[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 14th 2018
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) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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
196/12:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 215
8
196/17:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
9
197/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
7
199/15:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
5
201/19:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 215
3
203/18:49:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 215
1
206/03:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
8
207/15:56:37
575 -1
2 1
2 1
2
N/A 0
2 0
0 221
8
000/00:03:15
150 -0
4 0
0 215
4
Coasting Arc #1 (Orbit 259)
---------------------------------------
Vector Time (GMT): 2018/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959643
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3063702
65 A = 6789798
53 meter
Y = -6029537
91 meter E =
0011391
Z = -515645
36 I = 51
30690
XDOT = 4082
996155 Wp = 21
03151
YDOT = -2579
774250 meter/sec RA = 246
56519 deg
ZDOT = 5958
140715 TA = 333
37899
MA = 333
43744
Ha = 220
473 n
mi
Hp = 216
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10051517
87 X = -2993546
31
Y = -19781948
51 feet Y = -6063406
00 meter
Z = -1691749
88 Z = -530358
01
XDOT = 13395
656675 XDOT = 4082
599490
YDOT = -8463
826278 feet/sec YDOT = -2534
118491 meter/sec
ZDOT = 19547
705757 ZDOT = 5977
972770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15029213
26 X = -4580904
20
Y = 16317380
18 feet Y = 4973537
48 meter
Z = -1756806
45 Z = -535474
61
XDOT = -11372
965989 XDOT = -3466
480034
YDOT = -8378
442145 feet/sec YDOT = -2553
749166 meter/sec
ZDOT = 19636
790984 ZDOT = 5985
293892
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 18194
50103487
00016717 00000-0 10270-3 0 9008
2 25544 51
6380 247
5599 0003986 307
3687 52
7102 15
53925203 2606
Satellite: ISS
Catalog Number: 25544
Epoch time: 18194
50103487 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 247
5599 deg
Eccentricity:
0003986
Arg of perigee: 307
3687 deg
Mean anomaly: 52
7102 deg
Mean motion: 15
53925203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 260
Checksum: 308
Coasting Arc #2 (Orbit 275)
---------------------------------------
Vector Time (GMT): 2018/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959643
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2341847
59 A = 6789198
85 meter
Y = 6264446
58 meter E =
0005592
Z = -1152497
80 I = 51
32014
XDOT = -4904
910798 Wp = 149
10864
YDOT = 762
171319 meter/sec RA = 241
57284 deg
ZDOT = -5841
202501 TA = 43
45602
MA = 43
41196
Ha = 220
555 n
mi
Hp = 215
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7683227
01 X = 2277220
88
Y = 20552646
25 feet Y = 6290273
53 meter
Z = -3781160
77 Z = -1141278
35
XDOT = -16092
227026 XDOT = -4884
696226
YDOT = 2500
562069 feet/sec YDOT = 707
434986 meter/sec
ZDOT = -19164
050199 ZDOT = -5864
979132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16315310
04 X = 4972906
50
Y = -14684181
11 feet Y = -4475738
40 meter
Z = -3731742
92 Z = -1137435
24
XDOT = 7088
307766 XDOT = 2160
516207
YDOT = 12758
316515 feet/sec YDOT = 3888
734874 meter/sec
ZDOT = -19270
561294 ZDOT = -5873
667082
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 18195
52997410
00016717 00000-0 10270-3 0 9019
2 25544 51
6386 242
4313 0003867 311
8306 48
2516 15
53983566 2768
Satellite: ISS
Catalog Number: 25544
Epoch time: 18195
52997410 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 242
4313 deg
Eccentricity:
0003867
Arg of perigee: 311
8306 deg
Mean anomaly: 48
2516 deg
Mean motion: 15
53983566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 276
