[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 1st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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
185/03:48:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 213
6
187/04:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
6
189/01:36:41
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 213
5
191/04:12:02
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
4
194/19:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
2
198/02:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2016/183/11:39:38
283
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3886092
86 A = 6778167
28 meter
Y = 2908234
58 meter E =
0007421
Z = 4726333
60 I = 51
54299
XDOT = -6120
393043 Wp = 110
83629
YDOT = 3738
305294 meter/sec RA = 346
15423 deg
ZDOT = 2725
995198 TA = 312
14929
MA = 312
21232
Ha = 220
135 n
mi
Hp = 213
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12749648
49 X = 3830324
91
Y = 9541452
05 feet Y = 2951379
02 meter
Z = 15506343
84 Z = 4745076
22
XDOT = -20080
029668 XDOT = -6174
982556
YDOT = 12264
781147 feet/sec YDOT = 3669
557393 meter/sec
ZDOT = 8943
553798 ZDOT = 2696
131722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8633792
39 X = 2631579
92
Y = -13286482
71 feet Y = -4049719
93 meter
Z = 15587384
30 Z = 4751034
73
XDOT = 12676
656166 XDOT = 3863
844799
YDOT = 18599
467221 feet/sec YDOT = 5669
117609 meter/sec
ZDOT = 8812
652659 ZDOT = 2686
096530
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 16183
53882387
00016717 00000-0 10270-3 0 9000
2 25544 51
6392 346
4358 0000900 11
0182 349
0990 15
54668487 7211
Satellite: ISS
Catalog Number: 25544
Epoch time: 16183
53882387 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 346
4358 deg
Eccentricity:
0000900
Arg of perigee: 11
0182 deg
Mean anomaly: 349
0990 deg
Mean motion: 15
54668487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 315
Coasting Arc #2 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2016/184/11:39:38
283
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2074810
52 A = 6775867
26 meter
Y = -3726846
49 meter E =
0015182
Z = -5278029
65 I = 51
50617
XDOT = 7029
563308 Wp = 81
71749
YDOT = -2963
869337 meter/sec RA = 341
14360 deg
ZDOT = -670
052954 TA = 181
86122
MA = 181
86687
Ha = 220
296 n
mi
Hp = 213
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6807121
14 X = -2007343
46
Y = -12227186
65 feet Y = -3749670
41 meter
Z = -17316370
25 Z = -5287945
21
XDOT = 23062
871746 XDOT = 7065
438409
YDOT = -9723
980764 feet/sec YDOT = -2885
059391 meter/sec
ZDOT = -2198
336462 ZDOT = -635
818463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11598659
99 X = -3535271
56
Y = 7735730
50 feet Y = 2357850
66 meter
Z = -17358779
63 Z = -5290956
03
XDOT = -11134
617628 XDOT = -3393
831453
YDOT = -21295
305174 feet/sec YDOT = -6490
809017 meter/sec
ZDOT = -2048
558290 ZDOT = -624
400567
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 16184
50301719
00016717 00000-0 10270-3 0 9014
2 25544 51
6411 341
6258 0000928 26
5403 333
5797 15
54684915 7369
Satellite: ISS
Catalog Number: 25544
Epoch time: 16184
50301719 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 341
6258 deg
Eccentricity:
0000928
Arg of perigee: 26
5403 deg
Mean anomaly: 333
5797 deg
Mean motion: 15
54684915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 307
Coasting Arc #3 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2016/185/03:48:30
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3479042
