[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 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) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
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
354/01:42:00
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 2545)
---------------------------------------
Vector Time (GMT): 2018/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944383
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2093215
25 A = 6778577
76 meter
Y = 4013298
14 meter E =
0017103
Z = -5060881
01 I = 51
31279
XDOT = -5448
202278 Wp = 88
29597
YDOT = -5076
354275 meter/sec RA = 233
99227 deg
ZDOT = -1776
876743 TA = 164
43214
MA = 164
37948
Ha = 222
756 n
mi
Hp = 213
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6867504
10 X = -2113354
10
Y = 13166988
65 feet Y = 3989778
35 meter
Z = -16603940
31 Z = -5071097
69
XDOT = -17874
679390 XDOT = -5382
400902
YDOT = -16654
705626 feet/sec YDOT = -5136
911730 meter/sec
ZDOT = -5829
648107 ZDOT = -1803
183338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11025210
82 X = -3360484
26
Y = -9870868
04 feet Y = -3008640
58 meter
Z = -16650337
14 Z = -5075022
76
XDOT = 19909
508610 XDOT = 6068
418224
YDOT = -12231
683117 feet/sec YDOT = -3728
217014 meter/sec
ZDOT = -5947
413702 ZDOT = -1812
771696
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
51925259
00016717 00000-0 10270-3 0 9002
2 25544 51
6411 234
9405 0004967 120
2902 239
8743 15
54082537 25462
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
51925259 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 234
9405 deg
Eccentricity:
0004967
Arg of perigee: 120
2902 deg
Mean anomaly: 239
8743 deg
Mean motion: 15
54082537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2546
Checksum: 308
Coasting Arc #2 (Orbit 2561)
---------------------------------------
Vector Time (GMT): 2018/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3270567
28 A = 6777430
76 meter
Y = -2687435
10 meter E =
0006976
Z = 5287250
44 I = 51
32972
XDOT = 4971
856600 Wp = 112
45606
YDOT = 5844
527434 meter/sec RA = 228
97152 deg
ZDOT = -107
286392 TA = 338
55537
MA = 338
58458
Ha = 222
576 n
mi
Hp = 213
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10730207
61 X = 3274692
95
Y = -8817044
30 feet Y = -2650838
95 meter
Z = 17346622
17 Z = 5303147
54
XDOT = 16311
865486 XDOT = 4906
653085
YDOT = 19174
958774 feet/sec YDOT = 5899
761627 meter/sec
ZDOT = -351
989474 ZDOT = -83
292244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6054176
41 X = 1845312
97
Y = 12398718
23 feet Y = 3779129
32 meter
Z = 17418428
76 Z = 5309137
09
XDOT = -21586
147837 XDOT = -6579
457861
YDOT = 10872
561583 feet/sec YDOT = 3313
956770 meter/sec
ZDOT = -244
687204 ZDOT = -74
580660
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
54812683
00016717 00000-0 10270-3 0 9013
2 25544 51
6412 229
8120 0004914 124
5855 235
5762 15
54098494 25627
Satellite: ISS
Catalog Number: 25544
Epoch time: 18342
54812683 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 229
8120 deg
Eccentricity:
0004914
Arg of perigee: 124
5855 deg
Mean anomaly: 235
5762 deg
Mean motion: 15
54098494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2562
Checksum: 314
Coasting Arc #3 (Orbit 2576)
---------------------------------------
Vector Time (GMT): 2018/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4401278
71 A = 6778775
85 meter
Y = 1312123
28 meter E =
0017505
Z = -5001983
07 I = 51
35561
XDOT = -4094
344425 Wp = 111
01372
