[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 2nd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
277/07:57:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 216
4
280/14:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
283/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
6
284/08:40:17
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
284/14:44:01
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
7
287/02:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
6
Coasting Arc #1 (Orbit 1503)
---------------------------------------
Vector Time (GMT): 2018/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5909008
02 A = 6785607
62 meter
Y = -104604
51 meter E =
0002731
Z = -3338009
00 I = 51
46034
XDOT = -2534
795430 Wp = 140
91192
YDOT = -5528
601028 meter/sec RA = 207
75217 deg
ZDOT = 4660
405476 TA = 180
13043
MA = 180
13050
Ha = 220
786 n
mi
Hp = 216
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19386509
25 X = -5891184
63
Y = -343190
64 feet Y = -170583
61 meter
Z = -10951473
11 Z = -3366670
00
XDOT = -8316
257972 XDOT = -2495
422774
YDOT = -18138
454817 feet/sec YDOT = -5556
726540 meter/sec
ZDOT = 15290
044211 ZDOT = 4648
188006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19115340
21 X = 5826355
70
Y = -2779243
19 feet Y = -847113
33 meter
Z = -11080111
00 Z = -3377217
83
XDOT = 11033
434221 XDOT = 3362
990751
YDOT = 15146
097272 feet/sec YDOT = 4616
530448 meter/sec
ZDOT = 15235
723648 ZDOT = 4643
848568
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 18274
50704705
00016717 00000-0 10270-3 0 9007
2 25544 51
6383 208
8888 0003793 233
7266 126
3537 15
53746741 15041
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
50704705 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 208
8888 deg
Eccentricity:
0003793
Arg of perigee: 233
7266 deg
Mean anomaly: 126
3537 deg
Mean motion: 15
53746741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1504
Checksum: 322
Coasting Arc #2 (Orbit 1519)
---------------------------------------
Vector Time (GMT): 2018/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6415385
95 A = 6788715
33 meter
Y = 1005642
17 meter E =
0012091
Z = 1955317
16 I = 51
50164
XDOT = 892
537021 Wp = 126
77018
YDOT = 5187
377939 meter/sec RA = 202
76583 deg
ZDOT = -5579
494195 TA = 31
61267
MA = 31
54010
Ha = 220
595 n
mi
Hp = 216
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21047854
17 X = 6394165
79
Y = 3299350
96 feet Y = 1077264
89 meter
Z = 6415082
56 Z = 1986429
58
XDOT = 2928
271065 XDOT = 861
566465
YDOT = 17018
956492 feet/sec YDOT = 5197
185540 meter/sec
ZDOT = -18305
427149 ZDOT = -5575
233930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21256446
77 X = -6478964
98
Y = 501056
63 feet Y = 152722
06 meter
Z = 6554660
88 Z = 1997860
64
XDOT = -6000
946223 XDOT = -1829
088409
YDOT = -14650
284000 feet/sec YDOT = -4465
406563 meter/sec
ZDOT = -18286
783683 ZDOT = -5573
811667
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 18275
53612474
00016717 00000-0 10270-3 0 9013
2 25544 51
6394 203
7615 0003778 238
1463 121
9322 15
53758521 15206
Satellite: ISS
Catalog Number: 25544
Epoch time: 18275
53612474 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 203
7615 deg
Eccentricity:
0003778
Arg of perigee: 238
1463 deg
Mean anomaly: 121
9322 deg
Mean motion: 15
53758521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1520
Checksum: 303
Coasting Arc #3 (Orbit 1534)
---------------------------------------
