[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 7th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
315/12:37:22
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
4
317/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
3
317/21:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 387)
---------------------------------------
Vector Time (GMT): 2017/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2324434
23 A = 6786395
00 meter
Y = -5776529
81 meter E =
0008714
Z = -2701405
29 I = 51
93547
XDOT = 5618
418513 Wp = 110
47234
YDOT = 166
988250 meter/sec RA = 48
21919 deg
ZDOT = -5207
998066 TA = 99
89338
MA = 99
79500
Ha = 222
595 n
mi
Hp = 213
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7626096
55 X = -2246544
30
Y = -18951869
46 feet Y = -5802087
64 meter
Z = -8862878
24 Z = -2712507
95
XDOT = 18433
131603 XDOT = 5641
432235
YDOT = 547
861714 feet/sec YDOT = 229
946053 meter/sec
ZDOT = -17086
607829 ZDOT = -5180
648865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18756432
33 X = 5716960
57
Y = 8041681
09 feet Y = 2451104
40 meter
Z = -8911168
66 Z = -2716124
21
XDOT = -12907
355868 XDOT = -3934
162068
YDOT = 11365
340939 feet/sec YDOT = 3464
155918 meter/sec
ZDOT = -16965
247212 ZDOT = -5171
007350
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 17310
52672209
00016717 00000-0 10270-3 0 9002
2 25544 51
6424 48
7379 0004113 95
9547 264
2074 15
54060883 3884
Satellite: ISS
Catalog Number: 25544
Epoch time: 17310
52672209 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 48
7379 deg
Eccentricity:
0004113
Arg of perigee: 95
9547 deg
Mean anomaly: 264
2074 deg
Mean motion: 15
54060883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 388
Checksum: 310
Coasting Arc #2 (Orbit 403)
---------------------------------------
Vector Time (GMT): 2017/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1127437
39 A = 6782622
76 meter
Y = 5358460
20 meter E =
0014983
Z = 3991790
53 I = 51
90064
XDOT = -6335
935841 Wp = 100
25106
YDOT = -1656
955247 meter/sec RA = 43
25707 deg
ZDOT = 3998
442780 TA = 308
21534
MA = 308
35015
Ha = 222
531 n
mi
Hp = 213
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3698941
58 X = 1048043
26
Y = 17580249
98 feet Y = 5370623
91 meter
Z = 13096425
61 Z = 3997074
75
XDOT = -20787
191080 XDOT = -6336
359340
YDOT = -5436
204879 feet/sec YDOT = -1727
810519 meter/sec
ZDOT = 13118
250589 ZDOT = 3967
662972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15158690
65 X = -4620368
91
Y = -9610978
92 feet Y = -2929426
37 meter
Z = 13118952
09 Z = 3998656
60
XDOT = 17706
013995 XDOT = 5396
793066
YDOT = -10137
629327 feet/sec YDOT = -3089
949419 meter/sec
ZDOT = 12981
920567 ZDOT = 3956
889389
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 17311
55559322
00016717 00000-0 10270-3 0 9017
2 25544 51
6424 43
6101 0004111 99
3671 260
7947 15
54100616 4043
Satellite: ISS
Catalog Number: 25544
Epoch time: 17311
55559322 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 43
6101 deg
Eccentricity:
0004111
Arg of perigee: 99
3671 deg
Mean anomaly: 260
7947 deg
Mean motion: 15
54100616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 404
Checksum: 274
Coasting Arc #3 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2017/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 308068
44 A = 6779323
16 meter
Y = -4673462
49 meter E =
0015696
Z = -4915664
20 I = 51
86418
XDOT = 6676
702630 Wp = 79
96993
YDOT = 2913
783609 meter/sec RA = 38
28315 deg
ZDOT = -2355
516193 TA = 167
02392
MA = 166
98349
Ha = 222
546 n
mi
