[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 24th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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
182/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
8
183/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 215
0
Coasting Arc #1 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2017/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6610367
84 A = 6789178
13 meter
Y = -1334559
02 meter E =
0005204
Z = -760466
78 I = 51
70366
XDOT = 1601
705322 Wp = 147
95838
YDOT = -4553
643381 meter/sec RA = 6
30524 deg
ZDOT = -5954
554644 TA = 40
25037
MA = 40
21185
Ha = 220
445 n
mi
Hp = 216
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21687558
52 X = -6591259
17
Y = -4378474
46 feet Y = -1408373
66 meter
Z = -2494969
76 Z = -792531
79
XDOT = 5254
938722 XDOT = 1681
430680
YDOT = -14939
774873 feet/sec YDOT = -4535
285249 meter/sec
ZDOT = -19535
940433 ZDOT = -5946
581167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4006232
67 X = -1221099
72
Y = 21742727
76 feet Y = 6627183
42 meter
Z = -2636284
64 Z = -803539
56
XDOT = -13446
177051 XDOT = -4098
394765
YDOT = -4833
221028 feet/sec YDOT = -1473
165769 meter/sec
ZDOT = -19499
832019 ZDOT = -5943
548800
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 17174
53062184
00016717 00000-0 10270-3 0 9006
2 25544 51
6393 6
7155 0005170 312
4359 47
6356 15
54085089 22733
Satellite: ISS
Catalog Number: 25544
Epoch time: 17174
53062184 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 6
7155 deg
Eccentricity:
0005170
Arg of perigee: 312
4359 deg
Mean anomaly: 47
6356 deg
Mean motion: 15
54085089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 303
Coasting Arc #2 (Orbit 2288)
---------------------------------------
Vector Time (GMT): 2017/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6021652
91 A = 6786968
23 meter
Y = 2017516
46 meter E =
0012118
Z = 2373176
25 I = 51
66286
XDOT = -3525
673392 Wp = 52
51979
YDOT = 4176
513870 meter/sec RA = 1
33458 deg
ZDOT = 5383
747728 TA = 333
98525
MA = 334
04610
Ha = 220
428 n
mi
Hp = 215
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19756079
09 X = 5987117
29
Y = 6619148
48 feet Y = 2084661
15 meter
Z = 7786011
33 Z = 2402343
93
XDOT = -11567
169922 XDOT = -3598
265733
YDOT = 13702
473326 feet/sec YDOT = 4136
680593 meter/sec
ZDOT = 17663
214330 ZDOT = 5366
445561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5939003
20 X = 1810208
18
Y = -19920550
04 feet Y = -6071783
65 meter
Z = 7914397
47 Z = 2412308
35
XDOT = 12644
677363 XDOT = 3854
097660
YDOT = 10771
616790 feet/sec YDOT = 3283
188798 meter/sec
ZDOT = 17585
990724 ZDOT = 5360
209973
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 17175
55948959
00016717 00000-0 10270-3 0 9013
2 25544 51
6383 1
5856 0005006 314
8881 45
1864 15
54092457 22898
Satellite: ISS
Catalog Number: 25544
Epoch time: 17175
55948959 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 1
5856 deg
Eccentricity:
0005006
Arg of perigee: 314
8881 deg
Mean anomaly: 45
1864 deg
Mean motion: 15
54092457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2289
Checksum: 335
Coasting Arc #3 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2017/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4983554
67 A = 6783346
79 meter
Y = -2665451
30 meter E =
0005887
Z = -3758315
50 I = 51
61777
XDOT = 5187
978825 Wp = 27
11929
YDOT = -3703
745254 meter/sec RA = 356
35475 deg
ZDOT = -4250
055130 TA = 197
82377
MA = 197
84442
Ha = 220
697 n
mi
Hp = 215
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16350244
99 X = -4935122
63
Y = -8744918
95 feet Y = -2720909
38 meter
Z = -12330431
43 Z = -3782406
64
XDOT = 17020
927902 XDOT = 5249
653988
YDOT = -12151
395191 feet/sec YDOT = -3645
384234 meter/sec
ZDOT = -13943
750426 ZDOT = -4224
704556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7895880