Vector Time (GMT): 2018/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6542243
85 A = 6790316
73 meter
Y = -1755061
67 meter E =
0007779
Z = -412188
92 I = 51
53736
XDOT = 889
541603 Wp = 32
53172
YDOT = -4707
666359 meter/sec RA = 197
78767 deg
ZDOT = 5985
060590 TA = 323
01924
MA = 323
07284
Ha = 220
555 n
mi
Hp = 216
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21464054
63 X = -6520129
82
Y = -5758076
36 feet Y = -1828097
95 meter
Z = -1352325
85 Z = -443915
24
XDOT = 2918
443581 XDOT = 913
045511
YDOT = -15445
099602 feet/sec YDOT = -4697
587202 meter/sec
ZDOT = 19636
025559 ZDOT = 5989
438993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22166068
08 X = 6756217
55
Y = 1456511
37 feet Y = 443944
67 meter
Z = -1494613
70 Z = -455558
26
XDOT = 388
745588 XDOT = 118
489655
YDOT = 14074
360014 feet/sec YDOT = 4289
864932 meter/sec
ZDOT = 19656
116517 ZDOT = 5991
184314
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 18276
50088081
00016717 00000-0 10270-3 0 9023
2 25544 51
6389 198
9548 0003712 242
7106 117
3669 15
53757533 15354
Satellite: ISS
Catalog Number: 25544
Epoch time: 18276
50088081 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 198
9548 deg
Eccentricity:
0003712
Arg of perigee: 242
7106 deg
Mean anomaly: 117
3669 deg
Mean motion: 15
53757533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1535
Checksum: 331
Coasting Arc #4 (Orbit 1547)
---------------------------------------
Vector Time (GMT): 2018/277/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6220785
34 A = 6787351
03 meter
Y = 645903
29 meter E =
0001413
Z = -2635713
74 I = 51
55183
XDOT = -2718
001489 Wp = 33
89973
YDOT = -4916
901825 meter/sec RA = 193
62032 deg
ZDOT = 5212
571582 TA = 296
37308
MA = 296
38759
Ha = 220
546 n
mi
Hp = 216
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20409400
71 X = -6214742
72
Y = 2119105
27 feet Y = 576371
78 meter
Z = -8647354
78 Z = -2665917
60
XDOT = -8917
327719 XDOT = -2688
137313
YDOT = -16131
567666 feet/sec YDOT = -4947
129113 meter/sec
ZDOT = 17101
612801 ZDOT = 5199
441265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15061939
94 X = 4590879
29
Y = 13849444
38 feet Y = 4221310
65 meter
Z = -8783043
02 Z = -2677071
51
XDOT = -5099
534777 XDOT = -1554
338200
YDOT = 16349
266791 feet/sec YDOT = 4983
256518 meter/sec
ZDOT = 17043
098006 ZDOT = 5194
736272
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 18277
33700028
00016717 00000-0 10270-3 0 9038
2 25544 51
6366 194
7890 0003653 243
3413 116
7365 15
53763602 15489
Satellite: ISS
Catalog Number: 25544
Epoch time: 18277
33700028 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 194
7890 deg
Eccentricity:
0003653
Arg of perigee: 243
3413 deg
Mean anomaly: 116
7365 deg
Mean motion: 15
53763602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 311
Coasting Arc #5 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2018/278/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6686299
19 A = 6789738
07 meter
Y = 106014
34 meter E =
0011818
Z = 1135284
43 I = 51
59320
XDOT = 924
605248 Wp = 137
13010
YDOT = 4848
245193 meter/sec RA = 188
64340 deg
ZDOT = -5870
744157 TA = 30
53686
MA = 30
46810
Ha = 220
358 n
mi
Hp = 216
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21936677
12 X = 6679102
14
Y = 347816
08 feet Y = 180745
03 meter
Z = 3724686
46 Z = 1167746
73
XDOT = 3033
481786 XDOT = 898
839141
YDOT = 15906
316251 feet/sec YDOT = 4858
440225 meter/sec
ZDOT = -19260
971644 ZDOT = -5866
315714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14530567
