[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 28th 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
0 221
0
000/00:00:00
000 0
0 0
0 213
5
Coasting Arc #1 (Orbit 3709)
---------------------------------------
Vector Time (GMT): 2016/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3698164
06 A = 6776937
92 meter
Y = 2139523
98 meter E =
0004130
Z = 5256982
15 I = 51
34206
XDOT = -4516
502049 Wp = 95
96249
YDOT = 6166
135039 meter/sec RA = 310
22364 deg
ZDOT = 666
842695 TA = 347
64202
MA = 347
65215
Ha = 221
123 n
mi
Hp = 213
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12133084
17 X = 3648428
03
Y = 7019435
61 feet Y = 2180601
23 meter
Z = 17247316
75 Z = 5274826
32
XDOT = -14817
920108 XDOT = -4588
356908
YDOT = 20230
101834 feet/sec YDOT = 6115
226746 meter/sec
ZDOT = 2187
804118 ZDOT = 644
727836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13873725
23 X = 4228711
45
Y = -1157432
91 feet Y = -352785
55 meter
Z = 17324382
82 Z = 5280471
88
XDOT = -606
221113 XDOT = -184
776195
YDOT = 24067
616193 feet/sec YDOT = 7335
809416 meter/sec
ZDOT = 2090
566375 ZDOT = 637
204631
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 16118
54933041
00016717 00000-0 10270-3 0 9003
2 25544 51
6402 310
6295 0001647 60
7438 299
3880 15
54314198 37103
Satellite: ISS
Catalog Number: 25544
Epoch time: 16118
54933041 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 310
6295 deg
Eccentricity:
0001647
Arg of perigee: 60
7438 deg
Mean anomaly: 299
3880 deg
Mean motion: 15
54314198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3710
Checksum: 300
Coasting Arc #2 (Orbit 3724)
---------------------------------------
Vector Time (GMT): 2016/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2497451
49 A = 6777308
64 meter
Y = -3629788
17 meter E =
0015294
Z = -5163240
22 I = 51
32340
XDOT = 5180
657897 Wp = 96
74918
YDOT = -5475
952337 meter/sec RA = 305
19879 deg
ZDOT = 1345
428250 TA = 186
24785
MA = 186
26695
Ha = 221
197 n
mi
Hp = 213
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8193738
48 X = -2431595
63
Y = -11908753
85 feet Y = -3657348
13 meter
Z = -16939764
51 Z = -5175212
37
XDOT = 16996
909112 XDOT = 5234
970748
YDOT = -17965
722891 feet/sec YDOT = -5417
715089 meter/sec
ZDOT = 4414
134677 ZDOT = 1370
726778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13544697
57 X = -4128423
82
Y = -4874108
56 feet Y = -1485628
29 meter
Z = -16991045
40 Z = -5178870
64
XDOT = 2795
085995 XDOT = 851
942211
YDOT = -23522
402200 feet/sec YDOT = -7169
628191 meter/sec
ZDOT = 4525
054474 ZDOT = 1379
236604
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 16119
51372111
00016717 00000-0 10270-3 0 9017
2 25544 51
6399 305
8192 0001662 66
5266 293
6062 15
54361559 37258
Satellite: ISS
Catalog Number: 25544
Epoch time: 16119
51372111 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 305
8192 deg
Eccentricity:
0001662
Arg of perigee: 66
5266 deg
Mean anomaly: 293
6062 deg
Mean motion: 15
54361559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3725
Checksum: 309
Coasting Arc #3 (Orbit 3740)
---------------------------------------
Vector Time (GMT): 2016/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1252508
46 A = 6780210
86 meter
Y = 4946862
05 meter E =
0010705
Z = 4457933
57 I = 51
31517
XDOT = -5480
433847 Wp = 68
53248
YDOT = 4297
349748 meter/sec RA = 300
17893 deg
ZDOT = -3218
777178 TA = 54
02783
MA = 53
92860
Ha = 221
166 n
mi
Hp = 213
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4109279
72 X = 1175443
43
Y = 16229862
35 feet Y = 4960437
57 meter
Z = 14625766
30 Z = 4463830
76
XDOT = -17980
426008 XDOT = -5512
445010
YDOT = 14098
916495 feet/sec YDOT = 4235
884875 meter/sec
ZDOT = -10560
292579 ZDOT = -3245
