[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 11th 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) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 67 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
104/12:22:23
007 1
8 1
8 1
8
N/A 0
3 -0
2 221
3
000/00:04:42
014 -0
1 -0
0 214
4
109/04:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 214
0
113/16:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 3413)
---------------------------------------
Vector Time (GMT): 2016/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1849830
32 A = 6777099
04 meter
Y = -3933345
56 meter E =
0016031
Z = -5213732
76 I = 51
88780
XDOT = 6011
472008 Wp = 73
48601
YDOT = 4559
144888 meter/sec RA = 44
97826 deg
ZDOT = -1305
528971 TA = 183
99205
MA = 184
00485
Ha = 221
259 n
mi
Hp = 213
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6068997
12 X = 1919002
94
Y = -12904677
02 feet Y = -3912273
35 meter
Z = -17105422
46 Z = -5204578
16
XDOT = 19722
677191 XDOT = 5966
385519
YDOT = 14957
824436 feet/sec YDOT = 4626
116925 meter/sec
ZDOT = -4283
231531 ZDOT = -1276
436341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2301231
30 X = 701415
30
Y = -14122779
78 feet Y = -4304623
28 meter
Z = -17064885
53 Z = -5201377
11
XDOT = 22128
507211 XDOT = 6744
768998
YDOT = 8633
949872 feet/sec YDOT = 2631
627921 meter/sec
ZDOT = -4157
661753 ZDOT = -1267
255302
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 16099
51827351
00016717 00000-0 10270-3 0 9004
2 25544 51
6423 45
5226 0002614 36
5494 323
5837 15
54400486 34141
Satellite: ISS
Catalog Number: 25544
Epoch time: 16099
51827351 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 45
5226 deg
Eccentricity:
0002614
Arg of perigee: 36
5494 deg
Mean anomaly: 323
5837 deg
Mean motion: 15
54400486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3414
Checksum: 299
Coasting Arc #2 (Orbit 3429)
---------------------------------------
Vector Time (GMT): 2016/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3308165
43 A = 6776685
28 meter
Y = 2643288
26 meter E =
0005774
Z = 5287351
70 I = 51
86375
XDOT = -5459
073654 Wp = 50
47991
YDOT = -5339
864327 meter/sec RA = 39
99271 deg
ZDOT = -741
944149 TA = 46
60629
MA = 46
55823
Ha = 221
393 n
mi
Hp = 213
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10853561
11 X = -3363161
54
Y = 8672205
57 feet Y = 2605987
12 meter
Z = 17346954
41 Z = 5271147
40
XDOT = -17910
346634 XDOT = -5395
352128
YDOT = -17519
239918 feet/sec YDOT = -5400
555097 meter/sec
ZDOT = -2434
199965 ZDOT = -768
308122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7886716
98 X = -2403871
33
Y = 11543938
91 feet Y = 3518592
58 meter
Z = 17276021
97 Z = 5265731
50
XDOT = -21455
585600 XDOT = -6539
662491
YDOT = -10825
124785 feet/sec YDOT = -3299
498035 meter/sec
ZDOT = -2547
746015 ZDOT = -776
552985
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 16100
54691999
00016717 00000-0 10270-3 0 9018
2 25544 51
6428 40
3938 0002707 38
4984 321
6362 15
54423556 34300
Satellite: ISS
Catalog Number: 25544
Epoch time: 16100
54691999 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 40
3938 deg
Eccentricity:
0002707
Arg of perigee: 38
4984 deg
Mean anomaly: 321
6362 deg
Mean motion: 15
54423556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3430
Checksum: 312
Coasting Arc #3 (Orbit 3444)
---------------------------------------
Vector Time (GMT): 2016/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4639228
47 A = 6778937
39 meter
Y = -1328117
10 meter E =
0012378
Z = -4772308
85 I = 51
