[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 18th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
170/13:08:23
692 -1
0 3
3 3
3
N/A 2
7 -0
4 230
2
000/00:06:47
383 1
6 -0
1 217
7
Coasting Arc #1 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2013/168/12:41:05
268
Vector Time (MET): N/A
Weight (LBS) : 922039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2115573
62 A = 6798896
13 meter
Y = -6447759
29 meter E =
0018896
Z = -363831
38 I = 52
00730
XDOT = 4390
572167 Wp = 108
16631
YDOT = 1765
725416 meter/sec RA = 105
76505 deg
ZDOT = -6023
901164 TA = 75
72905
MA = 75
51927
Ha = 230
055 n
mi
Hp = 216
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6940858
34 X = 2189284
03
Y = -21154065
90 feet Y = -6423689
44 meter
Z = -1193672
49 Z = -353375
53
XDOT = 14404
764328 XDOT = 4399
763787
YDOT = 5793
062389 feet/sec YDOT = 1814
875449 meter/sec
ZDOT = -19763
455264 ZDOT = -6002
549555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21713287
23 X = -6618209
95
Y = -4930285
99 feet Y = -1502751
17 meter
Z = -1149047
66 Z = -350229
73
XDOT = 4041
830940 XDOT = 1231
950070
YDOT = -13423
221731 feet/sec YDOT = -4091
397984 meter/sec
ZDOT = -19674
390204 ZDOT = -5996
754134
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 13168
56015828
00016717 00000-0 10270-3 0 9001
2 25544 51
6474 106
4972 0010561 76
4558 283
7769 15
50823998 34768
Satellite: ISS
Catalog Number: 25544
Epoch time: 13168
56015828 = yrday
fracday
Element set: 900
Inclination: 51
6474 deg
RA of node: 106
4972 deg
Eccentricity:
0010561
Arg of perigee: 76
4558 deg
Mean anomaly: 283
7769 deg
Mean motion: 15
50823998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3476
Checksum: 343
Coasting Arc #2 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2013/169/12:41:05
268
Vector Time (MET): N/A
Weight (LBS) : 922039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1979829
67 A = 6798547
53 meter
Y = 6425555
81 meter E =
0023482
Z = 943494
02 I = 52
01338
XDOT = -4303
838482 Wp = 65
86093
YDOT = -2214
894337 meter/sec RA = 100
83385 deg
ZDOT = 5946
198559 TA = 304
29423
MA = 304
51632
Ha = 230
043 n
mi
Hp = 216
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6495504
15 X = -2056117
75
Y = 21081219
86 feet Y = 6402989
47 meter
Z = 3095452
82 Z = 933691
39
XDOT = -14120
204995 XDOT = -4307
636468
YDOT = -7266
713703 feet/sec YDOT = -2263
044359 meter/sec
ZDOT = 19508
525455 ZDOT = 5925
281276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21674487
93 X = 6606383
92
Y = 4133236
72 feet Y = 1259810
55 meter
Z = 3053548
83 Z = 930721
68
XDOT = -5337
495615 XDOT = -1626
868663
YDOT = 13378
826397 feet/sec YDOT = 4077
866286 meter/sec
ZDOT = 19421
339606 ZDOT = 5919
624312
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 13169
59117380
00016717 00000-0 10270-3 0 9012
2 25544 51
6471 101
3834 0010557 79
6872 280
5469 15
50839634 34929
Satellite: ISS
Catalog Number: 25544
Epoch time: 13169
59117380 = yrday
fracday
Element set: 901
Inclination: 51
6471 deg
RA of node: 101
3834 deg
Eccentricity:
0010557
Arg of perigee: 79
6872 deg
Mean anomaly: 280
5469 deg
Mean motion: 15
50839634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 325
Coasting Arc #3 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2013/170/12:41:05
268
Vector Time (MET): N/A
Weight (LBS) : 922039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1905182
