[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 29th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
273/17:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
5
278/01:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
1
284/02:47:17
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
2
286/10:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 211
9
Coasting Arc #1 (Orbit 2104)
---------------------------------------
Vector Time (GMT): 2016/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3345827
55 A = 6785297
74 meter
Y = -4926537
47 meter E =
0009535
Z = -3249392
80 I = 51
27637
XDOT = 3075
556901 Wp = 41
42725
YDOT = -5194
901442 meter/sec RA = 261
76256 deg
ZDOT = 4724
362951 TA = 280
69843
MA = 280
80578
Ha = 222
847 n
mi
Hp = 213
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10977124
49 X = -3274704
91
Y = -16163180
67 feet Y = -4963555
53 meter
Z = -10660737
55 Z = -3265472
59
XDOT = 10090
409780 XDOT = 3110
470086
YDOT = -17043
639900 feet/sec YDOT = -5160
312646 meter/sec
ZDOT = 15499
878447 ZDOT = 4739
388754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12755117
97 X = 3887759
96
Y = 14750189
34 feet Y = 4495857
71 meter
Z = -10730138
70 Z = -3270546
28
XDOT = -6813
790213 XDOT = -2076
843257
YDOT = 17180
492242 feet/sec YDOT = 5236
614035 meter/sec
ZDOT = 15566
360290 ZDOT = 4744
626617
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 16272
50677776
00016717 00000-0 10270-3 0 9000
2 25544 51
6393 262
6469 0006828 14
4091 345
7255 15
53953784 21056
Satellite: ISS
Catalog Number: 25544
Epoch time: 16272
50677776 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 262
6469 deg
Eccentricity:
0006828
Arg of perigee: 14
4091 deg
Mean anomaly: 345
7255 deg
Mean motion: 15
53953784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2105
Checksum: 330
Coasting Arc #2 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2016/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2845225
21 A = 6788319
01 meter
Y = 5900477
90 meter E =
0014717
Z = 1769844
63 I = 51
29200
XDOT = -3806
775439 Wp = 86
65665
YDOT = 3538
365747 meter/sec RA = 256
76100 deg
ZDOT = -5635
198364 TA = 73
81665
MA = 73
65474
Ha = 222
917 n
mi
Hp = 213
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9334728
37 X = 2770435
92
Y = 19358523
28 feet Y = 5931877
20 meter
Z = 5806576
86 Z = 1783483
56
XDOT = -12489
420732 XDOT = -3818
685935
YDOT = 11608
811505 feet/sec YDOT = 3495
728416 meter/sec
ZDOT = -18488
183609 ZDOT = -5653
720242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11845970
23 X = -3610651
73
Y = -17913086
75 feet Y = -5459908
84 meter
Z = 5865170
47 Z = 1787703
96
XDOT = 9367
862177 XDOT = 2855
324392
YDOT = -12319
296371 feet/sec YDOT = -3754
921534 meter/sec
ZDOT = -18569
651156 ZDOT = -5660
029672
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 16273
53571090
00016717 00000-0 10270-3 0 9017
2 25544 51
6387 257
5177 0006970 16
7888 343
3494 15
54010656 21215
Satellite: ISS
Catalog Number: 25544
Epoch time: 16273
53571090 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 257
5177 deg
Eccentricity:
0006970
Arg of perigee: 16
7888 deg
Mean anomaly: 343
3494 deg
Mean motion: 15
54010656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2121
Checksum: 316
Coasting Arc #3 (Orbit 2123)
---------------------------------------
Vector Time (GMT): 2016/273/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3989315
13 A = 6777771
80 meter
Y = 1508405
84 meter E =
0018429
Z = -5282767
