[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 18th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
270/16:51:48
844 -0
9 1
4 1
4
N/A -0
9 0
0 220
6
000/00:03:37
689 -0
6 0
0 215
8
274/01:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 215
6
Coasting Arc #1 (Orbit 3625)
---------------------------------------
Vector Time (GMT): 2017/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3397536
81 A = 6788442
31 meter
Y = 5752783
98 meter E =
0006060
Z = -1182331
90 I = 51
31309
XDOT = -3666
673571 Wp = 160
69671
YDOT = -3361
564134 meter/sec RA = 292
41889 deg
ZDOT = -5833
797795 TA = 32
20288
MA = 32
16589
Ha = 219
681 n
mi
Hp = 215
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11146774
31 X = -3455870
30
Y = 18873963
17 feet Y = 5714464
10 meter
Z = -3879041
67 Z = -1198978
36
XDOT = -12029
768935 XDOT = -3600
473571
YDOT = -11028
753720 feet/sec YDOT = -3402
197924 meter/sec
ZDOT = -19139
756544 ZDOT = -5851
448074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12179115
73 X = 3712194
48
Y = -18208848
10 feet Y = -5550056
90 meter
Z = -3953608
28 Z = -1205059
80
XDOT = 9927
905616 XDOT = 3026
025632
YDOT = 10802
998737 feet/sec YDOT = 3292
754015 meter/sec
ZDOT = -19217
329371 ZDOT = -5857
441992
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 17261
52983304
00016717 00000-0 10270-3 0 9008
2 25544 51
6409 293
0091 0003944 292
4893 67
5842 15
54220914 36260
Satellite: ISS
Catalog Number: 25544
Epoch time: 17261
52983304 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 293
0091 deg
Eccentricity:
0003944
Arg of perigee: 292
4893 deg
Mean anomaly: 67
5842 deg
Mean motion: 15
54220914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 312
Coasting Arc #2 (Orbit 3641)
---------------------------------------
Vector Time (GMT): 2017/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3853729
64 A = 6785788
86 meter
Y = -4834912
80 meter E =
0010662
Z = 2781929
24 I = 51
29059
XDOT = 2682
994396 Wp = 66
97368
YDOT = 5073
565261 meter/sec RA = 287
42039 deg
ZDOT = 5089
538539 TA = 324
75060
MA = 324
82107
Ha = 219
797 n
mi
Hp = 215
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12643469
95 X = 3893995
28
Y = -15862574
82 feet Y = -4791592
26 meter
Z = 9127064
45 Z = 2800747
87
XDOT = 8802
475051 XDOT = 2601
338596
YDOT = 16645
555318 feet/sec YDOT = 5103
112447 meter/sec
ZDOT = 16697
961087 ZDOT = 5102
372662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13205208
26 X = -4024947
48
Y = 15347974
52 feet Y = 4678062
63 meter
Z = 9211084
11 Z = 2807538
44
XDOT = -6903
561595 XDOT = -2104
205574
YDOT = -16017
052259 feet/sec YDOT = -4881
997528 meter/sec
ZDOT = 16753
963878 ZDOT = 5106
608190
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 17262
55861103
00016717 00000-0 10270-3 0 9015
2 25544 51
6390 287
8798 0003835 298
6407 61
4360 15
54196812 36427
Satellite: ISS
Catalog Number: 25544
Epoch time: 17262
55861103 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 287
8798 deg
Eccentricity:
0003835
Arg of perigee: 298
6407 deg
Mean anomaly: 61
4360 deg
Mean motion: 15
54196812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3642
Checksum: 326
Coasting Arc #3 (Orbit 3656)
---------------------------------------
Vector Time (GMT): 2017/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4133078
15 A = 6781816
70 meter
Y = 3488412
51 meter E =
0005811
Z = -4098060
75 I = 51
27009
XDOT = -1687
990222 Wp = 39
36401
YDOT = -6445
751665 meter/sec RA = 282
41197 deg
ZDOT = -3782
981439 TA = 191
36522
MA = 191
37835
Ha = 219
864 n
