[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 26th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 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
090/14:15:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
2
091/16:23:58
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
2
093/17:58:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
0
094/19:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
1
098/16:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 213
8
Coasting Arc #1 (Orbit 3195)
---------------------------------------
Vector Time (GMT): 2016/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1973076
71 A = 6788439
48 meter
Y = 6397638
58 meter E =
0010995
Z = -1088633
30 I = 51
99232
XDOT = -4853
685725 Wp = 30
54353
YDOT = -496
104856 meter/sec RA = 114
44076 deg
ZDOT = 5916
826075 TA = 317
70340
MA = 317
78814
Ha = 220
839 n
mi
Hp = 214
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6473348
79 X = -2039181
91
Y = 20989627
88 feet Y = 6375204
54 meter
Z = -3571631
56 Z = -1098379
57
XDOT = -15924
165764 XDOT = -4876
518970
YDOT = -1627
640604 feet/sec YDOT = -550
508795 meter/sec
ZDOT = 19412
159039 ZDOT = 5893
192577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5517613
18 X = -1681768
50
Y = 21253533
66 feet Y = 6478077
06 meter
Z = -3615041
75 Z = -1101864
73
XDOT = -14554
910531 XDOT = -4436
336730
YDOT = -513
681360 feet/sec YDOT = -156
570078 meter/sec
ZDOT = 19309
540033 ZDOT = 5885
547802
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 16085
50213813
00016717 00000-0 10270-3 0 9000
2 25544 51
6409 115
4128 0002081 351
6731 8
4387 15
54256639 31961
Satellite: ISS
Catalog Number: 25544
Epoch time: 16085
50213813 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 115
4128 deg
Eccentricity:
0002081
Arg of perigee: 351
6731 deg
Mean anomaly: 8
4387 deg
Mean motion: 15
54256639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3196
Checksum: 295
Coasting Arc #2 (Orbit 3211)
---------------------------------------
Vector Time (GMT): 2016/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2753650
75 A = 6788775
25 meter
Y = -6162899
28 meter E =
0009014
Z = -690205
99 I = 52
00573
XDOT = 4083
667004 Wp = 131
97114
YDOT = 2489
404760 meter/sec RA = 109
49447 deg
ZDOT = -5991
771270 TA = 55
44502
MA = 55
35999
Ha = 220
908 n
mi
Hp = 214
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9034287
22 X = 2825713
91
Y = -20219485
81 feet Y = -6131703
29 meter
Z = -2264455
35 Z = -676653
49
XDOT = 13397
857624 XDOT = 4084
632016
YDOT = 8167
338451 feet/sec YDOT = 2535
075631 meter/sec
ZDOT = -19658
042224 ZDOT = -5971
931685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7791907
81 X = 2374973
50
Y = -20736439
91 feet Y = -6320466
88 meter
Z = -2204527
81 Z = -671940
08
XDOT = 12487
033250 XDOT = 3806
047735
YDOT = 6752
841542 feet/sec YDOT = 2058
266102 meter/sec
ZDOT = -19572
241111 ZDOT = -5965
619091
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 16086
53088950
00016717 00000-0 10270-3 0 9017
2 25544 51
6409 110
2832 0002081 355
8086 4
3049 15
54252156 32124
Satellite: ISS
Catalog Number: 25544
Epoch time: 16086
53088950 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 110
2832 deg
Eccentricity:
0002081
Arg of perigee: 355
8086 deg
Mean anomaly: 4
3049 deg
Mean motion: 15
54252156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3212
Checksum: 285
Coasting Arc #3 (Orbit 3227)
---------------------------------------
Vector Time (GMT): 2016/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3313940
24 A = 6786616
61 meter
Y = 5420520
04 meter E =
0014705
Z = 2363852
80 I = 52
00821
XDOT = -3243
520054 Wp = 64
69128
YDOT = -4355
457937 meter/sec RA = 104
54614 deg
ZDOT = 5420
190844 TA = 321
57053
MA = 321
67517
Ha = 221
047 n
mi
Hp = 214
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10872507
36 X = -3385790
22
Y = 17783858
40 feet Y = 5383059
90 meter
Z = 7755422
57 Z = 2347579
21
XDOT = -10641
469992 XDOT = -3220
