[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 30th 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) : 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
245/12:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 215
4
246/19:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
4
250/21:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
1
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
2
254/00:41:11
035 3
1 3
6 3
6
N/A -1
3 0
0 220
0
000/00:10:18
071 -1
3 -0
0 217
0
Coasting Arc #1 (Orbit 1638)
---------------------------------------
Vector Time (GMT): 2016/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5214601
83 A = 6781745
43 meter
Y = -1399071
84 meter E =
0007466
Z = 4099158
91 I = 51
92893
XDOT = -1299
910617 Wp = 74
89224
YDOT = -6496
980105 meter/sec RA = 51
51007 deg
ZDOT = -3863
354548 TA = 54
92239
MA = 54
85240
Ha = 219
660 n
mi
Hp = 215
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17108273
72 X = -5218481
10
Y = -4590130
72 feet Y = -1457406
49 meter
Z = 13448684
08 Z = 4073818
77
XDOT = -4264
798613 XDOT = -1208
396937
YDOT = -21315
551524 feet/sec YDOT = -6511
005092 meter/sec
ZDOT = -12675
047729 ZDOT = -3869
446471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14086484
16 X = 4293560
37
Y = 10876292
08 feet Y = 3315093
82 meter
Z = 13338165
84 Z = 4065472
95
XDOT = -3585
282661 XDOT = -1092
794155
YDOT = 20250
158710 feet/sec YDOT = 6172
248375 meter/sec
ZDOT = -12700
458069 ZDOT = -3871
099619
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 16242
54108086
00016717 00000-0 10270-3 0 9004
2 25544 51
6395 52
0055 0003215 263
1231 96
9556 15
54324514 16390
Satellite: ISS
Catalog Number: 25544
Epoch time: 16242
54108086 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 52
0055 deg
Eccentricity:
0003215
Arg of perigee: 263
1231 deg
Mean anomaly: 96
9556 deg
Mean motion: 15
54324514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1639
Checksum: 288
Coasting Arc #2 (Orbit 1653)
---------------------------------------
Vector Time (GMT): 2016/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5564009
49 A = 6785562
98 meter
Y = 2743134
58 meter E =
0002693
Z = -2747085
66 I = 51
92190
XDOT = -232
434734 Wp = 23
56072
YDOT = 5650
052532 meter/sec RA = 46
54484 deg
ZDOT = 5175
297914 TA = 305
48316
MA = 305
50829
Ha = 219
599 n
mi
Hp = 215
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18254624
29 X = 5546265
46
Y = 8999785
38 feet Y = 2805255
66 meter
Z = -9012748
22 Z = -2720100
86
XDOT = -762
581148 XDOT = -320
736708
YDOT = 18536
917757 feet/sec YDOT = 5646
959929 meter/sec
ZDOT = 16979
323864 ZDOT = 5173
953956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13675878
05 X = -4168407
63
Y = -15142692
05 feet Y = -4615492
54 meter
Z = -8895297
21 Z = -2711286
59
XDOT = 6573
751677 XDOT = 2003
679511
YDOT = -15898
988602 feet/sec YDOT = -4846
011726 meter/sec
ZDOT = 16972
382206 ZDOT = 5173
182096
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 16243
50547786
00016717 00000-0 10270-3 0 9016
2 25544 51
6402 47
1958 0002972 265
6406 94
4407 15
54350801 16549
Satellite: ISS
Catalog Number: 25544
Epoch time: 16243
50547786 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 47
1958 deg
Eccentricity:
0002972
Arg of perigee: 265
6406 deg
Mean anomaly: 94
4407 deg
Mean motion: 15
54350801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1654
Checksum: 309
Coasting Arc #3 (Orbit 1669)
---------------------------------------
Vector Time (GMT): 2016/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5524385
11 A = 6788167
02 meter
Y = -3787656
16 meter E =
0011048
