[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 16th 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) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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
288/09:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
2
290/21:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
0
291/00:03:07
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
1
293/08:05:14
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 211
9
293/11:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
0
294/03:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 211
9
295/09:59:09
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 211
9
298/03:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 211
9
Coasting Arc #1 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2016/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622822
64 A = 6784548
61 meter
Y = 3678631
78 meter E =
0011242
Z = -3348308
99 I = 51
56633
XDOT = -5470
703001 Wp = 74
85230
YDOT = 2639
263874 meter/sec RA = 191
78373 deg
ZDOT = -4663
689613 TA = 144
15769
MA = 144
08221
Ha = 223
392 n
mi
Hp = 212
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15166740
96 X = 4597608
45
Y = 12069001
90 feet Y = 3730185
92 meter
Z = -10985265
72 Z = -3325913
95
XDOT = -17948
500658 XDOT = -5477
154930
YDOT = 8659
002210 feet/sec YDOT = 2578
050192 meter/sec
ZDOT = -15300
818939 ZDOT = -4690
281121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18513181
62 X = -5642817
76
Y = -5923043
93 feet Y = -1805343
79 meter
Z = -10887908
79 Z = -3318634
60
XDOT = 13220
303123 XDOT = 4029
548392
YDOT = -13043
074946 feet/sec YDOT = -3975
529244 meter/sec
ZDOT = -15417
467745 ZDOT = -4699
244169
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 16286
52531556
00016717 00000-0 10270-3 0 9002
2 25544 51
6436 192
7750 0007020 61
1970 298
9887 15
54168275 23236
Satellite: ISS
Catalog Number: 25544
Epoch time: 16286
52531556 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 192
7750 deg
Eccentricity:
0007020
Arg of perigee: 61
1970 deg
Mean anomaly: 298
9887 deg
Mean motion: 15
54168275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 322
Coasting Arc #2 (Orbit 2338)
---------------------------------------
Vector Time (GMT): 2016/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3185665
83 A = 6780740
47 meter
Y = -3956573
94 meter E =
0014905
Z = 4479080
46 I = 51
58496
XDOT = 6739
790660 Wp = 91
79080
YDOT = -1769
407008 meter/sec RA = 186
79299 deg
ZDOT = 3220
842320 TA = 325
78440
MA = 325
88036
Ha = 223
487 n
mi
Hp = 212
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10451659
54 X = -3162943
34
Y = -12980885
65 feet Y = -3992070
57 meter
Z = 14695145
85 Z = 4463660
81
XDOT = 22112
174082 XDOT = 6743
430059
YDOT = -5805
141102 feet/sec YDOT = -1694
017382 meter/sec
ZDOT = 10567
067979 ZDOT = 3253
591969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14587390
10 X = 4446236
50
Y = 8179749
12 feet Y = 2493187
53 meter
Z = 14628316
55 Z = 4458710
89
XDOT = -17756
712939 XDOT = -5412
246104
YDOT = 12454
997847 feet/sec YDOT = 3796
283344 meter/sec
ZDOT = 10710
521811 ZDOT = 3264
567048
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 16287
55412053
00016717 00000-0 10270-3 0 9017
2 25544 51
6431 187
6467 0007042 65
5230 294
6656 15
54174974 23397
Satellite: ISS
Catalog Number: 25544
Epoch time: 16287
55412053 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 187
6467 deg
Eccentricity:
0007042
Arg of perigee: 65
5230 deg
Mean anomaly: 294
6656 deg
Mean motion: 15
54174974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2339
Checksum: 318
Coasting Arc #3 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2016/288/09:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2572779
