[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 27th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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
179/14:22:30
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
1
180/09:42:42
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
0
183/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 216
2
187/05:25:00
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
1
Coasting Arc #1 (Orbit 3980)
---------------------------------------
Vector Time (GMT): 2018/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6279606
03 A = 6787024
57 meter
Y = -531973
99 meter E =
0010501
Z = 2509307
87 I = 51
50162
XDOT = -1670
803411 Wp = 86
69247
YDOT = 5297
509573 meter/sec RA = 336
69427 deg
ZDOT = 5285
756110 TA = 301
51536
MA = 301
61790
Ha = 220
614 n
mi
Hp = 215
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20602381
98 X = 6272899
07
Y = -1745321
50 feet Y = -461788
99 meter
Z = 8232637
38 Z = 2539795
73
XDOT = -5481
638487 XDOT = -1755
592909
YDOT = 17380
280750 feet/sec YDOT = 5278
350619 meter/sec
ZDOT = 17341
719522 ZDOT = 5277
434760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2711645
03 X = -826509
41
Y = -20442250
30 feet Y = -6230797
89 meter
Z = 8369109
43 Z = 2550904
55
XDOT = 16135
569233 XDOT = 4918
121502
YDOT = 4968
281361 feet/sec YDOT = 1514
332159 meter/sec
ZDOT = 17303
619849 ZDOT = 5274
143330
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 18176
55918965
00016717 00000-0 10270-3 0 9008
2 25544 51
6377 336
9772 0003910 225
4028 134
6805 15
53973338 39819
Satellite: ISS
Catalog Number: 25544
Epoch time: 18176
55918965 = yrday
fracday
Element set: 900
Inclination: 51
6377 deg
RA of node: 336
9772 deg
Eccentricity:
0003910
Arg of perigee: 225
4028 deg
Mean anomaly: 134
6805 deg
Mean motion: 15
53973338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3981
Checksum: 341
Coasting Arc #2 (Orbit 3995)
---------------------------------------
Vector Time (GMT): 2018/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5573165
88 A = 6783395
83 meter
Y = -473767
83 meter E =
0003355
Z = -3840143
94 I = 51
45994
XDOT = 3319
296946 Wp = 103
20496
YDOT = -5531
116006 meter/sec RA = 331
70415 deg
ZDOT = -4138
682958 TA = 123
15024
MA = 123
11804
Ha = 220
455 n
mi
Hp = 215
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18284664
95 X = -5548800
48
Y = -1554356
41 feet Y = -535953
96 meter
Z = -12598897
45 Z = -3867157
35
XDOT = 10890
081843 XDOT = 3401
004240
YDOT = -18146
706056 feet/sec YDOT = -5493
539816 meter/sec
ZDOT = -13578
356163 ZDOT = -4122
361406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -381275
63 X = -116212
81
Y = 18263136
06 feet Y = 5566603
87 meter
Z = -12719658
14 Z = -3876951
80
XDOT = -17484
780237 XDOT = -5329
361016
YDOT = -9761
798209 feet/sec YDOT = -2975
396094 meter/sec
ZDOT = -13504
434995 ZDOT = -4116
151786
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 18177
52382121
00016717 00000-0 10270-3 0 9016
2 25544 51
6380 332
1703 0003810 229
4612 130
6209 15
53978055 39968
Satellite: ISS
Catalog Number: 25544
Epoch time: 18177
52382121 = yrday
fracday
Element set: 901
Inclination: 51
6380 deg
RA of node: 332
1703 deg
Eccentricity:
0003810
Arg of perigee: 229
4612 deg
Mean anomaly: 130
6209 deg
Mean motion: 15
53978055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3996
Checksum: 298
Coasting Arc #3 (Orbit 4011)
---------------------------------------
Vector Time (GMT): 2018/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4550966
75 A = 6779919
68 meter
Y = 1567466
14 meter E =
0006697
Z = 4774515
20 I = 51
42051
XDOT = -4637
251182 Wp = 151
45350
YDOT = 5526
151530 meter/sec RA = 326
70072 deg
ZDOT = 2598
619819 TA = 272
81715
MA = 272
89380
Ha = 220
250 n
mi
Hp = 216
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14930993