Z = 1064025
37 I = 51
90690
XDOT = 1930
196182 Wp = 132
04413
YDOT = -4485
653997 meter/sec RA = 41
58891 deg
ZDOT = -5914
192172 TA = 36
45720
MA = 36
38202
Ha = 219
484 n
mi
Hp = 215
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18124623
05 X = -5486788
48
Y = -12426693
42 feet Y = -3849223
22 meter
Z = 3490896
88 Z = 1037281
38
XDOT = 6332
664638 XDOT = 2008
940579
YDOT = -14716
712587 feet/sec YDOT = -4463
629488 meter/sec
ZDOT = -19403
517624 ZDOT = -5904
624261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12564624
32 X = 3829697
49
Y = 18051388
58 feet Y = 5502063
24 meter
Z = 3374702
55 Z = 1028609
34
XDOT = -9939
034783 XDOT = -3029
417802
YDOT = 10557
889205 feet/sec YDOT = 3218
044630 meter/sec
ZDOT = -19360
842825 ZDOT = -5901
184893
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 16244
53416328
00016717 00000-0 10270-3 0 9028
2 25544 51
6391 42
0662 0003120 272
2417 87
8379 15
54374490 16706
Satellite: ISS
Catalog Number: 25544
Epoch time: 16244
53416328 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 42
0662 deg
Eccentricity:
0003120
Arg of perigee: 272
2417 deg
Mean anomaly: 87
8379 deg
Mean motion: 15
54374490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1670
Checksum: 298
Coasting Arc #4 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2016/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5056785
76 A = 6788372
74 meter
Y = 4462248
11 meter E =
0011097
Z = 717960
16 I = 51
88512
XDOT = -3630
952830 Wp = 42
71327
YDOT = 3145
324711 meter/sec RA = 36
63526 deg
ZDOT = 5978
978008 TA = 325
01926
MA = 325
09211
Ha = 219
506 n
mi
Hp = 215
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16590504
45 X = 5003024
44
Y = 14639921
62 feet Y = 4518495
95 meter
Z = 2355512
33 Z = 742393
37
XDOT = -11912
574902 XDOT = -3694
897690
YDOT = 10319
306794 feet/sec YDOT = 3104
364053 meter/sec
ZDOT = 19616
069580 ZDOT = 5961
184353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10645167
18 X = -3244646
96
Y = -19384069
93 feet Y = -5908264
51 meter
Z = 2461469
10 Z = 750255
78
XDOT = 13407
365336 XDOT = 4086
564954
YDOT = -4863
598228 feet/sec YDOT = -1482
424740 meter/sec
ZDOT = 19537
692688 ZDOT = 5955
088731
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 16245
56284635
00016717 00000-0 10270-3 0 9037
2 25544 51
6413 36
9364 0003039 272
4082 87
6723 15
54376320 16863
Satellite: ISS
Catalog Number: 25544
Epoch time: 16245
56284635 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 36
9364 deg
Eccentricity:
0003039
Arg of perigee: 272
4082 deg
Mean anomaly: 87
6723 deg
Mean motion: 15
54376320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 314
Coasting Arc #5 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2016/245/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3699928
42 A = 6786043
88 meter
Y = 5133392
29 meter E =
0010827
Z = 2436266
06 I = 51
87713
XDOT = -5327
766272 Wp = 69
44287
YDOT = 1286
006586 meter/sec RA = 36
63173 deg
ZDOT = 5365
971522 TA = 317
73303
MA = 317
81642
Ha = 219
457 n
mi
Hp = 215
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12138872
76 X = 3630416
37
Y = 16841838
22 feet Y = 5174378
96 meter
Z = 7992998
89 Z = 2454069
77
XDOT = -17479
548138 XDOT = -5367
815975
YDOT = 4219
181711 feet/sec YDOT = 1226
204565 meter/sec
ZDOT = 17604
893446 ZDOT = 5339
993520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6111503
57 X = -1862786
29
Y = -19809463
28 feet Y = -6037924
41 meter
Z = 8069849
23 Z = 2459690
05
XDOT = 16578
109198 XDOT = 5053
007684
YDOT = 2031
385468 feet/sec YDOT = 619
166291 meter/sec
ZDOT = 17491
093609 ZDOT = 5331
285332