09 A = 6797804
28 meter
Y = -6327471
60 meter E =
0016202
Z = -1593741
22 I = 52
01702
XDOT = 4244
830243 Wp = 108
55806
YDOT = 2716
966188 meter/sec RA = 95
90237 deg
ZDOT = -5765
470323 TA = 88
74722
MA = 88
56160
Ha = 230
016 n
mi
Hp = 216
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6250597
41 X = 1983537
70
Y = -20759421
26 feet Y = -6305728
36 meter
Z = -5228809
77 Z = -1584296
29
XDOT = 13926
608410 XDOT = 4242
140450
YDOT = 8913
931064 feet/sec YDOT = 2764
420161 meter/sec
ZDOT = -18915
585048 ZDOT = -5744
855323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21393712
28 X = -6520803
50
Y = -3571214
65 feet Y = -1088506
22 meter
Z = -5188399
70 Z = -1581424
23
XDOT = 6779
280407 XDOT = 2066
324668
YDOT = -13509
506463 feet/sec YDOT = -4117
697570 meter/sec
ZDOT = -18829
735770 ZDOT = -5739
303463
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 13170
55774150
00016717 00000-0 10270-3 0 9025
2 25544 51
6482 96
5884 0010507 83
5438 276
6909 15
50852845 35079
Satellite: ISS
Catalog Number: 25544
Epoch time: 13170
55774150 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 96
5884 deg
Eccentricity:
0010507
Arg of perigee: 83
5438 deg
Mean anomaly: 276
6909 deg
Mean motion: 15
50852845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3507
Checksum: 328
Coasting Arc #4 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2013/170/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2398860
00 A = 6794832
04 meter
Y = 5164140
28 meter E =
0013922
Z = -3718191
22 I = 52
00196
XDOT = -3911
285189 Wp = 83
51104
YDOT = 4935
978355 meter/sec RA = 95
75690 deg
ZDOT = 4347
552400 TA = 232
55626
MA = 232
68300
Ha = 230
249 n
mi
Hp = 217
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7870275
59 X = 2358997
34
Y = 16942717
45 feet Y = 5190743
38 meter
Z = -12198790
08 Z = -3706633
89
XDOT = -12832
300490 XDOT = -3987
309130
YDOT = 16194
154707 feet/sec YDOT = 4891
814336 meter/sec
ZDOT = 14263
623359 ZDOT = 4328
367409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14295856
13 X = 4357376
95
Y = -12074135
04 feet Y = -3680196
36 meter
Z = -12151179
05 Z = -3703679
37
XDOT = 18115
332246 XDOT = 5521
553269
YDOT = 7226
833420 feet/sec YDOT = 2202
738827 meter/sec
ZDOT = 14182
666653 ZDOT = 4322
876796
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 13170
55774077
00016717 00000-0 10270-3 0 9034
2 25544 51
6488 96
5879 0008671 72
3178 287
8919 15
50254216 35078
Satellite: ISS
Catalog Number: 25544
Epoch time: 13170
55774077 = yrday
fracday
Element set: 903
Inclination: 51
6488 deg
RA of node: 96
5879 deg
Eccentricity:
0008671
Arg of perigee: 72
3178 deg
Mean anomaly: 287
8919 deg
Mean motion: 15
50254216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3507
Checksum: 346
Coasting Arc #5 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2013/171/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2555795
79 A = 6795883
62 meter
Y = -5309221
47 meter E =
0021028
Z = 3369775
93 I = 52
00757
XDOT = 3729
864662 Wp = 84
91687
YDOT = -4787
116241 meter/sec RA = 90
82571 deg
ZDOT = -4686
490342 TA = 56
03843
MA = 55
83875
Ha = 230
312 n
mi
Hp = 217
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8385156
78 X = -2512606
60
Y = -17418705
61 feet Y = -5337560
97 meter
Z = 11055695
30 Z = 3357464
15
XDOT = 12237
088787 XDOT = 3805
883958
YDOT = -15705
761946 feet/sec YDOT = -4744
980855 meter/sec
ZDOT = -15375