84566
XDOT = 4392
601482 Wp = 97
07823
YDOT = 5664
603334 meter/sec RA = 35
00754 deg
ZDOT = 2698
178734 TA = 199
51319
MA = 199
56061
Ha = 221
327 n
mi
Hp = 213
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15220565
86 X = 4676917
15
Y = -4357339
57 feet Y = -1276027
75 meter
Z = -15657181
28 Z = -4749680
70
XDOT = 14411
422184 XDOT = 4315
825235
YDOT = 18584
656607 feet/sec YDOT = 5713
295222 meter/sec
ZDOT = 8852
292434 ZDOT = 2719
330328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13177578
08 X = 4016525
80
Y = -8948811
56 feet Y = -2727597
76 meter
Z = -15558584
98 Z = -4742256
70
XDOT = 18811
229879 XDOT = 5733
662867
YDOT = 12177
698223 feet/sec YDOT = 3711
762418 meter/sec
ZDOT = 8943
109577 ZDOT = 2725
859799
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 16101
51126828
00016717 00000-0 10270-3 0 9021
2 25544 51
6424 35
5849 0002700 43
1310 317
0054 15
54428713 34455
Satellite: ISS
Catalog Number: 25544
Epoch time: 16101
51126828 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 35
5849 deg
Eccentricity:
0002700
Arg of perigee: 43
1310 deg
Mean anomaly: 317
0054 deg
Mean motion: 15
54428713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3445
Checksum: 270
Coasting Arc #4 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2016/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5696389
54 A = 6782786
81 meter
Y = 41371
65 meter E =
0013994
Z = 3672508
26 I = 51
83250
XDOT = -2866
023880 Wp = 78
42180
YDOT = -5619
912336 meter/sec RA = 30
03014 deg
ZDOT = -4365
358181 TA = 58
01204
MA = 57
87610
Ha = 221
361 n
mi
Hp = 213
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18688942
05 X = -5714268
45
Y = 135733
77 feet Y = -22428
94 meter
Z = 12048911
60 Z = 3644792
89
XDOT = -9402
965486 XDOT = -2781
762350
YDOT = -18438
032600 feet/sec YDOT = -5651
491212 meter/sec
ZDOT = -14322
041277 ZDOT = -4379
075806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17667851
83 X = -5385161
24
Y = 6326934
19 feet Y = 1928449
54 meter
Z = 11928460
30 Z = 3635794
70
XDOT = -14416
752119 XDOT = -4394
226046
YDOT = -13041
294827 feet/sec YDOT = -3974
986663 meter/sec
ZDOT = -14380
550194 ZDOT = -4383
191699
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 16102
53989712
00016717 00000-0 10270-3 0 9034
2 25544 51
6430 30
4557 0002628 45
0177 315
1189 15
54449524 34612
Satellite: ISS
Catalog Number: 25544
Epoch time: 16102
53989712 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 30
4557 deg
Eccentricity:
0002628
Arg of perigee: 45
0177 deg
Mean anomaly: 315
1189 deg
Mean motion: 15
54449524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 300
Coasting Arc #5 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2016/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6335725
40 A = 6786436
11 meter
Y = 1075297
00 meter E =
0009001
Z = -2173928
02 I = 51
81670
XDOT = 992
127886 Wp = 43
22604
YDOT = 5243
053339 meter/sec RA = 25
06144 deg
ZDOT = 5504
715799 TA = 292
71525
MA = 292
81036
Ha = 221
348 n
mi
Hp = 213
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20786500
65 X = 6333790
36
Y = 3527877
28 feet Y = 1146136
37 meter
Z = -7132309
76 Z = -2143155
17
XDOT = 3255
012750 XDOT = 906
685282
YDOT = 17201
618566 feet/sec YDOT = 5253
670491 meter/sec
ZDOT = 18060
091203 ZDOT = 5509
327568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20763784
12 X = 6328801
40
Y = -3908517
76 feet Y = -1191316
21 meter
Z = -6998794
73 Z = -2133232
63
XDOT = 8619
520688 XDOT = 2627
229906
YDOT = 13536
237717 feet/sec YDOT = 4125
845256 meter/sec
