[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 25th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
239/10:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
6
246/19:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
4
250/21:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
1
250/21:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 215
2
Coasting Arc #1 (Orbit 1561)
---------------------------------------
Vector Time (GMT): 2016/237/12:45:53
942
Vector Time (MET): N/A
Weight (LBS) : 929160
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -769899
78 A = 6785368
39 meter
Y = 6117341
29 meter E =
0010259
Z = 2823074
31 I = 52
00926
XDOT = -4857
194880 Wp = 84
90770
YDOT = -2985
452329 meter/sec RA = 76
21964 deg
ZDOT = 5129
473259 TA = 306
97883
MA = 307
07270
Ha = 219
723 n
mi
Hp = 215
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2525917
90 X = -851961
45
Y = 20070017
34 feet Y = 6108273
04 meter
Z = 9262054
82 Z = 2819134
75
XDOT = -15935
678740 XDOT = -4848
366483
YDOT = -9794
791105 feet/sec YDOT = -3039
719141 meter/sec
ZDOT = 16828
980507 ZDOT = 5105
899882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8066866
05 X = 2458780
77
Y = -18559382
85 feet Y = -5656899
89 meter
Z = 9243727
46 Z = 2817488
13
XDOT = 11333
310884 XDOT = 3454
393157
YDOT = 13281
567314 feet/sec YDOT = 4048
221717 meter/sec
ZDOT = 16726
468990 ZDOT = 5098
227748
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 16237
59045550
00016717 00000-0 10270-3 0 9009
2 25544 51
6394 76
6927 0003283 245
1282 114
9529 15
54333632 15627
Satellite: ISS
Catalog Number: 25544
Epoch time: 16237
59045550 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 76
6927 deg
Eccentricity:
0003283
Arg of perigee: 245
1282 deg
Mean anomaly: 114
9529 deg
Mean motion: 15
54333632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1562
Checksum: 310
Coasting Arc #2 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2016/238/12:45:53
942
Vector Time (MET): N/A
Weight (LBS) : 929160
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1717400
95 A = 6781441
82 meter
Y = -5072165
81 meter E =
0004626
Z = -4165513
13 I = 51
98730
XDOT = 4719
657512 Wp = 71
61083
YDOT = 4704
308941 meter/sec RA = 71
25957 deg
ZDOT = -3784
379628 TA = 159
58515
MA = 159
56665
Ha = 219
741 n
mi
Hp = 215
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5634517
54 X = 1794225
71
Y = -16640963
95 feet Y = -5052531
26 meter
Z = -13666381
66 Z = -4156983
72
XDOT = 15484
440656 XDOT = 4685
084753
YDOT = 15434
084452 feet/sec YDOT = 4756
893888 meter/sec
ZDOT = -12415
943663 ZDOT = -3761
536948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9877222
49 X = -3010577
42
Y = 14565472
54 feet Y = 4439556
03 meter
Z = -13628167
24 Z = -4153865
37
XDOT = -9922
805864 XDOT = -3024
471227
YDOT = -18247
043675 feet/sec YDOT = -5561
698912 meter/sec
ZDOT = -12316
945010 ZDOT = -3754
204839
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 16238
55487386
00016717 00000-0 10270-3 0 9014
2 25544 51
6392 71
8837 0003054 248
8520 111
2307 15
54326230 15779
Satellite: ISS
Catalog Number: 25544
Epoch time: 16238
55487386 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 71
8837 deg
Eccentricity:
0003054
Arg of perigee: 248
8520 deg
Mean anomaly: 111
2307 deg
Mean motion: 15
54326230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1577
Checksum: 307
Coasting Arc #3 (Orbit 1590)
---------------------------------------
Vector Time (GMT): 2016/239/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2378347
01 A = 6788779
15 meter
Y = -6339796
24 meter E =
0010157
Z = -396250
67 I = 52
00553
XDOT = 4550
371934 Wp = 154
11653
YDOT = -1334
499105 meter/sec RA = 66
81665 deg
ZDOT = -6027
530892 TA = 30
13472
MA = 30
07632
Ha = 219
639 n
mi
Hp = 215