45 X = -2406664
36
Y = 16698437
02 feet Y = 5089683
60 meter
Z = -12436274
80 Z = -3790576
56
XDOT = -11800
764001 XDOT = -3596
872867
YDOT = -15886
847969 feet/sec YDOT = -4842
311261 meter/sec
ZDOT = -13831
086452 ZDOT = -4215
715151
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 17176
52405320
00016717 00000-0 10270-3 0 9022
2 25544 51
6378 356
7775 0004947 320
8204 39
2590 15
54093443 23040
Satellite: ISS
Catalog Number: 25544
Epoch time: 17176
52405320 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 356
7775 deg
Eccentricity:
0004947
Arg of perigee: 320
8204 deg
Mean anomaly: 39
2590 deg
Mean motion: 15
54093443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 306
Coasting Arc #4 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2017/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3570483
46 A = 6779832
82 meter
Y = 3265708
86 meter E =
0003602
Z = 4745699
35 I = 51
57376
XDOT = -6457
245920 Wp = 82
55227
YDOT = 3142
869764 meter/sec RA = 351
36174 deg
ZDOT = 2694
152497 TA = 340
80247
MA = 340
81603
Ha = 220
723 n
mi
Hp = 215
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11714184
56 X = 3510648
08
Y = 10714267
91 feet Y = 3305301
20 meter
Z = 15569879
77 Z = 4762898
57
XDOT = -21185
190027 XDOT = -6504
997110
YDOT = 10311
252506 feet/sec YDOT = 3070
393095 meter/sec
ZDOT = 8839
082995 ZDOT = 2662
670039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9892455
13 X = 3015220
32
Y = -12320982
79 feet Y = -3755435
55 meter
Z = 15645175
85 Z = 4768649
60
XDOT = 10848
805223 XDOT = 3306
715832
YDOT = 19762
398002 feet/sec YDOT = 6023
578911 meter/sec
ZDOT = 8699
461317 ZDOT = 2651
595809
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 17177
55291819
00016717 00000-0 10270-3 0 9033
2 25544 51
6382 351
6481 0005052 322
8428 37
2374 15
54074156 23207
Satellite: ISS
Catalog Number: 25544
Epoch time: 17177
55291819 = yrday
fracday
Element set: 903
Inclination: 51
6382 deg
RA of node: 351
6481 deg
Eccentricity:
0005052
Arg of perigee: 322
8428 deg
Mean anomaly: 37
2374 deg
Mean motion: 15
54074156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 304
Coasting Arc #5 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2017/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1932672
99 A = 6777675
96 meter
Y = -3829652
48 meter E =
0013227
Z = -5258441
61 I = 51
53563
XDOT = 7205
367095 Wp = 63
97109
YDOT = -2450
972402 meter/sec RA = 346
35941 deg
ZDOT = -859
235479 TA = 197
76834
MA = 197
81463
Ha = 220
907 n
mi
Hp = 215
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6340790
64 X = -1864162
58
Y = -12564476
65 feet Y = -3850881
27 meter
Z = -17252105
02 Z = -5267663
86
XDOT = 23639
655823 XDOT = 7236
412687
YDOT = -8041
248038 feet/sec YDOT = -2370
223417 meter/sec
ZDOT = -2819
014038 ZDOT = -824
159374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11984878
65 X = -3652991
01
Y = 7283798
45 feet Y = 2220101
77 meter
Z = -17292073
06 Z = -5270623
87
XDOT = -9511
933712 XDOT = -2899
237395
YDOT = -22005
806488 feet/sec YDOT = -6707
369818 meter/sec
ZDOT = -2663
670156 ZDOT = -811
886663
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 17178
51747640
00016717 00000-0 10270-3 0 9049
2 25544 51
6392 346
8403 0004822 328
6769 31
4095 15
54094296 23353
Satellite: ISS
Catalog Number: 25544
Epoch time: 17178
51747640 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 346
8403 deg
Eccentricity:
0004822
Arg of perigee: 328
6769 deg
Mean anomaly: 31
4095 deg
Mean motion: 15
54094296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 326
Coasting Arc #6 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2017/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 180366
63 A = 6777997
17 meter
Y = 4320481
85 meter E =
0006428
Z = 5219577
14 I = 51
50351
XDOT = -7421
519818 Wp = 8
47121
YDOT = 1608
018206 meter/sec RA = 341