38 A = 6776778
34 meter
Y = 2906032
75 meter E =
0005181
Z = 5033814
42 I = 51
49121
XDOT = -6181
146689 Wp = 111
32729
YDOT = 4138
432881 meter/sec RA = 337
79452 deg
ZDOT = 1879
468661 TA = 320
41070
MA = 320
44852
Ha = 220
132 n
mi
Hp = 213
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11414181
04 X = 3421835
86
Y = 9534228
17 feet Y = 2944617
11 meter
Z = 16515139
19 Z = 5050576
13
XDOT = -20279
352655 XDOT = -6236
093888
YDOT = 13577
535699 feet/sec YDOT = 4069
003675 meter/sec
ZDOT = 6166
235765 ZDOT = 1849
309510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6884295
73 X = 2098333
34
Y = 13091772
59 feet Y = 3990372
29 meter
Z = 16587550
17 Z = 5055885
29
XDOT = -22981
397046 XDOT = -7004
729820
YDOT = 4425
481232 feet/sec YDOT = 1348
886679 meter/sec
ZDOT = 6033
965320 ZDOT = 1839
152629
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 16185
21008808
00016717 00000-0 10270-3 0 9027
2 25544 51
6431 338
1019 0001230 12
9684 347
1500 15
54708184 7474
Satellite: ISS
Catalog Number: 25544
Epoch time: 16185
21008808 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 338
1019 deg
Eccentricity:
0001230
Arg of perigee: 12
9684 deg
Mean anomaly: 347
1500 deg
Mean motion: 15
54708184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 285
Coasting Arc #4 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2016/186/03:48:30
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1686139
94 A = 6775728
02 meter
Y = -3883562
23 meter E =
0015302
Z = -5303333
46 I = 51
45856
XDOT = 6893
754321 Wp = 86
91229
YDOT = -3326
358698 meter/sec RA = 332
77795 deg
ZDOT = 245
472139 TA = 185
42808
MA = 185
44469
Ha = 220
322 n
mi
Hp = 213
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5531955
17 X = -1616826
61
Y = -12741345
89 feet Y = -3902029
44 meter
Z = -17399387
98 Z = -5311356
44
XDOT = 22617
304202 XDOT = 6929
245758
YDOT = -10913
250321 feet/sec YDOT = -3249
069735 meter/sec
ZDOT = 805
354787 ZDOT = 279
045651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -460299
89 X = -140299
41
Y = -13839924
28 feet Y = -4218408
92 meter
Z = -17433523
61 Z = -5313738
00
XDOT = 24016
328168 XDOT = 7320
176825
YDOT = -1992
497468 feet/sec YDOT = -607
313228 meter/sec
ZDOT = 952
325962 ZDOT = 290
268953
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 16186
17427503
00016717 00000-0 10270-3 0 9031
2 25544 51
6437 333
2917 0001372 19
5085 340
6120 15
54697527 7629
Satellite: ISS
Catalog Number: 25544
Epoch time: 16186
17427503 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 333
2917 deg
Eccentricity:
0001372
Arg of perigee: 19
5085 deg
Mean anomaly: 340
6120 deg
Mean motion: 15
54697527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 304
Coasting Arc #5 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2016/187/03:48:30
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -169623
96 A = 6777519
56 meter
Y = 4701787
86 meter E =
0007931
Z = 4874827
82 I = 51
43651
XDOT = -6970
084977 Wp = 51
93648
YDOT = 2186
504500 meter/sec RA = 327
76126 deg
ZDOT = -2344
021024 TA = 61
10452
MA = 61
02498
Ha = 220
265 n
mi
Hp = 213
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -556509
05 X = -245867
40
Y = 15425813
19 feet Y = 4699464
05 meter
Z = 15993529
59 Z = 4873819
30
XDOT = -22867
732864 XDOT = -6982
630911
YDOT = 7173
571195 feet/sec YDOT = 2108
490536 meter/sec
ZDOT = -7690
357690 ZDOT = -2377
909648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5933578