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7802975
75 X = -2305352
24
Y = -20799856
43 feet Y = -6365984
38 meter
Z = -1300035
02 Z = -407626
55
XDOT = 14929
041779 XDOT = 4594
235362
YDOT = -4378
277902 feet/sec YDOT = -1283
368686 meter/sec
ZDOT = -19775
363820 ZDOT = -6005
319934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12006208
66 X = -3659492
40
Y = 18688038
66 feet Y = 5696114
18 meter
Z = -1348596
93 Z = -411052
34
XDOT = -11153
627385 XDOT = -3399
625627
YDOT = -8570
467428 feet/sec YDOT = -2612
278472 meter/sec
ZDOT = -19678
018449 ZDOT = -5997
860023
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 16239
45499254
00016717 00000-0 10270-3 0 9022
2 25544 51
6432 67
3988 0003247 255
4663 104
6130 15
54293111 15914
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
45499254 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 67
3988 deg
Eccentricity:
0003247
Arg of perigee: 255
4663 deg
Mean anomaly: 104
6130 deg
Mean motion: 15
54293111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1591
Checksum: 310
Coasting Arc #4 (Orbit 1606)
---------------------------------------
Vector Time (GMT): 2016/240/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1474212
07 A = 6786762
03 meter
Y = 6270803
78 meter E =
0010744
Z = 2119372
96 I = 51
98449
XDOT = -5259
543331 Wp = 66
61523
YDOT = -643
695781 meter/sec RA = 61
86706 deg
ZDOT = 5544
997959 TA = 316
75582
MA = 316
84012
Ha = 219
497 n
mi
Hp = 215
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4836653
78 X = 1393685
91
Y = 20573503
23 feet Y = 6286839
21 meter
Z = 6953323
36 Z = 2126338
49
XDOT = -17255
719589 XDOT = -5278
889356
YDOT = -2111
862800 feet/sec YDOT = -702
619547 meter/sec
ZDOT = 18192
250522 ZDOT = 5519
401744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13341643
04 X = 4066532
80
Y = -16378482
90 feet Y = -4992161
59 meter
Z = 6982608
37 Z = 2128299
03
XDOT = 7766
396090 XDOT = 2367
197528
YDOT = 14059
732023 feet/sec YDOT = 4285
406321 meter/sec
ZDOT = 18080
469732 ZDOT = 5510
927174
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 16240
48369323
00016717 00000-0 10270-3 0 9031
2 25544 51
6419 62
2683 0003240 261
0262 99
0524 15
54351666 16078
Satellite: ISS
Catalog Number: 25544
Epoch time: 16240
48369323 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 62
2683 deg
Eccentricity:
0003240
Arg of perigee: 261
0262 deg
Mean anomaly: 99
0524 deg
Mean motion: 15
54351666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1607
Checksum: 293
Coasting Arc #5 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2016/241/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -342515
97 A = 6783159
71 meter
Y = -5723620
72 meter E =
0002225
Z = -3626460
91 I = 51
95493
XDOT = 5746
215178 Wp = 76
03653
YDOT = 2463
797424 meter/sec RA = 56
90978 deg
ZDOT = -4433
072406 TA = 146
70895
MA = 146
69495
Ha = 219
506 n
mi
Hp = 215
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1123740
06 X = -260872
02
Y = -18778283
21 feet Y = -5726994
59 meter
Z = -11897837
63 Z = -3627926
24
XDOT = 18852
412002 XDOT = 5739
770933
YDOT = 8083
324881 feet/sec YDOT = 2528
019261 meter/sec
ZDOT = -14544
200808 ZDOT = -4405
174892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13999345
76 X = -4267000
59
Y = 12560973
67 feet Y = 3828584
78 meter
Z = -11903172
32 Z = -3628086
92
XDOT = -4625
859498 XDOT = -1409
961975
YDOT = -18817
531640 feet/sec YDOT = -5735
583644 meter/sec
ZDOT = -14422
699566 ZDOT = -4396
038828
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 16241
44809921
00016717 00000-0 10270-3 0 9042
2 25544 51
6405 57
4598 0003236 265
0647 95
0137 15
54331070 16220
Satellite: ISS
Catalog Number: 25544
Epoch time: 16241
44809921 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 57
4598 deg
Eccentricity:
0003236
Arg of perigee: 265
0647 deg
