[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 3rd 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 ET - UTC (sec) : 68 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
332/03:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 217
7
336/14:51:52
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 217
6
338/15:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 217
5
338/16:38:45
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 217
5
Coasting Arc #1 (Orbit 3006)
---------------------------------------
Vector Time (GMT): 2016/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -262250
41 A = 6779465
10 meter
Y = -4443667
70 meter E =
0008465
Z = -5120661
30 I = 51
45901
XDOT = 7156
916742 Wp = 120
79917
YDOT = -2237
194819 meter/sec RA = 333
02400 deg
ZDOT = 1572
574817 TA = 164
42757
MA = 164
40152
Ha = 219
903 n
mi
Hp = 217
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -860401
60 X = -187666
27
Y = -14578962
28 feet Y = -4446183
30 meter
Z = -16800069
87 Z = -5121754
14
XDOT = 23480
697974 XDOT = 7173
762679
YDOT = -7339
878016 feet/sec YDOT = -2157
067188 meter/sec
ZDOT = 5159
366196 ZDOT = 1607
382857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13434737
21 X = 4094907
90
Y = 5715200
94 feet Y = 1741993
25 meter
Z = -16803960
67 Z = -5121847
21
XDOT = -3263
082362 XDOT = -994
587504
YDOT = 23311
794255 feet/sec YDOT = 7105
434889 meter/sec
ZDOT = 5312
180502 ZDOT = 1619
152617
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 16330
51329439
00016717 00000-0 10270-3 0 9006
2 25544 51
6408 333
5634 0006155 255
7021 104
3448 15
53701844 30074
Satellite: ISS
Catalog Number: 25544
Epoch time: 16330
51329439 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 333
5634 deg
Eccentricity:
0006155
Arg of perigee: 255
7021 deg
Mean anomaly: 104
3448 deg
Mean motion: 15
53701844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3007
Checksum: 284
Coasting Arc #2 (Orbit 3022)
---------------------------------------
Vector Time (GMT): 2016/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1188936
46 A = 6781969
09 meter
Y = 4951461
32 meter E =
0003237
Z = 4478551
19 I = 51
43837
XDOT = -6848
341762 Wp = 46
24009
YDOT = 1260
787220 meter/sec RA = 328
01950 deg
ZDOT = -3208
324646 TA = 76
13246
MA = 76
09645
Ha = 219
602 n
mi
Hp = 217
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3900710
17 X = -1265971
90
Y = 16244951
85 feet Y = 4937735
02 meter
Z = 14693409
42 Z = 4472588
51
XDOT = -22468
312868 XDOT = -6846
346256
YDOT = 4136
441010 feet/sec YDOT = 1184
215684 meter/sec
ZDOT = -10525
999496 ZDOT = -3241
587960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13033605
77 X = -3972643
04
Y = -10489735
17 feet Y = -3197271
28 meter
Z = 14666317
11 Z = 4470293
46
XDOT = 4957
328822 XDOT = 1510
993825
YDOT = -21097
236009 feet/sec YDOT = -6430
437536 meter/sec
ZDOT = -10671
848038 ZDOT = -3252
779282
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 16331
54239316
00016717 00000-0 10270-3 0 9015
2 25544 51
6397 328
4362 0006211 260
2317 99
8135 15
53746063 30235
Satellite: ISS
Catalog Number: 25544
Epoch time: 16331
54239316 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 328
4362 deg
Eccentricity:
0006211
Arg of perigee: 260
2317 deg
Mean anomaly: 99
8135 deg
Mean motion: 15
53746063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3023
Checksum: 294
Coasting Arc #3 (Orbit 3032)
---------------------------------------
Vector Time (GMT): 2016/332/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4916785
07 A = 6781447
89 meter
Y = 994753
19 meter E =
0004940
Z = 4564392
74 I = 51
42216
XDOT = -4003
705344 Wp = 162
09868
YDOT = 5783
831015 meter/sec RA = 324
90361 deg
ZDOT = 3046
805445 TA = 257
31609
MA = 257
37131
Ha = 219
557 n
mi
Hp = 217
