[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 3rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
253/23:02:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 219
3
257/02:09:17
693 1
2 1
2 1
2
N/A 0
2 -0
2 228
0
000/00:02:35
386 0
1 0
0 220
0
Coasting Arc #1 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2014/246/12:32:42
389
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4522360
15 A = 6790701
84 meter
Y = 1240019
73 meter E =
0014922
Z = -4925263
26 I = 51
97001
XDOT = 590
841366 Wp = 99
78992
YDOT = 7249
514186 meter/sec RA = 70
56752 deg
ZDOT = 2371
346764 TA = 193
36358
MA = 193
40314
Ha = 228
438 n
mi
Hp = 219
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14837139
62 X = 4532083
09
Y = 4068306
19 feet Y = 1290645
83 meter
Z = -16159000
20 Z = -4903270
81
XDOT = 1938
455925 XDOT = 498
212527
YDOT = 23784
495360 feet/sec YDOT = 7255
603542 meter/sec
ZDOT = 7780
009068 ZDOT = 2373
991669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13995633
22 X = -4265869
01
Y = -6619928
45 feet Y = -2017754
19 meter
Z = -16065612
75 Z = -4896798
77
XDOT = 1821
951350 XDOT = 555
330771
YDOT = -22727
946508 feet/sec YDOT = -6927
478096 meter/sec
ZDOT = 7790
019343 ZDOT = 2374
397896
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 14246
53467415
00016717 00000-0 10270-3 0 9009
2 25544 51
6419 71
2642 0003439 74
2801 285
8729 15
50194250 23481
Satellite: ISS
Catalog Number: 25544
Epoch time: 14246
53467415 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 71
2642 deg
Eccentricity:
0003439
Arg of perigee: 74
2801 deg
Mean anomaly: 285
8729 deg
Mean motion: 15
50194250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 304
Coasting Arc #2 (Orbit 2363)
---------------------------------------
Vector Time (GMT): 2014/247/12:32:42
389
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4674155
13 A = 6791433
84 meter
Y = -1344151
62 meter E =
0011244
Z = 4733172
40 I = 51
96094
XDOT = -806
426463 Wp = 67
29897
YDOT = -7091
002405 meter/sec RA = 65
63191 deg
ZDOT = -2800
597377 TA = 50
38455
MA = 50
28534
Ha = 228
547 n
mi
Hp = 219
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15335154
64 X = -4681769
17
Y = -4409946
27 feet Y = -1396463
40 meter
Z = 15528780
84 Z = 4710447
77
XDOT = -2645
756112 XDOT = -713
469013
YDOT = -23264
443586 feet/sec YDOT = -7099
500763 meter/sec
ZDOT = -9188
311604 ZDOT = -2804
288733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14541222
45 X = 4432164
60
Y = 6793731
03 feet Y = 2070729
22 meter
Z = 15432293
96 Z = 4703763
20
XDOT = -628
578739 XDOT = -191
590800
YDOT = 22321
353877 feet/sec YDOT = 6803
548662 meter/sec
ZDOT = -9202
794048 ZDOT = -2805
011626
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 14247
56611346
00016717 00000-0 10270-3 0 9018
2 25544 51
6416 66
1524 0003378 77
1970 282
9558 15
50195295 23647
Satellite: ISS
Catalog Number: 25544
Epoch time: 14247
56611346 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 66
1524 deg
Eccentricity:
0003378
Arg of perigee: 77
1970 deg
Mean anomaly: 282
9558 deg
Mean motion: 15
50195295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2364
Checksum: 319
Coasting Arc #3 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2014/248/12:32:42
389
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4863443
22 A = 6792096
37 meter
Y = 1403452
80 meter E =
0012719
Z = -4540985
28 I = 51
95042
XDOT = 993
739843 Wp = 102
59340
YDOT = 6880
770023 meter/sec RA = 60
69530 deg
ZDOT = 3195
750851 TA = 199
41359
MA = 199
46208
Ha = 228
411 n
mi
Hp = 219
