[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 28th 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
337/11:31:53
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
0
337/17:35:42
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
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
0 213
0
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
Coasting Arc #1 (Orbit 2405)
---------------------------------------
Vector Time (GMT): 2018/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4235797
98 A = 6777691
83 meter
Y = -415797
42 meter E =
0019988
Z = -5292072
66 I = 51
24295
XDOT = 1025
910604 Wp = 88
65641
YDOT = -7581
068725 meter/sec RA = 279
06439 deg
ZDOT = -225
782251 TA = 179
17719
MA = 179
17389
Ha = 223
049 n
mi
Hp = 212
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13896974
98 X = -4205127
40
Y = -1364164
77 feet Y = -462993
15 meter
Z = -17362443
12 Z = -5312574
33
XDOT = 3365
848437 XDOT = 1111
704721
YDOT = -24872
272721 feet/sec YDOT = -7569
116558 meter/sec
ZDOT = -740
755417 ZDOT = -220
590934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6756151
91 X = 2059275
10
Y = -12088597
63 feet Y = -3684604
56 meter
Z = -17454555
54 Z = -5320148
53
XDOT = 20574
378550 XDOT = 6271
070582
YDOT = 12531
885574 feet/sec YDOT = 3819
718723 meter/sec
ZDOT = -716
453982 ZDOT = -218
375174
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 18332
51648093
00016717 00000-0 10270-3 0 9000
2 25544 51
6394 279
8120 0005142 90
0655 270
1087 15
54020670 24063
Satellite: ISS
Catalog Number: 25544
Epoch time: 18332
51648093 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 279
8120 deg
Eccentricity:
0005142
Arg of perigee: 90
0655 deg
Mean anomaly: 270
1087 deg
Mean motion: 15
54020670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2406
Checksum: 287
Coasting Arc #2 (Orbit 2421)
---------------------------------------
Vector Time (GMT): 2018/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3930218
61 A = 6778571
41 meter
Y = 2165281
07 meter E =
0009772
Z = 5073250
44 I = 51
24136
XDOT = -1849
467863 Wp = 74
07743
YDOT = 7260
949280 meter/sec RA = 274
03907 deg
ZDOT = -1660
915015 TA = 32
06511
MA = 32
00570
Ha = 222
933 n
mi
Hp = 212
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12894418
03 X = 3881070
46
Y = 7103940
53 feet Y = 2208956
41 meter
Z = 16644522
46 Z = 5092222
91
XDOT = -6067
807949 XDOT = -1922
456491
YDOT = 23822
012072 feet/sec YDOT = 7239
859235 meter/sec
ZDOT = -5449
196245 ZDOT = -1670
075987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11465145
33 X = -3494576
30
Y = 9079912
54 feet Y = 2767557
34 meter
Z = 16729547
09 Z = 5099165
95
XDOT = -19023
702094 XDOT = -5798
424398
YDOT = -13871
585731 feet/sec YDOT = -4228
059331 meter/sec
ZDOT = -5491
283660 ZDOT = -1673
743260
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 18333
54537890
00016717 00000-0 10270-3 0 9017
2 25544 51
6389 274
6845 0005219 92
9609 267
2141 15
54025786 24228
Satellite: ISS
Catalog Number: 25544
Epoch time: 18333
54537890 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 274
6845 deg
Eccentricity:
0005219
Arg of perigee: 92
9609 deg
Mean anomaly: 267
2141 deg
Mean motion: 15
54025786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2422
Checksum: 329
Coasting Arc #3 (Orbit 2436)
---------------------------------------
Vector Time (GMT): 2018/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3576425
28 A = 6781449
42 meter
Y = -3765447
80 meter E =
0013989
Z = -4374994
40 I = 51
24946
XDOT = 2593
409987 Wp = 105
59210
YDOT = -6368
801130 meter/sec RA = 269
01807 deg
ZDOT = 3366
771265 TA = 198
70379
MA = 198
75525
Ha = 223
016 n
mi
Hp = 212
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11733678
72 X = -3512801
64
Y = -12353831
37 feet Y = -3805085
96 meter
Z = -14353656
16 Z = -4392213
15
XDOT = 8508
562950 XDOT = 2648
080859
YDOT = -20895
