[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 4th 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) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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
153/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 216
3
154/21:07:26
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 216
3
155/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
4
156/14:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
4
156/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
5
160/01:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 216
6
165/09:20:13
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 216
7
167/11:41:11
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
6
167/16:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
6
Coasting Arc #1 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2017/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900773
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1429808
33 A = 6789157
70 meter
Y = 6521938
81 meter E =
0004488
Z = -1217260
71 I = 52
00394
XDOT = -4914
229887 Wp = 28
52271
YDOT = 18
138078 meter/sec RA = 110
55309 deg
ZDOT = 5882
240213 TA = 318
32192
MA = 318
35611
Ha = 220
619 n
mi
Hp = 216
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4690972
20 X = -1496719
21
Y = 21397437
03 feet Y = 6505575
68 meter
Z = -3993637
50 Z = -1224368
42
XDOT = -16122
801467 XDOT = -4942
640647
YDOT = 59
508130 feet/sec YDOT = -36
975387 meter/sec
ZDOT = 19298
688363 ZDOT = 5858
299288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18569259
81 X = 5659910
39
Y = 11609386
60 feet Y = 3538541
04 meter
Z = -4026090
57 Z = -1227152
40
XDOT = -4577
016725 XDOT = -1395
074698
YDOT = 13962
621754 feet/sec YDOT = 4255
807111 meter/sec
ZDOT = 19192
984014 ZDOT = 5850
021528
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 17153
50238668
00016717 00000-0 10270-3 0 9002
2 25544 51
6376 111
5238 0004732 226
9152 133
1605 15
53966340 19465
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
50238668 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 111
5238 deg
Eccentricity:
0004732
Arg of perigee: 226
9152 deg
Mean anomaly: 133
1605 deg
Mean motion: 15
53966340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 301
Coasting Arc #2 (Orbit 1946)
---------------------------------------
Vector Time (GMT): 2017/153/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900773
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4296156
20 A = 6778272
27 meter
Y = 217743
32 meter E =
0010546
Z = -5247246
87 I = 51
96932
XDOT = -1771
494924 Wp = 95
47472
YDOT = 7364
185318 meter/sec RA = 110
33271 deg
ZDOT = -1147
769673 TA = 163
57732
MA = 163
54313
Ha = 220
639 n
mi
Hp = 216
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14095000
67 X = 4318890
72
Y = 714380
97 feet Y = 265913
29 meter
Z = -17215376
87 Z = -5226322
14
XDOT = -5811
991222 XDOT = -1848
136186
YDOT = 24160
712985 feet/sec YDOT = 7343
946805 meter/sec
ZDOT = -3765
648535 ZDOT = -1156
560787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1249501
07 X = 380847
93
Y = -14170012
18 feet Y = -4319019
71 meter
Z = -17123027
97 Z = -5219098
92
XDOT = 22890
996081 XDOT = 6977
175606
YDOT = 6605
497391 feet/sec YDOT = 2013
355605 meter/sec
ZDOT = -3805
673080 ZDOT = -1159
969155
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 17153
56669576
00016717 00000-0 10270-3 0 9015
2 25544 51
6388 111
2031 0004724 227
9922 132
0829 15
53965796 19474
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
56669576 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 111
2031 deg
Eccentricity:
0004724
Arg of perigee: 227
9922 deg
Mean anomaly: 132
0829 deg
Mean motion: 15
53965796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1947
Checksum: 333
Coasting Arc #3 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2017/154/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900773
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3779696
18 A = 6777939
00 meter
Y = -1887472
57 meter E =
0001822
Z = 5300971
11 I = 51
97953
XDOT = 2566
959353 Wp = 217
43833
YDOT = -7188
