[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 4th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25144 4947 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
337/19:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
0
338/16:07:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
9
338/18:38:53
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
340/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
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
Coasting Arc #1 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/18:47:57
545
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3981248
75 A = 6785659
98 meter
Y = -4596833
21 meter E =
0009210
Z = -3019215
91 I = 51
27801
XDOT = 2451
087787 Wp = 92
84098
YDOT = -5341
428593 meter/sec RA = 252
56224 deg
ZDOT = 4912
944681 TA = 232
41035
MA = 232
49401
Ha = 222
986 n
mi
Hp = 212
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13061839
72 X = -3914883
78
Y = -15081473
78 feet Y = -4640983
08 meter
Z = -9905564
01 Z = -3038394
79
XDOT = 8041
626598 XDOT = 2486
770078
YDOT = -17524
372024 feet/sec YDOT = -5313
819552 meter/sec
ZDOT = 16118
584913 ZDOT = 4924
937822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11249244
51 X = -3428769
73
Y = -16425946
72 feet Y = -5006628
56 meter
Z = -9991270
15 Z = -3045339
14
XDOT = 8624
074623 XDOT = 2628
617945
YDOT = -15718
766825 feet/sec YDOT = -4791
080128 meter/sec
ZDOT = 16173
124645 ZDOT = 4929
568392
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 18337
78954911
00016717 00000-0 10270-3 0 9003
2 25544 51
6369 253
5258 0005252 110
7148 249
4568 15
54038067 24887
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78954911 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 253
5258 deg
Eccentricity:
0005252
Arg of perigee: 110
7148 deg
Mean anomaly: 249
4568 deg
Mean motion: 15
54038067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 334
Coasting Arc #2 (Orbit 2488)
---------------------------------------
Vector Time (GMT): 2018/337/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4430218
96 A = 6782366
34 meter
Y = 3057714
47 meter E =
0014989
Z = 4113382
43 I = 51
26674
XDOT = -1064
226931 Wp = 87
90187
YDOT = 6608
873757 meter/sec RA = 252
41456 deg
ZDOT = -3754
144626 TA = 40
98791
MA = 40
87535
Ha = 222
925 n
mi
Hp = 213
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14534839
12 X = 4375716
51
Y = 10031871
64 feet Y = 3106951
32 meter
Z = 13495349
18 Z = 4134771
02
XDOT = -3491
558174 XDOT = -1119
814155
YDOT = 21682
656684 feet/sec YDOT = 6596
662208 meter/sec
ZDOT = -12316
747462 ZDOT = -3759
449048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15139708
25 X = 4614583
08
Y = 8949515
24 feet Y = 2727812
25 meter
Z = 13591168
35 Z = 4142588
11
XDOT = -1161
823787 XDOT = -354
123890
YDOT = 20769
027862 feet/sec YDOT = 6330
399692 meter/sec
ZDOT = -12341
357967 ZDOT = -3761
645908
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 18337
85385544
00016717 00000-0 10270-3 0 9012
2 25544 51
6366 253
2048 0005281 111
8010 248
3705 15
54015814 24897
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
85385544 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 253
2048 deg
Eccentricity:
0005281
Arg of perigee: 111
8010 deg
Mean anomaly: 248
3705 deg
Mean motion: 15
54015814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2489
Checksum: 303
Coasting Arc #3 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2018/338/16:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3328826
