[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 6th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
250/21:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 215
0
250/21:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 215
1
254/00:41:33
991 3
4 3
8 3
9
N/A -1
5 -0
4 220
0
000/00:11:03
983 -0
9 0
1 217
1
257/20:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 216
9
Coasting Arc #1 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2016/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -749350
86 A = 6776473
84 meter
Y = 4146294
38 meter E =
0000643
Z = 5307595
28 I = 51
73458
XDOT = -7422
500398 Wp = 322
54500
YDOT = -1882
651202 meter/sec RA = 16
73151 deg
ZDOT = 423
310139 TA = 123
42687
MA = 123
42072
Ha = 219
586 n
mi
Hp = 215
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2458500
20 X = -821442
08
Y = 13603328
01 feet Y = 4137512
14 meter
Z = 17413370
34 Z = 5303779
56
XDOT = -24352
035427 XDOT = -7402
952715
YDOT = -6176
677172 feet/sec YDOT = -1965
545229 meter/sec
ZDOT = 1388
812792 ZDOT = 387
301211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6184769
69 X = 1885117
80
Y = -12387556
43 feet Y = -3775727
20 meter
Z = 17395898
72 Z = 5302269
93
XDOT = 20848
453607 XDOT = 6354
608660
YDOT = 12136
491593 feet/sec YDOT = 3699
202638 meter/sec
ZDOT = 1231
820256 ZDOT = 375
458814
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 16249
54887188
00016717 00000-0 10270-3 0 9008
2 25544 51
6437 17
0592 0003149 293
8782 66
2041 15
54444140 17489
Satellite: ISS
Catalog Number: 25544
Epoch time: 16249
54887188 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 17
0592 deg
Eccentricity:
0003149
Arg of perigee: 293
8782 deg
Mean anomaly: 66
2041 deg
Mean motion: 15
54444140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 321
Coasting Arc #2 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2016/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2609903
95 A = 6777313
73 meter
Y = -3593690
16 meter E =
0010577
Z = -5128553
07 I = 51
70593
XDOT = 6964
457915 Wp = 97
68427
YDOT = 2751
410048 meter/sec RA = 11
73599 deg
ZDOT = 1617
693857 TA = 187
91500
MA = 187
93170
Ha = 219
635 n
mi
Hp = 215
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8562677
01 X = 2674807
87
Y = -11790322
05 feet Y = -3564142
10 meter
Z = -16825961
50 Z = -5115716
78
XDOT = 22849
271374 XDOT = 6925
315265
YDOT = 9026
935854 feet/sec YDOT = 2829
072590 meter/sec
ZDOT = 5307
394545 ZDOT = 1651
430130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11402930
65 X = -3475613
26
Y = 9176705
35 feet Y = 2797059
79 meter
Z = -16769178
98 Z = -5111245
75
XDOT = -19071
075936 XDOT = -5812
863945
YDOT = -13739
570969 feet/sec YDOT = -4187
821231 meter/sec
ZDOT = 5454
275868 ZDOT = 1662
463285
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 16250
51321406
00016717 00000-0 10270-3 0 9014
2 25544 51
6434 12
2516 0003011 298
1791 61
9058 15
54456093 17632
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
51321406 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 12
2516 deg
Eccentricity:
0003011
Arg of perigee: 298
1791 deg
Mean anomaly: 61
9058 deg
Mean motion: 15
54456093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1763
Checksum: 280
Coasting Arc #3 (Orbit 1768)
---------------------------------------
Vector Time (GMT): 2016/250/21:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2174769
67 A = 6778533
10 meter
Y = -4247085
82 meter E =
0010182
Z = -4824291
41 I = 51
69538
XDOT = 7183
064759 Wp = 56
67973
YDOT = -787
365788 meter/sec RA = 9
88623 deg
ZDOT = -2543
351624 TA = 188
28253
MA = 188
29935
Ha = 219
802 n
mi
Hp = 215
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7135071
09 X = -2103681
67
Y = -13934008
59 feet Y = -4271008
