[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 6th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 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
283/16:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
4
285/09:32:03
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
1
285/12:56:35
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
0
286/19:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
290/03:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
6
294/08:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2017/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6472219
97 A = 6788945
69 meter
Y = 1743598
37 meter E =
0010848
Z = 1055903
72 I = 51
51152
XDOT = -354
801598 Wp = 105
28376
YDOT = 4906
563563 meter/sec RA = 202
27267 deg
ZDOT = -5879
660837 TA = 63
24933
MA = 63
13837
Ha = 221
482 n
mi
Hp = 214
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21234317
49 X = 6447112
39
Y = 5720467
11 feet Y = 1815834
90 meter
Z = 3464251
06 Z = 1087283
18
XDOT = -1164
047239 XDOT = -381
080650
YDOT = 16097
649486 feet/sec YDOT = 4902
448262 meter/sec
ZDOT = -19290
225842 ZDOT = -5881
448827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21967762
42 X = -6695773
99
Y = -238266
35 feet Y = -72623
58 meter
Z = 3603007
35 Z = 1098196
64
XDOT = -3035
456290 XDOT = -925
207077
YDOT = -14242
674131 feet/sec YDOT = -4341
167075 meter/sec
ZDOT = -19298
765022 ZDOT = -5882
263579
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 17279
53431594
00016717 00000-0 10270-3 0 9007
2 25544 51
6409 203
2543 0004752 348
6563 11
4481 15
54084400 39067
Satellite: ISS
Catalog Number: 25544
Epoch time: 17279
53431594 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 203
2543 deg
Eccentricity:
0004752
Arg of perigee: 348
6563 deg
Mean anomaly: 11
4481 deg
Mean motion: 15
54084400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 298
Coasting Arc #2 (Orbit 3921)
---------------------------------------
Vector Time (GMT): 2017/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6278475
00 A = 6789295
44 meter
Y = -2479636
08 meter E =
0016143
Z = 630785
44 I = 51
54313
XDOT = 2284
796226 Wp = 36
86508
YDOT = -4250
693147 meter/sec RA = 197
29510 deg
ZDOT = 5965
389448 TA = 329
95847
MA = 330
05098
Ha = 221
586 n
mi
Hp = 214
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20598671
25 X = -6253344
53
Y = -8135288
96 feet Y = -2549705
69 meter
Z = 2069506
04 Z = 600347
16
XDOT = 7496
050611 XDOT = 2303
181189
YDOT = -13945
843659 feet/sec YDOT = -4225
039558 meter/sec
ZDOT = 19571
487691 ZDOT = 5976
533648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22034468
72 X = 6716106
07
Y = 2347127
95 feet Y = 715404
60 meter
Z = 1934998
01 Z = 589787
39
XDOT = -3213
233700 XDOT = -979
393632
YDOT = 13796
713691 feet/sec YDOT = 4205
238333 meter/sec
ZDOT = 19621
386036 ZDOT = 5980
598464
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 17280
56316992
00016717 00000-0 10270-3 0 9017
2 25544 51
6408 198
1258 0004859 352
7631 7
3451 15
54091553 39227
Satellite: ISS
Catalog Number: 25544
Epoch time: 17280
56316992 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 198
1258 deg
Eccentricity:
0004859
Arg of perigee: 352
7631 deg
Mean anomaly: 7
3451 deg
Mean motion: 15
54091553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3922
Checksum: 318
Coasting Arc #3 (Orbit 3936)
---------------------------------------
Vector Time (GMT): 2017/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5599415
00 A = 6787224
50 meter
Y = 3081346
24 meter E =
0003834
Z = -2288453
59 I = 51
56838
XDOT = -4136
312334 Wp = 83
42343
YDOT = 3497
699950 meter/sec RA = 192
31783 deg
ZDOT = -5418