66 A = 6778110
99 meter
Y = 2862836
03 meter E =
0018437
Z = -5180034
84 I = 51
26516
XDOT = -3715
779543 Wp = 88
11363
YDOT = -6574
714453 meter/sec RA = 248
15032 deg
ZDOT = -1249
044580 TA = 169
83050
MA = 169
79315
Ha = 222
846 n
mi
Hp = 212
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10921347
32 X = -3335429
97
Y = 9392506
67 feet Y = 2825574
19 meter
Z = -16994864
97 Z = -5196221
27
XDOT = -12190
877765 XDOT = -3635
915775
YDOT = -21570
585476 feet/sec YDOT = -6615
820256 meter/sec
ZDOT = -4097
915289 ZDOT = -1266
901314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14269415
44 X = -4349317
82
Y = -1178327
33 feet Y = -359154
17 meter
Z = -17067975
04 Z = -5202318
79
XDOT = 6860
867270 XDOT = 2091
192344
YDOT = -22729
006760 feet/sec YDOT = -6927
801261 meter/sec
ZDOT = -4177
461854 ZDOT = -1273
290373
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 18338
68982733
00016717 00000-0 10270-3 0 9028
2 25544 51
6397 249
0414 0004903 110
4770 249
6909 15
54054624 25027
Satellite: ISS
Catalog Number: 25544
Epoch time: 18338
68982733 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 249
0414 deg
Eccentricity:
0004903
Arg of perigee: 110
4770 deg
Mean anomaly: 249
6909 deg
Mean motion: 15
54054624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 319
Coasting Arc #4 (Orbit 2503)
---------------------------------------
Vector Time (GMT): 2018/338/18:38:53
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4674457
80 A = 6782239
43 meter
Y = 2630011
33 meter E =
0014644
Z = 4138649
87 I = 51
27790
XDOT = -463
853166 Wp = 88
20230
YDOT = 6696
971937 meter/sec RA = 247
58331 deg
ZDOT = -3719
980914 TA = 40
25999
MA = 40
15163
Ha = 222
834 n
mi
Hp = 213
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15336147
65 X = 4624597
13
Y = 8628646
10 feet Y = 2682005
30 meter
Z = 13578247
60 Z = 4161236
24
XDOT = -1521
827971 XDOT = -520
636082
YDOT = 21971
692706 feet/sec YDOT = 6691
467564 meter/sec
ZDOT = -12204
661790 ZDOT = -3722
371662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13963768
44 X = 4256156
62
Y = 10578463
73 feet Y = 3224315
74 meter
Z = 13679511
77 Z = 4169515
19
XDOT = -3575
031491 XDOT = -1089
669598
YDOT = 20566
432731 feet/sec YDOT = 6268
648696 meter/sec
ZDOT = -12216
173430 ZDOT = -3723
489662
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 18338
81843956
00016717 00000-0 10270-3 0 9037
2 25544 51
6375 248
3972 0005137 114
3353 245
8337 15
54026647 25043
Satellite: ISS
Catalog Number: 25544
Epoch time: 18338
81843956 = yrday
fracday
Element set: 903
Inclination: 51
6375 deg
RA of node: 248
3972 deg
Eccentricity:
0005137
Arg of perigee: 114
3353 deg
Mean anomaly: 245
8337 deg
Mean motion: 15
54026647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2504
Checksum: 324
Coasting Arc #5 (Orbit 2518)
---------------------------------------
Vector Time (GMT): 2018/339/18:38:53
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4685059
67 A = 6785868
06 meter
Y = -3953984
64 meter E =
0009010
Z = -2918083
82 I = 51
30437
XDOT = 1609
174386 Wp = 94
52670
YDOT = -5581
994694 meter/sec RA = 242
57589 deg
ZDOT = 4992
666948 TA = 232
06032
MA = 232
14178
Ha = 222
974 n
mi
Hp = 212
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15370930
68 X = -4626322
15
Y = -12972390
57 feet Y = -4006047
56 meter
Z = -9573765
82 Z = -2940700
29
XDOT = 5279
443522 XDOT = 1647
222059
YDOT = -18313
630886 feet/sec YDOT = -5563
787487 meter/sec
ZDOT = 16380
140907 ZDOT = 5000