016832 feet/sec YDOT = -6339
494267 meter/sec
ZDOT = 11045
837482 ZDOT = 3379
501761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15768205
53 X = 4806149
04
Y = -6280525
21 feet Y = -1914304
08 meter
Z = -14430610
13 Z = -4398449
97
XDOT = 15871
922222 XDOT = 4837
761893
YDOT = 14375
842874 feet/sec YDOT = 4381
756908 meter/sec
ZDOT = 11103
845887 ZDOT = 3384
452226
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 18334
50996899
00016717 00000-0 10270-3 0 9023
2 25544 51
6387 269
8768 0005118 96
9090 263
2645 15
54024789 24375
Satellite: ISS
Catalog Number: 25544
Epoch time: 18334
50996899 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 269
8768 deg
Eccentricity:
0005118
Arg of perigee: 96
9090 deg
Mean anomaly: 263
2645 deg
Mean motion: 15
54024789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2437
Checksum: 362
Coasting Arc #4 (Orbit 2452)
---------------------------------------
Vector Time (GMT): 2018/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3114234
28 A = 6785183
50 meter
Y = 5099728
83 meter E =
0017854
Z = 3197212
32 I = 51
26471
XDOT = -3313
752276 Wp = 95
14617
YDOT = 5022
679784 meter/sec RA = 264
00614 deg
ZDOT = -4762
267203 TA = 47
63919
MA = 47
48816
Ha = 222
917 n
mi
Hp = 212
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10217304
06 X = 3041445
71
Y = 16731393
79 feet Y = 5134147
27 meter
Z = 10489541
75 Z = 3212163
70
XDOT = -10871
890669 XDOT = -3346
538204
YDOT = 16478
608214 feet/sec YDOT = 4985
439933 meter/sec
ZDOT = -15624
236231 ZDOT = -4778
443888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19231554
28 X = -5861777
75
Y = 3616387
80 feet Y = 1102275
00 meter
Z = 10556153
92 Z = 3217515
72
XDOT = -11375
904428 XDOT = -3467
375670
YDOT = -14471
022213 feet/sec YDOT = -4410
767571 meter/sec
ZDOT = -15697
564124 ZDOT = -4784
617545
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 18335
53886247
00016717 00000-0 10270-3 0 9033
2 25544 51
6396 264
7481 0005088 99
7680 260
4048 15
54044176 24539
Satellite: ISS
Catalog Number: 25544
Epoch time: 18335
53886247 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 264
7481 deg
Eccentricity:
0005088
Arg of perigee: 99
7680 deg
Mean anomaly: 260
4048 deg
Mean motion: 15
54044176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2453
Checksum: 336
Coasting Arc #5 (Orbit 2467)
---------------------------------------
Vector Time (GMT): 2018/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2591933
30 A = 6788293
58 meter
Y = -6026948
88 meter E =
0010762
Z = -1739699
39 I = 51
27913
XDOT = 3967
634141 Wp = 63
84853
YDOT = -3327
856727 meter/sec RA = 259
00435 deg
ZDOT = 5649
562378 TA = 276
97243
MA = 277
09483
Ha = 222
986 n
mi
Hp = 212
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8503718
16 X = -2515894
98
Y = -19773454
32 feet Y = -6055508
46 meter
Z = -5707675
18 Z = -1752105
78
XDOT = 13017
172377 XDOT = 3977
109332
YDOT = -10918
165114 feet/sec YDOT = -3283
435092 meter/sec
ZDOT = 18535
309639 ZDOT = 5668
858923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21467877
02 X = 6543408
92
Y = -1342108
22 feet Y = -409074
59 meter
Z = -5762748
99 Z = -1756485
89
XDOT = 5861
495515 XDOT = 1786
583833
YDOT = 14242
790235 feet/sec YDOT = 4341
202464 meter/sec
ZDOT = 18622
458123 ZDOT = 5676
125236
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 18336
50344805
00016717 00000-0 10270-3 0 9041
2 25544 51
6392 259
9404 0005129 102
6829 257
4897 15
54032585 24686
Satellite: ISS
Catalog Number: 25544
Epoch time: 18336
50344805 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 259
9404 deg
Eccentricity:
0005129
Arg of perigee: 102
6829 deg
Mean anomaly: 257
4897 deg
Mean motion: 15
54032585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2468
Checksum: 331
Coasting Arc #6 (Orbit 2483)
---------------------------------------
Vector Time (GMT): 2018/337/11:31:53