Checksum: 321
Coasting Arc #3 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2018/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959643
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1422196
59 A = 6786806
20 meter
Y = -6059841
76 meter E =
0012096
Z = 2687289
77 I = 51
32772
XDOT = 5593
274297 Wp = 62
11958
YDOT = 980
202191 meter/sec RA = 236
57761 deg
ZDOT = 5158
232181 TA = 328
39018
MA = 328
46277
Ha = 220
760 n
mi
Hp = 215
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4665999
31 X = -1367381
21
Y = -19881370
60 feet Y = -6075439
51 meter
Z = 8816567
48 Z = 2680513
93
XDOT = 18350
637458 XDOT = 5556
842316
YDOT = 3215
886452 feet/sec YDOT = 1042
545839 meter/sec
ZDOT = 16923
333927 ZDOT = 5185
313353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16577133
31 X = -5052710
23
Y = 11948211
63 feet Y = 3641814
91 meter
Z = 8786990
29 Z = 2678274
64
XDOT = -3108
967406 XDOT = -947
613265
YDOT = -16877
971333 feet/sec YDOT = -5144
405662 meter/sec
ZDOT = 17044
428736 ZDOT = 5195
141879
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 18196
55891191
00016717 00000-0 10270-3 0 9023
2 25544 51
6379 237
3029 0003881 318
5652 41
5206 15
53950708 2923
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
55891191 = yrday
fracday
Element set: 902
Inclination: 51
6379 deg
RA of node: 237
3029 deg
Eccentricity:
0003881
Arg of perigee: 318
5652 deg
Mean anomaly: 41
5206 deg
Mean motion: 15
53950708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 292
Checksum: 320
Coasting Arc #4 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2018/196/12:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4463948
26 A = 6789086
73 meter
Y = 4962137
68 meter E =
0010042
Z = 1218196
95 I = 51
33671
XDOT = -2904
786852 Wp = 115
51245
YDOT = 4051
448710 meter/sec RA = 236
42227 deg
ZDOT = -5825
286196 TA = 51
19375
MA = 51
10412
Ha = 220
682 n
mi
Hp = 215
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14645499
53 X = 4402211
28
Y = 16279979
26 feet Y = 5011711
32 meter
Z = 3996709
17 Z = 1239731
30
XDOT = -9530
140592 XDOT = -2921
579867
YDOT = 13292
154560 feet/sec YDOT = 4018
872045 meter/sec
ZDOT = -19111
831351 ZDOT = -5839
436714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6356722
53 X = 1937529
03
Y = -20936707
67 feet Y = -6381508
50 meter
Z = 4092482
89 Z = 1247388
78
XDOT = 14712
482856 XDOT = 4484
364774
YDOT = 697
777444 feet/sec YDOT = 212
682565 meter/sec
ZDOT = -19175
672004 ZDOT = -5844
744827
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 18196
55891067
00016717 00000-0 10270-3 0 9036
2 25544 51
6383 237
3033 0003907 317
1089 42
9758 15
53985161 2929
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
55891067 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 237
3033 deg
Eccentricity:
0003907
Arg of perigee: 317
1089 deg
Mean anomaly: 42
9758 deg
Mean motion: 15
53985161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 292
Checksum: 329
Coasting Arc #5 (Orbit 294)
---------------------------------------
Vector Time (GMT): 2018/196/17:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4852092
03 A = 6780197
69 meter
Y = 385456
25 meter E =
0007749
Z = 4719544
31 I = 51
30795
XDOT = 2091
948303 Wp = 31
36188
YDOT = 6864
020780 meter/sec RA = 235
49218 deg
ZDOT = -2702
792057 TA = 85
52889
MA = 85
44037
Ha = 220
624 n
mi
Hp = 215
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15918937
11 X = 4824496
61
Y = 1264620
25 feet Y = 439560
97 meter
Z = 15484069
24 Z = 4743046
56
XDOT = 6863
347450 XDOT = 2028
165894
YDOT = 22519
753215 feet/sec YDOT = 6887
058008 meter/sec
ZDOT = -8867
428007 ZDOT = -2692
784614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15844062
43 X = -4829270
23
Y = 842675
