[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 13th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
257/20:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 216
5
265/22:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 215
0
267/18:16:53
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
7
269/19:33:04
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
4
Coasting Arc #1 (Orbit 1856)
---------------------------------------
Vector Time (GMT): 2016/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5866703
64 A = 6785495
98 meter
Y = 832030
05 meter E =
0008868
Z = 3295115
09 I = 51
53781
XDOT = -3361
816209 Wp = 62
18693
YDOT = 5037
062813 meter/sec RA = 341
85690 deg
ZDOT = 4707
932711 TA = 336
17904
MA = 336
22005
Ha = 220
709 n
mi
Hp = 216
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19247715
35 X = 5840957
50
Y = 2729757
38 feet Y = 897491
75 meter
Z = 10810745
03 Z = 3323551
28
XDOT = -11029
580737 XDOT = -3440
761030
YDOT = 16525
796630 feet/sec YDOT = 4999
027680 meter/sec
ZDOT = 15445
973462 ZDOT = 4691
409831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18520959
55 X = -5645188
47
Y = -5674726
00 feet Y = -1729656
48 meter
Z = 10934800
95 Z = 3332927
33
XDOT = 13146
231664 XDOT = 4006
971411
YDOT = -13248
512626 feet/sec YDOT = -4038
146649 meter/sec
ZDOT = 15372
827763 ZDOT = 4685
637902
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 16256
55738741
00016717 00000-0 10270-3 0 9007
2 25544 51
6450 342
1202 0006027 309
0700 50
9916 15
53826501 18578
Satellite: ISS
Catalog Number: 25544
Epoch time: 16256
55738741 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 342
1202 deg
Eccentricity:
0006027
Arg of perigee: 309
0700 deg
Mean anomaly: 50
9916 deg
Mean motion: 15
53826501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1857
Checksum: 289
Coasting Arc #2 (Orbit 1871)
---------------------------------------
Vector Time (GMT): 2016/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4879086
27 A = 6781961
07 meter
Y = -1717191
77 meter E =
0008362
Z = -4394227
43 I = 51
49440
XDOT = 4778
078626 Wp = 28
70025
YDOT = -4952
899711 meter/sec RA = 336
86587 deg
ZDOT = -3365
265198 TA = 207
12807
MA = 207
17179
Ha = 220
990 n
mi
Hp = 216
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16007500
88 X = -4838176
48
Y = -5633831
27 feet Y = -1771524
65 meter
Z = -14416756
66 Z = -4417829
09
XDOT = 15676
110979 XDOT = 4849
454970
YDOT = -16249
670967 feet/sec YDOT = -4899
069257 meter/sec
ZDOT = -11040
896319 ZDOT = -3341
880858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14982220
87 X = 4566580
92
Y = 7780717
60 feet Y = 2371562
72 meter
Z = -14519521
46 Z = -4425550
14
XDOT = -17274
916987 XDOT = -5265
394698
YDOT = 12825
472780 feet/sec YDOT = 3909
204103 meter/sec
ZDOT = -10937
805366 ZDOT = -3333
843076
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 16257
52211283
00016717 00000-0 10270-3 0 9013
2 25544 51
6439 337
3148 0006070 312
5490 47
5149 15
53812095 18723
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
52211283 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 337
3148 deg
Eccentricity:
0006070
Arg of perigee: 312
5490 deg
Mean anomaly: 47
5149 deg
Mean motion: 15
53812095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1872
Checksum: 300
Coasting Arc #3 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2016/257/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3416553
80 A = 6779004
03 meter
Y = 2885288
90 meter E =
0001797
Z = 5094612
49 I = 51
47283
XDOT = -6120
899468 Wp = 351
12874
YDOT = 4307
908801 meter/sec RA = 335
07541 deg
ZDOT = 1666
875689 TA = 82
74891
MA = 82
72849
Ha = 221
081 n
mi
Hp = 216
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11209166
02 X = 3359288
62
Y = 9466170
