[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 10th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10 7639 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
048/10:50:37
613 1
5 2
8 2
8
N/A -2
2 -0
3 222
2
000/00:07:15
226 0
7 -0
0 213
2
050/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 213
4
Coasting Arc #1 (Orbit 2480)
---------------------------------------
Vector Time (GMT): 2016/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6628459
41 A = 6787780
58 meter
Y = 1080852
04 meter E =
0014666
Z = -960872
78 I = 51
56475
XDOT = 48
890832 Wp = 120
23100
YDOT = -4886
083110 meter/sec RA = 344
21925 deg
ZDOT = -5908
105098 TA = 70
18590
MA = 70
02785
Ha = 222
751 n
mi
Hp = 211
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21746914
08 X = -6635385
74
Y = 3546102
49 feet Y = 1006689
44 meter
Z = -3152469
75 Z = -993088
23
XDOT = 160
402993 XDOT = 132
222883
YDOT = -16030
456396 feet/sec YDOT = -4885
070738 meter/sec
ZDOT = -19383
546908 ZDOT = -5907
664962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18348515
81 X = -5592627
62
Y = -12162792
08 feet Y = -3707219
03 meter
Z = -3292360
37 Z = -1003511
44
XDOT = 10216
783587 XDOT = 3114
075637
YDOT = -10230
124702 feet/sec YDOT = -3118
142009 meter/sec
ZDOT = -19380
645525 ZDOT = -5907
220756
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 16039
53026564
00016717 00000-0 10270-3 0 9007
2 25544 51
6420 344
6243 0006534 89
0317 271
1585 15
54512915 24814
Satellite: ISS
Catalog Number: 25544
Epoch time: 16039
53026564 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 344
6243 deg
Eccentricity:
0006534
Arg of perigee: 89
0317 deg
Mean anomaly: 271
1585 deg
Mean motion: 15
54512915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2481
Checksum: 295
Coasting Arc #2 (Orbit 2496)
---------------------------------------
Vector Time (GMT): 2016/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6231191
74 A = 6785024
56 meter
Y = -99647
58 meter E =
0019860
Z = 2662283
95 I = 51
52572
XDOT = -2147
825437 Wp = 82
75933
YDOT = 5226
854114 meter/sec RA = 339
23774 deg
ZDOT = 5191
918755 TA = 307
35965
MA = 307
54038
Ha = 222
651 n
mi
Hp = 211
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20443542
44 X = 6218911
00
Y = -326927
77 feet Y = -30034
74 meter
Z = 8734527
39 Z = 2692522
95
XDOT = -7046
671382 XDOT = -2231
333268
YDOT = 17148
471503 feet/sec YDOT = 5202
369153 meter/sec
ZDOT = 17033
854184 ZDOT = 5181
282220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15410056
61 X = 4696985
25
Y = 13351696
98 feet Y = 4069597
24 meter
Z = 8865642
75 Z = 2702247
91
XDOT = -15795
194780 XDOT = -4814
375369
YDOT = 6884
845722 feet/sec YDOT = 2098
500976 meter/sec
ZDOT = 16986
687262 ZDOT = 5177
542277
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 16040
55883281
00016717 00000-0 10270-3 0 9019
2 25544 51
6424 339
4947 0006485 93
4155 266
7740 15
54545016 24973
Satellite: ISS
Catalog Number: 25544
Epoch time: 16040
55883281 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 339
4947 deg
Eccentricity:
0006485
Arg of perigee: 93
4155 deg
Mean anomaly: 266
7740 deg
Mean motion: 15
54545016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2497
Checksum: 326
Coasting Arc #3 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2016/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5305682
96 A = 6780777
13 meter
Y = -1063015
91 meter E =
0013812
Z = -4099658
52 I = 51
48271
XDOT = 4001
316857 Wp = 81
82432
YDOT = -5300
447746 meter/sec RA = 334
24268 deg
ZDOT = -3813
150453 TA = 148
69331
MA = 148
61099
Ha = 222
663 n
mi
Hp = 211
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17407096
33 X = -5273487
78
Y = -3487585
01 feet Y = -1122167
92 meter
Z = -13450323
22 Z = -4125353
34
XDOT = 13127
679978 XDOT = 4078
812631
YDOT = -17389
920427 feet/sec YDOT = -5255
269395 meter/sec
ZDOT = -12510
336132 ZDOT = -3793
524797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10822657