35122 deg
ZDOT = -1068
175340 TA = 91
81763
MA = 91
74401
Ha = 221
111 n
mi
Hp = 215
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 591754
05 X = 106686
62
Y = 14174809
22 feet Y = 4322086
36 meter
Z = 17124596
91 Z = 5220274
75
XDOT = -24348
818302 XDOT = -7433
760912
YDOT = 5275
650281 feet/sec YDOT = 1524
957397 meter/sec
ZDOT = -3504
512271 ZDOT = -1104
255933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14051544
80 X = 4282910
85
Y = -1937198
05 feet Y = -590457
96 meter
Z = 17126837
45 Z = 5220260
05
XDOT = 7611
211782 XDOT = 2319
897351
YDOT = 22628
092082 feet/sec YDOT = 6897
042467 meter/sec
ZDOT = -3664
116232 ZDOT = -1116
822628
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 17179
54633770
00016717 00000-0 10270-3 0 9052
2 25544 51
6380 341
7112 0004777 332
4442 27
6457 15
54048640 23510
Satellite: ISS
Catalog Number: 25544
Epoch time: 17179
54633770 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 341
7112 deg
Eccentricity:
0004777
Arg of perigee: 332
4442 deg
Mean anomaly: 27
6457 deg
Mean motion: 15
54048640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 306
Coasting Arc #7 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2017/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1487307
63 A = 6780270
00 meter
Y = -4701050
09 meter E =
0007862
Z = -4660392
04 I = 51
48263
XDOT = 7077
753303 Wp = 83
51322
YDOT = -603
810211 meter/sec RA = 336
34574 deg
ZDOT = 2872
902685 TA = 215
09390
MA = 215
14573
Ha = 221
118 n
mi
Hp = 215
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4879618
21 X = 1562403
15
Y = -15423392
67 feet Y = -4683997
74 meter
Z = -15290000
13 Z = -4652985
22
XDOT = 23220
975404 XDOT = 7070
024219
YDOT = -1981
004629 feet/sec YDOT = -524
705425 meter/sec
ZDOT = 9425
533744 ZDOT = 2907
265070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15911082
15 X = -4849697
84
Y = -3091230
83 feet Y = -942207
16 meter
Z = -15256394
60 Z = -4650149
07
XDOT = -4972
195575 XDOT = -1515
525211
YDOT = -21593
234685 feet/sec YDOT = -6581
617932 meter/sec
ZDOT = 9577
347345 ZDOT = 2919
175471
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 17180
51089122
00016717 00000-0 10270-3 0 9068
2 25544 51
6397 336
9038 0004809 335
0162 25
0757 15
54093538 23662
Satellite: ISS
Catalog Number: 25544
Epoch time: 17180
51089122 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 336
9038 deg
Eccentricity:
0004809
Arg of perigee: 335
0162 deg
Mean anomaly: 25
0757 deg
Mean motion: 15
54093538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 314
Coasting Arc #8 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2017/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2995740
95 A = 6784030
27 meter
Y = 4904742
26 meter E =
0011497
Z = 3600447
98 I = 51
46522
XDOT = -6252
638157 Wp = 63
03494
YDOT = -577
009081 meter/sec RA = 331
34537 deg
ZDOT = -4400
476445 TA = 74
22381
MA = 74
09706
Ha = 221
279 n
mi
Hp = 215
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9828546
42 X = -3067853
51
Y = 16091674
09 feet Y = 4870838
37 meter
Z = 11812493
39 Z = 3585720
93
XDOT = -20513
904714 XDOT = -6224
345967
YDOT = -1893
074413 feet/sec YDOT = -646
771790 meter/sec
ZDOT = -14437
258678 ZDOT = -4430
780956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17299125
84 X = 5272773
56
Y = 7605017
46 feet Y = 2318009
32 meter
Z = 11746542
23 Z = 3580346
07
XDOT = 1478
383943 XDOT = 450
611426
YDOT = 19224
455220 feet/sec YDOT = 5859
613951 meter/sec
ZDOT = -14570
922956 ZDOT = -4441
217317
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 17181
53974685
00016717 00000-0 10270-3 0 9079
2 25544 51
6393 331
7744 0004826 339
0051 21
0903 15
54082507 23826
Satellite: ISS
Catalog Number: 25544
Epoch time: 17181
53974685 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 331
7744 deg
Eccentricity:
0004826
Arg of perigee: 339
0051 deg
Mean anomaly: 21