Hp = 213
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1010723
23 X = 384183
76
Y = -15332882
19 feet Y = -4669591
70 meter
Z = -16127507
20 Z = -4913982
96
XDOT = 21905
192355 XDOT = 6655
065840
YDOT = 9559
657511 feet/sec YDOT = 2988
326160 meter/sec
ZDOT = -7728
071498 ZDOT = -2323
134712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10452760
63 X = 3186001
44
Y = 11274997
84 feet Y = 3436619
34 meter
Z = -16119229
05 Z = -4913141
01
XDOT = -21142
825913 XDOT = -6444
333338
YDOT = 8774
850002 feet/sec YDOT = 2674
574281 meter/sec
ZDOT = -7584
853854 ZDOT = -2311
863455
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 17312
52015765
00016717 00000-0 10270-3 0 9024
2 25544 51
6419 38
8028 0003985 102
5356 257
6243 15
54060528 4193
Satellite: ISS
Catalog Number: 25544
Epoch time: 17312
52015765 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 38
8028 deg
Eccentricity:
0003985
Arg of perigee: 102
5356 deg
Mean anomaly: 257
6243 deg
Mean motion: 15
54060528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 419
Checksum: 301
Coasting Arc #4 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2017/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1827230
29 A = 6777437
69 meter
Y = 3790736
48 meter E =
0006683
Z = 5307322
72 I = 51
83289
XDOT = -6604
774032 Wp = 105
71360
YDOT = -3875
754428 meter/sec RA = 33
29965 deg
ZDOT = 492
040300 TA = 339
59508
MA = 339
62177
Ha = 222
529 n
mi
Hp = 213
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5994850
03 X = -1895264
24
Y = 12436799
49 feet Y = 3769922
62 meter
Z = 17412476
12 Z = 5298281
32
XDOT = -21669
206142 XDOT = -6563
333551
YDOT = -12715
729750 feet/sec YDOT = -3949
381825 meter/sec
ZDOT = 1614
305446 ZDOT = 460
056467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5151899
03 X = -1570298
83
Y = -12864260
21 feet Y = -3921026
51 meter
Z = 17371680
37 Z = 5294888
18
XDOT = 23019
991386 XDOT = 7016
493374
YDOT = -7219
805054 feet/sec YDOT = -2200
596580 meter/sec
ZDOT = 1473
025912 ZDOT = 448
978298
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 17313
54901814
00016717 00000-0 10270-3 0 9037
2 25544 51
6427 33
6742 0004001 104
0125 256
1473 15
54118490 4358
Satellite: ISS
Catalog Number: 25544
Epoch time: 17313
54901814 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 33
6742 deg
Eccentricity:
0004001
Arg of perigee: 104
0125 deg
Mean anomaly: 256
1473 deg
Mean motion: 15
54118490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 435
Checksum: 269
Coasting Arc #5 (Orbit 449)
---------------------------------------
Vector Time (GMT): 2017/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3353977
20 A = 6778170
23 meter
Y = -2825779
25 meter E =
0017817
Z = -5183932
60 I = 51
80590
XDOT = 6012
998639 Wp = 101
66824
YDOT = 4516
543779 meter/sec RA = 28
31323 deg
ZDOT = 1429
041421 TA = 182
06913
MA = 182
07651
Ha = 222
513 n
mi
Hp = 213
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11003862
22 X = 3410507
85
Y = -9270929
30 feet Y = -2787956
67 meter
Z = -17007652
88 Z = -5167502
53
XDOT = 19727
685825 XDOT = 5955
104874
YDOT = 14818
057019 feet/sec YDOT = 4583
461523 meter/sec
ZDOT = 4688
456107 ZDOT = 1458
110470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -302242
36 X = -92123
47
Y = 14471896
92 feet Y = 4411034
18 meter
Z = -16934232
17 Z = -5161553
97
XDOT = -23053
164054 XDOT = -7026
604404
YDOT = 5152
266529 feet/sec YDOT = 1570
410838 meter/sec
ZDOT = 4816
679519 ZDOT = 1468
123918
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 17314
51357255