55 meter
Z = -15827727
74 Z = -4834682
83
XDOT = 23566
485429 XDOT = 7203
689950
YDOT = -2583
221089 feet/sec YDOT = -706
924876 meter/sec
ZDOT = -8344
329475 ZDOT = -2508
407864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8142740
86 X = 2481907
41
Y = -13317218
05 feet Y = -4059088
06 meter
Z = -15872311
57 Z = -4837880
57
XDOT = 13664
662266 XDOT = 4164
989059
YDOT = 18124
496765 feet/sec YDOT = 5524
346614 meter/sec
ZDOT = -8191
492602 ZDOT = -2496
766945
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 16250
89894829
00016717 00000-0 10270-3 0 9020
2 25544 51
6407 10
3308 0003198 307
9414 52
1449 15
54433576 17690
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
89894829 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 10
3308 deg
Eccentricity:
0003198
Arg of perigee: 307
9414 deg
Mean anomaly: 52
1449 deg
Mean motion: 15
54433576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1769
Checksum: 324
Coasting Arc #4 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2016/250/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1876473
71 A = 6778045
46 meter
Y = 4265061
74 meter E =
0003140
Z = 4920485
61 I = 51
69319
XDOT = -7300
344759 Wp = 117
01893
YDOT = 577
372852 meter/sec RA = 9
72241 deg
ZDOT = 2281
076089 TA = 310
69624
MA = 310
72351
Ha = 219
686 n
mi
Hp = 215
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6156409
83 X = 1804739
60
Y = 13992984
71 feet Y = 4285645
12 meter
Z = 16143325
48 Z = 4929426
40
XDOT = -23951
262332 XDOT = -7317
339016
YDOT = 1894
267887 feet/sec YDOT = 495
640712 meter/sec
ZDOT = 7483
845436 ZDOT = 2245
571451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5970487
61 X = -1819804
62
Y = 14029330
66 feet Y = 4276139
99 meter
Z = 16181567
28 Z = 4932141
71
XDOT = -16888
500669 XDOT = -5147
615004
YDOT = -15649
639709 feet/sec YDOT = -4770
010183 meter/sec
ZDOT = 7328
598758 ZDOT = 2233
756901
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 16250
96323700
00016717 00000-0 10270-3 0 9034
2 25544 51
6410 10
0106 0003366 306
6349 53
4494 15
54456354 17702
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
96323700 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 10
0106 deg
Eccentricity:
0003366
Arg of perigee: 306
6349 deg
Mean anomaly: 53
4494 deg
Mean motion: 15
54456354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 280
Coasting Arc #5 (Orbit 1784)
---------------------------------------
Vector Time (GMT): 2016/251/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 44367
12 A = 6776431
32 meter
Y = -4215667
98 meter E =
0012627
Z = -5316058
64 I = 51
65597
XDOT = 7643
830173 Wp = 77
47905
YDOT = 419
682335 meter/sec RA = 4
72282 deg
ZDOT = -266
878075 TA = 189
96236
MA = 189
98741
Ha = 219
829 n
mi
Hp = 215
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 145561
40 X = 117327
67
Y = -13830931
70 feet Y = -4214764
36 meter
Z = -17441137
26 Z = -5315665
53
XDOT = 25078
182982 XDOT = 7639
865454
YDOT = 1376
910547 feet/sec YDOT = 505
138573 meter/sec
ZDOT = -875
584236 ZDOT = -229
755849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10039415
40 X = 3060013
81
Y = -9519159
98 feet Y = -2901439
96 meter
Z = -17438602
60 Z = -5315286
07
XDOT = 15920
209702 XDOT = 4852
479917
YDOT = 18110
203490 feet/sec YDOT = 5519
990024 meter/sec
ZDOT = -713
472909 ZDOT = -217
466543
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 16251
92756742
00016717 00000-0 10270-3 0 9048
2 25544 51
6413 5
2010 0003328 311
3465 48
7402 15
54451357 17855
Satellite: ISS
Catalog Number: 25544
Epoch time: 16251
92756742 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 5
2010 deg
Eccentricity:
0003328
Arg of perigee: 311
3465 deg
Mean anomaly: 48
7402 deg
Mean motion: 15
54451357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1785
