[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 6th 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) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
339/18:16:16
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
9
341/20:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
1
344/23:07:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
4
348/03:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
6
354/01:40:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 2514)
---------------------------------------
Vector Time (GMT): 2018/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944383
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 156541
05 A = 6785426
03 meter
Y = 6025750
74 meter E =
0009565
Z = -3119905
92 I = 51
30225
XDOT = -5457
180083 Wp = 108
87702
YDOT = -2354
254332 meter/sec RA = 244
01569 deg
ZDOT = -4836
029025 TA = 107
20701
MA = 107
10228
Ha = 222
899 n
mi
Hp = 213
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 513586
11 X = 104302
90
Y = 19769523
43 feet Y = 6027209
47 meter
Z = -10235911
81 Z = -3119271
87
XDOT = -17904
134129 XDOT = -5406
957276
YDOT = -7723
931534 feet/sec YDOT = -2414
999103 meter/sec
ZDOT = -15866
236960 ZDOT = -4862
416785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19107292
52 X = -5823902
76
Y = -5104277
83 feet Y = -1555783
88 meter
Z = -10233740
20 Z = -3119244
01
XDOT = 12126
602780 XDOT = 3696
188527
YDOT = -13446
678529 feet/sec YDOT = -4098
547616 meter/sec
ZDOT = -15984
635389 ZDOT = -4872
116867
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 18339
52579699
00016717 00000-0 10270-3 0 9003
2 25544 51
6415 244
8758 0005068 112
4832 247
6857 15
54051712 25155
Satellite: ISS
Catalog Number: 25544
Epoch time: 18339
52579699 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 244
8758 deg
Eccentricity:
0005068
Arg of perigee: 112
4832 deg
Mean anomaly: 247
6857 deg
Mean motion: 15
54051712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2515
Checksum: 332
Coasting Arc #2 (Orbit 2518)
---------------------------------------
Vector Time (GMT): 2018/339/18:16:16
000
Vector Time (MET): N/A
Weight (LBS) : 944383
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1620772
87 A = 6780777
42 meter
Y = 4785491
63 meter E =
0014103
Z = -4535078
08 I = 51
28668
XDOT = -5207
243755 Wp = 85
64206
YDOT = -4686
477615 meter/sec RA = 242
70157 deg
ZDOT = -3091
545079 TA = 153
23530
MA = 153
16246
Ha = 222
960 n
mi
Hp = 212
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5317496
31 X = -1652135
73
Y = 15700431
87 feet Y = 4767192
06 meter
Z = -14878865
10 Z = -4543027
13
XDOT = -17084
133055 XDOT = -5139
433886
YDOT = -15375
582727 feet/sec YDOT = -4744
329215 meter/sec
ZDOT = -10142
864434 ZDOT = -3116
676206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8447364
85 X = -2574756
80
Y = 14224635
78 feet Y = 4335668
99 meter
Z = -14915150
63 Z = -4546137
91
XDOT = -12306
745206 XDOT = -3751
095939
YDOT = -18036
586063 feet/sec YDOT = -5497
551432 meter/sec
ZDOT = -10255
353193 ZDOT = -3125
831653
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 18339
78301784
00016717 00000-0 10270-3 0 9010
2 25544 51
6375 243
5899 0005359 115
3021 244
8687 15
54063064 25194
Satellite: ISS
Catalog Number: 25544
Epoch time: 18339
78301784 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 243
5899 deg
Eccentricity:
0005359
Arg of perigee: 115
3021 deg
Mean anomaly: 244
8687 deg
Mean motion: 15
54063064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2519
Checksum: 328
Coasting Arc #3 (Orbit 2534)
