[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 7th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 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
344/13:26:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 216
7
345/20:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 216
4
348/10:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 216
1
349/01:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 215
9
352/04:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 3162)
---------------------------------------
Vector Time (GMT): 2016/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3878480
33 A = 6778566
71 meter
Y = 1875064
60 meter E =
0005286
Z = 5236488
93 I = 51
26071
XDOT = -2364
576739 Wp = 329
43568
YDOT = 7243
637855 meter/sec RA = 283
01467 deg
ZDOT = -838
320967 TA = 128
64759
MA = 128
60027
Ha = 220
337 n
mi
Hp = 217
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12724673
01 X = 3831787
97
Y = 6151786
75 feet Y = 1918175
00 meter
Z = 17180081
78 Z = 5255216
35
XDOT = -7757
797701 XDOT = -2441
329005
YDOT = 23765
216061 feet/sec YDOT = 7216
766470 meter/sec
ZDOT = -2750
396873 ZDOT = -849
993521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9416937
28 X = -2870282
48
Y = 10405378
78 feet Y = 3171559
45 meter
Z = 17261702
65 Z = 5261366
97
XDOT = -19918
117328 XDOT = -6071
042162
YDOT = -13354
096956 feet/sec YDOT = -4070
328752 meter/sec
ZDOT = -2802
861714 ZDOT = -854
312251
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
54678914
00016717 00000-0 10270-3 0 9005
2 25544 51
6410 283
5754 0006271 297
6303 62
4213 15
53794153 31633
Satellite: ISS
Catalog Number: 25544
Epoch time: 16340
54678914 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 283
5754 deg
Eccentricity:
0006271
Arg of perigee: 297
6303 deg
Mean anomaly: 62
4213 deg
Mean motion: 15
53794153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3163
Checksum: 302
Coasting Arc #2 (Orbit 3177)
---------------------------------------
Vector Time (GMT): 2016/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3390837
44 A = 6780514
51 meter
Y = -3419403
05 meter E =
0005381
Z = -4778216
79 I = 51
26092
XDOT = 3003
446964 Wp = 94
03951
YDOT = -6565
508857 meter/sec RA = 277
99411 deg
ZDOT = 2569
187599 TA = 201
40490
MA = 201
42741
Ha = 220
439 n
mi
Hp = 217
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11124794
76 X = -3329138
21
Y = -11218513
94 feet Y = -3456976
48 meter
Z = -15676564
27 Z = -4794538
96
XDOT = 9853
828622 XDOT = 3064
160910
YDOT = -21540
383389 feet/sec YDOT = -6531
582935 meter/sec
ZDOT = 8429
093174 ZDOT = 2583
924809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13711302
77 X = 4179205
08
Y = -7706566
70 feet Y = -2348961
53 meter
Z = -15747373
96 Z = -4799799
58
XDOT = 17667
122155 XDOT = 5384
938833
YDOT = 14089
014412 feet/sec YDOT = 4294
331593 meter/sec
ZDOT = 8494
831112 ZDOT = 2589
224523
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
51152249
00016717 00000-0 10270-3 0 9012
2 25544 51
6410 278
7687 0006320 300
3465 59
7062 15
53803447 31784
Satellite: ISS
Catalog Number: 25544
Epoch time: 16341
51152249 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 278
7687 deg
Eccentricity:
0006320
Arg of perigee: 300
3465 deg
Mean anomaly: 59
7062 deg
Mean motion: 15
53803447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3178
Checksum: 300
Coasting Arc #3 (Orbit 3193)
---------------------------------------
Vector Time (GMT): 2016/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2857520