Checksum: 287
Coasting Arc #6 (Orbit 1800)
---------------------------------------
Vector Time (GMT): 2016/252/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1998661
13 A = 6777453
38 meter
Y = 4025975
09 meter E =
0005982
Z = 5072248
19 I = 51
62804
XDOT = -7329
408785 Wp = 20
47413
YDOT = -1379
308811 meter/sec RA = 359
72041 deg
ZDOT = -1787
155839 TA = 86
85161
MA = 86
78317
Ha = 219
955 n
mi
Hp = 214
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6557287
16 X = -2068170
90
Y = 13208579
68 feet Y = 4003236
46 meter
Z = 16641234
22 Z = 5062370
04
XDOT = -24046
616749 XDOT = -7304
759018
YDOT = -4525
291376 feet/sec YDOT = -1461
133483 meter/sec
ZDOT = -5863
372176 ZDOT = -1822
700351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14010062
12 X = -4270266
93
Y = 4758487
07 feet Y = 1450386
86 meter
Z = 16597295
82 Z = 5058855
77
XDOT = -13615
862020 XDOT = -4150
114744
YDOT = -19026
181335 feet/sec YDOT = -5799
180071 meter/sec
ZDOT = -6018
395170 ZDOT = -1834
406848
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 16252
95617409
00016717 00000-0 10270-3 0 9059
2 25544 51
6420
0712 0003443 316
0431 44
0448 15
54476260 18016
Satellite: ISS
Catalog Number: 25544
Epoch time: 16252
95617409 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node:
0712 deg
Eccentricity:
0003443
Arg of perigee: 316
0431 deg
Mean anomaly: 44
0448 deg
Mean motion: 15
54476260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1801
Checksum: 269
Coasting Arc #7 (Orbit 1815)
---------------------------------------
Vector Time (GMT): 2016/253/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3763603
98 A = 6780770
80 meter
Y = -3723080
59 meter E =
0005302
Z = -4241631
47 I = 51
60627
XDOT = 6350
802238 Wp = 89
48601
YDOT = 2296
633506 meter/sec RA = 354
72245 deg
ZDOT = 3623
175598 TA = 217
59459
MA = 217
63167
Ha = 220
038 n
mi
Hp = 214
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12347782
07 X = 3825560
71
Y = -12214831
34 feet Y = -3680647
32 meter
Z = -13916113
75 Z = -4223198
09
XDOT = 20835
965347 XDOT = 6307
048866
YDOT = 7534
886830 feet/sec YDOT = 2367
408037 meter/sec
ZDOT = 11887
059049 ZDOT = 3653
919777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17430764
91 X = 5312897
15
Y = -305136
13 feet Y = -93005
49 meter
Z = -13834860
86 Z = -4216865
59
XDOT = 9854
194513 XDOT = 3003
558488
YDOT = 18481
582239 feet/sec YDOT = 5633
186267 meter/sec
ZDOT = 12020
925216 ZDOT = 3663
978006
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 16253
92048270
00016717 00000-0 10270-3 0 9062
2 25544 51
6414 355
2620 0003523 320
8741 39
2156 15
54479176 18165
Satellite: ISS
Catalog Number: 25544
Epoch time: 16253
92048270 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 355
2620 deg
Eccentricity:
0003523
Arg of perigee: 320
8741 deg
Mean anomaly: 39
2156 deg
Mean motion: 15
54479176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1816
Checksum: 301
Coasting Arc #8 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2016/254/00:47:05
983
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -660724
40 A = 6778430
57 meter
Y = -4167358
24 meter E =
0010006
Z = -5313610
95 I = 51
58996
XDOT = 7599
880316 Wp = 78
70830
YDOT = -942
542100 meter/sec RA = 354
14170 deg
ZDOT = -204
206342 TA = 189
33294
MA = 189
35154
Ha = 220
006 n
mi
Hp = 217
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2167730
98 X = -588263
61
Y = -13672435
18 feet Y = -4174342
11 meter
Z = -17433106
79 Z = -5316644
31
XDOT = 24933
990539 XDOT = 7610
847168
YDOT = -3092
329726 feet/sec YDOT = -857
493843 meter/sec
ZDOT = -669
968315 ZDOT = -167
261338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2153279
01 X = -656319
44
Y = -13658841
36 feet Y = -4163214
85 meter