93 feet Y = 2923175
41 meter
Z = 16714607
91 Z = 5111069
74
XDOT = -20081
691167 XDOT = -6176
713578
YDOT = 14133
559058 feet/sec YDOT = 4239
148892 meter/sec
ZDOT = 5468
752262 ZDOT = 1637
006151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2421472
53 X = -738064
83
Y = 14387512
53 feet Y = 4385313
82 meter
Z = 16785942
53 Z = 5116355
28
XDOT = -21410
659179 XDOT = -6525
968918
YDOT = -9823
791393 feet/sec YDOT = -2994
291617 meter/sec
ZDOT = 5337
461627 ZDOT = 1626
858304
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 16257
90799991
00016717 00000-0 10270-3 0 9023
2 25544 51
6424 335
3938 0006367 317
0791 42
9864 15
53859672 18786
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
90799991 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 335
3938 deg
Eccentricity:
0006367
Arg of perigee: 317
0791 deg
Mean anomaly: 42
9864 deg
Mean motion: 15
53859672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 363
Coasting Arc #4 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2016/258/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1973707
93 A = 6778211
33 meter
Y = -3742741
36 meter E =
0011812
Z = -5304637
13 I = 51
44151
XDOT = 6692
947144 Wp = 66
65404
YDOT = -3723
501038 meter/sec RA = 330
06623 deg
ZDOT = 141
731990 TA = 204
67347
MA = 204
73002
Ha = 221
320 n
mi
Hp = 216
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6475419
72 X = -1905941
51
Y = -12279335
16 feet Y = -3764434
42 meter
Z = -17403665
12 Z = -5314059
79
XDOT = 21958
488006 XDOT = 6733
398379
YDOT = -12216
210754 feet/sec YDOT = -3648
429823 meter/sec
ZDOT = 464
999966 ZDOT = 174
343088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7065429
74 X = 2153542
99
Y = -11890471
35 feet Y = -3624215
67 meter
Z = -17444113
22 Z = -5316965
71
XDOT = 21104
339262 XDOT = 6432
602607
YDOT = 11671
441632 feet/sec YDOT = 3557
455409 meter/sec
ZDOT = 608
140267 ZDOT = 185
361154
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 16258
87271414
00016717 00000-0 10270-3 0 9036
2 25544 51
6428 330
5868 0006366 321
4048 38
6649 15
53837694 18932
Satellite: ISS
Catalog Number: 25544
Epoch time: 16258
87271414 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 330
5868 deg
Eccentricity:
0006366
Arg of perigee: 321
4048 deg
Mean anomaly: 38
6649 deg
Mean motion: 15
53837694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 342
Coasting Arc #5 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2016/259/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 474097
29 A = 6779491
95 meter
Y = 4544458
29 meter E =
0008697
Z = 5009913
59 I = 51
41847
XDOT = -6833
702532 Wp = 8
49540
YDOT = 2874
964895 meter/sec RA = 325
05648 deg
ZDOT = -1952
302408 TA = 100
56502
MA = 100
46704
Ha = 221
535 n
mi
Hp = 216
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1555437
32 X = 398908
90
Y = 14909640
04 feet Y = 4549340
24 meter
Z = 16436724
37 Z = 5012033
37
XDOT = -22420
283896 XDOT = -6855
859832
YDOT = 9432
299523 feet/sec YDOT = 2798
421694 meter/sec
ZDOT = -6405
191626 ZDOT = -1985
552848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11736147
02 X = -3577177
61
Y = 9311454
12 feet Y = 2838131
22 meter
Z = 16445131
04 Z = 5012475
94
XDOT = -19390
147729 XDOT = -5910
117028
YDOT = -12818
182826 feet/sec YDOT = -3906
982125 meter/sec
ZDOT = -6550
949811 ZDOT = -1996
729502
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 16259
90173302
00016717 00000-0 10270-3 0 9049
2 25544 51
6429 325
4603 0006408 326
2995 33
7750 15
53848388 19093
Satellite: ISS
Catalog Number: 25544
Epoch time: 16259
90173302 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 325
4603 deg
Eccentricity:
0006408
Arg of perigee: 326
2995 deg
Mean anomaly: 33
7750 deg
Mean motion: 15
53848388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1909