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15956178
54 X = 4869446
42
Y = 4604503
93 feet Y = 1457872
26 meter
Z = -14898245
68 Z = -4517345
14
XDOT = 3260
301321 XDOT = 901
199876
YDOT = 22574
704800 feet/sec YDOT = 6891
365436 meter/sec
ZDOT = 10484
746885 ZDOT = 3200
353059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15239334
98 X = -4644949
30
Y = -6822351
16 feet Y = -2079452
63 meter
Z = -14797871
75 Z = -4510391
31
XDOT = -473
499838 XDOT = -144
322751
YDOT = -21689
175949 feet/sec YDOT = -6610
860829 meter/sec
ZDOT = 10503
136399 ZDOT = 3201
355975
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 14248
53307346
00016717 00000-0 10270-3 0 9029
2 25544 51
6422 61
3595 0003490 81
6157 278
5389 15
50238601 23799
Satellite: ISS
Catalog Number: 25544
Epoch time: 14248
53307346 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 61
3595 deg
Eccentricity:
0003490
Arg of perigee: 81
6157 deg
Mean anomaly: 278
5389 deg
Mean motion: 15
50238601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 312
Coasting Arc #4 (Orbit 2394)
---------------------------------------
Vector Time (GMT): 2014/249/12:32:42
389
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5056512
48 A = 6793018
47 meter
Y = -1468866
53 meter E =
0013395
Z = 4282583
31 I = 51
93673
XDOT = -1126
076137 Wp = 76
23059
YDOT = -6671
710620 meter/sec RA = 55
75800 deg
ZDOT = -3605
330669 TA = 50
50413
MA = 50
38575
Ha = 228
503 n
mi
Hp = 219
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16589607
87 X = -5060514
60
Y = -4819115
91 feet Y = -1525433
75 meter
Z = 14050470
17 Z = 4258010
21
XDOT = -3694
475516 XDOT = -1033
874534
YDOT = -21888
814370 feet/sec YDOT = -6683
787897 meter/sec
ZDOT = -11828
512695 ZDOT = -3610
576422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15951022
12 X = 4861871
54
Y = 6850169
74 feet Y = 2087931
74 meter
Z = 13946137
36 Z = 4250782
67
XDOT = 1375
236444 XDOT = 419
172068
YDOT = 21006
664368 feet/sec YDOT = 6402
831299 meter/sec
ZDOT = -11849
673525 ZDOT = -3611
780490
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 14249
56448215
00016717 00000-0 10270-3 0 9035
2 25544 51
6415 56
2469 0003444 84
5939 275
5604 15
50240751 23957
Satellite: ISS
Catalog Number: 25544
Epoch time: 14249
56448215 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 56
2469 deg
Eccentricity:
0003444
Arg of perigee: 84
5939 deg
Mean anomaly: 275
5604 deg
Mean motion: 15
50240751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2395
Checksum: 316
Coasting Arc #5 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2014/250/12:32:42
389
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5275511
38 A = 6793804
23 meter
Y = 1478693
64 meter E =
0010228
Z = -4027330
77 I = 51
92280
XDOT = 1224
636776 Wp = 100
47863
YDOT = 6426
717613 meter/sec RA = 50
82037 deg
ZDOT = 3970
606697 TA = 210
72273
MA = 210
78264
Ha = 228
360 n
mi
Hp = 219
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17308108
21 X = 5278147
43
Y = 4851357
10 feet Y = 1537702
14 meter
Z = -13213027
46 Z = -4001697
17
XDOT = 4017
837192 XDOT = 1133
393040
YDOT = 21085
031540 feet/sec YDOT = 6439
902541 meter/sec
ZDOT = 13026
924858 ZDOT = 3976
333428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16772156
92 X = -5112153
43
Y = -6683221
49 feet Y = -2037045
91 meter
Z = -13104185
32 Z = -3994155
68
XDOT = -2144
270516 XDOT = -653
573653
YDOT = -20163
164546 feet/sec YDOT = -6145
732553 meter/sec
ZDOT = 13050
172104 ZDOT = 3977
692457
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 14250
53141269
00016717 00000-0 10270-3 0 9044
