[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 8th 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) : 72 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 438 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
190/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 216
1
191/01:39:12
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
1
191/20:25:30
000 -0
0 0
2 0
2
N/A -0
2 0
0 220
1
000/00:01:00
000 0
0 -0
0 216
0
193/18:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
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
8
000/00:00:00
000 0
0 0
0 215
7
199/12:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
5
Coasting Arc #1 (Orbit 151)
---------------------------------------
Vector Time (GMT): 2018/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3988443
38 A = 6783059
54 meter
Y = -3856067
71 meter E =
0007449
Z = 3898083
63 I = 51
26745
XDOT = 2030
843729 Wp = 103
93677
YDOT = 6193
637988 meter/sec RA = 281
66277 deg
ZDOT = 4040
680364 TA = 303
53980
MA = 303
61093
Ha = 219
678 n
mi
Hp = 216
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13085444
16 X = 4012331
80
Y = -12651140
77 feet Y = -3811332
96 meter
Z = 12788988
29 Z = 3917515
71
XDOT = 6662
873128 XDOT = 1941
806414
YDOT = 20320
334605 feet/sec YDOT = 6215
850084 meter/sec
ZDOT = 13256
825342 ZDOT = 4050
329760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15343007
55 X = -4676548
70
Y = -9676120
80 feet Y = -2949281
62 meter
Z = 12876460
64 Z = 3924745
20
XDOT = 17510
774771 XDOT = 5337
284150
YDOT = -10032
461954 feet/sec YDOT = -3057
894404 meter/sec
ZDOT = 13299
093997 ZDOT = 4053
563850
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
55581090
00016717 00000-0 10270-3 0 9005
2 25544 51
6406 282
1722 0003730 270
9546 89
1179 15
54038025 1520
Satellite: ISS
Catalog Number: 25544
Epoch time: 18187
55581090 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 282
1722 deg
Eccentricity:
0003730
Arg of perigee: 270
9546 deg
Mean anomaly: 89
1179 deg
Mean motion: 15
54038025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 152
Checksum: 299
Coasting Arc #2 (Orbit 166)
---------------------------------------
Vector Time (GMT): 2018/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4168613
79 A = 6779747
03 meter
Y = 2321764
39 meter E =
0008310
Z = -4824240
64 I = 51
25005
XDOT = -1148
883240 Wp = 61
91701
YDOT = -7165
685692 meter/sec RA = 276
64677 deg
ZDOT = -2455
289116 TA = 183
81642
MA = 183
82276
Ha = 219
807 n
mi
Hp = 216
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13676554
42 X = -4170832
99
Y = 7617337
24 feet Y = 2275136
15 meter
Z = -15827561
15 Z = -4844495
45
XDOT = -3769
301970 XDOT = -1056
742703
YDOT = -23509
467494 feet/sec YDOT = -7178
017864 meter/sec
ZDOT = -8055
410486 ZDOT = -2460
646905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10777391
68 X = 3284948
98
Y = 11226450
90 feet Y = 3421822
24 meter
Z = -15918488
87 Z = -4851955
41
XDOT = -21007
242203 XDOT = -6403
007424
YDOT = 8709
524898 feet/sec YDOT = 2654
663189 meter/sec
ZDOT = -8078
357690 ZDOT = -2462
283424
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
52041518
00016717 00000-0 10270-3 0 9010
2 25544 51
6403 277
3651 0003854 275
3432 84
7281 15
53996309 1672
Satellite: ISS
Catalog Number: 25544
Epoch time: 18188
52041518 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 277
3651 deg
Eccentricity:
0003854
Arg of perigee: 275
3432 deg
Mean anomaly: 84
7281 deg
Mean motion: 15
53996309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 167
Checksum: 316
Coasting Arc #3 (Orbit 182)
---------------------------------------