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 16245
56284633
00016717 00000-0 10270-3 0 9046
2 25544 51
6411 36
9363 0003093 272
6000 87
4798 15
54376718 16863
Satellite: ISS
Catalog Number: 25544
Epoch time: 16245
56284633 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 36
9363 deg
Eccentricity:
0003093
Arg of perigee: 272
6000 deg
Mean anomaly: 87
4798 deg
Mean motion: 15
54376718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 323
Coasting Arc #6 (Orbit 1700)
---------------------------------------
Vector Time (GMT): 2016/246/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2362241
62 A = 6782196
55 meter
Y = -5039544
49 meter E =
0003951
Z = -3880330
03 I = 51
83855
XDOT = 6449
838517 Wp = 55
07901
YDOT = 160
083372 meter/sec RA = 31
66452 deg
ZDOT = -4135
171730 TA = 171
58734
MA = 171
58072
Ha = 219
541 n
mi
Hp = 215
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7750136
54 X = -2286863
81
Y = -16533938
61 feet Y = -5065539
64 meter
Z = -12730741
55 Z = -3891621
42
XDOT = 21160
887524 XDOT = 6467
655734
YDOT = 525
207913 feet/sec YDOT = 232
308930 meter/sec
ZDOT = -13566
836383 ZDOT = -4103
797106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2330007
76 X = 710186
36
Y = 18076843
01 feet Y = 5509821
75 meter
Z = -12779136
65 Z = -3895080
85
XDOT = -18784
979949 XDOT = -5725
661888
YDOT = -7070
861427 feet/sec YDOT = -2155
198563 meter/sec
ZDOT = -13429
730840 ZDOT = -4093
381960
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 16246
52723258
00016717 00000-0 10270-3 0 9055
2 25544 51
6418 32
1276 0003000 279
4544 80
6270 15
54370256 17016
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
52723258 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 32
1276 deg
Eccentricity:
0003000
Arg of perigee: 279
4544 deg
Mean anomaly: 80
6270 deg
Mean motion: 15
54370256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1701
Checksum: 285
Coasting Arc #7 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2016/246/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 423988
20 A = 6777516
61 meter
Y = -4417395
14 meter E =
0010960
Z = -5132454
31 I = 51
81606
XDOT = 7026
500432 Wp = 70
26075
YDOT = 2576
015698 meter/sec RA = 30
03286 deg
ZDOT = -1635
899041 TA = 183
97061
MA = 183
97931
Ha = 219
600 n
mi
Hp = 215
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1391037
39 X = 498284
14
Y = -14492766
21 feet Y = -4412239
01 meter
Z = -16838760
87 Z = -5130213
73
XDOT = 23052
822940 XDOT = 7005
118967
YDOT = 8451
495072 feet/sec YDOT = 2654
470989 meter/sec
ZDOT = -5367
122839 ZDOT = -1601
818622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14529101
48 X = 4428470
13
Y = -1112875
73 feet Y = -339204
52 meter
Z = -16828126
54 Z = -5129212
97
XDOT = -4272
948235 XDOT = -1302
394622
YDOT = 23165
733568 feet/sec YDOT = 7060
915592 meter/sec
ZDOT = -5218
654337 ZDOT = -1590
645842
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 16246
84869292
00016717 00000-0 10270-3 0 9060
2 25544 51
6441 30
5284 0003031 285
3533 74
7284 15
54360572 17065
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
84869292 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 30
5284 deg
Eccentricity:
0003031
Arg of perigee: 285
3533 deg
Mean anomaly: 74
7284 deg
Mean motion: 15
54360572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 309
Coasting Arc #8 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2016/247/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2164381
79 A = 6776685
81 meter
Y = 3606724
61 meter E =
0001912
Z = 5313508
12 I = 51
78328
XDOT = -6805
712474 Wp = 354
12876
YDOT = -3514
222402 meter/sec RA = 25