2 25544 51
6428 51
4542 0003510 87
9236 272
2316 15
50284667 24107
Satellite: ISS
Catalog Number: 25544
Epoch time: 14250
53141269 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 51
4542 deg
Eccentricity:
0003510
Arg of perigee: 87
9236 deg
Mean anomaly: 272
2316 deg
Mean motion: 15
50284667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 285
Coasting Arc #6 (Orbit 2425)
---------------------------------------
Vector Time (GMT): 2014/251/12:32:42
389
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5490341
05 A = 6794829
50 meter
Y = -1492740
57 meter E =
0015274
Z = 3702212
55 I = 51
90532
XDOT = -1257
879725 Wp = 86
38188
YDOT = -6190
133672 meter/sec RA = 45
88137 deg
ZDOT = -4344
927228 TA = 49
74899
MA = 49
61551
Ha = 228
423 n
mi
Hp = 219
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18012929
96 X = -5491224
80
Y = -4897442
82 feet Y = -1554141
59 meter
Z = 12146366
63 Z = 3675539
57
XDOT = -4126
901984 XDOT = -1167
460689
YDOT = -20308
837505 feet/sec YDOT = -6203
695083 meter/sec
ZDOT = -14255
010590 ZDOT = -4350
817366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17575751
44 X = 5357089
04
Y = 6502466
76 feet Y = 1981951
87 meter
Z = 12033108
56 Z = 3667691
49
XDOT = 2669
389428 XDOT = 813
629898
YDOT = 19309
056738 feet/sec YDOT = 5885
400494 meter/sec
ZDOT = -14278
990495 ZDOT = -4352
236303
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 14251
56278989
00016717 00000-0 10270-3 0 9059
2 25544 51
6423 46
3412 0003475 91
1733 268
9816 15
50289857 24260
Satellite: ISS
Catalog Number: 25544
Epoch time: 14251
56278989 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 46
3412 deg
Eccentricity:
0003475
Arg of perigee: 91
1733 deg
Mean anomaly: 268
9816 deg
Mean motion: 15
50289857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2426
Checksum: 333
Coasting Arc #7 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2014/252/12:32:42
389
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5717007
82 A = 6795659
27 meter
Y = 1444535
26 meter E =
0008206
Z = -3384843
25 I = 51
88788
XDOT = 1256
952978 Wp = 89
13875
YDOT = 5936
396963 meter/sec RA = 40
94256 deg
ZDOT = 4666
341564 TA = 231
60935
MA = 231
68308
Ha = 228
282 n
mi
Hp = 219
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18756587
35 X = 5716872
19
Y = 4739288
93 feet Y = 1508465
32 meter
Z = -11105128
77 Z = -3357071
52
XDOT = 4123
861475 XDOT = 1167
809937
YDOT = 19476
367988 feet/sec YDOT = 5949
955236 meter/sec
ZDOT = 15309
519568 ZDOT = 4672
230294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18431632
64 X = -5617961
63
Y = -6095145
92 feet Y = -1857800
48 meter
Z = -10987193
82 Z = -3348896
68
XDOT = -3044
438131 XDOT = -927
944742
YDOT = -18374
956791 feet/sec YDOT = -5600
686830 meter/sec
ZDOT = 15333
532286 ZDOT = 4673
660641
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 14252
52969024
00016717 00000-0 10270-3 0 9064
2 25544 51
6441 41
5489 0003481 93
2036 266
9513 15
50331103 24418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14252
52969024 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 41
5489 deg
Eccentricity:
0003481
Arg of perigee: 93
2036 deg
Mean anomaly: 266
9513 deg
Mean motion: 15
50331103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 286
Coasting Arc #8 (Orbit 2456)
---------------------------------------
Vector Time (GMT): 2014/253/12:32:42
389
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5929294
82 A = 6796664
87 meter
Y = -1401570
44 meter E =
0016633
Z = 2995391
01 I = 51
86708
XDOT = -1183
471589 Wp = 97
09957