54 A = 6783817
31 meter
Y = 4783977
14 meter E =
0007934
Z = 3868164
63 I = 51
26920
XDOT = -3557
267788 Wp = 47
39863
YDOT = 5430
140418 meter/sec RA = 272
98046 deg
ZDOT = -4077
274624 TA = 85
63207
MA = 85
54143
Ha = 220
703 n
mi
Hp = 217
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9375067
39 X = 2785022
55
Y = 15695463
07 feet Y = 4815526
37 meter
Z = 12690828
83 Z = 3881869
87
XDOT = -11670
826077 XDOT = -3597
918901
YDOT = 17815
421319 feet/sec YDOT = 5390
133498 meter/sec
ZDOT = -13376
885250 ZDOT = -4094
653574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17493683
95 X = -5332074
87
Y = 5167846
60 feet Y = 1575159
64 meter
Z = 12749939
97 Z = 3886181
70
XDOT = -14060
127297 XDOT = -4285
526800
YDOT = -14316
105380 feet/sec YDOT = -4363
548920 meter/sec
ZDOT = -13453
964625 ZDOT = -4100
768418
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
54056501
00016717 00000-0 10270-3 0 9021
2 25544 51
6416 273
6416 0006398 304
8954 55
1596 15
53823673 31944
Satellite: ISS
Catalog Number: 25544
Epoch time: 16342
54056501 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 273
6416 deg
Eccentricity:
0006398
Arg of perigee: 304
8954 deg
Mean anomaly: 55
1596 deg
Mean motion: 15
53823673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3194
Checksum: 319
Coasting Arc #4 (Orbit 3208)
---------------------------------------
Vector Time (GMT): 2016/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2301442
42 A = 6787312
91 meter
Y = -5821224
15 meter E =
0007071
Z = -2612277
05 I = 51
27939
XDOT = 4035
995980 Wp = 352
54907
YDOT = -3928
558628 meter/sec RA = 267
97561 deg
ZDOT = 5203
985892 TA = 337
87182
MA = 337
90232
Ha = 220
829 n
mi
Hp = 216
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7550664
09 X = -2223487
54
Y = -19098504
44 feet Y = -5846524
49 meter
Z = -8570462
77 Z = -2623267
78
XDOT = 13241
456626 XDOT = 4054
347265
YDOT = -12888
971878 feet/sec YDOT = -3883
322945 meter/sec
ZDOT = 17073
444529 ZDOT = 5223
636356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20305241
89 X = 6189037
73
Y = -2941745
71 feet Y = -896644
09 meter
Z = -8617512
18 Z = -2626617
71
XDOT = 9338
847420 XDOT = 2846
480694
YDOT = 14242
728030 feet/sec YDOT = 4341
183503 meter/sec
ZDOT = 17160
184264 ZDOT = 5230
424164
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
50528779
00016717 00000-0 10270-3 0 9030
2 25544 51
6409 268
8349 0006373 309
0129 51
0456 15
53815061 32090
Satellite: ISS
Catalog Number: 25544
Epoch time: 16343
50528779 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 268
8349 deg
Eccentricity:
0006373
Arg of perigee: 309
0129 deg
Mean anomaly: 51
0456 deg
Mean motion: 15
53815061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3209
Checksum: 314
Coasting Arc #5 (Orbit 3224)
---------------------------------------
Vector Time (GMT): 2016/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1683070
05 A = 6789693
26 meter
Y = 6482704
67 meter E =
0007430
Z = 1095625
11 I = 51
29044
XDOT = -4459
926314 Wp = 115
16809
YDOT = 2151
593570 meter/sec RA = 262
97912 deg
ZDOT = -5851
420817 TA = 52
89200
MA = 52
82412
Ha = 221
022 n
mi
Hp = 216
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5521883
35 X = 1605131
56
Y = 21268716
11 feet Y = 6501090
08 meter
Z = 3594570
56 Z = 1103612
02
XDOT = -14632
304181 XDOT = -4455
230540
YDOT = 7059
034023 feet/sec YDOT = 2101
746117 meter/sec
ZDOT = -19197
574860 ZDOT = -5873
074774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21950617