77 I = 51
26162
XDOT = -2207
427520 Wp = 66
12453
YDOT = -7318
485872 meter/sec RA = 255
72107 deg
ZDOT = -416
553946 TA = 199
83946
MA = 199
91122
Ha = 222
918 n
mi
Hp = 213
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13088304
25 X = -3980224
48
Y = 4948838
05 feet Y = 1463844
70 meter
Z = -17331915
24 Z = -5302125
09
XDOT = -7242
216274 XDOT = -2123
402836
YDOT = -24010
780421 feet/sec YDOT = -7342
701059 meter/sec
ZDOT = -1366
646806 ZDOT = -427
071969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3630209
69 X = -1106487
91
Y = -13404111
60 feet Y = -4085573
22 meter
Z = -17416697
79 Z = -5308609
49
XDOT = 23634
533870 XDOT = 7203
805924
YDOT = -4540
859015 feet/sec YDOT = -1384
053828 meter/sec
ZDOT = -1411
381535 ZDOT = -430
189092
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 16273
72863561
00016717 00000-0 10270-3 0 9026
2 25544 51
6421 256
5574 0006946 17
5352 342
6039 15
54008315 21241
Satellite: ISS
Catalog Number: 25544
Epoch time: 16273
72863561 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 256
5574 deg
Eccentricity:
0006946
Arg of perigee: 17
5352 deg
Mean anomaly: 342
6039 deg
Mean motion: 15
54008315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2124
Checksum: 301
Coasting Arc #4 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2016/274/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4430296
91 A = 6778264
79 meter
Y = 223221
46 meter E =
0010958
Z = 5121889
81 I = 51
27248
XDOT = 1342
498626 Wp = 33
84759
YDOT = 7407
776941 meter/sec RA = 250
69686 deg
ZDOT = -1473
593176 TA = 70
46611
MA = 70
34780
Ha = 222
745 n
mi
Hp = 213
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14535094
84 X = 4402591
37
Y = 732353
87 feet Y = 272609
86 meter
Z = 16804100
44 Z = 5143343
94
XDOT = 4404
523051 XDOT = 1266
721343
YDOT = 24303
730120 feet/sec YDOT = 7422
365746 meter/sec
ZDOT = -4834
623280 ZDOT = -1467
256751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1921155
56 X = -585568
21
Y = 14316355
11 feet Y = 4363625
04 meter
Z = 16897758
83 Z = 5150436
89
XDOT = -23542
385700 XDOT = -7175
719161
YDOT = 2556
235730 feet/sec YDOT = 779
140651 meter/sec
ZDOT = -4808
150515 ZDOT = -1465
524277
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 16274
75754892
00016717 00000-0 10270-3 0 9037
2 25544 51
6419 251
4296 0006852 19
6985 340
4431 15
54058957 21401
Satellite: ISS
Catalog Number: 25544
Epoch time: 16274
75754892 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 251
4296 deg
Eccentricity:
0006852
Arg of perigee: 19
6985 deg
Mean anomaly: 340
4431 deg
Mean motion: 15
54058957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2140
Checksum: 332
Coasting Arc #5 (Orbit 2154)
---------------------------------------
Vector Time (GMT): 2016/275/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4762668
71 A = 6780968
69 meter
Y = -1833373
96 meter E =
0012058
Z = -4473678
01 I = 51
29427
XDOT = -324
285811 Wp = 76
02771
YDOT = -6950
843235 meter/sec RA = 245
67750 deg
ZDOT = 3203
928494 TA = 226
33041
MA = 226
43042
Ha = 222
901 n
mi
Hp = 213
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15625553
52 X = -4720082
02
Y = -6015006
44 feet Y = -1886395
85 meter
Z = -14677421
30 Z = -4496710
44
XDOT = -1063
929827 XDOT = -262
099106
YDOT = -22804
603791 feet/sec YDOT = -6954
121449 meter/sec
ZDOT = 10511
576424 ZDOT = 3202
505222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7017924
68 X = 2139063
44
Y = -15104062
97 feet Y = -4603718
39 meter
Z = -14777717
