[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 24th 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) : 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
113/17:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 213
8
Coasting Arc #1 (Orbit 3629)
---------------------------------------
Vector Time (GMT): 2016/113/08:50:29
423
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4520265
49 A = 6785988
76 meter
Y = 4315900
62 meter E =
0014774
Z = 2628333
80 I = 51
50700
XDOT = -5169
343180 Wp = 97
16565
YDOT = -2225
702906 meter/sec RA = 335
86311 deg
ZDOT = -5212
223015 TA = 53
14495
MA = 53
00958
Ha = 221
319 n
mi
Hp = 213
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14830267
35 X = -4580958
56
Y = 14159778
94 feet Y = 4265012
83 meter
Z = 8623142
40 Z = 2606227
37
XDOT = -16959
787337 XDOT = -5118
751407
YDOT = -7302
174890 feet/sec YDOT = -2283
227414 meter/sec
ZDOT = -17100
469210 ZDOT = -5237
211827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18435763
53 X = -5619220
72
Y = 9067521
09 feet Y = 2763780
43 meter
Z = 8526279
29 Z = 2598809
93
XDOT = -13237
182506 XDOT = -4034
693228
YDOT = -10659
078793 feet/sec YDOT = -3248
887216 meter/sec
ZDOT = -17208
552840 ZDOT = -5245
166906
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
40581334
00016717 00000-0 10270-3 0 9007
2 25544 51
6433 336
2795 0001797 50
4408 309
6903 15
54293174 36307
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
40581334 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 336
2795 deg
Eccentricity:
0001797
Arg of perigee: 50
4408 deg
Mean anomaly: 309
6903 deg
Mean motion: 15
54293174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3630
Checksum: 298
Coasting Arc #2 (Orbit 3634)
---------------------------------------
Vector Time (GMT): 2016/113/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -238652
11 A = 6777623
91 meter
Y = -4430332
37 meter E =
0014943
Z = -5136902
28 I = 51
46749
XDOT = 7193
038245 Wp = 97
71902
YDOT = -2143
997864 meter/sec RA = 334
14177 deg
ZDOT = 1516
747851 TA = 186
93811
MA = 186
95881
Ha = 221
255 n
mi
Hp = 213
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -782979
38 X = -164139
96
Y = -14535211
17 feet Y = -4432584
82 meter
Z = -16853353
93 Z = -5137880
36
XDOT = 23599
206839 XDOT = 7209
110509
YDOT = -7034
113727 feet/sec YDOT = -2063
470567 meter/sec
ZDOT = 4976
206861 ZDOT = 1551
729669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13675262
08 X = -4168219
88
Y = 4975847
26 feet Y = 1516638
24 meter
Z = -16856723
00 Z = -5137929
17
XDOT = -13374
112671 XDOT = -4076
429542
YDOT = -19402
732757 feet/sec YDOT = -5913
952944 meter/sec
ZDOT = 5128
553200 ZDOT = 1563
183015
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
72728660
00016717 00000-0 10270-3 0 9018
2 25544 51
6417 334
6723 0001621 65
4582 294
6740 15
54314491 36350
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
72728660 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 334
6723 deg
Eccentricity:
0001621
Arg of perigee: 65
4582 deg
Mean anomaly: 294
6740 deg
Mean motion: 15
54314491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3635
Checksum: 302
Coasting Arc #3 (Orbit 3650)
---------------------------------------
Vector Time (GMT): 2016/114/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1458450
26 A = 6780718
64 meter
Y = 4949613
98 meter E =
0011062
Z = 4392269
22 I = 51
44835
XDOT = -6832
188661 Wp = 70
38287
YDOT = 971
223005 meter/sec RA = 329
13207 deg
ZDOT = -3352
550824 TA = 53
63832
MA = 53
53630
Ha = 221
344 n
mi
Hp = 213
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4784941
79 X = -1535025
86
Y = 16238891
02 feet Y = 4932876
66 meter
Z = 14410332
08 Z = 4384998
08
XDOT = -22415
317128 XDOT = -6826
255760
YDOT = 3186
427181 feet/sec YDOT = 894
853951 meter/sec
ZDOT = -10999
182493 ZDOT = -3385
726177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16950180