68 X = -6690548
27
Y = 880791
77 feet Y = 268465
33 meter
Z = 3628361
54 Z = 1105924
60
XDOT = -3768
722491 XDOT = -1148
706615
YDOT = -14070
298697 feet/sec YDOT = -4288
627043 meter/sec
ZDOT = -19292
759615 ZDOT = -5880
433131
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
53432106
00016717 00000-0 10270-3 0 9043
2 25544 51
6419 263
7078 0006359 312
2534 47
8078 15
53824531 32257
Satellite: ISS
Catalog Number: 25544
Epoch time: 16344
53432106 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 263
7078 deg
Eccentricity:
0006359
Arg of perigee: 312
2534 deg
Mean anomaly: 47
8078 deg
Mean motion: 15
53824531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3225
Checksum: 304
Coasting Arc #6 (Orbit 3225)
---------------------------------------
Vector Time (GMT): 2016/344/13:26:46
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3105497
77 A = 6786349
28 meter
Y = 5227958
34 meter E =
0008797
Z = 3009263
85 I = 51
27987
XDOT = -3353
264832 Wp = 71
94913
YDOT = 4830
918627 meter/sec RA = 262
66483 deg
ZDOT = -4917
630905 TA = 73
40599
MA = 73
30940
Ha = 221
009 n
mi
Hp = 216
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10188640
96 X = 3032188
73
Y = 17152094
29 feet Y = 5262276
11 meter
Z = 9872912
90 Z = 3024171
85
XDOT = -11001
525039 XDOT = -3383
148199
YDOT = 15849
470561 feet/sec YDOT = 4793
253236 meter/sec
ZDOT = -16133
959662 ZDOT = -4933
992826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15234635
23 X = -4643516
82
Y = 12830997
44 feet Y = 3910888
02 meter
Z = 9937230
33 Z = 3028867
81
XDOT = -16501
122958 XDOT = -5029
542278
YDOT = -7004
084951 feet/sec YDOT = -2134
845093 meter/sec
ZDOT = -16206
462092 ZDOT = -4939
729645
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
59863578
00016717 00000-0 10270-3 0 9051
2 25544 51
6423 263
3884 0006279 312
2696 47
7924 15
53816988 32260
Satellite: ISS
Catalog Number: 25544
Epoch time: 16344
59863578 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 263
3884 deg
Eccentricity:
0006279
Arg of perigee: 312
2696 deg
Mean anomaly: 47
7924 deg
Mean motion: 15
53816988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3226
Checksum: 355
Coasting Arc #7 (Orbit 3240)
---------------------------------------
Vector Time (GMT): 2016/345/13:26:46
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2609577
36 A = 6789064
24 meter
Y = -6060898
26 meter E =
0010974
Z = -1565757
48 I = 51
29576
XDOT = 3992
130552 Wp = 2
13375
YDOT = -3193
037793 meter/sec RA = 257
66531 deg
ZDOT = 5718
504711 TA = 340
65837
MA = 340
69999
Ha = 221
058 n
mi
Hp = 216
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8561605
50 X = -2534003
01
Y = -19884836
81 feet Y = -6089657
67 meter
Z = -5136999
61 Z = -1578251
04
XDOT = 13097
541182 XDOT = 3999
760824
YDOT = -10475
845778 feet/sec YDOT = -3148
352709 meter/sec
ZDOT = 18761
498396 ZDOT = 5737
916119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17989865
61 X = 5483311
04
Y = -12021602
31 feet Y = -3664184
38 meter
Z = -5190607
07 Z = -1582097
04
XDOT = 11794
223812 XDOT = 3594
879418
YDOT = 9528
859296 feet/sec YDOT = 2904
396313 meter/sec
ZDOT = 18847
053890 ZDOT = 5744
582026
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 16345
56334734
00016717 00000-0 10270-3 0 9067
2 25544 51
6437 258
5808 0006465 315
5701 44
4933 15
53854341 32413
Satellite: ISS
Catalog Number: 25544
Epoch time: 16345
56334734 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 258
5808 deg
Eccentricity:
0006465