597615 TA = 122
06531
MA = 122
02807
Ha = 221
651 n
mi
Hp = 214
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18370784
13 X = 5575658
86
Y = 10109403
69 feet Y = 3143829
70 meter
Z = -7508049
82 Z = -2261310
67
XDOT = -13570
578525 XDOT = -4148
795595
YDOT = 11475
393538 feet/sec YDOT = 3451
374616 meter/sec
ZDOT = -17777
551231 ZDOT = -5438
721648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20527775
07 X = -6256865
84
Y = -4481238
55 feet Y = -1365881
51 meter
Z = -7388201
17 Z = -2251923
72
XDOT = 9328
657085 XDOT = 2843
374680
YDOT = -13316
074659 feet/sec YDOT = -4058
739556 meter/sec
ZDOT = -17867
140023 ZDOT = -5445
904279
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 17281
52771167
00016717 00000-0 10270-3 0 9024
2 25544 51
6413 193
3183 0004820 356
2564 3
8552 15
54111919 39377
Satellite: ISS
Catalog Number: 25544
Epoch time: 17281
52771167 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 193
3183 deg
Eccentricity:
0004820
Arg of perigee: 356
2564 deg
Mean anomaly: 3
8552 deg
Mean motion: 15
54111919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3937
Checksum: 305
Coasting Arc #4 (Orbit 3952)
---------------------------------------
Vector Time (GMT): 2017/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4465600
27 A = 6783674
67 meter
Y = -3520864
59 meter E =
0012421
Z = 3685040
63 I = 51
58798
XDOT = 5723
462822 Wp = 72
23510
YDOT = -2722
262295 meter/sec RA = 187
33430 deg
ZDOT = 4326
521642 TA = 331
71493
MA = 331
78232
Ha = 221
796 n
mi
Hp = 214
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14650919
52 X = -4443797
66
Y = -11551393
03 feet Y = -3570679
84 meter
Z = 12090028
32 Z = 3663400
82
XDOT = 18777
765163 XDOT = 5732
461895
YDOT = -8931
306742 feet/sec YDOT = -2658
208028 meter/sec
ZDOT = 14194
624809 ZDOT = 4354
347126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17513306
04 X = 5338055
68
Y = 6608066
76 feet Y = 2014138
75 meter
Z = 11994601
84 Z = 3655954
64
XDOT = -14669
701065 XDOT = -4471
324885
YDOT = 12839
487963 feet/sec YDOT = 3913
475931 meter/sec
ZDOT = 14318
248917 ZDOT = 4364
202270
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 17282
55654943
00016717 00000-0 10270-3 0 9031
2 25544 51
6406 188
1898 0004814
0121
1031 15
54121448 39538
Satellite: ISS
Catalog Number: 25544
Epoch time: 17282
55654943 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 188
1898 deg
Eccentricity:
0004814
Arg of perigee:
0121 deg
Mean anomaly:
1031 deg
Mean motion: 15
54121448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3953
Checksum: 283
Coasting Arc #5 (Orbit 3967)
---------------------------------------
Vector Time (GMT): 2017/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2969303
14 A = 6779868
67 meter
Y = 3867377
99 meter E =
0013371
Z = -4723755
76 I = 51
60915
XDOT = -6882
728118 Wp = 51
30859
YDOT = 1908
137576 meter/sec RA = 182
34264 deg
ZDOT = -2761
319101 TA = 191
28460
MA = 191
31461
Ha = 221
728 n
mi
Hp = 214
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9741808
21 X = 2948782
55
Y = 12688248
01 feet Y = 3900467
80 meter
Z = -15497886
37 Z = -4709381
56
XDOT = -22581
128997 XDOT = -6890
140478
YDOT = 6260
293884 feet/sec YDOT = 1831
128633 meter/sec
ZDOT = -9059
445869 ZDOT = -2794
772023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13347002
07 X = -4068166
23
Y = -8927875
49 feet Y = -2721216
45 meter
Z = -15434685
67 Z = -4704492
19
XDOT = 18739
593532 XDOT = 5711
828109
YDOT = -12080
077105 feet/sec YDOT = -3682
007502 meter/sec
ZDOT = -9207
920948 ZDOT = -2806
574305
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 17283
52107481
00016717 00000-0 10270-3 0 9040
2 25544 51
6415 183
3820 0004887 2