50 X = 5166415
02
Y = -475275
18 feet Y = -144863
87 meter
Z = 14377775
02 Z = 4382345
83
XDOT = 10013
689801 XDOT = 3052
172651
YDOT = 18973
776734 feet/sec YDOT = 5783
207149 meter/sec
ZDOT = -11143
443626 ZDOT = -3396
521617
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 16114
75600000
00016717 00000-0 10270-3 0 9020
2 25544 51
6410 329
5422 0001602 71
6095 288
5232 15
54284930 36519
Satellite: ISS
Catalog Number: 25544
Epoch time: 16114
75600000 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 329
5422 deg
Eccentricity:
0001602
Arg of perigee: 71
6095 deg
Mean anomaly: 288
5232 deg
Mean motion: 15
54284930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3651
Checksum: 273
Coasting Arc #4 (Orbit 3665)
---------------------------------------
Vector Time (GMT): 2016/115/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2912867
78 A = 6784547
70 meter
Y = -5237760
11 meter E =
0006039
Z = -3183055
34 I = 51
43553
XDOT = 5962
967635 Wp = 75
00855
YDOT = 407
117562 meter/sec RA = 324
13156 deg
ZDOT = 4796
053468 TA = 248
12954
MA = 248
19377
Ha = 221
246 n
mi
Hp = 213
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9556652
82 X = 2986683
44
Y = -17184252
33 feet Y = -5204773
85 meter
Z = -10443094
94 Z = -3168725
64
XDOT = 19563
542111 XDOT = 5934
674349
YDOT = 1335
687539 feet/sec YDOT = 473
641369 meter/sec
ZDOT = 15735
083558 ZDOT = 4824
951899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19400676
49 X = -5913326
19
Y = -3399885
43 feet Y = -1036285
08 meter
Z = -10379831
59 Z = -3163772
67
XDOT = -5421
244852 XDOT = -1652
395431
YDOT = -17394
601925 feet/sec YDOT = -5301
874667 meter/sec
ZDOT = 15860
493804 ZDOT = 4834
278511
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 16115
72041174
00016717 00000-0 10270-3 0 9030
2 25544 51
6421 324
7336 0001516 68
1469 291
9845 15
54312706 36669
Satellite: ISS
Catalog Number: 25544
Epoch time: 16115
72041174 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 324
7336 deg
Eccentricity:
0001516
Arg of perigee: 68
1469 deg
Mean anomaly: 291
9845 deg
Mean motion: 15
54312706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3666
Checksum: 303
Coasting Arc #5 (Orbit 3681)
---------------------------------------
Vector Time (GMT): 2016/116/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4071250
41 A = 6787729
78 meter
Y = 5187776
30 meter E =
0015053
Z = 1579624
24 I = 51
42123
XDOT = -4721
133869 Wp = 113
05547
YDOT = -1951
245300 meter/sec RA = 319
13943 deg
ZDOT = -5722
068694 TA = 49
60830
MA = 49
47702
Ha = 221
238 n
mi
Hp = 213
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13357120
78 X = -4136632
11
Y = 17020263
46 feet Y = 5141883
33 meter
Z = 5182494
23 Z = 1559687
90
XDOT = -15489
284347 XDOT = -4671
167834
YDOT = -6401
723424 feet/sec YDOT = -2003
760864 meter/sec
ZDOT = -18773
191252 ZDOT = -5744
881794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20608429
94 X = 6281449
45
Y = 6655442
54 feet Y = 2028578
89 meter
Z = 5094898
47 Z = 1552925
05
XDOT = -190
269251 XDOT = -57
994068
YDOT = 15132
378289 feet/sec YDOT = 4612
348903 meter/sec
ZDOT = -18871
868991 ZDOT = -5752
145669
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 16116
74911255
00016717 00000-0 10270-3 0 9040
2 25544 51
6424 319
6037 0001548 73
3580 286
7743 15
54328043 36828
Satellite: ISS
Catalog Number: 25544
Epoch time: 16116
74911255 = yrday
fracday
Element set: 904
Inclination: 51
6424 deg
RA of node: 319
6037 deg
Eccentricity:
0001548
Arg of perigee: 73
3580 deg
Mean anomaly: 286
7743 deg
Mean motion: 15
54328043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3682
Checksum: 312
Coasting Arc #6 (Orbit 3697)
---------------------------------------
Vector Time (GMT): 2016/117/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4816399
65 A = 6788713
76 meter
Y = -4772425
16 meter E =
0013984
Z = 164583
38 I = 51
40138
XDOT = 3259
845284 Wp = 50
08216