ZDOT = 18079
096042 ZDOT = 5510
508473
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 16103
50422565
00016717 00000-0 10270-3 0 9041
2 25544 51
6431 25
6463 0002675 48
2529 311
8852 15
54458080 34766
Satellite: ISS
Catalog Number: 25544
Epoch time: 16103
50422565 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 25
6463 deg
Eccentricity:
0002675
Arg of perigee: 48
2529 deg
Mean anomaly: 311
8852 deg
Mean motion: 15
54458080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3476
Checksum: 301
Coasting Arc #6 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6455553
89 A = 6788297
09 meter
Y = -2048823
77 meter E =
0013508
Z = 374105
82 I = 51
79411
XDOT = 1112
278082 Wp = 119
67842
YDOT = -4630
643118 meter/sec RA = 20
09983 deg
ZDOT = -6010
575260 TA = 56
29690
MA = 56
16820
Ha = 221
310 n
mi
Hp = 213
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21179638
75 X = -6433980
90
Y = -6721862
77 feet Y = -2120893
43 meter
Z = 1227381
29 Z = 342798
72
XDOT = 3649
206306 XDOT = 1193
173334
YDOT = -15192
398682 feet/sec YDOT = -4617
752877 meter/sec
ZDOT = -19719
735104 ZDOT = -6004
975349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22182609
21 X = -6761259
29
Y = 1416668
55 feet Y = 431800
57 meter
Z = 1091741
96 Z = 332762
95
XDOT = -1886
094159 XDOT = -574
881500
YDOT = -13911
852282 feet/sec YDOT = -4240
332575 meter/sec
ZDOT = -19694
481889 ZDOT = -6002
878080
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 16104
53283183
00016717 00000-0 10270-3 0 9057
2 25544 51
6436 20
5164 0002675 53
2501 306
8897 15
54467460 34922
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53283183 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 20
5164 deg
Eccentricity:
0002675
Arg of perigee: 53
2501 deg
Mean anomaly: 306
8897 deg
Mean motion: 15
54467460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 303
Coasting Arc #7 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1661011
02 A = 6777309
17 meter
Y = -3864203
17 meter E =
0015599
Z = -5327617
84 I = 51
75417
XDOT = 7133
017018 Wp = 85
99111
YDOT = 2776
143194 meter/sec RA = 20
01541 deg
ZDOT = 211
905790 TA = 186
01889
MA = 186
03765
Ha = 221
296 n
mi
Hp = 214
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5449511
21 X = 1729977
43
Y = -12677831
91 feet Y = -3845243
29 meter
Z = -17479061
16 Z = -5319381
32
XDOT = 23402
286805 XDOT = 7100
414000
YDOT = 9108
081345 feet/sec YDOT = 2855
727050 meter/sec
ZDOT = 695
228969 ZDOT = 246
477019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -910819
53 X = -277617
79
Y = -13815631
80 feet Y = -4211004
57 meter
Z = -17442502
66 Z = -5316474
81
XDOT = 23953
974640 XDOT = 7301
171470
YDOT = -2639
286688 feet/sec YDOT = -804
454582 meter/sec
ZDOT = 844
908284 ZDOT = 257
528045
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 16104
53283226
00016717 00000-0 10270-3 0 9066
2 25544 51
6439 20
5161 0001659 26
2931 333
8305 15
54152367 34921
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53283226 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 20
5161 deg
Eccentricity:
0001659
Arg of perigee: 26
2931 deg
Mean anomaly: 333
8305 deg
Mean motion: 15
54152367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 291
Coasting Arc #8 (Orbit 3507)
---------------------------------------
Vector Time (GMT): 2016/105/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3333687
87 A = 6778729
62 meter
Y = 3169616
07 meter E =
0007696
Z = 4975574
38 I = 51
72852
XDOT = -6496
057339 Wp = 50
25478
YDOT = -3481
519055 meter/sec RA = 15
02427 deg