Arg of perigee: 315
5701 deg
Mean anomaly: 44
4933 deg
Mean motion: 15
53854341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3241
Checksum: 314
Coasting Arc #8 (Orbit 3245)
---------------------------------------
Vector Time (GMT): 2016/345/20:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4427349
39 A = 6779416
30 meter
Y = -1186111
89 meter E =
0008267
Z = -5002061
35 I = 51
26338
XDOT = -218
757034 Wp = 83
23953
YDOT = -7405
707175 meter/sec RA = 256
09726 deg
ZDOT = 1953
442584 TA = 205
81710
MA = 205
85838
Ha = 220
922 n
mi
Hp = 216
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14525424
52 X = -4389458
75
Y = -3891443
21 feet Y = -1235409
36 meter
Z = -16410962
45 Z = -5023476
63
XDOT = -717
706803 XDOT = -145
417366
YDOT = -24296
939550 feet/sec YDOT = -7407
743499 meter/sec
ZDOT = 6408
932361 ZDOT = 1952
557647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14200233
73 X = -4328231
24
Y = 4626619
10 feet Y = 1410193
50 meter
Z = -16504506
47 Z = -5030573
57
XDOT = -13586
313165 XDOT = -4141
108253
YDOT = -18889
858958 feet/sec YDOT = -5757
629010 meter/sec
ZDOT = 6406
385579 ZDOT = 1952
666324
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 16345
88491738
00016717 00000-0 10270-3 0 9071
2 25544 51
6414 256
9741 0006010 314
6371 45
4291 15
53851938 32467
Satellite: ISS
Catalog Number: 25544
Epoch time: 16345
88491738 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 256
9741 deg
Eccentricity:
0006010
Arg of perigee: 314
6371 deg
Mean anomaly: 45
4291 deg
Mean motion: 15
53851938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3246
Checksum: 322
Coasting Arc #9 (Orbit 3261)
---------------------------------------
Vector Time (GMT): 2016/346/20:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4530828
00 A = 6782509
44 meter
Y = 2741355
20 meter E =
0009184
Z = 4237646
10 I = 51
28185
XDOT = -721
682642 Wp = 37
66368
YDOT = 6741
403511 meter/sec RA = 251
08056 deg
ZDOT = -3578
168847 TA = 89
13104
MA = 89
02581
Ha = 221
142 n
mi
Hp = 216
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14864921
25 X = 4479251
78
Y = 8993947
52 feet Y = 2791733
27 meter
Z = 13903038
38 Z = 4259530
96
XDOT = -2367
725204 XDOT = -779
631675
YDOT = 22117
465586 feet/sec YDOT = 6733
009430 meter/sec
ZDOT = -11739
399104 ZDOT = -3581
814889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17276568
42 X = 5265898
05
Y = -846928
58 feet Y = -258143
83 meter
Z = 13998369
47 Z = 4266703
01
XDOT = 10454
144528 XDOT = 3186
423252
YDOT = 18331
009150 feet/sec YDOT = 5587
291589 meter/sec
ZDOT = -11756
564099 ZDOT = -3583
400737
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 16346
91393880
00016717 00000-0 10270-3 0 9086
2 25544 51
6412 251
8464 0005923 318
5767 41
4935 15
53820999 32627
Satellite: ISS
Catalog Number: 25544
Epoch time: 16346
91393880 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 251
8464 deg
Eccentricity:
0005923
Arg of perigee: 318
5767 deg
Mean anomaly: 41
4935 deg
Mean motion: 15
53820999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3262
Checksum: 337
Coasting Arc #10 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2016/347/20:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4496872
50 A = 6786037
97 meter
Y = -4028016
92 meter E =
0005969
Z = -3092334
49 I = 51
30566
XDOT = 1742
124364 Wp = 6
04858
YDOT = -5669
900643 meter/sec RA = 246
07460 deg
ZDOT = 4858
796247 TA = 318
21124
MA = 318
25681
Ha = 221
225 n
mi
Hp = 216
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14753518
