[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 23rd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 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
237/06:36:20
931 0
5 1
1 1
1
N/A 0
9 -0
1 221
6
000/00:02:41
861 0
3 -0
0 215
1
242/05:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
6
246/10:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 215
8
Coasting Arc #1 (Orbit 3190)
---------------------------------------
Vector Time (GMT): 2017/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -434633
62 A = 6785454
57 meter
Y = 6094627
61 meter E =
0014430
Z = 2942752
89 I = 52
00514
XDOT = -5052
878621 Wp = 101
74386
YDOT = -2805
435228 meter/sec RA = 71
97975 deg
ZDOT = 5040
255700 TA = 291
66504
MA = 291
81865
Ha = 221
883 n
mi
Hp = 213
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1425963
32 X = -517047
21
Y = 19995497
41 feet Y = 6089306
56 meter
Z = 9654701
08 Z = 2940441
20
XDOT = -16577
685763 XDOT = -5045
614552
YDOT = -9204
183820 feet/sec YDOT = -2861
899132 meter/sec
ZDOT = 16536
271981 ZDOT = 5015
728645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11536953
39 X = 3516463
39
Y = -16400269
99 feet Y = -4998802
29 meter
Z = 9643463
67 Z = 2939327
73
XDOT = 8405
311590 XDOT = 2561
938973
YDOT = 15618
362717 feet/sec YDOT = 4760
476956 meter/sec
ZDOT = 16428
057785 ZDOT = 5007
272013
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 17233
55830533
00016717 00000-0 10270-3 0 9005
2 25544 51
6389 72
4440 0004897 168
2794 191
8473 15
54202522 31915
Satellite: ISS
Catalog Number: 25544
Epoch time: 17233
55830533 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 72
4440 deg
Eccentricity:
0004897
Arg of perigee: 168
2794 deg
Mean anomaly: 191
8473 deg
Mean motion: 15
54202522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3191
Checksum: 314
Coasting Arc #2 (Orbit 3205)
---------------------------------------
Vector Time (GMT): 2017/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1429817
14 A = 6781597
27 meter
Y = -5106233
23 meter E =
0008747
Z = -4233557
60 I = 51
98000
XDOT = 5023
201252 Wp = 103
05984
YDOT = 4457
919535 meter/sec RA = 67
01825 deg
ZDOT = -3688
652523 TA = 129
31199
MA = 129
23441
Ha = 221
902 n
mi
Hp = 214
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4691001
10 X = 1507374
29
Y = -16752733
69 feet Y = -5089810
66 meter
Z = -13889624
67 Z = -4226423
42
XDOT = 16480
319068 XDOT = 4990
895620
YDOT = 14625
720260 feet/sec YDOT = 4513
911526 meter/sec
ZDOT = -12101
878356 ZDOT = -3664
330563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12492831
77 X = -3807815
12
Y = 12144506
55 feet Y = 3701645
60 meter
Z = -13857177
41 Z = -4223667
67
XDOT = -6186
611532 XDOT = -1885
679195
YDOT = -20019
264661 feet/sec YDOT = -6101
871869 meter/sec
ZDOT = -11994
848257 ZDOT = -3656
029749
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 17234
52280351
00016717 00000-0 10270-3 0 9011
2 25544 51
6378 67
6343 0004844 168
6149 191
5114 15
54187892 32069
Satellite: ISS
Catalog Number: 25544
Epoch time: 17234
52280351 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 67
6343 deg
Eccentricity:
0004844
Arg of perigee: 168
6149 deg
Mean anomaly: 191
5114 deg
Mean motion: 15
54187892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3206
Checksum: 314
Coasting Arc #3 (Orbit 3221)
---------------------------------------
Vector Time (GMT): 2017/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2448393
88 A = 6778542
04 meter
Y = 3806534
36 meter E =
0009689
Z = 5043877
49 I = 51
95526
XDOT = -4760
050618 Wp = 145
60832
YDOT = -5683
