDOT = 12249
911277 feet/sec YDOT = 3733
772957 meter/sec
ZDOT = 13841
929415 ZDOT = 4219
020086
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
14025271
00016717 00000-0 10270-3 0 9151
2 25544 51
6475 257
3033 0008809 294
7653 65
2581 15
50299057 30041
Satellite: ISS
Catalog Number: 25544
Epoch time: 13138
14025271 = yrday
fracday
Element set: 915
Inclination: 51
6475 deg
RA of node: 257
3033 deg
Eccentricity:
0008809
Arg of perigee: 294
7653 deg
Mean anomaly: 65
2581 deg
Mean motion: 15
50299057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 306
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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