Z = -17445549
46 Z = -5317403
48
XDOT = 23918
880835 XDOT = 7290
474879
YDOT = -3114
766512 feet/sec YDOT = -949
380833 meter/sec
ZDOT = -508
384426 ZDOT = -154
955573
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 16254
04906042
00016717 00000-0 10270-3 0 9077
2 25544 51
6437 354
6206 0005271 287
3253 72
7323 15
53761140 18184
Satellite: ISS
Catalog Number: 25544
Epoch time: 16254
04906042 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 354
6206 deg
Eccentricity:
0005271
Arg of perigee: 287
3253 deg
Mean anomaly: 72
7323 deg
Mean motion: 15
53761140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 295
Coasting Arc #9 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2016/255/00:47:05
983
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -994364
60 A = 6779197
19 meter
Y = 4330404
20 meter E =
0004925
Z = 5122263
04 I = 51
56071
XDOT = -7498
973134 Wp = 347
34565
YDOT = 157
660812 meter/sec RA = 349
14248 deg
ZDOT = -1584
618441 TA = 117
98073
MA = 117
93088
Ha = 220
106 n
mi
Hp = 217
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3262351
04 X = -1067596
05
Y = 14207362
85 feet Y = 4318875
41 meter
Z = 16805324
94 Z = 5117254
53
XDOT = -24602
930231 XDOT = -7492
481425
YDOT = 517
259882 feet/sec YDOT = 73
838467 meter/sec
ZDOT = -5198
879401 ZDOT = -1621
030716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3023336
91 X = -921513
09
Y = 14286868
23 feet Y = 4354637
44 meter
Z = 16782606
17 Z = 5115338
36
XDOT = -23507
046822 XDOT = -7164
947871
YDOT = 1336
509084 feet/sec YDOT = 407
367969 meter/sec
ZDOT = -5357
976843 ZDOT = -1633
111342
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 16255
07814057
00016717 00000-0 10270-3 0 9086
2 25544 51
6435 349
4944 0005500 290
7530 69
3033 15
53797970 18342
Satellite: ISS
Catalog Number: 25544
Epoch time: 16255
07814057 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 349
4944 deg
Eccentricity:
0005500
Arg of perigee: 290
7530 deg
Mean anomaly: 69
3033 deg
Mean motion: 15
53797970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 322
Coasting Arc #10 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2016/256/00:47:05
983
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2539884
44 A = 6781898
32 meter
Y = -4418863
82 meter E =
0003914
Z = -4477815
43 I = 51
53925
XDOT = 6914
212388 Wp = 103
60743
YDOT = 703
000846 meter/sec RA = 344
14442 deg
ZDOT = 3229
575838 TA = 198
94549
MA = 198
96006
Ha = 220
303 n
mi
Hp = 217
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8332954
20 X = 2610859
71
Y = -14497584
70 feet Y = -4390064
59 meter
Z = -14690995
52 Z = -4465304
68
XDOT = 22684
423845 XDOT = 6890
149571
YDOT = 2306
433222 feet/sec YDOT = 780
185883 meter/sec
ZDOT = 10595
721253 ZDOT = 3263
104672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7817521
98 X = 2382780
70
Y = -14836851
81 feet Y = -4522272
43 meter
Z = -14635491
65 Z = -4460897
86
XDOT = 21609
876897 XDOT = 6586
690478
YDOT = 794
753511 feet/sec YDOT = 242
240870 meter/sec
ZDOT = 10742
050276 ZDOT = 3274
176924
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 16256
04289410
00016717 00000-0 10270-3 0 9094
2 25544 51
6447 344
6876 0005473 295
1643 64
8941 15
53784620 18491
Satellite: ISS
Catalog Number: 25544
Epoch time: 16256
04289410 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 344
6876 deg
Eccentricity:
0005473
Arg of perigee: 295
1643 deg
Mean anomaly: 64
8941 deg
Mean motion: 15
53784620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 339
Coasting Arc #11 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2016/257/00:47:05
983
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3891741
77 A = 6785455
01 meter
Y = 4384468
92 meter E =
0008240
Z = 3412535
86 I = 51
51989
XDOT = -5908
475459 Wp = 71