241219 meter/sec RA = 62
04679 deg
ZDOT = 1968
805595 TA = 285
31626
MA = 285
42332
Ha = 221
927 n
mi
Hp = 214
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8032788
33 X = -2515277
91
Y = 12488629
80 feet Y = 3778781
18 meter
Z = 16548154
51 Z = 5031821
38
XDOT = -15616
963970 XDOT = -4705
708685
YDOT = -18645
804524 feet/sec YDOT = -5736
167346 meter/sec
ZDOT = 6459
335943 ZDOT = 1945
815526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13162741
41 X = 4012003
58
Y = -7001394
30 feet Y = -2134024
98 meter
Z = 16494110
97 Z = 5027405
02
XDOT = 4189
673545 XDOT = 1277
012496
YDOT = 22930
679657 feet/sec YDOT = 6989
271159 meter/sec
ZDOT = 6358
417608 ZDOT = 1938
045687
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 17235
55159919
00016717 00000-0 10270-3 0 9021
2 25544 51
6373 62
5049 0004843 172
2962 187
8266 15
54147960 32220
Satellite: ISS
Catalog Number: 25544
Epoch time: 17235
55159919 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 62
5049 deg
Eccentricity:
0004843
Arg of perigee: 172
2962 deg
Mean anomaly: 187
8266 deg
Mean motion: 15
54147960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3222
Checksum: 325
Coasting Arc #4 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2017/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3501713
58 A = 6777166
53 meter
Y = -2291635
75 meter E =
0016049
Z = -5343840
95 I = 51
93473
XDOT = 4176
445272 Wp = 107
89639
YDOT = 6418
173058 meter/sec RA = 57
06692 deg
ZDOT = -20
453698 TA = 161
93778
MA = 161
88070
Ha = 221
771 n
mi
Hp = 214
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11488561
61 X = 3553036
49
Y = -7518490
00 feet Y = -2252190
71 meter
Z = -17532286
57 Z = -5326706
04
XDOT = 13702
248267 XDOT = 4104
464511
YDOT = 21056
998221 feet/sec YDOT = 6464
474443 meter/sec
ZDOT = -67
105310 ZDOT = -
341428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13773516
05 X = -4198167
69
Y = 1214249
00 feet Y = 370103
10 meter
Z = -17455992
30 Z = -5320586
45
XDOT = -2164
079197 XDOT = -659
611339
YDOT = -24017
180722 feet/sec YDOT = -7320
436684 meter/sec
ZDOT = 20
929171 ZDOT = 6
379211
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 17236
51609039
00016717 00000-0 10270-3 0 9032
2 25544 51
6372 57
6954 0004998 175
7508 184
3688 15
54194597 32378
Satellite: ISS
Catalog Number: 25544
Epoch time: 17236
51609039 = yrday
fracday
Element set: 903
Inclination: 51
6372 deg
RA of node: 57
6954 deg
Eccentricity:
0004998
Arg of perigee: 175
7508 deg
Mean anomaly: 184
3688 deg
Mean motion: 15
54194597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 354
Coasting Arc #5 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2017/237/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4773529
64 A = 6779959
86 meter
Y = 70992
87 meter E =
0012814
Z = -4826089
80 I = 51
93298
XDOT = 2519
861277 Wp = 128
32055
YDOT = 6752
289949 meter/sec RA = 53
19736 deg
ZDOT = 2588
665572 TA = 167
12320
MA = 167
09045
Ha = 221
592 n
mi
Hp = 215
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15661186
49 X = 4795823
60
Y = 232916
24 feet Y = 124497
97 meter
Z = -15833627
94 Z = -4802847
51
XDOT = 8267
261408 XDOT = 2431
593730
YDOT = 22153
182248 feet/sec YDOT = 6779
975444 meter/sec
ZDOT = 8492
997282 ZDOT = 2600
691211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5018676
92 X = 1529692
72
Y = -14946222
60 feet Y = -4555608
65 meter
Z = -15730673
80 Z = -4794709
37
XDOT = 22512
181606 XDOT = 6861
712954
YDOT = -1445
144105 feet/sec YDOT = -440
479923 meter/sec
ZDOT = 8545
140135 ZDOT = 2604
558713
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 17237