00016717 00000-0 10270-3 0 9040
2 25544 51
6415 28
8669 0004072 105
2611 254
8993 15
54095264 4502
Satellite: ISS
Catalog Number: 25544
Epoch time: 17314
51357255 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 28
8669 deg
Eccentricity:
0004072
Arg of perigee: 105
2611 deg
Mean anomaly: 254
8993 deg
Mean motion: 15
54095264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 450
Checksum: 306
Coasting Arc #6 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2017/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4725053
56 A = 6780822
95 meter
Y = 1820879
63 meter E =
0012370
Z = 4500357
87 I = 51
78625
XDOT = -4958
382191 Wp = 80
31056
YDOT = -4895
500774 meter/sec RA = 23
32894 deg
ZDOT = -3215
641882 TA = 41
96608
MA = 41
87136
Ha = 222
529 n
mi
Hp = 213
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15502144
22 X = -4766924
74
Y = 5974014
52 feet Y = 1767806
78 meter
Z = 14764953
64 Z = 4477303
03
XDOT = -16267
658107 XDOT = -4887
650674
YDOT = -16061
354246 feet/sec YDOT = -4950
553338 meter/sec
ZDOT = -10550
006174 ZDOT = -3239
556609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5461947
64 X = 1664801
64
Y = -15785846
68 feet Y = -4811526
07 meter
Z = 14662310
65 Z = 4469072
29
XDOT = 21566
804870 XDOT = 6573
562124
YDOT = -2464
024819 feet/sec YDOT = -751
034765 meter/sec
ZDOT = -10655
278978 ZDOT = -3247
729032
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 17315
54242456
00016717 00000-0 10270-3 0 9051
2 25544 51
6419 23
7382 0003978 109
3817 250
7766 15
54135160 4669
Satellite: ISS
Catalog Number: 25544
Epoch time: 17315
54242456 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 23
7382 deg
Eccentricity:
0003978
Arg of perigee: 109
3817 deg
Mean anomaly: 250
7766 deg
Mean motion: 15
54135160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 314
Coasting Arc #7 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2017/315/12:37:22
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1382693
04 A = 6777526
89 meter
Y = -3974414
06 meter E =
0018687
Z = -5329004
47 I = 51
77291
XDOT = 7109
447022 Wp = 92
32593
YDOT = 2824
842195 meter/sec RA = 23
22543 deg
ZDOT = -263
670842 TA = 175
16995
MA = 175
15190
Ha = 222
517 n
mi
Hp = 213
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4536394
50 X = 1452919
24
Y = -13039416
21 feet Y = -3958559
24 meter
Z = -17483610
47 Z = -5322117
08
XDOT = 23324
957420 XDOT = 7078
611289
YDOT = 9267
854970 feet/sec YDOT = 2904
172472 meter/sec
ZDOT = -865
061819 ZDOT = -229
209862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8842669
18 X = 2695245
57
Y = 10653866
94 feet Y = 3247298
64 meter
Z = -17452341
00 Z = -5319473
54
XDOT = -19097
265463 XDOT = -5820
846513
YDOT = 14691
581514 feet/sec YDOT = 4477
994045 meter/sec
ZDOT = -712
617304 ZDOT = -217
205754
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 17315
54242597
00016717 00000-0 10270-3 0 9068
2 25544 51
6408 23
7387 0004049 109
3622 250
7969 15
54076647 4665
Satellite: ISS
Catalog Number: 25544
Epoch time: 17315
54242597 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 23
7387 deg
Eccentricity:
0004049
Arg of perigee: 109
3622 deg
Mean anomaly: 250
7969 deg
Mean motion: 15
54076647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 327
Coasting Arc #8 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2017/316/12:37:22
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3033606
65 A = 6778280
94 meter
Y = 3245172
93 meter E =
0008100
Z = 5113204
01 I = 51
74634
XDOT = -6598
383366 Wp = 79
01052
YDOT = -3550
114570 meter/sec RA = 18
23468 deg