26 X = 4509908
68
Y = 5142605
44 feet Y = 1618127
81 meter
Z = 15664419
96 Z = 4796522
69
XDOT = -15214
078681 XDOT = -4711
324158
YDOT = 18130
418406 feet/sec YDOT = 5473
879988 meter/sec
ZDOT = 8525
655574 ZDOT = 2575
914746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3918561
95 X = 1194377
68
Y = -15196712
46 feet Y = -4631957
96 meter
Z = 15762607
83 Z = 4804442
87
XDOT = 18206
973312 XDOT = 5549
485466
YDOT = 13456
253274 feet/sec YDOT = 4101
465998 meter/sec
ZDOT = 8423
186804 ZDOT = 2567
387338
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 18178
55275710
00016717 00000-0 10270-3 0 9026
2 25544 51
6386 327
0414 0004003 234
5209 125
5570 15
53997615 40127
Satellite: ISS
Catalog Number: 25544
Epoch time: 18178
55275710 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 327
0414 deg
Eccentricity:
0004003
Arg of perigee: 234
5209 deg
Mean anomaly: 125
5570 deg
Mean motion: 15
53997615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4012
Checksum: 297
Coasting Arc #4 (Orbit 4026)
---------------------------------------
Vector Time (GMT): 2018/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3304636
12 A = 6777924
83 meter
Y = -2738522
00 meter E =
0011353
Z = -5255752
68 I = 51
38783
XDOT = 5566
277966 Wp = 92
38702
YDOT = -5202
715280 meter/sec RA = 321
68922 deg
ZDOT = -790
942937 TA = 170
03082
MA = 170
00828
Ha = 220
292 n
mi
Hp = 215
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10841982
02 X = -3248238
11
Y = -8984652
24 feet Y = -2775160
50 meter
Z = -17243283
06 Z = -5271668
83
XDOT = 18262
066817 XDOT = 5627
884418
YDOT = -17069
275854 feet/sec YDOT = -5140
124729 meter/sec
ZDOT = -2594
957141 ZDOT = -763
755299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7884300
66 X = -2403134
84
Y = 11561374
06 feet Y = 3523906
81 meter
Z = -17314034
58 Z = -5277317
74
XDOT = -17945
852054 XDOT = -5469
895706
YDOT = -15931
438481 feet/sec YDOT = -4855
902449 meter/sec
ZDOT = -2472
497908 ZDOT = -753
617362
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 18179
51738186
00016717 00000-0 10270-3 0 9035
2 25544 51
6397 322
2347 0003760 237
4251 122
6539 15
53997155 40277
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
51738186 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 322
2347 deg
Eccentricity:
0003760
Arg of perigee: 237
4251 deg
Mean anomaly: 122
6539 deg
Mean motion: 15
53997155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4027
Checksum: 326
Coasting Arc #5 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2018/179/14:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2050754
86 A = 6777856
48 meter
Y = 3745783
61 meter E =
0000863
Z = 5263838
35 I = 51
38710
XDOT = -6270
140267 Wp = 226
82708
YDOT = 4364
366172 meter/sec RA = 321
18212 deg
ZDOT = -663
558157 TA = 229
52733
MA = 229
53486
Ha = 220
123 n
mi
Hp = 216
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6728198
37 X = 1983147
30
Y = 12289316
32 feet Y = 3768337
67 meter
Z = 17269810
84 Z = 5273636
55
XDOT = -20571
326334 XDOT = -6315
254607
YDOT = 14318
786652 feet/sec YDOT = 4293
997002 meter/sec
ZDOT = -2177
028074 ZDOT = -694
124967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4849806
70 X = 1478221
08
Y = -13087420
84 feet Y = -3989045
87 meter
Z = 17313032
84 Z = 5277012
41
XDOT = 23378
565993 XDOT = 7125
786915
YDOT = 5604
452347 feet/sec YDOT = 1708
237075 meter/sec
ZDOT = -2314
466144 ZDOT = -705
449281
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 18179
64599685
00016717 00000-0 10270-3 0 9049
2 25544 51
6417 321
5937 0003900 239
7696 120
3071 15
54010044 40293
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
64599685 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 321
5937 deg
Eccentricity:
0003900
Arg of perigee: 239
7696 deg
Mean anomaly: 120
3071 deg
Mean motion: 15