72 A = 6779063
65 meter
Y = -3954935
79 meter E =
0012436
Z = 4857481
69 I = 51
60781
XDOT = 7098
445312 Wp = 95
32515
YDOT = -1636
010851 meter/sec RA = 182
29128 deg
ZDOT = 2421
218261 TA = 330
91040
MA = 330
97963
Ha = 223
311 n
mi
Hp = 212
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8440878
35 X = -2551959
32
Y = -12975511
13 feet Y = -3983589
28 meter
Z = 15936619
71 Z = 4845034
68
XDOT = 23288
862571 XDOT = 7104
450614
YDOT = -5367
489670 feet/sec YDOT = -1556
597369 meter/sec
ZDOT = 7943
629465 ZDOT = 2455
716049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5441170
61 X = 1658468
80
Y = 14550569
32 feet Y = 4435013
53 meter
Z = 15882781
85 Z = 4841071
91
XDOT = -22787
527073 XDOT = -6945
638252
YDOT = -337
702200 feet/sec YDOT = -102
931630 meter/sec
ZDOT = 8094
718616 ZDOT = 2467
270234
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 16288
45431243
00016717 00000-0 10270-3 0 9020
2 25544 51
6420 183
1590 0006754 68
4868 291
7004 15
54230167 23539
Satellite: ISS
Catalog Number: 25544
Epoch time: 16288
45431243 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 183
1590 deg
Eccentricity:
0006754
Arg of perigee: 68
4868 deg
Mean anomaly: 291
7004 deg
Mean motion: 15
54230167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 303
Coasting Arc #4 (Orbit 2367)
---------------------------------------
Vector Time (GMT): 2016/289/09:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 774372
24 A = 6777205
12 meter
Y = 4168353
82 meter E =
0021542
Z = -5305975
81 I = 51
63429
XDOT = -7597
542008 Wp = 81
49400
YDOT = 762
480012 meter/sec RA = 177
29077 deg
ZDOT = -508
468517 TA = 183
63692
MA = 183
65261
Ha = 223
360 n
mi
Hp = 212
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2540591
34 X = 753477
75
Y = 13675701
52 feet Y = 4176895
86 meter
Z = -17408057
11 Z = -5302265
32
XDOT = -24926
318924 XDOT = -7603
033614
YDOT = 2501
574843 feet/sec YDOT = 677
488426 meter/sec
ZDOT = -1668
203797 ZDOT = -545
389640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 217948
80 X = 66430
79
Y = -13927490
26 feet Y = -4245099
03 meter
Z = -17392451
87 Z = -5301219
33
XDOT = 23880
800171 XDOT = 7278
867892
YDOT = 2664
202582 feet/sec YDOT = 812
048947 meter/sec
ZDOT = -1829
773740 ZDOT = -557
715036
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 16289
41879689
00016717 00000-0 10270-3 0 9038
2 25544 51
6425 178
3502 0006979 71
2538 288
9372 15
54218031 23686
Satellite: ISS
Catalog Number: 25544
Epoch time: 16289
41879689 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 178
3502 deg
Eccentricity:
0006979
Arg of perigee: 71
2538 deg
Mean anomaly: 288
9372 deg
Mean motion: 15
54218031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2368
Checksum: 348
Coasting Arc #5 (Orbit 2383)
---------------------------------------
Vector Time (GMT): 2016/290/09:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1090339
63 A = 6777652
78 meter
Y = -4257745
48 meter E =
0011260
Z = 5151386
82 I = 51
66769
XDOT = 7533
246170 Wp = 67
05554
YDOT = 148
944045 meter/sec RA = 172
29222 deg
ZDOT = -1464
536249 TA = 37
06092
MA = 36
98321
Ha = 223
267 n
mi
Hp = 212
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3577229
76 X = 1112845
97
Y = -13968981
24 feet Y = -4245426
15 meter
Z = 16900875
41 Z = 5156738
70
XDOT = 24715
374573 XDOT = 7538
135007
YDOT = 488
661566 feet/sec YDOT = 233
213031 meter/sec
ZDOT = -4804
908953 ZDOT = -1427
928890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6044480
44 X = -1842357
64
Y = 13060627
38 feet Y = 3980879
22 meter
Z = 16924918
56 Z = 5158715
18
XDOT = -23255
535209 XDOT = -7088
287132
YDOT = -4714
545567 feet/sec YDOT = -1436
993489 meter/sec
ZDOT = -4644
831986 ZDOT = -1415
744789
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 16290