03 feet Y = 256847
35 meter
Z = 15589220
89 Z = 4751594
53
XDOT = -9785
684350 XDOT = -2982
676590
YDOT = -20246
881665 feet/sec YDOT = -6171
249532 meter/sec
ZDOT = -8823
480654 ZDOT = -2689
396903
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 18196
75183685
00016717 00000-0 10270-3 0 9049
2 25544 51
6360 236
3419 0004123 318
1034 41
9803 15
53975765 2955
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
75183685 = yrday
fracday
Element set: 904
Inclination: 51
6360 deg
RA of node: 236
3419 deg
Eccentricity:
0004123
Arg of perigee: 318
1034 deg
Mean anomaly: 41
9803 deg
Mean motion: 15
53975765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 295
Checksum: 318
Coasting Arc #6 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -786352
67 A = 6784208
23 meter
Y = -5661265
44 meter E =
0009821
Z = 3644450
44 I = 51
33812
XDOT = 6011
378694 Wp = 77
24046
YDOT = 1965
115414 meter/sec RA = 231
41889 deg
ZDOT = 4341
881048 TA = 326
27334
MA = 326
33578
Ha = 220
874 n
mi
Hp = 215
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2579897
22 X = -740690
85
Y = -18573705
51 feet Y = -5669803
93 meter
Z = 11956858
41 Z = 3640741
19
XDOT = 19722
371042 XDOT = 5967
867336
YDOT = 6447
229048 feet/sec YDOT = 2032
095203 meter/sec
ZDOT = 14245
016561 ZDOT = 4370
976088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13759804
77 X = -4193988
49
Y = 12754865
32 feet Y = 3887682
95 meter
Z = 11940940
17 Z = 3639598
57
XDOT = -4935
533984 XDOT = -1504
350758
YDOT = -18806
018218 feet/sec YDOT = -5732
074353 meter/sec
ZDOT = 14375
021154 ZDOT = 4381
506448
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 18197
58784794
00016717 00000-0 10270-3 0 9050
2 25544 51
6372 232
1747 0003841 323
5337 36
5554 15
53956749 3087
Satellite: ISS
Catalog Number: 25544
Epoch time: 18197
58784794 = yrday
fracday
Element set: 905
Inclination: 51
6372 deg
RA of node: 232
1747 deg
Eccentricity:
0003841
Arg of perigee: 323
5337 deg
Mean anomaly: 36
5554 deg
Mean motion: 15
53956749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 341
Coasting Arc #7 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2018/198/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -475575
88 A = 6780551
26 meter
Y = 4909046
25 meter E =
0010166
Z = -4662857
22 I = 51
34882
XDOT = -6293
444653 Wp = 49
01472
YDOT = -3313
006592 meter/sec RA = 226
41133 deg
ZDOT = -2843
570104 TA = 192
58940
MA = 192
61481
Ha = 220
882 n
mi
Hp = 215
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1560288
34 X = -507785
55
Y = 16105794
78 feet Y = 4903548
20 meter
Z = -15298087
98 Z = -4665245
31
XDOT = -20647
784295 XDOT = -6242
117644
YDOT = -10869
444199 feet/sec YDOT = -3383
097088 meter/sec
ZDOT = -9329
298241 ZDOT = -2874
016463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13934242
54 X = 4247157
13
Y = -8205055
17 feet Y = -2500900
82 meter
Z = -15309362
35 Z = -4666293
64
XDOT = 2573
403548 XDOT = 784
373401
YDOT = 22046
024064 feet/sec YDOT = 6719
628135 meter/sec
ZDOT = -9465
208015 ZDOT = -2884
995403
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 18198
55247318
00016717 00000-0 10270-3 0 9065
2 25544 51
6385 227
3676 0003921 324
0961 35
9927 15
53978992 3234
Satellite: ISS
Catalog Number: 25544
Epoch time: 18198
55247318 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 227
3676 deg
Eccentricity:
0003921
Arg of perigee: 324
0961 deg
Mean anomaly: 35
9927 deg
Mean motion: 15
53978992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 343
Coasting Arc #8 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2018/199/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1844015
70 A = 6778178
98 meter
Y = -3924418
95 meter E =
0001802
Z = 5208558
31 I = 51
36392
XDOT = 6227
141808 Wp = 42
40242
YDOT = 4347