575818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13701845
48 X = -4176322
50
Y = -14658058
15 feet Y = -4467776
12 meter
Z = -9675028
74 Z = -2948948
76
XDOT = 6186
672336 XDOT = 1885
697728
YDOT = -16591
510234 feet/sec YDOT = -5057
092319 meter/sec
ZDOT = 16416
335161 ZDOT = 5003
698957
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
78302215
00016717 00000-0 10270-3 0 9043
2 25544 51
6379 243
5892 0005392 117
2838 242
8864 15
54050543 25198
Satellite: ISS
Catalog Number: 25544
Epoch time: 18339
78302215 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 243
5892 deg
Eccentricity:
0005392
Arg of perigee: 117
2838 deg
Mean anomaly: 242
8864 deg
Mean motion: 15
54050543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2519
Checksum: 325
Coasting Arc #6 (Orbit 2529)
---------------------------------------
Vector Time (GMT): 2018/340/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3399945
74 A = 6789598
02 meter
Y = 5867750
45 meter E =
0016869
Z = -106116
04 I = 51
32983
XDOT = -4189
192682 Wp = 129
80138
YDOT = 2330
726605 meter/sec RA = 239
19323 deg
ZDOT = -5987
484950 TA = 51
34686
MA = 51
19601
Ha = 222
918 n
mi
Hp = 213
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11154677
64 X = 3334593
69
Y = 19251149
76 feet Y = 5905405
61 meter
Z = -348149
73 Z = -89758
16
XDOT = -13744
070478 XDOT = -4185
859666
YDOT = 7646
740829 feet/sec YDOT = 2283
899382 meter/sec
ZDOT = -19643
979495 ZDOT = -6007
826589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22249136
07 X = -6781536
67
Y = -234514
66 feet Y = -71480
07 meter
Z = -275237
14 Z = -83892
28
XDOT = 358
439345 XDOT = 109
252313
YDOT = -13985
841820 feet/sec YDOT = -4262
884587 meter/sec
ZDOT = -19735
723634 ZDOT = -6015
448564
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
49038195
00016717 00000-0 10270-3 0 9057
2 25544 51
6404 240
0680 0005115 116
4823 243
6855 15
54035580 25308
Satellite: ISS
Catalog Number: 25544
Epoch time: 18340
49038195 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 240
0680 deg
Eccentricity:
0005115
Arg of perigee: 116
4823 deg
Mean anomaly: 243
6855 deg
Mean motion: 15
54035580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2530
Checksum: 289
Coasting Arc #7 (Orbit 2545)
---------------------------------------
Vector Time (GMT): 2018/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2619009
36 A = 6788326
35 meter
Y = -6009728
69 meter E =
0017326
Z = 1738975
70 I = 51
34315
XDOT = 5147
720349 Wp = 78
63606
YDOT = -594
344353 meter/sec RA = 234
20197 deg
ZDOT = 5654
201354 TA = 300
53173
MA = 300
70263
Ha = 222
860 n
mi
Hp = 213
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8592550
40 X = -2560059
38
Y = -19716957
63 feet Y = -6038686
86 meter
Z = 5705300
86 Z = 1726395
77
XDOT = 16888
846290 XDOT = 5126
518403
YDOT = -1949
948664 feet/sec YDOT = -536
898178 meter/sec
ZDOT = 18550
529375 ZDOT = 5679
155955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21401919
53 X = 6523305
07
Y = 2276650
53 feet Y = 693923
08 meter
Z = 5649380
62 Z = 1721931
21
XDOT = -6450
992278 XDOT = -1966
262446
YDOT = 13965
815871 feet/sec YDOT = 4256
780678 meter/sec
ZDOT = 18662
838663 ZDOT = 5688
433224
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
51926661
00016717 00000-0 10270-3 0 9066
2 25544 51
6400 234
9401 0005024 119
8094 240
3559 15
54042750 25462
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
51926661 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 234
9401 deg
Eccentricity:
0005024
Arg of perigee: 119