485547 meter/sec RA = 105
35838 deg
ZDOT = -730
791162 TA = 239
50116
MA = 239
51915
Ha = 220
517 n
mi
Hp = 216
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12400578
01 X = -3784058
77
Y = -6192495
30 feet Y = -1929764
42 meter
Z = 17391637
50 Z = 5282599
66
XDOT = 8421
782654 XDOT = 2650
701955
YDOT = -23584
270167 feet/sec YDOT = -7159
311789 meter/sec
ZDOT = -2397
608800 ZDOT = -718
118618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6447601
90 X = -1965229
06
Y = 12383609
31 feet Y = 3774524
12 meter
Z = 17310835
86 Z = 5276342
77
XDOT = -22502
513067 XDOT = -6858
765983
YDOT = -8451
475144 feet/sec YDOT = -2576
009624 meter/sec
ZDOT = -2340
459689 ZDOT = -713
372113
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 17154
59563486
00016717 00000-0 10270-3 0 9023
2 25544 51
6395 106
0758 0004785 233
6024 126
4688 15
53983228 19632
Satellite: ISS
Catalog Number: 25544
Epoch time: 17154
59563486 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 106
0758 deg
Eccentricity:
0004785
Arg of perigee: 233
6024 deg
Mean anomaly: 126
4688 deg
Mean motion: 15
53983228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 339
Coasting Arc #4 (Orbit 1967)
---------------------------------------
Vector Time (GMT): 2017/154/21:07:26
000
Vector Time (MET): N/A
Weight (LBS) : 900773
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -408767
19 A = 6787250
12 meter
Y = -6318940
72 meter E =
0011440
Z = 2424188
30 I = 52
01132
XDOT = 4911
935120 Wp = 126
12349
YDOT = -2388
520251 meter/sec RA = 103
69534 deg
ZDOT = -5386
622628 TA = 26
89868
MA = 26
83942
Ha = 220
434 n
mi
Hp = 216
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1341099
70 X = -349852
38
Y = -20731432
82 feet Y = -6323182
58 meter
Z = 7953373
69 Z = 2422345
31
XDOT = 16115
272704 XDOT = 4964
444919
YDOT = -7836
352529 feet/sec YDOT = -2333
297718 meter/sec
ZDOT = -17672
646416 ZDOT = -5362
634367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11117252
12 X = 3388538
45
Y = 17553066
93 feet Y = 5350174
80 meter
Z = 7946291
89 Z = 2422029
77
XDOT = -9242
578235 XDOT = -2817
137846
YDOT = 13822
583134 feet/sec YDOT = 4213
123339 meter/sec
ZDOT = -17566
330147 ZDOT = -5354
217429
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 17154
91717624
00016717 00000-0 10270-3 0 9035
2 25544 51
6373 104
4690 0004977 233
3025 126
7671 15
53988442 19689
Satellite: ISS
Catalog Number: 25544
Epoch time: 17154
91717624 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 104
4690 deg
Eccentricity:
0004977
Arg of perigee: 233
3025 deg
Mean anomaly: 126
7671 deg
Mean motion: 15
53988442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1968
Checksum: 328
Coasting Arc #5 (Orbit 1977)
---------------------------------------
Vector Time (GMT): 2017/155/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 885087
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3210607
30 A = 6779908
16 meter
Y = 3498267
58 meter E =
0009404
Z = -4848144
13 I = 51
99389
XDOT = -3208
088040 Wp = 130
75162
YDOT = 6474
469569 meter/sec RA = 100
38504 deg
ZDOT = 2544
517715 TA = 164
19533
MA = 164
16596
Ha = 220
292 n
mi
Hp = 216
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10533488
52 X = 3194800
29
Y = 11477255
83 feet Y = 3534082
72 meter
Z = -15905984
66 Z = -4832585
97
XDOT = -10525
223229 XDOT = -3292
608976
YDOT = 21241
698062 feet/sec YDOT = 6438
121791 meter/sec
ZDOT = 8348
155234 ZDOT = 2528
728813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11512086
93 X = 3508884
10
Y = -10597906
53 feet Y = -3230241
91 meter
Z = -15837877
43 Z = -4827385
04
XDOT = 20433
387995 XDOT = 6228
096661
YDOT = 9812
490815 feet/sec YDOT = 2990
847200 meter/sec
ZDOT = 8277
347969 ZDOT = 2522
935661
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 17155
56026326
00016717 00000-0 10270-3 0 9040
2 25544 51
6397 101
2674 0004639 236
4937 123
5773 15
53976426 19781
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
56026326 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 101
2674 deg
Eccentricity:
0004639
Arg of perigee: 236
4937 deg
Mean anomaly: 123
5773 deg
Mean motion: 15