624480 ZDOT = -4668
186801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14403245
53 X = -4390109
24
Y = 12937850
20 feet Y = 3943456
74 meter
Z = 11004958
36 Z = 3354311
31
XDOT = -17559
909222 XDOT = -5352
260331
YDOT = -6460
574834 feet/sec YDOT = -1969
183209 meter/sec
ZDOT = -15298
360301 ZDOT = -4662
940220
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 13171
58914911
00016717 00000-0 10270-3 0 9042
2 25544 51
6488 91
4765 0008689 76
1853 284
0264 15
50248226 35231
Satellite: ISS
Catalog Number: 25544
Epoch time: 13171
58914911 = yrday
fracday
Element set: 904
Inclination: 51
6488 deg
RA of node: 91
4765 deg
Eccentricity:
0008689
Arg of perigee: 76
1853 deg
Mean anomaly: 284
0264 deg
Mean motion: 15
50248226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 327
Coasting Arc #6 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2013/172/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2780689
71 A = 6796630
70 meter
Y = 5400343
11 meter E =
0013087
Z = -3056415
61 I = 52
01111
XDOT = -3551
471744 Wp = 76
34237
YDOT = 4623
915161 meter/sec RA = 85
89505 deg
ZDOT = 4959
653224 TA = 248
88526
MA = 249
02521
Ha = 230
211 n
mi
Hp = 217
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9122997
75 X = 2734942
59
Y = 17717661
13 feet Y = 5431183
24 meter
Z = -10027610
28 Z = -3043017
42
XDOT = -11651
810184 XDOT = -3627
006244
YDOT = 15170
325332 feet/sec YDOT = 4583
777236 meter/sec
ZDOT = 16271
828162 ZDOT = 4942
217622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14250276
30 X = 4343484
22
Y = -13970663
38 feet Y = -4258258
20 meter
Z = -9972349
86 Z = -3039572
24
XDOT = 16929
392445 XDOT = 5160
078817
YDOT = 5754
822055 feet/sec YDOT = 1754
069762 meter/sec
ZDOT = 16198
202678 ZDOT = 4937
212176
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 13172
55608471
00016717 00000-0 10270-3 0 9052
2 25544 51
6500 86
6846 0008596 79
1004 281
1114 15
50282664 35382
Satellite: ISS
Catalog Number: 25544
Epoch time: 13172
55608471 = yrday
fracday
Element set: 905
Inclination: 51
6500 deg
RA of node: 86
6846 deg
Eccentricity:
0008596
Arg of perigee: 79
1004 deg
Mean anomaly: 281
1114 deg
Mean motion: 15
50282664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 308
Coasting Arc #7 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2013/173/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2974432
98 A = 6797635
98 meter
Y = -5494329
64 meter E =
0021888
Z = 2656605
62 I = 52
01117
XDOT = 3441
790704 Wp = 94
93550
YDOT = -4413
875745 meter/sec RA = 80
96522 deg
ZDOT = -5239
905749 TA = 55
29620
MA = 55
09019
Ha = 230
276 n
mi
Hp = 217
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9758638
38 X = -2925678
23
Y = -18026015
88 feet Y = -5527319
49 meter
Z = 8715897
69 Z = 2642273
52
XDOT = 11291
964252 XDOT = 3516
345916
YDOT = -14481
219635 feet/sec YDOT = -4374
969696 meter/sec
ZDOT = -17191
291826 ZDOT = -5223
005471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14107125
88 X = -4299851
97
Y = 14905865
44 feet Y = 4543307
78 meter
Z = 8656749
93 Z = 2638577
38
XDOT = -16210
632768 XDOT = -4941
000868
YDOT = -5331
833484 feet/sec YDOT = -1625
142846 meter/sec
ZDOT = -17119
922262 ZDOT = -5218
152305
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 13173
58747551
00016717 00000-0 10270-3 0 9060
2 25544 51
6500 81
5733 0008640 83
1645 277
0488 15
50269560 35543
Satellite: ISS
Catalog Number: 25544