YDOT = 3507
862866 meter/sec RA = 314
15251 deg
ZDOT = 5991
073585 TA = 311
69713
MA = 311
81669
Ha = 221
265 n
mi
Hp = 213
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15801836
14 X = 4868608
65
Y = -15657562
87 feet Y = -4718273
06 meter
Z = 539971
72 Z = 188107
43
XDOT = 10695
030459 XDOT = 3191
274711
YDOT = 11508
736438 feet/sec YDOT = 3543
933255 meter/sec
ZDOT = 19655
753230 ZDOT = 6006
742766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20323454
95 X = -6194589
07
Y = -9038391
61 feet Y = -2754901
76 meter
Z = 643059
84 Z = 196004
64
XDOT = 6231
120808 XDOT = 1899
245622
YDOT = -12543
235252 feet/sec YDOT = -3823
178105 meter/sec
ZDOT = 19723
103839 ZDOT = 6011
602050
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 16117
77780813
00016717 00000-0 10270-3 0 9059
2 25544 51
6428 314
4746 0001664 73
9996 286
1340 15
54335459 36981
Satellite: ISS
Catalog Number: 25544
Epoch time: 16117
77780813 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 314
4746 deg
Eccentricity:
0001664
Arg of perigee: 73
9996 deg
Mean anomaly: 286
1340 deg
Mean motion: 15
54335459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3698
Checksum: 344
Coasting Arc #7 (Orbit 3712)
---------------------------------------
Vector Time (GMT): 2016/118/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5187448
06 A = 6787028
52 meter
Y = 3924033
26 meter E =
0007725
Z = -1932284
69 I = 51
37447
XDOT = -1694
476845 Wp = 129
66359
YDOT = -4977
117234 meter/sec RA = 309
16325 deg
ZDOT = -5578
114900 TA = 71
71393
MA = 71
62989
Ha = 221
175 n
mi
Hp = 213
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17019186
54 X = -5221555
71
Y = 12874124
86 feet Y = 3865833
05 meter
Z = -6339516
70 Z = -1957567
17
XDOT = -5559
307235 XDOT = -1611
599132
YDOT = -16329
124783 feet/sec YDOT = -4995
602615 meter/sec
ZDOT = -18300
901902 ZDOT = -5586
145033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18346636
03 X = 5592054
66
Y = 10834335
66 feet Y = 3302305
51 meter
Z = -6450069
04 Z = -1965981
04
XDOT = -12261
323968 XDOT = -3737
251545
YDOT = 9885
599841 feet/sec YDOT = 3013
130831 meter/sec
ZDOT = -18334
797541 ZDOT = -5588
446291
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 16118
74220495
00016717 00000-0 10270-3 0 9063
2 25544 51
6429 309
6660 0001571 79
0557 281
0772 15
54354676 37133
Satellite: ISS
Catalog Number: 25544
Epoch time: 16118
74220495 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 309
6660 deg
Eccentricity:
0001571
Arg of perigee: 79
0557 deg
Mean anomaly: 281
0772 deg
Mean motion: 15
54354676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3713
Checksum: 320
Coasting Arc #8 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2016/119/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5169276
93 A = 6783441
78 meter
Y = -2710763
79 meter E =
0013841
Z = 3444151
84 I = 51
34435
XDOT = 200
871723 Wp = 89
83563
YDOT = 6178
031418 meter/sec RA = 304
16461 deg
ZDOT = 4545
199691 TA = 310
76344
MA = 310
88349
Ha = 221
071 n
mi
Hp = 213
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16959569
98 X = 5182474
81
Y = -8893581
98 feet Y = -2652883
69 meter
Z = 11299710
77 Z = 3469295
20
XDOT = 659
027962 XDOT = 109
693674
YDOT = 20269
131950 feet/sec YDOT = 6179
767912 meter/sec
ZDOT = 14912
072477 ZDOT = 4545
953997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14836479
67 X = -4522159
00
Y = -12004596
15 feet Y = -3659000
91 meter
Z = 11409418
05 Z = 3477590
62
XDOT = 17526
524680 XDOT = 5342
084723
YDOT = -7437
478673 feet/sec YDOT = -2266
943499 meter/sec
ZDOT = 14914
147997 ZDOT = 4545
832310
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 16119
77088789
00016717 00000-0 10270-3 0 9076
2 25544 51
6439 304
5367 0001588 81
6491 278
4841 15
54388516 37290
Satellite: ISS
Catalog Number: 25544
Epoch time: 16119
77088789 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 304
5367 deg
Eccentricity:
0001588