3394 357
7780 15
54163465 39680
Satellite: ISS
Catalog Number: 25544
Epoch time: 17283
52107481 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 183
3820 deg
Eccentricity:
0004887
Arg of perigee: 2
3394 deg
Mean anomaly: 357
7780 deg
Mean motion: 15
54163465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3968
Checksum: 324
Coasting Arc #6 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2017/283/16:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 973648
71 A = 6777635
36 meter
Y = 4187195
22 meter E =
0015916
Z = -5253283
80 I = 51
60385
XDOT = -7577
035824 Wp = 65
77370
YDOT = 570
902019 meter/sec RA = 181
34828 deg
ZDOT = -945
171083 TA = 195
14067
MA = 195
18837
Ha = 221
730 n
mi
Hp = 214
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3194385
54 X = 952272
38
Y = 13737517
14 feet Y = 4197963
46 meter
Z = -17235183
07 Z = -5248606
14
XDOT = -24859
041416 XDOT = -7578
265392
YDOT = 1873
038121 feet/sec YDOT = 486
163515 meter/sec
ZDOT = -3100
954997 ZDOT = -981
981692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13779124
41 X = -4199877
12
Y = 3123283
82 feet Y = 951976
91 meter
Z = -17214988
82 Z = -5247128
59
XDOT = -1312
462566 XDOT = -400
038590
YDOT = -23856
208742 feet/sec YDOT = -7271
372425 meter/sec
ZDOT = -3264
142912 ZDOT = -994
910760
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 17283
71397817
00016717 00000-0 10270-3 0 9056
2 25544 51
6373 182
4170 0004740 2
8769 357
2410 15
54147056 39717
Satellite: ISS
Catalog Number: 25544
Epoch time: 17283
71397817 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 182
4170 deg
Eccentricity:
0004740
Arg of perigee: 2
8769 deg
Mean anomaly: 357
2410 deg
Mean motion: 15
54147056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 317
Coasting Arc #7 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2017/284/16:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 873554
16 A = 6777667
09 meter
Y = -4209805
36 meter E =
0007435
Z = 5237224
14 I = 51
63620
XDOT = 7597
741029 Wp = 29
05447
YDOT = 314
213169 meter/sec RA = 176
34668 deg
ZDOT = -1007
750138 TA = 70
63131
MA = 70
55095
Ha = 221
797 n
mi
Hp = 214
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2865991
33 X = 895124
15
Y = -13811697
38 feet Y = -4199915
86 meter
Z = 17182493
90 Z = 5241520
23
XDOT = 24926
971879 XDOT = 7598
557960
YDOT = 1030
883101 feet/sec YDOT = 399
180819 meter/sec
ZDOT = -3306
266856 ZDOT = -970
840148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13820690
85 X = 4212546
57
Y = 2700417
20 feet Y = 823087
16 meter
Z = 17202070
77 Z = 5243191
17
XDOT = -738
402505 XDOT = -225
065083
YDOT = 23944
062938 feet/sec YDOT = 7298
150384 meter/sec
ZDOT = -3142
726099 ZDOT = -957
902915
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 17284
74279763
00016717 00000-0 10270-3 0 9060
2 25544 51
6369 177
2878 0004711 6
8617 353
2600 15
54123828 39878
Satellite: ISS
Catalog Number: 25544
Epoch time: 17284
74279763 = yrday
fracday
Element set: 906
Inclination: 51
6369 deg
RA of node: 177
2878 deg
Eccentricity:
0004711
Arg of perigee: 6
8617 deg
Mean anomaly: 353
2600 deg
Mean motion: 15
54123828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 342
Coasting Arc #8 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2017/285/09:32:03
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3343360
21 A = 6779435
22 meter
Y = -3410923
11 meter E =
0007336
Z = 4804546
84 I = 51
66774
XDOT = 6632
723246 Wp = 81
26679
YDOT = -2876
611570 meter/sec RA = 172
88447 deg
ZDOT = 2571
067982 TA = 343
43423
MA = 343
45818
Ha = 221
886 n
mi
Hp = 214
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10969029
57 X = -3328308
29
Y = -11190692