21 X = -4428916
88
Y = -16404089
97 feet Y = -4999966
62 meter
Z = 3870467
34 Z = 1179718
45
XDOT = 8406
955905 XDOT = 2562
440160
YDOT = -12007
213238 feet/sec YDOT = -3659
798595 meter/sec
ZDOT = -19241
517637 ZDOT = -5864
814576
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 18278
36606843
00016717 00000-0 10270-3 0 9043
2 25544 51
6375 189
6611 0003732 249
4687 110
6065 15
53785810 15644
Satellite: ISS
Catalog Number: 25544
Epoch time: 18278
36606843 = yrday
fracday
Element set: 904
Inclination: 51
6375 deg
RA of node: 189
6611 deg
Eccentricity:
0003732
Arg of perigee: 249
4687 deg
Mean anomaly: 110
6065 deg
Mean motion: 15
53785810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 331
Coasting Arc #6 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2018/279/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6723748
45 A = 6790186
13 meter
Y = -790065
43 meter E =
0009408
Z = 451718
82 I = 51
62844
XDOT = 957
881129 Wp = 41
54694
YDOT = -4690
538786 meter/sec RA = 183
67336 deg
ZDOT = 5989
362364 TA = 323
32435
MA = 323
38870
Ha = 220
304 n
mi
Hp = 216
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22059542
17 X = -6716608
22
Y = -2592078
19 feet Y = -865215
08 meter
Z = 1482017
14 Z = 419074
50
XDOT = 3142
654622 XDOT = 981
167578
YDOT = -15388
906779 feet/sec YDOT = -4679
696277 meter/sec
ZDOT = 19650
138990 ZDOT = 5994
072475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13289312
50 X = 4050582
45
Y = 17808687
75 feet Y = 5428088
03 meter
Z = 1335461
97 Z = 407048
81
XDOT = -11946
588906 XDOT = -3641
320299
YDOT = 7422
034903 feet/sec YDOT = 2262
236238 meter/sec
ZDOT = 19671
710484 ZDOT = 5995
937356
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 18279
39513121
00016717 00000-0 10270-3 0 9054
2 25544 51
6382 184
5342 0003765 251
0461 109
0284 15
53809965 15803
Satellite: ISS
Catalog Number: 25544
Epoch time: 18279
39513121 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 184
5342 deg
Eccentricity:
0003765
Arg of perigee: 251
0461 deg
Mean anomaly: 109
0284 deg
Mean motion: 15
53809965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 311
Coasting Arc #7 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2018/280/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6311378
63 A = 6788653
16 meter
Y = 1456043
26 meter E =
0006002
Z = -2020824
55 I = 51
65651
XDOT = -2809
016575 Wp = 173
61899
YDOT = 4465
128289 meter/sec RA = 178
70378 deg
ZDOT = -5563
239654 TA = 28
69869
MA = 28
66568
Ha = 220
290 n
mi
Hp = 216
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20706622
80 X = 6304443
85
Y = 4777044
81 feet Y = 1526582
46 meter
Z = -6630001
80 Z = -1990182
86
XDOT = -9215
933644 XDOT = -2831
714631
YDOT = 14649
371026 feet/sec YDOT = 4433
588347 meter/sec
ZDOT = -18252
098602 ZDOT = -5576
940632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11110391
34 X = -3386447
28
Y = -18164474
83 feet Y = -5536531
93 meter
Z = -6492485
46 Z = -1978909
57
XDOT = 15503
021349 XDOT = 4725
320907
YDOT = -2945
436153 feet/sec YDOT = -897
768939 meter/sec
ZDOT = -18314
037149 ZDOT = -5582
118523
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 18280
35987665
00016717 00000-0 10270-3 0 9061
2 25544 51
6385 179
7274 0003719 258
6759 101
3975 15
53789473 15957
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
35987665 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 179
7274 deg
Eccentricity:
0003719
Arg of perigee: 258
6759 deg
Mean anomaly: 101
3975 deg
Mean motion: 15