54010044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 316
Coasting Arc #6 (Orbit 4040)
---------------------------------------
Vector Time (GMT): 2018/180/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1328769
47 A = 6778792
83 meter
Y = -4302402
19 meter E =
0010768
Z = -5076764
89 I = 51
36550
XDOT = 6313
508473 Wp = 115
68341
YDOT = -3981
960339 meter/sec RA = 317
14457 deg
ZDOT = 1720
400072 TA = 171
03571
MA = 171
01647
Ha = 220
228 n
mi
Hp = 216
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4359479
88 X = -1255900
06
Y = -14115492
76 feet Y = -4316853
15 meter
Z = -16656052
80 Z = -5083043
24
XDOT = 20713
610476 XDOT = 6349
209900
YDOT = -13064
174339 feet/sec YDOT = -3911
158993 meter/sec
ZDOT = 5644
357191 ZDOT = 1751
154694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14470453
00 X = -4410594
07
Y = -2818675
25 feet Y = -859132
22 meter
Z = -16683445
54 Z = -5085114
20
XDOT = -2129
762445 XDOT = -649
151593
YDOT = -23326
027702 feet/sec YDOT = -7109
773244 meter/sec
ZDOT = 5782
567233 ZDOT = 1762
526492
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 18180
41769420
00016717 00000-0 10270-3 0 9053
2 25544 51
6376 317
7476 0003645 242
3951 117
6832 15
53988752 40419
Satellite: ISS
Catalog Number: 25544
Epoch time: 18180
41769420 = yrday
fracday
Element set: 905
Inclination: 51
6376 deg
RA of node: 317
7476 deg
Eccentricity:
0003645
Arg of perigee: 242
3951 deg
Mean anomaly: 117
6832 deg
Mean motion: 15
53988752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4041
Checksum: 326
Coasting Arc #7 (Orbit 4056)
---------------------------------------
Vector Time (GMT): 2018/181/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -21889
76 A = 6781792
80 meter
Y = 5203688
85 meter E =
0005872
Z = 4345042
19 I = 51
35126
XDOT = -6252
042908 Wp = 74
47614
YDOT = 2834
166432 meter/sec RA = 312
13264 deg
ZDOT = -3420
327754 TA = 50
37222
MA = 50
32041
Ha = 220
120 n
mi
Hp = 216
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -71816
78 X = -101182
88
Y = 17072469
97 feet Y = 5203000
05 meter
Z = 14255387
77 Z = 4344744
06
XDOT = -20511
951799 XDOT = -6266
656724
YDOT = 9298
446299 feet/sec YDOT = 2764
170581 meter/sec
ZDOT = -11221
547750 ZDOT = -3450
732724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15166319
00 X = 4622694
03
Y = 7843386
39 feet Y = 2390664
17 meter
Z = 14253228
64 Z = 4344384
09
XDOT = -339
167541 XDOT = -103
378267
YDOT = 21328
181310 feet/sec YDOT = 6500
829663 meter/sec
ZDOT = -11358
002813 ZDOT = -3461
919258
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 18181
44661943
00016717 00000-0 10270-3 0 9069
2 25544 51
6371 312
6198 0003776 246
6820 113
3935 15
53966319 40575
Satellite: ISS
Catalog Number: 25544
Epoch time: 18181
44661943 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 312
6198 deg
Eccentricity:
0003776
Arg of perigee: 246
6820 deg
Mean anomaly: 113
3935 deg
Mean motion: 15
53966319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4057
Checksum: 328
Coasting Arc #8 (Orbit 4071)
---------------------------------------
Vector Time (GMT): 2018/182/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1230181
34 A = 6785382
93 meter
Y = -5859028
28 meter E =
0001087
Z = -3195034
87 I = 51
34424
XDOT = 5833
882698 Wp = 109
81869
YDOT = -1378
383845 meter/sec RA = 307
12770 deg
ZDOT = 4774
849673 TA = 213
10206
MA = 213
10887
Ha = 220
044 n
mi
Hp = 216
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4036028
03 X = 1311126
76
Y = -19222533
74 feet Y = -5844818
52 meter
Z = -10482397
85 Z = -3188863
35
XDOT = 19140
035097 XDOT = 5825
669189
YDOT = -4522
256708 feet/sec YDOT = -1313
191920 meter/sec
ZDOT = 15665
517300 ZDOT = 4803
168145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15519839
43 X = -4730447
06
Y = -12063459
30 feet Y = -3676942
40 meter
Z = -10453876
