[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 8th 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) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
160/14:01:59
311 -0
8 1
4 1
4
N/A 0
6 -0
1 220
3
000/00:03:58
622 1
1 0
0 214
2
161/01:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 214
2
166/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
1
170/05:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 214
0
171/22:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 333)
---------------------------------------
Vector Time (GMT): 2016/158/14:32:13
705
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4414619
76 A = 6781447
86 meter
Y = 3455933
85 meter E =
0012164
Z = 3806840
83 I = 51
98755
XDOT = -1249
248679 Wp = 100
84582
YDOT = -6274
733948 meter/sec RA = 109
88942 deg
ZDOT = 4233
985493 TA = 304
63306
MA = 304
74769
Ha = 220
314 n
mi
Hp = 213
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14483660
63 X = -4471428
83
Y = 11338365
66 feet Y = 3406248
45 meter
Z = 12489635
28 Z = 3785258
15
XDOT = -4098
584904 XDOT = -1199
557131
YDOT = -20586
397467 feet/sec YDOT = -6288
426645 meter/sec
ZDOT = 13891
028519 ZDOT = 4228
036725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16072024
42 X = 4898753
04
Y = 9076395
14 feet Y = 2766485
24 meter
Z = 12394959
99 Z = 3777983
81
XDOT = -16724
724236 XDOT = -5097
695947
YDOT = 10617
498418 feet/sec YDOT = 3236
213518 meter/sec
ZDOT = 13866
269507 ZDOT = 4226
438946
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 16158
66190516
00016717 00000-0 10270-3 0 9002
2 25544 51
6424 110
5376 0001021 150
9705 209
1505 15
54755394 3348
Satellite: ISS
Catalog Number: 25544
Epoch time: 16158
66190516 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 110
5376 deg
Eccentricity:
0001021
Arg of perigee: 150
9705 deg
Mean anomaly: 209
1505 deg
Mean motion: 15
54755394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 334
Checksum: 284
Coasting Arc #2 (Orbit 348)
---------------------------------------
Vector Time (GMT): 2016/159/14:32:13
705
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4399653
74 A = 6777366
09 meter
Y = -1634707
44 meter E =
0012128
Z = -4900305
22 I = 51
98536
XDOT = 15
686281 Wp = 77
19661
YDOT = 7269
702270 meter/sec RA = 104
91749 deg
ZDOT = -2413
441829 TA = 169
24336
MA = 169
21740
Ha = 220
183 n
mi
Hp = 213
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14434559
51 X = 4441410
01
Y = -5363213
38 feet Y = -1585273
44 meter
Z = -16077116
87 Z = -4878831
62
XDOT = 51
464176 XDOT = -53
883067
YDOT = 23850
729232 feet/sec YDOT = 7269
489030 meter/sec
ZDOT = -7918
116236 ZDOT = -2413
533607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10741359
91 X = -3273966
50
Y = -11169308
04 feet Y = -3404405
09 meter
Z = -15983241
16 Z = -4871691
91
XDOT = 20995
315336 XDOT = 6399
372114
YDOT = -8868
929945 feet/sec YDOT = -2703
249847 meter/sec
ZDOT = -7919
871777 ZDOT = -2413
976918
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 16159
62604132
00016717 00000-0 10270-3 0 9014
2 25544 51
6435 105
7274 0000967 148
5774 211
5437 15
54787024 3492
Satellite: ISS
Catalog Number: 25544
Epoch time: 16159
62604132 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 105
7274 deg
Eccentricity:
0000967
Arg of perigee: 148
5774 deg
Mean anomaly: 211
5437 deg
Mean motion: 15
54787024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 349
Checksum: 310
Coasting Arc #3 (Orbit 363)
---------------------------------------
Vector Time (GMT): 2016/160/14:03:58
622
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 499959
88 A = 6786420
49 meter
Y = 6442878
29 meter E =
0006456
Z = -2065500