Mean anomaly: 95
0137 deg
Mean motion: 15
54331070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 296
Coasting Arc #6 (Orbit 1637)
---------------------------------------
Vector Time (GMT): 2016/242/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -941113
27 A = 6779418
24 meter
Y = 4782978
09 meter E =
0005253
Z = 4709746
07 I = 51
92416
XDOT = -5922
996006 Wp = 132
35157
YDOT = -3962
160959 meter/sec RA = 51
93882 deg
ZDOT = 2834
760433 TA = 289
61481
MA = 289
67150
Ha = 219
583 n
mi
Hp = 215
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3087641
96 X = -1017405
32
Y = 15692185
33 feet Y = 4772027
59 meter
Z = 15451922
82 Z = 4704988
92
XDOT = -19432
401593 XDOT = -5892
019719
YDOT = -12999
215746 feet/sec YDOT = -4028
222524 meter/sec
ZDOT = 9300
395120 ZDOT = 2806
063932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14111311
53 X = 4301127
75
Y = -7570940
49 feet Y = -2307622
66 meter
Z = 15430226
15 Z = 4703132
93
XDOT = 1896
041717 XDOT = 577
913515
YDOT = 22271
387804 feet/sec YDOT = 6788
319003 meter/sec
ZDOT = 9175
685326 ZDOT = 2796
748887
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 16242
47679482
00016717 00000-0 10270-3 0 9054
2 25544 51
6409 52
3292 0003209 270
3205 89
7580 15
54308455 16388
Satellite: ISS
Catalog Number: 25544
Epoch time: 16242
47679482 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 52
3292 deg
Eccentricity:
0003209
Arg of perigee: 270
3205 deg
Mean anomaly: 89
7580 deg
Mean motion: 15
54308455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1638
Checksum: 316
Coasting Arc #7 (Orbit 1652)
---------------------------------------
Vector Time (GMT): 2016/243/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2327530
99 A = 6776956
30 meter
Y = -3572062
75 meter E =
0011421
Z = -5277789
27 I = 51
89434
XDOT = 5689
342799 Wp = 80
41923
YDOT = 5048
768390 meter/sec RA = 46
95703 deg
ZDOT = -907
850618 TA = 180
91745
MA = 180
91954
Ha = 219
507 n
mi
Hp = 215
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7636256
54 X = 2392938
50
Y = -11719365
98 feet Y = -3545669
39 meter
Z = -17315581
61 Z = -5266323
80
XDOT = 18665
822832 XDOT = 5636
873219
YDOT = 16564
200754 feet/sec YDOT = 5112
096993 meter/sec
ZDOT = -2978
512525 ZDOT = -880
341489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13939124
08 X = -4248645
02
Y = 1764472
28 feet Y = 537811
15 meter
Z = -17264784
29 Z = -5262306
25
XDOT = 510
378394 XDOT = 155
563334
YDOT = -23950
250361 feet/sec YDOT = -7300
036310 meter/sec
ZDOT = -2859
203869 ZDOT = -871
485339
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 16243
44118971
00016717 00000-0 10270-3 0 9064
2 25544 51
6396 47
5191 0003115 272
6745 87
4051 15
54351949 16538
Satellite: ISS
Catalog Number: 25544
Epoch time: 16243
44118971 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 47
5191 deg
Eccentricity:
0003115
Arg of perigee: 272
6745 deg
Mean anomaly: 87
4051 deg
Mean motion: 15
54351949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 316
Coasting Arc #8 (Orbit 1668)
---------------------------------------
Vector Time (GMT): 2016/244/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3685666
84 A = 6777212
28 meter
Y = 2215112
72 meter E =
0002465
Z = 5238614
59 I = 51
87208
XDOT = -5015
238442 Wp = 2
20731
YDOT = -5692
605768 meter/sec RA = 41
97175 deg
ZDOT = -1119
009738 TA = 98
49668
MA = 98
46874
Ha = 219
664 n
mi
Hp = 215
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12092082
81 X = -3735609
39
Y = 7267430
17 feet Y = 2173618
33 meter
Z = 17187055
73 Z = 5220589
34
XDOT = -16454
194362 XDOT = -4945
773960
YDOT = -18676
528110 feet/sec YDOT = -5748
301221 meter/sec
ZDOT = -3671
291790 ZDOT = -1143
202892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13542586
38 X = 4127780
33
Y = 4283582
72 feet Y = 1305636
01 meter