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3191220
83 A = 6778933
90 meter
Y = -3330526
12 meter E =
0011013
Z = 4960654
08 I = 51
25567
XDOT = 3557
451201 Wp = 116
48858
YDOT = 6481
623626 meter/sec RA = 254
12504 deg
ZDOT = 2054
775983 TA = 313
38712
MA = 313
47878
Ha = 222
768 n
mi
Hp = 212
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10469884
62 X = 3204129
90
Y = -10926922
98 feet Y = -3294767
71 meter
Z = 16275111
82 Z = 4976187
38
XDOT = 11671
427824 XDOT = 3474
726298
YDOT = 21265
169376 feet/sec YDOT = 6520
942884 meter/sec
ZDOT = 6741
391020 ZDOT = 2071
856479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5361018
08 X = 1634038
31
Y = 14070706
78 feet Y = 4288751
43 meter
Z = 16345338
48 Z = 4982059
17
XDOT = -23176
948375 XDOT = -7064
333865
YDOT = 879
215789 feet/sec YDOT = 267
984972 meter/sec
ZDOT = 6817
440909 ZDOT = 2077
955989
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
53233680
00016717 00000-0 10270-3 0 9054
2 25544 51
6395 254
8125 0005010 108
2314 251
9384 15
54075241 24847
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
53233680 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 254
8125 deg
Eccentricity:
0005010
Arg of perigee: 108
2314 deg
Mean anomaly: 251
9384 deg
Mean motion: 15
54075241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2484
Checksum: 295
Coasting Arc #7 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/17:35:42
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1396651
21 A = 6783745
85 meter
Y = -5511299
99 meter E =
0016481
Z = 3688879
44 I = 51
27213
XDOT = 4861
059821 Wp = 99
62018
YDOT = 4110
966992 meter/sec RA = 252
86645 deg
ZDOT = 4282
359436 TA = 304
62245
MA = 304
77776
Ha = 222
805 n
mi
Hp = 213
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4582189
00 X = 1440257
38
Y = -18081692
88 feet Y = -5495438
02 meter
Z = 12102622
83 Z = 3695769
65
XDOT = 15948
358993 XDOT = 4793
926768
YDOT = 13487
424515 feet/sec YDOT = 4164
951174 meter/sec
ZDOT = 14049
735684 ZDOT = 4305
810307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11583615
92 X = 3530686
13
Y = -14594439
46 feet Y = -4448385
15 meter
Z = 12134237
99 Z = 3698515
74
XDOT = 7782
593175 XDOT = 2372
134400
YDOT = 17997
645966 feet/sec YDOT = 5485
682490 meter/sec
ZDOT = 14154
705352 ZDOT = 4314
354191
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
78955816
00016717 00000-0 10270-3 0 9064
2 25544 51
6378 253
5285 0004847 109
9543 250
2132 15
54052936 24883
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78955816 = yrday
fracday
Element set: 906
Inclination: 51
6378 deg
RA of node: 253
5285 deg
Eccentricity:
0004847
Arg of perigee: 109
9543 deg
Mean anomaly: 250
2132 deg
Mean motion: 15
54052936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 341
Coasting Arc #8 (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 = 4431152
66 A = 6782337
51 meter
Y = 3051663
98 meter E =
0014905
Z = 4116847
69 I = 51
26675
XDOT = -1059
112684 Wp = 88
07271
YDOT = 6612
439668 meter/sec RA = 252
41537 deg
ZDOT = -3749
304549 TA = 40
75706
MA = 40
64565
Ha = 222
897 n
mi
Hp = 213
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14537902
41 X = 4376700
96
Y = 10012020
92 feet Y = 3100911
55 meter
Z = 13506718
15 Z = 4138240
95
XDOT = -3474
779148 XDOT = -1114
763674
YDOT = 21694
355867 feet/sec YDOT = 6600
284954 meter/sec
ZDOT = -12300
867944 ZDOT = -3754
584282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15141235
86 X = 4615048
69
Y = 8929500
04 feet Y = 2721711
61 meter
Z = 13602558
96 Z = 4146059
97
XDOT = -1145
799368 XDOT = -349
239647
YDOT = 20779
366028 feet/sec YDOT = 6333
550765 meter/sec
ZDOT = -12325
367851 ZDOT = -3756
772121
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
85386549
00016717 00000-0 10270-3 0 9074
2 25544 51
6365 253
2053 0005241 112
6536 247
5162 15
54021506 24893
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