---------------------------------------
Vector Time (GMT): 2018/340/18:16:16
000
Vector Time (MET): N/A
Weight (LBS) : 944383
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2677232
90 A = 6778271
66 meter
Y = -3489627
88 meter E =
0009679
Z = 5151421
70 I = 51
29287
XDOT = 4904
763009 Wp = 122
20532
YDOT = 5748
010143 meter/sec RA = 237
68244 deg
ZDOT = 1337
801174 TA = 314
84623
MA = 314
92483
Ha = 222
888 n
mi
Hp = 213
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8783572
49 X = 2691032
65
Y = -11448910
37 feet Y = -3459612
59 meter
Z = 16900989
84 Z = 5164460
12
XDOT = 16091
742154 XDOT = 4833
624188
YDOT = 18858
300995 feet/sec YDOT = 5802
460707 meter/sec
ZDOT = 4389
111463 ZDOT = 1361
455000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10751168
41 X = 3276956
13
Y = -9520624
43 feet Y = -2901886
33 meter
Z = 16960018
88 Z = 5169413
75
XDOT = 11348
940954 XDOT = 3459
157203
YDOT = 20863
222072 feet/sec YDOT = 6359
110088 meter/sec
ZDOT = 4494
855879 ZDOT = 1370
032072
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 18340
81190247
00016717 00000-0 10270-3 0 9027
2 25544 51
6362 238
4613 0005282 119
7030 240
4648 15
54024615 25356
Satellite: ISS
Catalog Number: 25544
Epoch time: 18340
81190247 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node: 238
4613 deg
Eccentricity:
0005282
Arg of perigee: 119
7030 deg
Mean anomaly: 240
4648 deg
Mean motion: 15
54024615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2535
Checksum: 287
Coasting Arc #4 (Orbit 2549)
---------------------------------------
Vector Time (GMT): 2018/341/18:16:16
000
Vector Time (MET): N/A
Weight (LBS) : 944383
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3753351
38 A = 6777650
26 meter
Y = 2046469
43 meter E =
0019548
Z = -5276301
32 I = 51
31146
XDOT = -4258
295222 Wp = 102
29133
YDOT = -6334
444103 meter/sec RA = 232
66058 deg
ZDOT = 570
015386 TA = 173
19692
MA = 173
17034
Ha = 222
899 n
mi
Hp = 212
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12314144
96 X = -3750326
83
Y = 6714138
57 feet Y = 2004514
40 meter
Z = -17310699
88 Z = -5294526
43
XDOT = -13970
784848 XDOT = -4189
914076
YDOT = -20782
296926 feet/sec YDOT = -6381
681045 meter/sec
ZDOT = 1870
129220 ZDOT = 549
495139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13205790
66 X = -4025124
99
Y = 4412727
36 feet Y = 1344999
30 meter
Z = -17392903
24 Z = -5301356
91
XDOT = -9701
135366 XDOT = -2956
906059
YDOT = -21992
673093 feet/sec YDOT = -6703
366759 meter/sec
ZDOT = 1778
523652 ZDOT = 542
094009
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 18341
77647790
00016717 00000-0 10270-3 0 9034
2 25544 51
6379 233
6540 0005351 123
9440 236
2221 15
54063216 25506
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
77647790 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 233
6540 deg
Eccentricity:
0005351
Arg of perigee: 123
9440 deg
Mean anomaly: 236
2221 deg
Mean motion: 15
54063216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2550
Checksum: 294
Coasting Arc #5 (Orbit 2551)
---------------------------------------
Vector Time (GMT): 2018/341/20:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 944383
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1356542
79 A = 6785281
03 meter
Y = -5854327
51 meter E =
0017239
Z = 3138397
84 I = 51
34072
XDOT = 5837
536993 Wp = 97
35527
YDOT = 1243
914585 meter/sec RA = 232
25887 deg
ZDOT = 4818
639360 TA = 299
00213
MA = 299
17479
Ha = 222
812 n
mi
Hp = 213
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4450599
71 X = -1306222
10
Y = -19207111