53789473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 372
Coasting Arc #8 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2018/280/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6135457
42 A = 6788358
87 meter
Y = 1973846
09 meter E =
0004031
Z = -2123473
28 I = 51
66625
XDOT = -3261
062019 Wp = 4
59528
YDOT = -4209
417204 meter/sec RA = 177
26698 deg
ZDOT = 5514
192965 TA = 331
89365
MA = 331
91540
Ha = 220
125 n
mi
Hp = 216
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20129453
47 X = -6146758
71
Y = 6475872
99 feet Y = 1905171
70 meter
Z = -6966775
87 Z = -2153305
14
XDOT = -10699
022371 XDOT = -3240
534043
YDOT = -13810
423896 feet/sec YDOT = -4245
769220 meter/sec
ZDOT = 18091
184267 ZDOT = 5498
402093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5882017
65 X = 1792838
98
Y = -20264403
09 feet Y = -6176590
06 meter
Z = -7100959
79 Z = -2164372
54
XDOT = 16021
789492 XDOT = 4883
441437
YDOT = -1658
915675 feet/sec YDOT = -505
637498 meter/sec
ZDOT = 18020
618652 ZDOT = 5492
684565
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 18280
61714018
00016717 00000-0 10270-3 0 9071
2 25544 51
6398 178
4466 0003948 261
1627 98
9079 15
53778384 15996
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
61714018 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 178
4466 deg
Eccentricity:
0003948
Arg of perigee: 261
1627 deg
Mean anomaly: 98
9079 deg
Mean motion: 15
53778384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 361
Coasting Arc #9 (Orbit 1614)
---------------------------------------
Vector Time (GMT): 2018/281/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6625560
45 A = 6790188
75 meter
Y = -1344040
95 meter E =
0010690
Z = 562663
23 I = 51
70580
XDOT = 1440
233566 Wp = 144
18893
YDOT = 4573
795044 meter/sec RA = 172
30071 deg
ZDOT = -5984
786651 TA = 29
74477
MA = 29
68404
Ha = 220
131 n
mi
Hp = 216
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21737403
06 X = 6637364
31
Y = -4409583
16 feet Y = -1269883
26 meter
Z = 1846007
96 Z = 594877
16
XDOT = 4725
175743 XDOT = 1418
052402
YDOT = 15005
889252 feet/sec YDOT = 4589
775975 meter/sec
ZDOT = -19635
126809 ZDOT = -5977
844844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8159795
94 X = -2487105
80
Y = 20611188
78 feet Y = 6282290
34 meter
Z = 1990851
05 Z = 606811
40
XDOT = -13720
271349 XDOT = -4181
938707
YDOT = -3523
744172 feet/sec YDOT = -1074
037224 meter/sec
ZDOT = -19604
342249 ZDOT = -5975
403518
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 18281
64619794
00016717 00000-0 10270-3 0 9081
2 25544 51
6403 173
3200 0003951 263
4082 96
6620 15
53779647 16156
Satellite: ISS
Catalog Number: 25544
Epoch time: 18281
64619794 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 173
3200 deg
Eccentricity:
0003951
Arg of perigee: 263
4082 deg
Mean anomaly: 96
6620 deg
Mean motion: 15
53779647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1615
Checksum: 321
Coasting Arc #10 (Orbit 1630)
---------------------------------------
Vector Time (GMT): 2018/282/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6671813
96 A = 6789833
17 meter
Y = 663369
74 meter E =
0010347
Z = 1033830
70 I = 51
73655
XDOT = 435
147946 Wp = 44
34189
YDOT = -4872
077516 meter/sec RA = 167
33644 deg
ZDOT = 5906
001599 TA = 326
84966
MA = 326
91445
Ha = 220
034 n
mi
Hp = 216
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21889153
41 X = -6683757
97
Y = 2176409
92 feet Y = 588694
22 meter
Z = 3391833
02 Z = 1001391
68
XDOT = 1427
650741 XDOT = 460
907774