56 Z = -4504248
31
XDOT = 21727
511715 XDOT = 6622
545571
YDOT = -151
693048 feet/sec YDOT = -46
236041 meter/sec
ZDOT = 10506
475444 ZDOT = 3202
373715
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 16275
72214034
00016717 00000-0 10270-3 0 9045
2 25544 51
6431 246
6218 0006856 23
3039 336
8423 15
54049018 21555
Satellite: ISS
Catalog Number: 25544
Epoch time: 16275
72214034 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 246
6218 deg
Eccentricity:
0006856
Arg of perigee: 23
3039 deg
Mean anomaly: 336
8423 deg
Mean motion: 15
54049018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2155
Checksum: 294
Coasting Arc #6 (Orbit 2170)
---------------------------------------
Vector Time (GMT): 2016/276/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4906467
87 A = 6784705
75 meter
Y = 3288383
58 meter E =
0016871
Z = 3330953
80 I = 51
32100
XDOT = -874
733965 Wp = 69
73222
YDOT = 6037
655706 meter/sec RA = 240
66836 deg
ZDOT = -4647
085941 TA = 71
27414
MA = 71
09112
Ha = 222
998 n
mi
Hp = 213
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16097335
55 X = 4853151
08
Y = 10788660
04 feet Y = 3342953
33 meter
Z = 10928326
13 Z = 3354658
61
XDOT = -2869
862089 XDOT = -919
609669
YDOT = 19808
581711 feet/sec YDOT = 6027
622302 meter/sec
ZDOT = -15246
344950 ZDOT = -4651
445056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11548748
87 X = -3520058
65
Y = 15488181
86 feet Y = 4720797
83 meter
Z = 11031334
07 Z = 3362350
62
XDOT = -18521
425788 XDOT = -5645
330580
YDOT = -2879
438176 feet/sec YDOT = -877
652756 meter/sec
ZDOT = -15266
344122 ZDOT = -4653
181688
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 16276
75101951
00016717 00000-0 10270-3 0 9053
2 25544 51
6430 241
4937 0006921 28
4818 331
6712 15
54071176 21711
Satellite: ISS
Catalog Number: 25544
Epoch time: 16276
75101951 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 241
4937 deg
Eccentricity:
0006921
Arg of perigee: 28
4818 deg
Mean anomaly: 331
6712 deg
Mean motion: 15
54071176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2171
Checksum: 298
Coasting Arc #7 (Orbit 2185)
---------------------------------------
Vector Time (GMT): 2016/277/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4819444
83 A = 6787813
91 meter
Y = -4384692
56 meter E =
0013782
Z = -1884458
39 I = 51
34860
XDOT = 2164
280479 Wp = 35
40691
YDOT = -4771
964490 meter/sec RA = 235
66987 deg
ZDOT = 5599
766026 TA = 303
75287
MA = 303
88411
Ha = 222
926 n
mi
Hp = 213
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15811826
88 X = -4760901
84
Y = -14385474
28 feet Y = -4438259
72 meter
Z = -6182606
26 Z = -1907727
71
XDOT = 7100
657739 XDOT = 2190
279222
YDOT = -15656
051476 feet/sec YDOT = -4747
615998 meter/sec
ZDOT = 18371
935782 ZDOT = 5610
343474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14867407
98 X = 4531585
95
Y = -15318536
54 feet Y = -4669089
94 meter
Z = -6283548
20 Z = -1915225
49
XDOT = 14313
731726 XDOT = 4362
825430
YDOT = 6378
755455 feet/sec YDOT = 1944
244663 meter/sec
ZDOT = 18418
889668 ZDOT = 5614
077571
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 16277
71557631
00016717 00000-0 10270-3 0 9061
2 25544 51
6432 236
6860 0006817 30
8451 329
3101 15
54113158 21867
Satellite: ISS
Catalog Number: 25544
Epoch time: 16277
71557631 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 236
6860 deg
Eccentricity:
0006817
Arg of perigee: 30
8451 deg
Mean anomaly: 329
3101 deg
Mean motion: 15
54113158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2186