Checksum: 326
Coasting Arc #6 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2016/260/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 912244
17 A = 6782441
22 meter
Y = -5199913
23 meter E =
0005229
Z = -4260022
47 I = 51
40170
XDOT = 6548
520215 Wp = 57
97904
YDOT = -1769
589807 meter/sec RA = 320
05019 deg
ZDOT = 3568
261412 TA = 248
55419
MA = 248
60997
Ha = 221
643 n
mi
Hp = 215
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2992927
07 X = 991016
45
Y = -17060082
76 feet Y = -5189272
08 meter
Z = -13976451
66 Z = -4255398
93
XDOT = 21484
646376 XDOT = 6550
488462
YDOT = -5805
740837 feet/sec YDOT = -1696
348336 meter/sec
ZDOT = 11706
894395 ZDOT = 3600
077476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15885215
76 X = 4841813
76
Y = -6946576
54 feet Y = -2117316
53 meter
Z = -13955294
06 Z = -4253573
63
XDOT = 16242
621403 XDOT = 4950
751004
YDOT = 13384
035506 feet/sec YDOT = 4079
454022 meter/sec
ZDOT = 11846
168366 ZDOT = 3610
712118
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 16260
86643087
00016717 00000-0 10270-3 0 9059
2 25544 51
6420 320
6538 0006443 329
7871 30
2909 15
53859611 19244
Satellite: ISS
Catalog Number: 25544
Epoch time: 16260
86643087 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 320
6538 deg
Eccentricity:
0006443
Arg of perigee: 329
7871 deg
Mean anomaly: 30
2909 deg
Mean motion: 15
53859611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 317
Coasting Arc #7 (Orbit 1939)
---------------------------------------
Vector Time (GMT): 2016/261/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2162233
11 A = 6786047
66 meter
Y = 5641486
81 meter E =
0010989
Z = 3086929
08 I = 51
39032
XDOT = -5909
076747 Wp = 65
54591
YDOT = 407
845706 meter/sec RA = 315
05102 deg
ZDOT = -4866
194962 TA = 78
84407
MA = 78
72055
Ha = 221
763 n
mi
Hp = 215
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7093940
64 X = -2240151
97
Y = 18508814
98 feet Y = 5616872
04 meter
Z = 10127720
08 Z = 3076235
38
XDOT = -19386
734734 XDOT = -5889
560239
YDOT = 1338
076464 feet/sec YDOT = 341
874862 meter/sec
ZDOT = -15965
206568 ZDOT = -4894
852531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19281123
44 X = -5876886
43
Y = 4701401
91 feet Y = 1432987
30 meter
Z = 10079982
07 Z = 3072378
54
XDOT = -11772
773471 XDOT = -3588
341354
YDOT = -13655
010779 feet/sec YDOT = -4162
047286 meter/sec
ZDOT = -16090
424737 ZDOT = -4904
361460
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 16261
89543452
00016717 00000-0 10270-3 0 9069
2 25544 51
6425 315
5268 0006503 333
2555 26
8261 15
53882281 19407
Satellite: ISS
Catalog Number: 25544
Epoch time: 16261
89543452 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 315
5268 deg
Eccentricity:
0006503
Arg of perigee: 333
2555 deg
Mean anomaly: 26
8261 deg
Mean motion: 15
53882281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1940
Checksum: 310
Coasting Arc #8 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2016/262/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3144255
05 A = 6788932
94 meter
Y = -5779409
31 meter E =
0012511
Z = -1643265
31 I = 51
37767
XDOT = 5013
041445 Wp = 10
37453
YDOT = 1112
369027 meter/sec RA = 310
05827 deg
ZDOT = 5698
658285 TA = 331
55688
MA = 331
62510
Ha = 221
907 n
mi
Hp = 215
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10315797
40 X = 3216630
52
Y = -18961316
65 feet Y = -5743843
69 meter
Z = -5391290
39 Z = -1627814
61
XDOT = 16446
986368 XDOT = 4972
548222
YDOT = 3649
504682 feet/sec YDOT = 1168
202579 meter/sec
ZDOT = 18696
385448 ZDOT = 5722
912068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21432161
96 X = 6532522
97
Y = -2709950
21 feet Y = -825992
82 meter
Z = -5322764
37 Z = -1622378
58
XDOT = 6400
214603 XDOT = 1950