YDOT = -15984
506286 feet/sec YDOT = -4867
066674 meter/sec
ZDOT = 19376
645666 ZDOT = 5908
178566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9794901
10 X = 2985485
85
Y = -19720536
69 feet Y = -6010819
58 meter
Z = 3246024
23 Z = 989388
18
XDOT = 11413
789545 XDOT = 3478
923053
YDOT = 8876
214290 feet/sec YDOT = 2705
470116 meter/sec
ZDOT = 19386
858519 ZDOT = 5909
114477
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 18282
67525010
00016717 00000-0 10270-3 0 9093
2 25544 51
6394 168
1914 0004017 267
8294 92
2398 15
53813270 16319
Satellite: ISS
Catalog Number: 25544
Epoch time: 18282
67525010 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 168
1914 deg
Eccentricity:
0004017
Arg of perigee: 267
8294 deg
Mean anomaly: 92
2398 deg
Mean motion: 15
53813270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1631
Checksum: 316
Coasting Arc #11 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2018/283/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6284537
79 A = 6787614
20 meter
Y = 117183
47 meter E =
0003269
Z = -2556617
02 I = 51
75915
XDOT = -2242
622505 Wp = 179
37198
YDOT = 5081
164438 meter/sec RA = 162
37249 deg
ZDOT = -5283
049728 TA = 29
29404
MA = 29
27572
Ha = 220
106 n
mi
Hp = 216
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20618562
30 X = 6295179
29
Y = 384460
22 feet Y = 187520
79 meter
Z = -8387851
13 Z = -2526062
44
XDOT = -7357
685385 XDOT = -2273
612008
YDOT = 16670
487002 feet/sec YDOT = 5055
912077 meter/sec
ZDOT = -17332
840316 ZDOT = -5294
019615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11007570
84 X = -3355107
59
Y = 17504014
93 feet Y = 5335223
75 meter
Z = -8250564
41 Z = -2514772
03
XDOT = -9255
939957 XDOT = -2821
210499
YDOT = -14008
903706 feet/sec YDOT = -4269
913850 meter/sec
ZDOT = -17382
589423 ZDOT = -5298
213256
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 18283
63998586
00016717 00000-0 10270-3 0 9104
2 25544 51
6375 163
3847 0003971 272
1916 87
8782 15
53795931 16464
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
63998586 = yrday
fracday
Element set: 910
Inclination: 51
6375 deg
RA of node: 163
3847 deg
Eccentricity:
0003971
Arg of perigee: 272
1916 deg
Mean anomaly: 87
8782 deg
Mean motion: 15
53795931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 362
Coasting Arc #12 (Orbit 1647)
---------------------------------------
Vector Time (GMT): 2018/283/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2806032
45 A = 6778981
00 meter
Y = 3372285
46 meter E =
0010122
Z = -5177018
94 I = 51
73505
XDOT = -6713
522453 Wp = 76
91925
YDOT = 3404
211248 meter/sec RA = 161
67800 deg
ZDOT = -1421
461145 TA = 179
41088
MA = 179
40969
Ha = 220
159 n
mi
Hp = 216
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9206143
20 X = 2793261
83
Y = 11063928
67 feet Y = 3403592
56 meter
Z = -16984970
26 Z = -5163419
26
XDOT = -22025
992301 XDOT = -6744
185468
YDOT = 11168
672075 feet/sec YDOT = 3328
964394 meter/sec
ZDOT = -4663
586434 ZDOT = -1454
148611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7553534
89 X = -2302317
43
Y = 12335706
09 feet Y = 3759923
22 meter
Z = -16924162
34 Z = -5158484
68
XDOT = -16643
320594 XDOT = -5072
884117
YDOT = -16790
966609 feet/sec YDOT = -5117
886622 meter/sec
ZDOT = -4810
776064 ZDOT = -1466
324544
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 18283
76861886
00016717 00000-0 10270-3 0 9111
2 25544 51
6377 162
7411 0003666 265
5574 94
5160 15
53814737 16486
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