26 feet Y = -5869216
34 meter
Z = 10296580
83 Z = 3131929
65
XDOT = 19152
024254 XDOT = 5799
786657
YDOT = 4081
084596 feet/sec YDOT = 1308
982317 meter/sec
ZDOT = 15809
184253 ZDOT = 4846
904884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11008101
41 X = -3355269
31
Y = -16374607
38 feet Y = -4990980
33 meter
Z = 10268129
04 Z = 3129725
73
XDOT = 18067
066274 XDOT = 5506
841800
YDOT = -2101
176866 feet/sec YDOT = -640
438709 meter/sec
ZDOT = 15936
190037 ZDOT = 4857
350723
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 18341
90508618
00016717 00000-0 10270-3 0 9045
2 25544 51
6397 233
0121 0005288 127
4481 232
7153 15
54093334 25529
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
90508618 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 233
0121 deg
Eccentricity:
0005288
Arg of perigee: 127
4481 deg
Mean anomaly: 232
7153 deg
Mean motion: 15
54093334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2552
Checksum: 298
Coasting Arc #6 (Orbit 2566)
---------------------------------------
Vector Time (GMT): 2018/342/20:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 94691
85 A = 6781572
29 meter
Y = 5217651
59 meter E =
0012204
Z = -4341277
48 I = 51
34895
XDOT = -6273
325437 Wp = 91
82009
YDOT = -2738
203767 meter/sec RA = 227
25408 deg
ZDOT = -3436
571458 TA = 143
15501
MA = 143
07109
Ha = 222
833 n
mi
Hp = 213
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 310668
79 X = 57427
36
Y = 17118279
51 feet Y = 5218502
70 meter
Z = -14243036
37 Z = -4340907
34
XDOT = -20581
776368 XDOT = -6225
546653
YDOT = -8983
608160 feet/sec YDOT = -2808
088863 meter/sec
ZDOT = -11274
840743 ZDOT = -3466
929638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6693995
91 X = 2040329
95
Y = 15759243
32 feet Y = 4803417
37 meter
Z = -14241936
74 Z = -4340942
32
XDOT = -21225
149645 XDOT = -6469
425612
YDOT = -1270
709677 feet/sec YDOT = -387
312310 meter/sec
ZDOT = -11411
118210 ZDOT = -3478
108830
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 18342
86966091
00016717 00000-0 10270-3 0 9055
2 25544 51
6395 228
2046 0005286 129
3479 230
8143 15
54053124 25672
Satellite: ISS
Catalog Number: 25544
Epoch time: 18342
86966091 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 228
2046 deg
Eccentricity:
0005286
Arg of perigee: 129
3479 deg
Mean anomaly: 230
8143 deg
Mean motion: 15
54053124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2567
Checksum: 321
Coasting Arc #7 (Orbit 2582)
---------------------------------------
Vector Time (GMT): 2018/343/20:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1267538
87 A = 6778494
96 meter
Y = -4317339
63 meter E =
0010592
Z = 5064342
63 I = 51
36192
XDOT = 6368
906666 Wp = 129
24249
YDOT = 3912
662429 meter/sec RA = 222
24123 deg
ZDOT = 1732
463214 TA = 303
90521
MA = 304
00590
Ha = 222
691 n
mi
Hp = 213
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4158592
09 X = 1291122
37
Y = -14164500
10 feet Y = -4303033
91 meter
Z = 16615297
36 Z = 5070556
66
XDOT = 20895
363077 XDOT = 6316
265407
YDOT = 12836
818994 feet/sec YDOT = 3983
589414 meter/sec
ZDOT = 5683
934428 ZDOT = 1763
273911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1716774
70 X = -523272
93
Y = -14629914
47 feet Y = -4459197
93 meter
Z = 16643717
88 Z = 5073005
21
XDOT = 23124
695973 XDOT = 7048
407333
YDOT = 3943
552938 feet/sec YDOT = 1201
994936 meter/sec
ZDOT = 5822
146497 ZDOT = 1774
590252
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 18343
89853652
00016717 00000-0 10270-3 0 9068
2 25544 51
6390 223
0764 0005263 133
3493 226