53976426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1978
Checksum: 335
Coasting Arc #6 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2017/156/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 885087
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2604885
50 A = 6783349
67 meter
Y = -4886440
25 meter E =
0007007
Z = 3911583
91 I = 52
01040
XDOT = 3730
869635 Wp = 94
65489
YDOT = -5288
285939 meter/sec RA = 95
42161 deg
ZDOT = -4115
939866 TA = 38
28474
MA = 38
23502
Ha = 220
273 n
mi
Hp = 216
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8546212
27 X = -2569051
24
Y = -16031628
12 feet Y = -4915369
81 meter
Z = 12833280
54 Z = 3899016
65
XDOT = 12240
385943 XDOT = 3809
720818
YDOT = -17350
019485 feet/sec YDOT = -5246
123600 meter/sec
ZDOT = -13503
739719 ZDOT = -4097
625148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15909973
12 X = -4849359
81
Y = 8850055
15 feet Y = 2697496
81 meter
Z = 12778623
28 Z = 3894924
38
XDOT = -16874
198155 XDOT = -5143
255598
YDOT = -10927
726103 feet/sec YDOT = -3330
770916 meter/sec
ZDOT = -13421
963607 ZDOT = -4091
014507
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 17156
58919845
00016717 00000-0 10270-3 0 9051
2 25544 51
6398 96
1404 0004690 240
5079 119
5606 15
53971412 19943
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
58919845 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 96
1404 deg
Eccentricity:
0004690
Arg of perigee: 240
5079 deg
Mean anomaly: 119
5606 deg
Mean motion: 15
53971412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1994
Checksum: 338
Coasting Arc #7 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2017/156/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1726166
95 A = 6786225
61 meter
Y = 5891465
69 meter E =
0000294
Z = -2892468
95 I = 52
02112
XDOT = -4329
768733 Wp = 167
68997
YDOT = 3763
534249 meter/sec RA = 95
25124 deg
ZDOT = 5081
574131 TA = 159
57746
MA = 159
57628
Ha = 220
149 n
mi
Hp = 216
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5663277
39 X = 1674209
11
Y = 19328955
66 feet Y = 5910478
58 meter
Z = -9489727
54 Z = -2884209
36
XDOT = -14205
277994 XDOT = -4396
215869
YDOT = 12347
553312 feet/sec YDOT = 3714
743887 meter/sec
ZDOT = 16671
831140 ZDOT = 5060
380111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17488401
77 X = 5330464
86
Y = -10025410
97 feet Y = -3055745
26 meter
Z = -9454263
85 Z = -2881659
62
XDOT = 14584
345893 XDOT = 4445
308628
YDOT = 9807
292574 feet/sec YDOT = 2989
262777 meter/sec
ZDOT = 16577
601237 ZDOT = 5052
852857
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 17156
58919829
00016717 00000-0 10270-3 0 9064
2 25544 51
6406 96
1401 0004697 240
2315 119
8371 15
53984954 19944
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
58919829 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 96
1401 deg
Eccentricity:
0004697
Arg of perigee: 240
2315 deg
Mean anomaly: 119
8371 deg
Mean motion: 15
53984954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1994
Checksum: 342
Coasting Arc #8 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2017/156/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1540499
74 A = 6789000
14 meter
Y = 6468366
79 meter E =
0008882
Z = 1348797
49 I = 52
02821
XDOT = -4406
626407 Wp = 59
16346
YDOT = -2273
906227 meter/sec RA = 94
28644 deg
ZDOT = 5847
916148 TA = 315
44331
MA = 315
51469
Ha = 220
121 n
mi
Hp = 216
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5054133
00 X = -1619268
10
Y = 21221675
83 feet Y = 6450699
34 meter
Z = 4425188
61 Z = 1341123
37
XDOT = -14457
435719 XDOT = -4409
278156
YDOT = -7460
322267 feet/sec YDOT = -2323
199446 meter/sec
ZDOT = 19186
076600 ZDOT = 5826
503203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6542654
35 X = 1994201
05
Y = -20818404
56 feet Y = -6345449
71 meter
Z = 4390191
97 Z = 1338130
51
XDOT = 12511
875871 XDOT = 3813
619766
YDOT = 7974
999878 feet/sec YDOT = 2430
779963 meter/sec
ZDOT = 19091
913329 ZDOT = 5819
215183
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 17156
84642963
00016717 00000-0 10270-3 0 9076
2 25544 51
6379 94
8562 0004923 241
2653 118
8005 15
53981048 19982