57 X = -3298746
03
Y = -13965575
22 feet Y = -4256707
33 meter
Z = -13561498
38 Z = -4133544
71
XDOT = 20346
434727 XDOT = 6201
593305
YDOT = -3731
594630 feet/sec YDOT = -1137
390043 meter/sec
ZDOT = -12424
197237 ZDOT = -3786
895318
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 16041
52309756
00016717 00000-0 10270-3 0 9028
2 25544 51
6428 334
6848 0006577 95
5714 264
6189 15
54582119 25127
Satellite: ISS
Catalog Number: 25544
Epoch time: 16041
52309756 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 334
6848 deg
Eccentricity:
0006577
Arg of perigee: 95
5714 deg
Mean anomaly: 264
6189 deg
Mean motion: 15
54582119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 329
Coasting Arc #4 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2016/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3971646
76 A = 6777162
10 meter
Y = 2267506
43 meter E =
0011931
Z = 4993140
13 I = 51
44209
XDOT = -5409
247832 Wp = 111
41933
YDOT = 5068
591011 meter/sec RA = 329
23513 deg
ZDOT = 1992
740736 TA = 319
14669
MA = 319
23605
Ha = 222
414 n
mi
Hp = 211
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13030337
15 X = 3921741
67
Y = 7439325
56 feet Y = 2311641
46 meter
Z = 16381693
33 Z = 5012311
62
XDOT = -17746
876088 XDOT = -5475
203750
YDOT = 16629
235602 feet/sec YDOT = 5007
732624 meter/sec
ZDOT = 6537
863308 ZDOT = 1966
303753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5154383
88 X = 1571056
21
Y = 13994669
11 feet Y = 4265575
15 meter
Z = 16464346
05 Z = 5018332
67
XDOT = -23292
252464 XDOT = -7099
478551
YDOT = 992
000567 feet/sec YDOT = 302
361773 meter/sec
ZDOT = 6422
258194 ZDOT = 1957
504297
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 16042
55162847
00016717 00000-0 10270-3 0 9031
2 25544 51
6423 329
5557 0006377 101
0243 259
1628 15
54627589 25285
Satellite: ISS
Catalog Number: 25544
Epoch time: 16042
55162847 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 329
5557 deg
Eccentricity:
0006377
Arg of perigee: 101
0243 deg
Mean anomaly: 259
1628 deg
Mean motion: 15
54627589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 320
Coasting Arc #5 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2016/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2381728
14 A = 6775920
63 meter
Y = -3503284
57 meter E =
0021188
Z = -5306775
18 I = 51
41130
XDOT = 6255
369175 Wp = 94
53095
YDOT = -4408
829059 meter/sec RA = 324
21566 deg
ZDOT = 101
749821 TA = 176
45112
MA = 176
43607
Ha = 222
541 n
mi
Hp = 211
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7814068
71 X = -2316598
86
Y = -11493715
78 feet Y = -3529554
98 meter
Z = -17410679
73 Z = -5318186
34
XDOT = 20522
864749 XDOT = 6303
710632
YDOT = -14464
662268 feet/sec YDOT = -4338
607069 meter/sec
ZDOT = 333
824873 ZDOT = 132
254247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1216372
27 X = 370750
27
Y = -13783505
83 feet Y = -4201212
58 meter
Z = -17459448
63 Z = -5321639
94
XDOT = 24048
876915 XDOT = 7330
097684
YDOT = 1525
501451 feet/sec YDOT = 464
972842 meter/sec
ZDOT = 466
916538 ZDOT = 142
316161
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 16043
51586220
00016717 00000-0 10270-3 0 9044
2 25544 51
6428 324
7453 0006428 103
8088 256
3781 15
54625880 25434
Satellite: ISS
Catalog Number: 25544
Epoch time: 16043
51586220 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 324
7453 deg
Eccentricity:
0006428
Arg of perigee: 103
8088 deg
Mean anomaly: 256
3781 deg
Mean motion: 15
54625880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 312
Coasting Arc #6 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2016/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 695362
82 A = 6777434
99 meter
Y = 4594470
73 meter E =
0011717
Z = 4924169
35 I = 51
39103
XDOT = -6552
723919 Wp = 81
76163
YDOT = 3346
050814 meter/sec RA = 319
19583 deg
ZDOT = -2190
558263 TA = 29
68938
MA = 29
62293
Ha = 222
424 n
mi
Hp = 211