Checksum: 302
Coasting Arc #8 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2016/278/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1302853
86 A = 6779823
71 meter
Y = 4669530
88 meter E =
0016622
Z = -4755666
57 I = 51
32794
XDOT = -5757
201848 Wp = 58
54135
YDOT = -4298
247191 meter/sec RA = 233
85731 deg
ZDOT = -2641
508055 TA = 185
21939
MA = 185
23674
Ha = 222
904 n
mi
Hp = 213
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4274454
92 X = -1331871
52
Y = 15319983
19 feet Y = 4654798
68 meter
Z = -15602580
60 Z = -4762066
65
XDOT = -18888
457508 XDOT = -5695
878325
YDOT = -14101
860864 feet/sec YDOT = -4362
285516 meter/sec
ZDOT = -8666
365011 ZDOT = -2669
326138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6984780
01 X = 2128960
95
Y = 14257964
95 feet Y = 4345827
72 meter
Z = -15631271
70 Z = -4764411
61
XDOT = -22414
575278 XDOT = -6831
962545
YDOT = 1341
083646 feet/sec YDOT = 408
762295 meter/sec
ZDOT = -8787
192998 ZDOT = -2678
336426
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 16278
10139514
00016717 00000-0 10270-3 0 9072
2 25544 51
6428 234
7586 0006286 34
8673 325
2890 15
54099251 21920
Satellite: ISS
Catalog Number: 25544
Epoch time: 16278
10139514 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 234
7586 deg
Eccentricity:
0006286
Arg of perigee: 34
8673 deg
Mean anomaly: 325
2890 deg
Mean motion: 15
54099251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 326
Coasting Arc #9 (Orbit 2207)
---------------------------------------
Vector Time (GMT): 2016/279/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2567410
84 A = 6777413
28 meter
Y = -3434617
33 meter E =
0007543
Z = 5242082
31 I = 51
34126
XDOT = 5484
983545 Wp = 63
92609
YDOT = 5308
625677 meter/sec RA = 228
83837 deg
ZDOT = 794
208251 TA = 18
47199
MA = 18
44462
Ha = 222
736 n
mi
Hp = 212
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8423263
90 X = 2580162
54
Y = -11268429
57 feet Y = -3405834
98 meter
Z = 17198432
79 Z = 5254585
71
XDOT = 17995
352838 XDOT = 5421
355489
YDOT = 17416
750910 feet/sec YDOT = 5369
606760 meter/sec
ZDOT = 2605
670115 ZDOT = 820
698315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1441184
26 X = -439272
96
Y = -13926651
84 feet Y = -4244843
48 meter
Z = 17253588
80 Z = 5258893
87
XDOT = 24003
813473 XDOT = 7316
362347
YDOT = 876
861737 feet/sec YDOT = 267
267457 meter/sec
ZDOT = 2720
551889 ZDOT = 829
224216
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 16279
13022761
00016717 00000-0 10270-3 0 9082
2 25544 51
6435 229
6297 0006322 38
3914 321
7688 15
54181257 22080
Satellite: ISS
Catalog Number: 25544
Epoch time: 16279
13022761 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 229
6297 deg
Eccentricity:
0006322
Arg of perigee: 38
3914 deg
Mean anomaly: 321
7688 deg
Mean motion: 15
54181257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2208
Checksum: 316
Coasting Arc #10 (Orbit 2222)
---------------------------------------
Vector Time (GMT): 2016/280/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3816906
91 A = 6777578
29 meter
Y = 2104374
52 meter E =
0018618
Z = -5205791
10 I = 51
36361
XDOT = -4787
031239 Wp = 82
04548
YDOT = -5863
138332 meter/sec RA = 223
81966 deg
ZDOT = 1145
824037 TA = 198
96687
MA = 199
03630
Ha = 222
914 n
mi
Hp = 212
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12522660
45 X = -3814866
93
Y = 6904115
89 feet Y = 2061702
24 meter
Z = -17079367
12 Z = -5224328
24
XDOT = -15705
483069 XDOT = -4726