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
84642963 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 94
8562 deg
Eccentricity:
0004923
Arg of perigee: 241
2653 deg
Mean anomaly: 118
8005 deg
Mean motion: 15
53981048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1998
Checksum: 342
Coasting Arc #9 (Orbit 2012)
---------------------------------------
Vector Time (GMT): 2017/157/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2189448
08 A = 6786229
17 meter
Y = -5734072
56 meter E =
0004062
Z = -2889100
36 I = 52
02079
XDOT = 4018
055738 Wp = 183
75637
YDOT = 4094
908843 meter/sec RA = 89
33828 deg
ZDOT = -5085
804965 TA = 28
94756
MA = 28
92503
Ha = 220
015 n
mi
Hp = 216
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7183228
62 X = 2267439
28
Y = -18812574
02 feet Y = -5709152
29 meter
Z = -9478675
71 Z = -2878275
71
XDOT = 13182
597567 XDOT = 3996
671442
YDOT = 13434
740300 feet/sec YDOT = 4139
722426 meter/sec
ZDOT = -16685
711827 ZDOT = -5066
337742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8216983
94 X = -2504536
70
Y = 18409660
79 feet Y = 5611264
61 meter
Z = -9429876
59 Z = -2874226
38
XDOT = -11229
641445 XDOT = -3422
794712
YDOT = -13509
431669 feet/sec YDOT = -4117
674773 meter/sec
ZDOT = -16600
459917 ZDOT = -5059
820183
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 17157
81105352
00016717 00000-0 10270-3 0 9081
2 25544 51
6382 90
0482 0004826 245
8449 114
2199 15
53989495 20137
Satellite: ISS
Catalog Number: 25544
Epoch time: 17157
81105352 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 90
0482 deg
Eccentricity:
0004826
Arg of perigee: 245
8449 deg
Mean anomaly: 114
2199 deg
Mean motion: 15
53989495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2013
Checksum: 322
Coasting Arc #10 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2017/158/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2789721
34 A = 6782550
33 meter
Y = 4597960
94 meter E =
0007022
Z = 4130822
76 I = 52
00720
XDOT = -3558
340236 Wp = 126
77279
YDOT = -5608
209300 meter/sec RA = 84
38100 deg
ZDOT = 3830
738993 TA = 283
84523
MA = 283
92335
Ha = 219
870 n
mi
Hp = 216
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9152629
06 X = -2860995
37
Y = 15085173
69 feet Y = 4566365
37 meter
Z = 13552568
10 Z = 4117098
41
XDOT = -11674
344605 XDOT = -3513
971396
YDOT = -18399
636810 feet/sec YDOT = -5647
753449 meter/sec
ZDOT = 12568
041317 ZDOT = 3813
560545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9763380
67 X = 2975878
43
Y = -14753661
16 feet Y = -4496915
92 meter
Z = 13491147
70 Z = 4112101
82
XDOT = 10029
091971 XDOT = 3056
867233
YDOT = 18086
805374 feet/sec YDOT = 5512
858278 meter/sec
ZDOT = 12493
171326 ZDOT = 3807
918620
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 17158
83998174
00016717 00000-0 10270-3 0 9097
2 25544 51
6382 84
9194 0004928 249
1421 110
9204 15
53994576 20292
Satellite: ISS
Catalog Number: 25544
Epoch time: 17158
83998174 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 84
9194 deg
Eccentricity:
0004928
Arg of perigee: 249
1421 deg
Mean anomaly: 110
9204 deg
Mean motion: 15
53994576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 343
Coasting Arc #11 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2017/159/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3374541
78 A = 6779309
40 meter
Y = -3135006
81 meter E =
0007754
Z = -4981357
15 I = 51
99185
XDOT = 2994
761264 Wp = 76
25246
YDOT = 6703
482386 meter/sec RA = 79
41491 deg
ZDOT = -2191
129870 TA = 172
47214
MA = 172
46050
Ha = 219
870 n
mi
Hp = 216
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11071331
31 X = 3433544
71
Y = -10285455
41 feet Y = -3096939
83 meter
Z = -16343035
26 Z = -4964821
59
XDOT = 9825
332232 XDOT = 2930
222143
YDOT = 21993
052447 feet/sec YDOT = 6736
611267 meter/sec
ZDOT = -7188
746293 ZDOT = -2176
737943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11359267
36 X = -3462304
69
Y = 10086222
16 feet Y = 3074280
51 meter
Z = -16269448
03 Z = -4958927
76
XDOT = -8743
359289 XDOT = -2664
975911
YDOT = -21336
402476 feet/sec YDOT = -6503
335475 meter/sec
ZDOT = -7126