02 Z = -3186341
41
XDOT = 3335
761664 XDOT = 1016
740155
YDOT = -17974
038800 feet/sec YDOT = -5478
487026 meter/sec
ZDOT = 15792
404128 ZDOT = 4813
524778
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 18182
41123175
00016717 00000-0 10270-3 0 9078
2 25544 51
6390 307
8119 0003666 250
1660 109
9097 15
54005430 40721
Satellite: ISS
Catalog Number: 25544
Epoch time: 18182
41123175 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 307
8119 deg
Eccentricity:
0003666
Arg of perigee: 250
1660 deg
Mean anomaly: 109
9097 deg
Mean motion: 15
54005430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4072
Checksum: 293
Coasting Arc #9 (Orbit 4087)
---------------------------------------
Vector Time (GMT): 2018/183/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2256078
49 A = 6788459
06 meter
Y = 6163223
71 meter E =
0011384
Z = 1708954
06 I = 51
33408
XDOT = -5159
040978 Wp = 127
61903
YDOT = -311
798757 meter/sec RA = 302
13130 deg
ZDOT = -5667
101547 TA = 33
55326
MA = 33
48121
Ha = 219
935 n
mi
Hp = 216
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7401832
33 X = -2333130
76
Y = 20220550
22 feet Y = 6137563
65 meter
Z = 5606804
66 Z = 1697808
56
XDOT = -16925
987461 XDOT = -5127
643514
YDOT = -1022
961801 feet/sec YDOT = -369
314475 meter/sec
ZDOT = -18592
852843 ZDOT = -5692
085824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15231451
15 X = 4642546
31
Y = 15239021
29 feet Y = 4644853
69 meter
Z = 5556001
92 Z = 1693469
39
XDOT = -6870
873424 XDOT = -2094
242220
YDOT = 13710
061943 feet/sec YDOT = 4178
826880 meter/sec
ZDOT = -18704
560888 ZDOT = -5701
150159
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 18183
44014635
00016717 00000-0 10270-3 0 9083
2 25544 51
6376 302
6837 0003688 255
4590 104
6154 15
54010291 40883
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
44014635 = yrday
fracday
Element set: 908
Inclination: 51
6376 deg
RA of node: 302
6837 deg
Eccentricity:
0003688
Arg of perigee: 255
4590 deg
Mean anomaly: 104
6154 deg
Mean motion: 15
54010291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4088
Checksum: 310
Coasting Arc #10 (Orbit 4088)
---------------------------------------
Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1688818
69 A = 6787599
98 meter
Y = -6174164
24 meter E =
0003517
Z = -2252118
11 I = 51
33245
XDOT = 5399
805973 Wp = 8
21566
YDOT = -497
627034 meter/sec RA = 301
65066 deg
ZDOT = 5417
915091 TA = 326
62857
MA = 326
65074
Ha = 219
957 n
mi
Hp = 216
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5540743
74 X = 1768673
83
Y = -20256444
36 feet Y = -6154831
94 meter
Z = -7388838
95 Z = -2243721
31
XDOT = 17715
898862 XDOT = 5378
652235
YDOT = -1632
634625 feet/sec YDOT = -437
361601 meter/sec
ZDOT = 17775
311977 ZDOT = 5444
093690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20905602
96 X = -6372027
78
Y = -2132303
16 feet Y = -649926
00 meter
Z = -7350331
15 Z = -2240380
94
XDOT = -4699
234669 XDOT = -1432
326727
YDOT = -15554
578934 feet/sec YDOT = -4741
035659 meter/sec
ZDOT = 17892
486574 ZDOT = 5453
629908
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 18183
50445358
00016717 00000-0 10270-3 0 9091
2 25544 51
6407 302
3640 0003727 256
1047 103
9691 15
53990362 40890
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
50445358 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 302
3640 deg
Eccentricity:
0003727
Arg of perigee: 256
1047 deg
Mean anomaly: 103
9691 deg
Mean motion: 15
53990362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4089
Checksum: 315
Coasting Arc #11 (Orbit 4104)
---------------------------------------
Vector Time (GMT): 2018/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2568149
08 A = 6789523
81 meter
Y = 6245930
01 meter E =
0011130
Z = 633525
76 I = 51
32181
XDOT = -4666
069710 Wp = 143
57248
YDOT = -1311