097063 meter/sec RA = 221
39574 deg
ZDOT = 1071
804844 TA = 37
29793
MA = 37
28542
Ha = 220
941 n
mi
Hp = 215
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6049920
27 X = 1862462
50
Y = -12875390
27 feet Y = -3903695
03 meter
Z = 17088445
91 Z = 5217560
38
XDOT = 20430
255274 XDOT = 6172
862369
YDOT = 14262
129473 feet/sec YDOT = 4416
429713 meter/sec
ZDOT = 3516
420091 ZDOT = 1101
922117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13872275
99 X = -4228269
72
Y = 2922730
49 feet Y = 890848
25 meter
Z = 17129208
93 Z = 5220982
88
XDOT = -526
512571 XDOT = -160
481032
YDOT = -23874
032114 feet/sec YDOT = -7276
804988 meter/sec
ZDOT = 3650
753588 ZDOT = 1112
749693
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 18199
58140543
00016717 00000-0 10270-3 0 9072
2 25544 51
6378 222
2385 0003988 330
0797 30
0127 15
53983307 3395
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
58140543 = yrday
fracday
Element set: 907
Inclination: 51
6378 deg
RA of node: 222
2385 deg
Eccentricity:
0003988
Arg of perigee: 330
0797 deg
Mean anomaly: 30
0127 deg
Mean motion: 15
53983307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 321
Coasting Arc #9 (Orbit 339)
---------------------------------------
Vector Time (GMT): 2018/199/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5105991
18 A = 6781273
50 meter
Y = 294980
63 meter E =
0006846
Z = -4458612
22 I = 51
37535
XDOT = -3181
580001 Wp = 87
95640
YDOT = -6172
127159 meter/sec RA = 220
84287 deg
ZDOT = 3239
747788 TA = 214
78598
MA = 214
83076
Ha = 221
020 n
mi
Hp = 215
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16751939
55 X = -5087252
95
Y = 967784
23 feet Y = 237986
92 meter
Z = -14627992
84 Z = -4483369
49
XDOT = -10438
254595 XDOT = -3128
061889
YDOT = -20249
761020 feet/sec YDOT = -6207
406715 meter/sec
ZDOT = 10629
093794 ZDOT = 3224
422644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16291966
09 X = 4965791
26
Y = 3588836
72 feet Y = 1093877
43 meter
Z = -14738872
12 Z = -4492408
22
XDOT = 4881
423790 XDOT = 1487
857971
YDOT = 21152
670527 feet/sec YDOT = 6447
333976 meter/sec
ZDOT = 10561
199494 ZDOT = 3219
053606
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 18199
64571456
00016717 00000-0 10270-3 0 9081
2 25544 51
6364 221
9186 0004172 330
0993 29
9921 15
53958745 3408
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
64571456 = yrday
fracday
Element set: 908
Inclination: 51
6364 deg
RA of node: 221
9186 deg
Eccentricity:
0004172
Arg of perigee: 330
0993 deg
Mean anomaly: 29
9921 deg
Mean motion: 15
53958745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 340
Checksum: 333
Coasting Arc #10 (Orbit 355)
---------------------------------------
Vector Time (GMT): 2018/200/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5830815
17 A = 6784913
91 meter
Y = 925756
69 meter E =
0011195
Z = 3338254
01 I = 51
41301
XDOT = 1745
597780 Wp = 71
17405
YDOT = 5839
889272 meter/sec RA = 215
84045 deg
ZDOT = -4652
120517 TA = 69
79895
MA = 69
67860
Ha = 221
098 n
mi
Hp = 215
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19129971
04 X = 5803814
44
Y = 3037259
48 feet Y = 990809
73 meter
Z = 10952276
95 Z = 3366512
28
XDOT = 5727
026837 XDOT = 1702
762113
YDOT = 19159
741707 feet/sec YDOT = 5859
170511 meter/sec
ZDOT = -15262
862588 ZDOT = -4643
744797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17654159
68 X = -5380987
87
Y = -7792696
55 feet Y = -2375213
91 meter
Z = 11078701
81 Z = 3376788
31
XDOT = -1323
400497 XDOT = -403
372472
YDOT = -18723
815485 feet/sec YDOT = -5707
018960 meter/sec
ZDOT = -15226
032116 ZDOT = -4640
894589
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 18200
67464610
00016717 00000-0 10270-3 0 9091
2 25544 51
6360 216
7903 0004272 333
4686 26