28768211
00016717 00000-0 10270-3 0 9046
2 25544 51
6422 53
8521 0004482 189
6969 170
4098 15
54007276 32496
Satellite: ISS
Catalog Number: 25544
Epoch time: 17237
28768211 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 53
8521 deg
Eccentricity:
0004482
Arg of perigee: 189
6969 deg
Mean anomaly: 170
4098 deg
Mean motion: 15
54007276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 326
Coasting Arc #6 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2017/238/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5370025
48 A = 6783431
82 meter
Y = -1466231
48 meter E =
0010749
Z = 3865423
31 I = 51
92411
XDOT = -1274
365844 Wp = 104
48819
YDOT = -6319
602680 meter/sec RA = 48
22844 deg
ZDOT = -4160
536849 TA = 29
07963
MA = 29
01981
Ha = 221
649 n
mi
Hp = 215
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17618193
83 X = -5372006
82
Y = -4810470
75 feet Y = -1526293
54 meter
Z = 12681835
00 Z = 3839332
82
XDOT = -4180
990301 XDOT = -1183
393906
YDOT = -20733
604592 feet/sec YDOT = -6333
345179 meter/sec
ZDOT = -13650
055279 ZDOT = -4166
505839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9702314
76 X = -2957265
54
Y = 15566578
09 feet Y = 4744693
00 meter
Z = 12566505
34 Z = 3830270
83
XDOT = -19899
587367 XDOT = -6065
394229
YDOT = -1344
391751 feet/sec YDOT = -409
770606 meter/sec
ZDOT = -13675
427596 ZDOT = -4168
270331
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 17238
31659588
00016717 00000-0 10270-3 0 9058
2 25544 51
6421 48
7245 0004380 191
8076 168
2975 15
54014462 32654
Satellite: ISS
Catalog Number: 25544
Epoch time: 17238
31659588 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 48
7245 deg
Eccentricity:
0004380
Arg of perigee: 191
8076 deg
Mean anomaly: 168
2975 deg
Mean motion: 15
54014462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 326
Coasting Arc #7 (Orbit 3279)
---------------------------------------
Vector Time (GMT): 2017/239/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5713123
29 A = 6786970
55 meter
Y = 2643244
58 meter E =
0002811
Z = -2540548
59 I = 51
91378
XDOT = -198
177552 Wp = 105
45066
YDOT = 5524
097217 meter/sec RA = 43
26714 deg
ZDOT = 5305
891616 TA = 226
15773
MA = 226
18097
Ha = 221
355 n
mi
Hp = 215
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18743842
81 X = 5695481
92
Y = 8672062
28 feet Y = 2707033
81 meter
Z = -8335133
18 Z = -2512839
12
XDOT = -650
188818 XDOT = -285
708086
YDOT = 18123
678534 feet/sec YDOT = 5521
392006 meter/sec
ZDOT = 17407
780894 ZDOT = 5304
715964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13447880
50 X = 4098913
98
Y = -15738948
49 feet Y = -4797231
50 meter
Z = -8212841
37 Z = -2503274
05
XDOT = 16089
652642 XDOT = 4904
126125
YDOT = 4674
292319 feet/sec YDOT = 1424
724299 meter/sec
ZDOT = 17401
629206 ZDOT = 5304
016582
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 17239
28119941
00016717 00000-0 10270-3 0 9060
2 25544 51
6422 43
9168 0004428 197
4853 162
6148 15
54025209 32802
Satellite: ISS
Catalog Number: 25544
Epoch time: 17239
28119941 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 43
9168 deg
Eccentricity:
0004428
Arg of perigee: 197
4853 deg
Mean anomaly: 162
6148 deg
Mean motion: 15
54025209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3280
Checksum: 316
Coasting Arc #8 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2017/240/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5693526
83 A = 6789407
83 meter
Y = -3560045
63 meter E =
0015269
Z = 939140
65 I = 51
89760
XDOT = 1825
052445 Wp = 141
55838
YDOT = -4496
983200 meter/sec RA = 38