088390 meter/sec RA = 296
65788 deg
ZDOT = -5943
976439 TA = 29
55615
MA = 29
49329
Ha = 219
868 n
mi
Hp = 216
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8425685
97 X = -2640879
22
Y = 20491896
36 feet Y = 6216804
47 meter
Z = 2078496
59 Z = 620874
74
XDOT = -15308
627657 XDOT = -4622
189624
YDOT = -4301
471097 feet/sec YDOT = -1363
021636 meter/sec
ZDOT = -19501
235035 ZDOT = -5966
535872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21693816
60 X = 6612275
30
Y = 4530360
89 feet Y = 1380854
00 meter
Z = 2020965
11 Z = 615990
17
XDOT = -1110
400373 XDOT = -338
450034
YDOT = 14129
295543 feet/sec YDOT = 4306
609282 meter/sec
ZDOT = -19601
945110 ZDOT = -5974
672870
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 18184
53336460
00016717 00000-0 10270-3 0 9100
2 25544 51
6399 297
2363 0003795 257
4132 102
6596 15
54006778 41057
Satellite: ISS
Catalog Number: 25544
Epoch time: 18184
53336460 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 297
2363 deg
Eccentricity:
0003795
Arg of perigee: 257
4132 deg
Mean anomaly: 102
6596 deg
Mean motion: 15
54006778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4105
Checksum: 321
Coasting Arc #12 (Orbit 4120)
---------------------------------------
Vector Time (GMT): 2018/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3223651
07 A = 6789172
28 meter
Y = -5878817
15 meter E =
0010438
Z = 1030685
69 I = 51
30809
XDOT = 3816
735922 Wp = 46
93829
YDOT = 3127
512225 meter/sec RA = 291
66581 deg
ZDOT = 5870
440128 TA = 324
28704
MA = 324
35681
Ha = 219
821 n
mi
Hp = 216
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10576283
05 X = 3284143
56
Y = -19287457
86 feet Y = -5842429
92 meter
Z = 3381514
73 Z = 1046491
30
XDOT = 12522
099482 XDOT = 3752
964340
YDOT = 10260
866880 feet/sec YDOT = 3169
836490 meter/sec
ZDOT = 19259
974172 ZDOT = 5888
825724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21012345
31 X = -6404562
85
Y = -6469619
87 feet Y = -1971940
14 meter
Z = 3453085
44 Z = 1052500
44
XDOT = 7095
437651 XDOT = 2162
689396
YDOT = -12668
781144 feet/sec YDOT = -3861
444493 meter/sec
ZDOT = 19341
747048 ZDOT = 5895
364500
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 18185
56227058
00016717 00000-0 10270-3 0 9117
2 25544 51
6411 292
1081 0003703 263
7767 96
2964 15
54021728 41213
Satellite: ISS
Catalog Number: 25544
Epoch time: 18185
56227058 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 292
1081 deg
Eccentricity:
0003703
Arg of perigee: 263
7767 deg
Mean anomaly: 96
2964 deg
Mean motion: 15
54021728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4121
Checksum: 304
Coasting Arc #13 (Orbit 4135)
---------------------------------------
Vector Time (GMT): 2018/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3698767
45 A = 6786682
72 meter
Y = 5052586
33 meter E =
0003152
Z = -2612637
68 I = 51
28812
XDOT = -2910
172741 Wp = 174
19362
YDOT = -4818
956646 meter/sec RA = 286
66934 deg
ZDOT = -5203
029931 TA = 35
37607
MA = 35
35516
Ha = 219
769 n
mi
Hp = 216
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12135063
80 X = -3742301
23
Y = 16576726
82 feet Y = 5010980
98 meter
Z = -8571645
93 Z = -2630710
18
XDOT = -9547
810829 XDOT = -2830
796157
YDOT = -15810
225215 feet/sec YDOT = -4851
055931 meter/sec
ZDOT = -17070
308171 ZDOT = -5216
974071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18805708
61 X = 5731979
98
Y = 8184610
88 feet Y = 2494669
40 meter
Z = -8653220
68 Z = -2637501
66
XDOT = -12784
958902 XDOT = -3896
855473
YDOT = 11275
502998 feet/sec YDOT = 3436
773314 meter/sec
ZDOT = -17131
974264 ZDOT = -5221
825756
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 18186
52686550
00016717 00000-0 10270-3 0 9121
2 25544 51
6406 287
3008 0003728 267
4286 92
6439 15
54023823 41367
Satellite: ISS
Catalog Number: 25544
Epoch time: 18186