389394 ZDOT = -2172
123487
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 17159
80460140
00016717 00000-0 10270-3 0 9104
2 25544 51
6378 80
1121 0004685 250
4093 109
6554 15
53993039 20448
Satellite: ISS
Catalog Number: 25544
Epoch time: 17159
80460140 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 80
1121 deg
Eccentricity:
0004685
Arg of perigee: 250
4093 deg
Mean anomaly: 109
6554 deg
Mean motion: 15
53993039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 296
Coasting Arc #12 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2017/160/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3520324
84 A = 6778632
96 meter
Y = 2701617
94 meter E =
0004593
Z = 5125897
11 I = 51
99180
XDOT = -2831
196956 Wp = 186
50873
YDOT = -6919
647504 meter/sec RA = 77
97372 deg
ZDOT = 1698
338501 TA = 247
13885
MA = 247
18736
Ha = 219
815 n
mi
Hp = 216
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11549622
18 X = -3575172
76
Y = 8863575
90 feet Y = 2661943
91 meter
Z = 16817247
75 Z = 5108663
43
XDOT = -9288
703925 XDOT = -2761
859005
YDOT = -22702
255589 feet/sec YDOT = -6950
920405 meter/sec
ZDOT = 5571
976708 ZDOT = 1684
752741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11384780
82 X = -3470081
19
Y = -9214873
78 feet Y = -2808693
53 meter
Z = 16740652
29 Z = 5102550
82
XDOT = 19158
859958 XDOT = 5839
620515
YDOT = -13628
796845 feet/sec YDOT = -4154
057278 meter/sec
ZDOT = 5513
222851 ZDOT = 1680
430325
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 17160
12613904
00016717 00000-0 10270-3 0 9110
2 25544 51
6416 78
5113 0005004 251
2724 108
7886 15
54009664 20495
Satellite: ISS
Catalog Number: 25544
Epoch time: 17160
12613904 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 78
5113 deg
Eccentricity:
0005004
Arg of perigee: 251
2724 deg
Mean anomaly: 108
7886 deg
Mean motion: 15
54009664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 289
Coasting Arc #13 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2017/161/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4054751
86 A = 6777806
41 meter
Y = -1023826
63 meter E =
0010150
Z = -5342470
42 I = 51
98056
XDOT = 2102
156500 Wp = 98
93507
YDOT = 7364
703796 meter/sec RA = 72
99971 deg
ZDOT = 182
861497 TA = 172
80845
MA = 172
79388
Ha = 219
645 n
mi
Hp = 216
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13302991
65 X = 4091850
50
Y = -3359011
27 feet Y = -978275
45 meter
Z = -17527790
11 Z = -5322683
58
XDOT = 6896
838911 XDOT = 2018
757955
YDOT = 24162
414029 feet/sec YDOT = 7387
745198 meter/sec
ZDOT = 599
939295 ZDOT = 192
871706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6666155
50 X = 2031844
20
Y = 12119291
98 feet Y = 3693960
19 meter
Z = -17440215
09 Z = -5315777
56
XDOT = -20727
262963 XDOT = -6317
669751
YDOT = 12331
827656 feet/sec YDOT = 3758
741069 meter/sec
ZDOT = 642
807583 ZDOT = 195
927751
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 17161
09075487
00016717 00000-0 10270-3 0 9126
2 25544 51
6412 73
7042 0004977 256
0517 104
0083 15
53977396 20640
Satellite: ISS
Catalog Number: 25544
Epoch time: 17161
09075487 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 73
7042 deg
Eccentricity:
0004977
Arg of perigee: 256
0517 deg
Mean anomaly: 104
0083 deg
Mean motion: 15
53977396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 310
Coasting Arc #14 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2017/162/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4503448
01 A = 6779032
31 meter
Y = -661073
83 meter E =
0002528
Z = 5024323
43 I = 51
97535
XDOT = -1215
660003 Wp = 3
27857
YDOT = -7288
763348 meter/sec RA = 68
02573 deg
ZDOT = -2046
140487 TA = 106
53682
MA = 106
50904
Ha = 219
593 n
mi
Hp = 216
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14775091
89 X = -4520126
82
Y = -2168877
41 feet Y = -711528
44 meter
Z = 16484000
77 Z = 5002406
36
XDOT = -3988
385836 XDOT = -1124
125595
YDOT = -23913
265577 feet/sec YDOT = -7301
845580 meter/sec
ZDOT = -6713
059340 ZDOT = -2051
824567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1950266
65 X = -594441
28
Y = -14912470
54 feet Y = -4545321
02 meter
Z = 16387322