Epoch time: 13173
58747551 = yrday
fracday
Element set: 906
Inclination: 51
6500 deg
RA of node: 81
5733 deg
Eccentricity:
0008640
Arg of perigee: 83
1645 deg
Mean anomaly: 277
0488 deg
Mean motion: 15
50269560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 317
Coasting Arc #8 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2013/174/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3225168
34 A = 6798256
74 meter
Y = 5525741
32 meter E =
0013489
Z = -2299919
78 I = 52
00852
XDOT = -3342
648380 Wp = 68
73494
YDOT = 4208
125902 meter/sec RA = 76
03522 deg
ZDOT = 5453
430701 TA = 265
84630
MA = 266
00048
Ha = 230
148 n
mi
Hp = 217
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10581260
97 X = 3174310
95
Y = 18129072
57 feet Y = 5561523
23 meter
Z = -7545668
59 Z = -2284374
83
XDOT = -10966
694159 XDOT = -3415
947300
YDOT = 13806
187341 feet/sec YDOT = 4170
335505 meter/sec
ZDOT = 17891
833010 ZDOT = 5437
015176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13680707
58 X = 4169879
67
Y = -15950848
08 feet Y = -4861818
49 meter
Z = -7481454
14 Z = -2280347
22
XDOT = 15498
598650 XDOT = 4723
972869
YDOT = 4980
765073 feet/sec YDOT = 1518
137194 meter/sec
ZDOT = 17822
510093 ZDOT = 5432
301076
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 13174
55439414
00016717 00000-0 10270-3 0 9075
2 25544 51
6506 76
7815 0008483 85
7524 274
4596 15
50307998 35690
Satellite: ISS
Catalog Number: 25544
Epoch time: 13174
55439414 = yrday
fracday
Element set: 907
Inclination: 51
6506 deg
RA of node: 76
7815 deg
Eccentricity:
0008483
Arg of perigee: 85
7524 deg
Mean anomaly: 274
4596 deg
Mean motion: 15
50307998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 349
Coasting Arc #9 (Orbit 3584)
---------------------------------------
Vector Time (GMT): 2013/175/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3434662
32 A = 6799094
06 meter
Y = -5555746
33 meter E =
0022016
Z = 1856731
37 I = 52
00252
XDOT = 3319
548419 Wp = 104
70778
YDOT = -3961
428878 meter/sec RA = 71
10562 deg
ZDOT = -5662
322816 TA = 54
98966
MA = 54
78323
Ha = 230
208 n
mi
Hp = 217
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11268577
17 X = -3381300
90
Y = -18227514
20 feet Y = -5593856
83 meter
Z = 6091638
35 Z = 1840174
95
XDOT = 10890
906887 XDOT = 3391
105021
YDOT = -12996
813904 feet/sec YDOT = -3923
906576 meter/sec
ZDOT = -18577
174594 ZDOT = -5646
023739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13265093
87 X = -4043200
61
Y = 16854955
98 feet Y = 5137390
58 meter
Z = 6023197
38 Z = 1835870
56
XDOT = -14748
010456 XDOT = -4495
193587
YDOT = -4932
972871 feet/sec YDOT = -1503
570131 meter/sec
ZDOT = -18508
366803 ZDOT = -5641
350202
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 13175
58576740
00016717 00000-0 10270-3 0 9084
2 25544 51
6503 71
6700 0008550 90
1478 270
0652 15
50289916 35859
Satellite: ISS
Catalog Number: 25544
Epoch time: 13175
58576740 = yrday
fracday
Element set: 908
Inclination: 51
6503 deg
RA of node: 71
6700 deg
Eccentricity:
0008550
Arg of perigee: 90
1478 deg
Mean anomaly: 270
0652 deg
Mean motion: 15
50289916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3585
Checksum: 317
Coasting Arc #10 (Orbit 3599)
---------------------------------------
Vector Time (GMT): 2013/176/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3688381
44 A = 6799501
65 meter
Y = 5519160
97 meter E =