YDOT = -5700
279911 meter/sec RA = 36
00213 deg
ZDOT = -4988
144864 TA = 48
78183
MA = 48
63857
Ha = 228
302 n
mi
Hp = 219
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19453067
00 X = -5927732
10
Y = -4598328
23 feet Y = -1467866
51 meter
Z = 9827398
31 Z = 2966591
34
XDOT = -3882
780805 XDOT = -1095
410998
YDOT = -18701
705744 feet/sec YDOT = -5713
022561 meter/sec
ZDOT = -16365
304673 ZDOT = -4993
679327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19228933
18 X = 5860978
83
Y = 5674816
47 feet Y = 1729684
06 meter
Z = 9705090
55 Z = 2958111
60
XDOT = 3148
296549 XDOT = 959
600788
YDOT = 17482
034316 feet/sec YDOT = 5328
524060 meter/sec
ZDOT = -16387
844118 ZDOT = -4995
014887
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 14253
56103519
00016717 00000-0 10270-3 0 9079
2 25544 51
6440 36
4361 0003453 96
9268 263
2276 15
50342520 24573
Satellite: ISS
Catalog Number: 25544
Epoch time: 14253
56103519 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 36
4361 deg
Eccentricity:
0003453
Arg of perigee: 96
9268 deg
Mean anomaly: 263
2276 deg
Mean motion: 15
50342520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2457
Checksum: 296
Coasting Arc #9 (Orbit 2463)
---------------------------------------
Vector Time (GMT): 2014/253/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 113962
91 A = 6790142
49 meter
Y = 4704664
44 meter E =
0009800
Z = 4888138
64 I = 51
83387
XDOT = -6890
082550 Wp = 110
15228
YDOT = -2345
397663 meter/sec RA = 33
88857 deg
ZDOT = 2410
791483 TA = 316
23550
MA = 316
31313
Ha = 228
136 n
mi
Hp = 219
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 373894
06 X = 37600
76
Y = 15435250
77 feet Y = 4705512
53 meter
Z = 16037200
28 Z = 4888506
16
XDOT = -22605
257711 XDOT = -6875
054549
YDOT = -7694
874223 feet/sec YDOT = -2422
362677 meter/sec
ZDOT = 7909
420877 ZDOT = 2377
357217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6382505
65 X = -1945387
72
Y = 14057990
55 feet Y = 4284875
52 meter
Z = 16037926
27 Z = 4888359
93
XDOT = -16130
123157 XDOT = -4916
461538
YDOT = -16211
814157 feet/sec YDOT = -4941
360955 meter/sec
ZDOT = 7767
563440 ZDOT = 2367
553336
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 14254
01224188
00016717 00000-0 10270-3 0 9087
2 25544 51
6430 34
2038 0003330 89
0265 271
1267 15
50379469 24641
Satellite: ISS
Catalog Number: 25544
Epoch time: 14254
01224188 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 34
2038 deg
Eccentricity:
0003330
Arg of perigee: 89
0265 deg
Mean anomaly: 271
1267 deg
Mean motion: 15
50379469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2464
Checksum: 292
Coasting Arc #10 (Orbit 2478)
---------------------------------------
Vector Time (GMT): 2014/254/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 45031
93 A = 6789433
40 meter
Y = -4532686
46 meter E =
0016382
Z = -5069424
29 I = 51
80557
XDOT = 7074
767524 Wp = 78
81895
YDOT = 2198
967507 meter/sec RA = 28
94057 deg
ZDOT = -1905
436042 TA = 172
71527
MA = 172
69143
Ha = 228
153 n
mi
Hp = 219
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 147742
55 X = 120339
87
Y = -14871018
57 feet Y = -4531762
42 meter
Z = -16631969
45 Z = -5069022
07
XDOT = 23211
179540 XDOT = 7058
908382
YDOT = 7214
460324 feet/sec YDOT = 2277
993233 meter/sec
ZDOT = -6251
430583 ZDOT = -1871
106465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6384543
68 X = 1946008
91
Y = -13434678
82 feet Y = -4094890
10 meter
Z = -16629444
85 Z = -5068654
79
XDOT = 17200
748234 XDOT = 5242
788062
YDOT = 15723
311198 feet/sec YDOT = 4792
465253 meter/sec