mi
Hp = 215
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13559967
69 X = -4151872
92
Y = 11444922
94 feet Y = 3442087
94 meter
Z = -13445081
20 Z = -4118184
15
XDOT = -5538
025664 XDOT = -1597
410746
YDOT = -21147
479216 feet/sec YDOT = -6464
121997 meter/sec
ZDOT = -12411
356426 ZDOT = -3790
960275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13727152
48 X = 4184036
07
Y = -11135869
24 feet Y = -3394212
95 meter
Z = -13534655
32 Z = -4125362
94
XDOT = 4164
245167 XDOT = 1269
261927
YDOT = 20265
619656 feet/sec YDOT = 6176
960871 meter/sec
ZDOT = -12445
676118 ZDOT = -3793
442081
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 17263
52308406
00016717 00000-0 10270-3 0 9026
2 25544 51
6402 283
0715 0003968 300
6177 59
4584 15
54233100 36576
Satellite: ISS
Catalog Number: 25544
Epoch time: 17263
52308406 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 283
0715 deg
Eccentricity:
0003968
Arg of perigee: 300
6177 deg
Mean anomaly: 59
4584 deg
Mean motion: 15
54233100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3657
Checksum: 296
Coasting Arc #4 (Orbit 3672)
---------------------------------------
Vector Time (GMT): 2017/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247860
35 A = 6778492
88 meter
Y = -1821305
89 meter E =
0002193
Z = 4957106
16 I = 51
25162
XDOT = 726
418410 Wp = 117
27320
YDOT = 7347
528234 meter/sec RA = 277
39114 deg
ZDOT = 2075
396282 TA = 312
41531
MA = 312
43386
Ha = 219
873 n
mi
Hp = 215
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13936549
71 X = 4243831
62
Y = -5975413
01 feet Y = -1773825
24 meter
Z = 16263471
64 Z = 4977731
54
XDOT = 2383
262499 XDOT = 634
121082
YDOT = 24106
063761 feet/sec YDOT = 7355
135767 meter/sec
ZDOT = 6809
042921 ZDOT = 2078
699807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13861894
53 X = -4225105
45
Y = 5898738
81 feet Y = 1797935
59 meter
Z = 16355006
83 Z = 4985006
08
XDOT = -1777
216250 XDOT = -541
695513
YDOT = -23108
164376 feet/sec YDOT = -7043
368502 meter/sec
ZDOT = 6822
552168 ZDOT = 2079
513901
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 17264
55185257
00016717 00000-0 10270-3 0 9038
2 25544 51
6389 277
9413 0003926 306
6640 53
4151 15
54227086 36730
Satellite: ISS
Catalog Number: 25544
Epoch time: 17264
55185257 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 277
9413 deg
Eccentricity:
0003926
Arg of perigee: 306
6640 deg
Mean anomaly: 53
4151 deg
Mean motion: 15
54227086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3673
Checksum: 322
Coasting Arc #5 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2017/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4249360
67 A = 6777104
87 meter
Y = -15613
23 meter E =
0012029
Z = -5289603
58 I = 51
24321
XDOT = 204
385736 Wp = 76
47059
YDOT = -7656
141727 meter/sec RA = 272
36457 deg
ZDOT = -139
096407 TA = 192
18055
MA = 192
20966
Ha = 220
070 n
mi
Hp = 215
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13941472
03 X = -4223175
70
Y = -51224
51 feet Y = -62986
78 meter
Z = -17354342
44 Z = -5310182
25
XDOT = 670
556876 XDOT = 290
659228
YDOT = -25118
575219 feet/sec YDOT = -7653
373780 meter/sec
ZDOT = -456
353041 ZDOT = -137
892991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13827025
18 X = 4214477
27
Y = -109971
79 feet Y = -33519
40 meter
Z = -17445393
34 Z = -5317355
89
XDOT = -386
090682 XDOT = -117
680440
YDOT = 24116
513697 feet/sec YDOT = 7350
713375 meter/sec
ZDOT = -449
887571 ZDOT = -137
125732
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 17265
51632000
