[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 3rd 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
132/13:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
5
135/07:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2016/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1846502
81 A = 6788487
13 meter
Y = -6525656
92 meter E =
0013723
Z = 92827
51 I = 51
30510
XDOT = 4589
531329 Wp = 51
12275
YDOT = 1392
177921 meter/sec RA = 285
17122 deg
ZDOT = 5984
877192 TA = 309
88201
MA = 310
00261
Ha = 221
185 n
mi
Hp = 213
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6058080
07 X = 1918886
17
Y = -21409635
57 feet Y = -6504603
38 meter
Z = 304552
21 Z = 101973
54
XDOT = 15057
517482 XDOT = 4544
550288
YDOT = 4567
512864 feet/sec YDOT = 1443
249859 meter/sec
ZDOT = 19635
423858 ZDOT = 6007
062902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9116582
91 X = -2778734
47
Y = -20296160
62 feet Y = -6186269
76 meter
Z = 345487
72 Z = 105304
66
XDOT = 12896
597607 XDOT = 3930
882951
YDOT = -5427
961712 feet/sec YDOT = -1654
442730 meter/sec
ZDOT = 19731
500589 ZDOT = 6014
161380
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16123
56409040
00016717 00000-0 10270-3 0 9008
2 25544 51
6397 285
6196 0001772 86
3933 273
7423 15
54417256 37883
Satellite: ISS
Catalog Number: 25544
Epoch time: 16123
56409040 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 285
6196 deg
Eccentricity:
0001772
Arg of perigee: 86
3933 deg
Mean anomaly: 273
7423 deg
Mean motion: 15
54417256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 325
Coasting Arc #2 (Orbit 3802)
---------------------------------------
Vector Time (GMT): 2016/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2607990
13 A = 6786878
61 meter
Y = 5972979
71 meter E =
0008174
Z = -1886443
35 I = 51
29175
XDOT = -3928
501157 Wp = 130
18479
YDOT = -3474
372689 meter/sec RA = 280
17539 deg
ZDOT = -5590
931299 TA = 70
68792
MA = 70
59955
Ha = 221
138 n
mi
Hp = 213
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8556398
06 X = -2665423
99
Y = 19596390
12 feet Y = 5943494
21 meter
Z = -6189118
60 Z = -1899252
26
XDOT = -12888
783324 XDOT = -3862
199167
YDOT = -11398
860529 feet/sec YDOT = -3517
933345 meter/sec
ZDOT = -18342
950455 ZDOT = -5609
854034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6417385
98 X = 1956019
25
Y = 20379946
45 feet Y = 6211807
68 meter
Z = -6245845
19 Z = -1903733
61
XDOT = -15631
170463 XDOT = -4764
380757
YDOT = -703
310070 feet/sec YDOT = -214
368909 meter/sec
ZDOT = -18424
474313 ZDOT = -5615
779771
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16124
52844374
00016717 00000-0 10270-3 0 9019
2 25544 51
6390 280
8104 0001793 84
6744 275
4613 15
54441332 38036
Satellite: ISS
Catalog Number: 25544
Epoch time: 16124
52844374 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 280
8104 deg
Eccentricity:
0001793
Arg of perigee: 84
6744 deg
Mean anomaly: 275
4613 deg
Mean motion: 15
54441332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3803
Checksum: 299
Coasting Arc #3 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2016/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3199603
98 A = 6783352
94 meter
Y = -4896116
65 meter E =
0013996
Z = 3423830
64 I = 51
27634
XDOT = 3190
916574 Wp = 90
95099
YDOT = 5283
570253 meter/sec RA = 275
17072 deg
ZDOT = 4557
211961 TA = 309
40510
MA = 309
52894
Ha = 221
028 n
mi
Hp = 213
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10497388
39 X = 3237483
99
Y = -16063374
83 feet Y = -4860124