61 feet Y = -3448226
46 meter
Z = 15762948
95 Z = 4788342
35
XDOT = 21760
903037 XDOT = 6651
908186
YDOT = -9437
702001 feet/sec YDOT = -2802
332545 meter/sec
ZDOT = 8435
262408 ZDOT = 2603
334810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7389190
63 X = 2252225
31
Y = 13899516
96 feet Y = 4236572
77 meter
Z = 15691560
17 Z = 4782787
54
XDOT = -22487
999447 XDOT = -6854
342232
YDOT = 2261
862324 feet/sec YDOT = 689
415636 meter/sec
ZDOT = 8578
647610 ZDOT = 2614
771792
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 17285
45010634
00016717 00000-0 10270-3 0 9070
2 25544 51
6393 173
7648 0004804 8
7002 351
4234 15
54187753 39985
Satellite: ISS
Catalog Number: 25544
Epoch time: 17285
45010634 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 173
7648 deg
Eccentricity:
0004804
Arg of perigee: 8
7002 deg
Mean anomaly: 351
4234 deg
Mean motion: 15
54187753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 319
Coasting Arc #9 (Orbit 3999)
---------------------------------------
Vector Time (GMT): 2017/285/12:56:35
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4780966
83 A = 6784110
91 meter
Y = -3384797
64 meter E =
0014082
Z = 3415677
29 I = 51
68980
XDOT = 5382
737502 Wp = 69
27633
YDOT = 2931
868100 meter/sec RA = 172
13273 deg
ZDOT = -4608
688225 TA = 70
78630
MA = 70
63397
Ha = 221
815 n
mi
Hp = 214
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15685586
71 X = 4801869
33
Y = -11104979
14 feet Y = -3331216
58 meter
Z = 11206290
31 Z = 3438952
94
XDOT = 17659
899942 XDOT = 5371
939520
YDOT = 9618
989830 feet/sec YDOT = 2992
000952 meter/sec
ZDOT = -15120
368191 ZDOT = -4582
566620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6554425
32 X = -1997788
84
Y = 18001806
03 feet Y = 5486950
48 meter
Z = 11309890
49 Z = 3447254
62
XDOT = -18767
633516 XDOT = -5720
374696
YDOT = 2635
145105 feet/sec YDOT = 803
192228 meter/sec
ZDOT = -15004
959468 ZDOT = -4573
511646
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 17285
57870746
00016717 00000-0 10270-3 0 9082
2 25544 51
6408 173
1247 0005016 9
1695 350
9548 15
54190975 40007
Satellite: ISS
Catalog Number: 25544
Epoch time: 17285
57870746 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 173
1247 deg
Eccentricity:
0005016
Arg of perigee: 9
1695 deg
Mean anomaly: 350
9548 deg
Mean motion: 15
54190975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4000
Checksum: 323
Coasting Arc #10 (Orbit 4014)
---------------------------------------
Vector Time (GMT): 2017/286/12:56:35
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5812520
69 A = 6787533
55 meter
Y = 2901577
87 meter E =
0011411
Z = -1948806
56 I = 51
73357
XDOT = -3712
938467 Wp = 28
11596
YDOT = -3688
625559 meter/sec RA = 167
15919 deg
ZDOT = 5605
406272 TA = 310
41747
MA = 310
51697
Ha = 221
875 n
mi
Hp = 214
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19069949
77 X = -5835068
48
Y = 9519612
45 feet Y = 2836452
11 meter
Z = -6393722
32 Z = -1977097
17
XDOT = -12181
556650 XDOT = -3698
643871
YDOT = -12101
789891 feet/sec YDOT = -3730
065903 meter/sec
ZDOT = 18390
440526 ZDOT = 5587
404757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9944424
57 X = 3031060
61
Y = -18808778
17 feet Y = -5732915
59 meter
Z = -6519507
20 Z = -1987145
80
XDOT = 15672
986978 XDOT = 4777
126431
YDOT = 1965
331168 feet/sec YDOT = 599
032940 meter/sec
ZDOT = 18311
108693 ZDOT = 5581
225930
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 17286
54321389
00016717 00000-0 10270-3 0 9095
2 25544 51
6411 168
3161 0005001 10
8263 349
2996 15
54168832 40157
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
54321389 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 168