678368
YDOT = -19236
018148 feet/sec YDOT = -5916
332569 meter/sec
ZDOT = 3759
265212 ZDOT = 1122
716547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4296586
47 X = -1309599
56
Y = 13536585
03 feet Y = 4125951
12 meter
Z = -17160676
92 Z = -5230574
33
XDOT = -23653
171336 XDOT = -7209
486623
YDOT = -2893
797557 feet/sec YDOT = -882
029495 meter/sec
ZDOT = 3659
231912 ZDOT = 1115
333887
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 16280
09473930
00016717 00000-0 10270-3 0 9098
2 25544 51
6432 224
8230 0006477 42
2109 317
9542 15
54193530 22232
Satellite: ISS
Catalog Number: 25544
Epoch time: 16280
09473930 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 224
8230 deg
Eccentricity:
0006477
Arg of perigee: 42
2109 deg
Mean anomaly: 317
9542 deg
Mean motion: 15
54193530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2223
Checksum: 294
Coasting Arc #11 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2016/281/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4937440
89 A = 6780003
55 meter
Y = -724929
32 meter E =
0014611
Z = 4582903
36 I = 51
39568
XDOT = 3679
990242 Wp = 57
28643
YDOT = 6029
058192 meter/sec RA = 218
80448 deg
ZDOT = -2996
266792 TA = 62
76901
MA = 62
62021
Ha = 222
804 n
mi
Hp = 212
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16198953
06 X = 4922918
13
Y = -2378377
04 feet Y = -669796
38 meter
Z = 15035772
16 Z = 4606853
39
XDOT = 12073
458799 XDOT = 3626
853086
YDOT = 19780
374647 feet/sec YDOT = 6069
912965 meter/sec
ZDOT = -9830
271628 ZDOT = -2978
519573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9864285
60 X = 3006634
25
Y = -12945949
33 feet Y = -3945925
36 meter
Z = 15140524
02 Z = 4614831
72
XDOT = 21556
143606 XDOT = 6570
312571
YDOT = 4961
693762 feet/sec YDOT = 1512
324259 meter/sec
ZDOT = -9753
667838 ZDOT = -2972
917957
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 16281
12352944
00016717 00000-0 10270-3 0 9106
2 25544 51
6428 219
6941 0006441 46
1377 314
0307 15
54224946 22399
Satellite: ISS
Catalog Number: 25544
Epoch time: 16281
12352944 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 219
6941 deg
Eccentricity:
0006441
Arg of perigee: 46
1377 deg
Mean anomaly: 314
0307 deg
Mean motion: 15
54224946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 299
Coasting Arc #12 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2016/282/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5791814
72 A = 6783668
13 meter
Y = -520925
10 meter E =
0010568
Z = -3498162
54 I = 51
43370
XDOT = -2193
186739 Wp = 70
19367
YDOT = -5794
409290 meter/sec RA = 213
80111 deg
ZDOT = 4508
697774 TA = 248
56204
MA = 248
67480
Ha = 222
808 n
mi
Hp = 212
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19002016
79 X = -5768566
33
Y = -1709071
86 feet Y = -585563
32 meter
Z = -11476911
22 Z = -3526241
62
XDOT = -7195
494549 XDOT = -2150
130801
YDOT = -19010
529167 feet/sec YDOT = -5818
693908 meter/sec
ZDOT = 14792
315532 ZDOT = 4498
148669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14532817
05 X = -4429602
64
Y = 12246032
77 feet Y = 3732590
79 meter
Z = -11599524
55 Z = -3535535
08
XDOT = -17744
662758 XDOT = -5408
573209
YDOT = -7134
657678 feet/sec YDOT = -2174
643660 meter/sec
ZDOT = 14747
113854 ZDOT = 4494
920303
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 16282
08799773
00016717 00000-0 10270-3 0 9118
2 25544 51
6426 214
8867 0006299 49
2648 310
9051 15
54252322 22544
Satellite: ISS
Catalog Number: 25544
Epoch time: 16282