Arg of perigee: 81
6491 deg
Mean anomaly: 278
4841 deg
Mean motion: 15
54388516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 360
Coasting Arc #9 (Orbit 3743)
---------------------------------------
Vector Time (GMT): 2016/120/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4858553
69 A = 6779615
54 meter
Y = 1153037
27 meter E =
0011834
Z = -4597275
61 I = 51
31360
XDOT = 1158
127615 Wp = 71
31903
YDOT = -6962
660741 meter/sec RA = 299
15413 deg
ZDOT = -2972
829441 TA = 168
87461
MA = 168
84842
Ha = 221
193 n
mi
Hp = 213
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15940136
79 X = -4848754
39
Y = 3782930
67 feet Y = 1098760
43 meter
Z = -15082925
23 Z = -4620853
64
XDOT = 3799
631282 XDOT = 1250
340585
YDOT = -22843
375135 feet/sec YDOT = -6949
194228 meter/sec
ZDOT = -9753
377430 ZDOT = -2966
979449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9951810
79 X = 3033311
93
Y = 12893962
29 feet Y = 3930079
71 meter
Z = -15185531
18 Z = -4628549
90
XDOT = -21475
966794 XDOT = -6545
874679
YDOT = 5130
196807 feet/sec YDOT = 1563
683987 meter/sec
ZDOT = -9726
634363 ZDOT = -2964
678154
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 16120
73527507
00016717 00000-0 10270-3 0 9081
2 25544 51
6435 299
7287 0001536 81
3110 278
8217 15
54351290 37447
Satellite: ISS
Catalog Number: 25544
Epoch time: 16120
73527507 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 299
7287 deg
Eccentricity:
0001536
Arg of perigee: 81
3110 deg
Mean anomaly: 278
8217 deg
Mean motion: 15
54351290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3744
Checksum: 312
Coasting Arc #10 (Orbit 3759)
---------------------------------------
Vector Time (GMT): 2016/121/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4302365
29 A = 6776918
15 meter
Y = 588033
20 meter E =
0005031
Z = 5199159
35 I = 51
29019
XDOT = -2296
502018 Wp = 111
50612
YDOT = 7240
855787 meter/sec RA = 294
13209 deg
ZDOT = 1078
773205 TA = 328
09816
MA = 328
12862
Ha = 220
981 n
mi
Hp = 213
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14115371
67 X = 4270214
53
Y = 1929242
77 feet Y = 635965
46 meter
Z = 17057609
42 Z = 5219981
21
XDOT = -7534
455441 XDOT = -2382
540648
YDOT = 23756
088540 feet/sec YDOT = 7214
693727 meter/sec
ZDOT = 3539
282169 ZDOT = 1067
408155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4221399
46 X = -1286682
56
Y = -13492834
91 feet Y = -4112616
08 meter
Z = 17147913
19 Z = 5226683
94
XDOT = 23727
889689 XDOT = 7232
260777
YDOT = -2978
977010 feet/sec YDOT = -907
992193 meter/sec
ZDOT = 3488
551131 ZDOT = 1063
310385
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 16121
76394770
00016717 00000-0 10270-3 0 9090
2 25544 51
6435 294
5994 0001547 83
8431 276
2898 15
54403354 37604
Satellite: ISS
Catalog Number: 25544
Epoch time: 16121
76394770 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 294
5994 deg
Eccentricity:
0001547
Arg of perigee: 83
8431 deg
Mean anomaly: 276
2898 deg
Mean motion: 15
54403354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3760
Checksum: 338
Coasting Arc #11 (Orbit 3774)
---------------------------------------
Vector Time (GMT): 2016/122/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3609097
27 A = 6776904
02 meter
Y = -2389205
79 meter E =
0015912
Z = -5228629
23 I = 51
27745
XDOT = 3192
573250 Wp = 95
75917
YDOT = -6894
926079 meter/sec RA = 289
10525 deg
ZDOT = 947
849146 TA = 183
36484
MA = 183
37555
Ha = 221
154 n
mi
Hp = 213
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11840870
32 X = -3556713
70
Y = -7838601
67 feet Y = -2429272
40 meter
Z = -17154295
37 Z = -5246034
15
XDOT = 10474
321686 XDOT = 3264
832474
YDOT = -22621
148554 feet/sec YDOT = -6858
820543 meter/sec
ZDOT = 3109
741292 ZDOT = 963
533739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1853739
08 X = -565019
67
Y = 13986792
91 feet Y = 4263174
48 meter
Z = -17229422
84 Z = -5251528
08
XDOT = -23892