31335 deg
ZDOT = -5942
527977 TA = 28
30368
MA = 28
22080
Ha = 221
396 n
mi
Hp = 215
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18679549
97 X = -5657856
18
Y = -11679939
74 feet Y = -3623515
03 meter
Z = 3081170
12 Z = 911570
17
XDOT = 5987
704871 XDOT = 1904
069081
YDOT = -14753
881891 feet/sec YDOT = -4476
132744 meter/sec
ZDOT = -19496
482865 ZDOT = -5933
470290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16059015
73 X = -4894788
00
Y = 15105912
88 feet Y = 4604282
25 meter
Z = 2959661
91 Z = 902104
95
XDOT = -11608
605835 XDOT = -3538
303058
YDOT = -8502
365045 feet/sec YDOT = -2591
520866 meter/sec
ZDOT = -19455
586881 ZDOT = -5930
062881
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 17240
31010839
00016717 00000-0 10270-3 0 9073
2 25544 51
6428 38
7892 0004530 200
3682 159
7290 15
53984367 32962
Satellite: ISS
Catalog Number: 25544
Epoch time: 17240
31010839 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 38
7892 deg
Eccentricity:
0004530
Arg of perigee: 200
3682 deg
Mean anomaly: 159
7290 deg
Mean motion: 15
53984367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 319
Coasting Arc #9 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2017/241/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5299017
70 A = 6789337
22 meter
Y = 4175287
67 meter E =
0009599
Z = 730615
59 I = 51
87162
XDOT = -3459
562038 Wp = 64
52607
YDOT = 3335
469430 meter/sec RA = 33
35962 deg
ZDOT = 5973
100808 TA = 303
34093
MA = 303
43279
Ha = 221
077 n
mi
Hp = 215
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17385228
68 X = 5248385
73
Y = 13698450
35 feet Y = 4234261
82 meter
Z = 2397032
78 Z = 756233
33
XDOT = -11350
269154 XDOT = -3525
617336
YDOT = 10943
141174 feet/sec YDOT = 3296
413188 meter/sec
ZDOT = 19596
787428 ZDOT = 5956
134784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17440902
79 X = 5315987
17
Y = -13607182
86 feet Y = -4147469
33 meter
Z = 2509774
67 Z = 764979
32
XDOT = 6904
119415 XDOT = 2104
375598
YDOT = 12482
844422 feet/sec YDOT = 3804
770980 meter/sec
ZDOT = 19521
060819 ZDOT = 5950
019338
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 17241
33900989
00016717 00000-0 10270-3 0 9081
2 25544 51
6426 33
6603 0004362 206
8973 153
1954 15
54040395 33120
Satellite: ISS
Catalog Number: 25544
Epoch time: 17241
33900989 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 33
6603 deg
Eccentricity:
0004362
Arg of perigee: 206
8973 deg
Mean anomaly: 153
1954 deg
Mean motion: 15
54040395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 305
Coasting Arc #10 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2017/242/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4926799
31 A = 6781254
10 meter
Y = -1324457
74 meter E =
0009531
Z = -4476946
52 I = 51
81745
XDOT = 4412
152288 Wp = 136
69955
YDOT = 5337
176107 meter/sec RA = 28
59274 deg
ZDOT = 3273
914160 TA = 166
25346
MA = 166
22749
Ha = 220
993 n
mi
Hp = 215
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16164039
74 X = 4962990
31
Y = -4345333
79 feet Y = -1269160
73 meter
Z = -14688144
75 Z = -4452925
80
XDOT = 14475
565248 XDOT = 4336
239642
YDOT = 17510
420300 feet/sec YDOT = 5386
091473 meter/sec
ZDOT = 10741
188188 ZDOT = 3295
162356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4298238
35 X = 1310103
05
Y = -16272800
15 feet Y = -4959949
49 meter
Z = -14581523
40 Z = -4444448
33
XDOT = 21165
419211 XDOT = 6451
219776
YDOT = -4125
558724 feet/sec YDOT = -1257
470299 meter/sec
ZDOT = 10834
364883 ZDOT = 3302
314416
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 17242
23929944