0903 deg
Mean motion: 15
54082507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 309
Coasting Arc #9 (Orbit 2396)
---------------------------------------
Vector Time (GMT): 2017/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4171029
74 A = 6787419
54 meter
Y = -4877104
34 meter E =
0009678
Z = -2194976
60 I = 51
44928
XDOT = 5049
546386 Wp = 16
36514
YDOT = 1867
260578 meter/sec RA = 326
35459 deg
ZDOT = 5461
497583 TA = 319
19020
MA = 319
26264
Ha = 221
379 n
mi
Hp = 215
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13684480
77 X = 4235918
88
Y = -16000998
48 feet Y = -4830098
06 meter
Z = -7201366
79 Z = -2174557
88
XDOT = 16566
753235 XDOT = 5001
761716
YDOT = 6126
182998 feet/sec YDOT = 1923
460413 meter/sec
ZDOT = 17918
299156 ZDOT = 5485
910717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17927151
64 X = -5464195
82
Y = -11100334
55 feet Y = -3383381
97 meter
Z = -7110306
39 Z = -2167221
39
XDOT = 2709
280626 XDOT = 825
788735
YDOT = -15889
980349 feet/sec YDOT = -4843
266011 meter/sec
ZDOT = 18025
705166 ZDOT = 5494
234935
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 17182
50429648
00016717 00000-0 10270-3 0 9082
2 25544 51
6399 326
9672 0004855 343
2924 16
8068 15
54099077 23976
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
50429648 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 326
9672 deg
Eccentricity:
0004855
Arg of perigee: 343
2924 deg
Mean anomaly: 16
8068 deg
Mean motion: 15
54099077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2397
Checksum: 352
Coasting Arc #10 (Orbit 2402)
---------------------------------------
Vector Time (GMT): 2017/182/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3753479
80 A = 6778173
64 meter
Y = -2361177
58 meter E =
0014440
Z = -5138693
17 I = 51
40823
XDOT = 5354
358186 Wp = 57
66628
YDOT = -5269
772968 meter/sec RA = 324
53302 deg
ZDOT = -1485
095821 TA = 197
94237
MA = 197
99339
Ha = 221
481 n
mi
Hp = 214
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12314566
28 X = -3701836
35
Y = -7746645
61 feet Y = -2402862
36 meter
Z = -16859229
56 Z = -5156801
13
XDOT = 17566
791950 XDOT = 5420
102075
YDOT = -17289
281391 feet/sec YDOT = -5209
529184 meter/sec
ZDOT = -4872
361616 ZDOT = -1458
926828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13533930
96 X = 4125142
16
Y = -5079914
10 feet Y = -1548357
82 meter
Z = -16938709
16 Z = -5162918
55
XDOT = 2840
096706 XDOT = 865
661476
YDOT = 23473
788114 feet/sec YDOT = 7154
810617 meter/sec
ZDOT = -4755
848199 ZDOT = -1449
582531
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 17182
89011485
00016717 00000-0 10270-3 0 9091
2 25544 51
6398 325
0483 0005159 345
8322 14
2685 15
54088336 24034
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
89011485 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 325
0483 deg
Eccentricity:
0005159
Arg of perigee: 345
8322 deg
Mean anomaly: 14
2685 deg
Mean motion: 15
54088336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 319
Coasting Arc #11 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2017/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5009439
40 A = 6789265
52 meter
Y = 4547127
63 meter E =
0009434
Z = 532575
61 I = 51
42837
XDOT = -3574
571181 Wp = 111
31009
YDOT = -3230
059352 meter/sec RA = 321
36887 deg
ZDOT = -5962
390214 TA = 62
92904
MA = 62
83281
Ha = 221
406 n
mi
Hp = 214
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16435168
64 X = -5062501
26
Y = 14918397
74 feet Y = 4490811
95 meter
Z = 1747295
32 Z = 508112
86
XDOT = -11727
595738 XDOT = -3509
223812
YDOT = -10597
307584 feet/sec YDOT = -3269
666725 meter/sec
ZDOT = -19561
647683 ZDOT = -5979
595918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17512948
74 X = 5337946
77
Y = 13650585
55 feet Y = 4160698
48 meter
Z = 1638456
93 Z = 499401
67
XDOT = -7462
243566 XDOT = -2274
491839
