[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 26th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 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
124/02:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 3677)
---------------------------------------
Vector Time (GMT): 2016/116/10:22:01
355
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5875223
36 A = 6786732
41 meter
Y = -2619680
28 meter E =
0015516
Z = 2139260
07 I = 51
42625
XDOT = 379
014027 Wp = 68
11562
YDOT = 5350
834562 meter/sec RA = 320
58821 deg
ZDOT = 5485
248714 TA = 315
68988
MA = 315
81397
Ha = 221
140 n
mi
Hp = 213
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19275667
20 X = 5893688
83
Y = -8594751
57 feet Y = -2553876
34 meter
Z = 7018569
78 Z = 2167845
85
XDOT = 1243
484340 XDOT = 292
506029
YDOT = 17555
231501 feet/sec YDOT = 5354
589351 meter/sec
ZDOT = 17996
222814 ZDOT = 5486
879687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17744219
01 X = 5408437
96
Y = -11348944
51 feet Y = -3459158
29 meter
Z = 7143218
63 Z = 2177253
04
XDOT = 2889
426789 XDOT = 880
697285
YDOT = 15901
983529 feet/sec YDOT = 4846
924580 meter/sec
ZDOT = 18002
247440 ZDOT = 5487
085020
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
49194078
00016717 00000-0 10270-3 0 9004
2 25544 51
6436 320
8910 0001723 50
1326 309
9978 15
54331604 36781
Satellite: ISS
Catalog Number: 25544
Epoch time: 16116
49194078 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 320
8910 deg
Eccentricity:
0001723
Arg of perigee: 50
1326 deg
Mean anomaly: 309
9978 deg
Mean motion: 15
54331604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3678
Checksum: 309
Coasting Arc #2 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2016/117/10:22:01
355
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5561075
62 A = 6783039
16 meter
Y = 1380376
34 meter E =
0007137
Z = -3638046
19 I = 51
38860
XDOT = 1317
660205 Wp = 73
51656
YDOT = -6161
941662 meter/sec RA = 315
59119 deg
ZDOT = -4357
307804 TA = 149
79534
MA = 149
75418
Ha = 221
192 n
mi
Hp = 213
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18244998
74 X = -5558425
67
Y = 4528793
76 feet Y = 1318203
48 meter
Z = -11935847
09 Z = -3665054
51
XDOT = 4323
032168 XDOT = 1407
632904
YDOT = -20216
344037 feet/sec YDOT = -6146
703674 meter/sec
ZDOT = -14295
629279 ZDOT = -4350
688258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17170375
36 X = -5233530
41
Y = 7466471
42 feet Y = 2275780
49 meter
Z = -12053398
36 Z = -3673875
82
XDOT = 1559
168663 XDOT = 475
234608
YDOT = -19417
101031 feet/sec YDOT = -5918
332394 meter/sec
ZDOT = -14265
671128 ZDOT = -4348
176560
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
45634567
00016717 00000-0 10270-3 0 9014
2 25544 51
6424 316
0818 0001684 53
2116 306
9191 15
54325088 36939
Satellite: ISS
Catalog Number: 25544
Epoch time: 16117
45634567 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 316
0818 deg
Eccentricity:
0001684
Arg of perigee: 53
2116 deg
Mean anomaly: 306
9191 deg
Mean motion: 15
54325088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 307
Coasting Arc #3 (Orbit 3708)
---------------------------------------
Vector Time (GMT): 2016/118/10:22:01
355
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4883132
02 A = 6779287
59 meter
Y = 71035
00 meter E =
0008824
Z = 4695811
29 I = 51
35375
XDOT = -2755
640598 Wp = 106
84755
YDOT = 6608
081553 meter/sec RA = 310
58207 deg
ZDOT = 2758
786076 TA = 315
70622
MA = 315
77680
Ha = 221
147 n
mi
Hp = 213
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16020774
35 X = 4859164
24
Y = 233054
46 feet Y = 125507
43 meter
Z = 15406205
03 Z = 4719474
42
XDOT = -9040
815609 XDOT = -2842
730177
YDOT = 21680
057587 feet/sec YDOT = 6576
779206 meter/sec
ZDOT = 9051
135419 ZDOT = 2745
188142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15697753
27 X = 4784675
20
Y = -2669058