00016717 00000-0 10270-3 0 9049
2 25544 51
6385 273
1335 0004054 308
6693 51
4097 15
54216881 36884
Satellite: ISS
Catalog Number: 25544
Epoch time: 17265
51632000 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 273
1335 deg
Eccentricity:
0004054
Arg of perigee: 308
6693 deg
Mean anomaly: 51
4097 deg
Mean motion: 15
54216881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 307
Coasting Arc #6 (Orbit 3703)
---------------------------------------
Vector Time (GMT): 2017/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4132896
40 A = 6778128
22 meter
Y = 1875736
25 meter E =
0006092
Z = 5034566
40 I = 51
24603
XDOT = -1119
026335 Wp = 14
58005
YDOT = 7364
902042 meter/sec RA = 267
33578 deg
ZDOT = -1819
059263 TA = 93
16408
MA = 93
09437
Ha = 220
068 n
mi
Hp = 215
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13559371
40 X = 4087158
50
Y = 6153990
33 feet Y = 1921697
98 meter
Z = 16517606
30 Z = 5054531
66
XDOT = -3671
346242 XDOT = -1192
463254
YDOT = 24163
064443 feet/sec YDOT = 7351
977499 meter/sec
ZDOT = -5968
042203 ZDOT = -1824
674459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13623369
32 X = -4152402
97
Y = -5763246
80 feet Y = -1756637
62 meter
Z = 16605669
59 Z = 5061408
09
XDOT = 2510
611472 XDOT = 765
234377
YDOT = -23264
190852 feet/sec YDOT = -7090
925372 meter/sec
ZDOT = -5993
973294 ZDOT = -1826
963060
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 17266
54508142
00016717 00000-0 10270-3 0 9053
2 25544 51
6379 268
0034 0004090 313
1930 46
8881 15
54242051 37047
Satellite: ISS
Catalog Number: 25544
Epoch time: 17266
54508142 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 268
0034 deg
Eccentricity:
0004090
Arg of perigee: 313
1930 deg
Mean anomaly: 46
8881 deg
Mean motion: 15
54242051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3704
Checksum: 294
Coasting Arc #7 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2017/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3916616
96 A = 6781324
33 meter
Y = -3558911
93 meter E =
0005075
Z = -4244599
64 I = 51
25957
XDOT = 2017
219603 Wp = 87
15069
YDOT = -6474
046651 meter/sec RA = 262
31456 deg
ZDOT = 3570
814960 TA = 219
51196
MA = 219
54897
Ha = 220
303 n
mi
Hp = 215
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12849793
16 X = -3855910
71
Y = -11676220
25 feet Y = -3602371
23 meter
Z = -13925851
83 Z = -4263477
78
XDOT = 6618
174551 XDOT = 2072
118691
YDOT = -21240
310536 feet/sec YDOT = -6451
181394 meter/sec
ZDOT = 11715
272179 ZDOT = 3580
748133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13283495
64 X = 4048809
47
Y = 11076150
75 feet Y = 3376010
75 meter
Z = -14008864
37 Z = -4269901
86
XDOT = -4746
369048 XDOT = -1446
693286
YDOT = 20549
937892 feet/sec YDOT = 6263
621069 meter/sec
ZDOT = 11760
168980 ZDOT = 3584
499505
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 17267
50954141
00016717 00000-0 10270-3 0 9065
2 25544 51
6384 263
1952 0004129 319
1083 40
9759 15
54223704 37195
Satellite: ISS
Catalog Number: 25544
Epoch time: 17267
50954141 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 263
1952 deg
Eccentricity:
0004129
Arg of perigee: 319
1083 deg
Mean anomaly: 40
9759 deg
Mean motion: 15
54223704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3719
Checksum: 314
Coasting Arc #8 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2017/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3556500
99 A = 6785114
19 meter
Y = 4952908
10 meter E =
0010566
Z = 2969426
96 I = 51
27686
XDOT = -2923
447540 Wp = 80
27061
YDOT = 5075