279105 XDOT = -7282
366671
YDOT = 745
883893 feet/sec YDOT = 227
345411 meter/sec
ZDOT = 3179
149299 ZDOT = 969
004706
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 16122
72832425
00016717 00000-0 10270-3 0 9103
2 25544 51
6432 289
7910 0001574 81
7208 278
4123 15
54390947 37758
Satellite: ISS
Catalog Number: 25544
Epoch time: 16122
72832425 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 289
7910 deg
Eccentricity:
0001574
Arg of perigee: 81
7208 deg
Mean anomaly: 278
4123 deg
Mean motion: 15
54390947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3775
Checksum: 315
Coasting Arc #12 (Orbit 3790)
---------------------------------------
Vector Time (GMT): 2016/123/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2810950
15 A = 6779294
49 meter
Y = 4065624
19 meter E =
0009746
Z = 4633860
15 I = 51
27621
XDOT = -3873
715493 Wp = 66
95486
YDOT = 5965
861694 meter/sec RA = 284
08020 deg
ZDOT = -2875
861169 TA = 51
80317
MA = 51
71544
Ha = 221
042 n
mi
Hp = 213
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9222277
38 X = 2742768
86
Y = 13338662
05 feet Y = 4096677
09 meter
Z = 15202953
23 Z = 4647349
41
XDOT = -12709
040330 XDOT = -3926
169497
YDOT = 19573
037053 feet/sec YDOT = 5922
249817 meter/sec
ZDOT = -9435
240056 ZDOT = -2894
806577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7695767
83 X = 2345670
03
Y = -14212114
01 feet Y = -4331852
35 meter
Z = 15260768
84 Z = 4651482
34
XDOT = 22152
587580 XDOT = 6752
108695
YDOT = 1744
384355 feet/sec YDOT = 531
688351 meter/sec
ZDOT = -9518
620256 ZDOT = -2901
275454
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 16123
75698535
00016717 00000-0 10270-3 0 9110
2 25544 51
6433 284
6610 0001613 80
7781 279
3554 15
54418206 37914
Satellite: ISS
Catalog Number: 25544
Epoch time: 16123
75698535 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 284
6610 deg
Eccentricity:
0001613
Arg of perigee: 80
7781 deg
Mean anomaly: 279
3554 deg
Mean motion: 15
54418206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 318
Coasting Arc #13 (Orbit 3805)
---------------------------------------
Vector Time (GMT): 2016/124/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1997725
90 A = 6783187
77 meter
Y = -5440932
36 meter E =
0006790
Z = -3530075
23 I = 51
28095
XDOT = 4333
409973 Wp = 93
54793
YDOT = -4478
596779 meter/sec RA = 279
06536 deg
ZDOT = 4457
581120 TA = 224
64019
MA = 224
69488
Ha = 221
130 n
mi
Hp = 213
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6554218
84 X = -1919587
72
Y = -17850827
95 feet Y = -5462835
53 meter
Z = -11581611
63 Z = -3539589
78
XDOT = 14217
224321 XDOT = 4361
515364
YDOT = -14693
558985 feet/sec YDOT = -4429
980353 meter/sec
ZDOT = 14624
609974 ZDOT = 4478
700520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12676139
16 X = -3863687
21
Y = 14141783
52 feet Y = 4310415
62 meter
Z = -11621920
07 Z = -3542361
24
XDOT = -18588
815552 XDOT = -5665
870980
YDOT = -4586
415589 feet/sec YDOT = -1397
939471 meter/sec
ZDOT = 14717
144357 ZDOT = 4485
785600
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 16124
72135162
00016717 00000-0 10270-3 0 9121
2 25544 51
6420 279
8528 0001615 87
9139 272
2198 15
54411193 38063
Satellite: ISS
Catalog Number: 25544
Epoch time: 16124
72135162 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 279
8528 deg
Eccentricity:
0001615
Arg of perigee: 87
9139 deg
Mean anomaly: 272
2198 deg
Mean motion: 15
54411193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3806
Checksum: 308
Coasting Arc #14 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2016/125/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1139765
30 A = 6786803
06 meter
Y = 6382610
57 meter E =
0015448
Z = 1982454
27 I = 51
28926
XDOT = -4638
969416 Wp = 109
17980
YDOT = 2560
887517 meter/sec RA = 274
06050 deg
ZDOT = -5547
369915 TA = 48
81294
MA = 48
67982
Ha = 221
118 n
mi
Hp = 213