ZDOT = -2127
584204 TA = 60
47121
MA = 60
39449
Ha = 221
301 n
mi
Hp = 214
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10937296
17 X = -3393052
79
Y = 10399002
84 feet Y = 3132004
92 meter
Z = 16324062
93 Z = 4959235
74
XDOT = -21312
524077 XDOT = -6446
308414
YDOT = -11422
306612 feet/sec YDOT = -3553
884255 meter/sec
ZDOT = -6980
263136 ZDOT = -2159
019444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4755833
54 X = -1449578
06
Y = 14404135
54 feet Y = 4390380
51 meter
Z = 16252435
66 Z = 4953742
39
XDOT = -23090
259421 XDOT = -7037
911072
YDOT = 431
555180 feet/sec YDOT = 131
538019 meter/sec
ZDOT = -7116
168780 ZDOT = -2169
008244
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 16105
56165104
00016717 00000-0 10270-3 0 9075
2 25544 51
6436 15
3882 0001596 23
2436 336
8789 15
54189550 35088
Satellite: ISS
Catalog Number: 25544
Epoch time: 16105
56165104 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 15
3882 deg
Eccentricity:
0001596
Arg of perigee: 23
2436 deg
Mean anomaly: 336
8789 deg
Mean motion: 15
54189550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 317
Coasting Arc #9 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2016/106/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4799727
41 A = 6782088
42 meter
Y = -2455300
11 meter E =
0007740
Z = -4121976
66 I = 51
70964
XDOT = 5311
690938 Wp = 96
49571
YDOT = 3995
213230 meter/sec RA = 10
03668 deg
ZDOT = 3810
559374 TA = 212
80352
MA = 212
85159
Ha = 221
272 n
mi
Hp = 214
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15747137
17 X = 4846849
28
Y = -8055446
57 feet Y = -2401363
20 meter
Z = -13523545
47 Z = -4098546
12
XDOT = 17426
807538 XDOT = 5248
110609
YDOT = 13107
654955 feet/sec YDOT = 4054
256873 meter/sec
ZDOT = 12501
835217 ZDOT = 3836
207548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9832418
15 X = 2996921
05
Y = -14796705
26 feet Y = -4510035
76 meter
Z = -13421247
97 Z = -4090796
38
XDOT = 20469
670125 XDOT = 6239
155454
YDOT = 2177
908931 feet/sec YDOT = 663
826642 meter/sec
ZDOT = 12612
485990 ZDOT = 3844
285730
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 16106
52615893
00016717 00000-0 10270-3 0 9088
2 25544 51
6449 10
5798 0001600 26
6663 333
4571 15
54180706 35233
Satellite: ISS
Catalog Number: 25544
Epoch time: 16106
52615893 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 10
5798 deg
Eccentricity:
0001600
Arg of perigee: 26
6663 deg
Mean anomaly: 333
4571 deg
Mean motion: 15
54180706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 305
Coasting Arc #10 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2016/107/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5937958
03 A = 6785959
04 meter
Y = 1695072
40 meter E =
0014222
Z = 2799929
85 I = 51
69032
XDOT = -3672
312630 Wp = 94
21377
YDOT = -4381
275256 meter/sec RA = 5
05833 deg
ZDOT = -5114
287765 TA = 54
03222
MA = 53
90040
Ha = 221
386 n
mi
Hp = 214
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19481489
59 X = -5970072
31
Y = 5561261
15 feet Y = 1628490
88 meter
Z = 9186121
54 Z = 2771006
53
XDOT = -12048
269783 XDOT = -3598
204123
YDOT = -14374
262650 feet/sec YDOT = -4421
927574 meter/sec
ZDOT = -16779
159334 ZDOT = -5131
946598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14035647
34 X = -4278065
31
Y = 14688627
98 feet Y = 4477093
81 meter
Z = 9060116
05 Z = 2761523
37
XDOT = -16503
491760 XDOT = -5030
264288
YDOT = -5329
632606 feet/sec YDOT = -1624
472018 meter/sec
ZDOT = -16855
013982 ZDOT = -5137
408262
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 16107