44401
YDOT = -1658
693181 meter/sec RA = 339
15359 deg
ZDOT = -4595
378281 TA = 68
56733
MA = 68
47945
Ha = 220
486 n
mi
Hp = 216
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12768181
66 X = -3957057
28
Y = 14384740
56 feet Y = 4340583
94 meter
Z = 11195983
79 Z = 3393471
89
XDOT = -19384
762003 XDOT = -5867
166199
YDOT = -5441
906761 feet/sec YDOT = -1724
535124 meter/sec
ZDOT = -15076
700397 ZDOT = -4623
979483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11972701
92 X = -3649279
55
Y = 15115490
85 feet Y = 4607201
61 meter
Z = 11111868
51 Z = 3386897
52
XDOT = -18471
140546 XDOT = -5630
003638
YDOT = -3427
290727 feet/sec YDOT = -1044
638214 meter/sec
ZDOT = -15201
316102 ZDOT = -4633
361148
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 16257
07195403
00016717 00000-0 10270-3 0 9108
2 25544 51
6441 339
5614 0005344 299
9552 60
1070 15
53789426 18655
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
07195403 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 339
5614 deg
Eccentricity:
0005344
Arg of perigee: 299
9552 deg
Mean anomaly: 60
1070 deg
Mean motion: 15
53789426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1865
Checksum: 317
Coasting Arc #12 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2016/257/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3448019
69 A = 6779106
44 meter
Y = 2863622
01 meter E =
0000557
Z = 5086456
75 I = 51
47246
XDOT = -6098
694722 Wp = 269
15642
YDOT = 4325
647600 meter/sec RA = 335
07694 deg
ZDOT = 1699
056745 TA = 164
39016
MA = 164
38844
Ha = 220
382 n
mi
Hp = 216
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11312400
56 X = 3391034
07
Y = 9395085
35 feet Y = 2901861
96 meter
Z = 16687850
23 Z = 5103067
53
XDOT = -20008
840951 XDOT = -6154
865163
YDOT = 14191
757219 feet/sec YDOT = 4257
134011 meter/sec
ZDOT = 5574
333154 ZDOT = 1669
294204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2307365
44 X = -703284
99
Y = 14439721
30 feet Y = 4401227
05 meter
Z = 16759859
61 Z = 5108405
21
XDOT = -21419
727191 XDOT = -6528
732848
YDOT = -9740
295973 feet/sec YDOT = -2968
842213 meter/sec
ZDOT = 5443
506492 ZDOT = 1659
180779
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 16257
90805574
00016717 00000-0 10270-3 0 9118
2 25544 51
6418 335
3946 0005538 301
8683 58
1930 15
53837337 18785
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
90805574 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 335
3946 deg
Eccentricity:
0005538
Arg of perigee: 301
8683 deg
Mean anomaly: 58
1930 deg
Mean motion: 15
53837337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 337
Coasting Arc #13 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2016/258/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2012058
75 A = 6778270
42 meter
Y = -3721192
80 meter E =
0010830
Z = -5305125
44 I = 51
44100
XDOT = 6678
294380 Wp = 73
66652
YDOT = -3751
559674 meter/sec RA = 330
06791 deg
ZDOT = 101
770122 TA = 197
28848
MA = 197
32539
Ha = 220
640 n
mi
Hp = 216
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6601242
63 X = -1944528
08
Y = -12208637
80 feet Y = -3743316
04 meter
Z = -17405267
19 Z = -5314734
97
XDOT = 21910
414631 XDOT = 6719
254578
YDOT = -12308
266648 feet/sec YDOT = -3676
649475 meter/sec
ZDOT = 333
891475 ZDOT = 134
311280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6938936
43 X = 2114987
82
Y = -11959938
33 feet Y = -3645389
20 meter
Z = -17446535
57 Z = -5317704
04
XDOT = 21152
493262 XDOT = 6447
279946
YDOT = 11591
928920 feet/sec YDOT = 3533
219935 meter/sec
ZDOT = 476
731609 ZDOT = 145
307795
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 16258
87278351
00016717 00000-0 10270-3 0 9123
2 25544 51
6423 330
5875 0005515 306
2998 53
7645 15
53815935 18933
Satellite: ISS