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2281374
08 X = 620015
40
Y = 15073722
86 feet Y = 4601825
86 meter
Z = 16155411
24 Z = 4927363
81
XDOT = -21498
438054 XDOT = -6579
012604
YDOT = 10977
857000 feet/sec YDOT = 3272
626733 meter/sec
ZDOT = -7186
870940 ZDOT = -2222
453538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7537676
25 X = -2297483
72
Y = 13235818
39 feet Y = 4034277
44 meter
Z = 16168353
33 Z = 4928114
09
XDOT = -22706
795824 XDOT = -6921
031367
YDOT = -3957
933556 feet/sec YDOT = -1206
378148 meter/sec
ZDOT = -7325
770556 ZDOT = -2232
894866
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 16044
54435780
00016717 00000-0 10270-3 0 9053
2 25544 51
6425 319
6152 0006389 106
9058 253
2796 15
54664135 25592
Satellite: ISS
Catalog Number: 25544
Epoch time: 16044
54435780 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 319
6152 deg
Eccentricity:
0006389
Arg of perigee: 106
9058 deg
Mean anomaly: 253
2796 deg
Mean motion: 15
54664135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 329
Coasting Arc #7 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2016/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 892572
89 A = 6781127
78 meter
Y = -5448078
13 meter E =
0013097
Z = -3951705
82 I = 51
38017
XDOT = 6261
822208 Wp = 108
36920
YDOT = -1865
787794 meter/sec RA = 314
18141 deg
ZDOT = 3993
527774 TA = 203
47395
MA = 203
53378
Ha = 222
422 n
mi
Hp = 211
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2928388
76 X = 972623
81
Y = -17874272
08 feet Y = -5437649
48 meter
Z = -12964914
11 Z = -3947175
15
XDOT = 20544
036117 XDOT = 6262
821871
YDOT = -6121
351031 feet/sec YDOT = -1795
758075 meter/sec
ZDOT = 13102
125243 ZDOT = 4023
948396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13139995
49 X = 4005070
63
Y = -12487672
55 feet Y = -3806242
59 meter
Z = -12944211
60 Z = -3945395
69
XDOT = 19125
826481 XDOT = 5829
551911
YDOT = 6430
144658 feet/sec YDOT = 1959
908092 meter/sec
ZDOT = 13234
335802 ZDOT = 4033
825552
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 16045
50855760
00016717 00000-0 10270-3 0 9065
2 25544 51
6428 314
8045 0006439 110
8619 249
3224 15
54682663 25741
Satellite: ISS
Catalog Number: 25544
Epoch time: 16045
50855760 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 314
8045 deg
Eccentricity:
0006439
Arg of perigee: 110
8619 deg
Mean anomaly: 249
3224 deg
Mean motion: 15
54682663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 320
Coasting Arc #8 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2016/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2296984
34 A = 6785271
57 meter
Y = 5892676
35 meter E =
0020116
Z = 2430386
44 I = 51
37208
XDOT = -5529
764856 Wp = 108
68183
YDOT = 52
225477 meter/sec RA = 309
17889 deg
ZDOT = -5323
014711 TA = 43
98508
MA = 43
82516
Ha = 222
394 n
mi
Hp = 211
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7536037
86 X = -2374512
63
Y = 19332927
66 feet Y = 5866556
60 meter
Z = 7973708
79 Z = 2419039
75
XDOT = -18142
273149 XDOT = -5504
081234
YDOT = 171
343429 feet/sec YDOT = -9
468709 meter/sec
ZDOT = -17463
959024 ZDOT = -5349
814257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17484399
32 X = -5329244
91
Y = 11209359
52 feet Y = 3416612
78 meter
Z = 7923385
00 Z = 2415047
75
XDOT = -13885
281348 XDOT = -4232
233755
YDOT = -9162
062452 feet/sec YDOT = -2792
596635 meter/sec
ZDOT = -17580
118576 ZDOT = -5358
420142
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 16046
53702412
00016717 00000-0 10270-3 0 9075
2 25544 51
6426 309
6741 0006413 115
8490 244
3325 15
54674376 25905
Satellite: ISS
Catalog Number: 25544
Epoch time: 16046
53702412 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 309
6741 deg
Eccentricity:
0006413
Arg of perigee: 115
8490 deg
Mean anomaly: 244
3325 deg
Mean motion: 15
54674376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 304
Coasting Arc #9 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2016/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3360560