61 meter
Z = 11233040
16 Z = 3439466
00
XDOT = 10468
886396 XDOT = 3109
459844
YDOT = 17334
548074 feet/sec YDOT = 5318
797942 meter/sec
ZDOT = 14951
482813 ZDOT = 4572
514842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2985439
24 X = -909961
88
Y = -18914652
66 feet Y = -5765186
13 meter
Z = 11301833
15 Z = 3444798
75
XDOT = 17924
176923 XDOT = 5463
289126
YDOT = 6175
762923 feet/sec YDOT = 1882
372539 meter/sec
ZDOT = 15016
960479 ZDOT = 4577
169554
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16125
55707889
00016717 00000-0 10270-3 0 9023
2 25544 51
6400 275
6800 0001653 93
9357 266
1985 15
54452266 38195
Satellite: ISS
Catalog Number: 25544
Epoch time: 16125
55707889 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 275
6800 deg
Eccentricity:
0001653
Arg of perigee: 93
9357 deg
Mean anomaly: 266
1985 deg
Mean motion: 15
54452266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3819
Checksum: 332
Coasting Arc #4 (Orbit 3833)
---------------------------------------
Vector Time (GMT): 2016/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3696527
83 A = 6779348
82 meter
Y = 3357811
67 meter E =
0011927
Z = -4596441
75 I = 51
26205
XDOT = -2361
238451 Wp = 73
15279
YDOT = -6654
991245 meter/sec RA = 270
15474 deg
ZDOT = -2965
703439 TA = 167
09870
MA = 167
06816
Ha = 221
118 n
mi
Hp = 213
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12127715
99 X = -3711472
97
Y = 11016442
47 feet Y = 3316390
95 meter
Z = -15080189
46 Z = -4614435
32
XDOT = -7746
845311 XDOT = -2272
238765
YDOT = -21833
960776 feet/sec YDOT = -6680
898634 meter/sec
ZDOT = -9729
998160 ZDOT = -2976
957645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1303363
57 X = -397265
21
Y = 16259258
72 feet Y = 4955822
06 meter
Z = -15158936
74 Z = -4620443
92
XDOT = -19314
153114 XDOT = -5886
953869
YDOT = -10655
035383 feet/sec YDOT = -3247
654785 meter/sec
ZDOT = -9777
651201 ZDOT = -2980
228086
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16126
52141624
00016717 00000-0 10270-3 0 9031
2 25544 51
6410 270
8708 0001757 91
6095 268
5259 15
54453556 38349
Satellite: ISS
Catalog Number: 25544
Epoch time: 16126
52141624 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 270
8708 deg
Eccentricity:
0001757
Arg of perigee: 91
6095 deg
Mean anomaly: 268
5259 deg
Mean motion: 15
54453556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3834
Checksum: 314
Coasting Arc #5 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2016/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4059256
76 A = 6776700
47 meter
Y = -1530776
11 meter E =
0005236
Z = 5202218
82 I = 51
25419
XDOT = 1474
160135 Wp = 114
21329
YDOT = 7457
416658 meter/sec RA = 265
12813 deg
ZDOT = 1041
158267 TA = 325
75021
MA = 325
78396
Ha = 220
916 n
mi
Hp = 213
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13317771
51 X = 4050801
87
Y = -5022231
32 feet Y = -1485430
06 meter
Z = 17067647
04 Z = 5221917
59
XDOT = 4836
483383 XDOT = 1385
602262
YDOT = 24466
590085 feet/sec YDOT = 7473
406543 meter/sec
ZDOT = 3415
873578 ZDOT = 1048
104416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6029820
73 X = 1837889
36
Y = -12778508
32 feet Y = -3894889
34 meter
Z = 17153466
35 Z = 5228376
54
XDOT = 19508
896784 XDOT = 5946
311740
YDOT = 13842
627573 feet/sec YDOT = 4219
232884 meter/sec
ZDOT = 3444
680521 ZDOT = 1049
938623
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16127
55003334
00016717 00000-0 10270-3 0 9041
2 25544 51
6409 265
7403 0001662 94
8688 265
2655 15
54475246 38502