Catalog Number: 25544
Epoch time: 16258
87278351 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 330
5875 deg
Eccentricity:
0005515
Arg of perigee: 306
2998 deg
Mean anomaly: 53
7645 deg
Mean motion: 15
53815935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 340
Coasting Arc #14 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2016/259/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 525712
57 A = 6779489
73 meter
Y = 4522636
98 meter E =
0006905
Z = 5024511
66 I = 51
41777
XDOT = -6829
013012 Wp = 4
99753
YDOT = 2917
637092 meter/sec RA = 325
05834 deg
ZDOT = -1904
745680 TA = 103
57241
MA = 103
49548
Ha = 220
857 n
mi
Hp = 216
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1724778
76 X = 450693
44
Y = 14838047
84 feet Y = 4528097
08 meter
Z = 16484618
31 Z = 5026882
60
XDOT = -22404
898333 XDOT = -6851
878841
YDOT = 9572
300172 feet/sec YDOT = 2841
142378 meter/sec
ZDOT = -6249
165616 ZDOT = -1937
975067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11584268
45 X = -3530885
02
Y = 9414547
27 feet Y = 2869554
01 meter
Z = 16494125
94 Z = 5027409
59
XDOT = -19492
414372 XDOT = -5941
287901
YDOT = -12741
177922 feet/sec YDOT = -3883
511031 meter/sec
ZDOT = -6394
839851 ZDOT = -1949
147186
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 16259
90181635
00016717 00000-0 10270-3 0 9137
2 25544 51
6424 325
4612 0005525 311
4587 48
6091 15
53827191 19092
Satellite: ISS
Catalog Number: 25544
Epoch time: 16259
90181635 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 325
4612 deg
Eccentricity:
0005525
Arg of perigee: 311
4587 deg
Mean anomaly: 48
6091 deg
Mean motion: 15
53827191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1909
Checksum: 313
Coasting Arc #15 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2016/260/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 859308
45 A = 6782395
07 meter
Y = -5185643
21 meter E =
0004039
Z = -4288918
77 I = 51
40086
XDOT = 6557
581689 Wp = 74
74629
YDOT = -1823
968628 meter/sec RA = 320
05188 deg
ZDOT = 3522
990937 TA = 231
26246
MA = 231
29857
Ha = 220
969 n
mi
Hp = 216
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2819253
44 X = 938065
46
Y = -17013265
13 feet Y = -5175594
12 meter
Z = -14071255
81 Z = -4284552
42
XDOT = 21514
375620 XDOT = 6560
377244
YDOT = -5984
149041 feet/sec YDOT = -1750
621206 meter/sec
ZDOT = 11558
369216 ZDOT = 3554
853037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15749916
94 X = 4800574
68
Y = -7064194
23 feet Y = -2153166
40 meter
Z = -14051224
03 Z = -4282813
08
XDOT = 16399
300501 XDOT = 4998
506793
YDOT = 13319
966033 feet/sec YDOT = 4059
925647 meter/sec
ZDOT = 11697
854339 ZDOT = 3565
506003
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 16260
86652681
00016717 00000-0 10270-3 0 9149
2 25544 51
6415 320
6547 0005560 315
0359 45
0343 15
53839738 19240
Satellite: ISS
Catalog Number: 25544
Epoch time: 16260
86652681 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 320
6547 deg
Eccentricity:
0005560
Arg of perigee: 315
0359 deg
Mean anomaly: 45
0343 deg
Mean motion: 15
53839738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 313
Coasting Arc #16 (Orbit 1939)
---------------------------------------
Vector Time (GMT): 2016/261/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2104181
41 A = 6785979
90 meter
Y = 5636712
71 meter E =
0009684
Z = 3134135
55 I = 51
38940
XDOT = -5935
861924 Wp = 71
06276
YDOT = 477
207875 meter/sec RA = 315
05256 deg
ZDOT = -4828
107125 TA = 72
69309
MA = 72
58717
Ha = 221
095 n
mi
Hp = 216
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6903482
30 X = -2182280
51
Y = 18493151
93 feet Y = 5612746
12 meter
Z = 10282596
94 Z = 3123723
41
XDOT = -19474
612611 XDOT = -5917
304065
YDOT = 1565
642635 feet/sec YDOT = 410