85386549 = yrday
fracday
Element set: 907
Inclination: 51
6365 deg
RA of node: 253
2053 deg
Eccentricity:
0005241
Arg of perigee: 112
6536 deg
Mean anomaly: 247
5162 deg
Mean motion: 15
54021506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2489
Checksum: 311
Coasting Arc #9 (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 = -3326339
28 A = 6778103
02 meter
Y = 2867164
74 meter E =
0018359
Z = -5179151
27 I = 51
26522
XDOT = -3718
567798 Wp = 88
24488
YDOT = -6572
373417 meter/sec RA = 248
15113 deg
ZDOT = -1253
492108 TA = 169
65598
MA = 169
61815
Ha = 222
818 n
mi
Hp = 212
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10913186
63 X = -3332995
47
Y = 9406708
47 feet Y = 2829930
42 meter
Z = -16991966
10 Z = -5195325
74
XDOT = -12200
025584 XDOT = -3638
708397
YDOT = -21562
904912 feet/sec YDOT = -6613
510424 meter/sec
ZDOT = -4112
506916 ZDOT = -1271
362397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14273896
23 X = -4350683
57
Y = -1162582
53 feet Y = -354355
15 meter
Z = -17065022
91 Z = -5201418
98
XDOT = 6850
198515 XDOT = 2087
940507
YDOT = -22729
795674 feet/sec YDOT = -6928
041721 meter/sec
ZDOT = -4192
114697 ZDOT = -1277
756560
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
68983495
00016717 00000-0 10270-3 0 9080
2 25544 51
6396 249
0419 0004857 111
3328 248
8344 15
54058628 25020
Satellite: ISS
Catalog Number: 25544
Epoch time: 18338
68983495 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 249
0419 deg
Eccentricity:
0004857
Arg of perigee: 111
3328 deg
Mean anomaly: 248
8344 deg
Mean motion: 15
54058628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 344
Coasting Arc #10 (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 = 4674732
12 A = 6782219
60 meter
Y = 2625603
03 meter E =
0014563
Z = 4141137
60 I = 51
27792
XDOT = -459
984001 Wp = 88
36509
YDOT = 6699
176483 meter/sec RA = 247
58410 deg
ZDOT = -3716
468168 TA = 40
05383
MA = 39
94653
Ha = 222
807 n
mi
Hp = 213
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15337047
63 X = 4624908
64
Y = 8614183
19 feet Y = 2677600
28 meter
Z = 13586409
44 Z = 4163725
39
XDOT = -1509
133862 XDOT = -516
808920
YDOT = 21978
925469 feet/sec YDOT = 6693
715143 meter/sec
ZDOT = -12193
137033 ZDOT = -3718
840223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13966527
78 X = 4256997
67
Y = 10564241
94 feet Y = 3219980
94 meter
Z = 13687680
51 Z = 4172005
02
XDOT = -3564
524332 XDOT = -1086
467016
YDOT = 20575
077157 feet/sec YDOT = 6271
283518 meter/sec
ZDOT = -12204
564868 ZDOT = -3719
951372
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
81844686
00016717 00000-0 10270-3 0 9094
2 25544 51
6374 248
3977 0005095 115
1767 244
9914 15
54030429 25042
Satellite: ISS
Catalog Number: 25544
Epoch time: 18338
81844686 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 248
3977 deg
Eccentricity:
0005095
Arg of perigee: 115
1767 deg
Mean anomaly: 244
9914 deg
Mean motion: 15
54030429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2504
Checksum: 340
Coasting Arc #11 (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 = -4685758
37 A = 6785855
74 meter
Y = -3951413
36 meter E =
0008945
Z = -2920431
64 I = 51
30440
XDOT = 1606
389751 Wp = 94
90473
YDOT = -5584
382824 meter/sec RA = 242
57664 deg
ZDOT = 4990
891251 TA = 231
65186
MA = 231
73228
Ha = 222
950 n
mi
Hp = 212
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15373223
01 X = -4627038
15
Y = -12963954
60 feet Y = -4003484
19 meter
Z = -9581468
64 Z = -2943051
54
XDOT = 5270
307581 XDOT = 1644
472961
YDOT = -18321
465957 feet/sec YDOT = -5566
206557 meter/sec
ZDOT = 16374
315127 ZDOT = 4998
786680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13705047
98 X = -4177298
62
Y = -14649938
93 feet Y = -4465301
39 meter
Z = -9682747
29 Z = -2951301
37
XDOT = 6179
135843 XDOT = 1883
400605
YDOT = -16600