6247 15
53985256 3569
Satellite: ISS
Catalog Number: 25544
Epoch time: 18200
67464610 = yrday
fracday
Element set: 909
Inclination: 51
6360 deg
RA of node: 216
7903 deg
Eccentricity:
0004272
Arg of perigee: 333
4686 deg
Mean anomaly: 26
6247 deg
Mean motion: 15
53985256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 356
Checksum: 314
Coasting Arc #11 (Orbit 370)
---------------------------------------
Vector Time (GMT): 2018/201/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6213173
88 A = 6788146
62 meter
Y = -1935647
66 meter E =
0009586
Z = -1912923
80 I = 51
45138
XDOT = -84
172840 Wp = 17
09725
YDOT = -5243
493812 meter/sec RA = 210
84974 deg
ZDOT = 5595
294420 TA = 321
76585
MA = 321
83379
Ha = 221
169 n
mi
Hp = 215
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20384428
74 X = -6181775
26
Y = -6350550
07 feet Y = -2004951
97 meter
Z = -6275996
73 Z = -1943028
88
XDOT = -276
157613 XDOT = -52
711166
YDOT = -17203
063687 feet/sec YDOT = -5244
259558 meter/sec
ZDOT = 18357
265159 ZDOT = 5594
961599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18245331
29 X = 5561176
98
Y = 11011574
17 feet Y = 3356327
81 meter
Z = -6410590
98 Z = -1953948
13
XDOT = -2905
932546 XDOT = -885
728240
YDOT = 15471
266866 feet/sec YDOT = 4715
642141 meter/sec
ZDOT = 18356
373799 ZDOT = 5595
022734
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 18201
63926863
00016717 00000-0 10270-3 0 9103
2 25544 51
6363 211
9829 0004215 337
1207 22
9757 15
53977442 3713
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
63926863 = yrday
fracday
Element set: 910
Inclination: 51
6363 deg
RA of node: 211
9829 deg
Eccentricity:
0004215
Arg of perigee: 337
1207 deg
Mean anomaly: 22
9757 deg
Mean motion: 15
53977442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 371
Checksum: 310
Coasting Arc #12 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2018/201/19:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1675810
71 A = 6777798
25 meter
Y = 3905409
30 meter E =
0013884
Z = -5291556
43 I = 51
42563
XDOT = -6791
104009 Wp = 69
60651
YDOT = -3513
106866 meter/sec RA = 209
97353 deg
ZDOT = -438
318543 TA = 196
17313
MA = 196
21749
Ha = 221
204 n
mi
Hp = 215
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5498066
63 X = -1693654
13
Y = 12813022
64 feet Y = 3886569
83 meter
Z = -17360749
44 Z = -5299739
94
XDOT = -22280
524964 XDOT = -6749
185650
YDOT = -11525
941160 feet/sec YDOT = -3588
815270 meter/sec
ZDOT = -1438
052963 ZDOT = -471
205557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6601912
16 X = -2012262
83
Y = -12228152
88 feet Y = -3727141
00 meter
Z = -17397842
97 Z = -5302862
54
XDOT = 22053
931454 XDOT = 6722
038307
YDOT = -9634
089899 feet/sec YDOT = -2936
470601 meter/sec
ZDOT = -1584
928483 ZDOT = -483
086202
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 18201
83219273
00016717 00000-0 10270-3 0 9116
2 25544 51
6399 211
0227 0004331 336
3398 23
7554 15
54003758 3744
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
83219273 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 211
0227 deg
Eccentricity:
0004331
Arg of perigee: 336
3398 deg
Mean anomaly: 23
7554 deg
Mean motion: 15
54003758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 294
Coasting Arc #13 (Orbit 389)
---------------------------------------
Vector Time (GMT): 2018/202/19:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3213459
67 A = 6778288
40 meter
Y = -3024800
12 meter E =
0007031
Z = 5144417
32 I = 51
45699
XDOT = 6262
318274 Wp = 17
86185
YDOT = 4184
283377 meter/sec RA = 204
96132 deg
ZDOT = -1444
405439 TA = 86
11269
MA = 86
03231
Ha = 221
159 n
mi
Hp = 215
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10542846
68 X = 3222056
30
Y = -9923884