932147 meter/sec
ZDOT = -15840
246473 ZDOT = -4856
897149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19160024
34 X = -5839975
42
Y = 4847935
44 feet Y = 1477650
72 meter
Z = 10236089
36 Z = 3119960
04
XDOT = -11999
527301 XDOT = -3657
455921
YDOT = -13606
579757 feet/sec YDOT = -4147
285510 meter/sec
ZDOT = -15966
055846 ZDOT = -4866
453822
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 16261
89554350
00016717 00000-0 10270-3 0 9158
2 25544 51
6419 315
5277 0005629 318
6124 41
4602 15
53862323 19404
Satellite: ISS
Catalog Number: 25544
Epoch time: 16261
89554350 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 315
5277 deg
Eccentricity:
0005629
Arg of perigee: 318
6124 deg
Mean anomaly: 41
4602 deg
Mean motion: 15
53862323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1940
Checksum: 306
Coasting Arc #17 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2016/262/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3092617
83 A = 6788902
61 meter
Y = -5791205
04 meter E =
0010685
Z = -1702368
59 I = 51
37690
XDOT = 5054
224801 Wp = 6
86307
YDOT = 1034
858044 meter/sec RA = 310
05954 deg
ZDOT = 5675
449415 TA = 334
39709
MA = 334
44996
Ha = 221
245 n
mi
Hp = 216
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10146383
96 X = 3165416
15
Y = -19000016
55 feet Y = -5756214
51 meter
Z = -5585198
79 Z = -1687167
71
XDOT = 16582
102364 XDOT = 5014
708004
YDOT = 3395
203557 feet/sec YDOT = 1091
157592 meter/sec
ZDOT = 18620
240864 ZDOT = 5699
905641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21365103
84 X = 6512083
65
Y = -2868942
08 feet Y = -874453
55 meter
Z = -5517761
44 Z = -1681813
69
XDOT = 6674
180657 XDOT = 2034
290264
YDOT = 13776
023539 feet/sec YDOT = 4198
931975 meter/sec
ZDOT = 18726
841180 ZDOT = 5707
941192
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 16262
86023881
00016717 00000-0 10270-3 0 9167
2 25544 51
6418 310
7204 0005666 322
8439 37
2321 15
53862227 19557
Satellite: ISS
Catalog Number: 25544
Epoch time: 16262
86023881 = yrday
fracday
Element set: 916
Inclination: 51
6418 deg
RA of node: 310
7204 deg
Eccentricity:
0005666
Arg of perigee: 322
8439 deg
Mean anomaly: 37
2321 deg
Mean motion: 15
53862227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 308
Coasting Arc #18 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2016/263/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3844332
52 A = 6790077
71 meter
Y = 5593182
84 meter E =
0006872
Z = 84400
79 I = 51
36135
XDOT = -3989
071550 Wp = 123
07602
YDOT = -2646
159398 meter/sec RA = 305
07129 deg
ZDOT = -5986
125947 TA = 56
01182
MA = 55
94654
Ha = 221
360 n
mi
Hp = 216
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12612639
51 X = -3907001
18
Y = 18350337
39 feet Y = 5549842
54 meter
Z = 276905
48 Z = 65572
91
XDOT = -13087
505085 XDOT = -3930
106718
YDOT = -8681
625321 feet/sec YDOT = -2690
438888 meter/sec
ZDOT = -19639
520825 ZDOT = -6005
360524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22249570
18 X = -6781668
99
Y = 899639
45 feet Y = 274210
10 meter
Z = 193675
66 Z = 59032
34
XDOT = -750
330426 XDOT = -228
700714
YDOT = -13956
391949 feet/sec YDOT = -4253
908266 meter/sec
ZDOT = -19723
024047 ZDOT = -6011
577729
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 16263
88924026
00016717 00000-0 10270-3 0 9172
2 25544 51
6422 305
5929 0005606 326
9759 33
1043 15
53869314 19710
Satellite: ISS
Catalog Number: 25544
Epoch time: 16263
88924026 = yrday
fracday
Element set: 917
Inclination: 51
6422 deg
RA of node: 305
5929 deg
Eccentricity:
0005606
Arg of perigee: 326
9759 deg
Mean anomaly: 33
1043 deg
Mean motion: 15
53869314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 326
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