04213 deg
ZDOT = -384
967474 TA = 99
54517
MA = 99
52356
Ha = 219
765 n
mi
Hp = 215
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7100990
12 X = -2230362
83
Y = 11833085
98 feet Y = 3582152
76 meter
Z = 17432769
43 Z = 5302833
47
XDOT = -22328
453000 XDOT = -6764
039738
YDOT = -11529
601058 feet/sec YDOT = -3590
095479 meter/sec
ZDOT = -1263
016648 ZDOT = -417
926086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13016514
01 X = -3967433
47
Y = -4760748
07 feet Y = -1451076
01 meter
Z = 17385427
10 Z = 5299078
18
XDOT = 6596
591528 XDOT = 2010
641098
YDOT = -23194
000368 feet/sec YDOT = -7069
531312 meter/sec
ZDOT = -1406
389427 ZDOT = -428
667497
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 16247
87736622
00016717 00000-0 10270-3 0 9075
2 25544 51
6424 25
3991 0002903 291
2907 68
7936 15
54376495 17227
Satellite: ISS
Catalog Number: 25544
Epoch time: 16247
87736622 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 25
3991 deg
Eccentricity:
0002903
Arg of perigee: 291
2907 deg
Mean anomaly: 68
7936 deg
Mean motion: 15
54376495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 336
Coasting Arc #9 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2016/248/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3822784
95 A = 6778579
09 meter
Y = -2717140
60 meter E =
0008775
Z = -4902272
63 I = 51
76089
XDOT = 5983
312393 Wp = 104
09199
YDOT = 4163
295617 meter/sec RA = 20
05131 deg
ZDOT = 2359
678594 TA = 188
98666
MA = 189
00238
Ha = 219
712 n
mi
Hp = 215
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12541945
38 X = 3876697
66
Y = -8914503
29 feet Y = -2674090
79 meter
Z = -16083571
64 Z = -4883571
29
XDOT = 19630
290003 XDOT = 5924
850397
YDOT = 13659
106354 feet/sec YDOT = 4229
878420 meter/sec
ZDOT = 7741
727669 ZDOT = 2388
601467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11397783
52 X = 3474044
42
Y = 10464139
45 feet Y = 3189469
71 meter
Z = -16001323
56 Z = -4877203
42
XDOT = -8427
686846 XDOT = -2568
758951
YDOT = 21202
680887 feet/sec YDOT = 6462
577134 meter/sec
ZDOT = 7867
325103 ZDOT = 2397
960691
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 16248
84174274
00016717 00000-0 10270-3 0 9083
2 25544 51
6435 20
5909 0003157 294
9153 65
1672 15
54360681 17374
Satellite: ISS
Catalog Number: 25544
Epoch time: 16248
84174274 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 20
5909 deg
Eccentricity:
0003157
Arg of perigee: 294
9153 deg
Mean anomaly: 65
1672 deg
Mean motion: 15
54360681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 321
Coasting Arc #10 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2016/249/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5239361
56 A = 6782104
94 meter
Y = 1786089
84 meter E =
0009106
Z = 3914108
77 I = 51
74171
XDOT = -4613
356157 Wp = 67
83477
YDOT = -4572
131963 meter/sec RA = 15
06577 deg
ZDOT = -4078
059671 TA = 64
83596
MA = 64
74155
Ha = 219
818 n
mi
Hp = 215
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17189506
43 X = -5277957
73
Y = 5859874
81 feet Y = 1727284
42 meter
Z = 12841564
19 Z = 3888563
32
XDOT = -15135
682929 XDOT = -4542
077082
YDOT = -15000
432950 feet/sec YDOT = -4623
323505 meter/sec
ZDOT = -13379
460863 ZDOT = -4100
296569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9662448
98 X = -2945114
45
Y = -15469892
91 feet Y = -4715223
36 meter
Z = 12729592
62 Z = 3879979
83
XDOT = 10026
544721 XDOT = 3056
090831
YDOT = -17381
041116 feet/sec YDOT = -5297
741332 meter/sec
ZDOT = -13475
750460 ZDOT = -4107
408740
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
87040532
00016717 00000-0 10270-3 0 9097
2 25544 51