981005 meter/sec RA = 257
30324 deg
ZDOT = -4948
297339 TA = 65
59108
MA = 65
48086
Ha = 220
377 n
mi
Hp = 215
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11668310
34 X = 3486427
72
Y = 16249698
50 feet Y = 4992287
79 meter
Z = 9742214
43 Z = 2986532
92
XDOT = -9591
363321 XDOT = -2955
954513
YDOT = 16653
480989 feet/sec YDOT = 5043
106815 meter/sec
ZDOT = -16234
571321 ZDOT = -4962
578141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12609944
15 X = -3843510
98
Y = -15483053
48 feet Y = -4719234
70 meter
Z = 9817192
74 Z = 2992280
35
XDOT = 7282
104347 XDOT = 2219
585405
YDOT = -16299
806624 feet/sec YDOT = -4968
181059 meter/sec
ZDOT = -16298
496573 ZDOT = -4967
781755
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 17268
53829413
00016717 00000-0 10270-3 0 9073
2 25544 51
6372 258
0655 0004324 322
4085 37
6765 15
54273066 37355
Satellite: ISS
Catalog Number: 25544
Epoch time: 17268
53829413 = yrday
fracday
Element set: 907
Inclination: 51
6372 deg
RA of node: 258
0655 deg
Eccentricity:
0004324
Arg of perigee: 322
4085 deg
Mean anomaly: 37
6765 deg
Mean motion: 15
54273066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3735
Checksum: 322
Coasting Arc #9 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2017/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3050595
13 A = 6788069
55 meter
Y = -5895356
70 meter E =
0010588
Z = -1390492
28 I = 51
29488
XDOT = 3797
962930 Wp = 16
40939
YDOT = -3322
719393 meter/sec RA = 252
30348 deg
ZDOT = 5775
964839 TA = 328
35845
MA = 328
42206
Ha = 220
433 n
mi
Hp = 215
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10008514
21 X = -2977690
54
Y = -19341721
47 feet Y = -5929063
02 meter
Z = -4561982
54 Z = -1405133
75
XDOT = 12460
508301 XDOT = 3806
779042
YDOT = -10901
310346 feet/sec YDOT = -3280
198223 meter/sec
ZDOT = 18950
015875 ZDOT = 5794
436068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11502714
23 X = 3506027
30
Y = 18476269
76 feet Y = 5631567
02 meter
Z = -4625932
55 Z = -1409984
24
XDOT = -10071
384810 XDOT = -3069
758090
YDOT = 11018
423586 feet/sec YDOT = 3358
415509 meter/sec
ZDOT = 19032
230122 ZDOT = 5801
023741
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 17269
50274804
00016717 00000-0 10270-3 0 9080
2 25544 51
6372 253
2575 0004068 326
3116 33
7777 15
54271171 37508
Satellite: ISS
Catalog Number: 25544
Epoch time: 17269
50274804 = yrday
fracday
Element set: 908
Inclination: 51
6372 deg
RA of node: 253
2575 deg
Eccentricity:
0004068
Arg of perigee: 326
3116 deg
Mean anomaly: 33
7777 deg
Mean motion: 15
54271171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3750
Checksum: 312
Coasting Arc #10 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2017/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2337710
69 A = 6788848
61 meter
Y = 6359836
26 meter E =
0007245
Z = -370409
65 I = 51
30930
XDOT = -4615
481440 Wp = 129
56377
YDOT = 1353
706451 meter/sec RA = 247
30861 deg
ZDOT = -5968
950116 TA = 54
44634
MA = 54
37882
Ha = 220
644 n
mi
Hp = 215
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7669654
48 X = 2268218
85
Y = 20865604
52 feet Y = 6385589
55 meter
Z = -1215254
76 Z = -359222
91
XDOT = -15142
655643 XDOT = -4601
281373
YDOT = 4441
294132 feet/sec YDOT = 1302
171948 meter/sec
ZDOT = -19583
169671 ZDOT = -5991
336538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9677608
54 X = -2949735
08
Y = -20016411
48 feet Y = -6101002
22 meter
Z = -1166644
88 Z = -355593
36
XDOT = 13049
177672 XDOT = 3977
389354
YDOT = -5178
366453 feet/sec YDOT = -1578