15 X = -1808554
62
Y = 14255878
19 feet Y = 4345191
67 meter
Z = 15988151
59 Z = 4873188
61
XDOT = -22852
396050 XDOT = -6965
410316
YDOT = -693
447854 feet/sec YDOT = -211
362906 meter/sec
ZDOT = -7838
458553 ZDOT = -2389
162167
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 16187
20273561
00016717 00000-0 10270-3 0 9040
2 25544 51
6437 328
1615 0001371 15
7763 344
3433 15
54719698 7786
Satellite: ISS
Catalog Number: 25544
Epoch time: 16187
20273561 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 328
1615 deg
Eccentricity:
0001371
Arg of perigee: 15
7763 deg
Mean anomaly: 344
3433 deg
Mean motion: 15
54719698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 320
Coasting Arc #6 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2016/187/04:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6156109
81 A = 6785622
33 meter
Y = 1819032
98 meter E =
0005493
Z = -2197307
17 I = 51
46375
XDOT = 357
557959 Wp = 125
76298
YDOT = -5368
880262 meter/sec RA = 327
71749 deg
ZDOT = -5459
112245 TA = 78
69469
MA = 78
63297
Ha = 220
267 n
mi
Hp = 213
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20197210
65 X = -6165319
74
Y = 5967955
96 feet Y = 1750140
06 meter
Z = -7209013
04 Z = -2227233
71
XDOT = 1173
090416 XDOT = 444
085185
YDOT = -17614
436555 feet/sec YDOT = -5364
397266 meter/sec
ZDOT = -17910
473245 ZDOT = -5457
165912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20999239
79 X = -6400568
29
Y = 820556
11 feet Y = 250105
50 meter
Z = -7339775
29 Z = -2237163
51
XDOT = 5647
541267 XDOT = 1721
370578
YDOT = -15224
784065 feet/sec YDOT = -4640
514183 meter/sec
ZDOT = -17900
869833 ZDOT = -5456
185125
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 16187
20273626
00016717 00000-0 10270-3 0 9053
2 25544 51
6445 328
1615 0001182 14
5925 345
5267 15
54672215 7783
Satellite: ISS
Catalog Number: 25544
Epoch time: 16187
20273626 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 328
1615 deg
Eccentricity:
0001182
Arg of perigee: 14
5925 deg
Mean anomaly: 345
5267 deg
Mean motion: 15
54672215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 310
Coasting Arc #7 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2016/188/04:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5623268
10 A = 6781619
60 meter
Y = -528474
47 meter E =
0011974
Z = 3743221
61 I = 51
42439
XDOT = -2269
035383 Wp = 89
72828
YDOT = 5978
461156 meter/sec RA = 322
72010 deg
ZDOT = 4241
013840 TA = 315
23334
MA = 315
32991
Ha = 220
243 n
mi
Hp = 213
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18449042
33 X = 5610577
06
Y = -1733840
11 feet Y = -465662
74 meter
Z = 12280910
80 Z = 3770506
70
XDOT = -7444
341809 XDOT = -2356
320070
YDOT = 19614
373870 feet/sec YDOT = 5952
598747 meter/sec
ZDOT = 13914
087402 ZDOT = 4229
780329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18276515
02 X = 5570681
78
Y = 2530964
85 feet Y = 771438
09 meter
Z = 12399893
16 Z = 3779487
43
XDOT = -11651
671962 XDOT = -3551
429614
YDOT = 16029
266580 feet/sec YDOT = 4885
720453 meter/sec
ZDOT = 13863
905597 ZDOT = 4225
718426
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 16188
23119136
00016717 00000-0 10270-3 0 9063
2 25544 51
6450 323
0301 0001448 21
5456 338
5758 15
54693860 7941
Satellite: ISS
Catalog Number: 25544
Epoch time: 16188
23119136 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 323
0301 deg
Eccentricity:
0001448
Arg of perigee: 21
5456 deg
Mean anomaly: 338
5758 deg
Mean motion: 15