785411
YDOT = 13810
081015 feet/sec YDOT = 4209
312693 meter/sec
ZDOT = 18802
087573 ZDOT = 5730
876292
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 16262
86011801
00016717 00000-0 10270-3 0 9076
2 25544 51
6423 310
7195 0006556 337
2951 22
7911 15
53880544 19556
Satellite: ISS
Catalog Number: 25544
Epoch time: 16262
86011801 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 310
7195 deg
Eccentricity:
0006556
Arg of perigee: 337
2951 deg
Mean anomaly: 22
7911 deg
Mean motion: 15
53880544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 306
Coasting Arc #9 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2016/263/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3891520
93 A = 6790022
38 meter
Y = 5562290
40 meter E =
0006932
Z = 13706
15 I = 51
36185
XDOT = -3930
650464 Wp = 109
19194
YDOT = -2729
116904 meter/sec RA = 305
07010 deg
ZDOT = -5986
050133 TA = 70
65996
MA = 70
58501
Ha = 222
015 n
mi
Hp = 215
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12767457
11 X = -3953497
22
Y = 18248984
25 feet Y = 5518426
27 meter
Z = 44967
68 Z = -5349
27
XDOT = -12895
834855 XDOT = -3870
762691
YDOT = -8953
795617 feet/sec YDOT = -2772
737930 meter/sec
ZDOT = -19639
272090 ZDOT = -6004
998660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22260300
78 X = -6784939
68
Y = 716154
97 feet Y = 218284
03 meter
Z = -39250
06 Z = -11963
42
XDOT = -430
966932 XDOT = -131
358721
YDOT = -13965
292143 feet/sec YDOT = -4256
621045 meter/sec
ZDOT = -19721
511178 ZDOT = -6011
116607
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 16263
88910723
00016717 00000-0 10270-3 0 9081
2 25544 51
6427 305
5919 0006505 341
4898 18
6017 15
53888381 19713
Satellite: ISS
Catalog Number: 25544
Epoch time: 16263
88910723 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 305
5919 deg
Eccentricity:
0006505
Arg of perigee: 341
4898 deg
Mean anomaly: 18
6017 deg
Mean motion: 15
53888381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 338
Coasting Arc #10 (Orbit 1986)
---------------------------------------
Vector Time (GMT): 2016/264/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4342710
56 A = 6788895
28 meter
Y = -4954958
68 meter E =
0016561
Z = 1592960
43 I = 51
34026
XDOT = 2795
374621 Wp = 40
14885
YDOT = 4293
503687 meter/sec RA = 300
08025 deg
ZDOT = 5713
592765 TA = 337
36572
MA = 337
43867
Ha = 222
066 n
mi
Hp = 215
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14247738
04 X = 4390057
40
Y = -16256426
13 feet Y = -4906130
69 meter
Z = 5226248
13 Z = 1614171
95
XDOT = 9171
176578 XDOT = 2719
401338
YDOT = 14086
298187 feet/sec YDOT = 4324
339217 meter/sec
ZDOT = 18745
383087 ZDOT = 5726
987181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21556487
61 X = 6570417
42
Y = 1265331
60 feet Y = 385673
07 meter
Z = 5319762
91 Z = 1621463
73
XDOT = -5491
136922 XDOT = -1673
698534
YDOT = 14213
927507 feet/sec YDOT = 4332
405104 meter/sec
ZDOT = 18803
088373 ZDOT = 5731
181336
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 16264
91809038
00016717 00000-0 10270-3 0 9093
2 25544 51
6425 300
4642 0006592 345
1897 14
9062 15
53896324 19876
Satellite: ISS
Catalog Number: 25544
Epoch time: 16264
91809038 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 300
4642 deg
Eccentricity:
0006592
Arg of perigee: 345
1897 deg
Mean anomaly: 14
9062 deg
Mean motion: 15
53896324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1987
Checksum: 333
Coasting Arc #11 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2016/265/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4573715
99 A = 6785861
07 meter
Y = 3967683
39 meter E =
0006014
Z = -3072715
22 I = 51
31645
XDOT = -1650
040048 Wp = 29
00786
YDOT = -5675
739171 meter/sec RA = 295
08410 deg
ZDOT = -4871
658737 TA = 186