YDOT = -6154
805465 meter/sec RA = 223
95255 deg
ZDOT = 1987
602228 TA = 178
40654
MA = 178
40095
Ha = 222
688 n
mi
Hp = 213
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14439890
77 X = -4391327
01
Y = 4304866
41 feet Y = 1262961
41 meter
Z = -16410705
60 Z = -5023338
73
XDOT = -13432
888534 XDOT = -4034
870139
YDOT = -20192
931316 feet/sec YDOT = -6200
258981 meter/sec
ZDOT = 6521
004684 ZDOT = 1967
856887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1047929
77 X = -319409
00
Y = -14925705
98 feet Y = -4549355
18 meter
Z = -16506929
53 Z = -5031312
12
XDOT = 21572
675147 XDOT = 6575
351385
YDOT = -8630
758395 feet/sec YDOT = -2630
655159 meter/sec
ZDOT = 6432
827502 ZDOT = 1960
725823
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
51269631
00016717 00000-0 10270-3 0 9021
2 25544 51
6401 225
0043 0004900 126
8690 233
2912 15
54080003 25779
Satellite: ISS
Catalog Number: 25544
Epoch time: 18343
51269631 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 225
0043 deg
Eccentricity:
0004900
Arg of perigee: 126
8690 deg
Mean anomaly: 233
2912 deg
Mean motion: 15
54080003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2577
Checksum: 274
Coasting Arc #4 (Orbit 2592)
---------------------------------------
Vector Time (GMT): 2018/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964842
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5332691
72 A = 6781831
98 meter
Y = 19807
55 meter E =
0013392
Z = 4177988
08 I = 51
39062
XDOT = 2867
480566 Wp = 91
88912
YDOT = 6094
598740 meter/sec RA = 218
94194 deg
ZDOT = -3679
098702 TA = 35
99658
MA = 35
90646
Ha = 222
420 n
mi
Hp = 213
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17495707
76 X = 5311779
40
Y = 64985
39 feet Y = 79323
97 meter
Z = 13707309
97 Z = 4203841
70
XDOT = 9407
744640 XDOT = 2816
987087
YDOT = 19995
402689 feet/sec YDOT = 6126
383021 meter/sec
ZDOT = -12070
533800 ZDOT = -3665
291351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3598193
14 X = -1096729
27
Y = 17028041
80 feet Y = 5190147
14 meter
Z = 13823644
90 Z = 4213446
96
XDOT = -20262
718212 XDOT = -6176
076511
YDOT = 5493
270532 feet/sec YDOT = 1674
348858 meter/sec
ZDOT = -12009
047078 ZDOT = -3660
357549
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
54156738
00016717 00000-0 10270-3 0 9039
2 25544 51
6399 219
8762 0004769 130
4422 229
7147 15
54112528 25937
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
54156738 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 219
8762 deg
Eccentricity:
0004769
Arg of perigee: 130
4422 deg
Mean anomaly: 229
7147 deg
Mean motion: 15
54112528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2593
Checksum: 330
Coasting Arc #5 (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 = 4018729
25 A = 6787717
07 meter
Y = 5056295
21 meter E =
0011726
Z = -2076235
58 I = 51
42027
XDOT = -5029
867068 Wp = 138
21488
YDOT = 1742
930690 meter/sec RA = 216
66408 deg
ZDOT = -5517
714548 TA = 64
83160
MA = 64
71003
Ha = 222
716 n
mi
Hp = 213
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13184807
25 X = 3971974
92
Y = 16588895
06 feet Y = 5100974
26 meter
Z = -6811796
54 Z = -2056826
95
XDOT = -16502
188543 XDOT = -5022
181027
YDOT = 5718
276542 feet/sec YDOT = 1686
726844 meter/sec
ZDOT = -18102
738017 ZDOT = -5542
129034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20570521
99 X = 6269895
10
Y = -5201860
19 feet Y = -1585526
99 meter
Z = -6724985
46 Z = -2049775
57
XDOT = -1934
841084 XDOT = -589
739562
YDOT = 15780