72 X = -4436474
58
Y = -13215278
61 feet Y = -4077965
96 meter
Z = -10145454
36 Z = -3114033
11
XDOT = 5715
631117 XDOT = 1781
794980
YDOT = -18602
036231 feet/sec YDOT = -5650
197708 meter/sec
ZDOT = 15940
932570 ZDOT = 4867
354937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19616976
62 X = -5979254
47
Y = -2358348
52 feet Y = -718824
63 meter
Z = -10239754
30 Z = -3121077
11
XDOT = -6284
520335 XDOT = -1915
521798
YDOT = -17011
650169 feet/sec YDOT = -5185
150971 meter/sec
ZDOT = 15979
413826 ZDOT = 4870
525334
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 16347
87864143
00016717 00000-0 10270-3 0 9098
2 25544 51
6416 247
0402 0006120 321
9725 38
0994 15
53838917 32774
Satellite: ISS
Catalog Number: 25544
Epoch time: 16347
87864143 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 247
0402 deg
Eccentricity:
0006120
Arg of perigee: 321
9725 deg
Mean anomaly: 38
0994 deg
Mean motion: 15
53838917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 326
Coasting Arc #11 (Orbit 3285)
---------------------------------------
Vector Time (GMT): 2016/348/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3901856
22 A = 6789377
18 meter
Y = -5389252
69 meter E =
0012549
Z = -1311656
01 I = 51
32507
XDOT = 3288
917354 Wp = 8
37471
YDOT = -3788
847863 meter/sec RA = 243
17422 deg
ZDOT = 5802
862407 TA = 337
28111
MA = 337
33660
Ha = 221
503 n
mi
Hp = 216
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12801365
55 X = -3834930
71
Y = -17681275
22 feet Y = -5432511
52 meter
Z = -4303333
36 Z = -1330448
44
XDOT = 10790
411266 XDOT = 3302
852755
YDOT = -12430
603226 feet/sec YDOT = -3751
991700 meter/sec
ZDOT = 19038
262490 ZDOT = 5818
872706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21390247
56 X = 6519747
46
Y = -4272359
91 feet Y = -1302215
30 meter
Z = -4384675
74 Z = -1336449
16
XDOT = 6562
140093 XDOT = 2000
140300
YDOT = 13306
444904 feet/sec YDOT = 4055
804407 meter/sec
ZDOT = 19109
041748 ZDOT = 5824
435925
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 16348
45746224
00016717 00000-0 10270-3 0 9104
2 25544 51
6420 244
1606 0006544 326
8229 33
2513 15
53851511 32865
Satellite: ISS
Catalog Number: 25544
Epoch time: 16348
45746224 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 244
1606 deg
Eccentricity:
0006544
Arg of perigee: 326
8229 deg
Mean anomaly: 33
2513 deg
Mean motion: 15
53851511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3286
Checksum: 293
Coasting Arc #12 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2016/349/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1477895
66 A = 6787894
36 meter
Y = 6223569
81 meter E =
0001460
Z = -2274105
25 I = 51
32952
XDOT = -5387
360984 Wp = 39
72110
YDOT = -694
870548 meter/sec RA = 240
11132 deg
ZDOT = -5403
624694 TA = 165
68574
MA = 165
68160
Ha = 221
586 n
mi
Hp = 215
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4848739
03 X = 1419238
93
Y = 20418536
13 feet Y = 6239768
93 meter
Z = -7460975
23 Z = -2267067
71
XDOT = -17675
068846 XDOT = -5352
941767
YDOT = -2279
759015 feet/sec YDOT = -754
922554 meter/sec
ZDOT = -17728
427475 ZDOT = -5429
711748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17797158
18 X = 5424573
81
Y = -11141397
86 feet Y = -3395898
07 meter
Z = -7431248
45 Z = -2265044
53
XDOT = 2614
063247 XDOT = 796
766478
YDOT = 16074
743499 feet/sec YDOT = 4899
581818 meter/sec
ZDOT = -17842
551863 ZDOT = -5438
409808
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 16349
10059317