00016717 00000-0 10270-3 0 9094
2 25544 51
6422 29
1736 0004324 210
0628 150
0277 15
54030899 33262
Satellite: ISS
Catalog Number: 25544
Epoch time: 17242
23929944 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 29
1736 deg
Eccentricity:
0004324
Arg of perigee: 210
0628 deg
Mean anomaly: 150
0277 deg
Mean motion: 15
54030899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3326
Checksum: 300
Coasting Arc #11 (Orbit 3341)
---------------------------------------
Vector Time (GMT): 2017/243/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5892040
08 A = 6784942
45 meter
Y = 290936
18 meter E =
0011010
Z = 3338774
99 I = 51
80106
XDOT = -2928
267896 Wp = 110
59060
YDOT = -5313
506374 meter/sec RA = 23
61932 deg
ZDOT = -4695
872927 TA = 30
59772
MA = 30
53354
Ha = 220
977 n
mi
Hp = 215
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19330840
15 X = -5911073
53
Y = 954515
02 feet Y = 224941
07 meter
Z = 10953986
19 Z = 3310107
21
XDOT = -9607
178138 XDOT = -2845
823108
YDOT = -17432
763693 feet/sec YDOT = -5345
791444 meter/sec
ZDOT = -15406
407241 ZDOT = -4709
897035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8502698
73 X = -2591622
57
Y = 17466057
63 feet Y = 5323654
37 meter
Z = 10826968
11 Z = 3300059
88
XDOT = -18583
510817 XDOT = -5664
254097
YDOT = 559
397884 feet/sec YDOT = 170
504475 meter/sec
ZDOT = -15467
585186 ZDOT = -4714
519965
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 17243
26819762
00016717 00000-0 10270-3 0 9106
2 25544 51
6424 24
0459 0004242 213
8073 146
2809 15
54047973 33421
Satellite: ISS
Catalog Number: 25544
Epoch time: 17243
26819762 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 24
0459 deg
Eccentricity:
0004242
Arg of perigee: 213
8073 deg
Mean anomaly: 146
2809 deg
Mean motion: 15
54047973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3342
Checksum: 301
Coasting Arc #12 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2017/244/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6490780
14 A = 6788126
00 meter
Y = 627078
47 meter E =
0002979
Z = -1881706
18 I = 51
78168
XDOT = 1141
800213 Wp = 37
75625
YDOT = 5068
222075 meter/sec RA = 18
65198 deg
ZDOT = 5634
538721 TA = 301
57975
MA = 301
60883
Ha = 220
707 n
mi
Hp = 215
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21295210
44 X = 6492425
91
Y = 2057344
06 feet Y = 699671
93 meter
Z = -6173576
72 Z = -1850172
27
XDOT = 3746
063691 XDOT = 1057
671543
YDOT = 16628
025179 feet/sec YDOT = 5080
520268 meter/sec
ZDOT = 18486
019426 ZDOT = 5639
880676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11767065
85 X = 3586601
67
Y = -17915309
70 feet Y = -5460586
40 meter
Z = -6034031
96 Z = -1839172
94
XDOT = 15095
084349 XDOT = 4600
981710
YDOT = 3688
707021 feet/sec YDOT = 1124
317900 meter/sec
ZDOT = 18508
784738 ZDOT = 5641
477588
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 17244
23278444
00016717 00000-0 10270-3 0 9111
2 25544 51
6427 19
2373 0004261 219
1706 140
9139 15
54047634 33575
Satellite: ISS
Catalog Number: 25544
Epoch time: 17244
23278444 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 19
2373 deg
Eccentricity:
0004261
Arg of perigee: 219
1706 deg
Mean anomaly: 140
9139 deg
Mean motion: 15
54047634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 300
Coasting Arc #13 (Orbit 3372)
---------------------------------------
Vector Time (GMT): 2017/245/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6623477
40 A = 6789671
67 meter
Y = -1439969
20 meter E =
0013306
Z = 213824
81 I = 51
75452
XDOT = 819
346608 Wp = 151
40469
YDOT = -4683
927535 meter/sec RA = 13