91 feet Y = -2988817
36 meter
Z = 16878009
56 Z = 5160047
70
XDOT = 20545
663630 XDOT = 6222
079147
YDOT = 13727
963834 feet/sec YDOT = 4254
088074 meter/sec
ZDOT = -4738
862989 ZDOT = -1414
082870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1432224
56 X = 436542
05
Y = 14324950
56 feet Y = 4366244
93 meter
Z = 16948358
01 Z = 5165859
52
XDOT = -22422
185323 XDOT = -6834
282087
YDOT = 7715
790870 feet/sec YDOT = 2351
773057 meter/sec
ZDOT = -4603
528238 ZDOT = -1403
155407
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 18202
86111918
00016717 00000-0 10270-3 0 9128
2 25544 51
6401 205
8943 0004428 339
3897 20
7077 15
54030722 3904
Satellite: ISS
Catalog Number: 25544
Epoch time: 18202
86111918 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 205
8943 deg
Eccentricity:
0004428
Arg of perigee: 339
3897 deg
Mean anomaly: 20
7077 deg
Mean motion: 15
54030722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 390
Checksum: 296
Coasting Arc #14 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2018/203/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5001728
22 A = 6781992
00 meter
Y = -1751496
47 meter E =
0011038
Z = 4229337
63 I = 51
49743
XDOT = 4754
333925 Wp = 50
23530
YDOT = 4806
581157 meter/sec RA = 200
11069 deg
ZDOT = -3618
838735 TA = 76
91370
MA = 76
79052
Ha = 221
381 n
mi
Hp = 215
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16409869
50 X = 5000398
49
Y = -5746379
50 feet Y = -1695571
53 meter
Z = 13875779
63 Z = 4253630
69
XDOT = 15598
208416 XDOT = 4717
810322
YDOT = 15769
623220 feet/sec YDOT = 4859
543534 meter/sec
ZDOT = -11872
830496 ZDOT = -3595
832267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8323117
02 X = -2536886
07
Y = 15165525
64 feet Y = 4622452
21 meter
Z = 13984795
67 Z = 4262565
72
XDOT = -21092
023809 XDOT = -6428
848857
YDOT = -682
096947 feet/sec YDOT = -207
903149 meter/sec
ZDOT = -11770
316986 ZDOT = -3587
592617
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 18203
82573981
00016717 00000-0 10270-3 0 9138
2 25544 51
6389 201
0869 0004422 345
6267 14
4759 15
54002293 4055
Satellite: ISS
Catalog Number: 25544
Epoch time: 18203
82573981 = yrday
fracday
Element set: 913
Inclination: 51
6389 deg
RA of node: 201
0869 deg
Eccentricity:
0004422
Arg of perigee: 345
6267 deg
Mean anomaly: 14
4759 deg
Mean motion: 15
54002293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 307
Coasting Arc #15 (Orbit 419)
---------------------------------------
Vector Time (GMT): 2018/204/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5998178
78 A = 6785671
98 meter
Y = 883399
51 meter E =
0006507
Z = -3043438
65 I = 51
54150
XDOT = -3216
840838 Wp = 31
17363
YDOT = -4918
849515 meter/sec RA = 195
11868 deg
ZDOT = 4922
332499 TA = 293
87247
MA = 293
94064
Ha = 221
424 n
mi
Hp = 215
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19679064
24 X = -5992828
14
Y = 2898292
36 feet Y = 816353
97 meter
Z = -9985034
93 Z = -3072562
33
XDOT = -10553
939756 XDOT = -3185
507665
YDOT = -16137
957727 feet/sec YDOT = -4954
647776 meter/sec
ZDOT = 16149
384839 ZDOT = 4906
781948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12413432
44 X = 3783614
21
Y = -15457933
69 feet Y = -4711578
19 meter
Z = -10115610
31 Z = -3083238
02
XDOT = 17661
317704 XDOT = 5383
169636
YDOT = 3681
531799 feet/sec YDOT = 1122
130892 meter/sec
ZDOT = 16080
268785 ZDOT = 4901
265926
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 18204
79035758
00016717 00000-0 10270-3 0 9141
2 25544 51
6393 196
2790 0004445 346
8776 13
2260 15
53998878 4204
Satellite: ISS
Catalog Number: 25544
Epoch time: 18204
79035758 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 196
2790 deg
Eccentricity:
0004445
Arg of perigee: 346
8776 deg
Mean anomaly: 13
2260 deg