54693860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 308
Coasting Arc #8 (Orbit 807)
---------------------------------------
Vector Time (GMT): 2016/189/01:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5130794
64 A = 6787657
28 meter
Y = -4430986
85 meter E =
0013839
Z = 141683
28 I = 51
41955
XDOT = 3027
074345 Wp = 44
38222
YDOT = 3707
864885 meter/sec RA = 318
23061 deg
ZDOT = 5994
353450 TA = 317
14942
MA = 317
25718
Ha = 220
385 n
mi
Hp = 213
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16833315
76 X = 5179273
50
Y = -14537358
44 feet Y = -4373339
84 meter
Z = 464840
16 Z = 166724
26
XDOT = 9931
346275 XDOT = 2956
269617
YDOT = 12164
911041 feet/sec YDOT = 3741
319153 meter/sec
ZDOT = 19666
513943 ZDOT = 6008
886363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21873613
70 X = 6667077
46
Y = 4015714
35 feet Y = 1223989
73 meter
Z = 574846
32 Z = 175213
16
XDOT = -3051
850853 XDOT = -930
204140
YDOT = 13668
160211 feet/sec YDOT = 4166
055232 meter/sec
ZDOT = 19729
065317 ZDOT = 6013
419109
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 16189
13108544
00016717 00000-0 10270-3 0 9075
2 25544 51
6425 318
5402 0001507 24
3818 335
7406 15
54700408 8085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16189
13108544 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 318
5402 deg
Eccentricity:
0001507
Arg of perigee: 24
3818 deg
Mean anomaly: 335
7406 deg
Mean motion: 15
54700408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 808
Checksum: 294
Coasting Arc #9 (Orbit 822)
---------------------------------------
Vector Time (GMT): 2016/190/01:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5473265
94 A = 6785820
49 meter
Y = 3461758
03 meter E =
0006135
Z = -2023202
26 I = 51
39125
XDOT = -1220
512595 Wp = 126
33298
YDOT = -5157
399025 meter/sec RA = 313
24107 deg
ZDOT = -5537
975197 TA = 76
10013
MA = 76
03190
Ha = 220
338 n
mi
Hp = 213
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17956909
24 X = -5501741
72
Y = 11357473
86 feet Y = 3400393
27 meter
Z = -6637802
68 Z = -2049858
45
XDOT = -4004
306413 XDOT = -1135
849908
YDOT = -16920
600477 feet/sec YDOT = -5170
573788 meter/sec
ZDOT = -18169
209963 ZDOT = -5543
698825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20187808
68 X = -6153244
08
Y = -6506188
81 feet Y = -1983086
35 meter
Z = -6754636
49 Z = -2058813
20
XDOT = 10047
527625 XDOT = 3062
486420
YDOT = -12339
504596 feet/sec YDOT = -3761
081001 meter/sec
ZDOT = -18193
094247 ZDOT = -5545
255126
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 16190
09525301
00016717 00000-0 10270-3 0 9087
2 25544 51
6434 313
7304 0001457 26
0986 334
0240 15
54715726 8236
Satellite: ISS
Catalog Number: 25544
Epoch time: 16190
09525301 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 313
7304 deg
Eccentricity:
0001457
Arg of perigee: 26
0986 deg
Mean anomaly: 334
0240 deg
Mean motion: 15
54715726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 823
Checksum: 287
Coasting Arc #10 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2016/191/01:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5333712
83 A = 6781958
51 meter
Y = -2104335
37 meter E =
0012589
Z = 3610538
69 I = 51
35691
XDOT = -493
877210 Wp = 87
78920
YDOT = 6282
172918 meter/sec RA = 308
24040 deg
ZDOT = 4378
277133 TA = 315
22838
MA = 315
32991
Ha = 220
274 n
mi
Hp = 213
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17499057
83 X = 5339309
45
Y = -6903987
43 feet Y = -2044659
18 meter
Z = 11845599