366095 meter/sec
ZDOT = -19682
433253 ZDOT = -5999
205656
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 17270
53149274
00016717 00000-0 10270-3 0 9098
2 25544 51
6381 248
1273 0004313 331
0792 29
0121 15
54274200 37666
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
53149274 = yrday
fracday
Element set: 909
Inclination: 51
6381 deg
RA of node: 248
1273 deg
Eccentricity:
0004313
Arg of perigee: 331
0792 deg
Mean anomaly: 29
0121 deg
Mean motion: 15
54274200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 288
Coasting Arc #11 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/270/16:53:37
689
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2414909
08 A = 6779728
26 meter
Y = 4118633
55 meter E =
0010482
Z = -4823115
34 I = 51
28217
XDOT = -4613
855354 Wp = 49
60011
YDOT = -5595
593469 meter/sec RA = 246
30426 deg
ZDOT = -2465
025178 TA = 196
02453
MA = 196
05771
Ha = 220
627 n
mi
Hp = 215
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7922930
06 X = -2437356
69
Y = 13512577
27 feet Y = 4091502
53 meter
Z = -15823869
23 Z = -4834901
16
XDOT = -15137
320716 XDOT = -4538
967021
YDOT = -18358
246291 feet/sec YDOT = -5646
770200 meter/sec
ZDOT = -8087
352947 ZDOT = -2487
255783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11808588
36 X = -3599257
73
Y = -10210187
66 feet Y = -3112065
20 meter
Z = -15876608
94 Z = -4839190
41
XDOT = 20113
672520 XDOT = 6130
647384
YDOT = -10519
176098 feet/sec YDOT = -3206
244875 meter/sec
ZDOT = -8184
949624 ZDOT = -2494
772645
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 17270
72438389
00016717 00000-0 10270-3 0 9109
2 25544 51
6414 247
1670 0004512 316
3499 43
7297 15
54022503 37691
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
72438389 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 247
1670 deg
Eccentricity:
0004512
Arg of perigee: 316
3499 deg
Mean anomaly: 43
7297 deg
Mean motion: 15
54022503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 314
Coasting Arc #12 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2017/271/16:53:37
689
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3346059
12 A = 6777776
02 meter
Y = -2663445
01 meter E =
0002087
Z = 5258193
40 I = 51
28912
XDOT = 4116
011594 Wp = 352
62227
YDOT = 6438
402542 meter/sec RA = 241
28304 deg
ZDOT = 644
091281 TA = 91
21065
MA = 91
18675
Ha = 220
559 n
mi
Hp = 215
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10977884
26 X = 3350051
86
Y = -8738336
65 feet Y = -2626004
40 meter
Z = 17251290
68 Z = 5274457
53
XDOT = 13503
975047 XDOT = 4040
581047
YDOT = 21123
367921 feet/sec YDOT = 6484
008879 meter/sec
ZDOT = 2113
160371 ZDOT = 663
902083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6759231
63 X = 2060213
80
Y = 12193587
48 feet Y = 3716605
46 meter
Z = 17323646
05 Z = 5280247
32
XDOT = -22222
991123 XDOT = -6773
567694
YDOT = 9202
864599 feet/sec YDOT = 2805
033130 meter/sec
ZDOT = 2199
948481 ZDOT = 670
544297
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 17271
75329948
00016717 00000-0 10270-3 0 9114
2 25544 51
6407 242
0389 0004511 318
9157 41
1655 15
54032063 37852
Satellite: ISS
Catalog Number: 25544
Epoch time: 17271
75329948 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 242
0389 deg
Eccentricity:
0004511
Arg of perigee: 318
9157 deg
Mean anomaly: 41
1655 deg
Mean motion: 15
54032063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3785
Checksum: 310
Coasting Arc #13 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2017/272/16:53:37
689
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4230614