0014921
Z = -1464688
16 I = 51
99325
XDOT = -3309
564969 Wp = 64
77889
YDOT = 3738
864347 meter/sec RA = 66
17484 deg
ZDOT = 5806
754432 TA = 279
35128
MA = 279
51996
Ha = 230
064 n
mi
Hp = 217
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12100988
98 X = 3633505
83
Y = 18107483
51 feet Y = 5560100
16 meter
Z = -4805407
35 Z = -1446903
07
XDOT = -10858
152784 XDOT = -3379
335060
YDOT = 12266
615312 feet/sec YDOT = 3701
463778 meter/sec
ZDOT = 19051
031600 ZDOT = 5790
508128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12566153
04 X = 3830163
45
Y = -17807540
86 feet Y = -5427738
46 meter
Z = -4731819
85 Z = -1442258
69
XDOT = 14085
208705 XDOT = 4293
171613
YDOT = 4941
730619 feet/sec YDOT = 1506
239493 meter/sec
ZDOT = 18982
472058 ZDOT = 5785
857483
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 13176
55266923
00016717 00000-0 10270-3 0 9092
2 25544 51
6500 66
8776 0008355 92
5433 267
6675 15
50332312 36009
Satellite: ISS
Catalog Number: 25544
Epoch time: 13176
55266923 = yrday
fracday
Element set: 909
Inclination: 51
6500 deg
RA of node: 66
8776 deg
Eccentricity:
0008355
Arg of perigee: 92
5433 deg
Mean anomaly: 267
6675 deg
Mean motion: 15
50332312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3600
Checksum: 315
Coasting Arc #11 (Orbit 3615)
---------------------------------------
Vector Time (GMT): 2013/177/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3888674
76 A = 6800057
67 meter
Y = -5479972
61 meter E =
0021306
Z = 988515
48 I = 51
98133
XDOT = 3378
819630 Wp = 113
82025
YDOT = -3484
568094 meter/sec RA = 61
24427 deg
ZDOT = -5933
000889 TA = 55
53343
MA = 55
33232
Ha = 230
100 n
mi
Hp = 217
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12758119
29 X = -3831909
38
Y = -17978912
75 feet Y = -5523140
94 meter
Z = 3243161
02 Z = 969762
13
XDOT = 11085
366241 XDOT = 3446
354230
YDOT = -11432
310021 feet/sec YDOT = -3446
405699 meter/sec
ZDOT = -19465
226013 ZDOT = -5916
423474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11896763
54 X = -3626133
53
Y = 18573516
72 feet Y = 5661207
90 meter
Z = 3165517
12 Z = 964849
62
XDOT = -13439
998940 XDOT = -4096
511677
YDOT = -5250
113376 feet/sec YDOT = -1600
234557 meter/sec
ZDOT = -19395
315598 ZDOT = -5911
692194
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 13177
58402484
00016717 00000-0 10270-3 0 9102
2 25544 51
6497 61
7657 0008414 97
1612 263
0496 15
50312118 36162
Satellite: ISS
Catalog Number: 25544
Epoch time: 13177
58402484 = yrday
fracday
Element set: 910
Inclination: 51
6497 deg
RA of node: 61
7657 deg
Eccentricity:
0008414
Arg of perigee: 97
1612 deg
Mean anomaly: 263
0496 deg
Mean motion: 15
50312118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3616
Checksum: 308
Coasting Arc #12 (Orbit 3630)
---------------------------------------
Vector Time (GMT): 2013/178/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4120179
50 A = 6800182
04 meter
Y = 5375129
48 meter E =
0016755
Z = -571197
38 I = 51
96593
XDOT = -3458
665418 Wp = 65
79417
YDOT = 3273
343045 meter/sec RA = 56
31167 deg
ZDOT = 6000
026666 TA = 288
08074
MA = 288
26318
Ha = 229
961 n
mi
Hp = 217
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13517649
29 X = 4062542
11
Y = 17634939
23 feet Y = 5420881
71 meter
Z = -1874007
16 Z = -551321
62
XDOT = -11347
327486 XDOT = -3524
157759
YDOT = 10739
314452 feet/sec YDOT = 3234
299292 meter/sec
ZDOT = 19685