112743 feet/sec YDOT = -5059
714364 meter/sec
ZDOT = 16410
449206 ZDOT = 5001
904918
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
78302760
00016717 00000-0 10270-3 0 9105
2 25544 51
6378 243
5897 0005350 118
0621 242
1073 15
54052781 25196
Satellite: ISS
Catalog Number: 25544
Epoch time: 18339
78302760 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 243
5897 deg
Eccentricity:
0005350
Arg of perigee: 118
0621 deg
Mean anomaly: 242
1073 deg
Mean motion: 15
54052781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2519
Checksum: 305
Coasting Arc #12 (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 = 3401679
04 A = 6789595
05 meter
Y = 5866750
96 meter E =
0016845
Z = -103508
58 I = 51
32988
XDOT = -4187
369512 Wp = 130
05092
YDOT = 2333
901717 meter/sec RA = 239
19396 deg
ZDOT = -5987
573151 TA = 51
06911
MA = 50
91906
Ha = 222
894 n
mi
Hp = 213
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11160364
31 X = 3336325
37
Y = 19247870
60 feet Y = 5904425
49 meter
Z = -339595
09 Z = -87142
28
XDOT = -13738
088951 XDOT = -4184
071709
YDOT = 7657
157865 feet/sec YDOT = 2287
094686 meter/sec
ZDOT = -19644
268868 ZDOT = -6007
906019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22249190
90 X = -6781553
38
Y = -228000
28 feet Y = -69494
48 meter
Z = -266644
54 Z = -81273
26
XDOT = 346
902536 XDOT = 105
735893
YDOT = -13986
010921 feet/sec YDOT = -4262
936129 meter/sec
ZDOT = -19735
973914 ZDOT = -6015
524849
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
49038666
00016717 00000-0 10270-3 0 9117
2 25544 51
6403 240
0685 0005069 117
2584 242
9086 15
54036680 25303
Satellite: ISS
Catalog Number: 25544
Epoch time: 18340
49038666 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 240
0685 deg
Eccentricity:
0005069
Arg of perigee: 117
2584 deg
Mean anomaly: 242
9086 deg
Mean motion: 15
54036680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2530
Checksum: 304
Coasting Arc #13 (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 = -2620971
55 A = 6788330
71 meter
Y = -6009562
37 meter E =
0017244
Z = 1736765
22 I = 51
34321
XDOT = 5146
360390 Wp = 78
67652
YDOT = -597
332052 meter/sec RA = 234
20270 deg
ZDOT = 5655
060002 TA = 300
46581
MA = 300
63602
Ha = 222
838 n
mi
Hp = 213
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8598988
02 X = -2562012
54
Y = -19716411
97 feet Y = -6038542
44 meter
Z = 5698048
63 Z = 1724175
78
XDOT = 16884
384483 XDOT = 5125
187784
YDOT = -1959
750826 feet/sec YDOT = -539
900921 meter/sec
ZDOT = 18553
346463 ZDOT = 5680
008068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21404612
81 X = 6524125
99
Y = 2270831
21 feet Y = 692149
35 meter
Z = 5642085
59 Z = 1719707
69
XDOT = -6440
682654 XDOT = -1963
120073
YDOT = 13966
586328 feet/sec YDOT = 4257
015513 meter/sec
ZDOT = 18665
626684 ZDOT = 5689
283013
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
51927112
00016717 00000-0 10270-3 0 9125
2 25544 51
6400 234
9406 0004977 120
5771 239
5873 15
54042348 25466
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
51927112 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 234
9406 deg
Eccentricity:
0004977
Arg of perigee: 120
5771 deg
Mean anomaly: 239
5873 deg
Mean motion: 15
54042348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2546
Checksum: 305
Coasting Arc #14 (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 = 1540078
31 A = 6785099
54 meter
Y = 5757654
41 meter E =
0009268
Z = -3246246
19 I = 51
35386
XDOT = -5928
457086 Wp = 112
10442
YDOT = -1075
459081 meter/sec RA = 229
20652 deg
ZDOT = -4734
338486 TA = 105
66095
MA = 105
55867
Ha = 222
759 n
mi
Hp = 213
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5052750
37 X = 1491348
84
Y = 18889942
29 feet Y = 5774604
58 meter
Z = -10650414
01 Z = -3238882
58
XDOT = -19450
318523 XDOT = -5892
993258
YDOT = -3528
409057 feet/sec YDOT = -1141
556317 meter/sec
ZDOT = -15532