Satellite: ISS
Catalog Number: 25544
Epoch time: 16127
55003334 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 265
7403 deg
Eccentricity:
0001662
Arg of perigee: 94
8688 deg
Mean anomaly: 265
2655 deg
Mean motion: 15
54475246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 317
Coasting Arc #6 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2016/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4322110
87 A = 6776658
33 meter
Y = -419565
26 meter E =
0016077
Z = -5216716
54 I = 51
25843
XDOT = -492
813770 Wp = 98
02098
YDOT = -7573
107129 meter/sec RA = 260
09900 deg
ZDOT = 1017
885745 TA = 181
78915
MA = 181
79491
Ha = 221
063 n
mi
Hp = 213
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14180153
79 X = -4291756
85
Y = -1376526
43 feet Y = -467728
13 meter
Z = -17115211
73 Z = -5237639
01
XDOT = -1616
843079 XDOT = -413
037326
YDOT = -24846
151999 feet/sec YDOT = -7578
172069 meter/sec
ZDOT = 3339
520161 ZDOT = 1015
685316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10937201
26 X = -3333658
94
Y = 8957309
83 feet Y = 2730188
04 meter
Z = -17205995
71 Z = -5244387
49
XDOT = -18048
397022 XDOT = -5501
151412
YDOT = -15641
764325 feet/sec YDOT = -4767
609766 meter/sec
ZDOT = 3331
335682 ZDOT = 1015
391116
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16128
51435497
00016717 00000-0 10270-3 0 9058
2 25544 51
6415 260
9320 0001735 99
0960 261
0389 15
54486147 38651
Satellite: ISS
Catalog Number: 25544
Epoch time: 16128
51435497 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 260
9320 deg
Eccentricity:
0001735
Arg of perigee: 99
0960 deg
Mean anomaly: 261
0389 deg
Mean motion: 15
54486147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 323
Coasting Arc #7 (Orbit 3880)
---------------------------------------
Vector Time (GMT): 2016/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4421228
95 A = 6779302
84 meter
Y = 2303390
03 meter E =
0009882
Z = 4587545
43 I = 51
27452
XDOT = -584
148223 Wp = 71
51625
YDOT = 7051
094882 meter/sec RA = 255
07232 deg
ZDOT = -2969
008612 TA = 48
26078
MA = 48
17632
Ha = 220
992 n
mi
Hp = 213
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14505344
34 X = 4372858
55
Y = 7557053
91 feet Y = 2352560
49 meter
Z = 15051002
07 Z = 4608905
67
XDOT = -1916
496795 XDOT = -648
529482
YDOT = 23133
513392 feet/sec YDOT = 7044
202706 meter/sec
ZDOT = -9740
841903 ZDOT = -2972
002366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15455063
82 X = 4710703
45
Y = -5085914
57 feet Y = -1550186
76 meter
Z = 15143355
53 Z = 4615694
77
XDOT = 14950
145063 XDOT = 4556
804215
YDOT = 16303
450048 feet/sec YDOT = 4969
291575 meter/sec
ZDOT = -9755
114141 ZDOT = -2973
358790
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16129
54295501
00016717 00000-0 10270-3 0 9063
2 25544 51
6425 255
8013 0001797 101
3969 258
7386 15
54463350 38817
Satellite: ISS
Catalog Number: 25544
Epoch time: 16129
54295501 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 255
8013 deg
Eccentricity:
0001797
Arg of perigee: 101
3969 deg
Mean anomaly: 258
7386 deg
Mean motion: 15
54463350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 324
Coasting Arc #8 (Orbit 3895)
---------------------------------------
Vector Time (GMT): 2016/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4348471
78 A = 6783209
37 meter
Y = -3918536
70 meter E =
0006615
Z = -3433721
59 I = 51
29689
XDOT = 1736
822977 Wp = 94
07557
YDOT = -5911
905281 meter/sec RA = 250
05795 deg
ZDOT = 4554
253820 TA = 225
50668
MA = 225