33 Z = 4994855
85
XDOT = 20860
262831 XDOT = 6358
208111
YDOT = -10140
316768 feet/sec YDOT = -3090
768551 meter/sec
ZDOT = -6736
821576 ZDOT = -2053
383216
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 17162
11967223
00016717 00000-0 10270-3 0 9139
2 25544 51
6418 68
5765 0004954 260
9281 99
1311 15
54030073 20806
Satellite: ISS
Catalog Number: 25544
Epoch time: 17162
11967223 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 68
5765 deg
Eccentricity:
0004954
Arg of perigee: 260
9281 deg
Mean anomaly: 99
1311 deg
Mean motion: 15
54030073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2080
Checksum: 299
Coasting Arc #15 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2017/163/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4828705
29 A = 6782203
99 meter
Y = 2218311
35 meter E =
0004165
Z = -4218848
63 I = 51
97170
XDOT = 157
574300 Wp = 138
28496
YDOT = 6705
849436 meter/sec RA = 63
05730 deg
ZDOT = 3705
424868 TA = 169
58834
MA = 169
57971
Ha = 219
498 n
mi
Hp = 216
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15842208
95 X = 4824033
80
Y = 7277924
38 feet Y = 2272283
69 meter
Z = -13841366
88 Z = -4195403
25
XDOT = 516
976050 XDOT = 64
576854
YDOT = 22000
818359 feet/sec YDOT = 6707
091022 meter/sec
ZDOT = 12156
905736 ZDOT = 3705
965410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2384641
67 X = -726838
78
Y = 17352286
17 feet Y = 5288976
82 meter
Z = -13738226
01 Z = -4187411
29
XDOT = -19680
192040 XDOT = -5998
522534
YDOT = 6923
694658 feet/sec YDOT = 2110
342132 meter/sec
ZDOT = 12158
046779 ZDOT = 3705
772658
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 17163
08428258
00016717 00000-0 10270-3 0 9147
2 25544 51
6407 63
7695 0004651 264
1770 95
8852 15
54024161 20956
Satellite: ISS
Catalog Number: 25544
Epoch time: 17163
08428258 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 63
7695 deg
Eccentricity:
0004651
Arg of perigee: 264
1770 deg
Mean anomaly: 95
8852 deg
Mean motion: 15
54024161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2095
Checksum: 317
Coasting Arc #16 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2017/164/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4954184
81 A = 6785881
03 meter
Y = -3541535
79 meter E =
0008431
Z = 2984251
21 I = 51
96870
XDOT = 1059
289037 Wp = 102
17658
YDOT = -5710
390963 meter/sec RA = 58
09694 deg
ZDOT = -5008
048414 TA = 43
86031
MA = 43
79340
Ha = 219
430 n
mi
Hp = 216
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16253887
18 X = -4928710
24
Y = -11619211
92 feet Y = -3596794
81 meter
Z = 9790850
44 Z = 2960246
72
XDOT = 3475
357732 XDOT = 1147
392021
YDOT = -18734
878488 feet/sec YDOT = -5698
051979 meter/sec
ZDOT = -16430
605033 ZDOT = -5002
689510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6104575
15 X = 1860674
50
Y = -19078290
00 feet Y = -5815062
79 meter
Z = 9685489
11 Z = 2952137
08
XDOT = 17547
103831 XDOT = 5348
357248
YDOT = -2731
276101 feet/sec YDOT = -832
492955 meter/sec
ZDOT = -16405
866047 ZDOT = -5000
507971
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 17164
11319443
00016717 00000-0 10270-3 0 9158
2 25544 51
6408 58
6413 0004858 269
6177 90
4419 15
54043696 21111
Satellite: ISS
Catalog Number: 25544
Epoch time: 17164
11319443 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 58
6413 deg
Eccentricity:
0004858
Arg of perigee: 269
6177 deg
Mean anomaly: 90
4419 deg
Mean motion: 15
54043696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 313
Coasting Arc #17 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2017/165/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4830659
07 A = 6788787
05 meter
Y = 4532444
33 meter E =
0007066
Z = -1465585
79 I = 51
96055
XDOT = -2375
376847 Wp = 3
61205
YDOT = 4406
907258 meter/sec RA = 53
14421 deg
ZDOT = 5807
716744 TA = 340
46824
MA = 340
49530
Ha = 219
512 n
mi
Hp = 216
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15848618
99 X = 4786736
14
Y = 14870224
18 feet Y = 4586218
63 meter
Z = -4808352
32 Z = -1442226
12
XDOT = -7793
231126 XDOT = -2452
690466
YDOT = 14458
357146 feet/sec YDOT = 4379
911178 meter/sec
ZDOT = 19054