55495688
00016717 00000-0 10270-3 0 9091
2 25544 51
6444 5
4517 0001640 35
7361 324
3901 15
54176133 35392
Satellite: ISS
Catalog Number: 25544
Epoch time: 16107
55495688 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 5
4517 deg
Eccentricity:
0001640
Arg of perigee: 35
7361 deg
Mean anomaly: 324
3901 deg
Mean motion: 15
54176133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 307
Coasting Arc #11 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2016/108/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6607382
61 A = 6788480
11 meter
Y = -946970
71 meter E =
0010813
Z = -1210270
67 I = 51
66748
XDOT = 1730
868152 Wp = 36
59369
YDOT = 4634
793338 meter/sec RA =
08637 deg
ZDOT = 5858
515473 TA = 310
26003
MA = 310
35454
Ha = 221
242 n
mi
Hp = 214
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21677764
48 X = 6623359
80
Y = -3106859
30 feet Y = -872993
35 meter
Z = -3970704
31 Z = -1178134
63
XDOT = 5678
701287 XDOT = 1650
453830
YDOT = 15206
014889 feet/sec YDOT = 4653
699994 meter/sec
ZDOT = 19220
851288 ZDOT = 5866
727871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16905861
27 X = 5152906
51
Y = -13959248
17 feet Y = -4254778
84 meter
Z = -3830898
82 Z = -1167657
96
XDOT = 11646
705604 XDOT = 3549
915868
YDOT = 8853
844497 feet/sec YDOT = 2698
651803 meter/sec
ZDOT = 19255
609916 ZDOT = 5869
109902
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 16108
51944383
00016717 00000-0 10270-3 0 9101
2 25544 51
6446
6436 0001550 31
1921 328
9323 15
54220558 35549
Satellite: ISS
Catalog Number: 25544
Epoch time: 16108
51944383 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node:
6436 deg
Eccentricity:
0001550
Arg of perigee: 31
1921 deg
Mean anomaly: 328
9323 deg
Mean motion: 15
54220558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 284
Coasting Arc #12 (Orbit 3564)
---------------------------------------
Vector Time (GMT): 2016/109/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5498819
68 A = 6784489
00 meter
Y = -2273461
16 meter E =
0005814
Z = -3265241
60 I = 51
62888
XDOT = 4475
595130 Wp = 82
37276
YDOT = -4020
107142 meter/sec RA = 356
70968 deg
ZDOT = -4744
562302 TA = 135
47887
MA = 135
43214
Ha = 221
305 n
mi
Hp = 214
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18040746
99 X = -5457127
35
Y = -7458862
07 feet Y = -2334719
83 meter
Z = -10712734
90 Z = -3291852
16
XDOT = 14683
711055 XDOT = 4543
263517
YDOT = -13189
327895 feet/sec YDOT = -3969
680174 meter/sec
ZDOT = -15566
149284 ZDOT = -4722
656092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4757800
58 X = 1450177
62
Y = -18867591
80 feet Y = -5750841
98 meter
Z = -10827888
88 Z = -3300340
53
XDOT = 13830
764874 XDOT = 4215
617133
YDOT = 12353
730904 feet/sec YDOT = 3765
417180 meter/sec
ZDOT = -15470
183049 ZDOT = -4715
311793
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 16109
22672893
00016717 00000-0 10270-3 0 9115
2 25544 51
6412 357
1161 0001608 44
1045 316
0235 15
54205366 35654
Satellite: ISS
Catalog Number: 25544
Epoch time: 16109
22672893 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 357
1161 deg
Eccentricity:
0001608
Arg of perigee: 44
1045 deg
Mean anomaly: 316
0235 deg
Mean motion: 15
54205366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3565
Checksum: 283
Coasting Arc #13 (Orbit 3580)
---------------------------------------
Vector Time (GMT): 2016/110/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4192982
51 A = 6780560
17 meter
Y = 2943779
99 meter E =
0009747
Z = 4434623
54 I = 51
58408
XDOT = -5967