156695 feet/sec YDOT = 4809
791761 meter/sec
ZDOT = -18212
789176 ZDOT = -5551
258141
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
99169895
00016717 00000-0 10270-3 0 9047
2 25544 51
6384 217
6297 0005142 135
9748 224
1815 15
54068828 26000
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
99169895 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 217
6297 deg
Eccentricity:
0005142
Arg of perigee: 135
9748 deg
Mean anomaly: 224
1815 deg
Mean motion: 15
54068828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 341
Coasting Arc #6 (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 = -2882130
69 A = 6784340
97 meter
Y = -5047242
95 meter E =
0016156
Z = 3489973
99 I = 51
43679
XDOT = 6192
350541 Wp = 104
89101
YDOT = -403
434414 meter/sec RA = 211
67115 deg
ZDOT = 4508
818458 TA = 296
28391
MA = 296
44981
Ha = 222
643 n
mi
Hp = 213
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9455809
34 X = -2842429
22
Y = -16559196
04 feet Y = -5079251
32 meter
Z = 11450045
90 Z = 3476069
52
XDOT = 20316
110699 XDOT = 6174
500210
YDOT = -1323
603719 feet/sec YDOT = -334
287529 meter/sec
ZDOT = 14792
711477 ZDOT = 4538
855301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18981964
61 X = -5785702
81
Y = 2172936
63 feet Y = 662311
09 meter
Z = 11387985
81 Z = 3471058
07
XDOT = 6972
819688 XDOT = 2125
315441
YDOT = -17695
686200 feet/sec YDOT = -5393
645154 meter/sec
ZDOT = 14927
941931 ZDOT = 4550
036701
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
02056598
00016717 00000-0 10270-3 0 9059
2 25544 51
6388 212
5008 0005075 138
8282 221
3254 15
54087623 26165
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
02056598 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 212
5008 deg
Eccentricity:
0005075
Arg of perigee: 138
8282 deg
Mean anomaly: 221
3254 deg
Mean motion: 15
54087623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 308
Coasting Arc #7 (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 = 1407304
25 A = 6780632
90 meter
Y = 4799102
60 meter E =
0012632
Z = -4589386
22 I = 51
45235
XDOT = -6992
484297 Wp = 92
87123
YDOT = -824
614860 meter/sec RA = 206
67068 deg
ZDOT = -3014
305512 TA = 146
95515
MA = 146
87615
Ha = 222
621 n
mi
Hp = 213
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4617139
93 X = 1375827
51
Y = 15745087
29 feet Y = 4814664
48 meter
Z = -15057041
40 Z = -4582626
05
XDOT = -22941
221447 XDOT = -6968
101662
YDOT = -2705
429331 feet/sec YDOT = -902
673072 meter/sec
ZDOT = -9889
453778 ZDOT = -3048
213343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16353373
34 X = 4984508
19
Y = 1641262
00 feet Y = 500256
66 meter
Z = -15027098
52 Z = -4580259
63
XDOT = -11103
129446 XDOT = -3384
233855
YDOT = 18922
834716 feet/sec YDOT = 5767
680021 meter/sec
ZDOT = -10042
002176 ZDOT = -3060
802263
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
98512964
00016717 00000-0 10270-3 0 9069
2 25544 51
6381 207
6932 0005120 141
3259 218
8261 15
54065904 26317
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
98512964 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 207
6932 deg
Eccentricity:
0005120
Arg of perigee: 141
3259 deg
Mean anomaly: 218
8261 deg
Mean motion: 15
54065904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 310
Coasting Arc #8 (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 = 222164
81 A = 6778012
68 meter
Y = -4354125
17 meter E =
0009107
Z = 5185510
71 I = 51
47391
XDOT = 7340
894098 Wp = 136
24019
YDOT = 1856
500835 meter/sec RA = 201