ZDOT = -1657
879611 TA = 26
97911
MA = 26
93703
Ha = 222
499 n
mi
Hp = 213
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9952777
73 X = -3094507
36
Y = 10646892
81 feet Y = 3210908
67 meter
Z = 16775603
71 Z = 5098319
49
XDOT = -21648
239389 XDOT = -6550
141349
YDOT = -11647
357514 feet/sec YDOT = -3623
632502 meter/sec
ZDOT = -5439
237570 ZDOT = -1689
815704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4265561
28 X = -1300143
08
Y = -14016068
89 feet Y = -4272097
80 meter
Z = 16708973
36 Z = 5092895
08
XDOT = 19801
811569 XDOT = 6035
592166
YDOT = -12693
502856 feet/sec YDOT = -3868
979670 meter/sec
ZDOT = -5580
337805 ZDOT = -1700
886963
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 17316
57127191
00016717 00000-0 10270-3 0 9075
2 25544 51
6417 18
6103 0004007 111
8580 248
2999 15
54135499 4823
Satellite: ISS
Catalog Number: 25544
Epoch time: 17316
57127191 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 18
6103 deg
Eccentricity:
0004007
Arg of perigee: 111
8580 deg
Mean anomaly: 248
2999 deg
Mean motion: 15
54135499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 312
Coasting Arc #9 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2017/317/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5334151
90 A = 6786599
00 meter
Y = -3349630
34 meter E =
0009258
Z = -2525497
21 I = 51
74557
XDOT = 4512
915475 Wp = 122
66838
YDOT = -3203
176765 meter/sec RA = 13
69752 deg
ZDOT = -5302
371753 TA = 85
62083
MA = 85
51506
Ha = 222
420 n
mi
Hp = 213
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17500498
38 X = -5284031
16
Y = -10989600
85 feet Y = -3409000
30 meter
Z = -8285752
00 Z = -2551287
47
XDOT = 14806
153132 XDOT = 4574
155599
YDOT = -10509
110120 feet/sec YDOT = -3152
367999 meter/sec
ZDOT = -17396
232785 ZDOT = -5280
300202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20618541
11 X = 6284531
33
Y = 121939
33 feet Y = 37167
11 meter
Z = -8399604
15 Z = -2560199
34
XDOT = -7112
189987 XDOT = -2167
795508
YDOT = 15300
387234 feet/sec YDOT = 4663
558029 meter/sec
ZDOT = -17297
719910 ZDOT = -5272
345028
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 17317
47151028
00016717 00000-0 10270-3 0 9082
2 25544 51
6419 14
1222 0004139 116
0594 244
0986 15
54110308 4963
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
47151028 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 14
1222 deg
Eccentricity:
0004139
Arg of perigee: 116
0594 deg
Mean anomaly: 244
0986 deg
Mean motion: 15
54110308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 289
Coasting Arc #10 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2017/317/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4948063
20 A = 6782475
74 meter
Y = -2273535
19 meter E =
0011123
Z = -4055207
54 I = 51
71724
XDOT = 5107
084832 Wp = 108
61784
YDOT = 4163
666647 meter/sec RA = 11
32097 deg
ZDOT = 3902
505915 TA = 201
83854
MA = 201
88599
Ha = 222
457 n
mi
Hp = 213
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16233803
14 X = 4992817
30
Y = -7459104
97 feet Y = -2217952
46 meter
Z = -13304486
68 Z = -4031062
17
XDOT = 16755
527665 XDOT = 5041
189217
YDOT = 13660
323645 feet/sec YDOT = 4220
409230 meter/sec
ZDOT = 12803
497096 ZDOT = 3927
154829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12572796
78 X = 3832188
46
Y = -12804278
37 feet Y = -3902744
05 meter
Z = -13196939
57 Z = -4022427
18
XDOT = 19520
866316 XDOT = 5949
960053
YDOT = 5877
959362 feet/sec YDOT = 1791
602013 meter/sec
ZDOT = 12912
134909 ZDOT = 3935
618720
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 17317