6427 15
4612 0003133 302
1494 57
9354 15
54416661 17537
Satellite: ISS
Catalog Number: 25544
Epoch time: 16249
87040532 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 15
4612 deg
Eccentricity:
0003133
Arg of perigee: 302
1494 deg
Mean anomaly: 57
9354 deg
Mean motion: 15
54416661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 298
Coasting Arc #11 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2016/250/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6244413
89 A = 6785964
56 meter
Y = -889132
91 meter E =
0005629
Z = -2495730
63 I = 51
72236
XDOT = 2800
101368 Wp = 15
91715
YDOT = 4760
769061 meter/sec RA = 10
09055 deg
ZDOT = 5318
007370 TA = 316
13377
MA = 316
17845
Ha = 219
902 n
mi
Hp = 215
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20486922
22 X = 6266015
51
Y = -2917102
73 feet Y = -819183
16 meter
Z = -8188092
63 Z = -2465344
23
XDOT = 9186
684279 XDOT = 2720
824497
YDOT = 15619
321065 feet/sec YDOT = 4791
638938 meter/sec
ZDOT = 17447
530742 ZDOT = 5331
416553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7877428
72 X = 2401040
27
Y = 19191899
99 feet Y = 5849691
12 meter
Z = -8055148
83 Z = -2455209
36
XDOT = -11511
489874 XDOT = -3508
702114
YDOT = 12060
800042 feet/sec YDOT = 3676
131853 meter/sec
ZDOT = 17505
201449 ZDOT = 5335
585402
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
83477387
00016717 00000-0 10270-3 0 9109
2 25544 51
6419 10
6533 0003030 305
8665 54
2206 15
54405259 17686
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
83477387 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 10
6533 deg
Eccentricity:
0003030
Arg of perigee: 305
8665 deg
Mean anomaly: 54
2206 deg
Mean motion: 15
54405259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 299
Coasting Arc #12 (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 = -2246938
50 A = 6778780
54 meter
Y = -4239003
60 meter E =
0009975
Z = -4798420
15 I = 51
69553
XDOT = 7154
674902 Wp = 56
43633
YDOT = -841
687279 meter/sec RA = 9
88824 deg
ZDOT = -2605
250988 TA = 187
87374
MA = 187
88941
Ha = 219
855 n
mi
Hp = 215
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7371845
48 X = -2176061
19
Y = -13907492
14 feet Y = -4263734
55 meter
Z = -15742848
27 Z = -4809162
66
XDOT = 23473
342854 XDOT = 7176
210321
YDOT = -2761
441204 feet/sec YDOT = -761
558758 meter/sec
ZDOT = -8547
411377 ZDOT = -2570
442923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7995212
19 X = 2436940
68
Y = -13504991
48 feet Y = -4116321
40 meter
Z = -15788967
75 Z = -4812477
37
XDOT = 13754
128337 XDOT = 4192
258317
YDOT = 17963
326443 feet/sec YDOT = 5475
221900 meter/sec
ZDOT = -8395
156910 ZDOT = -2558
843826
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
89906566
00016717 00000-0 10270-3 0 9112
2 25544 51
6406 10
3317 0003162 306
4343 53
6518 15
54384249 17690
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
89906566 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 10
3317 deg
Eccentricity:
0003162
Arg of perigee: 306
4343 deg
Mean anomaly: 53
6518 deg
Mean motion: 15
54384249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1769
Checksum: 306
Coasting Arc #13 (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 = 1950692
44 A = 6778281
38 meter
Y = 4259062
08 meter E =
0003326
Z = 4897035
09 I = 51
69332
XDOT = -7275
344233 Wp = 117
82512
YDOT = 632
682591 meter/sec RA = 9
72449 deg
ZDOT = 2345
078896 TA = 309
22872
MA = 309
25824
Ha = 219
732 n
mi
Hp = 215
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6399909
57 X = 1879133
81
Y = 13973300
79 feet Y = 4280476
41 meter
Z = 16066388
07 Z = 4906336
85
XDOT = -23869