32 I = 52
01974
XDOT = -4800
506537 Wp = 38
59237
YDOT = 2155
240238 meter/sec RA = 100
01320 deg
ZDOT = 5575
084255 TA = 298
68616
MA = 298
75105
Ha = 220
317 n
mi
Hp = 214
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1640288
32 X = 437910
12
Y = 21138052
15 feet Y = 6448122
49 meter
Z = -6776575
87 Z = -2063221
57
XDOT = -15749
693364 XDOT = -4851
331452
YDOT = 7070
998155 feet/sec YDOT = 2101
272915 meter/sec
ZDOT = 18290
958841 ZDOT = 5551
641490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19648626
22 X = 5988901
27
Y = -7972288
90 feet Y = -2429953
66 meter
Z = -6767855
81 Z = -2062842
45
XDOT = 10942
112824 XDOT = 3335
155989
YDOT = 11567
322848 feet/sec YDOT = 3525
720004 meter/sec
ZDOT = 18188
393689 ZDOT = 5543
822397
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 16160
59017408
00016717 00000-0 10270-3 0 9027
2 25544 51
6430 100
9170 0000276 289
7583 70
3540 15
54506769 3646
Satellite: ISS
Catalog Number: 25544
Epoch time: 16160
59017408 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 100
9170 deg
Eccentricity:
0000276
Arg of perigee: 289
7583 deg
Mean anomaly: 70
3540 deg
Mean motion: 15
54506769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 364
Checksum: 297
Coasting Arc #4 (Orbit 371)
---------------------------------------
Vector Time (GMT): 2016/161/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3733655
28 A = 6777043
21 meter
Y = -2359399
97 meter E =
0004505
Z = 5137605
23 I = 51
99208
XDOT = 2255
156807 Wp = 55
34642
YDOT = -7146
736248 meter/sec RA = 97
66773 deg
ZDOT = -1639
672881 TA = 50
41320
MA = 50
37342
Ha = 220
359 n
mi
Hp = 214
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12249525
19 X = -3731950
55
Y = -7740813
55 feet Y = -2401143
24 meter
Z = 16855660
21 Z = 5119472
01
XDOT = 7398
808423 XDOT = 2342
870586
YDOT = -23447
297403 feet/sec YDOT = -7121
026959 meter/sec
ZDOT = -5379
504202 ZDOT = -1628
505709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5885531
00 X = 1793909
85
Y = -13340706
18 feet Y = -4066247
24 meter
Z = 16777080
40 Z = 5113654
10
XDOT = 23299
057931 XDOT = 7101
552857
YDOT = 3562
020257 feet/sec YDOT = 1085
703774 meter/sec
ZDOT = -5329
490446 ZDOT = -1624
428688
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 16161
10446490
00016717 00000-0 10270-3 0 9033
2 25544 51
6438 98
3485 0000489 231
7355 128
3754 15
54532693 3728
Satellite: ISS
Catalog Number: 25544
Epoch time: 16161
10446490 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 98
3485 deg
Eccentricity:
0000489
Arg of perigee: 231
7355 deg
Mean anomaly: 128
3754 deg
Mean motion: 15
54532693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 372
Checksum: 315
Coasting Arc #5 (Orbit 386)
---------------------------------------
Vector Time (GMT): 2016/162/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3206792
46 A = 6780203
91 meter
Y = 4105768
27 meter E =
0008367
Z = -4348039
39 I = 52
00604
XDOT = -3036
052571 Wp = 113
09245
YDOT = 6092
196733 meter/sec RA = 92
69538 deg
ZDOT = 3515
742750 TA = 192
51053
MA = 192
53131
Ha = 220
236 n
mi
Hp = 214
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10520972
65 X = 3181763
20
Y = 13470368
36 feet Y = 4141489
24 meter
Z = -14265221
11 Z = -4332522
06
XDOT = -9960
802398 XDOT = -3121
029283
YDOT = 19987
522090 feet/sec YDOT = 6057
770100 meter/sec
ZDOT = 11534
589076 ZDOT = 3500
788621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11590822
37 X = -3532882
66
Y = 12637139
09 feet Y = 3851799
99 meter
Z = -14198372
25 Z = -4327663
86
XDOT = -20418
695978 XDOT = -6223
618534
YDOT = -5851
037963 feet/sec YDOT = -1783
396371 meter/sec
ZDOT = 11468
258672 ZDOT = 3495