92162873
00016717 00000-0 10270-3 0 9093
2 25544 51
6424 11
8806 0004108 111
1942 248
9650 15
54130407 5032
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
92162873 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 11
8806 deg
Eccentricity:
0004108
Arg of perigee: 111
1942 deg
Mean anomaly: 248
9650 deg
Mean motion: 15
54130407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 289
Coasting Arc #11 (Orbit 518)
---------------------------------------
Vector Time (GMT): 2017/318/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6023362
61 A = 6786338
02 meter
Y = 1495323
54 meter E =
0017538
Z = 2724360
65 I = 51
69727
XDOT = -3463
313017 Wp = 104
72232
YDOT = -4492
145196 meter/sec RA = 6
34447 deg
ZDOT = -5168
097886 TA = 44
46685
MA = 44
32620
Ha = 222
521 n
mi
Hp = 213
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19761688
37 X = -6052869
95
Y = 4905917
11 feet Y = 1427801
26 meter
Z = 8938191
11 Z = 2695028
68
XDOT = -11362
575515 XDOT = -3387
718613
YDOT = -14738
009174 feet/sec YDOT = -4530
451789 meter/sec
ZDOT = -16955
701726 ZDOT = -5184
738225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16550551
79 X = -5044608
19
Y = 11957671
82 feet Y = 3644698
37 meter
Z = 8807776
70 Z = 2684610
34
XDOT = -15071
852375 XDOT = -4593
900604
YDOT = -8260
408446 feet/sec YDOT = -2517
772494 meter/sec
ZDOT = -17028
735257 ZDOT = -5190
358506
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 17318
95046687
00016717 00000-0 10270-3 0 9103
2 25544 51
6421 6
7530 0004104 116
4307 243
7267 15
54106808 5197
Satellite: ISS
Catalog Number: 25544
Epoch time: 17318
95046687 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 6
7530 deg
Eccentricity:
0004104
Arg of perigee: 116
4307 deg
Mean anomaly: 243
7267 deg
Mean motion: 15
54106808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 519
Checksum: 294
Coasting Arc #12 (Orbit 533)
---------------------------------------
Vector Time (GMT): 2017/319/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6645825
22 A = 6788756
46 meter
Y = -750763
07 meter E =
0010803
Z = -1150938
62 I = 51
67424
XDOT = 1537
717999 Wp = 58
87544
YDOT = 4680
278683 meter/sec RA = 1
37307 deg
ZDOT = 5872
471485 TA = 288
63964
MA = 288
75691
Ha = 222
343 n
mi
Hp = 213
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21803888
50 X = 6659317
35
Y = -2463133
44 feet Y = -676369
49 meter
Z = -3776045
33 Z = -1118621
69
XDOT = 5045
006557 XDOT = 1456
741298
YDOT = 15355
245023 feet/sec YDOT = 4697
021817 meter/sec
ZDOT = 19266
638730 ZDOT = 5879
744669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19143837
43 X = 5835041
65
Y = -10772804
39 feet Y = -3283550
78 meter
Z = -3632529
76 Z = -1107195
07
XDOT = 9727
016460 XDOT = 2964
794617
YDOT = 10831
401032 feet/sec YDOT = 3301
411035 meter/sec
ZDOT = 19298
070518 ZDOT = 5882
051894
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 17319
91499665
00016717 00000-0 10270-3 0 9119
2 25544 51
6431 1
9446 0003942 119
0300 241
1248 15
54144712 5346
Satellite: ISS
Catalog Number: 25544
Epoch time: 17319
91499665 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 1
9446 deg
Eccentricity:
0003942
Arg of perigee: 119
0300 deg
Mean anomaly: 241
1248 deg
Mean motion: 15
54144712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 534
Checksum: 289
Coasting Arc #13 (Orbit 549)
---------------------------------------
Vector Time (GMT): 2017/320/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6757177
21 A = 6789234
16 meter
Y = -43781
21 meter E =
0014632
Z = -590583