56077
Ha = 221
009 n
mi
Hp = 213
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14266639
69 X = -4287650
76
Y = -12856091
53 feet Y = -3966823
94 meter
Z = -11265490
79 Z = -3454698
18
XDOT = 5698
238114 XDOT = 1780
679382
YDOT = -19396
014703 feet/sec YDOT = -5892
238018 meter/sec
ZDOT = 14941
777626 ZDOT = 4562
797174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19086563
97 X = -5817584
70
Y = 1572889
87 feet Y = 479416
83 meter
Z = -11355900
40 Z = -3461278
44
XDOT = -10213
453691 XDOT = -3113
060685
YDOT = -15953
577829 feet/sec YDOT = -4862
650522 meter/sec
ZDOT = 14979
943315 ZDOT = 4565
886722
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16130
50725549
00016717 00000-0 10270-3 0 9072
2 25544 51
6424 250
9928 0001648 99
3931 260
7408 15
54486318 38960
Satellite: ISS
Catalog Number: 25544
Epoch time: 16130
50725549 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 250
9928 deg
Eccentricity:
0001648
Arg of perigee: 99
3931 deg
Mean anomaly: 260
7408 deg
Mean motion: 15
54486318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3896
Checksum: 336
Coasting Arc #9 (Orbit 3911)
---------------------------------------
Vector Time (GMT): 2016/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4011068
60 A = 6786771
83 meter
Y = 5150169
11 meter E =
0015683
Z = 1829751
31 I = 51
32015
XDOT = -2955
539638 Wp = 113
19317
YDOT = 4309
090052 meter/sec RA = 245
05533 deg
ZDOT = -5617
422339 TA = 46
58026
MA = 46
44983
Ha = 220
977 n
mi
Hp = 213
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13159673
89 X = 3944291
78
Y = 16896880
27 feet Y = 5194650
07 meter
Z = 6003121
11 Z = 1849074
38
XDOT = -9696
652357 XDOT = -2976
218013
YDOT = 14137
434553 feet/sec YDOT = 4275
923948 meter/sec
ZDOT = -18429
863317 ZDOT = -5631
829728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21333099
23 X = 6502328
65
Y = 1605230
46 feet Y = 489274
24 meter
Z = 6086144
54 Z = 1855056
86
XDOT = 4174
855540 XDOT = 1272
495968
YDOT = 15030
122846 feet/sec YDOT = 4581
181443 meter/sec
ZDOT = -18493
212429 ZDOT = -5636
731148
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16131
53583413
00016717 00000-0 10270-3 0 9089
2 25544 51
6418 245
8628 0001734 108
0165 252
1177 15
54507439 39121
Satellite: ISS
Catalog Number: 25544
Epoch time: 16131
53583413 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 245
8628 deg
Eccentricity:
0001734
Arg of perigee: 108
0165 deg
Mean anomaly: 252
1177 deg
Mean motion: 15
54507439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3912
Checksum: 304
Coasting Arc #10 (Orbit 3926)
---------------------------------------
Vector Time (GMT): 2016/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3410806
35 A = 6788151
04 meter
Y = -5862641
81 meter E =
0012959
Z = -37218
25 I = 51
34053
XDOT = 4128
417801 Wp = 51
69135
YDOT = -2430
809745 meter/sec RA = 240
06125 deg
ZDOT = 5988
413029 TA = 307
90603
MA = 308
02313
Ha = 220
951 n
mi
Hp = 213
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11190309
56 X = -3344814
54
Y = -19234389
14 feet Y = -5900414
73 meter
Z = -122107
13 Z = -53627
21
XDOT = 13544
677825 XDOT = 4126
203567
YDOT = -7975
097588 feet/sec YDOT = -2384
655708 meter/sec
ZDOT = 19647
024372 ZDOT = 6008
462485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21846470
17 X = -6658804
11
Y = -4230177
46 feet Y = -1289358
09 meter
Z = -192362
79 Z = -58632
18
XDOT = 2516
275231 XDOT = 766
960691
YDOT = -13757
313269 feet/sec YDOT = -4193
229085 meter/sec
ZDOT = 19734
553558 ZDOT = 6015
091924