66345 deg
ZDOT = 1236
589574 TA = 301
82621
MA = 301
91485
Ha = 222
501 n
mi
Hp = 213
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 728887
17 X = 245648
93
Y = -14285187
56 feet Y = -4351509
86 meter
Z = 17012830
40 Z = 5186646
61
XDOT = 24084
298222 XDOT = 7313
581911
YDOT = 6090
882005 feet/sec YDOT = 1938
439009 meter/sec
ZDOT = 4057
052408 ZDOT = 1272
182821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13071985
55 X = -3984341
19
Y = -5790699
55 feet Y = -1765005
22 meter
Z = 17018379
80 Z = 5187202
16
XDOT = 14035
717532 XDOT = 4278
086704
YDOT = -19215
928152 feet/sec YDOT = -5857
014901 meter/sec
ZDOT = 4217
106437 ZDOT = 1285
374042
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
01399390
00016717 00000-0 10270-3 0 9072
2 25544 51
6380 202
5648 0005036 145
3812 214
7669 15
54088491 26479
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
01399390 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 202
5648 deg
Eccentricity:
0005036
Arg of perigee: 145
3812 deg
Mean anomaly: 214
7669 deg
Mean motion: 15
54088491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 325
Coasting Arc #9 (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 = 4441004
74 A = 6780352
34 meter
Y = -2239005
52 meter E =
0010397
Z = 4599168
29 I = 51
48601
XDOT = 5397
417719 Wp = 92
80764
YDOT = 4568
283060 meter/sec RA = 200
63071 deg
ZDOT = -2982
502384 TA = 26
99989
MA = 26
94583
Ha = 222
351 n
mi
Hp = 213
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14570225
53 X = 4443371
58
Y = -7345818
63 feet Y = -2189330
23 meter
Z = 15089134
83 Z = 4620746
69
XDOT = 17708
063383 XDOT = 5360
420145
YDOT = 14987
805316 feet/sec YDOT = 4628
434094 meter/sec
ZDOT = -9785
112809 ZDOT = -2956
373172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15860764
33 X = -4834360
97
Y = -3426470
71 feet Y = -1044388
27 meter
Z = 15186506
06 Z = 4628847
05
XDOT = -4589
243516 XDOT = -1398
801424
YDOT = -21683
272486 feet/sec YDOT = -6609
061454 meter/sec
ZDOT = -9667
932577 ZDOT = -2946
785849
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
20690643
00016717 00000-0 10270-3 0 9089
2 25544 51
6359 201
6035 0004875 144
0787 216
0694 15
54083573 26505
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
20690643 = yrday
fracday
Element set: 908
Inclination: 51
6359 deg
RA of node: 201
6035 deg
Eccentricity:
0004875
Arg of perigee: 144
0787 deg
Mean anomaly: 216
0694 deg
Mean motion: 15
54083573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 318
Coasting Arc #10 (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 = -5630134
10 A = 6784076
76 meter
Y = 1350993
87 meter E =
0009213
Z = -3546973
94 I = 51
53068
XDOT = -3962
548878 Wp = 120
67887
YDOT = -4794
982849 meter/sec RA = 195
63409 deg
ZDOT = 4467
493837 TA = 197
46975
MA = 197
50146
Ha = 222
450 n
mi
Hp = 213
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18471568
57 X = -5627593
53
Y = 4432394
60 feet Y = 1288048
23 meter
Z = -11637053
62 Z = -3574316
92
XDOT = -13000
488446 XDOT = -3930
336253
YDOT = -15731
571027 feet/sec YDOT = -4839
114993 meter/sec
ZDOT = 14657
132012 ZDOT = 4448
323093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17206537
82 X = 5244552
73
Y = 7867421
64 feet Y = 2397990
12 meter
Z = -11760302
59 Z = -3584540
23
XDOT = 1168
408904 XDOT = 356
131034
YDOT = 19206
230054 feet/sec YDOT = 5854
058920 meter/sec
ZDOT = 14571
285771 ZDOT = 4441
327903
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
17146463
00016717 00000-0 10270-3 0 9093