87 feet Y = -813529
14 meter
Z = 15508944
04 Z = 4727126
14
XDOT = -5192
775245 XDOT = -1582
757895
YDOT = 21830
690251 feet/sec YDOT = 6653
994388 meter/sec
ZDOT = 8990
793753 ZDOT = 2740
393936
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
48504141
00016717 00000-0 10270-3 0 9023
2 25544 51
6425 310
9526 0001811 57
7714 302
3614 15
54316651 37098
Satellite: ISS
Catalog Number: 25544
Epoch time: 16118
48504141 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 310
9526 deg
Eccentricity:
0001811
Arg of perigee: 57
7714 deg
Mean anomaly: 302
3614 deg
Mean motion: 15
54316651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3709
Checksum: 285
Coasting Arc #4 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2016/119/10:22:01
355
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3966456
68 A = 6776889
32 meter
Y = -1674182
85 meter E =
0016066
Z = -5247687
38 I = 51
32547
XDOT = 3867
991285 Wp = 80
95769
YDOT = -6555
577769 meter/sec RA = 305
56049 deg
ZDOT = -831
883407 TA = 181
04133
MA = 181
04468
Ha = 221
170 n
mi
Hp = 213
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13013309
32 X = -3921949
49
Y = -5492725
89 feet Y = -1718289
57 meter
Z = -17216822
10 Z = -5266847
52
XDOT = 12690
260122 XDOT = 3945
050886
YDOT = -21507
801079 feet/sec YDOT = -6511
892454 meter/sec
ZDOT = -2729
276271 ZDOT = -812
906294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13737598
54 X = -4187220
03
Y = -2816758
67 feet Y = -858548
04 meter
Z = -17299695
87 Z = -5272947
30
XDOT = 7967
705094 XDOT = 2428
556513
YDOT = -22604
981500 feet/sec YDOT = -6889
998361 meter/sec
ZDOT = -2645
595406 ZDOT = -806
377480
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
44943624
00016717 00000-0 10270-3 0 9034
2 25544 51
6420 306
1424 0001668 58
6885 301
4431 15
54363556 37246
Satellite: ISS
Catalog Number: 25544
Epoch time: 16119
44943624 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 306
1424 deg
Eccentricity:
0001668
Arg of perigee: 58
6885 deg
Mean anomaly: 301
4431 deg
Mean motion: 15
54363556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 304
Coasting Arc #5 (Orbit 3739)
---------------------------------------
Vector Time (GMT): 2016/120/10:22:01
355
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2891231
44 A = 6777181
31 meter
Y = 3267660
25 meter E =
0005748
Z = 5182193
55 I = 51
30839
XDOT = -4639
641683 Wp = 57
83885
YDOT = 5994
053329 meter/sec RA = 300
53579 deg
ZDOT = -1187
074704 TA = 43
61729
MA = 43
57186
Ha = 221
117 n
mi
Hp = 213
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9485667
45 X = 2829303
70
Y = 10720670
11 feet Y = 3299645
71 meter
Z = 17001947
35 Z = 5196088
10
XDOT = -15221
921533 XDOT = -4700
557511
YDOT = 19665
529293 feet/sec YDOT = 5941
829158 meter/sec
ZDOT = -3894
602046 ZDOT = -1209
761114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11469313
17 X = 3495846
66
Y = 8445813
70 feet Y = 2574284
02 meter
Z = 17061651
58 Z = 5200391
40
XDOT = -9978
031430 XDOT = -3041
303980
YDOT = 21645
253276 feet/sec YDOT = 6597
473199 meter/sec
ZDOT = -3994
271104 ZDOT = -1217
453833
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
47812029
00016717 00000-0 10270-3 0 9044
2 25544 51
6419 301
0129 0001694 63
7176 296
4150 15
54353432 37400
Satellite: ISS
Catalog Number: 25544
Epoch time: 16120
47812029 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 301
0129 deg
Eccentricity:
0001694
Arg of perigee: 63
7176 deg
Mean anomaly: 296
4150 deg
Mean motion: 15
54353432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3740
Checksum: 288
Coasting Arc #6 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2016/121/10:22:01
355
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1792014
21 A = 6779827
17 meter
Y = -4707096
33 meter E =
0011217
Z = -4549391
55 I = 51
30005
XDOT = 5047
772612 Wp = 104
43011
YDOT = -4878
786425 meter/sec RA = 295
51386 deg