525243
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 16162
06875903
00016717 00000-0 10270-3 0 9045
2 25544 51
6438 93
5400 0000449 231
8926 128
2187 15
54538535 3879
Satellite: ISS
Catalog Number: 25544
Epoch time: 16162
06875903 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 93
5400 deg
Eccentricity:
0000449
Arg of perigee: 231
8926 deg
Mean anomaly: 128
2187 deg
Mean motion: 15
54538535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 387
Checksum: 318
Coasting Arc #6 (Orbit 402)
---------------------------------------
Vector Time (GMT): 2016/163/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2571591
65 A = 6784368
67 meter
Y = -5500817
39 meter E =
0012871
Z = 3012648
85 I = 52
01995
XDOT = 3722
113044 Wp = 97
80712
YDOT = -4482
413799 meter/sec RA = 87
73365 deg
ZDOT = -4990
820317 TA = 47
87034
MA = 47
76102
Ha = 220
315 n
mi
Hp = 214
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8436980
49 X = -2524523
11
Y = -18047301
14 feet Y = -5529311
71 meter
Z = 9884018
54 Z = 3000270
61
XDOT = 12211
656967 XDOT = 3796
203057
YDOT = -14706
082018 feet/sec YDOT = -4440
375980 meter/sec
ZDOT = -16374
082404 ZDOT = -4972
559695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16251272
82 X = 4953387
96
Y = -11568350
14 feet Y = -3526033
12 meter
Z = 9831121
36 Z = 2996525
79
XDOT = 15816
504311 XDOT = 4820
870514
YDOT = 8326
144184 feet/sec YDOT = 2537
808747 meter/sec
ZDOT = -16293
637767 ZDOT = -4966
300791
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 16163
09733336
00016717 00000-0 10270-3 0 9053
2 25544 51
6434 88
4101 0000340 242
6884 117
4234 15
54524772 4039
Satellite: ISS
Catalog Number: 25544
Epoch time: 16163
09733336 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 88
4101 deg
Eccentricity:
0000340
Arg of perigee: 242
6884 deg
Mean anomaly: 117
4234 deg
Mean motion: 15
54524772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 403
Checksum: 286
Coasting Arc #7 (Orbit 417)
---------------------------------------
Vector Time (GMT): 2016/164/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1863352
15 A = 6787513
95 meter
Y = 6383516
23 meter E =
0008541
Z = -1340917
94 I = 52
02761
XDOT = -4290
594510 Wp = 35
18229
YDOT = 2476
437873 meter/sec RA = 82
78262 deg
ZDOT = 5852
229722 TA = 310
29598
MA = 310
37060
Ha = 220
275 n
mi
Hp = 214
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6113360
09 X = 1798345
18
Y = 20943294
71 feet Y = 6403990
10 meter
Z = -4399337
08 Z = -1332023
67
XDOT = -14076
753642 XDOT = -4346
395350
YDOT = 8124
796171 feet/sec YDOT = 2428
145151 meter/sec
ZDOT = 19200
228748 ZDOT = 5831
251761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19349660
41 X = -5897776
49
Y = 10095258
86 feet Y = 3077034
90 meter
Z = -4361802
60 Z = -1329477
43
XDOT = -9995
626772 XDOT = -3046
667040
YDOT = -10938
779490 feet/sec YDOT = -3334
139989 meter/sec
ZDOT = 19108
318767 ZDOT = 5824
215560
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 16164
06161606
00016717 00000-0 10270-3 0 9067
2 25544 51
6430 83
6008 0000453 271
6052 88
5049 15
54493767 4189
Satellite: ISS
Catalog Number: 25544
Epoch time: 16164
06161606 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 83
6008 deg
Eccentricity:
0000453
Arg of perigee: 271
6052 deg
Mean anomaly: 88
5049 deg
Mean motion: 15
54493767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 418
Checksum: 300
Coasting Arc #8 (Orbit 433)
---------------------------------------
Vector Time (GMT): 2016/165/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1019296
61 A = 6788005
32 meter
Y = -6685032
81 meter E =
0010759
Z = -527875
93 I = 52
02473
XDOT = 4748
944874 Wp = 140