2 25544 51
6368 196
7956 0004824 145
9892 214
1571 15
54064032 26650
Satellite: ISS
Catalog Number: 25544
Epoch time: 18349
17146463 = yrday
fracday
Element set: 909
Inclination: 51
6368 deg
RA of node: 196
7956 deg
Eccentricity:
0004824
Arg of perigee: 145
9892 deg
Mean anomaly: 214
1571 deg
Mean motion: 15
54064032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2665
Checksum: 337
Coasting Arc #11 (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 = 6427084
87 A = 6787508
94 meter
Y = -484099
11 meter E =
0017792
Z = 2096891
12 I = 51
57437
XDOT = 2176
335816 Wp = 120
09862
YDOT = 4865
859521 meter/sec RA = 190
64963 deg
ZDOT = -5520
927428 TA = 36
64124
MA = 36
51970
Ha = 222
267 n
mi
Hp = 213
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21086236
44 X = 6421834
91
Y = -1588251
68 feet Y = -412256
45 meter
Z = 6879564
03 Z = 2128098
96
XDOT = 7140
209371 XDOT = 2148
580475
YDOT = 15964
106039 feet/sec YDOT = 4890
041940 meter/sec
ZDOT = -18113
278963 ZDOT = -5510
422660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17732448
78 X = -5404850
39
Y = -11434951
63 feet Y = -3485373
26 meter
Z = 7020146
25 Z = 2139740
58
XDOT = 3013
404495 XDOT = 918
485690
YDOT = -15816
229956 feet/sec YDOT = -4820
786891 meter/sec
ZDOT = -18066
449995 ZDOT = -5506
653958
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
20032513
00016717 00000-0 10270-3 0 9101
2 25544 51
6366 191
6666 0004733 149
8991 210
2435 15
54088163 26817
Satellite: ISS
Catalog Number: 25544
Epoch time: 18350
20032513 = yrday
fracday
Element set: 910
Inclination: 51
6366 deg
RA of node: 191
6666 deg
Eccentricity:
0004733
Arg of perigee: 149
8991 deg
Mean anomaly: 210
2435 deg
Mean motion: 15
54088163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2681
Checksum: 302
Coasting Arc #12 (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 = -6764488
75 A = 6789294
35 meter
Y = -299836
82 meter E =
0010152
Z = -467790
40 I = 51
61312
XDOT = -194
366794 Wp = 67
93319
YDOT = -4784
079406 meter/sec RA = 185
67541 deg
ZDOT = 5984
980724 TA = 287
02235
MA = 287
13356
Ha = 222
258 n
mi
Hp = 213
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22193204
57 X = -6758360
85
Y = -983716
61 feet Y = -375447
75 meter
Z = -1534745
42 Z = -500635
25
XDOT = -637
686332 XDOT = -169
927461
YDOT = -15695
798576 feet/sec YDOT = -4786
116646 meter/sec
ZDOT = 19635
763529 ZDOT = 5984
095636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17332338
10 X = 5282896
65
Y = 13878769
66 feet Y = 4230248
99 meter
Z = -1682640
70 Z = -512868
89
XDOT = -7624
555991 XDOT = -2323
964666
YDOT = 11862
868354 feet/sec YDOT = 3615
802274 meter/sec
ZDOT = 19632
243646 ZDOT = 5983
907863
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
16488067
00016717 00000-0 10270-3 0 9117
2 25544 51
6365 186
8591 0004831 154
3390 205
8004 15
54100086 26969
Satellite: ISS
Catalog Number: 25544
Epoch time: 18351
16488067 = yrday
fracday
Element set: 911
Inclination: 51
6365 deg
RA of node: 186
8591 deg
Eccentricity:
0004831
Arg of perigee: 154
3390 deg
Mean anomaly: 205
8004 deg
Mean motion: 15
54100086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 310
Coasting Arc #13 (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 = 6578341
56 A = 6788801
17 meter
Y = 1073417
71 meter E =
0013655
Z = -1254204
43 I = 51
64590
XDOT = -1858
136129 Wp = 147
96134
YDOT = 4603
667355 meter/sec RA = 180
70465 deg
ZDOT = -5846
389535 TA = 45
67823
MA = 45
56636
Ha = 222
199 n
mi
Hp = 213