Vector Time (GMT): 2018/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4238401
50 A = 6777725
10 meter
Y = -596243
62 meter E =
0001181
Z = 5256258
63 I = 51
24185
XDOT = 290
794777 Wp = 244
80661
YDOT = 7636
365816 meter/sec RA = 271
62232 deg
ZDOT = 631
364979 TA = 199
13004
MA = 199
13447
Ha = 219
645 n
mi
Hp = 216
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13905516
73 X = 4219221
72
Y = -1956179
85 feet Y = -548954
74 meter
Z = 17244943
02 Z = 5276800
67
XDOT = 954
051107 XDOT = 202
314385
YDOT = 25053
693622 feet/sec YDOT = 7639
122886 meter/sec
ZDOT = 2071
407410 ZDOT = 632
563540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5572683
65 X = -1698553
98
Y = -12765374
21 feet Y = -3890886
06 meter
Z = 17336911
87 Z = 5284290
74
XDOT = 22958
412669 XDOT = 6997
724181
YDOT = -7201
679284 feet/sec YDOT = -2195
071846 meter/sec
ZDOT = 2075
697568 ZDOT = 632
672619
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
54932176
00016717 00000-0 10270-3 0 9023
2 25544 51
6412 272
2366 0003812 281
5298 78
5426 15
54044470 1836
Satellite: ISS
Catalog Number: 25544
Epoch time: 18189
54932176 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 272
2366 deg
Eccentricity:
0003812
Arg of perigee: 281
5298 deg
Mean anomaly: 78
5426 deg
Mean motion: 15
54044470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 183
Checksum: 313
Coasting Arc #4 (Orbit 197)
---------------------------------------
Vector Time (GMT): 2018/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4230156
09 A = 6778200
09 meter
Y = -1177489
84 meter E =
0010333
Z = -5172803
86 I = 51
24206
XDOT = 562
338404 Wp = 96
93717
YDOT = -7535
938300 meter/sec RA = 266
59656 deg
ZDOT = 1256
491476 TA = 185
19948
MA = 185
21022
Ha = 219
929 n
mi
Hp = 215
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13878464
85 X = -4191547
93
Y = -3863155
63 feet Y = -1224577
79 meter
Z = -16971141
28 Z = -5193258
88
XDOT = 1844
942269 XDOT = 640
462172
YDOT = -24724
207022 feet/sec YDOT = -7529
213198 meter/sec
ZDOT = 4122
347363 ZDOT = 1259
411848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 204637
55 X = 62373
52
Y = 14296340
03 feet Y = 4357524
44 meter
Z = -17062478
71 Z = -5200643
51
XDOT = -23179
322754 XDOT = -7065
057576
YDOT = 5264
920581 feet/sec YDOT = 1604
747793 meter/sec
ZDOT = 4136
455361 ZDOT = 1260
791594
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
51392250
00016717 00000-0 10270-3 0 9036
2 25544 51
6399 267
4297 0003761 287
1916 72
8824 15
54018618 1981
Satellite: ISS
Catalog Number: 25544
Epoch time: 18190
51392250 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 267
4297 deg
Eccentricity:
0003761
Arg of perigee: 287
1916 deg
Mean anomaly: 72
8824 deg
Mean motion: 15
54018618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 198
Checksum: 331
Coasting Arc #5 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2018/190/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4254969
14 A = 6777779
13 meter
Y = 577825
26 meter E =
0002709
Z = 5245066
35 I = 51
24112
XDOT = -121
121682 Wp = 340
68592
YDOT = 7631
083940 meter/sec RA = 266
44462 deg
ZDOT = -740
020320 TA = 116
43736
MA = 116
40957
Ha = 219
734 n
mi
Hp = 216
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13959872
50 X = 4222713
74
Y = 1895752
17 feet Y = 625226
20 meter
Z = 17208222
92 Z = 5265657
25
XDOT = -397
380847 XDOT = -202
850931
YDOT = 25036
364632 feet/sec YDOT = 7629
272598 meter/sec
ZDOT = -2427
888188 ZDOT = -740
806152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4775105
67 X = -1455452
21
Y = -13133716
79 feet Y = -4003156
88 meter
Z = 17300251
50 Z = 5273116