8094 deg
Mean anomaly: 240
3559 deg
Mean motion: 15
54042750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2546
Checksum: 292
Coasting Arc #8 (Orbit 2560)
---------------------------------------
Vector Time (GMT): 2018/342/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1537350
69 A = 6785087
98 meter
Y = 5757160
76 meter E =
0009327
Z = -3248506
63 I = 51
35379
XDOT = -5929
358066 Wp = 111
71025
YDOT = -1078
823212 meter/sec RA = 229
20576 deg
ZDOT = -4732
352635 TA = 106
08579
MA = 105
98307
Ha = 222
779 n
mi
Hp = 213
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5043801
48 X = 1488637
92
Y = 18888322
70 feet Y = 5774080
52 meter
Z = -10657830
17 Z = -3241156
24
XDOT = -19453
274494 XDOT = -5893
866198
YDOT = -3539
446234 feet/sec YDOT = -1144
930367 meter/sec
ZDOT = -15526
091321 ZDOT = -4761
069601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19021207
14 X = -5797663
94
Y = -4592683
67 feet Y = -1399849
98 meter
Z = -10625391
63 Z = -3238619
37
XDOT = 12069
831524 XDOT = 3678
884649
YDOT = -13879
112453 feet/sec YDOT = -4230
353476 meter/sec
ZDOT = -15655
157518 ZDOT = -4771
692011
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
48384185
00016717 00000-0 10270-3 0 9073
2 25544 51
6410 230
1325 0004957 123
5604 236
6023 15
54057395 25611
Satellite: ISS
Catalog Number: 25544
Epoch time: 18342
48384185 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 230
1325 deg
Eccentricity:
0004957
Arg of perigee: 123
5604 deg
Mean anomaly: 236
6023 deg
Mean motion: 15
54057395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2561
Checksum: 298
Coasting Arc #9 (Orbit 2576)
---------------------------------------
Vector Time (GMT): 2018/343/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -280541
46 A = 6781405
01 meter
Y = -5160248
95 meter E =
0014379
Z = 4383293
64 I = 51
36294
XDOT = 6427
403899 Wp = 115
36447
YDOT = 2511
531734 meter/sec RA = 224
20108 deg
ZDOT = 3353
401014 TA = 300
53963
MA = 300
68146
Ha = 222
802 n
mi
Hp = 213
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -920411
61 X = -244109
10
Y = -16929950
62 feet Y = -5163183
01 meter
Z = 14380884
63 Z = 4382018
68
XDOT = 21087
283133 XDOT = 6382
552414
YDOT = 8239
933509 feet/sec YDOT = 2583
156221 meter/sec
ZDOT = 11001
971830 ZDOT = 3384
514664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15456127
99 X = 4711027
81
Y = 6980508
92 feet Y = 2127659
12 meter
Z = 14375702
80 Z = 4381714
21
XDOT = -16565
801605 XDOT = -5049
256329
YDOT = 13635
253235 feet/sec YDOT = 4156
025186 meter/sec
ZDOT = 11141
687139 ZDOT = 3395
986240
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
51272176
00016717 00000-0 10270-3 0 9085
2 25544 51
6401 225
0042 0005053 125
9720 234
1902 15
54050590 25779
Satellite: ISS
Catalog Number: 25544
Epoch time: 18343
51272176 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 225
0042 deg
Eccentricity:
0005053
Arg of perigee: 125
9720 deg
Mean anomaly: 234
1902 deg
Mean motion: 15
54050590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2577
Checksum: 278
Coasting Arc #10 (Orbit 2591)
---------------------------------------
Vector Time (GMT): 2018/344/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1169048
97 A = 6778392
83 meter
Y = 4314423
23 meter E =
0016855
Z = -5110188
14 I = 51
37770
XDOT = -6526
905649 Wp = 91
29861
YDOT = -3665
288054 meter/sec RA = 219
18880 deg
ZDOT = -1606
353156 TA = 163
15123
MA = 163
09518
Ha = 222
631 n
mi
Hp = 213
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3835462