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16131184
61 X = 4883123
75
Y = 3263625
94 feet Y = 1049547
63 meter
Z = 14975041
81 Z = 4588196
01
XDOT = -13135
516219 XDOT = -4082
884425
YDOT = 18975
823540 feet/sec YDOT = 5738
616085 meter/sec
ZDOT = 9996
080855 ZDOT = 3027
163904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3291050
08 X = -1003112
06
Y = -16028416
80 feet Y = -4885461
44 meter
Z = 15079028
24 Z = 4596087
81
XDOT = 21466
337531 XDOT = 6542
939679
YDOT = 4931
259998 feet/sec YDOT = 1503
048047 meter/sec
ZDOT = 9908
951794 ZDOT = 3020
248507
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 16332
18557813
00016717 00000-0 10270-3 0 9022
2 25544 51
6421 325
2275 0006387 259
0488 100
9946 15
53760299 30332
Satellite: ISS
Catalog Number: 25544
Epoch time: 16332
18557813 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 325
2275 deg
Eccentricity:
0006387
Arg of perigee: 259
0488 deg
Mean anomaly: 100
9946 deg
Mean motion: 15
53760299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3033
Checksum: 318
Coasting Arc #4 (Orbit 3047)
---------------------------------------
Vector Time (GMT): 2016/333/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3850912
76 A = 6779058
51 meter
Y = -2142541
62 meter E =
0007714
Z = -5158153
14 I = 51
38815
XDOT = 4991
820436 Wp = 76
41287
YDOT = -5646
393351 meter/sec RA = 319
89611 deg
ZDOT = -1381
358558 TA = 180
24738
MA = 180
24776
Ha = 219
423 n
mi
Hp = 217
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12634228
22 X = -3801611
51
Y = -7029336
04 feet Y = -2185329
22 meter
Z = -16923074
62 Z = -5176740
64
XDOT = 16377
363636 XDOT = 5061
299028
YDOT = -18524
912570 feet/sec YDOT = -5590
182921 meter/sec
ZDOT = -4532
016265 ZDOT = -1356
940554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1304364
26 X = -397570
22
Y = 14303438
22 feet Y = 4359687
97 meter
Z = -17004000
45 Z = -5182819
34
XDOT = -22566
582517 XDOT = -6878
294351
YDOT = -7317
320768 feet/sec YDOT = -2230
319370 meter/sec
ZDOT = -4424
014060 ZDOT = -1348
439485
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 16333
15035117
00016717 00000-0 10270-3 0 9039
2 25544 51
6421 320
4219 0006240 263
4092 96
6351 15
53749190 30489
Satellite: ISS
Catalog Number: 25544
Epoch time: 16333
15035117 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 320
4219 deg
Eccentricity:
0006240
Arg of perigee: 263
4092 deg
Mean anomaly: 96
6351 deg
Mean motion: 15
53749190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3048
Checksum: 282
Coasting Arc #5 (Orbit 3063)
---------------------------------------
Vector Time (GMT): 2016/334/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2669570
16 A = 6778464
91 meter
Y = 3305875
95 meter E =
0003762
Z = 5284565
61 I = 51
36210
XDOT = -5626
026738 Wp = 278
42266
YDOT = 5190
743713 meter/sec RA = 314
88152 deg
ZDOT = -404
826440 TA = 175
45584
MA = 175
45242
Ha = 219
190 n
mi
Hp = 217
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8758432
29 X = 2606733
97
Y = 10846049
71 feet Y = 3335377
22 meter
Z = 17337813
69 Z = 5297381
54
XDOT = -18458
092974 XDOT = -5681
686314
YDOT = 17029
999060 feet/sec YDOT = 5127
518518 meter/sec
ZDOT = -1328
170736 ZDOT = -432
291663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6159164
01 X = 1877313
19
Y = -12429254
76 feet Y = -3788436
85 meter
Z = 17393246
94 Z = 5301461
67
XDOT = 22338
846579 XDOT = 6808
880437
YDOT = 9040
117309 feet/sec YDOT = 2755
427756 meter/sec
ZDOT = -1449
414054 ZDOT = -441
781404
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 16334
17943650
00016717 00000-0 10270-3 0 9043
2 25544 51
6420 315
2944 0006261 267
3464 92
6972 15
53767722 30648
Satellite: ISS
Catalog Number: 25544
Epoch time: 16334
17943650 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 315
2944 deg
Eccentricity:
0006261