239611 XDOT = -7293
269735
YDOT = 2075
730287 feet/sec YDOT = 551
224823 meter/sec
ZDOT = 7693
828399 ZDOT = 2309
693437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5788078
07 X = -1764206
19
Y = 14192568
89 feet Y = 4325895
00 meter
Z = 16106208
24 Z = 4909172
27
XDOT = -16952
519640 XDOT = -5167
127986
YDOT = -15479
426532 feet/sec YDOT = -4718
129207 meter/sec
ZDOT = 7539
091769 ZDOT = 2297
915171
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
96335634
00016717 00000-0 10270-3 0 9123
2 25544 51
6408 10
0115 0003332 305
1113 54
9727 15
54408495 17703
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
96335634 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 10
0115 deg
Eccentricity:
0003332
Arg of perigee: 305
1113 deg
Mean anomaly: 54
9727 deg
Mean motion: 15
54408495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 280
Coasting Arc #14 (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 = -55672
64 A = 6776611
21 meter
Y = -4220814
23 meter E =
0012588
Z = -5312078
18 I = 51
65583
XDOT = 7643
656676 Wp = 77
06320
YDOT = 349
490202 meter/sec RA = 4
72558 deg
ZDOT = -355
761049 TA = 189
52991
MA = 189
55382
Ha = 219
889 n
mi
Hp = 215
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -182653
02 X = 17333
56
Y = -13847815
71 feet Y = -4221029
06 meter
Z = -17428078
03 Z = -5312170
93
XDOT = 25077
613766 XDOT = 7640
908632
YDOT = 1146
621399 feet/sec YDOT = 434
951295 meter/sec
ZDOT = -1167
195042 ZDOT = -318
636704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9821155
21 X = 2993488
11
Y = -9764971
25 feet Y = -2976363
24 meter
Z = -17427665
15 Z = -5311952
34
XDOT = 16067
350296 XDOT = 4897
328370
YDOT = 17965
495007 feet/sec YDOT = 5475
882878 meter/sec
ZDOT = -1005
060846 ZDOT = -306
342546
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
92771981
00016717 00000-0 10270-3 0 9130
2 25544 51
6411 5
2021 0003285 309
7869 50
2995 15
54394910 17852
Satellite: ISS
Catalog Number: 25544
Epoch time: 16251
92771981 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 5
2021 deg
Eccentricity:
0003285
Arg of perigee: 309
7869 deg
Mean anomaly: 50
2995 deg
Mean motion: 15
54394910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1785
Checksum: 316
Coasting Arc #15 (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 = -1877629
91 A = 6777516
17 meter
Y = 4048096
47 meter E =
0005681
Z = 5100958
53 I = 51
62744
XDOT = -7370
063833 Wp = 18
82395
YDOT = -1294
522356 meter/sec RA = 359
72365 deg
ZDOT = -1679
763079 TA = 87
43165
MA = 87
36661
Ha = 220
022 n
mi
Hp = 215
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6160203
13 X = -1947535
51
Y = 13281156
41 feet Y = 4026709
08 meter
Z = 16735428
24 Z = 5091667
35
XDOT = -24179
999451 XDOT = -7346
880816
YDOT = -4247
120592 feet/sec YDOT = -1376
809852 meter/sec
ZDOT = -5511
033724 ZDOT = -1715
508653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13777973
89 X = -4199526
44
Y = 5088015
98 feet Y = 1550827
27 meter
Z = 16694050
00 Z = 5088346
44
XDOT = -13883
527866 XDOT = -4231
699294
YDOT = -18939
599494 feet/sec YDOT = -5772
789926 meter/sec
ZDOT = -5666
951608 ZDOT = -1727
286850
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
95636657
00016717 00000-0 10270-3 0 9145
2 25544 51
6418
0725 0003389 314
4617 45
6258 15
54411136 18011
Satellite: ISS
Catalog Number: 25544
Epoch time: 16252
95636657 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node:
0725 deg
Eccentricity:
0003389
Arg of perigee: 314
4617 deg
Mean anomaly: 45
6258 deg
Mean motion: 15
54411136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1801
Checksum: 300