00016717 00000-0 10270-3 0 9118
2 25544 51
6420 240
9546 0006290 329
6157 30
4630 15
53873408 32960
Satellite: ISS
Catalog Number: 25544
Epoch time: 16349
10059317 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 240
9546 deg
Eccentricity:
0006290
Arg of perigee: 329
6157 deg
Mean anomaly: 30
4630 deg
Mean motion: 15
53873408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 302
Coasting Arc #13 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2016/350/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -463134
30 A = 6784567
26 meter
Y = -5716798
96 meter E =
0010398
Z = 3611594
64 I = 51
33409
XDOT = 5869
097691 Wp = 62
06910
YDOT = 2293
077193 meter/sec RA = 235
11267 deg
ZDOT = 4377
463681 TA = 340
96531
MA = 341
00414
Ha = 221
720 n
mi
Hp = 215
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1519469
49 X = -416716
71
Y = -18755902
09 feet Y = -5721718
93 meter
Z = 11849063
78 Z = 3609456
92
XDOT = 19255
569853 XDOT = 5821
755914
YDOT = 7523
219137 feet/sec YDOT = 2358
444161 meter/sec
ZDOT = 14361
757482 ZDOT = 4405
859532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17139960
53 X = -5224259
97
Y = 7778986
26 feet Y = 2371035
01 meter
Z = 11840696
31 Z = 3609044
23
XDOT = 1247
357522 XDOT = 380
194573
YDOT = -19325
286267 feet/sec YDOT = -5890
347254 meter/sec
ZDOT = 14485
732812 ZDOT = 4415
251361
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 16350
12960109
00016717 00000-0 10270-3 0 9123
2 25544 51
6409 235
8276 0006309 334
0828 26
0008 15
53864994 33125
Satellite: ISS
Catalog Number: 25544
Epoch time: 16350
12960109 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 235
8276 deg
Eccentricity:
0006309
Arg of perigee: 334
0828 deg
Mean anomaly: 26
0008 deg
Mean motion: 15
53864994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 302
Coasting Arc #14 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2016/351/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -705575
41 A = 6781040
93 meter
Y = 4921219
09 meter E =
0011756
Z = -4622353
79 I = 51
34176
XDOT = -6079
690533 Wp = 38
12212
YDOT = -3624
098272 meter/sec RA = 230
10572 deg
ZDOT = -2925
310378 TA = 202
56780
MA = 202
61954
Ha = 221
846 n
mi
Hp = 215
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2314879
97 X = -738100
06
Y = 16145731
92 feet Y = 4913147
51 meter
Z = -15165202
73 Z = -4625859
74
XDOT = -19946
491250 XDOT = -6024
503280
YDOT = -11890
086195 feet/sec YDOT = -3691
776569 meter/sec
ZDOT = -9597
474995 ZDOT = -2954
710149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15896165
85 X = 4845151
35
Y = -3586561
65 feet Y = -1093183
99 meter
Z = -15181409
33 Z = -4627293
56
XDOT = -4423
527502 XDOT = -1348
291182
YDOT = 21632
014523 feet/sec YDOT = 6593
438027 meter/sec
ZDOT = -9725
640096 ZDOT = -2964
375101
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 16351
09429415
00016717 00000-0 10270-3 0 9131
2 25544 51
6411 231
0209 0006293 336
8275 23
2593 15
53864827 33279
Satellite: ISS
Catalog Number: 25544
Epoch time: 16351
09429415 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 231
0209 deg
Eccentricity:
0006293
Arg of perigee: 336
8275 deg
Mean anomaly: 23
2593 deg
Mean motion: 15
53864827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 304
Coasting Arc #15 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2016/352/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1980170
62 A = 6778562
06 meter
Y = -3887386
33 meter E =
0004008
Z = 5186178
71 I = 51
35443
XDOT = 5984
575925 Wp = 20
61052