840288 Wp = 101
85576
YDOT = 3514
307219 meter/sec RA = 351
72127 deg
ZDOT = 3301
692789 TA = 314
79067
MA = 314
86990
Ha = 221
146 n
mi
Hp = 214
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13756504
29 X = 4138211
10
Y = 9658070
83 feet Y = 2990362
91 meter
Z = 14549289
84 Z = 4454858
86
XDOT = -19579
528505 XDOT = -6022
732959
YDOT = 11529
879329 feet/sec YDOT = 3447
264264 meter/sec
ZDOT = 10832
325424 ZDOT = 3272
568566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7304649
78 X = -2226457
25
Y = 15053683
40 feet Y = 4588362
70 meter
Z = 14636607
69 Z = 4461238
02
XDOT = -13479
968695 XDOT = -4108
694458
YDOT = -16975
235614 feet/sec YDOT = -5174
051815 meter/sec
ZDOT = 10705
112893 ZDOT = 3262
918410
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 16110
25549807
00016717 00000-0 10270-3 0 9129
2 25544 51
6412 351
9877 0001578 40
4586 319
6684 15
54237065 35811
Satellite: ISS
Catalog Number: 25544
Epoch time: 16110
25549807 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 351
9877 deg
Eccentricity:
0001578
Arg of perigee: 40
4586 deg
Mean anomaly: 319
6684 deg
Mean motion: 15
54237065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3581
Checksum: 324
Coasting Arc #14 (Orbit 3595)
---------------------------------------
Vector Time (GMT): 2016/111/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2573217
23 A = 6777743
51 meter
Y = -3595721
31 meter E =
0015236
Z = -5150459
59 I = 51
54226
XDOT = 6950
499105 Wp = 75
11531
YDOT = -2850
270254 meter/sec RA = 346
72001 deg
ZDOT = -1482
504352 TA = 180
56912
MA = 180
57085
Ha = 221
316 n
mi
Hp = 213
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8442313
76 X = -2507798
69
Y = -11796985
93 feet Y = -3624131
45 meter
Z = -16897833
30 Z = -5162800
56
XDOT = 22803
474754 XDOT = 6989
056421
YDOT = -9351
280361 feet/sec YDOT = -2772
329701 meter/sec
ZDOT = -4863
859423 ZDOT = -1448
646215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10107336
76 X = 3080716
24
Y = -10319543
81 feet Y = -3145396
95 meter
Z = -16950724
70 Z = -5166580
89
XDOT = 12553
502136 XDOT = 3826
307451
YDOT = 20042
980589 feet/sec YDOT = 6109
100483 meter/sec
ZDOT = -4716
226835 ZDOT = -1437
505939
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 16111
21996277
00016717 00000-0 10270-3 0 9134
2 25544 51
6405 347
1793 0001684 45
8191 314
3099 15
54231330 35963
Satellite: ISS
Catalog Number: 25544
Epoch time: 16111
21996277 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 347
1793 deg
Eccentricity:
0001684
Arg of perigee: 45
8191 deg
Mean anomaly: 314
3099 deg
Mean motion: 15
54231330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3596
Checksum: 311
Coasting Arc #15 (Orbit 3611)
---------------------------------------
Vector Time (GMT): 2016/112/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 789985
47 A = 6777102
62 meter
Y = 4164732
50 meter E =
0004329
Z = 5284662
01 I = 51
50893
XDOT = -7382
618924 Wp = 59
25521
YDOT = 2027
841099 meter/sec RA = 341
71162 deg
ZDOT = -492
028559 TA = 35
45922
MA = 35
43044
Ha = 221
247 n
mi
Hp = 214
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2591815
83 X = 717684
65
Y = 13663820
54 feet Y = 4173162
83 meter
Z = 17338129
94 Z = 5288323
66
XDOT = -24221
190694 XDOT = -7402
355953
YDOT = 6653
021977 feet/sec YDOT = 1945
173344 meter/sec
ZDOT = -1614
266927 ZDOT = -527
940155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12910314
76 X = -3935063
94
Y = 5120372
13 feet Y = 1560689
43 meter
Z = 17353207
57 Z = 5289257
67
XDOT = -10912
739336 XDOT = -3326