904348
YDOT = -14289
560161 feet/sec YDOT = -4391
602033 meter/sec
ZDOT = 17782
778360 ZDOT = 5404
489961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9492855
27 X = -2893422
29
Y = 18586792
62 feet Y = 5665254
39 meter
Z = 7683778
62 Z = 2342015
72
XDOT = -10488
242129 XDOT = -3196
816201
YDOT = -12707
666739 feet/sec YDOT = -3873
296822 meter/sec
ZDOT = 17715
282459 ZDOT = 5399
618094
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 16087
55963353
00016717 00000-0 10270-3 0 9020
2 25544 51
6407 105
1539 0002296 1
8673 358
2488 15
54262542 32282
Satellite: ISS
Catalog Number: 25544
Epoch time: 16087
55963353 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 105
1539 deg
Eccentricity:
0002296
Arg of perigee: 1
8673 deg
Mean anomaly: 358
2488 deg
Mean motion: 15
54262542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3228
Checksum: 316
Coasting Arc #4 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2016/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3729295
02 A = 6782831
86 meter
Y = -4199414
21 meter E =
0006976
Z = -3811365
64 I = 52
00207
XDOT = 2353
846405 Wp = 58
99744
YDOT = 5933
027028 meter/sec RA = 99
59032 deg
ZDOT = -4236
160446 TA = 166
44739
MA = 166
42865
Ha = 220
985 n
mi
Hp = 214
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12235219
89 X = 3794490
87
Y = -13777605
69 feet Y = -4157346
63 meter
Z = -12504480
43 Z = -3793090
71
XDOT = 7722
593192 XDOT = 2307
904488
YDOT = 19465
311773 feet/sec YDOT = 5959
091977 meter/sec
ZDOT = -13898
164194 ZDOT = -4224
838178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10941560
48 X = 3334987
63
Y = -14893061
07 feet Y = -4539405
01 meter
Z = -12424332
64 Z = -3786936
59
XDOT = 8550
920172 XDOT = 2606
320469
YDOT = 17830
153911 feet/sec YDOT = 5434
630912 meter/sec
ZDOT = -13849
976792 ZDOT = -4221
472926
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 16088
52407486
00016717 00000-0 10270-3 0 9039
2 25544 51
6400 100
3456 0002230 3
3619 356
7548 15
54274182 32435
Satellite: ISS
Catalog Number: 25544
Epoch time: 16088
52407486 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 100
3456 deg
Eccentricity:
0002230
Arg of perigee: 3
3619 deg
Mean anomaly: 356
7548 deg
Mean motion: 15
54274182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3243
Checksum: 288
Coasting Arc #5 (Orbit 3258)
---------------------------------------
Vector Time (GMT): 2016/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3987562
78 A = 6779149
97 meter
Y = 2607793
53 meter E =
0006878
Z = 4817128
91 I = 51
99373
XDOT = -1470
030115 Wp = 100
84445
YDOT = -7065
600199 meter/sec RA = 94
62302 deg
ZDOT = 2603
748753 TA = 323
61974
MA = 323
66647
Ha = 221
181 n
mi
Hp = 214
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13082555
06 X = -4039827
11
Y = 8555753
04 feet Y = 2562910
18 meter
Z = 15804228
70 Z = 4797631
01
XDOT = -4822
933447 XDOT = -1403
559534
YDOT = -23181
103016 feet/sec YDOT = -7081
667147 meter/sec
ZDOT = 8542
482785 ZDOT = 2596
769788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12135321
70 X = -3698846
05
Y = 9988687
44 feet Y = 3044551
93 meter
Z = 15719029
62 Z = 4791160
23
XDOT = -6731
114519 XDOT = -2051
643705
YDOT = -21597
881049 feet/sec YDOT = -6583
034144 meter/sec
ZDOT = 8513
381410 ZDOT = 2594
878654
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 16089
55280654
00016717 00000-0 10270-3 0 9040
2 25544 51
6395 95
2157 0002303 7
1164 353
0021 15
54275217 32599
Satellite: ISS
Catalog Number: 25544
Epoch time: 16089
55280654 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 95
2157 deg
Eccentricity:
0002303
Arg of perigee: 7
1164 deg
Mean anomaly: 353
0021 deg
Mean motion: 15
54275217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3259
Checksum: 293
Coasting Arc #6 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2016/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4149108
68 A = 6777057
50 meter
Y = -781091
68 meter E =
0015481
Z = -5314558
12 I = 51