477757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12979550
71 X = 3956167
06
Y = 10540593
69 feet Y = 3212772
96 meter
Z = 14650419
78 Z = 4465447
95
XDOT = -5042
259738 XDOT = -1536
880768
YDOT = 21095
040049 feet/sec YDOT = 6429
768207 meter/sec
ZDOT = -10677
064522 ZDOT = -3254
369266
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 16120
54239919
00016717 00000-0 10270-3 0 9021
2 25544 51
6398 300
6895 0001610 68
8423 291
2901 15
54351778 37419
Satellite: ISS
Catalog Number: 25544
Epoch time: 16120
54239919 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 300
6895 deg
Eccentricity:
0001610
Arg of perigee: 68
8423 deg
Mean anomaly: 291
2901 deg
Mean motion: 15
54351778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3741
Checksum: 314
Coasting Arc #4 (Orbit 3755)
---------------------------------------
Vector Time (GMT): 2016/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -100035
47 A = 6784078
79 meter
Y = -5945344
73 meter E =
0006349
Z = -3270408
50 I = 51
31234
XDOT = 5422
230524 Wp = 81
62461
YDOT = -2675
760689 meter/sec RA = 295
16796 deg
ZDOT = 4707
234060 TA = 240
24901
MA = 240
31219
Ha = 221
225 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -328200
36 X = -17659
36
Y = -19505724
19 feet Y = -5946002
87 meter
Z = -10729686
68 Z = -3270694
25
XDOT = 17789
470224 XDOT = 5428
882676
YDOT = -8778
742419 feet/sec YDOT = -2615
088414 meter/sec
ZDOT = 15443
681299 ZDOT = 4733
590297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12216817
70 X = -3723686
03
Y = -15209473
96 feet Y = -4635847
66 meter
Z = -10729791
95 Z = -3270440
59
XDOT = 7423
136114 XDOT = 2262
571887
YDOT = -16918
364924 feet/sec YDOT = -5156
717629 meter/sec
ZDOT = 15558
640337 ZDOT = 4742
273575
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 16121
50678107
00016717 00000-0 10270-3 0 9035
2 25544 51
6391 295
8803 0001720 78
0914 282
0432 15
54374110 37564
Satellite: ISS
Catalog Number: 25544
Epoch time: 16121
50678107 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 295
8803 deg
Eccentricity:
0001720
Arg of perigee: 78
0914 deg
Mean anomaly: 282
0432 deg
Mean motion: 15
54374110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3756
Checksum: 293
Coasting Arc #5 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2016/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -961701
86 A = 6787341
59 meter
Y = 6500750
30 meter E =
0015107
Z = 1671328
22 I = 51
31100
XDOT = -5107
076754 Wp = 111
85891
YDOT = 713
731196 meter/sec RA = 290
16716 deg
ZDOT = -5678
941158 TA = 49
73312
MA = 49
60113
Ha = 221
100 n
mi
Hp = 213
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3155189
83 X = -1042442
05
Y = 21327920
93 feet Y = 6489544
52 meter
Z = 5483360
30 Z = 1666460
16
XDOT = -16755
501162 XDOT = -5087
092235
YDOT = 2341
637781 feet/sec YDOT = 656
732027 meter/sec
ZDOT = -18631
696712 ZDOT = -5703
701737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10942089
94 X = 3335149
01
Y = 18583619
10 feet Y = 5664287
10 meter
Z = 5460992
85 Z = 1664510
62
XDOT = -10100
917999 XDOT = -3078
759806
YDOT = 11488
900883 feet/sec YDOT = 3501
816989 meter/sec
ZDOT = -18739
350378 ZDOT = -5711
753995
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 16122
53544742
00016717 00000-0 10270-3 0 9047
2 25544 51
6393 290
7504 0001563 72
6224 287
5099 15
54409205 37728
Satellite: ISS
Catalog Number: 25544
Epoch time: 16122
53544742 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 290
7504 deg
Eccentricity:
0001563
Arg of perigee: 72
6224 deg
Mean anomaly: 287
5099 deg
Mean motion: 15
54409205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3772
Checksum: 309
Coasting Arc #6 (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 = 1839103
82 A = 6788536
77 meter
Y = -6527916