44756784
00016717 00000-0 10270-3 0 9044
2 25544 51
6417 173
2225 0006904 74
2963 285
8951 15
54250345 23847
Satellite: ISS
Catalog Number: 25544
Epoch time: 16290
44756784 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 173
2225 deg
Eccentricity:
0006904
Arg of perigee: 74
2963 deg
Mean anomaly: 285
8951 deg
Mean motion: 15
54250345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2384
Checksum: 325
Coasting Arc #6 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2016/290/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 423018
62 A = 6777040
15 meter
Y = 4197148
59 meter E =
0021510
Z = -5322648
85 I = 51
68177
XDOT = -7565
118648 Wp = 88
73265
YDOT = 1119
526026 meter/sec RA = 169
90628 deg
ZDOT = 283
011190 TA = 183
96049
MA = 183
97755
Ha = 223
273 n
mi
Hp = 212
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1387856
36 X = 401909
39
Y = 13770172
54 feet Y = 4201760
50 meter
Z = -17462758
71 Z = -5320645
58
XDOT = -24819
943070 XDOT = -7578
449994
YDOT = 3672
985651 feet/sec YDOT = 1034
853281 meter/sec
ZDOT = 928
514403 ZDOT = 246
228312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2719186
37 X = -828808
01
Y = 13580638
64 feet Y = 4139378
66 meter
Z = -17454627
42 Z = -5320170
44
XDOT = -23787
616922 XDOT = -7250
465638
YDOT = -3782
614910 feet/sec YDOT = -1152
941025 meter/sec
ZDOT = 767
471562 ZDOT = 233
925332
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 16290
89765204
00016717 00000-0 10270-3 0 9051
2 25544 51
6427 170
9753 0006753 80
5052 279
6864 15
54245248 23917
Satellite: ISS
Catalog Number: 25544
Epoch time: 16290
89765204 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 170
9753 deg
Eccentricity:
0006753
Arg of perigee: 80
5052 deg
Mean anomaly: 279
6864 deg
Mean motion: 15
54245248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 332
Coasting Arc #7 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2016/291/00:03:07
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5201444
18 A = 6782940
48 meter
Y = 2096773
42 meter E =
0012845
Z = -3828316
41 I = 51
70359
XDOT = -4791
096962 Wp = 78
85930
YDOT = 4263
854182 meter/sec RA = 169
33662 deg
ZDOT = -4183
730176 TA = 147
06166
MA = 146
98156
Ha = 223
339 n
mi
Hp = 212
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17065105
57 X = 5196207
73
Y = 6879177
88 feet Y = 2154909
80 meter
Z = -12560093
21 Z = -3803061
38
XDOT = -15718
822054 XDOT = -4818
097097
YDOT = 13989
022906 feet/sec YDOT = 4210
125539 meter/sec
ZDOT = -13726
148872 ZDOT = -4207
070725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18429270
23 X = 5617241
57
Y = -1287471
26 feet Y = -392421
24 meter
Z = -12449950
78 Z = -3794745
00
XDOT = -8059
256466 XDOT = -2456
461371
YDOT = 18059
630968 feet/sec YDOT = 5504
575519 meter/sec
ZDOT = -13828
873900 ZDOT = -4215
040765
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 16291
02624744
00016717 00000-0 10270-3 0 9061
2 25544 51
6412 170
3357 0006820 80
0740 280
1183 15
54229275 23934
Satellite: ISS
Catalog Number: 25544
Epoch time: 16291
02624744 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 170
3357 deg
Eccentricity:
0006820
Arg of perigee: 80
0740 deg
Mean anomaly: 280
1183 deg
Mean motion: 15
54229275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2393
Checksum: 289
Coasting Arc #8 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2016/292/00:03:07
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3806868
94 A = 6779205
01 meter
Y = -2873196
36 meter E =
0013476
Z = 4807468
73 I = 51
72292
XDOT = 6140
347483 Wp = 102
16856
YDOT = -3824
398042 meter/sec RA = 164
35065 deg
ZDOT = 2567
820058 TA = 322
56267
MA = 322
65646
Ha = 223
354 n
mi
Hp = 212
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12489727
49 X = -3797810
41