38 Z = 3636461
60
XDOT = -1620
332053 XDOT = -585
356808
YDOT = 20610
803538 feet/sec YDOT = 6276
138275 meter/sec
ZDOT = 14364
426288 ZDOT = 4375
656257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16601699
59 X = 5060198
03
Y = 8692943
50 feet Y = 2649609
18 meter
Z = 11958954
65 Z = 3645089
38
XDOT = -16099
615087 XDOT = -4907
162679
YDOT = 10946
047781 feet/sec YDOT = 3336
355364 meter/sec
ZDOT = 14351
741395 ZDOT = 4374
410777
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 16191
12369279
00016717 00000-0 10270-3 0 9093
2 25544 51
6433 308
5996 0001501 29
5055 330
6182 15
54723279 8395
Satellite: ISS
Catalog Number: 25544
Epoch time: 16191
12369279 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 308
5996 deg
Eccentricity:
0001501
Arg of perigee: 29
5055 deg
Mean anomaly: 330
6182 deg
Mean motion: 15
54723279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 839
Checksum: 322
Coasting Arc #11 (Orbit 839)
---------------------------------------
Vector Time (GMT): 2016/191/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1972592
11 A = 6776650
60 meter
Y = -4069098
35 meter E =
0013483
Z = -5059275
25 I = 51
33805
XDOT = 5594
282416 Wp = 97
07689
YDOT = -4919
913132 meter/sec RA = 307
66032 deg
ZDOT = 1778
279928 TA = 190
20716
MA = 190
23457
Ha = 220
288 n
mi
Hp = 213
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6471758
88 X = -1902368
40
Y = -13350060
21 feet Y = -4090764
23 meter
Z = -16598672
09 Z = -5068687
17
XDOT = 18353
944933 XDOT = 5640
244355
YDOT = -16141
447282 feet/sec YDOT = -4857
097260 meter/sec
ZDOT = 5834
251732 ZDOT = 1805
566474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3872746
37 X = -1180413
09
Y = -14274944
91 feet Y = -4351003
21 meter
Z = -16638854
20 Z = -5071522
76
XDOT = 19867
475693 XDOT = 6055
606591
YDOT = -12320
711996 feet/sec YDOT = -3755
353016 meter/sec
ZDOT = 5954
114007 ZDOT = 1814
813949
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 16191
18796845
00016717 00000-0 10270-3 0 9104
2 25544 51
6443 308
2795 0001480 22
6348 337
4870 15
54744650 8402
Satellite: ISS
Catalog Number: 25544
Epoch time: 16191
18796845 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 308
2795 deg
Eccentricity:
0001480
Arg of perigee: 22
6348 deg
Mean anomaly: 337
4870 deg
Mean motion: 15
54744650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 840
Checksum: 320
Coasting Arc #12 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2016/192/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 541628
47 A = 6780083
14 meter
Y = 5323274
37 meter E =
0011394
Z = 4157599
20 I = 51
33036
XDOT = -5747
474666 Wp = 68
72787
YDOT = 3483
870760 meter/sec RA = 302
64003 deg
ZDOT = -3699
637564 TA = 59
47254
MA = 59
36012
Ha = 220
262 n
mi
Hp = 213
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1776996
29 X = 461866
44
Y = 17464810
94 feet Y = 5328885
01 meter
Z = 13640417
32 Z = 4160036
84
XDOT = -18856
544181 XDOT = -5768
033995
YDOT = 11430
022178 feet/sec YDOT = 3419
483922 meter/sec
ZDOT = -12137
918517 ZDOT = -3727
606760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1162569
45 X = -354351
17
Y = 17508996
75 feet Y = 5336742
21 meter
Z = 13649973
88 Z = 4160512
04
XDOT = -19104
301205 XDOT = -5822
991007
YDOT = 8321
076930 feet/sec YDOT = 2536
264248 meter/sec
ZDOT = -12260
455148 ZDOT = -3736
986729
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 16192
21640079
00016717 00000-0 10270-3 0 9117
2 25544 51
6437 303
1484 0001630 23
1692 336
9534 15