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21582485
43 X = 6571941
70
Y = 3521711
65 feet Y = 1146945
60 meter
Z = -4114843
94 Z = -1222264
35
XDOT = -6096
247143 XDOT = -1881
078629
YDOT = 15103
895522 feet/sec YDOT = 4582
760509 meter/sec
ZDOT = -19181
068029 ZDOT = -5855
471194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15638717
70 X = -4766681
15
Y = -15323155
55 feet Y = -4670497
81 meter
Z = -3971080
89 Z = -1210385
46
XDOT = 12458
928145 XDOT = 3797
481299
YDOT = -7769
572072 feet/sec YDOT = -2368
165567 meter/sec
ZDOT = -19222
423775 ZDOT = -5858
994767
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
19373712
00016717 00000-0 10270-3 0 9122
2 25544 51
6379 181
7298 0004629 158
2915 201
8435 15
54096143 27124
Satellite: ISS
Catalog Number: 25544
Epoch time: 18352
19373712 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 181
7298 deg
Eccentricity:
0004629
Arg of perigee: 158
2915 deg
Mean anomaly: 201
8435 deg
Mean motion: 15
54096143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 320
Coasting Arc #14 (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 = -5910762
94 A = 6786129
43 meter
Y = -1783985
95 meter E =
0014823
Z = 2806551
35 I = 51
66952
XDOT = 3742
596487 Wp = 98
10624
YDOT = -4327
551900 meter/sec RA = 175
73223 deg
ZDOT = 5106
188247 TA = 293
73250
MA = 293
88792
Ha = 222
124 n
mi
Hp = 214
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19392266
86 X = -5904007
48
Y = -5852972
29 feet Y = -1850046
69 meter
Z = 9207845
63 Z = 2777854
89
XDOT = 12278
859865 XDOT = 3765
906824
YDOT = -14198
004920 feet/sec YDOT = -4285
569700 meter/sec
ZDOT = 16752
586113 ZDOT = 5124
424891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12806793
54 X = 3903510
67
Y = 15769087
99 feet Y = 4806418
02 meter
Z = 9078745
67 Z = 2767201
68
XDOT = -16890
691289 XDOT = -5148
282705
YDOT = 3977
036751 feet/sec YDOT = 1212
200802 meter/sec
ZDOT = 16835
165138 ZDOT = 5131
358334
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
22259077
00016717 00000-0 10270-3 0 9135
2 25544 51
6372 176
6016 0004679 161
8651 198
2670 15
54113821 27280
Satellite: ISS
Catalog Number: 25544
Epoch time: 18353
22259077 = yrday
fracday
Element set: 913
Inclination: 51
6372 deg
RA of node: 176
6016 deg
Eccentricity:
0004679
Arg of perigee: 161
8651 deg
Mean anomaly: 198
2670 deg
Mean motion: 15
54113821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 319
Coasting Arc #15 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2018/354/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 949610
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2960818
37 A = 6778970
90 meter
Y = -3521886
03 meter E =
0010191
Z = 4975428
88 I = 51
67379
XDOT = 6841
374690 Wp = 141
11054
YDOT = -2749
678057 meter/sec RA = 171
20809 deg
ZDOT = 2114
737228 TA = 288
25910
MA = 288
36998
Ha = 222
086 n
mi
Hp = 214
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9713971
04 X = -2945383
84
Y = -11554744
20 feet Y = -3554910
21 meter
Z = 16323585
56 Z = 4961083
21
XDOT = 22445
455021 XDOT = 6861
341520
YDOT = -9021
253468 feet/sec YDOT = -2673
061640 meter/sec
ZDOT = 6938
114264 ZDOT = 2148
018769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6745242
78 X = -2055950
00
Y = 13581961
60 feet Y = 4139781
90 meter
Z = 16259299
23 Z = 4955834
40
XDOT = -16130
235825 XDOT = -4916
495879
YDOT = -16536
276018 feet/sec YDOT = -5040
256930 meter/sec
ZDOT = 7088
336674 ZDOT = 2160
525018
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