08799773 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 214
8867 deg
Eccentricity:
0006299
Arg of perigee: 49
2648 deg
Mean anomaly: 310
9051 deg
Mean motion: 15
54252322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 326
Coasting Arc #13 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2016/283/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6273163
04 A = 6787129
68 meter
Y = 1657874
97 meter E =
0018184
Z = 1972250
09 I = 51
47273
XDOT = 372
647392 Wp = 94
39690
YDOT = 5263
052365 meter/sec RA = 208
80928 deg
ZDOT = -5566
423280 TA = 63
77977
MA = 63
59295
Ha = 222
868 n
mi
Hp = 212
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20581243
58 X = 6244577
57
Y = 5439222
35 feet Y = 1727866
00 meter
Z = 6470636
77 Z = 2002654
35
XDOT = 1222
596430 XDOT = 340
806509
YDOT = 17267
232170 feet/sec YDOT = 5267
041128 meter/sec
ZDOT = -18262
543569 ZDOT = -5564
690745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18129095
59 X = 5525748
34
Y = -11080379
77 feet Y = -3377299
75 meter
Z = 6603252
55 Z = 2012671
38
XDOT = 12594
566162 XDOT = 3838
823766
YDOT = 9644
795212 feet/sec YDOT = 2939
733581 meter/sec
ZDOT = -18255
778511 ZDOT = -5564
361290
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 16283
11673597
00016717 00000-0 10270-3 0 9129
2 25544 51
6423 209
7574 0006448 53
4507 306
7239 15
54295677 22705
Satellite: ISS
Catalog Number: 25544
Epoch time: 16283
11673597 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 209
7574 deg
Eccentricity:
0006448
Arg of perigee: 53
4507 deg
Mean anomaly: 306
7239 deg
Mean motion: 15
54295677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 328
Coasting Arc #14 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2016/284/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6281329
72 A = 6788803
68 meter
Y = -2541111
93 meter E =
0017841
Z = -267792
43 I = 51
50648
XDOT = 1582
176230 Wp = 48
02695
YDOT = -4514
604156 meter/sec RA = 203
82687 deg
ZDOT = 5996
826790 TA = 309
08092
MA = 309
23948
Ha = 222
894 n
mi
Hp = 212
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20608037
15 X = -6251146
69
Y = -8336981
39 feet Y = -2611185
23 meter
Z = -878584
10 Z = -298232
34
XDOT = 5190
866895 XDOT = 1603
411813
YDOT = -14811
693424 feet/sec YDOT = -4496
791998 meter/sec
ZDOT = 19674
628576 ZDOT = 6004
564608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20106201
47 X = -6128370
21
Y = 9470291
52 feet Y = 2886544
86 meter
Z = -1011239
29 Z = -308225
73
XDOT = -6748
379388 XDOT = -2056
906038
YDOT = -12304
605954 feet/sec YDOT = -3750
443895 meter/sec
ZDOT = 19709
134644 ZDOT = 6007
344239
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 16284
08115161
00016717 00000-0 10270-3 0 9135
2 25544 51
6419 204
9491 0006468 55
8158 304
3607 15
54295625 22857
Satellite: ISS
Catalog Number: 25544
Epoch time: 16284
08115161 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 204
9491 deg
Eccentricity:
0006468
Arg of perigee: 55
8158 deg
Mean anomaly: 304
3607 deg
Mean motion: 15
54295625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 316
Coasting Arc #15 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2016/284/02:47:17
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5460447
89 A = 6787746
55 meter
Y = 3727677
93 meter E =
0010962
Z = -1536887
64 I = 51
50361
XDOT = -3856
547017 Wp = 106
41608
YDOT = 3296
759876 meter/sec RA = 203
66599 deg
ZDOT = -5742
927968 TA = 90
39993
MA = 90
27432
Ha = 222
911 n
mi
Hp = 212
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17914855