76861886 = yrday
fracday
Element set: 911
Inclination: 51
6377 deg
RA of node: 162
7411 deg
Eccentricity:
0003666
Arg of perigee: 265
5574 deg
Mean anomaly: 94
5160 deg
Mean motion: 15
53814737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1648
Checksum: 341
Coasting Arc #13 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2018/284/08:40:17
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2804704
67 A = 6778752
16 meter
Y = -3311299
90 meter E =
0002151
Z = 5208534
46 I = 51
75464
XDOT = 6627
660209 Wp = 193
27134
YDOT = -3648
010338 meter/sec RA = 158
64008 deg
ZDOT = 1247
732915 TA = 244
75906
MA = 244
78135
Ha = 220
103 n
mi
Hp = 216
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9201786
98 X = -2792769
22
Y = -10863844
82 feet Y = -3342596
88 meter
Z = 17088367
65 Z = 5194939
14
XDOT = 21744
292025 XDOT = 6661
899727
YDOT = -11968
537853 feet/sec YDOT = -3573
703690 meter/sec
ZDOT = 4093
611926 ZDOT = 1280
011977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2410518
58 X = 734726
06
Y = 14105300
07 feet Y = 4299295
46 meter
Z = 17027572
55 Z = 5190004
11
XDOT = -23751
584794 XDOT = -7239
483045
YDOT = -1065
920423 feet/sec YDOT = -324
892545 meter/sec
ZDOT = 4239
001419 ZDOT = 1292
047633
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 18284
41177325
00016717 00000-0 10270-3 0 9123
2 25544 51
6387 159
5404 0003973 274
5743 85
4956 15
53836771 16587
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
41177325 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 159
5404 deg
Eccentricity:
0003973
Arg of perigee: 274
5743 deg
Mean anomaly: 85
4956 deg
Mean motion: 15
53836771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 344
Coasting Arc #14 (Orbit 1661)
---------------------------------------
Vector Time (GMT): 2018/284/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5133657
32 A = 6782975
50 meter
Y = -1437616
27 meter E =
0006349
Z = 4190121
35 I = 51
77429
XDOT = 4445
748827 Wp = 110
46912
YDOT = -5022
245694 meter/sec RA = 157
39612 deg
ZDOT = 3717
009193 TA = 301
40082
MA = 301
46290
Ha = 220
173 n
mi
Hp = 216
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16842707
73 X = -5137553
80
Y = -4716588
81 feet Y = -1495045
85 meter
Z = 13747117
28 Z = 4165173
91
XDOT = 14585
790115 XDOT = 4483
522878
YDOT = -16477
184037 feet/sec YDOT = -4972
318745 meter/sec
ZDOT = 12194
912049 ZDOT = 3738
697726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12493571
95 X = 3808040
73
Y = -12365274
83 feet Y = -3768935
77 meter
Z = 13635134
23 Z = 4155988
91
XDOT = 6211
295282 XDOT = 1893
202802
YDOT = 19855
521421 feet/sec YDOT = 6051
962929 meter/sec
ZDOT = 12292
838492 ZDOT = 3746
857172
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 18284
66903508
00016717 00000-0 10270-3 0 9131
2 25544 51
6369 158
2565 0004080 275
6840 84
3847 15
53794882 16629
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
66903508 = yrday
fracday
Element set: 913
Inclination: 51
6369 deg
RA of node: 158
2565 deg
Eccentricity:
0004080
Arg of perigee: 275
6840 deg
Mean anomaly: 84
3847 deg
Mean motion: 15
53794882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1662
Checksum: 344
Coasting Arc #15 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2018/285/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3942676
40 A = 6779829
00 meter
Y = 2370278
29 meter E =
0009028
Z = -4988575
24 I = 51
79355
XDOT = -5577
604195 Wp = 64
28726
YDOT = 4801
837711 meter/sec RA = 152
41542 deg
ZDOT = -2125
833293 TA = 185
02830