98 meter E =
0013741
Z = 83082
17 I = 51
30532
XDOT = 4593
328346 Wp = 50
98851
YDOT = 1378
639100 meter/sec RA = 285
17185 deg
ZDOT = 5985
078867 TA = 309
91076
MA = 310
03146
Ha = 221
219 n
mi
Hp = 213
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6033805
20 X = 1911560
35
Y = -21417050
45 feet Y = -6506945
76 meter
Z = 272579
29 Z = 92192
43
XDOT = 15069
974887 XDOT = 4548
497438
YDOT = 4523
094161 feet/sec YDOT = 1429
754339 meter/sec
ZDOT = 19636
085522 ZDOT = 6007
283387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9139791
55 X = -2785808
47
Y = -20286378
94 feet Y = -6183288
30 meter
Z = 313359
92 Z = 95512
10
XDOT = 12878
311218 XDOT = 3925
309259
YDOT = -5468
306220 feet/sec YDOT = -1666
739736 meter/sec
ZDOT = 19732
246465 ZDOT = 6014
388723
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
56410996
00016717 00000-0 10270-3 0 9055
2 25544 51
6399 285
6202 0001795 85
3294 274
8063 15
54400461 37889
Satellite: ISS
Catalog Number: 25544
Epoch time: 16123
56410996 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 285
6202 deg
Eccentricity:
0001795
Arg of perigee: 85
3294 deg
Mean anomaly: 274
8063 deg
Mean motion: 15
54400461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 328
Coasting Arc #7 (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 = -2597681
95 A = 6786960
65 meter
Y = 5982190
04 meter E =
0008216
Z = -1871666
62 I = 51
29205
XDOT = -3937
207016 Wp = 130
06635
YDOT = -3454
176790 meter/sec RA = 280
17616 deg
ZDOT = -5597
276351 TA = 70
63501
MA = 70
54621
Ha = 221
179 n
mi
Hp = 213
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8522578
56 X = -2655291
35
Y = 19626607
73 feet Y = 5952818
83 meter
Z = -6140638
52 Z = -1884425
89
XDOT = -12917
345853 XDOT = -3871
099392
YDOT = -11332
601017 feet/sec YDOT = -3497
835888 meter/sec
ZDOT = -18363
767557 ZDOT = -5616
241852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6462500
87 X = 1969770
27
Y = 20380797
75 feet Y = 6212067
15 meter
Z = -6197151
24 Z = -1888891
70
XDOT = -15609
132181 XDOT = -4757
663489
YDOT = -637
932116 feet/sec YDOT = -194
441709 meter/sec
ZDOT = -18445
480851 ZDOT = -5622
182563
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
52847484
00016717 00000-0 10270-3 0 9069
2 25544 51
6391 280
8110 0001821 83
8065 276
3295 15
54421329 38033
Satellite: ISS
Catalog Number: 25544
Epoch time: 16124
52847484 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 280
8110 deg
Eccentricity:
0001821
Arg of perigee: 83
8065 deg
Mean anomaly: 276
3295 deg
Mean motion: 15
54421329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3803
Checksum: 306
Coasting Arc #8 (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 = 3187292
42 A = 6783474
38 meter
Y = -4916523
65 meter E =
0014064
Z = 3406176
41 I = 51
27674
XDOT = 3206
647833 Wp = 90
57522
YDOT = 5259
286082 meter/sec RA = 275
17176 deg
ZDOT = 4574
198282 TA = 309
52948
MA = 309
65370
Ha = 221
077 n
mi
Hp = 213
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10456996
12 X = 3225487
29
Y = -16130326
93 feet Y = -4880667
52 meter
Z = 11175119
45 Z = 3421752
73
XDOT = 10520
498141 XDOT = 3125
378973
YDOT = 17254
875596 feet/sec YDOT = 5294
690739 meter/sec
ZDOT = 15007
212212 ZDOT = 4589
578041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3059963
72 X = -932676
94
Y = -18937693
76 feet Y = -5772209
06 meter
Z = 11243659
82 Z = 3427067
51
XDOT = 17907
351548 XDOT = 5458
160752
YDOT = 6087
686478 feet/sec YDOT = 1855
526839 meter/sec
ZDOT = 15073
028161 ZDOT = 4594
258983
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
55712466
00016717 00000-0 10270-3 0 9075
2 25544 51
6401 275
6807 0001682 93
0717 267
0628 15
54428363 38191
Satellite: ISS
Catalog Number: 25544
Epoch time: 16125