59 A = 6787431
03 meter
Y = -5859319
00 meter E =
0013512
Z = -640571
09 I = 51
36147
XDOT = 4446
440514 Wp = 67
32715
YDOT = 1911
813720 meter/sec RA = 304
18380 deg
ZDOT = 5945
053805 TA = 285
73060
MA = 285
87959
Ha = 222
236 n
mi
Hp = 211
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11025461
25 X = 3428942
76
Y = -19223487
55 feet Y = -5821356
67 meter
Z = -2101611
18 Z = -624080
19
XDOT = 14588
059430 XDOT = 4395
853543
YDOT = 6272
354726 feet/sec YDOT = 1961
254186 meter/sec
ZDOT = 19504
769702 ZDOT = 5966
530260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20056089
84 X = 6113096
18
Y = -9442268
41 feet Y = -2878003
41 meter
Z = -2029006
27 Z = -618441
11
XDOT = 7577
623942 XDOT = 2309
659778
YDOT = 11961
319578 feet/sec YDOT = 3645
810207 meter/sec
ZDOT = 19597
478999 ZDOT = 5973
311599
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 16047
50119576
00016717 00000-0 10270-3 0 9087
2 25544 51
6437 304
8632 0006243 118
6946 241
4836 15
54723855 26050
Satellite: ISS
Catalog Number: 25544
Epoch time: 16047
50119576 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 304
8632 deg
Eccentricity:
0006243
Arg of perigee: 118
6946 deg
Mean anomaly: 241
4836 deg
Mean motion: 15
54723855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 321
Coasting Arc #10 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2016/048/10:54:15
226
Vector Time (MET): N/A
Weight (LBS) : 922211
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1682492
54 A = 6779808
41 meter
Y = -4632852
79 meter E =
0014655
Z = -4669722
24 I = 51
31398
XDOT = 5282
458872 Wp = 115
01059
YDOT = -4766
988600 meter/sec RA = 299
38549 deg
ZDOT = 2827
007159 TA = 183
21545
MA = 183
22488
Ha = 222
207 n
mi
Hp = 213
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5519988
64 X = -1607878
66
Y = -15199648
25 feet Y = -4651250
54 meter
Z = -15320611
02 Z = -4677713
81
XDOT = 17330
901812 XDOT = 5321
639761
YDOT = -15639
726379 feet/sec YDOT = -4707
697449 meter/sec
ZDOT = 9274
957872 ZDOT = 2852
762962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8261585
85 X = 2518131
37
Y = -13864003
48 feet Y = -4225748
26 meter
Z = -15354358
01 Z = -4680008
32
XDOT = 22046
765165 XDOT = 6719
854022
YDOT = 2744
393025 feet/sec YDOT = 836
490994 meter/sec
ZDOT = 9387
499743 ZDOT = 2861
309922
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 16048
46535619
00016717 00000-0 10270-3 0 9094
2 25544 51
6432 300
0518 0004218 129
8633 230
2891 15
54218071 26206
Satellite: ISS
Catalog Number: 25544
Epoch time: 16048
46535619 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 300
0518 deg
Eccentricity:
0004218
Arg of perigee: 129
8633 deg
Mean anomaly: 230
2891 deg
Mean motion: 15
54218071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 294
Coasting Arc #11 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2016/049/10:54:15
226
Vector Time (MET): N/A
Weight (LBS) : 922211
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 562039
10 A = 6783587
32 meter
Y = 5720469
98 meter E =
0015205
Z = 3587238
04 I = 51
31118
XDOT = -5358
569476 Wp = 98
51480
YDOT = 3292
974627 meter/sec RA = 294
37444 deg
ZDOT = -4397
862544 TA = 38
77518
MA = 38
66616
Ha = 222
135 n
mi
Hp = 213
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1843960
31 X = 480604
71
Y = 18767946
13 feet Y = 5726299
92 meter
Z = 11769153
66 Z = 3589770
17
XDOT = -17580
608516 XDOT = -5373
631582
YDOT = 10803
722531 feet/sec YDOT = 3232
967125 meter/sec
ZDOT = -14428
682887 ZDOT = -4423
929347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13108046
86 X = -3995332
68
Y = 13549252
92 feet Y = 4129812
29 meter
Z = 11779041
65 Z = 3590251
89
XDOT = -18590
669079 XDOT = -5666
435935
YDOT = -5303
674072 feet/sec YDOT = -1616
559857 meter/sec
ZDOT = -14542
285620 ZDOT = -4432
488657
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 16049
49412699
00016717 00000-0 10270-3 0 9102