8099 15
54093555 25838
Satellite: ISS
Catalog Number: 25544
Epoch time: 18343
89853652 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 223
0764 deg
Eccentricity:
0005263
Arg of perigee: 133
3493 deg
Mean anomaly: 226
8099 deg
Mean motion: 15
54093555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2583
Checksum: 330
Coasting Arc #8 (Orbit 2597)
---------------------------------------
Vector Time (GMT): 2018/344/20:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2718015
25 A = 6777511
81 meter
Y = 3254776
09 meter E =
0018951
Z = -5303258
19 I = 51
38426
XDOT = -6010
622971 Wp = 102
64352
YDOT = -4736
812520 meter/sec RA = 217
22480 deg
ZDOT = 169
872708 TA = 169
00477
MA = 168
96330
Ha = 222
705 n
mi
Hp = 213
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8917372
87 X = -2728448
62
Y = 10678399
25 feet Y = 3224323
65 meter
Z = -17399141
05 Z = -5316486
33
XDOT = -19719
891636 XDOT = -5958
033038
YDOT = -15540
723492 feet/sec YDOT = -4803
733454 meter/sec
ZDOT = 557
325156 ZDOT = 140
802337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3784012
55 X = -1153367
02
Y = 13309472
52 feet Y = 4056727
22 meter
Z = -17459010
54 Z = -5321506
41
XDOT = -23327
827667 XDOT = -7110
321873
YDOT = -6056
973135 feet/sec YDOT = -1846
165412 meter/sec
ZDOT = 427
004578 ZDOT = 130
150995
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 18344
86310787
00016717 00000-0 10270-3 0 9074
2 25544 51
6394 218
2693 0005245 135
8469 224
3103 15
54078712 25982
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
86310787 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 218
2693 deg
Eccentricity:
0005245
Arg of perigee: 135
8469 deg
Mean anomaly: 224
3103 deg
Mean motion: 15
54078712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2598
Checksum: 330
Coasting Arc #9 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2018/344/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4026447
72 A = 6787750
26 meter
Y = 5053662
03 meter E =
0011736
Z = -2067763
06 I = 51
42025
XDOT = -5021
962530 Wp = 138
14246
YDOT = 1752
824000 meter/sec RA = 216
66441 deg
ZDOT = -5521
762911 TA = 64
80450
MA = 64
68286
Ha = 222
725 n
mi
Hp = 213
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13210130
30 X = 3979681
10
Y = 16580256
00 feet Y = 5098427
32 meter
Z = -6783999
53 Z = -2048316
96
XDOT = -16476
255020 XDOT = -5014
368042
YDOT = 5750
734909 feet/sec YDOT = 1696
708036 meter/sec
ZDOT = -18116
020049 ZDOT = -5546
139221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20573032
59 X = 6270660
33
Y = -5228320
93 feet Y = -1593592
22 meter
Z = -6697019
59 Z = -2041251
57
XDOT = -1896
465788 XDOT = -578
042772
YDOT = 15769
672175 feet/sec YDOT = 4806
596079 meter/sec
ZDOT = -18225
900447 ZDOT = -5555
254456
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 18344
99171686
00016717 00000-0 10270-3 0 9082
2 25544 51
6383 217
6300 0005127 135
6696 224
4868 15
54062504 26002
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
99171686 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 217
6300 deg
Eccentricity:
0005127
Arg of perigee: 135
6696 deg
Mean anomaly: 224
4868 deg
Mean motion: 15
54062504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 318
Coasting Arc #10 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2018/345/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2893834
18 A = 6784386
00 meter
Y = -5046486
19 meter E =
0016170
Z = 3481413
05 I = 51
43680
XDOT = 6185
360329 Wp = 104
65154
YDOT = -415
646547 meter/sec RA = 211
67157 deg
ZDOT = 4517
299786 TA = 296
40039