ZDOT = 3063
200352 TA = 196
37868
MA = 196
41495
Ha = 221
187 n
mi
Hp = 213
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5879311
70 X = -1717145
95
Y = -15443229
41 feet Y = -4726717
29 meter
Z = -14925825
29 Z = -4557914
83
XDOT = 16560
933767 XDOT = 5087
073443
YDOT = -16006
517144 feet/sec YDOT = -4822
119072 meter/sec
ZDOT = 10049
869920 ZDOT = 3087
816892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9216936
19 X = -2809322
15
Y = -13675834
12 feet Y = -4168394
24 meter
Z = -14961936
70 Z = -4560398
31
XDOT = 11323
323717 XDOT = 3451
349069
YDOT = -18731
433666 feet/sec YDOT = -5709
340981 meter/sec
ZDOT = 10157
696057 ZDOT = 3096
065758
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
44250758
00016717 00000-0 10270-3 0 9058
2 25544 51
6401 296
2035 0001660 69
0206 291
1125 15
54368781 37551
Satellite: ISS
Catalog Number: 25544
Epoch time: 16121
44250758 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 296
2035 deg
Eccentricity:
0001660
Arg of perigee: 69
0206 deg
Mean anomaly: 291
1125 deg
Mean motion: 15
54368781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 293
Coasting Arc #7 (Orbit 3770)
---------------------------------------
Vector Time (GMT): 2016/122/10:22:01
355
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 697617
98 A = 6783712
44 meter
Y = 5840055
45 meter E =
0013871
Z = 3368737
85 I = 51
30122
XDOT = -5174
209977 Wp = 87
74239
YDOT = 3288
335561 meter/sec RA = 290
50088 deg
ZDOT = -4612
145544 TA = 52
70172
MA = 52
57535
Ha = 221
061 n
mi
Hp = 213
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2288772
90 X = 615897
17
Y = 19160286
90 feet Y = 5847399
85 meter
Z = 11052289
53 Z = 3371928
06
XDOT = -16975
754517 XDOT = -5188
192414
YDOT = 10788
502496 feet/sec YDOT = 3230
395781 meter/sec
ZDOT = -15131
711102 ZDOT = -4637
314820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6924401
84 X = 2110557
68
Y = 18003493
40 feet Y = 5487464
79 meter
Z = 11065037
91 Z = 3372623
55
XDOT = -12343
139869 XDOT = -3762
189032
YDOT = 14149
206202 feet/sec YDOT = 4312
678050 meter/sec
ZDOT = -15241
626592 ZDOT = -4645
647785
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
47118122
00016717 00000-0 10270-3 0 9061
2 25544 51
6410 291
0734 0001512 64
8653 295
2657 15
54400616 37712
Satellite: ISS
Catalog Number: 25544
Epoch time: 16122
47118122 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 291
0734 deg
Eccentricity:
0001512
Arg of perigee: 64
8653 deg
Mean anomaly: 295
2657 deg
Mean motion: 15
54400616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3771
Checksum: 287
Coasting Arc #8 (Orbit 3785)
---------------------------------------
Vector Time (GMT): 2016/123/10:22:01
355
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 285184
59 A = 6787180
91 meter
Y = -6526058
68 meter E =
0008669
Z = -1833574
17 I = 51
30073
XDOT = 5042
183893 Wp = 45
32948
YDOT = -1350
823177 meter/sec RA = 285
49758 deg
ZDOT = 5614
470608 TA = 294
41062
MA = 294
50105
Ha = 221
204 n
mi
Hp = 213
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 935644
99 X = 367046
22
Y = -21410953
68 feet Y = -6522411
92 meter
Z = -6015663
29 Z = -1831989
70
XDOT = 16542
598073 XDOT = 5029
641433
YDOT = -4431
834570 feet/sec YDOT = -1294
508020 meter/sec
ZDOT = 18420
179159 ZDOT = 5638
934111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4754409
47 X = -1449144
01
Y = -20899697
83 feet Y = -6370227
90 meter
Z = -6007561
48 Z = -1831104
74
XDOT = 13130
320343 XDOT = 4002
121641
YDOT = -8291
276675 feet/sec YDOT = -2527
181131 meter/sec
ZDOT = 18526
660103 ZDOT = 5646
926000
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
43555995
00016717 00000-0 10270-3 0 9072
2 25544 51
6394 286
2635 0001685 75
8882 284
2458 15
54376656 37865
Satellite: ISS
Catalog Number: 25544
Epoch time: 16123
43555995 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 286
2635 deg
Eccentricity:
0001685
Arg of perigee: 75
8882 deg
Mean anomaly: 284
2458 deg
Mean motion: 15
54376656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3786
Checksum: 361
Coasting Arc #9 (Orbit 3796)
---------------------------------------
Vector Time (GMT): 2016/124/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4156795
78 A = 6776559
94 meter
Y = 831380
30 meter E =
0004137
Z = 5283357
71 I = 51
26142
XDOT = -1575
304331 Wp = 83
00751
YDOT = 7508
921734 meter/sec RA = 282
19741 deg
ZDOT = 58
269492 TA = 6
43728
MA = 6
43197
Ha = 221
059 n
mi
Hp = 213
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13637781
44 X = 4121525
55
Y = 2727625
67 feet Y = 877667
39 meter
Z = 17333850
74 Z = 5303464
92
XDOT = -5168
321296 XDOT = -1659
436940
YDOT = 24635
569992 feet/sec YDOT = 7490
835221 meter/sec
ZDOT = 191
172875 ZDOT = 50
412275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6229847
69 X = -1898857
57
Y = 12312144
48 feet Y = 3752741
64 meter
Z = 17421007
49 Z = 5309923
08
XDOT = -21474
163402 XDOT = -6545
325005
YDOT = -11083
897641 feet/sec YDOT = -3378
372001 meter/sec
ZDOT = 155
658097 ZDOT = 47
444588
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
14276798
00016717 00000-0 10270-3 0 9083
2 25544 51
6408 282
7396 0001802 70
9978 289
1370 15
54397928 37973
Satellite: ISS
Catalog Number: 25544
Epoch time: 16124
14276798 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 282
7396 deg
Eccentricity:
0001802
Arg of perigee: 70
9978 deg
Mean anomaly: 289
1370 deg
Mean motion: 15
54397928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3797
Checksum: 360
Coasting Arc #10 (Orbit 3811)
---------------------------------------
Vector Time (GMT): 2016/125/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3710813
89 A = 6777865
47 meter
Y = -2688656
41 meter E =
0014481
Z = -5007228
43 I = 51
25975
XDOT = 2448
918433 Wp = 101
09587
YDOT = -6991
111031 meter/sec RA = 277
16865 deg
ZDOT = 1941
097605 TA = 187
85721
MA = 187
87992
Ha = 221
220 n
mi
Hp = 213
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12174586
27 X = -3656149
51
Y = -8821051
22 feet Y = -2729847
78 meter
Z = -16427914
81 Z = -5025122
04
XDOT = 8034
509293 XDOT = 2517
483603
YDOT = -22936
715982 feet/sec YDOT = -6963
342138 meter/sec
ZDOT = 6368
430463 ZDOT = 1953
160881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11554290
43 X = 3521747
72
Y = -9486165
72 feet Y = -2891383
31 meter
Z = -16505117
78 Z = -5030759
90
XDOT = 19525
213735 XDOT = 5951
285146
YDOT = 12619
783994 feet/sec YDOT = 3846
510161 meter/sec
ZDOT = 6422
101452 ZDOT = 1957
456523
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
10713848
00016717 00000-0 10270-3 0 9093
2 25544 51
6407 277
9300 0001788 75
9702 284
1650 15
54389346 38125
Satellite: ISS
Catalog Number: 25544
Epoch time: 16125
10713848 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 277
9300 deg
Eccentricity:
0001788
Arg of perigee: 75
9702 deg
Mean anomaly: 284
1650 deg
Mean motion: 15
54389346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3812
Checksum: 322
Coasting Arc #11 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2016/126/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3149540
76 A = 6781221
30 meter
Y = 4354442
21 meter E =
0012116
Z = 4127557
86 I = 51
26898
XDOT = -3217
890057 Wp = 75
87662
YDOT = 5879
087720 meter/sec RA = 272
14709 deg
ZDOT = -3734
688225 TA = 52
78644
MA = 52
67593
Ha = 221
110 n
mi
Hp = 213
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10333138
96 X = 3080563
91
Y = 14286227
73 feet Y = 4389276
94 meter
Z = 13541856
50 Z = 4142690
17
XDOT = -10557
382076 XDOT = -3265
250450
YDOT = 19288
345537 feet/sec YDOT = 5842
838200 meter/sec
ZDOT = -12252
914123 ZDOT = -3750
435474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16279914
77 X = -4962118
02
Y = 6638688
81 feet Y = 2023472
35 meter
Z = 13606767
69 Z = 4147342
79