3161 deg
Eccentricity:
0005001
Arg of perigee: 10
8263 deg
Mean anomaly: 349
2996 deg
Mean motion: 15
54168832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4015
Checksum: 306
Coasting Arc #11 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2017/286/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 283633
27 A = 6777669
77 meter
Y = -4318230
71 meter E =
0007864
Z = 5213442
24 I = 51
70864
XDOT = 7520
550166 Wp = 35
23014
YDOT = -943
208706 meter/sec RA = 165
77173 deg
ZDOT = -1183
229713 TA = 66
14452
MA = 66
06212
Ha = 221
878 n
mi
Hp = 213
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 930555
34 X = 306575
24
Y = -14167423
59 feet Y = -4314930
31 meter
Z = 17104469
29 Z = 5214876
06
XDOT = 24673
721017 XDOT = 7536
286031
YDOT = -3094
516753 feet/sec YDOT = -859
020875 meter/sec
ZDOT = -3881
987249 ZDOT = -1146
658631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10376867
44 X = 3162869
20
Y = -9678125
13 feet Y = -2949892
54 meter
Z = 17111376
62 Z = 5215547
60
XDOT = 19291
469888 XDOT = 5880
040022
YDOT = 14066
043201 feet/sec YDOT = 4287
329968 meter/sec
ZDOT = -3719
738057 ZDOT = -1133
776160
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 17286
86471628
00016717 00000-0 10270-3 0 9104
2 25544 51
6403 166
7077 0004486 16
2494 343
8801 15
54164390 40204
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
86471628 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 166
7077 deg
Eccentricity:
0004486
Arg of perigee: 16
2494 deg
Mean anomaly: 343
8801 deg
Mean motion: 15
54164390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 312
Coasting Arc #12 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2017/287/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2002896
93 A = 6780064
58 meter
Y = 4552841
69 meter E =
0011242
Z = -4616918
19 I = 51
74855
XDOT = -7044
720157 Wp = 86
89979
YDOT = -55
769853 meter/sec RA = 160
78250 deg
ZDOT = 3008
035690 TA = 213
06759
MA = 213
13793
Ha = 221
895 n
mi
Hp = 213
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6571184
16 X = -2031232
26
Y = 14937144
64 feet Y = 4530285
10 meter
Z = -15147369
39 Z = -4626716
93
XDOT = -23112
598941 XDOT = -7058
184625
YDOT = -182
971958 feet/sec YDOT = -134
623754 meter/sec
ZDOT = 9868
883496 ZDOT = 2973
781653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14885465
92 X = -4537090
01
Y = 6586800
98 feet Y = 2007656
94 meter
Z = -15191395
85 Z = -4630337
45
XDOT = -16428
093679 XDOT = -5007
282953
YDOT = -14767
163310 feet/sec YDOT = -4501
031377 meter/sec
ZDOT = 9717
014983 ZDOT = 2961
746167
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 17287
82921411
00016717 00000-0 10270-3 0 9112
2 25544 51
6404 161
9006 0004467 19
6238 340
5086 15
54192763 40356
Satellite: ISS
Catalog Number: 25544
Epoch time: 17287
82921411 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 161
9006 deg
Eccentricity:
0004467
Arg of perigee: 19
6238 deg
Mean anomaly: 340
5086 deg
Mean motion: 15
54192763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 302
Coasting Arc #13 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2017/288/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3536580
99 A = 6783944
24 meter
Y = -4607369
23 meter E =
0014660
Z = 3497404
76 I = 51
79157
XDOT = 6064
914332 Wp = 72
85978
YDOT = 1193
360226 meter/sec RA = 155
80304 deg
ZDOT = -4540
837929 TA = 66
10738
MA = 65
95385
Ha = 221
955 n
mi
Hp = 213
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11602956
00 X = 3570850
13
Y = -15116040
77 feet Y = -4567628
80 meter
Z = 11474425
08 Z = 3514668
24
XDOT = 19898
012899 XDOT = 6073
176483
YDOT = 3915
223840 feet/sec YDOT = 1261
227982 meter/sec