98905
XDOT = 570
749953 Wp = 76
52893
YDOT = 7606
603298 meter/sec RA = 89
64839 deg
ZDOT = -670
501494 TA = 187
07937
MA = 187
10126
Ha = 221
095 n
mi
Hp = 214
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13612561
30 X = 4183350
62
Y = -2562636
75 feet Y = -734502
59 meter
Z = -17436214
31 Z = -5294319
47
XDOT = 1872
539215 XDOT = 488
905625
YDOT = 24956
047567 feet/sec YDOT = 7612
528127 meter/sec
ZDOT = -2199
808051 ZDOT = -667
928375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13275471
07 X = 4046363
58
Y = -4323830
10 feet Y = -1317903
41 meter
Z = -17348108
34 Z = -5287703
42
XDOT = 4794
474724 XDOT = 1461
355896
YDOT = 23531
817648 feet/sec YDOT = 7172
498019 meter/sec
ZDOT = -2189
965902 ZDOT = -667
501607
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 16090
51723465
00016717 00000-0 10270-3 0 9051
2 25544 51
6401 90
4076 0002334 11
6898 348
4309 15
54282699 32748
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
51723465 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 90
4076 deg
Eccentricity:
0002334
Arg of perigee: 11
6898 deg
Mean anomaly: 348
4309 deg
Mean motion: 15
54282699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 313
Coasting Arc #7 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2016/090/14:15:30
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3899386
99 A = 6778116
22 meter
Y = 2320289
56 meter E =
0005230
Z = 5031092
34 I = 51
99294
XDOT = -1680
095062 Wp = 99
52313
YDOT = -7208
281447 meter/sec RA = 89
19202 deg
ZDOT = 2019
593759 TA = 330
94525
MA = 330
97434
Ha = 221
111 n
mi
Hp = 214
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12793264
39 X = -3949482
21
Y = 7612498
57 feet Y = 2276404
36 meter
Z = 16506208
47 Z = 5012028
14
XDOT = -5512
122906 XDOT = -1609
175754
YDOT = -23649
217346 feet/sec YDOT = -7226
672679 meter/sec
ZDOT = 6625
963775 ZDOT = 2011
605124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4634256
35 X = -1412521
34
Y = 14243719
37 feet Y = 4341485
66 meter
Z = 16422934
97 Z = 5005710
58
XDOT = -18773
244693 XDOT = -5722
084982
YDOT = -13719
064267 feet/sec YDOT = -4181
570789 meter/sec
ZDOT = 6592
513767 ZDOT = 2009
398196
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 16090
64582433
00016717 00000-0 10270-3 0 9064
2 25544 51
6400 89
7664 0002428 5
5181 354
5998 15
54323075 32760
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
64582433 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 89
7664 deg
Eccentricity:
0002428
Arg of perigee: 5
5181 deg
Mean anomaly: 354
5998 deg
Mean motion: 15
54323075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 318
Coasting Arc #8 (Orbit 3290)
---------------------------------------
Vector Time (GMT): 2016/091/14:15:30
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4154099
20 A = 6776858
48 meter
Y = -465084
66 meter E =
0015566
Z = -5347363
92 I = 51
98668
XDOT = 801
114879 Wp = 80
66324
YDOT = 7615
386704 meter/sec RA = 84
21488 deg
ZDOT = -37
637559 TA = 188
96540
MA = 188
99323
Ha = 221
099 n
mi
Hp = 214
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13628934
40 X = 4184966
39
Y = -1525868
32 feet Y = -418458
63 meter
Z = -17543844
87 Z = -5327109
30
XDOT = 2628
329656 XDOT = 716
081017
YDOT = 24984
864515 feet/sec YDOT = 7623
869848 meter/sec
ZDOT = -123
482806 ZDOT = -33
953118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9115500
39 X = 2778404
52
Y = -10395580
89 feet Y = -3168573
06 meter
Z = -17455720
27 Z = -5320503
54
XDOT = 18033
933499 XDOT = 5496
742930
YDOT = 16009
100277 feet/sec YDOT = 4879
573765 meter/sec
ZDOT = -108
826879 ZDOT = -33
170433
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 16091
61024665
00016717 00000-0 10270-3 0 9071
2 25544 51
6397 84
9573 0002493 11
2875 348
8333 15
54300291 32918
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
61024665 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 84
9573 deg
Eccentricity:
0002493
Arg of perigee: 11
2875 deg
Mean anomaly: 348
8333 deg