Coasting Arc #16 (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 = 3634508
88 A = 6780716
35 meter
Y = -3768555
82 meter E =
0005613
Z = -4313884
87 I = 51
60523
XDOT = 6445
996216 Wp = 92
49704
YDOT = 2200
210732 meter/sec RA = 354
72571 deg
ZDOT = 3512
479427 TA = 213
27430
MA = 213
30960
Ha = 220
108 n
mi
Hp = 215
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11924241
72 X = 3697334
70
Y = -12364028
27 feet Y = -3727561
32 meter
Z = -14153165
59 Z = -4296076
49
XDOT = 21148
281549 XDOT = 6403
851707
YDOT = 7218
539148 feet/sec YDOT = 2272
058774 meter/sec
ZDOT = 11523
882634 ZDOT = 3543
689948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17227250
83 X = 5250866
05
Y = -703796
94 feet Y = -214517
31 meter
Z = -14074634
30 Z = -4289948
54
XDOT = 10271
146766 XDOT = 3130
645534
YDOT = 18483
388759 feet/sec YDOT = 5633
736894 meter/sec
ZDOT = 11659
804847 ZDOT = 3553
908517
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
92071725
00016717 00000-0 10270-3 0 9153
2 25544 51
6412 355
2636 0003466 319
2076 40
8817 15
54407701 18166
Satellite: ISS
Catalog Number: 25544
Epoch time: 16253
92071725 = yrday
fracday
Element set: 915
Inclination: 51
6412 deg
RA of node: 355
2636 deg
Eccentricity:
0003466
Arg of perigee: 319
2076 deg
Mean anomaly: 40
8817 deg
Mean motion: 15
54407701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1816
Checksum: 303
Coasting Arc #17 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2016/254/00:46:20
071
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1164491
78 A = 6778602
83 meter
Y = -4093032
17 meter E =
0010163
Z = -5285152
20 I = 51
59056
XDOT = 7522
327614 Wp = 74
90182
YDOT = -1292
441186 meter/sec RA = 354
15219 deg
ZDOT = -654
961785 TA = 188
82524
MA = 188
84312
Ha = 220
042 n
mi
Hp = 217
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3820511
10 X = -1092962
92
Y = -13428583
23 feet Y = -4105654
71 meter
Z = -17339738
20 Z = -5290635
00
XDOT = 24679
552539 XDOT = 7539
402466
YDOT = -4240
292604 feet/sec YDOT = -1208
226052 meter/sec
ZDOT = -2148
824753 ZDOT = -618
378652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3759936
34 X = -1146028
60
Y = -13415751
56 feet Y = -4089121
08 meter
Z = -17362896
13 Z = -5292210
74
XDOT = 23698
137282 XDOT = 7223
192244
YDOT = -4061
318352 feet/sec YDOT = -1237
889834 meter/sec
ZDOT = -1988
753809 ZDOT = -606
172161
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
04930123
00016717 00000-0 10270-3 0 9164
2 25544 51
6438 354
6233 0004992 285
9051 74
1551 15
53741229 18189
Satellite: ISS
Catalog Number: 25544
Epoch time: 16254
04930123 = yrday
fracday
Element set: 916
Inclination: 51
6438 deg
RA of node: 354
6233 deg
Eccentricity:
0004992
Arg of perigee: 285
9051 deg
Mean anomaly: 74
1551 deg
Mean motion: 15
53741229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 307
Coasting Arc #18 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2016/255/00:46:20
071
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -481594
80 A = 6778854
34 meter
Y = 4306795
45 meter E =
0004246
Z = 5214815
28 I = 51
55953
XDOT = -7563
205747 Wp = 336
84392
YDOT = 532
281257 meter/sec RA = 349
15282 deg
ZDOT = -1134
563242 TA = 124
06753
MA = 124
02721
Ha = 220
095 n
mi
Hp = 217
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1580035
44 X = -555049
95
Y = 14129906
32 feet Y = 4300999
55 meter
Z = 17108974
00 Z = 5212297
13
XDOT = -24813
667150 XDOT = -7563
084534
YDOT = 1746
329583 feet/sec YDOT = 447
705029 meter/sec
ZDOT = -3722
320347 ZDOT = -1171
303038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1392837
86 X = -424536
98
Y = 14163883