Y = -9426497
25 feet Y = -2915716
32 meter
Z = 15772535
21 Z = 4788997
65
XDOT = 20145
496992 XDOT = 6170
182819
YDOT = -12547
237672 feet/sec YDOT = -3755
565547 meter/sec
ZDOT = 8424
606491 ZDOT = 2597
721859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15490536
61 X = -4721515
56
Y = -2724689
89 feet Y = -830485
48 meter
Z = 15692174
83 Z = 4782974
89
XDOT = 12062
835663 XDOT = 3676
752310
YDOT = -19136
108102 feet/sec YDOT = -5832
685750 meter/sec
ZDOT = 8555
982520 ZDOT = 2607
863472
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 16292
05500206
00016717 00000-0 10270-3 0 9072
2 25544 51
6411 165
2064 0006731 83
0243 277
1675 15
54263919 24096
Satellite: ISS
Catalog Number: 25544
Epoch time: 16292
05500206 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 165
2064 deg
Eccentricity:
0006731
Arg of perigee: 83
0243 deg
Mean anomaly: 277
1675 deg
Mean motion: 15
54263919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 292
Coasting Arc #9 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2016/293/00:03:07
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2154235
43 A = 6777184
59 meter
Y = 3656118
43 meter E =
0021452
Z = -5302781
90 I = 51
74700
XDOT = -6941
284027 Wp = 85
43726
YDOT = 3157
153338 meter/sec RA = 159
35816 deg
ZDOT = -643
684689 TA = 178
41735
MA = 178
41055
Ha = 223
312 n
mi
Hp = 212
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7067701
53 X = 2138950
92
Y = 11995139
21 feet Y = 3680122
80 meter
Z = -17397578
41 Z = -5292354
23
XDOT = -22773
241557 XDOT = -6972
945407
YDOT = 10358
114625 feet/sec YDOT = 3079
354179 meter/sec
ZDOT = -2111
826408 ZDOT = -677
481590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11948340
61 X = 3641854
22
Y = 7255255
32 feet Y = 2211401
82 meter
Z = -17352519
45 Z = -5289047
93
XDOT = -14763
633313 XDOT = -4499
955434
YDOT = 18912
444605 feet/sec YDOT = 5764
513116 meter/sec
ZDOT = -2260
163046 ZDOT = -688
897697
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 16293
01945242
00016717 00000-0 10270-3 0 9083
2 25544 51
6413 160
3977 0006825 85
7625 274
4308 15
54243609 24248
Satellite: ISS
Catalog Number: 25544
Epoch time: 16293
01945242 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 160
3977 deg
Eccentricity:
0006825
Arg of perigee: 85
7625 deg
Mean anomaly: 274
4308 deg
Mean motion: 15
54243609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2424
Checksum: 315
Coasting Arc #10 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2016/293/08:05:14
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5240545
06 A = 6787224
94 meter
Y = 3833101
26 meter E =
0012603
Z = -1974766
12 I = 51
79007
XDOT = -4291
197402 Wp = 63
02667
YDOT = -3000
446809 meter/sec RA = 157
66979 deg
ZDOT = 5596
848686 TA = 275
23731
MA = 275
38111
Ha = 223
274 n
mi
Hp = 211
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17193389
30 X = -5273425
50
Y = 12575791
54 feet Y = 3774314
03 meter
Z = -6478891
48 Z = -2000304
01
XDOT = -14078
731635 XDOT = -4284
514414
YDOT = -9843
985595 feet/sec YDOT = -3048
396229 meter/sec
ZDOT = 18362
364454 ZDOT = 5576
019017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21188441
52 X = 6458236
98
Y = -1828971
01 feet Y = -557470
36 meter
Z = -6591207
34 Z = -2009000
00
XDOT = 6880
121651 XDOT = 2097
061079
YDOT = 14242
479759 feet/sec YDOT = 4341
107830 meter/sec
ZDOT = 18271
695929 ZDOT = 5569
212919
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 16293
34093444
00016717 00000-0 10270-3 0 9098
2 25544 51
6404 158
7961 0006885 84
4155 275
7783 15
54261315 24292
Satellite: ISS
Catalog Number: 25544
Epoch time: 16293
34093444 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 158
7961 deg
Eccentricity:
0006885
Arg of perigee: 84
4155 deg
Mean anomaly: 275
7783 deg
Mean motion: 15