42351
MA = 186
43122
Ha = 222
191 n
mi
Hp = 214
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15005629
89 X = -4602817
64
Y = 13017333
95 feet Y = 3916374
06 meter
Z = -10081086
68 Z = -3095004
40
XDOT = -5413
517218 XDOT = -1562
785217
YDOT = -18621
191505 feet/sec YDOT = -5693
703560 meter/sec
ZDOT = -15983
132340 ZDOT = -4879
461884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19505201
90 X = -5945185
54
Y = -3490095
35 feet Y = -1063781
06 meter
Z = -10179123
43 Z = -3102596
82
XDOT = 10933
872331 XDOT = 3332
644286
YDOT = -14383
281319 feet/sec YDOT = -4384
024146 meter/sec
ZDOT = -16016
180084 ZDOT = -4881
731689
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 16265
88275356
00016717 00000-0 10270-3 0 9102
2 25544 51
6438 295
6574 0006603 347
7142 12
3849 15
53919262 20024
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
88275356 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 295
6574 deg
Eccentricity:
0006603
Arg of perigee: 347
7142 deg
Mean anomaly: 12
3849 deg
Mean motion: 15
53919262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 320
Coasting Arc #12 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2016/265/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2871161
72 A = 6778930
41 meter
Y = -3480659
95 meter E =
0011996
Z = -5068212
19 I = 51
29213
XDOT = 4322
273022 Wp = 72
86536
YDOT = -6081
962458 meter/sec RA = 294
65974 deg
ZDOT = 1735
163335 TA = 213
97013
MA = 214
04699
Ha = 222
122 n
mi
Hp = 214
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9419821
93 X = -2807407
29
Y = -11419488
01 feet Y = -3512411
15 meter
Z = -16627992
73 Z = -5082004
55
XDOT = 14180
685767 XDOT = 4381
533079
YDOT = -19953
945073 feet/sec YDOT = -6033
296418 meter/sec
ZDOT = 5692
793095 ZDOT = 1756
304480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4014690
21 X = -1223677
58
Y = -14178666
39 feet Y = -4321657
52 meter
Z = -16687587
48 Z = -5086376
66
XDOT = 19866
960196 XDOT = 6055
449468
YDOT = -12408
920969 feet/sec YDOT = -3782
239111 meter/sec
ZDOT = 5786
197704 ZDOT = 1763
633060
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 16265
94706320
00016717 00000-0 10270-3 0 9110
2 25544 51
6437 295
3370 0006686 347
6125 12
4862 15
53938482 20037
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
94706320 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 295
3370 deg
Eccentricity:
0006686
Arg of perigee: 347
6125 deg
Mean anomaly: 12
4862 deg
Mean motion: 15
53938482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 311
Coasting Arc #13 (Orbit 2018)
---------------------------------------
Vector Time (GMT): 2016/266/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1968925
99 A = 6781744
35 meter
Y = 4825948
12 meter E =
0012695
Z = 4337819
20 I = 51
28901
XDOT = -4696
237818 Wp = 39
25223
YDOT = 5003
646287 meter/sec RA = 289
64279 deg
ZDOT = -3419
916519 TA = 85
68359
MA = 85
53853
Ha = 222
244 n
mi
Hp = 214
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6459730
94 X = 1893743
29
Y = 15833163
13 feet Y = 4847545
92 meter
Z = 14231690
30 Z = 4347200
84
XDOT = -15407
604390 XDOT = -4735
228248
YDOT = 16416
162360 feet/sec YDOT = 4950
911545 meter/sec
ZDOT = -11220
198553 ZDOT = -3442
824876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -146039
75 X = -44512
92
Y = 17066130
82 feet Y = 5201756
67 meter
Z = 14271791
72 Z = 4350042
12
XDOT = -19187
947675 XDOT = -5848
486451
YDOT = 9344
758163 feet/sec YDOT = 2848
282288 meter/sec
ZDOT = -11321
119638 ZDOT = -3450
677266
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 16266
97602948
00016717 00000-0 10270-3 0 9126
2 25544 51
6434 290
2091 0006836 351
3302 8
7731 15
53978595 20193
Satellite: ISS
Catalog Number: 25544
Epoch time: 16266
97602948 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 290