51 X = -1192384
54
Y = 14154931
87 feet Y = 4301220
26 meter
Z = -16765709
13 Z = -5115923
14
XDOT = -21413
732443 XDOT = -6477
631451
YDOT = -12025
223274 feet/sec YDOT = -3738
000743 meter/sec
ZDOT = -5270
187521 ZDOT = -1637
939427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10962037
31 X = -3341228
97
Y = -9696663
93 feet Y = -2955543
16 meter
Z = -16791971
84 Z = -5118193
02
XDOT = 19655
077491 XDOT = 5990
867619
YDOT = -12876
229163 feet/sec YDOT = -3924
674649 meter/sec
ZDOT = -5411
931941 ZDOT = -1649
556856
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
47729406
00016717 00000-0 10270-3 0 9095
2 25544 51
6400 220
1968 0004880 130
6423 229
5155 15
54081757 25925
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
47729406 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 220
1968 deg
Eccentricity:
0004880
Arg of perigee: 130
6423 deg
Mean anomaly: 229
5155 deg
Mean motion: 15
54081757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2592
Checksum: 314
Coasting Arc #11 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2018/344/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4032968
39 A = 6787771
39 meter
Y = 5051376
41 meter E =
0011769
Z = -2060559
16 I = 51
42049
XDOT = -5015
254621 Wp = 138
31555
YDOT = 1761
208050 meter/sec RA = 216
66472 deg
ZDOT = -5525
240022 TA = 64
54691
MA = 64
42519
Ha = 222
730 n
mi
Hp = 213
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13231523
58 X = 3986191
86
Y = 16572757
24 feet Y = 5096214
56 meter
Z = -6760364
70 Z = -2041081
41
XDOT = -16454
247445 XDOT = -5007
737494
YDOT = 5778
241634 feet/sec YDOT = 1705
166667 meter/sec
ZDOT = -18127
427894 ZDOT = -5549
583934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20574970
70 X = 6271251
07
Y = -5250757
13 feet Y = -1600430
77 meter
Z = -6673242
09 Z = -2034004
19
XDOT = -1863
932750 XDOT = -568
126702
YDOT = 15760
772396 feet/sec YDOT = 4803
883426 meter/sec
ZDOT = -18237
163376 ZDOT = -5558
687397
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
99173198
00016717 00000-0 10270-3 0 9105
2 25544 51
6385 217
6301 0005137 135
9591 224
1972 15
54059547 26009
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
99173198 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 217
6301 deg
Eccentricity:
0005137
Arg of perigee: 135
9591 deg
Mean anomaly: 224
1972 deg
Mean motion: 15
54059547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 318
Coasting Arc #12 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2018/345/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2902901
08 A = 6784414
07 meter
Y = -5045894
92 meter E =
0016172
Z = 3474799
29 I = 51
43707
XDOT = 6179
894872 Wp = 104
64739
YDOT = -425
066934 meter/sec RA = 211
67196 deg
ZDOT = 4523
842922 TA = 296
30933
MA = 296
47536
Ha = 222
657 n
mi
Hp = 213
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9523953
66 X = -2863139
43
Y = -16554773
36 feet Y = -5078135
22 meter
Z = 11400260
15 Z = 3460794
07
XDOT = 20275
245643 XDOT = 6162
214387
YDOT = -1394
576556 feet/sec YDOT = -356
058389 meter/sec
ZDOT = 14842
004336 ZDOT = 4553
819670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19004836
49 X = -5792674
16
Y = 2236926
59 feet Y = 681815
23 meter
Z = 11337746
47 Z = 3455745
12
XDOT = 6895
994534 XDOT = 2101
899134
YDOT = -17684
394154 feet/sec YDOT = -5390
203338 meter/sec
ZDOT = 14976
966546 ZDOT = 4564
979403
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
02060527
00016717 00000-0 10270-3 0 9113
2 25544 51
6389 212