54261315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 334
Coasting Arc #11 (Orbit 2431)
---------------------------------------
Vector Time (GMT): 2016/293/11:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6452384
30 A = 6788089
96 meter
Y = 1513974
50 meter E =
0020191
Z = 1428676
69 I = 51
79869
XDOT = 122
006891 Wp = 68
74127
YDOT = -5014
138849 meter/sec RA = 157
02821 deg
ZDOT = 5805
745266 TA = 306
81293
MA = 306
99799
Ha = 223
260 n
mi
Hp = 212
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21169239
82 X = -6475774
44
Y = 4967107
93 feet Y = 1441688
89 meter
Z = 4687259
48 Z = 1397275
03
XDOT = 400
285074 XDOT = 149
864756
YDOT = -16450
586775 feet/sec YDOT = -5012
618463 meter/sec
ZDOT = 19047
720689 ZDOT = 5806
405848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18722376
20 X = 5706580
27
Y = -11115424
18 feet Y = -3387981
29 meter
Z = 4549643
02 Z = 1386731
19
XDOT = 3874
228697 XDOT = 1180
864907
YDOT = 14404
822562 feet/sec YDOT = 4390
589917 meter/sec
ZDOT = 19051
381397 ZDOT = 5806
861050
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 16293
53382175
00016717 00000-0 10270-3 0 9103
2 25544 51
6421 157
8350 0006757 84
8602 275
3321 15
54276536 24321
Satellite: ISS
Catalog Number: 25544
Epoch time: 16293
53382175 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 157
8350 deg
Eccentricity:
0006757
Arg of perigee: 84
8602 deg
Mean anomaly: 275
3321 deg
Mean motion: 15
54276536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2432
Checksum: 308
Coasting Arc #12 (Orbit 2441)
---------------------------------------
Vector Time (GMT): 2016/294/03:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3712485
91 A = 6784357
75 meter
Y = -4664406
71 meter E =
0019567
Z = 3221109
89 I = 51
80251
XDOT = 5842
935034 Wp = 91
46029
YDOT = 1320
690369 meter/sec RA = 153
67721 deg
ZDOT = -4797
179147 TA = 51
31935
MA = 51
14447
Ha = 223
188 n
mi
Hp = 211
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12180071
89 X = 3748721
50
Y = -15303171
62 feet Y = -4622688
47 meter
Z = 10567945
83 Z = 3239232
77
XDOT = 19169
734365 XDOT = 5851
035571
YDOT = 4332
973652 feet/sec YDOT = 1386
075097 meter/sec
ZDOT = -15738
776729 ZDOT = -4768
775441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12394719
88 X = -3777910
62
Y = -15073635
86 feet Y = -4594444
21 meter
Z = 10647962
85 Z = 3245499
08
XDOT = 7210
004863 XDOT = 2197
609482
YDOT = -17015
451209 feet/sec YDOT = -5186
309528 meter/sec
ZDOT = -15614
701503 ZDOT = -4759
361018
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 16294
17678040
00016717 00000-0 10270-3 0 9114
2 25544 51
6383 154
6278 0006846 87
8472 272
3464 15
54301524 24421
Satellite: ISS
Catalog Number: 25544
Epoch time: 16294
17678040 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 154
6278 deg
Eccentricity:
0006846
Arg of perigee: 87
8472 deg
Mean anomaly: 272
3464 deg
Mean motion: 15
54301524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2442
Checksum: 319
Coasting Arc #13 (Orbit 2456)
---------------------------------------
Vector Time (GMT): 2016/295/03:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4815228
92 A = 6787557
90 meter
Y = 4475526
42 meter E =
0013031
Z = -1685069
23 I = 51
84210
XDOT = -4394
607811 Wp = 64
62508
YDOT = -2589
295234 meter/sec RA = 148
71304 deg
ZDOT = 5720
745478 TA = 276
96725
MA = 277
11545
Ha = 223
269 n
mi
Hp = 211
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15797995
15 X = -4856732
05
Y = 14683485
65 feet Y = 4421447
18 meter
Z = -5528442
37 Z = -1708561
76
XDOT = -14418
004629 XDOT = -4393
116396
YDOT = -8495
063104 feet/sec YDOT = -2638
430134 meter/sec
ZDOT = 18768
849993 ZDOT = 5699
400952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11334241
65 X = 3454676
85
Y = 18318330