MA = 296
56628
Ha = 222
652 n
mi
Hp = 213
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9494206
62 X = -2854098
72
Y = -16556713
23 feet Y = -5078625
25 meter
Z = 11421958
82 Z = 3467451
81
XDOT = 20293
176931 XDOT = 6167
605879
YDOT = -1363
669775 feet/sec YDOT = -346
577297 meter/sec
ZDOT = 14820
537356 ZDOT = 4547
302905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18994860
62 X = -5789633
52
Y = 2208989
18 feet Y = 673299
90 meter
Z = 11359643
15 Z = 3462419
23
XDOT = 6929
498496 XDOT = 2112
111141
YDOT = -17689
437186 feet/sec YDOT = -5391
740454 meter/sec
ZDOT = 14955
617284 ZDOT = 4558
472148
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 18346
02058822
00016717 00000-0 10270-3 0 9095
2 25544 51
6387 212
5011 0005061 138
5114 221
6424 15
54080889 26163
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
02058822 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 212
5011 deg
Eccentricity:
0005061
Arg of perigee: 138
5114 deg
Mean anomaly: 221
6424 deg
Mean motion: 15
54080889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 292
Coasting Arc #11 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2018/346/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1423213
66 A = 6780679
92 meter
Y = 4801006
79 meter E =
0012604
Z = -4582521
64 I = 51
45237
XDOT = -6988
351670 Wp = 92
78765
YDOT = -810
741035 meter/sec RA = 206
67122 deg
ZDOT = -3027
616923 TA = 146
89125
MA = 146
81230
Ha = 222
631 n
mi
Hp = 213
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4669336
15 X = 1391681
09
Y = 15751334
62 feet Y = 4816746
27 meter
Z = -15034519
82 Z = -4575684
33
XDOT = -22927
662960 XDOT = -6964
059823
YDOT = -2659
911533 feet/sec YDOT = -888
753540 meter/sec
ZDOT = -9933
126387 ZDOT = -3061
504899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16378992
57 X = 4992316
93
Y = 1595530
43 feet Y = 486317
67 meter
Z = -15004229
86 Z = -4573289
26
XDOT = -11059
107256 XDOT = -3370
815892
YDOT = 18925
515616 feet/sec YDOT = 5768
497160 meter/sec
ZDOT = -10085
586814 ZDOT = -3074
086861
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 18346
98515610
00016717 00000-0 10270-3 0 9105
2 25544 51
6380 207
6934 0005107 141
0061 219
1461 15
54059024 26313
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
98515610 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 207
6934 deg
Eccentricity:
0005107
Arg of perigee: 141
0061 deg
Mean anomaly: 219
1461 deg
Mean motion: 15
54059024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 282
Coasting Arc #12 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2018/347/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 202615
62 A = 6778049
20 meter
Y = -4359066
14 meter E =
0009138
Z = 5182188
82 I = 51
47388
XDOT = 7341
612063 Wp = 136
03812
YDOT = 1841
682018 meter/sec RA = 201
66411 deg
ZDOT = 1254
327711 TA = 301
85504
MA = 301
94395
Ha = 222
513 n
mi
Hp = 213
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 664749
41 X = 226172
58
Y = -14301398
11 feet Y = -4356669
04 meter
Z = 17001931
81 Z = 5183229
93
XDOT = 24086
653751 XDOT = 7314
379368
YDOT = 6042
263838 feet/sec YDOT = 1923
628663 meter/sec
ZDOT = 4115
248395 ZDOT = 1289
924637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13110478
58 X = -3996073
87
Y = -5736985
04 feet Y = -1748633
04 meter
Z = 17007054
98 Z = 5183750
36
XDOT = 13995
098880 XDOT = 4265
706139
YDOT = -19232
710899 feet/sec YDOT = -5862
130282 meter/sec
ZDOT = 4275
320470 ZDOT = 1303
117679
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 18348
01402507