126856 ZDOT = 5983
066215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10966088
68 X = 3342463
83
Y = -19332995
20 feet Y = -5892696
94 meter
Z = -1791653
61 Z = -546096
02
XDOT = 12952
141586 XDOT = 3947
812755
YDOT = 5575
213835 feet/sec YDOT = 1699
325177 meter/sec
ZDOT = 19613
643388 ZDOT = 5978
238505
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 13178
55091040
00016717 00000-0 10270-3 0 9113
2 25544 51
6490 56
9726 0008234 99
6929 260
5152 15
50357597 36314
Satellite: ISS
Catalog Number: 25544
Epoch time: 13178
55091040 = yrday
fracday
Element set: 911
Inclination: 51
6490 deg
RA of node: 56
9726 deg
Eccentricity:
0008234
Arg of perigee: 99
6929 deg
Mean anomaly: 260
5152 deg
Mean motion: 15
50357597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3631
Checksum: 321
Coasting Arc #13 (Orbit 3646)
---------------------------------------
Vector Time (GMT): 2013/179/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4285332
85 A = 6800362
11 meter
Y = -5270388
31 meter E =
0019766
Z = 74777
11 I = 51
94844
XDOT = 3615
513523 Wp = 121
63631
YDOT = -3041
840164 meter/sec RA = 51
37928 deg
ZDOT = -6034
454008 TA = 57
56273
MA = 57
37172
Ha = 229
957 n
mi
Hp = 217
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14059490
98 X = -4226442
97
Y = -17291300
24 feet Y = -5317980
35 meter
Z = 245331
74 Z = 54102
12
XDOT = 11861
921007 XDOT = 3678
572816
YDOT = -9979
790564 feet/sec YDOT = -3001
056107 meter/sec
ZDOT = -19798
077454 ZDOT = -6016
737411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10102253
28 X = -3079166
80
Y = 19865486
08 feet Y = 6055000
16 meter
Z = 159623
36 Z = 48653
20
XDOT = -12535
599631 XDOT = -3820
850767
YDOT = -6169
272158 feet/sec YDOT = -1880
394154 meter/sec
ZDOT = -19723
463633 ZDOT = -6011
711715
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 13179
58224850
00016717 00000-0 10270-3 0 9125
2 25544 51
6489 51
8605 0008256 104
1520 256
0549 15
50340958 36475
Satellite: ISS
Catalog Number: 25544
Epoch time: 13179
58224850 = yrday
fracday
Element set: 912
Inclination: 51
6489 deg
RA of node: 51
8605 deg
Eccentricity:
0008256
Arg of perigee: 104
1520 deg
Mean anomaly: 256
0549 deg
Mean motion: 15
50340958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3647
Checksum: 314
Coasting Arc #14 (Orbit 3662)
---------------------------------------
Vector Time (GMT): 2013/180/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4470050
35 A = 6800173
89 meter
Y = 5105693
75 meter E =
0018414
Z = 355759
13 I = 51
92760
XDOT = -3775
981843 Wp = 70
97544
YDOT = 2869
302648 meter/sec RA = 46
44417 deg
ZDOT = 6017
432177 TA = 292
83775
MA = 293
03212
Ha = 229
846 n
mi
Hp = 217
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14665519
52 X = 4410896
98
Y = 16750963
75 feet Y = 5155349
90 meter
Z = 1167188
75 Z = 377330
86
XDOT = -12388
391872 XDOT = -3837
017267
YDOT = 9413
722599 feet/sec YDOT = 2826
735467 meter/sec
ZDOT = 19742
231552 ZDOT = 5998
940878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9017489
59 X = 2748530
83
Y = -20350436
05 feet Y = -6202812
91 meter
Z = 1256667
37 Z = 383032
22
XDOT = 12325
193433 XDOT = 3756
718958
YDOT = 6722
425061 feet/sec YDOT = 2048
995159 meter/sec
ZDOT = 19664
401201 ZDOT = 5993
709486
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 13180
61357605
00016717 00000-0 10270-3 0 9137
2 25544 51
6481 46
7475 0008145 107
4637 252