Mean motion: 15
53998878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 339
Coasting Arc #16 (Orbit 435)
---------------------------------------
Vector Time (GMT): 2018/205/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6611482
33 A = 6788748
09 meter
Y = -45592
17 meter E =
0011922
Z = 1524132
49 I = 51
58380
XDOT = 1368
223614 Wp = 100
55442
YDOT = 4879
503085 meter/sec RA = 190
13874 deg
ZDOT = -5753
042690 TA = 62
78533
MA = 62
66390
Ha = 221
645 n
mi
Hp = 214
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21691215
00 X = 6604097
45
Y = -149580
60 feet Y = 28300
54 meter
Z = 5000434
69 Z = 1556230
41
XDOT = 4488
922618 XDOT = 1341
502844
YDOT = 16008
868389 feet/sec YDOT = 4894
654731 meter/sec
ZDOT = -18874
811976 ZDOT = -5746
460788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15524212
62 X = -4731780
01
Y = 15102016
63 feet Y = 4603094
67 meter
Z = 5144263
38 Z = 1567971
48
XDOT = -13310
667911 XDOT = -4057
091579
YDOT = -7223
952126 feet/sec YDOT = -2201
860608 meter/sec
ZDOT = -18845
864127 ZDOT = -5744
219386
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 18205
81928206
00016717 00000-0 10270-3 0 9155
2 25544 51
6395 191
1509 0004348 352
0047 8
1035 15
53970324 4366
Satellite: ISS
Catalog Number: 25544
Epoch time: 18205
81928206 = yrday
fracday
Element set: 915
Inclination: 51
6395 deg
RA of node: 191
1509 deg
Eccentricity:
0004348
Arg of perigee: 352
0047 deg
Mean anomaly: 8
1035 deg
Mean motion: 15
53970324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 436
Checksum: 295
Coasting Arc #17 (Orbit 440)
---------------------------------------
Vector Time (GMT): 2018/206/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -851597
98 A = 6777702
76 meter
Y = 4137177
86 meter E =
0014810
Z = -5312897
36 I = 51
55739
XDOT = -7545
735602 Wp = 76
30437
YDOT = -1288
784411 meter/sec RA = 188
44557 deg
ZDOT = 209
835372 TA = 195
67756
MA = 195
72347
Ha = 221
531 n
mi
Hp = 214
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2793956
61 X = -871990
87
Y = 13573418
18 feet Y = 4127541
26 meter
Z = -17430765
60 Z = -5317083
14
XDOT = -24756
350401 XDOT = -7531
782504
YDOT = -4228
295312 feet/sec YDOT = -1373
088043 meter/sec
ZDOT = 688
436259 ZDOT = 173
215083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5684303
36 X = -1732575
67
Y = 12611988
70 feet Y = 3844134
16 meter
Z = -17449982
82 Z = -5318754
76
XDOT = -22238
263705 XDOT = -6778
222777
YDOT = -9315
028326 feet/sec YDOT = -2839
220634 meter/sec
ZDOT = 524
483486 ZDOT = 159
862566
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 18206
14081938
00016717 00000-0 10270-3 0 9165
2 25544 51
6386 189
5435 0003977 352
8537 7
2558 15
54012831 4411
Satellite: ISS
Catalog Number: 25544
Epoch time: 18206
14081938 = yrday
fracday
Element set: 916
Inclination: 51
6386 deg
RA of node: 189
5435 deg
Eccentricity:
0003977
Arg of perigee: 352
8537 deg
Mean anomaly: 7
2558 deg
Mean motion: 15
54012831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 320
Coasting Arc #18 (Orbit 456)
---------------------------------------
Vector Time (GMT): 2018/207/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2575054
02 A = 6779121
82 meter
Y = -3803324
47 meter E =
0008726
Z = 4984098
91 I = 51
59461
XDOT = 7087
771864 Wp = 33
92288
YDOT = 2071
969597 meter/sec RA = 183
44316 deg
ZDOT = -2071
982061 TA = 76
29200
MA = 76
19487
Ha = 221
599 n
mi
Hp = 214
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8448339
97 X = 2593182
77
Y = -12478098
66 feet Y = -3774427
59 meter
Z = 16352030
54 Z = 4996651
04
XDOT = 23253
844698 XDOT = 7074
140173
YDOT = 6797
800514 feet/sec YDOT = 2151
153953 meter/sec
ZDOT = -6797
841406 ZDOT = -2037
585617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10772066