YDOT = 4644
706940 meter/sec RA = 225
09153 deg
ZDOT = 1199
905538 TA = 57
85418
MA = 57
81530
Ha = 221
912 n
mi
Hp = 215
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6496622
76 X = 1998301
23
Y = -12753892
14 feet Y = -3865141
81 meter
Z = 17015022
00 Z = 5195841
48
XDOT = 19634
435449 XDOT = 5926
364267
YDOT = 15238
539831 feet/sec YDOT = 4711
304902 meter/sec
ZDOT = 3936
697959 ZDOT = 1228
835852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14205839
93 X = -4329940
01
Y = -1263702
03 feet Y = -385176
38 meter
Z = 17058019
08 Z = 5199284
21
XDOT = 6892
766722 XDOT = 2100
915297
YDOT = -22795
323174 feet/sec YDOT = -6948
014504 meter/sec
ZDOT = 4062
656590 ZDOT = 1238
297729
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 16352
12329557
00016717 00000-0 10270-3 0 9143
2 25544 51
6403 225
8931 0006395 341
9447 18
1478 15
53884309 33434
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
12329557 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 225
8931 deg
Eccentricity:
0006395
Arg of perigee: 341
9447 deg
Mean anomaly: 18
1478 deg
Mean motion: 15
53884309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 321
Coasting Arc #16 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2016/352/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2565837
31 A = 6778202
31 meter
Y = -3392906
98 meter E =
0005186
Z = 5276352
84 I = 51
35386
XDOT = 5728
745506 Wp = 5
99975
YDOT = 5075
967876 meter/sec RA = 224
43636 deg
ZDOT = 483
241729 TA = 79
40197
MA = 79
34355
Ha = 221
959 n
mi
Hp = 215
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8418101
40 X = 2577956
98
Y = -11131584
57 feet Y = -3364146
75 meter
Z = 17310868
89 Z = 5288846
05
XDOT = 18795
096803 XDOT = 5669
211601
YDOT = 16653
437912 feet/sec YDOT = 5139
697642 meter/sec
ZDOT = 1585
438743 ZDOT = 510
926101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11820147
21 X = -3602780
87
Y = 7289897
93 feet Y = 2221960
89 meter
Z = 17366182
54 Z = 5293212
44
XDOT = -10801
197171 XDOT = -3292
204898
YDOT = -21538
156629 feet/sec YDOT = -6564
830140 meter/sec
ZDOT = 1705
868480 ZDOT = 519
948713
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 16352
25192115
00016717 00000-0 10270-3 0 9156
2 25544 51
6382 225
2524 0006529 341
6948 18
3969 15
53865093 33452
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
25192115 = yrday
fracday
Element set: 915
Inclination: 51
6382 deg
RA of node: 225
2524 deg
Eccentricity:
0006529
Arg of perigee: 341
6948 deg
Mean anomaly: 18
3969 deg
Mean motion: 15
53865093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 322
Coasting Arc #17 (Orbit 3359)
---------------------------------------
Vector Time (GMT): 2016/353/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3797369
53 A = 6778701
41 meter
Y = 2221691
73 meter E =
0012751
Z = -5166768
54 I = 51
37931
XDOT = -5082
358082 Wp = 72
13336
YDOT = -5570
413362 meter/sec RA = 219
42073 deg
ZDOT = 1346
655651 TA = 210
83320
MA = 210
90815
Ha = 222
170 n
mi
Hp = 215
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12458561
46 X = -3796833
17
Y = 7289014
87 feet Y = 2179230
33 meter
Z = -16951340
37 Z = -5185213
57
XDOT = -16674
403157 XDOT = -5026
231960
YDOT = -18275
634391 feet/sec YDOT = -5626
933974 meter/sec
ZDOT = 4418
161585 ZDOT = 1322
103052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14123558
21 X = 4304860
54
Y = -2472089
21 feet Y = -753492
79 meter
Z = -17032536
81 Z = -5191517
22
XDOT = 9016
755546 XDOT = 2748
307090
YDOT = 21956