5013 0005071 138
8052 221
3484 15
54077997 26161
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
02060527 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 212
5013 deg
Eccentricity:
0005071
Arg of perigee: 138
8052 deg
Mean anomaly: 221
3484 deg
Mean motion: 15
54077997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 298
Coasting Arc #13 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2018/346/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1434508
50 A = 6780706
79 meter
Y = 4802300
56 meter E =
0012561
Z = -4577615
60 I = 51
45263
XDOT = -6985
408314 Wp = 92
93221
YDOT = -800
891701 meter/sec RA = 206
67172 deg
ZDOT = -3037
104492 TA = 146
64186
MA = 146
56265
Ha = 222
635 n
mi
Hp = 213
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4706392
73 X = 1402936
80
Y = 15755579
28 feet Y = 4818166
13 meter
Z = -15018423
89 Z = -4570723
52
XDOT = -22918
006279 XDOT = -6961
180738
YDOT = -2627
597444 feet/sec YDOT = -878
871649 meter/sec
ZDOT = -9964
253583 ZDOT = -3070
978326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16397004
38 X = 4997806
93
Y = 1562991
40 feet Y = 476399
78 meter
Z = -14987887
52 Z = -4568308
12
XDOT = -11027
848064 XDOT = -3361
288090
YDOT = 18927
402053 feet/sec YDOT = 5769
072146 meter/sec
ZDOT = -10116
651347 ZDOT = -3083
555330
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
98517487
00016717 00000-0 10270-3 0 9121
2 25544 51
6382 207
6937 0005116 141
2995 218
8525 15
54056371 26315
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
98517487 = yrday
fracday
Element set: 912
Inclination: 51
6382 deg
RA of node: 207
6937 deg
Eccentricity:
0005116
Arg of perigee: 141
2995 deg
Mean anomaly: 218
8525 deg
Mean motion: 15
54056371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 330
Coasting Arc #14 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2018/347/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 189616
29 A = 6778067
04 meter
Y = -4362320
23 meter E =
0009169
Z = 5179984
24 I = 51
47411
XDOT = 7342
023195 Wp = 136
20123
YDOT = 1831
851940 meter/sec RA = 201
66469 deg
ZDOT = 1266
098909 TA = 301
57672
MA = 301
66620
Ha = 222
516 n
mi
Hp = 213
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 622100
69 X = 213221
31
Y = -14312074
26 feet Y = -4360068
23 meter
Z = 16994698
96 Z = 5180962
33
XDOT = 24088
002607 XDOT = 7314
843214
YDOT = 6010
012925 feet/sec YDOT = 1913
803477 meter/sec
ZDOT = 4153
867811 ZDOT = 1301
697960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13135978
73 X = -4003846
32
Y = -5701229
55 feet Y = -1737734
77 meter
Z = 16999538
70 Z = 5181459
40
XDOT = 13968
085398 XDOT = 4257
472429
YDOT = -19243
647240 feet/sec YDOT = -5865
463679 meter/sec
ZDOT = 4313
950431 ZDOT = 1314
892091
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
01404561
00016717 00000-0 10270-3 0 9136
2 25544 51
6381 202
5653 0005031 145
3550 214
7931 15
54078589 26479
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
01404561 = yrday
fracday
Element set: 913
Inclination: 51
6381 deg
RA of node: 202
5653 deg
Eccentricity:
0005031
Arg of perigee: 145
3550 deg
Mean anomaly: 214
7931 deg
Mean motion: 15
54078589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 299
Coasting Arc #15 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2018/348/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4416428
65 A = 6780328
69 meter
Y = -2259708
36 meter E =
0010313
Z = 4612709
63 I = 51
48595
XDOT = 5423
143606 Wp = 92
73996
YDOT = 4555
235867 meter/sec RA = 200