55712466 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 275
6807 deg
Eccentricity:
0001682
Arg of perigee: 93
0717 deg
Mean anomaly: 267
0628 deg
Mean motion: 15
54428363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3819
Checksum: 320
Coasting Arc #9 (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 = -3684044
98 A = 6779490
98 meter
Y = 3393010
68 meter E =
0011867
Z = -4580727
44 I = 51
26248
XDOT = -2385
978408 Wp = 73
06527
YDOT = -6632
205025 meter/sec RA = 270
15618 deg
ZDOT = -2996
717949 TA = 166
84328
MA = 166
81230
Ha = 221
173 n
mi
Hp = 213
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12086761
75 X = -3699460
99
Y = 11131924
80 feet Y = 3351726
92 meter
Z = -15028633
34 Z = -4598661
52
XDOT = -7828
013150 XDOT = -2297
081026
YDOT = -21759
202838 feet/sec YDOT = -6658
389646 meter/sec
ZDOT = -9831
751801 ZDOT = -3008
092587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1194952
65 X = -364221
57
Y = 16316130
97 feet Y = 4973156
72 meter
Z = -15107128
71 Z = -4604652
83
XDOT = -19318
025162 XDOT = -5888
134070
YDOT = -10553
373000 feet/sec YDOT = -3216
668090 meter/sec
ZDOT = -9879
931956 ZDOT = -3011
403260
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
52147805
00016717 00000-0 10270-3 0 9083
2 25544 51
6411 270
8716 0001789 91
0489 269
0869 15
54425934 38347
Satellite: ISS
Catalog Number: 25544
Epoch time: 16126
52147805 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 270
8716 deg
Eccentricity:
0001789
Arg of perigee: 91
0489 deg
Mean anomaly: 269
0869 deg
Mean motion: 15
54425934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3834
Checksum: 334
Coasting Arc #10 (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 = 4048966
20 A = 6776821
34 meter
Y = -1582338
41 meter E =
0005352
Z = 5194910
25 I = 51
25453
XDOT = 1509
932363 Wp = 114
46906
YDOT = 7443
629413 meter/sec RA = 265
13004 deg
ZDOT = 1087
361274 TA = 325
04422
MA = 325
07935
Ha = 220
976 n
mi
Hp = 213
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13284009
84 X = 4041124
16
Y = -5191398
97 feet Y = -1537104
01 meter
Z = 17043668
80 Z = 5214560
52
XDOT = 4953
846336 XDOT = 1421
301564
YDOT = 24421
356341 feet/sec YDOT = 7460
018919 meter/sec
ZDOT = 3567
458247 ZDOT = 1094
481023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5888259
25 X = 1794741
42
Y = -12877038
51 feet Y = -3924921
34 meter
Z = 17129286
87 Z = 5221006
64
XDOT = 19554
167728 XDOT = 5960
110323
YDOT = 13739
642583 feet/sec YDOT = 4187
843059 meter/sec
ZDOT = 3597
021538 ZDOT = 1096
372165
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
55011460
00016717 00000-0 10270-3 0 9095
2 25544 51
6411 265
7413 0001694 94
4826 265
6520 15
54445073 38501
Satellite: ISS
Catalog Number: 25544
Epoch time: 16127
55011460 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 265
7413 deg
Eccentricity:
0001694
Arg of perigee: 94
4826 deg
Mean anomaly: 265
6520 deg
Mean motion: 15
54445073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 300
Coasting Arc #11 (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 = -4317633
11 A = 6776720
67 meter
Y = -353277
70 meter E =
0016176
Z = -5225496
53 I = 51
25852
XDOT = -540
759758 Wp = 97
59204
YDOT = -7577
337163 meter/sec RA = 260
10129 deg
ZDOT = 959
551412 TA = 181
65095
MA = 181
65629
Ha = 221
132 n
mi
Hp = 213
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14165462
96 X = -4287978
01
Y = -1159047
58 feet Y = -401394
41 meter
Z = -17144017
48 Z = -5246398
94
XDOT = -1774
146188 XDOT = -460
649079
YDOT = -24860
030063 feet/sec YDOT = -7582
936396 meter/sec
ZDOT = 3148
134555 ZDOT = 957
118880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10773126
52 X = -3283648
96
Y = 9100825
23 feet Y = 2773931
53 meter
Z = -17234726
36 Z = -5253144
59
XDOT = -18158