Arg of perigee: 267
3464 deg
Mean anomaly: 92
6972 deg
Mean motion: 15
53767722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3064
Checksum: 315
Coasting Arc #6 (Orbit 3078)
---------------------------------------
Vector Time (GMT): 2016/335/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1465459
09 A = 6779956
95 meter
Y = -4411337
83 meter E =
0006603
Z = -4941687
90 I = 51
34596
XDOT = 5905
853360 Wp = 120
36351
YDOT = -4379
716346 meter/sec RA = 309
86801 deg
ZDOT = 2157
180897 TA = 170
77325
MA = 170
76112
Ha = 219
264 n
mi
Hp = 217
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4807936
64 X = -1392016
47
Y = -14472893
16 feet Y = -4427314
57 meter
Z = -16212886
82 Z = -4948628
80
XDOT = 19376
159317 XDOT = 5943
910704
YDOT = -14369
148117 feet/sec YDOT = -4313
460496 meter/sec
ZDOT = 7077
365149 ZDOT = 2185
962647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10935076
07 X = -3333011
19
Y = 10585248
13 feet Y = 3226383
63 meter
Z = -16242389
71 Z = -4950680
38
XDOT = -20629
556749 XDOT = -6287
888897
YDOT = -10251
340715 feet/sec YDOT = -3124
608650 meter/sec
ZDOT = 7204
205180 ZDOT = 2195
841739
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 16335
14419947
00016717 00000-0 10270-3 0 9059
2 25544 51
6429 310
4890 0006208 270
5579 89
4862 15
53782231 30798
Satellite: ISS
Catalog Number: 25544
Epoch time: 16335
14419947 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 310
4890 deg
Eccentricity:
0006208
Arg of perigee: 270
5579 deg
Mean anomaly: 89
4862 deg
Mean motion: 15
53782231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3079
Checksum: 331
Coasting Arc #7 (Orbit 3094)
---------------------------------------
Vector Time (GMT): 2016/336/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 310590
07 A = 6783137
02 meter
Y = 5358371
09 meter E =
0005035
Z = 4146206
02 I = 51
33656
XDOT = -5875
581338 Wp = 52
58008
YDOT = 3225
288901 meter/sec RA = 304
85783 deg
ZDOT = -3721
958739 TA = 75
89117
MA = 75
83521
Ha = 219
426 n
mi
Hp = 217
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1018996
28 X = 230507
55
Y = 17579957
66 feet Y = 5361396
21 meter
Z = 13603038
11 Z = 4147520
74
XDOT = -19276
841661 XDOT = -5893
130741
YDOT = 10581
656498 feet/sec YDOT = 3159
486387 meter/sec
ZDOT = -12211
150720 ZDOT = -3750
543594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15233888
59 X = 4643289
24
Y = -8825763
88 feet Y = -2690092
83 meter
Z = 13607734
61 Z = 4147637
51
XDOT = 17510
989884 XDOT = 5337
349717
YDOT = 11172
964351 feet/sec YDOT = 3405
519534 meter/sec
ZDOT = -12336
897650 ZDOT = -3760
286404
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 16336
17327443
00016717 00000-0 10270-3 0 9063
2 25544 51
6432 305
3617 0006075 274
9054 85
1405 15
53750497 30953
Satellite: ISS
Catalog Number: 25544
Epoch time: 16336
17327443 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 305
3617 deg
Eccentricity:
0006075
Arg of perigee: 274
9054 deg
Mean anomaly: 85
1405 deg
Mean motion: 15
53750497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3095
Checksum: 310
Coasting Arc #8 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2016/336/14:51:52
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1917055
12 A = 6788533
70 meter
Y = -6157752
71 meter E =
0006443
Z = -2105278
95 I = 51
34419
XDOT = 5343
492003 Wp = 343
16841
YDOT = -214
448983 meter/sec RA = 302
42868 deg
ZDOT = 5494
821593 TA = 353
41691
MA = 353
42537
Ha = 219
679 n
mi
Hp = 217
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6289550
93 X = 1995996
87
Y = -20202600
77 feet Y = -6135873
35 meter
Z = -6907083
17 Z = -2095775
04
XDOT = 17531
141741 XDOT = 5318
801091
YDOT = -703
572780 feet/sec YDOT = -154
832988 meter/sec
ZDOT = 18027
629898 ZDOT = 5520
719263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21072061