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 16132
50011570
00016717 00000-0 10270-3 0 9098
2 25544 51
6430 241
0535 0001693 103
7978 256
3363 15
54532849 39270
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
50011570 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 241
0535 deg
Eccentricity:
0001693
Arg of perigee: 103
7978 deg
Mean anomaly: 256
3363 deg
Mean motion: 15
54532849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3927
Checksum: 302
Coasting Arc #11 (Orbit 3927)
---------------------------------------
Vector Time (GMT): 2016/132/13:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4675787
86 A = 6785875
52 meter
Y = -4337186
14 meter E =
0006679
Z = -2316298
17 I = 51
33357
XDOT = 2035
197175 Wp = 55
98602
YDOT = -5061
592096 meter/sec RA = 239
74369 deg
ZDOT = 5384
152717 TA = 278
08788
MA = 278
16364
Ha = 220
893 n
mi
Hp = 213
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15340511
37 X = -4615689
20
Y = -14229613
31 feet Y = -4389137
76 meter
Z = -7599403
43 Z = -2338866
36
XDOT = 6677
156086 XDOT = 2065
491839
YDOT = -16606
273282 feet/sec YDOT = -5038
664043 meter/sec
ZDOT = 17664
543034 ZDOT = 5394
112595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18533215
02 X = -5648923
94
Y = 9635615
08 feet Y = 2936935
48 meter
Z = -7696686
24 Z = -2345949
97
XDOT = -12740
710827 XDOT = -3883
368660
YDOT = -10398
728234 feet/sec YDOT = -3169
532366 meter/sec
ZDOT = 17708
701757 ZDOT = 5397
612296
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 16132
56440006
00016717 00000-0 10270-3 0 9106
2 25544 51
6428 240
7343 0001463 100
0730 260
0588 15
54512064 39280
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
56440006 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 240
7343 deg
Eccentricity:
0001463
Arg of perigee: 100
0730 deg
Mean anomaly: 260
0588 deg
Mean motion: 15
54512064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3928
Checksum: 270
Coasting Arc #12 (Orbit 3943)
---------------------------------------
Vector Time (GMT): 2016/133/13:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4232469
60 A = 6787988
29 meter
Y = 5273146
49 meter E =
0014530
Z = 516548
51 I = 51
35707
XDOT = -3456
117572 Wp = 126
65364
YDOT = 3368
652154 meter/sec RA = 234
74958 deg
ZDOT = -5961
869166 TA = 47
74971
MA = 47
62655
Ha = 220
921 n
mi
Hp = 213
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13886055
11 X = 4170680
21
Y = 17300349
38 feet Y = 5320131
28 meter
Z = 1694712
98 Z = 536959
00
XDOT = -11338
968411 XDOT = -3464
569486
YDOT = 11052
008378 feet/sec YDOT = 3329
956500 meter/sec
ZDOT = -19559
938209 ZDOT = -5978
678612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20822687
64 X = 6346755
19
Y = -7631194
36 feet Y = -2325988
04 meter
Z = 1782475
63 Z = 543298
57
XDOT = 6339
576222 XDOT = 1932
302832
YDOT = 12633
552203 feet/sec YDOT = 3850
706711 meter/sec
ZDOT = -19633
557750 ZDOT = -5984
308402
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 16133
59295651
00016717 00000-0 10270-3 0 9115
2 25544 51
6420 235
6043 0001649 104
0521 256
0815 15
54547547 39440
Satellite: ISS
Catalog Number: 25544
Epoch time: 16133
59295651 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 235
6043 deg
Eccentricity:
0001649
Arg of perigee: 104
0521 deg
Mean anomaly: 256
0815 deg
Mean motion: 15
54547547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3944
Checksum: 299
Coasting Arc #13 (Orbit 3959)
---------------------------------------
Vector Time (GMT): 2016/134/13:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3444168