00016717 00000-0 10270-3 0 9112
2 25544 51
6379 202
5650 0005022 145
0557 215
0926 15
54081201 26470
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
01402507 = yrday
fracday
Element set: 911
Inclination: 51
6379 deg
RA of node: 202
5650 deg
Eccentricity:
0005022
Arg of perigee: 145
0557 deg
Mean anomaly: 215
0926 deg
Mean motion: 15
54081201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 276
Coasting Arc #13 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2018/348/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4426187
87 A = 6780342
02 meter
Y = -2251526
75 meter E =
0010362
Z = 4607347
87 I = 51
48582
XDOT = 5412
980736 Wp = 92
62871
YDOT = 4560
413770 meter/sec RA = 200
63132 deg
ZDOT = -2966
249257 TA = 27
00037
MA = 26
94650
Ha = 222
364 n
mi
Hp = 213
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14521613
76 X = 4428656
09
Y = -7386898
79 feet Y = -2202016
58 meter
Z = 15115970
70 Z = 4628854
54
XDOT = 17759
123148 XDOT = 5375
991052
YDOT = 14961
987434 feet/sec YDOT = 4620
738883 meter/sec
ZDOT = -9731
788902 ZDOT = -2940
044427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15848811
72 X = -4830717
81
Y = -3363821
04 feet Y = -1025292
65 meter
Z = 15213020
26 Z = 4636928
57
XDOT = -4640
302490 XDOT = -1414
364199
YDOT = -21696
091524 feet/sec YDOT = -6612
968697 meter/sec
ZDOT = -9614
267447 ZDOT = -2930
428718
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 18348
20693851
00016717 00000-0 10270-3 0 9128
2 25544 51
6358 201
6038 0004863 143
7427 216
4056 15
54076193 26507
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
20693851 = yrday
fracday
Element set: 912
Inclination: 51
6358 deg
RA of node: 201
6038 deg
Eccentricity:
0004863
Arg of perigee: 143
7427 deg
Mean anomaly: 216
4056 deg
Mean motion: 15
54076193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 309
Coasting Arc #14 (Orbit 2664)
---------------------------------------
Vector Time (GMT): 2018/349/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5617552
87 A = 6784056
40 meter
Y = 1366165
13 meter E =
0009273
Z = -3561128
67 I = 51
53046
XDOT = -3985
194444 Wp = 120
65431
YDOT = -4789
531643 meter/sec RA = 195
63465 deg
ZDOT = 4453
108514 TA = 197
28920
MA = 197
32080
Ha = 222
463 n
mi
Hp = 213
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18430291
58 X = -5615114
13
Y = 4482169
05 feet Y = 1303359
60 meter
Z = -11683493
00 Z = -3588410
77
XDOT = -13074
784922 XDOT = -3952
971217
YDOT = -15713
686492 feet/sec YDOT = -4833
916965 meter/sec
ZDOT = 14609
936070 ZDOT = 4433
827791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17204542
83 X = 5243944
65
Y = 7802594
59 feet Y = 2378230
83 meter
Z = -11806469
40 Z = -3598611
87
XDOT = 1232
922732 XDOT = 375
794849
YDOT = 19237
973880 feet/sec YDOT = 5863
734439 meter/sec
ZDOT = 14523
594101 ZDOT = 4426
791482
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 18349
17150135
00016717 00000-0 10270-3 0 9139
2 25544 51
6368 196
7959 0004813 145
6510 214
4955 15
54056379 26659
Satellite: ISS
Catalog Number: 25544
Epoch time: 18349
17150135 = yrday
fracday
Element set: 913
Inclination: 51
6368 deg
RA of node: 196
7959 deg
Eccentricity:
0004813
Arg of perigee: 145
6510 deg
Mean anomaly: 214
4955 deg
Mean motion: 15
54056379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2665
Checksum: 332
Coasting Arc #15 (Orbit 2680)
---------------------------------------
Vector Time (GMT): 2018/350/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6419248
99 A = 6787495
78 meter
Y = -501532
16 meter E =
0017779
Z = 2116714
06 I = 51
57417