202950
YDOT = -21486
736807 feet/sec YDOT = -6549
157379 meter/sec
ZDOT = -1770
643736 ZDOT = -539
692211
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 16112
24871710
00016717 00000-0 10270-3 0 9143
2 25544 51
6402 342
0504 0001593 45
9793 314
1490 15
54244832 36125
Satellite: ISS
Catalog Number: 25544
Epoch time: 16112
24871710 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 342
0504 deg
Eccentricity:
0001593
Arg of perigee: 45
9793 deg
Mean anomaly: 314
1490 deg
Mean motion: 15
54244832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3612
Checksum: 282
Coasting Arc #16 (Orbit 3626)
---------------------------------------
Vector Time (GMT): 2016/113/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 976104
18 A = 6779003
49 meter
Y = -4633679
60 meter E =
0012653
Z = -4862552
75 I = 51
48576
XDOT = 7198
596116 Wp = 100
53914
YDOT = -1010
573144 meter/sec RA = 336
70274 deg
ZDOT = 2411
131893 TA = 193
16992
MA = 193
20299
Ha = 221
297 n
mi
Hp = 214
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3202441
54 X = 1051467
22
Y = -15202360
88 feet Y = -4622343
11 meter
Z = -15953257
06 Z = -4857627
62
XDOT = 23617
441325 XDOT = 7197
649122
YDOT = -3315
528687 feet/sec YDOT = -930
078780 meter/sec
ZDOT = 7910
537707 ZDOT = 2446
099282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15558867
68 X = 4742342
87
Y = -18531
47 feet Y = -5648
39 meter
Z = -15930948
25 Z = -4855753
03
XDOT = 8270
259479 XDOT = 2520
775089
YDOT = 21179
725020 feet/sec YDOT = 6455
580186 meter/sec
ZDOT = 8062
601311 ZDOT = 2457
480880
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 16113
21316532
00016717 00000-0 10270-3 0 9158
2 25544 51
6409 337
2420 0001678 47
2054 312
9239 15
54248637 36274
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
21316532 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 337
2420 deg
Eccentricity:
0001678
Arg of perigee: 47
2054 deg
Mean anomaly: 312
9239 deg
Mean motion: 15
54248637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3627
Checksum: 296
Coasting Arc #17 (Orbit 3634)
---------------------------------------
Vector Time (GMT): 2016/113/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3811586
58 A = 6784774
12 meter
Y = 4629896
57 meter E =
0014175
Z = 3160560
88 I = 51
49018
XDOT = -5788
223972 Wp = 91
12492
YDOT = -1464
301737 meter/sec RA = 334
25731 deg
ZDOT = -4817
016668 TA = 52
30342
MA = 52
17498
Ha = 221
315 n
mi
Hp = 214
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12505205
30 X = -3878428
89
Y = 15189949
38 feet Y = 4586899
33 meter
Z = 10369294
23 Z = 3141882
15
XDOT = -18990
236128 XDOT = -5748
020146
YDOT = -4804
139556 feet/sec YDOT = -1528
805011 meter/sec
ZDOT = -15803
860459 ZDOT = -4845
037207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16848867
73 X = 5135534
88
Y = 10243289
92 feet Y = 3122154
77 meter
Z = 10287256
80 Z = 3135555
87
XDOT = -1277
316985 XDOT = -389
326217
YDOT = 18155
872375 feet/sec YDOT = 5533
909900 meter/sec
ZDOT = -15925
259454 ZDOT = -4854
019082
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 16113
72753522
00016717 00000-0 10270-3 0 9169
2 25544 51
6403 334
6730 0001447 62
4102 297
7198 15
54261218 36353
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
72753522 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 334
6730 deg
Eccentricity:
0001447
Arg of perigee: 62
4102 deg
Mean anomaly: 297
7198 deg
Mean motion: 15
54261218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3635
Checksum: 296
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