29 X = 5425823
82
Y = 12229914
45 feet Y = 3788546
60 meter
Z = -5042282
29 Z = -1510446
30
XDOT = -12652
713311 XDOT = -3865
228664
YDOT = 10816
141326 feet/sec YDOT = 3253
584389 meter/sec
ZDOT = -18841
627192 ZDOT = -5761
683627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19546640
67 X = 5957816
08
Y = -9465103
09 feet Y = -2884963
42 meter
Z = -4927283
28 Z = -1501835
94
XDOT = 2441
062856 XDOT = 744
035958
YDOT = 14827
650172 feet/sec YDOT = 4519
467772 meter/sec
ZDOT = -18924
103194 ZDOT = -5768
066653
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 16284
14544567
00016717 00000-0 10270-3 0 9149
2 25544 51
6411 204
6287 0006524 57
2448 302
9333 15
54341679 22862
Satellite: ISS
Catalog Number: 25544
Epoch time: 16284
14544567 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 204
6287 deg
Eccentricity:
0006524
Arg of perigee: 57
2448 deg
Mean anomaly: 302
9333 deg
Mean motion: 15
54341679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2286
Checksum: 315
Coasting Arc #16 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2016/285/02:47:17
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4400832
22 A = 6784561
62 meter
Y = -4101741
16 meter E =
0019096
Z = 3115524
20 I = 51
52320
XDOT = 5515
686958 Wp = 77
24457
YDOT = -2211
463783 meter/sec RA = 198
68021 deg
ZDOT = 4858
685633 TA = 318
72965
MA = 318
87383
Ha = 222
898 n
mi
Hp = 212
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14438425
92 X = -4369772
42
Y = -13457156
04 feet Y = -4150780
27 meter
Z = 10221536
08 Z = 3094221
70
XDOT = 18096
085821 XDOT = 5516
404575
YDOT = -7255
458605 feet/sec YDOT = -2149
779214 meter/sec
ZDOT = 15940
569663 ZDOT = 4885
481620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18790739
47 X = -5727417
39
Y = 6193034
67 feet Y = 1887636
97 meter
Z = 10129038
62 Z = 3087330
97
XDOT = 2798
248958 XDOT = 852
906283
YDOT = -17887
082794 feet/sec YDOT = -5451
982836 meter/sec
ZDOT = 16058
033643 ZDOT = 4894
488655
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 16285
17412597
00016717 00000-0 10270-3 0 9151
2 25544 51
6412 199
4991 0006449 61
2351 298
9449 15
54377413 23026
Satellite: ISS
Catalog Number: 25544
Epoch time: 16285
17412597 = yrday
fracday
Element set: 915
Inclination: 51
6412 deg
RA of node: 199
4991 deg
Eccentricity:
0006449
Arg of perigee: 61
2351 deg
Mean anomaly: 298
9449 deg
Mean motion: 15
54377413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 331
Coasting Arc #17 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2016/286/02:47:17
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2890045
58 A = 6780401
16 meter
Y = 4295631
46 meter E =
0015334
Z = -4393970
92 I = 51
54154
XDOT = -6780
032998 Wp = 67
82557
YDOT = 1110
276055 meter/sec RA = 193
68531 deg
ZDOT = -3377
811360 TA = 167
89859
MA = 167
86171
Ha = 222
840 n
mi
Hp = 212
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9481776
83 X = 2863140
13
Y = 14093279
07 feet Y = 4327798
98 meter
Z = -14415915
08 Z = -4379997
50
XDOT = -22244
202748 XDOT = -6775
536390
YDOT = 3642
637976 feet/sec YDOT = 1034
481953 meter/sec
ZDOT = -11082
058267 ZDOT = -3410
736529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16935065
32 X = 5161807
91
Y = -1862038
60 feet Y = -567549
36 meter
Z = -14355472
45 Z = -4375548
00
XDOT = -7299
734307 XDOT = -2224
959017
YDOT = 20061
470607 feet/sec YDOT = 6114
736241 meter/sec
ZDOT = -11226
162617 ZDOT = -3421
734366
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 16286