39 I = 51
64227
XDOT = 544
523259 Wp = 134
60323
YDOT = -4774
008804 meter/sec RA = 356
40510 deg
ZDOT = -5977
423603 TA = 51
77167
MA = 51
64005
Ha = 222
344 n
mi
Hp = 213
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22169216
58 X = -6753316
59
Y = -143639
14 feet Y = -119322
99 meter
Z = -1937609
55 Z = -623399
15
XDOT = 1786
493631 XDOT = 626
903184
YDOT = -15662
758542 feet/sec YDOT = -4767
458953 meter/sec
ZDOT = -19610
969825 ZDOT = -5974
578319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20312254
19 X = -6191175
08
Y = 8849960
06 feet Y = 2697467
82 meter
Z = -2083185
96 Z = -634955
08
XDOT = -3953
709717 XDOT = -1205
090722
YDOT = -13614
857940 feet/sec YDOT = -4149
808700 meter/sec
ZDOT = -19597
489778 ZDOT = -5973
314884
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 17320
94382644
00016717 00000-0 10270-3 0 9123
2 25544 51
6426 356
8165 0004037 123
7421 236
4116 15
54102205 5502
Satellite: ISS
Catalog Number: 25544
Epoch time: 17320
94382644 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 356
8165 deg
Eccentricity:
0004037
Arg of perigee: 123
7421 deg
Mean anomaly: 236
4116 deg
Mean motion: 15
54102205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 550
Checksum: 279
Coasting Arc #14 (Orbit 565)
---------------------------------------
Vector Time (GMT): 2017/321/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6353733
23 A = 6787152
74 meter
Y = 823272
05 meter E =
0016485
Z = 2221698
45 I = 51
60244
XDOT = -2535
886633 Wp = 82
18927
YDOT = 4755
994904 meter/sec RA = 351
43145 deg
ZDOT = 5457
371967 TA = 302
52192
MA = 302
68110
Ha = 222
225 n
mi
Hp = 213
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20845581
47 X = 6333262
75
Y = 2701023
79 feet Y = 894209
34 meter
Z = 7289036
92 Z = 2252514
04
XDOT = -8319
838034 XDOT = -2615
390909
YDOT = 15603
657822 feet/sec YDOT = 4727
192244 meter/sec
ZDOT = 17904
763671 ZDOT = 5444
860072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20001504
93 X = 6096458
70
Y = -6305890
18 feet Y = -1922035
33 meter
Z = 7425591
25 Z = 2263320
21
XDOT = -1542
463744 XDOT = -470
142949
YDOT = 16248
438942 feet/sec YDOT = 4952
524190 meter/sec
ZDOT = 17848
402377 ZDOT = 5440
193045
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 17321
97265214
00016717 00000-0 10270-3 0 9131
2 25544 51
6420 351
6877 0003858 124
7827 235
3689 15
54131601 5662
Satellite: ISS
Catalog Number: 25544
Epoch time: 17321
97265214 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 351
6877 deg
Eccentricity:
0003858
Arg of perigee: 124
7827 deg
Mean anomaly: 235
3689 deg
Mean motion: 15
54131601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 566
Checksum: 317
Coasting Arc #15 (Orbit 580)
---------------------------------------
Vector Time (GMT): 2017/322/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5460090
09 A = 6783500
36 meter
Y = -1676835
03 meter E =
0008531
Z = -3665560
50 I = 51
55846
XDOT = 4323
531133 Wp = 98
75956
YDOT = -4593
112917 meter/sec RA = 346
44778 deg
ZDOT = -4348
968158 TA = 124
83656
MA = 124
75629
Ha = 222
117 n
mi
Hp = 213
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17913681
39 X = -5423127
51
Y = -5501427
27 feet Y = -1737686
68 meter
Z = -12026117
12 Z = -3691994
90
XDOT = 14184
813430 XDOT = 4395
696916
YDOT = -15069
268099 feet/sec YDOT = -4544
360570 meter/sec
ZDOT = -14268
268234 ZDOT = -4327
790128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18447165
76 X = -5622696
12
Y = 2835658
44 feet Y = 864308
69 meter
Z = -12143075
92 Z = -3701209
54
XDOT = 6473