618269 feet/sec YDOT = 6692
377249 meter/sec
ZDOT = 4311
513236 ZDOT = 1314
149234
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 16353
21660643
00016717 00000-0 10270-3 0 9160
2 25544 51
6382 220
4456 0006631 345
5800 14
5163 15
53861199 33601
Satellite: ISS
Catalog Number: 25544
Epoch time: 16353
21660643 = yrday
fracday
Element set: 916
Inclination: 51
6382 deg
RA of node: 220
4456 deg
Eccentricity:
0006631
Arg of perigee: 345
5800 deg
Mean anomaly: 14
5163 deg
Mean motion: 15
53861199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3360
Checksum: 295
Coasting Arc #18 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2016/354/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4922819
76 A = 6781132
60 meter
Y = -1027193
04 meter E =
0011931
Z = 4548584
47 I = 51
41287
XDOT = 4047
826940 Wp = 33
35672
YDOT = 5742
333159 meter/sec RA = 214
41042 deg
ZDOT = -3070
464765 TA = 87
53036
MA = 87
39377
Ha = 222
197 n
mi
Hp = 215
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16150983
45 X = 4911845
37
Y = -3370055
91 feet Y = -972204
34 meter
Z = 14923177
40 Z = 4572471
36
XDOT = 13280
272113 XDOT = 3998
228701
YDOT = 18839
675719 feet/sec YDOT = 5787
321508 meter/sec
ZDOT = -10073
703296 ZDOT = -3050
921817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16252286
00 X = -4953696
77
Y = -2221336
59 feet Y = -677063
39 meter
Z = 15028028
16 Z = 4580542
98
XDOT = -6401
552461 XDOT = -1951
193190
YDOT = -21042
456478 feet/sec YDOT = -6413
740734 meter/sec
ZDOT = -9989
015534 ZDOT = -3044
651935
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 16354
24560201
00016717 00000-0 10270-3 0 9174
2 25544 51
6377 215
3178 0006692 348
5512 11
5487 15
53888627 33767
Satellite: ISS
Catalog Number: 25544
Epoch time: 16354
24560201 = yrday
fracday
Element set: 917
Inclination: 51
6377 deg
RA of node: 215
3178 deg
Eccentricity:
0006692
Arg of perigee: 348
5512 deg
Mean anomaly: 11
5487 deg
Mean motion: 15
53888627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 325
Coasting Arc #19 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2016/355/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5797167
50 A = 6784708
49 meter
Y = -46085
90 meter E =
0007483
Z = -3522449
39 I = 51
45267
XDOT = -2674
830459 Wp = 35
56932
YDOT = -5611
353894 meter/sec RA = 209
41057 deg
ZDOT = 4486
360827 TA = 282
82982
MA = 282
91341
Ha = 222
341 n
mi
Hp = 214
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19019578
41 X = -5779110
89
Y = -151200
45 feet Y = -110812
63 meter
Z = -11556592
47 Z = -3550566
50
XDOT = -8775
690482 XDOT = -2633
676699
YDOT = -18409
953719 feet/sec YDOT = -5641
035714 meter/sec
ZDOT = 14719
031586 ZDOT = 4473
467011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17900897
71 X = 5456193
62
Y = 6201758
89 feet Y = 1890296
11 meter
Z = -11679816
01 Z = -3560007
92
XDOT = 2971
347983 XDOT = 905
666865
YDOT = 18973
365329 feet/sec YDOT = 5783
081752 meter/sec
ZDOT = 14663
446442 ZDOT = 4469
418475
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 16355
21028271
00016717 00000-0 10270-3 0 9189
2 25544 51
6385 210
5108 0006738 352
3343 7
7705 15
53868530 33910
Satellite: ISS
Catalog Number: 25544
Epoch time: 16355
21028271 = yrday
fracday
Element set: 918
Inclination: 51
6385 deg
RA of node: 210
5108 deg
Eccentricity:
0006738
Arg of perigee: 352
3343 deg
Mean anomaly: 7
7705 deg
Mean motion: 15
53868530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 303
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