188793 ZDOT = 5795
990690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8995752
60 X = -2741905
39
Y = 19807883
90 feet Y = 6037443
01 meter
Z = -4706029
51 Z = -1434397
79
XDOT = -14790
465330 XDOT = -4508
133833
YDOT = -2209
303610 feet/sec YDOT = -673
395740 meter/sec
ZDOT = 19001
565786 ZDOT = 5791
677251
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 17165
07779764
00016717 00000-0 10270-3 0 9161
2 25544 51
6412 53
8336 0004709 274
0216 86
0398 15
54014084 21268
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
07779764 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 53
8336 deg
Eccentricity:
0004709
Arg of perigee: 274
0216 deg
Mean anomaly: 86
0398 deg
Mean motion: 15
54014084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2126
Checksum: 313
Coasting Arc #18 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2017/165/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5018098
07 A = 6781098
98 meter
Y = 625177
52 meter E =
0004996
Z = -4522952
77 I = 51
92831
XDOT = 2063
977334 Wp = 122
59482
YDOT = 6645
897260 meter/sec RA = 51
57645 deg
ZDOT = 3208
500435 TA = 179
53627
MA = 179
53580
Ha = 219
518 n
mi
Hp = 216
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16463576
35 X = 5032704
44
Y = 2051107
34 feet Y = 681375
50 meter
Z = -14839083
88 Z = -4498540
91
XDOT = 6771
579181 XDOT = 1973
922490
YDOT = 21804
124870 feet/sec YDOT = 6668
474142 meter/sec
ZDOT = 10526
576231 ZDOT = 3218
308639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13668601
75 X = 4166189
81
Y = -9571344
09 feet Y = -2917345
68 meter
Z = -14731377
96 Z = -4490124
00
XDOT = 18885
269001 XDOT = 5756
229991
YDOT = 10703
018956 feet/sec YDOT = 3262
280178 meter/sec
ZDOT = 10568
643359 ZDOT = 3221
322496
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 17165
39933180
00016717 00000-0 10270-3 0 9171
2 25544 51
6408 52
2317 0004757 277
4363 82
6249 15
54021543 21319
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
39933180 = yrday
fracday
Element set: 917
Inclination: 51
6408 deg
RA of node: 52
2317 deg
Eccentricity:
0004757
Arg of perigee: 277
4363 deg
Mean anomaly: 82
6249 deg
Mean motion: 15
54021543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2131
Checksum: 304
Coasting Arc #19 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2017/166/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5526753
91 A = 6784831
07 meter
Y = -1961631
50 meter E =
0007839
Z = 3406018
84 I = 51
91971
XDOT = -718
524569 Wp = 83
94676
YDOT = -6058
502888 meter/sec RA = 46
61077 deg
ZDOT = -4645
222389 TA = 56
40822
MA = 56
33341
Ha = 219
613 n
mi
Hp = 216
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18132394
71 X = -5520952
40
Y = -6435798
88 feet Y = -2023403
33 meter
Z = 11174602
50 Z = 3379185
53
XDOT = -2357
364070 XDOT = -628
159245
YDOT = -19876
977979 feet/sec YDOT = -6066
032162 meter/sec
ZDOT = -15240
230934 ZDOT = -4648
493908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17697044
72 X = -5394059
23
Y = 7722974
89 feet Y = 2353962
75 meter
Z = 11056457
53 Z = 3370008
26
XDOT = -14654
790264 XDOT = -4466
780073
YDOT = -11696
411488 feet/sec YDOT = -3565
066221 meter/sec
ZDOT = -15253
531271 ZDOT = -4649
276332
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 17166
42823718
00016717 00000-0 10270-3 0 9182
2 25544 51
6407 47
1042 0004794 281
4467 78
6147 15
54019647 21478
Satellite: ISS
Catalog Number: 25544
Epoch time: 17166
42823718 = yrday
fracday
Element set: 918
Inclination: 51
6407 deg
RA of node: 47
1042 deg
Eccentricity:
0004794
Arg of perigee: 281
4467 deg
Mean anomaly: 78
6147 deg
Mean motion: 15
54019647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2147
Checksum: 324
Coasting Arc #20 (Orbit 2161)
---------------------------------------
Vector Time (GMT): 2017/167/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907826
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5736381
47 A = 6788053
16 meter
Y = 3043243
34 meter E =
0006639
Z = -1962722
82 I = 51
90798
XDOT = -818
881103 Wp = 357
01081
YDOT = 5159
754397 meter/sec RA = 41
65201 deg
ZDOT = 5612
596335 TA = 341
42019
MA = 341
44442
Ha = 219