Z = 17107839
31 Z = 5214469
42
XDOT = -2717
076504 XDOT = -828
164918
YDOT = 23702
458992 feet/sec YDOT = 7224
509501 meter/sec
ZDOT = -3775
975379 ZDOT = -1150
917296
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 16244
46987552
00016717 00000-0 10270-3 0 9077
2 25544 51
6395 42
3895 0003168 275
3568 84
7224 15
54326081 16690
Satellite: ISS
Catalog Number: 25544
Epoch time: 16244
46987552 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 42
3895 deg
Eccentricity:
0003168
Arg of perigee: 275
3568 deg
Mean anomaly: 84
7224 deg
Mean motion: 15
54326081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1669
Checksum: 341
Coasting Arc #9 (Orbit 1683)
---------------------------------------
Vector Time (GMT): 2016/245/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4894913
27 A = 6779727
40 meter
Y = -854801
14 meter E =
0007085
Z = -4619389
26 I = 51
85621
XDOT = 3873
258753 Wp = 115
14609
YDOT = 5882
999631 meter/sec RA = 36
98753 deg
ZDOT = 3016
331722 TA = 184
88660
MA = 184
89352
Ha = 219
529 n
mi
Hp = 215
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16059426
75 X = 4926546
77
Y = -2804465
68 feet Y = -799886
55 meter
Z = -15155476
58 Z = -4595534
41
XDOT = 12707
541842 XDOT = 3792
533856
YDOT = 19301
179891 feet/sec YDOT = 5925
861957 meter/sec
ZDOT = 9896
101450 ZDOT = 3034
950099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13010811
94 X = -3965695
48
Y = -9982168
33 feet Y = -3042564
91 meter
Z = -15051038
95 Z = -4587556
67
XDOT = 4901
961787 XDOT = 1494
117953
YDOT = -21428
156288 feet/sec YDOT = -6531
302037 meter/sec
ZDOT = 9976
371315 ZDOT = 3040
797977
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 16245
43426353
00016717 00000-0 10270-3 0 9083
2 25544 51
6395 37
5792 0003109 277
6832 82
3967 15
54364460 16844
Satellite: ISS
Catalog Number: 25544
Epoch time: 16245
43426353 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 37
5792 deg
Eccentricity:
0003109
Arg of perigee: 277
6832 deg
Mean anomaly: 82
3967 deg
Mean motion: 15
54364460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1684
Checksum: 331
Coasting Arc #10 (Orbit 1699)
---------------------------------------
Vector Time (GMT): 2016/246/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5814947
32 A = 6783649
22 meter
Y = -429463
61 meter E =
0009243
Z = 3459853
97 I = 51
84371
XDOT = -2314
349246 Wp = 84
88525
YDOT = -5695
626852 meter/sec RA = 32
01242 deg
ZDOT = -4585
367521 TA = 54
65094
MA = 54
56459
Ha = 219
569 n
mi
Hp = 215
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19077911
15 X = -5826519
07
Y = -1409001
33 feet Y = -494554
54 meter
Z = 11351226
93 Z = 3431578
66
XDOT = -7593
009337 XDOT = -2228
213793
YDOT = -18686
439803 feet/sec YDOT = -5721
026371 meter/sec
ZDOT = -15043
856695 ZDOT = -4596
400061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12197017
81 X = 3717651
03
Y = 14831500
86 feet Y = 4520641
46 meter
Z = 11227718
83 Z = 3422208
70
XDOT = -7270
457882 XDOT = -2216
035562
YDOT = 17431
621501 feet/sec YDOT = 5313
158234 meter/sec
ZDOT = -15090
996021 ZDOT = -4599
735587
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 16246
46293813
00016717 00000-0 10270-3 0 9091
2 25544 51
6402 32
4493 0003263 282
7938 77
2850 15
54373554 17007
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
46293813 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 32
4493 deg
Eccentricity:
0003263
Arg of perigee: 282
7938 deg
Mean anomaly: 77
2850 deg
Mean motion: 15
54373554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1700
Checksum: 312
Coasting Arc #11 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2016/246/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 425244
16 A = 6777498
81 meter
Y = -4416962
88 meter E =
0011001
Z = -5132734
19 I = 51
81595
XDOT = 7026
364300 Wp = 70
16741