606580 ZDOT = -4763
051143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19026905
14 X = -5799400
69
Y = -4585658
40 feet Y = -1397708
68 meter
Z = -10617916
10 Z = -3236340
83
XDOT = 12059
223914 XDOT = 3675
651449
YDOT = -13881
371326 feet/sec YDOT = -4231
041980 meter/sec
ZDOT = -15661
653757 ZDOT = -4773
672065
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
48384711
00016717 00000-0 10270-3 0 9135
2 25544 51
6410 230
1330 0004911 124
3253 235
8365 15
54055556 25613
Satellite: ISS
Catalog Number: 25544
Epoch time: 18342
48384711 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 230
1330 deg
Eccentricity:
0004911
Arg of perigee: 124
3253 deg
Mean anomaly: 235
8365 deg
Mean motion: 15
54055556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2561
Checksum: 282
Coasting Arc #15 (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 = -284321
34 A = 6781421
56 meter
Y = -5161796
34 meter E =
0014328
Z = 4381329
51 I = 51
36301
XDOT = 6427
099164 Wp = 115
54226
YDOT = 2507
637706 meter/sec RA = 224
20189 deg
ZDOT = 3356
748511 TA = 300
32302
MA = 300
46467
Ha = 222
784 n
mi
Hp = 213
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -932812
80 X = -247861
86
Y = -16935027
35 feet Y = -5164772
52 meter
Z = 14374440
65 Z = 4380036
26
XDOT = 21086
283345 XDOT = 6382
274985
YDOT = 8227
157827 feet/sec YDOT = 2579
258937 meter/sec
ZDOT = 11012
954431 ZDOT = 3387
860746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15466373
96 X = 4714150
78
Y = 6971934
69 feet Y = 2125045
69 meter
Z = 14369176
68 Z = 4379725
05
XDOT = -16554
620873 XDOT = -5045
848442
YDOT = 13639
502807 feet/sec YDOT = 4157
320456 meter/sec
ZDOT = 11152
663792 ZDOT = 3399
331924
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
51272866
00016717 00000-0 10270-3 0 9148
2 25544 51
6400 225
0047 0005005 126
6923 233
4690 15
54047507 25773
Satellite: ISS
Catalog Number: 25544
Epoch time: 18343
51272866 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 225
0047 deg
Eccentricity:
0005005
Arg of perigee: 126
6923 deg
Mean anomaly: 233
4690 deg
Mean motion: 15
54047507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2577
Checksum: 295
Coasting Arc #16 (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 = -1163816
39 A = 6778411
06 meter
Y = 4317342
34 meter E =
0016769
Z = -5108859
49 I = 51
37776
XDOT = -6528
098102 Wp = 91
34118
YDOT = -3660
969017 meter/sec RA = 219
18967 deg
ZDOT = -1611
630154 TA = 163
05632
MA = 163
00025
Ha = 222
614 n
mi
Hp = 213
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3818295
25 X = -1187191
44
Y = 14164509
00 feet Y = 4304197
66 meter
Z = -16761350
03 Z = -5114569
16
XDOT = -21417
644693 XDOT = -6478
846480
YDOT = -12011
053206 feet/sec YDOT = -3733
695166 meter/sec
ZDOT = -5287
500504 ZDOT = -1643
222271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10978304
51 X = -3346187
22
Y = -9685672
54 feet Y = -2952192
99 meter
Z = -16787499
10 Z = -5116829
73
XDOT = 19644
936404 XDOT = 5987
776616
YDOT = -12884
811707 feet/sec YDOT = -3927
290608 meter/sec
ZDOT = -5429
271687 ZDOT = -1654
842010
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
47730329
00016717 00000-0 10270-3 0 9158
2 25544 51
6400 220
1973 0004835 131
3858 228
7710 15
54077449 25922
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
47730329 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 220
1973 deg
Eccentricity:
0004835
Arg of perigee: 131
3858 deg
Mean anomaly: 228
7710 deg
Mean motion: 15
54077449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2592
Checksum: 314
Coasting Arc #17 (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 = 4037656
17 A = 6787794
95 meter
Y = 5049743
00 meter E =
0011745
Z = -2055302
41 I = 51
42057
XDOT = -5010
421041 Wp = 138
67475
YDOT = 1767
237175 meter/sec RA = 216
66553 deg
ZDOT = -5527
752989 TA = 64
12615
MA = 64
00510
Ha = 222
714 n
mi