7405 15
50384311 36630
Satellite: ISS
Catalog Number: 25544
Epoch time: 13180
61357605 = yrday
fracday
Element set: 913
Inclination: 51
6481 deg
RA of node: 46
7475 deg
Eccentricity:
0008145
Arg of perigee: 107
4637 deg
Mean anomaly: 252
7405 deg
Mean motion: 15
50384311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3663
Checksum: 301
Coasting Arc #15 (Orbit 3677)
---------------------------------------
Vector Time (GMT): 2013/181/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4576363
48 A = 6799919
11 meter
Y = -4948115
92 meter E =
0017567
Z = -857783
06 I = 51
90482
XDOT = 4005
077644 Wp = 127
10879
YDOT = -2688
387303 meter/sec RA = 41
50904 deg
ZDOT = -5953
740644 TA = 62
12260
MA = 61
94477
Ha = 229
799 n
mi
Hp = 217
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15014315
88 X = -4516525
58
Y = -16233976
12 feet Y = -4998957
06 meter
Z = -2814248
89 Z = -879869
67
XDOT = 13140
018517 XDOT = 4063
763697
YDOT = -8820
168317 feet/sec YDOT = -2643
271339 meter/sec
ZDOT = -19533
269829 ZDOT = -5934
142071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8053261
17 X = -2454634
00
Y = 20581360
55 feet Y = 6273198
70 meter
Z = -2905897
67 Z = -885717
61
XDOT = -12227
039276 XDOT = -3726
801571
YDOT = -7488
337509 feet/sec YDOT = -2282
445273 meter/sec
ZDOT = -19450
832840 ZDOT = -5928
613850
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 13181
58043936
00016717 00000-0 10270-3 0 9144
2 25544 51
6480 41
9550 0008133 111
0658 249
1363 15
50378277 36784
Satellite: ISS
Catalog Number: 25544
Epoch time: 13181
58043936 = yrday
fracday
Element set: 914
Inclination: 51
6480 deg
RA of node: 41
9550 deg
Eccentricity:
0008133
Arg of perigee: 111
0658 deg
Mean anomaly: 249
1363 deg
Mean motion: 15
50378277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3678
Checksum: 312
Coasting Arc #16 (Orbit 3693)
---------------------------------------
Vector Time (GMT): 2013/182/13:11:47
383
Vector Time (MET): N/A
Weight (LBS) : 921738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4693376
13 A = 6799433
11 meter
Y = 4740230
01 meter E =
0019548
Z = 1287916
70 I = 51
87921
XDOT = -4227
745979 Wp = 79
17016
YDOT = 2577
524124 meter/sec RA = 36
57064 deg
ZDOT = 5848
217684 TA = 294
77344
MA = 294
97671
Ha = 229
728 n
mi
Hp = 217
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15398215
66 X = 4633764
68
Y = 15551935
74 feet Y = 4792380
88 meter
Z = 4225448
49 Z = 1310572
37
XDOT = -13870
557674 XDOT = -4284
663242
YDOT = 8456
443977 feet/sec YDOT = 2529
927976 meter/sec
ZDOT = 19187
065893 ZDOT = 5827
541685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6920175
08 X = 2109269
36
Y = -20743076
99 feet Y = -6322489
87 meter
Z = 4319502
23 Z = 1316584
28
XDOT = 12357
070045 XDOT = 3766
434950
YDOT = 8147
777504 feet/sec YDOT = 2483
442583 meter/sec
ZDOT = 19100
136335 ZDOT = 5821
721555
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 13182
61175067
00016717 00000-0 10270-3 0 9151
2 25544 51
6473 36
8420 0008112 115
1608 245
0385 15
50409824 36942
Satellite: ISS
Catalog Number: 25544
Epoch time: 13182
61175067 = yrday
fracday
Element set: 915
Inclination: 51
6473 deg
RA of node: 36
8420 deg
Eccentricity:
0008112
Arg of perigee: 115
1608 deg
Mean anomaly: 245
0385 deg
Mean motion: 15
50409824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3694
Checksum: 297
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