270535 XDOT = -5534
640859
YDOT = -15553
384922 feet/sec YDOT = -4740
671724 meter/sec
ZDOT = 3138
942896 ZDOT = 956
749795
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
51445681
00016717 00000-0 10270-3 0 9100
2 25544 51
6417 260
9332 0001773 98
7596 261
3757 15
54451588 38652
Satellite: ISS
Catalog Number: 25544
Epoch time: 16128
51445681 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 260
9332 deg
Eccentricity:
0001773
Arg of perigee: 98
7596 deg
Mean anomaly: 261
3757 deg
Mean motion: 15
54451588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 336
Coasting Arc #12 (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 = 4427199
04 A = 6779292
21 meter
Y = 2227094
34 meter E =
0009746
Z = 4619391
76 I = 51
27433
XDOT = -523
076448 Wp = 71
08389
YDOT = 7082
400421 meter/sec RA = 255
07476 deg
ZDOT = -2905
099097 TA = 47
99059
MA = 47
90765
Ha = 221
069 n
mi
Hp = 213
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14524931
22 X = 4379526
64
Y = 7306739
95 feet Y = 2276335
46 meter
Z = 15155484
77 Z = 4640782
69
XDOT = -1716
130078 XDOT = -588
122763
YDOT = 23236
221855 feet/sec YDOT = 7076
187470 meter/sec
ZDOT = -9531
165015 ZDOT = -2907
797787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15288487
69 X = 4659931
05
Y = -5273697
33 feet Y = -1607422
95 meter
Z = 15247985
27 Z = 4647585
91
XDOT = 15148
723424 XDOT = 4617
330900
YDOT = 16244
183202 feet/sec YDOT = 4951
227040 meter/sec
ZDOT = -9544
161429 ZDOT = -2909
060403
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
54308144
00016717 00000-0 10270-3 0 9117
2 25544 51
6427 255
8026 0001840 101
2080 258
9279 15
54423859 38818
Satellite: ISS
Catalog Number: 25544
Epoch time: 16129
54308144 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 255
8026 deg
Eccentricity:
0001840
Arg of perigee: 101
2080 deg
Mean anomaly: 258
9279 deg
Mean motion: 15
54423859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 309
Coasting Arc #13 (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 = -4370765
52 A = 6783158
36 meter
Y = -3840717
35 meter E =
0006813
Z = -3493218
69 I = 51
29653
XDOT = 1664
010794 Wp = 95
99664
YDOT = -5976
687041 meter/sec RA = 250
06030 deg
ZDOT = 4496
087675 TA = 222
73597
MA = 222
78897
Ha = 221
092 n
mi
Hp = 213
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14339781
90 X = -4310524
03
Y = -12600778
71 feet Y = -3889257
13 meter
Z = -11460691
25 Z = -3514304
98
XDOT = 5459
352999 XDOT = 1708
879566
YDOT = -19608
553284 feet/sec YDOT = -5957
828348 meter/sec
ZDOT = 14750
943816 ZDOT = 4504
279776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18949344
86 X = -5775760
31
Y = 1799856
04 feet Y = 548596
12 meter
Z = -11551591
26 Z = -3520925
02
XDOT = -10514
493764 XDOT = -3204
817699
YDOT = -15935
393017 feet/sec YDOT = -4857
107791 meter/sec
ZDOT = 14787
595451 ZDOT = 4507
259093
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
50740769
00016717 00000-0 10270-3 0 9129
2 25544 51
6425 250
9944 0001691 99
7197 260
4147 15
54443395 38960
Satellite: ISS
Catalog Number: 25544
Epoch time: 16130
50740769 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 250
9944 deg
Eccentricity:
0001691
Arg of perigee: 99
7197 deg
Mean anomaly: 260
4147 deg
Mean motion: 15
54443395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3896
Checksum: 333
Coasting Arc #14 (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 = 4056633
84 A = 6786770
89 meter
Y = 5082077
83 meter E =
0015731
Z = 1917506
03 I = 51
31990
XDOT = -2874
707879 Wp = 112
15883
YDOT = 4411
606084 meter/sec RA = 245
05747 deg
ZDOT = -5579
699128 TA = 46
59861
MA = 46
46774
Ha = 221
068 n
mi
Hp = 213
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13309166
16 X = 3990188
77
Y = 16673483
70 feet Y = 5127070