66
XDOT = 21370
132450 XDOT = 6513
616371
YDOT = -10984
136444 feet/sec YDOT = -3347
964788 meter/sec
ZDOT = -2432
460655 ZDOT = -741
414008
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
57822825
00016717 00000-0 10270-3 0 9049
2 25544 51
6401 267
1095 0003825 286
8693 73
2040 15
54043301 1990
Satellite: ISS
Catalog Number: 25544
Epoch time: 18190
57822825 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 267
1095 deg
Eccentricity:
0003825
Arg of perigee: 286
8693 deg
Mean anomaly: 73
2040 deg
Mean motion: 15
54043301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 199
Checksum: 303
Coasting Arc #6 (Orbit 206)
---------------------------------------
Vector Time (GMT): 2018/191/01:39:12
000
Vector Time (MET): N/A
Weight (LBS) : 959630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2582702
87 A = 6783276
51 meter
Y = 4942212
48 meter E =
0004168
Z = -3867154
82 I = 51
26037
XDOT = -3860
718925 Wp = 37
71774
YDOT = -5211
243895 meter/sec RA = 263
78495 deg
ZDOT = -4080
651595 TA = 189
21904
MA = 189
22669
Ha = 220
043 n
mi
Hp = 216
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8473434
63 X = -2618991
53
Y = 16214607
89 feet Y = 4913128
58 meter
Z = -12687515
82 Z = -3879788
10
XDOT = -12666
400671 XDOT = -3782
336799
YDOT = -17097
256872 feet/sec YDOT = -5253
978256 meter/sec
ZDOT = -13387
964549 ZDOT = -4099
215999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17673520
81 X = -5386889
14
Y = 4572163
97 feet Y = 1393595
58 meter
Z = -12744710
26 Z = -3884587
69
XDOT = 4674
058156 XDOT = 1424
652926
YDOT = -19488
652435 feet/sec YDOT = -5940
141262 meter/sec
ZDOT = -13470
293866 ZDOT = -4105
745570
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
09268209
00016717 00000-0 10270-3 0 9058
2 25544 51
6400 264
5477 0003960 293
7031 66
3706 15
54011901 2070
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
09268209 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 264
5477 deg
Eccentricity:
0003960
Arg of perigee: 293
7031 deg
Mean anomaly: 66
3706 deg
Mean motion: 15
54011901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 207
Checksum: 292
Coasting Arc #7 (Orbit 218)
---------------------------------------
Vector Time (GMT): 2018/191/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4347412
00 A = 6778847
91 meter
Y = -1292534
49 meter E =
0009376
Z = -5046500
77 I = 51
24739
XDOT = 129
115690 Wp = 98
02051
YDOT = -7446
095912 meter/sec RA = 259
82266 deg
ZDOT = 1797
493223 TA = 189
47985
MA = 189
49756
Ha = 220
118 n
mi
Hp = 216
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14263162
73 X = -4308122
28
Y = -4240598
73 feet Y = -1340929
76 meter
Z = -16556761
04 Z = -5067523
69
XDOT = 423
607907 XDOT = 203
639146
YDOT = -24429
448530 feet/sec YDOT = -7444
235652 meter/sec
ZDOT = 5897
287476 ZDOT = 1798
300234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11698438
43 X = 3565684
03
Y = -9024947
70 feet Y = -2750804
06 meter
Z = -16650636
09 Z = -5075113
88
XDOT = 18964
375026 XDOT = 5780
341508
YDOT = 13703
066663 feet/sec YDOT = 4176
694719 meter/sec
ZDOT = 5901
912269 ZDOT = 1798
902860
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
86436195
00016717 00000-0 10270-3 0 9065
2 25544 51
6387 260
7002 0003967 296
7107 63
3639 15
53983054 2191
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
86436195 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 260
7002 deg
Eccentricity:
0003967
Arg of perigee: 296
7107 deg
Mean anomaly: 63
3639 deg
Mean motion: 15
53983054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 219
Checksum: 330
Coasting Arc #8 (Orbit 234)
---------------------------------------