YDOT = 2577
053386 meter/sec RA = 30
03341 deg
ZDOT = -1634
754630 TA = 184
07507
MA = 184
08403
Ha = 219
605 n
mi
Hp = 215
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1395158
01 X = 499536
54
Y = -14491348
04 feet Y = -4411792
73 meter
Z = -16839679
12 Z = -5130487
52
XDOT = 23052
376312 XDOT = 7004
965682
YDOT = 8454
899559 feet/sec YDOT = 2655
507058 meter/sec
ZDOT = -5363
368210 ZDOT = -1600
674914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14528443
18 X = 4428269
48
Y = -1108562
33 feet Y = -337889
80 meter
Z = -16829018
24 Z = -5129484
76
XDOT = -4276
067876 XDOT = -1303
345489
YDOT = 23165
926343 feet/sec YDOT = 7060
974349 meter/sec
ZDOT = -5214
902977 ZDOT = -1589
502428
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 16246
84869088
00016717 00000-0 10270-3 0 9108
2 25544 51
6440 30
5288 0003011 286
0928 73
9893 15
54366304 17068
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
84869088 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 30
5288 deg
Eccentricity:
0003011
Arg of perigee: 286
0928 deg
Mean anomaly: 73
9893 deg
Mean motion: 15
54366304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 320
Coasting Arc #12 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2016/247/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2168082
10 A = 6776666
07 meter
Y = 3604793
06 meter E =
0001948
Z = 5313259
16 I = 51
78317
XDOT = -6804
224267 Wp = 355
23449
YDOT = -3516
775532 meter/sec RA = 25
04260 deg
ZDOT = -388
623310 TA = 98
47450
MA = 98
45242
Ha = 219
769 n
mi
Hp = 215
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7113130
24 X = -2234040
05
Y = 11826748
89 feet Y = 3580179
96 meter
Z = 17431952
64 Z = 5302566
59
XDOT = -22323
570429 XDOT = -6762
505332
YDOT = -11537
977466 feet/sec YDOT = -3592
631708 meter/sec
ZDOT = -1275
010861 ZDOT = -421
574581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13012671
42 X = -3966262
25
Y = -4773887
41 feet Y = -1455080
88 meter
Z = 17384532
36 Z = 5298805
46
XDOT = 6604
818890 XDOT = 2013
148798
YDOT = -23191
054021 feet/sec YDOT = -7068
633266 meter/sec
ZDOT = -1418
351067 ZDOT = -432
313405
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 16247
87735989
00016717 00000-0 10270-3 0 9115
2 25544 51
6423 25
3995 0002884 292
1040 67
9806 15
54383644 17227
Satellite: ISS
Catalog Number: 25544
Epoch time: 16247
87735989 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 25
3995 deg
Eccentricity:
0002884
Arg of perigee: 292
1040 deg
Mean anomaly: 67
9806 deg
Mean motion: 15
54383644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 336
Coasting Arc #13 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2016/248/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3828568
42 A = 6778563
71 meter
Y = -2713097
62 meter E =
0008784
Z = -4899979
17 I = 51
76081
XDOT = 5978
561512 Wp = 103
87740
YDOT = 4166
696535 meter/sec RA = 20
05171 deg
ZDOT = 2365
731286 TA = 189
26367
MA = 189
27988
Ha = 219
715 n
mi
Hp = 215
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12560920
00 X = 3882424
35
Y = -8901238
91 feet Y = -2669983
45 meter
Z = -16076047
16 Z = -4881249
87
XDOT = 19614
703125 XDOT = 5920
032439
YDOT = 13670
264222 feet/sec YDOT = 4233
225837 meter/sec
ZDOT = 7761
585583 ZDOT = 2394
630917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11388839
59 X = 3471318
31
Y = 10485450
13 feet Y = 3195965
20 meter
Z = -15993677
69 Z = -4874872
96
XDOT = -8440
374891 XDOT = -2572
626267
YDOT = 21190
346085 feet/sec YDOT = 6458
817487 meter/sec
ZDOT = 7887
080797 ZDOT = 2403
982227
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 16248
84173150
00016717 00000-0 10270-3 0 9120
2 25544 51
6434 20
5912 0003140 295
7000 64
3829 15
54369249 17373
Satellite: ISS
Catalog Number: 25544
Epoch time: 16248
84173150 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 20