54780348 8561
Satellite: ISS
Catalog Number: 25544
Epoch time: 16192
21640079 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 303
1484 deg
Eccentricity:
0001630
Arg of perigee: 23
1692 deg
Mean anomaly: 336
9534 deg
Mean motion: 15
54780348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 302
Coasting Arc #13 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2016/193/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 748342
16 A = 6784379
30 meter
Y = -6160015
47 meter E =
0006174
Z = -2740998
91 I = 51
32658
XDOT = 5470
760427 Wp = 49
83718
YDOT = -1609
739543 meter/sec RA = 297
63099 deg
ZDOT = 5122
852079 TA = 278
99532
MA = 279
06520
Ha = 220
342 n
mi
Hp = 213
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2455190
81 X = 830483
85
Y = -20210024
51 feet Y = -6151187
57 meter
Z = -8992778
57 Z = -2737164
52
XDOT = 17948
689065 XDOT = 5463
469967
YDOT = -5281
297712 feet/sec YDOT = -1548
602906 meter/sec
ZDOT = 16807
257476 ZDOT = 5149
409618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5416865
01 X = 1651060
45
Y = -19632947
73 feet Y = -5984122
47 meter
Z = -8974856
86 Z = -2735536
37
XDOT = 16985
137407 XDOT = 5177
069882
YDOT = -3032
471316 feet/sec YDOT = -924
297257 meter/sec
ZDOT = 16923
264842 ZDOT = 5158
211124
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 16193
18055387
00016717 00000-0 10270-3 0 9127
2 25544 51
6425 298
3380 0001522 26
1817 333
9412 15
54737958 8718
Satellite: ISS
Catalog Number: 25544
Epoch time: 16193
18055387 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 298
3380 deg
Eccentricity:
0001522
Arg of perigee: 26
1817 deg
Mean anomaly: 333
9412 deg
Mean motion: 15
54737958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 871
Checksum: 319
Coasting Arc #14 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2016/194/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1881454
01 A = 6787197
91 meter
Y = 6448471
93 meter E =
0013478
Z = 930532
72 I = 51
32261
XDOT = -4876
212029 Wp = 118
45433
YDOT = -563
796401 meter/sec RA = 292
63222 deg
ZDOT = -5893
380207 TA = 51
42242
MA = 51
30175
Ha = 220
377 n
mi
Hp = 213
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6172749
37 X = -1957942
71
Y = 21156403
96 feet Y = 6427004
52 meter
Z = 3052928
86 Z = 921207
77
XDOT = -15998
070960 XDOT = -4840
917806
YDOT = -1849
725724 feet/sec YDOT = -618
127749 meter/sec
ZDOT = -19335
236901 ZDOT = -5916
981771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8848262
49 X = -2696950
41
Y = 20190554
86 feet Y = 6154081
12 meter
Z = 3011043
55 Z = 917766
07
XDOT = -14033
262467 XDOT = -4277
338400
YDOT = -3221
906500 feet/sec YDOT = -982
037101 meter/sec
ZDOT = -19437
936991 ZDOT = -5924
683195
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 16194
20897794
00016717 00000-0 10270-3 0 9138
2 25544 51
6432 293
2065 0001520 32
0823 328
0423 15
54739520 8872
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
20897794 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 293
2065 deg
Eccentricity:
0001520
Arg of perigee: 32
0823 deg
Mean anomaly: 328
0423 deg
Mean motion: 15
54739520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 304
Coasting Arc #15 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2016/194/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3669038
37 A = 6785486
89 meter
Y = -5297737
17 meter E =
0015232
Z = 2101000
55 I = 51
30725
XDOT = 3122
902233 Wp = 67
50313
YDOT = 4351
912263 meter/sec RA = 289
56803 deg
ZDOT = 5493