62 feet Y = 4317151
73 meter
Z = 17097138
93 Z = 5211207
95
XDOT = -23713
974644 XDOT = -7228
019471
YDOT = 2368
982060 feet/sec YDOT = 722
065732 meter/sec
ZDOT = -3882
921187 ZDOT = -1183
514378
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
07839798
00016717 00000-0 10270-3 0 9175
2 25544 51
6437 349
4972 0005232 288
9871 71
0714 15
53771208 18346
Satellite: ISS
Catalog Number: 25544
Epoch time: 16255
07839798 = yrday
fracday
Element set: 917
Inclination: 51
6437 deg
RA of node: 349
4972 deg
Eccentricity:
0005232
Arg of perigee: 288
9871 deg
Mean anomaly: 71
0714 deg
Mean motion: 15
53771208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 345
Coasting Arc #19 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2016/256/00:46:20
071
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2050090
27 A = 6781177
26 meter
Y = -4454249
93 meter E =
0005440
Z = -4689345
36 I = 51
53667
XDOT = 7118
208954 Wp = 105
26651
YDOT = 308
441974 meter/sec RA = 344
15355 deg
ZDOT = 2820
296747 TA = 192
76411
MA = 192
77788
Ha = 220
293 n
mi
Hp = 217
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6726017
95 X = 2122525
16
Y = -14613680
88 feet Y = -4430919
77 meter
Z = -15384991
34 Z = -4679210
34
XDOT = 23353
703917 XDOT = 7100
531124
YDOT = 1011
948732 feet/sec YDOT = 387
943909 meter/sec
ZDOT = 9252
942082 ZDOT = 2854
832076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6261468
21 X = 1908495
51
Y = -14865385
91 feet Y = -4530969
63 meter
Z = -15339858
62 Z = -4675588
91
XDOT = 22231
045051 XDOT = 6776
022531
YDOT = -335
398173 feet/sec YDOT = -102
229363 meter/sec
ZDOT = 9403
743974 ZDOT = 2866
261163
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
04317173
00016717 00000-0 10270-3 0 9182
2 25544 51
6448 344
6906 0005204 293
5171 66
5434 15
53747795 18494
Satellite: ISS
Catalog Number: 25544
Epoch time: 16256
04317173 = yrday
fracday
Element set: 918
Inclination: 51
6448 deg
RA of node: 344
6906 deg
Eccentricity:
0005204
Arg of perigee: 293
5171 deg
Mean anomaly: 66
5434 deg
Mean motion: 15
53747795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 330
Coasting Arc #20 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2016/257/00:46:20
071
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3453912
04 A = 6784590
73 meter
Y = 4489045
53 meter E =
0008009
Z = 3731845
59 I = 51
51688
XDOT = -6246
402864 Wp = 63
44786
YDOT = -1250
878228 meter/sec RA = 339
16060 deg
ZDOT = -4265
905243 TA = 71
89608
MA = 71
80887
Ha = 220
496 n
mi
Hp = 216
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11331732
41 X = -3521980
55
Y = 14727839
67 feet Y = 4450041
29 meter
Z = 12243587
91 Z = 3714901
78
XDOT = -20493
447718 XDOT = -6211
229206
YDOT = -4103
931194 feet/sec YDOT = -1320
533381 meter/sec
ZDOT = -13995
752110 ZDOT = -4296
162936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10576774
59 X = -3223800
90
Y = 15338745
45 feet Y = 4675249
61 meter
Z = 12168713
69 Z = 3709023
93
XDOT = -19480
128027 XDOT = -5937
543023
YDOT = -2196
737923 feet/sec YDOT = -669
565719 meter/sec
ZDOT = -14127
681859 ZDOT = -4306
117431
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
07225758
00016717 00000-0 10270-3 0 9194
2 25544 51
6443 339
5645 0005090 298
5232 61
5407 15
53753386 18654
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
07225758 = yrday
fracday
Element set: 919
Inclination: 51
6443 deg
RA of node: 339
5645 deg
Eccentricity:
0005090
Arg of perigee: 298
5232 deg
Mean anomaly: 61
5407 deg
Mean motion: 15
53753386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1865
Checksum: 332
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