5912 deg
Eccentricity:
0003140
Arg of perigee: 295
7000 deg
Mean anomaly: 64
3829 deg
Mean motion: 15
54369249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 297
Coasting Arc #14 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2016/249/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5246245
96 A = 6782096
17 meter
Y = 1779206
45 meter E =
0009163
Z = 3907978
21 I = 51
74166
XDOT = -4603
335575 Wp = 67
90584
YDOT = -4575
585529 meter/sec RA = 15
06611 deg
ZDOT = -4085
541950 TA = 64
86191
MA = 64
76689
Ha = 219
819 n
mi
Hp = 215
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17212093
04 X = -5284734
86
Y = 5837291
50 feet Y = 1720324
64 meter
Z = 12821450
82 Z = 3882399
58
XDOT = -15102
807005 XDOT = -4531
982281
YDOT = -15011
763545 feet/sec YDOT = -4626
664599 meter/sec
ZDOT = -13404
009023 ZDOT = -4107
729990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9645609
72 X = -2939981
84
Y = -15496926
22 feet Y = -4723463
11 meter
Z = 12709335
57 Z = 3873805
48
XDOT = 10043
173361 XDOT = 3061
159240
YDOT = -17352
710304 feet/sec YDOT = -5289
106101 meter/sec
ZDOT = -13500
084457 ZDOT = -4114
825743
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 16249
87038792
00016717 00000-0 10270-3 0 9137
2 25544 51
6425 15
4614 0003119 302
9833 57
1020 15
54426654 17531
Satellite: ISS
Catalog Number: 25544
Epoch time: 16249
87038792 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 15
4614 deg
Eccentricity:
0003119
Arg of perigee: 302
9833 deg
Mean anomaly: 57
1020 deg
Mean motion: 15
54426654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 302
Coasting Arc #15 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2016/250/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6250178
28 A = 6785953
62 meter
Y = -879206
96 meter E =
0005707
Z = -2484667
16 I = 51
72233
XDOT = 2783
475662 Wp = 16
10781
YDOT = 4763
163679 meter/sec RA = 10
09088 deg
ZDOT = 5324
653610 TA = 316
07756
MA = 316
12291
Ha = 219
902 n
mi
Hp = 215
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20505834
25 X = 6271614
73
Y = -2884537
28 feet Y = -809193
67 meter
Z = -8151795
15 Z = -2454253
16
XDOT = 9132
137999 XDOT = 2704
140964
YDOT = 15627
177423 feet/sec YDOT = 4793
847313 meter/sec
ZDOT = 17469
335992 ZDOT = 5337
981888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7850450
73 X = 2392817
38
Y = 19218009
98 feet Y = 5857649
44 meter
Z = -8018732
67 Z = -2444109
72
XDOT = -11530
646351 XDOT = -3514
541008
YDOT = 12011
691012 feet/sec YDOT = 3661
163420 meter/sec
ZDOT = 17526
652729 ZDOT = 5342
123752
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 16250
83474979
00016717 00000-0 10270-3 0 9147
2 25544 51
6417 10
6535 0003017 306
7399 53
3477 15
54416941 17685
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
83474979 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 10
6535 deg
Eccentricity:
0003017
Arg of perigee: 306
7399 deg
Mean anomaly: 53
3477 deg
Mean motion: 15
54416941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 326
Coasting Arc #16 (Orbit 1768)
---------------------------------------
Vector Time (GMT): 2016/250/21:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 909722
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2231785
18 A = 6778724
97 meter
Y = -4240792
71 meter E =
0010053
Z = -4803902
21 I = 51
69534
XDOT = 7160
692118 Wp = 56
53101
YDOT = -830
233047 meter/sec RA = 9
88842 deg
ZDOT = -2592
283512 TA = 187
91585
MA = 187
93173
Ha = 219
855 n
mi
Hp = 215
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7322129
85 X = -2160862
36
Y = -13913361
91 feet Y = -4265353
95 meter
Z = -15760834
02 Z = -4814571
00
XDOT = 23493
084378 XDOT = 7182
036016
YDOT = -2723
861703 feet/sec YDOT = -750
038307 meter/sec
ZDOT = -8504
867166 ZDOT = -2557