52686550 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 287
3008 deg
Eccentricity:
0003728
Arg of perigee: 267
4286 deg
Mean anomaly: 92
6439 deg
Mean motion: 15
54023823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4136
Checksum: 322
Coasting Arc #14 (Orbit 4146)
---------------------------------------
Vector Time (GMT): 2018/187/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2045004
52 A = 6783028
76 meter
Y = -5142738
28 meter E =
0002998
Z = -3925116
82 I = 51
26596
XDOT = 4411
852278 Wp = 118
97694
YDOT = -4814
675331 meter/sec RA = 282
98724 deg
ZDOT = 4010
557196 TA = 193
15442
MA = 193
16224
Ha = 219
767 n
mi
Hp = 216
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6709332
40 X = -1968278
96
Y = -16872500
92 feet Y = -5165177
59 meter
Z = -12877679
87 Z = -3934864
80
XDOT = 14474
580966 XDOT = 4445
882326
YDOT = -15796
178906 feet/sec YDOT = -4765
149033 meter/sec
ZDOT = 13157
996049 ZDOT = 4032
070575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7934169
24 X = -2418334
78
Y = -16298457
77 feet Y = -4967769
93 meter
Z = -12920537
92 Z = -3938179
96
XDOT = 11907
769931 XDOT = 3629
488275
YDOT = -16302
201710 feet/sec YDOT = -4968
911081 meter/sec
ZDOT = 13254
918487 ZDOT = 4040
099155
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 18187
23423223
00016717 00000-0 10270-3 0 9137
2 25544 51
6370 283
7761 0003776 276
6270 83
4453 15
54034982 41475
Satellite: ISS
Catalog Number: 25544
Epoch time: 18187
23423223 = yrday
fracday
Element set: 913
Inclination: 51
6370 deg
RA of node: 283
7761 deg
Eccentricity:
0003776
Arg of perigee: 276
6270 deg
Mean anomaly: 83
4453 deg
Mean motion: 15
54034982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4147
Checksum: 316
Coasting Arc #15 (Orbit 4162)
---------------------------------------
Vector Time (GMT): 2018/188/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1249659
06 A = 6786594
14 meter
Y = 6135799
72 meter E =
0009560
Z = 2605464
69 I = 51
27268
XDOT = -4658
518960 Wp = 103
18155
YDOT = 3164
923264 meter/sec RA = 277
98035 deg
ZDOT = -5204
923911 TA = 47
31785
MA = 47
23735
Ha = 219
685 n
mi
Hp = 216
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4099931
31 X = 1168298
04
Y = 20130576
52 feet Y = 6149319
11 meter
Z = 8548112
50 Z = 2611338
07
XDOT = -15283
854855 XDOT = -4668
281048
YDOT = 10383
606509 feet/sec YDOT = 3112
774407 meter/sec
ZDOT = -17076
522017 ZDOT = -5227
576746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5957428
20 X = 1815824
11
Y = 19650032
29 feet Y = 5989329
84 meter
Z = 8573508
94 Z = 2613205
53
XDOT = -12670
444076 XDOT = -3861
951354
YDOT = 11356
456663 feet/sec YDOT = 3461
447991 meter/sec
ZDOT = -17178
296695 ZDOT = -5235
944833
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 18188
26312658
00016717 00000-0 10270-3 0 9141
2 25544 51
6379 278
6474 0004044 282
4015 77
6685 15
54073795 41634
Satellite: ISS
Catalog Number: 25544
Epoch time: 18188
26312658 = yrday
fracday
Element set: 914
Inclination: 51
6379 deg
RA of node: 278
6474 deg
Eccentricity:
0004044
Arg of perigee: 282
4015 deg
Mean anomaly: 77
6685 deg
Mean motion: 15
54073795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4163
Checksum: 339
Coasting Arc #16 (Orbit 4177)
---------------------------------------
Vector Time (GMT): 2018/189/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -486010
87 A = 6789123
03 meter
Y = -6686138
58 meter E =
0008764
Z = -1038915
99 I = 51
27654
XDOT = 4775
830753 Wp = 15
33324
YDOT = -1255
687336 meter/sec RA = 272
98068 deg
ZDOT = 5866
720173 TA = 333
34621
MA = 333
39124
Ha = 219
836 n
mi
Hp = 216
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1594523
84 X = -406162
00
Y = -21936150
21 feet Y = -6691126
92 meter
Z = -3408517
03 Z = -1041083
67
XDOT = 15668
736067 XDOT = 4761
019820
YDOT = -4119
709107 feet/sec YDOT = -1202