81 feet Y = 5583427
23 meter
Z = -5631944
51 Z = -1716616
69
XDOT = -9825
104116 XDOT = -2994
691735
YDOT = 11781
497442 feet/sec YDOT = 3591
000420 meter/sec
ZDOT = 18675
847862 ZDOT = 5692
398428
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 16295
14121366
00016717 00000-0 10270-3 0 9127
2 25544 51
6387 149
8198 0007033 92
6821 267
5137 15
54305566 24572
Satellite: ISS
Catalog Number: 25544
Epoch time: 16295
14121366 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 149
8198 deg
Eccentricity:
0007033
Arg of perigee: 92
6821 deg
Mean anomaly: 267
5137 deg
Mean motion: 15
54305566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2457
Checksum: 323
Coasting Arc #14 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2016/295/09:59:09
000
Vector Time (MET): N/A
Weight (LBS) : 907687
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1273610
99 A = 6777032
33 meter
Y = -4085003
80 meter E =
0009721
Z = 5247311
34 I = 51
81925
XDOT = 6799
188240 Wp = 80
92342
YDOT = -3417
764374 meter/sec RA = 147
33750 deg
ZDOT = -1007
348548 TA = 18
70464
MA = 18
66894
Ha = 223
135 n
mi
Hp = 211
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4178513
74 X = -1253326
34
Y = -13402243
45 feet Y = -4099132
56 meter
Z = 17215588
38 Z = 5241173
79
XDOT = 22307
048030 XDOT = 6841
794559
YDOT = -11213
137710 feet/sec YDOT = -3341
493102 meter/sec
ZDOT = -3304
949304 ZDOT = -974
215680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4105426
53 X = 1251334
01
Y = 13458370
85 feet Y = 4102111
44 meter
Z = 17189366
39 Z = 5239318
88
XDOT = -21498
511631 XDOT = -6552
746345
YDOT = 10606
277082 feet/sec YDOT = 3232
793255 meter/sec
ZDOT = -3159
418509 ZDOT = -962
990762
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 16295
46268788
00016717 00000-0 10270-3 0 9133
2 25544 51
6430 148
2177 0006589 92
3994 267
7913 15
54339687 24625
Satellite: ISS
Catalog Number: 25544
Epoch time: 16295
46268788 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 148
2177 deg
Eccentricity:
0006589
Arg of perigee: 92
3994 deg
Mean anomaly: 267
7913 deg
Mean motion: 15
54339687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 362
Coasting Arc #15 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2016/296/09:59:09
000
Vector Time (MET): N/A
Weight (LBS) : 907687
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -337491
36 A = 6779486
76 meter
Y = 4905878
39 meter E =
0017174
Z = -4683255
21 I = 51
85378
XDOT = -6703
085745 Wp = 104
27521
YDOT = 2298
601949 meter/sec RA = 142
35236 deg
ZDOT = 2895
680387 TA = 194
45044
MA = 194
49961
Ha = 223
123 n
mi
Hp = 211
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1107255
12 X = -369575
55
Y = 16095401
55 feet Y = 4901924
72 meter
Z = -15365010
53 Z = -4684972
84
XDOT = -21991
751132 XDOT = -6742
357246
YDOT = 7541
344978 feet/sec YDOT = 2223
424105 meter/sec
ZDOT = 9500
263736 ZDOT = 2863
022589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 951951
69 X = 290154
88
Y = -16097422
01 feet Y = -4906494
23 meter
Z = -15373298
48 Z = -4685781
38
XDOT = 20852
707164 XDOT = 6355
905144
YDOT = -7687
967801 feet/sec YDOT = -2343
292586 meter/sec
ZDOT = 9356
965895 ZDOT = 2852
003205
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 16296
42710935
00016717 00000-0 10270-3 0 9147
2 25544 51
6428 143
4087 0006649 94
9681 265
2231 15
54321640 24779
Satellite: ISS
Catalog Number: 25544
Epoch time: 16296
42710935 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 143
4087 deg
Eccentricity:
0006649
Arg of perigee: 94
9681 deg
Mean anomaly: 265
2231 deg
Mean motion: 15
54321640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2477
Checksum: 320
Coasting Arc #16 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2016/297/09:59:09
000
Vector Time (MET): N/A