446684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8026446
24 X = 2446460
81
Y = -13465722
80 feet Y = -4104352
31 meter
Z = -15806631
03 Z = -4817861
14
XDOT = 13735
294208 XDOT = 4186
517675
YDOT = 17997
389401 feet/sec YDOT = 5485
604290 meter/sec
ZDOT = -8352
489231 ZDOT = -2545
838718
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 16250
89904110
00016717 00000-0 10270-3 0 9159
2 25544 51
6404 10
3319 0003150 307
2860 52
8005 15
54395823 17692
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
89904110 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 10
3319 deg
Eccentricity:
0003150
Arg of perigee: 307
2860 deg
Mean anomaly: 52
8005 deg
Mean motion: 15
54395823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1769
Checksum: 285
Coasting Arc #17 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2016/250/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894613
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1935081
29 A = 6778228
10 meter
Y = 4260384
02 meter E =
0003311
Z = 4901980
93 I = 51
69314
XDOT = -7280
706669 Wp = 117
22075
YDOT = 621
012227 meter/sec RA = 9
72466 deg
ZDOT = 2331
674344 TA = 309
97189
MA = 310
00096
Ha = 219
733 n
mi
Hp = 215
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6348691
91 X = 1863485
02
Y = 13977637
85 feet Y = 4281623
56 meter
Z = 16082614
59 Z = 4911206
76
XDOT = -23886
832904 XDOT = -7298
436158
YDOT = 2037
441688 feet/sec YDOT = 539
495586 meter/sec
ZDOT = 7649
850210 ZDOT = 2296
263313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5826588
80 X = -1775944
27
Y = 14158368
80 feet Y = 4315470
81 meter
Z = 16122102
75 Z = 4914016
92
XDOT = -16939
192794 XDOT = -5163
065964
YDOT = -15515
549031 feet/sec YDOT = -4729
139345 meter/sec
ZDOT = 7495
004100 ZDOT = 2284
477250
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 16250
96333132
00016717 00000-0 10270-3 0 9168
2 25544 51
6407 10
0117 0003319 305
9294 54
1551 15
54419779 17701
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
96333132 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 10
0117 deg
Eccentricity:
0003319
Arg of perigee: 305
9294 deg
Mean anomaly: 54
1551 deg
Mean motion: 15
54419779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 293
Coasting Arc #18 (Orbit 1784)
---------------------------------------
Vector Time (GMT): 2016/251/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894613
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -34050
97 A = 6776568
60 meter
Y = -4219808
70 meter E =
0012632
Z = -5313039
15 I = 51
65570
XDOT = 7643
807501 Wp = 77
14331
YDOT = 364
716405 meter/sec RA = 4
72557 deg
ZDOT = -336
589501 TA = 189
63278
MA = 189
65702
Ha = 219
887 n
mi
Hp = 215
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -111715
78 X = 38947
05
Y = -13844516
73 feet Y = -4219781
79 meter
Z = -17431230
79 Z = -5313026
88
XDOT = 25078
108599 XDOT = 7640
796055
YDOT = 1196
576132 feet/sec YDOT = 450
177713 meter/sec
ZDOT = -1104
296264 ZDOT = -299
465065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9868579
03 X = 3007942
89
Y = -9712088
01 feet Y = -2960244
43 meter
Z = -17430359
30 Z = -5312773
51
XDOT = 16035
662457 XDOT = 4887
669917
YDOT = 17997
145993 feet/sec YDOT = 5485
530099 meter/sec
ZDOT = -942
164619 ZDOT = -287
171776
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 16251
92768699
00016717 00000-0 10270-3 0 9176
2 25544 51
6410 5
2022 0003275 310
6319 49
4548 15
54408271 17852
Satellite: ISS
Catalog Number: 25544
Epoch time: 16251
92768699 = yrday
fracday
Element set: 917
Inclination: 51
6410 deg
RA of node: 5
2022 deg
Eccentricity:
0003275
Arg of perigee: 310
6319 deg
Mean anomaly: 49
4548 deg
Mean motion: 15
54408271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1785
Checksum: 312
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