ZDOT = -14897
762233 ZDOT = -4511
356221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18662968
66 X = 5688472
85
Y = -3611184
93 feet Y = -1100689
17 meter
Z = 11551564
88 Z = 3520916
98
XDOT = 12057
079310 XDOT = 3674
997774
YDOT = 14866
857879 feet/sec YDOT = 4531
418282 meter/sec
ZDOT = -14767
184670 ZDOT = -4501
037887
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 17288
85800822
00016717 00000-0 10270-3 0 9129
2 25544 51
6402 156
7715 0004397 24
3720 335
7640 15
54172946 40515
Satellite: ISS
Catalog Number: 25544
Epoch time: 17288
85800822 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 156
7715 deg
Eccentricity:
0004397
Arg of perigee: 24
3720 deg
Mean anomaly: 335
7640 deg
Mean motion: 15
54172946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 308
Coasting Arc #14 (Orbit 4065)
---------------------------------------
Vector Time (GMT): 2017/289/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4692355
06 A = 6787368
18 meter
Y = 4453894
22 meter E =
0011026
Z = -2039116
41 I = 51
83368
XDOT = -4688
799690 Wp = 34
78388
YDOT = -2399
303856 meter/sec RA = 150
83651 deg
ZDOT = 5572
746988 TA = 302
73709
MA = 302
84332
Ha = 222
029 n
mi
Hp = 213
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15394865
69 X = -4731905
79
Y = 14612513
85 feet Y = 4401199
73 meter
Z = -6690014
47 Z = -2062007
27
XDOT = -15383
201082 XDOT = -4688
691579
YDOT = -7871
731811 feet/sec YDOT = -2451
735994 meter/sec
ZDOT = 18283
290643 ZDOT = 5549
970487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21166877
90 X = -6451664
38
Y = 1055653
11 feet Y = 321763
07 meter
Z = -6792099
88 Z = -2070232
04
XDOT = -6534
943705 XDOT = -1991
850841
YDOT = -14536
336913 feet/sec YDOT = -4430
675491 meter/sec
ZDOT = 18182
591938 ZDOT = 5542
054023
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 17289
82249585
00016717 00000-0 10270-3 0 9131
2 25544 51
6414 151
9636 0004602 25
0886 335
0489 15
54176334 40662
Satellite: ISS
Catalog Number: 25544
Epoch time: 17289
82249585 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 151
9636 deg
Eccentricity:
0004602
Arg of perigee: 25
0886 deg
Mean anomaly: 335
0489 deg
Mean motion: 15
54176334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4066
Checksum: 327
Coasting Arc #15 (Orbit 4070)
---------------------------------------
Vector Time (GMT): 2017/290/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2168674
15 A = 6777196
55 meter
Y = 3594270
74 meter E =
0017740
Z = -5335413
39 I = 51
80546
XDOT = -6574
194724 Wp = 75
63537
YDOT = 3923
300993 meter/sec RA = 149
31959 deg
ZDOT = -24
998259 TA = 194
10178
MA = 194
15137
Ha = 222
210 n
mi
Hp = 213
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7115072
68 X = 2154238
07
Y = 11792226
82 feet Y = 3618441
01 meter
Z = -17504637
11 Z = -5324913
97
XDOT = -21568
880328 XDOT = -6617
456082
YDOT = 12871
722419 feet/sec YDOT = 3849
541966 meter/sec
ZDOT = -82
015284 ZDOT = -57
039627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13504954
31 X = 4116310
07
Y = -2984778
42 feet Y = -909760
46 meter
Z = -17458536
59 Z = -5321361
95
XDOT = 4908
356116 XDOT = 1496
066944
YDOT = 23603
373833 feet/sec YDOT = 7194
308344 meter/sec
ZDOT = -224
616925 ZDOT = -68
463239
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 17290
14399038
00016717 00000-0 10270-3 0 9148
2 25544 51
6384 150
3638 0004942 27
5629 332
5785 15
54185287 40716
Satellite: ISS
Catalog Number: 25544
Epoch time: 17290
14399038 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 150
3638 deg
Eccentricity:
0004942
Arg of perigee: 27
5629 deg
Mean anomaly: 332
5785 deg
Mean motion: 15
54185287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4071