YDOT = 11965
085430 feet/sec YDOT = 3646
958039 meter/sec
ZDOT = -19636
979038 ZDOT = -5985
351211
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 17183
53314757
00016717 00000-0 10270-3 0 9103
2 25544 51
6392 321
8383 0004924 345
8751 14
2263 15
54113211 24130
Satellite: ISS
Catalog Number: 25544
Epoch time: 17183
53314757 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 321
8383 deg
Eccentricity:
0004924
Arg of perigee: 345
8751 deg
Mean anomaly: 14
2263 deg
Mean motion: 15
54113211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 287
Coasting Arc #12 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2017/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5425761
06 A = 6788751
65 meter
Y = -3896606
18 meter E =
0016220
Z = 1154916
40 I = 51
40374
XDOT = 2007
009601 Wp = 41
45325
YDOT = 4539
550796 meter/sec RA = 316
38323 deg
ZDOT = 5852
039944 TA = 331
13712
MA = 331
22674
Ha = 221
458 n
mi
Hp = 214
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17801053
34 X = 5463320
66
Y = -12784141
00 feet Y = -3835721
74 meter
Z = 3789095
80 Z = 1181363
90
XDOT = 6584
677167 XDOT = 1927
671651
YDOT = 14893
539358 feet/sec YDOT = 4561
550347 meter/sec
ZDOT = 19199
606116 ZDOT = 5861
597130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15898549
88 X = -4845878
00
Y = -15054696
44 feet Y = -4588671
47 meter
Z = 3906563
07 Z = 1190720
42
XDOT = 12317
051976 XDOT = 3754
237442
YDOT = -7985
519926 feet/sec YDOT = -2433
986473 meter/sec
ZDOT = 19240
932423 ZDOT = 5864
636203
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 17184
56199558
00016717 00000-0 10270-3 0 9118
2 25544 51
6410 316
7095 0004904 350
5842 9
5218 15
54122497 24296
Satellite: ISS
Catalog Number: 25544
Epoch time: 17184
56199558 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 316
7095 deg
Eccentricity:
0004904
Arg of perigee: 350
5842 deg
Mean anomaly: 9
5218 deg
Mean motion: 15
54122497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 318
Coasting Arc #13 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2017/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5486945
49 A = 6786063
73 meter
Y = 2900134
00 meter E =
0004427
Z = -2751510
16 I = 51
37154
XDOT = -440
267195 Wp = 54
41255
YDOT = -5684
521718 meter/sec RA = 311
39196 deg
ZDOT = -5116
903696 TA = 156
83991
MA = 156
81995
Ha = 221
641 n
mi
Hp = 214
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18001789
65 X = -5505602
26
Y = 9514875
32 feet Y = 2838671
25 meter
Z = -9027264
31 Z = -2778209
03
XDOT = -1444
446178 XDOT = -351
813253
YDOT = -18650
005636 feet/sec YDOT = -5688
949928 meter/sec
ZDOT = -16787
741786 ZDOT = -5118
828182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12988928
83 X = 3959025
51
Y = 15611971
25 feet Y = 4758528
84 meter
Z = -9145647
34 Z = -2787593
31
XDOT = -16843
751526 XDOT = -5133
975465
YDOT = 4181
221772 feet/sec YDOT = 1274
436396 meter/sec
ZDOT = -16795
169368 ZDOT = -5119
167624
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 17185
52653844
00016717 00000-0 10270-3 0 9129
2 25544 51
6407 311
9017 0004985 354
7271 5
3828 15
54118573 24442
Satellite: ISS
Catalog Number: 25544
Epoch time: 17185
52653844 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 311
9017 deg
Eccentricity:
0004985
Arg of perigee: 354
7271 deg
Mean anomaly: 5
3828 deg
Mean motion: 15
54118573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2444
Checksum: 315
Coasting Arc #14 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2017/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5198290
10 A = 6782236
06 meter
Y = -1608673
16 meter E =
0010462
Z = 4037556
19 I = 51
33858
XDOT = -982
783060 Wp = 75
27952
YDOT = 6552
667003 meter/sec RA = 306
38983 deg
ZDOT = 3870
277113 TA = 334
45969
MA = 334
51134
Ha = 221
506 n
mi
Hp = 214
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17054757
56 X = 5196279