Vector Time (GMT): 2018/192/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4362138
96 A = 6781801
63 meter
Y = 2915665
83 meter E =
0007750
Z = 4295024
47 I = 51
26445
XDOT = -1066
298109 Wp = 48
82580
YDOT = 6745
355846 meter/sec RA = 254
80377 deg
ZDOT = -3486
971703 TA = 76
87818
MA = 76
79170
Ha = 220
189 n
mi
Hp = 216
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14311479
54 X = 4308348
22
Y = 9565832
77 feet Y = 2964144
79 meter
Z = 14091287
62 Z = 4316083
88
XDOT = -3498
353376 XDOT = -1124
709572
YDOT = 22130
432564 feet/sec YDOT = 6733
105751 meter/sec
ZDOT = -11440
195876 ZDOT = -3492
292102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15957208
72 X = -4863757
22
Y = 6248026
25 feet Y = 1904398
40 meter
Z = 14185120
65 Z = 4323624
77
XDOT = -15794
836159 XDOT = -4814
266061
YDOT = -14242
596219 feet/sec YDOT = -4341
143327 meter/sec
ZDOT = -11464
905551 ZDOT = -3494
503212
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 18192
89328883
00016717 00000-0 10270-3 0 9074
2 25544 51
6389 255
5725 0004022 301
9734 58
1027 15
53991179 2353
Satellite: ISS
Catalog Number: 25544
Epoch time: 18192
89328883 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 255
5725 deg
Eccentricity:
0004022
Arg of perigee: 301
9734 deg
Mean anomaly: 58
1027 deg
Mean motion: 15
53991179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 235
Checksum: 331
Coasting Arc #9 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2018/193/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3327151
35 A = 6778494
08 meter
Y = 2929177
18 meter E =
0011398
Z = -5138149
73 I = 51
26011
XDOT = -3599
591244 Wp = 64
38474
YDOT = -6607
584559 meter/sec RA = 250
21287 deg
ZDOT = -1433
658999 TA = 191
71788
MA = 191
74443
Ha = 220
380 n
mi
Hp = 215
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10915850
89 X = -3334700
89
Y = 9610161
34 feet Y = 2891929
30 meter
Z = -16857446
63 Z = -5154329
50
XDOT = -11809
682558 XDOT = -3518
472034
YDOT = -21678
427031 feet/sec YDOT = -6647
383871 meter/sec
ZDOT = -4703
605641 ZDOT = -1450
948367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4855179
80 X = 1479858
80
Y = -13619065
97 feet Y = -4151091
31 meter
Z = -16930232
71 Z = -5160334
93
XDOT = 19755
614102 XDOT = 6021
511178
YDOT = 12994
643164 feet/sec YDOT = 3960
767236 meter/sec
ZDOT = -4780
098352 ZDOT = -1456
973978
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 18193
79359901
00016717 00000-0 10270-3 0 9080
2 25544 51
6370 251
0848 0003983 305
4995 54
5786 15
53979796 2491
Satellite: ISS
Catalog Number: 25544
Epoch time: 18193
79359901 = yrday
fracday
Element set: 908
Inclination: 51
6370 deg
RA of node: 251
0848 deg
Eccentricity:
0003983
Arg of perigee: 305
4995 deg
Mean anomaly: 54
5786 deg
Mean motion: 15
53979796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 365
Coasting Arc #10 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2018/194/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4050408
11 A = 6777823
53 meter
Y = -1316849
70 meter E =
0003452
Z = 5273210
19 I = 51
27027
XDOT = 2886
297195 Wp = 350
10028
YDOT = 7090
316442 meter/sec RA = 245
18943 deg
ZDOT = -443
069871 TA = 104
16658
MA = 104
12822
Ha = 220
329 n
mi
Hp = 216
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13288740
52 X = 4039218
50
Y = -4320373
03 feet Y = -1271618
57 meter
Z = 17300558
38 Z = 5292857
91
XDOT = 9469
478985 XDOT = 2808
948969
YDOT = 23262
193051 feet/sec YDOT = 7122
160592 meter/sec
ZDOT = -1453
641309 ZDOT = -429
236350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9300534
79 X = -2834803
00
Y = 10281062
53 feet Y = 3133667