Weight (LBS) : 907687
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1825392
96 A = 6783261
23 meter
Y = -5469903
83 meter E =
0018658
Z = 3555751
54 I = 51
89130
XDOT = 6159
997821 Wp = 91
23213
YDOT = -878
545247 meter/sec RA = 137
37867 deg
ZDOT = -4493
900003 TA = 46
92786
MA = 46
77183
Ha = 223
057 n
mi
Hp = 211
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5988822
06 X = 1869150
67
Y = -17945878
72 feet Y = -5449246
18 meter
Z = 11665851
52 Z = 3564725
55
XDOT = 20209
966603 XDOT = 6191
193769
YDOT = -2882
366297 feet/sec YDOT = -809
485862 meter/sec
ZDOT = -14743
766415 ZDOT = -4463
900144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5541035
85 X = -1688907
73
Y = 18063200
00 feet Y = 5505663
36 meter
Z = 11705997
25 Z = 3567987
96
XDOT = -18923
912300 XDOT = -5768
008469
YDOT = 3706
733742 feet/sec YDOT = 1129
812444 meter/sec
ZDOT = -14612
309044 ZDOT = -4453
831796
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 16297
45581598
00016717 00000-0 10270-3 0 9153
2 25544 51
6424 138
2796 0006668 97
8263 262
3646 15
54356400 24931
Satellite: ISS
Catalog Number: 25544
Epoch time: 16297
45581598 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 138
2796 deg
Eccentricity:
0006668
Arg of perigee: 97
8263 deg
Mean anomaly: 262
3646 deg
Mean motion: 15
54356400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 348
Coasting Arc #17 (Orbit 2503)
---------------------------------------
Vector Time (GMT): 2016/298/03:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 907687
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1863372
28 A = 6784240
69 meter
Y = 5653809
03 meter E =
0011237
Z = -3264579
76 I = 51
90838
XDOT = -5935
711763 Wp = 94
41141
YDOT = 793
357941 meter/sec RA = 133
70028 deg
ZDOT = 4775
299604 TA = 227
92984
MA = 228
02549
Ha = 223
145 n
mi
Hp = 211
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6113426
10 X = -1910598
04
Y = 18549242
21 feet Y = 5632707
26 meter
Z = -10710563
51 Z = -3273746
75
XDOT = -19474
119958 XDOT = -5967
338723
YDOT = 2602
880385 feet/sec YDOT = 726
804327 meter/sec
ZDOT = 15666
993451 ZDOT = 4746
388238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18369564
26 X = 5599043
19
Y = 6567111
80 feet Y = 2001655
68 meter
Z = -10751590
01 Z = -3277084
63
XDOT = 2527
393831 XDOT = 770
349640
YDOT = 18301
589161 feet/sec YDOT = 5578
324376 meter/sec
ZDOT = 15540
304427 ZDOT = 4736
684789
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 16298
16304809
00016717 00000-0 10270-3 0 9161
2 25544 51
6393 134
7519 0006730 101
3836 258
8073 15
54312903 25044
Satellite: ISS
Catalog Number: 25544
Epoch time: 16298
16304809 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 134
7519 deg
Eccentricity:
0006730
Arg of perigee: 101
3836 deg
Mean anomaly: 258
8073 deg
Mean motion: 15
54312903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2504
Checksum: 309
Coasting Arc #18 (Orbit 2519)
---------------------------------------
Vector Time (GMT): 2016/299/03:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 907687
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3022539
55 A = 6787507
58 meter
Y = -5837213
71 meter E =
0020533
Z = 1654704
53 I = 51
94232
XDOT = 5001
922177 Wp = 112
59639
YDOT = 948
603996 meter/sec RA = 128
74168 deg
ZDOT = -5741
443212 TA = 49
34263
MA = 49
16432
Ha = 223
066 n
mi
Hp = 211
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9916468
34 X = 3079550
19
Y = -19150963
62 feet Y = -5803094
74 meter
Z = 5428820
64 Z = 1669526
39
XDOT = 16410
505829 XDOT = 5018
832663
YDOT = 3112
217836 feet/sec YDOT = 1004
632928 meter/sec
ZDOT = -18836
755944 ZDOT = -5717
103859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19039221
96 X = -5803154
85
Y = -10093798
67 feet Y = -3076589
84 meter
Z = 5494642