2 25544 51
6426 294
9240 0004263 134
6810 225
4691 15
54220900 26368
Satellite: ISS
Catalog Number: 25544
Epoch time: 16049
49412699 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 294
9240 deg
Eccentricity:
0004263
Arg of perigee: 134
6810 deg
Mean anomaly: 225
4691 deg
Mean motion: 15
54220900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 304
Coasting Arc #12 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2016/050/10:54:15
226
Vector Time (MET): N/A
Weight (LBS) : 922211
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 439065
08 A = 6786977
10 meter
Y = -6425352
35 meter E =
0007077
Z = -2144082
87 I = 51
31175
XDOT = 5160
239061 Wp = 76
74250
YDOT = -1467
428846 meter/sec RA = 289
37135 deg
ZDOT = 5471
156325 TA = 259
38692
MA = 259
46664
Ha = 221
990 n
mi
Hp = 213
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1440502
25 X = 521297
13
Y = -21080552
32 feet Y = -6419982
77 meter
Z = -7034392
61 Z = -2141749
95
XDOT = 16929
918179 XDOT = 5149
688783
YDOT = -4814
399102 feet/sec YDOT = -1409
782301 meter/sec
ZDOT = 17949
987943 ZDOT = 5496
197360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16761726
23 X = 5108974
15
Y = -12871222
29 feet Y = -3923148
55 meter
Z = -7023075
03 Z = -2140633
27
XDOT = 13815
889892 XDOT = 4211
083239
YDOT = 8168
560839 feet/sec YDOT = 2489
777344 meter/sec
ZDOT = 18058
797064 ZDOT = 5504
321345
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 16050
45858621
00016717 00000-0 10270-3 0 9110
2 25544 51
6437 290
1151 0004103 139
2091 220
9370 15
54267358 26513
Satellite: ISS
Catalog Number: 25544
Epoch time: 16050
45858621 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 290
1151 deg
Eccentricity:
0004103
Arg of perigee: 139
2091 deg
Mean anomaly: 220
9370 deg
Mean motion: 15
54267358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 287
Coasting Arc #13 (Orbit 2651)
---------------------------------------
Vector Time (GMT): 2016/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906710
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4531246
04 A = 6781501
19 meter
Y = 2851229
68 meter E =
0009968
Z = -4171005
96 I = 51
29264
XDOT = -808
442130 Wp = 91
95032
YDOT = -6666
469326 meter/sec RA = 289
18687 deg
ZDOT = -3686
812533 TA = 140
00952
MA = 139
93607
Ha = 221
909 n
mi
Hp = 213
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14866292
78 X = -4542531
94
Y = 9354428
08 feet Y = 2800494
93 meter
Z = -13684402
74 Z = -4193044
69
XDOT = -2652
369194 XDOT = -715
927400
YDOT = -21871
618524 feet/sec YDOT = -6674
992799 meter/sec
ZDOT = -12095
841645 ZDOT = -3690
514557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17488897
31 X = -5330615
90
Y = 110856
96 feet Y = 33789
20 meter
Z = -13780458
84 Z = -4200283
85
XDOT = 9403
941722 XDOT = 2866
321437
YDOT = -18643
587179 feet/sec YDOT = -5682
565372 meter/sec
ZDOT = -12110
636342 ZDOT = -3691
321957
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 16050
52288237
00016717 00000-0 10270-3 0 9129
2 25544 51
6434 289
7949 0003955 140
4855 219
6587 15
54250743 26521
Satellite: ISS
Catalog Number: 25544
Epoch time: 16050
52288237 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 289
7949 deg
Eccentricity:
0003955
Arg of perigee: 140
4855 deg
Mean anomaly: 219
6587 deg
Mean motion: 15
54250743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2652
Checksum: 334
Coasting Arc #14 (Orbit 2667)
---------------------------------------
Vector Time (GMT): 2016/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906710
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4426159
49 A = 6778242
09 meter
Y = -1172011
71 meter E =
0009727
Z = 4993551
13 I = 51
27146
XDOT = -253
617067 Wp = 131
04449
YDOT = 7414
303435 meter/sec RA = 284
16755 deg
ZDOT = 1956
195487 TA = 299
83031
MA = 299
92697
Ha = 221
830 n
mi
Hp = 213
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14521520
64 X = 4414680
33
Y = -3845182
78 feet Y = -1122579