36 X = 6422764
30
Y = -2064289
80 feet Y = -629195
53 meter
Z = -6864274
48 Z = -2092230
86
XDOT = 7300
397169 XDOT = 2225
161057
YDOT = 14218
348886 feet/sec YDOT = 4333
752741 meter/sec
ZDOT = 18141
022062 ZDOT = 5529
383524
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 16336
62349243
00016717 00000-0 10270-3 0 9076
2 25544 51
6415 303
1219 0006228 282
1832 77
8623 15
53763262 31026
Satellite: ISS
Catalog Number: 25544
Epoch time: 16336
62349243 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 303
1219 deg
Eccentricity:
0006228
Arg of perigee: 282
1832 deg
Mean anomaly: 77
8623 deg
Mean motion: 15
53763262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3102
Checksum: 296
Coasting Arc #9 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2016/337/14:51:52
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2715041
28 A = 6790248
41 meter
Y = 6193810
13 meter E =
0007741
Z = 555450
59 I = 51
33436
XDOT = -4599
314783 Wp = 148
10055
YDOT = -1479
381905 meter/sec RA = 297
43836 deg
ZDOT = -5953
276158 TA = 25
88160
MA = 25
84290
Ha = 219
841 n
mi
Hp = 217
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8907615
76 X = -2786798
43
Y = 20320899
37 feet Y = 6163047
45 meter
Z = 1822344
45 Z = 542087
72
XDOT = -15089
615429 XDOT = -4553
511426
YDOT = -4853
615174 feet/sec YDOT = -1530
557925 meter/sec
ZDOT = -19531
745926 ZDOT = -5975
507546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22192023
51 X = -6764128
77
Y = 112593
26 feet Y = 34318
43 meter
Z = 1762646
91 Z = 537254
78
XDOT = -1638
737918 XDOT = -499
487317
YDOT = -14025
977284 feet/sec YDOT = -4275
117876 meter/sec
ZDOT = -19628
762735 ZDOT = -5982
846882
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 16337
65255980
00016717 00000-0 10270-3 0 9085
2 25544 51
6424 297
9955 0006226 285
3418 74
7046 15
53770019 31186
Satellite: ISS
Catalog Number: 25544
Epoch time: 16337
65255980 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 297
9955 deg
Eccentricity:
0006226
Arg of perigee: 285
3418 deg
Mean anomaly: 74
7046 deg
Mean motion: 15
53770019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3118
Checksum: 335
Coasting Arc #10 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2016/338/14:51:52
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3306814
60 A = 6789879
37 meter
Y = -5830633
74 meter E =
0011033
Z = 1036512
55 I = 51
31922
XDOT = 3770
050949 Wp = 29
13974
YDOT = 3184
913146 meter/sec RA = 292
44814 deg
ZDOT = 5871
252175 TA = 342
14923
MA = 342
18795
Ha = 219
988 n
mi
Hp = 217
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10849129
27 X = 3366733
51
Y = -19129375
79 feet Y = -5793319
77 meter
Z = 3400631
72 Z = 1052721
39
XDOT = 12368
933559 XDOT = 3705
636069
YDOT = 10449
190112 feet/sec YDOT = 3226
711759 meter/sec
ZDOT = 19262
638370 ZDOT = 5889
410035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21911638
61 X = 6678667
45
Y = 1738196
09 feet Y = 529802
17 meter
Z = 3472706
13 Z = 1058480
83
XDOT = -4177
735732 XDOT = -1273
373851
YDOT = 13913
563066 feet/sec YDOT = 4240
854023 meter/sec
ZDOT = 19341
500872 ZDOT = 5895
289466
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 16338
68162130
00016717 00000-0 10270-3 0 9094
2 25544 51
6424 292
8684 0006301 289
8205 70
2268 15
53777034 31345
Satellite: ISS
Catalog Number: 25544
Epoch time: 16338
68162130 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 292
8684 deg
Eccentricity:
0006301
Arg of perigee: 289
8205 deg
Mean anomaly: 70
2268 deg
Mean motion: 15
53777034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 313
Coasting Arc #11 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2016/338/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4563833
84 A = 6784731
30 meter
Y = -3488655
39 meter E =
0006097
Z = 3603813
36 I = 51
30228