33904
YDOT = -254
991338 meter/sec RA = 77
83719 deg
ZDOT = -6016
044732 TA = 45
32689
MA = 45
23926
Ha = 220
216 n
mi
Hp = 214
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3344149
00 X = -941902
95
Y = -21932522
34 feet Y = -6695998
49 meter
Z = -1731876
43 Z = -532639
94
XDOT = 15580
527802 XDOT = 4780
666696
YDOT = -836
585753 feet/sec YDOT = -201
707664 meter/sec
ZDOT = -19737
679567 ZDOT = -5992
898479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20733867
91 X = 6319682
94
Y = -7890360
99 feet Y = -2404982
03 meter
Z = -1751339
40 Z = -533808
25
XDOT = 3561
881594 XDOT = 1085
661510
YDOT = 13664
031196 feet/sec YDOT = 4164
796709 meter/sec
ZDOT = -19636
746291 ZDOT = -5985
280269
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 16165
09017824
00016717 00000-0 10270-3 0 9074
2 25544 51
6429 78
4706 0000380 260
6728 99
4382 15
54542047 4346
Satellite: ISS
Catalog Number: 25544
Epoch time: 16165
09017824 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 78
4706 deg
Eccentricity:
0000380
Arg of perigee: 260
6728 deg
Mean anomaly: 99
4382 deg
Mean motion: 15
54542047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 434
Checksum: 314
Coasting Arc #9 (Orbit 449)
---------------------------------------
Vector Time (GMT): 2016/166/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 80656
38 A = 6785855
75 meter
Y = 6375706
86 meter E =
0013560
Z = 2303281
94 I = 52
01024
XDOT = -5045
155014 Wp = 71
67025
YDOT = -1914
029972 meter/sec RA = 72
88844 deg
ZDOT = 5452
837014 TA = 313
86590
MA = 313
97785
Ha = 220
236 n
mi
Hp = 214
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 264620
65 X = -1832
77
Y = 20917673
42 feet Y = 6376147
41 meter
Z = 7556699
29 Z = 2303473
89
XDOT = -16552
345846 XDOT = -5049
864524
YDOT = -6279
625894 feet/sec YDOT = -1970
475013 meter/sec
ZDOT = 17889
885217 ZDOT = 5428
317222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20318177
43 X = -6192980
48
Y = 4979663
41 feet Y = 1517801
41 meter
Z = 7556282
69 Z = 2303154
96
XDOT = 2675
517595 XDOT = 815
497763
YDOT = -16178
094100 feet/sec YDOT = -4931
083082 meter/sec
ZDOT = 17783
391205 ZDOT = 5420
377639
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 16166
11873192
00016717 00000-0 10270-3 0 9087
2 25544 51
6432 73
3401 0000325 284
1569 75
9548 15
54550502 4505
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
11873192 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 73
3401 deg
Eccentricity:
0000325
Arg of perigee: 284
1569 deg
Mean anomaly: 75
9548 deg
Mean motion: 15
54550502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 450
Checksum: 296
Coasting Arc #10 (Orbit 455)
---------------------------------------
Vector Time (GMT): 2016/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908273
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3700280
56 A = 6785927
64 meter
Y = 5218725
50 meter E =
0006154
Z = -2257610
04 I = 52
00684
XDOT = -2966
741295 Wp = 39
05641
YDOT = 4467
788399 meter/sec RA = 70
66217 deg
ZDOT = 5477
984100 TA = 295
96598
MA = 296
02936
Ha = 220
250 n
mi
Hp = 214
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12140028
08 X = 3652615
00
Y = 17121802
84 feet Y = 5259838
18 meter
Z = -7406857
10 Z = -2239750
26
XDOT = -9733
403200 XDOT = -3043
090554
YDOT = 14658
098421 feet/sec YDOT = 4434
184982 meter/sec
ZDOT = 17972
388778 ZDOT = 5463
387256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18588730
67 X = 5665845
11
Y = -9804461
87 feet Y = -2988399
98 meter
Z = -7330045
42 Z = -2234197
84
XDOT = 12506
124647 XDOT = 3811
866792
YDOT = 10354
163247 feet/sec YDOT = 3155
948958 meter/sec
ZDOT = 17907
885822 ZDOT = 5458