MA = 185
03737
Ha = 220
111 n
mi
Hp = 216
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12935290
02 X = 3940110
66
Y = 7776503
58 feet Y = 2414353
40 meter
Z = -16366716
67 Z = -4969429
03
XDOT = -18299
226363 XDOT = -5620
558734
YDOT = 15754
060731 feet/sec YDOT = 4739
224772 meter/sec
ZDOT = -6974
518677 ZDOT = -2153
032565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13090649
97 X = -3990030
11
Y = 7696290
63 feet Y = 2345829
38 meter
Z = -16280882
79 Z = -4962413
07
XDOT = -4471
540320 XDOT = -1362
925490
YDOT = -22625
001057 feet/sec YDOT = -6896
100322 meter/sec
ZDOT = -7097
213121 ZDOT = -2163
230559
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 18285
63376573
00016717 00000-0 10270-3 0 9146
2 25544 51
6364 153
4485 0003901 278
5702 81
5008 15
53811515 16779
Satellite: ISS
Catalog Number: 25544
Epoch time: 18285
63376573 = yrday
fracday
Element set: 914
Inclination: 51
6364 deg
RA of node: 153
4485 deg
Eccentricity:
0003901
Arg of perigee: 278
5702 deg
Mean anomaly: 81
5008 deg
Mean motion: 15
53811515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 319
Coasting Arc #16 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2018/286/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2578384
26 A = 6778438
75 meter
Y = -3317662
61 meter E =
0001231
Z = 5320104
49 I = 51
81722
XDOT = 6305
482370 Wp = 273
58754
YDOT = -4348
826922 meter/sec RA = 147
43115 deg
ZDOT = 344
124880 TA = 173
14006
MA = 173
13838
Ha = 220
330 n
mi
Hp = 216
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8459265
96 X = -2566936
39
Y = -10884719
85 feet Y = -3346431
66 meter
Z = 17454411
07 Z = 5307607
29
XDOT = 20687
278118 XDOT = 6351
971913
YDOT = -14267
804863 feet/sec YDOT = -4278
054688 meter/sec
ZDOT = 1129
018634 ZDOT = 374
868445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13625040
60 X = 4152912
38
Y = -2518248
90 feet Y = -767562
26 meter
Z = 17398547
75 Z = 5303077
35
XDOT = 2808
710420 XDOT = 856
094936
YDOT = 23951
333921 feet/sec YDOT = 7300
366579 meter/sec
ZDOT = 1267
626107 ZDOT = 386
372437
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 18286
66281021
00016717 00000-0 10270-3 0 9154
2 25544 51
6361 148
3205 0003830 282
8759 77
1965 15
53771472 16938
Satellite: ISS
Catalog Number: 25544
Epoch time: 18286
66281021 = yrday
fracday
Element set: 915
Inclination: 51
6361 deg
RA of node: 148
3205 deg
Eccentricity:
0003830
Arg of perigee: 282
8759 deg
Mean anomaly: 77
1965 deg
Mean motion: 15
53771472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 326
Coasting Arc #17 (Orbit 1699)
---------------------------------------
Vector Time (GMT): 2018/287/02:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1219028
78 A = 6778796
24 meter
Y = 4157367
02 meter E =
0010406
Z = -5222810
15 I = 51
83362
XDOT = -6697
789573 Wp = 97
38546
YDOT = 3508
019331 meter/sec RA = 145
01096 deg
ZDOT = 1229
888338 TA = 184
39330
MA = 184
40244
Ha = 220
271 n
mi
Hp = 216
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3999438
26 X = 1197819
48
Y = 13639655
59 feet Y = 4170880
27 meter
Z = -17135203
90 Z = -5216940
09
XDOT = -21974
375240 XDOT = -6742
493688
YDOT = 11509
249772 feet/sec YDOT = 3432
870089 meter/sec
ZDOT = 4035
066725 ZDOT = 1197
243471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13701478
48 X = 4176210
64
Y = 3898114
32 feet Y = 1188145
24 meter
Z = -17109211
44 Z = -5214887
65
XDOT = -1900
685668 XDOT = -579
328992
YDOT = 23733
996096 feet/sec YDOT = 7234
122010 meter/sec
ZDOT = 3887
979962 ZDOT = 1185