63187 deg
ZDOT = -2955
593277 TA = 26
77190
MA = 26
71871
Ha = 222
366 n
mi
Hp = 213
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14489595
29 X = 4418963
04
Y = -7413741
35 feet Y = -2210306
96 meter
Z = 15133561
78 Z = 4634169
06
XDOT = 17792
465900 XDOT = 5386
159308
YDOT = 14944
999563 feet/sec YDOT = 4615
674657 meter/sec
ZDOT = -9696
828335 ZDOT = -2929
339066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15840803
79 X = -4828277
00
Y = -3322723
74 feet Y = -1012766
20 meter
Z = 15230399
44 Z = 4642225
75
XDOT = -4673
711423 XDOT = -1424
547242
YDOT = -21704
377080 feet/sec YDOT = -6615
494134 meter/sec
ZDOT = -9579
084051 ZDOT = -2919
704819
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
20695937
00016717 00000-0 10270-3 0 9147
2 25544 51
6360 201
6041 0004871 144
0598 216
0883 15
54073591 26509
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
20695937 = yrday
fracday
Element set: 914
Inclination: 51
6360 deg
RA of node: 201
6041 deg
Eccentricity:
0004871
Arg of perigee: 144
0598 deg
Mean anomaly: 216
0883 deg
Mean motion: 15
54073591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 310
Coasting Arc #16 (Orbit 2664)
---------------------------------------
Vector Time (GMT): 2018/349/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5609846
33 A = 6784037
51 meter
Y = 1375373
60 meter E =
0009303
Z = -3569747
64 I = 51
53057
XDOT = -3998
993944 Wp = 120
92513
YDOT = -4786
164419 meter/sec RA = 195
63518 deg
ZDOT = 4444
304918 TA = 196
89332
MA = 196
92432
Ha = 222
464 n
mi
Hp = 213
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18405007
63 X = -5607469
26
Y = 4512380
58 feet Y = 1312653
91 meter
Z = -11711770
48 Z = -3596992
46
XDOT = -13120
058870 XDOT = -3966
764581
YDOT = -15702
639171 feet/sec YDOT = -4830
704023 meter/sec
ZDOT = 14581
052882 ZDOT = 4424
957178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17203150
41 X = 5243520
25
Y = 7763104
18 feet Y = 2366194
16 meter
Z = -11834579
89 Z = -3607179
95
XDOT = 1272
327750 XDOT = 387
805498
YDOT = 19257
212700 feet/sec YDOT = 5869
598431 meter/sec
ZDOT = 14494
408823 ZDOT = 4417
895809
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
17152376
00016717 00000-0 10270-3 0 9150
2 25544 51
6370 196
7962 0004820 145
9783 214
1679 15
54053927 26655
Satellite: ISS
Catalog Number: 25544
Epoch time: 18349
17152376 = yrday
fracday
Element set: 915
Inclination: 51
6370 deg
RA of node: 196
7962 deg
Eccentricity:
0004820
Arg of perigee: 145
9783 deg
Mean anomaly: 214
1679 deg
Mean motion: 15
54053927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2665
Checksum: 339
Coasting Arc #17 (Orbit 2680)
---------------------------------------
Vector Time (GMT): 2018/350/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6414653
78 A = 6787481
51 meter
Y = -511570
58 meter E =
0017761
Z = 2128156
94 I = 51
57430
XDOT = 2222
886862 Wp = 119
75865
YDOT = 4862
253922 meter/sec RA = 190
65061 deg
ZDOT = -5505
535939 TA = 36
61341
MA = 36
49215
Ha = 222
281 n
mi
Hp = 213
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21045452
04 X = 6409560
07
Y = -1678381
16 feet Y = -439866
06 meter
Z = 6982142
19 Z = 2159304
78
XDOT = 7292
935899 XDOT = 2195
093616
YDOT = 15952
276647 feet/sec YDOT = 4886
956695 meter/sec
ZDOT = -18062
781952 ZDOT = -5494
805134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17753791
07 X = -5411355
52
Y = -11338070
18 feet Y = -3455843
79 meter
Z = 7122456
87 Z = 2170924
85
XDOT = 2891
840922 XDOT = 881
433113
YDOT = -15897