Mean motion: 15
54300291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3291
Checksum: 313
Coasting Arc #9 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2016/091/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2656074
33 A = 6781931
21 meter
Y = 4749932
33 meter E =
0011106
Z = 4037232
63 I = 52
00494
XDOT = -3698
118671 Wp = 88
69388
YDOT = -5436
889954 meter/sec RA = 83
79815 deg
ZDOT = 3954
595623 TA = 320
42189
MA = 320
50292
Ha = 221
171 n
mi
Hp = 214
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8714154
62 X = -2728603
01
Y = 15583767
48 feet Y = 4719825
15 meter
Z = 13245513
88 Z = 4024153
51
XDOT = -12132
935272 XDOT = -3656
256911
YDOT = -17837
565465 feet/sec YDOT = -5478
010378 meter/sec
ZDOT = 12974
395087 ZDOT = 3936
733204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12692146
45 X = 3868566
24
Y = 12618436
18 feet Y = 3846099
35 meter
Z = 13187813
48 Z = 4019645
55
XDOT = -19517
993198 XDOT = -5949
084327
YDOT = 6120
948453 feet/sec YDOT = 1865
665088 meter/sec
ZDOT = 12897
722770 ZDOT = 3931
225900
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 16091
73883597
00016717 00000-0 10270-3 0 9082
2 25544 51
6410 84
3171 0002467 12
2758 347
8454 15
54312984 32931
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
73883597 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 84
3171 deg
Eccentricity:
0002467
Arg of perigee: 12
2758 deg
Mean anomaly: 347
8454 deg
Mean motion: 15
54312984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 327
Coasting Arc #10 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2016/092/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3328220
37 A = 6778356
94 meter
Y = -3205220
12 meter E =
0013837
Z = -4972184
70 I = 51
98969
XDOT = 3082
766161 Wp = 64
75992
YDOT = 6648
629547 meter/sec RA = 78
82893 deg
ZDOT = -2221
485104 TA = 183
63137
MA = 183
64142
Ha = 221
093 n
mi
Hp = 214
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10919358
17 X = 3387967
29
Y = -10515814
04 feet Y = -3167668
12 meter
Z = -16312941
94 Z = -4955871
66
XDOT = 10114
062209 XDOT = 3018
981423
YDOT = 21813
089066 feet/sec YDOT = 6682
746249 meter/sec
ZDOT = -7288
336955 ZDOT = -2206
665329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7445565
37 X = -2269408
32
Y = -13293064
47 feet Y = -4051726
05 meter
Z = -16241453
00 Z = -4950394
88
XDOT = 22684
592652 XDOT = 6914
263840
YDOT = -3874
512192 feet/sec YDOT = -1180
951316 meter/sec
ZDOT = -7225
115530 ZDOT = -2202
215214
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 16092
70325044
00016717 00000-0 10270-3 0 9099
2 25544 51
6419 79
5083 0002537 15
1055 345
0173 15
54337254 33080
Satellite: ISS
Catalog Number: 25544
Epoch time: 16092
70325044 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 79
5083 deg
Eccentricity:
0002537
Arg of perigee: 15
1055 deg
Mean anomaly: 345
0173 deg
Mean motion: 15
54337254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 293
Coasting Arc #11 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2016/093/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3928334
35 A = 6776654
37 meter
Y = 1424287
16 meter E =
0003654
Z = 5332312
75 I = 51
97725
XDOT = -2317
353237 Wp = 57
71999
YDOT = -7309
298653 meter/sec RA = 73
85207 deg
ZDOT = 246
924867 TA = 29
94886
MA = 29
92796
Ha = 221
182 n
mi
Hp = 214
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12888236
05 X = -3969871
14
Y = 4672858
15 feet Y = 1380126
20 meter
Z = 17494464
41 Z = 5313128
90
XDOT = -7602
864952 XDOT = -2236
646062
YDOT = -23980
638626 feet/sec YDOT = -7334
761553 meter/sec
ZDOT = 810
120954 ZDOT = 235
864524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1531169
74 X = 466700
54
Y = 13730170
86 feet Y = 4184956
08 meter
Z = 17410814
00 Z = 5306816
11
XDOT = -24090
043378 XDOT = -7342
645222
YDOT = 1725
913153 feet/sec YDOT = 526
058329 meter/sec
ZDOT = 763
369856 ZDOT = 232
675132
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 16093
73194929