86 meter
Z = 17388656
47 Z = 5300062
49
XDOT = -19013
413390 XDOT = -5795
288401
YDOT = -14826
417308 feet/sec YDOT = -4519
091996 meter/sec
ZDOT = -1392
649172 ZDOT = -424
479468
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
82252467
00016717 00000-0 10270-3 0 9095
2 25544 51
6371 245
9573 0004039 309
3044 50
7750 15
53986235 2653
Satellite: ISS
Catalog Number: 25544
Epoch time: 18194
82252467 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 245
9573 deg
Eccentricity:
0004039
Arg of perigee: 309
3044 deg
Mean anomaly: 50
7750 deg
Mean motion: 15
53986235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 322
Coasting Arc #11 (Orbit 279)
---------------------------------------
Vector Time (GMT): 2018/195/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 959612
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4686761
15 A = 6779453
30 meter
Y = -281744
16 meter E =
0008732
Z = -4898205
40 I = 51
29073
XDOT = -1946
691254 Wp = 94
72535
YDOT = -7053
353636 meter/sec RA = 240
16694 deg
ZDOT = 2271
167394 TA = 197
58656
MA = 197
61681
Ha = 220
506 n
mi
Hp = 215
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15376512
97 X = -4659469
94
Y = -924357
48 feet Y = -334001
58 meter
Z = -16070227
70 Z = -4920905
29
XDOT = -6386
782329 XDOT = -1878
705912
YDOT = -23140
924004 feet/sec YDOT = -7074
743020 meter/sec
ZDOT = 7451
336594 ZDOT = 2261
875545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13602098
04 X = 4145919
48
Y = -6999994
80 feet Y = -2133598
42 meter
Z = -16171790
50 Z = -4929161
74
XDOT = 16837
907928 XDOT = 5132
194336
YDOT = 15619
343149 feet/sec YDOT = 4760
775792 meter/sec
ZDOT = 7410
639030 ZDOT = 2258
762776
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
78713977
00016717 00000-0 10270-3 0 9101
2 25544 51
6372 241
1491 0004103 312
6536 47
4271 15
53986851 2808
Satellite: ISS
Catalog Number: 25544
Epoch time: 18195
78713977 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 241
1491 deg
Eccentricity:
0004103
Arg of perigee: 312
6536 deg
Mean anomaly: 47
4271 deg
Mean motion: 15
53986851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 280
Checksum: 313
Coasting Arc #12 (Orbit 295)
---------------------------------------
Vector Time (GMT): 2018/196/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5162000
40 A = 6782723
05 meter
Y = 1780142
82 meter E =
0009364
Z = 4020969
36 I = 51
31906
XDOT = 775
307299 Wp = 55
30279
YDOT = 6562
735149 meter/sec RA = 235
15305 deg
ZDOT = -3889
028989 TA = 75
26894
MA = 75
16519
Ha = 220
621 n
mi
Hp = 215
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16935696
85 X = 5122179
40
Y = 5840363
59 feet Y = 1837644
86 meter
Z = 13192156
68 Z = 4045947
44
XDOT = 2543
659116 XDOT = 720
753786
YDOT = 21531
283297 feet/sec YDOT = 6571
100492 meter/sec
ZDOT = -12759
281461 ZDOT = -3885
394810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17404745
94 X = -5304966
56
Y = 3878905
60 feet Y = 1182290
43 meter
Z = 13303743
18 Z = 4054980
92
XDOT = -13262
734867 XDOT = -4042
481588
YDOT = -15671
239498 feet/sec YDOT = -4776
593799 meter/sec
ZDOT = -12743
823102 ZDOT = -3884
317281
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
81606125
00016717 00000-0 10270-3 0 9113
2 25544 51
6371 236
0208 0004167 318
2421 41
8413 15
54003060 2967
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
81606125 = yrday
fracday
Element set: 911
Inclination: 51
6371 deg
RA of node: 236
0208 deg
Eccentricity:
0004167
Arg of perigee: 318
2421 deg
Mean anomaly: 41
8413 deg
Mean motion: 15
54003060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 296
Checksum: 274