Checksum: 328
Coasting Arc #16 (Orbit 4086)
---------------------------------------
Vector Time (GMT): 2017/291/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -544689
86 A = 6778287
39 meter
Y = -4489532
74 meter E =
0010349
Z = 5045020
73 I = 51
83582
XDOT = 6789
587703 Wp = 43
79009
YDOT = -3004
812822 meter/sec RA = 144
33187 deg
ZDOT = -1931
266887 TA = 64
93702
MA = 64
82964
Ha = 222
221 n
mi
Hp = 213
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1787040
21 X = -518952
90
Y = -14729438
12 feet Y = -4495479
35 meter
Z = 16551905
27 Z = 5042437
77
XDOT = 22275
550207 XDOT = 6832
065022
YDOT = -9858
309784 feet/sec YDOT = -2928
649731 meter/sec
ZDOT = -6336
177451 ZDOT = -1898
181065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14589787
31 X = -4446967
17
Y = -2765464
82 feet Y = -842913
68 meter
Z = 16541031
98 Z = 5041706
55
XDOT = -2653
311428 XDOT = -808
729323
YDOT = -23209
922588 feet/sec YDOT = -7074
384405 meter/sec
ZDOT = -6189
046897 ZDOT = -1886
421494
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 17291
17276962
00016717 00000-0 10270-3 0 9153
2 25544 51
6371 145
2344 0004996 29
5802 330
5632 15
54212307 40873
Satellite: ISS
Catalog Number: 25544
Epoch time: 17291
17276962 = yrday
fracday
Element set: 915
Inclination: 51
6371 deg
RA of node: 145
2344 deg
Eccentricity:
0004996
Arg of perigee: 29
5802 deg
Mean anomaly: 330
5632 deg
Mean motion: 15
54212307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4087
Checksum: 310
Coasting Arc #17 (Orbit 4101)
---------------------------------------
Vector Time (GMT): 2017/292/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -958839
91 A = 6781491
08 meter
Y = 5210570
88 meter E =
0010527
Z = -4241198
37 I = 51
87193
XDOT = -6488
323688 Wp = 82
50216
YDOT = 1780
574278 meter/sec RA = 139
35316 deg
ZDOT = 3663
523498 TA = 224
89428
MA = 224
97946
Ha = 222
312 n
mi
Hp = 213
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3145800
22 X = -996432
53
Y = 17095048
81 feet Y = 5199637
82 meter
Z = -13914692
81 Z = -4245948
09
XDOT = -21287
151207 XDOT = -6525
548307
YDOT = 5841
779128 feet/sec YDOT = 1707
809673 meter/sec
ZDOT = 12019
434048 ZDOT = 3631
913940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15442679
47 X = 4706928
70
Y = 7940692
68 feet Y = 2420323
13 meter
Z = -13936444
29 Z = -4247828
22
XDOT = -111
669113 XDOT = -34
036746
YDOT = 21013
196175 feet/sec YDOT = 6404
822194 meter/sec
ZDOT = 11878
996350 ZDOT = 3620
718088
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 17292
13724618
00016717 00000-0 10270-3 0 9167
2 25544 51
6367 140
4264 0005067 33
1416 327
0054 15
54195453 41027
Satellite: ISS
Catalog Number: 25544
Epoch time: 17292
13724618 = yrday
fracday
Element set: 916
Inclination: 51
6367 deg
RA of node: 140
4264 deg
Eccentricity:
0005067
Arg of perigee: 33
1416 deg
Mean anomaly: 327
0054 deg
Mean motion: 15
54195453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4102
Checksum: 288
Coasting Arc #18 (Orbit 4117)
---------------------------------------
Vector Time (GMT): 2017/293/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2309569
54 A = 6785289
49 meter
Y = -5655940
30 meter E =
0016206
Z = 2941491
44 I = 51
90940
XDOT = 5782
320471 Wp = 81
87758
YDOT = -269
171554 meter/sec RA = 134
38496 deg
ZDOT = -5031
788851 TA = 64
67327
MA = 64
50551
Ha = 222
259 n
mi
Hp = 213
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7577327
90 X = 2358355
45
Y = -18556234
57 feet Y = -5629840
05 meter
Z = 9650562
48 Z = 2952829
93
XDOT = 18970
867688 XDOT = 5809
343234
YDOT = -883
108772 feet/sec YDOT = -204
359085 meter/sec
ZDOT = -16508
493607 ZDOT = -5003