323598
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 16166
50443921
00016717 00000-0 10270-3 0 9094
2 25544 51
6437 71
4182 0000450 325
9682 34
1442 15
54568876 4563
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
50443921 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 71
4182 deg
Eccentricity:
0000450
Arg of perigee: 325
9682 deg
Mean anomaly: 34
1442 deg
Mean motion: 15
54568876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 456
Checksum: 311
Coasting Arc #11 (Orbit 471)
---------------------------------------
Vector Time (GMT): 2016/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908273
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3091502
63 A = 6788048
15 meter
Y = -6020620
56 meter E =
0012431
Z = 437365
64 I = 52
00250
XDOT = 4028
171954 Wp = 130
31040
YDOT = -2513
556892 meter/sec RA = 65
71393 deg
ZDOT = -6023
307826 TA = 44
99560
MA = 44
89494
Ha = 220
237 n
mi
Hp = 214
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10142725
17 X = -3026073
32
Y = -19752692
13 feet Y = -6054826
01 meter
Z = 1434926
64 Z = 422506
16
XDOT = 13215
787252 XDOT = 4085
238632
YDOT = -8246
577729 feet/sec YDOT = -2468
191559 meter/sec
ZDOT = -19761
508617 ZDOT = -6003
601458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20795316
71 X = -6338412
53
Y = 7795954
13 feet Y = 2376206
82 meter
Z = 1371363
19 Z = 417991
50
XDOT = -6079
222731 XDOT = -1852
947088
YDOT = -12691
959421 feet/sec YDOT = -3868
509231 meter/sec
ZDOT = -19675
116630 ZDOT = -5996
975549
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 16167
53298449
00016717 00000-0 10270-3 0 9103
2 25544 51
6440 66
2886 0000405 308
8732 51
2385 15
54544142 4720
Satellite: ISS
Catalog Number: 25544
Epoch time: 16167
53298449 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 66
2886 deg
Eccentricity:
0000405
Arg of perigee: 308
8732 deg
Mean anomaly: 51
2385 deg
Mean motion: 15
54544142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 472
Checksum: 307
Coasting Arc #12 (Orbit 487)
---------------------------------------
Vector Time (GMT): 2016/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908273
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2235148
26 A = 6787187
12 meter
Y = 6244819
81 meter E =
0013847
Z = 1406560
50 I = 51
98682
XDOT = -4965
918052 Wp = 57
93751
YDOT = 456
650744 meter/sec RA = 60
76530 deg
ZDOT = 5829
179905 TA = 317
32868
MA = 317
43615
Ha = 220
198 n
mi
Hp = 214
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7333163
58 X = 2158318
48
Y = 20488253
98 feet Y = 6269385
00 meter
Z = 4614699
79 Z = 1417232
42
XDOT = -16292
382061 XDOT = -4998
971222
YDOT = 1498
197979 feet/sec YDOT = 400
933117 meter/sec
ZDOT = 19124
605986 ZDOT = 5804
976290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21109511
53 X = 6434179
11
Y = -5245250
34 feet Y = -1598752
30 meter
Z = 4659953
36 Z = 1420353
78
XDOT = -510
107075 XDOT = -155
480636
YDOT = 14943
914794 feet/sec YDOT = 4554
905229 meter/sec
ZDOT = 19019
022664 ZDOT = 5796
998108
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 16168
56152047
00016717 00000-0 10270-3 0 9111
2 25544 51
6449 61
1578 0000642 329
1021 31
0094 15
54572502 4882
Satellite: ISS
Catalog Number: 25544
Epoch time: 16168
56152047 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 61
1578 deg
Eccentricity:
0000642
Arg of perigee: 329
1021 deg
Mean anomaly: 31
0094 deg
Mean motion: 15
54572502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 488
Checksum: 287
Coasting Arc #13 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2016/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908273
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1085115