364165 meter/sec
ZDOT = 19247
769596 ZDOT = 5889
883390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4043345
79 X = -1232411
80
Y = -21617788
66 feet Y = -6589101
98 meter
Z = -3417272
14 Z = -1041584
55
XDOT = 13398
762839 XDOT = 4083
942913
YDOT = -5554
934278 feet/sec YDOT = -1693
143968 meter/sec
ZDOT = 19351
555009 ZDOT = 5898
353967
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 18189
22771458
00016717 00000-0 10270-3 0 9156
2 25544 51
6371 273
8385 0003778 283
9669 76
1064 15
54040511 41789
Satellite: ISS
Catalog Number: 25544
Epoch time: 18189
22771458 = yrday
fracday
Element set: 915
Inclination: 51
6371 deg
RA of node: 273
8385 deg
Eccentricity:
0003778
Arg of perigee: 283
9669 deg
Mean anomaly: 76
1064 deg
Mean motion: 15
54040511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4178
Checksum: 339
Coasting Arc #17 (Orbit 4193)
---------------------------------------
Vector Time (GMT): 2018/190/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -287902
02 A = 6789263
49 meter
Y = 6747240
21 meter E =
0007532
Z = -654557
75 I = 51
27664
XDOT = -4789
915763 Wp = 153
02567
YDOT = -776
995495 meter/sec RA = 267
98608 deg
ZDOT = -5936
055072 TA = 34
07729
MA = 34
02895
Ha = 219
922 n
mi
Hp = 216
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -944560
43 X = -360150
62
Y = 22136614
86 feet Y = 6743616
81 meter
Z = -2147499
18 Z = -656130
88
XDOT = -15714
946730 XDOT = -4752
036964
YDOT = -2549
197819 feet/sec YDOT = -830
347071 meter/sec
ZDOT = -19475
246299 ZDOT = -5959
230929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1959751
48 X = 597332
25
Y = 22069140
66 feet Y = 6726674
07 meter
Z = -2155474
27 Z = -656988
56
XDOT = -14175
610321 XDOT = -4320
726026
YDOT = -642
741917 feet/sec YDOT = -195
907736 meter/sec
ZDOT = -19578
808047 ZDOT = -5967
620693
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 18190
25660264
00016717 00000-0 10270-3 0 9164
2 25544 51
6370 268
7100 0003758 291
8007 68
2746 15
54087488 41949
Satellite: ISS
Catalog Number: 25544
Epoch time: 18190
25660264 = yrday
fracday
Element set: 916
Inclination: 51
6370 deg
RA of node: 268
7100 deg
Eccentricity:
0003758
Arg of perigee: 291
8007 deg
Mean anomaly: 68
2746 deg
Mean motion: 15
54087488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4194
Checksum: 327
Coasting Arc #18 (Orbit 4209)
---------------------------------------
Vector Time (GMT): 2018/191/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1052435
50 A = 6787374
59 meter
Y = -6305432
33 meter E =
0011227
Z = 2262250
63 I = 51
27131
XDOT = 4705
110470 Wp = 60
46817
YDOT = 2730
708183 meter/sec RA = 262
98845 deg
ZDOT = 5407
394313 TA = 324
84970
MA = 324
92372
Ha = 219
948 n
mi
Hp = 216
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3452872
37 X = 1111877
56
Y = -20687113
94 feet Y = -6293331
25 meter
Z = 7422082
13 Z = 2267506
42
XDOT = 15436
714141 XDOT = 4647
959024
YDOT = 8959
016350 feet/sec YDOT = 2783
003611 meter/sec
ZDOT = 17740
794990 ZDOT = 5430
111674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 320725
98 X = 97757
28
Y = -20962196
48 feet Y = -6389277
49 meter
Z = 7446460
07 Z = 2269681
03
XDOT = 14942
490262 XDOT = 4554
471032
YDOT = 6583
951093 feet/sec YDOT = 2006
788293 meter/sec
ZDOT = 17842
045720 ZDOT = 5438
255536
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 18191
28549031
00016717 00000-0 10270-3 0 9177
2 25544 51
6361 263
5812 0003639 290
6620 69
4142 15
54050385 42106
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
28549031 = yrday
fracday
Element set: 917
Inclination: 51
6361 deg
RA of node: 263
5812 deg
Eccentricity:
0003639
Arg of perigee: 290
6620 deg
Mean anomaly: 69
4142 deg
Mean motion: 15
54050385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4210
Checksum: 297
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