ZDOT = -6105
748941 ZDOT = -1861
032277
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 14254
97910556
00016717 00000-0 10270-3 0 9094
2 25544 51
6435 29
4104 0003432 91
2700 268
8844 15
50382652 24796
Satellite: ISS
Catalog Number: 25544
Epoch time: 14254
97910556 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 29
4104 deg
Eccentricity:
0003432
Arg of perigee: 91
2700 deg
Mean anomaly: 268
8844 deg
Mean motion: 15
50382652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2479
Checksum: 314
Coasting Arc #11 (Orbit 2494)
---------------------------------------
Vector Time (GMT): 2014/255/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -224044
38 A = 6788733
47 meter
Y = 4370047
43 meter E =
0007340
Z = 5184912
54 I = 51
77634
XDOT = -7261
034559 Wp = 110
62761
YDOT = -2030
359578 meter/sec RA = 23
99171 deg
ZDOT = 1393
392741 TA = 325
97347
MA = 326
02052
Ha = 228
041 n
mi
Hp = 219
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -735053
73 X = -298081
38
Y = 14337425
96 feet Y = 4367128
59 meter
Z = 17010867
90 Z = 5183643
87
XDOT = -23822
291859 XDOT = -7244
559641
YDOT = -6661
284706 feet/sec YDOT = -2111
464903 meter/sec
ZDOT = 4571
498494 ZDOT = 1358
159703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6481031
00 X = -1975418
25
Y = 12818299
42 feet Y = 3907017
66 meter
Z = 17004680
27 Z = 5183026
55
XDOT = -18292
525410 XDOT = -5575
561745
YDOT = -15132
909914 feet/sec YDOT = -4612
510942 meter/sec
ZDOT = 4421
952679 ZDOT = 1347
811177
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 14256
01040870
00016717 00000-0 10270-3 0 9106
2 25544 51
6439 24
2988 0003278 92
9101 267
2425 15
50430923 24955
Satellite: ISS
Catalog Number: 25544
Epoch time: 14256
01040870 = yrday
fracday
Element set: 910
Inclination: 51
6439 deg
RA of node: 24
2988 deg
Eccentricity:
0003278
Arg of perigee: 92
9101 deg
Mean anomaly: 267
2425 deg
Mean motion: 15
50430923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2495
Checksum: 295
Coasting Arc #12 (Orbit 2509)
---------------------------------------
Vector Time (GMT): 2014/256/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 453618
16 A = 6788345
57 meter
Y = -4253048
23 meter E =
0017772
Z = -5286877
24 I = 51
74642
XDOT = 7376
415275 Wp = 85
46162
YDOT = 1838
727548 meter/sec RA = 19
03869 deg
ZDOT = -847
358354 TA = 176
43510
MA = 176
42242
Ha = 228
024 n
mi
Hp = 219
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1488248
55 X = 526825
08
Y = -13953570
32 feet Y = -4247566
72 meter
Z = -17345397
78 Z = -5284495
43
XDOT = 24200
837515 XDOT = 7359
422179
YDOT = 6032
570695 feet/sec YDOT = 1921
120306 meter/sec
ZDOT = -2780
047094 ZDOT = -811
566042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6810779
02 X = 2075925
44
Y = -12284484
53 feet Y = -3744310
88 meter
Z = -17334490
52 Z = -5283552
71
XDOT = 19176
688741 XDOT = 5845
054728
YDOT = 14335
392053 feet/sec YDOT = 4369
427498 meter/sec
ZDOT = -2628
095536 ZDOT = -801
043519
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 14256
97724006
00016717 00000-0 10270-3 0 9112
2 25544 51
6442 19
5052 0003313 95
1294 265
0235 15
50435627 25105
Satellite: ISS
Catalog Number: 25544
Epoch time: 14256
97724006 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 19
5052 deg
Eccentricity:
0003313
Arg of perigee: 95
1294 deg
Mean anomaly: 265
0235 deg
Mean motion: 15
50435627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2510
Checksum: 281
Coasting Arc #13 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2014/257/02:10:35
386