30 A = 6783908
33 meter
Y = -5930818
71 meter E =
0004021
Z = -3112216
76 I = 51
95932
XDOT = 5683
323623 Wp = 99
00683
YDOT = 1532
432244 meter/sec RA = 55
81087 deg
ZDOT = -4907
863387 TA = 116
61263
MA = 116
57143
Ha = 220
154 n
mi
Hp = 214
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3560089
57 X = -1003596
83
Y = -19458066
63 feet Y = -5942497
02 meter
Z = -10210684
92 Z = -3117290
74
XDOT = 18646
074880 XDOT = 5689
605649
YDOT = 5027
664841 feet/sec YDOT = 1596
022669 meter/sec
ZDOT = -16101
914000 ZDOT = -4880
239566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19679214
16 X = -5998224
48
Y = 1895194
83 feet Y = 577655
38 meter
Z = -10231590
69 Z = -3118588
84
XDOT = 6677
067245 XDOT = 2035
170096
YDOT = -16841
990948 feet/sec YDOT = -5133
438841 meter/sec
ZDOT = -15981
828410 ZDOT = -4871
261299
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 16169
52576604
00016717 00000-0 10270-3 0 9128
2 25544 51
6448 56
3490 0000633 319
8734 40
2372 15
54574081 5030
Satellite: ISS
Catalog Number: 25544
Epoch time: 16169
52576604 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 56
3490 deg
Eccentricity:
0000633
Arg of perigee: 319
8734 deg
Mean anomaly: 40
2372 deg
Mean motion: 15
54574081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 302
Coasting Arc #14 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2016/170/05:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 893042
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 421272
56 A = 6781402
89 meter
Y = 5522783
16 meter E =
0010796
Z = 3904517
65 I = 51
93381
XDOT = -5991
872737 Wp = 97
26831
YDOT = -2458
328988 meter/sec RA = 52
12892 deg
ZDOT = 4112
651072 TA = 309
77148
MA = 309
86651
Ha = 220
119 n
mi
Hp = 214
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1382127
81 X = 340517
51
Y = 18119367
32 feet Y = 5527042
07 meter
Z = 12810097
27 Z = 3906368
68
XDOT = -19658
375122 XDOT = -5983
915372
YDOT = -8065
383819 feet/sec YDOT = -2525
290147 meter/sec
ZDOT = 13492
949710 ZDOT = 4083
562861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -941759
37 X = -287048
26
Y = 18142688
60 feet Y = 5529891
49 meter
Z = 12817030
90 Z = 3906631
02
XDOT = -17278
694230 XDOT = -5266
546001
YDOT = -10365
469455 feet/sec YDOT = -3159
395090 meter/sec
ZDOT = 13366
673830 ZDOT = 4074
162183
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 16170
29715777
00016717 00000-0 10270-3 0 9131
2 25544 51
6409 52
5004 0000497 320
7979 39
3138 15
54626116 5155
Satellite: ISS
Catalog Number: 25544
Epoch time: 16170
29715777 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 52
5004 deg
Eccentricity:
0000497
Arg of perigee: 320
7979 deg
Mean anomaly: 39
3138 deg
Mean motion: 15
54626116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 310
Coasting Arc #15 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2016/171/05:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 893042
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1060206
46 A = 6777703
88 meter
Y = -4540968
92 meter E =
0012152
Z = -4929947
92 I = 51
90111
XDOT = 6140
645728 Wp = 70
47996
YDOT = 3948
581524 meter/sec RA = 47
15187 deg
ZDOT = -2317
151478 TA = 176
91593
MA = 176
90843
Ha = 220
194 n
mi
Hp = 214
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3478367
64 X = 1134853
58
Y = -14898191
99 feet Y = -4528694
90 meter
Z = -16174369
81 Z = -4924617
02
XDOT = 20146
475485 XDOT = 6107
291082
YDOT = 12954
663793 feet/sec YDOT = 4017
064148 meter/sec
ZDOT = -7602
203013 ZDOT = -2287
402076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5142526
69 X = 1567442
13
Y = -14435755
82 feet Y = -4400018
37 meter