27 meter
Z = 16383041
77 Z = 5015023
99
XDOT = -832
076990 XDOT = -346
008917
YDOT = 24325
142503 feet/sec YDOT = 7410
950874 meter/sec
ZDOT = 6417
964197 ZDOT = 1954
738551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14337908
00 X = 4370194
36
Y = 4125412
14 feet Y = 1257425
62 meter
Z = 16476329
05 Z = 5021985
09
XDOT = -12969
722548 XDOT = -3953
171433
YDOT = 19360
245928 feet/sec YDOT = 5901
002959 meter/sec
ZDOT = 6410
276709 ZDOT = 1953
852341
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 16051
55162763
00016717 00000-0 10270-3 0 9139
2 25544 51
6427 284
6656 0004045 141
7596 218
3845 15
54256381 26683
Satellite: ISS
Catalog Number: 25544
Epoch time: 16051
55162763 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 284
6656 deg
Eccentricity:
0004045
Arg of perigee: 141
7596 deg
Mean anomaly: 218
3845 deg
Mean motion: 15
54256381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2668
Checksum: 326
Coasting Arc #15 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2016/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906710
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4191410
41 A = 6776848
55 meter
Y = -692444
88 meter E =
0017363
Z = -5294810
88 I = 51
25888
XDOT = 1227
088259 Wp = 101
01723
YDOT = -7557
236486 meter/sec RA = 279
14034 deg
ZDOT = 13
729887 TA = 169
13329
MA = 169
09573
Ha = 221
776 n
mi
Hp = 213
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13751346
50 X = -4157636
53
Y = -2271800
79 feet Y = -739127
67 meter
Z = -17371426
76 Z = -5315089
10
XDOT = 4025
880116 XDOT = 1311
437257
YDOT = -24794
082960 feet/sec YDOT = -7543
042747 meter/sec
ZDOT = 45
045562 ZDOT = 19
896203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10676109
74 X = -3254078
25
Y = -8787735
83 feet Y = -2678501
88 meter
Z = -17459194
06 Z = -5321562
35
XDOT = 15240
940611 XDOT = 4645
438698
YDOT = -18682
238038 feet/sec YDOT = -5694
346154 meter/sec
ZDOT = 73
152235 ZDOT = 22
296801
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 16052
51606402
00016717 00000-0 10270-3 0 9140
2 25544 51
6413 279
8568 0003941 146
8020 213
3381 15
54303893 26836
Satellite: ISS
Catalog Number: 25544
Epoch time: 16052
51606402 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 279
8568 deg
Eccentricity:
0003941
Arg of perigee: 146
8020 deg
Mean anomaly: 213
3381 deg
Mean motion: 15
54303893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 300
Coasting Arc #16 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2016/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906710
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3828328
24 A = 6778052
80 meter
Y = 2525219
17 meter E =
0006639
Z = 4985110
79 I = 51
25961
XDOT = -2105
183426 Wp = 90
86771
YDOT = 7107
941891 meter/sec RA = 274
11333 deg
ZDOT = -1981
670508 TA = 18
47960
MA = 18
45550
Ha = 221
470 n
mi
Hp = 213
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12560132
03 X = 3775591
13
Y = 8284839
80 feet Y = 2567735
76 meter
Z = 16355350
36 Z = 5003579
04
XDOT = -6906
769769 XDOT = -2174
883852
YDOT = 23320
019328 feet/sec YDOT = 7084
010393 meter/sec
ZDOT = -6501
543661 ZDOT = -1992
066808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6873606
18 X = 2095075
16
Y = 13286801
03 feet Y = 4049816
95 meter
Z = 16434945
36 Z = 5009371
35
XDOT = -16343
728564 XDOT = -4981
568466
YDOT = 16563
214932 feet/sec YDOT = 5048
467911 meter/sec
ZDOT = -6547
884742 ZDOT = -1995
795269
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 16053
54478356
00016717 00000-0 10270-3 0 9150
2 25544 51
6418 274
7277 0003797 152
8799 207
2553 15
54337687 26999
Satellite: ISS
Catalog Number: 25544
Epoch time: 16053
54478356 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 274
7277 deg
Eccentricity:
0003797
Arg of perigee: 152
8799 deg
Mean anomaly: 207
2553 deg
Mean motion: 15
54337687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 363
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