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3739387
48 X = 1058678
56
Y = 20940323
41 feet Y = 6394902
88 meter
Z = 6504115
05 Z = 1987793
86
XDOT = -15219
715931 XDOT = -4640
313880
YDOT = 8401
861931 feet/sec YDOT = 2509
003740 meter/sec
ZDOT = -18200
032530 ZDOT = -5569
908654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16484196
39 X = 5024383
06
Y = -13433710
66 feet Y = -4094595
01 meter
Z = 6526129
25 Z = 1989164
20
XDOT = 13715
322682 XDOT = 4180
430353
YDOT = 7891
963046 feet/sec YDOT = 2405
470336 meter/sec
ZDOT = -18298
371753 ZDOT = -5577
343710
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 16125
75000185
00016717 00000-0 10270-3 0 9132
2 25544 51
6423 274
7227 0001646 86
5342 273
5999 15
54421404 38228
Satellite: ISS
Catalog Number: 25544
Epoch time: 16125
75000185 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 274
7227 deg
Eccentricity:
0001646
Arg of perigee: 86
5342 deg
Mean anomaly: 273
5999 deg
Mean motion: 15
54421404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 304
Coasting Arc #15 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2016/126/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -302436
21 A = 6788581
50 meter
Y = -6772007
70 meter E =
0013007
Z = -239177
49 I = 51
29370
XDOT = 4784
772569 Wp = 48
06012
YDOT = -417
127397 meter/sec RA = 269
06306 deg
ZDOT = 5978
740882 TA = 309
35003
MA = 309
46522
Ha = 221
208 n
mi
Hp = 213
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -992244
79 X = -225525
60
Y = -22217873
04 feet Y = -6774959
72 meter
Z = -784703
04 Z = -240459
73
XDOT = 15698
072732 XDOT = 4760
038590
YDOT = -1368
528205 feet/sec YDOT = -363
759055 meter/sec
ZDOT = 19615
291608 ZDOT = 6001
924550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18716233
71 X = -5704708
03
Y = 12013085
00 feet Y = 3661588
31 meter
Z = -789034
77 Z = -240497
80
XDOT = -8126
950834 XDOT = -2477
094614
YDOT = -11413
554051 feet/sec YDOT = -3478
851275 meter/sec
ZDOT = 19716
038749 ZDOT = 6009
448611
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 16126
71435466
00016717 00000-0 10270-3 0 9144
2 25544 51
6425 269
9132 0001693 81
0051 279
1293 15
54376753 38371
Satellite: ISS
Catalog Number: 25544
Epoch time: 16126
71435466 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 269
9132 deg
Eccentricity:
0001693
Arg of perigee: 81
0051 deg
Mean anomaly: 279
1293 deg
Mean motion: 15
54376753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 319
Coasting Arc #16 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2016/127/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -586431
48 A = 6787381
52 meter
Y = 6573046
99 meter E =
0009233
Z = -1575530
40 I = 51
29116
XDOT = -4788
932037 Wp = 133
35565
YDOT = -1790
033826 meter/sec RA = 264
06770 deg
ZDOT = -5712
822091 TA = 63
95734
MA = 63
86232
Ha = 221
165 n
mi
Hp = 213
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1923987
79 X = -652235
92
Y = 21565114
81 feet Y = 6566121
20 meter
Z = -5169062
98 Z = -1578539
01
XDOT = -15711
719283 XDOT = -4740
808442
YDOT = -5872
814391 feet/sec YDOT = -1843
317755 meter/sec
ZDOT = -18742
854628 ZDOT = -5735
969174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19435689
89 X = 5923998
28
Y = -9532169
06 feet Y = -2905405
13 meter
Z = -5183322
25 Z = -1579876
62
XDOT = 2338
189870 XDOT = 712
680272
YDOT = 14965
080095 feet/sec YDOT = 4561
356413 meter/sec
ZDOT = -18843
045254 ZDOT = -5743
360193
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 16127
74299281
00016717 00000-0 10270-3 0 9152
2 25544 51
6419 264
7837 0001796 89
2323 270
9036 15
54433021 38539
Satellite: ISS
Catalog Number: 25544
Epoch time: 16127
74299281 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 264
7837 deg
Eccentricity:
0001796
Arg of perigee: 89
2323 deg
Mean anomaly: 270
9036 deg
Mean motion: 15
54433021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 325
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