84 A = 6787387
52 meter
Y = -5691800
90 meter E =
0014990
Z = 1311503
13 I = 51
37410
XDOT = 4772
580440 Wp = 63
87810
YDOT = -1540
061820 meter/sec RA = 229
75853 deg
ZDOT = 5804
468579 TA = 310
45594
MA = 310
58655
Ha = 220
909 n
mi
Hp = 213
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11299766
55 X = -3386636
47
Y = -18673887
45 feet Y = -5729994
23 meter
Z = 4302831
79 Z = 1294911
76
XDOT = 15658
072311 XDOT = 4761
251351
YDOT = -5052
696259 feet/sec YDOT = -1486
755117 meter/sec
ZDOT = 19043
532083 ZDOT = 5827
625138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21225906
52 X = -6469656
31
Y = 5144570
73 feet Y = 1568065
16 meter
Z = 4231718
63 Z = 1289827
84
XDOT = 262
738539 XDOT = 80
082707
YDOT = -14787
412324 feet/sec YDOT = -4507
203276 meter/sec
ZDOT = 19144
417240 ZDOT = 5835
218375
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 16134
62150274
00016717 00000-0 10270-3 0 9122
2 25544 51
6418 230
4739 0001627 103
7721 256
3613 15
54555235 39606
Satellite: ISS
Catalog Number: 25544
Epoch time: 16134
62150274 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 230
4739 deg
Eccentricity:
0001627
Arg of perigee: 103
7721 deg
Mean anomaly: 256
3613 deg
Mean motion: 15
54555235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3960
Checksum: 292
Coasting Arc #14 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3669645
42 A = 6776235
67 meter
Y = 2244686
78 meter E =
0016333
Z = -5250006
64 I = 51
35105
XDOT = -4797
054961 Wp = 97
72319
YDOT = -5910
808308 meter/sec RA = 225
96094 deg
ZDOT = 825
883912 TA = 180
21467
MA = 180
21537
Ha = 220
918 n
mi
Hp = 213
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12039519
09 X = -3668970
92
Y = 7364457
95 feet Y = 2203654
20 meter
Z = -17224431
24 Z = -5267831
29
XDOT = -15738
369295 XDOT = -4734
614107
YDOT = -19392
415710 feet/sec YDOT = -5964
103052 meter/sec
ZDOT = 2709
592888 ZDOT = 802
732480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13453502
56 X = -4100627
58
Y = 3937124
14 feet Y = 1200035
44 meter
Z = -17302271
95 Z = -5273732
49
XDOT = -9763
660049 XDOT = -2975
963583
YDOT = -21894
140030 feet/sec YDOT = -6673
333881 meter/sec
ZDOT = 2609
998699 ZDOT = 795
527603
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 16135
32862274
00016717 00000-0 10270-3 0 9131
2 25544 51
6396 226
9446 0001815 107
5566 252
5786 15
54586410 39714
Satellite: ISS
Catalog Number: 25544
Epoch time: 16135
32862274 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 226
9446 deg
Eccentricity:
0001815
Arg of perigee: 107
5566 deg
Mean anomaly: 252
5786 deg
Mean motion: 15
54586410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 329
Coasting Arc #15 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2016/136/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4863294
20 A = 6778707
34 meter
Y = -711250
57 meter E =
0009344
Z = 4661949
08 I = 51
38196
XDOT = 3623
191859 Wp = 72
18981
YDOT = 6141
002534 meter/sec RA = 220
93912 deg
ZDOT = -2835
272829 TA = 46
07264
MA = 45
99556
Ha = 220
835 n
mi
Hp = 213
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15955689
63 X = 4848240
22
Y = -2333499
23 feet Y = -656950
17 meter
Z = 15295108
54 Z = 4685537
36
XDOT = 11887
112397 XDOT = 3568
024987
YDOT = 20147
646110 feet/sec YDOT = 6181
211037 meter/sec
ZDOT = -9302
076211 ZDOT = -2817
806095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15939032
05 X = 4858216
97
Y = 1681200
94 feet Y = 512430
05 meter
Z = 15397740
62 Z = 4693231