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1702791
86 A = 6788754
46 meter
Y = -3863580
29 meter E =
0017169
Z = -5330931
01 I = 51
74440
XDOT = 7159
397608 Wp = 93
18273
YDOT = 2670
812807 meter/sec RA = 18
38108 deg
ZDOT = 351
219730 TA = 180
16902
MA = 180
16960
Ha = 227
999 n
mi
Hp = 219
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5586587
45 X = 1771764
82
Y = -12675788
35 feet Y = -3844153
38 meter
Z = -17489931
13 Z = -5322491
18
XDOT = 23488
837298 XDOT = 7127
293738
YDOT = 8762
509209 feet/sec YDOT = 2750
694349 meter/sec
ZDOT = 1152
295703 ZDOT = 385
921019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -146708
36 X = -44716
71
Y = -13897603
52 feet Y = -4235989
55 meter
Z = -17453319
28 Z = -5319771
72
XDOT = 23977
633538 XDOT = 7308
382702
YDOT = -1884
831747 feet/sec YDOT = -574
496716 meter/sec
ZDOT = 1299
452871 ZDOT = 396
073235
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 14257
10615006
00016717 00000-0 10270-3 0 9128
2 25544 51
6466 18
8668 0002411 97
0072 263
1353 15
50240519 25125
Satellite: ISS
Catalog Number: 25544
Epoch time: 14257
10615006 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 18
8668 deg
Eccentricity:
0002411
Arg of perigee: 97
0072 deg
Mean anomaly: 263
1353 deg
Mean motion: 15
50240519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 277
Coasting Arc #14 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2014/258/02:10:35
386
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1878584
45 A = 6788776
11 meter
Y = 3832320
58 meter E =
0005295
Z = 5275114
32 I = 51
71486
XDOT = -7233
297193 Wp = 74
84130
YDOT = -2400
522553 meter/sec RA = 13
42850 deg
ZDOT = -829
932085 TA = 23
09802
MA = 23
07422
Ha = 227
912 n
mi
Hp = 219
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6163334
82 X = -1946923
61
Y = 12573230
26 feet Y = 3810931
34 meter
Z = 17306805
51 Z = 5265822
11
XDOT = -23731
290002 XDOT = -7201
884845
YDOT = -7875
730162 feet/sec YDOT = -2481
234388 meter/sec
ZDOT = -2722
874293 ZDOT = -864
994027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -177144
84 X = -53993
75
Y = 14051066
89 feet Y = 4282765
19 meter
Z = 17266570
92 Z = 5262850
82
XDOT = -23753
814648 XDOT = -7240
162705
YDOT = 3237
563348 feet/sec YDOT = 986
809309 meter/sec
ZDOT = -2871
608007 ZDOT = -875
266121
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 14258
13755999
00016717 00000-0 10270-3 0 9139
2 25544 51
6463 13
7553 0002243 99
2085 260
9320 15
50296785 25282
Satellite: ISS
Catalog Number: 25544
Epoch time: 14258
13755999 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 13
7553 deg
Eccentricity:
0002243
Arg of perigee: 99
2085 deg
Mean anomaly: 260
9320 deg
Mean motion: 15
50296785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 325
Coasting Arc #15 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2014/259/02:10:35
386
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2069870
60 A = 6789152
56 meter
Y = -3851917
16 meter E =
0016205
Z = -5207716
37 I = 51
68606
XDOT = 7232
895075 Wp = 99
90276
YDOT = 2121
270810 meter/sec RA = 8
47327 deg
ZDOT = 1306
546564 TA = 182
66530
MA = 182
67394
Ha = 227
874 n
mi
Hp = 219
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6790914
05 X = 2138087
21
Y = -12637523
49 feet Y = -3828389
50 meter
Z = -17085683
63 Z = -5197495
24
XDOT = 23729
970720 XDOT = 7202
290184
YDOT = 6959
549903 feet/sec YDOT = 2201
982698 meter/sec
ZDOT = 4286
570093 ZDOT = 1341
608454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 465519
01 X = 141890
19
Y = -14391487
41 feet Y = -4386525
36 meter
Z = -17041492