2091 deg
Eccentricity:
0006836
Arg of perigee: 351
3302 deg
Mean anomaly: 8
7731 deg
Mean motion: 15
53978595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2019
Checksum: 323
Coasting Arc #14 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2016/267/18:16:53
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4368912
25 A = 6778280
77 meter
Y = -219794
62 meter E =
0005101
Z = 5174654
27 I = 51
26748
XDOT = -1066
224145 Wp = 31
85288
YDOT = 7497
728753 meter/sec RA = 285
53216 deg
ZDOT = 1222
378639 TA = 46
38143
MA = 46
33913
Ha = 222
172 n
mi
Hp = 214
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14333701
61 X = 4345909
02
Y = -721110
97 feet Y = -171066
75 meter
Z = 16977212
16 Z = 5195821
56
XDOT = -3498
110711 XDOT = -1155
924218
YDOT = 24598
847614 feet/sec YDOT = 7485
304068 meter/sec
ZDOT = 4010
428605 ZDOT = 1216
980742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2298091
88 X = 700458
41
Y = 14055091
79 feet Y = 4283991
98 meter
Z = 17069677
92 Z = 5202837
83
XDOT = -23813
662380 XDOT = -7258
404293
YDOT = -931
989644 feet/sec YDOT = -284
070444 meter/sec
ZDOT = 3985
529650 ZDOT = 1214
789437
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 16267
81206236
00016717 00000-0 10270-3 0 9131
2 25544 51
6418 286
0429 0006635 354
5560 5
5519 15
53973708 20326
Satellite: ISS
Catalog Number: 25544
Epoch time: 16267
81206236 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 286
0429 deg
Eccentricity:
0006635
Arg of perigee: 354
5560 deg
Mean anomaly: 5
5519 deg
Mean motion: 15
53973708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 311
Coasting Arc #15 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2016/268/18:16:53
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4022545
93 A = 6778006
58 meter
Y = -1473773
98 meter E =
0015476
Z = -5264561
13 I = 51
25925
XDOT = 1888
666684 Wp = 69
38392
YDOT = -7394
378460 meter/sec RA = 280
50777 deg
ZDOT = 633
774873 TA = 206
66699
MA = 206
74666
Ha = 222
448 n
mi
Hp = 214
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13197329
16 X = -3980193
88
Y = -4835216
47 feet Y = -1518520
42 meter
Z = -17272182
17 Z = -5283998
65
XDOT = 6196
413004 XDOT = 1968
133530
YDOT = -24259
771852 feet/sec YDOT = -7372
813745 meter/sec
ZDOT = 2079
313889 ZDOT = 643
143166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3116981
02 X = 950055
81
Y = -13597904
37 feet Y = -4144641
25 meter
Z = -17356800
35 Z = -5290352
75
XDOT = 23860
982725 XDOT = 7272
827535
YDOT = 2790
181560 feet/sec YDOT = 850
447340 meter/sec
ZDOT = 2121
517177 ZDOT = 646
638436
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 16268
77670972
00016717 00000-0 10270-3 0 9140
2 25544 51
6424 281
2353 0006701 359
0920 1
0219 15
53951891 20473
Satellite: ISS
Catalog Number: 25544
Epoch time: 16268
77670972 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 281
2353 deg
Eccentricity:
0006701
Arg of perigee: 359
0920 deg
Mean anomaly: 1
0219 deg
Mean motion: 15
53951891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 307
Coasting Arc #16 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2016/269/18:16:53
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3583626
24 A = 6779839
17 meter
Y = 3141603
10 meter E =
0012205
Z = 4820645
02 I = 51
26036
XDOT = -2625
895848 Wp = 32
15428
YDOT = 6775
762255 meter/sec RA = 275
48572 deg
ZDOT = -2450
645826 TA = 82
10028
MA = 81
96177
Ha = 222
529 n
mi
Hp = 214
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11757303
95 X = 3524813
12
Y = 10307096
77 feet Y = 3181349
22 meter
Z = 15815764
52 Z = 4837910
20
XDOT = -8615
143859 XDOT = -2689
564825
YDOT = 22230
191124 feet/sec YDOT = 6746
041497 meter/sec
ZDOT = -8040
176593 ZDOT = -2463
557035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8504229