653683 TA = 315
89632
MA = 316
01770
Ha = 220
311 n
mi
Hp = 213
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12037527
45 X = 3717800
61
Y = -17381027
48 feet Y = -5256435
03 meter
Z = 6893046
43 Z = 2118941
80
XDOT = 10245
742234 XDOT = 3047
320310
YDOT = 14277
927372 feet/sec YDOT = 4386
411669 meter/sec
ZDOT = 18023
798173 ZDOT = 5508
640585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 236745
46 X = 72160
02
Y = 21115117
22 feet Y = 6435887
73 meter
Z = 6972234
10 Z = 2125136
95
XDOT = -14973
451657 XDOT = -4563
908065
YDOT = -5832
942505 feet/sec YDOT = -1777
880875 meter/sec
ZDOT = 18088
232935 ZDOT = 5513
293398
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 16194
85173806
00016717 00000-0 10270-3 0 9141
2 25544 51
6404 289
9990 0001446 44
5825 315
5444 15
54792658 8973
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
85173806 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 289
9990 deg
Eccentricity:
0001446
Arg of perigee: 44
5825 deg
Mean anomaly: 315
5444 deg
Mean motion: 15
54792658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 348
Coasting Arc #16 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2016/195/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4094739
85 A = 6781604
15 meter
Y = 3941410
43 meter E =
0007293
Z = -3707918
52 I = 51
28330
XDOT = -1963
650231 Wp = 70
81346
YDOT = -6051
612894 meter/sec RA = 284
56016 deg
ZDOT = -4268
729708 TA = 153
63726
MA = 153
60013
Ha = 220
486 n
mi
Hp = 213
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13434185
87 X = -4120497
99
Y = 12931136
57 feet Y = 3895476
58 meter
Z = -12165086
99 Z = -3727871
90
XDOT = -6442
422017 XDOT = -1875
098081
YDOT = -19854
373013 feet/sec YDOT = -6073
076289 meter/sec
ZDOT = -14005
018727 ZDOT = -4278
053967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3129732
91 X = 953942
59
Y = -18323629
41 feet Y = -5585042
24 meter
Z = -12252769
56 Z = -3734644
16
XDOT = 15523
769381 XDOT = 4731
644907
YDOT = 12032
958951 feet/sec YDOT = 3667
645888 meter/sec
ZDOT = -14044
464379 ZDOT = -4280
752743
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 16195
81587961
00016717 00000-0 10270-3 0 9150
2 25544 51
6397 285
1878 0001692 45
5171 314
6121 15
54752456 9127
Satellite: ISS
Catalog Number: 25544
Epoch time: 16195
81587961 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 285
1878 deg
Eccentricity:
0001692
Arg of perigee: 45
5171 deg
Mean anomaly: 314
6121 deg
Mean motion: 15
54752456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 331
Coasting Arc #17 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2016/196/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4266106
49 A = 6777548
77 meter
Y = -2158468
80 meter E =
0007700
Z = 4798418
50 I = 51
26283
XDOT = 824
771064 Wp = 108
31253
YDOT = 7206
537512 meter/sec RA = 279
53996 deg
ZDOT = 2502
744474 TA = 316
93958
MA = 316
99980
Ha = 220
275 n
mi
Hp = 213
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13996412
37 X = 4266617
43
Y = -7081590
55 feet Y = -2110759
92 meter
Z = 15742842
83 Z = 4819143
12
XDOT = 2705
941810 XDOT = 731
967253
YDOT = 23643
495775 feet/sec YDOT = 7215
241533 meter/sec
ZDOT = 8211
103916 ZDOT = 2506
526218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6781843
69 X = -2067105
96
Y = 14042479
73 feet Y = 4280147
82 meter
Z = 15833538
56 Z = 4826062
55
XDOT = -15390
411139 XDOT = -4690
997315
YDOT = -16729
173212 feet/sec YDOT = -5099
051995 meter/sec
ZDOT = 8226
193541 ZDOT = 2507