69025 deg
ZDOT = -6019
691137 TA = 26
29442
MA = 26
22693
Ha = 220
718 n
mi
Hp = 215
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21730568
88 X = -6607921
65
Y = -4724308
41 feet Y = -1513950
45 meter
Z = 701524
95 Z = 181688
18
XDOT = 2688
145039 XDOT = 900
903039
YDOT = -15367
216322 feet/sec YDOT = -4674
309291 meter/sec
ZDOT = -19749
642838 ZDOT = -6015
512760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14018100
04 X = -4272716
89
Y = 17268721
04 feet Y = 5263506
17 meter
Z = 559460
57 Z = 170523
58
XDOT = -11187
531204 XDOT = -3409
959511
YDOT = -8423
317384 feet/sec YDOT = -2567
427139 meter/sec
ZDOT = -19730
313360 ZDOT = -6013
799512
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 17245
26167498
00016717 00000-0 10270-3 0 9122
2 25544 51
6419 14
1090 0004335 220
9084 139
1744 15
54007495 33738
Satellite: ISS
Catalog Number: 25544
Epoch time: 17245
26167498 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 14
1090 deg
Eccentricity:
0004335
Arg of perigee: 220
9084 deg
Mean anomaly: 139
1744 deg
Mean motion: 15
54007495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3373
Checksum: 304
Coasting Arc #14 (Orbit 3388)
---------------------------------------
Vector Time (GMT): 2017/246/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909876
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6277527
21 A = 6788543
36 meter
Y = 2123751
37 meter E =
0009717
Z = 1453035
28 I = 51
71910
XDOT = -2766
428513 Wp = 67
70010
YDOT = 4197
688338 meter/sec RA = 8
72651 deg
ZDOT = 5789
086975 TA = 308
13294
MA = 308
22049
Ha = 220
425 n
mi
Hp = 215
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20595561
72 X = 6246254
26
Y = 6967688
23 feet Y = 2193776
18 meter
Z = 4767176
11 Z = 1483453
11
XDOT = -9076
209032 XDOT = -2841
282780
YDOT = 13771
943367 feet/sec YDOT = 4166
334047 meter/sec
ZDOT = 18993
067504 ZDOT = 5775
466638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15228867
33 X = 4641758
76
Y = -15476068
24 feet Y = -4717105
60 meter
Z = 4901501
96 Z = 1493977
80
XDOT = 7262
764925 XDOT = 2213
690749
YDOT = 13170
444981 feet/sec YDOT = 4014
351630 meter/sec
ZDOT = 18932
014030 ZDOT = 5770
477876
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 17246
29055902
00016717 00000-0 10270-3 0 9133
2 25544 51
6415 8
9804 0004364 227
4647 132
6138 15
54073882 33892
Satellite: ISS
Catalog Number: 25544
Epoch time: 17246
29055902 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 8
9804 deg
Eccentricity:
0004364
Arg of perigee: 227
4647 deg
Mean anomaly: 132
6138 deg
Mean motion: 15
54073882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3389
Checksum: 319
Coasting Arc #15 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2017/246/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909876
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6653371
06 A = 6788833
79 meter
Y = -153212
80 meter E =
0004401
Z = -1330614
80 I = 51
71209
XDOT = 1273
438326 Wp = 33
98944
YDOT = 4815
138292 meter/sec RA = 7
76198 deg
ZDOT = 5825
911724 TA = 311
54579
MA = 311
58352
Ha = 220
663 n
mi
Hp = 215
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21828645
21 X = 6661053
23
Y = -502666
66 feet Y = -78767
40 meter
Z = -4365534
11 Z = -1298276
51
XDOT = 4177
947263 XDOT = 1191
200451
YDOT = 15797
697808 feet/sec YDOT = 4828
919281 meter/sec
ZDOT = 19113
883609 ZDOT = 5831
897583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14961372
56 X = -4560226
36
Y = -15941448
66 feet Y = -4858953
55 meter
Z = -4222304
99 Z = -1286958
56
XDOT = 7898
959209 XDOT = 2407
602767