Coasting Arc #13 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -737252
60 A = 6784031
59 meter
Y = -5644937
37 meter E =
0009653
Z = 3679754
25 I = 51
33769
XDOT = 6019
359846 Wp = 78
07047
YDOT = 2024
127481 meter/sec RA = 231
41783 deg
ZDOT = 4303
492793 TA = 325
97345
MA = 326
03531
Ha = 220
816 n
mi
Hp = 215
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2418807
73 X = -691948
49
Y = -18520135
73 feet Y = -5652928
79 meter
Z = 12072684
56 Z = 3676282
64
XDOT = 19748
555926 XDOT = 5975
374473
YDOT = 6640
838191 feet/sec YDOT = 2091
193872 meter/sec
ZDOT = 14119
070843 ZDOT = 4332
625455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13806968
34 X = -4208363
95
Y = 12592544
50 feet Y = 3838207
56 meter
Z = 12057828
12 Z = 3675226
01
XDOT = -4803
543188 XDOT = -1464
119964
YDOT = -18934
958820 feet/sec YDOT = -5771
375448 meter/sec
ZDOT = 14249
236701 ZDOT = 4343
167346
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
58775244
00016717 00000-0 10270-3 0 9128
2 25544 51
6371 232
1737 0003826 322
7325 37
3561 15
53979380 3089
Satellite: ISS
Catalog Number: 25544
Epoch time: 18197
58775244 = yrday
fracday
Element set: 912
Inclination: 51
6371 deg
RA of node: 232
1737 deg
Eccentricity:
0003826
Arg of perigee: 322
7325 deg
Mean anomaly: 37
3561 deg
Mean motion: 15
53979380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 321
Coasting Arc #14 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2018/198/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -534732
26 A = 6780382
38 meter
Y = 4877517
97 meter E =
0010248
Z = -4689292
18 I = 51
34842
XDOT = -6287
499382 Wp = 49
59536
YDOT = -3371
564539 meter/sec RA = 226
40978 deg
ZDOT = -2787
432953 TA = 192
61802
MA = 192
64370
Ha = 220
827 n
mi
Hp = 215
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1754370
94 X = -566456
57
Y = 16002355
54 feet Y = 4871361
11 meter
Z = -15384816
87 Z = -4691966
46
XDOT = -20628
278812 XDOT = -6235
790683
YDOT = -11061
563447 feet/sec YDOT = -3441
586420 meter/sec
ZDOT = -9145
121237 ZDOT = -2817
849509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13963027
83 X = 4255930
88
Y = -7987532
92 feet Y = -2434600
03 meter
Z = -15397368
67 Z = -4693117
97
XDOT = 2422
535517 XDOT = 738
388826
YDOT = 22141
082854 feet/sec YDOT = 6748
602054 meter/sec
ZDOT = -9280
890635 ZDOT = -2828
815465
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
55236386
00016717 00000-0 10270-3 0 9136
2 25544 51
6384 227
3666 0003911 323
2771 36
8113 15
54000463 3238
Satellite: ISS
Catalog Number: 25544
Epoch time: 18198
55236386 = yrday
fracday
Element set: 913
Inclination: 51
6384 deg
RA of node: 227
3666 deg
Eccentricity:
0003911
Arg of perigee: 323
2771 deg
Mean anomaly: 36
8113 deg
Mean motion: 15
54000463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 298
Coasting Arc #15 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2018/199/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3662999
85 A = 6788074
48 meter
Y = -5349067
63 meter E =
0013934
Z = 1983967
31 I = 51
39733
XDOT = 5094
468718 Wp = 51
49366
YDOT = -1420
508545 meter/sec RA = 221
45540 deg
ZDOT = 5558
050085 TA = 330
49650
MA = 330
57507
Ha = 220
996 n
mi
Hp = 215
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12017716
03 X = -3612549
79
Y = -17549434
49 feet Y = -5389747
85 meter
Z = 6509079
09 Z = 1966296
22
XDOT = 16714
136214 XDOT = 5082
976905
YDOT = -4660
461105 feet/sec YDOT = -1363
603222 meter/sec
ZDOT = 18235
072456 ZDOT = 5582
768921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8185988
40 X = -2495089
26
Y = 19657400
70 feet Y = 5991575
73 meter
Z = 6430587
21 Z = 1960042