XDOT = 2205
871383 Wp = 119
79151
YDOT = 4863
598084 meter/sec RA = 190
65012 deg
ZDOT = -5511
173928 TA = 36
71527
MA = 36
59360
Ha = 222
281 n
mi
Hp = 213
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21060528
19 X = 6414098
27
Y = -1645446
72 feet Y = -429776
57 meter
Z = 6944599
92 Z = 2147884
07
XDOT = 7237
110835 XDOT = 2178
091757
YDOT = 15956
686626 feet/sec YDOT = 4888
110654 meter/sec
ZDOT = -18081
279292 ZDOT = -5500
525745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17746130
58 X = -5409020
60
Y = -11373576
55 feet Y = -3466666
13 meter
Z = 7085013
51 Z = 2159512
12
XDOT = 2936
320096 XDOT = 894
990365
YDOT = -15867
683705 feet/sec YDOT = -4836
469993 meter/sec
ZDOT = -18033
804280 ZDOT = -5496
703545
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 18350
20036698
00016717 00000-0 10270-3 0 9143
2 25544 51
6366 191
6669 0004722 149
5449 210
5979 15
54080273 26813
Satellite: ISS
Catalog Number: 25544
Epoch time: 18350
20036698 = yrday
fracday
Element set: 914
Inclination: 51
6366 deg
RA of node: 191
6669 deg
Eccentricity:
0004722
Arg of perigee: 149
5449 deg
Mean anomaly: 210
5979 deg
Mean motion: 15
54080273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2681
Checksum: 330
Coasting Arc #16 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2018/351/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6763638
83 A = 6789307
96 meter
Y = -280521
46 meter E =
0010115
Z = -492011
47 I = 51
61300
XDOT = -229
262934 Wp = 67
83505
YDOT = -4785
589573 meter/sec RA = 185
67587 deg
ZDOT = 5982
490200 TA = 286
85859
MA = 286
96949
Ha = 222
273 n
mi
Hp = 213
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22190416
11 X = -6757609
33
Y = -920346
01 feet Y = -356123
43 meter
Z = -1614210
86 Z = -524852
43
XDOT = -752
174980 XDOT = -204
792023
YDOT = -15700
753193 feet/sec YDOT = -4788
016870 meter/sec
ZDOT = 19627
592519 ZDOT = 5981
435674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17367034
07 X = 5293471
98
Y = 13825644
48 feet Y = 4214056
44 meter
Z = -1762090
50 Z = -537085
18
XDOT = -7538
947700 XDOT = -2297
871259
YDOT = 11931
837075 feet/sec YDOT = 3636
823941 meter/sec
ZDOT = 19623
309681 ZDOT = 5981
184791
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 18351
16492751
00016717 00000-0 10270-3 0 9156
2 25544 51
6364 186
8594 0004819 153
9816 206
1580 15
54091686 26963
Satellite: ISS
Catalog Number: 25544
Epoch time: 18351
16492751 = yrday
fracday
Element set: 915
Inclination: 51
6364 deg
RA of node: 186
8594 deg
Eccentricity:
0004819
Arg of perigee: 153
9816 deg
Mean anomaly: 206
1580 deg
Mean motion: 15
54091686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 343
Coasting Arc #17 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2018/352/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6586655
76 A = 6788853
14 meter
Y = 1052735
29 meter E =
0013726
Z = -1227867
01 I = 51
64591
XDOT = -1820
235464 Wp = 147
75932
YDOT = 4609
765559 meter/sec RA = 180
70515 deg
ZDOT = -5853
529330 TA = 45
58845
MA = 45
47618
Ha = 222
215 n
mi
Hp = 213
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21609762
98 X = 6580358
62
Y = 3453855
93 feet Y = 1126356
73 meter
Z = -4028435
07 Z = -1195886
29
XDOT = -5971
901128 XDOT = -1843
214291
YDOT = 15123
902751 feet/sec YDOT = 4589
282341 meter/sec
ZDOT = -19204
492553 ZDOT = -5862
426967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15699619
01 X = -4785243
87
Y = -15283062
18 feet Y = -4658277
35 meter
Z = -3884486
97 Z = -1183991
63
XDOT = 12371
589053 XDOT = 3770
860343
YDOT = -7853