00016717 00000-0 10270-3 0 9101
2 25544 51
6420 74
3791 0002499 15
3607 344
7621 15
54371440 33240
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
73194929 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 74
3791 deg
Eccentricity:
0002499
Arg of perigee: 15
3607 deg
Mean anomaly: 344
7621 deg
Mean motion: 15
54371440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 305
Coasting Arc #12 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2016/093/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4188533
31 A = 6776778
80 meter
Y = 462773
50 meter E =
0005004
Z = 5304733
39 I = 51
97850
XDOT = -1667
274539 Wp = 41
59875
YDOT = -7458
881368 meter/sec RA = 73
51804 deg
ZDOT = -661
756043 TA = 54
71108
MA = 54
66428
Ha = 221
170 n
mi
Hp = 214
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13741907
18 X = -4219164
91
Y = 1518285
75 feet Y = 415763
79 meter
Z = 17403980
93 Z = 5284312
14
XDOT = -5470
060822 XDOT = -1580
529036
YDOT = -24471
395565 feet/sec YDOT = -7477
040984 meter/sec
ZDOT = -2171
115628 ZDOT = -669
643786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3984435
81 X = 1214456
03
Y = 13354940
41 feet Y = 4070585
84 meter
Z = 17315126
18 Z = 5277650
46
XDOT = -22119
036171 XDOT = -6741
882225
YDOT = 9473
923655 feet/sec YDOT = 2887
651930 meter/sec
ZDOT = -2204
047710 ZDOT = -671
793742
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 16093
79624228
00016717 00000-0 10270-3 0 9118
2 25544 51
6434 74
0588 0002488 14
8517 345
2709 15
54374328 33250
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
79624228 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 74
0588 deg
Eccentricity:
0002488
Arg of perigee: 14
8517 deg
Mean anomaly: 345
2709 deg
Mean motion: 15
54374328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 322
Coasting Arc #13 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2016/094/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4580576
53 A = 6778937
70 meter
Y = 1339705
44 meter E =
0011682
Z = -4824775
53 I = 51
97474
XDOT = 635
786753 Wp = 95
54521
YDOT = 7176
581582 meter/sec RA = 68
54133 deg
ZDOT = 2600
645474 TA = 199
96359
MA = 200
00933
Ha = 221
155 n
mi
Hp = 214
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15028138
23 X = 4588691
81
Y = 4395359
05 feet Y = 1390973
31 meter
Z = -15829316
05 Z = -4802504
73
XDOT = 2085
914543 XDOT = 542
856387
YDOT = 23545
215163 feet/sec YDOT = 7183
172067 meter/sec
ZDOT = 8532
301424 ZDOT = 2603
507418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1333965
69 X = 406592
74
Y = -15698167
31 feet Y = -4784801
39 meter
Z = -15732750
73 Z = -4795342
42
XDOT = 21542
532746 XDOT = 6566
163981
YDOT = -6717
422886 feet/sec YDOT = -2047
470496 meter/sec
ZDOT = 8543
428885 ZDOT = 2604
037124
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 16094
76064250
00016717 00000-0 10270-3 0 9120
2 25544 51
6426 69
2499 0002559 19
2327 340
8922 15
54354545 33409
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
76064250 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 69
2499 deg
Eccentricity:
0002559
Arg of perigee: 19
2327 deg
Mean anomaly: 340
8922 deg
Mean motion: 15
54354545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 313
Coasting Arc #14 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2016/094/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1550588
15 A = 6788149
23 meter
Y = -6492346
77 meter E =
0008036
Z = -1222178
29 I = 52
00406
XDOT = 4914
947420 Wp = 127
37615
YDOT = -72
461430 meter/sec RA = 68
34416 deg
ZDOT = -5881
906615 TA = 65
83522
MA = 65
75123
Ha = 221
155 n
mi
Hp = 214
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5087231
47 X = -1471937
07
Y = -21300350
29 feet Y = -6509246
85 meter
Z = -4009771
28 Z = -1229518
85
XDOT = 16125
155579 XDOT = 4943
964129
YDOT = -237
734351 feet/sec YDOT = -17
337659 meter/sec
ZDOT = -19297
593882 ZDOT = -5857
960595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16446156
72 X = -5012788
57
Y = 14452040