633775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15744873
20 X = -4799037
35
Y = -12363688
65 feet Y = -3768452
30 meter
Z = 9701611
55 Z = 2957051
20
XDOT = 3538
142824 XDOT = 1078
425933
YDOT = -17427
971888 feet/sec YDOT = -5312
045832 meter/sec
ZDOT = -16383
566568 ZDOT = -4993
711090
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 17293
16601418
00016717 00000-0 10270-3 0 9174
2 25544 51
6369 135
2962 0005073 35
5434 324
6056 15
54243656 41180
Satellite: ISS
Catalog Number: 25544
Epoch time: 17293
16601418 = yrday
fracday
Element set: 917
Inclination: 51
6369 deg
RA of node: 135
2962 deg
Eccentricity:
0005073
Arg of perigee: 35
5434 deg
Mean anomaly: 324
6056 deg
Mean motion: 15
54243656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4118
Checksum: 308
Coasting Arc #19 (Orbit 4132)
---------------------------------------
Vector Time (GMT): 2017/294/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3340015
72 A = 6788159
37 meter
Y = 5743510
85 meter E =
0013744
Z = -1364045
80 I = 51
94125
XDOT = -4770
562643 Wp = 39
01679
YDOT = -1397
312870 meter/sec RA = 129
42904 deg
ZDOT = 5839
927749 TA = 306
18504
MA = 306
31208
Ha = 222
337 n
mi
Hp = 213
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10958056
82 X = -3397366
91
Y = 18843539
54 feet Y = 5705839
74 meter
Z = -4475215
89 Z = -1380410
75
XDOT = -15651
452241 XDOT = -4782
951220
YDOT = -4584
359810 feet/sec YDOT = -1450
729369 meter/sec
ZDOT = 19159
867942 ZDOT = 5816
723238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15342883
30 X = 4676510
83
Y = 15462593
46 feet Y = 4712998
49 meter
Z = -4548591
52 Z = -1386410
70
XDOT = -7409
455899 XDOT = -2258
402158
YDOT = 12917
939892 feet/sec YDOT = 3937
388079 meter/sec
ZDOT = 19057
117608 ZDOT = 5808
609447
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 17294
13047869
00016717 00000-0 10270-3 0 9187
2 25544 51
6369 130
4878 0005118 40
5248 319
6285 15
54249367 41332
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
13047869 = yrday
fracday
Element set: 918
Inclination: 51
6369 deg
RA of node: 130
4878 deg
Eccentricity:
0005118
Arg of perigee: 40
5248 deg
Mean anomaly: 319
6285 deg
Mean motion: 15
54249367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4133
Checksum: 333
Coasting Arc #20 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3286900
96 A = 6776974
77 meter
Y = 2595347
58 meter E =
0018489
Z = -5343576
15 I = 51
91247
XDOT = -4741
524531 Wp = 77
58222
YDOT = 6010
227314 meter/sec RA = 128
23240 deg
ZDOT = 6
451060 TA = 192
45624
MA = 192
50200
Ha = 222
308 n
mi
Hp = 213
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10783795
78 X = 3283591
97
Y = 8514919
88 feet Y = 2632085
05 meter
Z = -17531417
83 Z = -5327617
21
XDOT = -15556
182843 XDOT = -4808
411431
YDOT = 19718
593550 feet/sec YDOT = 5956
830362 meter/sec
ZDOT = 21
164894 ZDOT = -16
745322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7909558
06 X = -2410833
30
Y = -11344516
37 feet Y = -3457808
59 meter
Z = -17460972
56 Z = -5322104
44
XDOT = 19844
089457 XDOT = 6048
478466
YDOT = -13688
810331 feet/sec YDOT = -4172
349389 meter/sec
ZDOT = -82
557799 ZDOT = -25
163617
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 17294
38766783
00016717 00000-0 10270-3 0 9198
2 25544 51
6405 129
2065 0005110 38
2495 321
9019 15
54260956 41379
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
38766783 = yrday
fracday
Element set: 919
Inclination: 51
6405 deg
RA of node: 129
2065 deg
Eccentricity:
0005110
Arg of perigee: 38
2495 deg
Mean anomaly: 321
9019 deg
Mean motion: 15
54260956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4137
Checksum: 321
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