YDOT = -12471
131645 feet/sec YDOT = -3801
200925 meter/sec
ZDOT = 19139
543878 ZDOT = 5833
732974
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 17246
41917175
00016717 00000-0 10270-3 0 9147
2 25544 51
6399 8
3344 0004538 220
9558 139
1254 15
54055710 33912
Satellite: ISS
Catalog Number: 25544
Epoch time: 17246
41917175 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 8
3344 deg
Eccentricity:
0004538
Arg of perigee: 220
9558 deg
Mean anomaly: 139
1254 deg
Mean motion: 15
54055710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 313
Coasting Arc #16 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2017/247/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909876
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6743538
12 A = 6789389
53 meter
Y = -619960
26 meter E =
0012163
Z = -367348
16 I = 51
68180
XDOT = 756
371446 Wp = 158
49401
YDOT = -4713
545000 meter/sec RA = 2
79573 deg
ZDOT = -6004
070315 TA = 25
46472
MA = 25
40484
Ha = 220
406 n
mi
Hp = 215
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22124468
89 X = -6734319
99
Y = -2033990
34 feet Y = -695319
58 meter
Z = -1205210
50 Z = -400083
32
XDOT = 2481
533617 XDOT = 838
187808
YDOT = -15464
386483 feet/sec YDOT = -4704
629756 meter/sec
ZDOT = -19698
393421 ZDOT = -6000
197050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13549684
80 X = 4129943
93
Y = 17597305
86 feet Y = 5363658
83 meter
Z = -1350052
36 Z = -411495
96
XDOT = -11830
814938 XDOT = -3606
032393
YDOT = 7616
320989 feet/sec YDOT = 2321
454638 meter/sec
ZDOT = -19680
416942 ZDOT = -5998
591084
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 17247
44805153
00016717 00000-0 10270-3 0 9154
2 25544 51
6399 3
2055 0004388 226
5645 133
5143 15
54083647 34070
Satellite: ISS
Catalog Number: 25544
Epoch time: 17247
44805153 = yrday
fracday
Element set: 915
Inclination: 51
6399 deg
RA of node: 3
2055 deg
Eccentricity:
0004388
Arg of perigee: 226
5645 deg
Mean anomaly: 133
5143 deg
Mean motion: 15
54083647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 308
Coasting Arc #17 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2017/248/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909876
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6338436
92 A = 6787644
51 meter
Y = 1348524
38 meter E =
0009838
Z = 2006636
80 I = 51
64441
XDOT = -2728
844820 Wp = 77
78775
YDOT = 4511
753202 meter/sec RA = 357
82681 deg
ZDOT = 5566
621947 TA = 304
37296
MA = 304
46597
Ha = 220
352 n
mi
Hp = 215
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20795396
72 X = 6313139
13
Y = 4424292
59 feet Y = 1419263
85 meter
Z = 6583454
08 Z = 2037365
04
XDOT = -8952
902952 XDOT = -2806
133246
YDOT = 14802
339903 feet/sec YDOT = 4480
805800 meter/sec
ZDOT = 18263
195364 ZDOT = 5553
178054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11180964
33 X = -3407957
93
Y = -18033362
68 feet Y = -5496568
94 meter
Z = 6719272
63 Z = 2048034
30
XDOT = 15646
893429 XDOT = 4769
173117
YDOT = -2893
683269 feet/sec YDOT = -881
994660 meter/sec
ZDOT = 18202
883925 ZDOT = 5548
239020
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 17248
47692607
00016717 00000-0 10270-3 0 9167
2 25544 51
6407 358
0777 0004513 228
4994 131
5771 15
54097087 34236
Satellite: ISS
Catalog Number: 25544
Epoch time: 17248
47692607 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 358
0777 deg
Eccentricity:
0004513
Arg of perigee: 228
4994 deg
Mean anomaly: 131
5771 deg
Mean motion: 15
54097087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 337
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