056292
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 18287
11301465
00016717 00000-0 10270-3 0 9161
2 25544 51
6376 146
0801 0003764 284
9262 75
1473 15
53793216 17000
Satellite: ISS
Catalog Number: 25544
Epoch time: 18287
11301465 = yrday
fracday
Element set: 916
Inclination: 51
6376 deg
RA of node: 146
0801 deg
Eccentricity:
0003764
Arg of perigee: 284
9262 deg
Mean anomaly: 75
1473 deg
Mean motion: 15
53793216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1700
Checksum: 305
Coasting Arc #18 (Orbit 1715)
---------------------------------------
Vector Time (GMT): 2018/288/02:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 194293
70 A = 6781017
79 meter
Y = -4928447
81 meter E =
0006066
Z = 4652533
84 I = 51
86706
XDOT = 6613
390696 Wp = 38
29165
YDOT = -2526
063826 meter/sec RA = 140
03202 deg
ZDOT = -2945
356604 TA = 80
97491
MA = 80
90627
Ha = 220
244 n
mi
Hp = 216
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 637446
51 X = 226790
61
Y = -16169448
21 feet Y = -4926093
23 meter
Z = 15264218
65 Z = 4653556
76
XDOT = 21697
476036 XDOT = 6655
453544
YDOT = -8287
610977 feet/sec YDOT = -2451
873209 meter/sec
ZDOT = -9663
243451 ZDOT = -2913
128278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13477909
57 X = -4108066
84
Y = -8946974
56 feet Y = -2727037
84 meter
Z = 15269294
82 Z = 4654081
06
XDOT = 3722
282989 XDOT = 1134
551855
YDOT = -21888
794184 feet/sec YDOT = -6671
704467 meter/sec
ZDOT = -9518
100011 ZDOT = -2901
116883
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 18288
14205489
00016717 00000-0 10270-3 0 9175
2 25544 51
6367 140
9523 0003872 289
0799 70
9934 15
53828017 17165
Satellite: ISS
Catalog Number: 25544
Epoch time: 18288
14205489 = yrday
fracday
Element set: 917
Inclination: 51
6367 deg
RA of node: 140
9523 deg
Eccentricity:
0003872
Arg of perigee: 289
0799 deg
Mean anomaly: 70
9934 deg
Mean motion: 15
53828017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1716
Checksum: 344
Coasting Arc #19 (Orbit 1730)
---------------------------------------
Vector Time (GMT): 2018/289/02:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1458892
40 A = 6784534
53 meter
Y = 5518483
72 meter E =
0002211
Z = -3668445
54 I = 51
90407
XDOT = -6153
879053 Wp = 74
80551
YDOT = 1285
375194 meter/sec RA = 135
06324 deg
ZDOT = 4383
682947 TA = 241
80178
MA = 241
82411
Ha = 220
431 n
mi
Hp = 216
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4786392
38 X = -1502673
57
Y = 18105261
53 feet Y = 5501924
45 meter
Z = -12035582
49 Z = -3675638
96
XDOT = -20189
891905 XDOT = -6189
089018
YDOT = 4217
110215 feet/sec YDOT = 1216
361522 meter/sec
ZDOT = 14382
161901 ZDOT = 4353
703566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13165938
43 X = 4012978
03
Y = 13288166
83 feet Y = 4050233
25 meter
Z = -12068470
52 Z = -3678469
81
XDOT = -5758
136912 XDOT = -1755
080131
YDOT = 18636
468204 feet/sec YDOT = 5680
395509 meter/sec
ZDOT = 14247
231257 ZDOT = 4342
556087
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 18289
10677845
00016717 00000-0 10270-3 0 9182
2 25544 51
6375 136
1457 0003746 295
0405 65
0359 15
53805169 17314
Satellite: ISS
Catalog Number: 25544
Epoch time: 18289
10677845 = yrday
fracday
Element set: 918
Inclination: 51
6375 deg
RA of node: 136
1457 deg
Eccentricity:
0003746
Arg of perigee: 295
0405 deg
Mean anomaly: 65
0359 deg
Mean motion: 15
53805169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1731
Checksum: 330
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