343791
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 16196
84429159
00016717 00000-0 10270-3 0 9169
2 25544 51
6398 280
0570 0001560 43
6727 316
4549 15
54774907 9287
Satellite: ISS
Catalog Number: 25544
Epoch time: 16196
84429159 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 280
0570 deg
Eccentricity:
0001560
Arg of perigee: 43
6727 deg
Mean anomaly: 316
4549 deg
Mean motion: 15
54774907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 340
Coasting Arc #18 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2016/197/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4260404
41 A = 6775561
50 meter
Y = 112560
02 meter E =
0016171
Z = -5281373
28 I = 51
25248
XDOT = 286
253383 Wp = 83
15573
YDOT = -7642
194443 meter/sec RA = 274
50832 deg
ZDOT = -392
938940 TA = 183
06687
MA = 183
07680
Ha = 220
503 n
mi
Hp = 213
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13977704
75 X = -4235691
96
Y = 369291
41 feet Y = 65056
05 meter
Z = -17327340
17 Z = -5302009
11
XDOT = 939
151520 XDOT = 373
597768
YDOT = -25072
816414 feet/sec YDOT = -7638
504955 meter/sec
ZDOT = -1289
169751 ZDOT = -391
337029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10668098
11 X = 3251636
30
Y = -8864540
61 feet Y = -2701911
98 meter
Z = -17417259
43 Z = -5308780
68
XDOT = 14116
321362 XDOT = 4302
654751
YDOT = 19510
280691 feet/sec YDOT = 5946
733555 meter/sec
ZDOT = -1280
735280 ZDOT = -390
368113
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 16197
80842415
00016717 00000-0 10270-3 0 9171
2 25544 51
6406 275
2460 0001705 48
5205 311
6095 15
54763268 9435
Satellite: ISS
Catalog Number: 25544
Epoch time: 16197
80842415 = yrday
fracday
Element set: 917
Inclination: 51
6406 deg
RA of node: 275
2460 deg
Eccentricity:
0001705
Arg of perigee: 48
5205 deg
Mean anomaly: 311
6095 deg
Mean motion: 15
54763268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 310
Coasting Arc #19 (Orbit 947)
---------------------------------------
Vector Time (GMT): 2016/198/02:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 892614
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2520815
16 A = 6782151
05 meter
Y = 5240736
79 meter E =
0013368
Z = 3479844
69 I = 51
27741
XDOT = -3868
011108 Wp = 82
59779
YDOT = 4860
954908 meter/sec RA = 272
98310 deg
ZDOT = -4502
126011 TA = 56
24398
MA = 56
11669
Ha = 220
309 n
mi
Hp = 213
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8270390
94 X = 2445121
09
Y = 17194018
34 feet Y = 5268502
63 meter
Z = 11416813
30 Z = 3491906
80
XDOT = -12690
325158 XDOT = -3900
210811
YDOT = 15948
014791 feet/sec YDOT = 4817
520661 meter/sec
ZDOT = -14770
754628 ZDOT = -4520
993417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2820188
74 X = -859593
53
Y = 18838799
96 feet Y = 5742066
23 meter
Z = 11468365
64 Z = 3495557
85
XDOT = -17984
975601 XDOT = -5481
820563
YDOT = 6383
112792 feet/sec YDOT = 1945
572779 meter/sec
ZDOT = -14853
873279 ZDOT = -4527
460576
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 16198
12979887
00016717 00000-0 10270-3 0 9182
2 25544 51
6438 273
6436 0001724 36
6477 323
4794 15
54813832 9480
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
12979887 = yrday
fracday
Element set: 918
Inclination: 51
6438 deg
RA of node: 273
6436 deg
Eccentricity:
0001724
Arg of perigee: 36
6477 deg
Mean anomaly: 323
4794 deg
Mean motion: 15
54813832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 948
Checksum: 356
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list