18 meter
Z = 6291030
28 Z = 1937051
24
XDOT = -9431
456296 XDOT = -2896
721866
YDOT = 14473
773243 feet/sec YDOT = 4379
336426 meter/sec
ZDOT = -18306
099500 ZDOT = -5593
717091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21266489
28 X = 6482025
93
Y = 1345897
64 feet Y = 410229
60 meter
Z = 6375030
79 Z = 1943109
38
XDOT = 4582
748589 XDOT = 1396
821770
YDOT = 15064
544926 feet/sec YDOT = 4591
673293 meter/sec
ZDOT = -18367
775180 ZDOT = -5598
497875
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
53601675
00016717 00000-0 10270-3 0 9136
2 25544 51
6419 245
8645 0001783 108
2188 251
9159 15
54458947 39128
Satellite: ISS
Catalog Number: 25544
Epoch time: 16131
53601675 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 245
8645 deg
Eccentricity:
0001783
Arg of perigee: 108
2188 deg
Mean anomaly: 251
9159 deg
Mean motion: 15
54458947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3912
Checksum: 328
Coasting Arc #15 (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 = -3486186
58 A = 6788293
28 meter
Y = -5816742
52 meter E =
0012726
Z = -147825
06 I = 51
34071
XDOT = 4046
962770 Wp = 51
13672
YDOT = -2568
572896 meter/sec RA = 240
06340 deg
ZDOT = 5986
153897 TA = 307
26401
MA = 307
38000
Ha = 221
048 n
mi
Hp = 213
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11437620
02 X = -3420165
14
Y = -19083800
92 feet Y = -5855358
22 meter
Z = -484990
36 Z = -164600
13
XDOT = 13277
436910 XDOT = 4046
306066
YDOT = -8427
076429 feet/sec YDOT = -2523
321035 meter/sec
ZDOT = 19639
612522 ZDOT = 6005
811439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21894285
48 X = -6673378
21
Y = -3946645
74 feet Y = -1202937
62 meter
Z = -556844
58 Z = -169726
23
XDOT = 2020
790972 XDOT = 615
937088
YDOT = -13850
024372 feet/sec YDOT = -4221
487429 meter/sec
ZDOT = 19725
463311 ZDOT = 6012
321217
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
50032951
00016717 00000-0 10270-3 0 9140
2 25544 51
6431 241
0555 0001738 104
3293 255
8053 15
54480070 39278
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
50032951 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 241
0555 deg
Eccentricity:
0001738
Arg of perigee: 104
3293 deg
Mean anomaly: 255
8053 deg
Mean motion: 15
54480070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3927
Checksum: 282
Coasting Arc #16 (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 = -4712649
80 A = 6785820
98 meter
Y = -4242162
49 meter E =
0006472
Z = -2416227
62 I = 51
33310
XDOT = 1923
621456 Wp = 58
86322
YDOT = -5163
517546 meter/sec RA = 239
74630 deg
ZDOT = 5327
602474 TA = 274
00374
MA = 274
07772
Ha = 220
989 n
mi
Hp = 213
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15461449
47 X = -4653125
55
Y = -13917855
94 feet Y = -4294529
54 meter
Z = -7927255
98 Z = -2438976
28
XDOT = 6311
094015 XDOT = 1955
338866
YDOT = -16940
674364 feet/sec YDOT = -5141
829249 meter/sec
ZDOT = 17479
010740 ZDOT = 5337
023792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18279364
29 X = -5571550
24
Y = 9852070
27 feet Y = 3002911
02 meter
Z = -8025339
46 Z = -2446123
47
XDOT = -13162
311682 XDOT = -4011
872601
YDOT = -10185
608270 feet/sec YDOT = -3104
573401 meter/sec
ZDOT = 17520
847667 ZDOT = 5340
354369
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
56461605
00016717 00000-0 10270-3 0 9159
2 25544 51
6429 240
7363 0001508 101
1925 258
9398 15
54460902 39289
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
56461605 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 240
7363 deg
Eccentricity:
0001508
Arg of perigee: 101
1925 deg
Mean anomaly: 258
9398 deg
Mean motion: 15
54460902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3928
Checksum: 312
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