93 Z = 1674767
17
XDOT = 2558
450550 XDOT = 779
815728
YDOT = -15108
129211 feet/sec YDOT = -4604
957783 meter/sec
ZDOT = -18730
349991 ZDOT = -5709
010677
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 16299
19173914
00016717 00000-0 10270-3 0 9177
2 25544 51
6405 129
6217 0006681 104
7200 255
4694 15
54347979 25204
Satellite: ISS
Catalog Number: 25544
Epoch time: 16299
19173914 = yrday
fracday
Element set: 917
Inclination: 51
6405 deg
RA of node: 129
6217 deg
Eccentricity:
0006681
Arg of perigee: 104
7200 deg
Mean anomaly: 255
4694 deg
Mean motion: 15
54347979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2520
Checksum: 325
Coasting Arc #19 (Orbit 2535)
---------------------------------------
Vector Time (GMT): 2016/300/03:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 907687
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3831142
36 A = 6788631
60 meter
Y = 5598127
95 meter E =
0016480
Z = 89964
10 I = 51
96478
XDOT = -3847
386271 Wp = 67
47423
YDOT = -2744
075557 meter/sec RA = 123
79180 deg
ZDOT = 6038
297071 TA = 293
49047
MA = 293
66358
Ha = 223
025 n
mi
Hp = 211
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12569364
69 X = -3893894
33
Y = 18366561
53 feet Y = 5554934
69 meter
Z = 295157
80 Z = 71200
19
XDOT = -12622
658370 XDOT = -3845
747220
YDOT = -9002
872562 feet/sec YDOT = -2787
089901 meter/sec
ZDOT = 19810
685930 ZDOT = 6019
611408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18442462
57 X = 5621262
59
Y = 12459422
80 feet Y = 3797632
07 meter
Z = 212102
46 Z = 64648
83
XDOT = -8015
083104 XDOT = -2442
997330
YDOT = 11460
201482 feet/sec YDOT = 3493
069412 meter/sec
ZDOT = 19729
316755 ZDOT = 6013
495747
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 16300
22042064
00016717 00000-0 10270-3 0 9186
2 25544 51
6396 124
4926 0006701 108
4232 251
7650 15
54367952 25363
Satellite: ISS
Catalog Number: 25544
Epoch time: 16300
22042064 = yrday
fracday
Element set: 918
Inclination: 51
6396 deg
RA of node: 124
4926 deg
Eccentricity:
0006701
Arg of perigee: 108
4232 deg
Mean anomaly: 251
7650 deg
Mean motion: 15
54367952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2536
Checksum: 293
Coasting Arc #20 (Orbit 2550)
---------------------------------------
Vector Time (GMT): 2016/301/03:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 907687
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4355602
10 A = 6787126
24 meter
Y = -4846597
59 meter E =
0013292
Z = -1889325
26 I = 51
97764
XDOT = 2568
336456 Wp = 127
11953
YDOT = 4497
810895 meter/sec RA = 118
84231 deg
ZDOT = -5652
132891 TA = 73
58179
MA = 73
43573
Ha = 222
986 n
mi
Hp = 212
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14290033
13 X = 4418651
96
Y = -15900910
72 feet Y = -4797537
96 meter
Z = -6198573
67 Z = -1868012
88
XDOT = 8426
300710 XDOT = 2545
305993
YDOT = 14756
597426 feet/sec YDOT = 4526
402454 meter/sec
ZDOT = -18543
743080 ZDOT = -5639
712710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16230511
43 X = -4947059
89
Y = -13956084
22 feet Y = -4253814
47 meter
Z = -6104468
54 Z = -1860642
01
XDOT = 13534
448469 XDOT = 4125
299893
YDOT = -7703
619798 feet/sec YDOT = -2348
063314 meter/sec
ZDOT = -18490
092807 ZDOT = -5635
780288
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 16301
18480241
00016717 00000-0 10270-3 0 9196
2 25544 51
6402 119
6834 0006577 111
4762 248
7093 15
54379498 25510
Satellite: ISS
Catalog Number: 25544
Epoch time: 16301
18480241 = yrday
fracday
Element set: 919
Inclination: 51
6402 deg
RA of node: 119
6834 deg
Eccentricity:
0006577
Arg of perigee: 111
4762 deg
Mean anomaly: 248
7093 deg
Mean motion: 15
54379498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2551
Checksum: 320
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