05 A = 6778134
29 meter
Y = 1137902
80 meter E =
0011171
Z = -5181458
50 I = 51
30706
XDOT = -3337
269112 Wp = 83
33539
YDOT = -6783
103904 meter/sec RA = 236
26106 deg
ZDOT = 1238
787662 TA = 198
60181
MA = 198
64268
Ha = 220
755 n
mi
Hp = 215
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13879967
34 X = -4217854
81
Y = 3733276
92 feet Y = 1090664
14 meter
Z = -16999535
76 Z = -5201978
73
XDOT = -10949
045643 XDOT = -3267
188065
YDOT = -22254
277901 feet/sec YDOT = -6820
031584 meter/sec
ZDOT = 4064
263982 ZDOT = 1222
746875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1576944
17 X = -480652
58
Y = -14177529
85 feet Y = -4321311
10 meter
Z = -17090522
54 Z = -5209191
27
XDOT = 22639
678815 XDOT = 6900
574103
YDOT = -7318
956149 feet/sec YDOT = -2230
817834 meter/sec
ZDOT = 3994
190148 ZDOT = 1217
429157
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 17272
71790526
00016717 00000-0 10270-3 0 9126
2 25544 51
6408 237
2317 0004605 322
0763 38
0065 15
54028412 38004
Satellite: ISS
Catalog Number: 25544
Epoch time: 17272
71790526 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 237
2317 deg
Eccentricity:
0004605
Arg of perigee: 322
0763 deg
Mean anomaly: 38
0065 deg
Mean motion: 15
54028412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3800
Checksum: 284
Coasting Arc #14 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2017/273/16:53:37
689
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4992764
74 A = 6780522
38 meter
Y = 376036
73 meter E =
0008970
Z = 4571687
02 I = 51
33495
XDOT = 2266
528642 Wp = 34
44187
YDOT = 6676
151923 meter/sec RA = 231
24374 deg
ZDOT = -3014
252148 TA = 85
83873
MA = 85
73623
Ha = 220
789 n
mi
Hp = 215
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16380461
75 X = 4965981
61
Y = 1233716
31 feet Y = 431719
88 meter
Z = 14998973
15 Z = 4595875
34
XDOT = 7436
117591 XDOT = 2206
347505
YDOT = 21903
385574 feet/sec YDOT = 6701
161037 meter/sec
ZDOT = -9889
278700 ZDOT = -3003
388758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3442472
45 X = -1049265
60
Y = 15961483
05 feet Y = 4865060
03 meter
Z = 15105999
51 Z = 4604308
65
XDOT = -21556
561082 XDOT = -6570
439818
YDOT = 4696
763267 feet/sec YDOT = 1431
573444 meter/sec
ZDOT = -9842
089337 ZDOT = -2999
868830
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 17273
74681093
00016717 00000-0 10270-3 0 9139
2 25544 51
6413 232
1034 0004753 326
1221 33
9627 15
54065430 38164
Satellite: ISS
Catalog Number: 25544
Epoch time: 17273
74681093 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 232
1034 deg
Eccentricity:
0004753
Arg of perigee: 326
1221 deg
Mean anomaly: 33
9627 deg
Mean motion: 15
54065430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3816
Checksum: 287
Coasting Arc #15 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2017/274/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3481072
07 A = 6788933
03 meter
Y = -5670443
20 meter E =
0014129
Z = 1304972
65 I = 51
36941
XDOT = 4758
217037 Wp = 42
35171
YDOT = -1578
433704 meter/sec RA = 229
43673 deg
ZDOT = 5807
565745 TA = 331
91106
MA = 331
98722
Ha = 220
847 n
mi
Hp = 215
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11420840
11 X = -3423743
88
Y = -18603816
27 feet Y = -5709050
26 meter
Z = 4281406
33 Z = 1288202
38
XDOT = 15610
948285 XDOT = 4747
303438
YDOT = -5178
588269 feet/sec YDOT = -1525
284558 meter/sec
ZDOT = 19053
693388 ZDOT = 5830
653419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19990976
04 X = -6093249
50
Y = -8804671
79 feet Y = -2683663