XDOT = 1250
847731 Wp = 78
21207
YDOT = 6167
975128 meter/sec RA = 292
43563 deg
ZDOT = 4381
738522 TA = 324
70372
MA = 324
74407
Ha = 219
881 n
mi
Hp = 217
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14973208
15 X = 4584999
82
Y = -11445719
77 feet Y = -3437501
47 meter
Z = 11823534
63 Z = 3626034
58
XDOT = 4103
831138 XDOT = 1160
498174
YDOT = 20236
138873 feet/sec YDOT = 6181
457427 meter/sec
ZDOT = 14375
782553 ZDOT = 4387
595899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16961744
97 X = 5169939
87
Y = 8073111
27 feet Y = 2460684
32 meter
Z = 11921472
92 Z = 3633664
95
XDOT = -15619
471652 XDOT = -4760
814960
YDOT = 11527
707811 feet/sec YDOT = 3513
645341 meter/sec
ZDOT = 14400
228390 ZDOT = 4389
189613
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 16338
68162098
00016717 00000-0 10270-3 0 9109
2 25544 51
6426 292
8685 0006258 289
4478 70
5998 15
53784477 31349
Satellite: ISS
Catalog Number: 25544
Epoch time: 16338
68162098 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 292
8685 deg
Eccentricity:
0006258
Arg of perigee: 289
4478 deg
Mean anomaly: 70
5998 deg
Mean motion: 15
53784477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 362
Coasting Arc #12 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2016/338/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4616274
99 A = 6780180
90 meter
Y = -1010993
17 meter E =
0001432
Z = 4862605
72 I = 51
28761
XDOT = -898
827478 Wp = 184
79614
YDOT = 7239
947237 meter/sec RA = 292
08590 deg
ZDOT = 2357
212940 TA = 241
99161
MA = 242
00610
Ha = 219
886 n
mi
Hp = 217
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15145259
15 X = 4603616
52
Y = -3316906
71 feet Y = -959442
04 meter
Z = 15953430
84 Z = 4884999
72
XDOT = -2948
909047 XDOT = -991
170005
YDOT = 23753
107733 feet/sec YDOT = 7229
379442 meter/sec
ZDOT = 7733
638255 ZDOT = 2352
622916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13866943
85 X = 4226644
49
Y = 6704119
02 feet Y = 2043415
48 meter
Z = 16051646
55 Z = 4892541
87
XDOT = -16566
944797 XDOT = -5049
604774
YDOT = 15791
699787 feet/sec YDOT = 4813
310095 meter/sec
ZDOT = 7712
148833 ZDOT = 2350
662964
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 16338
74593645
00016717 00000-0 10270-3 0 9113
2 25544 51
6441 292
5488 0006281 289
5502 70
4972 15
53784082 31353
Satellite: ISS
Catalog Number: 25544
Epoch time: 16338
74593645 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 292
5488 deg
Eccentricity:
0006281
Arg of perigee: 289
5502 deg
Mean anomaly: 70
4972 deg
Mean motion: 15
53784082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 330
Coasting Arc #13 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2016/339/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4239019
02 A = 6778357
02 meter
Y = -580859
21 meter E =
0009587
Z = -5265313
28 I = 51
27008
XDOT = 1773
011039 Wp = 66
73096
YDOT = -7428
848616 meter/sec RA = 287
06620 deg
ZDOT = -605
046835 TA = 197
44231
MA = 197
47527
Ha = 220
146 n
mi
Hp = 217
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13907542
72 X = -4206631
96
Y = -1905706
08 feet Y = -628081
33 meter
Z = -17274649
86 Z = -5285826
81
XDOT = 5816
965352 XDOT = 1858
889621
YDOT = -24372
862915 feet/sec YDOT = -7408
541399 meter/sec
ZDOT = -1985
061794 ZDOT = -596
225880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9827092
10 X = -2995297
67
Y = -9867789
05 feet Y = -3007702
10 meter
Z = -17364330
92 Z = -5292648
06
XDOT = 18672
821694 XDOT = 5691
476052
YDOT = -15156
833394 feet/sec YDOT = -4619
802818 meter/sec
ZDOT = -1945
031487 ZDOT = -592
845597
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 16339
71067356
00016717 00000-0 10270-3 0 9127
2 25544 51
6435 287
7424 0006377 293
9863 66
0622 15
53823722 31502
Satellite: ISS
Catalog Number: 25544
Epoch time: 16339