36 X = 3283325
83
Y = -10449077
77 feet Y = -3184878
90 meter
Z = 16408706
76 Z = 5001373
82
XDOT = 20591
460847 XDOT = 6276
277266
YDOT = 10749
300949 feet/sec YDOT = 3276
386929 meter/sec
ZDOT = -6643
914896 ZDOT = -2025
065260
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 18207
16974139
00016717 00000-0 10270-3 0 9173
2 25544 51
6384 184
4146 0003990 357
6861 2
4272 15
53987878 4578
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
16974139 = yrday
fracday
Element set: 917
Inclination: 51
6384 deg
RA of node: 184
4146 deg
Eccentricity:
0003990
Arg of perigee: 357
6861 deg
Mean anomaly: 2
4272 deg
Mean motion: 15
53987878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 345
Coasting Arc #19 (Orbit 464)
---------------------------------------
Vector Time (GMT): 2018/207/15:58:15
150
Vector Time (MET): N/A
Weight (LBS) : 944798
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1630938
56 A = 6779154
81 meter
Y = 4106092
79 meter E =
0014202
Z = -5153981
63 I = 51
61052
XDOT = -7433
357814 Wp = 61
27710
YDOT = 1078
654400 meter/sec RA = 180
78185 deg
ZDOT = -1489
332277 TA = 194
33520
MA = 194
37553
Ha = 221
829 n
mi
Hp = 215
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5350848
29 X = 1609936
73
Y = 13471433
03 feet Y = 4124214
15 meter
Z = -16909388
53 Z = -5146109
84
XDOT = -24387
656869 XDOT = -7437
632914
YDOT = 3538
892390 feet/sec YDOT = 995
505704 meter/sec
ZDOT = -4886
260751 ZDOT = -1525
450543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6156527
22 X = -1876509
50
Y = -13167571
29 feet Y = -4013475
73 meter
Z = -16874559
09 Z = -5143365
61
XDOT = 23177
354898 XDOT = 7064
457773
YDOT = -4352
187275 feet/sec YDOT = -1326
546681 meter/sec
ZDOT = -5048
265915 ZDOT = -1538
711451
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 18207
68420268
00016717 00000-0 10270-3 0 9180
2 25544 51
6386 181
8547 0004278 347
1382 12
9660 15
53781754 4659
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
68420268 = yrday
fracday
Element set: 918
Inclination: 51
6386 deg
RA of node: 181
8547 deg
Eccentricity:
0004278
Arg of perigee: 347
1382 deg
Mean anomaly: 12
9660 deg
Mean motion: 15
53781754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 333
Coasting Arc #20 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2018/208/15:58:15
150
Vector Time (MET): N/A
Weight (LBS) : 944798
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 41690
67 A = 6778304
71 meter
Y = -4214730
47 meter E =
0004978
Z = 5307317
09 I = 51
64152
XDOT = 7656
606606 Wp = 18
29593
YDOT = -319
118185 meter/sec RA = 175
78544 deg
ZDOT = -308
867103 TA = 74
67548
MA = 74
62048
Ha = 221
782 n
mi
Hp = 215
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 136780
40 X = 63038
25
Y = -13827855
88 feet Y = -4214145
36 meter
Z = 17412457
64 Z = 5307571
09
XDOT = 25120
100415 XDOT = 7661
106306
YDOT = -1046
975672 feet/sec YDOT = -233
471535 meter/sec
ZDOT = -1013
343513 ZDOT = -271
663846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 935768
93 X = 285222
37
Y = 13794814
52 feet Y = 4204659
47 meter
Z = 17414058
03 Z = 5307804
89
XDOT = -23987
621074 XDOT = -7311
426903
YDOT = 2715
297354 feet/sec YDOT = 827
622634 meter/sec
ZDOT = -846
533738 ZDOT = -258
023483
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 18208
71327348
00016717 00000-0 10270-3 0 9191
2 25544 51
6390 176
7277 0004319 347
7519 12
3528 15
53807291 4811
Satellite: ISS
Catalog Number: 25544
Epoch time: 18208
71327348 = yrday
fracday
Element set: 919
Inclination: 51
6390 deg
RA of node: 176
7277 deg
Eccentricity:
0004319
Arg of perigee: 347
7519 deg
Mean anomaly: 12
3528 deg
Mean motion: 15
53807291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 326
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