672 n
mi
Hp = 216
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18820149
18 X = 5711458
72
Y = 9984394
16 feet Y = 3107252
28 meter
Z = -6439379
32 Z = -1934917
53
XDOT = -2686
617792 XDOT = -903
781181
YDOT = 16928
328075 feet/sec YDOT = 5150
121882 meter/sec
ZDOT = 18414
029970 ZDOT = 5608
412743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20500448
33 X = 6248536
65
Y = -5931015
16 feet Y = -1807773
42 meter
Z = -6317153
29 Z = -1925468
32
XDOT = 9316
010840 XDOT = 2839
520104
YDOT = 12628
437989 feet/sec YDOT = 3849
147899 meter/sec
ZDOT = 18394
569186 ZDOT = 5606
664688
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 17167
39283320
00016717 00000-0 10270-3 0 9199
2 25544 51
6411 42
2962 0004892 284
7819 75
2791 15
54025877 21623
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
39283320 = yrday
fracday
Element set: 919
Inclination: 51
6411 deg
RA of node: 42
2962 deg
Eccentricity:
0004892
Arg of perigee: 284
7819 deg
Mean anomaly: 75
2791 deg
Mean motion: 15
54025877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2162
Checksum: 326
Coasting Arc #21 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2017/167/11:41:11
000
Vector Time (MET): N/A
Weight (LBS) : 922259
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5607232
23 A = 6789090
21 meter
Y = -3611072
64 meter E =
0009236
Z = 1241746
98 I = 51
91019
XDOT = 1683
013718 Wp = 130
58801
YDOT = -4639
322369 meter/sec RA = 41
17306 deg
ZDOT = -5868
898412 TA = 35
96378
MA = 35
90166
Ha = 219
638 n
mi
Hp = 216
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18396431
20 X = -5572467
32
Y = -11847351
19 feet Y = -3673582
25 meter
Z = 4073973
04 Z = 1214592
91
XDOT = 5521
698550 XDOT = 1763
274960
YDOT = -15220
873913 feet/sec YDOT = -4620
052456 meter/sec
ZDOT = -19254
916049 ZDOT = -5860
528347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15042929
72 X = -4585084
98
Y = 15920302
32 feet Y = 4852508
15 meter
Z = 3954732
19 Z = 1205402
37
XDOT = -12758
208528 XDOT = -3888
701959
YDOT = -7262
362734 feet/sec YDOT = -2213
568161 meter/sec
ZDOT = -19217
064034 ZDOT = -5857
361117
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 17167
52144586
00016717 00000-0 10270-3 0 9206
2 25544 51
6425 41
6565 0004828 284
1940 75
8676 15
53999020 21647
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
52144586 = yrday
fracday
Element set: 920
Inclination: 51
6425 deg
RA of node: 41
6565 deg
Eccentricity:
0004828
Arg of perigee: 284
1940 deg
Mean anomaly: 75
8676 deg
Mean motion: 15
53999020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 327
Coasting Arc #22 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2017/167/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922259
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3500204
24 A = 6777959
68 meter
Y = -2457769
36 meter E =
0009738
Z = -5266687
93 I = 51
86503
XDOT = 5291
090956 Wp = 95
52058
YDOT = 5454
788109 meter/sec RA = 40
11253 deg
ZDOT = 971
503271 TA = 183
75341
MA = 183
76072
Ha = 219
583 n
mi
Hp = 216
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11483609
71 X = 3553010
50
Y = -8063547
77 feet Y = -2418331
97 meter
Z = -17279159
87 Z = -5249556
99
XDOT = 17359
222296 XDOT = 5224
981754
YDOT = 17896
286447 feet/sec YDOT = 5513
586947 meter/sec
ZDOT = 3187
346690 ZDOT = 997
045675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13860922
05 X = -4224809
04
Y = 2719197
59 feet Y = 828811
43 meter
Z = -17203030
68 Z = -5243483
75
XDOT = -8476
249319 XDOT = -2583
560792
YDOT = -22348
335924 feet/sec YDOT = -6811
772790 meter/sec
ZDOT = 3299
115781 ZDOT = 1005
570490
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 17167
71436413
00016717 00000-0 10270-3 0 9211
2 25544 51
6394 40
6896 0004629 281
6856 78
3777 15
54035344 21679
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
71436413 = yrday
fracday
Element set: 921
Inclination: 51
6394 deg
RA of node: 40
6896 deg
Eccentricity:
0004629
Arg of perigee: 281
6856 deg
Mean anomaly: 78
3777 deg
Mean motion: 15
54035344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 334
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