96 meter
Z = 4207925
93 Z = 1282575
82
XDOT = 9160
126721 XDOT = 2792
006624
YDOT = -11600
697329 feet/sec YDOT = -3535
892546 meter/sec
ZDOT = 19156
113137 ZDOT = 5838
783284
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 17274
13265078
00016717 00000-0 10270-3 0 9145
2 25544 51
6407 230
1751 0004162 325
6916 34
3967 15
54026556 38225
Satellite: ISS
Catalog Number: 25544
Epoch time: 17274
13265078 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 230
1751 deg
Eccentricity:
0004162
Arg of perigee: 325
6916 deg
Mean anomaly: 34
3967 deg
Mean motion: 15
54026556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 304
Coasting Arc #16 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2017/275/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2483893
39 A = 6786190
02 meter
Y = 5633525
22 meter E =
0002310
Z = -2857550
19 I = 51
38186
XDOT = -5768
284622 Wp = 55
82133
YDOT = -14
209920 meter/sec RA = 224
44487 deg
ZDOT = -5043
688297 TA = 156
78213
MA = 156
77170
Ha = 220
919 n
mi
Hp = 215
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8149256
51 X = 2434593
83
Y = 18482694
28 feet Y = 5661025
84 meter
Z = -9375164
66 Z = -2845604
52
XDOT = -18924
818315 XDOT = -5743
197144
YDOT = -46
620473 feet/sec YDOT = -78
575099 meter/sec
ZDOT = -16547
533783 ZDOT = -5071
648013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17436036
67 X = 5314503
98
Y = 10245973
75 feet Y = 3122972
80 meter
Z = -9323021
44 Z = -2841656
93
XDOT = -14578
645110 XDOT = -4443
571030
YDOT = 9644
540526 feet/sec YDOT = 2939
655952 meter/sec
ZDOT = -16671
319024 ZDOT = -5081
418038
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 17275
09724436
00016717 00000-0 10270-3 0 9150
2 25544 51
6403 225
3679 0004146 327
9114 32
1786 15
54030860 38377
Satellite: ISS
Catalog Number: 25544
Epoch time: 17275
09724436 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 225
3679 deg
Eccentricity:
0004146
Arg of perigee: 327
9114 deg
Mean anomaly: 32
1786 deg
Mean motion: 15
54030860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 311
Coasting Arc #17 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2017/276/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1224117
85 A = 6782360
67 meter
Y = -5251872
44 meter E =
0008338
Z = 4105380
16 I = 51
39426
XDOT = 6514
168785 Wp = 81
96774
YDOT = 1445
174552 meter/sec RA = 219
44494 deg
ZDOT = 3785
659934 TA = 328
84947
MA = 328
89887
Ha = 220
927 n
mi
Hp = 215
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4016134
67 X = -1185241
07
Y = -17230552
62 feet Y = -5265343
47 meter
Z = 13469095
00 Z = 4099528
83
XDOT = 21371
944834 XDOT = 6479
135323
YDOT = 4741
386324 feet/sec YDOT = 1517
825029 meter/sec
ZDOT = 12420
144139 ZDOT = 3817
218651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13566247
08 X = -4134992
11
Y = -11386706
04 feet Y = -3470668
00 meter
Z = 13443870
98 Z = 4097691
88
XDOT = 19090
351586 XDOT = 5818
739163
YDOT = -7894
502483 feet/sec YDOT = -2406
244357 meter/sec
ZDOT = 12559
688637 ZDOT = 3828
193097
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 17276
12613752
00016717 00000-0 10270-3 0 9164
2 25544 51
6410 220
2396 0004147 331
0161 29
0761 15
54073565 38539
Satellite: ISS
Catalog Number: 25544
Epoch time: 17276
12613752 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 220
2396 deg
Eccentricity:
0004147
Arg of perigee: 331
0161 deg
Mean anomaly: 29
0761 deg
Mean motion: 15
54073565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 287
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