34
XDOT = 6688
567240 XDOT = 2038
675295
YDOT = 21321
175305 feet/sec YDOT = 6498
694233 meter/sec
ZDOT = -9227
209167 ZDOT = -2812
453354
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 16136
35715260
00016717 00000-0 10270-3 0 9148
2 25544 51
6394 221
8126 0001876 110
3632 249
7722 15
54562002 39870
Satellite: ISS
Catalog Number: 25544
Epoch time: 16136
35715260 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 221
8126 deg
Eccentricity:
0001876
Arg of perigee: 110
3632 deg
Mean anomaly: 249
7722 deg
Mean motion: 15
54562002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 302
Coasting Arc #16 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2016/137/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5758855
58 A = 6782591
30 meter
Y = -705554
89 meter E =
0006998
Z = -3520252
86 I = 51
42097
XDOT = -2016
249136 Wp = 100
61436
YDOT = -5877
331885 meter/sec RA = 215
93123 deg
ZDOT = 4482
742892 TA = 217
81476
MA = 217
86394
Ha = 220
862 n
mi
Hp = 213
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18893883
13 X = -5733437
82
Y = -2314812
65 feet Y = -769812
12 meter
Z = -11549386
03 Z = -3548166
50
XDOT = -6614
990604 XDOT = -1972
152950
YDOT = -19282
584924 feet/sec YDOT = -5899
632389 meter/sec
ZDOT = 14707
161718 ZDOT = 4473
055434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17769854
72 X = -5416251
72
Y = -6614769
38 feet Y = -2016181
71 meter
Z = -11670586
28 Z = -3557194
70
XDOT = -2540
137988 XDOT = -774
234059
YDOT = -19015
513121 feet/sec YDOT = -5795
928399 meter/sec
ZDOT = 14666
047636 ZDOT = 4470
211319
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 16137
32139050
00016717 00000-0 10270-3 0 9154
2 25544 51
6402 217
0035 0001826 112
5324 247
6022 15
54601003 40027
Satellite: ISS
Catalog Number: 25544
Epoch time: 16137
32139050 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 217
0035 deg
Eccentricity:
0001826
Arg of perigee: 112
5324 deg
Mean anomaly: 247
6022 deg
Mean motion: 15
54601003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 245
Coasting Arc #17 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2016/138/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6206371
74 A = 6786332
07 meter
Y = 1950804
59 meter E =
0015681
Z = 1904784
85 I = 51
45985
XDOT = 78
515808 Wp = 113
51022
YDOT = 5245
997107 meter/sec RA = 210
93626 deg
ZDOT = -5598
097534 TA = 45
43611
MA = 45
30820
Ha = 220
774 n
mi
Hp = 213
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20362112
01 X = 6174843
33
Y = 6400277
53 feet Y = 2020032
07 meter
Z = 6249294
12 Z = 1934857
69
XDOT = 257
597795 XDOT = 47
041432
YDOT = 17211
276599 feet/sec YDOT = 5246
699192 meter/sec
ZDOT = -18366
461727 ZDOT = -5597
792519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18469861
60 X = 5629613
82
Y = 10620579
41 feet Y = 3237152
60 meter
Z = 6379681
83 Z = 1944527
02
XDOT = -2558
796283 XDOT = -779
921107
YDOT = 15541
026746 feet/sec YDOT = 4736
904952 meter/sec
ZDOT = -18366
015386 ZDOT = -5597
961490
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 16138
34990463
00016717 00000-0 10270-3 0 9161
2 25544 51
6400 211
8724 0001736 118
6080 241
5247 15
54609074 40183
Satellite: ISS
Catalog Number: 25544
Epoch time: 16138
34990463 = yrday
fracday
Element set: 916
Inclination: 51
6400 deg
RA of node: 211
8724 deg
Eccentricity:
0001736
Arg of perigee: 118
6080 deg
Mean anomaly: 241
5247 deg
Mean motion: 15
54609074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 298
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