Hp = 213
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13246903
43 X = 3990872
02
Y = 16567398
28 feet Y = 5094633
53 meter
Z = -6743118
13 Z = -2035801
91
XDOT = -16438
389243 XDOT = -5002
959486
YDOT = 5798
022229 feet/sec YDOT = 1711
249534 meter/sec
ZDOT = -18135
672535 ZDOT = -5552
073555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20576392
47 X = 6271684
42
Y = -5266871
99 feet Y = -1605342
58 meter
Z = -6655892
96 Z = -2028716
17
XDOT = -1840
522843 XDOT = -560
991362
YDOT = 15754
340825 feet/sec YDOT = 4801
923083 meter/sec
ZDOT = -18245
303589 ZDOT = -5561
168534
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
99174276
00016717 00000-0 10270-3 0 9169
2 25544 51
6385 217
6307 0005096 136
6894 223
4659 15
54054587 26006
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
99174276 = yrday
fracday
Element set: 916
Inclination: 51
6385 deg
RA of node: 217
6307 deg
Eccentricity:
0005096
Arg of perigee: 136
6894 deg
Mean anomaly: 223
4659 deg
Mean motion: 15
54054587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 339
Coasting Arc #18 (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 = -2910526
99 A = 6784448
95 meter
Y = -5045443
46 meter E =
0016108
Z = 3469208
65 I = 51
43717
XDOT = 6175
222949 Wp = 104
66202
YDOT = -433
013688 meter/sec RA = 211
67285 deg
ZDOT = 4529
363961 TA = 296
21414
MA = 296
37966
Ha = 222
643 n
mi
Hp = 213
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9548973
07 X = -2870742
67
Y = -16553292
19 feet Y = -5077768
91 meter
Z = 11381918
16 Z = 3455166
45
XDOT = 20259
917813 XDOT = 6157
604856
YDOT = -1420
648583 feet/sec YDOT = -364
057039 meter/sec
ZDOT = 14860
117982 ZDOT = 4559
318165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19013364
73 X = -5795273
57
Y = 2260363
69 feet Y = 688958
85 meter
Z = 11319237
96 Z = 3450103
73
XDOT = 6867
642079 XDOT = 2093
257306
YDOT = -17679
946782 feet/sec YDOT = -5388
847779 meter/sec
ZDOT = 14994
979545 ZDOT = 4570
469765
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
02061980
00016717 00000-0 10270-3 0 9173
2 25544 51
6389 212
5019 0005029 139
5244 220
6284 15
54071708 26165
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
02061980 = yrday
fracday
Element set: 917
Inclination: 51
6389 deg
RA of node: 212
5019 deg
Eccentricity:
0005029
Arg of perigee: 139
5244 deg
Mean anomaly: 220
6284 deg
Mean motion: 15
54071708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 302
Coasting Arc #19 (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 = 1445884
11 A = 6780747
89 meter
Y = 4803606
96 meter E =
0012458
Z = -4572615
46 I = 51
45274
XDOT = -6982
432191 Wp = 93
00575
YDOT = -791
002872 meter/sec RA = 206
67272 deg
ZDOT = -3046
675092 TA = 146
46223
MA = 146
38330
Ha = 222
623 n
mi
Hp = 213
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4743714
27 X = 1414272
66
Y = 15759865
37 feet Y = 4819599
51 meter
Z = -15002019
22 Z = -4565668
21
XDOT = -22908
242097 XDOT = -6958
268928
YDOT = -2595
153778 feet/sec YDOT = -868
949897 meter/sec
ZDOT = -9995
653190 ZDOT = -3080
534624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16415154
74 X = 5003339
17
Y = 1530225
14 feet Y = 466412
62 meter
Z = -14971234
68 Z = -4563232
33
XDOT = -10996
443995 XDOT = -3351
716130
YDOT = 18929
226721 feet/sec YDOT = 5769
628305 meter/sec
ZDOT = -10147
987577 ZDOT = -3093
106614
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
98519370
00016717 00000-0 10270-3 0 9180
2 25544 51
6382 207
6943 0005073 141
9924 218
1587 15
54048931 26317
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
98519370 = yrday
fracday
Element set: 918
Inclination: 51
6382 deg
RA of node: 207
6943 deg
Eccentricity:
0005073
Arg of perigee: 141
9924 deg
Mean anomaly: 218
1587 deg
Mean motion: 15
54048931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 331
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