Z = -16150194
37 Z = -4922579
24
XDOT = 17654
734215 XDOT = 5381
162989
YDOT = 14647
622501 feet/sec YDOT = 4464
595338 meter/sec
ZDOT = -7473
357908 ZDOT = -2277
879490
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 16171
26139432
00016717 00000-0 10270-3 0 9148
2 25544 51
6413 47
6897 0000558 339
0840 21
0290 15
54599178 5304
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
26139432 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 47
6897 deg
Eccentricity:
0000558
Arg of perigee: 339
0840 deg
Mean anomaly: 21
0290 deg
Mean motion: 15
54599178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 306
Coasting Arc #16 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2016/171/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893042
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5685808
68 A = 6784459
41 meter
Y = -2314762
81 meter E =
0012998
Z = 2874791
35 I = 51
91140
XDOT = -242
071147 Wp = 97
99082
YDOT = -5740
565005 meter/sec RA = 43
68468 deg
ZDOT = -5083
198566 TA = 49
40510
MA = 49
29208
Ha = 220
171 n
mi
Hp = 214
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18654227
97 X = -5673466
37
Y = -7594366
19 feet Y = -2378276
73 meter
Z = 9431730
16 Z = 2847200
69
XDOT = -794
196677 XDOT = -153
168680
YDOT = -18833
874689 feet/sec YDOT = -5742
774170 meter/sec
ZDOT = -16677
160651 ZDOT = -5084
159407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15327369
40 X = 4671782
19
Y = -13151857
17 feet Y = -4008686
07 meter
Z = 9311957
52 Z = 2838284
65
XDOT = 16095
706126 XDOT = 4905
971227
YDOT = 6906
094575 feet/sec YDOT = 2104
977626 meter/sec
ZDOT = -16680
153001 ZDOT = -5084
110635
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 16171
96849461
00016717 00000-0 10270-3 0 9156
2 25544 51
6443 44
1617 0000452 314
8773 45
2344 15
54628481 5418
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
96849461 = yrday
fracday
Element set: 915
Inclination: 51
6443 deg
RA of node: 44
1617 deg
Eccentricity:
0000452
Arg of perigee: 314
8773 deg
Mean anomaly: 45
2344 deg
Mean motion: 15
54628481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 308
Coasting Arc #17 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2016/172/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893042
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5731935
54 A = 6787472
21 meter
Y = 3439246
70 meter E =
0009639
Z = -1151193
94 I = 51
89642
XDOT = -1604
911963 Wp = 34
16336
YDOT = 4636
751785 meter/sec RA = 38
72603 deg
ZDOT = 5893
097251 TA = 313
38119
MA = 313
46143
Ha = 220
196 n
mi
Hp = 214
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18805562
80 X = 5698643
01
Y = 11283617
80 feet Y = 3503159
05 meter
Z = -3776883
01 Z = -1123430
01
XDOT = -5265
459195 XDOT = -1685
268089
YDOT = 15212
440239 feet/sec YDOT = 4618
354410 meter/sec
ZDOT = 19334
308565 ZDOT = 5885
106519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18457668
67 X = -5625897
41
Y = 11881829
09 feet Y = 3621581
51 meter
Z = -3656593
09 Z = -1114529
57
XDOT = -10385
217690 XDOT = -3165
414352
YDOT = -10226
716381 feet/sec YDOT = -3117
103153 meter/sec
ZDOT = 19298
509021 ZDOT = 5882
185550
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 16172
93271870
00016717 00000-0 10270-3 0 9168
2 25544 51
6434 39
3522 0000647 325
6263 34
4848 15
54585007 5560
Satellite: ISS
Catalog Number: 25544
Epoch time: 16172
93271870 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 39
3522 deg
Eccentricity:
0000647
Arg of perigee: 325
6263 deg
Mean anomaly: 34
4848 deg
Mean motion: 15
54585007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 312
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