54 X = -2592089
17
Y = 13029785
54 feet Y = 3971478
63 meter
Z = 15890614
08 Z = 4843459
17
XDOT = -22288
196759 XDOT = -6793
442372
YDOT = -4619
396292 feet/sec YDOT = -1407
991990 meter/sec
ZDOT = -8097
728074 ZDOT = -2468
187517
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 16269
80565726
00016717 00000-0 10270-3 0 9156
2 25544 51
6422 276
1082 0006788 3
2684 356
8512 15
53969626 20633
Satellite: ISS
Catalog Number: 25544
Epoch time: 16269
80565726 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 276
1082 deg
Eccentricity:
0006788
Arg of perigee: 3
2684 deg
Mean anomaly: 356
8512 deg
Mean motion: 15
53969626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 333
Coasting Arc #17 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2016/269/19:33:04
000
Vector Time (MET): N/A
Weight (LBS) : 908286
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3643964
90 A = 6782736
56 meter
Y = -4012153
70 meter E =
0011573
Z = 4065480
31 I = 51
27103
XDOT = 2512
216591 Wp = 67
74620
YDOT = 6161
235901 meter/sec RA = 275
26481 deg
ZDOT = 3824
235941 TA = 342
53419
MA = 342
57396
Ha = 222
512 n
mi
Hp = 214
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11955265
41 X = 3668810
68
Y = -13163233
91 feet Y = -3971265
12 meter
Z = 13338189
98 Z = 4083242
47
XDOT = 8242
180416 XDOT = 2424
556916
YDOT = 20214
028547 feet/sec YDOT = 6188
839426 meter/sec
ZDOT = 12546
705842 ZDOT = 3836
226125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17152042
10 X = 5227942
43
Y = 4462379
67 feet Y = 1360133
32 meter
Z = 13416446
24 Z = 4089332
81
XDOT = -13849
265904 XDOT = -4221
256247
YDOT = 15312
149138 feet/sec YDOT = 4667
143057 meter/sec
ZDOT = 12597
999527 ZDOT = 3839
870256
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 16269
86996643
00016717 00000-0 10270-3 0 9169
2 25544 51
6434 275
7874 0006768 3
7290 356
3912 15
53952435 20646
Satellite: ISS
Catalog Number: 25544
Epoch time: 16269
86996643 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 275
7874 deg
Eccentricity:
0006768
Arg of perigee: 3
7290 deg
Mean anomaly: 356
3912 deg
Mean motion: 15
53952435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 349
Coasting Arc #18 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2016/270/19:33:04
000
Vector Time (MET): N/A
Weight (LBS) : 908286
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3958843
51 A = 6779389
76 meter
Y = 2493888
14 meter E =
0016178
Z = -4920390
04 I = 51
25743
XDOT = -1738
889456 Wp = 50
94919
YDOT = -7122
207209 meter/sec RA = 270
24870 deg
ZDOT = -2205
696062 TA = 197
34608
MA = 197
40141
Ha = 222
643 n
mi
Hp = 214
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12988331
72 X = -3962535
49
Y = 8182047
72 feet Y = 2449596
51 meter
Z = -16143011
93 Z = -4939630
31
XDOT = -5705
017900 XDOT = -1648
403586
YDOT = -23366
821553 feet/sec YDOT = -7141
146948 meter/sec
ZDOT = -7236
535637 ZDOT = -2213
922554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13329599
81 X = -4062862
02
Y = -7431751
19 feet Y = -2265197
76 meter
Z = -16227456
45 Z = -4946128
73
XDOT = 17309
580926 XDOT = 5275
960266
YDOT = -15133
128973 feet/sec YDOT = -4612
577711 meter/sec
ZDOT = -7271
246412 ZDOT = -2216
275906
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 16270
83459717
00016717 00000-0 10270-3 0 9175
2 25544 51
6427 270
9809 0006792 6
3624 353
7613 15
53991539 20793
Satellite: ISS
Catalog Number: 25544
Epoch time: 16270
83459717 = yrday
fracday
Element set: 917
Inclination: 51
6427 deg
RA of node: 270
9809 deg
Eccentricity:
0006792
Arg of perigee: 6
3624 deg
Mean anomaly: 353
7613 deg
Mean motion: 15
53991539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2079
Checksum: 342
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