17 feet Y = 4404981
85 meter
Z = -4040492
07 Z = -1231541
98
XDOT = -6771
292693 XDOT = -2063
890013
YDOT = -13043
315037 feet/sec YDOT = -3975
602423 meter/sec
ZDOT = -19193
487938 ZDOT = -5850
175124
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 16094
82493577
00016717 00000-0 10270-3 0 9136
2 25544 51
6420 68
9292 0002411 19
3074 340
8169 15
54311691 33416
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
82493577 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 68
9292 deg
Eccentricity:
0002411
Arg of perigee: 19
3074 deg
Mean anomaly: 340
8169 deg
Mean motion: 15
54311691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 306
Coasting Arc #15 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2016/095/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 565373
53 A = 6785193
33 meter
Y = 6118919
45 meter E =
0014757
Z = 2858893
86 I = 51
98176
XDOT = -5409
556155 Wp = 71
95121
YDOT = -1892
171866 meter/sec RA = 63
39191 deg
ZDOT = 5102
542214 TA = 320
42217
MA = 320
52982
Ha = 221
156 n
mi
Hp = 213
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1854900
04 X = 483020
95
Y = 20075195
05 feet Y = 6124781
75 meter
Z = 9379573
03 Z = 2861439
48
XDOT = -17747
887648 XDOT = -5412
781326
YDOT = -6207
912945 feet/sec YDOT = -1952
682485 meter/sec
ZDOT = 16740
624063 ZDOT = 5076
256362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16703352
17 X = 5091181
74
Y = -11281206
10 feet Y = -3438511
62 meter
Z = 9389510
95 Z = 2861922
94
XDOT = 2381
582700 XDOT = 725
906407
YDOT = 17411
508715 feet/sec YDOT = 5307
027856 meter/sec
ZDOT = 16626
711439 ZDOT = 5067
821647
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 16095
85362020
00016717 00000-0 10270-3 0 9149
2 25544 51
6418 63
7991 0002570 20
3097 339
8158 15
54356481 33574
Satellite: ISS
Catalog Number: 25544
Epoch time: 16095
85362020 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 63
7991 deg
Eccentricity:
0002570
Arg of perigee: 20
3097 deg
Mean anomaly: 339
8158 deg
Mean motion: 15
54356481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 317
Coasting Arc #16 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2016/096/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 610989
42 A = 6781154
10 meter
Y = -5292505
32 meter E =
0009790
Z = -4205894
51 I = 51
95315
XDOT = 5637
600586 Wp = 58
83000
YDOT = 3608
501264 meter/sec RA = 58
42801 deg
ZDOT = -3723
263605 TA = 173
05984
MA = 173
04627
Ha = 221
130 n
mi
Hp = 213
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2004558
45 X = 690556
62
Y = -17363862
61 feet Y = -5285228
54 meter
Z = -13798866
50 Z = -4202732
46
XDOT = 18496
064916 XDOT = 5614
916511
YDOT = 11838
914908 feet/sec YDOT = 3671
417305 meter/sec
ZDOT = -12215
431774 ZDOT = -3695
933056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16095746
58 X = -4905983
56
Y = 6845081
22 feet Y = 2086380
75 meter
Z = -13784139
47 Z = -4201405
71
XDOT = 1497
625781 XDOT = 456
476338
YDOT = -20829
447137 feet/sec YDOT = -6348
815488 meter/sec
ZDOT = -12097
304037 ZDOT = -3687
258270
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 16096
81800383
00016717 00000-0 10270-3 0 9156
2 25544 51
6418 58
9891 0002538 22
2071 337
9191 15
54370305 33720
Satellite: ISS
Catalog Number: 25544
Epoch time: 16096
81800383 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 58
9891 deg
Eccentricity:
0002538
Arg of perigee: 22
2071 deg
Mean anomaly: 337
9191 deg
Mean motion: 15
54370305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3372
Checksum: 310
Coasting Arc #17 (Orbit 3387)
---------------------------------------
Vector Time (GMT): 2016/097/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1883513
60 A = 6777882
59 meter
Y = 4103194
79 meter E =
0006066
Z = 5050368
66 I = 51
92426
XDOT = -5547
015923 Wp = 98
30468
YDOT = -4934
507017 meter/sec RA = 53
45279 deg
ZDOT = 1937
490803 TA = 332
96976
MA = 333
00133
Ha = 221
357 n
mi
Hp = 213
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6179506