182063 feet/sec YDOT = -2393
649893 meter/sec
ZDOT = -19245
020003 ZDOT = -5865
882097
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 18352
19378948
00016717 00000-0 10270-3 0 9162
2 25544 51
6379 181
7302 0004618 157
9363 202
1989 15
54087510 27127
Satellite: ISS
Catalog Number: 25544
Epoch time: 18352
19378948 = yrday
fracday
Element set: 916
Inclination: 51
6379 deg
RA of node: 181
7302 deg
Eccentricity:
0004618
Arg of perigee: 157
9363 deg
Mean anomaly: 202
1989 deg
Mean motion: 15
54087510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 333
Coasting Arc #18 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2018/353/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5929321
83 A = 6786215
31 meter
Y = -1762434
54 meter E =
0014844
Z = 2781043
35 I = 51
66965
XDOT = 3704
915686 Wp = 97
64308
YDOT = -4338
829853 meter/sec RA = 175
73288 deg
ZDOT = 5124
040806 TA = 293
87250
MA = 294
02797
Ha = 222
141 n
mi
Hp = 214
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19453155
60 X = -5922682
08
Y = -5782265
55 feet Y = -1828703
46 meter
Z = 9124157
97 Z = 2752256
45
XDOT = 12155
235189 XDOT = 3728
268218
YDOT = -14235
006079 feet/sec YDOT = -4297
268791 meter/sec
ZDOT = 16811
157500 ZDOT = 5142
094509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12896419
53 X = 3930828
67
Y = 15744484
04 feet Y = 4798918
74 meter
Z = 8994648
50 Z = 2741568
86
XDOT = -16810
668693 XDOT = -5123
891818
YDOT = 4070
770262 feet/sec YDOT = 1240
770776 meter/sec
ZDOT = 16892
913499 ZDOT = 5148
960034
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 18353
22264884
00016717 00000-0 10270-3 0 9171
2 25544 51
6371 176
6020 0004669 161
4900 198
6423 15
54104891 27283
Satellite: ISS
Catalog Number: 25544
Epoch time: 18353
22264884 = yrday
fracday
Element set: 917
Inclination: 51
6371 deg
RA of node: 176
6020 deg
Eccentricity:
0004669
Arg of perigee: 161
4900 deg
Mean anomaly: 198
6423 deg
Mean motion: 15
54104891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 318
Coasting Arc #19 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2018/354/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 949610
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3595200
32 A = 6779931
22 meter
Y = -3239560
97 meter E =
0011424
Z = 4745005
83 I = 51
67692
XDOT = 6441
332854 Wp = 135
40000
YDOT = -3162
215924 meter/sec RA = 171
21792 deg
ZDOT = 2709
618862 TA = 287
77540
MA = 287
90003
Ha = 222
087 n
mi
Hp = 214
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11795276
64 X = -3581756
39
Y = -10628480
88 feet Y = -3279690
35 meter
Z = 15567604
43 Z = 4727573
72
XDOT = 21132
981806 XDOT = 6463
052881
YDOT = -10374
724161 feet/sec YDOT = -3090
063316 meter/sec
ZDOT = 8889
825662 ZDOT = 2740
961332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5174670
69 X = -1577239
63
Y = 15091230
09 feet Y = 4599806
93 meter
Z = 15489384
18 Z = 4721164
30
XDOT = -16640
694651 XDOT = -5072
083730
YDOT = -15015
921114 feet/sec YDOT = -4576
852755 meter/sec
ZDOT = 9031
352313 ZDOT = 2752
756185
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 18354
12290030
00016717 00000-0 10270-3 0 9184
2 25544 51
6354 172
1147 0004640 166
0108 194
1173 15
54107206 27427
Satellite: ISS
Catalog Number: 25544
Epoch time: 18354
12290030 = yrday
fracday
Element set: 918
Inclination: 51
6354 deg
RA of node: 172
1147 deg
Eccentricity:
0004640
Arg of perigee: 166
0108 deg
Mean anomaly: 194
1173 deg
Mean motion: 15
54107206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 275
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