12283756
00016717 00000-0 10270-3 0 9147
2 25544 51
6354 172
1141 0004623 165
8324 194
2959 15
54104856 27420
Satellite: ISS
Catalog Number: 25544
Epoch time: 18354
12283756 = yrday
fracday
Element set: 914
Inclination: 51
6354 deg
RA of node: 172
1141 deg
Eccentricity:
0004623
Arg of perigee: 165
8324 deg
Mean anomaly: 194
2959 deg
Mean motion: 15
54104856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 311
Coasting Arc #16 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2018/355/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 949610
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1233462
05 A = 6777492
45 meter
Y = 4026357
70 meter E =
0016261
Z = -5323962
76 I = 51
70204
XDOT = -7391
410714 Wp = 104
70914
YDOT = 1987
680605 meter/sec RA = 166
21221 deg
ZDOT = -213
800579 TA = 163
27876
MA = 163
22508
Ha = 221
965 n
mi
Hp = 214
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4046791
50 X = 1214207
71
Y = 13209834
97 feet Y = 4040044
18 meter
Z = -17467069
43 Z = -5318017
22
XDOT = -24250
035150 XDOT = -7412
049631
YDOT = 6521
261829 feet/sec YDOT = 1904
909342 meter/sec
ZDOT = -701
445469 ZDOT = -249
755628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10340451
11 X = 3151769
50
Y = -9212629
54 feet Y = -2808009
48 meter
Z = -17440679
57 Z = -5315919
13
XDOT = 15216
342903 XDOT = 4637
941317
YDOT = 18685
721217 feet/sec YDOT = 5695
407827 meter/sec
ZDOT = -863
666481 ZDOT = -263
245543
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 18355
08738586
00016717 00000-0 10270-3 0 9150
2 25544 51
6360 167
3051 0004620 168
4042 191
7218 15
54090581 27571
Satellite: ISS
Catalog Number: 25544
Epoch time: 18355
08738586 = yrday
fracday
Element set: 915
Inclination: 51
6360 deg
RA of node: 167
3051 deg
Eccentricity:
0004620
Arg of perigee: 168
4042 deg
Mean anomaly: 191
7218 deg
Mean motion: 15
54090581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2757
Checksum: 315
Coasting Arc #17 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2018/356/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 949610
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 514616
31 A = 6778325
12 meter
Y = -4426259
22 meter E =
0004989
Z = 5103262
78 I = 51
73745
XDOT = 7400
162726 Wp = 108
67002
YDOT = -1099
940811 meter/sec RA = 161
21885 deg
ZDOT = -1700
460472 TA = 357
72487
MA = 357
72714
Ha = 221
847 n
mi
Hp = 214
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1688373
73 X = 539284
71
Y = -14521847
84 feet Y = -4420367
26 meter
Z = 16742988
13 Z = 5105821
87
XDOT = 24278
749101 XDOT = 7420
172541
YDOT = -3608
729695 feet/sec YDOT = -1017
074913 meter/sec
ZDOT = -5578
938555 ZDOT = -1664
464494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13810751
42 X = -4209517
03
Y = 4753576
70 feet Y = 1448890
18 meter
Z = 16754968
69 Z = 5106914
46
XDOT = -13268
466932 XDOT = -4044
228721
YDOT = -19459
819828 feet/sec YDOT = -5931
353084 meter/sec
ZDOT = -5416
591956 ZDOT = -1650
977228
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 18356
11623433
00016717 00000-0 10270-3 0 9160
2 25544 51
6364 162
1763 0004499 172
4744 187
6476 15
54101463 27736
Satellite: ISS
Catalog Number: 25544
Epoch time: 18356
11623433 = yrday
fracday
Element set: 916
Inclination: 51
6364 deg
RA of node: 162
1763 deg
Eccentricity:
0004499
Arg of perigee: 172
4744 deg
Mean anomaly: 187
6476 deg
Mean motion: 15
54101463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 320
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