71067356 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 287
7424 deg
Eccentricity:
0006377
Arg of perigee: 293
9863 deg
Mean anomaly: 66
0622 deg
Mean motion: 15
53823722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 323
Coasting Arc #14 (Orbit 3165)
---------------------------------------
Vector Time (GMT): 2016/340/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3776911
29 A = 6778689
12 meter
Y = 2211244
07 meter E =
0005708
Z = 5179471
18 I = 51
26202
XDOT = -2515
270496 Wp = 335
50832
YDOT = 7139
572031 meter/sec RA = 282
04406 deg
ZDOT = -1209
279694 TA = 126
18623
MA = 126
13343
Ha = 220
266 n
mi
Hp = 217
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12391441
25 X = 3726744
20
Y = 7254737
75 feet Y = 2253199
24 meter
Z = 16993015
69 Z = 5197696
78
XDOT = -8252
199791 XDOT = -2589
045911
YDOT = 23423
792753 feet/sec YDOT = 7111
032149 meter/sec
ZDOT = -3967
453063 ZDOT = -1221
677075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5610645
94 X = 1710124
88
Y = 13114731
84 feet Y = 3997370
26 meter
Z = 17072377
67 Z = 5203660
71
XDOT = -19530
895794 XDOT = -5953
017038
YDOT = 13612
334118 feet/sec YDOT = 4149
039439 meter/sec
ZDOT = -4023
068097 ZDOT = -1226
231156
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 16340
73972054
00016717 00000-0 10270-3 0 9132
2 25544 51
6428 282
6156 0006429 296
9742 63
0754 15
53840281 31666
Satellite: ISS
Catalog Number: 25544
Epoch time: 16340
73972054 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 282
6156 deg
Eccentricity:
0006429
Arg of perigee: 296
9742 deg
Mean anomaly: 63
0754 deg
Mean motion: 15
53840281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3166
Checksum: 322
Coasting Arc #15 (Orbit 3180)
---------------------------------------
Vector Time (GMT): 2016/341/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3277955
01 A = 6781046
95 meter
Y = -3727344
54 meter E =
0004242
Z = -4623801
30 I = 51
26372
XDOT = 3134
026203 Wp = 92
95162
YDOT = -6360
754968 meter/sec RA = 277
02435 deg
ZDOT = 2907
834730 TA = 206
14243
MA = 206
16386
Ha = 220
427 n
mi
Hp = 217
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10754445
57 X = -3213570
77
Y = -12228820
68 feet Y = -3763640
65 meter
Z = -15169951
78 Z = -4639568
60
XDOT = 10282
238200 XDOT = 3190
795825
YDOT = -20868
618660 feet/sec YDOT = -6325
390883 meter/sec
ZDOT = 9540
140190 ZDOT = 2923
196710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1636197
23 X = -498712
92
Y = -16138381
77 feet Y = -4918978
76 meter
Z = -15238276
94 Z = -4644626
81
XDOT = 19218
002431 XDOT = 5857
647141
YDOT = -11014
604025 feet/sec YDOT = -3357
251307 meter/sec
ZDOT = 9608
572237 ZDOT = 2928
692818
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 16341
70444770
00016717 00000-0 10270-3 0 9140
2 25544 51
6425 277
8087 0006488 300
6187 59
4325 15
53833135 31813
Satellite: ISS
Catalog Number: 25544
Epoch time: 16341
70444770 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 277
8087 deg
Eccentricity:
0006488
Arg of perigee: 300
6187 deg
Mean anomaly: 59
4325 deg
Mean motion: 15
53833135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3181
Checksum: 317
Coasting Arc #16 (Orbit 3196)
---------------------------------------
Vector Time (GMT): 2016/342/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2733887
00 A = 6784452
64 meter
Y = 5038447
13 meter E =
0007999
Z = 3627607
67 I = 51
27284
XDOT = -3671
748194 Wp = 53
83900
YDOT = 5133
225954 meter/sec RA = 272
01189 deg
ZDOT = -4351
096057 TA = 82
88951
MA = 82
79856
Ha = 220
706 n
mi
Hp = 216
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8969445
54 X = 2659721
17
Y = 16530338
36 feet Y = 5068604
49 meter
Z = 11901599
97 Z = 3640708
29
XDOT = -12046
417959 XDOT = -3707
740502
YDOT = 16841
292500 feet/sec YDOT = 5091