025610 XDOT = 1972
978206
YDOT = -18446
765805 feet/sec YDOT = -5622
574217 meter/sec
ZDOT = -14173
494734 ZDOT = -4320
081195
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 17322
93717221
00016717 00000-0 10270-3 0 9149
2 25544 51
6423 346
8795 0003740 130
8414 229
3063 15
54136554 5818
Satellite: ISS
Catalog Number: 25544
Epoch time: 17322
93717221 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 346
8795 deg
Eccentricity:
0003740
Arg of perigee: 130
8414 deg
Mean anomaly: 229
3063 deg
Mean motion: 15
54136554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 581
Checksum: 301
Coasting Arc #16 (Orbit 596)
---------------------------------------
Vector Time (GMT): 2017/323/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4194462
74 A = 6779875
02 meter
Y = 2522065
12 meter E =
0011605
Z = 4685862
16 I = 51
51436
XDOT = -5719
269669 Wp = 121
03576
YDOT = 4273
961029 meter/sec RA = 341
45075 deg
ZDOT = 2808
104288 TA = 301
02941
MA = 301
14332
Ha = 222
086 n
mi
Hp = 213
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13761360
69 X = 4143186
42
Y = 8274491
86 feet Y = 2568683
51 meter
Z = 15373563
52 Z = 4706113
64
XDOT = -18764
008101 XDOT = -5780
277895
YDOT = 14022
181854 feet/sec YDOT = 4209
662983 meter/sec
ZDOT = 9212
940577 ZDOT = 2780
173222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15925667
09 X = 4854143
33
Y = 1208039
15 feet Y = 368210
33 meter
Z = 15462939
17 Z = 4713103
86
XDOT = -10365
285385 XDOT = -3159
338985
YDOT = 19855
771895 feet/sec YDOT = 6052
039274 meter/sec
ZDOT = 9088
272697 ZDOT = 2770
105518
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 17323
96599095
00016717 00000-0 10270-3 0 9151
2 25544 51
6419 341
7500 0003824 130
9097 229
2387 15
54135418 5975
Satellite: ISS
Catalog Number: 25544
Epoch time: 17323
96599095 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 341
7500 deg
Eccentricity:
0003824
Arg of perigee: 130
9097 deg
Mean anomaly: 229
2387 deg
Mean motion: 15
54135418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 597
Checksum: 330
Coasting Arc #17 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2017/324/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2653771
47 A = 6777503
74 meter
Y = -3397685
93 meter E =
0016991
Z = -5244112
00 I = 51
47464
XDOT = 6626
881573 Wp = 92
65996
YDOT = -3714
633180 meter/sec RA = 336
44281 deg
ZDOT = -950
230226 TA = 168
23168
MA = 168
19192
Ha = 222
056 n
mi
Hp = 213
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8706599
31 X = -2590106
54
Y = -11147263
56 feet Y = -3427005
91 meter
Z = -17205091
88 Z = -5256849
06
XDOT = 21741
737445 XDOT = 6672
542920
YDOT = -12187
116732 feet/sec YDOT = -3640
271496 meter/sec
ZDOT = -3117
553235 ZDOT = -917
927526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12806958
10 X = -3903560
83
Y = -5841409
31 feet Y = -1780461
56 meter
Z = -17260976
34 Z = -5261145
59
XDOT = 13119
251266 XDOT = 3998
747786
YDOT = -20009
668778 feet/sec YDOT = -6098
947044 meter/sec
ZDOT = -2973
599552 ZDOT = -906
353143
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 17324
93050435
00016717 00000-0 10270-3 0 9160
2 25544 51
6406 336
9412 0003748 135
6546 224
4908 15
54171732 6128
Satellite: ISS
Catalog Number: 25544
Epoch time: 17324
93050435 = yrday
fracday
Element set: 916
Inclination: 51
6406 deg
RA of node: 336
9412 deg
Eccentricity:
0003748
Arg of perigee: 135
6546 deg
Mean anomaly: 224
4908 deg
Mean motion: 15
54171732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 302
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