92 Z = -5194247
04
XDOT = 23247
243702 XDOT = 7085
759880
YDOT = -4497
149416 feet/sec YDOT = -1370
731142 meter/sec
ZDOT = 4435
348927 ZDOT = 1351
894353
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 14259
10449287
00016717 00000-0 10270-3 0 9148
2 25544 51
6469 8
9628 0002310 100
6664 259
4747 15
50293257 25436
Satellite: ISS
Catalog Number: 25544
Epoch time: 14259
10449287 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 8
9628 deg
Eccentricity:
0002310
Arg of perigee: 100
6664 deg
Mean anomaly: 259
4747 deg
Mean motion: 15
50293257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 318
Coasting Arc #16 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2014/260/02:10:35
386
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2270154
93 A = 6789484
63 meter
Y = 3885448
64 meter E =
0007176
Z = 5078958
95 I = 51
65664
XDOT = -7216
393250 Wp = 67
76424
YDOT = -1865
125038 meter/sec RA = 3
51620 deg
ZDOT = -1794
007620 TA = 39
62137
MA = 39
56896
Ha = 227
797 n
mi
Hp = 219
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7448014
86 X = -2338106
08
Y = 12747534
89 feet Y = 3859682
77 meter
Z = 16663251
16 Z = 5067765
53
XDOT = -23675
830874 XDOT = -7186
285959
YDOT = -6119
176633 feet/sec YDOT = -1945
655219 meter/sec
ZDOT = -5885
851773 ZDOT = -1828
990480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -745794
10 X = -227318
04
Y = 14799485
54 feet Y = 4510883
19 meter
Z = 16614918
88 Z = 5064227
28
XDOT = -22688
960855 XDOT = -6915
595269
YDOT = 5648
494384 feet/sec YDOT = 1721
661088 meter/sec
ZDOT = -6034
336286 ZDOT = -1839
265700
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 14260
13586844
00016717 00000-0 10270-3 0 9155
2 25544 51
6468 3
8508 0002169 102
0952 258
0442 15
50351568 25598
Satellite: ISS
Catalog Number: 25544
Epoch time: 14260
13586844 = yrday
fracday
Element set: 915
Inclination: 51
6468 deg
RA of node: 3
8508 deg
Eccentricity:
0002169
Arg of perigee: 102
0952 deg
Mean anomaly: 258
0442 deg
Mean motion: 15
50351568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 307
Coasting Arc #17 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2014/261/02:10:35
386
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2466826
03 A = 6790157
65 meter
Y = -3972344
14 meter E =
0014251
Z = -4936822
81 I = 51
62793
XDOT = 7127
669661 Wp = 105
92898
YDOT = 1614
020945 meter/sec RA = 358
55693 deg
ZDOT = 2264
482253 TA = 186
24234
MA = 186
26012
Ha = 227
736 n
mi
Hp = 219
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8093261
24 X = 2535043
76
Y = -13032625
12 feet Y = -3944377
51 meter
Z = -16196925
24 Z = -4924673
32
XDOT = 23384
742982 XDOT = 7098
091478
YDOT = 5295
344307 feet/sec YDOT = 1693
561980 meter/sec
ZDOT = 7429
403716 ZDOT = 2299
035334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 917184
50 X = 279557
83
Y = -15368932
02 feet Y = -4684450
48 meter
Z = -16144512
50 Z = -4920847
41
XDOT = 21887
834383 XDOT = 6671
411920
YDOT = -6646
549819 feet/sec YDOT = -2025
868385 meter/sec
ZDOT = 7576
100823 ZDOT = 2309
195531
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 14261
10276881
00016717 00000-0 10270-3 0 9161
2 25544 51
6471 359
0580 0002176 104
4080 255
7313 15
50345795 25747
Satellite: ISS
Catalog Number: 25544
Epoch time: 14261
10276881 = yrday
fracday
Element set: 916
Inclination: 51
6471 deg
RA of node: 359
0580 deg
Eccentricity:
0002176
Arg of perigee: 104
4080 deg
Mean anomaly: 255
7313 deg
Mean motion: 15
50345795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 302
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