234050 feet/sec YDOT = -4845
476939 meter/sec
ZDOT = -18014
934744 ZDOT = -5490
952110
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
20039097
00016717 00000-0 10270-3 0 9161
2 25544 51
6368 191
6673 0004729 149
8742 210
2684 15
54077958 26812
Satellite: ISS
Catalog Number: 25544
Epoch time: 18350
20039097 = yrday
fracday
Element set: 916
Inclination: 51
6368 deg
RA of node: 191
6673 deg
Eccentricity:
0004729
Arg of perigee: 149
8742 deg
Mean anomaly: 210
2684 deg
Mean motion: 15
54077958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2681
Checksum: 337
Coasting Arc #18 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2018/351/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6763130
03 A = 6789308
53 meter
Y = -270083
59 meter E =
0010053
Z = -505135
29 I = 51
61318
XDOT = -248
179485 Wp = 67
87530
YDOT = -4786
333050 meter/sec RA = 185
67636 deg
ZDOT = 5981
092174 TA = 286
67642
MA = 286
78674
Ha = 222
274 n
mi
Hp = 213
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22188746
82 X = -6757153
54
Y = -886101
01 feet Y = -345680
17 meter
Z = -1657268
00 Z = -537973
90
XDOT = -814
237154 XDOT = -223
692063
YDOT = -15703
192421 feet/sec YDOT = -4788
971792 meter/sec
ZDOT = 19623
005820 ZDOT = 5979
945798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17385651
72 X = 5299146
64
Y = 13796839
79 feet Y = 4205276
77 meter
Z = -1805138
10 Z = -550206
09
XDOT = -7492
396918 XDOT = -2283
682581
YDOT = 11969
037899 feet/sec YDOT = 3648
162752 meter/sec
ZDOT = 19618
309384 ZDOT = 5979
660700
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
16495290
00016717 00000-0 10270-3 0 9179
2 25544 51
6366 186
8598 0004826 154
2972 205
8421 15
54089394 26967
Satellite: ISS
Catalog Number: 25544
Epoch time: 18351
16495290 = yrday
fracday
Element set: 917
Inclination: 51
6366 deg
RA of node: 186
8598 deg
Eccentricity:
0004826
Arg of perigee: 154
2972 deg
Mean anomaly: 205
8421 deg
Mean motion: 15
54089394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 350
Coasting Arc #19 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2018/352/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6590837
88 A = 6788873
06 meter
Y = 1042092
36 meter E =
0013767
Z = -1214285
47 I = 51
64615
XDOT = -1800
741908 Wp = 147
83656
YDOT = 4612
843032 meter/sec RA = 180
70568 deg
ZDOT = -5857
186425 TA = 45
36089
MA = 45
24873
Ha = 222
215 n
mi
Hp = 213
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21623483
84 X = 6584593
47
Y = 3418938
20 feet Y = 1115760
86 meter
Z = -3983876
21 Z = -1182284
31
XDOT = -5907
945891 XDOT = -1823
738832
YDOT = 15133
999448 feet/sec YDOT = 4592
577704 meter/sec
ZDOT = -19216
490897 ZDOT = -5865
989412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15730699
38 X = -4794717
17
Y = -15262248
39 feet Y = -4651933
31 meter
Z = -3839835
00 Z = -1170381
71
XDOT = 12326
570465 XDOT = 3757
138678
YDOT = -7896
044632 feet/sec YDOT = -2406
714404 meter/sec
ZDOT = -19256
592314 ZDOT = -5869
409337
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
19381628
00016717 00000-0 10270-3 0 9183
2 25544 51
6381 181
7307 0004626 158
2758 201
8591 15
54085355 27126
Satellite: ISS
Catalog Number: 25544
Epoch time: 18352
19381628 = yrday
fracday
Element set: 918
Inclination: 51
6381 deg
RA of node: 181
7307 deg
Eccentricity:
0004626
Arg of perigee: 158
2758 deg
Mean anomaly: 201
8591 deg
Mean motion: 15
54085355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 323
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