XDOT = -15834
333418 XDOT = -4826
304826
YDOT = -13492
781773 feet/sec YDOT = -4112
599884 meter/sec
ZDOT = -12322
369791 ZDOT = -3755
858312
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
13579340
00016717 00000-0 10270-3 0 9106
2 25544 51
6416 272
8002 0001744 76
7297 283
4050 15
54404960 38281
Satellite: ISS
Catalog Number: 25544
Epoch time: 16126
13579340 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 272
8002 deg
Eccentricity:
0001744
Arg of perigee: 76
7297 deg
Mean anomaly: 283
4050 deg
Mean motion: 15
54404960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 301
Coasting Arc #12 (Orbit 3842)
---------------------------------------
Vector Time (GMT): 2016/127/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2527963
28 A = 6785169
75 meter
Y = -5641604
66 meter E =
0006465
Z = -2797841
27 I = 51
28178
XDOT = 3864
119528 Wp = 65
55672
YDOT = -4244
176832 meter/sec RA = 267
13634 deg
ZDOT = 5078
542585 TA = 262
54260
MA = 262
61607
Ha = 221
201 n
mi
Hp = 213
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8293842
78 X = -2451098
55
Y = -18509201
63 feet Y = -5669444
28 meter
Z = -9179269
27 Z = -2809935
00
XDOT = 12677
557507 XDOT = 3886
621852
YDOT = -13924
464673 feet/sec YDOT = -4200
839796 meter/sec
ZDOT = 16661
885123 ZDOT = 5097
368644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19851779
25 X = 6050822
32
Y = -4041948
28 feet Y = -1231985
84 meter
Z = -9230756
84 Z = -2813534
69
XDOT = 10584
310917 XDOT = 3226
097968
YDOT = 13833
110664 feet/sec YDOT = 4216
332131 meter/sec
ZDOT = 16744
408214 ZDOT = 5103
695624
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
10015202
00016717 00000-0 10270-3 0 9117
2 25544 51
6415 267
9909 0001825 78
2568 281
8789 15
54403377 38438
Satellite: ISS
Catalog Number: 25544
Epoch time: 16127
10015202 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 267
9909 deg
Eccentricity:
0001825
Arg of perigee: 78
2568 deg
Mean anomaly: 281
8789 deg
Mean motion: 15
54403377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 319
Coasting Arc #13 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2016/128/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1783768
94 A = 6787993
51 meter
Y = 6448680
51 meter E =
0015080
Z = 1104131
13 I = 51
29468
XDOT = -4425
555760 Wp = 118
51625
YDOT = 2235
471510 meter/sec RA = 262
13663 deg
ZDOT = -5852
689403 TA = 49
44091
MA = 49
30972
Ha = 221
199 n
mi
Hp = 213
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5852260
30 X = 1706162
09
Y = 21157088
30 feet Y = 6468193
86 meter
Z = 3622477
48 Z = 1112608
02
XDOT = -14519
539896 XDOT = -4421
793957
YDOT = 7334
224113 feet/sec YDOT = 2186
003115 meter/sec
ZDOT = -19201
736885 ZDOT = -5874
178962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21894473
02 X = -6673435
38
Y = 1497963
38 feet Y = 456579
24 meter
Z = 3658119
19 Z = 1114994
73
XDOT = -4209
013990 XDOT = -1282
907464
YDOT = -13971
103075 feet/sec YDOT = -4258
392217 meter/sec
ZDOT = -19295
462470 ZDOT = -5881
256961
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 16128
12879675
00016717 00000-0 10270-3 0 9123
2 25544 51
6424 262
8613 0001799 83
1198 277
0159 15
54407672 38595
Satellite: ISS
Catalog Number: 25544
Epoch time: 16128
12879675 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 262
8613 deg
Eccentricity:
0001799
Arg of perigee: 83
1198 deg
Mean anomaly: 277
0159 deg
Mean motion: 15
54407672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 342
Coasting Arc #14 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2016/129/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -965076
66 A = 6788302
33 meter
Y = -6678042
20 meter E =
0014722
Z = 680643
06 I = 51
30132
XDOT = 4857
303890 Wp = 55
78651
YDOT = -88
404162 meter/sec RA = 257
14160 deg
ZDOT = 5935
703973 TA = 311
60219
MA = 311
72825
Ha = 221
166 n
mi
Hp = 213
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3166262