13848737
00016717 00000-0 10270-3 0 9168
2 25544 51
6421 194
6898 0006511 64
6140 295
5687 15
54414768 23170
Satellite: ISS
Catalog Number: 25544
Epoch time: 16286
13848737 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 194
6898 deg
Eccentricity:
0006511
Arg of perigee: 64
6140 deg
Mean anomaly: 295
5687 deg
Mean motion: 15
54414768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 342
Coasting Arc #18 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2016/286/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 907704
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6274072
89 A = 6785733
50 meter
Y = 690970
38 meter E =
0011767
Z = -2489308
32 I = 51
56976
XDOT = -2631
999863 Wp = 57
85816
YDOT = -4862
439677 meter/sec RA = 191
95046 deg
ZDOT = 5308
536775 TA = 274
21563
MA = 274
35010
Ha = 222
775 n
mi
Hp = 211
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20584228
65 X = -6269241
10
Y = 2266963
18 feet Y = 620836
22 meter
Z = -8167022
05 Z = -2519774
80
XDOT = -8635
170155 XDOT = -2603
218018
YDOT = -15952
886079 feet/sec YDOT = -4891
710933 meter/sec
ZDOT = 17416
459236 ZDOT = 5295
821531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20300344
72 X = 6187545
07
Y = -3814517
03 feet Y = -1162664
79 meter
Z = -8300319
52 Z = -2529937
39
XDOT = 9652
456494 XDOT = 2942
068739
YDOT = 13762
758134 feet/sec YDOT = 4194
888679 meter/sec
ZDOT = 17361
598372 ZDOT = 5291
815184
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 16286
45993591
00016717 00000-0 10270-3 0 9173
2 25544 51
6415 193
0881 0006592 63
1273 297
0553 15
54429614 23229
Satellite: ISS
Catalog Number: 25544
Epoch time: 16286
45993591 = yrday
fracday
Element set: 917
Inclination: 51
6415 deg
RA of node: 193
0881 deg
Eccentricity:
0006592
Arg of perigee: 63
1273 deg
Mean anomaly: 297
0553 deg
Mean motion: 15
54429614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2322
Checksum: 326
Coasting Arc #19 (Orbit 2337)
---------------------------------------
Vector Time (GMT): 2016/287/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 907704
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6739475
47 A = 6788096
17 meter
Y = 245944
87 meter E =
0017558
Z = 724573
88 I = 51
61043
XDOT = 476
658804 Wp = 108
59752
YDOT = 4810
438235 meter/sec RA = 186
97315 deg
ZDOT = -5953
584079 TA = 63
56922
MA = 63
38915
Ha = 222
778 n
mi
Hp = 211
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22111140
00 X = 6732704
65
Y = 806905
74 feet Y = 321272
44 meter
Z = 2377210
91 Z = 757296
45
XDOT = 1563
841220 XDOT = 451
752104
YDOT = 15782
277674 feet/sec YDOT = 4815
628531 meter/sec
ZDOT = -19532
756164 ZDOT = -5951
329675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22074752
93 X = -6728384
69
Y = 1248353
22 feet Y = 380498
06 meter
Z = 2520245
56 Z = 768170
85
XDOT = -3057
477431 XDOT = -931
919121
YDOT = -13945
660797 feet/sec YDOT = -4250
637411 meter/sec
ZDOT = -19523
616057 ZDOT = -5950
798174
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 16287
48855162
00016717 00000-0 10270-3 0 9189
2 25544 51
6423 187
9583 0006521 67
5582 292
6261 15
54467216 23386
Satellite: ISS
Catalog Number: 25544
Epoch time: 16287
48855162 = yrday
fracday
Element set: 918
Inclination: 51
6423 deg
RA of node: 187
9583 deg
Eccentricity:
0006521
Arg of perigee: 67
5582 deg
Mean anomaly: 292
6261 deg
Mean motion: 15
54467216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2338
Checksum: 339
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