964889 meter/sec
ZDOT = -14275
249532 ZDOT = -4369
019838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1966873
28 X = -599502
98
Y = 18667841
26 feet Y = 5689958
02 meter
Z = 11958019
62 Z = 3644804
38
XDOT = -18002
007967 XDOT = -5487
012028
YDOT = 7322
210825 feet/sec YDOT = 2231
809859 meter/sec
ZDOT = -14354
657306 ZDOT = -4375
299547
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 16342
73348079
00016717 00000-0 10270-3 0 9150
2 25544 51
6429 272
6810 0006626 305
6297 54
4238 15
53870122 31977
Satellite: ISS
Catalog Number: 25544
Epoch time: 16342
73348079 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 272
6810 deg
Eccentricity:
0006626
Arg of perigee: 305
6297 deg
Mean anomaly: 54
4238 deg
Mean motion: 15
53870122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3197
Checksum: 321
Coasting Arc #17 (Orbit 3211)
---------------------------------------
Vector Time (GMT): 2016/343/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2164349
09 A = 6787909
26 meter
Y = -6000334
56 meter E =
0008253
Z = -2305471
26 I = 51
28199
XDOT = 4138
131577 Wp = 352
69041
YDOT = -3560
053378 meter/sec RA = 267
00817 deg
ZDOT = 5386
652670 TA = 341
48285
MA = 341
51286
Ha = 220
816 n
mi
Hp = 216
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7100882
83 X = -2085891
87
Y = -19686137
01 feet Y = -6024099
02 meter
Z = -7563882
09 Z = -2315794
81
XDOT = 13576
547169 XDOT = 4151
467212
YDOT = -11679
965150 feet/sec YDOT = -3513
703594 meter/sec
ZDOT = 17672
744981 ZDOT = 5406
787126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4916179
36 X = 1498451
47
Y = -20325566
49 feet Y = -6195232
67 meter
Z = -7607980
45 Z = -2318912
44
XDOT = 16180
981371 XDOT = 4931
963122
YDOT = -2727
312482 feet/sec YDOT = -831
284844 meter/sec
ZDOT = 17761
535303 ZDOT = 5413
715960
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 16343
69819516
00016717 00000-0 10270-3 0 9166
2 25544 51
6410 267
8735 0006568 308
4488 51
6075 15
53831975 32126
Satellite: ISS
Catalog Number: 25544
Epoch time: 16343
69819516 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 267
8735 deg
Eccentricity:
0006568
Arg of perigee: 308
4488 deg
Mean anomaly: 51
6075 deg
Mean motion: 15
53831975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3212
Checksum: 336
Coasting Arc #18 (Orbit 3227)
---------------------------------------
Vector Time (GMT): 2016/344/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1528391
57 A = 6789908
76 meter
Y = 6569939
21 meter E =
0006842
Z = 749592
44 I = 51
29192
XDOT = -4547
593941 Wp = 122
24926
YDOT = 1737
591332 meter/sec RA = 262
01323 deg
ZDOT = -5920
905944 TA = 49
61397
MA = 49
55427
Ha = 221
002 n
mi
Hp = 216
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5014408
02 X = 1451169
99
Y = 21554918
67 feet Y = 6586598
91 meter
Z = 2459292
79 Z = 756829
72
XDOT = -14919
927628 XDOT = -4537
924623
YDOT = 5700
758962 feet/sec YDOT = 1686
791343 meter/sec
ZDOT = -19425
544437 ZDOT = -5942
973715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7299903
66 X = -2225010
63
Y = 20888257
18 feet Y = 6366740
79 meter
Z = 2489788
37 Z = 758887
49
XDOT = -14025
498905 XDOT = -4274
972066
YDOT = -2560
591431 feet/sec YDOT = -780
468268 meter/sec
ZDOT = -19522
466006 ZDOT = -5950
447639
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 16344
72721776
00016717 00000-0 10270-3 0 9172
2 25544 51
6415 262
7467 0006496 311
9177 48
1421 15
53844474 32282
Satellite: ISS
Catalog Number: 25544
Epoch time: 16344
72721776 = yrday
fracday
Element set: 917
Inclination: 51
6415 deg
RA of node: 262
7467 deg
Eccentricity:
0006496
Arg of perigee: 311
9177 deg
Mean anomaly: 48
1421 deg
Mean motion: 15
53844474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3228
Checksum: 328
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