02 X = -893635
74
Y = -21909587
27 feet Y = -6688434
91 meter
Z = 2233080
89 Z = 676128
13
XDOT = 15936
036384 XDOT = 4829
097772
YDOT = -290
039903 feet/sec YDOT = -34
244494 meter/sec
ZDOT = 19474
094399 ZDOT = 5959
231498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22122072
20 X = 6742807
61
Y = 866602
16 feet Y = 264140
34 meter
Z = 2214678
86 Z = 675034
12
XDOT = -2535
488488 XDOT = -772
816891
YDOT = 13984
831029 feet/sec YDOT = 4262
576498 meter/sec
ZDOT = 19576
287720 ZDOT = 5966
852497
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 16129
15743526
00016717 00000-0 10270-3 0 9133
2 25544 51
6426 257
7316 0001741 83
0843 277
0507 15
54416526 38756
Satellite: ISS
Catalog Number: 25544
Epoch time: 16129
15743526 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 257
7316 deg
Eccentricity:
0001741
Arg of perigee: 83
0843 deg
Mean anomaly: 277
0507 deg
Mean motion: 15
54416526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 313
Coasting Arc #15 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2016/130/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4961
71 A = 6785939
73 meter
Y = 6335226
64 meter E =
0006818
Z = -2430765
09 I = 51
30275
XDOT = -5130
966988 Wp = 122
06860
YDOT = -2038
302085 meter/sec RA = 252
14445 deg
ZDOT = -5316
425471 TA = 85
25360
MA = 85
17575
Ha = 221
152 n
mi
Hp = 213
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16278
57 X = -63995
63
Y = 20784864
30 feet Y = 6334841
21 meter
Z = -7974951
08 Z = -2430932
24
XDOT = -16833
881193 XDOT = -5081
967526
YDOT = -6687
342799 feet/sec YDOT = -2095
405711 meter/sec
ZDOT = -17442
340783 ZDOT = -5341
231915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20503825
30 X = -6249565
95
Y = -3402098
91 feet Y = -1036959
75 meter
Z = -7976814
18 Z = -2431332
96
XDOT = 9113
680283 XDOT = 2777
849750
YDOT = -13889
900766 feet/sec YDOT = -4233
641754 meter/sec
ZDOT = -17549
716232 ZDOT = -5349
153508
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 16130
12177585
00016717 00000-0 10270-3 0 9149
2 25544 51
6437 252
9228 0001740 86
5725 273
5627 15
54430857 38907
Satellite: ISS
Catalog Number: 25544
Epoch time: 16130
12177585 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 252
9228 deg
Eccentricity:
0001740
Arg of perigee: 86
5725 deg
Mean anomaly: 273
5627 deg
Mean motion: 15
54430857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 320
Coasting Arc #16 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2016/131/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1050243
44 A = 6782073
11 meter
Y = -5469478
39 meter E =
0013083
Z = 3860244
97 I = 51
29971
XDOT = 5196
163287 Wp = 97
25655
YDOT = 3892
925400 meter/sec RA = 247
13838 deg
ZDOT = 4088
518442 TA = 309
62422
MA = 309
73962
Ha = 221
142 n
mi
Hp = 213
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3445680
56 X = 1092574
83
Y = -17944482
89 feet Y = -5457497
40 meter
Z = 12664845
71 Z = 3865449
35
XDOT = 17047
779812 XDOT = 5132
384944
YDOT = 12772
064961 feet/sec YDOT = 3950
675506 meter/sec
ZDOT = 13413
774417 ZDOT = 4113
605712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17245630
40 X = 5256468
15
Y = 5988953
63 feet Y = 1825433
07 meter
Z = 12688426
38 Z = 3867432
36
XDOT = -14711
611514 XDOT = -4484
099189
YDOT = 13620
730971 feet/sec YDOT = 4151
598800 meter/sec
ZDOT = 13522
053017 ZDOT = 4121
521760
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 16131
15040081
00016717 00000-0 10270-3 0 9154
2 25544 51
6428 247
7933 0001830 88
3493 271
7869 15
54440229 39064
Satellite: ISS
Catalog Number: 25544
Epoch time: 16131
15040081 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 247
7933 deg
Eccentricity:
0001830
Arg of perigee: 88
3493 deg
Mean anomaly: 271
7869 deg
Mean motion: 15
54440229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 312
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