98
XDOT = -11489
660921 XDOT = -3502
048649
YDOT = -10805
750243 feet/sec YDOT = -3293
592674 meter/sec
ZDOT = 18345
910009 ZDOT = 5591
833371
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
58128182
00016717 00000-0 10270-3 0 9145
2 25544 51
6383 222
2378 0004032 329
5178 30
5740 15
54001129 3390
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
58128182 = yrday
fracday
Element set: 914
Inclination: 51
6383 deg
RA of node: 222
2378 deg
Eccentricity:
0004032
Arg of perigee: 329
5178 deg
Mean anomaly: 30
5740 deg
Mean motion: 15
54001129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 299
Coasting Arc #16 (Orbit 353)
---------------------------------------
Vector Time (GMT): 2018/200/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2543329
97 A = 6784795
84 meter
Y = 5279013
70 meter E =
0004628
Z = -3426304
39 I = 51
41057
XDOT = -6147
311941 Wp = 40
54739
YDOT = -5
884573 meter/sec RA = 216
46234 deg
ZDOT = -4572
227543 TA = 179
67671
MA = 179
67642
Ha = 221
077 n
mi
Hp = 215
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8344258
43 X = 2500752
57
Y = 17319598
74 feet Y = 5307217
10 meter
Z = -11241156
14 Z = -3414053
02
XDOT = -20168
346262 XDOT = -6124
580022
YDOT = -19
306343 feet/sec YDOT = -74
500701 meter/sec
ZDOT = -15000
746531 ZDOT = -4602
033532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9685662
65 X = 2952189
97
Y = -16643309
70 feet Y = -5072880
80 meter
Z = -11186908
52 Z = -3409769
72
XDOT = 9956
015655 XDOT = 3034
593572
YDOT = 15966
423132 feet/sec YDOT = 4866
565771 meter/sec
ZDOT = -15134
206042 ZDOT = -4612
906001
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
54589154
00016717 00000-0 10270-3 0 9155
2 25544 51
6371 217
4304 0004016 332
2768 27
8170 15
53994012 3544
Satellite: ISS
Catalog Number: 25544
Epoch time: 18200
54589154 = yrday
fracday
Element set: 915
Inclination: 51
6371 deg
RA of node: 217
4304 deg
Eccentricity:
0004016
Arg of perigee: 332
2768 deg
Mean anomaly: 27
8170 deg
Mean motion: 15
53994012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 354
Checksum: 293
Coasting Arc #17 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2018/201/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944898
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1157652
27 A = 6781123
43 meter
Y = -4924870
64 meter E =
0006613
Z = 4509505
57 I = 51
42468
XDOT = 6880
431132 Wp = 86
75277
YDOT = 1267
428984 meter/sec RA = 211
46070 deg
ZDOT = 3146
845360 TA = 331
58083
MA = 331
61689
Ha = 221
194 n
mi
Hp = 215
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3798071
75 X = -1124399
59
Y = -16157712
08 feet Y = -4937630
68 meter
Z = 14794965
77 Z = 4503962
57
XDOT = 22573
592953 XDOT = 6850
461436
YDOT = 4158
231575 feet/sec YDOT = 1344
202936 meter/sec
ZDOT = 10324
295801 ZDOT = 3180
195135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11029552
13 X = -3361807
49
Y = 12432345
53 feet Y = 3789378
92 meter
Z = 14770706
99 Z = 4502111
49
XDOT = -8545
079378 XDOT = -2604
540195
YDOT = -20038
483326 feet/sec YDOT = -6107
729718 meter/sec
ZDOT = 10473
494538 ZDOT = 3192
321135
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
57480843
00016717 00000-0 10270-3 0 9165
2 25544 51
6363 212
3017 0004129 336
2208 23
8753 15
53990832 3705
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
57480843 = yrday
fracday
Element set: 916
Inclination: 51
6363 deg
RA of node: 212
3017 deg
Eccentricity:
0004129
Arg of perigee: 336
2208 deg
Mean anomaly: 23
8753 deg
Mean motion: 15
53990832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 294
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