92
Y = -5277799
08 feet Y = -1550554
10 meter
Z = 13246575
44 Z = 4062802
77
XDOT = -3224
353870 XDOT = -1074
783547
YDOT = 21498
251323 feet/sec YDOT = 6541
161964 meter/sec
ZDOT = 12697
759558 ZDOT = 3865
280432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8907479
51 X = -2714999
76
Y = -15375441
88 feet Y = -4686434
69 meter
Z = 13358303
59 Z = 4071610
94
XDOT = 20576
364114 XDOT = 6271
675782
YDOT = -892
444518 feet/sec YDOT = -272
017089 meter/sec
ZDOT = 12674
484990 ZDOT = 3863
183025
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 17186
55538042
00016717 00000-0 10270-3 0 9136
2 25544 51
6410 306
7733 0004941 357
3787 2
7339 15
54146191 24609
Satellite: ISS
Catalog Number: 25544
Epoch time: 17186
55538042 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 306
7733 deg
Eccentricity:
0004941
Arg of perigee: 357
3787 deg
Mean anomaly: 2
7339 deg
Mean motion: 15
54146191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 309
Coasting Arc #15 (Orbit 2474)
---------------------------------------
Vector Time (GMT): 2017/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4672596
69 A = 6778994
33 meter
Y = 88150
84 meter E =
0014644
Z = -4923881
27 I = 51
30978
XDOT = 2196
753883 Wp = 54
49397
YDOT = -6995
671322 meter/sec RA = 301
37665 deg
ZDOT = -2206
187451 TA = 193
82395
MA = 193
86409
Ha = 221
803 n
mi
Hp = 214
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15330041
62 X = -4649317
42
Y = 289208
79 feet Y = 36029
52 meter
Z = -16154466
12 Z = -4946522
68
XDOT = 7207
197779 XDOT = 2285
534594
YDOT = -22951
677566 feet/sec YDOT = -6970
609029 meter/sec
ZDOT = -7238
147806 ZDOT = -2195
301646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3909899
95 X = 1191737
51
Y = 14716226
48 feet Y = 4485505
83 meter
Z = -16254413
37 Z = -4954345
20
XDOT = -22946
965847 XDOT = -6994
235190
YDOT = -1856
832927 feet/sec YDOT = -565
962676 meter/sec
ZDOT = -7188
808144 ZDOT = -2191
148722
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 17187
51991932
00016717 00000-0 10270-3 0 9145
2 25544 51
6419 301
9660 0005029
8624 359
2536 15
54113909 24758
Satellite: ISS
Catalog Number: 25544
Epoch time: 17187
51991932 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 301
9660 deg
Eccentricity:
0005029
Arg of perigee:
8624 deg
Mean anomaly: 359
2536 deg
Mean motion: 15
54113909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2475
Checksum: 317
Coasting Arc #16 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2017/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3949470
65 A = 6777271
40 meter
Y = 1559586
10 meter E =
0005386
Z = 5279412
20 I = 51
28866
XDOT = -3173
072837 Wp = 32
26775
YDOT = 6977
257005 meter/sec RA = 296
35386 deg
ZDOT = 316
923594 TA = 54
72258
MA = 54
67221
Ha = 221
735 n
mi
Hp = 214
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12957580
86 X = 3906092
77
Y = 5116752
29 feet Y = 1603508
48 meter
Z = 17320906
18 Z = 5298492
26
XDOT = -10410
343954 XDOT = -3252
397983
YDOT = 22891
263141 feet/sec YDOT = 6941
329975 meter/sec
ZDOT = 1039
775572 ZDOT = 301
318190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1671927
49 X = 509603
50
Y = -13724803
77 feet Y = -4183320
19 meter
Z = 17404834
57 Z = 5304993
58
XDOT = 23790
673439 XDOT = 7251
397264
YDOT = 4109
817531 feet/sec YDOT = 1252
672383 meter/sec
ZDOT = 969
619267 ZDOT = 295
539952
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 17188
54875502
00016717 00000-0 10270-3 0 9154
2 25544 51
6422 296
8369 0005152 4
9903 355
1300 15
54163114 24917
Satellite: ISS
Catalog Number: 25544
Epoch time: 17188
54875502 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 296
8369 deg
Eccentricity:
0005152
Arg of perigee: 4
9903 deg
Mean anomaly: 355
1300 deg
Mean motion: 15
54163114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 305
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