57 X = -1953789
29
Y = 13461925
16 feet Y = 4081739
86 meter
Z = 16569450
98 Z = 5041047
67
XDOT = -18198
871139 XDOT = -5500
836348
YDOT = -16189
327484 feet/sec YDOT = -4996
278962 meter/sec
ZDOT = 6356
597123 ZDOT = 1910
657418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14780613
45 X = 4505130
98
Y = -1519713
74 feet Y = -463208
75 meter
Z = 16528169
05 Z = 5037785
93
XDOT = -4636
087487 XDOT = -1413
079466
YDOT = 22886
170139 feet/sec YDOT = 6975
704658 meter/sec
ZDOT = 6240
890754 ZDOT = 1902
223502
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 16097
84667362
00016717 00000-0 10270-3 0 9169
2 25544 51
6416 53
8590 0002632 30
2171 329
9133 15
54355251 33880
Satellite: ISS
Catalog Number: 25544
Epoch time: 16097
84667362 = yrday
fracday
Element set: 916
Inclination: 51
6416 deg
RA of node: 53
8590 deg
Eccentricity:
0002632
Arg of perigee: 30
2171 deg
Mean anomaly: 329
9133 deg
Mean motion: 15
54355251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3388
Checksum: 313
Coasting Arc #18 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2016/098/16:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4318784
15 A = 6777595
87 meter
Y = -1134388
40 meter E =
0014261
Z = -5111211
95 I = 51
90845
XDOT = 3760
995031 Wp = 93
27028
YDOT = 6436
732304 meter/sec RA = 49
08218 deg
ZDOT = 1752
744013 TA = 193
61655
MA = 193
65506
Ha = 221
205 n
mi
Hp = 213
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14169239
32 X = 4355976
56
Y = -3721746
71 feet Y = -1085885
59 meter
Z = -16769068
07 Z = -5090141
63
XDOT = 12339
222542 XDOT = 3680
224178
YDOT = 21117
888135 feet/sec YDOT = 6478
338864 meter/sec
ZDOT = 5750
472485 ZDOT = 1770
817188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -289971
18 X = -88383
22
Y = -14751432
22 feet Y = -4496236
54 meter
Z = -16677276
44 Z = -5083233
86
XDOT = 22329
888848 XDOT = 6806
150121
YDOT = -7014
835697 feet/sec YDOT = -2138
121920 meter/sec
ZDOT = 5827
806908 ZDOT = 1776
315545
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 16098
68246153
00016717 00000-0 10270-3 0 9174
2 25544 51
6436 49
6928 0002549 31
9769 328
1538 15
54404101 34013
Satellite: ISS
Catalog Number: 25544
Epoch time: 16098
68246153 = yrday
fracday
Element set: 917
Inclination: 51
6436 deg
RA of node: 49
6928 deg
Eccentricity:
0002549
Arg of perigee: 31
9769 deg
Mean anomaly: 328
1538 deg
Mean motion: 15
54404101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 321
Coasting Arc #19 (Orbit 3416)
---------------------------------------
Vector Time (GMT): 2016/099/16:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5236297
94 A = 6780739
03 meter
Y = -397494
57 meter E =
0012099
Z = 4283478
12 I = 51
89852
XDOT = -2468
653779 Wp = 65
20266
YDOT = -6313
829928 meter/sec RA = 44
10424 deg
ZDOT = -3590
808293 TA = 61
35733
MA = 61
23571
Ha = 221
270 n
mi
Hp = 213
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17179455
17 X = -5252271
49
Y = -1304116
03 feet Y = -456139
18 meter
Z = 14053405
89 Z = 4258002
35
XDOT = -8099
257805 XDOT = -2380
424617
YDOT = -20714
665119 feet/sec YDOT = -6340
943132 meter/sec
ZDOT = -11780
867104 ZDOT = -3602
585584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5011186
32 X = -1527409
59
Y = 16577695
78 feet Y = 5052881
67 meter
Z = 13942762
63 Z = 4249754
05
XDOT = -20752
668816 XDOT = -6325
413455
YDOT = 3713
003044 feet/sec YDOT = 1131
723328 meter/sec
ZDOT = -11830
845384 ZDOT = -3606
041673
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 16099
71111428
00016717 00000-0 10270-3 0 9186
2 25544 51
6445 44
5635 0002611 33
1754 326
9562 15
54445781 34179
Satellite: ISS
Catalog Number: 25544
Epoch time: 16099
71111428 = yrday
fracday
Element set: 918
Inclination: 51
6445 deg
RA of node: 44
5635 deg
Eccentricity:
0002611
Arg of perigee: 33
1754 deg
Mean anomaly: 326
9562 deg
Mean motion: 15
54445781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3417
Checksum: 309
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